diff --git a/LaTeX/approach.tex b/LaTeX/approach.tex
index b20cf76..58f4dd4 100644
--- a/LaTeX/approach.tex
+++ b/LaTeX/approach.tex
@@ -234,6 +234,15 @@
Earth. From knowledge of the mass flow rate, we can then decrement the mass
appropriately based on the magnitude of the thrust vector at each point.
+ In the implementation provided in this thesis, a Sims-Flanagan $n$ value of 20 was
+ chosen for each of the phases. This value, as tested by
+ Englander\cite{englander2012automated}, is sufficient for trajectories that maintain a
+ reasonably small number of solar revolutions. In the future, a more intelligent solution
+ could be to determine, roughly, the number of revolutions around the sun that the orbit
+ will likely take (perhaps by using the period of the orbit at the beginning of the
+ propagation and the time of flight), and scaling $n$ according to the number of
+ revolutions.
+
\subsection{Non-Linear Problem Solver}
Now that we have the basic building blocks of a continuous-thrust trajectory, we can
@@ -434,15 +443,24 @@
generator produces two random missions as described in
Section~\ref{random_gen_section} that differ only in that one contains random flyby
velocities and control thrusts and the other contains Lambert's-solved flyby
- velocities and zero control thrusts. For each of these guesses, the NLP solver is
- called. If either of these mission guesses have converged onto a valid solution, the
- lower loop, the ``drill loop'' is entered for the valid solution. After the
- convergence checks and potentially drill loops are performed, if a valid solution
- has been found, this solution is stored in an archive. If the solution found is
- better than the current best solution in the archive (as determined by a
- user-provided cost function of fuel usage, $C_3$ at launch, and $v-\infty$ at
- arrival) then the new solution replaces the current best solution and the loop is
- repeated. Taken by itself, the search loop should quickly generate enough random
+ velocities and zero control thrusts.
+
+ The choice of adding a ``Lambert's solution-seeded'' random mission is an attempt to
+ improve upon previous low-thrust MBH iterations by more intelligently choosing some of
+ the initial guesses. Because the majority of the initial guesses that are truly random
+ don't converge, this provides a greater number of valid initial guesses for the MBH
+ algorithm to use to find better trajectories. However, each MBH loop does then take
+ twice the time, which increases the amount of time required to truly traverse the entire
+ space.
+
+ For each of these guesses, the NLP solver is called. If either of these mission guesses
+ have converged onto a valid solution, the lower loop, the ``drill loop'' is entered for
+ the valid solution. After the convergence checks and potentially drill loops are
+ performed, if a valid solution has been found, this solution is stored in an archive. If
+ the solution found is better than the current best solution in the archive (as
+ determined by a user-provided cost function of fuel usage, $C_3$ at launch, and
+ $v-\infty$ at arrival) then the new solution replaces the current best solution and the
+ loop is repeated. Taken by itself, the search loop should quickly generate enough random
mission guesses to find all ``basins'' or areas in the solution space with valid
trajectories, but never attempts to more thoroughly explore the space around valid
solutions within these basins.
@@ -489,4 +507,25 @@
iterations to perform without improvement in a row before ending the drill loop.
This process can be repeated essentially ''search patience`` number of times in
order to fully traverse all basins.
+
+ It is worth validating whether the described Monotonic Basin Hopping algorithm
+ actually provides significant improvements in global cost-function minimization over
+ a single NLP-optimization run for the particular problem of low-thrust
+ interplanetary trajectories. Therefore, a simple sample Earth to Saturn trajectory
+ was selected and every single valid trajectory discovered by the MBH algorithm was
+ stored. In Figure~\ref{mbh_analysis}, the cost function values for each of these
+ valid trajectories is plotted in the order in which they were found. The line
+ indicates the minimum cost function discovered until that point in time. This
+ validates that the MBH, over sufficient number of iterations, will find optimal
+ values that the NLP optimization scheme could not discover on its own. It is also
+ worth noting that the ``basin drilling'' feature of the MBH scheme can be clearly
+ seen in the plot, where the algorithm continues to improve its own ``basin-best''
+ until it no longer can do so over a number of attempts.
+
+ \begin{figure}[H]
+ \centering
+ \includegraphics[width=\textwidth]{LaTeX/fig/mbh_analysis}
+ \caption{MBH cost function reduction over time}
+ \label{mbh_analysis}
+ \end{figure}
diff --git a/LaTeX/conclusion.tex b/LaTeX/conclusion.tex
index 79c8594..bd932d0 100644
--- a/LaTeX/conclusion.tex
+++ b/LaTeX/conclusion.tex
@@ -5,7 +5,9 @@
parameters. This makes the mission designer's job significantly simpler in that they can
simply explore a number of different flyby selection options in order to get a good
understanding of the mission scope and search space for a given spacecraft, launch window,
- and target.
+ and target. The aim of this exploration was to examine whether a Monotonic Basin Hopping
+ algorithm utilizing an inner-loop NLP solver would be an appropriate choice for the
+ particular problem of low-thrust interplanetary trajectory optimization.
In performing this examination, two results were selected for further analysis. These
results are outlined in Table~\ref{results_table}. As can be seen in the table, both
diff --git a/LaTeX/fig/mbh_analysis.png b/LaTeX/fig/mbh_analysis.png
new file mode 100644
index 0000000..6a0c3d1
Binary files /dev/null and b/LaTeX/fig/mbh_analysis.png differ
diff --git a/LaTeX/results.tex b/LaTeX/results.tex
index 57a9a7c..303ad3a 100644
--- a/LaTeX/results.tex
+++ b/LaTeX/results.tex
@@ -101,6 +101,47 @@
\item EVVJS
\end{itemize}
+ For each of these trajectories, the optimization algorithm was run. During the MBH phase
+ of the optimization algorithm, anytime a new ``basin best'' mission was discovered, it
+ was recorded. The resultant cost function values of each of those discovered missions
+ can be found in the table below:
+
+ \begin{table}[H]
+ \centering
+ \begin{adjustbox}{height=0.3\textheight}
+ \begin{tabular}{ | c c c c | }
+ \hline
+ \bfseries Flyby Selection &
+ \bfseries Cost Function Value &
+ \bfseries Flyby Selection &
+ \bfseries Cost Function Value \\
+ \hline
+ EMS & 0.64797 & EMJS & 0.66014 \\
+ EMS & 0.68828 & EMS & 0.69704 \\
+ EMJS & 0.74576 & EMJS & 0.79745 \\
+ EMJS & 0.80372 & EMJS & 0.82510 \\
+ EMMJS & 0.91149 & EMJS & 0.94148 \\
+ EMJS & 0.96141 & EMS & 1.02972 \\
+ EJS & 1.12848 & ES & 1.23167 \\
+ EVMS & 1.32600 & EMS & 1.32879 \\
+ EMS & 1.33779 & EMJS & 1.39527 \\
+ EVMS & 1.41517 & EVMS & 1.45960 \\
+ EVMS & 1.46649 & EVMS & 1.52207 \\
+ EVMS & 1.59234 & EVMJS & 1.66943 \\
+ EMS & 1.70295 & EMJS & 1.70438 \\
+ EMS & 1.78107 & EVVJS & 2.0106 \\
+ EMJS & 2.15952 & EJS & 2.16216 \\
+ EMJS & 2.22167 & EMMJS & 2.38431 \\
+ EMJS & 2.42457 & EMMJS & 2.46453 \\
+ EVVJS & 2.49257 & EMJS & 2.49485 \\
+ EVMS & 2.71118 & EMJS & 2.76812 \\
+ \hline
+ \end{tabular}
+ \end{adjustbox}
+ \caption{Table of resultant cost function values for every discovered mission}
+ \label{cost_fn_table}
+ \end{table}
+
\section{Faster, Less Efficient Trajectory}
In order to showcase the flexibility of the optimization algorithm (and the chosen cost
@@ -120,11 +161,14 @@
The mission begins in late June of 2024 and proceeds first to an initial gravity assist with
Mars after three and one half years to rendezvous in mid-December 2027. Unfortunately, the
launch energy required to effectively use the gravity assist with Mars at this time is
- quite high. The $C_3$ value was found to be $60.4102 \frac{\text{km}^2}{\text{s}^2}$. However,
- for this phase, the thrust magnitudes are quite low, raising slowly only as the spacecraft
- approaches Mars, allowing for a nearly-natural trajectory to Mars rendezvous. Note also that
- the in-plane thrust angle was neither zero nor $\pi$, implying that these thrusts were
- steering thrusts rather than momentum-increasing thrusts.
+ quite high. The $C_3$ value was found to be $60.4102 \frac{\text{km}^2}{\text{s}^2}$. While
+ not as low as some of the other missions found to be very optimal, it should be noted that
+ missions with this $C_3$ and launch mass are still quite feasible.
+
+ However, for this phase, the thrust magnitudes are quite low, raising slowly only as the
+ spacecraft approaches Mars, allowing for a nearly-natural trajectory to Mars rendezvous.
+ Note also that the in-plane thrust angle was neither zero nor $\pi$, implying that these
+ thrusts were steering thrusts rather than momentum-increasing thrusts.
\begin{figure}[H]
\centering
diff --git a/LaTeX/thesis.tex b/LaTeX/thesis.tex
index eee3a48..3b1d0ff 100644
--- a/LaTeX/thesis.tex
+++ b/LaTeX/thesis.tex
@@ -7,6 +7,7 @@
\usepackage{amsfonts}
\usepackage{float}
\usepackage{xfrac}
+\usepackage{adjustbox}
\title{Designing Optimal Low-Thrust Interplanetary Trajectories Utilizing Monotonic Basin Hopping}
\author{Richard C.}{Johnstone}
diff --git a/LaTeX/trajectory_design.tex b/LaTeX/trajectory_design.tex
index c659e6f..d50814e 100644
--- a/LaTeX/trajectory_design.tex
+++ b/LaTeX/trajectory_design.tex
@@ -34,7 +34,6 @@
the end, we'll also assume that the mass of the spacecraft ($m_2$) is much much smaller
than the mass of the planetary body ($m_1$) and enough so as to be considered
negligible.
-
\begin{figure}[H]
\centering
\includegraphics[width=0.65\textwidth]{LaTeX/fig/2bp}
@@ -42,21 +41,18 @@
the center of mass in the two body problem}
\label{2bp_fig}
\end{figure}
-
Under these assumptions, the force acting on the body due to the law of universal
gravitation is:
\begin{align}
F_2 &= - \frac{G m_1 m_2}{r^2} \frac{\vec{r}}{\left| r \right|} \\
F_1 &= \frac{G m_2 m_1}{r^2} \frac{\vec{r}}{\left| r \right|}
\end{align}
-
And by Newton's second law (force is the product of mass and acceleration), we can
derive the following differential equations for $r_1$ and $r_2$:
\begin{align}
m_2 \ddot{\vec{r}}_2 &= - \frac{G m_1 m_2}{r^2} \frac{\vec{r}}{\left| r \right|} \\
m_1 \ddot{\vec{r}}_1 &= \frac{G m_2 m_1}{r^2} \frac{\vec{r}}{\left| r \right|}
\end{align}
-
Where $\vec{r}$ is the position of the spacecraft relative to the primary body,
$\vec{r}_1$ is the position of the primary body relative to the origin of the inertial
frame, and $\vec{r}_2$ is the position of the spacecraft relative to the center of the
@@ -177,7 +173,6 @@
&= \frac{abE}{2} - \frac{ab}{2} \left( \cos E \sin E \right) \\
&= \frac{ab}{2} \left( E - \cos E \sin E \right)
\end{align}
-
By substituting the two areas back into Equation~\ref{areas_eq} we can get the $k$ area
swept out by the spacecraft:
\begin{equation}
@@ -224,7 +219,6 @@
\frac{-d^2\ln|g(x)|}{dx^2} &= \frac{1}{(x - x_1)^2} + \frac{1}{(x - x_2)^2} + ... +
\frac{1}{(x - x_m)^2} = G_2(x)
\end{align}
-
Now we define the targeted root as $x_1$ and make the approximation that all of the
other roots are equidistant from the targeted root, which means:
\begin{equation}
@@ -333,7 +327,6 @@
\begin{equation}
\xi = \frac{v^2}{2} - \frac{\mu}{r} = \frac{v_\infty^2}{2}
\end{equation}
-
We can then leverage the conservation of energy to determine the velocity at a
particular point, $r_{ins}$:
\begin{align}
@@ -482,14 +475,12 @@
\cos (\Delta \theta) &= \frac{\vec{r}_1 \cdot \vec{r}_2}{|\vec{r}_1| |\vec{r}_2|} \\
\Delta \theta &= \arctan(y_2/x_2) - \arctan(y_1/x_1)
\end{align}
-
The direction of motion is then chosen such that counter-clockwise orbits are
considered, as travelling in the same direction as the planets is generally more
efficient. Next, the variable $A$ is defined:
\begin{equation}
A = DM \sqrt{|r_1| |r_2| (1 - \cos(\Delta \theta))}
\end{equation}
-
A is independent of $\psi$, and therefore won't need updating as the iteration
proceeds. Then $\psi$ is initialized to any number within its bounds
($[-4\pi,4\pi^2]$), arbitrarily set to 0, representing a parabolic arc as a starting
@@ -520,7 +511,6 @@
\begin{equation}
y = |r_1| + |r_2| + \frac{A (c_3 \psi - 1)}{\sqrt{c_2}}
\end{equation}
-
We can then finally calculate the variable $\chi$, and from that, the time of
flight:
\begin{equation}
diff --git a/archive/EMS_0.885200034193802 b/archive/EMS_0.885200034193802
new file mode 100644
index 0000000..bd0f006
--- /dev/null
+++ b/archive/EMS_0.885200034193802
@@ -0,0 +1,29 @@
+archive/EMS_0.885200034193802---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-09-20T14:03:44.662
+Launch V∞: [-0.9544125442488793, 4.650055637860991, 0.8829883975591813] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-2.686848874040082, 5.69557833738042, -0.3426867301634786] km/s
+ V∞_out: [-5.006830246285463, 3.8244101442357286, -0.28590492992060296] km/s
+ time of flight: 1.2959473202133252e8 seconds
+ arrival date: 2028-10-29T12:35:56.662
+ thrust profile: [-0.028074398281491695 0.03725829642101633 0.011493562796176157; -0.04057241823105847 -0.0036979634745522238 0.004188100162030408; -0.018576540265103334 -0.016670623079762328 -0.0036538504180610655; -0.00926818068907572 -0.029823872248843347 -0.00788998730301693; 0.0056536273790355335 -0.039471274595512786 -0.015505661293943124; 0.01795773380852956 -0.024832086810877792 -0.012157101567918709; 0.020276654954958836 -0.008918038755765955 -0.0074245383137495295; 0.026868221096269136 0.007263820280035479 -0.004654400052923847; 0.011894893359756988 0.03223774798632351 0.004633535267024402; -0.047141055295386355 0.040019079580037704 0.013364609633569504; -0.04520469085369964 -0.010120922532993988 0.0020777538652468844; -0.024235864777124916 -0.02628842319518715 -0.005178953753261158; -0.020104196631084845 -0.08663986569488229 -0.025957813503050115; 0.04562945777248198 -0.18858114469692783 -0.07388958835417316; 0.1654642046172344 -0.19639566019786459 -0.09899123711104271; 0.20836768567311814 -0.07684473602532182 -0.06621134288112417; 0.17451643722399424 0.054856569336227734 -0.019947666848185868; 0.09171150949789851 0.24766459803783164 0.03479747010758981; -0.23524183946575974 0.2601294101394598 0.07688820773607916; -0.21879974186036938 -0.008020833470565012 0.021595583194403873] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [2.746703786000276, 2.98969776442552, -1.0550945579969648] km/s
+ V∞_out: [-2.364529965587132, -1.1050142331661583, -3.0819068226828907] km/s
+ time of flight: 2.2586692153285405e8 seconds
+ arrival date: 2035-12-26T17:24:37.662
+ thrust profile: [-0.17155197556204754 -0.12803647772004534 -0.0010987042854903337; -0.0035589134881411667 -0.06490801713537507 0.0007426295065205218; 0.25580929199297914 -0.3791453683925915 0.015541598652070847; 0.9999998062826643 -0.5828839766311769 0.041611387112901736; 0.9999998812648976 -0.13591929443541234 0.04367451973443414; 0.9999999269970672 0.45531454218125245 0.04521667689652659; 0.9999999228048742 0.9999999183342614 0.04613770201743983; 0.840757310010811 0.9999999579385513 0.026030995407658575; 0.11987829006679744 1.0 -0.0008893319442928411; -0.16626331436648592 0.8682210906007626 -0.017523530916658536; -0.010554991808101162 0.026008419906682182 -0.0010654160560760403; -0.00038326527134042613 0.00042430859777888713 0.00034930741189383597; 8.526053802782655e-5 -0.0008985199777937706 0.000160878965697085; -0.0003967771857136998 0.0010341920913412306 -0.0002243904620731941; -0.001455496554504259 -3.155267804676458e-5 0.00028821667601580344; -0.0002685807673767674 0.000826989980715048 -0.0008420052914367241; -0.0007719825562061786 -0.0008609199968383217 -5.4081725930572875e-5; -0.00011547325119660988 0.00024382875164120964 -0.0003906884145274092; 0.0010448953162641168 -0.0012700408455061536 0.001398368665761554; -0.0009243989271800159 -0.0004827763788561335 -0.00016362116690873035] %
+
+Mass Used: 896.7374359341643 kg
+Launch C3: 23.313589250046537 km²/s²
+||V∞_in||: 4.1947465879304335 km/s
diff --git a/archive/EMS_0.956419624778337 b/archive/EMS_0.956419624778337
new file mode 100644
index 0000000..528ce1c
--- /dev/null
+++ b/archive/EMS_0.956419624778337
@@ -0,0 +1,29 @@
+archive/EMS_0.956419624778337---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-09-17T04:51:36.159
+Launch V∞: [-1.135592828872187, 4.562737698529162, 1.3727576611586305] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-3.557470090326179, 6.118653602166694, -0.5798401682157046] km/s
+ V∞_out: [-5.645943535485121, 4.274383608710339, -0.5316919206121211] km/s
+ time of flight: 1.3085999999776801e8 seconds
+ arrival date: 2028-11-09T18:51:35.159
+ thrust profile: [-0.09484105234506424 0.13109265638731943 0.010936530688181876; -0.1814554654952118 -0.01317670830456729 -0.013056779511401079; -0.03810385790137717 -0.03831609614699233 -0.0090400245120533; -0.011547804227375344 -0.045340160916842225 -0.010789638825569993; 0.010850150398340981 -0.04880193320022692 -0.012185437423926783; 0.013978839278259155 -0.01840779353950528 -0.004665802971635902; 0.015830676636944672 -0.006108261481050007 -0.001974030494045432; 0.02222629553617521 0.007131223648098273 -0.000366596741242515; 0.05551908016805829 0.2775937664715688 0.01624399186055875; -0.11493741715972325 0.07648127820140446 0.005075332093053433; -0.07281410027212154 -0.023271489715626266 -0.00280576336716608; -0.03991641354611127 -0.052482033366050736 -0.012070494591368944; -0.010823677700697571 -0.06926247781385951 -0.014965378527982062; 0.014553072546870926 -0.0531151232441876 -0.012334544418377249; 0.027433879698947325 -0.03222960647822717 -0.008091377392690582; 0.027896088095082885 -0.010765686776681731 -0.0035677146904594865; 0.1474887355876181 0.04194010217566325 0.0075472784087007245; 0.08740136907489779 0.2476740961050621 0.025348796622511757; -0.3587107107731137 0.3658303122853691 -0.024033216941170596; -0.30793493577932085 -0.02489759271709177 -0.029516702132738652] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [3.7155109082507987, 4.436831582591491, -1.1732520095761172] km/s
+ V∞_out: [-2.9774108815083147, -1.2560337688716137, -4.9297276650048545] km/s
+ time of flight: 2.0467080000004956e8 seconds
+ arrival date: 2035-05-06T15:51:35.159
+ thrust profile: [-0.05767594934959341 -0.04617371221776187 -0.0018460762847027803; -0.00242135160333423 -0.04166237973886581 0.0014630203665685387; 0.29042498349326934 -0.4463318141243284 0.034252710040742367; 0.9999918983032768 -0.6810996795092573 0.08973482264944235; 0.999994193014499 -0.30520092641941937 0.09457239144251212; 0.9999870255556219 0.2194024540716046 0.09015740448455901; 0.9999831603785917 0.9750561249047252 0.0872456396613651; 0.9999985694625713 0.9999931657134729 0.05615632466445174; 0.687392266640871 0.9999956716419007 0.01734725859208972; 0.029368471497984026 0.99992751557616 -0.014405154294501676; -0.20296396601376304 0.9423006803678043 -0.03524904229410645; -0.12775237609043735 0.3694446313295914 -0.02368746549915993; -0.00034842736779606184 0.0005678692895095884 -0.00031598317940006337; -0.0003712455053865169 -1.6935819288267125e-5 -0.00019252189104459086; -0.0005996017322677676 -0.00028098465395757154 2.2184451692068863e-5; 0.0002022591204715913 -0.00018951661125293372 0.000189711737865895; -0.0007251432775536019 0.0002897166773871866 -3.9173461655229126e-5; -0.000850251276017041 -0.0005646508814492377 0.0013737659604325715; 0.00040972949658941917 -0.0005145490913947212 5.515738964126715e-5; -0.00046082039982410966 -0.0003000114452015229 -0.00026022069154713355] %
+
+Mass Used: 975.8660040548566 kg
+Launch C3: 23.992609974834842 km²/s²
+||V∞_in||: 5.9048298942125665 km/s
diff --git a/archive/EMS_1.4088814420596534 b/archive/EMS_1.4088814420596534
new file mode 100644
index 0000000..bf831aa
--- /dev/null
+++ b/archive/EMS_1.4088814420596534
@@ -0,0 +1,29 @@
+archive/EMS_1.4088814420596534---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-16T06:12:17.261
+Launch V∞: [-1.7148923713366755, 3.9298192178302784, 2.8299200745152713] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-3.423654294372138, 2.5650341612477567, -0.5338967704352118] km/s
+ V∞_out: [-4.266996673560502, -0.5839080002997025, 0.19402466913132768] km/s
+ time of flight: 1.3088384355378014e8 seconds
+ arrival date: 2028-12-09T02:49:40.261
+ thrust profile: [-0.16843253076284767 0.015174387284071982 -0.2568833411269522; -0.04051411441266916 -0.1706697462481348 -0.09202063132953058; 0.045219798511790026 -0.3096747505733966 -0.15447868293737022; 0.1891430434005993 -0.38802384440125315 0.254163650929716; 0.2878269718158013 -0.2521241423300037 0.1694504332526969; 0.2669620698102962 -0.07974891300102108 0.22353096596670005; 0.25838781033301184 -0.013302459740443208 0.1575979105416097; 0.18877094120583682 -0.1090841631358866 0.0675029255999918; -0.36014421578836414 -0.39909210387062594 -0.10424720248437652; 0.007505343447408759 -0.37070440668154536 -0.020703856519349483; 0.18623264501774142 -0.18772468781032164 -0.012898204728801035; -0.07776052053136313 -0.2150791981555987 0.17906646004157736; 0.0933903030286568 -0.351389278618167 0.2513185206003883; 0.15582528052167877 -0.27898764592860065 0.25820541552552223; 0.1705037874283403 -0.15120215929987232 0.22048201505740622; 0.2478320676125178 -0.0553823274204888 0.008131367787768651; 0.3160196179605864 0.06497580000323308 -0.08737918006790793; 0.18787792768517483 0.24030042469215662 -0.02336463045670074; -0.4500653157082868 -0.43615701512016586 0.031249984200407536; -0.5597015227203471 0.026975117825268798 0.05914640634236509] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [-0.4447430233297146, -0.5103236773782882, 0.17690937986451852] km/s
+ V∞_out: [0.4026479925582012, 0.16697609141693656, 0.5486720695904586] km/s
+ time of flight: 2.2369063570553738e8 seconds
+ arrival date: 2036-01-11T03:06:55.261
+ thrust profile: [-0.20026176608455784 -0.29694390627659506 -0.03656336874049517; 0.19219210775821996 -0.2745039023151382 -0.008910114775166253; 0.5380981511022175 -0.1752113671787406 0.2750415301381581; 0.8091604929924738 0.059336617760770226 0.16452081995331563; 0.8019293953199363 0.3703939998509808 0.12716583651365265; 0.7628458054564177 0.6219877057473859 0.08804354131656808; 0.6790691189945572 0.7151724861702393 0.07257080916983001; 0.605711392602211 0.7556960844929883 0.05668728294284225; 0.5019330343132242 0.7202977352394476 0.05464681963849307; 0.4355136362347505 0.5812218127189013 0.0598464640192131; 0.2792323417761552 0.6365652142420161 0.06200031759875403; -0.0031648597009793127 0.6439660654725341 0.021229855541562564; -0.22740032522428177 0.585273186623273 -0.0005797994707257422; -0.29907327416889895 0.5556200894768929 0.016308953313994647; -0.3305919828650731 0.6000464102363009 0.008217747003379565; -0.2760568905961062 0.534608626086542 -0.02767524280228222; -0.21717555650995973 0.3271478959702166 -0.000487395179347153; -0.15788889898326117 0.24115731722004857 -0.0013939275969228635; -0.08909459626676448 0.1483902552290073 -0.0013811701172317676; -0.028408442047604864 0.04951927705463767 -0.0006587817095277265] %
+
+Mass Used: 1489.7371174798539 kg
+Launch C3: 26.39278255824143 km²/s²
+||V∞_in||: 0.699659589498638 km/s
diff --git a/archive/EMS_1.7849375588806782 b/archive/EMS_1.7849375588806782
new file mode 100644
index 0000000..bc36692
--- /dev/null
+++ b/archive/EMS_1.7849375588806782
@@ -0,0 +1,29 @@
+archive/EMS_1.7849375588806782---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-12-27T01:12:40.730
+Launch V∞: [1.8466699553948345, 1.3678562790010131, -0.0153057964937058] km/s
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+ Planet: Mars
+ V∞_in: [-3.1633872892711388, 1.766847714739104, 1.5906318484460866] km/s
+ V∞_out: [-2.6570752417451518, -1.5623087854586397, 2.48153623885944] km/s
+ time of flight: 1.3537387772095194e8 seconds
+ arrival date: 2029-04-11T21:03:57.730
+ thrust profile: [0.9929900810043344 0.9999987852496462 -0.10337727636552446; -0.9999989527606722 0.9999992090099894 -0.3047289804175132; -0.9638713659439484 0.0450322438551014 -0.4055337795064804; -0.22495106561402115 0.7848677069324818 0.3831319023782979; -0.7738893421351393 0.9999990172621287 0.39494769205095726; -0.990946731002965 0.8417897053927665 -0.3815221486365675; -0.9734982361035388 0.7893313668448306 -0.2704704369660258; -0.38723803350107505 0.9976585911266805 0.3624717872401706; -0.6369591805380839 0.9888790443583878 0.2130500370042681; -0.9999988687936101 0.9999990044599046 -0.3329147869188805; -0.5789162319974664 0.1999123448513483 0.028083803862645515; 0.7985291692991425 0.7881953295377477 0.17388971281195142; 0.988850032987504 0.9999996591217118 -0.5009694317683372; -0.9999994842664317 -0.3956604351616602 0.20708177708047873; -0.4450447334188467 -0.9872965011676511 0.25277979453414506; 0.9999992382496556 -0.2261999230664443 0.0610408161667454; 0.9999995915291495 0.9999997964336237 -0.5276666165499095; -0.9999998232725931 0.9999996435539122 -0.2721356921234991; -0.9999996876222519 -0.99999900073252 0.10007758955670606; -0.4315629068159034 -0.9999994920612009 0.07571074821215397] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [1.327202961748595, -0.2335174765716992, 0.19517799010581816] km/s
+ V∞_out: [-0.10390899330694657, 0.5823202662968701, -1.2235226316464973] km/s
+ time of flight: 1.315170240574828e8 seconds
+ arrival date: 2033-06-12T01:34:21.730
+ thrust profile: [0.9999991434090886 -0.9999989109820826 -0.18840484920575698; 0.999999642574456 -0.7892776436332918 -0.12931408694138657; 0.9999997178412163 0.5267393788441906 -0.06956780561709845; 0.9999997101961674 0.9999994336962261 -0.018610639490947056; 0.9999995326675502 0.9999996674548184 0.04055505772364419; 0.9999985272401802 0.9999997166093685 0.0964843343858098; 0.5108611241098074 0.9999996665528476 0.11541241396889583; 0.11915209802429379 0.9999995788468198 0.1254892030062545; -0.06577608027600101 0.9999995097151354 0.1358163701800956; -0.15786944384121993 0.9999996754541017 0.1375960485939181; -0.19165177643017128 0.9999893885682953 0.12875243461837188; -0.1283595672922781 0.6138567630147376 0.07671724293817712; -0.012317449010467607 0.047087977571726294 0.006452581509892722; -6.34335149466746e-5 0.00091471809306928 8.53716230858717e-5; -0.0002753957972021203 0.0008379366569403406 0.000253847549893273; -0.00012249698733454806 0.000620864691591944 0.0001747719954028129; -0.0007703906582188425 0.00036864647470518063 -0.00026313495806057455; -0.0003679676279671012 0.000462432306598997 -0.0005969365300740931; 0.00010307940670236174 6.503004811360405e-5 0.00016002455788454703; 5.626567684290205e-5 0.00028538089451470705 0.0003865580217838497] %
+
+Mass Used: 2051.6186645766516 kg
+Launch C3: 5.281454991566764 km²/s²
+||V∞_in||: 1.3616506752322357 km/s
diff --git a/archive/EMS_1.7964973464843803 b/archive/EMS_1.7964973464843803
new file mode 100644
index 0000000..d56cff9
--- /dev/null
+++ b/archive/EMS_1.7964973464843803
@@ -0,0 +1,29 @@
+archive/EMS_1.7964973464843803---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-12-28T06:03:36.902
+Launch V∞: [1.9113115422257663, 1.0939752985973668, -0.2878460457456588] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-2.396005235896576, 1.5910968460984156, 2.4553745598827215] km/s
+ V∞_out: [-0.738879248789918, -1.3198053438616348, 3.466044691382917] km/s
+ time of flight: 1.3682159997877434e8 seconds
+ arrival date: 2029-04-29T20:03:35.902
+ thrust profile: [0.935248482226924 0.9999431292980571 -0.1290404928548267; -0.9999476163597248 0.9999515515170286 -0.24823663597926307; -0.8795731397232727 0.11883370193334312 -0.6198238490789577; -0.47255877270571917 0.8460911087046892 0.5425122446091334; -0.8842186442310318 0.9999442668703385 0.632114794955067; -0.9467809827443692 0.7397804470130911 -0.5827972578364147; -0.9202889335527289 0.8035048754026284 -0.5573817193425457; -0.7074755326919293 0.9999898297887988 0.5385761857415082; -0.778563476191167 0.9440695192200221 0.5088248662337462; -0.999935848670154 0.9999298047351639 -0.5166619290742501; -0.7958311273920875 0.4445916834284018 -0.20253835385960575; 0.799628199463289 0.787390476804687 0.10921619103766879; 0.6775585821251879 0.9999859279862128 -0.056976618126330265; -0.9999708212123471 -0.6329649627446755 0.30597984975011394; -0.3379623142939624 -0.9999302294951131 0.5845511928965047; 0.9999796032643747 -0.12435864928204078 0.05360464346939001; 0.9999735389912225 0.9999936940242244 -0.6858853667949919; -0.9999932115686956 0.9999647789195363 -0.4065818129789695; -0.9999828349783968 -0.9999811809194908 0.2562488369803276; 0.8477193677430503 -0.9999888051388031 0.44654176461357903] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [1.687679365659058, -0.3106760396582122, 0.25789343385832764] km/s
+ V∞_out: [-0.13000691471236564, 0.7123751472156044, -1.4816590595134704] km/s
+ time of flight: 1.3038840000839666e8 seconds
+ arrival date: 2033-06-16T23:03:35.902
+ thrust profile: [0.9999943154178064 -0.9999793447580555 0.06826775331348747; 0.9999973057987236 -0.7577830174110806 0.09936609510988814; 0.9999978386167154 0.999996910634015 0.12385129639736782; 0.9999970143501956 0.9999984909994136 0.18181347514052054; 0.9999901589869835 0.9999988995839434 0.2578219962691517; 0.676991268524474 0.9999990090764392 0.2880018307347756; 0.20873881951717477 0.9999990450745354 0.2788781951149253; -0.003991942078742135 0.9999990863624453 0.27800285072408; -0.10377137001550704 0.99999919042469 0.26254279367539807; -0.11890106720112337 0.7958208463902771 0.19525684108652674; -0.05544439551611033 0.27388175650220187 0.07106727942943497; -0.036288195450646675 0.14031424139484425 0.03530510666426885; -0.004277653916611693 0.016826893422196152 0.004178638953119427; 9.200391005419325e-5 0.004147286559672669 -0.00015203464796320339; -0.0001527325932206235 0.0003004840617325797 0.00013127411825929072; -0.000154649294574425 0.0010525030105100078 0.0008862518960764552; -0.0009285177821710427 -0.0009909987221447562 0.002296370239222059; 0.0005316057188195457 0.0015595065628119108 0.00010356134502627535; 0.0034358308362445874 -0.0028793310522562256 -6.702429154429191e-5; -0.00030910308067229515 -0.0011037999999218894 -7.645215422836016e-5] %
+
+Mass Used: 2067.1392010817217 kg
+Launch C3: 4.932749111438047 km²/s²
+||V∞_in||: 1.7353069659620202 km/s
diff --git a/archive/EMS_1.8179951828877143 b/archive/EMS_1.8179951828877143
new file mode 100644
index 0000000..bf72b72
--- /dev/null
+++ b/archive/EMS_1.8179951828877143
@@ -0,0 +1,29 @@
+archive/EMS_1.8179951828877143---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-12-26T20:04:12.197
+Launch V∞: [2.2631654921869386, 1.185081360708154, 0.009257038518396843] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-1.819421900582889, 2.4878162265474044, 1.9652452646560326] km/s
+ V∞_out: [-1.3203444171650183, -0.6998249118520182, 3.335963173120055] km/s
+ time of flight: 1.332502281347756e8 seconds
+ arrival date: 2029-03-18T02:01:20.197
+ thrust profile: [0.9998287069413306 0.9999191371392129 0.1213662202450064; -0.9999116954167637 0.9999384805827953 -0.12816381654311323; -0.8828170417862063 0.8028517826222941 -0.49870520497687526; 0.4565104064071078 0.9273836393237869 0.5018109850322613; -0.6327164570700743 0.999925849841719 0.4784105400321262; -0.830428721827531 0.9619162741068041 -0.4768142744373306; -0.8673070786916957 0.8947170888203538 -0.20042275389292005; 0.006746002981440682 0.9998684851484286 0.44190370405202867; -0.43972848998205877 0.9935765596102941 0.1925917898116161; -0.9998921566708584 0.9999191466596513 -0.28295229283611234; -0.5708873223359694 0.3773361758460382 0.3615474185713707; 0.885961186451299 0.9060683313648012 0.2199266449664907; 0.9998597552900677 0.9999744957399328 -0.6986700034250672; -0.9999501734393813 -0.053191236063163554 0.2422651192105141; -0.2946407843080661 -0.9108509783200093 0.30366986723671646; 0.9999502617365811 -0.6719510540879361 0.08569312009428964; 0.999977035033471 0.9999843531322284 -0.8250795371244247; -0.9999843642335481 0.9999752522544111 -0.38417007411620746; -0.9999749850418986 -0.9911828413853273 0.03074032591695355; -0.7555359458601892 -0.9999499953971228 0.1307993165243738] %
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+ Planet: Saturn
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+ V∞_out: [-0.06497216787939741, 0.36319158740168506, -0.9132347096518814] km/s
+ time of flight: 1.2866032712000416e8 seconds
+ arrival date: 2033-04-15T05:00:07.197
+ thrust profile: [0.9999179790353537 -0.9999061112069662 -0.3847027839240411; 0.9999670827320215 -0.9993196899255067 -0.3520428584517027; 0.9999749413896841 0.10728670306699271 -0.20347892697858028; 0.9999770064758384 0.9999429473541616 -0.15892509767413687; 0.9999642130850989 0.9999708004076064 -0.027062892163153125; 0.9999246588230427 0.9999756917747938 0.09553319711816699; 0.575862503562761 0.9999718804815532 0.16723368288218737; 0.1348698059357536 0.9999631099154952 0.18699745173223745; -0.04347818851670972 0.9999540138326606 0.2054654512161514; -0.12936889157582143 0.999966768321729 0.21144524989026273; -0.1589938838387372 0.9999936224369557 0.1997164588314596; -0.12853648815272445 0.6832485852279477 0.14447679147858372; -0.010355042246881451 0.051188278828012496 0.010667915325539963; -0.0014752719235167427 0.00547355770049997 0.0010936545500989869; -0.0031143585237226163 0.0019098863155813648 0.0007045674243290908; -0.0018146510605806672 -0.0020603912304730005 -0.001272418113780502; -0.0015580679285132912 0.0013209738024154483 0.0008370880567315606; -0.005476076545704018 -0.004478067280660263 0.005715586687551187; -0.0006343098431029113 -0.0020565792501144866 -0.003103123685946313; 0.00014069293580912002 -0.0036504980181857414 -0.010638484561936872] %
+
+Mass Used: 2082.9235875481663 kg
+Launch C3: 6.526421569285769 km²/s²
+||V∞_in||: 0.9905900139445544 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:26:22.750/mission b/archive/EM_3-29/EM_2022-03-29T21:26:22.750/mission
new file mode 100644
index 0000000..b0d39ea
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:26:22.750/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:26:22.750/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-22T09:55:35.770
+Launch V∞: [7.3434961975052575, 2.1070520149056207, -1.014351173307538] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-4.0891408313442243e-10, -1.3519558171080589e-9, -2.9347938509608335e-9] km/s
+ V∞_out: [-1.009960237699357e-8, -1.009960237699357e-8, 7.767450588932219e-10] km/s
+ time of flight: 8.599031774086058e7 seconds
+ arrival date: 2027-01-12T16:07:32.770
+ thrust profile: [0.10180817450485931 0.010765994728988202 -0.007544294859875064; 0.16235850598372423 0.10642344368168269 -0.0003675622257710981; 0.1012089195326011 0.215498048785662 0.009263152266136488; -0.005263860097698059 0.23018146612119708 0.014653161556634695; -0.07216616837405394 0.1886632498893549 0.01482047592832661; -0.09398125027080778 0.12777759796739516 0.011338047777898999; -0.08181401680555038 0.06911303246065172 0.005833525852290107; -0.046580710304300145 0.02548722787737307 -0.000870777813142698; 0.0008108654501895264 -0.002069527547353827 -0.010201717802848145; 0.034561814232433444 -0.014025534635558886 -0.008973491598575703; 0.08747966934536043 -0.003895559625340753 -0.007112515261902957; 0.15550075175184433 0.018424169433452726 -0.005669922341139337; 0.20248982822207362 0.14526574995002947 0.0013158139705482853; 0.1119856201004996 0.257928321038749 0.011672620538172137; -0.013956968702964088 0.25905748898149866 0.016710191647944732; -0.08713823665180384 0.20616330494298554 0.01620667875500915; -0.10696574449396443 0.13889689572070454 0.012648766692620108; -0.09152920511480982 0.07897071043001104 0.008095327395193714; -0.05734765938030889 0.03602736492249166 0.004000200225081728; -0.018669314030212245 0.009667853783132363 0.0010959107001852323] %
+
+Mass Used: 102.10077631610102 kg
+Launch C3: 59.395512899082384 km²/s²
+||V∞_in||: 3.256994044580908e-9 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:26:22.750/plot.html b/archive/EM_3-29/EM_2022-03-29T21:26:22.750/plot.html
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:29:32.797/mission b/archive/EM_3-29/EM_2022-03-29T21:29:32.797/mission
new file mode 100644
index 0000000..efd6cc4
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+++ b/archive/EM_3-29/EM_2022-03-29T21:29:32.797/mission
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+/home/connor/projects/thesis/archive/EM_2022-03-29T21:29:32.797/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-23T04:29:27.925
+Launch V∞: [3.3948803973755504, -2.4577679470301823, -0.9108626328289409] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-9.533352172826976e-10, -9.477177141496064e-10, -1.6329568148050564e-9] km/s
+ V∞_out: [-4.993330429282141e-10, -4.2879092581858787e-10, -2.3614363530159443e-10] km/s
+ time of flight: 1.7632014328727353e8 seconds
+ arrival date: 2029-12-23T22:18:30.925
+ thrust profile: [0.03456534559612611 0.003378817240313221 -0.005847373254693159; 0.00947257573188261 0.018201878458255185 0.007200303057438418; -0.004323909654354275 0.01249526284025378 0.0148773281730713; -0.01158118824683763 0.0035968703342061353 0.015269664673521784; -0.014059676447250516 -0.008412132946442719 0.008604541649422459; -0.005532635332091579 -0.0222637656012968 -0.0034383221186402285; 0.021986188048601012 -0.02106400050803527 -0.008639248086466517; 0.017681089333976076 0.009993783002874504 0.003021725433334957; 0.0019228014351383971 0.011070063719295309 0.013061259255238647; -0.006139542196052064 0.004677076522798168 0.015910259868307026; -0.008545089251963688 -0.004479324701411431 0.011537788412234507; -0.0016877898391656034 -0.011682836725100527 0.0011701415189322448; -0.0003566125916268421 -0.01179761558953741 -0.008519419526240076; 0.014749885872094748 -0.0029190252507672954 -0.0019352156873499635; 0.00424054036493813 0.005291076160963761 0.010144665911928733; -0.002562774524319081 0.0018319412240714573 0.0157273231044577; -0.004535441668234806 -0.00482430642022855 0.014079386327258895; 0.0021824954095405903 -0.011442073033427643 0.0056673371449387985; 0.00910349572655102 -0.00026356393299342343 -0.0060482701344148565; 0.0010618127127533534 0.0009141380026824337 -0.006122360667166782] %
+
+Mass Used: 24.97711287513448 kg
+Launch C3: 18.395506929817802 km²/s²
+||V∞_in||: 2.1150803439214027e-9 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:29:32.797/plot.html b/archive/EM_3-29/EM_2022-03-29T21:29:32.797/plot.html
new file mode 100644
index 0000000..4626989
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:30:57.022/mission b/archive/EM_3-29/EM_2022-03-29T21:30:57.022/mission
new file mode 100644
index 0000000..8c4359a
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:30:57.022/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:30:57.022/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-12T01:36:00.330
+Launch V∞: [-0.34441487078455013, 3.9103321083115397, 2.032019563693426] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-1.323280834421365e-9, -1.305249079827022e-9, -1.756498248174488e-9] km/s
+ V∞_out: [-2.072434338771005e-9, 3.1188692292717017e-10, -9.96060247089551e-10] km/s
+ time of flight: 1.9187428749374934e7 seconds
+ arrival date: 2025-05-22T03:26:28.330
+ thrust profile: [-0.0006647023892816537 0.004035322252316528 0.002450694309122812; -0.0010810936123367345 0.0033648421104130093 0.003041727879478422; -0.0013507121101609906 0.0028319436906776322 0.003294754033895274; -0.0013817337282281677 0.002283246633035519 0.003911472841560675; -0.0014099790469406482 0.0016622747910402052 0.004243346099566735; -0.0012603732201070137 0.0013617718291820912 0.004609732990326976; -0.001109687893062513 0.0010166792245012248 0.005257291391887101; -0.0009765487656423202 0.0007701050283466614 0.0045962916304727545; -0.0008511110507625 0.0005562454707099463 0.004264167411226241; -0.0007373982279473773 0.00044288704744547956 0.0042335052666390175; -0.0005724074417038922 0.0002590516109966243 0.003593127587839534; -0.00048097983471947337 0.00027784548514532824 0.0036573739539471012; -0.0004010082145124844 0.00023837273061184575 0.00295844216959782; -0.00030319886238157107 0.000188351968848797 0.0026590665546669954; -0.00013453010791864773 0.00015049323913512056 0.002533970064140107; -0.00017918516868998714 0.00011876509991415298 0.0020961759015662375; -0.0001309746244392474 9.400293297511669e-5 0.0016359370993405285; -8.735433670043718e-5 6.50059985134959e-5 0.0011999019334906667; -5.205594667799379e-5 3.959950287622984e-5 0.0007255745258836434; -1.69083877031164e-5 1.3250954732018612e-5 0.0002522304876801491] %
+
+Mass Used: 0.5263628244356369 kg
+Launch C3: 19.53842230774253 km²/s²
+||V∞_in||: 2.5573489052095017e-9 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:30:57.022/plot.html b/archive/EM_3-29/EM_2022-03-29T21:30:57.022/plot.html
new file mode 100644
index 0000000..7f9ce08
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:33:01.420/mission b/archive/EM_3-29/EM_2022-03-29T21:33:01.420/mission
new file mode 100644
index 0000000..ffb4f56
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:33:01.420/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:33:01.420/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-03-11T16:02:09.080
+Launch V∞: [7.290339628882368, -1.8288440801615886, -6.632030600228825] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-0.003664456556782759, -0.0036510052522354575, -0.0017682821659383713] km/s
+ V∞_out: [-0.1893444115511239, 0.18934441155112372, -0.07646642757306271] km/s
+ time of flight: 9.309960005487782e7 seconds
+ arrival date: 2026-02-21T05:02:09.080
+ thrust profile: [-0.1746457094907778 -0.05324520729862655 0.49134886061939687; -0.627027503294072 -0.40066969942751784 0.5818755748236487; -0.4247709197544459 -0.70455535681447 -0.18137441849457178; 0.39985450427415964 -0.6472758630327436 -0.6430237844213548; 0.4656645028614102 -0.26488366431804417 -0.7314105489598725; 0.1191067639913546 0.2223158565414293 -0.7468478853961351; -0.3933541564722199 0.058176480588614785 -0.7289724142316767; -0.5058338906252844 -0.4156231661282735 -0.5643546902998223; -0.5318185912755031 -0.6386622831457283 0.08080900296257724; 0.27321630774062744 -0.7220941798748955 -0.042143171437234374; 0.5425105272566577 -0.48807460643793443 -0.3531814327468772; 0.3522022888052473 0.06262879123129814 -0.6401364976996247; -0.1561236716305922 0.5164836976614604 -0.7196848157274702; -0.6067507933991897 0.5079757344850814 -0.7392991893046754; -0.7130116758304386 0.10035106755129632 -0.6845824948634448; -0.6878836289874771 -0.5954631055945753 -0.6809457412241607; -0.3269757395259158 -0.7281706083760071 -0.725121591528696; 0.5029082823724691 -0.7211592525685994 -0.6308100968795103; 0.5368458661526178 -0.4216537659711369 -0.14188422812553816; 0.16194407043490938 -0.2071575272584137 0.018329982767622783] %
+
+Mass Used: 633.2884274220719 kg
+Launch C3: 100.4775524563663 km²/s²
+||V∞_in||: 0.005466708610011581 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:33:01.420/plot.html b/archive/EM_3-29/EM_2022-03-29T21:33:01.420/plot.html
new file mode 100644
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:44:52.679/mission b/archive/EM_3-29/EM_2022-03-29T21:44:52.679/mission
new file mode 100644
index 0000000..6732d8e
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:44:52.679/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:44:52.679/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-01-22T12:08:19.865
+Launch V∞: [9.999999510580688, -9.997198712980596, 0.2367016801977378] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-0.000819918545143649, -0.0012451509155042646, -0.001250921976389137] km/s
+ V∞_out: [0.0019338785602035886, -0.0019338785602035886, -0.0006601321083539838] km/s
+ time of flight: 1.7233962915051136e7 seconds
+ arrival date: 2024-08-08T23:21:01.865
+ thrust profile: [-2.3909756762714905e-7 3.7137254328500285e-7 6.84557970113123e-10; -6.490849187612506e-7 -1.6923622503113822e-7 7.597297006308147e-8; -1.3462011970258392e-7 5.4785730096847575e-8 3.065595287593101e-8; 0.15976947743667638 -0.2920794439050224 0.002394761620150665; 0.5616910709675398 -0.7901992734350411 0.010726222487855458; 1.0 -1.0 -0.0032456678933753843; 1.0 -0.6953371235997132 -0.00807847832727659; 1.0 -0.23068593990468247 -0.009476805297354552; 1.0 0.06616898317798338 -0.009396139547492788; 0.8458292750604345 0.20752997653151717 -0.009416373557718996; 0.4899942520164369 0.18998472141046954 -0.007666776709170746; 0.03957676169176063 0.0210088124260986 -0.0012531497610165998; -5.452577185178014e-7 -3.4799035186607614e-7 -1.0511021967736704e-7; -1.3251613739747719e-8 3.0514099445579054e-7 4.002333800730656e-8; 1.6516923938790852e-8 -9.029916507496571e-8 8.144270988392475e-8; 6.025616118742147e-7 -5.477234118696148e-7 1.5445834673209101e-6; 1.2522336398625811e-7 -1.1634639614565971e-6 3.2890058545783734e-7; -1.8707392087284995e-7 1.037143716480063e-7 2.3487962795435016e-7; -1.0032847526436222e-6 -9.961208338104671e-7 1.0945507651240803e-6; 1.5694593639258316e-6 -4.2952948369892885e-7 -3.8494467904625947e-7] %
+
+Mass Used: 50.813640071233294 kg
+Launch C3: 200.0000000038433 km²/s²
+||V∞_in||: 0.0019461431124315834 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:44:52.679/plot.html b/archive/EM_3-29/EM_2022-03-29T21:44:52.679/plot.html
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index 0000000..9bcfd5c
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:46:54.102/mission b/archive/EM_3-29/EM_2022-03-29T21:46:54.102/mission
new file mode 100644
index 0000000..5a15e22
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:46:54.102/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:46:54.102/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-11-11T17:47:11.536
+Launch V∞: [-2.637789291564701, 7.365806125093766, 1.1946168639279173] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-0.044388255339722446, 0.05279424355864281, 0.05040248633053719] km/s
+ V∞_out: [-0.014690038570962082, 6.047928149069252, 0.0402218040709599] km/s
+ time of flight: 9.338400004077721e6 seconds
+ arrival date: 2025-02-27T19:47:11.536
+ thrust profile: [4.550817449124052e-7 7.763476095695704e-6 -8.951834889878114e-5; -1.683989066220231e-5 6.926242475714976e-5 -2.8801022778955843e-6; -3.2857446755970286e-5 0.000111131319945128 5.116462056209784e-6; -1.8729031546388233e-5 5.436146435025702e-5 8.422047807261321e-5; -3.937488649940267e-5 0.00012696227955243206 -8.532134224201484e-5; -1.0059863865866885e-5 2.4658136117281536e-5 -1.684375841787375e-5; 4.906742377377519e-5 -0.00012829316592757872 0.00011336735200215563; 2.089328062485444e-5 -4.091796173674061e-5 4.91054297730873e-5; 3.6303103564460345e-6 -8.192507389662463e-6 0.00018463100624064758; 9.183017844786658e-5 -0.000102961513685098 -2.2996942742832565e-5; -3.570454906404795e-6 7.063475253086773e-7 4.489457323974194e-5; 4.501722144285221e-6 -1.4070298502410475e-5 0.00012324041685903012; -1.7478055220611036e-6 2.873220524346435e-5 -0.0002474631986841141; -2.3178341505326345e-7 6.162662443854e-5 -0.00036775871159988626; 5.113474717292926e-6 0.00011622972164925676 -6.003368153265286e-5; 3.496467618704115e-6 2.008310733865503e-6 -3.261195379666672e-5; 7.630237920042993e-6 1.1841800841292385e-5 -5.3531357169394734e-5; -2.435474741947106e-5 -3.088566762921298e-5 8.568030368819686e-5; 2.05686426229734e-5 2.1197875883934535e-5 -3.1608864977248355e-5; 2.6389349541919505e-5 2.927984365861755e-5 9.508078462673436e-6] %
+
+Mass Used: 0.00865322013714831 kg
+Launch C3: 62.64014167074321 km²/s²
+||V∞_in||: 0.08542809838298922 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:46:54.102/plot.html b/archive/EM_3-29/EM_2022-03-29T21:46:54.102/plot.html
new file mode 100644
index 0000000..17dca8d
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:49:25.266/mission b/archive/EM_3-29/EM_2022-03-29T21:49:25.266/mission
new file mode 100644
index 0000000..500aca1
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:49:25.266/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:49:25.266/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-01-22T05:21:14.524
+Launch V∞: [9.999636707630842, -9.999711031426283, 0.11421476860707167] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-0.0005668718069816592, -0.00031760816291536434, -0.000716139266867567] km/s
+ V∞_out: [4.602661802552677e-5, -0.0002767853386654524, -0.0009253970079822862] km/s
+ time of flight: 1.8504181207751602e7 seconds
+ arrival date: 2024-08-23T09:24:15.524
+ thrust profile: [7.857635262435799e-9 -1.3269126706634187e-9 -2.6678444933858832e-8; -1.0637360281620793e-8 -2.286988515481341e-8 -8.80823866575928e-9; 6.0952069265027294e-9 -2.83469800266583e-8 -1.490175153809855e-8; 0.0226345802482894 -0.0425037954420528 0.00013571022638739796; 0.3150512263564853 -0.3307029057599246 6.642556817831003e-5; 0.7436637294478844 -0.4801347645399363 -0.0017893772307274593; 0.8606779112586623 -0.24141142990090325 -0.0037932113948367296; 0.8040060250257044 0.016198399857395514 -0.004471603451557433; 0.6399746211803117 0.16197029278741412 -0.0044542497883041455; 0.3727551022451268 0.16851762370795223 -0.0032249765404340643; 2.1347115495508663e-7 1.2358201767787164e-7 -9.95030121314948e-9; -3.2446413607840104e-9 -4.6723722793820385e-9 -1.7929106379494995e-8; 5.182519495541647e-9 3.4030707061963687e-9 1.3576577417457207e-9; 7.77921539082814e-9 8.910703811213887e-9 -2.795024270457183e-9; -6.239445899255738e-9 -5.3493145318475e-9 -1.0884699785346293e-8; -4.6105410818633964e-8 1.0422534641378147e-8 -3.1989587412074714e-8; -5.043811123979896e-10 -1.5735249773983739e-9 -2.485221976312311e-9; -2.9761057764991258e-9 5.873921191568738e-9 -9.103537944568155e-9; 5.14444314540825e-9 2.6244355859150998e-8 -4.4579652417185817e-8; 1.7864549904100225e-9 -5.672782066774026e-9 -8.346804698233242e-9] %
+
+Mass Used: 30.632832509893888 kg
+Launch C3: 200.00000000999466 km²/s²
+||V∞_in||: 0.0009669922648350091 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:49:25.266/plot.html b/archive/EM_3-29/EM_2022-03-29T21:49:25.266/plot.html
new file mode 100644
index 0000000..40e3fed
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:49:36.826/mission b/archive/EM_3-29/EM_2022-03-29T21:49:36.826/mission
new file mode 100644
index 0000000..8b2d34e
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:49:36.826/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:49:36.826/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T10:56:11.057
+Launch V∞: [6.441902798268679, 10.0, -0.8580312930039031] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [1.1346777920325148e-7, -1.6337616718675993e-7, 1.0330204534180961e-7] km/s
+ V∞_out: [-1.0317733873112507e-7, 2.3171717331048837e-6, -1.93986714938645e-8] km/s
+ time of flight: 3.4632733537038654e7 seconds
+ arrival date: 2025-06-20T07:08:24.057
+ thrust profile: [-1.6714820918342543e-8 -1.528466539382287e-8 -2.1954025843586096e-8; -3.349740604524035e-8 1.7981805687302658e-7 -7.022649953046174e-9; 1.8833170950448843e-8 8.548553623260635e-8 -4.108646810746605e-9; 0.015250670354150446 0.8084120898285189 0.022810952919723303; -0.4471453131878308 0.9999999903024106 0.04006905981158459; -0.940578331193299 0.999999993466643 0.0463151648707486; -0.9999999926560775 0.8872505298154237 0.043065678915645736; -0.9999999865564515 0.5078822642356666 0.04002774379588722; -0.962703858267274 0.25286276492713566 0.031382869157176016; -0.7756546264427393 0.08215017131953659 0.018158411737504068; -0.5391748150704597 -0.00685832535402532 0.010123577086814562; -0.28342464446445065 -0.029810747488727737 0.006770186169348639; -1.123224049355356e-8 -1.3141710495594749e-8 -1.7542653699628666e-8; -1.7528478886241226e-7 5.358445351823748e-9 -6.699375227774894e-8; -1.3135303081170559e-7 -1.2185271425829965e-7 -3.228097411495359e-10; 1.1373627184214759e-8 3.001014188079098e-8 -2.51036875849398e-8; 3.6364423359808617e-12 -1.1453961586869118e-7 3.15681037477465e-8; -2.2731576792249495e-8 -7.140875056921905e-9 -4.234566273922648e-9; -8.105071719032486e-8 -1.2311649733884225e-7 5.2532523546505e-9; 3.7930997639741155e-9 2.2050999807275034e-9 -1.6994076482759186e-8] %
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+Mass Used: 114.99761554896395 kg
+Launch C3: 142.2343293621158 km²/s²
+||V∞_in||: 2.2413839807974726e-7 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:49:36.826/plot.html b/archive/EM_3-29/EM_2022-03-29T21:49:36.826/plot.html
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:49:40.929/mission b/archive/EM_3-29/EM_2022-03-29T21:49:40.929/mission
new file mode 100644
index 0000000..08c82aa
--- /dev/null
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+/home/connor/projects/thesis/archive/EM_2022-03-29T21:49:40.929/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-07-14T20:37:13.182
+Launch V∞: [-1.1330208167169828, 8.150093305408548, -0.42599383797196094] km/s
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+ Planet: Mars
+ V∞_in: [0.06785386315763219, 0.08160526029107552, 0.10069188976102801] km/s
+ V∞_out: [-0.06019693846168101, 0.1154681190090172, 0.0013638641321443625] km/s
+ time of flight: 3.3249599821579646e7 seconds
+ arrival date: 2025-08-03T16:37:12.182
+ thrust profile: [-3.2390308133578046e-6 -8.205592041810102e-7 -1.7023725789005115e-6; -4.254648394564359e-6 -1.0681074705420982e-5 7.03349069144519e-6; -3.6503599525277004e-5 1.211591857880556e-5 4.998821545861222e-5; 5.8142912412027884e-6 1.815497639490963e-5 4.755326622471413e-6; 2.1131283188873194e-5 -2.658343343429692e-5 -1.3407885571598285e-5; -4.61924068664863e-6 1.233572876146752e-5 5.931451952243551e-6; -1.0093023108865622e-6 -6.117529097643235e-6 -1.4487022912767236e-5; 3.255742051919883e-5 2.414843899996706e-6 -1.6802467693339598e-6; -3.755099218079546e-7 -7.03737787215465e-6 3.678113986874362e-7; 5.000413950443672e-6 -6.750857750004181e-6 -3.69195982831641e-6; -4.843006060165484e-6 -3.981873834068709e-6 -8.39506817046051e-6; 1.9138464837736528e-5 -1.1967250409666853e-5 -5.84236755572486e-5; 1.9835599971523244e-5 -7.450220189850961e-6 -3.2160727631147586e-6; 5.835552646320366e-6 -1.8859087544603728e-5 -9.49615711370029e-6; -2.455723410768635e-5 6.327003737755019e-6 -1.2577725131349784e-5; -5.262439904045446e-6 6.952002003737397e-6 -6.5460093506210335e-6; 1.29796109554274e-5 1.82478532330856e-5 -1.5041887536003234e-5; -9.627406878153045e-6 -5.772049645592626e-6 -1.4348219890042947e-7; -9.78894081123465e-6 3.3042544258109555e-5 1.5879718352840226e-5; -5.425039696689593e-7 -9.226404572856256e-6 9.61839430152342e-6] %
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+Mass Used: 0.006099916057792143 kg
+Launch C3: 67.88922780796933 km²/s²
+||V∞_in||: 0.14629566608835642 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:49:40.929/plot.html b/archive/EM_3-29/EM_2022-03-29T21:49:40.929/plot.html
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:51:28.498/mission b/archive/EM_3-29/EM_2022-03-29T21:51:28.498/mission
new file mode 100644
index 0000000..7ef879a
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:51:28.498/mission
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+/home/connor/projects/thesis/archive/EM_2022-03-29T21:51:28.498/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-09-29T06:36:19.325
+Launch V∞: [-2.587284640962116, 4.633341500696843, 1.7167586419161047] km/s
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+ Planet: Mars
+ V∞_in: [-0.19753746109783032, 0.25819074680887755, 0.26503536879040035] km/s
+ V∞_out: [-0.315758776271297, -0.8539914904213332, 0.8539914904213984] km/s
+ time of flight: 1.5073200002586758e7 seconds
+ arrival date: 2025-03-22T17:36:19.325
+ thrust profile: [-7.450599065824146e-9 -7.450584303466995e-9 -7.450590836663176e-9; -7.450587576906885e-9 -7.450589090923008e-9 -7.450558189003243e-9; -7.450565194803655e-9 -7.450611457729077e-9 -7.45054991590754e-9; -7.450600513649451e-9 -7.450590716301945e-9 -7.450607153363093e-9; -7.450528020006835e-9 -7.450561990165038e-9 -7.450526461597745e-9; -7.450555250204573e-9 -7.450607011409635e-9 -7.450602548674602e-9; -7.450564628439462e-9 -7.450600629100434e-9 -7.450588565463268e-9; -7.450619650423247e-9 -7.450608473513382e-9 -7.4505692480758075e-9; -7.45064263594121e-9 -7.450567115419777e-9 -7.450562075663264e-9; -7.450580126235538e-9 -7.450587476295809e-9 -7.450568854754488e-9; -7.4505366612824064e-9 -7.450589324902333e-9 -7.450584239263405e-9; -7.450489666957581e-9 -7.450537925286817e-9 -7.450498460628677e-9; -7.450552685353022e-9 -7.450579447503591e-9 -7.450633939663657e-9; -7.450616725224094e-9 -7.45060730810255e-9 -7.450610502067296e-9; -7.450581072447471e-9 -7.4505612150820725e-9 -7.450606871304834e-9; -7.450563685058705e-9 -7.450550577646896e-9 -7.450584512906325e-9; -7.45058338424796e-9 -7.45058208960814e-9 -7.45059162827976e-9; -7.450547249176265e-9 -7.450555252809561e-9 -7.450551428356576e-9; -7.45060469168066e-9 -7.450619817820747e-9 -7.450626574693086e-9; -7.450591348730228e-9 -7.450569077582649e-9 -7.4505992975666e-9] %
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+Mass Used: 1.549092758068582e-6 kg
+Launch C3: 31.109155510031766 km²/s²
+||V∞_in||: 0.4194368331281437 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:51:28.498/plot.html b/archive/EM_3-29/EM_2022-03-29T21:51:28.498/plot.html
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:58:30.321/mission b/archive/EM_3-29/EM_2022-03-29T21:58:30.321/mission
new file mode 100644
index 0000000..e4bf142
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:58:30.321/mission
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+/home/connor/projects/thesis/archive/EM_2022-03-29T21:58:30.321/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-12-10T18:17:03.345
+Launch V∞: [-0.22142913746497983, 8.613702367564114, 0.395646369589788] km/s
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+ Planet: Mars
+ V∞_in: [-0.003807700964755288, -0.05635954129158412, -0.008059749565666045] km/s
+ V∞_out: [-0.004673762071972183, 0.023969198600263253, 0.0032827185153388007] km/s
+ time of flight: 2.211840042633046e7 seconds
+ arrival date: 2025-08-23T18:17:03.345
+ thrust profile: [-2.7099961488351806e-5 -1.4871074056565297e-5 -2.4409683044127975e-5; 9.646611740529691e-6 -0.0003420396277143331 -1.4868108643254946e-5; 2.133935422770787e-5 -4.4306217453697985e-6 -4.803508959276009e-5; 2.4459845792704493e-5 -3.6995123289765117e-5 -2.9925040076576046e-5; -3.650950167903471e-6 -7.838803352580581e-5 2.4747499455879648e-5; -6.523041671648795e-5 3.5087934323253556e-6 -2.4005599476677803e-5; 2.5824401386028627e-5 -5.305113471826212e-5 4.630647640937965e-5; 3.106981203665597e-5 3.544948660180863e-5 5.523446183421823e-5; 5.22286273436312e-5 0.000123040814806458 -0.00012676926781162037; -7.230267382777404e-5 -0.000260285686999283 0.00028378411056846934; -6.687818964937921e-5 0.00010386642943476749 -1.7433504223833023e-5; 1.628396440937132e-5 9.706470918419143e-6 -2.010464752776144e-5; 1.7691694085809603e-5 1.8769928239818888e-5 8.64374415484856e-5; -1.9940109128613944e-5 -2.4978683584950083e-5 8.154400491960929e-5; 3.746496390446149e-5 -7.996841154215747e-5 8.731190252691787e-5; 8.384626723016047e-5 0.00012055180341030887 -9.12903721447452e-5; 0.00030557244279303915 -1.0874417231438263e-5 0.00027076266521899666; 0.00010797337086871226 2.418131034629288e-6 2.46314050788356e-7; -4.8544246038547224e-5 8.023388406493804e-6 -1.3321622294600293e-6; -2.1337222473883922e-5 0.000161247930621023 -9.715049457277587e-5] %
+
+Mass Used: 0.024185192960430868 kg
+Launch C3: 74.4014353896677 km²/s²
+||V∞_in||: 0.05706010904560232 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:58:30.321/plot.html b/archive/EM_3-29/EM_2022-03-29T21:58:30.321/plot.html
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diff --git a/archive/EM_3-29/EM_2022-03-29T21:59:56.201/mission b/archive/EM_3-29/EM_2022-03-29T21:59:56.201/mission
new file mode 100644
index 0000000..4340585
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T21:59:56.201/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:59:56.201/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-11-02T06:44:24.402
+Launch V∞: [-0.049611423370383025, 4.3887768099156235, 0.2397844149782377] km/s
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+ Planet: Mars
+ V∞_in: [-0.28117135821620853, 1.194065776563358, -0.1878338484580809] km/s
+ V∞_out: [-0.6401552299219904, 1.0676650444881157, -0.004843562733730455] km/s
+ time of flight: 2.8675341966952853e7 seconds
+ arrival date: 2025-09-30T04:06:45.402
+ thrust profile: [-6.75010685435156e-9 -7.128389367903114e-9 -6.764569952771536e-9; -7.854492591597582e-9 -7.999190980986096e-9 -7.56171297045386e-9; -7.411321266505082e-9 -7.3114050701082215e-9 -7.55580573230112e-9; -7.651530680516069e-9 -7.666997827122132e-9 -8.49436628413585e-9; -8.211778239957757e-9 -7.712874354717269e-9 -7.531646409796486e-9; -1.3041223632506712e-8 -1.1505347567528765e-8 -1.1327175955299429e-8; -7.4382917597938215e-9 -7.470595276285478e-9 -7.436526503122886e-9; -7.4066384907957325e-9 -7.477391356913722e-9 -7.393627041672364e-9; -8.490728461637439e-9 -7.447948593375514e-9 -8.223435454942976e-9; -7.243567265436005e-9 -6.990848569720015e-9 -7.311069521989123e-9; -7.470925069700345e-9 -7.517096742281904e-9 -7.2858921115831336e-9; -5.251447999281985e-9 -5.273780973491265e-9 -6.675361320542912e-9; -7.558627194101523e-9 -7.492146820031137e-9 -7.45645012297696e-9; -7.2878343544302096e-9 -7.2766617254979426e-9 -7.221830929334092e-9; -1.5590145011707196e-9 -1.974892338935215e-9 -1.3189839304906718e-9; -4.649692239474741e-9 -5.02145900568508e-9 -3.3671118225301505e-9; -7.850732664606476e-9 -7.768068826428585e-9 -7.4479836858425065e-9; -7.24166072771011e-9 -7.280881665927263e-9 -7.234374477741455e-9; -5.484578641350827e-9 -5.45192526011684e-9 -5.410771310297238e-9; -7.621367481763838e-9 -7.564226463702764e-9 -7.592122009986836e-9] %
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+Mass Used: 2.8080553420295473e-6 kg
+Launch C3: 19.321319746248445 km²/s²
+||V∞_in||: 1.2410205341039189 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T21:59:56.201/plot.html b/archive/EM_3-29/EM_2022-03-29T21:59:56.201/plot.html
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diff --git a/archive/EM_3-29/EM_2022-03-29T22:02:40.626/mission b/archive/EM_3-29/EM_2022-03-29T22:02:40.626/mission
new file mode 100644
index 0000000..ed548d2
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:02:40.626/mission
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+/home/connor/projects/thesis/archive/EM_2022-03-29T22:02:40.626/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-12-05T12:41:35.605
+Launch V∞: [0.34208345982054794, 9.685722102267114, 1.0135726196799333] km/s
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+ Planet: Mars
+ V∞_in: [-1.044189695816697, 5.606992695460721, 0.6669749140025341] km/s
+ V∞_out: [-1.663147851968031, 4.139628155579746, 0.7399548282520139] km/s
+ time of flight: 1.1581200001669213e7 seconds
+ arrival date: 2025-04-18T13:41:35.605
+ thrust profile: [-4.6079105664078877e-5 -0.00012331290696458524 3.857290588633784e-5; 1.080629253868903e-5 -7.862558725402423e-5 -1.577782579822753e-5; 0.00012294508889228685 0.0001157766111977547 -7.561217621375722e-5; 7.982229075851814e-5 -3.220285538923316e-5 -4.4317366310939693e-5; -2.379024823156827e-5 -7.848301760916924e-5 1.0173976438826385e-5; -5.0258317369872474e-5 -9.493318759847104e-5 2.0214040124684093e-5; -5.091418646156128e-5 -0.0001217205174737956 1.2898657418352046e-5; 2.8918514216456975e-6 4.8713183689657356e-5 8.218982364067898e-7; -7.013970277251351e-5 0.00016984599894599242 4.472426555147454e-5; 4.101982487628375e-5 -0.00014567448690259096 -4.20309304000344e-5; -4.70029927248979e-5 -8.284004507475568e-5 1.8925597178656232e-5; 8.670365778542101e-5 7.723828389414057e-5 -4.728960557142774e-5; -1.1273042710496325e-5 1.5796318007177794e-6 1.004719027628209e-5; 1.156788959809497e-5 -9.12107530024284e-5 -4.421958910455016e-5; 5.8489607768559684e-5 -3.186318691478282e-5 -7.568690979128904e-5; -4.101390839132036e-5 -6.912092662580811e-5 1.875683893727222e-5; -9.282793252271017e-5 1.8581365311066747e-5 0.0001607242504965489; 2.5608653889505896e-5 2.5749263651290097e-5 -2.663654795135107e-5; 6.471735913709624e-6 -1.582848279061017e-5 -3.144105357929748e-5; -2.0418356210322056e-5 -5.206011476136069e-5 1.0750219832116774e-6] %
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+Mass Used: 0.009526397249373986 kg
+Launch C3: 94.95756319119332 km²/s²
+||V∞_in||: 5.742260421097979 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T22:02:40.626/plot.html b/archive/EM_3-29/EM_2022-03-29T22:02:40.626/plot.html
new file mode 100644
index 0000000..13a6921
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diff --git a/archive/EM_3-29/EM_2022-03-29T22:11:59.808/mission b/archive/EM_3-29/EM_2022-03-29T22:11:59.808/mission
new file mode 100644
index 0000000..ff0331e
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:11:59.808/mission
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+/home/connor/projects/thesis/archive/EM_2022-03-29T22:11:59.808/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-07-12T14:57:14.038
+Launch V∞: [-2.1356055281697612, 10.0, -9.769298185542464] km/s
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+ Planet: Mars
+ V∞_in: [-1.4198898735875047, 1.3740951409636546, -1.4192321863480188] km/s
+ V∞_out: [1.4110404995307853, -2.1212048062899553, -0.6728408923695377] km/s
+ time of flight: 1.5440221824979678e7 seconds
+ arrival date: 2025-01-07T07:54:15.038
+ thrust profile: [0.05956977091681903 1.0 -0.10922677780373319; 0.23817833345981507 1.0 0.09826946570814477; 0.40293966085543176 1.0 0.3551237041998419; 0.5317072540959735 1.0 0.7307023601163831; 0.5078043727484851 1.0 0.9982992529843099; 0.33655425425041224 1.0 1.0; 0.1360349738666649 1.0 1.0; -0.026672364591518467 1.0 1.0; -0.19610649486002443 1.0 1.0; -0.29528444695253986 1.0 1.0; -0.35123463549962813 1.0 1.0; -0.3634631832054668 1.0 1.0; -0.34243556937322644 1.0 1.0; -0.2988969593988343 1.0 1.0; -0.23211645533604322 0.8701239790258618 1.0; -0.13699199073043578 0.48199643592034935 0.6802560133378645; -4.9400538315483375e-8 1.4543622135653008e-7 2.2274035599587473e-7; -2.6590282235167093e-8 6.069199505306199e-8 7.406086114073912e-8; 7.262188061710368e-8 -2.6660015831706114e-8 -1.054025466018286e-8; 7.299781920337516e-9 5.276251956583804e-9 -2.5519508317922344e-8] %
+
+Mass Used: 130.30806476829775 kg
+Launch C3: 199.99999800999254 km²/s²
+||V∞_in||: 2.432785380649605 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T22:11:59.808/plot.html b/archive/EM_3-29/EM_2022-03-29T22:11:59.808/plot.html
new file mode 100644
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diff --git a/archive/EM_3-29/EM_2022-03-29T22:26:29.640/mission b/archive/EM_3-29/EM_2022-03-29T22:26:29.640/mission
new file mode 100644
index 0000000..0dd48a4
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:26:29.640/mission
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+/home/connor/projects/thesis/archive/EM_2022-03-29T22:26:29.640/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T14:47:37.584
+Launch V∞: [8.454590640928295, 9.260765024912534, -0.9885318724952183] km/s
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+ Planet: Mars
+ V∞_in: [-0.006319696103929528, -0.0412349395695302, 0.025407019305862494] km/s
+ V∞_out: [0.022415695471427622, -0.032554221329412304, 0.028687979305271248] km/s
+ time of flight: 1.8230010689416587e7 seconds
+ arrival date: 2024-12-07T14:41:07.584
+ thrust profile: [-0.0002622529733463554 0.00010449975350988813 -0.00012030102951252053; 2.2564340820408038e-5 -3.981832926552484e-5 -7.923191359546866e-6; 5.169422416636556e-5 -5.810036687510864e-5 0.00011428268526115506; -0.00014971921355914664 -0.00014100200005065646 0.00016890254129742059; 0.00015620328410727985 -3.366292385390309e-5 -0.00020340087014733029; -3.210609078978168e-5 -6.498562052193143e-5 5.338807325839352e-5; -8.516237377437068e-5 -0.0001612296252470605 4.209812632127493e-6; 6.305171484191589e-5 -0.001682367723787057 3.8599641512170114e-5; 2.2345674659450702e-5 6.798172919803859e-5 -0.0001184406426706027; -1.6251278244512348e-5 -6.533351590187232e-5 -3.92438433311786e-6; -0.00036512149400096404 -4.6068321314717516e-5 -5.609213629078427e-5; -5.621377289755845e-5 2.1241246976381148e-5 -3.414115489177037e-5; -0.00034119461694600184 -6.972852980194507e-5 2.2003699273903694e-5; 0.00018976563510694219 -9.050300294247073e-6 0.00012300348192681063; 5.426150865573059e-5 -0.00010044444909460297 4.785290273646994e-5; -4.4309429079208605e-5 7.02628779669344e-5 -4.7916743218706474e-5; -8.408538773370183e-5 -4.412949196949812e-5 2.4492265814848663e-5; 0.00011172380033234707 6.642438716286984e-5 9.399896039444412e-6; 8.401331768830077e-6 4.877367093015932e-6 -1.2408399381198787e-6; 9.503407085636648e-5 -0.0002551562074474474 -1.3659784774574114e-5] %
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+Mass Used: 0.03575572314321107 kg
+Launch C3: 158.21906701525444 km²/s²
+||V∞_in||: 0.0488444001924202 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T22:26:29.640/plot.html b/archive/EM_3-29/EM_2022-03-29T22:26:29.640/plot.html
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diff --git a/archive/EM_3-29/EM_2022-03-29T22:29:19.608/mission b/archive/EM_3-29/EM_2022-03-29T22:29:19.608/mission
new file mode 100644
index 0000000..82ca627
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:29:19.608/mission
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+/home/connor/projects/thesis/archive/EM_2022-03-29T22:29:19.608/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-10T01:24:19.159
+Launch V∞: [-1.361280774218496, 4.248905515475195, 1.6131303371846983] km/s
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+ Planet: Mars
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+ V∞_out: [1.3258015388055073, 0.008890670618699885, -0.015202352520394155] km/s
+ time of flight: 1.6044052824580787e7 seconds
+ arrival date: 2025-04-13T18:05:11.159
+ thrust profile: [-9.649476733530478e-5 -3.874129604104022e-5 0.0001243676257598534; 0.00017944991783773494 -0.0003021068710903314 -0.00023906829442885233; -1.2520197657221369e-5 7.529839362963302e-5 5.22491643077963e-5; 6.0473365960938625e-5 -0.00010443015036179195 0.00013074051319186437; 0.0006044516898117107 -0.00017952114259198458 7.975422345770218e-5; -1.5105320951034641e-5 5.488422632601538e-5 -3.480125630187902e-5; -0.00035693490512667196 -2.9324170471654634e-5 9.386409045588269e-5; 0.0006536233376695634 -0.000323215551438777 -0.000991075858075292; -0.00048048705998534366 -0.0008846136053753608 7.485312552148982e-5; 0.0002457539906734169 2.3610783147200267e-5 0.00031354855012369744; 0.0003084291416236774 0.00030133549870160124 0.00012216085485925468; -3.145870054396133e-5 9.600064248608948e-5 -0.00017139285888021958; 0.0002323428803906647 -0.0003932431132474737 -0.00038269549666544874; -9.648756923300717e-5 7.371414257236465e-5 -0.00010492608262327025; -0.00016513882219009883 5.681301427250039e-5 -0.00023413816734468073; 0.0001688227002363334 3.9296604381294236e-5 -0.0002465079878323193; 4.223349001330004e-5 0.00018462477409466818 0.0004274596352430292; -7.266996009870076e-6 -0.00023420474628868667 3.054421622059266e-5; 4.4599716714522025e-5 -0.00015080232626015259 -0.00017624139057002226; 2.058233894174994e-5 -2.9681895453803056e-5 0.00010285445493880417] %
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+Mass Used: 0.04864906937473279 kg
+Launch C3: 22.508472910438055 km²/s²
+||V∞_in||: 1.3258674897215847 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T22:29:19.608/plot.html b/archive/EM_3-29/EM_2022-03-29T22:29:19.608/plot.html
new file mode 100644
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diff --git a/archive/EM_3-29/EM_2022-03-29T22:35:03.801/mission b/archive/EM_3-29/EM_2022-03-29T22:35:03.801/mission
new file mode 100644
index 0000000..5f23de7
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:35:03.801/mission
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+/home/connor/projects/thesis/archive/EM_2022-03-29T22:35:03.801/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-15T00:59:25.735
+Launch V∞: [0.08411754828864794, 3.867780292357817, 2.507975455218117] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-0.01111567461793714, -0.2019526290080634, -0.10099494494608693] km/s
+ V∞_out: [0.05863131293194478, -0.1437072200747788, -0.16341819092150492] km/s
+ time of flight: 2.122969403809613e7 seconds
+ arrival date: 2025-06-17T18:07:39.735
+ thrust profile: [-0.0019253353195135495 -0.006208595765491277 -0.0030413706831210283; -0.005094954059343889 -0.006884862652799308 -0.007716049803660748; -0.001169679362784149 -0.003040509785898553 -0.0023827736029818115; -0.0009800602675577555 -0.005005973318342694 -0.0007235675342944551; -0.0035541375195941027 -0.0010759580832810519 -0.0011368932928665326; -0.004023727803229634 -0.0024144419030426778 -0.0020601786180336804; -0.009415901341030907 -0.007648304620004416 0.008910953721132594; 0.00019160911662570728 -0.00041311185476429913 0.002747155966524439; -0.0005053512629044138 -0.000435305465528584 0.0010810134121178056; 0.0018400336528207576 -0.006748721129952468 0.002259933413232509; 0.00022745932395296879 0.010666778341568943 0.0035537786550811704; -0.0004423321131218159 -4.1278833244748e-6 0.0012966352168264361; 0.00584099379819922 0.010506361039734275 0.0023162665551785394; -0.0013489272396317838 -0.0016553055603146898 0.00247736021958195; -0.0003060718810677023 0.0030689000185227426 -0.00026453391075189313; -0.004902002300222478 -0.006091743775746333 -0.0007723370782334376; -0.0010727586684161662 -0.0015117821322166705 -0.0011100152254532457; 0.001981284413785558 0.002082711629710382 0.000757647029883398; 0.0002652136199514425 -0.004511943969868106 0.0007431379304516129; 0.0007883244474613861 -0.00476964812130089 3.034140598992801e-5] %
+
+Mass Used: 0.9889560483511559 kg
+Launch C3: 21.256741035858134 km²/s²
+||V∞_in||: 0.22607167334751047 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T22:35:03.801/plot.html b/archive/EM_3-29/EM_2022-03-29T22:35:03.801/plot.html
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diff --git a/archive/EM_3-29/EM_2022-03-29T22:38:25.802/mission b/archive/EM_3-29/EM_2022-03-29T22:38:25.802/mission
new file mode 100644
index 0000000..2ef267c
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:38:25.802/mission
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+/home/connor/projects/thesis/archive/EM_2022-03-29T22:38:25.802/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-07T17:37:26.448
+Launch V∞: [-1.132800064227913, 4.057296625668816, 1.8160423657393692] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-0.09025126720242063, -0.16294649165165395, 0.002018029101130675] km/s
+ V∞_out: [-0.18204756492089805, -0.026081869886201665, -0.0286582298370937] km/s
+ time of flight: 1.7138821243684784e7 seconds
+ arrival date: 2025-04-24T02:24:27.448
+ thrust profile: [-0.001053336200227854 -0.00028654474915887655 -0.0003820424031938627; 0.0008512529608243817 0.0008846317646016004 0.00025282033285603365; 0.00042096876484458586 -0.000407673670480482 -0.000928628092675361; -7.585307650884643e-5 -0.00013518461742213344 0.00156643510514752; 0.0008460627785635593 -0.0007843263217494761 -0.0007202803479853547; 0.002018749793184083 -0.00017983404176264242 -0.0006659097248956292; 0.00040668294946816447 0.0009420606711834561 -0.0007751842339076142; -0.0002948940003770048 1.1828072211327191e-5 -0.00013445879115795128; -0.0004411373325257146 0.002302823369497903 0.0007032460495624283; -0.0004305359949988352 0.0003086368359122586 -0.00012577020060691192; -0.0004796057040344445 0.00048325375373444216 -0.0012858708318398222; 0.0007082846291908338 0.0014131843493881463 0.0012334716036545182; 0.0007516628476279127 0.00019283672154011742 -0.00047698959544296255; 2.8585166048847224e-5 0.0004721397839283915 -0.0004494052618972365; 3.140121868826565e-5 1.8672409758238784e-5 -0.0010892419657405827; -0.0012387600934636242 0.0010224726118372646 0.0005096784526400515; 0.0004830392791164112 -0.00018504611294579005 -0.0007919144470676173; -0.0002823515956750592 0.00015118295801919124 -0.0004211043216927825; 0.000699667738192727 0.0008572250810665738 -0.00044787467026235686; -0.0013106710074165672 1.8187501171149852e-6 -0.0013087579926788614] %
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+Mass Used: 0.17400800233144764 kg
+Launch C3: 21.04290176833857 km²/s²
+||V∞_in||: 0.18628183704988058 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T22:38:25.802/plot.html b/archive/EM_3-29/EM_2022-03-29T22:38:25.802/plot.html
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diff --git a/archive/EM_3-29/EM_2022-03-29T22:49:56.957/mission b/archive/EM_3-29/EM_2022-03-29T22:49:56.957/mission
new file mode 100644
index 0000000..7caa4e9
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:49:56.957/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:49:56.957/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-09-12T20:18:50.704
+Launch V∞: [-1.2901325972737976, 3.5232401246782135, -4.555427856822656] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-0.47357409467459016, 0.6120735570744102, 0.2493748383223478] km/s
+ V∞_out: [-0.5474046060397546, 0.593375716049692, -0.4503838007744617] km/s
+ time of flight: 2.33568000005211e7 seconds
+ arrival date: 2025-06-10T04:18:50.704
+ thrust profile: [-3.7741093121961535e-8 -2.6257971335176648e-8 -2.1606384855810645e-8; -2.1363083523959785e-8 -4.234571308044473e-8 -8.269824340036801e-9; -1.7179727443085232e-8 -4.817903392853783e-9 1.1405733095493886e-8; 6.543773827193354e-8 7.63399812774497e-8 3.918240890364693e-8; 1.3414420888442994e-8 1.4060087327107107e-8 -8.242716667432803e-8; -1.8088388278070475e-10 -4.1359611682043475e-10 -9.03470171888568e-9; 4.3064264083954854e-9 3.2442366380236367e-9 -1.598356883588943e-8; 3.261934834405667e-8 6.450483621536437e-8 8.2007353416575e-8; -1.7993125019529573e-8 3.862145335097065e-9 5.231141768695811e-9; 2.5346874206765178e-8 2.0165133642770633e-8 5.961057304477184e-9; -1.8904868856526572e-8 -1.201092354618878e-8 -2.4170378084370648e-8; -1.1110813643371359e-8 -9.930972424447597e-9 -2.2310217231961474e-8; -2.3010965850571813e-8 -4.590923869358927e-9 -5.082758311888812e-8; -1.064446394813755e-8 -1.6835335671720645e-8 -4.524794179174139e-8; 1.6919283931076332e-9 2.0866300176185552e-9 -1.1111279350528446e-8; -4.352351680251087e-9 -5.215082497858078e-9 -1.2228449319478551e-8; 6.0054113300816905e-9 -7.05448971432868e-9 -5.6941027568265595e-9; -1.951082125424566e-8 1.1499547353566501e-8 -5.019589935213733e-8; 1.197134200084507e-8 -2.127430780809517e-9 4.800535709688631e-9; -1.311850186946498e-8 2.508766374053081e-8 3.5397163567430844e-8] %
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+Mass Used: 7.579702014481882e-6 kg
+Launch C3: 34.82958605340684 km²/s²
+||V∞_in||: 0.8130770396493041 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T22:49:56.957/plot.html b/archive/EM_3-29/EM_2022-03-29T22:49:56.957/plot.html
new file mode 100644
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diff --git a/archive/EM_3-29/EM_2022-03-29T22:58:44.883/mission b/archive/EM_3-29/EM_2022-03-29T22:58:44.883/mission
new file mode 100644
index 0000000..b6eedad
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:58:44.883/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:58:44.883/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-14T07:05:59.170
+Launch V∞: [1.6949045581275466, -1.1749158457323354, 0.4459844940604056] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [0.2807404173223861, -0.5148397948760617, -0.024574238754993954] km/s
+ V∞_out: [0.4816521199334624, -0.31105824990728403, 0.021223537272540942] km/s
+ time of flight: 1.0181159999765144e8 seconds
+ arrival date: 2026-07-05T16:05:58.170
+ thrust profile: [1.4156868146913603e-5 -8.937824771836181e-6 -1.4258721529256393e-6; 6.201501805968712e-6 4.891054084739865e-6 -2.4147768084891413e-5; 8.710377800639082e-6 -2.5247715656786118e-5 -4.228464809233087e-5; -5.49592858423698e-6 -5.956986519709633e-6 -6.0003598197038516e-6; -2.2049093171105036e-6 -2.489010425867444e-6 -3.9225913222362265e-6; 2.1078914306123458e-5 -1.1944173566312533e-5 1.8244198561717057e-5; 1.9561991087389005e-6 -1.1752657963774734e-5 1.683487450213938e-5; -6.055159240369156e-6 -2.206637657527475e-5 1.5277910735365964e-5; -2.1063568637137504e-5 1.0199794653949234e-5 -1.0165697723410959e-5; 0.0006945866286583284 -4.8718537131140276e-5 -0.0010004798714153944; 3.549819219472579e-6 -5.173787731590263e-6 -8.794510883495692e-6; -1.1187037009877784e-5 3.9873466996776687e-7 -1.2842230899218392e-5; 1.819371322436169e-5 -1.985114604615626e-5 7.40305445774715e-6; 4.351771410931808e-6 -1.2633771406394241e-5 4.02517242765969e-5; -0.00021811083392391314 -0.006360908650050679 0.007451776526230452; 0.4683451802604527 -0.7651039839559246 0.09069086407503833; 0.8713044694433868 -0.27831401933737787 -0.20462753606922815; 0.012344351227493076 0.0030669853424402133 -0.014728214668807213; 6.768683876914276e-6 7.65498676530381e-6 -2.3634699931764597e-5; 5.463932969042515e-8 1.6589754704890928e-6 -6.114493334584618e-6] %
+
+Mass Used: 75.80031539540141 kg
+Launch C3: 4.452030874656779 km²/s²
+||V∞_in||: 0.5869234102647126 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T22:58:44.883/plot.html b/archive/EM_3-29/EM_2022-03-29T22:58:44.883/plot.html
new file mode 100644
index 0000000..5d46c6d
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:58:44.883/plot.html
@@ -0,0 +1,30 @@
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diff --git a/archive/EM_3-29/EM_2022-03-29T22:59:31.051/mission b/archive/EM_3-29/EM_2022-03-29T22:59:31.051/mission
new file mode 100644
index 0000000..e671728
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:59:31.051/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:59:31.051/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-12-23T04:52:28.411
+Launch V∞: [-2.3721677208600336, -1.1471540814232561, 1.82724714241875] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [0.7657978493736273, 0.47268498190867225, 0.5669638080447448] km/s
+ V∞_out: [0.671344291602754, 0.7165876747149759, 0.4086328277033566] km/s
+ time of flight: 6.692110088878082e7 seconds
+ arrival date: 2026-02-04T18:04:08.411
+ thrust profile: [0.0008233730574660627 -0.0006089913686355275 -0.0003656792494954692; 9.277035119329392e-5 0.00018105994933842137 -0.00045064421020144603; -0.0009643656591043792 -0.0005295771327107068 -0.0003527133652685661; -0.0001829291084087302 -0.00028713103539127654 -0.0011612339233188311; 0.0002628094997902115 -0.00038049047451517036 -0.0004438420586700227; 0.00022847673868341134 -8.081668903608331e-5 -0.0004169573293423967; -0.00024469370633056417 -6.337239455279198e-5 0.0008380473882381952; 0.0007752101556583943 0.0006834443935228009 0.00015265143847038387; -5.4459788825500716e-5 -0.0014820986794018846 -0.0012653925633815618; -0.00021218967607504187 -0.00020847681093790597 -0.0002734855651715473; -0.00017082953277056904 -0.00011256508693154773 0.00152134489853549; -0.0007743596333968497 8.88770635961271e-5 0.001957585876424173; -0.0009465135793430943 -0.0008606487267644376 -0.000381605440474747; -0.002413182432020938 -0.0026073704810047824 -0.00027904268175806847; -0.0005254492375900773 -0.002157747734677348 -0.001799801241758866; -0.0005194698886906513 -0.001005331073405558 -0.0013843897937889358; 0.00048689741373146193 -0.001401700406807511 -0.0024375166130219906; 7.266464024313168e-5 -0.00033741672866423523 -0.0004478141428623512; -0.000586239166722991 0.00012793840622519977 -0.0009074360302595961; -0.00018809051058659194 9.565179941071708e-6 0.000633927457634841] %
+
+Mass Used: 0.7381269704351325 kg
+Launch C3: 10.281974301893808 km²/s²
+||V∞_in||: 1.0636378132897837 km/s
diff --git a/archive/EM_3-29/EM_2022-03-29T22:59:31.051/plot.html b/archive/EM_3-29/EM_2022-03-29T22:59:31.051/plot.html
new file mode 100644
index 0000000..2087a75
--- /dev/null
+++ b/archive/EM_3-29/EM_2022-03-29T22:59:31.051/plot.html
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diff --git a/archive/ES_0.5550120742732497 b/archive/ES_0.5550120742732497
new file mode 100644
index 0000000..6b537c5
--- /dev/null
+++ b/archive/ES_0.5550120742732497
@@ -0,0 +1,22 @@
+archive/ES_0.5550120742732497---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T21:35:13.618
+Launch V∞: [8.092028247187812, -5.690394550179761, 0.15870337020149677] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007258340410626599, -0.004915549405160574, -0.0003090327712008995] km/s
+ V∞_out: [0.0063943921161191295, 0.0029021314271309787, -0.005208376883488668] km/s
+ time of flight: 1.8749577773970667e8 seconds
+ arrival date: 2030-04-23T23:44:50.618
+ thrust profile: [0.23623549046119796 0.001523213801416841 -0.0746418855277079; 0.04989778371798442 0.028557974139368027 -0.05866465575542369; 0.035473791749751 0.032507089227488954 -0.0752484296384085; 0.022627986747173957 0.026966919764486865 -0.07156789250913552; 0.04964790396262216 0.0738833298025964 -0.19559483393516622; 0.030631999959579347 0.05365872568512533 -0.15864114884262576; 0.00671793812371244 0.012495789298607023 -0.044004855933096255; 0.006194981641432508 0.01299461151504057 -0.04773667381981179; 0.0013970455272782531 0.0035097621778593085 -0.014148581638031872; 0.0014625087521359605 0.004576093171820035 -0.01812047518926974; 0.0003621287391874434 0.001192919920759847 -0.003924447420406894; 0.0003136102108716024 0.0009510767434047032 -0.003683238027775159; 3.55672194873085e-5 0.0002056947097665128 -0.0009531573613879192; -0.0002219678836028774 0.0002992512020633661 -8.263424581589065e-5; -4.180089723821831e-6 8.500643051220536e-5 2.6176105870720138e-5; 3.966745018590377e-5 5.7559670861396866e-5 -0.0004168195496730593; 0.0002960669240380866 -0.00015608457398720793 9.887024972396908e-6; 2.993253329593611e-5 -0.0001879527007887196 -2.49699959259209e-5; 1.3018003450243295e-5 9.194287517786575e-5 -0.00012566784156294738; -0.0002730423797779337 -0.0001543084966874625 0.0006099289590901544] %
+
+Mass Used: 76.50834802879126 kg
+Launch C3: 97.8866980497143 km²/s²
+||V∞_in||: 0.00877163797273837 km/s
diff --git a/archive/ES_0.5550208270049417 b/archive/ES_0.5550208270049417
new file mode 100644
index 0000000..8aa873b
--- /dev/null
+++ b/archive/ES_0.5550208270049417
@@ -0,0 +1,22 @@
+archive/ES_0.5550208270049417---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:10:53.965
+Launch V∞: [7.99263082663398, -5.710825212380063, 0.28059984202471117] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.081837842560198e-10, -8.526455361768017e-10, -1.1565873973246667e-9] km/s
+ V∞_out: [4.964101468366639e-10, -4.5035093005423074e-10, 1.7219192649203768e-10] km/s
+ time of flight: 1.8749577787459874e8 seconds
+ arrival date: 2030-04-23T20:20:30.965
+ thrust profile: [0.32604352432509304 0.00497882797405257 -0.10153659307532245; 0.08445557926807248 0.04770044497023833 -0.09876572943386014; 0.033814070938876443 0.03018025570008468 -0.07300715991004297; 0.04608492411200257 0.0518833149313619 -0.1402660440388014; 0.03884834060219632 0.05278582239338074 -0.14923754573973316; 0.024518500102988346 0.03851013799255814 -0.12433716735236557; 0.00839084566979026 0.015974089948533197 -0.05717977600828847; 0.002497601368124247 0.0054421434781545845 -0.020810974438023645; 0.0012413447145525596 0.003104261838811333 -0.012454121622946294; 0.0002952832571111387 0.0006843670541546354 -0.0028868476886487614; 0.0002931078507387595 0.0009010664583775347 -0.0039940493932757075; 0.0006102507561287979 5.497645561287055e-5 -0.0019532697253708416; -3.7401073132043664e-5 0.00015948185812392776 -0.0007709409707993484; 1.226625166987844e-5 0.00024697253219265044 -0.0010752432398616358; 0.00014082333847703063 -0.0002924799291983615 -0.000786251473718327; 0.0003353336674723642 -0.000283886936406187 -0.00034286151268318505; -0.00015730876019493466 -0.00018136052791405924 -0.0005175862044128118; 0.0003787936943271113 -0.00016400095160184442 -0.0004126141053205723; 0.00016691849941922272 -8.257856256590926e-5 -0.0007529951300763956; 6.211451468212878e-5 -0.0006887860553681131 -0.00026154920097938784] %
+
+Mass Used: 84.17358245583273 kg
+Launch C3: 96.57440840855986 km²/s²
+||V∞_in||: 1.524122559570995e-9 km/s
diff --git a/archive/ES_0.5551378686311677 b/archive/ES_0.5551378686311677
new file mode 100644
index 0000000..8e77d2f
--- /dev/null
+++ b/archive/ES_0.5551378686311677
@@ -0,0 +1,22 @@
+archive/ES_0.5551378686311677---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:58:50.661
+Launch V∞: [8.11320959943097, -5.645724124239646, 0.16747696452458005] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8516363421996975e-10, 4.096121164742909e-9, -2.0697877390789584e-9] km/s
+ V∞_out: [2.0790724859932675e-9, 4.127970936657118e-9, 1.0865120878585403e-10] km/s
+ time of flight: 1.874916083184456e8 seconds
+ arrival date: 2030-04-24T01:58:58.661
+ thrust profile: [0.2754868791323259 -0.004110502019187116 -0.09891196486261492; 0.04324638696098478 0.02247517183605698 -0.05675135816253204; 0.03892904890147251 0.03216852322138361 -0.09100809525201009; 0.03303057370015382 0.035080690423428366 -0.11279234928351167; 0.02181869863261611 0.025269776676374003 -0.09431813772381838; 0.0169559793237119 0.03232455050637029 -0.13374662433915915; 0.016111389795168594 0.023249907977486148 -0.09458558132535513; 0.007205435769196988 0.014290387230894463 -0.07630245560011156; 0.0015616439293485633 0.002593925533434509 -0.014198480084020042; 0.0006398647395756223 0.0011455341196065034 -0.0066362673778835824; 0.00021448383373943162 0.00048461036268397813 -0.0020121857045428612; -0.0005031708667670048 -0.0003846320758830172 -0.0002312837647398825; 4.666007485336052e-5 0.00010280240718190181 -0.000841627809911724; -8.908260282730824e-5 -5.559857473515914e-5 -0.0008097588799996763; 1.4481010457650478e-6 -0.00016875008215481904 -0.0011842708445230653; 8.682995627457883e-5 8.033742269629829e-5 -4.432971042893808e-5; -0.00029798252705925894 0.00034156180315709714 -0.0006198193274259149; -0.0003061369792923545 -3.25929632625721e-5 -0.0007753052016491007; 2.7198081862265237e-5 -0.00015657437876687814 -0.00016057616392290677; -0.0005144350151837572 0.0002711169996963231 0.0005113294575712331] %
+
+Mass Used: 77.59006675738965 kg
+Launch C3: 97.72641942496672 km²/s²
+||V∞_in||: 4.598211410905106e-9 km/s
diff --git a/archive/ES_0.5552532074026435 b/archive/ES_0.5552532074026435
new file mode 100644
index 0000000..ecff99a
--- /dev/null
+++ b/archive/ES_0.5552532074026435
@@ -0,0 +1,22 @@
+archive/ES_0.5552532074026435---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T13:38:12.292
+Launch V∞: [8.091283750679898, -5.626635631419599, 0.189242070274835] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.760551537680362e-6, -5.050483257379123e-6, 3.7047645776349366e-6] km/s
+ V∞_out: [-1.1464642842370578e-6, -8.482842549920137e-6, 4.006955504298592e-7] km/s
+ time of flight: 1.8749577787195104e8 seconds
+ arrival date: 2030-04-23T15:47:49.292
+ thrust profile: [0.3001191479994197 -0.006491492540972167 -0.10464367891257732; 0.06669371816510525 0.03453350155639435 -0.08275270232210559; 0.03536397022771856 0.028803940826913527 -0.07940536141313202; 0.0479031470852905 0.05031449999723751 -0.15633707136393596; 0.0227660622647329 0.02810528294508086 -0.09968877657664008; 0.018663950493618714 0.02640831159581204 -0.10302780588601725; 0.0128353574734969 0.020056380762119467 -0.08538358674836405; 0.0031883438304667546 0.00558050655485686 -0.025950802036505877; 0.0027307797561800743 0.004971522664544287 -0.024911312123720334; 0.0028886832927905236 0.005725178841952505 -0.02999853498002678; 1.8498507329809847e-5 0.00026193660437474165 -0.0015378352139950996; 0.00017006631355532425 0.00033839543051414307 -0.0008140991473821627; 2.4363084752065985e-5 0.00025524852033090707 -0.0012725427249475124; 0.0001979064541212937 -0.00022515932940935895 -2.233079341374544e-5; -3.4010641263911365e-5 6.898200899598042e-5 0.0003681680601600602; 0.00014706194029745758 6.356885199978188e-5 0.00015283040927299658; 8.779556518282857e-5 -0.0002222581120165586 -0.0006308406782991736; 0.00038537671846016884 0.00019393847803101028 -0.000166612423212043; -0.00053483701939234 8.97317069416954e-5 -0.0002836580926078503; 0.0005714255507435241 -0.00021619220466183268 0.000304464977576498] %
+
+Mass Used: 81.00707799677275 kg
+Launch C3: 97.16371382393909 km²/s²
+||V∞_in||: 8.509795281147307e-6 km/s
diff --git a/archive/ES_0.5553166446815165 b/archive/ES_0.5553166446815165
new file mode 100644
index 0000000..b6dddd2
--- /dev/null
+++ b/archive/ES_0.5553166446815165
@@ -0,0 +1,22 @@
+archive/ES_0.5553166446815165---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:04:01.158
+Launch V∞: [8.077142685491271, -5.680604962234028, 0.22204191555666666] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.201127399571204e-5, 5.893101311930579e-5, 0.00409450763245035] km/s
+ V∞_out: [-0.0036567863569022425, -0.0012346203807321937, 0.001370498501299504] km/s
+ time of flight: 1.8749577787492463e8 seconds
+ arrival date: 2030-04-24T00:13:38.158
+ thrust profile: [0.23235381129437543 -0.003499034305839029 -0.08150403458003942; 0.101359804889319 0.053657256711614386 -0.12459306140607117; 0.05618052836256829 0.04661460558293996 -0.12432883331653731; 0.038855766875548 0.04125153478496184 -0.12666684845314194; 0.025324118959891024 0.03180040241628622 -0.11099802659340433; 0.018478048063072357 0.026519644261497784 -0.10244311481816155; 0.007574926049108344 0.012062456593750713 -0.051995067543366115; 0.002624539505975554 0.005028891200910454 -0.02411669381157359; 0.0006496950209796248 0.002177155222280389 -0.011592438398649882; 0.0028996826262880884 0.005977834449005585 -0.03111401744332391; 0.00030076578793983527 0.00014708272998598834 -0.001579162518567829; 0.00023884269622201395 0.000308440831864644 -0.0016554872014328096; 0.00016125989310068078 0.0002270644731231439 -0.0002677537550706303; -0.00013653939452338545 -0.00010107875347949283 -0.0006344926280171012; 0.000306835791899565 -2.9310951884917624e-6 -0.0007611802470456345; -0.00018689220058042605 -0.0006643014207581224 -0.00047628754239393363; -6.151749483983737e-5 -0.000734193329061956 -0.00030386985203754914; 2.7399404531041125e-5 -0.0001244879414403385 -6.18471749763314e-5; -3.344731595064874e-5 3.940331310237355e-5 0.00022350296642900322; -0.0008629912071055299 -0.0011018916049755144 -0.00047252733763793707] %
+
+Mass Used: 78.7763644808947 kg
+Launch C3: 97.55880931100707 km²/s²
+||V∞_in||: 0.004095752856992697 km/s
diff --git a/archive/ES_0.555321853072159 b/archive/ES_0.555321853072159
new file mode 100644
index 0000000..f51b308
--- /dev/null
+++ b/archive/ES_0.555321853072159
@@ -0,0 +1,22 @@
+archive/ES_0.555321853072159---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:57:24.826
+Launch V∞: [8.1332663571246, -5.661986515759155, 0.22766044177874376] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.123340652251088e-6, -3.7330513819710547e-6, -1.0846981586769346e-5] km/s
+ V∞_out: [-1.0492432785177735e-5, -1.2239051288617402e-6, 4.687451703815964e-6] km/s
+ time of flight: 1.859737203924726e8 seconds
+ arrival date: 2030-04-05T19:19:24.826
+ thrust profile: [0.22943973812293017 -0.004893967763726286 -0.0801253153441409; 0.03144507004413593 0.016005514878668727 -0.039605355975015175; 0.039054529766301194 0.03197291138034155 -0.08689490156094459; 0.0378685260709824 0.04018324616401574 -0.12252200644008435; 0.02803090143364196 0.03535274273841469 -0.12081216327733243; 0.022471665512052253 0.032497625582222536 -0.12157198448109055; 0.01926878492754949 0.03153169051058213 -0.1281842797483311; 0.004043038254003434 0.0066904694410549765 -0.031175306636595977; 0.005131609501874749 0.009234170160377442 -0.04469930754406368; 0.0003470121363472272 0.0008038663204159477 -0.0038167565883837525; 0.00017609752178919131 0.00036474064628598307 -0.001954724463038849; 1.130336567161233e-5 -3.20909344426444e-5 5.0861087076908916e-5; -1.4439041978965607e-5 6.264510601075898e-5 -3.5503708158925043e-5; 0.00012451312434083361 -0.00034084972505136796 -0.0002481717343390714; -2.1043042384554106e-5 -9.974133023427434e-5 0.00022586203596731763; 3.0325725366321253e-5 6.145296121523383e-5 -0.0003832387995866655; -0.0002927026986088235 0.0007786944928326911 0.00012097830464324579; 8.96770273673005e-6 3.9333968087291074e-5 4.9980603904861806e-5; -1.0699601379404263e-5 -2.0172052201893303e-6 0.000372228156627312; -0.0002084346014800331 0.00032609368117262434 -0.0008865061071454217] %
+
+Mass Used: 74.69249898312728 kg
+Launch C3: 98.25994221732427 km²/s²
+||V∞_in||: 1.152625595695103e-5 km/s
diff --git a/archive/ES_0.5553222117675201 b/archive/ES_0.5553222117675201
new file mode 100644
index 0000000..14db8d9
--- /dev/null
+++ b/archive/ES_0.5553222117675201
@@ -0,0 +1,22 @@
+archive/ES_0.5553222117675201---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T15:05:53.520
+Launch V∞: [7.978669656069434, -5.678185132210282, 0.06288544106185495] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.165312749478849e-9, -1.971227457841986e-9, -1.8369808751063008e-9] km/s
+ V∞_out: [-3.660281365501294e-10, 3.2999394084076575e-10, -1.267845070447127e-10] km/s
+ time of flight: 1.8749577786514547e8 seconds
+ arrival date: 2030-04-23T17:15:30.520
+ thrust profile: [0.39564242604082744 -0.006956512613986089 -0.13518366924321792; 0.06712585965363532 0.035648204482678 -0.08142867264258655; 0.04170290709783684 0.035350718096191905 -0.09174748789036437; 0.04352492608733409 0.04770407792297554 -0.14011401076264046; 0.02801348225631629 0.036772428672008674 -0.12141711140061484; 0.026283671902162534 0.04004047420482529 -0.1438274307468821; 0.00847703184692028 0.014366678634369039 -0.05804618230321489; 0.0021762412409529804 0.004185391744174946 -0.017954795552054398; 0.001079457307135401 0.0023049952563308574 -0.010602319561616915; 0.000416421577119403 0.0013468908459330865 -0.0071795189797770175; -0.0003591898924635163 0.0006952444828377452 -0.0024129927467661147; 0.0006183819299710211 -0.0002664932265487625 -0.0019776746683675757; 5.8125164000611285e-5 0.0014147292778764876 -0.001561111670186401; -0.00012928754371600046 0.0002918734607459714 5.5885149871641665e-5; 0.000284543764297461 -0.0011359149866518924 -0.0013977474530503884; 0.0004951169390097958 -0.0003759760138036172 -0.0003820916193990466; 0.0018513876583565177 0.00201643800302882 -0.0002718956342356863; -0.0007442531880618604 -0.0007661924223617269 0.0007792276363972396; 0.00012269135452268562 0.0002372284606531832 0.0005562980079682296; -0.00023389915358777323 -0.00021737906149740262 -0.0007771204183639985] %
+
+Mass Used: 88.43060274107165 kg
+Launch C3: 95.90491045503458 km²/s²
+||V∞_in||: 3.456705907234826e-9 km/s
diff --git a/archive/ES_0.5553496144128125 b/archive/ES_0.5553496144128125
new file mode 100644
index 0000000..77d1573
--- /dev/null
+++ b/archive/ES_0.5553496144128125
@@ -0,0 +1,22 @@
+archive/ES_0.5553496144128125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T09:43:55.880
+Launch V∞: [8.10317987564361, -5.696207769870157, 0.1553325957128171] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0071934236702311015, -0.004965730312843872, -0.0003038427526265429] km/s
+ V∞_out: [0.006087772048570902, 0.003123568422287049, -0.0054474103900420765] km/s
+ time of flight: 1.874957778749338e8 seconds
+ arrival date: 2030-04-24T11:53:32.880
+ thrust profile: [0.21852782341239765 -0.004394661947521582 -0.07648165853302688; 0.05449869864346815 0.02812137085624257 -0.06778772029616381; 0.04776021625029402 0.038940209444852 -0.1058035321485391; 0.04348954847800777 0.04581182105111091 -0.1413012320654695; 0.029637491747047877 0.03637476513769563 -0.12460063687764829; 0.018263366525342918 0.025934873925837477 -0.09882208381199613; 0.010393645054657355 0.016616604294121748 -0.06984618131900816; 0.0043639850761715785 0.007630836260250351 -0.035106101396778826; 0.004209775504114455 0.007980983235826225 -0.038849059552370294; 0.000718924087536708 0.0015240733431350023 -0.008551699639035671; 0.0007760856452014337 0.001683530519717075 -0.009501196753692152; 0.00011827705906626506 6.830871604105213e-5 -9.79778720163791e-5; -8.181060694363874e-5 0.00047577208223703674 0.0004365344581833665; 0.00024872050721913515 -8.8839932015217e-5 -0.0008270826346074116; 0.0003545586317562617 -0.00013431066679745396 -0.00023797145127221997; -0.0004402873533663245 -0.00047426965980170306 0.0007773248998385402; 0.000818115058563697 0.0006759914714488732 -0.00016756330756562723; -0.00014461160521534074 -0.000715703708641262 -0.00013038677619263433; 0.0005519329299552718 -0.0006737568257195225 -0.000598372441231225; 0.0006763866155410585 -7.404604347327747e-5 -7.334178511644998e-5] %
+
+Mass Used: 75.4686777407901 kg
+Launch C3: 98.13243526985563 km²/s²
+||V∞_in||: 0.008746207295603122 km/s
diff --git a/archive/ES_0.5553988801556101 b/archive/ES_0.5553988801556101
new file mode 100644
index 0000000..fc4a051
--- /dev/null
+++ b/archive/ES_0.5553988801556101
@@ -0,0 +1,22 @@
+archive/ES_0.5553988801556101---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T20:27:31.829
+Launch V∞: [8.099371067795309, -5.697342994428108, 0.23961816690038987] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.420794762497583e-5, 6.024451843937005e-5, 0.004113130410337279] km/s
+ V∞_out: [-0.003650496205091847, -0.0012380261530165364, 0.0013759417669957801] km/s
+ time of flight: 1.874957778743604e8 seconds
+ arrival date: 2030-04-23T22:37:08.829
+ thrust profile: [0.16756317248501923 -0.0019374981081347836 -0.05553507658755178; 0.12351319739523713 0.0664036700346333 -0.1347883651394778; 0.03980123203677707 0.03566992410321178 -0.0850533180454862; 0.034361614191466876 0.040110551269449644 -0.10705297980293457; 0.03179001997115301 0.046284771186835626 -0.1348862475845847; 0.023807484482126454 0.03937269394744734 -0.12716199488054153; 0.008510351716584706 0.01618435914970713 -0.05802343221350874; 0.004255308128100879 0.009668247630515946 -0.03506206856933895; 0.0012107204699053232 0.002937858550102232 -0.011983965172335811; 0.0017863449653847366 0.003622535975951511 -0.015110293216188748; 0.0002407023305336371 0.0008608860535842083 -0.00389658664661596; -2.1079710467773147e-5 0.0008793513857120929 -0.001967315590027195; -0.00028294766519093974 -0.00034677230489704204 -0.001748699402170058; 4.317707008927486e-5 0.00013589287252711998 -0.00013691337862167894; 0.0001980808409324128 0.0008587519378775326 -0.0025076539679062546; 7.812718254363428e-5 0.0001837438719466311 -0.0006467015644265338; 3.891451479560683e-5 5.552018762208875e-5 -0.0015245825687303762; -0.000110339294204162 0.0003131708817709915 -0.0006406566647075316; -0.0005329265181372854 -0.0006203983788751317 0.0002790052352122322; -6.293376876180599e-5 0.00012561731060751233 -0.0005034354105287017] %
+
+Mass Used: 75.61650993875173 kg
+Launch C3: 98.11694575590745 km²/s²
+||V∞_in||: 0.004114433393905717 km/s
diff --git a/archive/ES_0.5554018322688501 b/archive/ES_0.5554018322688501
new file mode 100644
index 0000000..1b53a5d
--- /dev/null
+++ b/archive/ES_0.5554018322688501
@@ -0,0 +1,22 @@
+archive/ES_0.5554018322688501---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T21:09:00.163
+Launch V∞: [8.033420980890492, -5.775163290254046, 0.29451139712426244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2438520727890286e-6, -1.0851062017930229e-6, 8.218168158950809e-7] km/s
+ V∞_out: [-2.1323339389682597e-7, -1.8295062666380425e-6, 8.40206204986971e-8] km/s
+ time of flight: 1.8749577787468156e8 seconds
+ arrival date: 2030-04-24T23:18:37.163
+ thrust profile: [0.2298938795132756 -0.002382363908888821 -0.07500215742641986; 0.05789187849475886 0.031280672979930334 -0.06995405575677786; 0.043907082176288324 0.03765212776011839 -0.09530427276167132; 0.0511006599696396 0.055510802804240936 -0.1554405077012778; 0.04029329912758011 0.05520684570387007 -0.16865780714135356; 0.013134088356955674 0.019584423155094222 -0.07046550534934869; 0.009439347751905882 0.01592941083088526 -0.06145197693708397; 0.004727927073174679 0.008293510721741467 -0.03720175207021022; 0.0021014155716788238 0.004328291914307116 -0.019935799743980753; 0.0012112852386704117 0.00292969921619415 -0.013082901486547826; 0.00023469430900969806 0.00042648361270350183 -0.002062777628420293; 0.00020187330956979768 0.0003684238860025964 -0.0006286919877773692; -0.00032872241235123545 0.00025130450434917044 -0.0005581186561390136; 8.960475279982197e-5 0.0009770010634579137 -0.001460084323412991; 0.00014360085872644344 -0.00040907257330352956 -0.0004549987596784359; -0.00033797952112663894 5.3210703241990886e-5 -5.717079881615997e-5; 0.00031278347133417337 9.296005909151565e-5 0.0009203157652921157; 0.00016286369672531434 0.00010157592025106992 -0.00042284841744769623; 9.893657168286076e-5 0.00037018789737870185 -0.0006018683982409329; 0.00025852793290105457 -0.00026993613811333384 -0.00035035178740521367] %
+
+Mass Used: 76.44738386497602 kg
+Launch C3: 97.97510064834557 km²/s²
+||V∞_in||: 1.84391060711716e-6 km/s
diff --git a/archive/ES_0.5554393651791023 b/archive/ES_0.5554393651791023
new file mode 100644
index 0000000..70963e0
--- /dev/null
+++ b/archive/ES_0.5554393651791023
@@ -0,0 +1,22 @@
+archive/ES_0.5554393651791023---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T02:36:40.662
+Launch V∞: [8.015320347594308, -5.650891123369662, 0.2072178508051127] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.841948938567232e-7, 3.0262022612951473e-6, -7.320127622421485e-5] km/s
+ V∞_out: [-2.8670139796813485e-6, 6.709990609312329e-5, -5.090481414750846e-7] km/s
+ time of flight: 1.874957778737431e8 seconds
+ arrival date: 2030-04-23T04:46:17.662
+ thrust profile: [0.3561233393051751 -0.006098174136111534 -0.10217464052682548; 0.075529100415085 0.042981935167420986 -0.085955833298707; 0.05625615221667444 0.05130512609124765 -0.11551167241473989; 0.028197870651471384 0.034050987079248286 -0.08872363919572951; 0.029633021923308987 0.044345294692114644 -0.12486581772974435; 0.01669701348555364 0.028429102130839184 -0.0882282269142744; 0.015070735029327714 0.029937519248560016 -0.09967715481440458; 0.004956474253619485 0.011120126539336708 -0.04064673764428253; 0.0029161054415206195 0.007261967087240697 -0.028496728159587727; 0.0007415412516860645 0.0024616981819384764 -0.00998170261897817; 0.0007314468835220106 0.0019219528185446752 -0.008196849127401115; 7.654371182347835e-5 5.175821500414929e-5 -0.0006458280190958221; 0.0004010858247077206 0.0003286324930280675 -0.0025331981139017036; -6.359708081627111e-5 0.00010070213111805287 -7.147574326211124e-5; 4.941999308085874e-5 -4.143989876220452e-5 9.688743444445332e-5; -6.842487568673179e-6 -0.0001350788482258876 -0.00026026602539886627; 3.6011482074926058e-6 3.396170081582984e-5 0.0003726245143131632; 1.3766361989915927e-5 9.16724968035497e-5 -0.0007902845208497627; -0.00014868028269059738 -0.0003371631928999702 -0.00011851450358111291; -7.681987945286134e-5 9.23427662999305e-5 7.590759767921873e-5] %
+
+Mass Used: 86.72418437311308 kg
+Launch C3: 96.22087000042966 km²/s²
+||V∞_in||: 7.3265402378444e-5 km/s
diff --git a/archive/ES_0.5554813218194097 b/archive/ES_0.5554813218194097
new file mode 100644
index 0000000..09a957c
--- /dev/null
+++ b/archive/ES_0.5554813218194097
@@ -0,0 +1,22 @@
+archive/ES_0.5554813218194097---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:31:28.392
+Launch V∞: [8.0891473400973, -5.692973902821432, 0.17080604884838232] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.624253055295607e-10, 2.6031116525534865e-9, -1.963240950595241e-9] km/s
+ V∞_out: [1.5057182218987104e-9, 3.0319245946678542e-9, 7.812492911139819e-11] km/s
+ time of flight: 1.8524360854352963e8 seconds
+ arrival date: 2030-03-28T00:04:56.392
+ thrust profile: [0.22235856867229353 -0.00847503054598866 -0.08028226199077587; 0.07529283563064769 0.03759533143754159 -0.09315704925425514; 0.048321534442807665 0.0383265421453116 -0.10749810607402345; 0.03802125053160061 0.038623386474410916 -0.1235390067423918; 0.035035407326052946 0.042471937457964466 -0.15068597133732428; 0.0221428992625299 0.030381962912583303 -0.11963989862423495; 0.012030072795253723 0.01812043871300703 -0.0786051663508672; 0.0035871556203987648 0.005845780417505831 -0.02754848675183922; 0.0017038630505681143 0.002812994055315353 -0.015134097962005714; 0.0004559181219149022 0.0007414201032812668 -0.004822885634474083; 0.00019366963896819508 0.0003134059853220376 -0.0007272799277156995; 0.000245281514840613 0.0005535934511823185 -0.002713600883880549; 0.0001552398158292699 0.0001613321569179683 -0.00028192567763878843; -6.622549407408435e-5 -5.6893192231886834e-5 0.0004896166245428691; 0.00023118820212565642 0.00015471716146732504 0.0006653987429265666; 0.00011596005606976002 -0.00011503710953939407 -0.0002432255567259898; 6.198729085098857e-6 -0.00014805820961753878 0.000805655991443695; 0.00036292064525340374 -0.00019917999642682892 -0.00015432941473323157; 0.00032732974457299555 0.0004531813500036276 -0.0005485052880291339; 0.000614074688792294 -0.0008165598404809293 0.000334425216688537] %
+
+Mass Used: 77.13319313903958 kg
+Launch C3: 97.8734312543323 km²/s²
+||V∞_in||: 3.270989505751453e-9 km/s
diff --git a/archive/ES_0.5555149418109946 b/archive/ES_0.5555149418109946
new file mode 100644
index 0000000..d0671b6
--- /dev/null
+++ b/archive/ES_0.5555149418109946
@@ -0,0 +1,22 @@
+archive/ES_0.5555149418109946---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:16:45.227
+Launch V∞: [7.886453692881989, -5.766146669242591, 0.17731826006147883] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.836910169257413e-10, -9.375329875181162e-10, -1.1582799285250461e-9] km/s
+ V∞_out: [9.504450631657843e-10, -9.110896323774704e-10, 3.2446331384196525e-10] km/s
+ time of flight: 1.8578408420707503e8 seconds
+ arrival date: 2030-04-03T22:58:09.227
+ thrust profile: [0.42007645142641625 -0.02131548891750738 -0.14069301019438915; 0.08953349621835163 0.04150785072471936 -0.11169464971176427; 0.06786122343006948 0.04954984121876103 -0.15101372550178468; 0.03674577054207439 0.033749736956093415 -0.12061690355354283; 0.022125015413372588 0.023934154012362156 -0.09634798551306989; 0.024730692216342626 0.029776021239070798 -0.1317667777392725; 0.0074123780950023236 0.009856747845124348 -0.048619156418719646; 0.002694714312697033 0.003884994057635316 -0.02125927372055324; 0.0017148813402562892 0.002663889746125444 -0.01530517929419418; 0.0005610342798146018 0.0008897162395053332 -0.005413768922161111; -6.208974296115196e-5 1.0228331061479925e-5 -0.0003640360929690432; 0.00010073726097622381 -3.56832836566312e-5 1.644789268456803e-5; -9.148431767651544e-6 9.923576995625314e-5 -0.0004964428076852081; -2.7239255440105487e-6 1.555041927077985e-5 -4.85747570741195e-5; 2.030947003099046e-6 2.4184634377666606e-5 -8.020747864168754e-5; 7.26642570323925e-5 0.00018837509337221064 -0.00039135500520177214; -0.00015038100314065543 0.00043575027422096396 -0.0005037035493860557; 0.0004557424872628663 -0.0003999451460967983 -6.622367583560193e-5; 1.2464616354565701e-5 0.0005183325062460401 2.1627829344008482e-5; 0.0003892447055876588 0.00022211057796742216 -0.0006804821734761649] %
+
+Mass Used: 91.1571927913401 kg
+Launch C3: 95.47604102654061 km²/s²
+||V∞_in||: 1.5666963634869674e-9 km/s
diff --git a/archive/ES_0.5555886306746982 b/archive/ES_0.5555886306746982
new file mode 100644
index 0000000..dea08fe
--- /dev/null
+++ b/archive/ES_0.5555886306746982
@@ -0,0 +1,22 @@
+archive/ES_0.5555886306746982---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T21:45:44.751
+Launch V∞: [8.097157966208412, -5.7235444752915985, 0.1306763857131603] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.354583227548992e-6, -2.033861909972328e-6, -1.9902747505106622e-7] km/s
+ V∞_out: [1.711149734140751e-7, -8.486974320046878e-7, -2.2954795020027925e-6] km/s
+ time of flight: 1.874957778749071e8 seconds
+ arrival date: 2030-04-23T23:55:21.751
+ thrust profile: [0.13697728884613816 -0.0012462171285798694 -0.04231430720767637; 0.09061310387649295 0.04941404808359705 -0.09301349514541098; 0.07206425953696069 0.06270967380872773 -0.1316019524779482; 0.05142325879063578 0.05789117521336941 -0.13907928980775816; 0.034724693966127596 0.04696247910122261 -0.1271640404615248; 0.021664043227228043 0.03406718740673748 -0.10162959083047443; 0.011526309808033661 0.02088953844172639 -0.06650568585777802; 0.0036540813082757075 0.007795868388542844 -0.026782258005114218; 0.002748998147299548 0.006167505533935089 -0.022833530110010134; 0.00045966652234908853 0.0020603589920435974 -0.004837216705160525; 8.331411168620227e-5 0.0012795607654485688 -0.0009501956463345632; 0.0009148806188941994 -0.0004167900274393787 -0.002174374051332414; -0.0013790567604535032 -0.0002999678699475404 -0.002259765855076702; 0.0002308293331623607 0.0003590641436721085 -0.0014202991854615767; -0.0006471076503101953 0.001336938439675547 -6.724792531199639e-5; 0.0017802574380088548 -0.00032790554594502115 -0.0007366313548920879; -0.0003033508980936425 -0.0026991605543110735 -0.0018136105163869749; -0.00024710811844636996 3.984844856063307e-5 0.0012667890406400152; -2.865006595770774e-5 -1.810085979889913e-5 -0.00011678869749445135; -0.00013489262485826345 0.0005807050881182493 -0.0005724390058631687] %
+
+Mass Used: 74.53670773956901 kg
+Launch C3: 98.34000480815638 km²/s²
+||V∞_in||: 2.4517548664208936e-6 km/s
diff --git a/archive/ES_0.5555895920983202 b/archive/ES_0.5555895920983202
new file mode 100644
index 0000000..3914579
--- /dev/null
+++ b/archive/ES_0.5555895920983202
@@ -0,0 +1,22 @@
+archive/ES_0.5555895920983202---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:32:29.766
+Launch V∞: [7.954026518859595, -5.651936525144275, 0.34283036341455375] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4772590225260715e-5, -1.2392091138211298e-5, 9.497081706989166e-6] km/s
+ V∞_out: [-2.7897781490311477e-6, -2.129279966966492e-5, 9.546532130825573e-7] km/s
+ time of flight: 1.8749577787603047e8 seconds
+ arrival date: 2030-04-22T17:42:06.766
+ thrust profile: [0.4221003625778134 0.0024543240573022336 -0.12460143742651807; 0.08841015987257779 0.05250420784808357 -0.0967517469099731; 0.05316870742999599 0.05056322435215213 -0.1062279546235885; 0.03886614863645844 0.04944665659247456 -0.11689275674361002; 0.02500576523814115 0.04066644559618659 -0.1069162014326775; 0.0195872956233084 0.03673437221585266 -0.10476406166276402; 0.010394089317653295 0.021034861908135444 -0.06272875518522406; 0.008328051608330151 0.01222352328662478 -0.043392320306426084; 0.002576596033412328 0.006661521160027185 -0.025507476262502757; 0.0009641193100614219 0.0026478188882584535 -0.01113969788388293; 0.00015409864763691586 0.0005497379206734901 -0.002113724698805902; 0.00016568269854158854 0.0006468183611313067 -0.0028208235559074465; 0.00019734230581279572 0.00011256427006853706 -0.00044691796679938736; -1.611920081808971e-5 0.0001536912782015656 -0.0006493926058376988; 1.2652188508059165e-5 0.00016496459316419325 -0.0006311914772119577; 0.00013136446789655573 -6.599013967282938e-5 -0.0010739640436663615; -4.070635175490843e-5 2.8819239964566348e-5 0.0002686223663615027; 0.0001988522613017184 5.7429486625579095e-5 -0.0008735736425061699; 0.00021337346157853458 -0.0001873608069724977 -0.00030585885166558896; 0.00018152047352259707 -0.0002772759720853931 -2.5427888388273304e-5] %
+
+Mass Used: 92.10519158518673 kg
+Launch C3: 95.32845700506059 km²/s²
+||V∞_in||: 2.1493903919261194e-5 km/s
diff --git a/archive/ES_0.5555981137552012 b/archive/ES_0.5555981137552012
new file mode 100644
index 0000000..717bce6
--- /dev/null
+++ b/archive/ES_0.5555981137552012
@@ -0,0 +1,22 @@
+archive/ES_0.5555981137552012---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T15:07:07.613
+Launch V∞: [8.082773809515784, -5.709511979563037, -0.08221754559998876] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.271618879525547e-10, -9.467188797709204e-10, 2.7925623958736294e-9] km/s
+ V∞_out: [2.0710433474319867e-10, -6.893777317405418e-10, 1.1086040371862895e-10] km/s
+ time of flight: 1.8749577786971304e8 seconds
+ arrival date: 2030-04-23T17:16:44.613
+ thrust profile: [0.19262882219372876 0.0017682977351410924 -0.06078570749456977; 0.07510854426601425 0.04483363097579235 -0.08152090897510195; 0.05247612556652213 0.05173429616485974 -0.10334129305288119; 0.03699212147964636 0.04836776779914272 -0.11420009851892877; 0.015257947545094692 0.023616672516294634 -0.06151535097167395; 0.05017375150264386 0.08830370298816641 -0.2186226342882601; 0.008321797426523236 0.020875746774835446 -0.0620611019471654; 0.0016554003603538512 0.004422884420023118 -0.014999979304444628; 0.0029079581542708643 0.008455953550443632 -0.03441057189742003; 0.0014578145592288889 0.005998444591665279 -0.021590817094686094; 0.00010189419917084582 0.00036538089525199125 -0.0013457387446312698; 3.4267406230693495e-5 0.00012128214999226729 -0.0004984499190272592; -3.630324776009653e-5 0.00013568298390632396 -0.0001933222589807255; -0.00011464061902182116 1.729493075479877e-5 -0.00022822609938822459; 3.130844266011417e-5 -6.033277523730223e-6 -0.00028834664280309296; -2.4080693230419574e-6 2.2064196459154254e-5 -0.00010496253498183353; 5.629619319618323e-5 -0.00017764941434590838 -8.429129071450761e-5; 4.5321256872056e-5 7.763583113794498e-5 3.631885057500916e-5; 0.0001761123035687706 0.00017277995294965204 6.818358448922729e-5; -0.0003107464502650623 6.280586170101499e-5 -5.122958464710797e-5] %
+
+Mass Used: 76.90143723306119 kg
+Launch C3: 97.9365192253726 km²/s²
+||V∞_in||: 2.979454421648595e-9 km/s
diff --git a/archive/ES_0.5557824943431257 b/archive/ES_0.5557824943431257
new file mode 100644
index 0000000..a5b7cd1
--- /dev/null
+++ b/archive/ES_0.5557824943431257
@@ -0,0 +1,22 @@
+archive/ES_0.5557824943431257---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:54:42.769
+Launch V∞: [7.947030030148891, -5.725766684710527, 0.24202104722470721] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.759344025344734e-6, -2.4204246885162136e-6, 1.776701782704104e-6] km/s
+ V∞_out: [-3.9976382777979477e-7, -4.0526356815121425e-6, 1.6070450518301959e-7] km/s
+ time of flight: 1.8749577787488315e8 seconds
+ arrival date: 2030-04-23T22:04:19.769
+ thrust profile: [0.3960965326719643 0.004259382470233035 -0.12416769816722709; 0.04264462785093866 0.024163839407926626 -0.05007198382581099; 0.04641569782912802 0.042447237818555895 -0.0976623070227238; 0.06000137009233807 0.07281320449422427 -0.1833637869953763; 0.027339463431665722 0.03988389687606256 -0.11532986210137897; 0.016392180324669884 0.02764688048304604 -0.088278672916249; 0.007684696982986988 0.014735717216941745 -0.051844821781153766; 0.005695678176768902 0.011978794011892344 -0.0450846309818904; 0.0015313692750855378 0.004017116318282095 -0.016246969671378612; 0.0013959084340388242 0.003510673757082177 -0.015182286932493894; 0.00018520527178236566 0.000528320331060851 -0.003527162039857431; 0.0005931763915346057 0.0019233939908585712 -0.008836752661479331; -0.00020609688838255314 -0.00029171179683564006 -0.00016409366406674344; -0.00035832118245100606 0.0009050915210500756 5.1892988268757245e-5; 0.0013802105825223643 -0.0002956780681465251 -0.00018081590039303056; 1.2820170612769873e-5 0.00021476799737743432 -0.0005181737657272314; -7.816440173557716e-5 0.00022768666887319221 0.001407493734060039; 0.002351769163508304 0.00013991003499428924 -0.0009362672492040228; -0.0002162265530962279 0.0020183627256214593 -0.0021072091822542283; 0.00052609584762935 9.227976670804017e-6 0.0008696703291690283] %
+
+Mass Used: 88.42303314539413 kg
+Launch C3: 95.998264615129 km²/s²
+||V∞_in||: 4.077879883916204e-6 km/s
diff --git a/archive/ES_0.5557834365111958 b/archive/ES_0.5557834365111958
new file mode 100644
index 0000000..44f5391
--- /dev/null
+++ b/archive/ES_0.5557834365111958
@@ -0,0 +1,22 @@
+archive/ES_0.5557834365111958---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T10:36:44.855
+Launch V∞: [7.998211811049221, -5.6889764199794595, 0.16579943332476535] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.607330122588107e-6, 7.585618519006446e-6, -5.516980767695332e-6] km/s
+ V∞_out: [1.7044773987531268e-6, 1.2573006635761295e-5, -5.978193920049432e-7] km/s
+ time of flight: 1.8749577787394667e8 seconds
+ arrival date: 2030-04-23T12:46:21.855
+ thrust profile: [0.33574349798395897 0.00022780531375672173 -0.10962357523730464; 0.08229530639165769 0.04774551014678654 -0.09587120157684394; 0.056042617861322704 0.05242218020328153 -0.11832645419653522; 0.040295755662508925 0.04970869349161298 -0.12699339828045553; 0.02595014094582373 0.03928316854813051 -0.11236569345355266; 0.013559779913649305 0.023658284920628166 -0.0767136924923864; 0.008592255150081909 0.016720570100730938 -0.059820306918130596; 0.004322661529306686 0.009315012365338918 -0.03486570051548452; 0.003482728722009579 0.008317889096073222 -0.03367490985583191; 0.0015227573128690293 0.005144050668324006 -0.022075030429857635; 0.00010926529240131475 0.0005843875807441641 -0.004574145172846127; 0.00027819379105144227 0.003182601609830852 -0.014891439446973666; -9.85304886924253e-5 -1.3426602311527778e-5 -0.0003835232730023135; 5.602341118698953e-5 0.0001880036072309773 -0.0006281716766106916; 0.00018122159141822488 0.00030927740320518685 0.0001018819378548282; 9.629454558657402e-5 0.00016123996751249526 -0.00017437142981505945; -0.00012885310087460235 0.00012253124744784178 -0.0001268114277722781; 0.0006014936861673025 0.0006988495319844413 -0.000446181986860041; -0.0003317729364954457 0.0008610760201880722 0.00045461438515241104; 0.0002603128653303449 0.0006148525916535956 -0.0001437275203020101] %
+
+Mass Used: 86.29455898384276 kg
+Launch C3: 96.3633343335804 km²/s²
+||V∞_in||: 1.2730468056840107e-5 km/s
diff --git a/archive/ES_0.5558224886874478 b/archive/ES_0.5558224886874478
new file mode 100644
index 0000000..97f3d80
--- /dev/null
+++ b/archive/ES_0.5558224886874478
@@ -0,0 +1,22 @@
+archive/ES_0.5558224886874478---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:54:28.525
+Launch V∞: [8.145087344616607, -5.6662314525547375, 0.16493094089055843] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.9367104147365403e-5, 4.8730360644439784e-5, 0.003145934483615344] km/s
+ V∞_out: [-0.002776269848909524, -0.0009653862811910221, 0.0011239259333138203] km/s
+ time of flight: 1.8749577787493294e8 seconds
+ arrival date: 2030-04-24T02:04:05.525
+ thrust profile: [0.1821993945438948 -0.0013631485982507586 -0.062188082882081594; 0.06155488770018268 0.03373818926367287 -0.07381192082647672; 0.055309765667404066 0.04719652683531835 -0.11759484451663701; 0.026038131174086047 0.029379113849091566 -0.08364320573355498; 0.022595436497182136 0.029956681404161033 -0.09658388251120247; 0.02470275525312149 0.0430988355309665 -0.14207007999096813; 0.010827262712412224 0.018390342920860427 -0.07097463884429948; 0.00875532657762532 0.01796682364984792 -0.0717923864930178; 0.0024836625650917917 0.004959870337903752 -0.022261877516037677; 0.0021411689330728535 0.004837123252528673 -0.022278748740835415; 0.0001663714690442312 0.00026262274430156245 -0.0015855030381359092; 4.403396740945333e-5 0.0002216138020192659 -0.001114785770396187; 0.00014639728872106348 0.00038526343831065714 -0.0024171809464598295; 0.0004986791055819131 -6.42503190641782e-5 -0.0005868243646974211; -5.389137094538407e-5 0.0010913791581246219 -0.0018423804824721113; 0.00013191521534491798 0.0004661208244784152 -0.0015385708622525952; -0.00047700244518037284 0.00025406105242428267 -0.0008935614130410638; 9.71062850629971e-5 -0.0005652859915543438 -0.0001187656591950957; -0.0016289619577609972 0.0004241308900837115 -0.00292004875705; -0.0012074844002367266 0.0005798686307722407 0.002719243510055672] %
+
+Mass Used: 74.01723464842189 kg
+Launch C3: 98.47582894061723 km²/s²
+||V∞_in||: 0.0031468719192721396 km/s
diff --git a/archive/ES_0.5558472505548713 b/archive/ES_0.5558472505548713
new file mode 100644
index 0000000..b3d154f
--- /dev/null
+++ b/archive/ES_0.5558472505548713
@@ -0,0 +1,22 @@
+archive/ES_0.5558472505548713---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:16:40.858
+Launch V∞: [8.020180222127914, -5.691590916263975, 0.20675721586302248] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.382218630453822e-5, -3.120871769234988e-5, 3.069687137628679e-5] km/s
+ V∞_out: [-7.839920172447044e-6, -5.6989678678280376e-5, 2.735496097299929e-6] km/s
+ time of flight: 1.8749577785753152e8 seconds
+ arrival date: 2030-04-23T20:26:17.858
+ thrust profile: [0.34397332976981154 0.0019211086043523901 -0.1103007434085456; 0.03571069754629575 0.020356200595922438 -0.04085081866609469; 0.03200885481060013 0.029341661430218265 -0.06612625343035164; 0.03950983503425282 0.04789285610425227 -0.12053667359073973; 0.04016880692530358 0.05952065499594405 -0.1639035370673269; 0.021250394462809602 0.0368045310211113 -0.1122121732957696; 0.016518228898727245 0.03280018690991797 -0.10764831048231813; 0.004215834930408646 0.009162092268123402 -0.03277710819320587; 0.0008073122802082747 0.0023318159176960044 -0.007903723016192054; 0.001409980353398891 0.002700844883547664 -0.00874442461005192; 9.533975278373994e-5 -0.0011954719260895883 -0.0020415622386658547; -0.0008676221505528904 -0.0006095180246605739 -0.0015822111759879734; -0.00015129546579974043 -0.0005662361412312537 -0.0016584937869259728; 0.0015362115192581556 -0.00020190711922243073 -0.0006597526367618477; 0.0012586546184986695 0.00134936604139315 -0.002215507211306132; -5.4933173473768835e-5 0.0006124746382959935 -0.002220402869587243; 0.000248654535235742 -0.0004993183743947807 -0.004208702729329133; -0.002003849507640907 -0.0020632617955001096 -0.0039084560839903705; -0.001956170593537257 -0.0005413529933416728 -0.0030028792644693483; -0.0017721652231622361 -0.0001376039351070372 -0.00040273531230205605] %
+
+Mass Used: 84.05368773172268 kg
+Launch C3: 96.76024649982179 km²/s²
+||V∞_in||: 5.531927565245211e-5 km/s
diff --git a/archive/ES_0.5558533611237318 b/archive/ES_0.5558533611237318
new file mode 100644
index 0000000..d486f3c
--- /dev/null
+++ b/archive/ES_0.5558533611237318
@@ -0,0 +1,22 @@
+archive/ES_0.5558533611237318---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:03:16.528
+Launch V∞: [8.06850332079006, -5.665661254292966, 0.16779196569355997] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1412983953857728e-5, 0.00026462375915336475, 4.662268940587834e-6] km/s
+ V∞_out: [0.00025609049237426706, -3.840562420470978e-5, 5.5895068284245824e-5] km/s
+ time of flight: 1.8749577787493658e8 seconds
+ arrival date: 2030-04-23T19:12:53.528
+ thrust profile: [0.2879444151060303 -0.0032769099727066897 -0.09518863084849954; 0.056111400619534034 0.030923793956691526 -0.06594970344083223; 0.04269376209902795 0.036674028395639435 -0.08984553707155178; 0.050502627129324816 0.05696895048537511 -0.15680529977596813; 0.027928103604976745 0.03767267671133755 -0.11509610760991872; 0.017376446035021677 0.02631384642025439 -0.08953117211467436; 0.01248684645883106 0.023326248304538836 -0.08370693572956045; 0.003280702289041826 0.006223618897104122 -0.0295749332692172; 0.0019037768824084992 0.0040702658780207256 -0.018410000949822602; 0.000922524644747056 0.0020770697469395865 -0.010977767708480605; 0.0010429375350594734 0.002914841776064981 -0.015177405498180483; 0.0003537499932884955 0.0009101101778355857 -0.0041892756669427746; 0.000967335997969096 0.002460335295015552 -0.013385888495663535; 0.00028186841488487754 0.0008509651947054618 -0.0046533703124217556; 0.0007182624812921339 0.0008198796909274933 -0.0014994399709984977; 0.00028118878779284976 5.9385975795101474e-5 -0.0007068045823105662; 0.0007259756114810482 0.0007491114555815853 -0.0007497066843321215; -0.0001598865576742702 -0.000516621021246607 -0.0007915945292954795; 0.0007526444827450972 0.00026007121398408475 -0.0004884519648876557; 0.00199177897272931 -1.9999228634536795e-5 -0.0010394116855884233] %
+
+Mass Used: 81.32865297082344 kg
+Launch C3: 97.22861742974807 km²/s²
+||V∞_in||: 0.0002649107903858644 km/s
diff --git a/archive/ES_0.5558662372895594 b/archive/ES_0.5558662372895594
new file mode 100644
index 0000000..9ad22df
--- /dev/null
+++ b/archive/ES_0.5558662372895594
@@ -0,0 +1,22 @@
+archive/ES_0.5558662372895594---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T05:44:11.020
+Launch V∞: [8.139803167680254, -5.647315242872821, 0.15738329700479445] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.016631203558507637, 0.10220769452895039, 0.1066376381916789] km/s
+ V∞_out: [-0.02558744762007931, 0.02319501815077483, -0.14455664775647756] km/s
+ time of flight: 1.8749577787516823e8 seconds
+ arrival date: 2030-04-24T07:53:48.020
+ thrust profile: [0.2412491490531724 -0.0075435708360372545 -0.08696910011384751; 0.025358972834204803 0.012681760164543929 -0.033362581146555055; 0.0491675035584243 0.037898367149471826 -0.11011123911971735; 0.034761469088207 0.03393001069771068 -0.11395322206213486; 0.02877504164106272 0.032905220949458365 -0.12448552493786565; 0.02597432034420042 0.033565966041392385 -0.1399317638039783; 0.015316436989942435 0.02157759060619915 -0.09926973307474879; 0.005115558445724777 0.007963819520976382 -0.041488742403563886; 0.0011703918745264534 0.0019490370220689147 -0.010656599371909783; 0.001065638256009031 0.0009347430282915833 -0.008334405585172372; 0.0004373664945973918 0.0007342543411028775 -0.0035260864822668474; 0.00044598933615717007 0.001055043566326496 -0.001739393971164116; 0.00010611527132477588 0.0003757715991527618 0.000535072055176574; -9.790043793468507e-5 1.7093336149475233e-5 0.0004061769557542628; 0.00143390439412798 0.0005842142186828458 0.0016107682429857407; -0.000501502132164686 -0.0006540398062925176 0.0016923685271037713; -0.0026708940402657643 -0.0007461704232461983 0.0017946241364393137; -0.0008577638507745552 -0.001801082441750256 0.001369975426384974; 0.0007874515174102044 -0.001659216035796467 0.001191550306468037; 0.00271791041746247 -0.002136020899016181 -0.00036446217710833415] %
+
+Mass Used: 75.83282521951833 kg
+Launch C3: 98.17333456313732 km²/s²
+||V∞_in||: 0.14864250950460695 km/s
diff --git a/archive/ES_0.5558687243860738 b/archive/ES_0.5558687243860738
new file mode 100644
index 0000000..d9b86bb
--- /dev/null
+++ b/archive/ES_0.5558687243860738
@@ -0,0 +1,22 @@
+archive/ES_0.5558687243860738---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T04:44:44.406
+Launch V∞: [7.926674977701113, -5.704295701074707, 0.18612421009155877] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.267040665413368e-10, 1.479066662287573e-9, -1.6399911979666534e-9] km/s
+ V∞_out: [1.0817865429485196e-9, 2.1201569902862085e-9, 5.45134206289995e-11] km/s
+ time of flight: 1.8696668599230942e8 seconds
+ arrival date: 2030-04-17T03:56:09.406
+ thrust profile: [0.41070806098542656 -0.008787243861247296 -0.12842175329010364; 0.1050983721593386 0.05482007971439309 -0.1151227079934063; 0.047489037678421796 0.04004617616998803 -0.09435952858893684; 0.024118304218830853 0.027298630096615345 -0.07331617603572899; 0.03332830151352836 0.04318034811654563 -0.12845753288179196; 0.0224471018473126 0.03536855993795905 -0.11206153554862952; 0.013863252896323904 0.028595534434234866 -0.09142079495876052; 0.0063894129470417746 0.012958688182379718 -0.04836183136475473; 0.0015196675707367946 0.002115234339886667 -0.00889135073026112; 0.000882564864626453 0.0022296862624698443 -0.009532497920043634; 0.00020505950604224126 0.000791393167795662 -0.0038024885840200005; -2.9277205689760225e-5 -7.923410806971189e-5 -0.0022771331454883104; -0.0006133391353344056 0.0005498496943153982 -0.00252758957448163; 0.00015738844184753708 0.0011873677091615027 -0.00361278984725187; 7.574085962876566e-6 0.0005895940058300447 -0.00204990573982413; -0.0005471488810656964 0.0003339056838708725 0.0006812693995493719; 0.0004495756325669218 0.0008664988009671715 -0.00024822004333460213; 0.0008356148738293636 -0.0012464050318468027 -0.001502825834394564; 4.594851882598074e-5 4.346039730665198e-5 -0.00017049846874473491; -7.192850005651835e-5 -0.0003729149276862026 -0.00020869961771174307] %
+
+Mass Used: 91.9796325479515 kg
+Launch C3: 95.40580786899451 km²/s²
+||V∞_in||: 2.2492855935388716e-9 km/s
diff --git a/archive/ES_0.5558779781677604 b/archive/ES_0.5558779781677604
new file mode 100644
index 0000000..cdd9bc7
--- /dev/null
+++ b/archive/ES_0.5558779781677604
@@ -0,0 +1,22 @@
+archive/ES_0.5558779781677604---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T08:10:09.677
+Launch V∞: [7.894381291534464, -5.785139007377959, -0.08494684631296423] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9034379560346155e-9, 2.302025376630676e-9, 9.233393374906011e-10] km/s
+ V∞_out: [2.508998396217692e-9, -2.308370756981814e-9, -1.8870685581830936e-9] km/s
+ time of flight: 1.8749577787470794e8 seconds
+ arrival date: 2030-04-24T10:19:46.677
+ thrust profile: [0.3795819420374527 -0.003768633453468938 -0.1239326663584129; 0.09794470904025773 0.05578611794694805 -0.11743536837114588; 0.06504884963741392 0.05744204155321652 -0.1393410922487926; 0.027549147915339748 0.03144574045624916 -0.09023581588392661; 0.02843485432910916 0.03967245820343552 -0.12453309035323756; 0.01434010947560126 0.02322679269369038 -0.08178498720083793; 0.01057921776971638 0.019018700672330743 -0.07394958555043603; 0.004791032285740364 0.00972817550556817 -0.041161520238384854; 0.001423368274942205 0.004597516902262278 -0.018419472303710577; 0.0010348087333635588 0.0026947177146075772 -0.011409050605615628; 5.150679715794969e-5 0.00016032361211856425 -0.0006044108486849174; 0.00020403454557339372 0.0005272748954227537 -0.0026084863602975046; 3.084653317123268e-5 -5.281500999293916e-5 -0.00019017181288307898; -0.00011666855441256528 -7.987156532713148e-5 -0.0003686507106282742; 0.00023745646356933872 0.00018793775512487935 -0.00023735984487069752; 1.2671917395674077e-5 -7.244969914968518e-6 -0.00018704249470194272; -9.849995183951334e-5 -3.900843859143215e-5 1.7210650528979242e-5; 9.357834425714433e-5 0.00023348563805860174 8.355049469364135e-5; -0.00023633066851157567 9.058746275186138e-5 0.00020906591152564878; 0.00014150045409054975 0.00026982721645029464 -0.00012436396049234023] %
+
+Mass Used: 89.71252707688927 kg
+Launch C3: 95.79630527751392 km²/s²
+||V∞_in||: 3.1264920309001944e-9 km/s
diff --git a/archive/ES_0.5559128041821125 b/archive/ES_0.5559128041821125
new file mode 100644
index 0000000..1ee4c55
--- /dev/null
+++ b/archive/ES_0.5559128041821125
@@ -0,0 +1,22 @@
+archive/ES_0.5559128041821125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T08:14:42.991
+Launch V∞: [7.866779426893698, -5.752572268964739, 0.1606977487911105] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5378864130849763e-7, 9.510877930514063e-7, -2.2789178909471312e-5] km/s
+ V∞_out: [-9.56708492923167e-7, 2.2781984183249892e-5, -2.7450486135648703e-7] km/s
+ time of flight: 1.8749577787769815e8 seconds
+ arrival date: 2030-04-24T10:24:19.991
+ thrust profile: [0.49396114761661103 -0.0078125974697869 -0.16236485369121081; 0.05758971629702417 0.02946467299117961 -0.07080284190262136; 0.039999863532085074 0.03237501568425605 -0.08844071540389459; 0.03883900656247109 0.040086274856215603 -0.1252504154874446; 0.03480336417898244 0.04306180378055577 -0.14962433154364452; 0.016438242231518248 0.023045497470434155 -0.08963878147683864; 0.013567856729339283 0.021258593539582437 -0.08984742550691868; 0.003427296949281673 0.005669910290559113 -0.026280883826344588; 0.0011385696824643288 0.002106972691260799 -0.010234048341935321; 0.0007988372538301461 -0.0003610677249334009 -0.002008719135664823; 0.0008669085246602328 0.0009496156917026651 -0.0034578577157030783; -0.00011560835650556488 0.00021091875123499992 -0.0008096808214678602; 0.0010719971133464862 0.0010273816009384125 -0.0020109467302602477; 0.0013017474524907244 0.0015761826496794532 -0.0024755448736099514; 0.000529278404990742 -0.00013970788348503815 -0.003159726912437057; 0.000464366846193499 0.0009515824620475557 -0.0025551226987178947; 0.0007408115557011497 -0.0003502607794663498 0.0012445939403221298; -0.0010785848917700405 0.0010126033272391233 -0.0003719420652615623; 2.3394232892742024e-5 0.0003407428464003145 -0.0010848168493393505; -0.00011114850434629472 0.0008863352816601983 -0.0013988737116514469] %
+
+Mass Used: 94.37417971855939 kg
+Launch C3: 95.0041300275266 km²/s²
+||V∞_in||: 2.2809535161948808e-5 km/s
diff --git a/archive/ES_0.5559161153091994 b/archive/ES_0.5559161153091994
new file mode 100644
index 0000000..b854237
--- /dev/null
+++ b/archive/ES_0.5559161153091994
@@ -0,0 +1,22 @@
+archive/ES_0.5559161153091994---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:59:25.220
+Launch V∞: [7.902723530690704, -5.792477101021152, 0.1737027323535227] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.034636198766216e-6, 0.0001907281087354548, 3.167142492142628e-6] km/s
+ V∞_out: [0.00018481747137806098, -2.7201160346527105e-5, 3.908934538923173e-5] km/s
+ time of flight: 1.8749577787493783e8 seconds
+ arrival date: 2030-04-24T01:09:02.220
+ thrust profile: [0.3620603035699699 0.012159716002029659 -0.10953393936396177; 0.07170183015250459 0.044084045654540896 -0.07812291295302695; 0.04923935872859461 0.049179750328895176 -0.09719646613221114; 0.048535758756893754 0.06485744175314566 -0.14225317021866515; 0.033218282523832465 0.055075959769179 -0.13361715337862104; 0.014293842185512976 0.028195630940955806 -0.07652366322881445; 0.009381512368472284 0.021467421967629862 -0.06295310538846842; 0.006958176455256972 0.01840877546629484 -0.05757115538475504; 0.0007250001900832797 0.0020864928070601853 -0.007224342686006196; 0.002277093475859385 0.006662324032877546 -0.021197251161165477; 0.0006013625066908898 0.0023591314556498486 -0.008634526017830496; 0.0004563211966331974 0.00046385842723694275 -0.0016054051345550159; 4.327730777362032e-5 0.00037731618149751975 -0.0014634664029315931; 8.267248029622195e-5 9.417518517602528e-5 -0.0015402683930081295; 2.2894819858776736e-5 0.0004011241181129774 -0.0011518083629152116; -3.772530601714994e-5 -3.006590994584059e-5 -0.00046134586183175824; -0.00052409624316835 0.00015814867361838453 -0.0002361334461810562; 3.451441574399709e-5 3.5704795107332522e-6 -0.0003387605449442791; -0.0010367677148064383 0.0006457575305781564 -0.0003675513769867823; 0.0002867443419824131 -1.2678068253483936e-6 0.00010788365830646774] %
+
+Mass Used: 88.35878481631744 kg
+Launch C3: 96.03600280761403 km²/s²
+||V∞_in||: 0.0001909235387065082 km/s
diff --git a/archive/ES_0.5559693300195112 b/archive/ES_0.5559693300195112
new file mode 100644
index 0000000..79f1081
--- /dev/null
+++ b/archive/ES_0.5559693300195112
@@ -0,0 +1,22 @@
+archive/ES_0.5559693300195112---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:54:50.914
+Launch V∞: [7.893881542191968, -5.743320917542883, 0.09410066992205839] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.013829842857239922, 0.08168756947303946, 0.08820781891562242] km/s
+ V∞_out: [-0.02024455280426549, 0.016985601979819583, -0.11809683592844607] km/s
+ time of flight: 1.8749577787481755e8 seconds
+ arrival date: 2030-04-24T02:04:27.914
+ thrust profile: [0.4698812886512025 0.00405169311527297 -0.1341825961133661; 0.03974264128039248 0.022907543953622298 -0.04831735116269752; 0.038400310211136324 0.03581951439682803 -0.08358392928334225; 0.042486995450291574 0.05309119044314119 -0.13944240667536403; 0.0194666635200238 0.029291109529296828 -0.08644074057221786; 0.022305226642502483 0.03893847326800887 -0.11938622389380085; 0.009872303978145501 0.019878876170097485 -0.06918525480489314; 0.007245122172076016 0.015755221220914356 -0.05853855688214914; 0.004663008204886656 0.01205068483745449 -0.047700619314320104; 0.0016301363501435224 0.0044449912778004265 -0.019218082193361758; -5.75837314365134e-5 0.0001742326096727427 -0.0009881465442945336; 0.0001961581380384227 0.00013202424354580094 -0.0010822060824034955; 3.606976344926237e-5 0.00014787281395743217 -0.0009757612826137514; 0.00014210403974397037 6.853552489620142e-5 -4.954186134583017e-5; 0.00019824228142912035 -0.00018488805427729514 0.00017871478620425053; 9.103183446312459e-5 5.430793403065097e-6 -0.0005474906021920855; 0.0005241259162657827 -0.0006130877428198804 0.0007668452528134871; -0.0004158557459833994 6.971107237432257e-6 -0.00026789388219205406; -6.658654484561944e-5 9.180813007019012e-5 0.0009257463267008579; -2.2397049279271184e-5 -2.353979297216595e-5 0.0015844168659277218] %
+
+Mass Used: 92.66780893870373 kg
+Launch C3: 95.30795590012445 km²/s²
+||V∞_in||: 0.12101546544851131 km/s
diff --git a/archive/ES_0.5560023625989194 b/archive/ES_0.5560023625989194
new file mode 100644
index 0000000..a636620
--- /dev/null
+++ b/archive/ES_0.5560023625989194
@@ -0,0 +1,22 @@
+archive/ES_0.5560023625989194---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T06:34:46.393
+Launch V∞: [8.019768550322814, -5.762585550766168, 0.15592824132622102] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5397457769996804e-7, 1.79859652476901e-6, -3.795133629857484e-5] km/s
+ V∞_out: [-1.6182366639426836e-6, 3.79366641569337e-5, -4.587397153004402e-7] km/s
+ time of flight: 1.8575911038327533e8 seconds
+ arrival date: 2030-04-04T06:19:56.393
+ thrust profile: [0.2932666836496181 -0.01127882232179828 -0.10388398643169922; 0.04120691869588206 0.01967251708117255 -0.05154606938094552; 0.033674926163999086 0.025014252895920883 -0.0767826687184777; 0.037689131354553894 0.03614401336451646 -0.12315711774590254; 0.031051299498785052 0.034434984424217906 -0.13258811839182447; 0.01655970843213068 0.021474705746660414 -0.09222980426779685; 0.01049487537677418 0.013874083890883876 -0.06693379488480816; 0.011094537508937123 0.01967682073210263 -0.09382542533317158; 0.005952188684591435 0.011493125496033695 -0.054673176780492945; 0.000660621520467849 0.0009910740975231736 -0.0059534464524647205; 0.000232208780465853 0.000398464208772207 -0.002206355718936093; 0.0003943354523319499 3.16418906137669e-5 -0.0021414276319304693; 2.093281856220758e-5 2.6129636005569296e-5 -8.078960795866518e-6; 0.0003693299385592538 7.414781677347502e-5 -0.0010191500192014773; 0.00023664881841307196 6.253126493881319e-5 -0.0005935132984557998; 0.0007073775979540668 4.0786655041411506e-5 -0.0003182305673431377; 0.00011229044146784778 0.00029861110859407867 -5.189931865070917e-5; -0.00021907177799839787 0.0001355462961031466 0.00015916691965242613; -0.0003131245683582538 0.0016190785013516507 -0.0005917641706069743; -0.00043890199740328687 -8.119840112083315e-5 -0.0012534850045604429] %
+
+Mass Used: 79.6371279240534 kg
+Launch C3: 97.54839344708901 km²/s²
+||V∞_in||: 3.799478094939558e-5 km/s
diff --git a/archive/ES_0.556013249386611 b/archive/ES_0.556013249386611
new file mode 100644
index 0000000..518e76e
--- /dev/null
+++ b/archive/ES_0.556013249386611
@@ -0,0 +1,22 @@
+archive/ES_0.556013249386611---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T03:04:26.321
+Launch V∞: [7.860055737462318, -5.770346641046264, 0.13126190673015026] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.780528110510979e-7, 1.257296816235238e-6, -2.7674229954392286e-5] km/s
+ V∞_out: [-1.2390797064589474e-6, 2.7649896296446224e-5, -3.436463492247878e-7] km/s
+ time of flight: 1.874957778748942e8 seconds
+ arrival date: 2030-04-23T05:14:03.321
+ thrust profile: [0.4040972067581099 0.0066691001844249405 -0.10601385558904793; 0.10842522070857775 0.07262866076216816 -0.11232715120771936; 0.05150874710098178 0.05518904184317547 -0.09794082800724666; 0.04134498120444533 0.060171850452838335 -0.11944749889127763; 0.026929261261852022 0.04904725828100288 -0.10760239757433428; 0.014482155790442064 0.0321467323606286 -0.07805715465805463; 0.014497420463849213 0.03896075885744918 -0.09910348734346512; 0.00452490303535214 0.014224191094648477 -0.0396962442170688; 0.0036389526340463913 0.013332741365621526 -0.03918794977692933; 0.00016667747800087798 0.0007068519258547016 -0.0022904287205072187; 2.3030407275853384e-5 0.00010294885002174494 -0.0004996703244217485; 7.550139780316485e-5 0.0005565665590839297 -0.0018640089835188158; 9.797591208025272e-6 9.09476222569212e-5 -0.0003985768136785482; 3.446165778294029e-5 0.00010825519461137625 -0.0002635579317005486; -3.113299492526941e-5 8.598651094866844e-5 -0.00018954214640476264; 0.0001248300354535298 3.1980079119587945e-5 -0.00029995776623381647; -6.131439183365271e-5 -0.00012208516898036016 -5.962791999395442e-5; 1.2008978010398535e-6 -1.2784673008928594e-5 -0.0001364094496309427; -7.816250330869851e-6 6.979989161552864e-5 -6.447141034883412e-5; -2.0630840590022804e-5 4.1609265474520745e-5 -4.904760252452483e-5] %
+
+Mass Used: 93.963587872674 kg
+Launch C3: 95.09460624200665 km²/s²
+||V∞_in||: 2.770334820299203e-5 km/s
diff --git a/archive/ES_0.5560302497517988 b/archive/ES_0.5560302497517988
new file mode 100644
index 0000000..d2a7b23
--- /dev/null
+++ b/archive/ES_0.5560302497517988
@@ -0,0 +1,22 @@
+archive/ES_0.5560302497517988---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:21:43
+Launch V∞: [8.175820328617231, -5.61236489028906, 0.18882384579332034] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.168139797155562e-5, 4.353242590452324e-5, 0.003124951683313912] km/s
+ V∞_out: [-0.002784224841869423, -0.0009429441653261373, 0.0010636702884266906] km/s
+ time of flight: 1.8749577787493032e8 seconds
+ arrival date: 2030-04-23T20:31:20
+ thrust profile: [0.21424751822530164 -0.004488215407538177 -0.0749524558706452; 0.04380350731932066 0.022649588264893553 -0.05468378907646266; 0.040901215299517 0.033445499325271466 -0.09086470825672996; 0.03592289942819118 0.037650075424484515 -0.11630801413668601; 0.028933583636193073 0.03600334192359639 -0.12437433237327482; 0.02033828752079127 0.028841544259281048 -0.11028968800855075; 0.008572561489180496 0.01339468392754076 -0.057216055103303985; 0.008561177218199661 0.014611192617317949 -0.06661577505108238; 0.004305397866699969 0.008213352322026527 -0.04056695290613526; 0.003074124756722263 0.0061095084045968235 -0.031069072709701162; 4.826429810440261e-6 0.00033009013609806246 -0.0023352553646753655; -0.00034185936816452216 0.001139773532927608 -0.0010767950152590783; 0.00016506232235703896 -0.00018623645763275536 -0.0017262347971008225; -0.00013610643114529664 4.781679918323283e-6 -0.0021424397482258358; 0.0001961406580849718 -0.0005049602424059507 -0.0006887504663028065; -0.0012013844022803603 -0.0009288556579991438 0.0005553683168763423; 0.0006065761208679061 -0.0004457019037639432 -9.158038670636264e-5; 4.755794232342467e-5 0.000801979987108398 0.0005954378070580379; -0.0017009066650779236 0.0008577468821495283 -0.001097911697316282; -0.0032857123637384626 -0.002816437507060091 0.0019778627083701034] %
+
+Mass Used: 74.82835382189705 kg
+Launch C3: 98.37833215232027 km²/s²
+||V∞_in||: 0.0031258635110969434 km/s
diff --git a/archive/ES_0.5560374439181403 b/archive/ES_0.5560374439181403
new file mode 100644
index 0000000..d0f6a9a
--- /dev/null
+++ b/archive/ES_0.5560374439181403
@@ -0,0 +1,22 @@
+archive/ES_0.5560374439181403---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T13:22:22.606
+Launch V∞: [7.977094935339214, -5.629467385291354, 0.12262804555276433] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.3291627875915337e-9, 4.8061379968936765e-9, 2.2561512131985537e-9] km/s
+ V∞_out: [5.263662050021237e-9, -4.284312731265208e-9, -3.2299445724439386e-9] km/s
+ time of flight: 1.874957778743274e8 seconds
+ arrival date: 2030-04-22T15:31:59.606
+ thrust profile: [0.42982459188051314 0.00033391528064536074 -0.13220541781913384; 0.08298643851081082 0.04905838543330085 -0.0929251231599317; 0.03748281398495657 0.03578659708158271 -0.07774928881366648; 0.027150537573928272 0.034404339401630055 -0.08441281119000543; 0.034718564425490366 0.05583328243760254 -0.14633643861803497; 0.025769228632634394 0.04488197014848682 -0.12930402776556438; 0.006814914141279407 0.014546570499290893 -0.04691292308625726; 0.009420397941352934 0.022653686388950142 -0.076782430709424; 0.0007977958289987305 0.0021332806987351353 -0.008068076726435723; 0.0012817640562851791 0.0036619443471817563 -0.014697579364420304; -0.00048432605339396935 0.0007266961950264273 -0.0018595074443775745; -0.0005920941836886345 0.000242133758275587 -0.0021854062181277762; 0.00026730526921683 -5.4348624965472164e-5 -0.0003245639992068103; 5.938304729268088e-6 -0.0002734049570118541 0.0006479316813806919; -7.521624505774308e-5 -7.745164632033674e-5 -0.0001413634737957698; 0.00047078147890202153 -0.0003393890663026521 -0.0007943744501436677; 1.7308548580803184e-5 0.00024186683665299328 0.000859823467169212; -0.00040877405401792434 0.0007544480048381153 -0.0011335020722359063; -0.0014289387307418434 0.000956750450570228 0.0014149461717393077; -0.0003628643338636456 0.0009164399988649448 -0.0028179549765405855] %
+
+Mass Used: 92.56044289682359 kg
+Launch C3: 95.33998428702971 km²/s²
+||V∞_in||: 6.266777928751481e-9 km/s
diff --git a/archive/ES_0.5560870254138799 b/archive/ES_0.5560870254138799
new file mode 100644
index 0000000..e3ed1bf
--- /dev/null
+++ b/archive/ES_0.5560870254138799
@@ -0,0 +1,22 @@
+archive/ES_0.5560870254138799---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T13:32:06.515
+Launch V∞: [7.903065764802332, -5.792316445107079, 0.3083610575150852] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.25768836959837e-10, 1.4580617739244298e-9, -1.6937858056399061e-9] km/s
+ V∞_out: [1.1375085310421245e-9, 2.3260719565537642e-9, 5.373748706892441e-11] km/s
+ time of flight: 1.874957778745525e8 seconds
+ arrival date: 2030-04-24T15:41:43.515
+ thrust profile: [0.3696328595298713 -0.0017046628995985166 -0.12236812379129403; 0.08808420068997598 0.04704190944210103 -0.10285984276130947; 0.05445452322788845 0.04590595821794026 -0.11482589116475486; 0.04414271438733674 0.04802040815156267 -0.13676870805893138; 0.02995775693059061 0.0387952832147744 -0.12440942145301179; 0.02146437241207627 0.03185216244736576 -0.11270546382895284; 0.007957289717921178 0.013029892839934625 -0.05166477250968133; 0.0007693073548604535 0.0019472194922008788 -0.007932009125578827; 0.0029925976004348746 0.005740806213503708 -0.02317267455240455; 0.0006785758564463566 0.0006746741030396582 -0.004934139255073625; 0.0005241115922694668 0.0010075616422508362 -0.00305096316410143; 0.00012329225078680473 -0.00048206263576244335 -0.002781246906259885; 0.0009968447366107008 -0.00046316481151804695 -0.00045749570160252167; -7.595831158165186e-5 0.0002491443017233471 -0.0011690537249802893; -0.0010096842349010715 0.0002247292151953849 0.0004561681405349905; -0.0008507861782000201 -0.00025585398371807033 0.0005041926851223604; 0.0017934420019823955 0.000798526781430935 4.547414197557072e-5; -4.6166936751702064e-5 -0.0008366793345247841 -0.0005750832542669003; -0.0005177441703119367 -0.0007546362239652093 0.0022457776481607213; 0.00027734073629828444 -0.001366899095811771 -0.00046366890814128925] %
+
+Mass Used: 88.15881817129093 kg
+Launch C3: 96.10446482484039 km²/s²
+||V∞_in||: 2.3825928447934368e-9 km/s
diff --git a/archive/ES_0.5560874775745556 b/archive/ES_0.5560874775745556
new file mode 100644
index 0000000..ed32122
--- /dev/null
+++ b/archive/ES_0.5560874775745556
@@ -0,0 +1,22 @@
+archive/ES_0.5560874775745556---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T02:37:22.285
+Launch V∞: [8.059048907325149, -5.789222085958995, -0.052814026822099534] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008101640233206347, 0.004636423144843509, 0.0003437910228109302] km/s
+ V∞_out: [-0.006558377623227536, -0.003980297906074802, 0.0053213597199697335] km/s
+ time of flight: 1.8721552247903374e8 seconds
+ arrival date: 2030-04-21T22:56:04.285
+ thrust profile: [0.19288507967070875 -0.0030351649052160735 -0.06721323693916974; 0.053435756921278665 0.029024475651374414 -0.0687732658918533; 0.05385297317309167 0.04576333633912538 -0.1194930502886739; 0.03015621313237178 0.0337682861839777 -0.09792416476897234; 0.03118229608088767 0.03823372413238957 -0.12790113736322029; 0.025051447488358417 0.03676571518139263 -0.13388813168328012; 0.008702887075439255 0.015375587405900398 -0.06188084906649945; 0.004304690088545971 0.00820062000923867 -0.036448707179338576; 0.003031519378471675 0.0059370934059777706 -0.02851403137673227; 0.0018026455986934408 0.004001278661552307 -0.020307937126150782; 0.0009731479925805949 0.002970260761437112 -0.015025340678370042; -7.154980115031677e-5 0.00022070237685704007 -0.0008160283821290135; 0.00055729180289763 0.0011333220573740966 -0.0030747260192279455; 0.00014823998087049923 -0.0003626515290210627 -9.248512692142135e-6; 0.00018763701032183255 -0.0001428144848600594 -0.00011055444444791392; 0.0012572232853799168 0.00021650469476896313 0.00016459258264557314; -0.00045423171752781194 -0.000727643281446375 -0.0006877395181767211; -4.570700454201523e-5 -3.0316813520102153e-5 0.0004488125568823444; 1.2505717814651011e-5 0.0012441290724357773 -0.0004696073422551325; -0.0003225799667493989 -0.00014533600383023353 0.00029923520233446176] %
+
+Mass Used: 74.38284316322915 kg
+Launch C3: 98.46615097264325 km²/s²
+||V∞_in||: 0.009340834347836053 km/s
diff --git a/archive/ES_0.5561011640998079 b/archive/ES_0.5561011640998079
new file mode 100644
index 0000000..10bcce7
--- /dev/null
+++ b/archive/ES_0.5561011640998079
@@ -0,0 +1,22 @@
+archive/ES_0.5561011640998079---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:33:48.018
+Launch V∞: [8.136785866217704, -5.6108123773319765, 0.16635255336121602] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.743508066376803e-5, -5.284079246828859e-5, -0.003806607070357464] km/s
+ V∞_out: [0.0033910820765135834, 0.001161289185733922, -0.0012833003272395072] km/s
+ time of flight: 1.874957778723651e8 seconds
+ arrival date: 2030-04-23T07:43:25.018
+ thrust profile: [0.2631484320350599 9.567403825654108e-6 -0.08574611049775405; 0.04778965567959356 0.0269111258372699 -0.05525765070838081; 0.03220871364657565 0.03032348879986112 -0.06694072808394749; 0.026037870040057726 0.03209144379321027 -0.07984021924694645; 0.035887801328755214 0.05202182656116313 -0.1472476674867993; 0.018922345225183067 0.03266389326355718 -0.10101075726415451; 0.013124036826892123 0.02776643207145547 -0.09353318627751943; 0.008816746821852758 0.01813571498455634 -0.06868743029893457; 0.0018175698800015237 0.004302157065089874 -0.017082739766439266; 0.005973748731999345 0.011771059183948857 -0.04704251272970921; 0.0012711184243173945 0.003950313504367576 -0.01665487907704195; 0.00033318475385444196 0.00017464977151404894 -0.00019045177386834138; 0.00012001822978138366 0.00035950067644101487 -0.0005960267236749759; 0.00016246693835486096 0.0002968059510191588 -0.0006796474103684337; -6.93499709032203e-5 -8.822683831477103e-5 -0.0005318131092575221; 0.00014580107377388458 0.0005355578142923454 -0.0008389303020718026; -1.2317176240896576e-5 0.00022726288611488724 -0.00030111365374299587; 0.0008562573234067433 0.0011441704572721226 0.000877785583802155; 0.0010614115537103744 -0.0010983013187446343 0.0008523094605073745; 0.0008920575556642776 0.0005631268941302771 0.0007150596216535855] %
+
+Mass Used: 78.77368264295774 kg
+Launch C3: 97.71617293831169 km²/s²
+||V∞_in||: 0.0038077612489705176 km/s
diff --git a/archive/ES_0.5561264364833008 b/archive/ES_0.5561264364833008
new file mode 100644
index 0000000..14fec31
--- /dev/null
+++ b/archive/ES_0.5561264364833008
@@ -0,0 +1,22 @@
+archive/ES_0.5561264364833008---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:34:56.158
+Launch V∞: [8.032208547438772, -5.726167465226698, 0.13870423021830933] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.02703561651502518, 0.16106811098990528, 0.19719097401921765] km/s
+ V∞_out: [-0.10235312189412307, 0.08676047284261586, -0.21143623279213805] km/s
+ time of flight: 1.8749577787456104e8 seconds
+ arrival date: 2030-04-23T13:44:33.158
+ thrust profile: [0.21321238735723233 0.00400893211866124 -0.06602388092475038; 0.12450801559252848 0.07654693110174048 -0.13324796736979574; 0.06037172207118899 0.06247508621636275 -0.12300109846806825; 0.031718851838400404 0.042565952140561095 -0.09752872445269818; 0.018866952814463968 0.030960174368132642 -0.0790693111416094; 0.015794869132650678 0.033732143371118885 -0.09058142301871015; 0.012424268461498644 0.031142262449133443 -0.0923556364410218; 0.0050340831982655055 0.013297196119518333 -0.044178151936650235; 0.005256944487111725 0.016412852896715464 -0.05512479448330896; 0.0002696059330315718 0.001117009849965937 -0.004354525063726138; 0.0004920012097072178 0.00042933567721857005 -0.0017729365656286758; 7.7131965890521e-5 0.0007268608820895097 -0.0025414618108920294; 0.00030976099748762686 0.0005037289180718109 -0.0008066770904854534; -0.00012173503799693643 0.00025500351140371133 -4.9442178078216905e-5; -1.0845532998783925e-5 -6.850718292982015e-5 -0.00041023548521164387; 0.00041051200748146746 -0.00039798839018583416 -0.00040737649524699384; -0.0005634833649246254 -0.0007997049331625739 0.001673802951129837; -8.207510070822402e-5 -0.0005021872012619433 -0.0004145739209143182; 5.56966262901298e-5 6.679141781831236e-5 0.0006188275817338835; 0.0008135835213642441 0.0005371090523874223 0.0010708658060042094] %
+
+Mass Used: 81.08730258889454 kg
+Launch C3: 97.32460685284967 km²/s²
+||V∞_in||: 0.25604324082633334 km/s
diff --git a/archive/ES_0.5561276911100703 b/archive/ES_0.5561276911100703
new file mode 100644
index 0000000..0cacf2a
--- /dev/null
+++ b/archive/ES_0.5561276911100703
@@ -0,0 +1,22 @@
+archive/ES_0.5561276911100703---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T13:27:03.306
+Launch V∞: [8.033834090000655, -5.734791319251567, 0.09618856412200412] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.748281168927652e-6, 5.97195052503164e-6, 1.649403194239303e-5] km/s
+ V∞_out: [1.5896145849374433e-5, 1.8243646362326788e-6, -7.493022032934087e-6] km/s
+ time of flight: 1.8749577787442285e8 seconds
+ arrival date: 2030-04-23T15:36:40.306
+ thrust profile: [0.20436313858422048 0.0034186653681458853 -0.06551799214084561; 0.08935399720026313 0.054426067820856516 -0.09885803321382577; 0.09455658289520254 0.09222947739232118 -0.18065619909418312; 0.03452501271017344 0.044864157884528036 -0.1036944133021147; 0.034368589239506586 0.05504332216848672 -0.13780597534497735; 0.010040758826226048 0.019541314525257744 -0.05572607086280189; 0.008975519402685294 0.020361248327724835 -0.06150973791960264; 0.0032165237676891173 0.008568802263322486 -0.02837695935976615; 0.003230125809448937 0.0089418060186422 -0.03113855450595036; 0.0007719115995401342 0.0020577948704138325 -0.007643342879693757; -3.802208650925643e-5 0.0031926651137841747 -0.01008392031315767; 0.000892926454246069 0.0017414957581578065 -0.0066977399170250465; 0.0003881408823427289 0.0002581554891886638 -0.00033719853428887674; 0.0006488662620209648 1.697590245959118e-6 0.00039249896201878985; -0.0005119669831484476 6.825433105681566e-5 -0.000848576325261672; 0.0006286622058894219 -1.018709788807425e-5 -0.0004904655591295383; -0.000739863588299794 -0.000251478999338206 -0.0005007777143807247; 0.0001762159683788523 0.0005298397826739485 0.0001263221522621134; 0.0016488451634691485 -0.002541763854843176 0.0030517822426111667; -0.0008082467024551653 0.0006602120930592517 -0.0019204759636704644] %
+
+Mass Used: 80.41812520657095 kg
+Launch C3: 97.43957390088762 km²/s²
+||V∞_in||: 1.762877675381177e-5 km/s
diff --git a/archive/ES_0.5561380803810103 b/archive/ES_0.5561380803810103
new file mode 100644
index 0000000..83e7c0b
--- /dev/null
+++ b/archive/ES_0.5561380803810103
@@ -0,0 +1,22 @@
+archive/ES_0.5561380803810103---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T03:28:18.582
+Launch V∞: [7.984121408349645, -5.788783842562156, 0.1755785013379551] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00805718138184867, 0.0492072515693576, 0.051127278249547096] km/s
+ V∞_out: [-0.012665856690740664, 0.011503680394021486, -0.06929252027017112] km/s
+ time of flight: 1.8564504115553725e8 seconds
+ arrival date: 2030-04-02T19:32:19.582
+ thrust profile: [0.2928369957458383 -0.009850827455999219 -0.09971612535620156; 0.05484379155015243 0.027717502523168666 -0.06923241810819644; 0.05118808248990834 0.04084512334647802 -0.11310259190799817; 0.038067001092212206 0.03881510256910821 -0.12257319895747562; 0.028766274614566826 0.034802752402215247 -0.12361425360239242; 0.018470171763442962 0.02540514321646908 -0.10015568175602826; 0.008987649365247506 0.013886760182312462 -0.05998638148921535; 0.0059573031181198235 0.009875527278910128 -0.04662543606591987; 0.005169250355174384 0.009438563103148986 -0.046665532931321106; 0.0026727244135037625 0.004979827679025973 -0.026202265210032938; 0.0001921314645709331 0.000470063211107469 -0.0020036583982912934; 0.00046031816194102367 0.0006224545670291271 -0.00012961790065043314; 0.0006312629522750017 0.0003235114945988985 -0.0018869832485753182; -0.0001893407362844905 0.0004946789112764906 -0.0015955309721358503; 0.00012027283276977343 0.00029424606087547156 -0.00046911067032127875; 2.588698966784201e-6 -0.0008892267844187104 -0.0008669860323820746; 0.0009743501688219969 -0.0011863856682516802 0.00012727728130620117; 0.0005416791859201043 0.0004524383713462943 -0.0006957209059125842; -0.0004395530443599832 -0.00028135169685047 -5.522714856387055e-5; -7.966190914947963e-5 0.00015506798197468022 -0.0002264310559178331] %
+
+Mass Used: 81.32002215688271 kg
+Launch C3: 97.28704084930789 km²/s²
+||V∞_in||: 0.071416177159217 km/s
diff --git a/archive/ES_0.5561480297794383 b/archive/ES_0.5561480297794383
new file mode 100644
index 0000000..1a6fdc6
--- /dev/null
+++ b/archive/ES_0.5561480297794383
@@ -0,0 +1,22 @@
+archive/ES_0.5561480297794383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:17:06.686
+Launch V∞: [8.05686883960453, -5.675490287023429, 0.1913923308160258] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7981597377956777e-9, 2.4380682274238045e-9, -1.6781606586687267e-8] km/s
+ V∞_out: [-4.5283431465007624e-9, 1.5386183270836245e-8, -2.4235799592677374e-9] km/s
+ time of flight: 1.8749577787468255e8 seconds
+ arrival date: 2030-04-23T09:26:43.686
+ thrust profile: [0.2842766313507401 0.008618124120600937 -0.08833633971289807; 0.06454524319737817 0.0395682191920952 -0.07078003128776984; 0.04130222674373952 0.04030089047990399 -0.08168045795577117; 0.03328417016265319 0.04120712876171342 -0.09392731935569407; 0.022043949910966296 0.03474336144748383 -0.08898524407686317; 0.020539150476048325 0.037455157277705306 -0.09573272920866281; 0.012492274383750498 0.03087919280449132 -0.08970454934773445; 0.010877399096420012 0.02827503663671588 -0.08617007776127436; 0.0074775603040285795 0.02386537637443098 -0.07484847545400576; 0.00042614487449763364 0.001422535031628905 -0.005290195529747284; 0.00014179322267750247 0.000556207475985408 -0.0017312678268648957; 0.0005104581073287853 0.0024366594865118454 -0.009904534975192938; 8.852812594451507e-5 0.00011324567752714042 -0.00041723141482252226; 8.047312543386085e-5 9.896567783169478e-5 0.00014616731485464588; -0.0002329436162685858 -0.00019540645182076905 -7.64768093689025e-5; -8.092737685868826e-5 0.00039070478746223953 0.0003106937498334129; 0.00038944748209258196 -0.0002742375355007434 0.00044035227038678585; -0.00040618912685672147 -1.5662514147617412e-5 -0.0003714552348321847; -0.00034188576826118584 0.0002713762744145082 -0.0003366232619460354; -0.00020299051090066314 0.00017740492457031973 0.00026766512805021653] %
+
+Mass Used: 82.06712170361106 kg
+Launch C3: 97.16095652098291 km²/s²
+||V∞_in||: 1.7187093827350208e-8 km/s
diff --git a/archive/ES_0.5561590027368806 b/archive/ES_0.5561590027368806
new file mode 100644
index 0000000..eb80009
--- /dev/null
+++ b/archive/ES_0.5561590027368806
@@ -0,0 +1,22 @@
+archive/ES_0.5561590027368806---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:13:10.152
+Launch V∞: [7.910804763341061, -5.75484703150925, 0.030349790124664714] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1836617333835936e-7, 7.617443157912226e-7, 2.0325113918312785e-6] km/s
+ V∞_out: [1.9563160249610422e-6, 2.3139393335139954e-7, -9.60946102492032e-7] km/s
+ time of flight: 1.8545759332913393e8 seconds
+ arrival date: 2030-03-30T03:13:03.152
+ thrust profile: [0.374892664154981 -0.004401962746722948 -0.1189229001207687; 0.0898968208738814 0.050665803205791005 -0.10066991766189176; 0.06015409353499101 0.05599416499709398 -0.12237428302858107; 0.04550507560992256 0.05238870148090309 -0.13152841647762276; 0.02590660257731984 0.04001529778707843 -0.11090959445415628; 0.012572233129052798 0.02422971638648206 -0.07140771573933906; 0.011208315011794135 0.02305143229866413 -0.08171482824046922; 0.006208753830170395 0.015596837615068398 -0.05222142500515871; 0.005097803586050039 0.012452806018483753 -0.04325113296086274; 7.385873430252425e-5 0.0003557915689571783 -0.0012056936949037841; 6.933365112441645e-5 0.00029082057324171393 -0.0011950950051528271; -4.50708819181819e-6 0.0003327436449706307 -0.0010803027313554137; -0.00024721517877412914 0.00010911354525311174 -0.0011146615010595184; 0.0003392360438967832 -0.0003894153267512227 -0.0003648348238856744; 0.00017790562726655484 -0.0001804269278521017 -0.00027522504066699693; -0.0002149174787822908 -6.432329396567331e-5 0.0006146345648820094; 0.0007385350536031465 -0.0003389028479287518 -0.00025159333724003076; 0.0004568846828998333 1.72880937963582e-5 -0.00012048647556499407; -0.0012143533036206712 0.0010639340793232106 -0.00021526486456007336; 0.0009071270700400297 0.00014406266471610085 -0.00015951556831188035] %
+
+Mass Used: 90.60206795409613 kg
+Launch C3: 95.70001746953108 km²/s²
+||V∞_in||: 2.18152257522644e-6 km/s
diff --git a/archive/ES_0.5561719499322813 b/archive/ES_0.5561719499322813
new file mode 100644
index 0000000..5cd7cb8
--- /dev/null
+++ b/archive/ES_0.5561719499322813
@@ -0,0 +1,22 @@
+archive/ES_0.5561719499322813---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T04:09:10.155
+Launch V∞: [8.032130051181392, -5.766518363452874, 0.0032123316159313594] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.087530029024174e-5, 2.9342305234332196e-5, 0.002079762830204299] km/s
+ V∞_out: [-0.0017859833215184175, -0.000597276087013964, 0.0007603354829672767] km/s
+ time of flight: 1.8749577783417055e8 seconds
+ arrival date: 2030-04-25T06:18:47.155
+ thrust profile: [0.26940527919740853 -0.0060371361457184965 -0.09200259852219836; 0.05148020352203567 0.026478090712171356 -0.06589903775716009; 0.032846237198447585 0.026198243977540458 -0.07481453170206952; 0.04397710730864932 0.04409032901843058 -0.14159364613904712; 0.02531016374993345 0.03177744911312903 -0.11691668805230443; 0.01411082267396785 0.01980144527846995 -0.08013341009215466; 0.01613796154915824 0.025048444064241778 -0.10868715694876956; 0.00436496465805453 0.007217581057247228 -0.03543344734242776; 0.0038938987577567755 0.007191430163534389 -0.03706789698792049; 0.0021472189526367037 0.003918199418540527 -0.021763797336637084; 0.0006909987741909884 0.0011250026406242212 -0.006272541194071535; 6.652241901006434e-5 0.0003863646375625869 -0.0019838232082962652; 0.0006652090368581302 0.0006266695760953256 -0.00515086205967088; 0.0006169111643024998 0.0002214140111147006 -0.001448199468146083; 0.0006159122217725991 0.00020349688137261173 -0.0010833007248630508; -0.00020885882207855803 0.0005986898923906168 -0.001857390672635219; -0.00039044448414460786 0.0009151608227066553 -0.00046107652450588397; -0.0001276448176629487 -5.942905269653365e-5 0.0004425301209376; 0.0006967830698892568 -0.00014609635708542332 -0.000459884726307329; -0.00144528884873883 -1.9203717946881733e-5 -0.0005070952239310121] %
+
+Mass Used: 78.55477275480007 kg
+Launch C3: 97.7678575142048 km²/s²
+||V∞_in||: 0.0020803714069727256 km/s
diff --git a/archive/ES_0.556173115144034 b/archive/ES_0.556173115144034
new file mode 100644
index 0000000..7d33c47
--- /dev/null
+++ b/archive/ES_0.556173115144034
@@ -0,0 +1,22 @@
+archive/ES_0.556173115144034---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T16:42:25.298
+Launch V∞: [8.120421029921634, -5.553019904241112, 0.1808065598788059] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0070876117012233e-6, 8.623258299894336e-7, -6.791286710067611e-7] km/s
+ V∞_out: [2.0069410611519762e-7, 1.485140648867359e-6, -7.03332809219279e-8] km/s
+ time of flight: 1.8749577787436914e8 seconds
+ arrival date: 2030-04-21T18:52:02.298
+ thrust profile: [0.28956869447172673 0.002996571896207132 -0.08717070811175409; 0.10146618555582897 0.06348179433533103 -0.11108830795987491; 0.05093128276329364 0.050783122603167766 -0.10256745222012534; 0.030263408697206087 0.04047338694027824 -0.09266375602176198; 0.024978895965809086 0.041976018672915144 -0.105261978631947; 0.03260143190268559 0.06605720545800628 -0.17444055205453576; 0.007506751164035362 0.016858797733696324 -0.05089946096596279; 0.004064686362502569 0.010492092607441139 -0.03385253816675186; 0.0012290734806084302 0.003622209742881372 -0.012511817810463234; 0.0013910774618823383 0.004681609242925643 -0.016843009934624988; 5.198319084335421e-6 5.30751000258269e-5 -7.942514038192838e-5; -0.00016029612666726387 0.00017814676438240092 -0.001049583915319562; -8.715073309810184e-5 -5.322259490898618e-6 -0.00013151674764369498; -0.00013683391888942017 -2.8102048856150458e-5 0.0004129594485976515; 1.3324279057530064e-5 0.0001884941539050306 -0.0004937901219686702; 9.223840019632586e-5 8.007746562158048e-6 0.00013759861518830406; -0.0004035808670023167 0.00016781114949710642 0.00011423683453309495; -0.00011334226481852251 -0.0004233465343648505 -0.0003799753025531257; -0.0001596944441242512 -0.00010331813951498578 0.00012988475073011233; 0.0004564622720252193 0.000828685300655314 -2.2513079683920994e-5] %
+
+Mass Used: 84.14387483028395 kg
+Launch C3: 96.8099587721867 km²/s²
+||V∞_in||: 1.4896466179911424e-6 km/s
diff --git a/archive/ES_0.5561731275157772 b/archive/ES_0.5561731275157772
new file mode 100644
index 0000000..c0c66db
--- /dev/null
+++ b/archive/ES_0.5561731275157772
@@ -0,0 +1,22 @@
+archive/ES_0.5561731275157772---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T01:36:08.002
+Launch V∞: [8.19898523640216, -5.626852509498531, 0.18940819306915288] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.945228258766911e-5, 4.789592736658699e-5, 0.003497752817573441] km/s
+ V∞_out: [-0.0031116020697351, -0.0010811527739861472, 0.0011795634865478409] km/s
+ time of flight: 1.8749577787493315e8 seconds
+ arrival date: 2030-04-24T03:45:45.002
+ thrust profile: [0.1874026789659382 -0.0018822235907613265 -0.06583504036325655; 0.02142739686259087 0.011560024997370192 -0.0279332026293689; 0.03491572367684594 0.029954163620636923 -0.07891549400328492; 0.037274948809126525 0.041286809875666935 -0.12155463956889404; 0.026226930353550497 0.03475143464575377 -0.11490959680688238; 0.01059112040109375 0.01610506116769849 -0.06075687546452033; 0.017821101098869124 0.030862959850764954 -0.12162346733180018; 0.006585323985976016 0.01289011303575781 -0.05629235654218949; 0.004902725684135928 0.01008747487602747 -0.049207844865204235; 0.0034136240781789968 0.007914085424128546 -0.03799879158605521; 0.0020914941272018833 0.006694844795630415 -0.032621872004285145; 0.00021267592222676035 0.0007177651379407908 -0.00032546213288465033; 0.0005056244901402163 0.0002901683094584019 -0.0007240577067134429; 4.265634821078321e-5 0.00026100931065118184 -0.0002851015137542201; 0.00039938337121284606 -0.0013204790800375545 0.0005206321966106097; 0.000678571748374258 0.0003484812954542824 0.0002960122377893321; -0.00016266014735206611 0.00017657995711139942 -0.00011543757728172007; 0.0008004767124208212 2.5580499895879122e-5 0.0007536405581800854; -0.00036855575191544577 -0.0006563360378001036 0.0001887568957560531; 3.1550487351711485e-5 -8.032728311577458e-5 0.0005459277811983059] %
+
+Mass Used: 71.83121148678538 kg
+Launch C3: 98.92070353399222 km²/s²
+||V∞_in||: 0.0034987701285248635 km/s
diff --git a/archive/ES_0.5561797351550313 b/archive/ES_0.5561797351550313
new file mode 100644
index 0000000..7fb6d29
--- /dev/null
+++ b/archive/ES_0.5561797351550313
@@ -0,0 +1,22 @@
+archive/ES_0.5561797351550313---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:45:27.867
+Launch V∞: [8.193808270284642, -5.603753599096904, 0.20148368731909969] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.911550041451792e-7, 3.5811495056189518e-6, -7.503792871737149e-5] km/s
+ V∞_out: [-2.8336082897694593e-6, 7.51291332039698e-5, -7.919741990117348e-7] km/s
+ time of flight: 1.8749577787486872e8 seconds
+ arrival date: 2030-04-23T20:55:04.867
+ thrust profile: [0.20024956580833073 -0.004280925600555811 -0.07163844565672738; 0.03565198690123371 0.018167152446924083 -0.046149584525059344; 0.045954424845413865 0.03695622124186724 -0.10562311134218387; 0.04398758005824856 0.046285347289047325 -0.1466644890455148; 0.02632741474398909 0.03184677872761241 -0.11770683548585188; 0.017291355218550276 0.02379305154464671 -0.09700471749217046; 0.010904566686430323 0.016704767654548505 -0.0729078299105698; 0.0054309574878449495 0.007918609013721335 -0.0398375962039399; 0.00437639658744474 0.00754144358181329 -0.035227762546660116; 0.003831631665184442 0.005141183545630159 -0.030164750115637195; 0.00016989387644755245 0.0004505713956210019 -0.003353014440906028; -5.7883789891014685e-5 -0.00018190596187511396 -0.0012556784564079536; 0.0008546503770848638 -0.0008159556726637155 -0.0022422999194003645; -0.0006353752903941651 0.0005165728609032789 -0.0010418134962016648; 0.00041643402747462775 -0.0008420719451342611 0.0013341724482328924; -0.001326442677242782 -6.162675383916233e-5 -0.0028070353488134662; -0.00015443626335676184 -0.00023532164659002906 0.0006186115595341445; 0.00041899817236557555 0.0032641105258323496 0.0029764688697350786; 0.0013691772545511324 -0.0010712256261342248 -2.4090387193235205e-5; 0.000484138712525303 -0.00023003526672924846 0.004068044169468118] %
+
+Mass Used: 73.81968408018201 kg
+Launch C3: 98.5811440458322 km²/s²
+||V∞_in||: 7.512494000804937e-5 km/s
diff --git a/archive/ES_0.5561892056404947 b/archive/ES_0.5561892056404947
new file mode 100644
index 0000000..5960903
--- /dev/null
+++ b/archive/ES_0.5561892056404947
@@ -0,0 +1,22 @@
+archive/ES_0.5561892056404947---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T02:20:03.395
+Launch V∞: [7.907450915723662, -5.735662032452591, -0.05482976031895736] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.0648310876227926e-6, -5.918592349052711e-6, -0.00030418141691352925] km/s
+ V∞_out: [0.00026652305570219704, 0.0001002339701951301, -0.00010579919723512146] km/s
+ time of flight: 1.874957778749824e8 seconds
+ arrival date: 2030-04-24T04:29:40.395
+ thrust profile: [0.4508411556921118 -0.004843814451252359 -0.14715656391857976; 0.051661908583571566 0.027897634129117548 -0.06190778849358008; 0.05164013481575603 0.0448270742990032 -0.11205608421050545; 0.028236254812222143 0.031461101239789194 -0.09056680694755549; 0.025140780032653125 0.034363977440869775 -0.10957378969644513; 0.026541949990862714 0.04228065278622367 -0.14575161543518528; 0.007463451221640484 0.01399700523390372 -0.05125331550858389; 0.009454225980832434 0.018796773601277364 -0.08006480685574532; 0.0006157821090766226 0.0016748450981424942 -0.007252999385283989; 0.0002785639781026136 0.0011687581511533958 -0.00612108913665062; 0.00030111200432571646 0.0014820899787182206 -0.006222332568585003; 0.00027165983260965147 0.00041416372990727487 -0.004325121775252804; 8.99847745973115e-5 9.93437337360307e-5 -0.0007013705996035578; -0.0004076990325248415 0.0005643078168044189 -0.0006358541893851453; 0.0004518298665346684 -0.0009574590308797817 -0.00014532796060477823; 0.0004292406938670514 -8.45761216520439e-5 1.7550134956497983e-5; -0.0008709885906169896 -0.00021497227782448685 -0.0006246710401863578; -0.0004025521114127919 0.001405841134071568 -0.0005429790486696494; 0.0014948723372927059 0.001873240720871087 -0.00014620551815396163; -0.0012364002884880866 -0.001970278030018346 0.0028375932511998376] %
+
+Mass Used: 92.2205426939131 kg
+Launch C3: 95.42860523771382 km²/s²
+||V∞_in||: 0.0003042994352722955 km/s
diff --git a/archive/ES_0.5561938424496837 b/archive/ES_0.5561938424496837
new file mode 100644
index 0000000..db140a1
--- /dev/null
+++ b/archive/ES_0.5561938424496837
@@ -0,0 +1,22 @@
+archive/ES_0.5561938424496837---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T22:11:45.639
+Launch V∞: [8.08167560450891, -5.7227068323935475, 0.08545705794820577] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.591682274959652e-6, -4.017620824949709e-6, 3.1523118538749e-6] km/s
+ V∞_out: [-4.172854223149595e-6, -5.448334253686599e-6, 2.5197687711517505e-7] km/s
+ time of flight: 1.8435769892530313e8 seconds
+ arrival date: 2030-03-17T16:40:03.639
+ thrust profile: [0.22156120247374733 -0.010787403429675869 -0.07872440322313176; 0.047633059225183 0.023338474629914095 -0.05798335212722743; 0.04677333247823071 0.03649636743711749 -0.10104865579807687; 0.042430779910364085 0.04221763647952102 -0.13342136958718329; 0.03613689543457661 0.04238450081415168 -0.14992415380171076; 0.022561579287247523 0.03020532541892673 -0.11771652515743077; 0.012059548405890857 0.01797942738514685 -0.07650761987366188; 0.004673669786334387 0.007547053795668128 -0.034988495468994366; 0.004254127253875417 0.007516193686084113 -0.03844846249368848; 0.0005757440359198045 0.0011147327633809904 -0.006162805425979033; 0.0012997943349540523 0.002148424312998176 -0.0108301417128356; -0.0005051984627676864 -6.906149533262342e-5 -0.0009377697039247837; 0.0002573174717377667 -6.046325672607884e-5 -0.000876407044013612; -0.0007100491411729331 -0.0003698258071045472 -0.0009755556960248295; -0.0009167039824503323 0.001374756575503857 -0.0016443666051496688; -0.0003253637601406058 -0.0015813719132574695 -0.00014809238558500962; -0.0007652958371285692 9.519268620761584e-5 -0.00015795068391920823; 0.0007110309755948892 -0.0011078902120798696 -0.0008322409928800468; 0.0003619370628440967 0.0001028750543753845 0.00021583025097960935; -0.0007178242264271592 -0.0003489902512637355 -0.0029971611101825262] %
+
+Mass Used: 76.81690050501447 kg
+Launch C3: 98.0701569747914 km²/s²
+||V∞_in||: 6.867451727630012e-6 km/s
diff --git a/archive/ES_0.5561948554952668 b/archive/ES_0.5561948554952668
new file mode 100644
index 0000000..5676175
--- /dev/null
+++ b/archive/ES_0.5561948554952668
@@ -0,0 +1,22 @@
+archive/ES_0.5561948554952668---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:19:51.086
+Launch V∞: [8.027257771426303, -5.751029742465006, 0.1332415757372591] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.996704513595591e-9, -2.8872595064365186e-9, -1.698222051698766e-9] km/s
+ V∞_out: [-3.763168813343039e-9, 3.5323913902041604e-9, -1.3096993558089484e-9] km/s
+ time of flight: 1.8566238283265916e8 seconds
+ arrival date: 2030-04-02T16:12:53.086
+ thrust profile: [0.27011754470687466 -0.006788958430169067 -0.09578769835213245; 0.06747294728421041 0.03511777475448707 -0.0832653851106804; 0.03154083920002875 0.026401029320391782 -0.07186440392301507; 0.03672728710830956 0.03914617170684921 -0.12110595144850904; 0.023936028510890498 0.030436904958904675 -0.10439172603420367; 0.022780991713095576 0.03365951098157784 -0.12387430576467613; 0.010174497362932635 0.0173773577030187 -0.0711691767840183; 0.005848639306299848 0.010802316391505064 -0.048532454539923255; 0.00480814153615586 0.007486704052793657 -0.04013851328129602; 0.003415466018552759 0.007740631446456661 -0.03404779727895638; 0.0002969032935140123 0.0005399420346092684 -0.002904757101885378; 0.0014217940840119702 0.0035854264794126364 -0.019904284203254016; 1.4722210025941665e-5 1.5206434210977642e-5 -0.0002680635990710089; 4.0161696444535055e-5 1.3549201179789951e-6 3.9094005441680556e-5; 0.00010710897230466654 -1.7092843794915374e-5 -1.9145966940746148e-5; 2.4042287697298816e-5 -7.506572619830177e-5 -0.0001261706526671556; 1.3079608336918317e-6 0.0002093422883720336 -0.00012193093537209886; -5.54742825427106e-5 2.5849767443424473e-5 -0.0001337513594711011; -0.00019794414385452915 -0.00032359234100760197 -0.000631925222085503; 2.231779451480098e-6 0.00011838883407374892 0.00011126627900560291] %
+
+Mass Used: 79.97504289779272 kg
+Launch C3: 97.52896374514604 km²/s²
+||V∞_in||: 5.21477444990475e-9 km/s
diff --git a/archive/ES_0.5562020916383685 b/archive/ES_0.5562020916383685
new file mode 100644
index 0000000..526c1d7
--- /dev/null
+++ b/archive/ES_0.5562020916383685
@@ -0,0 +1,22 @@
+archive/ES_0.5562020916383685---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:41:53.166
+Launch V∞: [7.935724665466227, -5.656935627619406, 0.1061141911262979] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9884631857575654e-6, -6.5130306262571246e-6, -2.0009288723121455e-5] km/s
+ V∞_out: [-1.903239302969869e-5, -2.1197570399444525e-6, 8.762895756363906e-6] km/s
+ time of flight: 1.874957778750094e8 seconds
+ arrival date: 2030-04-22T07:51:30.166
+ thrust profile: [0.411815291441716 0.0019266891296865639 -0.1209404991523113; 0.11509326937515059 0.06876826318532162 -0.12208040266768645; 0.03562776641473194 0.034709998675473065 -0.07160171282973812; 0.08538734108849168 0.11526650257348511 -0.2480095869135355; 0.018104609898845676 0.02927648289523184 -0.07520909755097234; 0.012661898330917375 0.0245367357514424 -0.06859488313839816; 0.008475894105964466 0.0194009289030977 -0.058243316592229866; 0.0020856945411607763 0.00584581787750294 -0.018527658464429466; 0.0026220306545456295 0.007459503976725075 -0.02734041943670308; 0.0005798436532745287 0.00041903511594556397 -0.001428527449533837; 0.0003841626685938299 0.0010775095799965698 -0.00558732143309185; -0.0005943953431658296 0.00016674644530877364 0.0001667438022250776; 0.00013442382949538094 0.00016350620901402067 -0.0009797905524080702; -0.00030641350922870847 0.00035861088095533026 -0.00022109337285728336; -0.00031666168704010133 -0.0014753355373796667 0.0010439310310423825; -8.941475687217367e-5 -0.00010056622194245472 0.00037245359257663535; -0.00014639511836445106 -1.1064428914317733e-5 -0.0006717895052917565; 0.0005012204158268666 -0.00010819607122515568 0.0011301889779361215; -0.0006689292593342476 -0.0024120405828170935 0.002076608983694658; 0.0007153805347624246 -0.0008661507873466079 0.0018049653902717589] %
+
+Mass Used: 94.80631676247958 kg
+Launch C3: 94.98790688267721 km²/s²
+||V∞_in||: 2.1136347579109116e-5 km/s
diff --git a/archive/ES_0.5562144942417704 b/archive/ES_0.5562144942417704
new file mode 100644
index 0000000..62d9c4b
--- /dev/null
+++ b/archive/ES_0.5562144942417704
@@ -0,0 +1,22 @@
+archive/ES_0.5562144942417704---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T03:09:29.085
+Launch V∞: [8.13226833585522, -5.720522122428139, -0.01727944396362524] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8516005925855352e-9, -3.5183752827035535e-9, -1.3650123281008072e-9] km/s
+ V∞_out: [-3.716129571324953e-10, -7.206457627365289e-10, -1.9413099317132367e-11] km/s
+ time of flight: 1.874957778285881e8 seconds
+ arrival date: 2030-04-25T05:19:06.085
+ thrust profile: [0.17297663392795634 -0.005813865671514518 -0.06554665234998883; 0.07698640028098168 0.038108240362766777 -0.10022283046622824; 0.023897152775425277 0.0183900515565031 -0.05719366117824951; 0.02233916174500774 0.021801076981441098 -0.07791887279132514; 0.017870877834223524 0.02043239074993292 -0.08241654878019193; 0.029544662287432494 0.03790808433097948 -0.16470659258155526; 0.01173997899678 0.016613189291630026 -0.08082770852486933; 0.005565377122945846 0.008361903144700974 -0.04490274347624029; 0.007081814336593071 0.01259173738655228 -0.06753527016615514; 0.002562778299436524 0.004287984924557698 -0.026559118548457473; 0.0009171940198085114 0.0016195574455995744 -0.010850701384827069; 0.0002406295784645114 0.00036524753497753717 -0.0038262581546032047; -0.00030303412254813276 0.0004985349199515131 -0.00019289451948708116; 5.0129451419451665e-5 -0.0001926177256225175 -6.33106357259528e-5; 0.00013078994567063975 -7.859142598146433e-5 -0.0005351998420609445; 0.0002899605348062295 0.00022451006383329117 -0.00013302381411019193; -4.495081350664495e-5 0.00012800086059366647 0.00030662013142715504; -0.00042733262001677186 0.0003479356679245188 0.00016202125667504405; 0.00028348095857510136 -0.00038036198325791266 -6.673108403826641e-5; -4.4970524822372814e-5 -0.00012639588656092137 -7.502688013723063e-5] %
+
+Mass Used: 72.24255867282545 kg
+Launch C3: 98.85846021872686 km²/s²
+||V∞_in||: 4.20364699282297e-9 km/s
diff --git a/archive/ES_0.5562197375115379 b/archive/ES_0.5562197375115379
new file mode 100644
index 0000000..966a695
--- /dev/null
+++ b/archive/ES_0.5562197375115379
@@ -0,0 +1,22 @@
+archive/ES_0.5562197375115379---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:28:50.579
+Launch V∞: [7.956671817294117, -5.6609425768938895, 0.11973664872421869] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.019878572294108564, 0.10427627679277217, 0.12006622688413132] km/s
+ V∞_out: [-0.02676632273548786, 0.02189633982126089, -0.1558156646357244] km/s
+ time of flight: 1.8749577787445086e8 seconds
+ arrival date: 2030-04-23T10:38:27.579
+ thrust profile: [0.4648787306776494 -0.0031563383720204694 -0.14915979745654925; 0.04630326927273945 0.02632964781177669 -0.056191469301530655; 0.029571421099710983 0.026564785473289658 -0.06526801184618221; 0.04177086330508981 0.050043352174588586 -0.13280570786583762; 0.022143421392631556 0.03242493024593908 -0.09813955069981342; 0.022863486293339588 0.038555045199634604 -0.1246412950611614; 0.007114131506312907 0.013926363434566557 -0.05247987051428653; 0.007714379756863674 0.018170153570327342 -0.07143606394022103; 0.0026707829113815657 0.008874632353841654 -0.035179848297938264; 0.0008901896187547407 0.005536157616539366 -0.023511368521118164; 3.12433084353212e-5 0.0007284117239459563 -0.005003592753462291; 0.0012524034857838747 0.0010040435889489489 -0.006807836453621714; 0.00018123887032720453 -0.0008460842030461877 6.41196324002581e-5; -2.1448239926234996e-5 -0.00015769869089187302 0.0004623395606891327; 0.00021693698034784946 0.0007395556466645929 -0.002229446767603577; -6.644170939234048e-5 7.879387051352798e-6 0.00022166914151218963; -0.0007977345736629328 -0.0010504694316545993 0.0038839663933359315; -2.9427167962621298e-5 -0.0002383630291785339 -0.0002911089991752324; -0.0003506301789865338 0.0015186669215371544 -0.00020858886800227423; -0.0004353193789490946 -0.00033088004581315647 0.00041390605859531346] %
+
+Mass Used: 92.60249465977631 kg
+Launch C3: 95.3692341320602 km²/s²
+||V∞_in||: 0.16026415187560392 km/s
diff --git a/archive/ES_0.5562220537045965 b/archive/ES_0.5562220537045965
new file mode 100644
index 0000000..de15859
--- /dev/null
+++ b/archive/ES_0.5562220537045965
@@ -0,0 +1,22 @@
+archive/ES_0.5562220537045965---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:10:33.051
+Launch V∞: [8.045164437683578, -5.777964254959389, 0.04372429826548816] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.128125857281559e-8, -3.582147337412846e-7, 6.559515324281963e-8] km/s
+ V∞_out: [-5.599925458845692e-8, 2.118411329356043e-7, 2.9134652447163585e-7] km/s
+ time of flight: 1.8413400555543283e8 seconds
+ arrival date: 2030-03-15T22:30:38.051
+ thrust profile: [0.24095170232792676 -0.014805279136572131 -0.0900973169178653; 0.04173220072204486 0.018399110732672492 -0.05455053440346438; 0.0323959673912624 0.021946130299743988 -0.07584726907556752; 0.04728611825482717 0.04232477138512754 -0.1552631054688613; 0.020943526193409726 0.02167153116696021 -0.09167323073023946; 0.01543988181929244 0.01716202460759593 -0.08275271298757393; 0.026200737200073765 0.03375256695682178 -0.163514316874026; 0.009681242379791993 0.013323669035190762 -0.07649069908352486; 0.000779951070194407 0.0009611999048348986 -0.005878722181700076; 0.0010895632415221445 0.0016042759295462803 -0.011115758764907608; -7.419073643775475e-5 0.0006974900857695035 -0.006833204131912234; 6.498709022141998e-5 0.00015418177687738185 -0.0009617220794172908; 0.00040470167936263173 0.0009299858834650126 -0.004045335309101823; -0.0009732003952138246 0.0002922892620210598 0.00044136416150637693; -0.00021332723198969365 -0.00043731713070828236 0.00044391638920447793; 7.089302070753496e-5 -0.00010006535245239749 0.00040546531789413314; 0.000378761560292466 0.00014321748404199774 0.0005282753546669299; -1.58942881672127e-5 4.656071512661858e-5 0.000533334805037912; 8.216218161112965e-5 6.566837148102434e-5 0.00021861832904864113; 1.2212094270325173e-5 -0.00033554658052710625 -0.00020816456995118417] %
+
+Mass Used: 76.60891679993756 kg
+Launch C3: 98.11145357521572 km²/s²
+||V∞_in||: 3.6650329044586224e-7 km/s
diff --git a/archive/ES_0.55622458679228 b/archive/ES_0.55622458679228
new file mode 100644
index 0000000..90e3d2c
--- /dev/null
+++ b/archive/ES_0.55622458679228
@@ -0,0 +1,22 @@
+archive/ES_0.55622458679228---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:12:54.063
+Launch V∞: [7.791072820890714, -5.673967766846109, 0.16264909596831953] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.794065398150124e-7, 3.065917402427462e-6, -7.378483898997969e-5] km/s
+ V∞_out: [-3.3345907167243076e-6, 7.377744482158675e-5, -6.238905007499991e-7] km/s
+ time of flight: 1.874957778722758e8 seconds
+ arrival date: 2030-04-23T19:22:31.063
+ thrust profile: [0.7043964905226117 -0.024865909037818254 -0.28044430930469916; 0.053101312331490104 0.025827479218780723 -0.07156377989356918; 0.020269752347601675 0.015364619412377427 -0.04920166842153996; 0.02064464686184358 0.020584148331658555 -0.07088873568651183; 0.026466181501567217 0.030542393814944047 -0.12416931389326653; 0.01504454348050522 0.01945912718451589 -0.08797436724052599; 0.010425656616628651 0.014989307295612382 -0.07650601161884615; 0.011852577821654069 0.015233565064559092 -0.08059230439623605; 0.0036522692089506247 0.005686633224643127 -0.03421656393286802; 0.001989243593622041 0.003104108094302863 -0.020292548335601485; 0.0004490641039262389 0.0006636256564858003 -0.004900037590447789; 0.00013464869228578443 0.00021366044803509658 -0.0014626257581353162; 4.060066641916758e-5 1.8458411974688405e-5 -0.00015009887087472708; -1.4702689650468529e-5 0.00010268922906498748 -0.00043859507577945656; 0.00010026420466771866 1.7317523486680528e-5 -0.00031995724306473734; -0.00019810485120764799 0.0002896276529254302 -0.0003212216154656995; 3.502688899805606e-5 -4.7938853885433255e-5 -0.00013309751006694673; -0.00016127505392672772 2.5047222342183577e-5 -0.0005681531629119806; -0.0003826120494029358 4.9553332602014864e-5 0.00045677788256457373; 4.107898458077866e-5 -2.0847311880247955e-5 -0.00012381540066078417] %
+
+Mass Used: 106.88846414403542 kg
+Launch C3: 92.92118064804993 km²/s²
+||V∞_in||: 7.385006530075754e-5 km/s
diff --git a/archive/ES_0.5562292946760028 b/archive/ES_0.5562292946760028
new file mode 100644
index 0000000..3dc4734
--- /dev/null
+++ b/archive/ES_0.5562292946760028
@@ -0,0 +1,22 @@
+archive/ES_0.5562292946760028---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T06:21:03.694
+Launch V∞: [8.072829769562393, -5.6686225664550784, 0.039825828515544295] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0743702849138356e-9, 1.792613538281328e-9, 6.453697929980482e-10] km/s
+ V∞_out: [1.8149995455872945e-9, -1.682836675262756e-9, -1.5171865470949052e-9] km/s
+ time of flight: 1.874957778749373e8 seconds
+ arrival date: 2030-04-24T08:30:40.694
+ thrust profile: [0.3200829367496012 -0.006131089532859198 -0.10762860900789813; 0.03702979533824831 0.01975550070418427 -0.04968277281245009; 0.029404150372518513 0.02411417719225704 -0.06839709166635681; 0.023685353226410223 0.02506274372566499 -0.08148044613527004; 0.031055800598294273 0.039231006200855845 -0.14024055586308357; 0.019025538828337994 0.02718734055455895 -0.10750321547114701; 0.011119607733655163 0.016009657790216906 -0.07090600964496051; 0.01353054230493389 0.025397411892784428 -0.1157273548462994; 0.003172554062577975 0.005210932779193469 -0.02892624247428481; 0.001348828095487573 0.0028572186716521604 -0.015176071016053033; 0.0004993859783163988 0.001424990405302918 -0.007475099618249152; -5.0938001343614855e-5 -7.630839548662384e-5 -0.00037154844127085685; 0.0003005923178437805 -0.0005767770210878797 0.0006648354902506982; 0.0002518457586671541 -6.846475193022649e-5 0.0007169453281812637; 0.0012698017698899407 0.0003896392001396768 -6.12513662651853e-5; -0.0009453423791256094 0.00044940072416309746 1.492154427134532e-5; -0.00024058804450514438 -6.712924519445373e-5 0.0006184526648229984; -0.00031115139205516125 -0.0017723935470692236 2.282486336357498e-5; 0.00019783116764195358 0.0003094490424907458 0.0005987415514312842; -0.0024550432358699504 -0.00434514613780464 0.0013777441105501235] %
+
+Mass Used: 81.31906153774116 kg
+Launch C3: 97.3054483858735 km²/s²
+||V∞_in||: 2.8165541972909656e-9 km/s
diff --git a/archive/ES_0.5562316837349265 b/archive/ES_0.5562316837349265
new file mode 100644
index 0000000..0eb9ef9
--- /dev/null
+++ b/archive/ES_0.5562316837349265
@@ -0,0 +1,22 @@
+archive/ES_0.5562316837349265---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T12:12:35.638
+Launch V∞: [7.842473500518278, -5.6823216895560735, 0.07110415368837396] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012492169707333443, -0.07278861243118376, -0.08892540397053275] km/s
+ V∞_out: [0.04686139709754182, -0.04200028633149332, 0.09770317455579101] km/s
+ time of flight: 1.8749577787412393e8 seconds
+ arrival date: 2030-04-22T14:22:12.638
+ thrust profile: [0.5588734623223511 0.002041695520075867 -0.14889558420357762; 0.07652499490644163 0.04809624476691515 -0.08169679483743598; 0.0453656544225105 0.046890354543532915 -0.08932452102970183; 0.01534861614558179 0.02115512946392221 -0.04636046675511737; 0.028559966069613137 0.051598987928369415 -0.12095594649244419; 0.019123377438297173 0.04119882109434367 -0.1049776522085689; 0.01980988193655218 0.045184136374812826 -0.1181670820284998; 0.007748751757307355 0.019988911692728664 -0.06046091107545968; 0.004372687909475424 0.013820454268136396 -0.04519326450864582; 0.00027631859193087184 0.0011754171374268858 -0.0037291391489465953; 0.0003967969567222399 0.0009332625274108937 -0.00357958565834821; 0.00019714464580817948 0.00044544596172300715 -0.0018535511315365774; 2.8881740524611802e-5 8.102228609407618e-5 -7.462444060710502e-6; 2.3342449347446507e-5 4.2432968828922174e-5 -9.750262755083786e-5; 3.511743019789995e-5 -0.0001468081228174993 2.0655039546893742e-5; 6.919033731682827e-5 -0.00010076780436466472 -0.0001109007297710204; -4.2663931995505e-5 2.479608141355966e-6 9.371879877209289e-5; -5.260588282412993e-5 -0.0001069136493668413 1.779141302320489e-6; -0.0001542438802566449 3.004464768117509e-5 8.990164996230441e-5; -7.827394078823842e-5 7.37359769143997e-5 -9.788963418734588e-5] %
+
+Mass Used: 101.78064491223267 kg
+Launch C3: 93.79822619060255 km²/s²
+||V∞_in||: 0.11559396123922884 km/s
diff --git a/archive/ES_0.5562375018971242 b/archive/ES_0.5562375018971242
new file mode 100644
index 0000000..e52e70b
--- /dev/null
+++ b/archive/ES_0.5562375018971242
@@ -0,0 +1,22 @@
+archive/ES_0.5562375018971242---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T18:52:48.237
+Launch V∞: [8.04816467605246, -5.818455401404698, 0.08818879663096181] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.123582342591271e-6, -3.5862845476537174e-6, 2.7653330216419305e-6] km/s
+ V∞_out: [-7.190247503880072e-7, -6.0758171722829145e-6, 2.4026498147374915e-7] km/s
+ time of flight: 1.87495777874386e8 seconds
+ arrival date: 2030-04-24T21:02:25.237
+ thrust profile: [0.1317264535103792 0.004429638631719539 -0.044575429884413244; 0.10175618173007424 0.062496960175588846 -0.10874714941005367; 0.041085909266565794 0.04099186228564162 -0.08320865622467276; 0.040280655510543766 0.05358281233068253 -0.12090883890118204; 0.012332288474159488 0.01978190553155146 -0.05196296371560908; 0.03077095365978735 0.06209565931980983 -0.16101588305056386; 0.008985755746333124 0.02091775684994339 -0.06271185310342038; 0.00582731251144602 0.015509581380784444 -0.04962379993651034; 0.004634498565898775 0.017459722907080588 -0.05850062143790997; 0.001796448173657657 0.0073024523207256145 -0.02589591264295165; 0.000299131300211915 0.0006861978288537837 -0.00276426891563273; 2.2326644349929122e-5 0.00014068452776228388 -0.0005086897020760953; 8.010894147942075e-5 4.6604642820499436e-5 -0.00039762570833782457; 0.00010932940129589676 0.00011130726162606053 -0.00014664871525679106; 1.5495460026340182e-5 2.555268900259619e-5 -0.00012263366495981744; 4.454457723367194e-6 -0.00014469176909850685 3.080348687020906e-5; 8.643132423661866e-5 -3.429998732631972e-5 -0.0001443712324007921; 5.549974630634008e-7 0.00020815646321052325 -0.00021881213737864723; 1.8513731110559548e-5 -0.0002475052025021945 0.0004659445823905034; -0.00016909228470198196 0.00017656415463493077 0.00022335619336042673] %
+
+Mass Used: 73.57201369338054 kg
+Launch C3: 98.63515517484532 km²/s²
+||V∞_in||: 6.124739579235482e-6 km/s
diff --git a/archive/ES_0.55625217697733 b/archive/ES_0.55625217697733
new file mode 100644
index 0000000..db8bc96
--- /dev/null
+++ b/archive/ES_0.55625217697733
@@ -0,0 +1,22 @@
+archive/ES_0.55625217697733---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:38:35.538
+Launch V∞: [8.046088344241051, -5.652378048605773, 0.1389634793281044] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.518516430731863e-6, 0.00031169171381448827, 5.4905548239158295e-6] km/s
+ V∞_out: [0.00030088188176591833, -4.535392637570595e-5, 6.75722955563407e-5] km/s
+ time of flight: 1.874957778755925e8 seconds
+ arrival date: 2030-04-23T20:48:12.538
+ thrust profile: [0.35319514102270644 -0.004960133774600993 -0.1187158422937653; 0.06142820549892926 0.03291412486502021 -0.07650552009369398; 0.027777431150982166 0.023855584277770115 -0.06313036343502194; 0.02291519838000222 0.02591431627370204 -0.07745377759214399; 0.03161090763678797 0.04247656457156513 -0.13900261498765867; 0.012250552672136874 0.018589694683673375 -0.06962898653202255; 0.013392409333781502 0.02477950520296157 -0.09456959073387206; 0.008834461746139444 0.01667613901311813 -0.07209393156421848; 0.005413964071452249 0.012276423214892347 -0.05626718998585247; 0.0023355561259112054 0.005328995150148281 -0.02639738040340673; 0.00048069253076436216 0.0012056126233005982 -0.007530219049521989; 6.726780866610227e-6 0.0005525289647180416 -0.0034436136316615988; 0.000421169366792315 0.00010339657939288627 -0.0025966952033424856; -0.0008869632711293561 -0.0005215055716657171 -0.0016667944135864234; -7.630100513272721e-5 -0.00023876847271766462 0.0003931147419731667; -0.0002953346786695379 -1.6317284786888692e-6 -8.244785333918461e-5; 0.0013329879738901602 -0.00042246079126344197 8.890488728601083e-5; 0.0005187811907525474 -0.0015275573077811145 5.088382405734433e-5; -0.0003021096381955473 -0.0008440131850113305 0.0007074008212547118; -0.0014045871672622619 -0.0009005179678093594 -0.00038431920156767026] %
+
+Mass Used: 84.82955424525699 kg
+Launch C3: 96.70822609627908 km²/s²
+||V∞_in||: 0.0003117728141509809 km/s
diff --git a/archive/ES_0.5562593755418843 b/archive/ES_0.5562593755418843
new file mode 100644
index 0000000..53c09a4
--- /dev/null
+++ b/archive/ES_0.5562593755418843
@@ -0,0 +1,22 @@
+archive/ES_0.5562593755418843---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:50:34.681
+Launch V∞: [8.094277052181504, -5.682616871235704, 0.1439085954112707] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.173607180433048e-7, 7.215618294064355e-6, -0.0001427991666944308] km/s
+ V∞_out: [-5.199898476874588e-6, 0.00014286739378125232, -1.510564433699304e-6] km/s
+ time of flight: 1.874957778552182e8 seconds
+ arrival date: 2030-04-23T17:00:11.681
+ thrust profile: [0.21741964407833736 0.002418058786083503 -0.0686045788900542; 0.07711241768779158 0.04687307968320896 -0.08842491928640214; 0.05087516691939036 0.05007705505084838 -0.10355395375056933; 0.0286464168300595 0.03635178084024177 -0.09115142895568606; 0.028203897937983346 0.043461667349034575 -0.11757564210263892; 0.014247775509320463 0.026273014916584146 -0.07747058114632009; 0.009327943294096485 0.019637790975345827 -0.06377536262561827; 0.005490955999304933 0.016357646540641327 -0.05356698538190621; 0.004850785392924953 0.012829684886172688 -0.04791418004177885; 0.00603645543709881 0.01854597844005935 -0.06815333262363722; 0.00011364514437787676 0.0006717742226719169 -0.0024617046710780034; 1.543871115319964e-5 7.870323525741005e-5 -0.0007657840665959195; 9.483564476080094e-5 0.00022170389627914318 -0.0015355680253119751; 0.00023032836935371972 -0.00018530822652799094 -0.0004978946009415081; -0.0004188666287663404 0.0012624424837672623 -0.0010973815021602562; -0.0002891921407696384 0.000332493540999302 -0.0009252021316323256; 5.6287295929559325e-5 -0.00015457143832811848 -7.618707397726704e-5; 0.0003196977695431987 0.0003514166630894811 -0.000944903844840935; 0.00012520403573604972 8.53716107528959e-5 -0.00021269167381410625; 0.00043335484389051535 6.294188014377986e-5 0.0005718752619689181] %
+
+Mass Used: 78.29330787727667 kg
+Launch C3: 97.83016518655799 km²/s²
+||V∞_in||: 0.00014298429531482286 km/s
diff --git a/archive/ES_0.5562670349024289 b/archive/ES_0.5562670349024289
new file mode 100644
index 0000000..a11789a
--- /dev/null
+++ b/archive/ES_0.5562670349024289
@@ -0,0 +1,22 @@
+archive/ES_0.5562670349024289---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:21:26.140
+Launch V∞: [8.097259450198298, -5.647371772873598, 0.19212414726284108] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.808337731049971e-7, 8.042929174659176e-6, -0.00016372307953177432] km/s
+ V∞_out: [-6.6206995315789225e-6, 0.00016374352878456837, -1.8403940251027962e-6] km/s
+ time of flight: 1.8749577786700535e8 seconds
+ arrival date: 2030-04-23T10:31:03.140
+ thrust profile: [0.262128801603767 0.004098368581842202 -0.08166278598378517; 0.06497506255291106 0.0389617230467301 -0.07749408618008023; 0.04904844275740915 0.04763840085965942 -0.10658174272329574; 0.03383687873451126 0.0433258682134567 -0.1103679711601282; 0.01328206016659131 0.02016491559114037 -0.058793306770411495; 0.017969816335666473 0.03563099882241178 -0.1098379229217318; 0.009952205365695087 0.02140561923811605 -0.07162566239202624; 0.00873473249809182 0.01995633982022239 -0.06892770725929932; 0.007096886794780024 0.021065785045555254 -0.07671425902910807; 0.0013173662823713298 0.003230919392837012 -0.013867343683590355; 0.0006365060776652373 0.0016713579442264696 -0.0075576210196731134; -0.0005004416057684938 0.0009810119058860658 -0.00254531005101241; -0.0002806789530153028 0.0009896566762914358 -0.002316337774532641; 8.879576553635575e-5 -0.000204290706902386 -0.0006929487561675222; -0.00037044492762816975 -0.0003843272678596398 4.097625827126101e-5; -0.000569648133075653 0.0002444510087488285 0.0008080733508224896; 0.00019236403038164145 -9.713368585782391e-5 0.000531457824877234; -0.0007961667673533979 -0.0007765860020240311 -0.00015568063918828807; 0.0005772666480023479 0.00036784719882110284 0.0002674872163210103; 0.0014653589797821408 0.0001324111307050866 0.0013365655153756235] %
+
+Mass Used: 80.25544769462022 kg
+Launch C3: 97.4953302328366 km²/s²
+||V∞_in||: 0.0001639234501710074 km/s
diff --git a/archive/ES_0.5562796315062899 b/archive/ES_0.5562796315062899
new file mode 100644
index 0000000..74f6159
--- /dev/null
+++ b/archive/ES_0.5562796315062899
@@ -0,0 +1,22 @@
+archive/ES_0.5562796315062899---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:28:18.202
+Launch V∞: [8.12992981265982, -5.577510070455327, 0.00200039813095532] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0001331933479727936, -0.00010624652418647584, -8.770588811038806e-5] km/s
+ V∞_out: [-1.726109507708867e-5, 0.00011991753471927823, -0.0001484234307516442] km/s
+ time of flight: 1.8749577787450722e8 seconds
+ arrival date: 2030-04-23T01:37:55.202
+ thrust profile: [0.29159384413626654 -0.006702234063907008 -0.10241623437870487; 0.06436542491230056 0.03398931442440642 -0.07876259820003126; 0.048227783496674045 0.040585567236088235 -0.10660192394459723; 0.03798873455970438 0.04126462865014483 -0.1238858791941057; 0.027623846635882996 0.0356245462980573 -0.12031089272051466; 0.01650093683011378 0.024515605415448335 -0.09114922718790132; 0.011385611327214992 0.019145282633977405 -0.07668963748033499; 0.004536054132294971 0.008684768551741743 -0.03703602864809354; 0.004784696528348455 0.009901477741050988 -0.04497458110151557; 0.0003115077718753826 0.0008479342335226303 -0.005007573173389734; 0.00024091731630583168 0.0009462544855744103 -0.007318802563757665; 0.0005099284420298474 0.0011568832342178292 -0.006183995426355499; 0.00018095917862621697 2.734860630861395e-6 -0.0017166112698059782; 0.0007105536608930116 -0.0011083025908537852 0.00010270541166066674; -2.9228544231501728e-5 -0.00015306860754560618 -0.001572977822292371; -0.0015501979727764023 0.0003776370597886542 -0.00040177219694325673; 0.00030674504446821733 0.00014677024819406334 0.00018896848379033535; 0.003511238589161673 -0.0023466797133891394 -0.0008645207300046187; -0.00042750161086696264 -0.000431974882005667 -0.0009845239734611842; -0.0005881043606433692 -6.35060646226458e-5 0.0019080622221690387] %
+
+Mass Used: 81.96734557001537 kg
+Launch C3: 97.2043813463982 km²/s²
+||V∞_in||: 0.00019162754148384045 km/s
diff --git a/archive/ES_0.5562916957769931 b/archive/ES_0.5562916957769931
new file mode 100644
index 0000000..954caed
--- /dev/null
+++ b/archive/ES_0.5562916957769931
@@ -0,0 +1,22 @@
+archive/ES_0.5562916957769931---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T04:00:53.891
+Launch V∞: [8.066902753092151, -5.677935973437284, 0.17984326486712762] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.844763423693337e-10, -8.583289286472929e-10, -1.2016495499857555e-9] km/s
+ V∞_out: [1.0556057902101706e-9, -8.156340402830587e-10, 3.7679198138379746e-10] km/s
+ time of flight: 1.8749577787493923e8 seconds
+ arrival date: 2030-04-23T06:10:30.891
+ thrust profile: [0.24751278535891508 0.005629043344501724 -0.06923296175479231; 0.0453014457554187 0.027011861801084964 -0.051077483914084454; 0.11741861175579996 0.11031995647848629 -0.2137602227308119; 0.019791146466582425 0.025251442219654714 -0.061211954233691614; 0.011625892841174044 0.021623875216749553 -0.05044411762156397; 0.013183820976948339 0.026469217006948556 -0.07649869532073898; 0.019783610271697137 0.0507165117584335 -0.1345047571399123; 0.004946975687093556 0.012710442332185237 -0.03929121601968355; 0.002764672854573372 0.008743849433555793 -0.03082111577119357; 0.0038791319504123405 0.011008843864292241 -0.03944366778713176; 0.0004254836661480858 0.0018739647696677472 -0.009136194255795196; 7.098834015006566e-6 8.93110805806936e-5 -0.0013333732881500135; 0.0007128173477872063 0.0013059446062094883 -0.006077127507145822; 6.232256233593506e-5 0.000282720274717117 -0.0006483339877994086; 0.0002715774740429018 -0.00014988232744884966 -0.0010680594312519305; -0.00046108267438821945 0.0005201826131686167 -0.00039624774576229205; -0.00019744232199927532 0.00012986706622034644 -0.0004248925779197092; -0.0002857916039910297 0.00014508865366269865 -0.0005008067762013025; -0.00016234223443850057 0.0004735116217128469 0.0004608222232512553; 2.10196375510306e-5 0.00018955573479628057 -0.0002262686915826176] %
+
+Mass Used: 81.15402522022623 kg
+Launch C3: 97.34622054621698 km²/s²
+||V∞_in||: 1.5881759302807774e-9 km/s
diff --git a/archive/ES_0.5563001108588564 b/archive/ES_0.5563001108588564
new file mode 100644
index 0000000..1f29e8b
--- /dev/null
+++ b/archive/ES_0.5563001108588564
@@ -0,0 +1,22 @@
+archive/ES_0.5563001108588564---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:18:19.218
+Launch V∞: [8.104067845338282, -5.646184900786559, 0.13498815687918383] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.224712470141917e-6, -4.8323445274698015e-6, -4.7222298699825655e-7] km/s
+ V∞_out: [4.2042883452361186e-7, -2.045334061034309e-6, -5.441838382339706e-6] km/s
+ time of flight: 1.8749577787493488e8 seconds
+ arrival date: 2030-04-23T20:27:56.218
+ thrust profile: [0.2581144174126622 -0.005121005173709089 -0.0902606842342302; 0.06686591260093645 0.035341196617427274 -0.08270603354301473; 0.04730493867524743 0.039733062107686436 -0.1050937944441249; 0.037169841293372904 0.03999802794819754 -0.12162057509978359; 0.02851983934890735 0.03663175766638757 -0.1232848694343891; 0.022201292241992708 0.03209726665005207 -0.12221617083582795; 0.007779923573999654 0.010763775800055343 -0.04572230707018219; 0.003340442622177863 0.0061398661560276135 -0.03166040761477285; 0.002044211597326514 0.004099695533728453 -0.01890370757251553; 0.001881734952414254 0.004458191245429814 -0.021354139926800724; 0.0010440365071825194 0.0033394301743804463 -0.023618039287240284; 0.0001303362810128667 0.00032869505226932775 -0.0014149722113793609; 0.00022479298285744934 -3.819411474763481e-5 -0.0012653169667333518; -0.0006437487327983245 -0.00021795242986417398 -0.002880897761026361; -0.0002535873059604251 -0.0007586345014018914 -0.0028130930936190682; 0.0022713147866162595 0.0032135008135703667 -0.00038197469402130905; 0.00034657073041199677 -0.00045835342910864217 -0.003115177906925708; -0.00025694229640513657 -0.000493175378614492 0.0014529396337802669; 7.743586953980455e-5 0.00037089801777648464 0.001989540150271113; -0.002951386471654754 -0.0019578932957419666 -0.001772721316064423] %
+
+Mass Used: 79.83780462908635 kg
+Launch C3: 97.57354137821362 km²/s²
+||V∞_in||: 5.828663542932091e-6 km/s
diff --git a/archive/ES_0.556320485438071 b/archive/ES_0.556320485438071
new file mode 100644
index 0000000..bead104
--- /dev/null
+++ b/archive/ES_0.556320485438071
@@ -0,0 +1,22 @@
+archive/ES_0.556320485438071---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:19:23.232
+Launch V∞: [8.112420802695114, -5.632133223887257, 0.284283991766965] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00012087515272960752, 0.0007096821500533491, 0.000965690754317985] km/s
+ V∞_out: [-0.00018694338247535866, 0.000159038742821661, -0.0010881476917271795] km/s
+ time of flight: 1.8749577786354506e8 seconds
+ arrival date: 2030-04-24T00:29:00.232
+ thrust profile: [0.2969107835847222 -0.006012666513507273 -0.10369906772533086; 0.023789197322200122 0.012198961004706813 -0.02899138395802826; 0.03571605148080903 0.02849655033672604 -0.07907690594367046; 0.04151570772328668 0.042292495628158996 -0.13418108670664947; 0.03390956662432094 0.040769368828844854 -0.14516162240515204; 0.023639964348217378 0.03215693160362289 -0.12673072985813638; 0.008131163887585162 0.012267226205647817 -0.05235582959323779; 0.005368758788128612 0.008901982331745774 -0.04030526392413871; 0.0018451971934466014 0.0036065793574082943 -0.014590545958412469; 0.0036275280961146263 0.006929659674730249 -0.03504062727962855; 0.000659922571744193 0.0007632396975893602 -0.007753969921905335; 0.0003101284306357475 0.0008961124865239508 -0.007405334677077284; 0.0002529587477766396 0.0006694759114061837 -0.004241658369666919; -0.00024292230483459313 -0.000915068917999462 0.0005313298837240094; 0.0004154069677126133 -6.347742718918088e-5 -0.0013621344956081245; -0.002191056277436247 -0.0020461051037112387 -0.0025534007220042298; -0.002087154297123176 -0.0035041089894319215 -0.0018639900263310593; -0.001261738369307909 0.0004875664811382959 0.0005097952413634275; 2.3549698266360844e-5 -2.8993390791787546e-5 -0.0011655573717432636; 0.002035166266145119 0.006640244219905859 -0.0007637101894839686] %
+
+Mass Used: 79.63073864680746 kg
+Launch C3: 97.61311331959007 km²/s²
+||V∞_in||: 0.001204499144718247 km/s
diff --git a/archive/ES_0.5563232968515609 b/archive/ES_0.5563232968515609
new file mode 100644
index 0000000..98721c2
--- /dev/null
+++ b/archive/ES_0.5563232968515609
@@ -0,0 +1,22 @@
+archive/ES_0.5563232968515609---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T12:47:22.400
+Launch V∞: [8.023862113072175, -5.753969003180376, 0.2653697215186752] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.084224980658193e-6, 4.631395226825892e-5, -0.0008947202681808113] km/s
+ V∞_out: [-3.3409629785642654e-5, 0.0008982359397937342, -9.455413607753698e-6] km/s
+ time of flight: 1.8749577787319884e8 seconds
+ arrival date: 2030-04-24T14:56:59.400
+ thrust profile: [0.26346742603430423 0.0016081518837608964 -0.08770278731728298; 0.057779409479677586 0.03265639662472012 -0.06917718997849694; 0.054763546085235065 0.049795357146214136 -0.11627984129633956; 0.04162963225541715 0.04946028068412449 -0.13108773467559084; 0.022691574483548207 0.032345800785809856 -0.09845167798921046; 0.014734540525574796 0.02447730996307944 -0.08406614483867363; 0.008058553866641085 0.015286966812605898 -0.059064795728698105; 0.005580041505216085 0.012525216280103049 -0.04888072674464517; 0.006505630516411324 0.01593518705695376 -0.058387386765680546; 0.0009158461015144536 0.005068469973340566 -0.025965393635823328; -4.745689331933363e-5 0.0006237048813201249 -0.005770698093560796; 0.0003381306719239622 0.0007137599044717588 -0.0028105817716917968; -1.536417472796644e-5 -0.0004642656481724161 -0.0017601902120920254; -0.0003647044642231094 -0.00042597897683426705 8.725659865287702e-5; 4.2816350445997896e-5 -0.00033536673014033516 -0.0001528371006601052; -0.0004969253460600034 0.00013323068151578372 -0.0004222749741067323; 9.763432019851972e-5 -0.001302681024042177 0.0012470343478480695; -0.0008216517385674688 0.001309509952665346 0.002741380627675141; -0.0008802454035230702 8.944001480018309e-5 0.0006159285891895942; -0.00012761977302881092 -0.0003006546299085162 -0.0003162223132190657] %
+
+Mass Used: 79.9383420620029 kg
+Launch C3: 97.56094358825455 km²/s²
+||V∞_in||: 0.0008959325810639455 km/s
diff --git a/archive/ES_0.5563357498497346 b/archive/ES_0.5563357498497346
new file mode 100644
index 0000000..adec7a8
--- /dev/null
+++ b/archive/ES_0.5563357498497346
@@ -0,0 +1,22 @@
+archive/ES_0.5563357498497346---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T04:10:23.878
+Launch V∞: [8.128153894799135, -5.540876369370793, 0.15142448350448556] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002056282823173879, -0.0014248091865356409, -8.772024414116838e-5] km/s
+ V∞_out: [0.0017981952211316517, 0.0008347662892617659, -0.0014996489104877604] km/s
+ time of flight: 1.8749577787427032e8 seconds
+ arrival date: 2030-04-22T06:20:00.878
+ thrust profile: [0.3401062331689023 0.0008207511289443208 -0.1033772478259673; 0.057522963613330376 0.03387194567405578 -0.06687502247599024; 0.03550338912707878 0.03373614417870392 -0.07571009851283757; 0.03104962360596151 0.03916663268848533 -0.09843905112437967; 0.021586756679002474 0.033472341333313976 -0.09334946203603812; 0.01521048959565544 0.02780301335809527 -0.08357835568735326; 0.0228541027009061 0.04881581586200314 -0.15325460887463888; 0.009079755483040011 0.021348459332847226 -0.07446316880407758; 0.0026012405033822715 0.006780978757683788 -0.026231402649214555; 0.0010874725071562009 0.003066156652317066 -0.012383263104317546; 0.00019158419417024253 0.00048770639966739767 -0.0018325970087056803; 8.738668876609618e-5 0.0004420925665048226 -5.0473521288643154e-5; 4.317744400203608e-5 -0.00010891314469866636 -0.0005036735853198013; -3.827077315114876e-5 -0.00016167141744813222 -0.0007716092487322576; 7.800251812988701e-5 0.00012857034293181158 -0.000562204555660379; -0.0005884046946973078 6.299549946597687e-5 0.0006888456031900719; 8.555307200252561e-6 0.00016769604473925546 0.0001560423437926392; -0.0011454178114238336 -0.0002773016816337077 0.0008872551109111558; -0.00019955602758959336 -0.00035154165521138344 0.001223382590832669; -0.0009617956211076421 -3.404606662222909e-5 0.00035097048930621976] %
+
+Mass Used: 84.44347285238837 kg
+Launch C3: 96.79112605239462 km²/s²
+||V∞_in||: 0.0025032129570111447 km/s
diff --git a/archive/ES_0.5563367398217933 b/archive/ES_0.5563367398217933
new file mode 100644
index 0000000..e1f7ffd
--- /dev/null
+++ b/archive/ES_0.5563367398217933
@@ -0,0 +1,22 @@
+archive/ES_0.5563367398217933---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T20:57:06.638
+Launch V∞: [7.914707428432795, -5.816065815495599, 0.11887764695952768] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.144073723717656e-6, -2.1287971324352457e-5, 0.0004198339403643236] km/s
+ V∞_out: [1.716795295812701e-5, -0.0004348556109659098, 4.574140462881242e-6] km/s
+ time of flight: 1.8547440968231925e8 seconds
+ arrival date: 2030-03-30T13:37:15.638
+ thrust profile: [0.3021886145127397 0.009167228612621712 -0.08848183298406144; 0.08902144423199151 0.05637766266156552 -0.09232298087367086; 0.04742252227663238 0.04848788356184531 -0.08959893673563933; 0.03608977722939886 0.04979079906745624 -0.10220931277244714; 0.02435981489840355 0.04207675629712788 -0.09498030776713726; 0.028261451388329157 0.061651535985147256 -0.14549531383602973; 0.013038903616641985 0.032122405693714474 -0.0838083863061221; 0.010795842237732538 0.03135164942199987 -0.08601872191829545; 0.00204105173481929 0.006489025629436067 -0.019591879513196707; 0.00023758572718190902 0.0003077133654948414 -0.0006826604756272805; 0.0002218805742850732 0.0009223051725401595 -0.003129461779759877; 0.0002940527047313086 0.00011257611735154721 -0.00047736772033366926; 0.00011679430768212666 1.8154482509680854e-5 -0.0005081268099169485; -0.00018778403410202164 0.00023114518158042546 -0.0007789066421782223; -9.473560848148192e-6 0.0007642428844475191 -0.00032093486813433865; 0.00011025463622197149 0.00024662705553464456 -0.000843217145808478; -0.000710269151990514 -0.0001368514623607506 -0.0005224243037694596; -1.1652793526554744e-5 -0.0004252688100442612 -0.00025753571289121354; -0.0004939297667734108 1.4653762635387293e-5 8.147054268121831e-6; 0.00015021929979941836 0.00038236530558005677 0.00030784796855248944] %
+
+Mass Used: 86.24000479235337 kg
+Launch C3: 96.48334714281238 km²/s²
+||V∞_in||: 0.00042037877236734213 km/s
diff --git a/archive/ES_0.5563463052005911 b/archive/ES_0.5563463052005911
new file mode 100644
index 0000000..4e54fb5
--- /dev/null
+++ b/archive/ES_0.5563463052005911
@@ -0,0 +1,22 @@
+archive/ES_0.5563463052005911---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T04:52:46.553
+Launch V∞: [7.935073306386561, -5.670648111593541, 0.05054490190352387] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.7102527091732403e-7, 2.909063098183447e-6, 5.6408774671114975e-5] km/s
+ V∞_out: [-2.4809224274040262e-6, 5.63139185609536e-5, -8.643250289631941e-8] km/s
+ time of flight: 1.8749577787509483e8 seconds
+ arrival date: 2030-04-22T07:02:23.553
+ thrust profile: [0.4064897309275018 0.01160452574354589 -0.12022833514934482; 0.09495793018301489 0.061391850107288155 -0.10177514665276305; 0.07270657210195267 0.07952393710206006 -0.14126484663731265; 0.032696857276487204 0.04736156299791973 -0.09940689112549493; 0.027880882820734535 0.05091020824180222 -0.11625213564207187; 0.015006831340701939 0.03350651404676139 -0.08412376607275603; 0.007550380558749055 0.021131777827152802 -0.058519721081114244; 0.0035055107660401964 0.011489141857241498 -0.03352170610145313; 0.0042971173335260675 0.01648532319035591 -0.04961743567632555; 0.00035501329088569715 0.0011451505794553255 -0.004362633029200867; 0.0005942272197288058 0.002891933705852663 -0.010270264259300823; -8.243651548668195e-5 0.00018523639681398334 -0.00041334938145474786; 4.1500193528975356e-5 9.064500033359219e-5 -0.00040704299512358595; -0.00019756763518160341 0.00021043653094830097 1.171395829849156e-6; 0.00027951439946503356 0.00015021255231538718 -0.0007141548068395249; -0.00012457704470786605 0.00031664399023377174 -0.001097021064733945; -1.3785019728656186e-5 -0.0003916024482059737 0.0002614750171946094; -0.00031844869377841616 -0.00023600635425054912 -0.00011960070223435837; 7.537459940525364e-5 9.936613559532038e-5 -0.0007476940007510748; -5.05672628156861e-5 5.670775625682897e-5 -0.0003118632891768653] %
+
+Mass Used: 94.17956257361084 kg
+Launch C3: 95.12419317035638 km²/s²
+||V∞_in||: 5.648570060476968e-5 km/s
diff --git a/archive/ES_0.5563688414034799 b/archive/ES_0.5563688414034799
new file mode 100644
index 0000000..bf16a1f
--- /dev/null
+++ b/archive/ES_0.5563688414034799
@@ -0,0 +1,22 @@
+archive/ES_0.5563688414034799---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:34:30.577
+Launch V∞: [7.982171543574743, -5.767966830280234, 0.2718950876879564] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3581077101822798e-6, 2.170519075106689e-6, 1.7700309062819317e-7] km/s
+ V∞_out: [-1.5567873080152833e-7, 1.601904276245438e-6, 2.0122237684418567e-6] km/s
+ time of flight: 1.8533108131916425e8 seconds
+ arrival date: 2030-03-29T17:25:51.577
+ thrust profile: [0.32403869058426266 -0.010612028259953495 -0.1062657306004611; 0.04270305773166122 0.021855445365826624 -0.051300392792558734; 0.041420690277916526 0.034297965287149415 -0.08891509344527002; 0.03641709504289913 0.039269266024189085 -0.11452321194295136; 0.02723359440887181 0.035656816307398094 -0.11528423170252608; 0.02292881305584842 0.03241873457272673 -0.11727486404719319; 0.011318518758871065 0.018187992321586736 -0.0719235630788546; 0.004122231730822253 0.007137939796617302 -0.030678082247564936; 0.009646999128876486 0.019025802721688554 -0.08347107074834628; 0.002407283830972264 0.004808115731350414 -0.022589521572817996; 0.00029280781409511285 0.0009293010705391381 -0.004822765851401018; 0.0001550043049060419 0.00048241547770001397 -0.002097982991946756; 0.00032718336454856504 -0.0001752434654545094 -0.0016153724328138545; 0.00027286292588574694 0.0008654835600125036 -0.005174446976766829; -0.00011012804704344946 0.00016301030033199782 -0.0008491743335200628; 4.6086887104638315e-5 -4.875639849243805e-5 -0.00038095494121579603; 2.2062388786907446e-5 8.410688199001769e-5 -0.0005966545808886905; -7.002401281518589e-5 0.0011027485073213938 -0.00038885686580844114; -0.00039501811513144986 0.000713940475679574 -0.0001612663197291073; -0.00021656343321672152 -0.0001654894940412439 0.00020000876231436333] %
+
+Mass Used: 82.92280170836511 kg
+Launch C3: 97.05843084497624 km²/s²
+||V∞_in||: 2.5665033999491377e-6 km/s
diff --git a/archive/ES_0.556379476664724 b/archive/ES_0.556379476664724
new file mode 100644
index 0000000..3ccab74
--- /dev/null
+++ b/archive/ES_0.556379476664724
@@ -0,0 +1,22 @@
+archive/ES_0.556379476664724---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T08:02:53.723
+Launch V∞: [7.953607288584012, -5.726569936467895, -0.049838782534767284] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7514332746346832e-9, 1.7066557313156922e-8, -3.235300663004519e-9] km/s
+ V∞_out: [6.009779874527611e-9, 1.163420541354604e-8, 3.047072731192993e-10] km/s
+ time of flight: 1.8749577787542868e8 seconds
+ arrival date: 2030-04-24T10:12:30.723
+ thrust profile: [0.4298812924290394 -0.0064177943371909185 -0.12828780506147713; 0.02479541700709001 0.013805959977579194 -0.03148248110264898; 0.02415167155773564 0.021613481116200775 -0.05534701769507178; 0.04134149771479199 0.04902535820455649 -0.12883859739730044; 0.024294111719879524 0.034844102791797005 -0.11402998216931963; 0.01235736852506763 0.020205654767273536 -0.07065377269116206; 0.013208980959058664 0.02479052299764 -0.08971471734694081; 0.00885553321190949 0.019398727384319202 -0.07755100773097164; 0.00702613399149062 0.01641605706099377 -0.06944094919422043; 0.0022477436159855416 0.006170648401294449 -0.028756346078988443; 0.0008906710567866432 0.0023028976961963453 -0.011177436107058613; 8.032196597362396e-5 0.000435142556153088 -0.0008324466231360518; 5.3168308273066894e-5 8.501700242869608e-7 -0.0003469026396771801; 6.625381647879093e-5 0.00012048674542188424 -0.0007638537364698147; -4.3421695994378114e-5 0.00029148965324462227 -0.00042804830048383496; -2.4611012293565646e-7 -0.0004414244802838014 -0.0013085828466105106; 0.00031798316041778017 0.00025186339504227814 1.862766691567382e-5; 0.00038850942749870006 -9.23422746120679e-5 -0.0006326753775180054; 8.690821567747335e-5 0.00014318679657854662 -0.00018706482772424464; -0.0013320186687692738 0.00041274532693452145 -0.00024415369045794656] %
+
+Mass Used: 88.78297919414945 kg
+Launch C3: 96.05595604251917 km²/s²
+||V∞_in||: 1.758706723612764e-8 km/s
diff --git a/archive/ES_0.5563837240366725 b/archive/ES_0.5563837240366725
new file mode 100644
index 0000000..ca8a351
--- /dev/null
+++ b/archive/ES_0.5563837240366725
@@ -0,0 +1,22 @@
+archive/ES_0.5563837240366725---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T04:24:27.107
+Launch V∞: [8.032330976480676, -5.700321124346888, -0.026165881348433128] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.725707587352335e-7, -5.080851414585784e-6, 0.00010251004532585993] km/s
+ V∞_out: [4.047737139849744e-6, -0.00010254756030430121, 1.1295403741900243e-6] km/s
+ time of flight: 1.874957778741298e8 seconds
+ arrival date: 2030-04-24T06:34:04.107
+ thrust profile: [0.31328743777734747 -0.00538325566679614 -0.110275230138395; 0.05087608924088358 0.027638861492647243 -0.06493974188417692; 0.04922618164622671 0.04209816134015035 -0.11151617892323394; 0.03935372238859779 0.0429321489898381 -0.13005057085844213; 0.036373309903503785 0.047694331451678035 -0.16066694355932196; 0.015614122132635756 0.021135325497500322 -0.08329689608513387; 0.006807243269712739 0.010889357374181924 -0.04785090104015447; 0.00422823518471769 0.007723654880291505 -0.03842125448234989; 0.0021330591905422743 0.005455306679262272 -0.02593518057339993; 0.0010785850289117553 0.0020603966716626026 -0.01078579765169964; 0.0016816062731383051 0.002599399881049107 -0.015790786950261412; -0.0007098641736800671 -9.588398173617299e-5 -0.0024163933237217597; -0.00012899121799479654 -9.868664292895672e-5 -0.0011164758032075543; -0.0003313449873073018 -0.0004931847076799804 -0.0011769164632420108; -0.0001926912356411053 0.0006174828958284836 -0.0025394655330050492; -0.0017401028680774978 0.00102265650673161 0.001718808815746905; 1.908160091657632e-5 -0.0005550621824928263 0.0032028964461373807; -9.413563759096531e-5 -0.0024406908033213267 -0.0005740681248170864; 0.0011555327614157923 0.0036268168188669362 -0.0007282806312025722; 5.441050815552467e-6 0.000987348542914495 -0.0022631949277660598] %
+
+Mass Used: 83.20700685255815 kg
+Launch C3: 97.01268648975311 km²/s²
+||V∞_in||: 0.00010263808647491663 km/s
diff --git a/archive/ES_0.5563858221213411 b/archive/ES_0.5563858221213411
new file mode 100644
index 0000000..20edcd5
--- /dev/null
+++ b/archive/ES_0.5563858221213411
@@ -0,0 +1,22 @@
+archive/ES_0.5563858221213411---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T10:26:26.205
+Launch V∞: [7.965308015200673, -5.715309319106427, -0.04656264382124691] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0432457721677403e-6, 4.142347158997334e-10, -1.1280512285045085e-9] km/s
+ V∞_out: [-3.0417171000949335e-7, 9.818733400268896e-7, -1.6587975292428685e-7] km/s
+ time of flight: 1.8749577787627596e8 seconds
+ arrival date: 2030-04-24T12:36:03.205
+ thrust profile: [0.40157192214342435 -0.012473366106765154 -0.14203224141679124; 0.05665437627079589 0.026556714166603768 -0.07204709815706775; 0.04732231533611698 0.03711352868659208 -0.10813917134759668; 0.031377586153895715 0.030866944831256203 -0.10465366991413504; 0.023072491463478947 0.026714967227132756 -0.10171756795321887; 0.017182458398979677 0.022931746854506184 -0.09698241996188295; 0.014819977232607957 0.019412313954861152 -0.09195059251756364; 0.0055424168364568765 0.008275281394481615 -0.04233879627994707; 0.0030802021155194627 0.005387667465936223 -0.02886445645257164; 0.004235635020417118 0.0059569924101938575 -0.028073784462159822; 0.000723394500809361 0.001012061495277632 -0.006719718948093539; 0.00033972200318636934 0.000845541344782683 -0.003959210999568731; 8.648160847353524e-5 -0.000375411257053046 0.000433014292289957; 0.0009521627269362544 -0.0007521337703859552 -0.0003580738176626533; 0.00017270743690475464 -0.00057020744707071 -0.0005635659553563674; -0.0011242397701783252 0.0020498686785124535 0.0019198190466833255; 0.00024811308217484093 0.0012560099770099395 0.00010433009977453577; -0.0005329151371843089 0.0001211595147876014 0.0004581335573934519; 4.583733895264914e-5 -0.0005209013159474399 0.0007306663796634472; 0.0005276061520297137 -5.734619055339143e-5 0.00012155537166888195] %
+
+Mass Used: 88.45727306723848 kg
+Launch C3: 96.11306046988449 km²/s²
+||V∞_in||: 1.043246464281494e-6 km/s
diff --git a/archive/ES_0.5563966388063993 b/archive/ES_0.5563966388063993
new file mode 100644
index 0000000..16448f4
--- /dev/null
+++ b/archive/ES_0.5563966388063993
@@ -0,0 +1,22 @@
+archive/ES_0.5563966388063993---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T11:50:00.792
+Launch V∞: [8.040609189563137, -5.518391825003857, 0.3442662056401217] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007326936228913312, -0.004861191501926881, -0.0003335292787359413] km/s
+ V∞_out: [0.006178171993210259, 0.0032774666821061204, -0.005354041065952694] km/s
+ time of flight: 1.8749577778215215e8 seconds
+ arrival date: 2030-04-21T13:59:37.792
+ thrust profile: [0.4832146130871717 0.0021960688565287887 -0.13703088035839484; 0.065116061927048 0.03884516296853074 -0.07248330348361447; 0.027580734746131624 0.026540042661917635 -0.056614245000815425; 0.020395027051028868 0.026014181878272275 -0.06254809692330536; 0.01890256222259721 0.029808968103921373 -0.07853231909501936; 0.032832038913681146 0.06176399715490186 -0.16965817497318195; 0.026354183111224415 0.05758529846888205 -0.16837917257819016; 0.0014123697494541202 0.0033580771830993366 -0.01162903126311395; 0.00252575886627879 0.006914076140403246 -0.024536141263489495; 0.0009946321555998816 0.002963115112942538 -0.01133575798817308; -0.00030058217551388 5.9668376067011935e-5 -0.0007251159816416146; 0.00023456714597121922 0.0009253885430993807 -0.003847380475736117; 0.00017264419527801805 0.0009002179915384094 -0.0006486892159972909; -0.00017303695763611613 -0.0001388698874017246 -0.00021097603004723194; 2.8171370649751504e-5 -0.00016449941841181927 -0.00033485792677394376; -2.6975769491970677e-5 0.00018883655971543929 6.714211225803665e-5; 0.0003865320374203835 -2.5906049786575516e-5 0.0001044794320344748; -0.0004824535505037578 -0.0010343580629126332 0.0005932158894935927; 0.0004016791728949829 0.00028020351502304106 0.00031413063810689233; 2.2789655480578427e-6 -5.9496123044041015e-5 0.00020662090437933094] %
+
+Mass Used: 93.66445705970182 kg
+Launch C3: 95.2225636939024 km²/s²
+||V∞_in||: 0.008799228324162446 km/s
diff --git a/archive/ES_0.5564048549413042 b/archive/ES_0.5564048549413042
new file mode 100644
index 0000000..1544272
--- /dev/null
+++ b/archive/ES_0.5564048549413042
@@ -0,0 +1,22 @@
+archive/ES_0.5564048549413042---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T02:16:42.076
+Launch V∞: [8.106019039293454, -5.749402944357282, -0.01764408852833544] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.019390677124978384, 0.12867779726983442, 0.15438281814718638] km/s
+ V∞_out: [-0.08442131866292248, 0.06795777202425991, -0.1706277029235823] km/s
+ time of flight: 1.874957778770099e8 seconds
+ arrival date: 2030-04-25T04:26:19.076
+ thrust profile: [0.17696723280162294 -0.0020790192009619373 -0.06544341379978084; 0.04374158706263178 0.022792073987474785 -0.055871474583363265; 0.06289621876219645 0.05328115953628962 -0.14281840185029146; 0.028530354362034265 0.030826009216158152 -0.09527463491435076; 0.01742566069169801 0.022498906394578966 -0.07952436718936659; 0.01781485687928065 0.025869238050137612 -0.09839980452363024; 0.011937582102736273 0.020787422759922857 -0.0842008966417584; 0.0055828563939743035 0.00998359946871324 -0.04528112248971227; 0.005010136992623528 0.009104124168313214 -0.04315612151891958; 0.005804964041417466 0.011787457221582818 -0.061167836610635254; 0.0008206272273259728 0.0016946640207294538 -0.009203598203342737; 2.686020818959074e-5 0.00036729666935340455 -0.0011054273222438529; 0.00017336167881622472 -1.49020818459693e-5 -0.0009694558059525206; 0.00017115674418187693 -0.00025541094195160235 -3.511926122925802e-5; -0.00017899820990559782 -0.00014893296391419207 -0.00031327317420853376; 0.0002537663947340923 -0.0002571052219102797 -0.0007959044251347252; -0.0004378232495403716 0.0005894881730827729 -0.000296695365557894; 0.0004603162509315707 -0.0004462301139326054 -0.000421630776842283; 0.0005010874023713811 0.00025509493559874223 0.0015716556386789887; -1.6135092068641902e-5 -0.00022509537381867287 -0.0004259952321964195] %
+
+Mass Used: 73.01863795583404 kg
+Launch C3: 98.76349019583215 km²/s²
+||V∞_in||: 0.20191094177544958 km/s
diff --git a/archive/ES_0.5564363738948065 b/archive/ES_0.5564363738948065
new file mode 100644
index 0000000..90b39ee
--- /dev/null
+++ b/archive/ES_0.5564363738948065
@@ -0,0 +1,22 @@
+archive/ES_0.5564363738948065---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T16:51:04.770
+Launch V∞: [8.099568210362404, -5.7845842437940975, 0.005404131044590708] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.938319357768089e-7, 1.080036062574388e-6, 1.1242581668997849e-7] km/s
+ V∞_out: [-4.885843097749587e-8, 2.418269870683512e-7, 1.2756560110723293e-6] km/s
+ time of flight: 1.874957778411716e8 seconds
+ arrival date: 2030-04-25T19:00:41.770
+ thrust profile: [0.17736942818297258 -0.002430214960336201 -0.06713446948744745; 0.03607391727292012 0.018407135861431556 -0.04772848400768622; 0.03520665889415732 0.02832841389691329 -0.08297309788799628; 0.03136354888272034 0.03227024654736667 -0.10774110692192508; 0.0273355516599659 0.03336279295512417 -0.12432031915617292; 0.020511049280521453 0.028366845920646262 -0.11688595777321885; 0.013764555712134368 0.021080805713037467 -0.09529216133226312; 0.009570202604325848 0.015785957655054896 -0.0776049951803667; 0.0018073905206281906 0.0028637067848076387 -0.015666913384920027; 0.0006917379938450014 0.0011149475513277365 -0.007134609910967412; 0.0013108064924325603 0.0027111740036453317 -0.017901323426933655; 0.0004768990673599347 0.0008032471832153285 -0.00564080610902237; 0.0006330837217237338 5.854508461336776e-5 -0.0019256511918450143; -0.00018288110987994095 0.00010163139099624257 -0.00029996276057294726; 5.845759816005243e-5 -0.00044157434930618567 -0.00040427738423127384; 0.00026965289911152346 0.0010523134536892071 -0.0005227178275819698; -0.002169854954836291 0.0022415156559497697 -0.0025376733273192215; -0.00018566848077623493 0.0003808253135281303 0.0006259127048756813; 0.0005616320249161662 -0.0017140642951747607 0.0010632987790184937; 0.0006517810048161747 0.0011198465422447446 0.0003456943651564364] %
+
+Mass Used: 71.29981545437795 kg
+Launch C3: 99.06444927249652 km²/s²
+||V∞_in||: 1.2886117397507248e-6 km/s
diff --git a/archive/ES_0.5564363770530413 b/archive/ES_0.5564363770530413
new file mode 100644
index 0000000..2631daf
--- /dev/null
+++ b/archive/ES_0.5564363770530413
@@ -0,0 +1,22 @@
+archive/ES_0.5564363770530413---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:09:12.332
+Launch V∞: [8.138419671025236, -5.671012753185021, 0.14727780598264123] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.41414114770841e-6, 7.753674917914915e-6, -5.507169748343572e-6] km/s
+ V∞_out: [1.7428341731620618e-6, 1.2561886987644351e-5, -6.407314704359091e-7] km/s
+ time of flight: 1.8749577787571076e8 seconds
+ arrival date: 2030-04-23T19:18:49.332
+ thrust profile: [0.16889622989263242 0.0006557386384139777 -0.0567951779513878; 0.06375951774839977 0.03600158187714391 -0.07435984293728454; 0.05735497694585939 0.05483033185440871 -0.11831281375196039; 0.04803933773457518 0.05781274550546303 -0.14903397283849493; 0.021976396236308798 0.03158479918851183 -0.09134327609646735; 0.01924301759743878 0.03135479920013264 -0.09857875711156501; 0.011370032122927747 0.023274137933670978 -0.0789393497234036; 0.004112256049024175 0.01118492886580402 -0.043502081347838235; 0.003514405270641238 0.00974460686515755 -0.03573432054651548; 4.17712984952028e-5 0.003683454506208085 -0.010366215153871719; 0.002376744779913328 0.0005322186748513845 -0.00036362564493878534; 0.0007427189525668697 0.00044073118546957663 -0.002114659124763614; -0.0002813313650267636 0.002112207933576904 -0.007148807777926926; -0.0003530240814564466 0.0004828623220112195 -0.0025474687881119652; -0.0002992417046183979 -0.0005448392726820325 -0.0008650877110684832; 0.0019171166948573695 -0.001861001525222093 -0.0023296778007397944; -0.0003738770870787148 0.000825886297786625 -0.0016384791682172782; 0.000809815345330659 -0.006243249895049249 -0.0027187747007090587; -0.0009651232775133942 -0.00019493189558856852 0.003665040458391701; -0.0003143376147886832 0.0008035511920265485 0.000622795475269557] %
+
+Mass Used: 75.08272490807394 kg
+Launch C3: 98.41595114065272 km²/s²
+||V∞_in||: 1.269827408049351e-5 km/s
diff --git a/archive/ES_0.5564377168218299 b/archive/ES_0.5564377168218299
new file mode 100644
index 0000000..d96ec4d
--- /dev/null
+++ b/archive/ES_0.5564377168218299
@@ -0,0 +1,22 @@
+archive/ES_0.5564377168218299---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T15:40:01.998
+Launch V∞: [7.962764552186467, -5.760044303445141, 0.15581866243487813] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.39524555723968e-6, -3.670310854255633e-6, -3.436241570301458e-7] km/s
+ V∞_out: [3.1729861061332957e-7, -1.5356882863370838e-6, -4.105288726869645e-6] km/s
+ time of flight: 1.874957778749533e8 seconds
+ arrival date: 2030-04-24T17:49:38.998
+ thrust profile: [0.36467485833261676 -0.001922877675134856 -0.11691374076729943; 0.06075854833321263 0.034007737767762385 -0.07552225850916898; 0.026863638510537025 0.023589967376629228 -0.060036108638667575; 0.026741793537258942 0.030707453820900704 -0.0870636828466365; 0.024079812818442275 0.03370860793177039 -0.10448455392191588; 0.01774022560243313 0.028674603363547612 -0.09745101061694864; 0.017165389065045326 0.0324013971582745 -0.11775255837664361; 0.007107724396954574 0.014229973663736694 -0.05762407675228467; 0.0039505707353406656 0.00842899199636437 -0.0368998050157474; 0.0036687934396962044 0.009072557512889998 -0.04179476955665205; 0.00016166440824387951 0.000633237731654422 -0.0030335220681314834; -3.1044969735291236e-5 0.00012730724461997326 -0.002802743855987649; -1.593866516361067e-5 0.0010532883854992693 -0.0007761985329475555; -0.00013484632508129515 -0.0002286344852597959 -0.0010013931251418328; 0.0003698960179581699 0.0008290797801300078 -0.0016329671006390762; 0.0007241511968443519 0.00030830229547325165 -0.0011018958648434218; -0.00010209622980766669 0.000864606770953332 -0.0008505457571467818; 0.0005050777859006345 -0.0016700957146199061 -0.0009345397542663027; -0.00025969086840038917 5.7128363230766685e-5 0.0002077973571903021; -0.00020921186814704248 -5.647354651849104e-5 0.0006286485423795385] %
+
+Mass Used: 85.63061626930312 kg
+Launch C3: 96.60800914677115 km²/s²
+||V∞_in||: 4.396187053304013e-6 km/s
diff --git a/archive/ES_0.5564434531045578 b/archive/ES_0.5564434531045578
new file mode 100644
index 0000000..dc23da1
--- /dev/null
+++ b/archive/ES_0.5564434531045578
@@ -0,0 +1,22 @@
+archive/ES_0.5564434531045578---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:24:58.345
+Launch V∞: [8.113201032863756, -5.7634653127589335, 0.14726092827531723] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.551783293745554e-5, 4.5571525310886154e-5, 0.0030637172432847787] km/s
+ V∞_out: [-0.002701430571110147, -0.001045452579011371, 0.0010014117481979468] km/s
+ time of flight: 1.8475135381723052e8 seconds
+ arrival date: 2030-03-23T07:14:11.345
+ thrust profile: [0.1675493762068367 -0.007403225559824914 -0.05962835838757743; 0.02099833731732138 0.010042463278717698 -0.026277494202824533; 0.03765266166708532 0.02956445315270752 -0.08833590267218168; 0.048179567417945816 0.046606966393791235 -0.15208849647414147; 0.02515617869164546 0.030222959476121584 -0.11361223935397692; 0.01646010683827155 0.024118404592269646 -0.09651195898183124; 0.012382972241247415 0.01788061710892062 -0.0814310104956395; 0.012939957304730597 0.020078513060932536 -0.09702426641577319; 0.0030205398068730792 0.005289384788816254 -0.02655244601842374; 0.002105943811247495 0.003560225063737444 -0.020411547003725043; 0.002537885004155893 0.004132209529639089 -0.024972841119392766; 0.00013024540916935592 7.801677451883814e-5 -0.0006355087912401178; 9.351396384979399e-5 0.00027237281091289586 -0.0022169897248843604; -0.000421843163852482 0.0002661121250948574 -9.858844237532825e-5; 0.00040860224132136295 0.0006713954923714145 0.00023396201670981918; -0.0005720650937356367 -0.00034702518447636755 -0.0010976364586265308; -0.0005597777817396459 0.0006161267056839751 -0.001156771601210218; -7.370735405014798e-5 -0.00023790581863294827 -0.0010798497689532948; 9.270107466222987e-5 -0.0003252552548215845 -0.0009628065557222465; 0.0012777552690851725 0.0012331537195211587 0.0002160658860817905] %
+
+Mass Used: 71.31507500178895 kg
+Launch C3: 99.06324919203345 km²/s²
+||V∞_in||: 0.003064756547778708 km/s
diff --git a/archive/ES_0.556453650248578 b/archive/ES_0.556453650248578
new file mode 100644
index 0000000..db4f8ba
--- /dev/null
+++ b/archive/ES_0.556453650248578
@@ -0,0 +1,22 @@
+archive/ES_0.556453650248578---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:19:12.896
+Launch V∞: [7.900186867940902, -5.80195513699686, 0.10857680200473334] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.947583884805263e-6, 4.0646650161173365e-6, -4.552817890949358e-6] km/s
+ V∞_out: [1.1518682539750074e-6, 9.164077841516948e-6, -4.0806772567926667e-7] km/s
+ time of flight: 1.8749577787492922e8 seconds
+ arrival date: 2030-04-23T07:28:49.896
+ thrust profile: [0.28442046836813084 0.013585284393893145 -0.08228666789852464; 0.14732123927234791 0.09862080801127338 -0.14168146984469707; 0.04240453031035516 0.045786027156268325 -0.08222227029211844; 0.03775120048006673 0.05745811298979494 -0.1105363034046098; 0.0451247977271028 0.09238869612463685 -0.18058723805956717; 0.013903954766717587 0.03228045561611711 -0.07402976841114384; 0.010306019683664062 0.03217604174662431 -0.0800549005101562; 0.0028140238716943063 0.010085338483080243 -0.026960908398847367; 0.000733011428638324 0.002632828992658677 -0.007770470082948786; 0.0005963431206027347 0.0026116461682093957 -0.007900661213048613; -0.0003542206865349215 9.043644330434186e-5 -0.00018519053804282536; 0.0004847976892110061 -0.00018052661237337038 0.00030540366720943824; -0.000785230044513999 -0.0003741287992273252 -0.0002682890107020895; 1.5881845965823356e-5 -0.0006549100921842162 0.0009395816081688684; -0.0002306124467296757 9.781665913671892e-5 0.0004646771881352666; 0.0003618486005749187 -0.0012214690212970871 -0.0010190122249592601; -0.0014053259199849585 6.431359687201566e-7 0.0006871368050395453; -0.0006030996248448406 -0.0006164324265606628 0.0010977859609292303; -2.9634007788058726e-6 5.605698929381583e-5 -0.00017705983945475321; 0.00022665715127808244 0.0005436971193447212 0.00019837296607864768] %
+
+Mass Used: 88.6859468114194 kg
+Launch C3: 96.0874248820437 km²/s²
+||V∞_in||: 9.247625331824516e-6 km/s
diff --git a/archive/ES_0.5564601179423717 b/archive/ES_0.5564601179423717
new file mode 100644
index 0000000..90b4a9e
--- /dev/null
+++ b/archive/ES_0.5564601179423717
@@ -0,0 +1,22 @@
+archive/ES_0.5564601179423717---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:38:07.842
+Launch V∞: [7.986047732806254, -5.827284172257835, 0.12724435991569819] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.009469707616372e-9, -3.781947545125003e-9, -1.947348624295784e-9] km/s
+ V∞_out: [-1.2969340261409135e-9, 1.2062431979258725e-9, -4.3999453525323683e-10] km/s
+ time of flight: 1.8362533409172624e8 seconds
+ arrival date: 2030-03-09T14:40:21.842
+ thrust profile: [0.22721700861225136 -0.0087244561956508 -0.08143734249682963; 0.0748870327120334 0.03745892108866105 -0.0929394123776199; 0.06026002691793584 0.048752097930575826 -0.1317889348187575; 0.0362536596776956 0.03757772433107415 -0.11729527393346809; 0.022848144800549523 0.028003836253501172 -0.09886545358064358; 0.021909622437835168 0.030881685807812337 -0.11749566274257725; 0.011442679277301986 0.01821560019390227 -0.07638153354871098; 0.0065757939540994235 0.010787151381581712 -0.049592158776623395; 0.004400780511843783 0.0075029496502346015 -0.035836250444389574; 0.0020816061373412523 0.004114381834397901 -0.020706102587582587; 0.0008517402314998661 0.0011505369438333357 -0.007729089540707536; 0.00018054390840442156 -4.598604554586173e-5 -0.0004543244901445807; 0.00027310595671868685 -0.00021047585158356317 -0.000342637615937151; -0.00023405382512398218 0.00021427291530226047 -0.00061863896769209; 0.00027082970013329183 -0.0007472510224790676 3.769881478543505e-5; -6.773546800078906e-5 -0.00012037434098476828 -0.0005336145241999951; 0.0006319659680754829 -5.390222705266702e-5 -0.00022008888075173712; -0.0010479886486267761 0.0007226935797564434 -0.0005831132350890566; 0.00012249196695049823 0.00015882182257460496 -0.0015488023512434943; -0.00016288474139572088 -0.00030091136545854717 -0.0004893317388762569] %
+
+Mass Used: 78.9928606042181 kg
+Launch C3: 97.75039034203695 km²/s²
+||V∞_in||: 6.571916056231225e-9 km/s
diff --git a/archive/ES_0.5564751721201552 b/archive/ES_0.5564751721201552
new file mode 100644
index 0000000..589ea76
--- /dev/null
+++ b/archive/ES_0.5564751721201552
@@ -0,0 +1,22 @@
+archive/ES_0.5564751721201552---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T01:03:03.314
+Launch V∞: [8.045938266075552, -5.857847060964657, 0.2870955984115263] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2790916103480883e-7, 3.622443359873358e-7, 3.604829626772987e-8] km/s
+ V∞_out: [-3.02117794123761e-8, 1.6038135167891249e-7, 3.968134332942582e-7] km/s
+ time of flight: 1.874957777450277e8 seconds
+ arrival date: 2030-04-26T03:12:40.314
+ thrust profile: [0.1605766551091104 -0.0013333677172681167 -0.05792076498691961; 0.0339104437981193 0.018853309818040186 -0.044420883468852895; 0.06278503476661522 0.05262520446883015 -0.1381563369142007; 0.04380077504164051 0.04730582093497278 -0.14250537847283443; 0.03391190269578709 0.0434959097134492 -0.1479862142119474; 0.016110990093135883 0.023955456239811785 -0.0933216206839893; 0.009244121873590532 0.014776522274250704 -0.06400115694059814; 0.006611351188192431 0.010902814945825633 -0.05146907735585712; 0.0004204642135259049 0.0009537705099455903 -0.00541338297546679; 0.00019996779897676548 0.0007170035933164988 -0.0033048309664184127; -0.00023581467653815556 -0.000465441766600295 -0.0011052789126555405; 0.0008799913486879146 0.0017661171970764448 -0.01125355441950569; 0.0001544929533336903 -0.0004293435814397853 -2.969685841356989e-5; -0.00033769589081578203 0.00026550177739586244 0.00046430419064938107; 0.00015927461009044295 0.0005332780379339277 0.0005989228580178935; 0.0003104175247963377 0.0003007002623770859 0.00026957903742338025; 0.0008885421909136024 0.0006913247259037375 0.0008990176256375537; 0.00019138748586696515 -0.0006000161630834221 0.00013489024685742874; -5.3995944512950965e-5 -7.887330742195652e-5 0.0015564949568362767; -0.0007139032721588839 -0.00020977857487244453 0.00048025361621361956] %
+
+Mass Used: 70.93984199314036 kg
+Launch C3: 99.13391865377841 km²/s²
+||V∞_in||: 4.294915881624485e-7 km/s
diff --git a/archive/ES_0.5564764652276207 b/archive/ES_0.5564764652276207
new file mode 100644
index 0000000..f86b012
--- /dev/null
+++ b/archive/ES_0.5564764652276207
@@ -0,0 +1,22 @@
+archive/ES_0.5564764652276207---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T00:33:23.480
+Launch V∞: [8.033275083777607, -5.7904862002295445, 0.14079069896782878] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2471419348311014e-7, -3.0899439091853077e-6, -8.40316162382349e-6] km/s
+ V∞_out: [-8.063779398123415e-6, -9.338355179917807e-7, 3.7250046975060856e-6] km/s
+ time of flight: 1.8409208841894504e8 seconds
+ arrival date: 2030-03-14T17:14:51.480
+ thrust profile: [0.20576078994989389 -0.0035904991597399583 -0.06809484018929217; 0.05445396349744519 0.0292324226855392 -0.0636623255207566; 0.055910465309966385 0.04898468894844096 -0.1138111160675574; 0.03307154944525983 0.03879304051784428 -0.10261725788529195; 0.029915312472368644 0.041012310589904476 -0.1212279078091535; 0.021601218658688 0.03595357231636211 -0.1129220859795636; 0.00796784966360771 0.014603884993546527 -0.05311499247816327; 0.006946977676832486 0.013753634547846913 -0.04985809247898795; 0.011340612507708193 0.02738625806116569 -0.1016684917037708; 0.00218665546518584 0.0053733800110175945 -0.022546693744996113; 0.00021349586457912478 0.00032178700565089184 -0.001593686770827736; -2.8014071597327032e-5 0.0003336722559657919 -0.0009920302840583342; 0.00012613448152225596 0.00015097965430436094 -0.000864606012831154; -4.2837856108034165e-5 8.379977861705404e-5 -0.00024374582737722464; 8.189744365942877e-5 0.00029738700739578936 -0.00022430693275853633; 5.9844753754391996e-5 2.453227298197146e-5 -0.0003045536185589977; -9.866837593986599e-5 0.0006343202683508065 -0.000451349365827163; 4.6180913694850664e-5 0.00023542526727946228 -0.00021070233395343446; 0.00011004667709463815 -1.6334118716774973e-5 -0.0007878061555716611; -2.540365164302753e-5 1.0010304479109915e-5 -3.619702842170614e-5] %
+
+Mass Used: 77.07135343785149 kg
+Launch C3: 98.08306102760676 km²/s²
+||V∞_in||: 8.954129341709744e-6 km/s
diff --git a/archive/ES_0.5564935169751245 b/archive/ES_0.5564935169751245
new file mode 100644
index 0000000..7743159
--- /dev/null
+++ b/archive/ES_0.5564935169751245
@@ -0,0 +1,22 @@
+archive/ES_0.5564935169751245---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T06:14:48.261
+Launch V∞: [7.962983801992237, -5.593639169173562, 0.19060583631564892] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4759183629858538e-6, -2.1730781948953434e-6, -2.1738137269354375e-7] km/s
+ V∞_out: [1.8827556168489388e-7, -9.491090550894298e-7, -2.4469132204201863e-6] km/s
+ time of flight: 1.8749577787431568e8 seconds
+ arrival date: 2030-04-21T08:24:25.261
+ thrust profile: [0.44537339888532246 0.009786591989909324 -0.12376260141834956; 0.10371211484836004 0.06651983840906536 -0.10967013872696135; 0.062209401570522654 0.05907543182995611 -0.10919844208429155; 0.04509512125925015 0.06688531819544563 -0.1219754908929271; 0.015918450100807262 0.02844042178007741 -0.06430038425437297; 0.027209827542380757 0.05989646485276328 -0.14532641663435267; 0.009024475532857318 0.0233400207299952 -0.061913475890794226; 0.005639209093772342 0.01698436132752913 -0.04744363882577337; 0.0022072928981543985 0.007837116553918808 -0.023127700739754703; 0.0001754580682484258 0.0006433460776174155 -0.00219588429750559; 7.693904067687814e-5 0.0007865450851426236 -0.002494860187634203; 7.648692868127851e-5 0.0004656565631956716 -0.0009983574789280323; -6.869631162132616e-5 8.084068417744281e-5 5.977106504955707e-6; 1.2708634947930794e-5 6.0985503368215463e-5 -0.00022687566684238085; 4.731845734532193e-5 2.3246774185525082e-5 -0.00016465548058845276; 7.088168453596369e-6 9.873079260665377e-5 0.00013177136655100394; 8.604733330794857e-5 0.00016812293169693465 0.00016617966245264121; 0.00035428255879681625 -0.00034109760197690057 7.105806676355373e-6; -0.00028629358183109943 -0.00013300020754871745 0.00017042785014878903; 3.6410539801755235e-5 0.00012872000538802572 -0.00038497920901656125] %
+
+Mass Used: 96.6260319761559 kg
+Launch C3: 94.73424077054104 km²/s²
+||V∞_in||: 2.6358790785092127e-6 km/s
diff --git a/archive/ES_0.5564985051651921 b/archive/ES_0.5564985051651921
new file mode 100644
index 0000000..88747bc
--- /dev/null
+++ b/archive/ES_0.5564985051651921
@@ -0,0 +1,22 @@
+archive/ES_0.5564985051651921---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T16:48:06.233
+Launch V∞: [7.9953981817748705, -5.8752644467484085, 0.26443836526359327] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.258207980797215e-7, -1.1076663480807069e-6, -3.12923634677649e-6] km/s
+ V∞_out: [-3.0242795704220225e-6, -3.475804377326947e-7, 1.4266096367878298e-6] km/s
+ time of flight: 1.8749577790180814e8 seconds
+ arrival date: 2030-04-25T18:57:43.233
+ thrust profile: [0.19243496965231946 0.002425808250269783 -0.0674659609961534; 0.036947541617770065 0.021281330546524244 -0.045821542308167346; 0.07833951718098237 0.0697595509095331 -0.15471124894321436; 0.038388291185417665 0.04760147734307 -0.12322375828448229; 0.031814656617960325 0.04480842252638674 -0.1312234996249144; 0.02006590085561957 0.032681706629563295 -0.10632816536013469; 0.009818799731926972 0.017634543537136574 -0.06434141060985676; 0.005860209908437293 0.01235472222059704 -0.04730958928763586; 0.001212406180277202 0.002561916013187308 -0.012058867346872124; 0.000427178445128908 0.0008121627470830772 -0.004631832940735927; 0.00030298631747831316 0.0007363462332932627 -0.004704528684062553; 0.0002516746520534238 0.0010951371291630044 -0.003155876738361365; 0.0006547289726589859 0.0009818979353995955 -0.0017390626013508667; -0.0006267215609487345 -0.0005339713447507803 -0.0004064624852413108; 0.000202470581749504 0.0010944789167284742 0.0010542933202841078; 0.0012176184823842742 0.0004250838024835833 0.0003547340635481305; 0.00010574033324215837 0.0006053223588505692 -0.0018169448579405023; 0.00027134517327533146 -1.858235803415295e-6 -0.00025102758535461967; -0.00021357987801782656 0.0009341329874029451 -0.0005531224567261015; -0.0003200866886889414 0.0011025973576178475 0.0008045240376974236] %
+
+Mass Used: 74.57711904801863 kg
+Launch C3: 98.51505205337807 km²/s²
+||V∞_in||: 3.335446603547841e-6 km/s
diff --git a/archive/ES_0.5565048523915862 b/archive/ES_0.5565048523915862
new file mode 100644
index 0000000..dbdcff3
--- /dev/null
+++ b/archive/ES_0.5565048523915862
@@ -0,0 +1,22 @@
+archive/ES_0.5565048523915862---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:07:27.015
+Launch V∞: [8.1036072460034, -5.545983945817414, 0.18871637620983372] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.411652041146096e-6, 0.0004974596314582155, 8.733532883504261e-6] km/s
+ V∞_out: [0.0004912089030341886, -7.407945624551098e-5, 0.00010983827399483356] km/s
+ time of flight: 1.8749577787450632e8 seconds
+ arrival date: 2030-04-22T09:17:04.015
+ thrust profile: [0.36675403456836375 -0.006621347793537658 -0.11898889643705601; 0.029602126010166457 0.0160798158391227 -0.03507025517527013; 0.05196141949500942 0.04512427587628056 -0.10773202768974213; 0.07041909434615473 0.08035607613787285 -0.21259469176146725; 0.02404331700352571 0.03259722339534148 -0.09986509225951935; 0.021351094624951668 0.03364323921211178 -0.1121146208283415; 0.006840056174605599 0.012279354913432503 -0.04551621234656278; 0.0018926679834415012 0.004033579557919578 -0.015730913391671195; 0.0009760820593679782 0.0017064452255255008 -0.007644378851182835; 0.002380844299778934 0.0059093331912317935 -0.025806756184059594; -0.0002868611496860232 -0.00034790373540889924 -0.0011678817752882324; 0.0005531542504948867 0.0015756558616897153 -0.00472088513123951; -0.0005877114491106862 0.00031852778474492994 -0.0062143165758710515; -0.0013103150777036517 -0.0005634478182181017 -0.005183388814086386; 5.08562576563184e-5 -0.001339670031137206 0.0002215509938258409; 0.00034958229799413184 -0.0025136318759262726 0.00127711412369097; -0.0021160096165637092 -0.0021469761820454344 0.0011527763121951208; -0.0026264435782275427 0.003773073935125235 0.00039745426756724136; 0.0009862330677511298 0.00020861197257756448 -0.001712597481597463; -0.00017128428093669484 -0.0011682809088978086 -0.0019205335263556768] %
+
+Mass Used: 86.56064831705771 kg
+Launch C3: 96.46200219539305 km²/s²
+||V∞_in||: 0.000497591491198503 km/s
diff --git a/archive/ES_0.5565089627296943 b/archive/ES_0.5565089627296943
new file mode 100644
index 0000000..fde85df
--- /dev/null
+++ b/archive/ES_0.5565089627296943
@@ -0,0 +1,22 @@
+archive/ES_0.5565089627296943---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T05:21:35.699
+Launch V∞: [8.08277405045621, -5.719977582966368, 0.29355714001533006] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.993104181362316e-7, -1.9488563995708566e-6, 4.343790442794995e-5] km/s
+ V∞_out: [1.9638173435728887e-6, -4.352508741201566e-5, 3.5742628288460966e-7] km/s
+ time of flight: 1.874957778737147e8 seconds
+ arrival date: 2030-04-24T07:31:12.699
+ thrust profile: [0.19840761664818418 -0.00042655076623316084 -0.06539013718412945; 0.08884907909030788 0.055253690783975136 -0.10316888037697566; 0.04382699223499236 0.040463745759893976 -0.09342902182096037; 0.022764308203199905 0.02868176550795606 -0.07335539010548561; 0.023762373642313515 0.033221257333422516 -0.0989535002498104; 0.019497527405425062 0.03233664061812452 -0.1054239145586473; 0.015863291301123426 0.03128521369805607 -0.1064856371294612; 0.007944152899054781 0.016290295870837395 -0.058816107620292386; 0.0030003623924879526 0.006764159922310405 -0.02688741653821328; 0.0025725229681284475 0.0073701047733163595 -0.03124655441094639; 0.001101280164720699 0.0025235910431309154 -0.011528742563444088; 0.00021948727479896536 0.0006501014903700356 -0.0041188360032629314; 7.822590349595049e-6 0.00017663794785909207 -0.0004730850068614357; 0.0022484235197819014 -0.001216064617090474 -0.00041296500720878744; -0.00010917458561624688 0.0004543121569221145 -0.000527519642830352; -0.000317727001685733 -0.0003890639688803847 0.00024629185914394104; -0.0007827271630870214 0.0003157982281328227 0.0008672130076036878; -0.0004503695340129371 0.0011067039022519044 0.0009588658377119863; -0.0018820737982809682 0.0016969302467102448 0.0015532801148627853; -0.0004052745217788513 -0.00010308274963941023 0.0010706291319293579] %
+
+Mass Used: 76.80304829819306 kg
+Launch C3: 98.13555569482004 km²/s²
+||V∞_in||: 4.348263065965843e-5 km/s
diff --git a/archive/ES_0.5565193330264565 b/archive/ES_0.5565193330264565
new file mode 100644
index 0000000..75ae899
--- /dev/null
+++ b/archive/ES_0.5565193330264565
@@ -0,0 +1,22 @@
+archive/ES_0.5565193330264565---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T17:04:33.406
+Launch V∞: [7.994961595461683, -5.704492430869547, 0.16681178356890938] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0187573093575471e-9, -8.123861588234068e-9, -4.980786612281384e-9] km/s
+ V∞_out: [-6.7682296853732616e-9, 5.607937468967704e-9, 4.0829428319462215e-9] km/s
+ time of flight: 1.8453517671230564e8 seconds
+ arrival date: 2030-03-18T12:50:49.406
+ thrust profile: [0.2729261660126905 -0.008785238230462532 -0.08900176628291909; 0.16336567799588453 0.08634310915119567 -0.17975216725593618; 0.050051199599726655 0.043372161163153455 -0.10100628756459577; 0.032519991677149605 0.03677367643734779 -0.09730449127881804; 0.018748107848214263 0.025767884640264208 -0.07607436362938039; 0.02830966891200543 0.04506468067631571 -0.14204195710199236; 0.011411216402132666 0.020819436948219618 -0.07202407077294039; 0.007201921643557157 0.014755657747607773 -0.054738031473941705; 0.0024452231971141673 0.005832129651665346 -0.021180643101899495; 0.00038532690532368013 0.001007060925254518 -0.004140466770601655; 0.0004473682039568537 -5.2490265569420927e-5 -0.00034094703552905114; -6.135826056895483e-5 0.00025531871935435347 -0.001656827999776894; 3.0586157698744886e-5 0.00023152630344886488 -0.0014115186099974543; -9.95667820635998e-6 5.133598594453517e-5 -0.00038061360753434355; 2.160398349913939e-5 0.00020013690226941338 -0.0005301222047399974; -4.407750192211046e-5 -7.219514290635943e-6 0.00024110839881527342; -0.0004409906040567268 -0.0004607100317395134 0.0002239269238146493; 0.00016080027919503732 0.00013334888809300586 0.00015359049225694712; 0.000916146731662871 -0.00025928422153602746 0.0009352821329402581; -0.00027313640000855633 0.0006510829623317694 -7.335495591039021e-5] %
+
+Mass Used: 86.42314115982572 kg
+Launch C3: 96.4884709778926 km²/s²
+||V∞_in||: 9.583487300416057e-9 km/s
diff --git a/archive/ES_0.5565209753655865 b/archive/ES_0.5565209753655865
new file mode 100644
index 0000000..4aaada7
--- /dev/null
+++ b/archive/ES_0.5565209753655865
@@ -0,0 +1,22 @@
+archive/ES_0.5565209753655865---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:04:47.420
+Launch V∞: [8.166719581636144, -5.632281261244687, 0.19290909874404047] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.568035120216844e-5, 5.670559319547664e-5, 0.003939823131744744] km/s
+ V∞_out: [-0.003529692002661069, -0.001173311598842904, 0.0013018481387125328] km/s
+ time of flight: 1.8749577787493864e8 seconds
+ arrival date: 2030-04-24T02:14:24.420
+ thrust profile: [0.18127561016256588 -0.00799541492131119 -0.06020817505758873; 0.08946900740174697 0.041431924581167054 -0.10347135105336443; 0.04328188071201928 0.03370613240403856 -0.09637568700286255; 0.030978084370424614 0.030564852728168786 -0.1011063851488519; 0.025903405893636457 0.02965218266789441 -0.11147651809235848; 0.01457700495406818 0.018544927445141225 -0.08124351284058345; 0.01013715843074136 0.014168955255365377 -0.06740395579984508; 0.006902228758898641 0.010168313860203044 -0.0527995010451023; 0.00803104140889518 0.013352035559800262 -0.06843193752818348; 0.002502984528900236 0.004464248957171614 -0.024432689278936107; -2.1567604160510254e-5 0.0018135397378304444 -0.0013712641432837612; 0.0005135105190907889 0.0007516742214930708 -0.0052502534518198895; -0.00043287023895767225 -0.0007935550071490534 0.001097074980339235; -0.000473828638859879 0.001734622508695422 -0.0066367754940413306; 0.00020449143531161266 0.0005659521639635788 -0.0003205882212457367; 0.0006781160947813422 -0.0003173524140599642 -0.0018852197848218102; 0.0019154359796337615 -0.0031996185034499675 -0.0029039682388373672; -0.00018312182367554968 0.0001329401726334013 -0.0018625605765799152; 0.0003577679201241528 -0.00019559707803577418 3.550702198742994e-5; -2.817038534506152e-5 -0.0004347991635068882 -0.001372134721497091] %
+
+Mass Used: 74.95296796103548 kg
+Launch C3: 98.45511485122552 km²/s²
+||V∞_in||: 0.003940957922801092 km/s
diff --git a/archive/ES_0.5565298946620401 b/archive/ES_0.5565298946620401
new file mode 100644
index 0000000..cc86823
--- /dev/null
+++ b/archive/ES_0.5565298946620401
@@ -0,0 +1,22 @@
+archive/ES_0.5565298946620401---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T11:14:40.098
+Launch V∞: [8.123123553940351, -5.74473148482225, 0.21982528026986167] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00019206522782090713, -0.00035639429905729916, -0.00013593254455629547] km/s
+ V∞_out: [-3.864444832692073e-5, 0.0002627487740817254, -0.0003323407927126987] km/s
+ time of flight: 1.874957778756263e8 seconds
+ arrival date: 2030-04-25T13:24:17.098
+ thrust profile: [0.17857640169166464 -0.005796642145264387 -0.06591908418747956; 0.02549491699288305 0.012206349414403883 -0.032711770540785; 0.04485740997989577 0.032797466030325635 -0.10165720190143723; 0.044495059945414216 0.04057283970150244 -0.14541269373968055; 0.0408967935430743 0.04323377634787657 -0.175419527883327; 0.01716778228015056 0.019927282355282617 -0.09278647101492979; 0.006994165062827945 0.009006915705099042 -0.044792598831293697; 0.00281828046036278 0.0030059412373995404 -0.021845474142226862; 0.0021823169222589182 0.003569887020822766 -0.017627977546360044; 0.0037602973371897576 0.005541047881131758 -0.03392830660382507; 0.0038146265030394497 0.0019338672131861395 -0.02130836378641468; 0.00012013304251192835 0.0006171121818763638 -0.002783059117703256; 0.0006202295093446903 -0.0004004959114799981 -0.0020554527752387345; 0.0005182271799604927 0.0005945327412752656 -0.0025503752125993918; 0.0023060333021313146 -0.0019569082009718037 -0.005535796884283172; 0.0017137301739855813 0.000305585805054262 -0.0026164125055164324; -0.001203199835420157 0.000501244004237786 -0.0033329255495368436; 0.00013492856430069458 0.0005631779094394992 -0.0013484006345501802; -0.00010398011811108611 0.0029066192538717145 0.0011377542580777913; 0.0015162481664877324 -0.0005892930716514559 -0.0010301482342010993] %
+
+Mass Used: 71.57838142743003 kg
+Launch C3: 99.0353992591343 km²/s²
+||V∞_in||: 0.0004270639352696383 km/s
diff --git a/archive/ES_0.5565305951711936 b/archive/ES_0.5565305951711936
new file mode 100644
index 0000000..4b59970
--- /dev/null
+++ b/archive/ES_0.5565305951711936
@@ -0,0 +1,22 @@
+archive/ES_0.5565305951711936---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T05:36:55.508
+Launch V∞: [8.091344260133095, -5.792501000356863, 0.18303883928531914] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8520249368138994e-7, -4.26431937095134e-6, -7.05909023594422e-8] km/s
+ V∞_out: [-4.1667093702064975e-6, 7.249611620508433e-7, -1.0162737400364156e-6] km/s
+ time of flight: 1.874957778742033e8 seconds
+ arrival date: 2030-04-25T07:46:32.508
+ thrust profile: [0.12357522821681602 0.00011113208213694973 -0.04471860539346146; 0.08677298720711522 0.04851152820354428 -0.10506309860740995; 0.0506373340383325 0.044483040021943955 -0.11074082033280196; 0.030390776454024923 0.03443267703712971 -0.09889077567258858; 0.028173235550903095 0.03849615161164153 -0.1213735405253975; 0.013069724467028391 0.020089573736358078 -0.07223341724315793; 0.01364048385610444 0.02331451557000446 -0.0908311840544546; 0.0100040484363635 0.019030909902958925 -0.07955482103497698; 0.002414752908254611 0.005132160076898132 -0.02355299342085822; 0.0004397190320258517 0.0008684419860077282 -0.005679826533420215; 0.0004397832170240142 0.0009804261415808807 -0.00508335219860587; 0.0006886783315654956 0.0016267039385538253 -0.008926795412234888; 0.0006867375185265001 -0.00019781239873084983 -0.0008033797086321145; 0.00026338131151811667 -0.00010916948166470036 -0.0005174902136162139; -0.00030924038158438205 0.0006676822127091929 -0.0010125021207888333; 0.0007211133652459711 -0.000794850781046559 -0.0024408992236711717; -0.0019306399541317958 0.0020736591463463255 0.0006211058599961987; 0.0003723683604853424 7.548138340196932e-5 0.000473845503503731; -0.0004511693530846854 0.0012873722180414045 -0.0005388582957041202; -0.0024321117776460593 0.001613723584365665 -0.0024942317799565693] %
+
+Mass Used: 71.45656024749542 kg
+Launch C3: 99.05642299181095 km²/s²
+||V∞_in||: 4.268922901228429e-6 km/s
diff --git a/archive/ES_0.556531582995979 b/archive/ES_0.556531582995979
new file mode 100644
index 0000000..0293914
--- /dev/null
+++ b/archive/ES_0.556531582995979
@@ -0,0 +1,22 @@
+archive/ES_0.556531582995979---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:21:40.940
+Launch V∞: [8.03395379250204, -5.625721930921176, -0.1406279425842048] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.142213479652676e-6, 0.00019359714693956975, 3.414968918650208e-6] km/s
+ V∞_out: [0.00018793368788181346, -2.8522683154150063e-5, 4.1514873507424774e-5] km/s
+ time of flight: 1.8749577787837255e8 seconds
+ arrival date: 2030-04-22T07:31:17.940
+ thrust profile: [0.34448032567503517 0.0055486098265934486 -0.10668036476725423; 0.08090504029787349 0.052731692558594966 -0.089250957821484; 0.0312458473489649 0.03266100604022304 -0.06456005502321865; 0.04592215797932021 0.06723063636111902 -0.14301279320373358; 0.02221849091902015 0.040162724271196375 -0.09639132187927564; 0.02734130311054363 0.0582401754159723 -0.13814708981297838; 0.011108099585297574 0.032549935604251054 -0.08860160121962099; 0.0061756112395086405 0.0196482169489059 -0.05810759344361841; 0.0008939357267174772 0.0034097301428762275 -0.010483596075923762; 0.0007883376985772833 0.002032144086646871 -0.007426300914164813; 0.00023819751857506564 0.0006380256781959644 -0.0017978487650684239; 0.00012202123058696108 0.0002182213531806477 -0.001552020710120906; -1.555892902791066e-5 2.213912295320915e-5 -0.0001440960424583899; -0.0005648801955748456 -4.666496201067942e-5 -0.00030040144772363177; 0.0005515745622139161 0.0006774359339200597 1.4013592638286914e-5; 6.378413721510855e-5 -8.441556143670026e-5 -2.5224334190725658e-5; 7.03328670414421e-5 0.00025167766302756965 -0.0007442741671696388; -0.0002784360869930505 0.0009233792883597506 0.0010530707339470066; -0.0009202264057296134 0.0002010972350258497 0.00031533215539107754; 0.00026953557722118567 0.0005537891109768289 0.00013122089195521895] %
+
+Mass Used: 88.04471431498723 kg
+Launch C3: 96.21293700234085 km²/s²
+||V∞_in||: 0.0001937983822331986 km/s
diff --git a/archive/ES_0.5565401324209176 b/archive/ES_0.5565401324209176
new file mode 100644
index 0000000..3712cba
--- /dev/null
+++ b/archive/ES_0.5565401324209176
@@ -0,0 +1,22 @@
+archive/ES_0.5565401324209176---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T08:59:19.919
+Launch V∞: [7.846043529637481, -5.547883986049704, 0.22388209034881196] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.298967328314606e-7, -7.049157509627124e-6, 1.3143967375886576e-6] km/s
+ V∞_out: [-1.1022687807100678e-6, 4.180415643921846e-6, 5.781113002609703e-6] km/s
+ time of flight: 1.874957778749363e8 seconds
+ arrival date: 2030-04-21T11:08:56.919
+ thrust profile: [0.7214681064622175 -0.0010234042589326955 -0.21622525626616515; 0.05401387431195058 0.03152337229256775 -0.06353410909040054; 0.04495251288336156 0.04283341218508466 -0.094402165357385; 0.027295193967455788 0.03432875737760303 -0.08736674953848764; 0.019963591384784835 0.03106659823675618 -0.08710615669704923; 0.0175618357216597 0.0323074818518318 -0.09845770501703788; 0.011637123534895566 0.024394627276479952 -0.08114993773259392; 0.008935152737108978 0.021354458015282636 -0.07472133777994235; 0.0037076022082561458 0.011489126284724552 -0.042927789539279344; 0.0004638051461079437 0.0010998517420530748 -0.005116644686585123; 0.0004608075396544559 0.0015629496425723106 -0.007207439116490563; 6.778819048570637e-5 0.0002009958853916606 -0.0009697203856545161; 8.702612726300943e-6 -0.00021095906910783698 0.00039776088281598843; -0.00026967423759457874 0.00013406284430163675 -0.0006705753570236613; 0.00019814099628560634 0.00011444832718985472 -0.00025793040768813284; 0.00013374590932479732 5.152971509576976e-5 -0.00014054755545086245; 4.266728826631624e-5 0.0001079008844231031 -0.0001658834983465072; -6.457546884154732e-5 -0.00042392112725055456 -0.00015320791097636572; 0.00011961248480315406 0.00043947246127158906 -0.00014552644831944422; -0.0004543875724634332 0.00020017939585861892 -0.00015321423584301833] %
+
+Mass Used: 110.35784376266793 kg
+Launch C3: 92.38953898201189 km²/s²
+||V∞_in||: 7.218517089159e-6 km/s
diff --git a/archive/ES_0.55654451298577 b/archive/ES_0.55654451298577
new file mode 100644
index 0000000..38bcb66
--- /dev/null
+++ b/archive/ES_0.55654451298577
@@ -0,0 +1,22 @@
+archive/ES_0.55654451298577---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:28:28.650
+Launch V∞: [8.037812666128195, -5.716914143815294, 0.09180894210455366] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0940740281490478e-6, -1.634444041977909e-6, 4.547669707851481e-8] km/s
+ V∞_out: [1.375443341217791e-7, -6.960285916519898e-7, -1.8353672245782962e-6] km/s
+ time of flight: 1.8749577787493402e8 seconds
+ arrival date: 2030-04-23T18:38:05.650
+ thrust profile: [0.25630006668519706 0.0035497773026104133 -0.08054432810145458; 0.04647057666316938 0.02815903914172977 -0.055076986316424326; 0.104421198286988 0.10225078701942919 -0.20514182760931804; 0.02745587498737056 0.03641398838061966 -0.0879696984032154; 0.012574338682557163 0.021282579459169584 -0.057687134112207834; 0.011502616953582607 0.02281096264859676 -0.06743613922111116; 0.00940166504038064 0.021180301578704267 -0.06839971665387022; 0.013988236136201882 0.037178571339162386 -0.11831130540114625; 0.003273755873035468 0.009877373902539071 -0.03581271880928895; 0.0004558238061495042 0.0014601707339677754 -0.004989181208725469; 0.00015378414088348952 0.0005332335019742642 -0.0018835772604907492; 0.00025066632443515504 0.001163102852134381 -0.004022678844242774; 0.00014897863938136726 -8.056549546231809e-5 -0.0014943705398528873; -0.00015534534961990452 0.00013203364188411524 -0.0014133137314034448; 0.0005494008981869287 0.00047189970035308663 -0.0010466979704048898; -0.00042914260628591994 5.4092150505904285e-5 0.0002270678426429249; 0.00041921192086781116 0.0010608079898523247 -0.00018286467773309537; -0.0010155750897009035 -0.004102090773527174 -0.0026409228600387377; -8.727641073657741e-7 -0.0002195849612748233 1.1326749636882821e-5; -0.004892672860703079 -0.002886484704739282 -0.002178126847261162] %
+
+Mass Used: 81.73044793536837 kg
+Launch C3: 97.29796866537657 km²/s²
+||V∞_in||: 1.967351883981241e-6 km/s
diff --git a/archive/ES_0.5565546677766434 b/archive/ES_0.5565546677766434
new file mode 100644
index 0000000..655bd8a
--- /dev/null
+++ b/archive/ES_0.5565546677766434
@@ -0,0 +1,22 @@
+archive/ES_0.5565546677766434---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:17:10.697
+Launch V∞: [7.960558859839496, -5.81218132824179, 0.2031639471288138] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.364532870114473e-10, -9.237926294289154e-10, -1.1899607377445182e-9] km/s
+ V∞_out: [9.829864467162396e-10, -8.978278474016799e-10, 3.349943735037466e-10] km/s
+ time of flight: 1.8584873955044118e8 seconds
+ arrival date: 2030-04-04T23:56:09.697
+ thrust profile: [0.281796317730554 0.0035578944011281245 -0.0981309288631762; 0.07197850316398101 0.04154159705130649 -0.09028817205100675; 0.041019215054681174 0.03766101717755272 -0.0922406388961462; 0.041398433721470326 0.05141467204442501 -0.13938613282870546; 0.033599251556794954 0.05063189616646789 -0.15002498738078643; 0.019140803205260126 0.03383835490102266 -0.1158184859001496; 0.005753944392123871 0.010629123441298544 -0.039642155779810784; 0.004517010462613611 0.008976956943823888 -0.03449435509876245; 0.0017942465801876585 0.00346822656017307 -0.014709303158498829; 0.0021937080871339614 0.005397794015081407 -0.02262140561801366; 0.0005970458981319754 0.0016592488576758445 -0.002774300863391975; 1.4131224728213595e-5 0.00032150338480031553 -0.002411560402493508; -1.3068930883800142e-5 0.0010642427278510268 -0.002709602836558975; -0.00033600587264888404 0.001794483604602102 -0.0028350342560888985; -0.0003289662261814681 0.0014992429661934978 -0.004753973790767484; 1.60471548665993e-5 0.0006512845119996866 -0.001192238536598981; 0.00025451410040416167 0.00019147089246690675 -0.0027138611580069688; 0.00033945422265559545 -0.003292849662324633 0.0011592734896702238; 0.0001420113758888907 0.0023167155981203315 -0.0016052420944680696; -0.0009807991317648862 -0.0019440836875478603 -0.0008269429290343332] %
+
+Mass Used: 82.35330140674068 kg
+Launch C3: 97.19322474274456 km²/s²
+||V∞_in||: 1.6353813518896267e-9 km/s
diff --git a/archive/ES_0.556556163662663 b/archive/ES_0.556556163662663
new file mode 100644
index 0000000..3b8b370
--- /dev/null
+++ b/archive/ES_0.556556163662663
@@ -0,0 +1,22 @@
+archive/ES_0.556556163662663---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T01:28:33.770
+Launch V∞: [8.04179596594882, -5.656312077555281, 0.14017514819275506] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7114891744389737e-7, -3.6625338405248423e-9, -1.9523950011168097e-9] km/s
+ V∞_out: [-1.2262271860674178e-7, 1.117926357475745e-7, -4.229210234462799e-8] km/s
+ time of flight: 1.874957778746887e8 seconds
+ arrival date: 2030-04-23T03:38:10.770
+ thrust profile: [0.3109916550987736 0.00421526403723875 -0.09868904395935292; 0.0745786120739447 0.04372488276329143 -0.08269007517803152; 0.05717348713138897 0.05461369884100724 -0.11547657616134185; 0.03386760740508124 0.04216448126760052 -0.10072996487230387; 0.023432356046979637 0.03568183425136902 -0.09698808276269011; 0.01830203633718197 0.033555058675541906 -0.09632866555137772; 0.011078047042023677 0.02236246870726954 -0.07330061596737847; 0.011002756693090211 0.02275476272612157 -0.07320722581630977; 0.0013713230789444352 0.00333262549312148 -0.013058929660574273; 0.003713673043816429 0.009652918388065042 -0.035455812917360746; 0.0006159950415898553 0.0019600628497426797 -0.008480172861858135; -0.0001586353122192724 0.001172145089588671 -0.0017622582627842354; 9.372228433090198e-5 4.696450870888755e-5 -0.0014585097721028725; -0.0013552660386849879 4.366333307399443e-5 -0.0010169616683525498; -0.0006737612579934748 0.0012952257207064861 -0.0005870697666725349; -6.82060182855659e-5 0.000497769581395495 -0.0006657177656108912; -0.003071872907930869 -0.00032385488332705727 -0.00200685519624004; 8.97911324778054e-5 -0.0015271768537861885 -0.0009640495022206197; 0.0018191702650936026 0.0018506938627982387 0.0005531318172459815; -0.001980406585398768 -0.0020524796521508787 -0.0013018354992649908] %
+
+Mass Used: 85.32553740499407 kg
+Launch C3: 96.68399774881932 km²/s²
+||V∞_in||: 1.7119923464370795e-7 km/s
diff --git a/archive/ES_0.556561971576535 b/archive/ES_0.556561971576535
new file mode 100644
index 0000000..2473830
--- /dev/null
+++ b/archive/ES_0.556561971576535
@@ -0,0 +1,22 @@
+archive/ES_0.556561971576535---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:22:05.377
+Launch V∞: [8.015441601193968, -5.742932495576314, 0.08218329100998124] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3133837741476357e-6, 4.773482073520629e-6, 1.2556367673379784e-5] km/s
+ V∞_out: [1.21982937039143e-5, 1.3495649289375206e-6, -5.618025269560119e-6] km/s
+ time of flight: 1.8749577787493387e8 seconds
+ arrival date: 2030-04-23T13:31:42.377
+ thrust profile: [0.22649110769197658 0.009171158605902745 -0.07464819354488979; 0.08014812160283565 0.0517411713450257 -0.09357351952305026; 0.09183548578746728 0.09964863015468606 -0.18377681503238774; 0.036864444225420935 0.04946072601469375 -0.1055958745871158; 0.022877905135324554 0.040385283956153685 -0.10126490009176954; 0.015565699423956315 0.03276555521180076 -0.08750375416644085; 0.007969378437554731 0.020523133599909753 -0.059314574025122406; 0.006431358689547693 0.017845373961321187 -0.05593276116704196; 0.0010216219937874361 0.00321980800182736 -0.010743033968268988; 0.00028387215076030654 0.00041839169935411634 -0.0029566366418799996; 0.0009489156500000367 0.003390102515762745 -0.013517605514190317; 0.00015689802378159078 0.0004189792044449245 -0.002853809845805144; 0.00020328021521999148 0.00031310755287784005 -0.0006417225014019752; 0.0004767522608580911 -0.00027023348485325096 0.0005575069041338581; 0.0013893307416377849 0.0009642511715610788 0.0010638666610946201; -0.001010244854626998 -0.0007365314309608767 0.0014178950161875367; 0.0037904481067923754 0.001072855514900291 -0.0010377948284761873; -7.098974962469135e-5 0.00011134826787845032 -0.001487911748978059; 0.0013024143858245904 0.001454733029220987 -0.0017298632995187092; -0.002306683173671736 0.0020671289220429243 -0.0022237360452489305] %
+
+Mass Used: 82.11619798134916 kg
+Launch C3: 97.23533180421856 km²/s²
+||V∞_in||: 1.3497165524417115e-5 km/s
diff --git a/archive/ES_0.556573197658165 b/archive/ES_0.556573197658165
new file mode 100644
index 0000000..fb6a035
--- /dev/null
+++ b/archive/ES_0.556573197658165
@@ -0,0 +1,22 @@
+archive/ES_0.556573197658165---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:51:53.914
+Launch V∞: [8.069328682840506, -5.659907228237256, 0.24788546501135172] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.303494370212776e-5, 4.690286354521501e-5, 0.003495774043059707] km/s
+ V∞_out: [-0.003054137747594749, -0.0010935346139959213, 0.0013070296603484252] km/s
+ time of flight: 1.8749577787493575e8 seconds
+ arrival date: 2030-04-23T15:01:30.914
+ thrust profile: [0.27973402021112004 -0.005428854002900839 -0.08689460239729498; 0.07528555866590338 0.0407237922325126 -0.08391199925110492; 0.053507089239749006 0.04824385651357362 -0.10882866065771005; 0.03378929754152989 0.04042872863645549 -0.10503676995189501; 0.020082915717149347 0.029350163735663647 -0.08967780145188121; 0.014396163763693326 0.02209199647380804 -0.07864021830479494; 0.012517708609977005 0.023916323718932046 -0.08225619398258692; 0.006364501847050874 0.013978328697726654 -0.04998485352571579; 0.003356455589136783 0.01266802036222171 -0.054723707262826216; 0.004197038039165393 0.008875568853784469 -0.03650338468495984; 0.0011909136167426618 0.0022615187576337475 -0.011889237139760287; 0.0006836946436482067 0.0010701993640584442 -0.0016252204157108847; 0.001117493572673339 0.0005132669358617006 -0.0010430395018144799; -0.0008739106666389153 0.0015332172760084083 -0.00084496303764149; 0.0012420066629598321 0.0005910840030805768 -0.0006271306037705098; -0.00038836833811304206 -0.00017212780287776395 0.0005945833146728022; -0.0007975963827409899 0.0017126313594613787 -0.0019325959921385515; -0.0006679864942780091 -0.0014492396949616583 6.606622190289898e-5; -0.0015279389809717797 0.0017853107951553062 4.278988414825277e-6; -0.00043412335277016303 0.0011824848629884669 -0.0017251941805105542] %
+
+Mass Used: 82.27669977277492 kg
+Launch C3: 97.21006242772873 km²/s²
+||V∞_in||: 0.0034970746118169064 km/s
diff --git a/archive/ES_0.5565751456251395 b/archive/ES_0.5565751456251395
new file mode 100644
index 0000000..b0d1009
--- /dev/null
+++ b/archive/ES_0.5565751456251395
@@ -0,0 +1,22 @@
+archive/ES_0.5565751456251395---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:41:51.767
+Launch V∞: [7.990868201035679, -5.657990499804398, 0.3509658270497388] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8268516864075187e-9, -4.259076923229039e-9, -7.287044538715488e-10] km/s
+ V∞_out: [-1.0465955506924694e-9, -1.9782656914284773e-9, -5.343325072509831e-11] km/s
+ time of flight: 1.874957778643729e8 seconds
+ arrival date: 2030-04-22T17:51:28.767
+ thrust profile: [0.3533131717746401 0.007016741623410331 -0.10503875334963561; 0.08898240519783134 0.05391549403377176 -0.0985282667177463; 0.07318464758893231 0.07200667174757999 -0.14576906842201284; 0.04293155484668983 0.05611758442554684 -0.12978951509853287; 0.023192268750197403 0.03718899091268738 -0.09713954385885293; 0.011290054611442817 0.021699283820756445 -0.06297858675468053; 0.009032278165552717 0.019137996035018992 -0.060849774820657246; 0.005262461983800163 0.015028835290546615 -0.04929820915575751; 0.0016319277729111058 0.006685399222822556 -0.02556449513700696; 0.0001956163361691724 0.0008653404132323172 -0.0038698785339293; 0.0015058583791536736 0.0053008162183756004 -0.021235602359917727; -0.0001307529346780449 0.0007292579108135354 -0.0003342451563802811; -0.00017000391433985356 0.00017304347389554884 0.0003771169175416256; 0.0005558944556537096 0.0008002026478303914 -0.0008670451540343148; 0.0012384394614626943 0.0014663139723940727 -0.0004077129063939014; -0.0007669396473875679 -0.0011214154771772113 0.0006514355161289205; 0.000983441367880495 0.0019404493379901913 -0.001872211196137471; 0.00015074727471314873 0.0005935013461072789 -0.0005225709752882145; -0.0003726095504326909 -0.0014661458446716485 0.003822508552477522; -0.00014707653147340988 0.0004203852001370647 -0.0027603656605388405] %
+
+Mass Used: 89.39595589791543 kg
+Launch C3: 95.9900081139567 km²/s²
+||V∞_in||: 4.691282714056398e-9 km/s
diff --git a/archive/ES_0.5566019691002949 b/archive/ES_0.5566019691002949
new file mode 100644
index 0000000..9632918
--- /dev/null
+++ b/archive/ES_0.5566019691002949
@@ -0,0 +1,22 @@
+archive/ES_0.5566019691002949---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T02:29:49.950
+Launch V∞: [8.021699044520817, -5.752221790435776, 0.06331268053948352] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002724969774579242, 0.0001915574377838364, 0.012530708805207832] km/s
+ V∞_out: [-0.011694795249521597, -0.003975707144540381, 0.00213316942489075] km/s
+ time of flight: 1.8749577787491933e8 seconds
+ arrival date: 2030-04-25T04:39:26.950
+ thrust profile: [0.28495651909375325 -0.01110513620576851 -0.1057923105682466; 0.07754327820716317 0.037204936740850326 -0.1014681248616661; 0.03202633356416473 0.023558354710407764 -0.07583949768371191; 0.039077218549460724 0.035868029051525877 -0.1322776091889598; 0.03308456834412289 0.03667129102460999 -0.14804838120989156; 0.01576914995465892 0.018692484605488807 -0.08808072802739021; 0.005237689191798305 0.006645808109634825 -0.035037516578579515; 0.007045163579496689 0.009639579541698761 -0.054962975848279555; 0.00402905071685159 0.005579785635051347 -0.03446419875880498; 0.0021803840096826293 0.0032375208141675813 -0.020303950012354955; 0.0007742263422909088 0.000942399866883276 -0.006413471997769904; -0.0006947182864249202 0.0006525191242631504 -0.0019591264000990995; 0.00020383918620010211 0.0009442447793243495 -0.00020614433584093558; -0.0002450954261624832 -0.000713066052057468 -9.071169538088985e-5; 0.00017115135912938918 -0.00034931664808378256 0.00013612174375342723; 0.0008716179606212026 0.00030601545839085834 -4.0663732936094005e-5; -0.00018984395856919316 -0.00016067107648134912 0.002031217914709764; -0.0014604416944170924 -8.862749599291452e-5 -0.00047864950456458113; 0.0038670380005153587 0.00043516518194716333 -0.002522561016813623; 0.00044385876894278303 0.0019823000769147014 0.002981311135618534] %
+
+Mass Used: 80.97059971765066 kg
+Launch C3: 97.43971958274744 km²/s²
+||V∞_in||: 0.01253513510160968 km/s
diff --git a/archive/ES_0.5566030253780648 b/archive/ES_0.5566030253780648
new file mode 100644
index 0000000..720a697
--- /dev/null
+++ b/archive/ES_0.5566030253780648
@@ -0,0 +1,22 @@
+archive/ES_0.5566030253780648---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T12:54:29.353
+Launch V∞: [7.940411401699258, -5.798359622045848, 0.27841415476697534] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7299936877637103e-7, -9.401878556238121e-7, -2.52140525853954e-6] km/s
+ V∞_out: [-2.465172826585612e-6, -3.057522155576826e-7, 1.2017494091329004e-6] km/s
+ time of flight: 1.854069445751736e8 seconds
+ arrival date: 2030-03-31T10:50:13.353
+ thrust profile: [0.38345324523940577 -0.019802145460117104 -0.13962708033693325; 0.029237921628554795 0.0131094357665232 -0.03899152504956072; 0.04061696050601256 0.02826889067230152 -0.09409871253329123; 0.03885037714472721 0.03377952085749483 -0.12850205083166202; 0.017733281905743047 0.01777177701712255 -0.07749548124146982; 0.016019598156171128 0.01762166556360027 -0.08553986938178387; 0.0181268868188106 0.021347514866929672 -0.11373180579080026; 0.010243548385921918 0.012936313831769882 -0.07559688416257251; 0.0057527338529088316 0.00797898348951781 -0.04651141518663286; 0.0027392100612239445 0.003957156973188231 -0.02596192425075911; 0.00033953997082292674 0.0006595748778703303 -0.005782831262959735; 3.828586765314375e-5 -3.209994683209483e-5 -8.591081451202685e-5; 7.055352467613303e-5 1.3823968097460398e-5 6.800157426123333e-5; 0.0005364269761424772 -1.8901425687211325e-5 -5.658675549176983e-5; 0.0001961894010663533 4.6271115586423345e-5 -0.0004014754484366048; 7.231067126098265e-5 -0.00014839680788879386 0.00034892200672088735; 4.135465490292684e-6 0.00014196859953809668 -0.00018796471685866078; -0.00018128634345278188 -0.0003293670985276228 -0.00013014394877180533; 9.298143419713899e-5 -0.00047220337698537454 -8.988241946283146e-5; 0.00016253290048842467 0.00028807141877465795 0.00016093321393334975] %
+
+Mass Used: 85.00323474551487 kg
+Launch C3: 96.74862197638186 km²/s²
+||V∞_in||: 2.704804306600691e-6 km/s
diff --git a/archive/ES_0.5566196881235399 b/archive/ES_0.5566196881235399
new file mode 100644
index 0000000..e146d7e
--- /dev/null
+++ b/archive/ES_0.5566196881235399
@@ -0,0 +1,22 @@
+archive/ES_0.5566196881235399---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T12:15:12.563
+Launch V∞: [7.837579504506408, -5.651101628075554, 0.17464123980530596] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.520475546668853e-9, -5.048781916466262e-9, -2.239447930265591e-9] km/s
+ V∞_out: [-7.077624693100557e-9, 6.3070155336211214e-9, -2.3853000288092817e-9] km/s
+ time of flight: 1.8749577787475702e8 seconds
+ arrival date: 2030-04-22T14:24:49.563
+ thrust profile: [0.6053039944130199 0.0006899223983952663 -0.17908680248824177; 0.07824515076541232 0.04530406523766394 -0.09041815146286514; 0.03704939744130535 0.034433376792606205 -0.0798368056376209; 0.030389311133733825 0.03752588706468662 -0.09701777029633042; 0.037061180318701016 0.056419375442668306 -0.15620984297216578; 0.016181549112010824 0.028785042536908396 -0.08893265086806065; 0.008853817404517744 0.01818737881183852 -0.06222247137252502; 0.006017268370323275 0.013824797290018457 -0.05069121757832976; 0.0016635294303925432 0.004162048125716102 -0.01638198897031706; 0.0010396985819251196 0.0029079742167220464 -0.012458045741272272; 0.00023911742926164398 8.337243513734734e-5 -0.002807887922373834; -0.0008446511956149831 0.001043152456373 0.0004143504620775265; 0.0001290758506746684 0.0020301544209029203 -0.004558993187405521; 0.0012654906711832032 0.001426230147861318 -0.00016450152997422017; 0.0007629146499373107 0.0009848740966167417 -0.0011013119301987167; -5.411168557033211e-5 -0.0020305450557182663 -0.0007470137314857116; 0.00014561595097220905 0.0005992818667116941 -0.0018166123477661874; -0.00026595043748572824 -0.0015559900660348657 0.0024792946116032515; -4.1853180493061856e-5 -0.0010997580093221656 -0.003032526400027948; -0.001302918284557079 -0.0019947119483244105 0.001449556553940436] %
+
+Mass Used: 104.59654311032591 kg
+Launch C3: 93.39310166293782 km²/s²
+||V∞_in||: 9.330749076063068e-9 km/s
diff --git a/archive/ES_0.5566315118638512 b/archive/ES_0.5566315118638512
new file mode 100644
index 0000000..c9ae068
--- /dev/null
+++ b/archive/ES_0.5566315118638512
@@ -0,0 +1,22 @@
+archive/ES_0.5566315118638512---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T13:53:20.094
+Launch V∞: [8.041924940015964, -5.758932806746821, 0.13694074362883282] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4162025723800402e-5, 9.974582223769057e-6, 0.0007107589462809278] km/s
+ V∞_out: [-0.0006188888055969824, -0.00023762775180590965, 0.0002557924496816423] km/s
+ time of flight: 1.8363980032475007e8 seconds
+ arrival date: 2030-03-09T00:56:40.094
+ thrust profile: [0.23577755687127958 -0.0071874630235881165 -0.07760623681214428; 0.051115311923208465 0.026697168524299694 -0.06074369468695647; 0.039827247082705325 0.03367302371107593 -0.08291636600406131; 0.034087758923255745 0.03703212145652103 -0.10300070007975447; 0.03629347207863677 0.04944954956705227 -0.14950741466760087; 0.028047317620275757 0.04393644358960109 -0.14262416180763152; 0.012926818532523011 0.020693717969065557 -0.07945182708103844; 0.005720610162085937 0.01185566556373241 -0.0478567256032916; 0.0060399125884840225 0.012932759031051082 -0.05372067493668958; 0.0011893583151980107 0.0021055945605056845 -0.01081166964896968; 0.00035709918053846454 0.0006242953885042862 -0.004617968565516032; 4.741652592622882e-5 0.00033765058195846806 -0.0022873744130346694; -4.999729439486968e-5 -0.00029305683868026584 0.00019101131357931783; -0.0004049802696953789 -0.0010158396956874722 -0.00012723247860394805; -0.00032236353625011917 0.0011532940768782477 0.00013449205096291265; 0.00015110315172121988 -0.00021038188423430702 -0.0008677258742379387; -0.0008270010419782249 -0.0016748546468864803 0.0026119882054554465; -0.00014382962492279975 -0.00011622591303514995 0.0003575368025516793; -0.0003820064502324071 0.0008937344837922788 -0.0006685198182215099; -0.0010161966401385097 0.0004249769492182886 0.0012122926030899072] %
+
+Mass Used: 78.57316712016927 kg
+Launch C3: 97.85661658074122 km²/s²
+||V∞_in||: 0.0007109699958377394 km/s
diff --git a/archive/ES_0.5566359069470939 b/archive/ES_0.5566359069470939
new file mode 100644
index 0000000..360a5fc
--- /dev/null
+++ b/archive/ES_0.5566359069470939
@@ -0,0 +1,22 @@
+archive/ES_0.5566359069470939---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T20:01:24.222
+Launch V∞: [7.844104700750875, -5.685696889322961, 0.12429450128392736] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8113314147765482e-8, 2.0763227832842053e-7, -4.043697943010353e-6] km/s
+ V∞_out: [-1.439112414411018e-7, 4.04007997940317e-6, -3.4969380301135396e-8] km/s
+ time of flight: 1.8749577787407386e8 seconds
+ arrival date: 2030-04-21T22:11:01.222
+ thrust profile: [0.47904973592489974 -0.0059497640515311 -0.10146226438449821; 0.12304660547924579 0.07704826521921315 -0.11976874123369669; 0.08385939419361975 0.08957972822831099 -0.15272283363699013; 0.03920625364067188 0.055979940902088944 -0.1102655399253754; 0.023787641489872956 0.0424426561902685 -0.09320083907659615; 0.01386127766272554 0.030594623132010834 -0.07291324233839369; 0.015848802889363033 0.04227253805355907 -0.10457770279845562; 0.003015790932561019 0.009664104271554282 -0.02666890397483311; 0.0009563481829160872 0.003679460059169262 -0.011007607291853181; 0.0006736102908860311 0.0026830989472972264 -0.008475958115613948; 0.0001963481450904652 0.0006604034300517031 -0.003896467969094072; -0.000304375294707966 0.0010635708111983524 -0.002710947094352519; 7.849988101404692e-5 2.421595483341005e-5 -3.130537130245246e-5; 9.114671640278289e-5 -0.0007167697761452519 0.0003517904060048758; 8.420045972397467e-5 0.00037467665658460895 0.00020746115803686505; 0.00031921642800553844 5.019138189595898e-5 1.1318952016248863e-5; -0.0008759289880445895 0.0006078383805912366 -0.0006310262417121862; -0.00016091674925177514 -8.464642494900594e-5 -0.0006931694187412353; 0.00016907598506836393 -0.00048286834162072277 0.00045097880196119937; -2.1263110252037263e-5 -0.0004757617945221036 0.0004283957098864278] %
+
+Mass Used: 101.81852679116173 kg
+Launch C3: 93.87257679664819 km²/s²
+||V∞_in||: 4.049122692107808e-6 km/s
diff --git a/archive/ES_0.5566410051309979 b/archive/ES_0.5566410051309979
new file mode 100644
index 0000000..5b2b0eb
--- /dev/null
+++ b/archive/ES_0.5566410051309979
@@ -0,0 +1,22 @@
+archive/ES_0.5566410051309979---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:54:42.676
+Launch V∞: [7.938889175808598, -5.721289888445549, 0.022394513678795636] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.126399601975315e-10, -1.0433104624834696e-9, 1.1888897396324165e-9] km/s
+ V∞_out: [4.708665918614242e-10, -1.5871095203584354e-9, 2.523624790658423e-10] km/s
+ time of flight: 1.8749577785991123e8 seconds
+ arrival date: 2030-04-23T11:04:19.676
+ thrust profile: [0.383255191431606 0.006364051421795901 -0.11434873060160713; 0.07912463966619467 0.04845184670090699 -0.0874636045875017; 0.059984359105638686 0.05947049867982226 -0.11917254469203618; 0.0312778536995542 0.041558097953147265 -0.09637082603274663; 0.019313731224357273 0.03249360000717824 -0.08518182341095097; 0.01550413260002561 0.03222965544980895 -0.08833115206101098; 0.012882996777312332 0.02933589022891076 -0.0893566660211954; 0.004032017462523549 0.010392579373723256 -0.03494303428819367; 0.0028209133770775436 0.00857952412250399 -0.029821922081028646; 0.0048288801257716125 0.01879364760570276 -0.06576677957090481; 0.00035088792497949017 0.0013884772173374021 -0.0054738182161113355; -9.802475811122548e-5 -0.0002198469876090715 -0.00016047119763963835; 4.095263611168657e-5 0.00024139813787700938 -0.0006865154087776684; -3.238169443340664e-5 0.0005984869055250656 -0.0004305075875650202; -9.589970261021581e-5 0.00023405388670229093 -0.0006315431296312886; -0.0003479669007502964 0.0005700827804409462 -0.0005213707418780502; -5.460411242763069e-5 -5.724666813058794e-5 0.0004728878171271616; 0.0001573301417603173 -0.0003809535382806675 -0.0007432804318140629; 1.1879169077862502e-5 -0.00029569931735530817 -0.0002791215432035887; 0.000255395136063786 -0.0021755543562233283 0.0017859358887216215] %
+
+Mass Used: 90.81671770824596 kg
+Launch C3: 95.75962084764312 km²/s²
+||V∞_in||: 1.7348807587269639e-9 km/s
diff --git a/archive/ES_0.5566428561477481 b/archive/ES_0.5566428561477481
new file mode 100644
index 0000000..4a4a697
--- /dev/null
+++ b/archive/ES_0.5566428561477481
@@ -0,0 +1,22 @@
+archive/ES_0.5566428561477481---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T03:06:50.129
+Launch V∞: [7.9904655745217115, -5.816567765993122, 0.11449806474032297] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1839950232741977e-6, -1.9303196860649243e-5, 0.000374325913271446] km/s
+ V∞_out: [1.3129786916845373e-5, -0.0003745486882505314, 3.986103624987299e-6] km/s
+ time of flight: 1.8325537600658333e8 seconds
+ arrival date: 2030-03-05T03:23:06.129
+ thrust profile: [0.26733204128291443 -0.011972022521882373 -0.0913859369837037; 0.026010295435686285 0.013008571561396934 -0.03198959628647852; 0.043145078536829334 0.03520214084364385 -0.09213774232149849; 0.0450254563607517 0.047746901798687444 -0.13906582061685477; 0.02820914779573896 0.03539732877796254 -0.11622688186879702; 0.02072819226425234 0.029902571346641385 -0.10783128493668631; 0.02261070872321436 0.03732842667152103 -0.14317395202459665; 0.004382582593660741 0.007973503663411268 -0.03399918952692313; 0.004163054127867918 0.008224005523697144 -0.03809726832256122; 0.0015642603055045744 0.003012204185371825 -0.01454430185627503; 0.0008630042021587069 0.0017748542290626503 -0.008850391559611022; 0.0004597312758080904 -7.08382389103411e-5 -0.0025008897672467003; 0.0010844825241997785 -0.0011336429994132893 -0.0006114373568926342; 0.0005133400318256399 0.00024610646563474886 -0.0012798616417332399; -0.0005800013960069496 -0.0003503376349496729 -0.000633589402142731; 0.00010344522438565652 4.969986130715185e-5 -0.0003057487889581071; -4.2506385365939533e-5 0.0009942840826732636 -0.0017574116641948107; -0.0002915727543048273 0.0001918456669195535 -0.00026025705353087565; 0.00018706150287576802 0.00025316263627356864 -0.004940150777385431; -0.0015121015527075029 0.0003673949892106 -0.0006822584770575116] %
+
+Mass Used: 79.54018770082894 kg
+Launch C3: 97.69311048083608 km²/s²
+||V∞_in||: 0.00037482965809792156 km/s
diff --git a/archive/ES_0.5566479544444931 b/archive/ES_0.5566479544444931
new file mode 100644
index 0000000..af43e34
--- /dev/null
+++ b/archive/ES_0.5566479544444931
@@ -0,0 +1,22 @@
+archive/ES_0.5566479544444931---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:18:19.976
+Launch V∞: [8.22228274449351, -5.597598839194058, 0.10311976635182629] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9080461413955825e-6, -4.576043672103551e-6, -4.2116436447718056e-7] km/s
+ V∞_out: [4.032219743383376e-7, -1.9303303188687217e-6, -5.067948747601904e-6] km/s
+ time of flight: 1.8749577787493822e8 seconds
+ arrival date: 2030-04-23T19:27:56.976
+ thrust profile: [0.1507464093575284 -0.005806061108263433 -0.05178179020083776; 0.0598956777416664 0.029562256692794255 -0.07253562295473165; 0.04659659031582911 0.03625023616085347 -0.10213228964291551; 0.03896074576226394 0.038430507615483916 -0.12499965837042105; 0.029781269226459017 0.034470832967047976 -0.12650474238802326; 0.01995960362384621 0.026088097789899976 -0.10596381473974946; 0.010712957986064022 0.015350198465501888 -0.06776744990857668; 0.0031033663442137207 0.00484213783659237 -0.023793991440736944; 0.00556599835709237 0.010315135102854 -0.04987607917719697; 0.0008882174573683374 0.002940809573806901 -0.012630694728898412; 0.0021019209213082053 0.004011876107618907 -0.02130229888388595; 0.00011707471248282404 -0.00171873040191374 -0.005389866734805; -0.001652190821183809 0.0005611033918384314 -0.0025214126542355427; -0.0009529643444098515 0.001977825719070183 -0.0024674085113502034; 0.000458542412733525 -0.002669493058904048 -0.0027982125538825097; -0.0014677624564369393 0.0019491802095511924 0.0015729429127106591; 0.00010722566829821704 0.0031122003777236985 0.0008960985430686605; 0.0014948300043769417 -0.0011052878859519435 -0.0001447979125189288; -0.002461993180315713 -0.00208772770905492 -0.0007086815958620063; -0.0003198513822096378 0.0006886754592786055 0.0010901545081734797] %
+
+Mass Used: 72.2161469618386 kg
+Launch C3: 98.94967998115486 km²/s²
+||V∞_in||: 5.438224661724648e-6 km/s
diff --git a/archive/ES_0.5566649265097492 b/archive/ES_0.5566649265097492
new file mode 100644
index 0000000..48ab9c9
--- /dev/null
+++ b/archive/ES_0.5566649265097492
@@ -0,0 +1,22 @@
+archive/ES_0.5566649265097492---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:59:04.699
+Launch V∞: [8.007726694066836, -5.807959821500304, 0.050459157128087836] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8772408276960644e-9, -1.7891960872883832e-9, -1.764199804967869e-9] km/s
+ V∞_out: [-1.2490400118900416e-10, 1.1471192638799688e-10, -4.031932806805117e-11] km/s
+ time of flight: 1.858207195874263e8 seconds
+ arrival date: 2030-04-04T15:51:03.699
+ thrust profile: [0.20948659426792093 -0.0017898138990686866 -0.06929011181409345; 0.06267736609353818 0.03506153375018133 -0.07464662557696294; 0.07194487759310975 0.06523631579495859 -0.1474574903502224; 0.03919102835453825 0.04607967152886098 -0.12294882865455656; 0.02920494873973127 0.041862417145525264 -0.12302077610690532; 0.018077796651428345 0.03158007048496003 -0.10190889603692828; 0.010411523992255494 0.01902533590082631 -0.06808577012509097; 0.005818377012796228 0.011644962464947988 -0.04675547281795458; 0.002657774259521834 0.007173029755624085 -0.027274705176681218; 0.00041289355110058303 0.00144009068721909 -0.005476056682891572; 0.0009711537829821616 0.0014224781487203971 -0.0006766952454176811; -0.00011281357661001041 0.001152156272819 -0.002006431422243606; -0.0010716246779233585 -0.00010096516584266648 -0.0011787221586741323; 0.00016984270344945729 -0.00020841084418043868 -0.0015695306656314057; 0.0006505271351262165 0.0008912565130458885 -0.0015010875067607253; 0.0009064680870055005 0.00014418849390883696 -0.0008313956316111332; -0.0032447065141557965 0.0004170115921594476 -0.005694954443637709; 0.002152012175048872 -0.001999842248483579 -0.0010507806718290736; 0.001544979026370806 0.0021755374496570477 -0.00744682637961073; 0.0003842094900643467 -0.00016043989743963743 0.0009091011505272812] %
+
+Mass Used: 78.60040463554606 kg
+Launch C3: 97.85863022157051 km²/s²
+||V∞_in||: 3.1365039001706553e-9 km/s
diff --git a/archive/ES_0.5566656530593772 b/archive/ES_0.5566656530593772
new file mode 100644
index 0000000..59599ea
--- /dev/null
+++ b/archive/ES_0.5566656530593772
@@ -0,0 +1,22 @@
+archive/ES_0.5566656530593772---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T09:20:45.201
+Launch V∞: [8.03164474568984, -5.660756092365264, 0.14036610384581372] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5643034593353657e-9, 1.0802732201654378e-7, -1.989510298581819e-8] km/s
+ V∞_out: [1.6143837356586498e-8, -5.980940190948019e-8, -9.120012046656326e-8] km/s
+ time of flight: 1.8749577787302303e8 seconds
+ arrival date: 2030-04-23T11:30:22.201
+ thrust profile: [0.3646464973400846 0.003314963117705491 -0.111198134811415; 0.03990776003824378 0.023195045441828453 -0.04553734021800423; 0.03441324122523432 0.032440157503424306 -0.07112127708412379; 0.020492324108308774 0.025694211898845503 -0.06294275184010177; 0.01736949519265385 0.026660797567646766 -0.07304004678621479; 0.029265746518435203 0.05116732441892097 -0.14642229170778878; 0.021667346973427662 0.05141504892589728 -0.1480258688486603; 0.009538801083310235 0.020833197571732215 -0.07067482893417819; 0.002371763531283131 0.006685299046152553 -0.02606988896828864; 0.0010796563316518126 0.0036727890495220406 -0.012824728725735321; 0.0008021951714490292 0.0029505353201491648 -0.011227925758170618; 0.0003827294977155395 0.001772395779259978 -0.006810045732728555; -0.0009340749302413917 0.0008084435846178947 -0.004126424200596689; -0.0005014600919308372 0.00167374627483513 -0.0014342324795519274; 0.0019788123836492577 -0.0009386910389569546 -0.0025897235204507146; 0.00041805543147595725 0.002116208520967775 -0.0008691671569942572; -0.0009079359912489536 0.001101747040749716 -0.0020362078973365323; 0.0003056413165263876 0.0028748123385527974 -0.00158243839076031; 0.0005727846303872901 -0.0015842189073324213 0.0007806033521290317; 0.0007729898851895373 0.0014722151016473327 0.0008955770458627609] %
+
+Mass Used: 86.11138147820202 kg
+Launch C3: 96.57117950132653 km²/s²
+||V∞_in||: 1.0985519773863796e-7 km/s
diff --git a/archive/ES_0.5566757164241564 b/archive/ES_0.5566757164241564
new file mode 100644
index 0000000..bcd9d77
--- /dev/null
+++ b/archive/ES_0.5566757164241564
@@ -0,0 +1,22 @@
+archive/ES_0.5566757164241564---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:42:53.946
+Launch V∞: [8.133959146727136, -5.595936315362565, 0.17069887576260323] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.018323123841793e-7, -1.2894367178781934e-6, 2.9553103504161527e-5] km/s
+ V∞_out: [1.3805668870456881e-6, -3.3017244751319295e-5, 2.5004285592816633e-7] km/s
+ time of flight: 1.8749577787422088e8 seconds
+ arrival date: 2030-04-22T18:52:30.946
+ thrust profile: [0.27197547009129297 0.0024423430401138155 -0.07434935761521821; 0.05522130085621816 0.03414441827796581 -0.063284723537832; 0.02790562530616654 0.029077805028447392 -0.06119228982605035; 0.041764585334267475 0.06273975566688157 -0.14775325747276888; 0.015214967577598968 0.026765273896159892 -0.06868044799468953; 0.022667490060432425 0.04492544985801959 -0.11942615105644182; 0.009873364763180714 0.020413529904226194 -0.06582976387290905; 0.007343403139216577 0.019071604239225305 -0.060058023327490315; 0.008793547334647142 0.026595870451228958 -0.08666915111797112; 0.0017732111057531946 0.006162720504552517 -0.022524817496734212; 7.264101226903603e-5 0.0011843333286195518 -0.003454994701542673; -7.639769533259349e-5 0.00037080107641483304 -0.0006680532378057328; 0.00016283870081218818 0.00011552889225446161 0.00018587025767406447; -3.93696390902824e-5 0.0003482692776681049 -9.417618196555939e-6; 0.0005314195025936093 0.00027230777288923737 -0.0013426004650639455; -0.000720754380656012 0.00046990069101281255 -0.0011512789127675956; -0.000305532835075484 -0.001043956531780365 -0.0010643098554722966; -0.0008848926375048442 -0.0005594766836664048 0.0007661253788908655; 0.0005847555587812916 0.002245471583456533 -0.003397497268674377; 0.000492997584264017 -0.0013189643724220777 -0.0005550832599703818] %
+
+Mass Used: 80.6762281058127 kg
+Launch C3: 97.50493275240623 km²/s²
+||V∞_in||: 2.958190849251311e-5 km/s
diff --git a/archive/ES_0.5566813694959446 b/archive/ES_0.5566813694959446
new file mode 100644
index 0000000..63db305
--- /dev/null
+++ b/archive/ES_0.5566813694959446
@@ -0,0 +1,22 @@
+archive/ES_0.5566813694959446---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:21:17.174
+Launch V∞: [7.933540560712075, -5.633563947364451, 0.14346276363638885] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0010106852948599196, 0.00671336935810581, 0.006570517911830195] km/s
+ V∞_out: [-0.0015800105823609563, 0.001284501093670654, -0.009229593917173078] km/s
+ time of flight: 1.8749577787448955e8 seconds
+ arrival date: 2030-04-21T17:30:54.174
+ thrust profile: [0.44711582363968533 0.009547940273218277 -0.12321417980388562; 0.06992953128480452 0.04454400877720682 -0.07261481478354868; 0.11204171646546965 0.11682716563634038 -0.19720879962738053; 0.028522921858092746 0.03998837924647252 -0.08219372045631777; 0.014395532567849012 0.024315713770828338 -0.05555324917231866; 0.01458942621530391 0.029008914689985087 -0.06813343072876551; 0.011128870028833083 0.030063102195339107 -0.07311924444387435; 0.0125656881116821 0.040630056884393355 -0.10624932980972945; 0.0019773679850939715 0.008706060358203628 -0.027466826347249125; 0.000537850507274722 0.0024532110686676725 -0.008152786134623734; -5.990515771390375e-5 5.755173296217904e-5 -0.0001697759054218209; 4.124950151654232e-5 0.00017439237191695252 -0.0005891566308346598; 0.00027443753981798457 0.0008854784860894092 -0.0027984448215677264; -6.231461086152266e-6 0.00015105797753297843 -7.917506987878203e-5; -0.00018824896052186337 0.00032110457720606073 -0.0003178756230636566; -4.476575611964591e-5 -0.00013702264653702437 -0.0002978929999793607; 0.00018085237316563198 0.00015446619466306423 -0.0003187667243212166; -3.001640081576226e-5 5.3306153466494484e-5 -6.74227702887187e-5; 1.5565237599787573e-7 -7.341094958404939e-5 0.00016015796061190585; -2.1597586489482783e-5 -5.029919902491348e-6 5.2195835667332585e-5] %
+
+Mass Used: 97.05257191659484 kg
+Launch C3: 94.69869014205838 km²/s²
+||V∞_in||: 0.009447884341654566 km/s
diff --git a/archive/ES_0.556686708262119 b/archive/ES_0.556686708262119
new file mode 100644
index 0000000..3221c45
--- /dev/null
+++ b/archive/ES_0.556686708262119
@@ -0,0 +1,22 @@
+archive/ES_0.556686708262119---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:18:17.121
+Launch V∞: [8.210937277650453, -5.615709865831107, 0.050031696064599805] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3360849412951574e-9, 1.7681659612522372e-9, -1.3461866497399593e-8] km/s
+ V∞_out: [-4.001438088443357e-9, 1.3361971835744392e-8, -2.0632307514531503e-9] km/s
+ time of flight: 1.8749577787489948e8 seconds
+ arrival date: 2030-04-24T01:27:54.121
+ thrust profile: [0.16444933181177884 -0.004662077550327568 -0.06040063391799477; 0.041949659961277565 0.0217735574099636 -0.05446073392723116; 0.04093199854992218 0.033199544494032514 -0.09392295738903571; 0.03720897427399236 0.038398672899321466 -0.12445779173051101; 0.02940251612678629 0.03597937290195371 -0.13085048154256848; 0.020358922033292988 0.028649028754936638 -0.11465642935050017; 0.01164080477467494 0.018911716456843156 -0.08153357301352489; 0.005161751934058415 0.010105444684283786 -0.04583532272056799; 0.0017581815429288487 0.004790658109147385 -0.020650350985080935; 0.0022659553644219536 0.0037176562803789334 -0.01927997716694604; 0.0008687365020002341 0.0021910404602396836 -0.01314000805710749; 7.185577158402544e-5 -0.00019364187102850728 -0.004702965987461221; -0.000470574785939355 0.0002544287851584739 -0.0016691125350253692; 0.0012594897636153454 -0.00012451669617155462 -0.0006670722928079495; 0.0022147799921294832 -0.00023042239068921805 0.0003281223055588264; 6.874529562109742e-5 0.00041299282663782546 -0.002393408094518059; -0.003046569200696794 -0.002911892373096591 -0.0008190324496920507; 0.0012286606307986576 -0.0020672335131915395 -0.0015412653156104258; -0.0012933584541763876 -0.0031624892453944843 1.193074294263271e-5; -0.001012106883075078 0.007922253305325708 -0.0033867139384265834] %
+
+Mass Used: 72.2117095414751 kg
+Launch C3: 98.95819144531377 km²/s²
+||V∞_in||: 1.3776993623911083e-8 km/s
diff --git a/archive/ES_0.556687434282946 b/archive/ES_0.556687434282946
new file mode 100644
index 0000000..6c04a84
--- /dev/null
+++ b/archive/ES_0.556687434282946
@@ -0,0 +1,22 @@
+archive/ES_0.556687434282946---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:16:18.426
+Launch V∞: [8.039788652262494, -5.6939766753431345, 0.08847774225014597] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3620862758944222e-6, 4.714752859545077e-6, 1.3457093084522173e-5] km/s
+ V∞_out: [1.265225652309952e-5, 1.5260190685056685e-6, -6.540354736410248e-6] km/s
+ time of flight: 1.8749577787493438e8 seconds
+ arrival date: 2030-04-23T01:25:55.426
+ thrust profile: [0.23874820157433307 0.0053740263113093165 -0.07418146084576127; 0.08209605134520097 0.05106099255798661 -0.08720256999841865; 0.08610537185126017 0.0879132506535206 -0.16230366751054243; 0.03906653583951235 0.053103248880523056 -0.11368823995576957; 0.03349148348807441 0.05692185272146889 -0.13361218277058873; 0.015056419383443676 0.03079969515549298 -0.07944607402122561; 0.006101914873377614 0.015254781178242832 -0.041716566416597614; 0.006800222089385127 0.019133496715888383 -0.05587281422909873; 0.0012795057679044408 0.005808032810924066 -0.016905448360403932; 0.000446519129666132 0.0020795106517234475 -0.005905538056869538; 0.0006523253724172475 0.0014803212573294847 -0.0043774172516640895; 0.0011183049247911552 -0.001824914463423936 -0.0030648277327617593; 0.0005501331296086623 0.0003788379927661267 -0.003766605482397336; 0.005013985001249366 -0.002238944412689567 -0.0012159451207836693; -0.0020335053264804483 0.000816521221359233 -0.0035956562207755042; 0.0023214293856843697 -0.0011978870284915198 -0.0031790278935517257; 1.1793897073729713e-5 -0.00027705262429692564 -0.0037119591201199495; 0.00040830704634975954 0.00022353433297633883 -0.0019925199566566162; -1.051020492624918e-5 0.00041272055467148766 -0.001229762708312973; 0.0021742450431631224 -9.626271573009862e-5 -0.0007575452746793601] %
+
+Mass Used: 83.24217179433799 kg
+Launch C3: 97.06740026327411 km²/s²
+||V∞_in||: 1.4324019262590472e-5 km/s
diff --git a/archive/ES_0.5566914218323817 b/archive/ES_0.5566914218323817
new file mode 100644
index 0000000..4b9efac
--- /dev/null
+++ b/archive/ES_0.5566914218323817
@@ -0,0 +1,22 @@
+archive/ES_0.5566914218323817---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:40:47.612
+Launch V∞: [8.159906643507322, -5.565970183601232, 0.12546751436829423] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3689067395001908e-7, -2.009041232143948e-6, 3.6728304872507586e-7] km/s
+ V∞_out: [-3.1498635072161414e-7, 1.1521184168576734e-6, 1.6613281284732621e-6] km/s
+ time of flight: 1.8749577787480274e8 seconds
+ arrival date: 2030-04-22T21:50:24.612
+ thrust profile: [0.27631302269267505 -0.0016669015436635896 -0.09084897160839502; 0.040227440183402616 0.02244992706285571 -0.04880373913099234; 0.04668057970890209 0.040985617673847376 -0.09949176231986875; 0.038843788938931444 0.04618997988536466 -0.12486859598790885; 0.027276154905689378 0.03840323953514441 -0.11737301481315054; 0.01571429490910782 0.026143129529020214 -0.08865336716228543; 0.012487295633321351 0.022790139281131515 -0.08308299214872665; 0.008159981845477633 0.01691630925176721 -0.06617352946887349; 0.005193826163549197 0.010273775295013839 -0.04106087707613193; 0.0003870757958859502 0.000964080959189453 -0.004168076404630213; 0.0008283274558781274 0.001572099074257741 -0.005521930369562776; 0.00016328117869377423 0.00029479691694395734 -0.001969038665947937; -3.782033485239108e-5 0.00010440097683426662 -0.0009077793588152618; -0.0014074618958502018 -0.0012889089214725398 0.00019747904369540425; -0.0014602173784179035 0.0018081118375159347 -0.009250403382474874; -0.0031611670871243987 0.0016522404589035462 -0.006020553965736968; 0.0003119459814952862 0.0007774207987454131 -0.004335234368114971; 0.0005499679865434994 0.0006277465789059889 -0.001046494603410554; 0.0007306248540777455 -0.0009738118376293042 -0.003487924999966856; -4.646012997554954e-5 0.0012444264697074455 -0.0006476130122376508] %
+
+Mass Used: 80.25757689729335 kg
+Launch C3: 97.57984261265462 km²/s²
+||V∞_in||: 2.0560303260749226e-6 km/s
diff --git a/archive/ES_0.556693954810985 b/archive/ES_0.556693954810985
new file mode 100644
index 0000000..c589c0e
--- /dev/null
+++ b/archive/ES_0.556693954810985
@@ -0,0 +1,22 @@
+archive/ES_0.556693954810985---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:34:19.657
+Launch V∞: [7.934867025487971, -5.767868018800573, 0.0438668806909977] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2211505081222337e-6, 1.8872868991772588e-5, -3.5944742912113395e-6] km/s
+ V∞_out: [2.856790529320816e-6, -1.0599334073104502e-5, -1.5029484843103546e-5] km/s
+ time of flight: 1.8420914126354662e8 seconds
+ arrival date: 2030-03-15T16:46:40.657
+ thrust profile: [0.37506764755285404 -0.008318286140203999 -0.1262204106184834; 0.05108765453372539 0.027626149821552003 -0.06205033432471785; 0.03750376580529212 0.03285968433886196 -0.0815079614987811; 0.047035395677418136 0.05418107130372945 -0.14746621917103353; 0.03466127900594773 0.04853798156235666 -0.1463827136231242; 0.011620555194159865 0.01884833487695124 -0.06432941009677608; 0.006469089696393894 0.01187286798473986 -0.04384927780938856; 0.011545707708670666 0.024809819646506935 -0.09327192843133884; 0.0042353656629290064 0.009749547721036695 -0.04162420237035332; 0.0019540707566769546 0.005364688551303599 -0.02381054707747047; 0.0007434007247320615 0.001921366605500406 -0.008298672972685973; 0.0006418776408793609 0.0018344902491386904 -0.008806633175818663; -0.0007420314894348741 -0.0005362555595632393 -0.0005262168704933594; 5.0518102181081596e-5 -0.0006178185274587208 -0.0005837203099974528; -4.936240599308161e-5 -0.00012165450532257243 0.00016128627748827147; -0.0005046571715741714 -0.0010362643581235782 -0.0006934367430333048; -0.0004045136755746275 0.00028176056372206337 -0.0003025426831114198; -0.0007345261095208861 -6.415031005822917e-5 0.0001540687175538586; 0.00020461512920365098 1.8588815515834352e-6 0.00041804721952046165; -0.00013458755850398154 0.0014956200726316132 0.0003783136681684444] %
+
+Mass Used: 88.1209610428973 kg
+Launch C3: 96.23234049770033 km²/s²
+||V∞_in||: 1.9340086323243805e-5 km/s
diff --git a/archive/ES_0.5566941660750362 b/archive/ES_0.5566941660750362
new file mode 100644
index 0000000..211fd30
--- /dev/null
+++ b/archive/ES_0.5566941660750362
@@ -0,0 +1,22 @@
+archive/ES_0.5566941660750362---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T01:58:02.568
+Launch V∞: [7.951677713203706, -5.566022981042178, 0.23762683285748656] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.444200979710117e-6, -6.023476210815145e-6, 1.0713133204314155e-6] km/s
+ V∞_out: [-9.581349601794992e-7, 3.6506005978057216e-6, 5.027359572293955e-6] km/s
+ time of flight: 1.8749577787493068e8 seconds
+ arrival date: 2030-04-22T04:07:39.568
+ thrust profile: [0.5562611282967207 -0.006559039607227894 -0.161611149613492; 0.0525516210917335 0.029655381335413837 -0.0633553330688502; 0.05394641596828316 0.048860522534795885 -0.11272289845511806; 0.023182940291047116 0.02694862547041718 -0.07378599697929664; 0.02405510549258132 0.03626062751813803 -0.1024555099659654; 0.01477082781472045 0.02570730634009932 -0.0821534261511778; 0.007957072509201165 0.015346306620610317 -0.0543626276548184; 0.01510598110037829 0.030481662403695334 -0.11065884133689584; 0.005968687358478782 0.013983286420603949 -0.05747782037176957; -0.001086438639253237 8.575046824168002e-6 -0.0028840515933220637; -0.0007985781387333168 -0.000902595082652334 -0.0016085169671143187; -0.0005729824038799185 0.0018761054839033255 -0.0030240733739625323; 5.20085015653938e-5 0.0004654538785918478 -0.0017153994233838896; 0.0004552536338477851 -0.00072180235735298 -0.00013118975193806702; 0.0006782365611166872 0.0008921842632961006 1.4677013481626292e-5; 0.0009239347633101203 -0.000516138242245014 0.0012743989165617572; -0.0004570365917504146 0.0012618910978514687 -0.0011624223571139972; 3.075406552338305e-5 0.00017354198231468298 -0.0008216536985661195; -2.3663325951841778e-5 -0.00018196240215658655 -0.0020823786600055482; -0.00033778877809103615 0.001203894532005604 -0.00040019989844066145] %
+
+Mass Used: 99.59002913511858 kg
+Launch C3: 94.26625679184406 km²/s²
+||V∞_in||: 6.286150997437575e-6 km/s
diff --git a/archive/ES_0.5566993719336064 b/archive/ES_0.5566993719336064
new file mode 100644
index 0000000..f7f0006
--- /dev/null
+++ b/archive/ES_0.5566993719336064
@@ -0,0 +1,22 @@
+archive/ES_0.5566993719336064---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T22:24:47.812
+Launch V∞: [7.908514595732039, -5.689813489739828, 0.20706574695180052] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00010265042048802006, -7.982157947845489e-5, -7.530806757153221e-5] km/s
+ V∞_out: [-1.3142890002172777e-5, 9.425667852452337e-5, -0.0001159937033732057] km/s
+ time of flight: 1.874957778779079e8 seconds
+ arrival date: 2030-04-22T00:34:24.812
+ thrust profile: [0.3738618705822349 0.010852223688084047 -0.09712743077414895; 0.17013879916445615 0.108231338923921 -0.1584593990512569; 0.03259003628965468 0.03483510921234817 -0.06368062114453465; 0.06782871151906349 0.10031867049699296 -0.1827162375547689; 0.011769454917278375 0.02174614787898914 -0.048541882606280694; 0.01814243695591284 0.04181226680307449 -0.09766044559197512; 0.008433731631754279 0.02333626375979764 -0.05988151871516989; 0.006185242037144203 0.020054056278420312 -0.05297181383502852; 0.002201215925351586 0.007848317889080863 -0.02209418453603329; 0.0008966049953313654 0.0038442676970082876 -0.011546387790883869; 0.0010200921061937615 0.004420636119573773 -0.013376358023517972; -0.00031989647756589 0.00044895063065568814 -0.0004727027064108677; 2.0499147787555835e-5 0.0006802673013079653 -0.0005466252179510265; 0.0004560149349056612 -0.00022754693892321527 -0.0005614191870366335; 8.099858333765485e-6 2.4314457912922216e-7 0.0001687014311677843; -6.105982001170894e-5 -0.000159036695619466 -0.0003369303152440654; 7.470563517168944e-6 1.562897908034639e-5 -4.8345734593585165e-5; 6.498352652262228e-6 0.0004977253666507181 -0.0002918264213063829; -0.0001722986985016203 -7.87929037360033e-5 5.32188611975936e-5; -0.0002785799952268652 0.00022646340461377878 0.0001528375209590494] %
+
+Mass Used: 95.5407687746665 kg
+Launch C3: 94.96145688249274 km²/s²
+||V∞_in||: 0.00015026609204395075 km/s
diff --git a/archive/ES_0.5567060087197306 b/archive/ES_0.5567060087197306
new file mode 100644
index 0000000..0641840
--- /dev/null
+++ b/archive/ES_0.5567060087197306
@@ -0,0 +1,22 @@
+archive/ES_0.5567060087197306---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T13:37:32.400
+Launch V∞: [8.03675772505602, -5.730340381045582, -0.05354438886473433] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8486694041445924e-9, -1.6799348805208775e-9, -2.902623509060069e-9] km/s
+ V∞_out: [-1.1778511054679122e-10, 4.249342386954814e-10, -6.545851900870255e-11] km/s
+ time of flight: 1.8749577782180247e8 seconds
+ arrival date: 2030-04-24T15:47:09.400
+ thrust profile: [0.2775008349454669 -0.006479518104315044 -0.0927550540825407; 0.06882072815445903 0.03552041466843489 -0.08289356073135679; 0.03582941402394861 0.029734407561025175 -0.07860569882123708; 0.03220851922629351 0.03452544903944146 -0.10471260851588103; 0.01841917493866358 0.024030130614874284 -0.08038282527209882; 0.03530020130044689 0.05186417659650679 -0.18616749662815832; 0.013412010230020014 0.01989530871480375 -0.08227890960835879; 0.005304134401866167 0.009842151901773987 -0.04093044399694134; 0.0015077661572673114 0.003110540260061978 -0.014074263590529426; 0.0013773208054345865 0.0028849361072482847 -0.01576929326225288; -0.00048553895028502275 -0.00012959732256069426 -0.005461088650712352; -0.0016752873606700972 0.0013774734410030593 -0.0016601944290567062; 0.00016696719684283464 -0.00032414680674471615 -0.002150335400307397; 0.00013419747051182207 0.0006136708810681884 -0.002749817924378244; -0.00016446292834304543 0.0021375940821832433 -0.0019958190498081977; 0.0005863300252337858 0.00010553370379102773 0.0008445504664600333; -0.0033363973595943895 -0.005063865010159231 -0.0033644646037231307; 0.002266426451912092 0.0021440489155019303 -0.001210320099489591; 0.0008778035548811519 0.0018150701776709559 -0.0005666226314813001; 0.0015987139247649468 0.0033345856348718384 0.00160835105923983] %
+
+Mass Used: 81.15367824945497 kg
+Launch C3: 97.42914261546814 km²/s²
+||V∞_in||: 3.8294886086733834e-9 km/s
diff --git a/archive/ES_0.5567282644022926 b/archive/ES_0.5567282644022926
new file mode 100644
index 0000000..653d124
--- /dev/null
+++ b/archive/ES_0.5567282644022926
@@ -0,0 +1,22 @@
+archive/ES_0.5567282644022926---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:44:06.606
+Launch V∞: [8.083952027543507, -5.793557489447548, 0.1613725353728144] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.78012954051054e-5, 4.8514010998757816e-5, 0.0033553802593081308] km/s
+ V∞_out: [-0.003014086499950649, -0.0009793305626167386, 0.0011054279594046213] km/s
+ time of flight: 1.8387999093484792e8 seconds
+ arrival date: 2030-03-13T00:30:36.606
+ thrust profile: [0.1616772589284229 -0.009271023314156192 -0.06051389582079435; 0.049302206670705805 0.023072024916695816 -0.063211579280798; 0.04156767065894115 0.030692759327555736 -0.09433276654872193; 0.035167032959700834 0.03282539800169104 -0.11506761316034007; 0.027420442976143475 0.029932913399260016 -0.11792402735473695; 0.016654218145912957 0.020242776859532848 -0.08952144188462932; 0.012561170616344177 0.01731282493726441 -0.0802014299342283; 0.013861461985626402 0.02000693304370229 -0.10113879148634769; 0.004778092465971631 0.007318031550784841 -0.040169695661300235; 0.002716041742533553 0.004156579678873574 -0.023200227770736007; 0.0006093845492741475 0.0009225391202047017 -0.00621300216414867; 0.002105103236812151 0.0032304245301150495 -0.020256652189877124; 0.00012977488261115095 0.00035114910936799923 -0.0014051865849326905; -3.418005082316686e-5 -7.332359826028125e-7 -9.288612210416676e-7; -8.212070571746444e-5 -3.729286931836341e-6 -9.947787350068607e-5; 0.00010729886853929208 -1.9588409189492012e-5 0.000196864170363329; 0.0002616723489117656 -3.091624044482261e-5 0.0002165970556555703; 0.00022588637667151978 5.703930736309389e-5 -0.00013706098970280644; 4.888778578136381e-6 8.500680159766337e-5 -0.00016620196881944529; 0.0001863499104640938 6.011999878862223e-5 8.134874524348161e-5] %
+
+Mass Used: 72.35680093907604 kg
+Launch C3: 98.9416298623312 km²/s²
+||V∞_in||: 0.003356415842751982 km/s
diff --git a/archive/ES_0.5567388083291602 b/archive/ES_0.5567388083291602
new file mode 100644
index 0000000..c9d9d6b
--- /dev/null
+++ b/archive/ES_0.5567388083291602
@@ -0,0 +1,22 @@
+archive/ES_0.5567388083291602---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T21:49:12.918
+Launch V∞: [8.115166878930387, -5.637115282123151, 0.12369973068387127] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2025543153821452e-6, -1.7481429561788324e-6, -1.7737184390032894e-7] km/s
+ V∞_out: [1.4205338326733992e-7, -7.659422950187606e-7, -1.981768682985992e-6] km/s
+ time of flight: 1.8749577787493756e8 seconds
+ arrival date: 2030-04-23T23:58:49.918
+ thrust profile: [0.2849815353699612 -0.005035933425187356 -0.0976177342009599; 0.03081829158442058 0.015909806286110238 -0.03710529709196668; 0.027674005766729168 0.022437852796925218 -0.05959205962445651; 0.037246853033340376 0.03830995323524844 -0.11726356662354923; 0.04750526759547393 0.05822697031518707 -0.19738936001474966; 0.016279985422723704 0.022591663603694915 -0.08547142086538666; 0.011035889300596895 0.017029136867945667 -0.06991834416960188; 0.00930050581464454 0.01575000270279761 -0.06941897423220227; 0.000761107902541936 0.000890101468227836 -0.005810599649845885; 0.002243205843904727 0.0029461535943551835 -0.016649970197395024; 0.000890401459555441 0.003953080519785795 -0.01738466726186927; -0.0004154360710248824 0.0009334716483596071 -0.000845920102036365; -0.0010264998317835925 -0.003714291299344607 -0.002576768260450484; -0.001962589655081077 -0.0013187319501735146 -0.003332401265307339; 0.00010089784305719162 0.0005284523652964699 -0.0021805723465868738; -8.958676208164077e-5 -0.0011637183822226372 -0.002356250432539136; 2.1218071716276363e-5 -0.0003270244955170026 -0.0008682467402504595; -0.0008155682192557045 0.0005732549641255856 0.00596619582809831; -0.002988557575777041 0.0024733667259538017 -0.00023222302303013524; -0.0010859800463898324 -0.0013553323801445178 0.007501103444003338] %
+
+Mass Used: 79.9135042161497 kg
+Launch C3: 97.64830380020638 km²/s²
+||V∞_in||: 2.1292255511548066e-6 km/s
diff --git a/archive/ES_0.5567394375060006 b/archive/ES_0.5567394375060006
new file mode 100644
index 0000000..91b838a
--- /dev/null
+++ b/archive/ES_0.5567394375060006
@@ -0,0 +1,22 @@
+archive/ES_0.5567394375060006---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T16:51:18.025
+Launch V∞: [7.989022021545044, -5.875444044984834, 0.2681490049434584] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4322362938234669e-6, -3.419437197418909e-5, -5.998657211775617e-7] km/s
+ V∞_out: [-3.356313791554214e-5, 4.782195281223141e-6, -7.412153659309689e-6] km/s
+ time of flight: 1.8431923654381853e8 seconds
+ arrival date: 2030-03-19T00:38:34.025
+ thrust profile: [0.22840357101465492 -0.009794569980406793 -0.08246168901157727; 0.026269647807674053 0.012125567840983897 -0.03378577049977338; 0.03629478549487937 0.026124416332102923 -0.08171105426671012; 0.05416173450275137 0.05041262393502468 -0.16966790726636094; 0.03480082112963765 0.03711855318677577 -0.14318285230604375; 0.01706308129058297 0.02068188630597357 -0.09281096214092868; 0.01318846835061554 0.015821082143691274 -0.08275474086827993; 0.009395123040928008 0.013206670218299753 -0.06860714112287107; 0.005243633785912005 0.007932543449784892 -0.03848084380266947; 0.0003863972790801417 0.0007474660386001787 -0.003212010351116081; -0.0002692075372212925 0.0005497432992243895 -0.0017351422806212106; 0.00026702920283432763 0.0004686786282593304 -0.0027813050736971365; -9.830882520963182e-5 -0.00012142323385299928 0.0004751781956140531; 0.0005402986457601075 -0.00029645545610751194 0.0005159536648485345; -0.0007331099681194892 0.00022873674215605588 -0.0008611378742661376; -0.00022176445746241373 8.955568954260049e-5 -0.00206525664311868; 3.7897979195583944e-5 3.790242714343285e-5 -0.00029590565021027327; -0.00044628071726483527 -0.0008469023386473312 -0.0003715218473878013; -0.0012865546025796087 -0.0009045070010721537 0.0005916869918767217; 0.001932822544997883 0.0010097674313260126 0.001116885008461627] %
+
+Mass Used: 75.42889681756651 kg
+Launch C3: 98.41721947533158 km²/s²
+||V∞_in||: 3.422961019927042e-5 km/s
diff --git a/archive/ES_0.5567491638106882 b/archive/ES_0.5567491638106882
new file mode 100644
index 0000000..fa730d2
--- /dev/null
+++ b/archive/ES_0.5567491638106882
@@ -0,0 +1,22 @@
+archive/ES_0.5567491638106882---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T13:30:31.086
+Launch V∞: [7.982463808134823, -5.697392504472437, 0.22647345988929699] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.721896541050491e-6, -8.265555803916678e-6, 6.033506479304003e-6] km/s
+ V∞_out: [-1.5592638243521672e-6, -1.4016473188314196e-5, 4.6734126857896083e-7] km/s
+ time of flight: 1.8749577780236343e8 seconds
+ arrival date: 2030-04-24T15:40:08.086
+ thrust profile: [0.4105942928229981 -0.016701244105366372 -0.11236339339304821; 0.05444240865088711 0.025991204329687687 -0.07396594164524022; 0.04281083791613634 0.03281382686083598 -0.10779995813018808; 0.024278964888538344 0.02195672852472323 -0.08528211503016608; 0.019460843540170077 0.019523911103209883 -0.08587190003700335; 0.014794410891646095 0.01649719647097044 -0.07898833622681631; 0.014537357342132483 0.018930414027492407 -0.09794183042395395; 0.007390618220452364 0.009194769831073568 -0.05478768345591852; 0.006507560116193979 0.00951787553441458 -0.0619985734434218; 0.001925675680156836 0.005055132448050182 -0.029716845925111004; 0.0010248105268023371 0.0011564581215436933 -0.009005115386821614; 0.0010370082851060248 0.0007868870904067075 -0.010031258519183605; -0.0001508333856409663 -0.00026893400777077445 0.00012916953032542517; -0.000215758904167071 -0.0005626331389989722 0.00029414836921281217; -4.470190870315751e-5 0.0005609935863707447 0.0009244378742907036; -0.000487910095756255 -0.0006830841204923525 0.00035623231966373277; 0.0001515846799441174 0.0001162027725029647 0.0010995859718906159; -0.0005531547790748109 -0.0007022661286682872 7.52766240291251e-5; 8.880313090154676e-5 0.00016619465326825082 8.072203258901328e-6; 0.0005903740769996254 0.00046655943303535027 0.0008026616811391008] %
+
+Mass Used: 88.19144095943057 kg
+Launch C3: 96.23130002623525 km²/s²
+||V∞_in||: 1.4115165090722586e-5 km/s
diff --git a/archive/ES_0.5567787762422494 b/archive/ES_0.5567787762422494
new file mode 100644
index 0000000..998e3a5
--- /dev/null
+++ b/archive/ES_0.5567787762422494
@@ -0,0 +1,22 @@
+archive/ES_0.5567787762422494---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T00:23:45.626
+Launch V∞: [8.068477400617782, -5.628047046406362, 0.13230448107260975] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.916290968547276e-6, -1.89776113020791e-5, 0.0003739244427296238] km/s
+ V∞_out: [1.480035873759156e-5, -0.00037410876453076303, 4.124138384995763e-6] km/s
+ time of flight: 1.8749577787493765e8 seconds
+ arrival date: 2030-04-23T02:33:22.626
+ thrust profile: [0.32183193820169675 0.0012489805229971204 -0.10326640778771759; 0.061447563315034856 0.03587448214105782 -0.07170952408996066; 0.03690047968440975 0.03455496902432887 -0.07865179755466528; 0.04122913435769527 0.05145700659566763 -0.1280746785140881; 0.03001019967472108 0.04595531584435085 -0.1270471625029271; 0.022311000035355175 0.04051005017926068 -0.12204863940418383; 0.004659672730315286 0.008804132825920952 -0.032181137057565964; 0.003240880637287823 0.009135584794601956 -0.030408156951373222; 0.0031065898970564065 0.006115330310306011 -0.023356713335467565; 0.005430154514205593 0.016499335965308896 -0.06482799593045727; 0.00317061429136903 0.003791708629833139 -0.013198181109082982; 8.362870931459163e-5 0.001616347372918023 -0.006036948660823107; -3.9760797194675736e-5 0.0007689000788583899 -0.0031017523398088904; -0.00022172072204143124 0.0001640861612826618 0.0009777988546344973; -0.0003827712981388137 -4.315048533330636e-5 0.0013687196048565893; -0.0004489255139070807 -0.00037926003847571477 0.0007371783230220592; -0.0010012817766053789 -0.001729148766420185 0.0004892345532422665; 5.942854158965999e-5 -0.0002678766611274644 0.0001572261982835518; -0.0027181474060325142 -0.0021123517206462204 0.002155688347466322; 0.0006577536251311702 -0.0018351591137721083 -0.00016852865466505517] %
+
+Mass Used: 84.95088963605258 kg
+Launch C3: 96.79274559655514 km²/s²
+||V∞_in||: 0.0003744106178682285 km/s
diff --git a/archive/ES_0.5567856232646013 b/archive/ES_0.5567856232646013
new file mode 100644
index 0000000..7d58a61
--- /dev/null
+++ b/archive/ES_0.5567856232646013
@@ -0,0 +1,22 @@
+archive/ES_0.5567856232646013---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T13:54:27.173
+Launch V∞: [8.037709473556014, -5.7506409300225245, 0.13653252596995052] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01586576593425751, 0.09469594654720517, 0.10444711029297964] km/s
+ V∞_out: [-0.02539337963250553, 0.023958584812360458, -0.13750451102226013] km/s
+ time of flight: 1.8749577787498716e8 seconds
+ arrival date: 2030-04-24T16:04:04.173
+ thrust profile: [0.23528335353302055 0.0015235202534487687 -0.08845446477653805; 0.09212271801171133 0.05116489392816506 -0.11175377197429108; 0.039551102161428715 0.03460581440218975 -0.08799568696259806; 0.03434836641344457 0.03765246892692736 -0.10703083896995039; 0.023213894645043982 0.031438831172339685 -0.10069689806197406; 0.02182392101500936 0.03459189678007593 -0.11920542078575341; 0.01303022916448693 0.022338784649025407 -0.08888549919593303; 0.005796897753902007 0.010659774946652047 -0.045253048532848276; 0.0016054468737098058 0.0031562435621924016 -0.014413713265190914; 0.0011131624157754809 0.0025506609566110293 -0.0123418271111593; 0.001050600058164969 0.001039282374388603 -0.006099415063501303; 6.331348639614445e-5 0.0025475922939601704 -0.010182830178845474; -0.0008205691848128464 0.0008193006051575678 -0.0022273016749996813; -2.2040175038121447e-5 0.0004916114788373203 -0.00117320358270428; 0.0010686586404440312 -0.0023668203737810555 0.0008140559291197175; 0.0021453380592520886 0.0009422904887246995 -0.0005428193963046548; -0.00024725278941292294 0.00012973539374118502 -0.0015711732230982165; -0.00014770773043589754 0.0035020961269589933 -0.00016529290056377952; 0.0036871753378216144 -0.0002872123028779304 -0.0046256387336896295; 0.0016056820931224635 0.003448721918037898 -0.0009471922045695877] %
+
+Mass Used: 79.70572653709223 kg
+Launch C3: 97.69328581799016 km²/s²
+||V∞_in||: 0.14187404156400718 km/s
diff --git a/archive/ES_0.5567892072200812 b/archive/ES_0.5567892072200812
new file mode 100644
index 0000000..906cd59
--- /dev/null
+++ b/archive/ES_0.5567892072200812
@@ -0,0 +1,22 @@
+archive/ES_0.5567892072200812---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T02:38:05.393
+Launch V∞: [8.106925768322208, -5.594746841450655, 0.1264382946258132] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.7028466782882383e-5, 4.452338374183509e-5, 0.002399364455480093] km/s
+ V∞_out: [-0.002168840895628222, -0.0007238050765209528, 0.000730917611674215] km/s
+ time of flight: 1.874957778749158e8 seconds
+ arrival date: 2030-04-23T04:47:42.393
+ thrust profile: [0.33064730138156334 -0.004375223116426751 -0.1105348494612943; 0.02984499746895932 0.016009189463313825 -0.03537321768978247; 0.035873731502178284 0.03060390414371216 -0.07643158683630896; 0.04849726077308322 0.054862342441131626 -0.1520370790255734; 0.023304985811251427 0.03104804948594426 -0.09780279008671001; 0.026695040929391838 0.042224619358020604 -0.14058312259839717; 0.00524950053728053 0.009279776140632042 -0.03440178784232922; 0.00377855695124702 0.006628798304584989 -0.025484778830518674; 0.009309445378362233 0.01884573082743172 -0.07965161464402648; 0.0008764637061519115 0.004418535040866965 -0.016948097465726154; 0.00010062022017056889 0.002050216517592931 -0.007903844102092612; 0.0010877048619137104 0.0021412222949892925 -0.01201326641947945; -0.0037235690757574684 0.0034329216618975305 -0.004077145161953105; -0.0007800783224120459 4.275512809564564e-5 -0.002059128683467359; -0.002642481922363712 0.0002629576142405165 -0.0015464549701745436; -0.0009303208352047711 -0.00041988231838791445 -0.002423826012552442; 0.0003780887720555154 -0.000983868431433888 0.0021974587281188857; 0.00046096725639296877 0.0007498531149720321 9.381356772541734e-5; 0.0004276103103756084 0.0013846084627198239 -0.00540808280390585; 0.0013614615946872634 0.0006624993896741242 -0.0010598180787231234] %
+
+Mass Used: 83.52410015051464 kg
+Launch C3: 97.03942427535658 km²/s²
+||V∞_in||: 0.002400455033518585 km/s
diff --git a/archive/ES_0.556794893212953 b/archive/ES_0.556794893212953
new file mode 100644
index 0000000..7c998c9
--- /dev/null
+++ b/archive/ES_0.556794893212953
@@ -0,0 +1,22 @@
+archive/ES_0.556794893212953---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:21:41.181
+Launch V∞: [7.7898521563935414, -5.582908181331452, 0.1906864937262555] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.09984791707522e-8, 3.030932774109783e-7, 8.374525937268616e-7] km/s
+ V∞_out: [7.910601125001835e-7, 9.264243640832311e-8, -4.121591592227291e-7] km/s
+ time of flight: 1.874957778726392e8 seconds
+ arrival date: 2030-04-21T12:31:18.181
+ thrust profile: [0.7556998544533204 0.0028340976785461948 -0.22198656462888025; 0.04592384196318273 0.02721204487448653 -0.05216930185767581; 0.050648571911568616 0.04908950734822583 -0.10317473800115841; 0.029193271526711508 0.03759808122053543 -0.08989597837992017; 0.029517213103551723 0.047236859210338 -0.12308235577070137; 0.01800351831964049 0.03420527087392253 -0.09763899524746424; 0.011445932646310962 0.02547407169358731 -0.07860983476618874; 0.007362575491372818 0.018857398177959537 -0.0622527989731178; 0.0010787294821668766 0.003232172690896221 -0.011732492125225586; 0.000897953690465631 0.002550576502084718 -0.009689264877913393; 0.000194821001168328 0.0011758074938738195 -0.00484942659875966; 0.00045212627137163584 0.0006511134615579926 -0.0013180246738264756; 0.001301668297246253 0.0010632076350145234 -0.0024348873613477527; -0.0009128083893558683 -0.00016235619670867789 -0.00241540249187763; -0.00012045721029643448 0.0002288626506816536 -0.0003150195606985512; -0.0005454408721173064 -0.000641890985178111 -0.0003257795317122875; -0.00036836846784915253 -0.0006829666973378007 -0.0015901893064394254; 0.0009176083102089597 -5.943145558331183e-5 0.0028584457164447033; -0.0008751384450164251 -0.0006609267299177663 0.0009482679469948645; -0.0012870153758656583 0.0005699127679458891 0.0006308035918871193] %
+
+Mass Used: 113.58641539031623 kg
+Launch C3: 91.88702171853639 km²/s²
+||V∞_in||: 8.952503028555567e-7 km/s
diff --git a/archive/ES_0.556802545686968 b/archive/ES_0.556802545686968
new file mode 100644
index 0000000..b443485
--- /dev/null
+++ b/archive/ES_0.556802545686968
@@ -0,0 +1,22 @@
+archive/ES_0.556802545686968---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T16:03:58.517
+Launch V∞: [7.868059342370197, -5.718051386173258, 0.1176232620918661] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.6891776218737935e-5, -4.5365261642592314e-5, -3.738755694131246e-5] km/s
+ V∞_out: [-7.132585333484647e-6, 5.417512414804935e-5, -6.078213197497308e-5] km/s
+ time of flight: 1.8749577787477523e8 seconds
+ arrival date: 2030-04-21T18:13:35.517
+ thrust profile: [0.3973319255478581 0.019377696365972873 -0.10360870944252791; 0.12056248822356998 0.08325705512986674 -0.11512890148669036; 0.08230273206634396 0.09438852806468603 -0.14373159830712806; 0.04900979989834702 0.07600624236698078 -0.1304141594031303; 0.03965441205588092 0.08057297526767537 -0.14848883078974162; 0.01185608158625359 0.02957873532298814 -0.0626389800901609; 0.006851138542070647 0.021630120703862717 -0.04879061223652217; 0.00171753607706284 0.006574582004594449 -0.016280796822268507; 0.00046797725042140573 0.0020372945431614865 -0.005352970486863261; 0.0026313176106258548 0.012246816534040323 -0.03429669286498414; 5.82456493646957e-5 0.00025854497960411705 -0.0005893205294937959; 9.24792737352582e-5 3.8550508161238554e-5 -0.00048525097770660123; 1.670993854728389e-5 -0.00013766163888841745 0.000129083557161056; 5.052670524567248e-5 0.0003428068595038792 -0.0006376944258720293; 9.423635434400879e-5 -0.00020539883241804896 0.0003079693807508221; 0.00029798476835502647 0.00015120930555274055 0.00027629936651267224; -0.00014055866958419703 0.00019185976358437987 0.0001510875665059363; -7.143081269719327e-5 0.00033285306446043805 0.00010513144818754874; 2.8671362290301055e-5 0.0002617613610658515 -0.00014656164239028633; 9.147599264408519e-5 7.552941977085843e-6 -0.00016705637629950312] %
+
+Mass Used: 97.67452587451771 kg
+Launch C3: 94.61630470176199 km²/s²
+||V∞_in||: 8.1807766008269e-5 km/s
diff --git a/archive/ES_0.5568092578252446 b/archive/ES_0.5568092578252446
new file mode 100644
index 0000000..e7cca86
--- /dev/null
+++ b/archive/ES_0.5568092578252446
@@ -0,0 +1,22 @@
+archive/ES_0.5568092578252446---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T11:53:34.796
+Launch V∞: [7.948955373156012, -5.840489672821962, 0.07201777491365854] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0019383881229319, -0.010102529525442203, -0.014129007691393762] km/s
+ V∞_out: [0.0076633943716872275, -0.0013347784505927263, 0.01564585160051077] km/s
+ time of flight: 1.8479369442395842e8 seconds
+ arrival date: 2030-03-24T07:28:28.796
+ thrust profile: [0.31302919207868135 -0.01654357581999935 -0.11155106460539883; 0.039855971712648916 0.017997266847193324 -0.051061315284497893; 0.03533484931465438 0.02530306449207069 -0.08095564283635014; 0.05641676346742348 0.051224653884517427 -0.1825182306067035; 0.023536198993519237 0.02479043204841054 -0.10288631622317997; 0.023952087326128114 0.028147298532038314 -0.12768145565389472; 0.010236263304846406 0.01314221487447731 -0.0668435935958399; 0.003955680130925932 0.005196823554051221 -0.029386492689424053; 0.004305374447121606 0.00651602265615361 -0.03849621414599561; 0.0015779036693923682 0.0018266608355207814 -0.013820676841058392; 0.0007113840834064397 0.0004972054407924142 -0.005248149727811934; 0.0006032917150794186 0.001027862325387207 -0.007046504612597288; -0.000188440547487681 0.0001923924406021513 -0.0019424852839162532; 0.0006495372536260377 0.0007079421265066541 -0.0028566153902123436; 0.0010134369472273048 -0.00010269770229454122 -0.001999489912826142; 0.0003368502351640445 -0.0010907474925515336 -0.002882923459726716; 0.0004288393375279393 -0.0010299383968090233 -0.0001923945323858842; -0.00022348567871332712 0.0007495848911442978 -0.002032004131860064; -0.0004610929916250986 0.0011528416300519077 -0.0033656095883626046; -0.0012025413592014246 0.00012095530702986324 0.0010837869203959457] %
+
+Mass Used: 82.01348086388089 kg
+Launch C3: 97.30239770266934 km²/s²
+||V∞_in||: 0.017477050943194593 km/s
diff --git a/archive/ES_0.5568115814002677 b/archive/ES_0.5568115814002677
new file mode 100644
index 0000000..5479ff6
--- /dev/null
+++ b/archive/ES_0.5568115814002677
@@ -0,0 +1,22 @@
+archive/ES_0.5568115814002677---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T21:03:10.406
+Launch V∞: [8.036262831814527, -5.837683405430574, 0.05008209842111723] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.388736721047161e-9, -2.1510481492227593e-9, -1.9183079039650774e-9] km/s
+ V∞_out: [-5.271313589755634e-10, 4.5248540532133667e-10, -1.802211977073375e-10] km/s
+ time of flight: 1.8590056084458923e8 seconds
+ arrival date: 2030-04-06T12:05:50.406
+ thrust profile: [0.19364007411315867 -0.002007121100188125 -0.06747044514528563; 0.040545069674090044 0.021766700359306845 -0.049743105440115926; 0.030944571931383155 0.026435925786310547 -0.06692168363150605; 0.036940745200327404 0.04136112155026368 -0.11528652497495043; 0.02687426814591154 0.03587047340206054 -0.11140361449904213; 0.02049335920078443 0.03190548805845654 -0.10907576305820325; 0.015070965661248189 0.029383396127162186 -0.0991688782137945; 0.003280731754013905 0.007512633511606998 -0.03164401220220943; 0.007879567467533936 0.023303542017058244 -0.0929447326566452; 0.0007585763163219482 0.0015870326490035106 -0.007576670515370066; 0.0027426288115572446 0.0071916988214243485 -0.03353499795739827; 0.0006855616282959083 0.002029621651338952 -0.008446101006745364; -0.0002122999399100794 0.0001499737283628156 0.00024931446660527475; -3.418978372994956e-5 -2.568548129609942e-5 4.666267464924407e-5; -5.209532930824005e-5 9.279244580039762e-5 -0.00011220571935277468; 0.0004076300102758833 -1.601948509070339e-5 -0.00010385565750523006; 7.20350602275516e-5 0.00023503870276144482 0.00016150650810831165; -0.0001927230613513106 -0.00038538947107574415 -0.0001904336077169469; 2.0424746276207666e-6 -1.4767299853960214e-5 5.909719480245658e-5; -4.109685296674169e-6 2.3224566731445268e-6 -5.190730580198504e-5] %
+
+Mass Used: 74.08181794666416 kg
+Launch C3: 98.6625760606254 km²/s²
+||V∞_in||: 3.743391039841909e-9 km/s
diff --git a/archive/ES_0.5568167900407651 b/archive/ES_0.5568167900407651
new file mode 100644
index 0000000..a31b598
--- /dev/null
+++ b/archive/ES_0.5568167900407651
@@ -0,0 +1,22 @@
+archive/ES_0.5568167900407651---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T03:24:04.858
+Launch V∞: [8.242400567949108, -5.504068204868638, 0.19136384759706299] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.4025053975202905e-10, 2.3483286628383256e-9, -1.828081617927418e-9] km/s
+ V∞_out: [1.411561974731447e-9, 2.6815250103007946e-9, 7.091910931668837e-11] km/s
+ time of flight: 1.8749577787493795e8 seconds
+ arrival date: 2030-04-23T05:33:41.858
+ thrust profile: [0.24865311398962503 -0.012422996629875593 -0.0843741645105545; 0.041935843782416916 0.019168138009643433 -0.05550834881171693; 0.03516891530822882 0.024936239029055913 -0.08342372650149918; 0.030892194288710564 0.02721108800798504 -0.10649168417267435; 0.025193167622498288 0.025491163713619334 -0.11386343727939012; 0.019362586961066172 0.021628563927394266 -0.10795547410867837; 0.013954940591069723 0.016762161869779888 -0.09198236504481325; 0.00912137709048827 0.01149508367699603 -0.06850158520042071; 0.004797466088995169 0.006234918214274299 -0.039970012223630114; 0.0014709046861792014 0.0019563706333685605 -0.013258988745699399; 0.0006845781929857092 0.001050590785048768 -0.007582972784187721; -0.0011462675431651939 -0.00043590487531600005 -0.0028383883315592985; 4.139663815488481e-6 0.0002138881376781141 -0.0011709473357057977; 0.0007416207742738253 -0.00012020184449596351 -0.0025467504867805356; -0.0010953883636522074 -0.000831372911607519 5.121585878640426e-5; -0.00014567482708716562 0.0006244629053495309 0.0012070642744104656; -7.135168856334641e-6 0.0009541488977490211 0.004301308006397397; 0.0008081908807128497 0.0005973982809084248 7.493191704940178e-5; -4.948509653899928e-6 -0.0001855877350001266 -0.0012482592385845244; 0.001770512674753119 -0.000258255313283479 -0.005741478571771096] %
+
+Mass Used: 76.38635643107136 kg
+Launch C3: 98.26855404854079 km²/s²
+||V∞_in||: 2.9953798323941675e-9 km/s
diff --git a/archive/ES_0.5568289724095632 b/archive/ES_0.5568289724095632
new file mode 100644
index 0000000..83a93ae
--- /dev/null
+++ b/archive/ES_0.5568289724095632
@@ -0,0 +1,22 @@
+archive/ES_0.5568289724095632---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:14:42.327
+Launch V∞: [8.048706336804303, -5.710259137858266, 0.09218927388665737] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9546424557057783e-9, -3.863579633508357e-9, -1.0390182406697131e-9] km/s
+ V∞_out: [-4.2114226179646195e-10, -9.096644324756942e-10, -2.4984868130416756e-11] km/s
+ time of flight: 1.8546124138089928e8 seconds
+ arrival date: 2030-03-30T21:15:23.327
+ thrust profile: [0.2950076539274884 -0.009878343856885052 -0.09828935767676852; 0.044899822370405566 0.02300339718784481 -0.05612162667023928; 0.03667030173997157 0.030066955690502547 -0.08065798239282015; 0.027959818474594215 0.02967766955830638 -0.09223789238013556; 0.021184510009593056 0.0236686344289487 -0.08351137654585561; 0.02938458059901042 0.05002670344339094 -0.16873771374820165; 0.013035555085628293 0.021573562958698576 -0.08775829335076085; 0.007833827809443847 0.013708216322512689 -0.06073874562419035; 0.005227585153438144 0.009269787291824236 -0.04671492830741326; 0.001403684970112919 0.002615966727585396 -0.013665318709864127; 0.001794477660983414 0.0035709543245276225 -0.01954880652757752; 0.0008547097187018754 0.0014787574912569206 -0.002328100424585124; 8.350343869209894e-5 -4.161755349051826e-5 -0.00035617808689249837; -0.00031664206998353845 -0.0003557173632822547 -0.0012874025967681384; 0.0008621817179202908 0.0010383479672638621 -0.0001703818456398929; -0.0006409006465591697 -0.00021179302306489293 -0.0009781704352974548; 0.0012873863146558502 0.0022924316780602574 -0.0001364827410574546; 0.002164012060149866 -0.0002650097397184914 0.0003424012250764826; -0.00015304567674194914 -0.0012362546436675117 0.00014615273889141862; -0.00322762662081534 -0.0038814631380324144 0.001994007155501232] %
+
+Mass Used: 81.48328126216438 kg
+Launch C3: 97.39723197982731 km²/s²
+||V∞_in||: 4.452800648867235e-9 km/s
diff --git a/archive/ES_0.5568354631603809 b/archive/ES_0.5568354631603809
new file mode 100644
index 0000000..3519e05
--- /dev/null
+++ b/archive/ES_0.5568354631603809
@@ -0,0 +1,22 @@
+archive/ES_0.5568354631603809---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:19:00.209
+Launch V∞: [8.099438633957538, -5.576435374308113, 0.3931227373606848] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009024011104012663, 0.055258553056757115, 0.059821255252113396] km/s
+ V∞_out: [-0.013708338854385266, 0.013012765267808556, -0.07972941195067995] km/s
+ time of flight: 1.8749577787249544e8 seconds
+ arrival date: 2030-04-22T10:28:37.209
+ thrust profile: [0.33034965193904536 0.0027572595369012845 -0.09753400498142763; 0.060022588616662285 0.03587921654282729 -0.06643071455613025; 0.03200567582289811 0.03100254598951995 -0.06525814593519132; 0.03309512483789357 0.04241645343180989 -0.09876410435160557; 0.04020258445032674 0.06410223515619892 -0.16002898009179534; 0.02125904898720507 0.04036832665445866 -0.11168350887600338; 0.011537451269087196 0.026136826652465087 -0.07797125963258864; 0.0037596962282921485 0.009612706859771497 -0.03170141904726324; 0.0026673996910947665 0.006446340112249593 -0.023131408280082845; 0.003048907338698635 0.009764577319334902 -0.03576812675233783; -0.0001060797884633651 0.0003091687988759369 -0.0015868862910378195; 0.000640268576829549 0.001808637249814521 -0.007222012820230446; -0.0006995323213116506 -0.0011254706867472573 -0.0002581054860468369; 0.00010674378206516394 0.0008727574955838625 -0.00015072361122922258; -0.00027614651489668113 0.0007616355182608488 -0.0035457235587956016; -0.00018281459072491864 -0.002434809565760294 0.001853141764780896; -0.00014491533281790541 -0.0008496980433411608 0.0025198453391327307; 0.0003430226285995161 -0.0006321093739241604 0.00046305656087280945; -0.00042571389863764036 -0.0002249860177985074 0.001806030824306048; 0.0026120073799683068 0.0010947016716556478 0.0005038008094646587] %
+
+Mass Used: 84.67088861214324 kg
+Launch C3: 96.85208315570878 km²/s²
+||V∞_in||: 0.08193609120692961 km/s
diff --git a/archive/ES_0.5568360553502276 b/archive/ES_0.5568360553502276
new file mode 100644
index 0000000..a5748d1
--- /dev/null
+++ b/archive/ES_0.5568360553502276
@@ -0,0 +1,22 @@
+archive/ES_0.5568360553502276---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T19:09:42.348
+Launch V∞: [8.165385471813185, -5.775606428556177, 0.06978992667386873] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.3101126858295146e-7, -2.106723219747521e-6, 5.000615912644624e-5] km/s
+ V∞_out: [2.052500859758391e-6, -4.998806483248525e-5, 3.7419324161963604e-7] km/s
+ time of flight: 1.87495777875598e8 seconds
+ arrival date: 2030-04-25T21:19:19.348
+ thrust profile: [0.09376286793189159 -0.0021169562508475755 -0.03591844805775404; 0.019784722371740535 0.009903387943159621 -0.027025986014479673; 0.04206265778823043 0.0328573370412486 -0.09738359852757761; 0.05360330819484505 0.05339761346729455 -0.17464615279247817; 0.02896010772868831 0.033436807034887786 -0.12766713821502385; 0.017672670016268877 0.023399206665307634 -0.10175291348570525; 0.011098472483456188 0.01753667631773002 -0.0803541643227341; 0.004760824354604717 0.006597595160077748 -0.03531583585425295; 0.003769560134740099 0.005484131625470028 -0.03396167911680773; 0.0009370405742098939 0.0017030408207024746 -0.010982996759439815; 0.000616093720896038 0.001847327005425894 -0.010191844948572915; 0.0006531157987517964 0.000870665478946685 -0.006440444835419777; -0.0009884899008284224 6.168254116061054e-5 -0.00281715540221494; -0.001018338748423913 0.0017424287059814398 0.0006298238321856191; 0.001111138697577267 -0.0030110030881866424 -0.002115472874939406; 0.00148553962264032 0.00498992311615413 0.00038299783846925143; 0.001111944864041739 -0.00041149552067133385 -0.0031187651892033066; -0.001942200677940111 0.0008698195341135611 0.0020118180287337644; 0.00046001442679026493 -0.00043966697784553893 -0.0010945395533765434; 0.0005962300486119861 -0.0014011354333986125 0.003694582228672222] %
+
+Mass Used: 66.09861367260146 kg
+Launch C3: 100.03602015474242 km²/s²
+||V∞_in||: 5.005161138029439e-5 km/s
diff --git a/archive/ES_0.5568368431749066 b/archive/ES_0.5568368431749066
new file mode 100644
index 0000000..c1bb359
--- /dev/null
+++ b/archive/ES_0.5568368431749066
@@ -0,0 +1,22 @@
+archive/ES_0.5568368431749066---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T01:54:16.008
+Launch V∞: [8.07717201385351, -5.636422841791869, 0.194927195607676] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.5415055044631223e-5, -2.2172724315281104e-5, -1.992144945258943e-5] km/s
+ V∞_out: [-3.929768349540737e-6, 2.4742931198388833e-5, -2.9947639791756205e-5] km/s
+ time of flight: 1.8534971950669008e8 seconds
+ arrival date: 2030-03-28T07:56:15.008
+ thrust profile: [0.3064255596349677 -0.007903419784350075 -0.09849187039449041; 0.04943462653465565 0.026576091010302276 -0.058469075433495755; 0.057112382431875414 0.04828862555192197 -0.11735100383110846; 0.049366679965198404 0.054423989184452196 -0.14821460249067167; 0.02676818067081502 0.035334849258626455 -0.10938919445239163; 0.010421674041985856 0.017005868435964515 -0.058222907559819494; 0.006296289415837109 0.015488004391847481 -0.05202115919074029; 0.004858224798546693 0.015373297578120716 -0.04992731993916662; 0.010276948485396592 0.022291162893916378 -0.09249588489595117; 0.0015421048046019962 0.004597677581083669 -0.019980613489137232; 0.0007386910282815016 0.002030416912083271 -0.011286584058837725; 0.0002240475170544309 0.0004657391856991907 -0.0017690641580149307; -1.6046594632456042e-5 0.0001545018879378628 -0.0004473431422637337; 0.00045709286113933647 -0.00027925879693042476 -0.0006663841193498151; 0.00032921817554288474 -0.0004655111303368299 -0.00030403391077101047; -0.0007323774833753423 0.00027850838528123087 0.00012765389434798101; 1.809048273982599e-5 -0.00028420220580598223 0.0004724354966023828; -1.6420753644599386e-5 -0.0012814039891263598 -0.000667296989380351; 0.00028666928645785866 0.0008362172470606481 -0.0002482789381025868; -0.0015224951735148644 0.0015515311877316042 0.00043660418291081534] %
+
+Mass Used: 83.52984401149706 kg
+Launch C3: 97.04796680443896 km²/s²
+||V∞_in||: 3.917165907611227e-5 km/s
diff --git a/archive/ES_0.5568469393727292 b/archive/ES_0.5568469393727292
new file mode 100644
index 0000000..6ef2ea5
--- /dev/null
+++ b/archive/ES_0.5568469393727292
@@ -0,0 +1,22 @@
+archive/ES_0.5568469393727292---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T07:12:36.885
+Launch V∞: [7.884925566790435, -5.645171338764913, 0.18416274663591192] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.713628850537561e-8, 1.804312903151728e-7, -4.176371150130105e-8] km/s
+ V∞_out: [2.66190000155185e-8, -1.1124994751639856e-7, -1.4456610023733637e-7] km/s
+ time of flight: 1.85599129603425e8 seconds
+ arrival date: 2030-03-30T10:31:25.885
+ thrust profile: [0.564139099515729 0.0023235552010336053 -0.1577551218791741; 0.05334376004071884 0.031721605932327465 -0.06023254912377814; 0.043863550559149436 0.04268203492427431 -0.0881315925147324; 0.03263455277433495 0.04486484248044841 -0.09836442999479486; 0.022519095998302926 0.03906405959023102 -0.09875288751974808; 0.012510192605875187 0.024185897709922792 -0.06723325502674099; 0.015404621152670453 0.04480844753302753 -0.1281662107375338; 0.010127089894621038 0.02850887394899245 -0.09017636646427463; 0.0022343769221481805 0.007169034275354456 -0.02486617336503596; 0.001053203396642956 0.004598456955359581 -0.018194584716762913; 0.0010294538911050576 0.0037044210691616133 -0.01266946351864885; 1.9397767980880984e-5 4.093853419715233e-5 -0.00021615167721923144; -2.1635691149211232e-5 1.4433115545243069e-5 -0.00010626019517946882; -8.959106110068967e-6 5.354302552378939e-5 -4.3459343393854806e-5; 0.00011542425074831661 2.0799955363938772e-5 -0.0002809208994047857; 0.00016041981791434148 0.00018148738275570203 -7.050745735397562e-5; -0.00013011371413798503 9.965826742508895e-5 0.00013467242824498566; -0.00014334223134289983 0.0001209264168385453 0.0001011378222624326; 3.284117122579228e-6 -5.8201237450371344e-5 -6.267792401056692e-5; 8.80625498586852e-7 -0.000176039016188015 0.00026342587446531257] %
+
+Mass Used: 100.8901910301779 kg
+Launch C3: 94.07392655508679 km²/s²
+||V∞_in||: 1.8717915556228225e-7 km/s
diff --git a/archive/ES_0.5568611385490082 b/archive/ES_0.5568611385490082
new file mode 100644
index 0000000..48f428e
--- /dev/null
+++ b/archive/ES_0.5568611385490082
@@ -0,0 +1,22 @@
+archive/ES_0.5568611385490082---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T17:36:25.928
+Launch V∞: [8.132330911412947, -5.677707820886986, 0.12705898320323034] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.562244684503154e-6, -4.9956490634511965e-6, 3.6738886594120114e-6] km/s
+ V∞_out: [-9.23737049758318e-7, -6.641228592158301e-6, 2.3418774724574743e-7] km/s
+ time of flight: 1.8749577787452662e8 seconds
+ arrival date: 2030-04-24T19:46:02.928
+ thrust profile: [0.22310390206834346 -0.008449261239031882 -0.0822115624982724; 0.04526971827927271 0.021397519709930264 -0.057473697928695416; 0.03236758057900825 0.024249782621029618 -0.07549595964169628; 0.03598736249455909 0.0330092442093957 -0.11938976232909669; 0.027165735761480913 0.028572171470710363 -0.11723739722484923; 0.02673534286079588 0.03127815164938773 -0.14350891545473982; 0.015213902733498392 0.019647245226157573 -0.09714134721673943; 0.005149542816621 0.007403721740107414 -0.03995776741104459; 0.0013021898978568807 0.0010944727303414286 -0.008865956780390602; 0.0012594959098907702 0.0023840502903837747 -0.010199850241292531; 0.0010491838843156701 0.0015242374561963293 -0.006680482862847243; 0.0008961935057220352 0.0006154901560637408 -0.005994739395674121; 0.0005624225568672751 0.0014245137243730475 -0.006230649622350761; -0.0013236434984616823 0.0008175753062754056 -0.005006069945800442; 0.003787383619989749 -0.0004321120140272789 -0.001970520656094452; 0.001181232099193285 -0.0003753310239737787 -0.004163551953321975; 0.00047815423129318583 -0.0017446109479491733 -0.001421982362595128; -0.004956423976104008 -0.006468587375578762 6.18959100053885e-6; 0.00016921782354521395 -0.005627465980653208 0.00325233109457666; 0.0001268468039192477 0.00044786793072837654 0.0016417529360815816] %
+
+Mass Used: 75.74531750628057 kg
+Launch C3: 98.38731613729641 km²/s²
+||V∞_in||: 6.709624823355004e-6 km/s
diff --git a/archive/ES_0.5568816363246691 b/archive/ES_0.5568816363246691
new file mode 100644
index 0000000..33015e1
--- /dev/null
+++ b/archive/ES_0.5568816363246691
@@ -0,0 +1,22 @@
+archive/ES_0.5568816363246691---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T22:11:43.044
+Launch V∞: [8.038196673704933, -5.686712608019777, 0.1751068634980408] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.455729163573312e-10, 2.479721477883676e-9, -1.8819620966427537e-9] km/s
+ V∞_out: [1.5434123965239545e-9, 2.7243835393043334e-9, 7.526472025474295e-11] km/s
+ time of flight: 1.8749577787494007e8 seconds
+ arrival date: 2030-04-23T00:21:20.044
+ thrust profile: [0.2527112080915867 0.006849545780199215 -0.07838952890815644; 0.09835900324183125 0.061816055491393476 -0.10432081866483438; 0.061222798735079596 0.0624257105427418 -0.11750123515052478; 0.04153364305543445 0.05671701586541571 -0.11950149374021074; 0.02772546856493195 0.04747526931252415 -0.11010685878608042; 0.015616843765919606 0.03200993933167839 -0.081862079226805; 0.007708796298133462 0.01850375232425168 -0.0511781178279095; 0.0058837315871294316 0.017014372193490928 -0.050243843766121475; 0.0013630961586712101 0.003821203599900141 -0.012011804162234551; 0.004117185369307474 0.013773670827701036 -0.04615114806293968; 0.0011047916814767066 0.005345387916931159 -0.01840976753568846; -0.00024746994590017 0.0026027199716560675 -0.004830026750459761; -0.0005717433547990354 0.000255424962937394 -0.000525875590570929; -0.0011394107249986301 0.0001347050683913393 -0.0005759176220142986; -0.0012151536837755564 -0.0017626847581947804 -0.0002543253446601186; 0.0020807127755385676 -0.003197586549368052 0.0005101170993773249; -0.0012034885833899693 -0.0002212083137547271 0.00033547748488161125; -0.0006373348266306875 0.00011789972732348635 0.0006518038588564598; 0.001433374137144794 0.0008995146048102094 -0.000680091113001786; 0.00014680540212936379 -0.00016367889879392514 -9.847689669881482e-5] %
+
+Mass Used: 83.96709299951908 kg
+Launch C3: 96.98196846501627 km²/s²
+||V∞_in||: 3.1226760956471033e-9 km/s
diff --git a/archive/ES_0.5568912263370472 b/archive/ES_0.5568912263370472
new file mode 100644
index 0000000..ae0390c
--- /dev/null
+++ b/archive/ES_0.5568912263370472
@@ -0,0 +1,22 @@
+archive/ES_0.5568912263370472---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T09:28:48.325
+Launch V∞: [8.168219747107875, -5.675131589591791, 0.12813639055420523] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1592161603676856e-6, -1.7317057626969641e-6, -2.0699546272295235e-7] km/s
+ V∞_out: [1.4944028853767294e-7, -7.398620328859994e-7, -1.9536936859490796e-6] km/s
+ time of flight: 1.8749577787493402e8 seconds
+ arrival date: 2030-04-24T11:38:25.325
+ thrust profile: [0.1652452790141961 -0.0016811423487374918 -0.056802238781301306; 0.03489821208014453 0.01868452507055161 -0.04520759078835175; 0.0540458299314932 0.04556282319854855 -0.1178568888711151; 0.03600755932105725 0.0394004979775331 -0.11689288642741108; 0.019876400971185697 0.026090472309523997 -0.0880624036097395; 0.012139306210556757 0.018628291182375332 -0.06909489467334917; 0.012925452102616506 0.024729607977729377 -0.09721595640801194; 0.009213684120788273 0.019682336577664404 -0.08169059916011916; 0.005363668785187979 0.011121369444452342 -0.05154536085388512; 0.002926854862643365 0.007050415704604806 -0.034826104023000175; -0.00020761539065155402 0.0005254594770049649 0.00010070550339969669; 0.000887652281885593 0.001881254942123084 -0.011956397947928167; -0.00013973169602727903 -0.00028165138538838 0.0010308902679003686; 0.0001250608764737671 0.000543871780702263 0.00012330554990252346; -0.00039745207837097276 0.00011019318431714382 -0.0002415028373645773; 0.001815309942451253 0.0008446431238548223 0.0009161645109596543; -0.002543398823616415 -0.0015278058690802129 -0.00020559251411548195; 0.0009601645989351029 0.0006052113656725353 0.002662569962230254; -0.000746352597482661 -0.0014671967790153655 9.3043364626496e-5; -0.0023126505810634095 0.004551035394133705 0.0016555960468078545] %
+
+Mass Used: 72.53688129683042 kg
+Launch C3: 98.94335133080995 km²/s²
+||V∞_in||: 2.094142802342611e-6 km/s
diff --git a/archive/ES_0.556893711431268 b/archive/ES_0.556893711431268
new file mode 100644
index 0000000..05937a3
--- /dev/null
+++ b/archive/ES_0.556893711431268
@@ -0,0 +1,22 @@
+archive/ES_0.556893711431268---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T20:29:23.395
+Launch V∞: [7.991992446561054, -5.8854729340030945, 0.24099929834102668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4485216347465226e-7, 8.087367935167656e-7, 2.2935732428118037e-6] km/s
+ V∞_out: [2.191071604077049e-6, 2.804347749309365e-7, -1.0494130734665658e-6] km/s
+ time of flight: 1.8439994219393155e8 seconds
+ arrival date: 2030-03-19T02:41:45.395
+ thrust profile: [0.14827161220611806 7.097983232297596e-5 -0.04930062853365666; 0.06260901029896809 0.034209859489966514 -0.0668098411358857; 0.05873165018099181 0.053630608638031645 -0.11554889209274119; 0.04095735752335678 0.049792024992651986 -0.12017337746771779; 0.03522014385174709 0.05349746641570132 -0.14041893542913994; 0.025886748639091253 0.04480278142485854 -0.12644121535380984; 0.01545343904519865 0.031023322209623987 -0.09588542448347546; 0.004240306605469233 0.009357399059655505 -0.030813480743157883; 0.003076578448562602 0.008033718256884962 -0.027051197904612787; 0.0007361229442800247 0.0016090321227500556 -0.00492579399599788; 0.0003737062497413993 0.0008240630357830476 -0.004962692908081846; 0.0007138084292893851 -6.59335313053747e-5 -0.0026919732781492474; 0.0008881735089278873 0.0015107709367920652 -0.0007713102888181918; -0.0018919247393435843 0.0014282585199505936 -0.0032164676250615483; 0.0018145222500908099 -0.0005469016811612579 -0.0021186342881809516; 0.0005831944829995698 -0.00010223755005935812 -0.0016216310311224324; -0.0004917835264880831 -0.0007648171873916778 -0.0017701063144933556; -3.446250839463051e-5 -0.0006492850701024038 0.0013879610262945944; 0.0031599013082543592 -0.00243735886365507 1.1498113111617055e-5; -0.0014752396839460805 -0.0009968894285916634 -0.0012850167520000973] %
+
+Mass Used: 74.72457242647124 kg
+Launch C3: 98.5688155845728 km²/s²
+||V∞_in||: 2.4442761716484187e-6 km/s
diff --git a/archive/ES_0.5568988084780901 b/archive/ES_0.5568988084780901
new file mode 100644
index 0000000..b558536
--- /dev/null
+++ b/archive/ES_0.5568988084780901
@@ -0,0 +1,22 @@
+archive/ES_0.5568988084780901---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T04:15:03.774
+Launch V∞: [8.147544164743604, -5.655669278165524, 0.15053561395531267] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2128962425765673e-6, -1.941063495527119e-6, -1.964828514427009e-7] km/s
+ V∞_out: [1.615009722982283e-7, -7.842880361991345e-7, -2.1531680186355748e-6] km/s
+ time of flight: 1.8749577787493265e8 seconds
+ arrival date: 2030-04-24T06:24:40.774
+ thrust profile: [0.21478123498514753 -0.0013952989139965032 -0.07528485710468573; 0.043305512912885584 0.02266610513836069 -0.05388724518356436; 0.03824969995137775 0.03169136810962497 -0.08483711588897269; 0.03361535181490576 0.0365090862896845 -0.11064975758182516; 0.023922998445915944 0.02965634506619184 -0.10426423372505766; 0.015502687228828757 0.02194723641576895 -0.08424108054614861; 0.009782915953289437 0.015654429953041504 -0.0667147751266849; 0.020931996384109752 0.03924677702166452 -0.1641710246166222; 0.0014883757459887683 0.0015724811315167614 -0.011192226371829391; 0.0005375871867026148 -0.00044594328250804774 -0.001600991761596725; 0.00017515593820177552 0.001041281956974135 -0.004857878032622462; 0.0014381100448593602 0.002408990775183129 -0.015816428129671076; -0.0013657473132422649 -0.0006093962342532782 0.0006801663543410774; 0.002185404051019934 0.0016504040649683261 -0.0003248903906265028; -1.1318393755681356e-5 0.0017859873043566783 0.0017091052213320745; 0.0023264427830142075 0.0014108026991766134 0.0018572932930353567; 0.0024723867523847223 0.003828752767714319 0.0001739986118993015; -0.00016285303172207548 -9.235171502173617e-5 -0.0018454719740610152; 0.001166542241946989 0.00090453168753285 4.818193467594613e-5; -0.0032707891601238006 0.0015652921279433337 0.001382269420870046] %
+
+Mass Used: 75.76350730734475 kg
+Launch C3: 98.39173187150179 km²/s²
+||V∞_in||: 2.2972701843351746e-6 km/s
diff --git a/archive/ES_0.5569001658919375 b/archive/ES_0.5569001658919375
new file mode 100644
index 0000000..9360eb1
--- /dev/null
+++ b/archive/ES_0.5569001658919375
@@ -0,0 +1,22 @@
+archive/ES_0.5569001658919375---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:58:59.195
+Launch V∞: [8.126367248350341, -5.646961498057657, 0.14463052620426292] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005651351055291448, -0.003692486935026399, -0.00022621134541643003] km/s
+ V∞_out: [0.005100211911327009, 0.0021948308039084216, -0.0038471705237358724] km/s
+ time of flight: 1.874957778744823e8 seconds
+ arrival date: 2030-04-23T10:08:36.195
+ thrust profile: [0.22641310036403667 0.0009612670675059094 -0.06540590265795901; 0.050607899508490824 0.0304613838372685 -0.057894638463330005; 0.04346620260100731 0.04274785303023846 -0.08890614969435826; 0.042255306950117984 0.05378495889134822 -0.12340638731901804; 0.018512764586027915 0.029613398393859666 -0.07584690851353168; 0.014931522957120108 0.028606592611431104 -0.08164235861393628; 0.014356145124212577 0.03091166717089148 -0.09149463296727436; 0.008500563673618915 0.02275166361775405 -0.07312733182361912; 0.0071040153713105535 0.019967738793182786 -0.070359683214108; 0.0021991709643107353 0.010076864664732312 -0.03718365181835272; 0.000994261872762097 0.0017760567963262385 -0.008014623950796723; 0.00031765410700631354 0.000313603652918936 -0.0018113744865307416; 0.0001525629915126167 0.0005392804975623087 -0.0011632217981299548; 0.00010738045465398752 -0.00016066973658584798 0.00014393700325669896; 8.808493729919558e-5 -0.00014723654563868354 0.0010684765196047265; -0.001991779917602488 -0.00040953920093048205 0.0002940138150210145; 0.0001581122793021015 0.00027495512996792093 -0.0011303798168476376; -0.0019196654454162016 0.0008875799627498562 0.001350498794924982; -0.0014145422379358238 0.0011254935506737219 -0.00021544419889596704; -0.0022033716273799093 0.001982455141281667 0.002584179881511781] %
+
+Mass Used: 78.35972884641251 kg
+Launch C3: 97.94693680471678 km²/s²
+||V∞_in||: 0.006754509611236002 km/s
diff --git a/archive/ES_0.5569211513576282 b/archive/ES_0.5569211513576282
new file mode 100644
index 0000000..31e8b67
--- /dev/null
+++ b/archive/ES_0.5569211513576282
@@ -0,0 +1,22 @@
+archive/ES_0.5569211513576282---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T17:17:29.235
+Launch V∞: [7.892528495663367, -5.937520460768947, -0.15298850517327567] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1770747171455646e-5, 0.0002752506513806643, 4.8733445697078474e-6] km/s
+ V∞_out: [0.0002663173224934805, -4.036832323895735e-5, 5.785861599242453e-5] km/s
+ time of flight: 1.842617082933004e8 seconds
+ arrival date: 2030-03-18T09:05:57.235
+ thrust profile: [0.2827519129866825 -0.00863885618624201 -0.09993417333349347; 0.02807939167193266 0.013943055493086914 -0.035039691941492375; 0.06114949653007427 0.049770905042686255 -0.13269527190034797; 0.042160883881103804 0.043960091319575734 -0.13447206709241968; 0.04578279854004718 0.057981771004775896 -0.19256655607302833; 0.012649911938454666 0.017671508277677703 -0.0687832552629381; 0.007854834240416327 0.012255759903928505 -0.05183781139941816; 0.008432777807303905 0.014598016966455197 -0.06547732491265039; 0.003263177674361999 0.005930526690805018 -0.028594734841455104; 0.0005462815418162813 0.00010951242268720569 -0.0025107726299540244; -0.00013199959533512044 0.00043863340848186656 -0.002635339085817912; -0.0010992703927382482 0.0005148063460422196 -0.002166836792854279; 0.00034118652111029104 0.0001185924270593635 -0.000803038911233933; 0.0005234486308866486 0.00029384871517437055 -0.0018623650863562316; 0.0005968704242061338 -0.0003287106926409426 -0.002772992184434512; 0.0007401399713549101 -0.000268154036750685 -0.0023659560727608536; 0.0010050657542576892 0.0003710505202421423 -3.7757783110646016e-5; -0.0004415128697852367 -0.0002987638061861203 -0.0003390328464473833; 0.0008231554964572324 -0.0005639616572729513 -0.00015762118201538837; 0.0011972898065489147 0.0006999440822434981 -0.00044979149703789636] %
+
+Mass Used: 80.58557215276369 kg
+Launch C3: 97.56956075962329 km²/s²
+||V∞_in||: 0.00027554531580440523 km/s
diff --git a/archive/ES_0.5569224754808025 b/archive/ES_0.5569224754808025
new file mode 100644
index 0000000..43f3c02
--- /dev/null
+++ b/archive/ES_0.5569224754808025
@@ -0,0 +1,22 @@
+archive/ES_0.5569224754808025---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T15:19:01.746
+Launch V∞: [7.932660209205928, -5.737316430285942, 0.2382053267794903] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5675224613722287e-6, 2.258518217385415e-6, -1.566689756553814e-6] km/s
+ V∞_out: [4.935204383124824e-7, 3.7229612818907634e-6, -1.7619296854861007e-7] km/s
+ time of flight: 1.8749577787379253e8 seconds
+ arrival date: 2030-04-24T17:28:38.746
+ thrust profile: [0.4386436933617161 -0.01042437222065752 -0.1384359879560606; 0.04782029309928396 0.024184273730845952 -0.060858703461421415; 0.04018643374070453 0.03168684268670673 -0.09145292273855153; 0.02839185503118831 0.028399041376532125 -0.0941111625408937; 0.02299473855944315 0.027078109121283177 -0.10102355020748192; 0.01890272803667467 0.025215340223061197 -0.10445421357458658; 0.013240395896043956 0.019647449591938478 -0.0879228201926624; 0.007114385157786429 0.01082013063843551 -0.05356236701346624; 0.003951301301597373 0.006565590491005747 -0.03456342574150859; 0.0019962729726225896 0.003527555212590522 -0.019821026803950585; 0.002045098790486401 0.003825336110818567 -0.023615254091196938; -0.0003343957922940732 0.0007333249010176693 -0.0012269920110294663; 0.0005413486566567732 0.0006620711868255349 -0.00305507724933611; -0.0004276384024395481 -0.0002572599913417127 -5.641435153559118e-5; 0.00039706726296454226 0.00037957406988950367 -0.0020002997396697227; -0.0008322850673409274 0.0010199061823262284 -0.0010039474913528124; -4.618743901898219e-5 -0.00184599532002826 0.0010441745491832457; -0.0004153361439185203 -0.001961684496029757 -0.001914966237885875; -0.00024336016234179344 -0.0017028977764775453 0.0013123967884032981; -0.00012512592708170808 0.00024278962364190993 -0.003561306427500237] %
+
+Mass Used: 90.32249043128695 kg
+Launch C3: 95.90063959365418 km²/s²
+||V∞_in||: 3.7613286111696425e-6 km/s
diff --git a/archive/ES_0.5569239078938191 b/archive/ES_0.5569239078938191
new file mode 100644
index 0000000..0b672d8
--- /dev/null
+++ b/archive/ES_0.5569239078938191
@@ -0,0 +1,22 @@
+archive/ES_0.5569239078938191---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:33:00.366
+Launch V∞: [8.05290139340618, -5.59026908549591, 0.21816725842737913] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.173870356505618e-7, 5.014692618487364e-6, -0.00011903595034322622] km/s
+ V∞_out: [-4.894167335635953e-6, 0.00011814898833873108, -8.973577828960478e-7] km/s
+ time of flight: 1.8749577784759697e8 seconds
+ arrival date: 2030-04-22T18:42:37.366
+ thrust profile: [0.397331697766944 0.0006715288255646095 -0.1256332889280001; 0.04826828544838845 0.028270130754881016 -0.0563146605560614; 0.048882330243649706 0.04533739559306871 -0.10188030874907249; 0.02349712378357881 0.028227559633355336 -0.07317796578374768; 0.025639962083398155 0.03637162335931873 -0.10620563317210627; 0.016043513922817935 0.028008516432226488 -0.08933585057483186; 0.00971253895235133 0.020583842584437843 -0.06745249991246531; 0.0070013124918306665 0.015724329925887223 -0.05655159492521207; 0.007397735451645559 0.018492732504328122 -0.0695675035391026; 0.003085954700381552 0.013418101550062326 -0.05819613604556358; 9.890622024192102e-5 0.0010736476774882153 -0.0027718254194968248; 0.00022653525849240872 0.0006426780622764305 -0.003230992078717865; 3.9308937032783096e-5 4.836454509530354e-5 -0.0012282901419373683; -0.000378696803059329 -0.0011745529556513347 -0.00039806851294300026; 0.0002851542036608662 0.00042383026519041687 0.0009611796624021008; -0.0008617575211673849 -2.8119455225532034e-5 0.0002494555526907501; -0.00022857893033296773 -0.0007206458832291809 -0.0011951121822509473; -4.5194671445957605e-5 0.001258630685997555 0.0004967641689160617; -0.0029650110336656888 0.001929869613706304 0.0012851629732591652; -5.9497112482576926e-5 -6.592963554617419e-5 0.0008378992475461005] %
+
+Mass Used: 88.88165606798111 kg
+Launch C3: 96.14792625282419 km²/s²
+||V∞_in||: 0.00011914433573501924 km/s
diff --git a/archive/ES_0.5569302336919262 b/archive/ES_0.5569302336919262
new file mode 100644
index 0000000..37634cc
--- /dev/null
+++ b/archive/ES_0.5569302336919262
@@ -0,0 +1,22 @@
+archive/ES_0.5569302336919262---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T03:39:46.659
+Launch V∞: [7.987124783501919, -5.686232507142044, 0.07068890394274437] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.725028060680147e-8, -4.784447376117683e-7, 8.778687781986558e-8] km/s
+ V∞_out: [-7.476963315951472e-8, 2.828521349999218e-7, 3.9133602216765104e-7] km/s
+ time of flight: 1.8566769414296585e8 seconds
+ arrival date: 2030-04-01T02:01:20.659
+ thrust profile: [0.36291570875246004 0.0021567785125584005 -0.11362848983285487; 0.0469833747435148 0.02714546409699019 -0.05456666927612638; 0.08306535345476668 0.08068730642906814 -0.16585654481208856; 0.028666951463358136 0.03627082328934028 -0.08963983063303974; 0.02595797926065612 0.04065366441357393 -0.1092627221480437; 0.018968164312527243 0.03509704137808595 -0.10270710164124261; 0.009980600467994845 0.02161289137021542 -0.06881033782037624; 0.009076102375114302 0.02197643440162784 -0.07304072987900581; 0.0030166588583668864 0.008038009390672141 -0.029185378058872332; 7.316921796816838e-5 0.0002501336669968521 -0.002852267592334131; 0.001409022067447443 0.0039313532997081475 -0.014907916540020534; -0.00014183757345495422 -0.0006069918837266206 -0.000621909149535482; 0.0005385966815858372 0.00024454175446991686 -0.0013573034961386092; 4.885287620906494e-5 -0.0004996522886204634 0.0007244279258779179; -0.00030497000733200827 -0.0003784050300555961 -0.0006804557122909584; 5.139742724300281e-5 0.001899614098008355 0.00168231538026334; -0.0004446360460216672 -0.0007551213866241135 0.0009098303626429544; 7.07624339368754e-6 -0.000665071933332795 0.0019799586351304916; -9.635715706699934e-5 0.0014963504789704861 -0.0005775163145611338; -0.00044947965181402883 0.0014634242392943286 0.0032232610527931404] %
+
+Mass Used: 88.97960974428815 kg
+Launch C3: 96.13239935365011 km²/s²
+||V∞_in||: 4.897892378312444e-7 km/s
diff --git a/archive/ES_0.5569347443317517 b/archive/ES_0.5569347443317517
new file mode 100644
index 0000000..f839f07
--- /dev/null
+++ b/archive/ES_0.5569347443317517
@@ -0,0 +1,22 @@
+archive/ES_0.5569347443317517---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T02:28:22.231
+Launch V∞: [7.886588611989853, -5.837653095889188, -0.11426788266148159] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.536501387912668e-10, -1.1643322091779131e-9, 1.0460478631512696e-9] km/s
+ V∞_out: [5.40368079653142e-10, -1.791585468845959e-9, 3.146501058851286e-10] km/s
+ time of flight: 1.8192980200824758e8 seconds
+ arrival date: 2030-02-16T18:31:44.231
+ thrust profile: [0.34003267117294395 -0.019839122411122692 -0.11979560883261864; 0.08525906513524148 0.04165785459621938 -0.10214312875898536; 0.050095578933142114 0.03996785964565859 -0.10724633027264562; 0.03903067972685311 0.040706643767827635 -0.12235326067529194; 0.03880381115251034 0.04809664949416198 -0.1601142485645981; 0.0239785128553384 0.03408530048172002 -0.12509696726634387; 0.009930114507092521 0.016561509381177904 -0.06551413406153579; 0.0039353399049056135 0.0076090515727651395 -0.03292715984494706; 0.002909766639281396 0.005033445624278698 -0.024147678173859478; 0.0004658974263128564 0.0010806140247069326 -0.005222631306972615; 0.0008829107319014524 0.001567405886446123 -0.009504190126279696; 0.00039146987491427403 0.00023580529789884474 -0.0011704496676884504; -8.905785742721565e-5 0.00013259094698593702 -0.0010570095825308925; 0.00016338433199271845 -0.00045773169902323135 0.0005571080718723472; -0.0005515718698311757 -0.0016050201436550596 7.474812080818217e-5; 0.00043300897631092834 -2.649855736946901e-5 0.0006103723062134522; -5.529658573079192e-5 6.758516692167873e-5 -0.0007162131028081995; 0.000480444856791083 3.120062276807304e-5 0.0012575943257153348; -0.0002795798494258074 9.703908610540275e-5 -0.0007784607146381127; 0.0005054364300733522 -0.0005962134158834073 0.0012431974239657854] %
+
+Mass Used: 88.06827233534023 kg
+Launch C3: 96.28953075172059 km²/s²
+||V∞_in||: 1.782864039906242e-9 km/s
diff --git a/archive/ES_0.5569458763774435 b/archive/ES_0.5569458763774435
new file mode 100644
index 0000000..afc3c02
--- /dev/null
+++ b/archive/ES_0.5569458763774435
@@ -0,0 +1,22 @@
+archive/ES_0.5569458763774435---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T01:49:12.493
+Launch V∞: [8.143691211002126, -5.649461714732091, 0.127281930801699] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.909228493101782e-5, 2.3498873539871207e-5, 0.0018807541629390584] km/s
+ V∞_out: [-0.0017098054666126838, -0.0005330687600627395, 0.0005770771761059712] km/s
+ time of flight: 1.874957778749047e8 seconds
+ arrival date: 2030-04-24T03:58:49.493
+ thrust profile: [0.2237033271388743 -0.005823878211984363 -0.07804512526940506; 0.03395564428145016 0.01796165133210764 -0.043730721159875065; 0.031929747698897976 0.02571955692094262 -0.06983747903282835; 0.07433966717220242 0.07618636395548913 -0.23194420411347855; 0.015021220426940943 0.018440279133949935 -0.06506889050153869; 0.014119377671471452 0.020682045410589163 -0.08014715013857011; 0.007800624297014871 0.013376416607293266 -0.05587442024588815; 0.01259081960893915 0.0210808785350793 -0.09528114150812951; 0.0021691326159734296 0.0036632117815554974 -0.020863418839086493; 0.0011820780123853291 0.002395075323672529 -0.013252648695975115; 0.0002615450988444158 0.0022568626523986122 -0.007184704578313608; -7.58694226892793e-5 0.00033943819973273736 -0.006424608174684898; 0.0008052457703323424 0.0012101924881590092 -0.010150051582219276; -4.535828459657971e-5 0.0005371816310458517 -0.0014440702141738835; -0.00012763536612060396 -4.98366956762494e-6 0.0010494056769007232; -0.0005476706828608531 -3.3617984416876683e-6 0.0005838382571950306; -0.0010343313572952386 -0.0012251046519332971 0.003117017083354011; -0.0008774018896524911 0.002126148455689485 -0.0032127946965647557; 0.0007242090452789626 0.003667069047367009 -0.003465306104940309; -0.004634075254767374 0.009127338686893256 0.001943476274010778] %
+
+Mass Used: 76.63162721201843 kg
+Launch C3: 98.25232489628554 km²/s²
+||V∞_in||: 0.001881307158656281 km/s
diff --git a/archive/ES_0.5569550228777239 b/archive/ES_0.5569550228777239
new file mode 100644
index 0000000..dbe0273
--- /dev/null
+++ b/archive/ES_0.5569550228777239
@@ -0,0 +1,22 @@
+archive/ES_0.5569550228777239---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T18:22:37.859
+Launch V∞: [8.057270406005376, -5.8822771997712655, 0.08316178498048363] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.496958520856389e-7, -2.745376632738351e-6, -7.817804073319684e-6] km/s
+ V∞_out: [-7.642400123488118e-6, -8.502069861633496e-7, 3.202521182029747e-6] km/s
+ time of flight: 1.8351544934874797e8 seconds
+ arrival date: 2030-03-09T18:53:26.859
+ thrust profile: [0.1449166116797537 -0.006881282365223778 -0.05440508062507403; 0.02692371013557069 0.011807665614599819 -0.03490925510858501; 0.028939162329593756 0.02121065729736499 -0.06737537207715595; 0.024131011510704636 0.021956175077244705 -0.08126035217358653; 0.025630372796841886 0.027047877391284014 -0.11206603798506516; 0.0313301185259715 0.03275369477917744 -0.16863973554061645; 0.012873712126321546 0.015816618403015088 -0.0773685470016699; 0.01806237411287862 0.02691587876761598 -0.13204958352700974; 0.006371671720115631 0.007908384552944812 -0.04878727526486053; 0.0016845983831039763 0.002338740358728274 -0.015348486827360583; 0.0004593369146093358 0.0006163090326957242 -0.004275773031827576; 9.272989625324907e-6 1.9721038345006996e-5 0.00021119458797619117; 0.00017573744153622897 0.000217622797447616 -0.0016866961719909572; -2.1997327994489153e-5 -1.5602922916097628e-5 0.0002989878761401649; 5.932023388149644e-5 -9.69774647871143e-6 8.356849347427874e-5; 5.363416518068177e-5 -4.497420444408623e-5 -0.00019384470060526188; -0.00014416165554882585 -7.852244234606236e-5 -0.00016722209246596427; -9.47248516686372e-5 0.0003115650706655461 -0.00021999015179745832; -0.00014663479670514498 -0.00026074106444656255 3.415821335567816e-5; 0.0004383178669093834 -0.00026448077251960134 0.000266261364666487] %
+
+Mass Used: 69.2025672486443 kg
+Launch C3: 99.52770733292004 km²/s²
+||V∞_in||: 8.329293873159427e-6 km/s
diff --git a/archive/ES_0.5569683602344979 b/archive/ES_0.5569683602344979
new file mode 100644
index 0000000..b125d1f
--- /dev/null
+++ b/archive/ES_0.5569683602344979
@@ -0,0 +1,22 @@
+archive/ES_0.5569683602344979---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T15:17:01.016
+Launch V∞: [8.165923711738584, -5.618304627839137, 0.12779230501469058] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00011663117231967875, -8.918966747674067e-5, -7.581328312615239e-5] km/s
+ V∞_out: [-1.4948221893156676e-5, 0.00010743966305085309, -0.00012464436306039298] km/s
+ time of flight: 1.8749577787493473e8 seconds
+ arrival date: 2030-04-23T17:26:38.016
+ thrust profile: [0.21809669433353768 -0.005908392456868439 -0.07273697999650976; 0.034034999977079906 0.018156037196182067 -0.04284445693638851; 0.06333895879112082 0.053973513157438945 -0.13160589023406466; 0.026104941903822346 0.029000872900036567 -0.08399073897896868; 0.026456367875796756 0.03459646455842795 -0.110970551454366; 0.017750611828959227 0.026730006838462814 -0.09283926324432569; 0.014461487229985059 0.02481629360975247 -0.09528380821625378; 0.00612929978827339 0.012470809262961012 -0.053357293150462996; 0.0015232580890306002 0.007254824823252974 -0.031103332984636994; 0.0016862809893034463 0.005567682430738261 -0.030572414383969897; 0.0012526296381909774 0.0027821223241291763 -0.0125880758171735; -0.0005685083790538548 0.0007972958201413168 -0.004586690252328389; -0.00026775463094883185 0.0018442331360548768 -0.008664746547115531; -0.0019664278856803235 0.0012884639464924917 -0.0032101458404750908; 0.0004613595078250248 0.0012128077357057114 -0.005609224062001859; 0.002518639014796924 0.003100526739584273 -0.0021523839863721327; -0.0005034859196302506 0.000535892123838871 -0.003840726005973152; 0.002537287367608102 -0.003779007582056339 -0.002775103808307292; -0.0010778827765680933 0.0005838794348517872 -0.002071271329828435; 0.0013852712824744514 0.00042443303061202224 -0.0017727165244022934] %
+
+Mass Used: 76.58982459651543 kg
+Launch C3: 98.26398783035408 km²/s²
+||V∞_in||: 0.00016524309679874773 km/s
diff --git a/archive/ES_0.556976169892065 b/archive/ES_0.556976169892065
new file mode 100644
index 0000000..0ffd78e
--- /dev/null
+++ b/archive/ES_0.556976169892065
@@ -0,0 +1,22 @@
+archive/ES_0.556976169892065---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:50:51.132
+Launch V∞: [7.941504309227328, -5.7264956428477625, 0.18806180704693345] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.0714339155326172e-9, 3.6318423700853933e-9, 1.5008372677560557e-9] km/s
+ V∞_out: [3.510749586036117e-9, -3.011837480940782e-9, -2.341704424301353e-9] km/s
+ time of flight: 1.8749577787464023e8 seconds
+ arrival date: 2030-04-22T19:00:28.132
+ thrust profile: [0.35271368600760133 0.016822454948070796 -0.09652406413685669; 0.07524318873878152 0.051692446183880116 -0.07684228252873629; 0.04571285411038394 0.05269678534487871 -0.0883262538859753; 0.06073494173180636 0.09554292764059354 -0.16643157754507112; 0.020037277596577932 0.03983209227466125 -0.08331326855701413; 0.015506265596014979 0.035049124111484566 -0.08237899934087642; 0.007841876061326617 0.027862462175752313 -0.06448799015746973; 0.007302898671072495 0.023337387206618942 -0.06093083811699602; 0.0033149238394516085 0.015021504368423639 -0.03937598552724881; 0.002008300294961157 0.009715041850331958 -0.02777105320276966; 0.0002051471489812136 0.0009721306963447311 -0.0030675654234243043; 0.00041270264374271954 0.0006010110152569724 -0.001985279437039519; 0.0007901988102005843 0.0005657185356642813 -0.002314756433378076; -0.00047703053835214783 0.0009750900878546669 -0.0008554382584270352; -0.00014030648088045021 0.00018401715630479785 0.0001301858306946075; 0.0013917967622816359 -0.0003004961987064222 0.00033119915537975996; -0.0016732121734174517 0.0003585108727373152 -0.0005578373881729621; -0.00033425810086594356 0.0007648284457023222 0.001160050723899847; 0.001180323583185045 0.001376115713209185 0.0013131329486114449; 0.0005262836379051331 -0.0004868100445781797 0.0017737541862186761] %
+
+Mass Used: 90.41447154899015 kg
+Launch C3: 95.89561028430039 km²/s²
+||V∞_in||: 4.987634489707218e-9 km/s
diff --git a/archive/ES_0.5569787979121936 b/archive/ES_0.5569787979121936
new file mode 100644
index 0000000..e08fcb3
--- /dev/null
+++ b/archive/ES_0.5569787979121936
@@ -0,0 +1,22 @@
+archive/ES_0.5569787979121936---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:55:43.625
+Launch V∞: [7.904731104294778, -5.787353397402225, -0.03751266928483194] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.021577358180528028, -0.1354626761051116, -0.14125411496057502] km/s
+ V∞_out: [0.034581049495373405, -0.03134397214939471, 0.1911187711853276] km/s
+ time of flight: 1.8749577783769006e8 seconds
+ arrival date: 2030-04-23T15:05:20.625
+ thrust profile: [0.3449246437473752 0.012142232538701534 -0.09952048172830821; 0.08963791116856083 0.05992361376598598 -0.09452535215119108; 0.05122110891265486 0.05708118129263654 -0.10027360223552462; 0.037073078295154126 0.05508374265580772 -0.10814559316268496; 0.021437240328802443 0.04008413810578999 -0.08837625984313656; 0.02013989420811925 0.044525513344453996 -0.1025430852942217; 0.008694913134996993 0.022811922576000357 -0.05743734526389968; 0.009483425666435969 0.029899336098845396 -0.0793037537033674; 0.004305937742455664 0.015723955506609107 -0.04596499857748133; 0.001366413294286105 0.00668415324914959 -0.02062896772891558; 4.669095492673586e-5 0.0012033561016841104 -0.004480188360136267; 0.00017219946059959682 0.00014529070233048838 -0.0007123721304722164; 0.0002452949228829903 0.0017142482776620544 -0.006205420027202594; -0.0005543946166385561 0.000589792870416675 -0.0005871814929383314; 0.00019069086482967291 -4.363038948994416e-5 0.00020216563371869723; 0.00146965686550194 0.00040292026133812494 -0.0008107953860088167; 1.7958682137257216e-5 0.00039120552117482134 -0.00019288744882107472; -3.058376629021031e-6 -0.0006633200016990541 -0.0003548080842764698; 0.000834610409104248 0.00028293975830593357 0.000616979733018677; 0.0003622396375453208 -0.00021374305899643932 0.0002863946707465865] %
+
+Mass Used: 89.92736202597825 kg
+Launch C3: 95.9796403779853 km²/s²
+||V∞_in||: 0.19689703907602196 km/s
diff --git a/archive/ES_0.5569830181902086 b/archive/ES_0.5569830181902086
new file mode 100644
index 0000000..e9c575f
--- /dev/null
+++ b/archive/ES_0.5569830181902086
@@ -0,0 +1,22 @@
+archive/ES_0.5569830181902086---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T03:20:16.444
+Launch V∞: [8.084998820726751, -5.691960849834864, 0.25914613880941856] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007713751418651621, 0.047406152964000046, 0.04946551682988098] km/s
+ V∞_out: [-0.012139315120801079, 0.010591344198525194, -0.0673460292001428] km/s
+ time of flight: 1.874957778707123e8 seconds
+ arrival date: 2030-04-24T05:29:53.444
+ thrust profile: [0.2487647604370798 -0.0014831740652170213 -0.08152665711112714; 0.04068599338635611 0.019773029217454063 -0.04937017570891666; 0.05086687081517731 0.04330564270459084 -0.10246000668007646; 0.04580468376348358 0.05154999430085547 -0.1358497308403277; 0.028838425444253725 0.038902337276230936 -0.11680174848649956; 0.02026998858630215 0.03247535781524729 -0.10778235901494125; 0.008114184693587306 0.013396109497522918 -0.05718960530823715; 0.00850657394324139 0.01466804779903116 -0.05737376790568052; 0.003228156290618777 0.0101070273419312 -0.04570764280232467; 0.0012474649804393922 0.0022570225863299347 -0.010446641898177182; -6.232575980298291e-6 -0.000850587441571749 -0.0019555745306898656; -1.1193781215692016e-5 0.00017439037016743947 -0.0005388609889603042; -0.00011375303726248007 0.0012594736823943009 -0.001120198059917756; -0.0030152956438807034 -0.00019006240307087964 -0.002983048452389924; 0.0014319538274325315 0.002492372078673882 0.0020729343110329626; -0.00030697853207155225 -0.0007842710533921603 -0.0018704418037544493; -0.0004908627288219856 -0.005814643733546477 -0.003553640556290592; 4.168275873757207e-5 0.002791630875179107 -0.006256807958176987; 0.002653522272232697 -0.0018101920417293725 -0.0038957339217129882; 0.005117581240809452 -0.002647179618837656 -0.00044719762957196377] %
+
+Mass Used: 79.12229890586059 kg
+Launch C3: 97.83278096846561 km²/s²
+||V∞_in||: 0.06894695537180853 km/s
diff --git a/archive/ES_0.5569830599473213 b/archive/ES_0.5569830599473213
new file mode 100644
index 0000000..4aa7911
--- /dev/null
+++ b/archive/ES_0.5569830599473213
@@ -0,0 +1,22 @@
+archive/ES_0.5569830599473213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:13:22.081
+Launch V∞: [7.918290247594108, -5.669108285909923, 0.11953117411789438] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00011259161772235448, -8.096203348309613e-5, -0.005772830249057515] km/s
+ V∞_out: [0.00561386029870674, 0.0009098469851710632, -0.0010012815058499072] km/s
+ time of flight: 1.8554214171776602e8 seconds
+ arrival date: 2030-03-30T02:42:23.081
+ thrust profile: [0.4653730605385432 -0.004637553436371362 -0.14175856497271866; 0.0672434028693785 0.03919474558925687 -0.07519602943816209; 0.07457610364670036 0.07135007163437326 -0.14733587882520768; 0.033840669559549334 0.04216842990492148 -0.10195071307754301; 0.020358434250318004 0.03180174653459066 -0.0884017992152496; 0.02076245826012853 0.038205018851775366 -0.10980420427905044; 0.008979719837303968 0.020819970248861987 -0.06292919330578782; 0.006586267734552078 0.01613862982041382 -0.05315943338988389; 0.004206305274197006 0.011978771798732525 -0.04122860019857485; 0.0007977158560870576 0.002303183242389268 -0.008048026442295913; 0.000722909513437091 0.0024080011070219116 -0.00884223879332315; -0.0003304102952122859 0.00029790716400453763 -0.0030528667410859764; 0.0010337125345635332 -0.0003221417655719632 -0.002016827440453379; 0.00033377299142264003 0.00020195885209571524 -0.001628078982063575; 0.0004470691999081708 -0.0010535493140397722 -0.0013071984724273374; 0.00012695323151038404 0.00027078925750646885 -0.00027209654751117663; 0.0006558713084458428 -1.4169071015095625e-5 -0.0015044524738921066; 0.00054343940687877 0.0006087291134286538 -0.002901807850015444; 7.954475257344345e-5 0.0003172672172793576 -0.0008963691771213037; -0.0021600823818849514 0.0013245167535350178 -0.0026064589597815492] %
+
+Mass Used: 96.50792133127698 kg
+Launch C3: 94.8523969041025 km²/s²
+||V∞_in||: 0.005774495718907454 km/s
diff --git a/archive/ES_0.5569941602771104 b/archive/ES_0.5569941602771104
new file mode 100644
index 0000000..e420506
--- /dev/null
+++ b/archive/ES_0.5569941602771104
@@ -0,0 +1,22 @@
+archive/ES_0.5569941602771104---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:16:24.907
+Launch V∞: [8.055465083126876, -5.62197359649785, 0.135453538169315] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.619217493740487e-9, -7.000208840015935e-9, -2.1575535886404024e-9] km/s
+ V∞_out: [-7.294061326861378e-10, -1.3626087260131597e-9, -3.849767632556943e-11] km/s
+ time of flight: 1.8674208000544104e8 seconds
+ arrival date: 2030-04-13T17:04:24.907
+ thrust profile: [0.3446927825386957 0.0012671427481388779 -0.10500762258040744; 0.04868166309195818 0.027953075223538373 -0.05532435535911624; 0.05237002102489422 0.048997630337188215 -0.10651564207136982; 0.04024656247266472 0.04988887535231583 -0.12171777194472536; 0.031585079857106846 0.04827582982073993 -0.12961498214105757; 0.01600033216465185 0.0284170582134513 -0.08524850665308843; 0.017434640634322072 0.03654817531289654 -0.11747572102875335; 0.0059801759761963025 0.01371034389784038 -0.04781746007949104; 0.00221516129261824 0.005704897514508033 -0.02138783070386524; 0.0005061110854881918 0.0006855314195764032 -0.0033278958865994353; 5.391797918452742e-5 -0.00015353371279401784 -0.00018052635183944796; -0.0006681780044537156 -0.0009987366331633584 -0.001013742278507109; -0.00022585541338218193 0.0016851826529539137 -0.003234488128161462; 0.0008251527792053232 -0.0002609045082405021 0.001048364464405695; 0.0007057820924776784 -1.3942812113515023e-5 0.00023363424319004138; 0.00024085858845254992 0.0010348768963013672 -0.001235994752877914; -0.00016849828308056715 0.0004105703661339521 0.0031131187229443843; 0.002264903535038502 0.0050752863505667675 -0.004948820592159545; 0.0026256586593523517 -0.0015421848660407663 0.00252608688289373; -0.0008466047170064802 0.00135169489371879 0.005279947001739227] %
+
+Mass Used: 86.81971415380804 kg
+Launch C3: 96.51545248619783 km²/s²
+||V∞_in||: 8.170477131642283e-9 km/s
diff --git a/archive/ES_0.5569978613603004 b/archive/ES_0.5569978613603004
new file mode 100644
index 0000000..b5cb2c9
--- /dev/null
+++ b/archive/ES_0.5569978613603004
@@ -0,0 +1,22 @@
+archive/ES_0.5569978613603004---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:43:31.858
+Launch V∞: [7.8831945647758594, -5.6592870885734285, 0.2618871086935921] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.838501066410777e-9, -7.365712271064684e-8, 1.3949133230756318e-8] km/s
+ V∞_out: [-1.248146095418154e-8, 4.623101829599692e-8, 6.023627332854553e-8] km/s
+ time of flight: 1.8749577787390026e8 seconds
+ arrival date: 2030-04-22T17:53:08.858
+ thrust profile: [0.5448255133749392 0.005050476591077465 -0.15622762422541328; 0.05845909770799732 0.03609379549494891 -0.06637317406007755; 0.0369350854908033 0.03715967354572706 -0.07701040679330633; 0.04098738577183241 0.05419360193801117 -0.12332792450455854; 0.026948444657013137 0.04495082404516431 -0.11296013108849375; 0.006872086240490214 0.01303296469131534 -0.038546554133859386; 0.015093605685597472 0.03502417797358323 -0.10413585085518712; 0.004233554182606614 0.010942623792639166 -0.03812047940092276; 0.00418130451021542 0.010516154725796074 -0.037695738407276025; 0.006415239182331711 0.01934969369272656 -0.06755398791463622; 0.00046367311316293763 0.001635756573254079 -0.006545931529782103; -0.00022255087901666215 -0.00038709403639626864 0.0007102352936706778; 0.00011555396573711275 0.00029722991521125166 -0.0003473166450380079; 0.00039921120261493336 -0.00029206068133785963 0.0006715187404416562; -0.00031526186409194156 -5.0199802286866185e-6 9.461711922913044e-5; 7.703353355256803e-5 -0.0013180008110231874 0.0014038460830058032; -1.8506175190572825e-5 -0.0004158074030939091 -0.00021125877704439018; 6.591120975790043e-5 -0.0014874804062269835 -0.0016916573687898906; -0.0015441390249845712 0.00010782715718588891 -0.0004440404541254732; -0.0013329350752644006 0.00013707898951582898 0.0019715320588527298] %
+
+Mass Used: 100.09241968456854 kg
+Launch C3: 94.24087175470545 km²/s²
+||V∞_in||: 7.548555586999158e-8 km/s
diff --git a/archive/ES_0.5570024037167939 b/archive/ES_0.5570024037167939
new file mode 100644
index 0000000..c372f51
--- /dev/null
+++ b/archive/ES_0.5570024037167939
@@ -0,0 +1,22 @@
+archive/ES_0.5570024037167939---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:13:21.669
+Launch V∞: [8.099798407129446, -5.753747975827175, 0.02332493388617581] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.2230464440864306e-6, 2.458025530929363e-6, 0.00016968392674106107] km/s
+ V∞_out: [-0.00015325530602212283, -4.9276856749490085e-5, 5.400760374955828e-5] km/s
+ time of flight: 1.8552064317471892e8 seconds
+ arrival date: 2030-04-01T00:44:04.669
+ thrust profile: [0.1577732859420673 -0.003896057135050146 -0.05514587438366696; 0.05519767834696 0.028874739374611925 -0.06627431327474669; 0.040179925323878624 0.032885808611119116 -0.08616296419815456; 0.055688237173771284 0.05816364236071816 -0.16391649144755638; 0.026606307449552558 0.033836151714752086 -0.10840367914918254; 0.02201274020745001 0.03242342566051385 -0.1107888926959601; 0.009553872342756274 0.016247617036006114 -0.06166762606515438; 0.005701599009121842 0.009777352684026809 -0.037122004605155884; 0.0044073956227996475 0.008988868161013608 -0.04017459826622838; 0.0032836951255945652 0.0072002317890209645 -0.03289953403090742; 0.0014827534414813602 0.0033290861928891207 -0.016462982516276547; 0.0008499081858082446 0.0020621519141552427 -0.00805494753985953; -0.0018200175469174134 -0.00040634487595597973 -0.005004015454020126; -0.0014789450178763445 -1.1184332858121864e-5 4.618725393653743e-5; 0.0023836824670828596 0.0004883493281596918 -0.003707905851288386; 0.0013851134211309369 -0.0010364253131389602 -0.0004213584120765835; 0.0015685483524552363 -0.0001290865979202155 9.245023449715747e-5; 0.0002674260351031659 3.0001161036436992e-5 -0.0016187012531573412; 0.0006904608572974561 0.0011680261826655055 -0.0006616785059077781; 0.004092081163360876 0.002558133244652769 -0.00042740627761303404] %
+
+Mass Used: 74.0109223311847 kg
+Launch C3: 98.71289405801282 km²/s²
+||V∞_in||: 0.0001697323331370815 km/s
diff --git a/archive/ES_0.557013596661526 b/archive/ES_0.557013596661526
new file mode 100644
index 0000000..d94a1b1
--- /dev/null
+++ b/archive/ES_0.557013596661526
@@ -0,0 +1,22 @@
+archive/ES_0.557013596661526---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:57:10.759
+Launch V∞: [7.734691598842479, -5.636406772048409, 0.16828681279046273] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.892742081679698e-6, 5.5741822585277716e-6, -4.363736609895713e-6] km/s
+ V∞_out: [1.2945611890251977e-6, 9.785213417299372e-6, -4.527017173002405e-7] km/s
+ time of flight: 1.874957778736943e8 seconds
+ arrival date: 2030-04-21T13:06:47.759
+ thrust profile: [0.7442518262918557 0.0015411717173377322 -0.17928703249790773; 0.08162158219549379 0.051965501892338783 -0.08620131156065358; 0.04322840367619943 0.045113947340193535 -0.08437315399356088; 0.031077363454163138 0.04383193852268016 -0.091516753129675; 0.022171341108763155 0.03888410884339052 -0.09032252203361683; 0.014263877520249095 0.03110007533926713 -0.07818029385609858; 0.01903435465234267 0.0520719055224337 -0.1308046690738333; 0.005516522751934498 0.01621474749363578 -0.04607123423720609; 0.0023325297884909863 0.00871750180516353 -0.027844171841315653; 0.00019215661743317546 0.0008171801642721542 -0.002642432833087497; 0.0016941392915824163 0.007595781951985691 -0.025477858802481823; 8.665644327600282e-5 7.011036590076077e-5 -0.00036067764800721023; -0.00010335672477126761 0.00012965091266022691 -0.0003714732843011871; 1.8781211555149797e-5 1.4708846805853329e-5 -0.00033456210320997935; 1.584701120821235e-5 6.431152634651466e-6 -4.859013161296667e-6; -0.00016733431807192535 0.00035885215406563135 -0.0003674078339121533; 0.0004431603198058117 3.657654606239222e-5 -0.0010593548937351408; -3.81896129038071e-5 0.00024430896412544066 -2.0113144229171956e-5; -5.626221871978931e-5 1.515867391283811e-5 -3.522883937150616e-5; -3.410219727714996e-6 2.0593046162250086e-5 -8.110281968266602e-6] %
+
+Mass Used: 115.38253680186563 kg
+Launch C3: 91.62285588055678 km²/s²
+||V∞_in||: 9.880465497960513e-6 km/s
diff --git a/archive/ES_0.5570147599629904 b/archive/ES_0.5570147599629904
new file mode 100644
index 0000000..b0c52e2
--- /dev/null
+++ b/archive/ES_0.5570147599629904
@@ -0,0 +1,22 @@
+archive/ES_0.5570147599629904---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:58:14.315
+Launch V∞: [8.0602782732381, -5.701044182347609, -0.011770782385283786] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.822544267285288e-7, -4.2822846557692156e-7, -3.9985299391627705e-8] km/s
+ V∞_out: [3.707780844050393e-8, -1.810707142764927e-7, -4.799085060479377e-7] km/s
+ time of flight: 1.8749577788589105e8 seconds
+ arrival date: 2030-04-23T19:07:51.315
+ thrust profile: [0.22367753041933622 -4.101993749484686e-5 -0.06782604549321847; 0.10809668615350601 0.06802910859016346 -0.1138436181044433; 0.05756286535139866 0.05483134886346283 -0.11394173207170297; 0.03100939138108875 0.03579481635760684 -0.09482830704602362; 0.01675223744460955 0.024486030526841594 -0.07234505490198403; 0.013396146476133894 0.02262103776873713 -0.07444026797810288; 0.01207384614291533 0.022127512778940112 -0.08093209276741667; 0.007932454766029294 0.01815271881089099 -0.06505754105088381; 0.004666459624375247 0.011181035282967539 -0.044695368546343185; 0.0053127029546780604 0.014936009299946243 -0.05883511313520552; 0.0009046195482037813 0.001995410343909679 -0.01128101534024233; 5.182279503964148e-5 0.00018160414544429252 -0.0007879484378870303; -0.0008293280523239058 -0.0004744720292976114 -0.0004266318742561293; 0.00012748151437683207 -0.0005613679636032168 -0.0003024598966264631; 0.00029323166992488447 -0.0005825044984132041 -0.0007278842804112846; 0.0005282254052068941 -0.0008055692596521271 0.0006421188752040884; 0.000881228446883169 -0.0003197838289485189 0.0003418265972497937; 0.0004263841214481251 -0.0015284281515251135 0.0009641194434774167; 0.0008039168087084455 -0.0002880949431487346 0.0013823634093292798; -0.0004683141484854965 2.554659223175027e-5 0.0009794554933269602] %
+
+Mass Used: 81.27479984263755 kg
+Launch C3: 97.47012916243166 km²/s²
+||V∞_in||: 5.144375611341508e-7 km/s
diff --git a/archive/ES_0.5570202789624047 b/archive/ES_0.5570202789624047
new file mode 100644
index 0000000..f8c347a
--- /dev/null
+++ b/archive/ES_0.5570202789624047
@@ -0,0 +1,22 @@
+archive/ES_0.5570202789624047---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:50:40.989
+Launch V∞: [8.004458763600825, -5.792940013930459, 0.12999473466906358] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00665027649357375, -0.003045234777568145, -0.00029196081609196973] km/s
+ V∞_out: [0.0053699818967564055, 0.0024112638933436502, -0.0043809745526940305] km/s
+ time of flight: 1.8559513213829485e8 seconds
+ arrival date: 2030-04-01T08:02:52.989
+ thrust profile: [0.18173447892656716 0.0007432142700110369 -0.06042747030134057; 0.13549780158632452 0.08070983564998764 -0.14500589092850802; 0.05119821780498628 0.04878195111881612 -0.10362729603950978; 0.032016768142473555 0.04117667592710044 -0.09909248398856915; 0.027767197222636823 0.04380497718504365 -0.11583422556948059; 0.017982124775352087 0.03391765853386069 -0.09753898419965573; 0.006502972303806746 0.01417170413933407 -0.04682254402423057; 0.0043818920400608904 0.009936683337365804 -0.037543839397780554; 0.009668162738339318 0.02660165038909917 -0.09127312005883938; 0.0006322304192265048 0.002106563635617646 -0.009257362586867324; 0.0003799346334074247 0.0010482561929844865 -0.002116183678621947; 6.764119301489081e-5 0.0005633005552485029 -0.0022252346459202964; -4.9583472529027696e-5 -0.0007059656562440667 -0.0005264328557293889; 0.0004301780366866753 -0.00033470876047864714 6.516454549487989e-5; -0.0009010877298941075 0.0002112458188959545 -0.0002592760368887192; 0.00031132332526073394 0.0023317630719248018 0.0004633365749993752; 0.0010277342411440082 -0.00019204598140507045 0.0012455901061993958; 0.0027480093558511134 -0.0003355130649964938 0.000490727252010555; 0.00037927958746095526 -0.00033530810255989567 -0.0012058115503965558; -0.0008543162954532139 -0.0020021512310281816 0.0006127425916031375] %
+
+Mass Used: 80.25291783982993 kg
+Launch C3: 97.64641273422437 km²/s²
+||V∞_in||: 0.007320168946795092 km/s
diff --git a/archive/ES_0.5570250655506015 b/archive/ES_0.5570250655506015
new file mode 100644
index 0000000..34a34cd
--- /dev/null
+++ b/archive/ES_0.5570250655506015
@@ -0,0 +1,22 @@
+archive/ES_0.5570250655506015---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:41:30.938
+Launch V∞: [8.200246169464165, -5.628545991942911, 0.15012997906871356] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3054328439373257e-6, -1.8697816801940973e-6, -1.7943244623670203e-7] km/s
+ V∞_out: [1.856793860153983e-7, -8.248295352447902e-7, -2.125588705459775e-6] km/s
+ time of flight: 1.8749577787493798e8 seconds
+ arrival date: 2030-04-23T16:51:07.938
+ thrust profile: [0.1413399226822293 -0.0013881056931978695 -0.04720564338159558; 0.04433609274519939 0.024393025740273536 -0.05253126305506085; 0.04275438965722864 0.03795964228686389 -0.09044512361021528; 0.07369932564515705 0.08330071256787604 -0.22053317631609734; 0.02621001275260834 0.035996428985188705 -0.10929301702618258; 0.013671147699009041 0.021916740751289906 -0.07800451898540374; 0.006649819296016101 0.01274513231280738 -0.052203880974219956; 0.004556977693006866 0.011300156458239797 -0.044176043758484836; 0.001636191168852056 0.002795378156813618 -0.01357113326996558; 0.003371098743872557 0.009171719856217673 -0.035792481183202475; 0.00019934812965239496 0.00033931324125438783 -0.00419287964852287; 0.00048366594160495984 0.0016754055209119427 -0.006788966405089627; 0.0005186823919373709 0.002081717632079497 -0.0024554839624616634; 0.0016610776738198748 0.0014483402320656375 -0.0018568072237788672; -0.0005283910346676438 -0.0006536620875214602 -0.0006358901914367376; 0.004205171442169382 -0.0010210737959431 0.0021131083377863087; -0.00016293691288271435 -0.0009011636463634519 -0.0013142382589525858; 0.0008177108433320335 -0.00015322990316098562 -0.001223495761362103; -0.00539967055160491 -0.008085718485672189 -0.0022428171756308634; -0.0020928926620880166 0.008641060237944774 -0.004383503021641854] %
+
+Mass Used: 72.67112344494808 kg
+Launch C3: 98.9471062338435 km²/s²
+||V∞_in||: 2.2874515173839735e-6 km/s
diff --git a/archive/ES_0.5570259375399552 b/archive/ES_0.5570259375399552
new file mode 100644
index 0000000..a85793e
--- /dev/null
+++ b/archive/ES_0.5570259375399552
@@ -0,0 +1,22 @@
+archive/ES_0.5570259375399552---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T05:40:10.039
+Launch V∞: [8.02555717771048, -5.876915958837429, -0.04398804718114657] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007665612963078423, -0.004505237086478028, -0.00031869760603615957] km/s
+ V∞_out: [0.006253483141789119, 0.0035194066181027574, -0.005259495679218056] km/s
+ time of flight: 1.8556972520908165e8 seconds
+ arrival date: 2030-04-03T00:48:55.039
+ thrust profile: [0.16678636363975854 -0.004249549535136435 -0.06000362092354704; 0.037956615074145314 0.019001045536378654 -0.047960462573378104; 0.041520658181606156 0.03323772314872808 -0.09112580883667433; 0.06667257928614227 0.06901530924899163 -0.20561518910719143; 0.014508117755262923 0.01753465097365682 -0.06451841721130858; 0.019711222690722945 0.027420649642427998 -0.10583160947333095; 0.006338168745686472 0.010159192372211755 -0.04342892351276297; 0.009450967687250749 0.015837965421988547 -0.0727745349781348; 0.0018962169623514507 0.003420387500746031 -0.016927129994796987; 0.005715211676341633 0.010505311740637296 -0.054153696039190465; 0.0029403629650958576 0.005742522079473734 -0.030374182148199168; -7.40455063464639e-5 -5.958312514442595e-5 -0.0006567311705643352; -9.568069206940326e-5 0.00051616013984528 -0.0005366728274212568; 2.0791995180987596e-5 0.00020208596075825855 -0.0011036374046291676; 0.00010026929793949619 -0.00027101170738096905 -0.001149924250723796; 0.00010669055726430241 9.682881015052368e-5 -0.0011407625443937896; 2.2323133047818778e-5 0.0001433825547279578 7.566469422439263e-5; 0.00011137477047165541 -1.2291460103261434e-5 0.0002825711598965418; -8.70109149858468e-6 7.300830617886877e-5 -0.0002112394613160953; 0.00017553826161114636 0.0001755002343674865 -0.0003740222496306741] %
+
+Mass Used: 72.6573362652548 kg
+Launch C3: 98.94964414823308 km²/s²
+||V∞_in||: 0.008897210319487012 km/s
diff --git a/archive/ES_0.5570319951126492 b/archive/ES_0.5570319951126492
new file mode 100644
index 0000000..f397f49
--- /dev/null
+++ b/archive/ES_0.5570319951126492
@@ -0,0 +1,22 @@
+archive/ES_0.5570319951126492---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:44:04.205
+Launch V∞: [7.851449832278968, -5.59165860941578, 0.22712599659116078] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.765610698639095e-7, -8.950386629424183e-6, 1.5940423423619679e-6] km/s
+ V∞_out: [-1.4190317373035545e-6, 5.4075174921005435e-6, 7.237699834666521e-6] km/s
+ time of flight: 1.8570003767899886e8 seconds
+ arrival date: 2030-03-31T11:04:41.205
+ thrust profile: [0.6802270973829492 -0.01354749321368902 -0.21132358638761015; 0.050516814792716275 0.0272150391020783 -0.05984003770669329; 0.03898637446679091 0.034131411356071395 -0.08357861226883732; 0.03201422847926097 0.03687464050997473 -0.10132975444513671; 0.02624691519198888 0.03660587869294718 -0.11130812313810987; 0.016352343195267287 0.026982903117001987 -0.09001396332677093; 0.013137304790063883 0.024075267899490105 -0.08758520298101469; 0.004978034917468948 0.010440155270994674 -0.041503284524045586; 0.0057311561453231245 0.015242814091545811 -0.06075365394287212; 0.002405706127942512 0.0059823467955611035 -0.025587298342871243; 0.00011371855772846633 0.00030554305032994727 -0.00124023922962114; -7.013556430388726e-5 -0.00036741546879872733 -0.00038323554319713186; 7.613775486544559e-5 0.0002153344695368832 -0.0005274873152021467; -0.0005739892038614063 0.0005710044026275268 -0.00050784520647069; -7.962362310247803e-5 -0.000496971317475119 -0.00041043034217738976; -0.0008715253399406723 0.00046072725139556677 3.541618586326979e-5; 0.0010700799563353298 -0.0008399582030066133 0.0010130664784795936; 0.0008747204019654341 0.0002891362599477662 0.0003161130299992025; 0.0009095303304303365 -0.0001520115141852124 0.00026281846689007717; 0.00029547087546364303 0.0004498341928114996 0.00014948099521379615] %
+
+Mass Used: 107.58359693173907 kg
+Launch C3: 92.96349669137457 km²/s²
+||V∞_in||: 9.143525760262928e-6 km/s
diff --git a/archive/ES_0.5570407300806312 b/archive/ES_0.5570407300806312
new file mode 100644
index 0000000..6475a7c
--- /dev/null
+++ b/archive/ES_0.5570407300806312
@@ -0,0 +1,22 @@
+archive/ES_0.5570407300806312---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T23:36:15.057
+Launch V∞: [7.956472141553754, -5.760137599532887, 0.1781749255466063] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.819498577952439e-5, -6.268176051669051e-5, -5.723368089528662e-5] km/s
+ V∞_out: [-1.0464196686135288e-5, 6.9237729217566e-5, -9.167843163662791e-5] km/s
+ time of flight: 1.8749577787461713e8 seconds
+ arrival date: 2030-04-25T01:45:52.057
+ thrust profile: [0.3897976572313236 -0.009600643108820644 -0.13833931359436677; 0.02830997245571692 0.013915978551801062 -0.0371003658332214; 0.05057834576546019 0.03913792783079944 -0.115229123472527; 0.03674353724375314 0.035853429662486044 -0.12220858309133056; 0.033220176721345515 0.03831171187836216 -0.14609678805484616; 0.018002467912680318 0.023093316055723696 -0.09935778559271599; 0.010044792513182788 0.01404515811175919 -0.06727997729548586; 0.004965427130753921 0.006365734821431013 -0.03937610649997172; 0.00218445560766648 0.003433819983712412 -0.019899650056350453; 0.000537707617215876 0.002219436032751852 -0.012615341737419343; 0.0002580469504269086 0.00038655528372292397 -0.002066634441140075; -0.000492539331755771 0.0013096148046919218 -0.0017673956527995314; 0.00041465907940686406 -0.00022804828485600473 -0.00048027987145759284; -0.00109315692726334 0.0017386583343015501 -0.0030398802622474985; 0.0009701503753840077 -0.0003153590082605542 0.0009059920547098265; 0.002133563021837856 -0.00020371148089773047 0.0003414827787780611; 0.000725396982557574 0.0011722335793199897 -0.009518538621831683; -0.001192818560520601 -0.00015610978889715548 0.0018769462233424682; -0.000511197722954341 -0.000357948832387771 0.0008784373892250714; -0.000886745451830591 -0.010387615238414642 0.001787497417754472] %
+
+Mass Used: 86.86863270842878 kg
+Launch C3: 96.51638040896701 km²/s²
+||V∞_in||: 0.00011540863542800972 km/s
diff --git a/archive/ES_0.5570528277917399 b/archive/ES_0.5570528277917399
new file mode 100644
index 0000000..cf7d1be
--- /dev/null
+++ b/archive/ES_0.5570528277917399
@@ -0,0 +1,22 @@
+archive/ES_0.5570528277917399---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:05:04.336
+Launch V∞: [8.091672592927097, -5.661062532199839, 0.1846824754865586] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8393621380395607e-6, 2.779400314003157e-6, 2.6596907000376014e-7] km/s
+ V∞_out: [-1.9562725259275993e-7, 9.509885042631228e-7, 2.5305846397907267e-6] km/s
+ time of flight: 1.8749577787351194e8 seconds
+ arrival date: 2030-04-23T10:14:41.336
+ thrust profile: [0.2188261088401171 -0.0012344726753319257 -0.0734539141604156; 0.0921917797806232 0.04856138571157378 -0.10658535533371272; 0.05714235847979554 0.052227397167486096 -0.12290199238793971; 0.07055709668626198 0.08367267560321659 -0.21565063271566534; 0.014970750676740833 0.02217907942225917 -0.06399038515964973; 0.00896006943411329 0.015573007640262223 -0.05018541430431585; 0.007840040343766777 0.015128844612663355 -0.051630124535543755; 0.005401372697723914 0.01190404390242782 -0.04484836202834037; 0.004093395512560739 0.00962731421098384 -0.03549624574401738; 0.0007239914358001971 0.004836134088462555 -0.020580126368083325; 0.00032435637012154337 0.0028639110990938614 -0.010329310206997941; -0.00015884886481617983 -0.00019827422456169066 -0.0009128783007089291; -0.00022653635634510593 -0.0007451420544875767 0.0005243161138902429; -0.0005191586086273185 -0.0019075049238239088 0.0006490614860670176; 0.0014405229336570146 0.00053003951568626 0.004282166608174386; 0.0008238374180712757 0.0008931447626215514 0.0031541772010839422; -0.0007673433318723104 -0.0026404370152322146 0.0014241853135110968; -0.0008872904458706579 -0.001076942893973402 0.002817104017518943; -0.0006765622755542592 -0.0026579328089954258 0.002794421159294331; -0.0002907980205066271 0.0005719631174855543 0.00042920388096750594] %
+
+Mass Used: 80.81303764911854 kg
+Launch C3: 97.55690196135623 km²/s²
+||V∞_in||: 3.3435099411446315e-6 km/s
diff --git a/archive/ES_0.5570593007072622 b/archive/ES_0.5570593007072622
new file mode 100644
index 0000000..7d04bde
--- /dev/null
+++ b/archive/ES_0.5570593007072622
@@ -0,0 +1,22 @@
+archive/ES_0.5570593007072622---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:59:20.542
+Launch V∞: [8.182210506257084, -5.647158917875048, 0.15954016815277988] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.077038986407714e-5, 5.624732549863166e-5, 0.0038455903093542222] km/s
+ V∞_out: [-0.0034389634824691984, -0.0011514411532303653, 0.001282706248915901] km/s
+ time of flight: 1.8749577787390906e8 seconds
+ arrival date: 2030-04-24T03:08:57.542
+ thrust profile: [0.17357315097556894 0.00016548978074148202 -0.059598356579994315; 0.042659805301553166 0.023976323242564497 -0.052984449123175195; 0.03799435510055157 0.0334171866027867 -0.08363611560833038; 0.03254404958014319 0.038069689733289704 -0.10649916222200963; 0.019065393592423763 0.027232330243997026 -0.08712312382770178; 0.022293299895122024 0.03782854789057213 -0.1289198637727988; 0.009371331867427862 0.016879962013302722 -0.06639265374529947; 0.007911831547577838 0.016312597580419644 -0.06668768578315484; 0.0046956802667929886 0.011155145331102517 -0.04708976993655121; 0.0052854249129884985 0.014351724045678135 -0.05895552478273369; 0.00020075466102730075 0.0019017321411321335 -0.008146424230105373; -9.811115721248176e-5 0.0009090407726899793 -0.0036085090673707893; -0.0025054117913926414 0.00011648599461387379 0.00022260497456246127; -0.000651336255267408 -0.0005170120322247286 0.0014340390055129948; -4.412024780337899e-5 -0.00048412640355918 0.0003328433076546563; 0.000585751660608288 -0.00046191279827824253 -0.0017747218613405717; 0.0007768080213413534 -0.002331934586013977 -0.003256224629806681; -0.0012144563603695003 0.0008574143332904294 0.0015650867244533474; -0.0010436202147172833 -0.0031051471497264282 0.00016684961686694343; -0.0014150296761930685 -0.002768241196613171 0.00212224662556641] %
+
+Mass Used: 73.19336770525933 kg
+Launch C3: 98.8644256776937 km²/s²
+||V∞_in||: 0.003846849677970748 km/s
diff --git a/archive/ES_0.5570606627902951 b/archive/ES_0.5570606627902951
new file mode 100644
index 0000000..1ae8fad
--- /dev/null
+++ b/archive/ES_0.5570606627902951
@@ -0,0 +1,22 @@
+archive/ES_0.5570606627902951---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T22:30:37.966
+Launch V∞: [8.062251808107145, -5.621220124614465, -0.05678906941869655] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.1263243270427633e-7, 2.580167479095042e-6, -6.1031189727803244e-5] km/s
+ V∞_out: [-2.5367259676357063e-6, 6.102888604821259e-5, -4.041238747169956e-7] km/s
+ time of flight: 1.8749577787485334e8 seconds
+ arrival date: 2030-04-23T00:40:14.966
+ thrust profile: [0.350938556835529 0.004774354149320208 -0.10865668933031411; 0.04995834536882235 0.02961077558713762 -0.058970349531083585; 0.03794235775900737 0.03656937178325821 -0.08127013207797015; 0.025944550931942183 0.03319229348217413 -0.08331669856731735; 0.019804601874939702 0.03123811861922422 -0.08666886722092146; 0.020981633352938654 0.038646326229420276 -0.11566827194465107; 0.02171549036182236 0.04731095094114688 -0.14512549158157959; 0.008758134735300828 0.022539128365409167 -0.07792573278354634; 0.002189551762055257 0.005769718252378771 -0.02091294681454679; 0.00028841755428309513 0.00038415014247552784 -0.0016841301646866908; 0.0003038086090194288 0.0017515813885165283 -0.006475289122819519; -0.0007171034687662088 0.0013496725840184331 -0.0031820995479947697; 2.654222239807178e-5 0.0008556930642528164 -0.0011251193741552037; 0.0011208074305756044 0.0012253088051364343 -0.0021228833165684797; 0.0018856341611690544 0.004950003066600686 -0.00631114420767725; 0.0049583305673160044 -0.002100851334620526 -0.004789461231949542; 0.00030200962333989684 -0.00023190069868354564 -0.002993245899567334; -0.000586730744710804 0.0005699403768752308 -0.0020169059041789585; -0.002093319349917612 0.00019540331590613656 -0.0019626862533325892; 0.00041847378446128016 -0.001306091021499106 -0.0009209315809394168] %
+
+Mass Used: 86.3968446422432 kg
+Launch C3: 96.60124490510304 km²/s²
+||V∞_in||: 6.10870988780431e-5 km/s
diff --git a/archive/ES_0.5570646626227772 b/archive/ES_0.5570646626227772
new file mode 100644
index 0000000..5f60784
--- /dev/null
+++ b/archive/ES_0.5570646626227772
@@ -0,0 +1,22 @@
+archive/ES_0.5570646626227772---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:11:18.773
+Launch V∞: [7.772761690267896, -5.803774320628661, -0.1325753499196279] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.904631804107202e-6, -4.833516668924995e-5, 0.0009233384144674336] km/s
+ V∞_out: [3.7613372692176966e-5, -0.0009237262303283257, 9.537815661020136e-6] km/s
+ time of flight: 1.8749577777731198e8 seconds
+ arrival date: 2030-04-22T21:20:55.773
+ thrust profile: [0.46009617739187303 0.017525589711471164 -0.12256362405142268; 0.123894067669477 0.08409686487345036 -0.12338293848085252; 0.06638019864589685 0.07527711409056201 -0.12495544892681928; 0.03836503517421541 0.059562806884782334 -0.11215601228693944; 0.031520940097103205 0.06348855133032712 -0.1302889296389069; 0.01671612974820429 0.042333093179197305 -0.09470274489487154; 0.005707408951358588 0.01670186966863103 -0.04230145438175641; 0.004503013104167311 0.015547670601720546 -0.041214214141069475; 0.0019719335920110057 0.00847807914822148 -0.02270822551639506; 0.00044720555257042794 0.0037389159253343562 -0.011052671189657989; 9.42428313075651e-5 0.0008022563476920354 -0.0021022561621311304; 0.0001919308138292574 0.0003042815322642899 -0.0011200129859415342; 0.00023261120512587925 -5.284264107936927e-5 -0.0006520658336964556; -0.0001376890545061436 0.00016186222774768435 -0.0004461842417665781; 0.0002820100404944157 0.00013764027447978018 -0.0007859185434173245; -0.00016383503588047275 -2.7439757989773344e-5 0.00017245709231310862; 0.00011206907616466216 -3.795664388596344e-5 -0.0003252569241643836; 8.067772212633841e-5 -0.0006011911586232676 -0.000447672686308715; 0.00018043538361671912 0.00019182386230526385 0.0003398829513373148; -0.0003303515460674493 -0.0011506781570608626 0.00018003312833262232] %
+
+Mass Used: 100.8917912488746 kg
+Launch C3: 94.11719688189123 km²/s²
+||V∞_in||: 0.0009246156884799466 km/s
diff --git a/archive/ES_0.5570700716002794 b/archive/ES_0.5570700716002794
new file mode 100644
index 0000000..cac1007
--- /dev/null
+++ b/archive/ES_0.5570700716002794
@@ -0,0 +1,22 @@
+archive/ES_0.5570700716002794---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:11:52.270
+Launch V∞: [7.9255927966763124, -5.7171908332575185, 0.4047062376136154] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9030423175035168e-7, 1.9759953469565764e-6, -3.873699621148349e-5] km/s
+ V∞_out: [-1.4963695942181614e-6, 3.8572869660631455e-5, -4.150774246639298e-7] km/s
+ time of flight: 1.870118535307993e8 seconds
+ arrival date: 2030-04-17T23:56:05.270
+ thrust profile: [0.42815369134649334 -0.0010669092172282068 -0.13481447308318456; 0.054140245213706875 0.02980988217551389 -0.06420624932333063; 0.04914462745974193 0.04294357371986649 -0.10509247410354895; 0.041075844822566675 0.04798836339597491 -0.13056797891390756; 0.038771055688495024 0.05362717029569506 -0.1573192172990257; 0.019627728706090964 0.028881813228838992 -0.10123753881484565; 0.00996760271824292 0.018099025873678856 -0.06547175638879983; 0.004956541311568611 0.008480922572588864 -0.03510165691682386; 0.0008770776771343568 0.0007421207443639069 -0.00760647269430493; 0.001346118043876149 3.537530822899943e-5 -0.003908937773958786; 8.003583086079531e-5 -0.0010163862427601225 -0.0007470834459649557; 0.00032570870771299917 0.0021490320131205627 -0.0010190679029042056; -0.0019978045594255906 0.000915735031867892 0.002631770774460601; -0.0023422074424471477 0.00012968558127731327 0.002525848547059524; 0.0006516980917641701 0.0007450467735667288 -0.00035688395071025196; -0.00017814715366958606 0.0016542318314317964 -0.0008905310158409258; -0.000877999942125887 -0.001756652950088888 -0.00044190940992382; -0.000432607397759301 0.00025061196284960666 0.005938136818162808; 0.0023739009588463343 0.002083442434481315 -0.004033841369506867; -0.0007828514725290771 -0.0037761776487200104 0.004163899970864209] %
+
+Mass Used: 91.86878737564075 kg
+Launch C3: 95.66507934137461 km²/s²
+||V∞_in||: 3.878782861672334e-5 km/s
diff --git a/archive/ES_0.55707104061869 b/archive/ES_0.55707104061869
new file mode 100644
index 0000000..7676212
--- /dev/null
+++ b/archive/ES_0.55707104061869
@@ -0,0 +1,22 @@
+archive/ES_0.55707104061869---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:48:59.465
+Launch V∞: [7.814442672965079, -5.830770415219996, 0.006331966032875994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.808691997266607e-7, 3.6569031058801005e-6, -7.504486904287998e-5] km/s
+ V∞_out: [-2.792362632352996e-6, 7.506272493632529e-5, -8.133699495708111e-7] km/s
+ time of flight: 1.8299399528157067e8 seconds
+ arrival date: 2030-03-01T05:28:54.465
+ thrust profile: [0.43390063706412285 -0.01583799372685714 -0.14203485126653073; 0.09663741687899965 0.04898481501915026 -0.11275292091725911; 0.06826955305714587 0.05625373629084293 -0.14301926007031132; 0.03775666950005615 0.040215187606742704 -0.11697352707030756; 0.02390588385886091 0.030616321373069674 -0.09935943707581463; 0.01505498429451101 0.022267235108144528 -0.07880250785056514; 0.01056953957957516 0.017808399564750683 -0.06784179595490884; 0.006591311811703003 0.012129964181874118 -0.04823431904165337; 0.006842876621163924 0.014025189325335963 -0.06016150771705482; 0.00035691511895446376 0.001087647246825225 -0.004902601090067953; 0.0008679053641152717 0.001794354403577536 -0.009975719623898559; 0.00017201704623557516 1.2633373678765542e-5 -0.00031077859226887576; 0.00015548872377544833 0.00039208652938829675 -0.001919588441682856; 8.889444681626833e-5 -0.00042665494338675397 -0.0007890873759164597; -7.712069483222895e-5 0.00023433783029456746 0.0007918608451242268; 0.0005223673503917698 -0.0008050967989839103 -0.0011786346210069737; -0.00017439970029118143 -0.0009189489268483014 -0.0009124667861502842; -0.00017636692663433742 -1.5429826250956127e-5 -0.00012990668324812192; -0.0007746782679437915 -0.0009659781784768415 0.0007655198226837671; 0.0006977605209199639 -0.001046159874263352 0.00036159010293561285] %
+
+Mass Used: 95.37949228431034 kg
+Launch C3: 95.06343801785621 km²/s²
+||V∞_in||: 7.513545464809572e-5 km/s
diff --git a/archive/ES_0.5570866734138671 b/archive/ES_0.5570866734138671
new file mode 100644
index 0000000..8676169
--- /dev/null
+++ b/archive/ES_0.5570866734138671
@@ -0,0 +1,22 @@
+archive/ES_0.5570866734138671---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:17:19.258
+Launch V∞: [8.000435777062568, -5.75109833158379, 0.14349714812185047] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.779746120719809e-9, -4.001624997883758e-9, -3.2783579815492e-9] km/s
+ V∞_out: [-1.4511167836641834e-9, 1.275682044668724e-9, -4.693519833661155e-10] km/s
+ time of flight: 1.8495616882403237e8 seconds
+ arrival date: 2030-03-24T16:00:07.258
+ thrust profile: [0.2867226952013693 -0.006278490634531545 -0.09569840304979858; 0.05963049260234649 0.03080676228310942 -0.06750659953474254; 0.045246928894345395 0.037580129536778556 -0.09193710523156541; 0.05131793089914195 0.05653225627995191 -0.15349471377785898; 0.035594305393049856 0.04688021566020624 -0.14221445428141738; 0.020487169035536757 0.030526694565630407 -0.10298857222069087; 0.007803929602305972 0.012593011223499942 -0.04669270637262827; 0.005393997718212708 0.009410240010532863 -0.0375280593499314; 0.004464710538738848 0.008337759294623279 -0.0351082818357476; -0.0007959629124720344 0.004424900335571926 -0.008368725413003528; 0.001689474779257856 0.0030176893991939223 -0.01379427045361272; 0.00015223113885245965 0.004099150183015082 -0.010730991010774826; 0.0008561971508692574 0.0023436470499134127 -0.010208074524295528; -6.750551397964166e-5 4.792314312823437e-5 -0.00018065840162373014; 1.8397271597278813e-5 0.00018869089508503955 -2.3739731682085848e-5; 0.0005960564472513839 0.0005312820518504876 -0.00594579565395321; 0.00027063433999390766 0.0009530424895918439 -0.004842259991442496; -0.0005276033335990739 0.0005538881412535282 0.0005822813639910706; 0.0009267155656616077 0.0033536422208292217 -0.0063187931677777046; 7.735087537069521e-5 -0.0016885946892602575 -0.002220335523697458] %
+
+Mass Used: 83.50205855136664 kg
+Launch C3: 97.1026960739677 km²/s²
+||V∞_in||: 7.0431957702034374e-9 km/s
diff --git a/archive/ES_0.5571047093721792 b/archive/ES_0.5571047093721792
new file mode 100644
index 0000000..bc7534c
--- /dev/null
+++ b/archive/ES_0.5571047093721792
@@ -0,0 +1,22 @@
+archive/ES_0.5571047093721792---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:49:04.997
+Launch V∞: [7.946053766748336, -5.56270601640093, 0.2451193143380962] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.03953702452239721, -0.24091370000889267, -0.3230536548856244] km/s
+ V∞_out: [0.16365831977738146, -0.14091157405586374, 0.3423684780931016] km/s
+ time of flight: 1.8597850178150094e8 seconds
+ arrival date: 2030-04-03T16:30:45.997
+ thrust profile: [0.5686399670465884 -0.010280782213874354 -0.17373546013441915; 0.06646020717016372 0.03568687942016754 -0.07594739643627778; 0.039472452629094566 0.03433483395596054 -0.08258466635876391; 0.035941692241690026 0.04084805052241953 -0.10989281800206371; 0.017466692020659962 0.024252376738127624 -0.07285176059131213; 0.021288225379511264 0.03357665470689325 -0.1057010079585059; 0.01465085061472452 0.02426548076094228 -0.08656166334853523; 0.008954762135360061 0.01802759950682504 -0.0726981492706056; 0.003024330921094853 0.007170220400437456 -0.029174143801702728; 0.0017464739112072222 0.004586888072291931 -0.01966964645086985; 0.0015608201250590622 0.004185274267659538 -0.018813317331906394; 0.00040275167184653014 0.0014621000516621718 -0.006221587277515518; 9.577799364016119e-5 0.00030695148418736183 -0.0007193530507212611; -1.5980769244732277e-6 -0.0002922557482731524 -0.000679521644536734; -2.558524106476701e-7 0.00010292503821413462 -0.00033984637628339917; -0.0003228521560351246 -0.000510653217666485 -0.00018654570549371513; -1.7185375338397318e-6 -7.017986664024605e-5 0.0002449764253850825; -0.0004584492838174459 0.0006887512853069298 0.00037023176180831473; 0.0005902278690039851 -8.949705531176245e-5 0.0002671212292403235; -2.323534835647828e-6 -0.00010718967310525032 2.3074997094089386e-5] %
+
+Mass Used: 100.78477329209181 kg
+Launch C3: 94.1435521672201 km²/s²
+||V∞_in||: 0.40492746399203333 km/s
diff --git a/archive/ES_0.5571224699662749 b/archive/ES_0.5571224699662749
new file mode 100644
index 0000000..d8a7d2d
--- /dev/null
+++ b/archive/ES_0.5571224699662749
@@ -0,0 +1,22 @@
+archive/ES_0.5571224699662749---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T02:24:54.612
+Launch V∞: [8.133487471642537, -5.521160007054032, 0.23008763387310632] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.267202793172138e-10, -7.171253837917214e-10, -1.561276023919548e-10] km/s
+ V∞_out: [-5.996494347209683e-10, 2.1300080949351073e-9, -3.1433556827700474e-10] km/s
+ time of flight: 1.8749577787450263e8 seconds
+ arrival date: 2030-04-22T04:34:31.612
+ thrust profile: [0.35207036573178474 -0.0057345291654249215 -0.1144476577103727; 0.039311498998558576 0.021902945316582496 -0.049259564369664326; 0.05308296001336485 0.047781014995545115 -0.11424490879491932; 0.048364543182628984 0.056623881745667265 -0.15180193279725063; 0.030389990618891513 0.043491842225446234 -0.13087423013698507; 0.016961168803936524 0.028546252795761482 -0.09562925631022397; 0.006570716039642706 0.012080472607645248 -0.046664018637183724; 0.00580897815167805 0.011618286280977929 -0.050004326170218036; 0.003434810963619002 0.004456312460767376 -0.020467466218229168; -5.141664707316554e-5 0.0007888847693794101 -0.0038020341612196593; 0.000616689709168402 0.002005117400948102 -0.007857266339921589; 0.0010718584768457974 0.0005471445012782282 -0.004935201886941094; 0.0006276291242060378 0.002038076424763016 -0.0038162866947315122; 7.333312102611976e-6 -0.0014914216103036994 -0.001567658397607248; -0.0008474164086893165 -0.0010808959312027435 0.0016184134119192504; 0.0008709272404576521 0.0002409163170517929 0.0004298525169372688; -0.00102500155069392 0.000418923692625443 -0.0013169997467313466; 0.0041235186179413704 0.006341740464871134 0.0011049882033036156; 0.006230074010638226 0.003217357587845222 0.0014454627325500942; -0.0020264285003837746 0.0024767311470540745 -0.00029931853158645717] %
+
+Mass Used: 85.95257649495215 kg
+Launch C3: 96.68976659412031 km²/s²
+||V∞_in||: 1.1054913226893352e-9 km/s
diff --git a/archive/ES_0.5571266891840291 b/archive/ES_0.5571266891840291
new file mode 100644
index 0000000..3f73155
--- /dev/null
+++ b/archive/ES_0.5571266891840291
@@ -0,0 +1,22 @@
+archive/ES_0.5571266891840291---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:43:56.260
+Launch V∞: [7.9283852738932055, -5.708514993026255, 0.1440369112395644] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.472891558765643e-6, 6.283793342219102e-5, -0.0012235051563267234] km/s
+ V∞_out: [-5.134371315579071e-5, 0.0012239642398915677, -1.561521846105821e-5] km/s
+ time of flight: 1.8376753855678618e8 seconds
+ arrival date: 2030-03-09T14:16:14.260
+ thrust profile: [0.4415954291820292 -0.015272678366300717 -0.15470519261617116; 0.04421427067512761 0.02267563678511617 -0.050505916272684644; 0.06151329776902673 0.05160629556541561 -0.1241518681700936; 0.030743026805808565 0.03237436899831867 -0.09074547424311848; 0.027626741823042138 0.035007730713883335 -0.10801784532717353; 0.032711369353758415 0.05027872072723236 -0.16355273735592227; 0.014038062822758086 0.022662563786443168 -0.08027246836001252; 0.0066570376455832424 0.012377779358713587 -0.048576000485346854; 0.001000001174800232 0.0017062612670665017 -0.007335367907973082; 0.0008480274504335628 0.002015118544316039 -0.00893898221542172; 0.0006342493087628202 0.0019596471473709277 -0.0078647424463489; -0.00022351634088162565 0.0011493272546193023 -0.0039043925087349123; 0.0007596064324498033 0.0018025096807059004 -0.00840221803418292; -3.524779444951802e-5 0.0024781210547361824 -0.0042350124584157505; 0.0007565426219894646 -0.00012078359866892041 -0.002978677253631456; -0.00014170481979534845 0.00024392543353623857 -0.0009290396781358847; 0.00014172901195977318 0.0004439199750052176 -0.002086137571811867; -0.0007130857560414816 0.0004131845775142036 -0.0006517821402526056; -0.00032997443567802287 0.0007513759806593114 -0.0014014300314885613; 0.0016191312184905503 0.0016285676962912365 -0.0061217467173534535] %
+
+Mass Used: 93.08923591399935 kg
+Launch C3: 95.46718310869163 km²/s²
+||V∞_in||: 0.001225147037431107 km/s
diff --git a/archive/ES_0.5571504057691441 b/archive/ES_0.5571504057691441
new file mode 100644
index 0000000..b208ffb
--- /dev/null
+++ b/archive/ES_0.5571504057691441
@@ -0,0 +1,22 @@
+archive/ES_0.5571504057691441---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T06:45:13.181
+Launch V∞: [8.08392231532773, -5.747813924686484, 0.001594288483850045] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.969021493212289e-6, -1.8183418368487096e-5, -5.009479025942437e-5] km/s
+ V∞_out: [-4.9410251137864915e-5, -5.792374338888017e-6, 2.054891163176241e-5] km/s
+ time of flight: 1.8749577787410808e8 seconds
+ arrival date: 2030-04-25T08:54:50.181
+ thrust profile: [0.22774048411062092 -0.007678204771129941 -0.07968619339872378; 0.036729830584630266 0.01848765563608817 -0.04623010178311449; 0.04151273206850536 0.03225457244721509 -0.09138978153319371; 0.03404367547712535 0.03299209405250418 -0.10933837595427195; 0.02753746443420668 0.031011006877787704 -0.11631178574017044; 0.017676281890361634 0.02297187974199303 -0.0948502710480843; 0.00938561780332854 0.013649674420659572 -0.062445889101304504; 0.007105255708031321 0.013392546081126734 -0.06970189067774527; 0.004994770215809532 0.008428085357378353 -0.033810130957153045; 0.007438389163519181 0.00762870563036866 -0.06651089635737607; 0.000404037188629692 0.0009693601863689377 -0.0064041223873600546; -5.255322570737499e-5 0.0011121202607486844 -0.005466556573581447; 0.0005505526710712166 -0.00012079338375426546 -0.0036168829951894912; -0.0007408316788564954 0.0024868167168267874 -0.0016129043397843683; 0.00018941468346075153 -0.0006028931019288957 0.00030387813803640223; 0.0003728309291184031 -0.00043859170617467023 0.0014971479276167329; 0.0013426961105436808 -0.002108339509410456 0.0011141155421888955; -0.0007010507563672474 0.0008938892417970676 -0.0002068337353451949; -5.537821641401526e-5 0.00173159770231502 -0.0004039744544503971; -0.0018365707282460573 0.0024122816353689906 -0.0012569287489604284] %
+
+Mass Used: 76.0836632441642 kg
+Launch C3: 98.38716745482925 km²/s²
+||V∞_in||: 5.3746553147825284e-5 km/s
diff --git a/archive/ES_0.5571566669709154 b/archive/ES_0.5571566669709154
new file mode 100644
index 0000000..8610250
--- /dev/null
+++ b/archive/ES_0.5571566669709154
@@ -0,0 +1,22 @@
+archive/ES_0.5571566669709154---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T13:10:26.238
+Launch V∞: [7.874277478763028, -5.648277359056255, 0.27530608806032586] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.958557441687064e-5, -1.5932103728446926e-5, 1.2416440413355342e-5] km/s
+ V∞_out: [-3.906189993699086e-6, -2.7818443510651714e-5, 1.3450157473347513e-6] km/s
+ time of flight: 1.8466968638036224e8 seconds
+ arrival date: 2030-03-18T22:18:32.238
+ thrust profile: [0.551925728259488 -0.0043153652686594626 -0.15551002316138862; 0.060669948643924554 0.03544405216356664 -0.06579906905572346; 0.06696154450792338 0.0643440540014683 -0.12670906529338838; 0.036967819166987395 0.04780289463436591 -0.10720719993672873; 0.03225820770971471 0.054770345048081086 -0.13125576481236848; 0.026586740907749838 0.04440653331863459 -0.12205986519481592; 0.010310597250815156 0.02346323561738568 -0.0693024592465357; 0.0039791038190123505 0.010054483627846262 -0.03144380657384836; 0.0006440766254649482 0.0018183329205805885 -0.006311435927750337; 0.0012101665636271987 0.0038593602854218438 -0.013809520921617614; 0.0017058483584640567 0.005411703816383211 -0.019832068932800963; 8.6969947465001e-5 -7.591423553717465e-5 0.00017217051644518872; -0.00012686529828603954 0.00044039645133190893 -0.0007518973750623989; -8.983666992293867e-5 -4.342115548465551e-6 0.0003310419047669978; 0.0007340252804328515 -0.00037320580708734085 -0.000556908205517515; 0.00015360518657288655 0.00017820034280232114 0.00022310626194143218; 0.00010457288881428163 0.0004153455154869989 -0.00022047841780605226; 0.0006910598539688615 0.0008450145549661428 -0.0006482574922730868; 3.4150823807274015e-5 -0.00011323067384281745 0.0005177771718637445; 4.1707489152529976e-5 0.002073622544263157 0.00020139589090552965] %
+
+Mass Used: 101.78149925228763 kg
+Launch C3: 93.9830763795052 km²/s²
+||V∞_in||: 2.8135291841229833e-5 km/s
diff --git a/archive/ES_0.5571577042502565 b/archive/ES_0.5571577042502565
new file mode 100644
index 0000000..604bc87
--- /dev/null
+++ b/archive/ES_0.5571577042502565
@@ -0,0 +1,22 @@
+archive/ES_0.5571577042502565---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T13:41:15.214
+Launch V∞: [7.87371268531399, -5.838010490258048, 0.05719857376753647] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1347126462115192e-7, 7.080830532812686e-7, -1.6542323092742368e-5] km/s
+ V∞_out: [-7.177528240404394e-7, 1.6546225338101396e-5, -1.1921615727022213e-7] km/s
+ time of flight: 1.8749577787481713e8 seconds
+ arrival date: 2030-04-24T15:50:52.214
+ thrust profile: [0.33288253899314924 0.004465066798464282 -0.10637919894462666; 0.1428403529777365 0.08454642318401148 -0.1570493341664216; 0.041414646698346866 0.038823921852992466 -0.08750353382423931; 0.03378870972371067 0.04185184039527535 -0.1058556498910383; 0.022498122957993926 0.034139308860446485 -0.09614776241449821; 0.016202053871686765 0.029030292119356507 -0.08937349170844565; 0.008488131459079305 0.016766599396771456 -0.057575224566763755; 0.00627372523643864 0.013344686971816375 -0.04913682068276393; 0.004412476180337615 0.011415076959558915 -0.04361670480127293; 0.002753322588175494 0.005864275570716003 -0.023785462107328754; 0.0004229708680147564 0.0015538224255283012 -0.006717463451097491; 0.00020346327617772405 -4.382213985385235e-5 0.00012145589509169946; -0.0005161619619471024 -0.0015883494123480686 0.0008136383429388575; -0.00014435649747328842 -0.0003446644654628463 0.0007259988084345767; -9.927879572738979e-5 -3.764668052960371e-5 -0.00011236478882657273; 7.990812359819646e-5 -6.2738426791467e-5 0.00017690378020505427; 5.382289458976132e-5 -0.0003550816699836609 -0.0005927416938623315; 0.0009658762210181875 0.0011014899685500936 0.00047067653899737555; -0.0006875164916282221 0.0014896732814086498 0.0010088960368940284; 0.0005659631356728889 -0.001353367222106815 0.0018267308734869051] %
+
+Mass Used: 89.54488222150803 kg
+Launch C3: 96.08098961207848 km²/s²
+||V∞_in||: 1.6557859482521172e-5 km/s
diff --git a/archive/ES_0.5571605689970314 b/archive/ES_0.5571605689970314
new file mode 100644
index 0000000..e8169ea
--- /dev/null
+++ b/archive/ES_0.5571605689970314
@@ -0,0 +1,22 @@
+archive/ES_0.5571605689970314---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:47:03.484
+Launch V∞: [7.7549413682716155, -5.915287102429016, 0.26623962488999386] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1948567555019219e-9, -1.3150048722360626e-9, -1.424472205481999e-9] km/s
+ V∞_out: [4.334850944188826e-10, -4.665951252084524e-10, 1.7950494302356448e-10] km/s
+ time of flight: 1.8530332861303526e8 seconds
+ arrival date: 2030-03-29T04:55:51.484
+ thrust profile: [0.41743240103401186 0.006557902225726844 -0.11921804063700311; 0.08905961361221332 0.054596597457902685 -0.08825531443577686; 0.057499171264949064 0.05696330210170865 -0.10299186594496491; 0.045528276652753635 0.05932030650548161 -0.12053513009362488; 0.0310371904815635 0.050634820471693154 -0.11506786183543835; 0.01702011275655812 0.03432660580145133 -0.0869911605228964; 0.01890717414654488 0.040152187490962624 -0.10816763206108433; 0.004128142200550667 0.011492573536751233 -0.03334946144766615; 0.004465361860175855 0.012651342503986304 -0.03719167478414502; 9.814084168052473e-5 0.0003576229142729031 -0.0013129892175093424; 0.001028400563797033 0.0040109267823521646 -0.013494849402479308; -1.69324209154688e-5 4.368062455974714e-5 -9.253099656463275e-5; -0.0004915313404017284 0.00010724414373978265 -0.0009313297185638301; -1.1830118702750391e-5 -3.465662155775279e-5 -2.588074419881999e-5; -7.763637299483647e-5 -0.0003573440292003034 -0.0004715804245398608; 0.0009317240587464085 -0.00022280315473267151 -0.0008773530923007312; 8.259680743443532e-6 6.795304248599616e-5 -0.00026782370733251096; -0.00029718137054785167 0.0007535437218142993 -0.00028304194482750046; -0.0005272538401762111 0.0009142041930693413 2.0898623743612677e-5; -0.001315395557463238 -0.0017226239663436457 -6.448478965864394e-5] %
+
+Mass Used: 94.68370993696544 kg
+Launch C3: 95.20062066735505 km²/s²
+||V∞_in||: 2.277288199671687e-9 km/s
diff --git a/archive/ES_0.5571613023574139 b/archive/ES_0.5571613023574139
new file mode 100644
index 0000000..ec6a106
--- /dev/null
+++ b/archive/ES_0.5571613023574139
@@ -0,0 +1,22 @@
+archive/ES_0.5571613023574139---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T06:40:38.718
+Launch V∞: [8.022476553177302, -5.674448746778155, 0.15788833071945094] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.1197797491912957e-10, 3.6363044285138104e-9, -2.021086954900973e-9] km/s
+ V∞_out: [1.8447735066946334e-9, 3.611358745338875e-9, 9.234379597899233e-11] km/s
+ time of flight: 1.8559073211690566e8 seconds
+ arrival date: 2030-03-31T07:39:30.718
+ thrust profile: [0.32234027311259245 -0.006979511666895101 -0.09605000436424191; 0.10161002277553084 0.05786203919638955 -0.11406312081055504; 0.027214973100675305 0.02618410650029584 -0.05882028133138412; 0.02377153661251233 0.030752392278671464 -0.07889176938463649; 0.024436559234178545 0.03786189703716834 -0.10465147082411215; 0.02438208959988226 0.043472950206220065 -0.1278824026392854; 0.01341220206521915 0.02650074993001471 -0.0858665938230051; 0.008467217772328815 0.02100252610465444 -0.06889353330221215; 0.0030765809455221152 0.009662767124738472 -0.0358091541663635; 0.0021832135299253495 0.006746432621764751 -0.027618732737505747; 0.0012765401602268813 0.00446164082461813 -0.018236475139834552; 0.0003839434697888225 0.001428419573330487 -0.006724736591584206; -0.00025018091279816065 0.00047939075777762976 -0.0004884529358424799; -9.786888855747968e-6 -0.00032584574457063405 0.00040525244067461056; 0.0001476823715368713 9.462059478057452e-5 0.0013263571558145473; -0.001142344153289917 -0.0002907650310050163 0.001368718402709914; -0.0015294997370234175 0.0005589394978399258 0.00017383513374145813; 0.0007440351069053884 -0.0005110386814735034 0.0003743397084396259; 0.0007824532271556834 -0.0004135183598812717 0.0001168783680819025; -6.665316556531351e-5 -0.00023411395156054345 0.000425182785701386] %
+
+Mass Used: 86.61235986907968 kg
+Launch C3: 96.58442735106911 km²/s²
+||V∞_in||: 4.171909950242775e-9 km/s
diff --git a/archive/ES_0.5571859519148975 b/archive/ES_0.5571859519148975
new file mode 100644
index 0000000..fe7ad9b
--- /dev/null
+++ b/archive/ES_0.5571859519148975
@@ -0,0 +1,22 @@
+archive/ES_0.5571859519148975---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T22:32:52.888
+Launch V∞: [7.8471432711339855, -5.56245829347085, 0.1726363795340726] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.168732865344983e-7, -6.836614643828888e-6, 0.0001403341743182632] km/s
+ V∞_out: [6.714797757182307e-6, -0.00014162193421609403, 1.3237731655527073e-6] km/s
+ time of flight: 1.8749577790653732e8 seconds
+ arrival date: 2030-04-21T00:42:29.888
+ thrust profile: [0.6416957312500671 0.0006672770591223214 -0.1886354866210956; 0.12046052510746197 0.07169500868551942 -0.12859331356575385; 0.05220028720493126 0.050697753447525654 -0.10433873560852093; 0.04278596247484585 0.05608149766886216 -0.12747513862898308; 0.024105921277262216 0.039331338668287266 -0.10137663576725901; 0.013390433564396675 0.026163504458151993 -0.07485973930868374; 0.0044733192278336165 0.009244328758229574 -0.029150578340307477; 0.003915530721233015 0.010309895147902993 -0.03620564146864947; 0.0036034823010008903 0.011055895580634478 -0.03952003853148327; 0.002353897673510432 0.0075454885566139576 -0.031197883594473248; 0.00024552294910563585 0.0006010907223432179 -0.0027568518409208246; 0.0002104195477031787 -8.49420212537652e-5 -0.001234055625695646; -0.00022493612326322462 0.00048264193470891543 0.00011144347766817164; -0.0004442356396930822 0.0003846054272340573 0.00036983833937292044; 0.00024741443357489235 0.00033357990703053225 0.00047825196956493166; 0.0011906115657653268 -0.000990489002316298 -0.00023058664122640874; 0.00027314917769310164 0.00037461115571830946 -0.00015671975927480277; 1.0971518966831084e-5 0.00015922850601014636 -6.176217453369916e-6; -0.00024043878045482863 0.0010786458347744404 0.0003082218008132703; -7.107073616176887e-5 0.00024290793357354326 -0.0005506155108133251] %
+
+Mass Used: 110.18459246162001 kg
+Launch C3: 92.54840310384465 km²/s²
+||V∞_in||: 0.0001405024330347551 km/s
diff --git a/archive/ES_0.5571975028723698 b/archive/ES_0.5571975028723698
new file mode 100644
index 0000000..53e9b6a
--- /dev/null
+++ b/archive/ES_0.5571975028723698
@@ -0,0 +1,22 @@
+archive/ES_0.5571975028723698---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:19:22.570
+Launch V∞: [8.053828944578145, -5.639043553896613, 0.15108239647795504] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00522672506768673, -0.03559434284831813, -0.03731139062171237] km/s
+ V∞_out: [0.009139991998806858, -0.007998427625606012, 0.05038991196023864] km/s
+ time of flight: 1.8749577785759184e8 seconds
+ arrival date: 2030-04-23T07:28:59.570
+ thrust profile: [0.3362653614279587 -0.0005519588673914876 -0.10770596269048481; 0.05088482297901952 0.029430908357339736 -0.06125148839527195; 0.05395583416006075 0.04981461792219131 -0.11407999122119697; 0.03716696564342264 0.045086080975514024 -0.11755453760383909; 0.01686660925824626 0.024982525465490936 -0.07469117616714452; 0.02042858823380308 0.03560028076836749 -0.11248222020806019; 0.010401921600528587 0.01976150550938077 -0.07033394348837654; 0.006497042301728736 0.01444815790856428 -0.05324481227584056; 0.006673338837906606 0.017297188008760157 -0.06709894281324415; 0.001276880345298344 0.00166174609995262 -0.008745295145840095; -9.103088773260637e-5 0.002370200124495945 -0.011258456293861234; 0.0006240640641602174 0.001214264286778627 -0.0003141449706329999; 0.000737200257610347 -0.00010146160673170834 -0.0015816622397479222; 0.0016644631037228232 0.0021067603702677237 -0.0007630914728888032; -0.0007513963814001275 -6.871995405280964e-5 0.000699076222517271; 0.0031872463584165798 0.002008824298278327 0.002822082482363987; -0.0003441018699138288 -2.953660417088686e-5 0.0014588020770270674; -0.00048394087582598956 -0.0008576855000568241 -0.0034425038815166617; 0.0018734289348806491 -0.0014438212483474228 -0.002760124443912686; -0.0007370931830801683 -0.002001175234775816 0.0073825839483749] %
+
+Mass Used: 86.06326057397109 kg
+Launch C3: 96.6857987617932 km²/s²
+||V∞_in||: 0.05183064506508487 km/s
diff --git a/archive/ES_0.5572161488211104 b/archive/ES_0.5572161488211104
new file mode 100644
index 0000000..075ba3d
--- /dev/null
+++ b/archive/ES_0.5572161488211104
@@ -0,0 +1,22 @@
+archive/ES_0.5572161488211104---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:17:05.064
+Launch V∞: [8.033592761549102, -5.674012263379457, 0.11540658072588679] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.261173437933043e-7, 2.3953239651517872e-6, -4.9831750893984115e-5] km/s
+ V∞_out: [-1.8559459998288558e-6, 4.9820459086673896e-5, -5.434896221297775e-7] km/s
+ time of flight: 1.8749577787493497e8 seconds
+ arrival date: 2030-04-23T18:26:42.064
+ thrust profile: [0.34421353114339653 0.0012484562431380186 -0.10376135275783943; 0.06175628837976812 0.03537952053989993 -0.07207305183311048; 0.02920377909400948 0.026741053744606513 -0.06144829309351484; 0.020964991960121276 0.026623388038437758 -0.06907944519159; 0.018962237974386384 0.028408819468859793 -0.08267272377310296; 0.011944585235351057 0.021431054787790654 -0.06589847411419708; 0.02025147876558604 0.04229608425239501 -0.1350390081595593; 0.012186393322362725 0.026582212613539494 -0.09653341232131243; 0.004388698860003478 0.010886696917137577 -0.04614499058959983; 0.006286847851389524 0.01749080865698633 -0.06397327591675121; -0.0009228249644054225 3.930061527389903e-5 -0.0032492483778603447; -0.00021802582930464037 0.0004471986594263791 -0.0004236422763120606; -0.0013281645598174092 0.0010097415795170689 7.900709553786741e-5; -0.0018145310158068596 0.0002750662939282052 -0.0008407382520959255; -0.0006467781768874231 -0.0003400542176212011 -0.00022387661602512075; 1.3738042831273152e-5 3.2815371856248894e-5 -0.00032434691338185473; -0.0012825479072827756 -0.00031570498091947925 -0.0004368485860030858; -0.000981548953597549 0.002465141654606349 -0.002081410869640528; -0.00012532184714261692 0.0004420585461116963 -0.0010253383091150324; -0.0019862884087712435 0.004293059985244651 0.0014400011503882865] %
+
+Mass Used: 85.73181902805709 kg
+Launch C3: 96.74634650226943 km²/s²
+||V∞_in||: 4.9890353041244756e-5 km/s
diff --git a/archive/ES_0.5572183103571988 b/archive/ES_0.5572183103571988
new file mode 100644
index 0000000..eb0e692
--- /dev/null
+++ b/archive/ES_0.5572183103571988
@@ -0,0 +1,22 @@
+archive/ES_0.5572183103571988---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:41:52.575
+Launch V∞: [8.084203839634311, -5.689171335667318, 0.1261003253975276] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.962333241873952e-10, 3.595472467593179e-9, -2.021431325058881e-9] km/s
+ V∞_out: [1.8827047264911506e-9, 3.778249505038929e-9, 1.0544281753201308e-10] km/s
+ time of flight: 1.874957778749373e8 seconds
+ arrival date: 2030-04-24T01:51:29.575
+ thrust profile: [0.24161964756116172 -0.00025804604973539663 -0.08321055552669497; 0.06445450260903815 0.03640123876541847 -0.0784855018311313; 0.047486630411165257 0.04298027820125768 -0.10427769025218316; 0.03512711437773839 0.0415742926701217 -0.11450441725205496; 0.023315693328828505 0.03342164835154141 -0.10324205218799122; 0.019153044123918904 0.03206016012008074 -0.10781868750170488; 0.013063197046049553 0.024723008435576618 -0.08962233084729228; 0.004629988461059657 0.009657332207355821 -0.0390512557052476; 0.0036329984097734536 0.008007856180565027 -0.03456133119857856; 0.0018414995749118528 0.004551487860328526 -0.020452997539138353; 0.0006095955855514491 0.0013770001574606565 -0.0040360258199945275; 0.0004074044131332432 -7.230861731690404e-5 0.0003010786166023449; -0.0006906296558278205 -0.0007863990511805337 0.0011801600339863285; -0.00015047348902791203 1.1909157121176852e-6 -0.008204842132571756; 0.0017831176431549267 0.0040750384832100054 -0.0006199284970320113; 0.0008296969993316491 -0.004553373870679007 -0.0015042002187301193; -0.005544754557736278 0.002549676579797986 -0.000737951022696037; -0.0002384821859529789 0.00042253529351399455 -0.0018239684650923384; 0.0002984788276286437 0.006787258865638646 -0.0020236763523380293; 0.0019033227043587931 -0.002211112606638698 0.0010556505714429715] %
+
+Mass Used: 79.9559750035528 kg
+Launch C3: 97.73692349940215 km²/s²
+||V∞_in||: 4.143743200820543e-9 km/s
diff --git a/archive/ES_0.5572275366223713 b/archive/ES_0.5572275366223713
new file mode 100644
index 0000000..2d0e890
--- /dev/null
+++ b/archive/ES_0.5572275366223713
@@ -0,0 +1,22 @@
+archive/ES_0.5572275366223713---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:21:16.240
+Launch V∞: [8.032625216307306, -5.638371805863848, 0.17490380927743118] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.576802813186469e-6, 7.692434995960893e-6, -5.472918239663613e-6] km/s
+ V∞_out: [2.191289763248731e-6, 1.2551767887857921e-5, -5.766746926714453e-7] km/s
+ time of flight: 1.87495777876181e8 seconds
+ arrival date: 2030-04-22T01:30:53.240
+ thrust profile: [0.29841863780119837 0.009970030991702213 -0.08547917652465654; 0.11914757508012247 0.07876946364563454 -0.11987542275840311; 0.049697816367080434 0.05475858231567874 -0.09565454797906575; 0.028217927340549034 0.0415957395615782 -0.08215730719607886; 0.029112559751045215 0.05461581682632224 -0.11646667458671758; 0.020635287976658232 0.04821869471242786 -0.10867863349727051; 0.011280286689725664 0.03097338168427842 -0.07743761358938693; 0.007126871645215847 0.02271563860709458 -0.05946952698050631; 0.0022318101194403663 0.008325471059912213 -0.0234653577278942; 0.000809868684798401 0.0037091257102092453 -0.011023685234221847; 0.00032154371371286494 0.0009427031263154674 -0.004451190996292493; -2.8843046346596938e-5 0.00043764610683001063 -0.003722418301989725; -0.0006080953543197399 0.0008184805881664178 -0.0020499845990208385; 0.0006338760789477383 -2.4754803113955642e-5 -0.0019199785487985482; -0.0006188370878400769 0.005087363407484674 -0.0034652456737952623; 5.9268713968002885e-5 0.0006424720701158637 -0.0021507685479021277; -0.00033092150795007444 -3.092129550316463e-5 -0.0011144049286235685; 0.0004965472438087184 -0.0005029204533563468 0.0008764353137960042; 9.98877280355187e-5 -0.0011407235321077708 -0.00026964162599659846; -0.001666437356310629 -0.0031907584938946566 -0.00046343681008584846] %
+
+Mass Used: 88.08690038842269 kg
+Launch C3: 96.3448958293161 km²/s²
+||V∞_in||: 1.2754918138561684e-5 km/s
diff --git a/archive/ES_0.5572486334174265 b/archive/ES_0.5572486334174265
new file mode 100644
index 0000000..847c231
--- /dev/null
+++ b/archive/ES_0.5572486334174265
@@ -0,0 +1,22 @@
+archive/ES_0.5572486334174265---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:25:47.436
+Launch V∞: [7.8514745773614765, -5.689538795065171, 0.16686272190796203] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.9997404703387135e-6, -6.142184704647112e-6, 3.6035558825267803e-6] km/s
+ V∞_out: [-1.4633196609225385e-6, -8.561925904315002e-6, 5.077407965501944e-7] km/s
+ time of flight: 1.8749577787128222e8 seconds
+ arrival date: 2030-04-23T19:35:24.436
+ thrust profile: [0.6029487706868369 -0.008584091882690383 -0.1885780051003793; 0.04027585363348959 0.021095444015928853 -0.050225382316950624; 0.027897567031501272 0.024374168867994945 -0.06453458380000997; 0.02756671086032022 0.031177576670765466 -0.09462789472113106; 0.02233575559775639 0.03070780437542071 -0.1043267604201551; 0.013181343216617427 0.021100165558941116 -0.0788263253500349; 0.007344332900466916 0.01233776968863296 -0.05014295928454598; 0.009198325881668053 0.01832211081554179 -0.0772161442227149; 0.005096525390464789 0.009922752733113258 -0.047605512170228625; 0.006581684304082639 0.015759435232673234 -0.07387943914251538; 0.0012434846952863205 0.0031707023505633523 -0.01655137203846415; -8.390086177400983e-6 -8.048838449749464e-5 -0.0010527126731941915; 0.0007034011558945173 0.00046780921856243217 -0.000288835922466924; 0.0001141825996874496 -0.00018784112240590546 -0.001540851673704976; -0.00028047801199527247 0.0003724222107695215 -0.0003066165212937496; 0.0013544332432895484 -0.00016310426695845086 -0.0017747639192100815; -8.87089465700387e-5 0.0023795016735174796 -0.0021561121566562587; -0.0002729513118423171 -0.0004579847237408144 -0.0014981230793523384; -0.0003100330055427281 0.00040644858486801926 -0.0014825753942550326; 0.00073386802638345 0.0023655146336079218 -0.0006716533357926126] %
+
+Mass Used: 101.53137619343579 kg
+Launch C3: 94.04434790746774 km²/s²
+||V∞_in||: 8.701117900318157e-6 km/s
diff --git a/archive/ES_0.5572601509898316 b/archive/ES_0.5572601509898316
new file mode 100644
index 0000000..e564a95
--- /dev/null
+++ b/archive/ES_0.5572601509898316
@@ -0,0 +1,22 @@
+archive/ES_0.5572601509898316---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:40:11.530
+Launch V∞: [7.975545404651762, -5.765711611487309, 0.043721527484013784] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4137566334905268e-9, 6.698437597010045e-9, -1.5890796466587106e-9] km/s
+ V∞_out: [3.968923628956233e-9, 7.576021159519896e-9, 2.0451840333606396e-10] km/s
+ time of flight: 1.8749577785876164e8 seconds
+ arrival date: 2030-04-23T10:49:48.530
+ thrust profile: [0.1980941046154623 0.004858089599019669 -0.06352120029700548; 0.16728810209099684 0.10243699949932521 -0.16663744641665312; 0.10102391786424046 0.10340538447724773 -0.18751370322610547; 0.02812028430414226 0.03837232345161861 -0.09318118179292524; 0.020959256940278795 0.0362830348485854 -0.10281150553866684; 0.007938972332693162 0.01735337532385656 -0.04782351677242474; 0.004318556958154224 0.012122803703031171 -0.03611606778183448; 0.003686792632887655 0.010582828248774451 -0.03416519439560922; 0.0017556432659996553 0.006137906525614407 -0.018056059457921807; 0.00034142138646201144 0.013650935705018153 -0.047197534736545144; 0.0005577483696070408 0.002321089562434957 -0.0071436878199723965; -8.710749416766239e-5 -0.0004916339235604989 -0.0005722781387659866; -3.7364000943525575e-5 -0.0014585013271507198 -0.0022210550247810787; 0.002386532688081831 -0.0009747338614056801 -0.0035824584970056013; 0.0006137986907148681 0.0005284877706512637 -0.0018577827489910115; -0.0012363310566137161 0.00063354928739473 9.468138817473508e-5; -0.0012335632421244603 0.0008011035177853017 -0.0017283323303883247; -0.00024912136827901204 0.0009818234242667922 -0.0006348857187408482; -0.0003372760879056777 -1.1161474619786324e-5 -0.0021029519527419674; -0.003942551684961923 0.001374967493821187 0.00047340249331145233] %
+
+Mass Used: 85.15128846874632 kg
+Launch C3: 96.85466646046696 km²/s²
+||V∞_in||: 7.028011680639208e-9 km/s
diff --git a/archive/ES_0.5572703983382231 b/archive/ES_0.5572703983382231
new file mode 100644
index 0000000..2eec5ad
--- /dev/null
+++ b/archive/ES_0.5572703983382231
@@ -0,0 +1,22 @@
+archive/ES_0.5572703983382231---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T04:29:07.822
+Launch V∞: [8.06633460373422, -5.682283421071102, 0.08262528084652893] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.583477223514093e-8, -1.4682766685487822e-7, -1.3808263796625922e-8] km/s
+ V∞_out: [8.58791282382556e-9, -4.2401201587803495e-8, -1.7237398793693534e-7] km/s
+ time of flight: 1.8749577785428587e8 seconds
+ arrival date: 2030-04-24T06:38:44.822
+ thrust profile: [0.2887699866312239 -0.006224591471491044 -0.09855052763763804; 0.05245155786788203 0.02798796546690112 -0.06581861191505194; 0.057930129311804954 0.04743490647056758 -0.12257314437742002; 0.022481916287856733 0.02273319075176427 -0.07402363053558704; 0.022546631205815418 0.028716909870201642 -0.09971635265657477; 0.02818066828940111 0.03778773896291194 -0.14530876464200596; 0.006881294150831978 0.012244211353512714 -0.051261243887201755; 0.007556448056636039 0.013578112958990187 -0.05736534619156199; 0.00263590288994635 0.005203935459424108 -0.025609881708291992; 0.001259594308719551 0.008147906011790555 -0.03619991424954563; 0.0012951307546860387 0.003012254417750461 -0.023040030166156255; -0.00022379920546344552 0.0004162464816885535 -0.0020441396508533182; -1.221836320944948e-5 -0.00043930051226430134 -0.0008023727999483502; -0.0015137315815429732 -8.299666809380034e-5 -5.563430987345994e-5; 0.0015691581448450938 -0.0035722426420145698 0.0019006970897168611; 0.0006037472446666772 -0.0003563204924252704 0.00240546122009937; 0.0005769139307214866 0.0011159090383923713 0.0019382822456796842; 0.0006759193504375656 0.0006757465020123994 0.0020192101311727923; -0.0015920824449266932 -0.0016662284713455165 0.000984519108164837; 0.0015641207845429985 -0.006159811870656704 -0.00037746110566972286] %
+
+Mass Used: 82.21006449734205 kg
+Launch C3: 97.36092575381456 km²/s²
+||V∞_in||: 1.7587875219163243e-7 km/s
diff --git a/archive/ES_0.557278266014552 b/archive/ES_0.557278266014552
new file mode 100644
index 0000000..952e5c6
--- /dev/null
+++ b/archive/ES_0.557278266014552
@@ -0,0 +1,22 @@
+archive/ES_0.557278266014552---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T01:03:31.848
+Launch V∞: [7.95395627873384, -5.774044568048998, 0.10102173020772387] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.4331479333729274e-7, -3.992481273661181e-6, 5.261300697364575e-7] km/s
+ V∞_out: [-6.220073875136207e-7, 2.3687802064416663e-6, 3.2291844222027267e-6] km/s
+ time of flight: 1.8354583480016598e8 seconds
+ arrival date: 2030-03-07T10:00:45.848
+ thrust profile: [0.3204485388006095 -0.0050455182289238 -0.10298750885521278; 0.05873275882469127 0.034197627249121176 -0.07088523998378544; 0.05341285297941323 0.049121510586515066 -0.10785618504120954; 0.04820054228962866 0.061300719705725294 -0.14826686133381617; 0.028481607075682387 0.040767349158105606 -0.11288556189252111; 0.017071305547621495 0.035143531539309 -0.10458345966334118; 0.012032728128936576 0.0220658036127605 -0.07801084169933052; 0.005407243597917217 0.014589207120906977 -0.04985369436451022; 0.004464637770157425 0.01012702477666739 -0.0383113669274441; 0.0011237353374288818 0.0035787529145044055 -0.013358193079797102; 5.0154754933710334e-5 0.002728353237716062 -0.011247921277177112; -0.00025536549141231906 -0.00046503504077986856 -0.0020199257113593535; 0.0012062355911567333 0.00046785558864875684 -0.0004431245067422075; -0.00029364469028338256 -0.0015653740929026366 -0.00030974563633735905; -0.0012478892717861167 -4.807886922606212e-5 0.0012251497320427405; 0.0021307679908686345 0.0008549014352453956 0.0005762865956046631; 0.0016085984880205067 -0.0018541849599445445 0.0006961409131540084; -0.0019648050625331653 -0.0018271770693511294 0.0007149737964607912; -0.0002798821333713315 -0.00020313313163661354 -0.00026475284956436617; -0.0012473399244997926 -0.002158490246784808 0.0009323149019826631] %
+
+Mass Used: 86.56921382147857 kg
+Launch C3: 96.61521654779979 km²/s²
+||V∞_in||: 4.051326644052264e-6 km/s
diff --git a/archive/ES_0.5572844554976675 b/archive/ES_0.5572844554976675
new file mode 100644
index 0000000..9b9f834
--- /dev/null
+++ b/archive/ES_0.5572844554976675
@@ -0,0 +1,22 @@
+archive/ES_0.5572844554976675---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:19:49.220
+Launch V∞: [8.108166873812628, -5.696966223751774, 0.15360538488823738] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.727888217316075e-7, 9.080881114338038e-7, -5.858897737422581e-7] km/s
+ V∞_out: [-1.224097349888263e-7, -6.558380394861945e-7, -9.315897157228473e-7] km/s
+ time of flight: 1.874957778740231e8 seconds
+ arrival date: 2030-04-24T01:29:26.220
+ thrust profile: [0.17707743792848335 -0.00022761593484336594 -0.054471773711166294; 0.11166966829465717 0.06277100333151206 -0.12011295783360224; 0.03335703429165077 0.03065489249064752 -0.06918782542073591; 0.0223929112079949 0.025666101205554518 -0.06778205403620138; 0.020324347204505978 0.030325886830245244 -0.08547993740452842; 0.020616546946069417 0.03753925907011939 -0.11804919842771222; 0.015326692418924263 0.030385358758053115 -0.0999451033639915; 0.004301503227668133 0.009596531556777003 -0.035405958307113454; 0.005818438574325066 0.013741082451023488 -0.054935993645659376; 0.004581277655590877 0.012652901050693706 -0.04743674721880923; 0.0022250164393832904 0.006481604037067452 -0.023011664061603692; -0.0002094600213777408 0.0003447216085417245 -0.008536032708683652; -0.0007881600896904741 5.015246146374783e-5 -0.00023527481866331005; 0.00018039055835995446 0.0003866398272000762 -9.192553647528203e-5; -0.0006897237422596791 0.00048359848796798114 4.067569797341301e-5; 0.0007312685878646296 0.0005200213406077646 0.0011493783081711509; -0.0016605820748106558 0.0010178953913932006 -0.0015951028171913941; 0.00046217995180829316 0.00039113944036722845 0.00010150296827321666; 0.0015256065445882424 0.0013697090486752038 -0.0013424793607930675; 0.0023860450474033636 0.005192207970948499 0.0002464129135628535] %
+
+Mass Used: 77.2070966164506 kg
+Launch C3: 98.22138882242767 km²/s²
+||V∞_in||: 1.1431808040337307e-6 km/s
diff --git a/archive/ES_0.5572851342292358 b/archive/ES_0.5572851342292358
new file mode 100644
index 0000000..4e4529f
--- /dev/null
+++ b/archive/ES_0.5572851342292358
@@ -0,0 +1,22 @@
+archive/ES_0.5572851342292358---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T11:45:02.129
+Launch V∞: [8.064369330997282, -5.553878190749467, 0.17233208709169456] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.699420716992121e-5, -2.998279017009181e-5, 2.353207236429403e-5] km/s
+ V∞_out: [-7.83411484593416e-6, -5.2498973074970764e-5, 2.628111226459976e-6] km/s
+ time of flight: 1.8749577787484547e8 seconds
+ arrival date: 2030-04-21T13:54:39.129
+ thrust profile: [0.4017970913399872 0.001491358910692721 -0.09718693744534523; 0.03629699944939187 0.023207416255472124 -0.04015830128028357; 0.03859441133049831 0.04090546816853755 -0.07608596221762592; 0.026871711937893995 0.03823884128618194 -0.07985604037754303; 0.08549815887910107 0.12986779808811363 -0.2679865533547848; 0.011224737696540574 0.0247869062127818 -0.06380861812770323; 0.004147243050934812 0.011918862734664934 -0.03346052214448875; 0.004929139547550344 0.016018164305953517 -0.045350227368967044; 0.002446916222872919 0.009786093151371099 -0.028730419236069338; 0.002364965626957346 0.00883638878375048 -0.028628491948090255; 0.0012322966803048924 0.003294420366037297 -0.013191222328389568; 0.0004007639425816303 0.002026971876883924 -0.007704080189522672; -0.0007297024966689375 7.961764445029258e-5 0.00059158085126339; -0.0007078924827858672 -0.0002538353832279689 -2.9001712697334812e-5; -5.9188781421420365e-5 -0.00025644905494410727 0.0015068678040264635; 0.0006862184442035929 0.0010563073233910163 0.0006576790120174807; -0.0007109029759834117 -0.0003838190056914217 0.0007412621583821758; -0.0007359883489604115 -0.00047605297455847345 -0.00021066256523372866; -0.0004022076135348158 -0.00025583319010161903 0.0018791960722807906; 0.000981117110720091 -0.00018174573412027138 -0.0009032278149045613] %
+
+Mass Used: 90.6949915269629 kg
+Launch C3: 95.90931401265351 km²/s²
+||V∞_in||: 5.3115887456326805e-5 km/s
diff --git a/archive/ES_0.5572866645339087 b/archive/ES_0.5572866645339087
new file mode 100644
index 0000000..95b5393
--- /dev/null
+++ b/archive/ES_0.5572866645339087
@@ -0,0 +1,22 @@
+archive/ES_0.5572866645339087---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:08:14.905
+Launch V∞: [8.002911774658655, -5.694196325813209, 0.06155509305392578] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0093800585785909e-8, 4.072184346344646e-8, -7.979376349100631e-9] km/s
+ V∞_out: [1.955537680382789e-8, 3.879900079559411e-8, 1.0069737460886569e-9] km/s
+ time of flight: 1.8749577787139502e8 seconds
+ arrival date: 2030-04-23T14:17:51.905
+ thrust profile: [0.3323213037305157 0.001147942441325691 -0.1013365025161013; 0.07283289698343638 0.04215272597781039 -0.08241710089973911; 0.057997129467670785 0.05461735191599218 -0.11682683540225045; 0.031959644543075094 0.0396192697792273 -0.0986406953221809; 0.021990596906424888 0.033496928536549724 -0.09280339346018142; 0.016448994133021772 0.029416264322710866 -0.08889513144348445; 0.006674043817971155 0.014183774511566542 -0.04607366773256694; 0.00573727399804151 0.013610458489807034 -0.04824481016924983; 0.01067081065090987 0.027823762657363093 -0.09948937722090255; 0.002391964344950877 0.006956613585056085 -0.02785400221740518; 0.0006867540962333408 0.001105217140499934 -0.006888354684200388; 5.1176716839051035e-5 -0.0004392436118636746 -0.0005648413974138614; 0.00019691308817150122 -0.00020902958553818847 0.0004515810963494881; 0.001267717201096415 0.0022071143086527293 0.0008724102729732013; -0.0010761700174471227 5.437128575094902e-6 0.0013962612465425912; 0.00041377158781166556 0.0010899454447943352 -0.00022405282852813106; 0.0020819011214432514 -0.0025142425854313716 -0.00025273360519269717; -0.00019596341974857927 0.0001531764921376474 0.003254239179158752; -0.0005441654170683178 0.0002474714626222791 0.0011465230055350119; -0.002649693926868248 0.0020499370896896883 -0.00038503007744385696] %
+
+Mass Used: 87.40127204331884 kg
+Launch C3: 96.47425769935566 km²/s²
+||V∞_in||: 4.2706250037291213e-8 km/s
diff --git a/archive/ES_0.5572931027474869 b/archive/ES_0.5572931027474869
new file mode 100644
index 0000000..d8e3dec
--- /dev/null
+++ b/archive/ES_0.5572931027474869
@@ -0,0 +1,22 @@
+archive/ES_0.5572931027474869---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:31:21.173
+Launch V∞: [8.050556724995772, -5.798774143677779, 0.1257532836662107] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.704007452701553e-6, -4.0681127640797255e-6, 2.293784583577048e-6] km/s
+ V∞_out: [-1.0239464002048314e-6, -6.539542362222453e-6, 3.554134875193051e-7] km/s
+ time of flight: 1.8384860409760097e8 seconds
+ arrival date: 2030-03-12T21:34:45.173
+ thrust profile: [0.21370640619342973 -0.016525152231917906 -0.08208965853525893; 0.044570394218750815 0.018455098400192764 -0.06038486147223168; 0.04179782907824147 0.027288888816730035 -0.09963240070222365; 0.03736276737215027 0.03036499510084764 -0.12744063328177443; 0.02964300713699094 0.027533189829460118 -0.13149726644073267; 0.02113271903437784 0.021444780124804597 -0.11540841869541567; 0.013190040469464292 0.014124189065656653 -0.08556104753137218; 0.006705685760965562 0.007622144348494457 -0.05153006917930689; 0.0029939034175857373 0.004148875562380961 -0.02935736988998697; 0.0013435571218405522 0.0024577872069508023 -0.017465447031193175; 0.0012359961002226991 0.002144094008808992 -0.016801127393270388; 0.0002824868796730467 5.01046463469254e-5 -0.0005829144448420364; 0.0011242816606033782 -0.0005166601885015049 -0.0008903570560577444; -0.0003240672052305879 0.001990702720326195 -0.00046924199527243523; 0.0019995723868014327 0.00038461861850483565 -0.0021737515522144177; 0.0008024500669593761 -0.0004653026877388868 -0.0007301142027251548; 0.001415593279038374 0.00036374329624907023 0.0018315760386479868; -0.0021383467348738633 -0.00015710451965146664 0.0010232210416926866; -0.0006618397529466096 -0.000422450035119884 -1.1184378716461206e-5; -0.001896142364415423 -0.002826087797714063 0.0053855463076236485] %
+
+Mass Used: 75.86577547140632 kg
+Launch C3: 98.45305904011344 km²/s²
+||V∞_in||: 6.628625445157983e-6 km/s
diff --git a/archive/ES_0.5572994263328845 b/archive/ES_0.5572994263328845
new file mode 100644
index 0000000..7399b14
--- /dev/null
+++ b/archive/ES_0.5572994263328845
@@ -0,0 +1,22 @@
+archive/ES_0.5572994263328845---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:24:39.907
+Launch V∞: [7.89703169416093, -5.546063253325136, 0.18474146625847795] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.740274197000423e-7, -9.692993010841446e-7, -9.614306424468252e-8] km/s
+ V∞_out: [8.461425200465722e-8, -4.141527509628515e-7, -1.1069118325497583e-6] km/s
+ time of flight: 1.8580550320836234e8 seconds
+ arrival date: 2030-03-31T19:03:02.907
+ thrust profile: [0.6417752121771199 -0.010250435252795724 -0.1930834912018333; 0.06159643573381311 0.0349293355466915 -0.06895728236005465; 0.06811243360510963 0.06322102121674446 -0.13684699970818034; 0.028647227496823514 0.03528376153317794 -0.08696203228701212; 0.028959319640360984 0.0438356892584735 -0.11865907793575599; 0.015917522355315416 0.02870189728927539 -0.08470585315675831; 0.00717066142042776 0.0154824965729028 -0.04876834333627872; 0.013061910120531444 0.03107589414781507 -0.10368986021211732; 0.0011974824780309524 0.0037828913068900754 -0.013455028119758922; 0.0005153928368326155 0.0021744452081537903 -0.008093015840475453; 0.00012830856776113438 0.0003955049272966014 -0.0018121342024324059; 7.188471375200244e-5 0.0006051995535589624 -0.002363685021207309; -5.864629064419479e-5 0.00012961309817433 -0.0003106175322850024; 7.278852563384833e-5 0.000192647450119977 -0.000580742359674971; -1.3595172318208294e-5 -9.109603835562115e-5 0.0001245132017142702; 7.021653881970929e-5 -0.0001112475233493657 0.00016894040342440295; 0.00011392953384432183 8.818517415145848e-5 -0.00010373903504379853; 4.318939056077283e-5 -0.0002878570118908148 0.0002290155967575184; -8.669477441573296e-5 -0.00040181661434290043 -7.837212785870334e-5; 8.020628616706534e-5 0.00011335756000783293 -8.759811824441972e-5] %
+
+Mass Used: 106.77233390107631 kg
+Launch C3: 93.15605659782096 km²/s²
+||V∞_in||: 1.1845242025353746e-6 km/s
diff --git a/archive/ES_0.5573021311044974 b/archive/ES_0.5573021311044974
new file mode 100644
index 0000000..cd473b7
--- /dev/null
+++ b/archive/ES_0.5573021311044974
@@ -0,0 +1,22 @@
+archive/ES_0.5573021311044974---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:04:30.245
+Launch V∞: [7.95595306400246, -5.792334975169622, -0.10119947406439068] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008270151126278255, -0.005068573007302669, -0.005288824172896195] km/s
+ V∞_out: [0.0012699228266922183, -0.0011619310980680558, 0.007204244046807601] km/s
+ time of flight: 1.8538899443801466e8 seconds
+ arrival date: 2030-03-30T16:01:04.245
+ thrust profile: [0.3598736084380577 -0.009685052352476197 -0.1235446867658262; 0.020814180171350154 0.011280918561390909 -0.02657130794917272; 0.03351766425911056 0.030078534783641905 -0.07639193677678678; 0.03282915675780021 0.03843172487741725 -0.10808258491006882; 0.022561489177549153 0.03219853782154886 -0.1001850378614838; 0.02480377719990918 0.04108427139561527 -0.13810016154155064; 0.00741716288038516 0.015261696763328964 -0.058007348186142525; 0.003899432507376684 0.0075571582470796905 -0.031844558276007615; 0.009004715139754527 0.02125301478531207 -0.08962887863841108; 0.0020097189652007142 0.004709440613961862 -0.022283165771628043; 0.004316986847868187 0.012985200218933861 -0.05957153530567842; -5.8240534934847725e-5 9.202592003642405e-5 -0.00040210851057046306; 0.0001730413340878566 0.000349121187950928 -0.00046072274038269786; 3.3501366288921655e-5 0.0002849674915334276 -0.0007977247324424993; -0.00014266655382751115 -0.0006514768156452788 -0.00014830242297703876; 0.0002705754079745718 -0.0008337084394804315 -0.0005716032678838613; -6.7270570629478e-5 -0.0002801131703423121 -0.00037309946705072633; 5.822227026621026e-6 5.735813535254566e-5 4.3570963455870414e-5; 0.00019989189133575575 0.00012103584524959676 -0.0010685308470359716; 0.00020047771260200834 4.644442017208535e-5 0.0006227100033152394] %
+
+Mass Used: 85.17746571929683 kg
+Launch C3: 96.85857495473431 km²/s²
+||V∞_in||: 0.00737197717431919 km/s
diff --git a/archive/ES_0.5573043579050883 b/archive/ES_0.5573043579050883
new file mode 100644
index 0000000..f929de1
--- /dev/null
+++ b/archive/ES_0.5573043579050883
@@ -0,0 +1,22 @@
+archive/ES_0.5573043579050883---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:58:20.008
+Launch V∞: [8.05035118026241, -5.710600663614119, 0.1315527113572995] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.829417928128546e-7, 2.8276024679378806e-6, -6.457034964293802e-5] km/s
+ V∞_out: [-2.309458000593709e-6, 6.458858560298647e-5, -6.839728973130152e-7] km/s
+ time of flight: 1.874957778749322e8 seconds
+ arrival date: 2030-04-23T21:07:57.008
+ thrust profile: [0.2342841555256655 0.0016891378028846655 -0.07697983195229845; 0.09953873054595906 0.05799109415997657 -0.11333438229815804; 0.03683044658344314 0.034581923456854624 -0.07740629727681479; 0.052264518884794595 0.06515555128774327 -0.16091281971036858; 0.020612526656751343 0.030772007431887384 -0.08690691354278661; 0.01868872852659745 0.03521815740183598 -0.10710000497285585; 0.009788354063516842 0.018063516446386773 -0.06332180388223779; 0.0051609690713459505 0.011410706083000743 -0.040947388284897177; 0.0023545202547614738 0.006122759158591164 -0.022980356246519736; 0.0018349459557568768 0.004121798500182858 -0.014636679121154723; 0.0014041224297887318 0.004313136920277379 -0.017192537968018423; 0.002192067533936548 0.0008711241614730868 -0.003021378400122838; 0.0015886745042642582 0.0023146626109018156 -0.001373474833207987; 0.0012616411779110162 -0.00040811034942539925 -0.0014033671004523296; 0.001271633281444097 0.0007599447441752285 -0.0010988091589141853; 3.610734488604485e-5 0.0003278831378425034 0.00014152629564347834; 0.0012771754487855063 -0.0038199759489367094 -0.0013179276245718719; -0.0003201625871244169 0.0018668984337353956 -0.005340892365065443; 0.005863470090677942 -0.0020913963593112736 -0.009314687780244755; 8.123327497188147e-5 0.0017594079151577705 -0.006239624888470446] %
+
+Mass Used: 81.8092998352572 kg
+Launch C3: 97.43642018068785 km²/s²
+||V∞_in||: 6.463336625261473e-5 km/s
diff --git a/archive/ES_0.5573066538926623 b/archive/ES_0.5573066538926623
new file mode 100644
index 0000000..4463437
--- /dev/null
+++ b/archive/ES_0.5573066538926623
@@ -0,0 +1,22 @@
+archive/ES_0.5573066538926623---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T01:34:19.456
+Launch V∞: [8.000710778920736, -5.616694050411499, 0.1360525780898069] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.898451047167434e-8, 3.131017315989724e-7, -8.605015387512623e-8] km/s
+ V∞_out: [3.951563195483332e-8, -1.802224708442105e-7, -2.5350412715484575e-7] km/s
+ time of flight: 1.8618766490721798e8 seconds
+ arrival date: 2030-04-07T00:22:03.456
+ thrust profile: [0.4371934551662327 -0.006798254833549926 -0.14070869691596755; 0.060638742898855076 0.03402164171336792 -0.07068256500980862; 0.03566336326644543 0.03260586868107791 -0.07571978774509143; 0.03432662969305045 0.04099880239040122 -0.10699718070050682; 0.02969250203992681 0.04319263485742857 -0.12432951079807045; 0.013973294621724865 0.024377786317504084 -0.07691045294889139; 0.007924585580299945 0.01563729543018739 -0.05370843756252486; 0.010712200880287232 0.02533877623483284 -0.08880607222774999; 0.005238063381281436 0.014048241842560804 -0.05495537826163053; 0.002055633702004834 0.00596746712027195 -0.02428107757818598; 0.0004211597390151318 0.0012379828232634714 -0.005309129037861802; 0.00039731115082382616 0.0005073490595803944 -0.0045308480560406865; -5.283674997040034e-5 0.0011484214241306704 -0.0061059498929211505; 0.0009212702019279881 -0.0005793419532390803 -0.0025731829413746053; 0.00035151089520125376 -0.0007838957615478412 0.0001389263460710266; -0.0013647657520929433 0.0019447007356892714 -0.003137166894437131; -0.0009054359392302052 0.0010111776347191317 -0.003614807724253065; 5.6791759764639866e-5 0.0003723586370204633 0.0006868547446144697; 0.0002740338847563037 -0.0014200868057878523 -0.0009646906939640518; 0.002247027247638537 -0.002321383689997105 -0.0007382788606377444] %
+
+Mass Used: 92.65780679552381 kg
+Launch C3: 95.57713532787125 km²/s²
+||V∞_in||: 3.2704298703522744e-7 km/s
diff --git a/archive/ES_0.5573076608751073 b/archive/ES_0.5573076608751073
new file mode 100644
index 0000000..401ad1f
--- /dev/null
+++ b/archive/ES_0.5573076608751073
@@ -0,0 +1,22 @@
+archive/ES_0.5573076608751073---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T13:57:50.005
+Launch V∞: [7.843798759751223, -5.698388560914593, 0.1235731791676985] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6835961511212178e-9, 2.286257092971466e-10, -4.2484417975207604e-10] km/s
+ V∞_out: [1.433916052632812e-9, -4.715716649648249e-10, -3.856524843074508e-10] km/s
+ time of flight: 1.8538982609217688e8 seconds
+ arrival date: 2030-03-28T07:08:16.005
+ thrust profile: [0.5331751849919614 0.0003442200750574171 -0.1504559801369209; 0.08281353402746197 0.04895216998406223 -0.09049571610782381; 0.06486426153257442 0.06294065541739638 -0.12654262829891266; 0.02744045844384005 0.035572215598159915 -0.08338361994825712; 0.024571199221796805 0.039691851935907616 -0.10085069278292502; 0.01069712174589451 0.02044441417615944 -0.057771883597164966; 0.012117476603585118 0.02754577067456631 -0.08200296438015682; 0.0060000520248763255 0.015136941294065656 -0.05005270643203109; 0.005721029138194205 0.017203661463736086 -0.05588613280894659; 0.0044785852966871 0.014748968085651215 -0.052002709185314536; 0.0007231284631853647 0.0025598088696059313 -0.009808656150681693; 0.00014163184390322408 0.00041852074437560545 -0.0017449365626629196; 7.103605442702285e-5 0.00020523395125412257 -0.0007804041096780978; 5.689169025565564e-5 0.00019612935500386844 -0.0007253447806553219; 1.3778811915938038e-5 8.808375814280708e-5 -0.0005917809699882372; -1.7589230860561452e-5 1.7890100878497768e-5 3.123179488608058e-5; 0.00018141532629103964 0.00033066600710728966 -0.0003439698882764341; -0.0002720426557841577 -0.0004218111516111058 -0.00023168264886148322; -0.00036452419037221774 -0.0002713568994719057 0.00012408370715787545; 0.00020424184047401604 0.00041172787233862286 0.00030857829581694093] %
+
+Mass Used: 101.7884622403526 kg
+Launch C3: 94.01208150524673 km²/s²
+||V∞_in||: 1.751358984357866e-9 km/s
diff --git a/archive/ES_0.5573091509392426 b/archive/ES_0.5573091509392426
new file mode 100644
index 0000000..053dcc9
--- /dev/null
+++ b/archive/ES_0.5573091509392426
@@ -0,0 +1,22 @@
+archive/ES_0.5573091509392426---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:28:25.067
+Launch V∞: [7.916412515585392, -5.8577989225252995, 0.03724636466793853] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.787964580379473e-9, -1.2556514131145832e-8, -2.1427407056275698e-11] km/s
+ V∞_out: [-2.9453265611491104e-9, -5.97253506047358e-9, -1.5306608326111366e-10] km/s
+ time of flight: 1.8106874961507207e8 seconds
+ arrival date: 2030-02-06T16:20:54.067
+ thrust profile: [0.29820937982735907 -0.01396662803673338 -0.10006639454521657; 0.06945737187937066 0.03514829608967404 -0.08198229086337855; 0.03486647255211833 0.0285232808291748 -0.07378074916440801; 0.03316033162427442 0.03511036679487984 -0.10097495558205016; 0.0375687667515126 0.04823229806672234 -0.149720922159862; 0.023342092722386607 0.03493385549213456 -0.11926823506956541; 0.016857617296177102 0.02833593336503038 -0.10435588013914154; 0.012565789391044841 0.023406337256055346 -0.09204318933387644; 0.0033038831338398997 0.0068133202768387935 -0.029270322737778454; 0.0007419403174370888 0.0017955961060508107 -0.007772891202787391; -1.038598364781014e-5 0.00030296737527921175 -0.0008355037661357166; 0.0004729419550992722 0.0006854661418761272 -0.0015866136287662359; 0.00023218880710936546 -6.109152441084742e-5 -0.0001354469905438336; 0.001643617889495059 -0.0004903160135242015 -0.0010700157119676026; -0.0008943086757368594 -0.0015276220947850541 -0.0002516992665594622; 0.0005769434100349571 0.0006254830607950695 0.0008352741873583651; 0.0007257222455211127 -0.0010870082827923889 0.0005884492575102625; 0.0004034516362799865 -0.0018409318100294418 -0.0001428224611903765; 0.00029116309530394176 0.0009414777616965261 0.0003793456590663158; 0.0002690141196937133 0.0004889769607451331 -0.0008258938598726623] %
+
+Mass Used: 84.44944411465303 kg
+Launch C3: 96.98478262533658 km²/s²
+||V∞_in||: 1.343841921813747e-8 km/s
diff --git a/archive/ES_0.557309199010201 b/archive/ES_0.557309199010201
new file mode 100644
index 0000000..b583f2f
--- /dev/null
+++ b/archive/ES_0.557309199010201
@@ -0,0 +1,22 @@
+archive/ES_0.557309199010201---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T20:53:06.946
+Launch V∞: [8.154755891413345, -5.645120425758032, 0.12506303193612728] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0985928101197869e-6, -1.6005301962757704e-6, -1.5720310181173428e-7] km/s
+ V∞_out: [1.2206428359522106e-7, -5.990523808449981e-7, -1.8494522115651014e-6] km/s
+ time of flight: 1.8749577787493435e8 seconds
+ arrival date: 2030-04-23T23:02:43.946
+ thrust profile: [0.2197317847185517 -0.000916289794008389 -0.06981896962819478; 0.03508078567932597 0.02061758743504629 -0.04164684877632044; 0.03181558095996104 0.02895847029732388 -0.06780770003256588; 0.014710125760290025 0.01771653921075252 -0.04712120706104196; 0.011627393447894754 0.017057811195964855 -0.05023406519033227; 0.021601443752988413 0.03324998253768651 -0.1025700850074336; 0.05205784441115815 0.07595939615491364 -0.21721516476235714; 0.0027842149361532263 0.006581221995739112 -0.024734000489562216; 0.01341768907507961 0.02701561684954111 -0.10007482342420305; 0.00297563800264127 0.007160301839629536 -0.030820991391680087; 0.000618295770482607 0.0029417126509803703 -0.01552018285912667; 0.0009375159871796153 0.0022765993034615565 -0.0045643678994289096; 0.0005532882054236727 0.00044596182480983364 -0.00311158828993496; 0.00018701394503263063 0.0015255751361954919 0.0010502559648498206; 0.0005208437681216317 0.00031574287631266635 -0.0006821671164205692; -0.0011505368701910516 5.693408580163546e-6 -0.0009641765470791868; 0.0016996181814773353 -0.00363384982929893 -0.0020990172794206805; 0.000699213309359631 0.0004189797592720221 0.0005634491966531687; 0.0005733197096877244 0.000359565502408386 0.003775953527596975; -3.9317260507920604e-5 -3.851388501391697e-5 0.00026848043645319106] %
+
+Mass Used: 76.29282949301978 kg
+Launch C3: 98.38306903180825 km²/s²
+||V∞_in||: 1.947643675536333e-6 km/s
diff --git a/archive/ES_0.5573112794738022 b/archive/ES_0.5573112794738022
new file mode 100644
index 0000000..f4905e0
--- /dev/null
+++ b/archive/ES_0.5573112794738022
@@ -0,0 +1,22 @@
+archive/ES_0.5573112794738022---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:07:06.619
+Launch V∞: [8.139370491017818, -5.693058599144906, 0.008015415088956831] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.753668367630753e-10, -9.450572326471328e-10, 6.269454273218766e-9] km/s
+ V∞_out: [1.839266997835909e-9, -6.1204314736119556e-9, 9.567372268515215e-10] km/s
+ time of flight: 1.8568715369530958e8 seconds
+ arrival date: 2030-04-02T20:52:59.619
+ thrust profile: [0.19182598444450416 -0.006906779733544775 -0.06947566702628952; 0.04861738820331956 0.025555351133976268 -0.06424914032465319; 0.029987137476134722 0.02651121206017541 -0.07516127652590965; 0.03588474292120652 0.03414878734172369 -0.11042639702963769; 0.02046124327288168 0.02472085518324064 -0.09148461177885177; 0.014743058784825873 0.0228187879716768 -0.08980641871699041; 0.02168085956506914 0.024588369915103568 -0.1271535529866415; 0.007160031282409465 0.013841487254398701 -0.06394306909087727; 0.005637671482224747 0.014738048604469069 -0.07146634335592252; 0.0005325489283030495 0.0012232552086360545 -0.012412368891157441; 0.00041726324230993597 0.0022771279180150545 -0.008323901192986137; -0.0001242221219262227 2.4000733805770204e-5 -0.0035702352765090246; -0.0004710847700463434 7.628135257162558e-5 -0.00336095198516542; 0.00042181648560529836 -0.0010985908803296388 -0.00272764082098463; -0.0020133371840058154 0.0025501848334263037 -0.004111416173451576; 0.0008555999449621644 0.0018892897155200344 -0.005193161528599084; 0.001143651178194887 0.0017354958554048174 -0.00213018776505838; 0.003186091853439768 0.0019124234861525795 -0.0037977407618558588; -0.0014055732881547 -0.0009016782498081474 0.0016866515648065086; -0.0009615869495835 7.335681225384579e-5 -0.0011534792896980817] %
+
+Mass Used: 74.67788675976999 kg
+Launch C3: 98.66033245022845 km²/s²
+||V∞_in||: 6.358078615938453e-9 km/s
diff --git a/archive/ES_0.5573175278156579 b/archive/ES_0.5573175278156579
new file mode 100644
index 0000000..381e11a
--- /dev/null
+++ b/archive/ES_0.5573175278156579
@@ -0,0 +1,22 @@
+archive/ES_0.5573175278156579---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:01:41.475
+Launch V∞: [7.96686274703187, -5.685496791948874, 0.03829595181243253] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0033992964721067226, -0.020905020329393315, -0.020963657040611892] km/s
+ V∞_out: [0.004480345723789603, -0.003966775769295628, 0.029497953101753193] km/s
+ time of flight: 1.8588858297061807e8 seconds
+ arrival date: 2030-04-03T19:44:43.475
+ thrust profile: [0.38655955956696575 -0.004487723154880772 -0.12444749557287825; 0.051431021263370805 0.02883881611453841 -0.059111578784103294; 0.08476703785146998 0.07577402195424993 -0.1705858040375596; 0.03270523330527513 0.039337455110884864 -0.10062901202968953; 0.029515501595498633 0.043962231473917916 -0.12400261187337358; 0.02228885934002864 0.03770643848115954 -0.11735283966331791; 0.010720851806756847 0.021484691046516544 -0.07177842551808017; 0.0027900304294115807 0.007033668739705061 -0.02562548939441188; 0.0026090871631766262 0.006792843338068408 -0.025835491044855635; 0.0013987384932079138 0.00134740571518711 -0.007442625665532066; -2.4244165303935288e-5 0.0005168136874742185 -0.001764359781272797; 0.00020792144520988685 5.053797041519137e-5 -0.0004159596079586266; 0.000404523054828477 -0.001323524055582997 0.0024612644993862983; 0.0005115997199834268 0.002265042733014487 0.0004525214712106495; 0.0010344527947594988 -0.0015383098567287084 0.0010611496914194611; 0.0018352911750162877 0.002955231718880292 0.0004067438568852615; -0.0038949204602555265 -0.0048600964240789945 -0.0005635283768348539; -0.0013252778095529595 -0.003231335528438585 -0.0024343886237598806; 0.000944447458461409 -0.00013792355628079422 -0.0004380869247929693; -0.0031921480810742243 -0.003304867273972318 0.0028334442784161635] %
+
+Mass Used: 91.38653522775712 kg
+Launch C3: 95.79724238123035 km²/s²
+||V∞_in||: 0.02980016791888968 km/s
diff --git a/archive/ES_0.5573190415666736 b/archive/ES_0.5573190415666736
new file mode 100644
index 0000000..0895204
--- /dev/null
+++ b/archive/ES_0.5573190415666736
@@ -0,0 +1,22 @@
+archive/ES_0.5573190415666736---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:13:08.394
+Launch V∞: [7.820349634101228, -5.715443132036966, 0.5171251330169147] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.0499604808121e-7, -8.589478584557919e-7, -8.678830676465312e-8] km/s
+ V∞_out: [7.465415661697105e-8, -3.8867821797653296e-7, -9.75017358578935e-7] km/s
+ time of flight: 1.8749577786696896e8 seconds
+ arrival date: 2030-04-22T17:22:45.394
+ thrust profile: [0.5107790099003183 0.012563611832829804 -0.13131232302940457; 0.1304015929863513 0.08195198893922678 -0.1348874107339132; 0.041546721430935414 0.04185643307655512 -0.08100099146682944; 0.04044156629376933 0.052820088454194204 -0.11751542958339065; 0.017660948660208953 0.030366063640950458 -0.07406901026791671; 0.018678002006170872 0.03179040151901748 -0.08569165023321586; 0.01112039353290766 0.029425597413589275 -0.0772920088857017; 0.0045754202359840354 0.013555219008527618 -0.03893236268140266; 0.002037232297757996 0.006155057637012368 -0.02054479484428478; 0.004298846547858358 0.014253278627115035 -0.0471408064291215; 0.0006082461569344561 0.0014987396349789887 -0.006298305841464134; 8.097458348201443e-5 0.00021094751542936446 -0.0010471224347098085; 1.0119717275710143e-5 0.000691889554986596 -0.0007330950170928322; 0.00043799265610846633 0.0007405547257088127 -0.00027187484083399414; 0.00022002191904214825 0.00020437779637208373 -0.0002851738265575184; 0.0008344997870621709 0.0003476168399316641 0.0007115016179527495; -0.00023584417722981934 0.0014439024933114736 -0.00017522841986741263; 6.084416281137438e-5 0.0008310986026146682 0.001554145485842838; -0.000933939826920665 -0.0007629716194224063 0.0014425965644485517; -0.0010163634380157818 -0.0006395560230235751 0.0021969946147601185] %
+
+Mass Used: 101.33801600417382 kg
+Launch C3: 94.0915769983335 km²/s²
+||V∞_in||: 1.0542029462730355e-6 km/s
diff --git a/archive/ES_0.5573249930041305 b/archive/ES_0.5573249930041305
new file mode 100644
index 0000000..108123a
--- /dev/null
+++ b/archive/ES_0.5573249930041305
@@ -0,0 +1,22 @@
+archive/ES_0.5573249930041305---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:32:07.566
+Launch V∞: [8.016114139079919, -5.654173774715693, 0.15590065485056592] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.668575496234315e-7, 3.210585881895954e-7, -2.3369137025052465e-7] km/s
+ V∞_out: [7.40437904338016e-8, 5.586608063714387e-7, -2.66022109872558e-8] km/s
+ time of flight: 1.8543643991572422e8 seconds
+ arrival date: 2030-03-28T20:39:26.566
+ thrust profile: [0.3470149429085503 -0.0071726930882184785 -0.09557107851887243; 0.0814897915636185 0.052077424047680884 -0.09314110151063319; 0.046987504878354375 0.049305178348874164 -0.10069887729167207; 0.033760682515570004 0.047221179641367274 -0.10894112642355946; 0.024889015345520404 0.04402496913939462 -0.1136041127354523; 0.021454603547350827 0.04336222356013562 -0.12436870061130043; 0.007940139509674158 0.016944072903465935 -0.051818542701943526; 0.009281068731075755 0.024985285813913013 -0.07738049009463147; 0.003978285366170055 0.011419563297941852 -0.03787786195159944; 0.00020655967015302025 0.0009558289090085174 -0.002743389080547207; -0.00018276503120957766 0.00042679913199270724 -0.0016071663021150861; -1.0513563050362423e-5 0.0012267670342786831 -0.001641840548533941; -0.0013763563121914416 0.00046959451128187875 -0.005846421521369746; -0.0002906370146651487 -0.0024645317301914835 -0.00090597390690288; 0.0011472137576644423 -0.0002908188266701747 0.0008991881818721467; -0.002530964397779714 -0.00031128025804124504 -0.00045882627008122677; 0.0024604195495183554 0.00292300972517828 -0.0035647947589536773; 0.0003079110415907211 0.0013368714736077152 0.0016950641342612567; 0.0001022327334364557 0.0006782641331334585 0.0005049075880998615; -0.00019431844501452454 -7.844607927803393e-5 0.0003553243873242451] %
+
+Mass Used: 88.74207195702093 kg
+Launch C3: 96.25207197962251 km²/s²
+||V∞_in||: 5.406243939146406e-7 km/s
diff --git a/archive/ES_0.5573417263894809 b/archive/ES_0.5573417263894809
new file mode 100644
index 0000000..be3b8a3
--- /dev/null
+++ b/archive/ES_0.5573417263894809
@@ -0,0 +1,22 @@
+archive/ES_0.5573417263894809---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T04:49:21.301
+Launch V∞: [7.901581833057909, -5.675626666064773, 0.10485802944695118] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0016439359542732, 0.003134694260821763, 0.0011903926033262902] km/s
+ V∞_out: [0.0013757112495837783, -0.001999979151218166, 0.002833369367711587] km/s
+ time of flight: 1.874957779021503e8 seconds
+ arrival date: 2030-04-23T06:58:58.301
+ thrust profile: [0.49397438840018815 -0.002451980615587702 -0.15668413733729603; 0.08970022772624833 0.049277834179606315 -0.10385774878317747; 0.03743734661690117 0.03274902646385795 -0.07895750652273426; 0.02417018148069196 0.02757212551020911 -0.07583079346872867; 0.023280945748222044 0.03226273449392815 -0.0982760620771042; 0.03491533606718081 0.057007866778396886 -0.18654874289733303; 0.008781344039661364 0.015954328579118687 -0.05839886823976863; 0.0037360810518703175 0.008110406949718903 -0.031110601203989695; 0.0018899725851478865 0.004690600414011389 -0.018163957410709804; 0.0010052111273597354 0.002896418403915868 -0.010844734447391766; 0.00010645148528286297 0.0006385621929980038 -0.002037848656136644; 0.0007184315127298651 0.00035184161452740713 -0.004023739138792502; 0.0006142668488646403 0.0023144979993210925 -0.0034840770888829166; 0.0012755464369140826 -0.0031580488515653817 -0.0064104610644267835; -0.0003999517162136389 -0.0010351718344074417 -0.0008928997127053261; -0.0007197687920568044 -0.0007435068342890351 -0.0008323415717241983; -0.007553054343483922 -0.0031789931289792784 -0.0019935370343756296; 0.000420877436652473 -0.0005114851299848075 0.002406441751043868; -0.0006440632757107262 0.004653108039246434 0.001011283215321456; 0.0025933411492545695 -0.006567602629107473 0.003129795389978998] %
+
+Mass Used: 98.05609656791876 kg
+Launch C3: 94.65872872339581 km²/s²
+||V∞_in||: 0.0037344166988480245 km/s
diff --git a/archive/ES_0.5573504258771251 b/archive/ES_0.5573504258771251
new file mode 100644
index 0000000..9b39e5d
--- /dev/null
+++ b/archive/ES_0.5573504258771251
@@ -0,0 +1,22 @@
+archive/ES_0.5573504258771251---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:08:50.424
+Launch V∞: [7.773890606106722, -5.6833969400256334, -0.1931976242675697] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2632104458759304e-9, -2.08529805709181e-9, -1.8347173070073828e-9] km/s
+ V∞_out: [-4.574616248483471e-10, 4.871047260605738e-10, -1.6084946614609166e-10] km/s
+ time of flight: 1.8749577779115948e8 seconds
+ arrival date: 2030-04-23T14:18:27.424
+ thrust profile: [0.6908471624882283 -0.03573622160919928 -0.21077504212368078; 0.05597332263137145 0.028265445835388963 -0.07218300460015523; 0.04610058862741706 0.03718519367271297 -0.1068906462033044; 0.023036156297627737 0.023455932178093976 -0.08100845646408084; 0.023055734468531975 0.02805343568728107 -0.1078491473432842; 0.021343006839548775 0.030278775643437658 -0.12358154134511388; 0.013245202250942147 0.019873160526963998 -0.09213345604661377; 0.003204694961943807 0.005286815763734327 -0.027443413301977058; 0.003371306794020839 0.0060454104657489925 -0.0326525928255866; 0.0007417282077020163 0.0014054489534466178 -0.010691693244444578; 0.00040960647694349026 0.0016013639660441164 -0.0047956071688092725; 5.121209150874681e-5 0.00010079549578110161 -0.0008600126592053035; 8.717346371296057e-6 7.384556309572349e-5 0.0004986108660111398; 2.688201411019247e-5 0.0002675743556214683 -0.00020392453446409654; -1.4958775586405254e-5 -0.0001261533578868224 -0.000993257911999475; 0.0004835958573758028 -0.0009441231327247191 0.001726057387663642; 0.0015917332362381336 0.002939219096496854 -0.003155462523288121; 0.0007365195309995688 -7.387874910194311e-5 0.0014221558310895791; 0.0010850150864721204 -0.0008800470706577868 0.0017452402247337601; -0.0027435507556502967 -0.0017697900852274085 0.002299417936780117] %
+
+Mass Used: 109.07390619880607 kg
+Launch C3: 92.77170125562971 km²/s²
+||V∞_in||: 3.5828448341876637e-9 km/s
diff --git a/archive/ES_0.5573515817453158 b/archive/ES_0.5573515817453158
new file mode 100644
index 0000000..32f87c7
--- /dev/null
+++ b/archive/ES_0.5573515817453158
@@ -0,0 +1,22 @@
+archive/ES_0.5573515817453158---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T12:06:36.341
+Launch V∞: [7.898095598303892, -5.762305350172817, 0.12531156891718334] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.249506423157479e-8, 3.9986941311856855e-8, -4.899543210088101e-6] km/s
+ V∞_out: [-2.0821682446269444e-7, 4.893722206830284e-6, -3.6601122170941655e-8] km/s
+ time of flight: 1.8749577787464133e8 seconds
+ arrival date: 2030-04-24T14:16:13.341
+ thrust profile: [0.45917842612425175 -0.0073390610931889765 -0.14325211374087446; 0.0286797892126475 0.015816006736218923 -0.03608300777447172; 0.04130184185755159 0.03512418760696304 -0.0912680689827167; 0.041852796083841126 0.046094127439603255 -0.13543676242030753; 0.03595268910615089 0.0474253901032396 -0.15367660851288426; 0.013832052206885805 0.021892583174785516 -0.08017918031022359; 0.008972701148496775 0.015883073815413127 -0.06172762207680014; 0.004482685354296798 0.008839402565689354 -0.03791599739932195; 0.005627746432072523 0.01165259457742161 -0.04983914484366717; 0.0015239001215005244 0.0033980382713772435 -0.016811121801020235; -3.362860307512392e-5 0.0007740815019732681 -0.0011714566070615445; 0.00020703111769256011 0.0001611641552258352 -0.0018264792598468487; 0.0010002113975894305 0.00020515261198073595 0.0002915298998246549; -0.0030905941353663435 -0.0013074663091984938 -0.004082181505321216; -0.0008611116175486649 0.0034919711082089942 0.0017665355150444791; -0.004801955784112659 0.004432952173330111 0.00023198654121941585; -0.0013626867961847296 -0.0005870221680998442 -0.0010749371430473773; -0.0013038686910431467 -0.002284370675242768 0.0038192449696700533; 0.0008430816318762151 1.4856162743661695e-5 -0.0008619913492864785; 0.0030949772034834866 -0.0036392738891422543 0.0033952926262976095] %
+
+Mass Used: 92.5781285985563 kg
+Launch C3: 95.59978001788208 km²/s²
+||V∞_in||: 4.89981413445401e-6 km/s
diff --git a/archive/ES_0.5573532603770052 b/archive/ES_0.5573532603770052
new file mode 100644
index 0000000..465bc42
--- /dev/null
+++ b/archive/ES_0.5573532603770052
@@ -0,0 +1,22 @@
+archive/ES_0.5573532603770052---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:04:27.263
+Launch V∞: [8.074897719446726, -5.669702004742475, 0.03702525401025064] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.6359789961926617e-10, -9.722749026240112e-10, 2.218532179988851e-9] km/s
+ V∞_out: [7.303191726653154e-10, -2.366769531355762e-9, 3.914066537025092e-10] km/s
+ time of flight: 1.874957778749338e8 seconds
+ arrival date: 2030-04-24T02:14:04.263
+ thrust profile: [0.27152335310791564 -0.0057181848443261405 -0.08096878377138776; 0.0864141126576709 0.04596170032108732 -0.09816886589102963; 0.045077067058060694 0.03793673041977936 -0.09780440001658434; 0.029000218040614967 0.031195506258401482 -0.09537040672325725; 0.017314384353803215 0.021790685635867255 -0.07781543144226698; 0.013394214717465797 0.019129193685174253 -0.07530241727582622; 0.008447391554578717 0.013117995804726161 -0.05748623958353035; 0.01789098469867881 0.026007591828277134 -0.13194628469835523; 0.005458393405293228 0.00958853678365839 -0.046933810768118846; 0.0027121445525878497 0.005497930176329462 -0.029174882553214262; 0.00017823390560254177 0.0006722776856617919 -0.0014127864871761125; 2.999905939621865e-5 0.00039143530029426535 -0.001227159340277639; -5.353173033206383e-5 -0.0004353704655359266 -0.0009477752619451009; -0.0006869968002160083 -0.0008824979496941958 0.00021766072390125616; -0.00024484966323481326 -0.00041375277047126186 -9.758657627099315e-5; -9.921267184215019e-5 -0.0013225429324853115 0.001179083417700687; 0.004676562272537278 0.004858178924411581 -0.003375522790441744; 0.0021178473216028186 -0.00043743993800304917 -0.0001866090732272434; -0.002421404001784362 0.0019207910154760335 -0.008295199888053054; -0.0017786297547929609 0.00032635770978645855 -0.0007303169990939978] %
+
+Mass Used: 82.3654253558484 kg
+Launch C3: 97.3508648715413 km²/s²
+||V∞_in||: 2.466196774884358e-9 km/s
diff --git a/archive/ES_0.5573582314784152 b/archive/ES_0.5573582314784152
new file mode 100644
index 0000000..b101759
--- /dev/null
+++ b/archive/ES_0.5573582314784152
@@ -0,0 +1,22 @@
+archive/ES_0.5573582314784152---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:06:56.511
+Launch V∞: [8.047913388637948, -5.649540251258871, 0.16746191985934528] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.120921028703875e-7, -7.448714584366031e-6, 1.3307527431501173e-6] km/s
+ V∞_out: [-1.181192309855768e-6, 4.383804501753365e-6, 6.107979109499203e-6] km/s
+ time of flight: 1.8749577787493584e8 seconds
+ arrival date: 2030-04-23T14:16:33.511
+ thrust profile: [0.3212323180965184 -0.0072494604662601495 -0.10667691405523096; 0.08936944777692282 0.04799474938124221 -0.10667649340323808; 0.04169948331916683 0.03652185269887154 -0.09184705512522744; 0.03067270047133568 0.035988031086508734 -0.10617058270132451; 0.021632857331026562 0.02921284377528113 -0.0940529329629678; 0.017924941651634427 0.02780222611660501 -0.10067603775304786; 0.013373568993756938 0.024836335957386924 -0.09587211490535821; 0.003983371326425269 0.008474480710221303 -0.03425989450895714; 0.003086517405664589 0.00707520541202714 -0.03171509525655946; 0.002420610808737147 0.004303701940928045 -0.02264655781163144; 0.0004919214204796523 0.001083223383296344 -0.0078138477864468; 0.0014021935537828231 0.0015922091035263143 -0.0033917473044053044; -0.0018805473773238315 -0.000958675756830112 -0.0008657087761377453; 0.0005323440194236278 -0.0030339582985456906 0.00017502315506135076; -0.0016239442861260642 0.005125132829713471 -0.0015477600159380736; 0.0005721116679907841 -0.0008036246142245607 -0.004401338348149955; -0.001523037921603625 -0.0021817435140161386 0.0013010471986086704; 5.6874767379083994e-5 -0.004354458699101221 -0.004273820011076563; -0.005129787459767908 0.0031552682462866444 -0.0025309250216649357; -0.00037057206470209004 -0.0007003742367315295 -0.0026007934831861748] %
+
+Mass Used: 86.08476239689662 kg
+Launch C3: 96.71425845621506 km²/s²
+||V∞_in||: 7.610108107398555e-6 km/s
diff --git a/archive/ES_0.5573586636641803 b/archive/ES_0.5573586636641803
new file mode 100644
index 0000000..6e1d94d
--- /dev/null
+++ b/archive/ES_0.5573586636641803
@@ -0,0 +1,22 @@
+archive/ES_0.5573586636641803---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T09:06:31.483
+Launch V∞: [8.074991359011044, -5.712468233345821, 0.17239530892323615] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.184612885017217e-9, 4.4994937922684836e-10, -9.711529633184179e-10] km/s
+ V∞_out: [3.213259495082611e-9, -2.955787055674678e-9, 1.0961086481511596e-9] km/s
+ time of flight: 1.8749577787457383e8 seconds
+ arrival date: 2030-04-24T11:16:08.483
+ thrust profile: [0.24404065829033275 0.0015509246105233105 -0.0842305111427979; 0.05503729777840466 0.030571054045058173 -0.06821256356892073; 0.05204187771448269 0.04616547926498562 -0.11616003850006276; 0.031991950016373 0.036984487030036435 -0.10524377100524007; 0.01817683243595681 0.02439464055922544 -0.08033872488789384; 0.011603169656431161 0.018279163924982855 -0.0664332840257242; 0.018355326080819415 0.03469516087914514 -0.12933817651333415; 0.007907729151849997 0.013683658460379469 -0.057576367839920484; 0.002666524449815966 0.006600832142274364 -0.029408652818676526; 0.002179250402912547 0.0075792825655283174 -0.035689189535531504; 0.0010118671479530258 0.0022468729713950985 -0.009178811524843795; 0.0008327310671315232 0.0011457556397033134 -0.0009043383754630413; -0.0006743051405527005 -0.0011350326431244263 -0.0013777993361011286; -0.0016509178476234927 -0.00043540402127338097 -0.00020703376264248933; 0.00255570686517273 0.0030234910525801244 -0.0006725341499517482; 0.0020105699035889053 0.002318115487689832 -0.006452401686513553; 0.0004955383478298025 0.0005730028002809886 0.0009678660723550474; 0.0008626845979977135 0.00036370068602293367 -0.006261327684067263; 0.00013838846268043485 0.0026254043801629077 0.0033067545837731937; 2.7043420666999436e-5 0.0005250773642585712 -0.005253071515506396] %
+
+Mass Used: 79.35803064705351 kg
+Launch C3: 97.86749890762688 km²/s²
+||V∞_in||: 1.5965275473281333e-9 km/s
diff --git a/archive/ES_0.5573631677640458 b/archive/ES_0.5573631677640458
new file mode 100644
index 0000000..bbdf036
--- /dev/null
+++ b/archive/ES_0.5573631677640458
@@ -0,0 +1,22 @@
+archive/ES_0.5573631677640458---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:40:20.156
+Launch V∞: [8.03472769538251, -5.522344109439439, 0.2303118295976067] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0649353502713266, -0.3801225231359816, -0.5545717877369495] km/s
+ V∞_out: [0.2814129342014199, -0.23420402352290987, 0.5676311895988809] km/s
+ time of flight: 1.8749577787488317e8 seconds
+ arrival date: 2030-04-21T02:49:57.156
+ thrust profile: [0.45489921126807564 0.003880569656687806 -0.12461059661717264; 0.08659067837325024 0.053722729318609816 -0.09040726034718415; 0.05098276953389686 0.052011298603366396 -0.09914427844450027; 0.023921555419256738 0.03349981667254638 -0.07329508612824281; 0.031644072046400296 0.05083101381760448 -0.12086286117769422; 0.020281056241580466 0.04067820586519013 -0.10276290385522119; 0.0075617384931585575 0.01819670039077959 -0.05314779604027482; 0.01126838100810582 0.03190610046818935 -0.09090505025937792; 0.004603616501847163 0.012000210692033003 -0.03717773320632567; 0.00038482948963453165 0.0013900696455438307 -0.0044827937059844615; 0.0008556295637904906 0.0035831727915657165 -0.011745941536250925; 8.83865197195051e-5 -0.0002787587864712974 -0.0002109387173157221; -0.0001676781740403009 -0.00015038293656219142 0.0002184212986254913; -0.00038798961033834284 -3.3748036227425956e-6 7.088805468646875e-5; 0.00012899116437049292 -0.0011521829377384631 0.0002539674562160261; 6.755608328464687e-5 -4.764477556490023e-5 0.0003313806120287555; 8.546915157415427e-5 0.0006540586012180423 0.00042561911182785884; 0.0004041746465336865 0.00045394694566787777 -0.00045674500512560734; 0.0006555094083924879 0.0005204604937859088 -0.0011272140552477804; -0.0004365931721279457 -0.00019820474014791561 0.000813202725855779] %
+
+Mass Used: 95.47099573637115 kg
+Launch C3: 95.10617714085983 km²/s²
+||V∞_in||: 0.6754699105540386 km/s
diff --git a/archive/ES_0.5573745230158477 b/archive/ES_0.5573745230158477
new file mode 100644
index 0000000..55b8c8c
--- /dev/null
+++ b/archive/ES_0.5573745230158477
@@ -0,0 +1,22 @@
+archive/ES_0.5573745230158477---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:25:19.734
+Launch V∞: [7.942100059342443, -5.748518709245292, 0.1214161875367799] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.60249024931391e-10, -1.0738487616580705e-9, -1.4426767823410483e-9] km/s
+ V∞_out: [1.6228261190537314e-9, -1.6284025465157315e-9, 6.633567830774283e-10] km/s
+ time of flight: 1.8577881179756567e8 seconds
+ arrival date: 2030-04-03T13:38:50.734
+ thrust profile: [0.3966633508852314 -0.0033627946187786834 -0.12401005698479305; 0.040992344077848415 0.022702554664168217 -0.04942891065797816; 0.03870755668764156 0.03465361226163772 -0.08306208226937029; 0.04196660695347464 0.04908563177944588 -0.1286185156459175; 0.021606387158944574 0.030539007050907674 -0.09151994760531584; 0.018430646828469854 0.030747146794112654 -0.09975260420829567; 0.01049007597228085 0.01946442663517981 -0.0701301549128422; 0.010118305804265069 0.02174310859995734 -0.08108151428265578; 0.004131069493431569 0.010041083194299244 -0.04003249081092107; 0.002802077541437506 0.003680738032509656 -0.02014323730941775; 0.0014999645410891797 0.006278819308382815 -0.02646745906836337; 0.000596221499098926 0.00411873330937695 -0.012951108176382474; 0.00023801585909824887 4.709532743205915e-5 -0.0016225288156470465; -0.0009290567655441341 0.0013360560877455146 -0.0029626565743699805; -0.002409472266795137 -0.0004502316421582499 -0.00021336342833370558; 0.00017057236575619098 0.001052957038915934 0.0009690989016806206; 0.0012721594929728697 -0.0007524348206267033 0.0027400268468747904; 0.001002645300721693 -0.001351796726885205 -0.0008641652337101747; 0.00016877643128609504 0.0002675409911455319 0.00013232262976437892; 0.00037597483410814296 -0.002426927792310208 0.002667833880474209] %
+
+Mass Used: 89.47016172163512 kg
+Launch C3: 96.13716259374637 km²/s²
+||V∞_in||: 1.915827820067175e-9 km/s
diff --git a/archive/ES_0.5573785037663962 b/archive/ES_0.5573785037663962
new file mode 100644
index 0000000..c3f805a
--- /dev/null
+++ b/archive/ES_0.5573785037663962
@@ -0,0 +1,22 @@
+archive/ES_0.5573785037663962---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:00:29.115
+Launch V∞: [8.085565848943663, -5.7076009641897505, 0.07893279768340732] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1141430234870854e-6, 3.833986490151016e-6, 1.0609421761772093e-5] km/s
+ V∞_out: [1.0281317001850898e-5, 1.121566932545931e-6, -4.622231434309705e-6] km/s
+ time of flight: 1.8749577787740067e8 seconds
+ arrival date: 2030-04-24T02:10:06.115
+ thrust profile: [0.21438714712152301 0.00031709709424999866 -0.0723713904902614; 0.0552200644448925 0.03255775794613997 -0.06427169063910353; 0.06514007337146924 0.0612129986581647 -0.13759671665969242; 0.03391354172896684 0.04248958466893847 -0.10499020508740908; 0.018896666378866975 0.029162290641649945 -0.08097281219880492; 0.015046866155353202 0.027635058841355583 -0.08315019667197066; 0.017029156244506103 0.03563442651692062 -0.11515956969114491; 0.004208469774424312 0.009624418628191557 -0.03402873582589866; 0.006801889778331985 0.01884482899112866 -0.06786194388280056; 0.0002993095875480576 0.001049889191265176 -0.003842238349395413; 0.0006688932030931931 0.002247609770195572 -0.00905038341163239; 0.0029024978133636364 0.0019447220399786786 -0.0015813896738054358; 0.0004971430261757405 -0.0023481615620461367 -0.002278351977297903; 0.0007581785121749542 0.0001417420094729639 -0.004612434440142968; 0.0006049468359909096 0.002126401853859398 -0.004640068380585527; -0.0010181518703238 0.0025784643626005324 -0.004925627520964162; 0.0026768838085111392 -0.0036883144178852124 0.003652555686922049; 0.001714450615395987 -0.001262418222208216 0.0037837702115381933; 0.00012030709882311467 0.0004893890835546194 -0.001426649472825507; -0.0009042523132027955 -0.0032267299589047744 0.0020510635593456008] %
+
+Mass Used: 78.84558793244742 kg
+Launch C3: 97.95931425057395 km²/s²
+||V∞_in||: 1.1335810390201871e-5 km/s
diff --git a/archive/ES_0.5573861613713115 b/archive/ES_0.5573861613713115
new file mode 100644
index 0000000..c02b58c
--- /dev/null
+++ b/archive/ES_0.5573861613713115
@@ -0,0 +1,22 @@
+archive/ES_0.5573861613713115---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:09:27.217
+Launch V∞: [7.990439449375878, -5.631128367316944, 0.33452046736576513] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.835841244287999e-8, 1.921285522125527e-7, 5.522062861279533e-7] km/s
+ V∞_out: [5.36823620554902e-7, 5.9183001622671725e-8, -2.396706117857578e-7] km/s
+ time of flight: 1.8749577785262096e8 seconds
+ arrival date: 2030-04-22T18:19:04.217
+ thrust profile: [0.41962657837865175 0.004957874344005614 -0.12408267884632032; 0.06339675560039781 0.0377708316657577 -0.0708337620321845; 0.04463890000159618 0.04232736751210791 -0.09014147107714075; 0.03404252929695308 0.0433109146093695 -0.10319119108704118; 0.03262740241653209 0.051747851704205816 -0.13336729273580353; 0.015486419619908627 0.02874426305879758 -0.08293681229894934; 0.011438932880453547 0.02429954704902311 -0.07671395212004051; 0.005150131573635217 0.012240824136400598 -0.042259461235142015; 0.0017071037999008198 0.004806190803321597 -0.01821279353862312; 0.003588163502662751 0.010628343225437957 -0.03997995109715732; 0.0004532607287496022 0.0021373831814795094 -0.007724079538240866; 0.0007148467245268371 0.003158890888913791 -0.012739894560959445; 0.0009681399393420693 -0.0014919160403968424 -0.0028240029854018525; -0.0007455095958666875 0.0007823563334681315 0.0007096636903005942; -0.0017054684339168412 0.000996293126504116 -0.0014816836542449214; -0.001803729357291017 0.0007642174018046902 0.0008884575494427019; 0.001809587375372816 0.002172777746624493 -0.004389739866608095; -0.001223841805919185 -0.0006602417049113683 0.006423321718950562; 0.0010054860865659856 -0.002780629546155159 -0.002522631351419934; 0.0010067400780210554 -0.0005028728109191484 0.00036381200008486856] %
+
+Mass Used: 92.21682777901879 kg
+Launch C3: 95.6686332264305 km²/s²
+||V∞_in||: 5.87580519858659e-7 km/s
diff --git a/archive/ES_0.5573863264083831 b/archive/ES_0.5573863264083831
new file mode 100644
index 0000000..2f615c1
--- /dev/null
+++ b/archive/ES_0.5573863264083831
@@ -0,0 +1,22 @@
+archive/ES_0.5573863264083831---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:42:40.294
+Launch V∞: [7.983593357394356, -5.751973702456421, 0.1712973038003311] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5560905107213794e-9, -2.933997128614424e-9, -9.317462798689731e-10] km/s
+ V∞_out: [-6.898776487013707e-10, -1.2048382276985037e-9, -3.435406878863557e-11] km/s
+ time of flight: 1.85733189324808e8 seconds
+ arrival date: 2030-04-03T17:15:49.294
+ thrust profile: [0.3436619170559288 -0.019096945753885576 -0.11993301641458327; 0.059504007169738055 0.029290228725497754 -0.07618727200866188; 0.038595440810850944 0.02981699712684163 -0.08861585632980341; 0.025420223259401617 0.02569997623352423 -0.08677776535600233; 0.027525558550418383 0.032054889782807905 -0.12047234240836181; 0.012560591817267373 0.014290874356595339 -0.0687709380583662; 0.012913340795269916 0.018483763280778862 -0.08220033282917963; 0.01188455824278952 0.01859226762998591 -0.0901428201102403; 0.0026121750615917564 0.007560420228671122 -0.04146178411300545; 0.003547003745003288 0.0048018996604501825 -0.03346993010280191; 0.00023638918327551734 0.0007522771480399842 -0.0014397631140312772; 0.00012405852749202984 0.002747070045461619 -0.013493963221612778; -1.7816929342164673e-5 1.0679227802846449e-5 -0.003571133428198847; 0.0007275066225652344 0.0010089952617440552 -0.003722804516497812; 7.86049884585854e-5 -0.0006548970556231658 -0.0009517141484804859; 0.0018805278724724982 0.0014800895573127601 -0.0001454557340161539; 0.0008811317061839306 0.0021091616363975198 -0.0059893267160723304; -0.0002729906911518674 -0.000706957682035249 -0.0015978951485846739; -0.0009828517414757975 -3.083559923816527e-5 -0.00012679547401045846; -0.0003491341141395922 0.00336631608148269 0.0020519545383373325] %
+
+Mass Used: 85.31225584820095 kg
+Launch C3: 96.85230713627077 km²/s²
+||V∞_in||: 3.4493344225117517e-9 km/s
diff --git a/archive/ES_0.5573877470077688 b/archive/ES_0.5573877470077688
new file mode 100644
index 0000000..5adede0
--- /dev/null
+++ b/archive/ES_0.5573877470077688
@@ -0,0 +1,22 @@
+archive/ES_0.5573877470077688---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T09:33:42.256
+Launch V∞: [8.02822921938364, -5.716136537224677, 0.22436219173816338] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5355648218274111e-6, 4.879872424747991e-6, 1.360768816204508e-5] km/s
+ V∞_out: [1.2934329941714541e-5, 1.628209282897189e-6, -6.421942187373411e-6] km/s
+ time of flight: 1.874957778747624e8 seconds
+ arrival date: 2030-04-23T11:43:19.256
+ thrust profile: [0.24622120228135305 0.0015203716090014534 -0.06804159922698082; 0.08899263082750956 0.055216829508625644 -0.09251525987543041; 0.07340463889998304 0.07205508315692809 -0.13310053170981667; 0.02466024050575881 0.033188316326013045 -0.07358232220951529; 0.016449738547376098 0.02740772067367028 -0.06763032716458922; 0.02959851183033262 0.055779378295816556 -0.1409011853298329; 0.009765371543069591 0.023693120350926297 -0.06760946084980786; 0.005593144692131894 0.015190953072272627 -0.04685079626844237; 0.0044853245132549955 0.01375553018063799 -0.04492338569015611; 0.0018633013464501012 0.007756710288231004 -0.025577572985872838; 0.0018250290830191575 0.00628661447975532 -0.02224532223275538; -8.919585251498808e-5 3.480882972126509e-5 -6.341945399782983e-5; 0.0009673046973403341 0.0010586849061016506 -0.001297350967985637; -0.0010903837155629265 0.0012786461223646115 0.0007054292867208986; 0.0019493458905277547 -0.00013360125742354213 0.0017349547503192433; 0.00024429435087922014 0.00022261551491110454 -0.0013855311219762181; -0.0005667861743071602 0.00041131054337686994 8.767132132861627e-5; -0.0015617761442166716 -0.0012359222731767809 -0.001259689643690192; -0.0017861469614992435 0.0025450951889432498 0.001509896400393751; -0.005681106408300905 0.0017258361947096975 -0.0034068088183153997] %
+
+Mass Used: 83.41975656765362 kg
+Launch C3: 97.17701970424172 km²/s²
+||V∞_in||: 1.4537547637731458e-5 km/s
diff --git a/archive/ES_0.5573893216226291 b/archive/ES_0.5573893216226291
new file mode 100644
index 0000000..ca95938
--- /dev/null
+++ b/archive/ES_0.5573893216226291
@@ -0,0 +1,22 @@
+archive/ES_0.5573893216226291---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T00:49:14.153
+Launch V∞: [7.958252309507001, -5.79278393479884, 0.07844031406786243] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.660246330778586e-7, -1.3317825681393625e-6, -4.9977919402311933e-8] km/s
+ V∞_out: [1.077398263014196e-7, -5.495961801455016e-7, -1.4872424637045649e-6] km/s
+ time of flight: 1.8749577787497368e8 seconds
+ arrival date: 2030-04-25T02:58:51.153
+ thrust profile: [0.3251334452987356 -0.00472232265447792 -0.11237076501965651; 0.0651605744309389 0.03413692573042094 -0.07826313413085323; 0.04785186072928293 0.03965900453000189 -0.10319233852616823; 0.04259119302015288 0.0454019251690112 -0.1344107711016766; 0.025830458754552327 0.03268878814821136 -0.10946448482738591; 0.015533931006251634 0.022369583311016634 -0.08317788301314118; 0.010074164649611243 0.01631893317477722 -0.06735991873826475; 0.005068948915049289 0.006773312693071503 -0.03643944124254347; 0.004272135054195199 0.008293968291825087 -0.03914270096374533; 0.004092832160841754 0.004037920720168872 -0.026616783019443778; -0.0004531619181788291 0.0011859789003712021 -0.006827840577669896; 0.0009134817071629604 -0.0009242091837818175 -0.0036299269544099234; 0.0018784554845365873 -0.0007886442127665318 -0.0023104868051114567; -0.0016792746938789197 0.0005951698671087483 -0.001018908624433964; -0.0002651732409224367 0.00043753300024474686 -0.004353710856738641; 0.00038129503405163155 -0.0005764313792704194 -0.0029293137547590576; 0.00280221723069996 0.002015993832510956 0.0006315937003234413; 1.5536572279501533e-5 0.0003648323426125562 -0.001460929470519448; 0.0005917069903488746 0.0011246836664928269 -0.000352710500654821; -0.007478811598864611 -0.0028015414221154804 -0.006092246439619804] %
+
+Mass Used: 85.05925111027 kg
+Launch C3: 96.89627841990811 km²/s²
+||V∞_in||: 1.5893839266600438e-6 km/s
diff --git a/archive/ES_0.5573913212753266 b/archive/ES_0.5573913212753266
new file mode 100644
index 0000000..cbe1314
--- /dev/null
+++ b/archive/ES_0.5573913212753266
@@ -0,0 +1,22 @@
+archive/ES_0.5573913212753266---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T11:05:27.894
+Launch V∞: [7.921878726171464, -5.696270027060228, -0.033473178800995027] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0752895522633617e-6, -6.829803951115467e-6, 0.00016119794173755718] km/s
+ V∞_out: [-3.620888185814303e-6, 8.754984204205643e-5, -6.816975052184099e-7] km/s
+ time of flight: 1.8749577788045898e8 seconds
+ arrival date: 2030-04-22T13:15:04.894
+ thrust profile: [0.392871992049629 0.009578637948972325 -0.11528789992196498; 0.10576392008869175 0.06781365760451985 -0.10975455240769705; 0.06161851265072739 0.0643623369897415 -0.11675806126807528; 0.03947325965697067 0.05568676528172786 -0.11370428980818899; 0.02436336255557945 0.04316694677699028 -0.09769813252140329; 0.014410608421805674 0.03114654938782882 -0.07697227612870064; 0.016194283172043394 0.04217675445857443 -0.10897863826675777; 0.004630693968091322 0.013818192778673475 -0.039893500764913555; 0.001959663722614904 0.004008865287732902 -0.020723132331395163; 0.0012053118179076218 0.003375742224853195 -0.013642523042985555; -0.0010847613328031072 0.0011496682284272417 -0.000568857388936671; 0.00019242386512327412 -0.00032192074494314304 -0.001022450555705712; -0.0007833607058187141 0.0012255127641409439 -0.0028685328044718763; -0.000273503045421427 0.005034826583305292 -5.3482229848852124e-5; 0.000251301883375428 0.0005763180399989203 -7.479547982629144e-5; 0.003906560693559926 -0.0011224810926823436 -0.0042520192980113536; 1.8199625066758464e-6 -0.0012723306999543923 0.0014862793027370141; -1.1652658662254962e-5 0.00016678059635409973 -0.0010522424655985995; -0.002425414763509712 0.003168636753804044 -0.001805947154370341; -0.00011114261930677906 0.0010289513295857352 0.00038702282515874114] %
+
+Mass Used: 94.92868599674557 kg
+Launch C3: 95.2047752270518 km²/s²
+||V∞_in||: 0.00016134614618904525 km/s
diff --git a/archive/ES_0.5573928853901288 b/archive/ES_0.5573928853901288
new file mode 100644
index 0000000..f628b2c
--- /dev/null
+++ b/archive/ES_0.5573928853901288
@@ -0,0 +1,22 @@
+archive/ES_0.5573928853901288---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:10:45.757
+Launch V∞: [7.916663834500388, -5.692261170803031, -0.008454589847078102] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4464948591226382e-9, -8.555838687275216e-10, -1.1377551838335707e-9] km/s
+ V∞_out: [8.694111509294776e-10, -8.095070391074417e-10, -7.033381155709282e-10] km/s
+ time of flight: 1.8749577787514612e8 seconds
+ arrival date: 2030-04-23T09:20:22.757
+ thrust profile: [0.4627575570619775 -0.005322371727279243 -0.14169122944836363; 0.05475102443069114 0.031990615196742234 -0.06445856322571704; 0.06690144002988195 0.06248215809035307 -0.13744755155439076; 0.03368676665443308 0.042157251854896875 -0.10596306789039409; 0.019294591417630194 0.02967508981223923 -0.08463213086284573; 0.010847185453557482 0.019375741277223153 -0.06186960642668976; 0.012002006611219614 0.025210497525651382 -0.08395688254714019; 0.005440571187114904 0.012673495891493497 -0.04699410797898651; 0.0029509761617889972 0.008915180875483819 -0.03222422563143714; 0.0007575653724426839 0.005074531169557027 -0.023137361088215274; 0.0032042623763781737 0.010260635401116599 -0.043558137118983924; -0.0005820122528529441 0.004048125672615707 -0.012541687316832702; 0.00018006227198855357 0.00044330795600234184 -0.00014609290121583239; -0.0010072802879380024 0.0011614728418460785 -0.0001709258961023175; 0.00013009849838924295 0.0006289164176586785 0.0011531036363827652; -0.0007366934328096966 9.901994816415168e-5 -0.00016125203042834145; -0.0012357990832264833 -0.0013241694797086537 0.0010754982238395212; 0.00019502747304682227 0.0008906193582366392 -0.0006676092207497329; -1.5604767468477233e-5 -0.0004083617899833269 0.0005482945575954135; -0.0034820094423408275 0.0030401644846332248 -0.0015076700082341488] %
+
+Mass Used: 95.68476220810498 kg
+Launch C3: 95.07547498520776 km²/s²
+||V∞_in||: 2.0294969801000287e-9 km/s
diff --git a/archive/ES_0.5574018967922434 b/archive/ES_0.5574018967922434
new file mode 100644
index 0000000..52b9dd3
--- /dev/null
+++ b/archive/ES_0.5574018967922434
@@ -0,0 +1,22 @@
+archive/ES_0.5574018967922434---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T09:08:11.509
+Launch V∞: [8.200564493133724, -5.590347840826253, 0.19398396938589205] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.495453274685581e-7, -9.807102536171478e-7, 2.4694608760167022e-5] km/s
+ V∞_out: [1.6065080459827302e-6, -2.953964005688682e-5, 2.8968406525720046e-7] km/s
+ time of flight: 1.874957778741785e8 seconds
+ arrival date: 2030-04-23T11:17:48.509
+ thrust profile: [0.20044051494695914 -0.0015342431091091924 -0.06820449703234614; 0.03281244517299592 0.01736532082786283 -0.03692415774343799; 0.03699490331768085 0.03128803394459263 -0.07704194256223074; 0.05335279994918585 0.060024648691782825 -0.16721542099627415; 0.021966118941447184 0.028795947173878414 -0.09015753277538452; 0.02890717799240204 0.04495296539837355 -0.15352471817948854; 0.010438288478474472 0.017337126033466186 -0.0643676579318086; 0.005067887974178122 0.009185124896844612 -0.0345284381592385; 0.002474953187706713 0.004670838805232224 -0.018680225535004463; -0.0012422399581130405 -0.0007027174515217001 -0.011119621645593122; 0.0018622726958299886 0.0034076371454316756 -0.012704526103919324; 0.00032909825136627317 0.00015048843345359469 -0.008780694361758925; 0.0016756170287926756 0.003215272101205673 -0.003056110827089968; -0.000279337904175806 0.003110654260167855 -0.008963220859310173; 5.297389855785269e-6 0.0016409223600959647 -0.005970790346646951; -0.006094573597273085 -0.009463446841130221 -0.013665491880028361; 0.003328248599752266 0.004323830825799405 -0.005473680026633261; 0.00026309163772384445 0.0006816784565889869 -0.0038812813776627937; 0.0007464408615274493 0.0015730940903991584 -0.00018391721115144596; -7.496487293285643e-5 -0.0029785522793336922 0.0004557375052205379] %
+
+Mass Used: 75.49209844512961 kg
+Launch C3: 98.53887676785503 km²/s²
+||V∞_in||: 2.471452727090355e-5 km/s
diff --git a/archive/ES_0.5574357436218887 b/archive/ES_0.5574357436218887
new file mode 100644
index 0000000..57b2fa6
--- /dev/null
+++ b/archive/ES_0.5574357436218887
@@ -0,0 +1,22 @@
+archive/ES_0.5574357436218887---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:56:44.797
+Launch V∞: [7.934576841555602, -5.661292984588326, 0.17043131881411766] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.642738255347654e-7, 2.122346131488568e-6, -4.1349972514288953e-7] km/s
+ V∞_out: [-4.367111558639829e-7, -1.2093353495153922e-6, -1.639965047111462e-6] km/s
+ time of flight: 1.87495777874696e8 seconds
+ arrival date: 2030-04-22T18:06:21.797
+ thrust profile: [0.4235481827646662 0.002529270805717998 -0.13420337303446803; 0.11452163288474367 0.0679072727579045 -0.13042366827996915; 0.061228614433736374 0.05866994990317605 -0.12803674595278197; 0.0373934895891522 0.04765296718126946 -0.11851766763972699; 0.020787425396570167 0.032608046151408464 -0.09140561329318805; 0.011101713302755974 0.020579882767784958 -0.0637920777506941; 0.0062813347279789735 0.013601714175702577 -0.04699958191780127; 0.0066195423732951595 0.014563982017288835 -0.05262922268440298; 0.0018219386860132438 0.005709975244628835 -0.019475713424264452; 0.0031206580184576387 0.0068606004757505385 -0.030420112135461124; 0.0014298838683240592 0.0035979643780272618 -0.015661077601632913; 0.0001593932930028432 0.0009808205647386708 -0.005696995383705283; 0.0002782200752857181 0.001602457167041773 0.0008900360670716866; -0.00023454451297358228 0.0004333698161072958 0.0004612871891041953; 0.0016484215126158046 0.00032380066682893203 0.002830324672383043; 0.004270304801579538 -0.0009348856118334768 -0.003526724810016424; 0.00025830528983822863 0.002403780489750557 -0.0009350966503139236; -0.0002936747510533415 0.0005022619953660701 0.0017360448285657346; 0.0016313596418751305 -0.002073173948942964 -0.0017028539230387872; 0.0007405853600078236 -0.003621344588268359 0.0008582502797419803] %
+
+Mass Used: 95.96039820526585 kg
+Launch C3: 95.03679474633218 km²/s²
+||V∞_in||: 2.1927221767719386e-6 km/s
diff --git a/archive/ES_0.5574362499758184 b/archive/ES_0.5574362499758184
new file mode 100644
index 0000000..ddb6579
--- /dev/null
+++ b/archive/ES_0.5574362499758184
@@ -0,0 +1,22 @@
+archive/ES_0.5574362499758184---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T10:45:31.943
+Launch V∞: [7.8868207644782595, -5.7213444482342, 0.23590713708362204] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.266911206238578e-7, -2.358486607562404e-6, -2.3320025531106938e-6] km/s
+ V∞_out: [-3.0989660778740537e-6, -3.6324379949981935e-7, 1.3923473798993421e-6] km/s
+ time of flight: 1.8749577787493747e8 seconds
+ arrival date: 2030-04-23T12:55:08.943
+ thrust profile: [0.48468933106330747 0.007742514493246365 -0.13782863421406263; 0.05510775363127657 0.03401523473432659 -0.06463296652283175; 0.04309921779902233 0.043138898733624455 -0.08791045661460502; 0.034311764612534844 0.04735006842785159 -0.10512237617753896; 0.017343187491943565 0.028575667888896074 -0.07666478245220507; 0.009600373151669906 0.018832106035208372 -0.055714532985177076; 0.010312046831219616 0.02508531580391528 -0.07768373152935328; 0.01169615743418581 0.02937554724546662 -0.0948016706452497; 0.00810850116767038 0.01937730779521261 -0.06395097678531923; 0.0036129443826953527 0.01392983306425655 -0.04761962892895029; 0.0011284882229065651 0.0023203498235043456 -0.010728250964586303; -0.0005039097301894929 0.0010586599284680654 0.0014072269195425735; -6.907377398842205e-5 -0.0007415242675210426 0.0005964642511540101; 0.0004747117558438452 0.00010100468577477293 -9.972245571393968e-6; 0.0011785903836821583 0.0009452701424785299 0.0010141730467557544; -6.167872153365467e-5 -0.0002605574381603094 0.0005978494168937477; -6.080412171441922e-5 0.0008844483969313539 0.00038243284070817705; 0.0004735117796233411 -0.00041459442729763045 -0.001042692775316304; -0.0002366983115904456 -0.0007022325643379361 -0.0007335649134978281; 9.09437203493232e-5 0.0017067120751674916 0.0031946307927459856] %
+
+Mass Used: 96.22593021703051 kg
+Launch C3: 94.99137624367273 km²/s²
+||V∞_in||: 3.4182032114378953e-6 km/s
diff --git a/archive/ES_0.5574414280471919 b/archive/ES_0.5574414280471919
new file mode 100644
index 0000000..54bdae0
--- /dev/null
+++ b/archive/ES_0.5574414280471919
@@ -0,0 +1,22 @@
+archive/ES_0.5574414280471919---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T22:18:02.664
+Launch V∞: [7.9153823526007665, -5.581065826468864, 0.11075541959956169] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.719133844802239e-5, -8.077188072787998e-5, 6.186900186065844e-5] km/s
+ V∞_out: [-2.047959902077251e-5, -0.000138890284684023, 6.338728146628654e-6] km/s
+ time of flight: 1.8749577787483945e8 seconds
+ arrival date: 2030-04-21T00:27:39.664
+ thrust profile: [0.5119538885294441 -0.00775369243288808 -0.12184563119007161; 0.12590007409240936 0.07881471560450493 -0.11976397328705317; 0.05580491960761319 0.05917757084996046 -0.10336025801330058; 0.032455894662742894 0.04325969171026215 -0.09016139765211781; 0.020580178485726644 0.03789718937544481 -0.07998094725715926; 0.031080426980840157 0.05964970106489196 -0.13510088747422686; 0.011429193476003362 0.03044339657077751 -0.07655833094473916; 0.005219714182046984 0.01822278691296763 -0.048741953622564546; 0.002904284648532839 0.009933095868519388 -0.029051385149194867; 0.0003018961402368658 0.0011114789391046538 -0.0037493062278164137; 0.00039892305199948027 0.0014269246239157055 -0.005316669906663123; 0.00012936100119449406 0.0007917422526813741 -0.0026587197760412637; 6.409805591046477e-5 0.00046614378869159296 -0.0009469591331124262; 0.00016492025376297498 -0.00023996490621965537 -0.0009521222007600612; -0.0008571783215247477 0.0011397219184365519 -0.0007546815617496619; 0.0002994637235668626 -0.00028651895204434536 0.0003338333499670026; -0.0002687054611289982 -0.00040992924587943716 0.00036800840606697634; -5.836177655776619e-5 -0.0008427619918951989 -0.0009196234392811251; 4.8797458917159645e-5 -0.00011111257331896282 0.00023551117644227799; -0.00012310494646587387 -0.00027265694805405066 0.0004407733549746742] %
+
+Mass Used: 103.10093091214867 kg
+Launch C3: 93.8138403102129 km²/s²
+||V∞_in||: 0.00014070545965551962 km/s
diff --git a/archive/ES_0.5574441035973889 b/archive/ES_0.5574441035973889
new file mode 100644
index 0000000..bce1148
--- /dev/null
+++ b/archive/ES_0.5574441035973889
@@ -0,0 +1,22 @@
+archive/ES_0.5574441035973889---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:11:33.141
+Launch V∞: [8.072759733085308, -5.661306813337714, 0.0674758852488196] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.394239357723936e-6, -5.078851157054381e-6, -4.7147681275824824e-7] km/s
+ V∞_out: [2.670428944155373e-7, -8.682370438158007e-7, -4.832127204936933e-6] km/s
+ time of flight: 1.8749577787396708e8 seconds
+ arrival date: 2030-04-23T19:21:10.141
+ thrust profile: [0.30851648460337505 -0.0003417681293612645 -0.09838150326774224; 0.03831450058931848 0.021789626427599157 -0.04617130304754803; 0.04141774795230572 0.0376781219418172 -0.08873303847522683; 0.025946123200251896 0.030864192093035103 -0.08365941517091001; 0.022876188935310068 0.033898243728019854 -0.10040579487650682; 0.024074084026423925 0.04139439618536503 -0.13146679588492124; 0.014831311683984154 0.02928819151136837 -0.10256189431386888; 0.011478906624156442 0.025084015950614394 -0.09276964990383268; 0.0037507224358528006 0.009024474353066369 -0.036624063395104225; -6.904798429105066e-5 0.0017270814976504945 -0.006146955252905873; -0.0004953311258692524 -0.0009443177836428812 -0.0009675639740432318; -0.001311960060346229 -0.0010173177008076153 -0.00032504233295943606; -0.0013790369781026385 -0.0005345846419139556 0.0006210681618095538; -0.0019170926107696111 -0.0006203377467131053 0.0013006266891836475; -0.0002926645438128306 -0.0006414056097202813 -0.00035044607944706614; -0.001110018826875531 0.0023571641064164027 0.0007675294987790435; -0.00036095681308187457 -0.0025353420728161354 0.003740838444615441; -0.00023856851897744816 -0.0017485756825395074 0.00250282463696425; 0.0033623986790901972 -0.003243514967158763 0.001791495023691675; 0.0016360384020554944 -0.0028390913842805928 0.008106589642593288] %
+
+Mass Used: 83.20913522553383 kg
+Launch C3: 97.2243975379577 km²/s²
+||V∞_in||: 6.126816488030591e-6 km/s
diff --git a/archive/ES_0.5574528807340511 b/archive/ES_0.5574528807340511
new file mode 100644
index 0000000..9697002
--- /dev/null
+++ b/archive/ES_0.5574528807340511
@@ -0,0 +1,22 @@
+archive/ES_0.5574528807340511---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T20:49:30.824
+Launch V∞: [7.821413892510043, -5.760555151731869, 0.05991381115264165] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00022676304939390915, -0.00015443549203892837, -0.009965182611486762] km/s
+ V∞_out: [0.009136249668349366, 0.00353680691742747, -0.0018510062938931194] km/s
+ time of flight: 1.8547409031275424e8 seconds
+ arrival date: 2030-03-29T13:24:20.824
+ thrust profile: [0.4485634348701106 0.0013573522610049627 -0.1319791373528247; 0.12066154782989925 0.07111572579585053 -0.12509907520858643; 0.07819938383327057 0.07547625542716731 -0.14693323997072136; 0.04453379748064874 0.05698750199855604 -0.12571525954497736; 0.026383512463437675 0.04165318366280191 -0.10194810975005401; 0.01450052376875381 0.027150630697302013 -0.07264283626995743; 0.014144391982718869 0.030932827969076558 -0.08801725260853656; 0.004169806095852567 0.010149905645106469 -0.031255344458412763; 0.0007988975878128234 0.0018903338922352324 -0.00559126813459033; 0.00032550450400646233 0.0018830458470837628 -0.004708154531555518; 0.00014105948176842595 0.0012623594128563457 -0.004021719502869983; 0.0007990709750389637 -0.0014000374907585907 -0.0018949367195235803; -0.0025994898393029075 0.0003642282729909444 -0.0028865884159127173; 0.00038643821032611537 0.0002993369392507335 -0.0015889236622999934; 0.0023361588776102307 0.002688577053799801 -0.008408292196349584; -0.0038072902265503454 0.0016733333035680068 -0.007472959608978907; -0.002154495435622302 0.0026267811663927463 -0.0031297849007381256; -2.568287217983743e-5 0.001002501446418674 -0.0013552583775869754; -0.0005185097439907322 0.0002306251375831514 -0.00183364762282392; 0.00032655220367820454 -0.0008038450044984885 0.0001328050796657941] %
+
+Mass Used: 99.91610736303983 kg
+Launch C3: 94.36210059886052 km²/s²
+||V∞_in||: 0.009968958635787884 km/s
diff --git a/archive/ES_0.5575009554546022 b/archive/ES_0.5575009554546022
new file mode 100644
index 0000000..149dd7d
--- /dev/null
+++ b/archive/ES_0.5575009554546022
@@ -0,0 +1,22 @@
+archive/ES_0.5575009554546022---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:10:14.255
+Launch V∞: [7.748532693326795, -5.771699707401629, 0.15890087807972997] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.118227044931901e-9, -6.871059017094676e-10, -1.7404768538039908e-9] km/s
+ V∞_out: [5.628447630405358e-10, 1.1293535391070944e-9, 2.910872544582238e-11] km/s
+ time of flight: 1.868976373811483e8 seconds
+ arrival date: 2030-04-15T20:10:51.255
+ thrust profile: [0.5607135400810981 0.0021029760479023 -0.15619979617284127; 0.09534144210665245 0.05809889468127011 -0.09799913926844755; 0.06124518966669872 0.06017437732849015 -0.11463306573347812; 0.036636208136034534 0.047832684842023604 -0.10376515186808634; 0.04651814605474139 0.07704537095316945 -0.17667310275707102; 0.014454283720508965 0.028815851985851817 -0.07576005461541895; 0.009007262484919192 0.023540416366923163 -0.06331057186599409; 0.0009395502592204622 0.004505266563264553 -0.011956165943808595; 0.0039715571465422875 0.006670149047515822 -0.022828264296957293; -8.925055737339356e-5 0.0011472771017134668 -0.003443247617262078; 0.00030065436087986226 0.0019948816423785536 -0.006556389163162423; -0.0002714965747346097 0.0005658991742032729 -0.0018986357241622045; 0.0002825138972800843 -0.0006418768429181636 -0.005712063767351336; -0.000658325903563389 -0.0012447220129599432 0.0009107379214949474; -0.0010256605782807179 0.00029634378509006725 0.0011892830828238786; -0.0001262807263889414 -0.001349624296225759 0.0016803134735056333; -0.0017328869655186974 0.0007258930425625982 -0.0013833557133280281; -0.00047596573268817496 0.0033095760315156285 0.00214331602661075; 0.0027863043256044274 -0.001966801010168543 -0.0013326836303027064; -0.00012093856621976671 -0.0022427851706777625 0.0069994467309293035] %
+
+Mass Used: 105.71554694103497 kg
+Launch C3: 93.37752590102873 km²/s²
+||V∞_in||: 2.1798637395049606e-9 km/s
diff --git a/archive/ES_0.5575014990680331 b/archive/ES_0.5575014990680331
new file mode 100644
index 0000000..7a22b6d
--- /dev/null
+++ b/archive/ES_0.5575014990680331
@@ -0,0 +1,22 @@
+archive/ES_0.5575014990680331---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T20:20:48.706
+Launch V∞: [8.008775466291075, -5.487819999352019, 0.20404014433350012] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007566894112668521, -0.00044307324544351544, -3.254499308046139e-5] km/s
+ V∞_out: [0.0006318922646576868, 0.0003607635118741413, -0.0004982446037331947] km/s
+ time of flight: 1.874957778743772e8 seconds
+ arrival date: 2030-04-20T22:30:25.706
+ thrust profile: [0.5580157217730158 0.005555529687210111 -0.15942207738361563; 0.0517058039982845 0.03138106015066642 -0.05965162902456656; 0.05297970348145327 0.05286758274871245 -0.10997377950369328; 0.030265187433999204 0.04027014657064129 -0.09573457978488005; 0.028610619637095283 0.0474397439742043 -0.12404194466597133; 0.014503110087029656 0.027830893387536915 -0.0814858809589429; 0.012193957140795833 0.028747158364465786 -0.08912622442000094; 0.004407015126979514 0.011261150894322525 -0.03750464383326264; 0.004030338972561874 0.010179116838477442 -0.035702372184558476; 0.0008000122559952424 0.003170487269915284 -0.01118425548972174; 0.002228153685758622 0.005962344482703764 -0.020289312613793322; 0.00028413484799354936 -6.966502608332425e-5 -0.0003388363800054016; -0.0004555742660515515 0.0008806577149018454 -0.002461788848189982; 0.00028657559073920285 -8.016784879848584e-5 4.193113119875134e-5; 0.00033702050469474904 8.678997445782805e-5 -0.0002980031030915632; -0.0007291768078059872 -0.00018107242797658338 -0.00024465219726385845; 0.00027776855254131485 -0.0009453662440177908 0.0004663440743423751; 1.4743153321697641e-5 -9.602996564647481e-5 -0.00036513791640401417; -9.139591010889463e-5 -0.001644557165640865 0.0020536348582475576; -0.0009407800737327176 -0.0009376489381775053 0.0006810821240826068] %
+
+Mass Used: 100.34508527372691 kg
+Launch C3: 94.29828519525346 km²/s²
+||V∞_in||: 0.0008774690550246386 km/s
diff --git a/archive/ES_0.5575053976330567 b/archive/ES_0.5575053976330567
new file mode 100644
index 0000000..f8a4a0a
--- /dev/null
+++ b/archive/ES_0.5575053976330567
@@ -0,0 +1,22 @@
+archive/ES_0.5575053976330567---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T01:06:30.429
+Launch V∞: [8.161525179180147, -5.750016855165054, 0.08474378021259556] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.278803795594108e-6, 3.690557773052243e-6, -2.794720802828638e-6] km/s
+ V∞_out: [8.484149281159444e-7, 6.2395477018722706e-6, -2.8841385048312707e-7] km/s
+ time of flight: 1.8749577787480396e8 seconds
+ arrival date: 2030-04-26T03:16:07.429
+ thrust profile: [0.15383389099854622 -0.007398621002043758 -0.06066490684245179; 0.014585596543941393 0.00634603139256457 -0.019692193098893668; 0.03129945876462599 0.020616141367341953 -0.07555016300202823; 0.035389674446183426 0.028662222606405774 -0.12244018142633573; 0.02761310100081473 0.025229496916286957 -0.12405158085462624; 0.016558493330200128 0.01625764465245982 -0.09104824100502487; 0.020291729810351333 0.021374630669690434 -0.1306659808391868; 0.010996268307996765 0.011999062569267976 -0.0808287497179574; 0.0036788650268109995 0.0040696315051910095 -0.029331000763834117; -2.0117715643696806e-5 -0.00043340682942855156 -0.0036273123489858504; -0.0002836062704907139 0.0010757583993612689 -0.004264835241356095; 0.0013491111124325503 -0.0009033454343945542 -0.006574355432411727; -0.00020512838952152246 -0.0008372328808534891 0.00026366602411670567; -0.0013620159725222093 0.0005103898390851855 -0.0033774716375600707; 0.006241141447847136 -0.00014429514600048114 -0.002140393497504884; 3.139769454139191e-5 7.031871563260474e-5 0.0009299673685136799; 0.001571061644275959 0.005823267084771535 -0.006999596911445852; 0.0013911664346198803 0.0007097287250669728 -0.0035179745639541413; -0.00040851247565548536 0.0008406337266120589 -0.0016634014076395802; -0.0027434534095396325 -0.004683898849804842 0.0027087566508813502] %
+
+Mass Used: 68.95414711064177 kg
+Launch C3: 99.68036859335847 km²/s²
+||V∞_in||: 6.303875233789929e-6 km/s
diff --git a/archive/ES_0.5575105515196037 b/archive/ES_0.5575105515196037
new file mode 100644
index 0000000..7657d30
--- /dev/null
+++ b/archive/ES_0.5575105515196037
@@ -0,0 +1,22 @@
+archive/ES_0.5575105515196037---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T20:27:51.979
+Launch V∞: [8.112314913472268, -5.701747963374397, 0.1678637808785557] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.9142961172661344e-5, 3.4187919814821006e-5, 0.0023769364257542123] km/s
+ V∞_out: [-0.002104775686850554, -0.0007230447293514633, 0.0008343442925706011] km/s
+ time of flight: 1.8597445966441485e8 seconds
+ arrival date: 2030-04-06T08:02:10.979
+ thrust profile: [0.2212216783182609 -0.005838865985060177 -0.0771201695974745; 0.03682827610235144 0.018010880073094624 -0.04629024719977236; 0.036402425380126335 0.028412362563744846 -0.08068114327975542; 0.039501804118070194 0.039797234745020615 -0.12680216653124302; 0.02152667129081593 0.025241657429971705 -0.0919916941554756; 0.0259289290801967 0.036331158508365546 -0.1410259503838196; 0.01509127608779145 0.021970475633338787 -0.09614295949896487; 0.003872110998625802 0.006494394669089352 -0.032449451933422004; 0.005996245725348582 0.011145996083781367 -0.05487334097158838; 0.0022164989109092876 0.003848294985981271 -0.01970329158969041; 0.0009532958861820362 0.0014289132305663668 -0.007904221147360401; 0.0018154743192653235 0.00011544779050545457 -0.0027618370765414707; -2.2870617453271593e-5 0.0005351818047687182 -0.0026218234456131732; 0.0013994270399150504 0.00040459441600500777 -0.0041763946006670855; -0.002155331980653764 -0.000591095518778615 -0.00762598374845544; 0.0021995520877717695 0.005633353760027092 -0.005956671781789187; -0.000389587093371654 0.00024642392522903267 0.0007606348163102421; 0.005596238697784508 0.004542600453256693 -0.001086863747090255; 0.0007468646329816213 0.00408071094250217 0.001668403381352656; 0.003374231005473234 -0.0012178793909353907 -0.0041818345204991106] %
+
+Mass Used: 76.73370227717396 kg
+Launch C3: 98.3477613421195 km²/s²
+||V∞_in||: 0.0023776901851526606 km/s
diff --git a/archive/ES_0.5575133998156266 b/archive/ES_0.5575133998156266
new file mode 100644
index 0000000..78e4456
--- /dev/null
+++ b/archive/ES_0.5575133998156266
@@ -0,0 +1,22 @@
+archive/ES_0.5575133998156266---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T20:57:03.110
+Launch V∞: [8.118310413737339, -5.616084951745107, 0.18102129768502379] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9280791546321237e-10, 6.945575155289942e-9, -1.956396119814013e-9] km/s
+ V∞_out: [3.132671201743203e-9, 6.5766403438877005e-9, 1.6320229115507217e-10] km/s
+ time of flight: 1.8749577787493888e8 seconds
+ arrival date: 2030-04-22T23:06:40.110
+ thrust profile: [0.2673078406837713 0.004723662247679899 -0.07679945447931029; 0.05798097417729404 0.037101207483281926 -0.06667072709469235; 0.05541707609421838 0.055430683067270795 -0.10906811261122913; 0.01904412086728647 0.0243655094004817 -0.06389167097089254; 0.011095362716350674 0.019780704808603174 -0.05155206118690476; 0.016815937453908452 0.0367363298770689 -0.09785193341444083; 0.014234399426436024 0.03459302952445429 -0.11122843038198438; 0.01934691763609087 0.046925585200339466 -0.13410455213965186; 0.002809800837599035 0.009100568118081628 -0.030626815273333767; 0.0012161382063895563 0.01024552426148534 -0.03332124004958466; -0.00033821154146283387 0.00012539435716997678 -0.002970182384875472; 0.00046836538238677263 0.0012901666567480949 -0.0016108193891059114; -0.00045825258565754517 -0.0012831772673604638 -2.9346819545505217e-5; -0.0010962908252458796 -0.0010958027742630021 0.001303308784973851; 0.0015593959554335212 -0.0005148302804104312 0.0007891629782493432; 0.0018351176531485034 -0.0004140073444483649 -0.00247166641743059; -0.002968351850808175 0.0007544051546239609 -0.004646904052530352; 0.0011359525115758418 0.0025809867016787346 -0.0032762998031133058; 0.0002607469178754341 -0.00039808711800044165 0.001571857586216894; 0.00022786242987381136 0.001060872880282772 -0.0010400255052021128] %
+
+Mass Used: 81.79813304772551 kg
+Launch C3: 97.48014286922952 km²/s²
+||V∞_in||: 7.221789009017235e-9 km/s
diff --git a/archive/ES_0.5575212469848503 b/archive/ES_0.5575212469848503
new file mode 100644
index 0000000..67ef98d
--- /dev/null
+++ b/archive/ES_0.5575212469848503
@@ -0,0 +1,22 @@
+archive/ES_0.5575212469848503---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T03:09:10.722
+Launch V∞: [8.044164601242912, -5.727978168489987, 0.3022434706727844] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00013062278782128658, 9.358581273879885e-5, 0.006127301769123305] km/s
+ V∞_out: [-0.005473329992668728, -0.0018354809626169545, 0.0020457347222361598] km/s
+ time of flight: 1.874957778742837e8 seconds
+ arrival date: 2030-04-24T05:18:47.722
+ thrust profile: [0.2470905558395874 -0.0009943233422439273 -0.06931998176471874; 0.043211172070279295 0.024564100719703257 -0.05019836705662811; 0.09216625257470179 0.08125759809547003 -0.1726535188201626; 0.028635522273774354 0.033296258211475964 -0.08815609288468769; 0.023099801946270797 0.032649267960604945 -0.09495665471848391; 0.01932754882364872 0.03305050848192864 -0.10721553462989461; 0.01275550631507739 0.023574838518657104 -0.08164153218975394; 0.006451352234641623 0.014571134660547718 -0.05498729483996053; 0.003967272160936365 0.011333708859130733 -0.044225248030935534; 0.0004193722383345145 0.0016222174736428368 -0.006657737407100816; -0.0003656515277457074 0.002266727272444426 -0.007927085814427203; 0.00026640618116283545 0.0010890837291451139 -0.000518208694889328; -0.00022411254191020958 -0.0014113873031559145 0.003956575668852385; 0.002046476268107861 -0.0013372193853817365 0.0015648740134165755; 0.001788144479180165 -0.0016912470880991258 0.0016062125232676314; 0.0008239840360152371 0.003252584867162759 0.0057167918404857285; -0.0012159736836651275 -0.0009732286385359007 0.0031969765964781627; 0.0005749786358805926 -0.0012793196198458573 0.001151943609456287; -0.000539059548397032 -0.0014987608174639412 0.002870733578432951; -0.0003390696404777032 -0.0001337626881025368 9.181620285181525e-5] %
+
+Mass Used: 81.05171812977323 kg
+Launch C3: 97.60966914615177 km²/s²
+||V∞_in||: 0.0061294084206345535 km/s
diff --git a/archive/ES_0.5575212823153023 b/archive/ES_0.5575212823153023
new file mode 100644
index 0000000..0df7dd4
--- /dev/null
+++ b/archive/ES_0.5575212823153023
@@ -0,0 +1,22 @@
+archive/ES_0.5575212823153023---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T01:35:25.141
+Launch V∞: [8.115916356801419, -5.575653925193688, 0.18852223375881777] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.021980847641255317, 0.13149051225028255, 0.16075670308805845] km/s
+ V∞_out: [-0.08763394130664147, 0.07314104637542977, -0.17475260756542174] km/s
+ time of flight: 1.8749577787482828e8 seconds
+ arrival date: 2030-04-23T03:45:02.141
+ thrust profile: [0.3417714976356789 -0.004636630591180254 -0.1105838681551122; 0.04329275163858146 0.023359913644332698 -0.052489011956505696; 0.03301919277327136 0.028469485479984735 -0.07190926965459211; 0.02682759643953445 0.030292876509913774 -0.08709545590907507; 0.016207155795868393 0.021375877046123308 -0.06860812486310662; 0.022889763392033302 0.03564319625584832 -0.1238062870712779; 0.01722287257297444 0.03072747517211965 -0.11515249367415639; 0.0081316381398153 0.017118102102902644 -0.06884918805414231; 0.0058789462989387005 0.012185814236169601 -0.05252148132748643; 0.002660761124754736 0.0060402030060378266 -0.027339996653461516; 0.0006325810262229474 0.0013581085545289581 -0.005426403120468325; 0.0016005095488177306 0.0003764304933637464 -0.004577016018887056; -9.429594750969689e-5 0.0004899104115649545 -0.002244268582827778; -0.0006893740381475258 -0.0005116225949769138 -0.00016023055962367306; -0.000832048106655566 -0.00048187714166750663 -0.0019520896744900588; 0.0006540320732138713 -0.0002684027198548455 -0.0006478887374970917; 0.00486364564662229 -0.0017244945823069466 -0.00657045031016687; -0.005840933746913567 0.0024936913300737645 -0.0024417607612712937; -0.002350428423895143 0.00584759622663588 -0.007287934446558135; 0.0015728212529562346 0.0016493717517539015 -0.00032756385784854427] %
+
+Mass Used: 84.65742148683421 kg
+Launch C3: 96.99155563674601 km²/s²
+||V∞_in||: 0.20884355403653704 km/s
diff --git a/archive/ES_0.5575240956841883 b/archive/ES_0.5575240956841883
new file mode 100644
index 0000000..5507fde
--- /dev/null
+++ b/archive/ES_0.5575240956841883
@@ -0,0 +1,22 @@
+archive/ES_0.5575240956841883---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T05:53:27.621
+Launch V∞: [8.03768840983625, -5.901558688712421, 0.02418332448319357] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.05038653250016059, 0.2979853620953217, 0.41928943842414124] km/s
+ V∞_out: [-0.21089180692615134, 0.17493437368974213, -0.43810916385744597] km/s
+ time of flight: 1.8430725569578576e8 seconds
+ arrival date: 2030-03-19T10:21:02.621
+ thrust profile: [0.13205373017348337 -0.0073262559744604475 -0.050793500700334816; 0.047672621184566985 0.020903292721186628 -0.062100285851894844; 0.053349092482396394 0.0366465286937011 -0.12096455621763141; 0.030559923649052047 0.026135865614272766 -0.1010560385773884; 0.02621086824211512 0.025830902930661887 -0.11285913786064586; 0.02349064401253856 0.02550715459724527 -0.12360634023401534; 0.014920002437034448 0.017552316105391885 -0.0938379086944092; 0.005889804532427677 0.0073317966870319945 -0.04410649982771391; 0.0030207901027095125 0.004097448839083934 -0.02616527525390876; 0.004939955588475515 0.006766392426681126 -0.04561809019212264; 0.0018209507808404088 0.00242199280235706 -0.020974495976567645; 0.0006731319840155977 0.00010514423722021002 -0.0004676902639324928; -0.0002539246006547203 0.0004503038439339425 -0.00021251510125899016; -2.808058451119681e-5 -5.9577620882257936e-5 -0.0003581337209717242; -7.491342341962573e-5 -0.00011237099003257847 0.0005472806781880051; 0.0001214276932247699 -0.0006813251781173206 0.0005435685579548725; 0.0008069911782565119 -0.0010283552400021188 0.0005368445618223462; 0.00016691326483634673 0.0005117981431967876 -0.00015248894750592772; -0.0012942972400129356 -0.0010677729641822365 0.0011957840564963173; 0.00040508111359966316 4.882118950414724e-5 -0.00039491224023219555] %
+
+Mass Used: 70.41652551337575 kg
+Launch C3: 99.4334147631161 km²/s²
+||V∞_in||: 0.5168536658034859 km/s
diff --git a/archive/ES_0.5575251945406304 b/archive/ES_0.5575251945406304
new file mode 100644
index 0000000..f09efaf
--- /dev/null
+++ b/archive/ES_0.5575251945406304
@@ -0,0 +1,22 @@
+archive/ES_0.5575251945406304---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T07:24:10.993
+Launch V∞: [7.83954677146921, -5.7320852440310235, 0.12459789674506681] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5705849308391812e-9, 5.831741270564715e-10, 1.999664712334413e-9] km/s
+ V∞_out: [2.0983457364917603e-9, -2.019804329764757e-9, -1.585235925577261e-9] km/s
+ time of flight: 1.8477124125016534e8 seconds
+ arrival date: 2030-03-20T20:44:51.993
+ thrust profile: [0.47177705666750663 -0.00017359971527440457 -0.1351276371018277; 0.10976189582120799 0.06654798521627943 -0.11758602502901098; 0.07789124490265041 0.07672891563860007 -0.150456619236737; 0.02793370747454769 0.03640368960922166 -0.08232352526108665; 0.024581775753014314 0.04038848694705111 -0.09960152126351024; 0.014659541198587827 0.028804935209615374 -0.07731622335701856; 0.013511916569144482 0.03147758719663842 -0.08957494210275342; 0.008007884398351279 0.02083140750552041 -0.06289131611677469; 0.0012571139616748812 0.00406480059315036 -0.01387866262196126; 0.001753970687185625 0.006174333412936009 -0.02116965688659543; 0.0008275549626496532 0.0009942124927954249 -0.0018425268292385695; 0.00013251709111151803 0.0010107646989135056 -0.0037654919462300806; 0.0005049124143237323 0.0011402255855003929 -0.003801810983104342; -0.00012349637463108425 0.0005508880183107423 -0.0024538745917548816; 0.0007068453932090021 4.562972131882904e-5 -0.0023910215331854785; -8.302337947665907e-6 -0.000848530019628411 0.0009956763658189173; -0.0006570506444575822 -0.00021924124668910383 0.0007881659879139591; -3.7423637073259676e-6 0.00021128395822149907 0.0007361167723411335; -0.0004792731210109931 3.0211380312796744e-5 -0.00048708116440733355; -0.0007305443738253267 0.003476541692562041 -0.0024218927182047415] %
+
+Mass Used: 100.18294676460755 kg
+Launch C3: 94.3308194627648 km²/s²
+||V∞_in||: 2.608733035249614e-9 km/s
diff --git a/archive/ES_0.5575279014922665 b/archive/ES_0.5575279014922665
new file mode 100644
index 0000000..f50552b
--- /dev/null
+++ b/archive/ES_0.5575279014922665
@@ -0,0 +1,22 @@
+archive/ES_0.5575279014922665---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T07:20:11.903
+Launch V∞: [7.928829646610438, -5.730875874921662, 0.18503083167558648] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.9641390929690006e-7, -1.2850448682088077e-6, -3.7087145994163877e-6] km/s
+ V∞_out: [-3.521015094889865e-6, -4.1252278168826093e-7, 1.7367633059514058e-6] km/s
+ time of flight: 1.837222898315919e8 seconds
+ arrival date: 2030-03-08T17:18:20.903
+ thrust profile: [0.37832992174971314 -0.007942401156741987 -0.10769099256390775; 0.09538178217970351 0.05397323716012524 -0.09984926301705403; 0.05317078128152602 0.04878344349623956 -0.10181999801503018; 0.02707295113967701 0.030981668159608906 -0.07280235449373207; 0.02150195164394008 0.03213605771731628 -0.08211104664732913; 0.022976690337020853 0.04295056905453565 -0.11523832186274223; 0.02839955409665937 0.06074221071727777 -0.17066023358964624; 0.00611398067161045 0.014029201537961663 -0.04381234808393991; 0.0021988720683994993 0.005780776076512487 -0.019712356408077766; 0.002366225201975653 0.006803202376217411 -0.024043478485416294; 0.00011702959386332629 0.0002742783929628383 -0.0008709052223372819; -0.00035770406190260417 -0.00017360441919995502 -0.0012089345609797631; 1.2985991972218663e-5 -0.0005045238978754451 -0.0006967955759403549; 0.0006173662371798315 -1.7892992218147363e-5 -0.001235417871565175; -0.000676510555900251 -0.0013380729728488109 -0.000809693261065819; -6.360893737326038e-5 0.0003216854911511867 -0.000458184378632177; -0.0014391492233579396 5.4360921512534304e-5 0.0004472494932887453; 0.00025679932686193145 0.002270317039471937 0.00010561534692181429; -0.0008918701201117814 -0.0010788899887581597 0.0005894489718957929; 0.0011678272370495267 0.0030713758377521787 -0.00029740579418866887] %
+
+Mass Used: 91.94538518115405 kg
+Launch C3: 95.74351426739831 km²/s²
+||V∞_in||: 3.945002950660253e-6 km/s
diff --git a/archive/ES_0.5575334030453498 b/archive/ES_0.5575334030453498
new file mode 100644
index 0000000..2268a5a
--- /dev/null
+++ b/archive/ES_0.5575334030453498
@@ -0,0 +1,22 @@
+archive/ES_0.5575334030453498---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T16:02:11.560
+Launch V∞: [7.9895104019610566, -5.898577261196799, 0.1490445432972797] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.0787940564189045e-6, -2.7703177766610098e-6, 1.991392145861211e-6] km/s
+ V∞_out: [-6.226974262967392e-7, -4.550233976565255e-6, 2.1536659057816952e-7] km/s
+ time of flight: 1.841139248825415e8 seconds
+ arrival date: 2030-03-16T14:47:35.560
+ thrust profile: [0.1680568502603158 -0.007752109556014475 -0.06279322459897356; 0.08606533375269271 0.040771713371100124 -0.107982184238869; 0.04487121044046773 0.033413880490664426 -0.10090910892972758; 0.0313449562998834 0.029567675103363368 -0.10255293303704842; 0.022415358881086384 0.024462597919824833 -0.09627236002490336; 0.02646167583179067 0.03379474393232936 -0.1435909930132851; 0.014715723488645183 0.019225544440932486 -0.09129387193294294; 0.005800068911124545 0.008509547856462454 -0.041748583614727275; 0.0028235673618892394 0.004017426388758298 -0.022229451105122117; 0.00040900409726416024 0.0006522621102003112 -0.0038817299481266223; 0.000710765930830221 0.0009532271516857792 -0.005289814441683971; 0.0037750913657627356 0.006012593228659117 -0.040603714912718795; 0.0003761903680344557 0.00044148164863518785 -0.001487523425536495; 0.00024954348172626426 -0.0004277819278044722 -0.0007101032687289745; 0.0007948331151957953 0.0006683694736705801 -0.0007886725935883548; 2.5568796687031135e-5 0.0001245575858083482 -0.0014330899542506082; 0.0003858051894446268 -4.3393224746118874e-5 -0.0013522986008617304; 0.0004369946140277048 0.0008953844789603891 8.12544054590806e-5; 0.0004008579090239912 -0.0003992393064480397 -0.0017555052995314123; 0.000143179639764926 0.0009383779006178498 0.0003946708182436332] %
+
+Mass Used: 75.01069428901656 kg
+Launch C3: 98.64770444523855 km²/s²
+||V∞_in||: 4.59557135774455e-6 km/s
diff --git a/archive/ES_0.5575411267319265 b/archive/ES_0.5575411267319265
new file mode 100644
index 0000000..46c7b1e
--- /dev/null
+++ b/archive/ES_0.5575411267319265
@@ -0,0 +1,22 @@
+archive/ES_0.5575411267319265---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:24:31.658
+Launch V∞: [8.028612567201757, -5.681245231729612, 0.23891871386261251] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.816102711702354e-7, -3.7123404395649365e-6, 7.052554155618727e-5] km/s
+ V∞_out: [2.6617942318635603e-6, -7.112710279300178e-5, 8.082342741286157e-7] km/s
+ time of flight: 1.874957778678628e8 seconds
+ arrival date: 2030-04-24T02:34:08.658
+ thrust profile: [0.36023628726688495 -0.0019242200398304655 -0.11781196285591451; 0.04260645049617232 0.024475507576068135 -0.054339458488004595; 0.032070840598959406 0.029191464776450213 -0.07313849196400639; 0.027207096021089852 0.03256519277652006 -0.09081421277388552; 0.01948566535609645 0.028118785057450833 -0.08808004716059092; 0.01278877664185575 0.021282335764041923 -0.07397513520049645; 0.010485236912269916 0.018740027630580948 -0.07310164335085484; 0.010384385505393803 0.022154998525153714 -0.08698636826334298; 0.012012617414704961 0.027553817027741644 -0.10858679230552419; 0.002782740714844294 0.004739128788940817 -0.02897399740176572; 5.623067618000424e-5 0.0014173234563256596 -0.007103934708276482; -0.001108645330781111 0.0002958328145807299 -0.00368115368568494; -0.0010718899839662847 0.0011703768245789926 0.0008802160796920031; -0.0006980602282055723 3.1601643954726156e-5 0.00038771350342195867; -0.0027150422612301477 0.0015408549596936552 -0.0017436099775815022; -7.902117250178106e-5 -0.00037444193498137096 0.0004991170344383585; 0.001301303685773512 0.0005531518722877626 0.0035121073764903354; 0.00017695858979800152 -0.00044957171618834795 0.0013947024840698422; -0.0007525632020861052 -0.003598379198765716 -0.0008479807343782453; -0.0024011285945802693 -0.0007969952133563671 -0.0031867387041486484] %
+
+Mass Used: 85.84319366741465 kg
+Launch C3: 96.79224928911421 km²/s²
+||V∞_in||: 7.062421050696277e-5 km/s
diff --git a/archive/ES_0.5575424637374314 b/archive/ES_0.5575424637374314
new file mode 100644
index 0000000..783e4fe
--- /dev/null
+++ b/archive/ES_0.5575424637374314
@@ -0,0 +1,22 @@
+archive/ES_0.5575424637374314---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T02:35:57.017
+Launch V∞: [7.857118276228186, -5.628667646301582, 0.26083104522426165] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.114196014200681e-9, 1.1389589342741032e-8, -3.1793564115798306e-9] km/s
+ V∞_out: [4.701153803204235e-9, 9.270264690761506e-9, 2.4356752446897843e-10] km/s
+ time of flight: 1.8749577787555006e8 seconds
+ arrival date: 2030-04-21T04:45:34.017
+ thrust profile: [0.5112779169712802 0.0054347052814448 -0.1364828576145419; 0.16970239735340129 0.10434694585978344 -0.15574397999394549; 0.04932720603519677 0.0509963618185067 -0.08770046848262311; 0.0400249892083083 0.05554712429560621 -0.10596974134466261; 0.02262370354909407 0.039751656384719794 -0.08579412225183357; 0.017248333538948276 0.03683035525868638 -0.08566332712736367; 0.009364525619791893 0.024604374372376527 -0.06214983597009437; 0.0043669007541370375 0.01641891069812428 -0.03981782273155087; 0.0020678046503071743 0.011244437674749166 -0.027787839398043326; 0.0017579726693331531 0.009693071138102846 -0.026881424297704303; 0.000971533577323655 0.006006423116424108 -0.02025585275747885; -0.00024135375596952513 0.0003614174359060745 2.4883647753946197e-5; -3.205752071873355e-5 7.00416785229549e-5 -0.00027313959452531953; 0.00017862705026686212 0.00028482325674841725 0.0004966517624022553; 0.000548850633592863 0.00025016386374799963 -0.00010606570362929439; 0.00040923234816907033 -0.00023846959456938689 -0.0002214198768914898; -0.00017885888481009553 -0.00034573495800783034 -0.00024095195155022156; 0.00020071405381627831 -5.1627351256157867e-5 -0.00010467776382143816; 0.00024517461367604555 0.00037547662663200217 -6.768384944250448e-5; -0.0006365117998056945 0.00037790793055224206 0.0006366392731069191] %
+
+Mass Used: 105.14147486600541 kg
+Launch C3: 93.48423991331394 km²/s²
+||V∞_in||: 1.1877393878549055e-8 km/s
diff --git a/archive/ES_0.5575447568397769 b/archive/ES_0.5575447568397769
new file mode 100644
index 0000000..c82728f
--- /dev/null
+++ b/archive/ES_0.5575447568397769
@@ -0,0 +1,22 @@
+archive/ES_0.5575447568397769---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T08:13:14.032
+Launch V∞: [7.839602892134635, -5.856017964795735, 0.13259791015807781] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.782603409879295e-10, -1.0796411410731644e-9, 1.0593979572294215e-9] km/s
+ V∞_out: [5.439038875019923e-10, -1.826353794467323e-9, 2.6379161831931955e-10] km/s
+ time of flight: 1.8749577787491965e8 seconds
+ arrival date: 2030-04-24T10:22:51.032
+ thrust profile: [0.3739337035056871 0.016997101898748944 -0.09588653633783943; 0.1014545427590717 0.06328420078237254 -0.10664336318513763; 0.054051671803158396 0.055351243238817245 -0.10549400524067097; 0.033410262441346955 0.04618927537621391 -0.09798946392468295; 0.013643249162389317 0.02471168279513486 -0.061977470139744625; 0.03003373041072285 0.05829833243320012 -0.14436473056377516; 0.006273707324003507 0.016350420171324397 -0.048203269754761614; 0.006367099043311449 0.01981551171547389 -0.05830840666147559; 0.0023810300753212693 0.006885189800635805 -0.023019093848570593; 0.0008472630838856047 0.002999563510778087 -0.010340861134569126; 0.0030587086247569556 0.016527311479957126 -0.05274346513924192; 0.00018016474624479352 0.00073213975410052 -0.003120463143200644; 2.719195310027612e-5 3.3930174432059775e-6 -0.00021107112431981612; 9.810629480631188e-5 -0.000595190312938343 -5.421126956150758e-5; 0.00010252695385546452 0.00025255288197606707 -0.00017986510348481108; 4.077764191529109e-5 -0.000463539600131369 -1.9263933920956678e-5; -7.91576120178111e-5 -0.0009483360251039108 0.00020422530248779777; -9.60825573421785e-5 -0.0007282198076106189 0.0009910716656321105; 0.00023189584514175557 0.0005808807581136983 0.00011448957208309309; -0.0005246951647352213 0.00054343924599025 -0.0007952204232244257] %
+
+Mass Used: 91.81112063550563 kg
+Launch C3: 95.76990211615441 km²/s²
+||V∞_in||: 1.7010697174526047e-9 km/s
diff --git a/archive/ES_0.5575539549479438 b/archive/ES_0.5575539549479438
new file mode 100644
index 0000000..606bec3
--- /dev/null
+++ b/archive/ES_0.5575539549479438
@@ -0,0 +1,22 @@
+archive/ES_0.5575539549479438---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T16:40:07.622
+Launch V∞: [7.91501915586407, -5.848057524895937, 0.131212003914939] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.915824055709587e-7, -1.1887290403014025e-6, 3.132068977046816e-5] km/s
+ V∞_out: [1.4368015920057226e-6, -3.134265821112296e-5, 2.419130044354483e-7] km/s
+ time of flight: 1.858790965070884e8 seconds
+ arrival date: 2030-04-06T01:45:03.622
+ thrust profile: [0.3278902253612864 -0.014176220852393262 -0.0970802086987531; 0.05760698027163614 0.029728386279506764 -0.07632450935151423; 0.06251720446605151 0.05022934681756704 -0.1407249520423999; 0.03772848802280659 0.03968524855380034 -0.1275128629137544; 0.03363001418102771 0.04069240396465751 -0.14408407878237348; 0.008638444859502666 0.01193128459700148 -0.04601405469817526; 0.00673223456814578 0.012452594443569958 -0.04855424191365939; 0.0053267127019360734 0.009953981504964838 -0.04977580181481766; 0.0053695004703750385 0.00977155106079513 -0.051694613082004924; 0.0017233657493029605 0.002941490319642197 -0.017408282244481897; 0.0011443386449249372 0.002005357416797522 -0.010912626622227707; 0.001521856622193801 0.0017101487548671472 -0.010905161044692701; 0.0008464211067006659 -0.00040633551274659406 0.00032466993570262506; 0.0002541809527829437 -0.0011057091658143452 0.001039762327229439; -0.0018087675532774048 0.00043313453997320114 0.0017985136509577444; -3.1615583467160845e-5 -0.000290432321421551 0.0014047644189653001; -0.0008103044802947293 0.0002923429321967558 0.001497914138251215; 0.0007872924311081507 0.001424224951468155 -0.0005092615902755778; -0.0011431667139908562 0.0017281276395165678 -3.9605192926310626e-5; -0.0013917768561895628 0.0015896184398286255 0.0018561918726194451] %
+
+Mass Used: 85.43657119334284 kg
+Launch C3: 96.86452164215855 km²/s²
+||V∞_in||: 3.13438253607834e-5 km/s
diff --git a/archive/ES_0.5575633113772067 b/archive/ES_0.5575633113772067
new file mode 100644
index 0000000..a26ee29
--- /dev/null
+++ b/archive/ES_0.5575633113772067
@@ -0,0 +1,22 @@
+archive/ES_0.5575633113772067---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T11:40:37.693
+Launch V∞: [7.852573643423757, -5.548063181709071, 0.2750685616249827] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5032754348917953e-9, 4.760890177927125e-10, -6.3174525640689765e-9] km/s
+ V∞_out: [-1.9529761391795367e-9, 6.876858195745231e-9, -1.0864238372136336e-9] km/s
+ time of flight: 1.874957778741773e8 seconds
+ arrival date: 2030-04-20T13:50:14.693
+ thrust profile: [0.6577919945672711 0.0007273318119973165 -0.17038917754168537; 0.09613848567199035 0.060424432700709456 -0.09574371461434814; 0.05465670412725712 0.05702719243744343 -0.1019298488260888; 0.052081795006155805 0.07179390780426102 -0.14052927566569134; 0.015335916965827395 0.027505181859755992 -0.06313375961869112; 0.01254031364692076 0.02738562797564909 -0.06784791612118253; 0.011901706828453556 0.031532924963926665 -0.08226001108785663; 0.006941441458028691 0.022068505061608203 -0.06140138752241862; 0.0020036229295855865 0.0069756313430837024 -0.0203288315954864; 0.001207125357674441 0.005541368285151253 -0.018864883905928755; 0.000879447284924116 0.0034390257977164112 -0.012219509486297065; 2.2300235175791872e-5 0.0005949048642786994 -0.0021204377073580183; 0.00013131633786300014 0.0004325645931848928 -0.0015786735981175638; -0.00010594503516549403 0.00016353768251275197 -0.0005508148571624078; -5.279077622562459e-5 0.00041047967077305597 -0.0005399116395913491; 7.060253205844282e-6 -4.718194580901366e-5 -0.0004969395885567097; 0.00023895232108799415 0.00015658438967314708 -0.0002615802433665631; -7.405409463817346e-5 3.049850075406864e-5 0.00018925458009889755; 0.0001602681785364353 -7.143979562023394e-5 -0.0004702909106885857; 0.00026654886003091185 0.0002904331496345976 -0.0007110268895467238] %
+
+Mass Used: 110.7929763979364 kg
+Launch C3: 92.51958060722369 km²/s²
+||V∞_in||: 6.511275196555098e-9 km/s
diff --git a/archive/ES_0.5575668726874371 b/archive/ES_0.5575668726874371
new file mode 100644
index 0000000..5782026
--- /dev/null
+++ b/archive/ES_0.5575668726874371
@@ -0,0 +1,22 @@
+archive/ES_0.5575668726874371---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T13:55:10.325
+Launch V∞: [7.940142160743537, -5.940969083765449, 0.32568773265147727] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.193151239343893e-10, -9.050904902047788e-10, -1.18723169736659e-9] km/s
+ V∞_out: [9.91327551642007e-10, -8.818493792747185e-10, 3.3605024241746995e-10] km/s
+ time of flight: 1.829663599404393e8 seconds
+ arrival date: 2030-03-02T05:54:29.325
+ thrust profile: [0.12742732210605393 -0.00299007743320023 -0.04427149556920487; 0.10590389079363782 0.05571963340139605 -0.11687029836048686; 0.07387593875460575 0.06251505267662176 -0.14491407322324257; 0.046844868500088815 0.05137120919158366 -0.1354005854889806; 0.030341362751020742 0.040187901171836085 -0.11846370030150861; 0.019563184435411107 0.029963477006421498 -0.09696530146310789; 0.015256630246326107 0.025892171570614627 -0.09007926658168779; 0.007805604461315446 0.014323823332449347 -0.05402674548114576; 0.0008506360583472101 0.0017872124605037727 -0.007342591764642361; 0.00051624631804151 0.0006248181390563745 -0.003269181494140175; 0.00010587385929907204 0.0004967658692396654 -0.0026035942670340822; 0.0004007714798528703 -0.00018280227789348337 -6.6092058578956e-5; -0.00011873346545432863 0.00019520266512545878 -0.00034281059668307993; 0.0004742259902278813 0.0006840526026885846 -0.0005276425756009807; 0.0010616990467198935 -0.0010310769330490529 0.0017248401639186157; 0.0009621525658740101 -0.0021476382612995244 -0.0015179814136507721; 0.00038250453922162404 0.0007499218242820746 0.0010281470000498795; -0.0024023186436899894 0.0029703460711347873 -0.00045256138670733383; -0.0011099385221844003 0.0011360986109954802 -0.0050698547227961185; -0.0006250083454657199 -0.0020517211555856384 0.0021163425824125325] %
+
+Mass Used: 76.22026329874734 kg
+Launch C3: 98.44704368627359 km²/s²
+||V∞_in||: 1.6162484714377765e-9 km/s
diff --git a/archive/ES_0.5575671778649723 b/archive/ES_0.5575671778649723
new file mode 100644
index 0000000..7da2749
--- /dev/null
+++ b/archive/ES_0.5575671778649723
@@ -0,0 +1,22 @@
+archive/ES_0.5575671778649723---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:23:40.906
+Launch V∞: [7.920120763024283, -5.715636369436291, 0.2063407330239252] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.012607900810386e-10, -9.066564235520408e-10, -1.1635700525736895e-9] km/s
+ V∞_out: [9.752140006556372e-10, -9.078059663250432e-10, 3.6823338994125925e-10] km/s
+ time of flight: 1.8749577787492839e8 seconds
+ arrival date: 2030-04-24T01:33:17.906
+ thrust profile: [0.42371300954245816 -0.006538647403415058 -0.14257040012838143; 0.10946922303718146 0.05746966142955317 -0.13308213434147217; 0.037096852533086866 0.029646699093527334 -0.08369031673018787; 0.03301829427040979 0.03248749626713855 -0.10498898885943779; 0.027962018583554134 0.031804109924054476 -0.11576136100217645; 0.019344778198774153 0.024320295817440007 -0.09838789948060749; 0.010552393784743604 0.015241928160254513 -0.07223263637615177; 0.005818865555544661 0.008789026537457938 -0.0458555649657552; 0.0015531615589438282 0.0019782399568555116 -0.014019734650269152; 0.000667714578277525 0.0008103937823890079 -0.006342067625365605; 0.0007005917170052997 0.001938645434673917 -0.009225193558084207; -0.0013960942845461393 0.002349799866967028 -0.0034045951959569146; -0.0010444240654213831 0.002412744201805651 -0.0004634078485530541; 0.0001586581797903169 0.0016191666156197132 -0.004708456618884124; -1.691134042057423e-5 -0.0005284127035678658 0.003411778304134629; 0.000931189594589401 -0.0003328368404187675 -0.0007634928589374569; -0.00010582132559157096 -0.0012686617313471633 0.006646255002295852; -0.0009278245127062031 -0.0004938715848019054 0.0009651670013669314; -0.0003967801343450323 0.0015997226581068637 -0.00816842005072663; -0.0015891732153223148 0.002089290100793111 0.003948050556323225] %
+
+Mass Used: 93.76527455387395 kg
+Launch C3: 95.43938850661607 km²/s²
+||V∞_in||: 1.5929330416886302e-9 km/s
diff --git a/archive/ES_0.5575697394889916 b/archive/ES_0.5575697394889916
new file mode 100644
index 0000000..ad9a71f
--- /dev/null
+++ b/archive/ES_0.5575697394889916
@@ -0,0 +1,22 @@
+archive/ES_0.5575697394889916---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:45:45.427
+Launch V∞: [7.948982547418675, -5.696940894840371, 0.28760480637584046] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2701453751926048e-8, 1.3978019655623154e-8, -1.8026661372712223e-8] km/s
+ V∞_out: [1.3308819628757198e-8, 2.7606777444141245e-8, 7.17523543416992e-10] km/s
+ time of flight: 1.8749577787593505e8 seconds
+ arrival date: 2030-04-23T19:55:22.427
+ thrust profile: [0.42322966731499356 -0.0021869570258122744 -0.13495480872858834; 0.06185162310583394 0.03398732883388272 -0.07360190059603816; 0.047823990713808655 0.04186538949326202 -0.10231578231910829; 0.03301240934929632 0.03745013203386509 -0.10487718122788345; 0.028430436323784232 0.038689012046994015 -0.12000948911967918; 0.018874108625302068 0.028932427582154186 -0.10120932137918197; 0.007257055559388397 0.012726824924319076 -0.04882335144984627; 0.004136446811848094 0.00789145613535547 -0.03258268449099498; 0.00534659802262627 0.011387507132104709 -0.049185643548898816; 0.0009879737483835488 0.0028213598984875507 -0.011110658299385408; 0.002005748790982397 0.005610154911356932 -0.02658477197150553; 0.000792619089970273 0.0008241538081092309 -0.0008447557018855525; -0.003201967463655239 0.0004917491227766701 -0.0025810615474218834; 0.002111672004567419 -0.001851898517418836 -0.0023522845379514885; -7.232280610763251e-6 0.0005772194372758578 -0.0036031704904926254; 0.004164133635708816 0.003082677827765391 -0.0027952175244293975; 0.001423151892047769 0.002217480780866172 -0.00459030104555879; -0.003184784557954394 0.004347493136990283 -0.0022627692005510835; 0.0016133416501109463 0.0009074138802770508 -0.0050039842700552424; -0.0005402675602266309 -0.004783274517319118 0.0019367636566950852] %
+
+Mass Used: 92.10700493561308 kg
+Launch C3: 95.72417562312178 km²/s²
+||V∞_in||: 3.2182317445924547e-8 km/s
diff --git a/archive/ES_0.5575782666702511 b/archive/ES_0.5575782666702511
new file mode 100644
index 0000000..5276b82
--- /dev/null
+++ b/archive/ES_0.5575782666702511
@@ -0,0 +1,22 @@
+archive/ES_0.5575782666702511---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:58:53.926
+Launch V∞: [7.96184033866873, -5.714061014875915, -0.11673473690851444] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1863426406825083e-9, 3.278378637869782e-9, 1.4800928517692178e-9] km/s
+ V∞_out: [2.4706149993752945e-9, -2.2779863046772084e-9, -1.8155580751676665e-9] km/s
+ time of flight: 1.8749577787492535e8 seconds
+ arrival date: 2030-04-24T01:08:30.926
+ thrust profile: [0.3812223783966551 -0.010089802381230738 -0.12199842341513419; 0.04292244949664458 0.023515608386207823 -0.05321502849456755; 0.09743540265046448 0.08306224158760449 -0.20787367264667858; 0.026149540170222828 0.029199231169579197 -0.08633044929625444; 0.026924004417681176 0.03382867610355115 -0.11542829558336332; 0.012723002159082555 0.020852932596996786 -0.07602902723105288; 0.008297885296539975 0.015651578295711576 -0.06160046691554002; 0.003488645014406265 0.007148636280244177 -0.031114262422890067; 0.0024047095089062623 0.0052924775427706195 -0.0246484162730106; 0.0006887182591149325 0.001701463063621246 -0.008026335025580244; 0.00040838916643562775 0.0011394910992285523 -0.007016967877157913; 0.0009825899630634665 0.004661900591418598 -0.029049233371081437; -0.0009921707877921084 0.0004136078774376475 -0.00025134321063553745; -0.0006097326120285068 -0.00036450464483617304 -0.0034990618158186374; -0.0022984114669614784 -0.001539924177955068 -0.0012380010071941843; -0.0004835799280762479 -0.0005844045543415549 -0.0008185020430043718; -0.0012928016526251882 0.0016079484531109347 -5.5854743675111656e-5; -0.0015078228444259966 -0.002637679033103176 0.003221541468931148; -0.006408777232016234 -0.002956732495567211 0.0019997148179308312; -0.00031826725585893414 -0.0009757105535681798 0.004118557308608955] %
+
+Mass Used: 90.18701693791854 kg
+Launch C3: 96.05502185897848 km²/s²
+||V∞_in||: 4.209339079423969e-9 km/s
diff --git a/archive/ES_0.5575838509040627 b/archive/ES_0.5575838509040627
new file mode 100644
index 0000000..aa59726
--- /dev/null
+++ b/archive/ES_0.5575838509040627
@@ -0,0 +1,22 @@
+archive/ES_0.5575838509040627---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T14:46:33.632
+Launch V∞: [8.116567841765836, -5.8291111320239795, 0.09742443636618735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7284360330470226e-7, -1.145582946985739e-6, 2.718831389997487e-5] km/s
+ V∞_out: [1.1872144167045966e-6, -2.7230543462544425e-5, 1.989314046704148e-7] km/s
+ time of flight: 1.8749577779163253e8 seconds
+ arrival date: 2030-04-26T16:56:10.632
+ thrust profile: [0.14047988560939886 -0.005466190684182983 -0.05469990809860809; 0.00802698173817677 0.00360646390935442 -0.01113620159613063; 0.041218735067299145 0.027930327891427176 -0.09807579269373895; 0.05003503101902487 0.042938307900599736 -0.16849389493969752; 0.02838711277718321 0.02771068897969539 -0.12805221483567256; 0.02401843182301109 0.025501864625598846 -0.13332872529119247; 0.007391009988067581 0.008076477453631504 -0.05057380061339835; 0.0035604218149702287 0.004249160112682024 -0.028049665417328444; 0.0046529583886436455 0.005814868792543679 -0.04145103267747284; 0.00240556228569932 0.003076428968388568 -0.024690756992419637; 0.002158475110222142 0.0024044132648930005 -0.018302001836367036; -8.284871563267565e-5 -6.351756831896412e-5 0.00029634466551753174; -0.0002719710458462209 -9.747256050856177e-5 0.0019180738684161803; -1.1264144577532135e-5 -0.00015901718938317826 0.0037056792777323405; 0.0007762480057839912 0.001054469664245231 0.00019577224702807625; -0.00036898569790387467 0.00033366596915916516 -0.000559009471496875; 0.00015393328434705017 -0.0025613981046807574 0.0012616500935356519; -0.0003628245233359039 -0.0005071920574942802 -0.00017522547716714202; 0.00014108587584948928 0.00022908327340435812 0.00022043561098207; -0.003408622059620314 0.002730077776705411 0.0008393071647373502] %
+
+Mass Used: 67.95873315313884 kg
+Launch C3: 99.86670164027446 km²/s²
+||V∞_in||: 2.7212986751240565e-5 km/s
diff --git a/archive/ES_0.5575907249752716 b/archive/ES_0.5575907249752716
new file mode 100644
index 0000000..d7eb3aa
--- /dev/null
+++ b/archive/ES_0.5575907249752716
@@ -0,0 +1,22 @@
+archive/ES_0.5575907249752716---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T01:31:12.797
+Launch V∞: [8.070300718170854, -5.669439747460093, 0.10835470047094313] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2406200222699859e-6, -1.584508935683764e-6, -1.7761677369263673e-7] km/s
+ V∞_out: [1.478724083136872e-7, -7.3014841152157e-7, -1.8778145522864114e-6] km/s
+ time of flight: 1.8749577787493762e8 seconds
+ arrival date: 2030-04-24T03:40:49.797
+ thrust profile: [0.30256904736773166 -0.008868938423534556 -0.0993497799151667; 0.033997763500605876 0.017653108359588672 -0.04350785956165616; 0.06078991968055965 0.05017226874066922 -0.1326606240819778; 0.03210122519686858 0.03411942037764887 -0.10423299203294442; 0.034661256368489685 0.04333956680005156 -0.1489918641626913; 0.011300414204607276 0.015818592005051403 -0.06338353715588053; 0.0064478737062164644 0.008703997052747789 -0.039658530083626235; 0.008766973424181795 0.015041220948025394 -0.07025266203874529; 0.005454830247771648 0.010371987148424456 -0.05080889330162655; 0.0007415214172512507 0.0044061845132678185 -0.018717881867680763; 0.0008418447698900471 0.004407715403203068 -0.024845966405732122; -0.00036873854579050835 -0.001283685733349566 -0.0007697875436888197; -0.0021087336480423687 0.0007075677316539717 0.0008892416352340509; -9.323058119425833e-5 0.0006391604164504345 -0.00019401950028938644; -0.0017972286702230829 0.0011723418235252267 0.0033415280095845383; -0.00019982234111707358 -0.002608626632506299 -0.0030451661925102644; 4.7745546528227904e-5 0.000983965301456584 0.0006592850146664101; 0.0003697849403054275 -0.001053430877255186 0.0004672126774164019; 0.004497099695039113 0.0043447207228328455 0.004436569237040113; 0.0012309932464212715 0.0050792595711001125 0.007251086632175839] %
+
+Mass Used: 83.03227054587978 kg
+Launch C3: 97.28404147290351 km²/s²
+||V∞_in||: 2.0202362053027004e-6 km/s
diff --git a/archive/ES_0.5575990793541679 b/archive/ES_0.5575990793541679
new file mode 100644
index 0000000..21986fb
--- /dev/null
+++ b/archive/ES_0.5575990793541679
@@ -0,0 +1,22 @@
+archive/ES_0.5575990793541679---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:31:46.770
+Launch V∞: [7.866299707650065, -5.806599621048596, 0.24473821307233304] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8699807523660788e-7, 6.31918440249951e-7, 1.7233241992042047e-6] km/s
+ V∞_out: [1.659114188464839e-6, 2.115941599758495e-7, -7.771407471138303e-7] km/s
+ time of flight: 1.84377765881583e8 seconds
+ arrival date: 2030-03-17T07:34:31.770
+ thrust profile: [0.3948733392241592 -0.005667604717025808 -0.11659195149257616; 0.05677690388031232 0.03455652096938419 -0.0607038649476579; 0.06965291140258127 0.06677076034619257 -0.12855022979825179; 0.03736050086362574 0.04892942745036349 -0.10545408771417819; 0.03419913513926078 0.0563690313614322 -0.13490815275065882; 0.016605031219279247 0.03156740113610145 -0.08151112570539203; 0.00471112381086912 0.010372205512074087 -0.030605583204477874; 0.0033853055505343303 0.008977974178966019 -0.027864445439103065; 0.006522591405330117 0.03019698511435361 -0.08697294494921022; 0.002118748144645064 0.008707115726076981 -0.029236627429956676; 0.0031764319861427716 0.012470203616970349 -0.041569392608162246; 0.00019854624373595359 0.00044878892913051313 -0.0019226202686502226; -6.182320111185229e-6 0.00043545050753648597 0.00017604261334853993; 0.0003013754159167896 0.00032295115033355055 -0.0004630395376385991; 0.00018146330361384726 0.00029431627663472525 0.0009182078914365875; -0.00029930162214552854 -2.0858226831161858e-5 -0.00029071924068786714; 7.542151074300482e-5 -0.00018043198457757701 0.0011864481838927846; -0.00035690244944044274 -0.00013581313129366649 -6.51014523716524e-5; 0.000726410002216889 -0.0004975063583919123 0.0004734731264819775; 0.00018818837102837322 -0.00035596015083531163 0.0010880844451206387] %
+
+Mass Used: 92.54378483092478 kg
+Launch C3: 95.65516704267503 km²/s²
+||V∞_in||: 1.8450299430721822e-6 km/s
diff --git a/archive/ES_0.5576035871325743 b/archive/ES_0.5576035871325743
new file mode 100644
index 0000000..be2c8ab
--- /dev/null
+++ b/archive/ES_0.5576035871325743
@@ -0,0 +1,22 @@
+archive/ES_0.5576035871325743---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:31:57.849
+Launch V∞: [8.093676073492025, -5.680573052439425, 0.1515947475942115] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.394921359851628e-10, -9.863396960462037e-10, -1.2651031664092544e-9] km/s
+ V∞_out: [8.78346598080244e-10, -7.95468704167364e-10, 3.0097773578519894e-10] km/s
+ time of flight: 1.8749577787493423e8 seconds
+ arrival date: 2030-04-23T20:41:34.849
+ thrust profile: [0.2296743438707066 0.0021008507659105455 -0.07714565646109095; 0.07074854109705009 0.04198233477371866 -0.08491973752671965; 0.050970467396824475 0.04872232859693336 -0.1107310914664177; 0.032516846699054774 0.0405079550794211 -0.10460450949701035; 0.020585056126743814 0.031236305751112352 -0.09050262307585089; 0.01865404703273847 0.0343315207740187 -0.10676137873798308; 0.010812376675633515 0.022199810229568632 -0.07660108914342083; 0.005004219223521254 0.011679503275617223 -0.042899440490194195; -0.0003437008712375712 0.00422234125233692 -0.02105536027728279; 0.002676532069041375 0.010350164977165099 -0.044317385023217665; 0.0011232900274555902 0.0022357767975813864 -0.011364922604309222; 0.0010129201681772094 0.0017778511382920683 -0.0029180483242309614; 8.206092536018053e-5 0.0036151015472901706 -0.021821120734809643; -0.0013972452489257466 -0.0034024144437218807 0.0013236250953448016; -0.0009539929075035886 0.0015887918627469036 0.0030588120358297473; 0.0007684507480188335 -0.0006384761867707095 -0.0016736344513372603; 0.0008096303928789098 -0.001060456597130163 -0.0015052586468727795; 0.002935135384271123 0.0022386678767000595 -0.002875559810361144; 0.00030917896450470864 -0.0002110794089483513 0.00282638719576966; 0.0015132989586283964 -0.0006349981375557855 -0.002844105961829785] %
+
+Mass Used: 80.04053092174081 kg
+Launch C3: 97.79948355421642 km²/s²
+||V∞_in||: 1.7664089664738282e-9 km/s
diff --git a/archive/ES_0.5576079396588647 b/archive/ES_0.5576079396588647
new file mode 100644
index 0000000..e609965
--- /dev/null
+++ b/archive/ES_0.5576079396588647
@@ -0,0 +1,22 @@
+archive/ES_0.5576079396588647---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T14:00:08.509
+Launch V∞: [7.919830016241076, -5.666198827471553, 0.3373488693110187] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3298562812930015e-6, -1.860142853866221e-6, -1.9535941259029115e-7] km/s
+ V∞_out: [1.2910526521135372e-7, -6.52734330990238e-7, -2.2290091570667223e-6] km/s
+ time of flight: 1.8749577787647307e8 seconds
+ arrival date: 2030-04-22T16:09:45.509
+ thrust profile: [0.47804436849848353 -0.003665510280434599 -0.10480133523834283; 0.056896958566257136 0.03686877293145449 -0.05925387957427914; 0.04216062253712404 0.044149655920354906 -0.07967444180655212; 0.02936916164387737 0.040692190922008445 -0.08346150806404716; 0.02911174035254889 0.04956924583184787 -0.10759090007010984; 0.01982400761132045 0.04453030103757502 -0.10544544099976581; 0.00948193809903083 0.025762972767339867 -0.0686636826284314; 0.007041277062890843 0.022595761437264824 -0.06269351714673226; 0.003183575826687708 0.01073854878201619 -0.03229570476217034; 0.0032993361862550296 0.014151259217516527 -0.045138856379474054; 0.002914205850961293 0.010357079869108308 -0.03387434361946768; 0.0014045781048638783 0.0024248271442672215 -0.010001883970781108; -0.00030775183549393834 0.00041207767027319063 0.0006080775429369125; -0.00032181210804656246 -0.00010892018513583286 -0.0002155105505354822; 0.0009326389472003821 0.0002761898235967191 -0.000799203278525421; -0.0007118455809047396 0.0008208157537405521 -0.0001370495311541879; 0.0018553199773256395 -0.002046780512322206 -0.0005613878879793989; -0.0006735738179748526 0.0007973092321519508 -0.0011370047285352795; -0.0001708493908363617 0.000926243983455093 -0.0013285655147394983; 0.0013286577156875006 0.0011517822415736192 0.0007409422973813815] %
+
+Mass Used: 96.70655769573386 kg
+Launch C3: 94.94332089821856 km²/s²
+||V∞_in||: 2.294954131518023e-6 km/s
diff --git a/archive/ES_0.5576133352590156 b/archive/ES_0.5576133352590156
new file mode 100644
index 0000000..4e4b9a7
--- /dev/null
+++ b/archive/ES_0.5576133352590156
@@ -0,0 +1,22 @@
+archive/ES_0.5576133352590156---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:23:10.956
+Launch V∞: [7.68614837810369, -5.906843288121089, 0.08654519828023574] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.014473136957586697, 0.08777621981130224, 0.092644538883336] km/s
+ V∞_out: [-0.0231098291517399, 0.02026732843837688, -0.12469377396699283] km/s
+ time of flight: 1.874957778749359e8 seconds
+ arrival date: 2030-04-24T02:32:47.956
+ thrust profile: [0.4846374689665833 0.015545548693498787 -0.13727171765529694; 0.1542835641665641 0.099880835711561 -0.15075327923564258; 0.05321628685114619 0.056141030037822004 -0.10089854122124171; 0.031240000452870696 0.04440265902546069 -0.09049329249598399; 0.023120649144760048 0.041381474155231995 -0.09301788536253033; 0.02529406172840207 0.05543096127918225 -0.12949094812639786; 0.004674468429950924 0.011656522841834365 -0.03322113145086905; 0.008039219055894118 0.022967288226572936 -0.06555942776580848; 0.001020358833554588 0.0038359892350391498 -0.01006664190119005; 0.001150933075532075 0.005340481769552882 -0.013825667423103401; 0.00032451793866683596 0.0018139374449906826 -0.005606942547355567; 1.8863689770770055e-5 0.0005822688827590639 -0.0019321795975920488; 0.00039533811203218015 0.0006303170169667707 -0.00206118646307362; 0.0005599872676565972 0.0010570396301058855 -0.00225282344545102; -0.0008828585187282414 0.00015892272875490048 -0.0010926708004868155; -0.00015351656311825485 0.000239791507376886 -0.0015314559541048747; 0.00023732884642165916 -2.1815496585182812e-5 -0.0007303513722357399; 0.0004183667417936585 -0.00017551263576331142 2.389601470237227e-5; -0.00047353951576721294 -0.0007193704797632912 0.0005455660315774592; -8.406919002639863e-5 0.00017753025217557682 -3.173254278643101e-5] %
+
+Mass Used: 102.36043101556197 kg
+Launch C3: 93.9751645919925 km²/s²
+||V∞_in||: 0.12844122018519236 km/s
diff --git a/archive/ES_0.5576153477242218 b/archive/ES_0.5576153477242218
new file mode 100644
index 0000000..32c685a
--- /dev/null
+++ b/archive/ES_0.5576153477242218
@@ -0,0 +1,22 @@
+archive/ES_0.5576153477242218---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T01:42:41.127
+Launch V∞: [7.843023519776234, -5.698529748673975, 0.0913104881010083] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.241583746226188e-5, 6.067157558886757e-5, 0.0042174265979514946] km/s
+ V∞_out: [-0.0037331700332730116, -0.0012976129885658814, 0.0014710235011925418] km/s
+ time of flight: 1.8749577787793297e8 seconds
+ arrival date: 2030-04-22T03:52:18.127
+ thrust profile: [0.4808331074617398 0.014592186404437628 -0.1266228559794766; 0.12745649660494018 0.08283551901589434 -0.1295346051565931; 0.061836764928113096 0.0661491073635672 -0.11892256670355623; 0.048472677295778664 0.070332051041713 -0.14016997163835312; 0.017306921417328005 0.03195379554472505 -0.07218123416593204; 0.013163901817326415 0.02814511839221439 -0.07006926166235079; 0.00829534526301205 0.0217023524445252 -0.05641004687370481; 0.004800962970769554 0.015446911140240568 -0.04410387604281479; 0.004104598438297986 0.01556247564263435 -0.046145618384627954; 0.00016143833356923004 0.0015126680746071965 -0.005006983209417089; -0.0009495955578624042 0.003441815431151929 -0.012549875304180589; 0.00023797675388162885 0.001175026227137652 -0.002434830112279843; 0.0020950321880270446 0.0010450292412757837 -0.0013508139736476189; -0.00047008808319174247 -0.0013939498359164188 -0.002737265210170637; -0.0005722842614158468 0.0012183949457846345 -0.0035676692905577886; 0.0008094606631977959 -0.0010675135957622355 -0.003130761649006503; 0.0016185981464061842 0.0035711153942747775 -0.004499384496952796; -0.0001722729738826978 1.2148237846780919e-5 -0.0004502144008540843; -0.00031308183776812136 -0.0009058729073000045 0.0017094431744888727; -0.00066945452598815 0.0015386799457808322 0.0011351202514170873] %
+
+Mass Used: 102.24942414937641 kg
+Launch C3: 93.9945968335227 km²/s²
+||V∞_in||: 0.004218668097807382 km/s
diff --git a/archive/ES_0.5576171132116512 b/archive/ES_0.5576171132116512
new file mode 100644
index 0000000..f451d92
--- /dev/null
+++ b/archive/ES_0.5576171132116512
@@ -0,0 +1,22 @@
+archive/ES_0.5576171132116512---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:40:08.474
+Launch V∞: [7.923071248677608, -5.798193375119363, 0.23864061014175458] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.864586455416233e-6, -8.298541190131823e-6, -2.8288628134862213e-5] km/s
+ V∞_out: [-2.733398810055804e-5, -3.0105744252777666e-6, 1.1677420978294566e-5] km/s
+ time of flight: 1.874957778699877e8 seconds
+ arrival date: 2030-04-23T13:49:45.474
+ thrust profile: [0.3135238935310064 0.005773768217986608 -0.0777347368025749; 0.052919491728196495 0.037902676075507416 -0.057176535886480424; 0.07582704501524559 0.10564053137848904 -0.14588569370101398; 0.026925009452612676 0.04678583147291108 -0.08687480769503454; 0.03507064104215869 0.06234911239797104 -0.1325260451975097; 0.00903050298755749 0.024715926736317242 -0.05389196853202462; 0.008293832721090206 0.031782001888084645 -0.07110752875448241; 0.005072607080809175 0.01861935768525753 -0.04704737683854005; 0.004021566330352549 0.021700135818424563 -0.057316391937043444; 0.0034998512459633773 0.01565875268387945 -0.04408141342863005; 0.001033179766165703 0.00418761514989229 -0.012333215308691872; 0.00018362784623293953 -0.0005963335006859477 0.0010616881378114691; 3.092165169384347e-5 -0.00030555042601145867 0.0012679632326046963; -0.0004778777087155243 -0.0009412974782013359 0.0005977698784318811; -5.83113080111235e-5 -0.0004145966295295896 0.0008042209881173416; 0.0007456236243716379 -0.00048421238765989673 5.682938243523777e-5; 0.00015693398702470944 0.00041056755224691863 0.0006395103034247749; -0.0007345271411759007 -0.00031465521506143166 0.000539164912062626; 0.00011691332623753412 -0.0004946230233905214 -9.970029561885859e-6; -0.001104744385335533 -1.647336827121258e-5 0.0006684125378422037] %
+
+Mass Used: 87.92215176862601 kg
+Launch C3: 96.45105376770864 km²/s²
+||V∞_in||: 2.9879365271354938e-5 km/s
diff --git a/archive/ES_0.5576249947114377 b/archive/ES_0.5576249947114377
new file mode 100644
index 0000000..dc0fa7f
--- /dev/null
+++ b/archive/ES_0.5576249947114377
@@ -0,0 +1,22 @@
+archive/ES_0.5576249947114377---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T11:17:28.091
+Launch V∞: [7.88572466022016, -5.614008233908944, 0.18657974448136438] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003119506155758927, 0.000242383576800247, 0.00020357211032180698] km/s
+ V∞_out: [4.0279009340785705e-5, -0.00027959442898431745, 0.00034300363073831464] km/s
+ time of flight: 1.874957778716765e8 seconds
+ arrival date: 2030-04-20T13:27:05.091
+ thrust profile: [0.507262532871372 0.012124578706087135 -0.11852497694348067; 0.08147861489755406 0.05562738578354473 -0.07725549334415757; 0.09562370216818583 0.1098856079900491 -0.1601473557603995; 0.05287819338658793 0.08393108589993878 -0.1388227220415343; 0.034869976314594125 0.0713826006222645 -0.1295653312650901; 0.010230683804331155 0.024711676000202455 -0.050623546904327084; 0.004739024775385061 0.013980350869659843 -0.03232702533677261; 0.008275624816156183 0.03099902952027832 -0.07008104455645775; 0.0018514471671571486 0.005867113116951394 -0.014901816932244781; 0.000751840768086425 0.003467538141321925 -0.009743369172093768; 0.0001284158339670068 0.0005684324985208535 -0.001593196248301962; 0.00011086429296500568 0.001280111768895015 -0.0033170708859118353; 4.539028884180384e-5 0.00034288642727066425 -0.0003910278826220629; -0.00011381293727681657 1.3780584301941812e-6 -0.00047043014935079137; 0.0002506828543874083 -5.620087576201176e-5 0.0001512159877970746; 4.2029699760736505e-5 -5.0493578482927555e-5 -0.0002222511809452729; -2.9133816797549817e-5 -4.235597766913456e-5 -7.741638675358152e-5; -0.0001085015092741494 -0.00013731788274314098 -0.0003654904583861232; -1.2903176402693388e-5 0.00013688372120659105 -4.3273679098602903e-5; -2.096550388468799e-5 -0.0002496583061934789 0.0005546509642177411] %
+
+Mass Used: 103.7659295985377 kg
+Launch C3: 93.7365538682525 km²/s²
+||V∞_in||: 0.00044441488382088824 km/s
diff --git a/archive/ES_0.5576312684967368 b/archive/ES_0.5576312684967368
new file mode 100644
index 0000000..e3b6994
--- /dev/null
+++ b/archive/ES_0.5576312684967368
@@ -0,0 +1,22 @@
+archive/ES_0.5576312684967368---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:22:23.760
+Launch V∞: [7.8745325575435885, -5.983804763449318, 0.02650355358888406] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00032312667896040425, 0.00021561585960987704, 0.013677678834209435] km/s
+ V∞_out: [-0.012930851243710052, -0.004253984757700942, 0.0019383870719968273] km/s
+ time of flight: 1.794331221709176e8 seconds
+ arrival date: 2030-01-19T13:54:25.760
+ thrust profile: [0.21618852866717528 -0.01821559253153798 -0.08129028681567639; 0.07865841758131696 0.033059530550815924 -0.09767074428126178; 0.06630844575209652 0.045085018641906956 -0.1445097015770676; 0.04832886378273081 0.04155052194469047 -0.151676338303486; 0.02707153126190124 0.026945925684811894 -0.11154190532874048; 0.016327052855455514 0.018090858449118834 -0.08341762573581038; 0.015927659766641553 0.01931303275825836 -0.09561360029657819; 0.008066916600719572 0.010721109861008708 -0.05809788728779484; 0.005086846325882985 0.00637827621795661 -0.039821641979414124; 0.0008763663277738872 0.0014425365131525555 -0.008348826839888803; 0.0009450284151922923 0.001272644614246269 -0.007924067115155944; -4.629519496832473e-6 -0.0001709986069281351 0.00025691731536017684; 0.0005340770752570031 0.00042461030286281926 0.0003940825352005716; -0.00022439123129145447 -0.00011033436868894181 -0.0003164417584557999; 0.0002828340500496331 0.00022063907376879734 -0.0011563150779968644; 0.0005328878056307815 -0.0008770635883549327 -0.0004530076575135636; -0.0004073526058855386 0.000857180338856659 -0.0013115472109995648; -0.0005736970332468076 -0.0003459635933370132 0.0005464883224241097; -2.781738633430371e-5 2.861838278291359e-5 -0.0001511705359251625; -7.142733153402797e-5 -0.0001451708304408035 0.0012874022741627524] %
+
+Mass Used: 79.98298474892727 kg
+Launch C3: 97.81488488524555 km²/s²
+||V∞_in||: 0.013683194047493153 km/s
diff --git a/archive/ES_0.557632381502807 b/archive/ES_0.557632381502807
new file mode 100644
index 0000000..4361af8
--- /dev/null
+++ b/archive/ES_0.557632381502807
@@ -0,0 +1,22 @@
+archive/ES_0.557632381502807---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T20:36:39.317
+Launch V∞: [8.031806699766179, -5.902897619082373, 0.3359102411474399] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9906064547302726e-7, -1.4046502159103165e-6, 3.0534822092372925e-5] km/s
+ V∞_out: [1.1571825451712023e-6, -3.068097947811129e-5, 3.2447888829204933e-7] km/s
+ time of flight: 1.874957778248467e8 seconds
+ arrival date: 2030-04-26T22:46:16.317
+ thrust profile: [0.16774605254132952 -0.0035155541840472663 -0.06411466602553037; 0.04140150225788928 0.01998477035372461 -0.054083209326539095; 0.03970524887459274 0.031038726621404274 -0.09202790900329569; 0.037991942538690544 0.03541315183256016 -0.12529738920099553; 0.03227366353259479 0.038311411547671766 -0.1420750986318413; 0.01954730655212704 0.025994542786902258 -0.11591507945164975; 0.012866120399415358 0.01580659508779187 -0.07907587965535207; 0.0031312408467692506 0.004046028757445238 -0.022900869101645103; 0.0022637284771185916 0.003087649562773442 -0.01878122134433985; 0.004803385858604612 0.006856397185595012 -0.04671826780206441; -0.0001937649918919692 0.0003866497645025056 -0.0010654202445994846; -0.00010560134691552076 -7.016615723702053e-5 -0.0017276619207995743; 5.986040485350559e-6 2.237978421048214e-6 -0.00035326941717909587; -5.546869395442407e-5 5.6830040883864636e-5 -0.0016582546132263049; -5.0827829091176186e-5 -0.00012634933739359404 -0.0008408320822295553; 4.5858489901442974e-5 0.0001456438540316185 -0.00011026485404299792; -0.0008891445498887264 -0.00048709527293312884 -0.00020280827619162953; -5.5728551465276045e-5 -0.0003314626629858262 -0.00022672297385927296; -2.7176629227051162e-5 0.00026929502122137927 -0.00031985864570352934; -0.0003335434461206681 0.0002884828723117704 0.00023647590893706785] %
+
+Mass Used: 70.34720843894593 kg
+Launch C3: 99.46695485388496 km²/s²
+||V∞_in||: 3.056776124583707e-5 km/s
diff --git a/archive/ES_0.5576431698223736 b/archive/ES_0.5576431698223736
new file mode 100644
index 0000000..ac65ab1
--- /dev/null
+++ b/archive/ES_0.5576431698223736
@@ -0,0 +1,22 @@
+archive/ES_0.5576431698223736---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T07:49:21.268
+Launch V∞: [8.142377340248155, -5.818755510349371, -0.055525696527998734] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.429957568350663e-6, -0.0004298904081971565, -7.891269323405533e-6] km/s
+ V∞_out: [-0.00040886842061043597, 7.40076078611763e-5, -0.00010992817318375688] km/s
+ time of flight: 1.8569249245861363e8 seconds
+ arrival date: 2030-04-04T13:04:13.268
+ thrust profile: [0.07837545938953132 -0.003342206535622957 -0.030018351296330098; 0.027932793486678032 0.0130198522292808 -0.03574333576606204; 0.051684380710892125 0.038633272443907365 -0.11843150512282903; 0.033129724442282564 0.03098269376566853 -0.11066699061606709; 0.027531928293801043 0.030035952464032817 -0.1212215775711302; 0.01916669565749521 0.02288229820648456 -0.10285149738189557; 0.01124085911200421 0.014602630206589175 -0.0720828910094066; 0.011105808153887616 0.015659303716460387 -0.0822437428217222; 0.008209752650038992 0.012071890910931336 -0.06849607005545906; -0.0003208199634808764 0.00040129954896899215 -0.008922143772919876; -0.0014808813918321159 0.0010503887701838633 -0.0036983859295462405; -0.00018104000946369528 -0.000549031370252595 -0.002891690090338354; -0.001303190196321866 -0.002579564279976857 -0.0056485647429338915; -0.0033713402580678384 0.0027405040535062866 -0.003349121765749015; -0.0007013765363729454 0.001476969612336552 -0.0017932445657259564; 0.004842132976546679 -0.0020256354962669993 -0.0011278988583584533; 0.0005402012813809339 -0.00045892501716782164 -0.0028034061562136276; 0.0025557843644511426 0.002373105728596974 -0.003093421355028935; -0.0016421222811264812 0.001461196032446705 -0.002708835201782756; -0.00011337517022500052 0.0004906619200658723 -0.0005417516453999453] %
+
+Mass Used: 66.32107079087018 kg
+Launch C3: 100.1593075431827 km²/s²
+||V∞_in||: 0.00043001090631027394 km/s
diff --git a/archive/ES_0.5576448860187597 b/archive/ES_0.5576448860187597
new file mode 100644
index 0000000..bd92eb9
--- /dev/null
+++ b/archive/ES_0.5576448860187597
@@ -0,0 +1,22 @@
+archive/ES_0.5576448860187597---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:02:15.443
+Launch V∞: [7.96155801280001, -5.735995708590061, 0.13128394938992288] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3277807297082063e-9, -1.4113583484019252e-9, -8.631068040156442e-10] km/s
+ V∞_out: [9.555462318669321e-11, -3.1835948573711575e-10, 5.207181822679176e-11] km/s
+ time of flight: 1.8244839298508394e8 seconds
+ arrival date: 2030-02-21T19:08:47.443
+ thrust profile: [0.3527654760215401 -0.013661569215016519 -0.1125357372049362; 0.06944888192842404 0.03733560324701295 -0.0790073538751697; 0.05929980943194743 0.05173243744132385 -0.11863145630287285; 0.03311191670661908 0.038662399891528615 -0.10125718553446719; 0.025689827239763655 0.03700252814409679 -0.10518930703183102; 0.01873655477928121 0.031051725493365778 -0.09644107312722307; 0.01068855068263239 0.02032688752239157 -0.06790702683291894; 0.008548404827947675 0.019359474778227376 -0.0688560412180403; 0.0075555032013184375 0.01732444912503638 -0.06619766673074608; 0.0030588883617899375 0.006847413942449294 -0.026855615559075643; 0.002391808697001963 0.00482323019576581 -0.02224194363826603; 0.0001229413284365671 0.0003919937666122732 -0.0012806474544276314; 7.828927979438882e-5 7.10831843641896e-5 7.825415553126456e-6; -4.825365484027604e-5 -0.00019020630916311262 -0.00013999547189914803; -0.00012776872019995848 -0.00014639343526584537 -3.7598560273495216e-5; -0.00012479238784201003 -0.0001339219873902093 -3.2970485901594274e-5; 0.0001011085629179829 -0.0003415218684562596 0.0004987362641260243; -0.00014929150821901935 0.00017666660208701362 1.0268475426592914e-6; -0.0002545086489590285 -9.158454449557707e-7 0.0004200600928994458; 0.00011994166995725594 -0.0002456585808588632 0.00018123056171645942] %
+
+Mass Used: 88.80485231473858 kg
+Launch C3: 96.30528823551106 km²/s²
+||V∞_in||: 2.121293805423088e-9 km/s
diff --git a/archive/ES_0.5576493082063702 b/archive/ES_0.5576493082063702
new file mode 100644
index 0000000..d600338
--- /dev/null
+++ b/archive/ES_0.5576493082063702
@@ -0,0 +1,22 @@
+archive/ES_0.5576493082063702---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:44:16.522
+Launch V∞: [8.131682320452056, -5.606457329448412, 0.16110317763518164] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6560937548049559e-9, 1.00608460030153e-9, -1.8932057163852388e-12] km/s
+ V∞_out: [1.8339632877085886e-9, -8.76567765017007e-10, -7.459430019083828e-10] km/s
+ time of flight: 1.8749577787202218e8 seconds
+ arrival date: 2030-04-23T13:53:53.522
+ thrust profile: [0.2894778427143901 -0.0008471921672279938 -0.09542241738551814; 0.03190879870587467 0.01690341556778817 -0.03935427132064095; 0.045033416392977976 0.038356408731395474 -0.09494038637411858; 0.03346907077849343 0.036688443221108695 -0.1035327511715648; 0.023421360230230448 0.030286068144700362 -0.09691538550231661; 0.017762768432853095 0.02668363112381253 -0.09374141323544684; 0.008489262889286817 0.014136950609411746 -0.05708204745967181; 0.00997699720474456 0.020093383197684347 -0.08003498076010898; 0.004247922334677326 0.008627595859171956 -0.03900934901617289; 0.0014573561451330594 0.0032287285524275457 -0.015881032077028196; 0.0017594766448349676 0.0035613234809392883 -0.01884702433908624; -0.0006498672719153911 0.008013058784085703 -0.06774017592233161; -0.000555425983807084 0.0007412843812203818 -0.0010759198697870267; 0.0007182012907446854 0.001087709338031349 0.0013556400435807523; 0.0012121425119230183 0.00011740187374131533 -0.0012868001089560628; 6.035599677226309e-5 0.0007454814653025273 -0.0007927601685525183; 0.0005353860973859689 -0.0008745424130444712 0.001953315401561315; 0.0001769564401861341 0.0002549898856826495 -0.0017633628965056727; -0.0015488148772625366 -0.00037038555764222166 4.5705590273243475e-5; -0.0025328931742004727 -0.002201063876255884 -7.978247366747886e-5] %
+
+Mass Used: 81.35916984855066 kg
+Launch C3: 97.58257538152249 km²/s²
+||V∞_in||: 1.9377451669132734e-9 km/s
diff --git a/archive/ES_0.5576511895378019 b/archive/ES_0.5576511895378019
new file mode 100644
index 0000000..0da8559
--- /dev/null
+++ b/archive/ES_0.5576511895378019
@@ -0,0 +1,22 @@
+archive/ES_0.5576511895378019---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T15:02:52.196
+Launch V∞: [7.984057121394839, -5.841382771449229, 0.21077882489181002] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.1732638815417596e-6, -4.652722953665783e-6, 3.3870452560838806e-6] km/s
+ V∞_out: [-1.0380111711952864e-6, -7.658939386643775e-6, 3.8217937101108384e-7] km/s
+ time of flight: 1.847230460818349e8 seconds
+ arrival date: 2030-03-22T15:00:18.196
+ thrust profile: [0.19337084376254807 1.382951597821576e-5 -0.06956482008389352; 0.08915236832628812 0.04790939621687941 -0.09788571515321114; 0.05708799629821752 0.04970948561551066 -0.11358429992553656; 0.04292921464381876 0.049597636997160126 -0.12991844486456458; 0.03007442833946195 0.04112348171906428 -0.11824821420014778; 0.01794306594178314 0.029099053556733243 -0.09258795268966943; 0.010687285988204598 0.019999549662776697 -0.06893167413981878; 0.0076456873394935634 0.01579513782155667 -0.05771511177461579; 0.002360093611101466 0.006416128829732105 -0.0266029839978327; 0.0023343307147531537 0.005364259487314003 -0.022101353888107925; 0.000645271418787772 0.0004536500716545638 -0.005233417567774772; 0.0011575404130020708 0.0008515639405218493 -0.0023209217741274133; -0.0008657194589243248 -0.0005115484236234224 -0.0015528956604295417; 0.003619954931261953 0.003701458244128666 -0.002882664405848054; 0.0009196366183866795 0.004302689651899933 0.0011321370763737143; 0.0031674020744446077 0.0013046865667030146 -0.003488164724443143; 0.004531636783708794 -0.002480483135972399 -0.004555770019464182; 0.00035155804922839715 0.0010026658527464822 -0.0044917566300431274; 0.0018646386723778522 0.0006683944108501431 -0.0014858254416819185; -0.0004482302427180388 0.0010927163562955476 -0.0013998281726499725] %
+
+Mass Used: 79.44352146650544 kg
+Launch C3: 97.9113485133023 km²/s²
+||V∞_in||: 7.738382624191782e-6 km/s
diff --git a/archive/ES_0.5576522867956324 b/archive/ES_0.5576522867956324
new file mode 100644
index 0000000..197d156
--- /dev/null
+++ b/archive/ES_0.5576522867956324
@@ -0,0 +1,22 @@
+archive/ES_0.5576522867956324---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T19:37:39.975
+Launch V∞: [7.927685628880574, -5.975696598137113, 3.802075640828754e-5] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.410142133751053e-8, 3.115579523656423e-7, -5.674166513089471e-8] km/s
+ V∞_out: [4.9768472317796476e-8, -1.7781222504512703e-7, -2.52907054203811e-7] km/s
+ time of flight: 1.8258567200862113e8 seconds
+ arrival date: 2030-02-27T01:52:11.975
+ thrust profile: [0.2126169584719164 -0.013145982236779338 -0.07967964967778252; 0.04198572754370985 0.018280219466120722 -0.05392973347179501; 0.03179957685783152 0.02160973675625763 -0.0715477403960559; 0.05873280458798984 0.05246737810668985 -0.18641831676369494; 0.02181485172297635 0.021567148567830426 -0.09158620854006633; 0.020938821862680954 0.023082906829004598 -0.1072359457530621; 0.013042586514669477 0.016795392117189327 -0.08320105824281476; 0.00844747880187101 0.01069005798294164 -0.06077330477060776; 0.0039052070229655734 0.005067537405663104 -0.03321873599922343; 0.006955768734342887 0.006600063016845801 -0.05825166587809925; 0.0006132041885275086 0.0008915185601143462 -0.006119606486699809; 2.965945258556425e-5 2.105114520417909e-5 -0.0009352130025497457; -6.1512101057947035e-6 9.874767385713868e-5 -0.0006738316876900858; -3.653303471602015e-6 -0.00013878393670557293 -0.000427092485809253; 1.0214001419130639e-5 1.1534434408194856e-5 8.2365401161178e-5; -0.00021991319954239792 -0.00012151993544487897 4.946523628613785e-5; 0.0003375365351434373 -0.00026313278214021307 -0.0004376945445034123; 0.0002527466882557998 9.104082183268147e-5 0.00026250014890216716; -6.820720944715204e-5 7.139215407458248e-5 -8.421568143617629e-5; -4.67748697581858e-7 -1.2592397814295358e-5 -0.00010030039906399265] %
+
+Mass Used: 75.67763055028081 kg
+Launch C3: 98.55714926479263 km²/s²
+||V∞_in||: 3.1851354944701626e-7 km/s
diff --git a/archive/ES_0.5576629973748468 b/archive/ES_0.5576629973748468
new file mode 100644
index 0000000..a07317d
--- /dev/null
+++ b/archive/ES_0.5576629973748468
@@ -0,0 +1,22 @@
+archive/ES_0.5576629973748468---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:02:36.943
+Launch V∞: [7.846989159372626, -5.627713198806423, 0.2337400568112146] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.2551424275793233e-6, 2.7193106938864777e-6, -1.9910353588926895e-6] km/s
+ V∞_out: [6.449094029918684e-7, 4.634160002402818e-6, -2.2791659653107884e-7] km/s
+ time of flight: 1.8749577787523264e8 seconds
+ arrival date: 2030-04-21T12:12:13.943
+ thrust profile: [0.5773141584401116 0.012808659431043468 -0.15597216642515077; 0.11011881825148953 0.07239371861473862 -0.11564231588454173; 0.05172610718284023 0.05669064574205897 -0.10261188501570015; 0.03209064298934267 0.04834866428397307 -0.09693434203907474; 0.01453185587302019 0.027571236249438802 -0.06520666767387989; 0.01708155422906417 0.03739718469731061 -0.0898467209114527; 0.007776235469261496 0.027310728524370272 -0.06717078155647997; 0.007238055988313509 0.02257671004930182 -0.05936129287880258; 0.003012120381267578 0.013700689562396208 -0.03707957407834843; 0.0015733446922093128 0.011384064692633656 -0.03869350556644823; 0.000497674856448249 0.0029808619384750876 -0.00866785096843618; 0.00023302498324617336 -3.243398661525196e-5 -0.00051854947077527; -0.001042413733065299 -4.0593064574573454e-5 -0.0010156501459970236; -1.8271461379554562e-5 0.0005078944670162988 -0.0011711828321631188; 0.0004067274437097643 0.0008033258542761549 -0.0006743599617060389; 0.00018129176777914813 0.000891724373758772 -0.0009548131085774015; -0.0021523752818798318 -0.0007981581830039336 -0.0016867227169307514; 0.0005733847023280465 -0.0008143279137439376 0.0007172944287520847; -0.0002812786533466793 0.0012589786053540351 0.0015311732934620331; 0.00022254944671193567 0.0007800010054224141 -0.0005105923890850842] %
+
+Mass Used: 106.35082701529836 kg
+Launch C3: 93.30102912948965 km²/s²
+||V∞_in||: 4.685597579185958e-6 km/s
diff --git a/archive/ES_0.5576632502484128 b/archive/ES_0.5576632502484128
new file mode 100644
index 0000000..6a74aa5
--- /dev/null
+++ b/archive/ES_0.5576632502484128
@@ -0,0 +1,22 @@
+archive/ES_0.5576632502484128---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T22:32:34.104
+Launch V∞: [8.032582797963453, -5.576715261988075, 0.21167536030378012] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.213560752197847e-6, 3.5972346384590674e-6, -2.568649363444519e-6] km/s
+ V∞_out: [8.154476091965734e-7, 6.0505069308051e-6, -2.848338261281613e-7] km/s
+ time of flight: 1.8588253555672488e8 seconds
+ arrival date: 2030-04-02T08:34:49.104
+ thrust profile: [0.41799636714334376 -0.0031178825691014736 -0.09916919142604985; 0.07556720290822398 0.05339447352059037 -0.08673592228053717; 0.03738487420899625 0.03632872092806188 -0.07324845406761685; 0.029609203918701615 0.04220564529152732 -0.09311321009711185; 0.025749960381502054 0.041505967064415436 -0.1014008344059862; 0.00958653979130884 0.019425847122622415 -0.05205909449530451; 0.03657627939367312 0.06533120928104923 -0.18201383654900521; 0.006218827503092788 0.015421415493583892 -0.04872245053787578; 0.003455179764229448 0.0109802365854813 -0.037692810196341846; 0.0017334637311703035 0.006023845213050861 -0.02156548805965442; 0.0010145666380626346 0.002725266868732829 -0.010493309481053379; 2.1438164985233676e-5 3.8834436913606004e-5 -0.0004807278187117349; 7.765806081666677e-5 0.00043030743829324924 -0.0015380489371978842; 0.00013146110931788423 0.0004682456513887107 -0.001199958184044489; 0.00017245105700224893 -0.000423002879868783 -0.0007562727463255711; 0.0004916673516169834 0.0001379878213464076 -0.0003815279837050111; -0.00028812541242772465 -0.00014226929567958484 0.00038858801153515915; -0.00031708810836053125 0.0007670397884124648 -8.37859674477887e-6; 2.1934686253651613e-5 0.00013123881199878884 3.613426287995473e-5; 0.0008027512195189872 -0.00020497445192936602 -0.0009496987190778444] %
+
+Mass Used: 92.54994042054659 kg
+Launch C3: 95.66694597758885 km²/s²
+||V∞_in||: 6.10672996037288e-6 km/s
diff --git a/archive/ES_0.557663496624229 b/archive/ES_0.557663496624229
new file mode 100644
index 0000000..87a06cd
--- /dev/null
+++ b/archive/ES_0.557663496624229
@@ -0,0 +1,22 @@
+archive/ES_0.557663496624229---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:53:50.149
+Launch V∞: [7.909964217649616, -5.6588170290751245, 0.2611209644804135] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.821259079336458e-7, -8.193416904376167e-6, 0.00016105046239357792] km/s
+ V∞_out: [5.830176981530154e-6, -0.0001620177432126763, 1.7006127910586642e-6] km/s
+ time of flight: 1.8749577784939054e8 seconds
+ arrival date: 2030-04-22T19:03:27.149
+ thrust profile: [0.4949955753285194 0.003485901640645004 -0.14365329396364207; 0.06963309456904043 0.04122024158216983 -0.07880238316574512; 0.05052998756247732 0.050335929455290626 -0.10390994831358481; 0.03660833625407815 0.049213526939748696 -0.11181479108674693; 0.023935778354278556 0.03764201642338385 -0.10027963324463897; 0.015367423993420507 0.03145272522874196 -0.092235042159731; 0.010555138063452088 0.02617406551769302 -0.08538526389782587; 0.006088957836169227 0.01717756840635243 -0.060205239255356216; 0.0018647389695125576 0.005721304970307222 -0.01946617509976584; 0.0011825415257560416 0.0009555311396580463 -0.0035995527009069768; 0.0016873103643730769 -0.00010028585002022151 -0.0025664511348777825; 0.0004776719955281798 0.0008799726217489922 -0.004241513917881447; 0.0006999500468909852 0.0015048694688448746 -0.0036773672258672506; 6.93853730096608e-5 2.563452873183996e-5 -0.00041452863875013997; -0.00042258533455400636 0.002052057459219478 -0.0022855341013850077; -0.00037684417584626543 -0.0005235542455534284 -0.011327909377304497; 0.0001647628103930428 -0.0008777315124350795 0.0011919086464772094; 0.0021046363218153855 -0.0073264456331309305 -0.005637739473116395; 0.003368238295036586 -0.004416150534891259 0.0030459204777145074; 0.0017510701341312547 0.0031446825852877508 -0.006429245161881885] %
+
+Mass Used: 98.43616459662235 kg
+Launch C3: 94.65792825113911 km²/s²
+||V∞_in||: 0.00016126173783341543 km/s
diff --git a/archive/ES_0.5576654810376426 b/archive/ES_0.5576654810376426
new file mode 100644
index 0000000..a4a0536
--- /dev/null
+++ b/archive/ES_0.5576654810376426
@@ -0,0 +1,22 @@
+archive/ES_0.5576654810376426---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:41:44.831
+Launch V∞: [7.878118399651701, -5.804922661746805, 0.10089448697717873] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.427183411938258e-8, -6.284508763122601e-7, 1.2849752626563746e-5] km/s
+ V∞_out: [4.902549433942204e-7, -1.2870816225324505e-5, 1.046279157760299e-7] km/s
+ time of flight: 1.8749577787448767e8 seconds
+ arrival date: 2030-04-23T18:51:21.831
+ thrust profile: [0.33522167566139816 -0.003955632905624646 -0.084891427798198; 0.14056509270190837 0.08347921727906017 -0.13096285405647856; 0.05395085902085666 0.061131950476003095 -0.10767813633600819; 0.030207111693920253 0.04533317158819511 -0.09231789618028863; 0.015066070606202908 0.02796240795941392 -0.0635044511277502; 0.012728513184644045 0.029747584485886353 -0.07397983352802803; 0.01602514383657347 0.0436092784142733 -0.10983204641738217; 0.006239737593405621 0.019059820005100363 -0.053391470217938206; 0.002822742321743708 0.011681293690718358 -0.036495312692151914; 0.0013212071932673427 0.005812733235165244 -0.018609467850493458; 0.0019278087655428505 0.008569669630617277 -0.03061010179422714; 0.00011440110212960155 0.0011197633256165005 -0.0026851560449536595; -0.0015898785042691263 -0.00012357322512607965 -0.0009866072920528344; 0.0005877116486164952 7.531307439387634e-5 -0.0010065640405695785; -0.00016126564648233366 -0.0009601641480170139 -0.0009815924267548549; -0.0011518063893062153 -0.0008758032127632679 0.0001310578131416551; 0.00032040432026970755 0.0010079458651333435 -0.0018955095469099053; 0.001616078058636618 -0.0012733304719137624 -0.0006212313089514233; -0.00044773991372455647 0.00108392527666934 -0.0014812856840314438; 0.00014540181366042568 0.00012728320156313555 0.001035638759132343] %
+
+Mass Used: 91.93939931303066 kg
+Launch C3: 95.77205632529468 km²/s²
+||V∞_in||: 1.2865387472200182e-5 km/s
diff --git a/archive/ES_0.5576691733841008 b/archive/ES_0.5576691733841008
new file mode 100644
index 0000000..ded5630
--- /dev/null
+++ b/archive/ES_0.5576691733841008
@@ -0,0 +1,22 @@
+archive/ES_0.5576691733841008---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T04:08:59.487
+Launch V∞: [8.002832124427638, -5.685707147911055, 0.30814458654234916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.709825071435678e-7, 4.084571078020627e-6, -0.00010157399662188578] km/s
+ V∞_out: [-3.4274495093625084e-6, 0.00010153794504693486, -6.845229197690587e-7] km/s
+ time of flight: 1.8526484742843738e8 seconds
+ arrival date: 2030-03-27T10:36:26.487
+ thrust profile: [0.3415396866806487 -0.0064786512667533575 -0.10616394058833628; 0.05835319920554517 0.03128358037909735 -0.06414053630116456; 0.06440935095502028 0.05635270612494935 -0.12429465641784024; 0.033168837082237126 0.037984205786681165 -0.09611318308323852; 0.04127976456141306 0.05734617992051883 -0.15698674314734562; 0.021751309312935008 0.03515938888182442 -0.10749093239481458; 0.0041061825149676205 0.006430131187442243 -0.02671486366289639; 0.005318278260961963 0.009600155409203833 -0.034654006232894906; 0.004358856168543918 0.01010441224293396 -0.039389677907283434; 0.004947463250452997 0.009193558804568498 -0.03786564966901658; -0.000322178125474421 0.003232032857427457 -0.014861378821050417; 0.0017241414250602455 0.0043346841203340345 -0.009867906370348355; 0.0003646888190628919 -0.000601774914793476 -0.0009357895929485598; 0.0007769923934053033 0.0025441596457878753 -0.002883653606317184; -0.001961057963556459 0.002776526028858742 -0.0011463475671195968; -0.005658610567704112 0.00110406823640562 0.0019268263162207566; 0.0007171200015483924 -0.00026516544916165355 6.906833365234732e-5; -0.0021418321849213454 0.0013282368407316703 0.002529360906583699; 0.0016915744434830592 0.0029982890833736876 -0.0023274410291236848; 4.465129617401239e-5 0.0009256632138761412 -0.0003388897488687801] %
+
+Mass Used: 87.88671387432396 kg
+Launch C3: 96.4675408697932 km²/s²
+||V∞_in||: 0.00010165830378360224 km/s
diff --git a/archive/ES_0.5576858140958981 b/archive/ES_0.5576858140958981
new file mode 100644
index 0000000..6edfb75
--- /dev/null
+++ b/archive/ES_0.5576858140958981
@@ -0,0 +1,22 @@
+archive/ES_0.5576858140958981---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:28:26.047
+Launch V∞: [7.734146365209024, -5.745041087838803, 0.112168833814958] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.906968921431473e-6, -2.3527657175292243e-6, -2.2990515441843843e-7] km/s
+ V∞_out: [2.200107172224988e-7, -1.090971079695687e-6, -2.8251871582298694e-6] km/s
+ time of flight: 1.8594205475985512e8 seconds
+ arrival date: 2030-04-04T19:02:40.047
+ thrust profile: [0.6604946466180579 -0.011949245965345363 -0.21109373205868517; 0.06457323840790961 0.03448296076983811 -0.07658355358122404; 0.06145963838245607 0.053618163767753475 -0.1307023412006972; 0.029743848271905318 0.033242613339952355 -0.09445666209788235; 0.01806018555401391 0.024149666200781385 -0.07692968676626377; 0.01668662994479152 0.02623494469180659 -0.09065208753970713; 0.021959688753683638 0.04002723537030553 -0.14349175150618038; 0.0022760092089162158 0.004346657885158977 -0.01793305070929878; 0.0020041946115747387 0.004166791343481433 -0.01813967883948824; -6.599991460951807e-5 0.0008162004176454915 -0.005090402017033416; 0.0007269613721393635 0.0023783621799641167 -0.010644090590192092; 0.0002934726011502921 0.00043713907156388195 0.0003354116536025063; -0.0006718788189169297 -0.000223880038767023 -0.0028134033536756867; -0.0012428128396402734 -0.0002471055748124482 -0.001651536593786867; -0.0017084372400470343 -0.0004613022193778884 -0.0021182041950477304; 0.000425142220449759 -0.0007455086765451422 0.0006785245917356191; -0.003718447995479515 0.006214036099242568 -0.0029137838287563245; -0.00031369295778649526 0.0005846285523204132 -0.0009580453422613332; 0.00046442715671888874 0.00698820932719592 -0.003029459788570917; 0.0047298016047101704 0.0002691411582306331 -0.005120863771332723] %
+
+Mass Used: 109.09537258939781 kg
+Launch C3: 92.83509894671143 km²/s²
+||V∞_in||: 3.0372509558669143e-6 km/s
diff --git a/archive/ES_0.5576861474866436 b/archive/ES_0.5576861474866436
new file mode 100644
index 0000000..119a6da
--- /dev/null
+++ b/archive/ES_0.5576861474866436
@@ -0,0 +1,22 @@
+archive/ES_0.5576861474866436---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T01:38:46.689
+Launch V∞: [7.820132201197437, -5.871109177337732, 0.3255432328679261] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6700478048868742e-9, 1.146483439235807e-9, 2.470922714547603e-10] km/s
+ V∞_out: [1.2819708473662045e-9, -1.202312056451759e-9, -8.854261697989127e-10] km/s
+ time of flight: 1.858826285458765e8 seconds
+ arrival date: 2030-04-04T11:42:34.689
+ thrust profile: [0.3062098409073693 0.003274468166572498 -0.08503255397566759; 0.1574239785159885 0.09584116510097948 -0.148971650798856; 0.051404813239262326 0.05168477413901896 -0.09414211409579708; 0.08118917090600318 0.1078191617963958 -0.20399784392025205; 0.020138546622632685 0.03350011730045913 -0.07595162209734801; 0.01411600780407973 0.028086691694800107 -0.06910388891764452; 0.009704604777367688 0.021929673439466422 -0.058198897620719725; 0.006611422957643372 0.018151324363660775 -0.04940207233498319; 0.0009877031948418318 0.0028396880268616396 -0.007556671791085172; 0.0004719359495715898 0.0014133750354258649 -0.004526841335316395; -0.0003835017760708895 0.0008473741026070061 -0.004147046491474717; 0.0009947660848207637 0.001093550181774485 -0.0041801568801304295; -0.00020163542941286283 0.0007259808569538763 -0.0014712934421724918; -0.0013688902713692302 0.000764872498227209 -0.0037506529830593415; 0.00018188251427430632 -0.0030777389280724435 -0.004742639517286062; -0.001464120330407802 0.00012911936783540923 -0.0012986028950974825; 9.691541193145449e-5 0.0005525244086103205 -0.003527434743392052; -0.0004114858829888272 -0.0037391270020575504 -0.0051971701679836; 5.792662253604997e-5 0.000471574633868013 -0.0012309446111108038; 0.00182676642121624 -0.00186552706332168 0.0026710317649180568] %
+
+Mass Used: 92.20668615922295 kg
+Launch C3: 95.73036901289049 km²/s²
+||V∞_in||: 2.0407201027240617e-9 km/s
diff --git a/archive/ES_0.557688298796874 b/archive/ES_0.557688298796874
new file mode 100644
index 0000000..c01c339
--- /dev/null
+++ b/archive/ES_0.557688298796874
@@ -0,0 +1,22 @@
+archive/ES_0.557688298796874---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T04:00:32.762
+Launch V∞: [8.129608484090797, -5.637957671124905, 0.18251743821014174] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.582768715442972e-5, 5.710133141322863e-5, 0.003894282479005268] km/s
+ V∞_out: [-0.003461405688169409, -0.001192552203878592, 0.0013299823438201702] km/s
+ time of flight: 1.8749577787493318e8 seconds
+ arrival date: 2030-04-24T06:10:09.762
+ thrust profile: [0.27876786134558856 -0.0070172914766467925 -0.09862171268490667; 0.025974756388608 0.013547843235087755 -0.03284372673629178; 0.031144984061809947 0.024450372890820946 -0.06953091132640263; 0.030103718901765684 0.030302427073461282 -0.09831294855369568; 0.02375192151992043 0.02808224460505071 -0.10232677499736793; 0.017871737220561762 0.023615542781884984 -0.09602413146514818; 0.015363398152840175 0.02359328036055325 -0.10169905344614191; 0.01272153371745894 0.02089769801381978 -0.09669368225785419; 0.0025961475098341164 0.004030994448440325 -0.020747574494123698; 0.004000196794561058 0.0024248306899880188 -0.024331761510322597; -0.0006682831329823524 0.0034327763003448083 -0.02014553221826094; 0.00020623844665042517 0.0008403222685073317 -0.003909779698929991; -0.0010196687275999304 0.0037028615085782555 -0.009895208596754114; -0.00047329335177814417 0.002554319788801199 -0.00824263133767269; 0.0002957069171732842 0.00032363416416368346 -0.003902519599750911; 0.0014016089898495666 -0.001002126238837511 0.00017769220310354008; -0.0019327081145906057 0.011919249544734367 -0.014459160003928552; -8.956665642887373e-5 0.0001534435488660485 -0.00021821118554098736; 0.0023643906260313284 -0.003614959893589635 -0.007228975470813908; 2.1817284930493707e-5 0.00013793191443858387 -0.00023161503907243182] %
+
+Mass Used: 79.49227030573957 kg
+Launch C3: 97.91041342124802 km²/s²
+||V∞_in||: 0.003895439182746378 km/s
diff --git a/archive/ES_0.5576964642191039 b/archive/ES_0.5576964642191039
new file mode 100644
index 0000000..f3cad07
--- /dev/null
+++ b/archive/ES_0.5576964642191039
@@ -0,0 +1,22 @@
+archive/ES_0.5576964642191039---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:22:13.275
+Launch V∞: [7.89873869024259, -5.780438413935151, 0.1266807299282805] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.02006205114251868, 0.0935148389289965, 0.14683729627597508] km/s
+ V∞_out: [-0.07416813936061475, 0.0605146795907285, -0.14679053734435743] km/s
+ time of flight: 1.8749577787491813e8 seconds
+ arrival date: 2030-04-23T21:31:50.275
+ thrust profile: [0.35701794744888476 -0.0007577487782631381 -0.10852277668630451; 0.12778523209493114 0.0767470519875878 -0.1345205656368859; 0.04471064866294925 0.045617241657842734 -0.09036345084958959; 0.028070969727525406 0.03900114802664597 -0.08771793993022232; 0.014930767016949046 0.027439257154610465 -0.07031893478865014; 0.008476688262548623 0.020972695737277915 -0.05768229929023865; 0.004958523732066082 0.01106053994219801 -0.03278765651989612; 0.009990450570768526 0.028197885378544688 -0.07504998512800282; 0.014693775159767412 0.04639042818536019 -0.12973606159047885; 0.0017501564741872317 0.006218077772060566 -0.02247634742601905; 0.00021281220025204405 0.0033100181244061556 -0.009943569302211906; -0.0008234958101453959 -0.0001239012141518433 9.015632958648306e-5; -0.00015573090827271586 0.0012116214532568385 -0.009883687644515766; 0.000419399092963918 0.00024025082878187997 -0.000967001752395101; 9.742083566031831e-5 -6.337508820070039e-5 -0.00034116582279223863; 6.980848068521671e-5 -0.00036184075363985434 0.0009403831989074023; 0.00023648521786078487 0.001354742112659993 0.0006594592496115559; -7.31225835332838e-5 9.069025256880792e-5 -0.0005953466741687723; 0.00031541447096823823 -0.0004658611976751556 -0.0001851872545876967; -0.00010811152716439251 -0.0005291697626929124 0.00014699116953523054] %
+
+Mass Used: 91.69827148097738 kg
+Launch C3: 95.81958916136752 km²/s²
+||V∞_in||: 0.17523898702514712 km/s
diff --git a/archive/ES_0.5576994381586479 b/archive/ES_0.5576994381586479
new file mode 100644
index 0000000..57acac3
--- /dev/null
+++ b/archive/ES_0.5576994381586479
@@ -0,0 +1,22 @@
+archive/ES_0.5576994381586479---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T22:17:06.385
+Launch V∞: [8.091173131422547, -5.549563363753686, 0.1892945526860599] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.5909859867006804e-6, 0.00010660673362173171, 1.6854571339484364e-6] km/s
+ V∞_out: [0.000102801946899946, -1.645467516456617e-5, 2.2993874240062438e-5] km/s
+ time of flight: 1.8749577787494847e8 seconds
+ arrival date: 2030-04-22T00:26:43.385
+ thrust profile: [0.3920911794640392 0.008470880988484164 -0.11473640395469434; 0.047433163982067504 0.030162469481467422 -0.05378199355284062; 0.03540149027152537 0.03696170162240545 -0.07331655296900626; 0.019232604305431708 0.026258629547848793 -0.059579294922213206; 0.017175401469800556 0.03005565378504363 -0.07350078558814839; 0.013952554474711304 0.0322984924470789 -0.08460015585649171; 0.010875692248185005 0.027523189009199176 -0.07734567215090496; 0.020067870503042762 0.06328316318959003 -0.1704290306040665; 0.005201765728495065 0.017628860875081528 -0.05562606334488472; 0.0011060519611341833 0.0038476614489915896 -0.012961415316696343; 0.001672619128277023 0.0069734130334132595 -0.024124209854984736; 0.00031079243096588673 0.001094361158135012 -0.0041634968780039664; 0.00030865366864156756 0.00020277724404536596 -0.0005670683662580456; 0.00023414466203312872 -3.765301636969511e-5 0.0002144164783419953; 0.0005353168700615158 2.698837638247443e-5 0.0006039982321117402; 0.00028687861556839244 -0.0006620357060651809 0.00013943329466393497; 0.000856429068041739 -0.0004164426095059181 0.0010608446937912116; 0.0003598933496701643 -0.0004665503279511359 0.0012158070800829374; -0.0009811081846751789 -0.00017045455145730338 0.0009909190913575962; 1.4380689148581715e-5 6.001240266897577e-6 -2.7890781821610414e-5] %
+
+Mass Used: 88.89602769297653 kg
+Launch C3: 96.30056859864789 km²/s²
+||V∞_in||: 0.00010671885293412463 km/s
diff --git a/archive/ES_0.5577011986221961 b/archive/ES_0.5577011986221961
new file mode 100644
index 0000000..62d5b53
--- /dev/null
+++ b/archive/ES_0.5577011986221961
@@ -0,0 +1,22 @@
+archive/ES_0.5577011986221961---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T12:33:10.666
+Launch V∞: [7.973857955338082, -5.6640394158069265, 0.15078615099752768] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.4571172664934866e-9, 4.557099227303111e-8, -8.262700656777477e-9] km/s
+ V∞_out: [7.3210150551364025e-9, -2.7034954603066573e-8, -3.651634690542943e-8] km/s
+ time of flight: 1.8652976581912372e8 seconds
+ arrival date: 2030-04-10T10:22:35.666
+ thrust profile: [0.3337682452768325 0.007050343106591057 -0.09886144558720877; 0.13596390984918116 0.08678471648208652 -0.13762231784098242; 0.0638343591327972 0.06616597023943864 -0.12194834349597691; 0.046275247415016256 0.06541450926620361 -0.13316558455798455; 0.025611225792110677 0.04521673206452789 -0.1036698249350419; 0.009655853534532839 0.02046113706092955 -0.05300883985994968; 0.008426681569807946 0.021617407171977052 -0.05921109572041219; 0.006968315088506374 0.02117535455022565 -0.061060135907883936; 0.002198276093213981 0.00735116605122934 -0.02376091928058066; 0.0013730175663987745 0.00626181752190888 -0.020421812526384964; 0.0005367469910112644 0.002900041802013804 -0.009229610196830532; -0.0009204797877206008 -6.564097130914157e-5 -0.0005870005231165083; 5.311330744140435e-5 0.0004831988271848311 0.0006437503426765323; 0.0002223609638857345 0.000285990704162885 -3.823874538380471e-5; -0.00014083495916210028 -8.365731768749253e-5 -0.0001979406155649203; -0.0013690812702666579 0.00027262876985762244 2.048633709867591e-5; -0.0020105147690877576 0.0033419766737437977 -0.0010696075119698825; 0.00034785747206316745 0.0006795648039978866 0.00032981209141628174; 3.354385529911578e-5 0.0016339230210158494 -0.0035364770881073882; 0.0005449184245903935 0.004872595500746797 -0.003143465560536954] %
+
+Mass Used: 92.48020871473818 kg
+Launch C3: 95.68648965905554 km²/s²
+||V∞_in||: 4.6634404550207703e-8 km/s
diff --git a/archive/ES_0.5577025376139346 b/archive/ES_0.5577025376139346
new file mode 100644
index 0000000..0dbe65d
--- /dev/null
+++ b/archive/ES_0.5577025376139346
@@ -0,0 +1,22 @@
+archive/ES_0.5577025376139346---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T18:19:22.728
+Launch V∞: [8.064056584293505, -5.62740857994159, 0.40851481377711785] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1198361635881181e-6, 7.316864404980914e-6, -0.0001630732526934587] km/s
+ V∞_out: [-7.876366364070246e-6, 0.00016314970688439533, -1.284895851062975e-6] km/s
+ time of flight: 1.8749577787519452e8 seconds
+ arrival date: 2030-04-22T20:28:59.728
+ thrust profile: [0.3106759469748791 0.004246885915738352 -0.09283362678496908; 0.057135202782318 0.03660073120755713 -0.06668696500610914; 0.06410683145847353 0.06109159361146465 -0.12685558463730495; 0.03365972026558772 0.04103741013480603 -0.09776861143376174; 0.03713210702821886 0.06029262217073841 -0.1542020674631312; 0.013352012546878752 0.021934346064894906 -0.06377653252462796; 0.015253889904388094 0.03235228564437776 -0.09024361296381848; 0.004893006624116817 0.0074408964490043725 -0.031025029379323592; 0.004235189002817859 0.009473332153482292 -0.029856538260319598; 0.0005179295686321152 0.0006841804356706579 -0.004096527643691767; -0.0014285243443203307 -0.002062022100059439 -0.004371473191147168; 0.00343040326542147 0.005678947523844167 -0.01238549188535442; 0.0010744634918951888 0.002782740084212824 -0.005463365108847141; -0.00029092969494899044 -0.0024884994853110734 -0.0008746719476685561; -0.002197923634220258 0.0016491788115077287 -0.0041814875147628775; 0.0033818476705477795 -0.001916594784483007 0.0023705505365650406; 0.0002245036803561703 0.0004075082397010707 -0.002866022754137863; -0.0012629161598525108 -0.0025239853428635894 0.005078058404023604; -0.0026078491319347762 0.0022999457234323274 -0.005088641696357362; -0.0004560942552607503 0.0028007606556637982 0.0045925097539971475] %
+
+Mass Used: 85.61517562163954 kg
+Launch C3: 96.863620273363 km²/s²
+||V∞_in||: 0.00016324115988861017 km/s
diff --git a/archive/ES_0.55770696747459 b/archive/ES_0.55770696747459
new file mode 100644
index 0000000..9586cdb
--- /dev/null
+++ b/archive/ES_0.55770696747459
@@ -0,0 +1,22 @@
+archive/ES_0.55770696747459---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T09:06:38.740
+Launch V∞: [7.905905233988366, -5.814463381832687, 0.06260362661589831] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9067498970675394e-6, -3.516097614408867e-6, -2.9667679615771013e-7] km/s
+ V∞_out: [2.762123657754316e-7, -1.4686179988269425e-6, -3.7153354873789934e-6] km/s
+ time of flight: 1.8369677074097547e8 seconds
+ arrival date: 2030-03-10T11:59:28.740
+ thrust profile: [0.39346737296893486 -0.023311960399654313 -0.13794522579430102; 0.025744845330034166 0.012436799007195416 -0.033003561560438814; 0.05529707843500096 0.040438486160446596 -0.12017750870567011; 0.04132532317245911 0.0382817912023306 -0.1314151417614821; 0.028247494886784595 0.03142093210865591 -0.1182309007606328; 0.02159725927734403 0.025596079241834345 -0.11320932688265967; 0.011149786180185091 0.015194185867519604 -0.0705559044494741; 0.0036061708724029655 0.006980767037690116 -0.028226666257229555; 0.0036672987796196365 0.006841025634542768 -0.03379050245732541; -0.000646792977539534 0.0031571154794173455 -0.024325696857303465; 0.002945067152935684 0.005331364875884975 -0.03709840453688085; 0.00012077888150232311 -8.056761232472375e-5 -0.001184823027902572; 0.0004597601079390892 0.0011098467701947665 -0.007351138696327194; -0.00047731713686969337 9.842068218730924e-5 -0.006633643852073385; -1.7861817338318267e-5 -0.0006731347711525568 0.0034201916384767345; -0.004695131424447144 0.001028353319405442 0.00033750802652246997; 0.0005810026793835742 0.0005735581157406225 -0.0005753442953221207; 0.0001064368887591857 0.00021650291604067044 -0.000427051926611308; -3.980413299700859e-5 0.0024718321179737846 -0.0009618070207790435; -0.00030238624508816236 0.0007348320450759032 0.0009062620017694807] %
+
+Mass Used: 88.81922171135238 kg
+Launch C3: 96.31524120154332 km²/s²
+||V∞_in||: 4.010817214159379e-6 km/s
diff --git a/archive/ES_0.5577137993372573 b/archive/ES_0.5577137993372573
new file mode 100644
index 0000000..31e21a0
--- /dev/null
+++ b/archive/ES_0.5577137993372573
@@ -0,0 +1,22 @@
+archive/ES_0.5577137993372573---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:12:19.534
+Launch V∞: [8.054723635975018, -5.780197997953262, -0.08222270313639338] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.350528486001623e-5, 4.739847746521461e-5, 1.1476732161792752e-5] km/s
+ V∞_out: [4.910141804620694e-6, -3.357174299811616e-5, 4.289902696131896e-5] km/s
+ time of flight: 1.8550734906015185e8 seconds
+ arrival date: 2030-03-31T20:01:28.534
+ thrust profile: [0.17775415239679876 -0.0029299275384472357 -0.062101229580743475; 0.0751704844263169 0.04134494084635545 -0.08938784972049739; 0.04971143915426151 0.043748697959039885 -0.1059184696374699; 0.038502744776599075 0.04442970519008038 -0.12124192481022593; 0.031010759243431624 0.04333559562636911 -0.13071946060351136; 0.013812372974612117 0.021891321657339136 -0.07497413822161095; 0.011386526393965488 0.021577192478008544 -0.07798517025380966; 0.007823458855071418 0.017047607142776863 -0.06632958346137731; 0.003267510814317188 0.007833772279366854 -0.03491153206849263; 0.0012200546595542024 0.003502423709422483 -0.01502438964796448; 0.0004744652727616107 0.0035007651666554935 -0.014971237841422076; 0.0007922895903609233 0.001484913902408933 -0.007569341833399924; -0.0004481573587914433 -0.0011780091180247586 -0.0030559663129723184; 0.00020757814127888782 0.00045975364947555 -0.002604672365125401; -0.00017525810951735696 0.00019426116568284002 -0.0007556464132168366; -0.0013393315529236344 0.0021898235379042667 -0.0012314960897846865; -0.0012039496477833616 -0.0027343682462578037 0.0006087893572483769; -0.0021474681452046465 0.002674930251508433 -0.00035655073448214933; -0.000814355838321304 -9.104769449027423e-5 0.002652674299584509; 0.004118587692993865 -0.0016971549790974895 0.008603742450386368] %
+
+Mass Used: 77.27263569120032 kg
+Launch C3: 98.29602232038856 km²/s²
+||V∞_in||: 5.413713571555567e-5 km/s
diff --git a/archive/ES_0.5577173796946676 b/archive/ES_0.5577173796946676
new file mode 100644
index 0000000..1ca58f6
--- /dev/null
+++ b/archive/ES_0.5577173796946676
@@ -0,0 +1,22 @@
+archive/ES_0.5577173796946676---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T00:03:40.588
+Launch V∞: [7.82837071942262, -5.918633982281683, 0.04262960623823549] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.681886255742581e-7, 6.586257337333013e-7, -5.482230808680141e-7] km/s
+ V∞_out: [1.6212884083210662e-7, 1.207115779889928e-6, -5.651671994037939e-8] km/s
+ time of flight: 1.7955749245685637e8 seconds
+ arrival date: 2030-01-20T05:08:32.588
+ thrust profile: [0.36963109189035764 -0.03325027093891209 -0.12130868584246149; 0.05656878101168813 0.025236578105439812 -0.06800601402307357; 0.03774427581360874 0.02801783306647439 -0.08240061967659987; 0.02807431082014258 0.026502810983390763 -0.08885346509020967; 0.060174658810518075 0.06602577532487114 -0.2330044027062936; 0.017792265175567187 0.02327363744959871 -0.09292541546498256; 0.014872225961767961 0.022161599079175334 -0.09431461757513375; 0.005698255795811218 0.008351193322018849 -0.04071992102369428; 0.0038563373724446685 0.005864181875100884 -0.03086476590074073; 0.0031051916024126642 0.004487214985158585 -0.026492757712373943; 0.0002667549477981413 0.0003024268687135496 -0.0021699301683233817; 6.48395819980187e-5 0.0007616026717472788 -0.0026948569317633286; 0.0005387622413263462 -1.9130886428807758e-5 -0.0018914925547403967; 5.551311116485378e-5 0.000583299272044834 -0.001181959611590185; -0.0005408388120059286 -0.0010868859469146312 -0.002172272495446573; -8.911258216277168e-5 0.00016646934675150572 -0.0020954156360028487; -0.0010496312971452646 -3.455853036478471e-5 -0.0012004236601536155; -0.001166731576038633 -0.0001582065007842792 -0.002477268609891804; 0.00010326682803574042 0.0002958320473491461 -0.0014415865276882368; 0.0031770627924171046 0.0021212022829670166 0.0006967045079593085] %
+
+Mass Used: 88.83024685892315 kg
+Launch C3: 96.31543362026099 km²/s²
+||V∞_in||: 1.2198720806333203e-6 km/s
diff --git a/archive/ES_0.5577253172076688 b/archive/ES_0.5577253172076688
new file mode 100644
index 0000000..801b340
--- /dev/null
+++ b/archive/ES_0.5577253172076688
@@ -0,0 +1,22 @@
+archive/ES_0.5577253172076688---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T16:58:42.277
+Launch V∞: [8.18098556999551, -5.690376279120456, 0.15233514225600095] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.013871333648257477, 0.08323352444822754, -0.45999577660446733] km/s
+ V∞_out: [-0.08503900227103806, 0.0753736736578598, -0.4536639256333048] km/s
+ time of flight: 1.8749577787492898e8 seconds
+ arrival date: 2030-04-25T19:08:19.277
+ thrust profile: [0.1919162936081352 -0.01318509016078507 -0.07091713470582099; 0.021727176526527493 0.009028508892504682 -0.0316447209532114; 0.020576395231703584 0.012397011360095682 -0.05182794424056189; 0.02590290196456876 0.018809113638862816 -0.09098924078941599; 0.012752999392721592 0.010505571380217613 -0.05983771766027663; 0.016002666376904912 0.013681577349152714 -0.08753120535239022; 0.035841790795625876 0.03129760463676063 -0.2072109039940551; 0.007874461599030064 0.006854495035040909 -0.05534047955966105; 0.005846565342329968 0.00360546234078373 -0.03802053308384878; 0.007169502004163855 0.006338555652652128 -0.061447004459212855; -0.0004657222105023821 0.0014683343592261499 -0.0023646938817677887; 0.00024221983702840569 -0.0011385380264968788 -0.0037905367323680496; -0.000996733750900586 -0.0007188350082974294 -0.004172251861339423; 0.0011810468147333876 0.0005741258081276315 -0.004833747065008412; 0.0001670107817944066 0.0013242516832894934 -0.0033303185219335564; -4.566657693198242e-5 0.00035529640919125565 0.0015943060345189404; 9.026496257468969e-5 0.00024798414595999423 -0.0029952911781208438; 0.0007780869527714188 -0.0021303418970214975 0.0010586497504695093; 0.0016334935380192424 -0.0036439622620542582 -0.0011017514095660538; 0.0008617036179468315 -0.0017420907345131295 -0.00269979354903743] %
+
+Mass Used: 71.24221038384394 kg
+Launch C3: 99.33211309001767 km²/s²
+||V∞_in||: 0.4676711964438285 km/s
diff --git a/archive/ES_0.5577267592161005 b/archive/ES_0.5577267592161005
new file mode 100644
index 0000000..ed12770
--- /dev/null
+++ b/archive/ES_0.5577267592161005
@@ -0,0 +1,22 @@
+archive/ES_0.5577267592161005---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T09:08:52.101
+Launch V∞: [7.999478693212082, -5.874483054896344, -0.10883470381214463] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0220682546647018e-7, 3.230252496594159e-7, 3.062909656773724e-8] km/s
+ V∞_out: [-2.8871989472839227e-8, 1.3056012588815918e-7, 3.58920540323567e-7] km/s
+ time of flight: 1.821591137529067e8 seconds
+ arrival date: 2030-02-20T16:54:05.101
+ thrust profile: [0.19264622207668547 -0.00840868157781318 -0.07171366434847515; 0.054731185821577946 0.026661137443356714 -0.07130109939755895; 0.041284564394935656 0.03241608014866511 -0.09560975398184689; 0.029361671187629473 0.02945891056400915 -0.0988643653035912; 0.015829263887643802 0.018782523404483335 -0.07048255111756903; 0.023791324896007084 0.03503961118209912 -0.1322707498671745; 0.011541104538264508 0.017462724507625947 -0.07754885351357592; 0.014176530487418059 0.025180938889852164 -0.11231126029606231; 0.006855461947954768 0.012322094474920735 -0.06183732583154131; 0.0029518112875753185 0.005528215200659713 -0.02976716653651579; 0.001934454575025385 0.003908691697721246 -0.02203863226383244; 0.00012149442200365783 0.00028269004091573965 -0.0010166348709925; 3.3233393668161896e-5 2.255199068146012e-5 0.00022748523915168796; 9.737922048550083e-5 -0.000734574158584268 -0.0008517176200750306; -0.0002202695625522157 -0.00034498335841825437 -0.00011114226016341105; -0.00017442904581562813 7.386040182454968e-5 -0.0006308438871092294; 3.098573602707374e-5 -0.00021136300016578576 0.0004066572341342512; -6.577726594787381e-5 0.00019963929782444614 1.6409631092137097e-5; -5.503897628666421e-5 0.00016802396983599894 -0.00021194869515988804; 0.0014645385793471803 0.0003158794392230132 0.0007716301998376244] %
+
+Mass Used: 76.02172856277912 kg
+Launch C3: 98.51305551817225 km²/s²
+||V∞_in||: 3.823232320161976e-7 km/s
diff --git a/archive/ES_0.5577379155863152 b/archive/ES_0.5577379155863152
new file mode 100644
index 0000000..aff1686
--- /dev/null
+++ b/archive/ES_0.5577379155863152
@@ -0,0 +1,22 @@
+archive/ES_0.5577379155863152---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:52:05.156
+Launch V∞: [7.845267648930825, -5.757014114332519, 0.05158453327093105] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.264260271636553e-7, -1.0999972039460771e-6, -1.0980405758349244e-7] km/s
+ V∞_out: [9.097567326694213e-8, -4.0781243708139653e-7, -1.2552484584558872e-6] km/s
+ time of flight: 1.839988661833933e8 seconds
+ arrival date: 2030-03-11T15:39:51.156
+ thrust profile: [0.42620080590989895 0.0011376831756676608 -0.12243908377454413; 0.1349712883795204 0.08211258393739553 -0.14036905384911777; 0.039139946485002595 0.03943926786900429 -0.07791286828180717; 0.055340656081291226 0.07530752250989942 -0.1563927598032733; 0.02395189531438529 0.03989238696995751 -0.09674714190810516; 0.027543260782721152 0.05673458306908534 -0.14648229251031464; 0.006770786332303762 0.015731015602184175 -0.044573322977312396; 0.004429595336119739 0.011359781604510484 -0.033675472295969816; 0.0021415516211155832 0.007491880430258745 -0.02225081715169788; 0.0005923137616615273 0.00020180910238691736 -0.003826350816470086; 0.0025778520991290507 0.00025824799164618885 -0.005896831530152026; 0.0002605050095223985 0.0012487436209075472 -0.002773742760072774; -0.0008691578123876111 -0.0010531029324611471 -0.002566111599189577; 0.0008114153551175817 0.0017773595416677313 -0.005114246707404567; 1.711502906385576e-5 0.0004533900455319606 -0.0026153308398968265; 0.0011049918760834409 -0.0011969126007189818 0.0005990076045214498; 0.0006539252298924274 -0.00016023966320525342 6.422951770598622e-5; 0.002436577324048409 -0.001448906250564015 -0.004481484195835622; 0.002383521601787864 0.0010332354433131526 0.0012931854361941863; -2.8588476903113752e-5 -3.508536506920644e-5 -0.00016936039362153155] %
+
+Mass Used: 98.31200258370063 kg
+Launch C3: 94.69409696005722 km²/s²
+||V∞_in||: 1.3227794799934562e-6 km/s
diff --git a/archive/ES_0.5577390184233735 b/archive/ES_0.5577390184233735
new file mode 100644
index 0000000..2aec16b
--- /dev/null
+++ b/archive/ES_0.5577390184233735
@@ -0,0 +1,22 @@
+archive/ES_0.5577390184233735---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T06:39:48.403
+Launch V∞: [7.876497402513212, -5.809482903510281, 0.06808191619149946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7841097265147956e-8, -2.8488231114479574e-7, 4.603924020547266e-8] km/s
+ V∞_out: [-4.489785159169477e-8, 1.6507345791153266e-7, 2.346947542494405e-7] km/s
+ time of flight: 1.856064121589475e8 seconds
+ arrival date: 2030-04-01T12:00:00.403
+ thrust profile: [0.37056591604047745 -0.00224641217367503 -0.11734520441296177; 0.09969665051566771 0.05683386823615241 -0.1089727438392025; 0.03697129389543633 0.03383043164870585 -0.07629113102266649; 0.06201441386548367 0.07506627870583588 -0.18368663390261067; 0.014961126774752306 0.022460110112712327 -0.06363501008622074; 0.008186061780309938 0.014366149288422248 -0.04400726526376195; 0.024083587514232667 0.04984807294449306 -0.14760300306191787; 0.00316654290093745 0.007047236068356764 -0.025744133721770965; 0.0045919245013912036 0.010254828914519344 -0.039949853650091814; 0.0010261140634844216 0.0032201961757322693 -0.013440544298528872; 0.0005002697422720374 0.0032809115039799932 -0.01486943052591408; 0.0005679129675867509 0.0011184352757464665 -0.0029821110998165456; -0.00040811539113323975 -0.00038449162934255473 -0.00129183253019619; 2.162870744362565e-5 0.00032111285254436434 0.002489702622794369; 0.0004768379339615824 -0.0005151590054035298 -0.0009723279493241933; -0.0002978217839514752 0.0025003095909269233 -0.0005750937789742061; -0.0023931998446298326 -0.001564239795744968 0.0014361025987154612; 0.0021423006401063145 -0.005278229724819991 0.0019853877797567218; 0.0004041377221949878 0.00040528655038534855 0.0029244664381743485; 0.0018474047425200801 0.002142073066310692 -0.0005969903313703814] %
+
+Mass Used: 91.8975493297562 kg
+Launch C3: 95.7939380852879 km²/s²
+||V∞_in||: 2.899183842718927e-7 km/s
diff --git a/archive/ES_0.557741310310728 b/archive/ES_0.557741310310728
new file mode 100644
index 0000000..81cf574
--- /dev/null
+++ b/archive/ES_0.557741310310728
@@ -0,0 +1,22 @@
+archive/ES_0.557741310310728---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T19:58:43.404
+Launch V∞: [7.824826223034047, -5.721913550073892, 0.3561615259315684] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.069193604544994e-5, 2.193047491589137e-5, 0.0016496174061372245] km/s
+ V∞_out: [-0.0014532414966244053, -0.0005073694339216863, 0.0005843445587907163] km/s
+ time of flight: 1.849185862278899e8 seconds
+ arrival date: 2030-03-23T02:15:09.404
+ thrust profile: [0.5325119933092456 -0.013834448796271189 -0.15689961731646546; 0.10876770762143326 0.062307337116067896 -0.12234159146051898; 0.034990573833874127 0.0317322769834925 -0.07415533448906386; 0.030715141358276823 0.03925116393655344 -0.10065883558901068; 0.03010375773460082 0.04794423411306 -0.13084392420888372; 0.01280373031946553 0.025531642197200555 -0.07993792145271685; 0.011843993930390932 0.023582851883250266 -0.08028750703807841; 0.008829520009443113 0.01966983416069678 -0.07149762027800408; 0.003258826256747507 0.007902505785128371 -0.031219900144172443; -0.00018022728677855016 0.001977009374237559 -0.004381331794705743; 0.00019429596992764114 0.0009705664900604071 -0.00021362892952221722; -0.0014415526341845079 -0.0011949152219358802 -0.003222138806171967; 0.0009413829721340168 1.2952895431331724e-5 0.000616421940141494; -0.0005685552973308973 0.0003444386648074811 0.0006087710443298683; 0.00037745435407116214 -0.0003122228283517251 -0.0017393989768558723; 0.0019398091242161558 0.0029820897928820042 0.00012991363789601113; -0.0003328209337177417 0.0001323465982155695 -0.0006335309692332371; 0.00017679972483980756 -0.0020298752957330396 0.002950938043109573; -0.006068910728846144 0.0019606940291847954 -0.0027953197735219515; 0.00035562508473642636 0.003908082232249297 -0.0026285632518210874] %
+
+Mass Used: 101.81039711728226 kg
+Launch C3: 94.09505112775437 km²/s²
+||V∞_in||: 0.0016500486439190692 km/s
diff --git a/archive/ES_0.5577415166180484 b/archive/ES_0.5577415166180484
new file mode 100644
index 0000000..3433295
--- /dev/null
+++ b/archive/ES_0.5577415166180484
@@ -0,0 +1,22 @@
+archive/ES_0.5577415166180484---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:30:11.399
+Launch V∞: [8.004945190077752, -5.800492006630012, 0.1509749746467123] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.664319504394213e-8, 3.6474291585388476e-7, -8.589451060650194e-6] km/s
+ V∞_out: [-3.687275495927058e-7, 8.580891523917874e-6, -6.3710769984963e-8] km/s
+ time of flight: 1.841302702603114e8 seconds
+ arrival date: 2030-03-15T21:48:01.399
+ thrust profile: [0.2594946540370043 -0.015485397764501014 -0.09501742756116362; 0.06048690032208209 0.02838385585196192 -0.07916257836716564; 0.051783642003175145 0.039710951953855725 -0.12487102323268073; 0.02486037128538942 0.023863815345162704 -0.08717974361554534; 0.023155988578426406 0.025887388078846954 -0.10718425725254388; 0.013901386475913168 0.017638856164770466 -0.07807577866087728; 0.010962860024498805 0.01621440166937728 -0.0783756886553517; 0.012296919790850845 0.018413141115085 -0.09660544212033939; 0.0047090854044021125 0.0076971554789611795 -0.04237497281568671; 0.0031943306507880524 0.005418776579290998 -0.03712814995300658; 0.0005758876178463332 0.0009338511245308094 -0.006633182304282053; 0.00026333053780413953 -0.001502571954554098 -0.0026820465253656212; 0.0003217935379269656 -0.0003321567069275432 -0.002153255616330842; 0.00010257726529327756 0.00012390587794754631 0.0006854363087906589; 0.0001674879030982809 -0.0005477587641690387 0.00031977004446435975; -0.000867485496862877 -0.00034237259312615775 0.0007345427069960786; -0.002344882437556802 0.004328108758101756 -0.000504349468869802; 8.963428101345532e-5 0.00040526595973572154 0.0004611928847778308; -0.0015050809628567568 0.0024775051255734033 0.0032109461621653884; 0.0012367456314116316 0.0007197750747784731 0.003463760138498308] %
+
+Mass Used: 80.50382004882294 kg
+Launch C3: 97.74764845809717 km²/s²
+||V∞_in||: 8.597378400972886e-6 km/s
diff --git a/archive/ES_0.5577595449707967 b/archive/ES_0.5577595449707967
new file mode 100644
index 0000000..f641ec7
--- /dev/null
+++ b/archive/ES_0.5577595449707967
@@ -0,0 +1,22 @@
+archive/ES_0.5577595449707967---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T14:37:22.356
+Launch V∞: [7.632583444186003, -5.781854903568401, 0.0553956504646637] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00029451625271304926, -0.00019661563844691375, -0.012006106640924136] km/s
+ V∞_out: [0.011254537264189528, 0.003827532328501, -0.0018091456653438567] km/s
+ time of flight: 1.8221414934231955e8 seconds
+ arrival date: 2030-02-18T13:39:51.356
+ thrust profile: [0.7381419321666345 -0.03563202596165325 -0.22859947367343664; 0.08192628303855827 0.041915496093991485 -0.09124724879027805; 0.061384133936804273 0.051664752759394444 -0.12236832993097924; 0.05441661875458789 0.06039162376406373 -0.15942337964674647; 0.022889962909202376 0.03072196784935484 -0.09072935612604406; 0.01425701438788243 0.022275671694219023 -0.07165292914370278; 0.010331969792707459 0.01840548770445254 -0.0635376032266977; 0.004308321465679833 0.008655040424817942 -0.03158591124666646; 0.006069998479850128 0.013444135514637351 -0.05185288093034141; 0.0013965481195091427 0.002854768408225975 -0.016394123137026477; 0.0004861333704759113 0.00063315934895603 -0.005024084690244075; 0.0009815579743776659 0.0014028249543794652 -0.005499629989648434; 0.00023404228598319481 0.00047009599215943037 -0.004164271935304248; 0.00026342836176607924 0.0006515791189860157 -0.0014401781989254437; -0.0005062497139209751 0.0011319343596254768 -0.0012584205807067597; 0.000557903061040453 0.00011882983611619989 -0.00045847538497559146; -0.00048381701857719457 -0.0005987052126712323 -0.001967072523019886; 0.00023492302191057698 0.0001311769968767437 -0.0005425785586596172; -0.00015925770824418552 -0.0003698055856129331 -0.00039069552170757464; 3.122049912637362e-5 -8.145447533475171e-5 -0.000598960788587277] %
+
+Mass Used: 115.8655409198509 kg
+Launch C3: 91.68924483647062 km²/s²
+||V∞_in||: 0.012011327745325937 km/s
diff --git a/archive/ES_0.5577652473416893 b/archive/ES_0.5577652473416893
new file mode 100644
index 0000000..635037f
--- /dev/null
+++ b/archive/ES_0.5577652473416893
@@ -0,0 +1,22 @@
+archive/ES_0.5577652473416893---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:04:53.747
+Launch V∞: [8.047518396728222, -5.654084331138808, 0.1757301113943622] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001686635209714849, 0.0011244984107767928, 8.617797255924886e-5] km/s
+ V∞_out: [-0.001437811431154941, -0.000678435519875021, 0.0012561838395124991] km/s
+ time of flight: 1.8749577777247402e8 seconds
+ arrival date: 2030-04-23T13:14:30.747
+ thrust profile: [0.32853377356668567 -0.00021551610431456498 -0.10335084251575616; 0.07567459373936299 0.04300078116952451 -0.08854452911817322; 0.032724685358808916 0.02988244231591365 -0.06981566353634537; 0.02852814160403995 0.03411995752991902 -0.08951332590823216; 0.021430428307725315 0.03165150445317881 -0.09216378299652873; 0.010208917061145262 0.017031926148657745 -0.05582290215948696; 0.02244354639263336 0.04351708012313381 -0.15003782262632948; 0.010702235925838867 0.022673083282169666 -0.08452149127233136; 0.0032376214120921057 0.00833871045888707 -0.0339712879222845; 0.0013717165054833698 0.0035434304621692774 -0.015248500029606274; 0.0002202076559634703 0.0011831499008232405 -0.00521022907634023; 0.000401576491911328 0.003184610198598351 -0.01004350334562464; 0.0005022242929292813 0.00127205005123949 -0.0017106526374081883; 0.0009350916551997105 -0.002986585392261227 -0.003903118160273901; -0.0002035072791905708 -0.00013254060148647977 0.00044541116096879184; 0.002817097463647571 0.0004938258887278854 0.0011502699397837614; 0.002295964092092758 -0.00034425939082575205 0.0026012902880166626; -0.0016590935302775033 -0.0020341995995989707 0.0029144937490876094; -0.00453331529981395 0.0003070941289348556 -0.0024527036676236015; 0.003967238242525814 0.008459985982912543 7.858830128535809e-6] %
+
+Mass Used: 86.28052082404201 kg
+Launch C3: 96.76210304135923 km²/s²
+||V∞_in||: 0.002028955802732974 km/s
diff --git a/archive/ES_0.557769953030391 b/archive/ES_0.557769953030391
new file mode 100644
index 0000000..4793123
--- /dev/null
+++ b/archive/ES_0.557769953030391
@@ -0,0 +1,22 @@
+archive/ES_0.557769953030391---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:14:32.090
+Launch V∞: [7.9970762642352025, -5.633774982678131, 0.1417157245329643] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0001104691845568029, -8.791940281891032e-5, -7.25044607818667e-5] km/s
+ V∞_out: [-1.1945163857681265e-5, 9.718253698933057e-5, -0.00012482419141583904] km/s
+ time of flight: 1.8749577787490457e8 seconds
+ arrival date: 2030-04-23T01:24:09.090
+ thrust profile: [0.41521368412865395 -0.0005489776561299086 -0.13080819986658182; 0.061509477939442496 0.03472926620224395 -0.07179802654234878; 0.04830428266305846 0.04401682326660837 -0.10182283784823752; 0.03785470718230513 0.04532070096676171 -0.11870638060563615; 0.02413178573171954 0.034910961903812376 -0.10309747590055555; 0.01490606351263695 0.02511780107520772 -0.08234330908744285; 0.010576297757964344 0.01988588360313606 -0.07278163337891372; 0.00820009999515338 0.018307894043647948 -0.06560208401341294; 0.0037109569303393716 0.008378356899533713 -0.035916955482152575; 0.001983103776917601 0.004624611029670474 -0.019115715172532577; 0.0008499758951449584 0.0030547113955449253 -0.012654414672548292; -0.00028605844330442816 0.00031498091584866044 4.622095811437693e-5; -0.0002193242663402447 0.0015700105969974681 -0.0017414128920114126; -0.00323344312576579 0.00032315801777491277 -9.938016880805742e-5; 0.0028334305748760743 -0.0024533869697646437 -0.0012128901953537918; -0.003545739922284254 -0.0012095300246849471 -0.0006538329471245151; -0.006848624504295954 -0.0010734749003886304 0.000762591385171033; 0.0009077915457300933 -0.005378237954667639 0.005043969085379161; 0.0015787437415428953 0.00019617659387734829 0.0033440333696826475; -0.0009178073086101102 -0.002523566101215417 0.00013780070949020453] %
+
+Mass Used: 92.40733791364983 kg
+Launch C3: 95.71273267802394 km²/s²
+||V∞_in||: 0.00015871407928078732 km/s
diff --git a/archive/ES_0.5577727312303149 b/archive/ES_0.5577727312303149
new file mode 100644
index 0000000..0d9949a
--- /dev/null
+++ b/archive/ES_0.5577727312303149
@@ -0,0 +1,22 @@
+archive/ES_0.5577727312303149---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T06:51:23.768
+Launch V∞: [7.939166665848077, -5.665585108710034, 0.17838366586878868] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.43155881130968e-6, -1.1840364588810362e-6, 8.634764307334079e-7] km/s
+ V∞_out: [-3.4144392678567025e-7, -2.0158239898064244e-6, 1.3038784709403767e-7] km/s
+ time of flight: 1.8749577786817852e8 seconds
+ arrival date: 2030-04-22T09:01:00.768
+ thrust profile: [0.4466923115374828 0.00905967292076207 -0.11363717230043231; 0.058169670171800074 0.038002215671802626 -0.06043714683941167; 0.04335054542736801 0.04950102677173345 -0.08263623626628655; 0.02194313994199356 0.03303520692110595 -0.06351051485391969; 0.03674085984284347 0.06872304979319169 -0.13639421436493732; 0.013100368101219083 0.030003211280243938 -0.0670512474615372; 0.01817191300676609 0.04860859456810092 -0.11491536412792724; 0.004882470683838969 0.02250433619945906 -0.057738999100670096; 0.006755555300944863 0.028121569875952948 -0.07170477678215537; 0.001891676473740525 0.0059664237087608835 -0.019358880505525852; 0.0001648446013160963 0.0014264634480913065 -0.0039783937093783635; 0.00043100151790472006 0.00289497730601182 -0.006027963800383008; -0.0003547760443654281 -8.409372211165382e-5 -0.001616204747175429; 0.00029536126121500834 -4.105552911431323e-5 -0.0002304438720123126; 0.002388162394145833 0.0012894101283907533 -0.0005309674871610904; -2.5400469115146882e-5 -0.0017303006237636624 -0.0005505572904582715; 0.00018723297773900812 0.0015447200264245152 -0.0009794358239177186; -9.666041608963241e-5 0.00036246712518863626 -0.0009287858520251228; 0.000985512089689525 0.00046591954281662343 0.002411305665873728; -0.0006982745971472425 -0.0054854415163441035 0.0036300403110789145] %
+
+Mass Used: 95.62877065970679 kg
+Launch C3: 95.16104270439895 km²/s²
+||V∞_in||: 2.048632351748364e-6 km/s
diff --git a/archive/ES_0.5577767992959153 b/archive/ES_0.5577767992959153
new file mode 100644
index 0000000..b3dee0f
--- /dev/null
+++ b/archive/ES_0.5577767992959153
@@ -0,0 +1,22 @@
+archive/ES_0.5577767992959153---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:06:11.522
+Launch V∞: [7.92301854403219, -5.926815883782274, 0.07127181898278742] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.162440842188592e-8, -3.402964761030955e-7, 6.3191297182673e-8] km/s
+ V∞_out: [-5.359503160067932e-8, 2.0974821889042727e-7, 2.732770648651183e-7] km/s
+ time of flight: 1.825473111845085e8 seconds
+ arrival date: 2030-02-25T13:41:22.522
+ thrust profile: [0.2385188385506486 -0.010761645029964687 -0.08269360554948374; 0.054068174691355754 0.027088113462390807 -0.0654234002145285; 0.03317783894021331 0.02675699110502639 -0.07157662011377869; 0.05008722071347194 0.057004473249492135 -0.16136891664948547; 0.022933992897262757 0.030765588152471317 -0.10043245579968454; 0.017677406574269285 0.02475646062421146 -0.09367438230657875; 0.02027586823660426 0.03046211048478535 -0.11876903168814011; 0.0058633150843044575 0.011110361753904986 -0.04710785288720381; 0.003932614164728085 0.007933300729187845 -0.0354707387924245; 0.00386479910253621 0.008357051146334726 -0.04178336979603198; 0.0017297337902681142 0.0029115914998990773 -0.01597772976795225; -0.00028782976332805823 0.0012617454539422066 -0.0016691010369282219; 0.00017473134036054844 0.0017165844377285474 -0.0006776444212693543; -0.00013393250813030326 -0.0002665629346779094 -0.0014582314171959735; -0.0006005914550766578 -0.0008023961453607009 -0.0010164841002703695; -0.00019789317949761183 -0.0017999378085772867 0.0010885027718271687; -0.0006477353074360417 -7.0519491565184615e-6 -0.0013266667493722316; 0.000946451997300314 -0.000789505299875177 -0.0021094412120120382; 0.0004201995713940523 0.00017319842556561547 -0.0017498913755098645; -9.342631315098157e-5 0.0024980954019035396 -0.00020199199230781849] %
+
+Mass Used: 79.61864643640911 kg
+Launch C3: 97.90644904151293 km²/s²
+||V∞_in||: 3.4860783563237e-7 km/s
diff --git a/archive/ES_0.5577797500509696 b/archive/ES_0.5577797500509696
new file mode 100644
index 0000000..cf6ebcb
--- /dev/null
+++ b/archive/ES_0.5577797500509696
@@ -0,0 +1,22 @@
+archive/ES_0.5577797500509696---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:32:56.924
+Launch V∞: [7.958484057424994, -5.60932260968089, 0.25856085475585605] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.768748619138364e-7, -7.956762040695331e-6, 1.4808481559448222e-6] km/s
+ V∞_out: [-1.5812578925181258e-6, 4.904673493908633e-6, 6.302091491050332e-6] km/s
+ time of flight: 1.8749577787493455e8 seconds
+ arrival date: 2030-04-21T17:42:33.924
+ thrust profile: [0.42337772001254453 0.001492695818244643 -0.1101195611295477; 0.11393324478791217 0.06816826442687056 -0.11743754495322291; 0.0702882096929421 0.06853223901412903 -0.1325540301900888; 0.04754181592978936 0.0617774257582239 -0.13488331651527113; 0.030411716376299528 0.04903175411907605 -0.1186762649960032; 0.015122319154084036 0.028975239663570546 -0.07720583172732597; 0.00668943515542164 0.014516143213724029 -0.04294893568867549; 0.004287847893659287 0.010871882482523021 -0.03296036242010294; 0.0009971011174266396 0.0021528784412297285 -0.009083129803841152; 0.0009891564217843199 0.0025821936519785176 -0.01185127770784835; 0.00041329304925580247 0.0016969992138399326 -0.005765220978336136; -0.0008562355350139085 0.0026688013532299463 -0.005974285883877394; -6.98697957108102e-5 0.0005830495535841681 -0.0005176109577477001; 0.0014862390923611399 0.000295795004584784 -0.004844705409842375; 2.6274269900925353e-5 0.0014370640188880925 -0.004065118005318214; 0.005685730736097497 0.004125779475940871 -0.004870288950483829; 0.002154343421834094 8.009724854202583e-5 -2.2147130998186396e-5; -0.0014748175906367264 0.004857209884145042 -0.0001738754204578508; 0.0011038105217411015 0.004415934267626599 -0.00032813347179699425; -0.0010598036834837661 0.0007943021977883523 -0.006938209414517486] %
+
+Mass Used: 97.3415780330979 kg
+Launch C3: 94.86882234737712 km²/s²
+||V∞_in||: 8.14075444640555e-6 km/s
diff --git a/archive/ES_0.5577828314509787 b/archive/ES_0.5577828314509787
new file mode 100644
index 0000000..0e34897
--- /dev/null
+++ b/archive/ES_0.5577828314509787
@@ -0,0 +1,22 @@
+archive/ES_0.5577828314509787---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T06:31:29.212
+Launch V∞: [8.12719610648311, -5.610862116183812, 0.43887677870434944] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00041450525161069654, 0.0003310454569038769, 0.0002711377658846593] km/s
+ V∞_out: [5.439380816627209e-5, -0.0003927267100462083, 0.00044480799505676986] km/s
+ time of flight: 1.874957778677965e8 seconds
+ arrival date: 2030-04-23T08:41:06.212
+ thrust profile: [0.27610932251848413 0.0006174398018991745 -0.0854622626891037; 0.0496519535008016 0.02778489745497459 -0.056136226580192836; 0.031134555566443445 0.027518508850587438 -0.06370805267047057; 0.026989637341647058 0.031213943793518936 -0.08069419006452318; 0.02679955506368715 0.03764446576671469 -0.10601927297330316; 0.014883947641331698 0.024069435507408914 -0.07612364496209563; 0.02957030775636677 0.05679605680822802 -0.17851908274362727; 0.004791364196606897 0.009506057210807843 -0.03739850843267621; 0.004744413969969548 0.011221613930671963 -0.04387440126827514; 0.000612210942282408 0.0011865160092176445 -0.0058148231809372185; 0.002144716071947398 0.0070295171011419254 -0.037098916713804636; 0.0007558685377119361 0.000586679136176375 -0.003511753714429299; -0.0017862869246017482 0.002208796780537911 0.0009324961592343914; -0.0005659977747829063 -0.0002889750172316247 0.0013563906943170265; 0.0006351566334409533 -0.00519812086295801 3.592234009244376e-5; -5.809750909560406e-5 0.0001849950577160858 0.0004504864031780971; -0.005044920084362336 0.0043842949309612755 -0.0020454779552744936; -0.0010977304762094886 0.0042153417077063545 0.0026438410750816554; 0.00018104480185465117 -0.00025853235235012196 -0.0011941800636497027; -0.0027173552803777014 0.000676498708762047 0.001301709926017589] %
+
+Mass Used: 80.68003546895216 kg
+Launch C3: 97.7257030669468 km²/s²
+||V∞_in||: 0.0005957527895347766 km/s
diff --git a/archive/ES_0.5577852702604125 b/archive/ES_0.5577852702604125
new file mode 100644
index 0000000..2ebcb0e
--- /dev/null
+++ b/archive/ES_0.5577852702604125
@@ -0,0 +1,22 @@
+archive/ES_0.5577852702604125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T20:05:15.532
+Launch V∞: [8.01786356313832, -5.689755837977987, 0.12886879880931024] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006703652426133094, -0.00509168060675119, -0.0003001066162655557] km/s
+ V∞_out: [0.006333940539664564, 0.002204969732200715, -0.00509599497855439] km/s
+ time of flight: 1.8749577787493944e8 seconds
+ arrival date: 2030-04-23T22:14:52.532
+ thrust profile: [0.3479540149120765 0.005121248479130735 -0.10622613087583975; 0.05585475742897683 0.03307060546970997 -0.07407606981530886; 0.03992145363105778 0.03925659502650456 -0.09774607255055309; 0.029327400757639437 0.03610652384846595 -0.1043057456187304; 0.020148403544279436 0.029125756634178865 -0.09181206107183995; 0.017160456793840033 0.029710104315552023 -0.1038037589606116; 0.007544616406492529 0.017121108570369935 -0.05656920272897872; 0.004468346832680893 0.009946261478947296 -0.037913312152781195; 0.009462576497345462 0.025005144993857573 -0.09041034131969042; 0.0015463944183671246 0.007389612134191354 -0.03663850810930519; 0.0005730893097077029 0.0014922161853061443 -0.00964476835735957; 0.0004639633358311684 -0.00024687608118864265 0.0029168074702527564; -0.0005281682082542014 -0.0006512566846228973 0.0026743317507739225; -7.182493784896207e-5 -0.000165197300787308 0.0005491833452143003; 0.0007877861003809948 0.0015297813413720886 -0.001076123306194458; 0.00020190345156173415 -0.0003050306783670618 -0.0005185192827722369; 0.0018654989528111088 -0.001092469759612022 0.0010555371854387085; -0.0012174942016810178 0.006636155327673434 -0.00019810172525945775; 0.0034667957699069845 -0.003538229395590336 0.0024798055764974976; 0.0005108503203473569 0.0010783742258076057 0.0010222364219558055] %
+
+Mass Used: 86.80577075257634 kg
+Launch C3: 96.67606478021227 km²/s²
+||V∞_in||: 0.008423433458673052 km/s
diff --git a/archive/ES_0.557795859654787 b/archive/ES_0.557795859654787
new file mode 100644
index 0000000..10ac324
--- /dev/null
+++ b/archive/ES_0.557795859654787
@@ -0,0 +1,22 @@
+archive/ES_0.557795859654787---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:46:40.833
+Launch V∞: [7.975424049784214, -5.748794300407147, 0.19628494757441] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.072685491289511e-10, -9.357802288388728e-10, -1.21709297512953e-9] km/s
+ V∞_out: [9.228295780470125e-10, -8.893492079968108e-10, 3.2253995103987676e-10] km/s
+ time of flight: 1.8749577787483138e8 seconds
+ arrival date: 2030-04-23T18:56:17.833
+ thrust profile: [0.3210236885013087 0.014430430950573626 -0.09377642386270031; 0.05870632495835611 0.03712730372873576 -0.06433684793856266; 0.03762543018470709 0.03868205379906367 -0.07527467222671375; 0.04138648420243932 0.05793322969961067 -0.12294855646284958; 0.029242003766453844 0.05102806902849716 -0.11971457302577972; 0.021951129310191504 0.046966321850924614 -0.11911757068760687; 0.00933995297496469 0.023146653074978187 -0.06412116988272024; 0.007031472194803151 0.020273205018782065 -0.060604530951651116; 0.004016641660362655 0.013178283211468881 -0.04207265828181557; 0.0005985059187766797 0.0017502952873097014 -0.007430886489217895; 0.0004611011838870558 0.00068165435691062 -0.0055269185892491725; 0.0005277084665234102 0.0028127099900698825 -0.0053283097379942775; -0.0034337970712285137 0.0002712875109683599 -0.0031340748306833517; -0.0011642588494299292 0.002097390787317298 0.0005300140709112865; -0.0009513252164067024 0.00011317588921863023 0.0017668905520680815; 0.0009718607157718622 -0.0006538593560121302 -0.003113826480851123; 0.0016511381136042839 -0.0010153190047746004 0.0014836400264483232; -0.0013928129654722848 0.00012148739528859606 -0.0046057415094472; 0.001581663404564496 0.0026594148013323743 -0.0028145662631171207; -0.009694769347455029 -0.006116240149941225 -0.007035131521730599] %
+
+Mass Used: 86.71028023025065 kg
+Launch C3: 96.69455246291443 km²/s²
+||V∞_in||: 1.7345554062087915e-9 km/s
diff --git a/archive/ES_0.5578041510973591 b/archive/ES_0.5578041510973591
new file mode 100644
index 0000000..f7d052a
--- /dev/null
+++ b/archive/ES_0.5578041510973591
@@ -0,0 +1,22 @@
+archive/ES_0.5578041510973591---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T23:27:43.674
+Launch V∞: [7.9856375630625, -5.830022024226737, 0.21650080876195207] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0480752243671387e-6, -3.5463019663633593e-6, -1.0515776677656446e-5] km/s
+ V∞_out: [-1.019725807441562e-5, -1.1674264860538984e-6, 4.347969115369377e-6] km/s
+ time of flight: 1.8749577787405452e8 seconds
+ arrival date: 2030-04-25T01:37:20.674
+ thrust profile: [0.20620920539025395 0.004484879129407838 -0.06964691734823818; 0.1135539094829683 0.06839690721910684 -0.12957575148067396; 0.05473377866576292 0.053061924930989164 -0.11750749274943685; 0.0327839994246312 0.04226427636690982 -0.10768078065630231; 0.019535233822420662 0.0316926558191732 -0.0915484867173932; 0.013480181891914777 0.026435321008672855 -0.08423268549685045; 0.0098270330371979 0.02191172367033763 -0.07555144549767967; 0.004371402236382642 0.007803565063119722 -0.03488015930585216; 0.007007994478852797 0.008602150990774129 -0.04498132861655965; 0.0020111882784604102 0.004133451654863654 -0.0277231975832671; -7.273494608390515e-5 0.002109760139240057 -0.009054116857051148; -0.00016269803580886382 -0.0006421258134300432 -0.0003367737068613588; -0.0008148292741752936 0.00045537230961754146 -0.0013098089743250147; -0.00014567853759485884 0.0006860019082751272 -0.0019651277660718055; -0.0007219931313343403 -0.002707342966421984 0.0004588361565137849; 0.0008619072802201633 0.0014768187930043473 0.002399995307430413; 0.00016461601658618219 -0.0015217107166619072 0.00419982243906771; -0.002774272527676308 0.0008592264907175087 0.0008988591430734924; 0.0016402042385413478 0.001264362271596302 -0.0023507435913258513; 0.001930480545192711 -0.0004635881309855643 -0.0026127930290612534] %
+
+Mass Used: 80.23396224499629 kg
+Launch C3: 97.80643669175818 km²/s²
+||V∞_in||: 1.1147030028079592e-5 km/s
diff --git a/archive/ES_0.5578199044625723 b/archive/ES_0.5578199044625723
new file mode 100644
index 0000000..273eb06
--- /dev/null
+++ b/archive/ES_0.5578199044625723
@@ -0,0 +1,22 @@
+archive/ES_0.5578199044625723---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T11:05:51.160
+Launch V∞: [7.742894184914409, -5.7896298177156345, 0.24845112658312588] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8273424796301933e-7, 1.7633475045608894e-6, -4.415854539059505e-5] km/s
+ V∞_out: [-2.008562575861191e-6, 4.412306306047675e-5, -3.42779814654054e-7] km/s
+ time of flight: 1.857645328749488e8 seconds
+ arrival date: 2030-04-01T12:21:23.160
+ thrust profile: [0.5180336125247006 0.02133960490601175 -0.1270890686188396; 0.11951023383216793 0.08085102738904414 -0.1139110824191251; 0.0605672552456431 0.0672241380854095 -0.10637185991971168; 0.039507658594430124 0.059495005955127925 -0.10512173314089575; 0.031000737936000868 0.05988834712995828 -0.11439409659549965; 0.018864039518906774 0.044665570528745355 -0.09295302097739239; 0.0109469543709915 0.03078572437054244 -0.0691136517914129; 0.007994699702008242 0.026961505063809194 -0.06375585636943648; 0.002665761082003214 0.010312125514732137 -0.025891608485788524; 0.00029976127821211226 0.0010692094411415215 -0.0032985089577269146; 0.0002812021270450186 0.0011678420336044507 -0.0036791308906030515; 0.0006789353293101845 0.0008158026434750974 -0.003878200629011114; -1.2985035752647332e-5 0.0012069595946437059 -0.0015937153510668313; -0.0013697106942341126 0.0006642239535922534 -0.001722534645924985; 0.0001244156659091927 0.00015662465125236108 -0.0008980364369784244; 0.00026229641086301545 0.00015469979178993234 -0.0014622693266178924; -0.0019021219950389736 -0.0002468284078984828 -0.00021077279023262274; -0.0015646765376911122 0.0004202630756037941 0.0005897803589922047; -0.00013250032728808652 0.0005606218779150502 0.00041818313923036555; 0.0024998779023513457 -0.000716114085686426 -0.001977426252077823] %
+
+Mass Used: 105.17517001396254 kg
+Launch C3: 93.53395174726376 km²/s²
+||V∞_in||: 4.419464293429755e-5 km/s
diff --git a/archive/ES_0.5578213026930944 b/archive/ES_0.5578213026930944
new file mode 100644
index 0000000..90f8602
--- /dev/null
+++ b/archive/ES_0.5578213026930944
@@ -0,0 +1,22 @@
+archive/ES_0.5578213026930944---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T18:20:42.978
+Launch V∞: [7.934808679693738, -5.646625275757218, 0.36876495419724453] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.147882176852829e-5, 4.402649528421355e-5, 0.00309366321826263] km/s
+ V∞_out: [-0.002691469485090709, -0.0010542576740641457, 0.0011003680913975573] km/s
+ time of flight: 1.859884514423328e8 seconds
+ arrival date: 2030-04-04T09:48:13.978
+ thrust profile: [0.42510739591290303 -0.0082639374698903 -0.12318800064356157; 0.15862442426382475 0.09061590789490298 -0.16728397221163757; 0.03809020276509802 0.034365947382289694 -0.08139313836305827; 0.02844756983479653 0.03146522664007201 -0.09022346686307307; 0.031156021304745082 0.04390956499984583 -0.13028849201723502; 0.012984729613825597 0.020941392616074497 -0.0721736926864759; 0.011005633076767888 0.019389809882287307 -0.07429868657038438; 0.004400195759803313 0.007574865107361518 -0.03082924438634615; 0.004319172789814626 0.009834200674797771 -0.04225627847616972; 0.0012143088083245565 0.00237340709226874 -0.013519671581320426; 0.0008791472170438478 0.0008852732493920106 -0.0035247485525036785; 0.0007901740501395704 0.001963033383671554 -0.004129092838822155; -0.0008022929947177869 -3.6607749068162557e-5 -0.0003573636049195453; 6.0829450732428035e-5 0.0002787636260491673 -0.0008661886988551343; -0.0008216569051725119 0.002391177021844113 -0.002513016261642514; -0.0013335726079930486 0.00011209321149794656 0.0010368260801557065; -0.0005541961799362801 -0.000370385206332563 -0.004231719128150022; 0.0007951595632327937 -0.0004636263835002053 -0.0019585797351407345; -0.006444403018891275 8.319143044472913e-5 0.0021557820609681296; 0.0025694639954133842 -0.006455307558340091 -0.00038973293580588206] %
+
+Mass Used: 96.7324584275666 kg
+Launch C3: 94.98155337960745 km²/s²
+||V∞_in||: 0.0030945872238222908 km/s
diff --git a/archive/ES_0.557824117309262 b/archive/ES_0.557824117309262
new file mode 100644
index 0000000..ec86ac9
--- /dev/null
+++ b/archive/ES_0.557824117309262
@@ -0,0 +1,22 @@
+archive/ES_0.557824117309262---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T21:54:37.348
+Launch V∞: [7.847450907590229, -5.851547867701127, 0.2948296116356903] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.747872381714361e-7, -7.408189571028727e-7, 5.56269362928375e-7] km/s
+ V∞_out: [-1.6703612073300693e-7, -1.2625904887361883e-6, 5.349967969065646e-8] km/s
+ time of flight: 1.8117388698144603e8 seconds
+ arrival date: 2030-02-06T19:59:23.348
+ thrust profile: [0.32139523942213455 -0.008266482467508017 -0.09745048701048206; 0.14561976502110885 0.08051478765662523 -0.15040077554759718; 0.06562724870977388 0.058832467131520835 -0.12472954299964602; 0.02940691151072188 0.03511092975039055 -0.0838474547017758; 0.022430368848156766 0.0329811971396844 -0.0856841697813867; 0.026167483519171888 0.045466548779694256 -0.1262476132834307; 0.015178824263731166 0.029196725303936077 -0.0878123318569592; 0.0106160622793781 0.023201702458743815 -0.07473691356490522; 0.0035850019777837767 0.00890529119249734 -0.03107108017337444; 0.0010823818318893466 0.00287117218050953 -0.010917899686462831; -0.00022516998584682008 4.3246575848130016e-5 -0.0006903009797254219; 0.00033491500234973486 -0.00018762773232518769 -0.0011072590485855394; 7.003657433646366e-5 1.4408631747856219e-6 -0.0005899154790551787; -0.0005359771797990134 4.6778513912729475e-5 0.00077584945027119; -0.0006386904363332529 -0.0003913161625168139 -0.0004183012356246513; -0.0013934938284043959 0.0012367040728417846 2.12507909360104e-5; -0.0010303320060548941 7.612845497493789e-6 0.0002525044699120915; 7.7730741139437e-5 -0.00027873558825319773 -0.0006358590046693974; 0.0012248764368637819 0.0005979883582698125 -0.0006145102300177578; 4.191656858757017e-7 7.862395755911511e-5 -1.6298523841393967e-5] %
+
+Mass Used: 91.31967114035979 kg
+Launch C3: 95.91002269493357 km²/s²
+||V∞_in||: 1.2741668036027846e-6 km/s
diff --git a/archive/ES_0.5578281758626383 b/archive/ES_0.5578281758626383
new file mode 100644
index 0000000..41d3bba
--- /dev/null
+++ b/archive/ES_0.5578281758626383
@@ -0,0 +1,22 @@
+archive/ES_0.5578281758626383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:22:24.324
+Launch V∞: [7.8430940147794646, -5.72383283252642, 0.21210334948422338] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.522682888517854e-10, -1.023679452659296e-9, -1.6735293893997457e-9] km/s
+ V∞_out: [1.1078267187189263e-9, -1.0330140634967168e-9, 3.9543840816511977e-10] km/s
+ time of flight: 1.8749577787493324e8 seconds
+ arrival date: 2030-04-23T07:32:01.324
+ thrust profile: [0.532204594020319 0.002215937403540617 -0.12319663343213506; 0.05120141188601409 0.0305423054461791 -0.057565340754721354; 0.03973906243795645 0.038591116679401016 -0.07800190399874568; 0.043641355408509865 0.05619237489143906 -0.12913557516531338; 0.03548042252586962 0.05646181964230544 -0.14011072039090902; 0.02055448840992152 0.0390826788775541 -0.10854550738754189; 0.0067175322772304496 0.014732243465330324 -0.046271479229995374; 0.0057444908226986155 0.014847498831467243 -0.04781236995576644; 0.0021818073943237716 0.0070918157695599 -0.025458265715514072; 0.00370065045288198 0.01144860773494124 -0.041087201493963985; -2.938149056783433e-5 -0.0009029482828885362 -0.005036325629101267; -0.0020046674074097205 0.0017443040411652217 -0.0002186927357345561; 0.001081137873928308 -0.00010343569251756185 0.0014029433337686722; 0.002756279680782664 0.0021243667872938793 0.0002679194649442488; -0.0023858351951326047 0.0008358638159827465 0.0008162832418330674; -0.00030764761029494195 -0.0032691959881390315 0.0011103468191141982; -0.000203351927657394 -0.0009455077786955486 0.004200283259999312; -0.0022353144179898675 -0.002654422560789879 -0.0017952208264417405; -0.0009862409565994032 -0.0005808512529547658 0.0023361232696246692; 0.000492160797081449 0.003906688028426213 0.0006498818216176619] %
+
+Mass Used: 100.59152438001547 kg
+Launch C3: 94.3213738502393 km²/s²
+||V∞_in||: 2.101077775189085e-9 km/s
diff --git a/archive/ES_0.5578321847691762 b/archive/ES_0.5578321847691762
new file mode 100644
index 0000000..967eaaa
--- /dev/null
+++ b/archive/ES_0.5578321847691762
@@ -0,0 +1,22 @@
+archive/ES_0.5578321847691762---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:14:20.462
+Launch V∞: [7.833275302412476, -5.694997267817892, 0.167276142898819] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.851176248012522e-6, 2.4990652279391555e-6, -1.783565163342548e-6] km/s
+ V∞_out: [5.84136832427408e-7, 4.141198569917391e-6, -2.242867716638107e-7] km/s
+ time of flight: 1.8593005611589506e8 seconds
+ arrival date: 2030-04-04T06:28:36.462
+ thrust profile: [0.586839300243645 -0.012714592256280566 -0.16787394622643798; 0.04191530821647954 0.023293756677909824 -0.04832065341361512; 0.05305397427858851 0.0433468092412204 -0.10265073955934649; 0.037620311574262405 0.04636260653482864 -0.11342206000845156; 0.022060701036357284 0.0348414186416088 -0.09670906990115347; 0.016225824930686625 0.028675928178679855 -0.08612993964080704; 0.017231854919845503 0.0322228838852087 -0.10464822113467173; 0.006862427743575858 0.014508888177247653 -0.05261590307349878; 0.003108065815472458 0.008015355222999712 -0.034171274868676695; 0.0019833848677679347 0.005067873912837813 -0.016870390243656153; -0.0013140574422294401 0.0053075539874830446 -0.02287097944247399; -1.6250578962302025e-5 0.0004093493413623083 0.001210149098278952; 0.002057869096197075 0.0009849399928248109 -0.00039873694011749396; -0.0010144476117652354 0.0008999226395851264 0.00011114691984310263; 0.0013677144434698241 0.003141575575245276 -0.004231539451708207; 3.965102905910791e-5 -4.727651756719761e-5 -0.0010507432445788986; -0.00023246016407633805 -0.0039903014600278335 -0.0034901658019453946; -0.002721150640768475 -0.0007473090155530853 0.0032618525816697098; 0.002612093143466258 0.005000575637750991 0.004157875487343372; 0.00013111339997697068 0.0001824660666516053 -1.3354924382708976e-5] %
+
+Mass Used: 103.51401551174604 kg
+Launch C3: 93.82117715182163 km²/s²
+||V∞_in||: 4.189944832884375e-6 km/s
diff --git a/archive/ES_0.5578379114512194 b/archive/ES_0.5578379114512194
new file mode 100644
index 0000000..831610a
--- /dev/null
+++ b/archive/ES_0.5578379114512194
@@ -0,0 +1,22 @@
+archive/ES_0.5578379114512194---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T02:58:29.727
+Launch V∞: [7.815099415116463, -5.712813843931132, 0.22808668910219665] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.406141968439283e-6, 0.0001449730659678172, 2.632305801194616e-6] km/s
+ V∞_out: [0.0001400530122453308, -2.2001585490916917e-5, 3.0427205332072978e-5] km/s
+ time of flight: 1.8749577787475732e8 seconds
+ arrival date: 2030-04-22T05:08:06.727
+ thrust profile: [0.4873923658289369 0.010956969430829728 -0.1371585525088027; 0.13718499688645794 0.0861322655063198 -0.13826858612433773; 0.07515600529693885 0.07669290908614629 -0.1394893316622414; 0.038740830211651076 0.05326868262159957 -0.11058078688410121; 0.04309943238632774 0.07420570544186972 -0.16539329615264992; 0.009595747141279646 0.020347951125025784 -0.051953774475188105; 0.004024754701702247 0.010467448566579352 -0.027683575105553457; 0.0019460152430830885 0.005884150556920195 -0.01694547984296659; 0.0013654392238724904 0.0013262941654977759 -0.00799899867667461; 0.0027625107618271306 0.004898314516807345 -0.013147625745247134; -1.2381180673984998e-5 0.004682556730671467 -0.016333272436064004; -0.0005485641053960711 0.0009736137534697948 -0.0024912028755882435; 0.0009260340643198362 0.0014054936550075834 -0.0017728285423852558; -0.0008667842311950575 0.003379676067072879 -0.003972132908101878; -0.003185663514818949 -0.0029856827878278224 -0.0003965007759170222; -0.0015286160823999974 -0.0030825484877009877 -0.0016773021709705694; 0.003041869673908096 -0.0012069356150839605 0.0001084732718229218; 0.0006144523372009611 0.00011541319977726328 -0.0030102766365463626; 0.0007610597309454076 0.0015545954720856145 0.0021923129220479567; 0.0021555981223764144 0.005911304139279803 -0.006006661275379945] %
+
+Mass Used: 103.85397090211154 kg
+Launch C3: 93.76404442131047 km²/s²
+||V∞_in||: 0.00014513840823455343 km/s
diff --git a/archive/ES_0.5578383905701928 b/archive/ES_0.5578383905701928
new file mode 100644
index 0000000..82d1ea7
--- /dev/null
+++ b/archive/ES_0.5578383905701928
@@ -0,0 +1,22 @@
+archive/ES_0.5578383905701928---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T22:32:13.974
+Launch V∞: [8.07732686160894, -5.6261945822151995, 0.15254472017852616] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.10552794676305e-10, 2.4009165651006984e-9, -2.0351304960160487e-9] km/s
+ V∞_out: [1.4451153268597388e-9, 2.835303668204948e-9, 7.30568776366802e-11] km/s
+ time of flight: 1.8737529165747845e8 seconds
+ arrival date: 2030-04-21T15:13:44.974
+ thrust profile: [0.2873701639662202 0.00015400501156201353 -0.0946158159831284; 0.08528542079782549 0.04683406263652301 -0.09668692533240654; 0.06743697788732247 0.06044569260957672 -0.13827145151835138; 0.031744335760616436 0.03697728396010384 -0.09846627872679424; 0.01807024573241676 0.02527932422450627 -0.07638234853789475; 0.015032127416429553 0.024059023610641127 -0.07872799682422657; 0.015733595122014235 0.02833063428212573 -0.09864919924263638; 0.009397485395882412 0.018210706583127942 -0.07196081758869247; 0.0023056580059990853 0.004188809819272621 -0.01850704015101568; 0.0021776838593609796 0.004684095625429339 -0.021119212580066538; 0.0009173317604300882 -0.0002904066854351698 -0.004556143457237688; 0.0005957733987155677 0.0005225993255636702 -0.00038557552611806663; -0.0010015512413265322 0.0004954294169577627 -0.0004910820934221427; 0.0004181458377158659 0.0008330495949786946 -0.0026954956165505806; 0.0011076129622830722 0.002333876629175045 0.002798729565338505; 0.0010375664791419067 0.007785561789189831 -0.0011337408670701122; 0.002323561898501346 -0.00587934899861995 -0.004360342191098537; 0.004513160184510264 -0.0031394446787565717 -0.0036766359522079845; -0.0046743756919561995 0.0018459041858616939 0.0021084833958669737; -0.002049397323042124 -0.00040863790764813883 0.0028482156225301276] %
+
+Mass Used: 85.44161217764213 kg
+Launch C3: 96.92054459787134 km²/s²
+||V∞_in||: 3.1626886547162252e-9 km/s
diff --git a/archive/ES_0.5578560465526554 b/archive/ES_0.5578560465526554
new file mode 100644
index 0000000..986126e
--- /dev/null
+++ b/archive/ES_0.5578560465526554
@@ -0,0 +1,22 @@
+archive/ES_0.5578560465526554---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:11:00.194
+Launch V∞: [8.076150475745225, -5.705643413643939, 0.024033039431151027] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.205265894519685e-10, -1.0143365335654291e-9, 1.9846772800480233e-9] km/s
+ V∞_out: [6.981062918065016e-10, -2.3233770264340667e-9, 3.82650542539576e-10] km/s
+ time of flight: 1.8529681159329292e8 seconds
+ arrival date: 2030-03-29T05:31:11.194
+ thrust profile: [0.2796071555744909 -0.015205307762577615 -0.10290746513517608; 0.019418333048326058 0.008945038503116424 -0.025547702989733863; 0.037221691356513126 0.027937005498367477 -0.0854050021937139; 0.042949758390638686 0.04027041861266196 -0.1408371448056782; 0.03420576385285525 0.037469948931475136 -0.14768368450599942; 0.02061516464504574 0.02568839747175512 -0.11203144751694377; 0.009617590162360235 0.013471547507943667 -0.064864945957218; 0.0054093814707439295 0.007887091066732816 -0.042213989417006596; 0.004264276291435489 0.006523464319335987 -0.03753969127722695; 0.0016724684586416527 0.002610629222188397 -0.017034968278552883; 0.003024630342406043 0.005008447264058215 -0.03228525185607599; 0.0002848390030013724 0.0015572961717256852 -0.005855669054665216; -0.00019008646341925133 -0.00018198542160662625 -0.0017422880785113756; -0.00038410086417467275 0.000459059383812672 -0.00017817170403300678; -1.4795177028579766e-6 0.0007049603767688567 0.0005476138236779446; 0.0013108923882008757 0.0007091682186066172 0.003625444616732129; -0.002868901719833172 0.0009805976569301387 -0.0008366793706089527; -0.0002876278545925837 -0.0002785398002600151 0.00236178204437167; -0.01229853076084345 0.0037984709768704634 0.0015852487278908236; -0.0001543970801820024 0.0025701404863819246 -0.004805255446064641] %
+
+Mass Used: 80.45367430921624 kg
+Launch C3: 97.7791508575226 km²/s²
+||V∞_in||: 2.313628266917839e-9 km/s
diff --git a/archive/ES_0.5578591282406365 b/archive/ES_0.5578591282406365
new file mode 100644
index 0000000..376e289
--- /dev/null
+++ b/archive/ES_0.5578591282406365
@@ -0,0 +1,22 @@
+archive/ES_0.5578591282406365---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T00:32:08.904
+Launch V∞: [7.9450757793836395, -5.748479606224134, 0.10505456991676117] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3916843376020123e-6, -2.019036811681612e-6, -1.9341585353106834e-7] km/s
+ V∞_out: [1.4590133762442497e-7, -1.4728849390232166e-6, -1.96291681499122e-6] km/s
+ time of flight: 1.8443696800196177e8 seconds
+ arrival date: 2030-03-17T17:01:36.904
+ thrust profile: [0.33486345925176114 -0.005294841975134288 -0.10321335430608976; 0.08230098792205089 0.04579988319756462 -0.0876953072196564; 0.06269798613259717 0.056914099170846444 -0.11948028022412657; 0.03687727594548879 0.044112870897776255 -0.10562942371711966; 0.04387993896180024 0.06450843055649107 -0.16509632986673028; 0.017187718734084336 0.029825901749299298 -0.08694838781456968; 0.007035808006593024 0.014249398566882844 -0.04515260127044257; 0.004494470029094474 0.00981940305839726 -0.033028741008202904; 0.004956697634161811 0.01271587644321737 -0.04520831501150258; 0.003033025330442388 0.009335645832912666 -0.03673652080182052; 0.00029113858971051905 0.00018567886253860163 -0.002171542805383461; -3.114086768786706e-5 -0.0002306937026373331 -0.003297565791295588; 0.00043255416176069537 0.00012426887362934202 0.0005259044631021059; -0.002489457075231615 0.0014916784162252274 -0.0031368740725891205; 0.0001621443216177123 0.0007579450443073038 0.002764905595329148; 0.0019050606072553238 -0.0014806227061741378 -0.0014036381404463056; -0.0012917981279513629 -0.0037819307209347895 -0.0004423948675474844; -0.0005156726354417169 -0.0011151790980908163 -0.005691589604728913; 0.00045290697805767976 0.0003531774513070552 -0.0032302752748472087; -0.000588935779805921 -0.0007303925881259662 0.003311685905886291] %
+
+Mass Used: 89.78399652917096 kg
+Launch C3: 96.18028338598373 km²/s²
+||V∞_in||: 2.4598180084813903e-6 km/s
diff --git a/archive/ES_0.5578652081042674 b/archive/ES_0.5578652081042674
new file mode 100644
index 0000000..4fa7f50
--- /dev/null
+++ b/archive/ES_0.5578652081042674
@@ -0,0 +1,22 @@
+archive/ES_0.5578652081042674---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:00:38.278
+Launch V∞: [8.054984103480795, -5.694565289509901, 0.06555947000194151] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1238881227204616e-5, -7.897980640541607e-6, -0.0005252067291566444] km/s
+ V∞_out: [0.0004696124267613665, 0.00015990523601933904, -0.00018298830536819102] km/s
+ time of flight: 1.8749577787058547e8 seconds
+ arrival date: 2030-04-23T13:10:15.278
+ thrust profile: [0.26469290520863353 0.006268248566530032 -0.08140514204995254; 0.0643571698721037 0.04007596440346908 -0.07172627011492981; 0.040313908400049225 0.04035726931603478 -0.08096745050008437; 0.04068257257903647 0.055281882709380586 -0.12216294554154807; 0.020885360432926308 0.03520071796988408 -0.08792773130572369; 0.021208191625686428 0.04117016434953468 -0.10733973426664763; 0.009718596851875563 0.023307947484289333 -0.06813908805381735; 0.00759858967542993 0.02142584011984219 -0.06590870018860695; 0.0073691242491234175 0.024120032928206817 -0.07699720234166087; -0.0006851069459962753 0.0047879076749027995 -0.013995930833627204; 0.0027802793267414304 0.002207479546415429 -0.008844730787152458; 0.00026580662854063246 0.001973435787122494 -0.007335434866882073; 0.0004171755441515113 -0.0001820775765866402 -0.0008223573665085172; 0.001427332619218602 -0.0005601672286088997 0.0036848778189188715; 0.0002314089464429032 -0.0009449039457695421 0.0003910085560094262; -0.002669115614809795 -0.0035514079064133085 0.004092328791910461; -0.0007991627649497387 -0.0014438941172173494 -0.00017727005459337538; -0.0005245404634621515 0.0013447169814103962 0.0018826117804938334; -0.00342664144005114 0.001104989808950383 0.0036178112390452895; -0.002341361495706544 -0.001972430997941417 -0.00033932854548725255] %
+
+Mass Used: 83.17108819207579 kg
+Launch C3: 97.31514078792621 km²/s²
+||V∞_in||: 0.000525386332997784 km/s
diff --git a/archive/ES_0.557881734356892 b/archive/ES_0.557881734356892
new file mode 100644
index 0000000..3352406
--- /dev/null
+++ b/archive/ES_0.557881734356892
@@ -0,0 +1,22 @@
+archive/ES_0.557881734356892---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:31:55.654
+Launch V∞: [7.866659184813449, -5.694300234105715, 0.16564571941555434] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.361951192981255e-6, -0.00020792338617737127, -3.7636602608554642e-6] km/s
+ V∞_out: [-0.0002012800958525212, 2.9971449707115766e-5, -4.388484994618195e-5] km/s
+ time of flight: 1.8749577787328154e8 seconds
+ arrival date: 2030-04-22T07:41:32.654
+ thrust profile: [0.46437434718781956 0.013831963574738633 -0.12566385951664652; 0.13978914810548168 0.08971753705563404 -0.13916015377576038; 0.04019735443673702 0.044387016937486694 -0.08010674846127071; 0.030607276871051223 0.04623070061529843 -0.09286007276928089; 0.016141567220468007 0.029995922507221027 -0.0687702752905253; 0.017744574754476505 0.03936106225019483 -0.09527057702905531; 0.012706968222310088 0.035269593688508995 -0.08939788814173749; 0.008886595069717495 0.029361146447578108 -0.07857139529252116; 0.0021905450182869383 0.008569684054199505 -0.02595760300135466; 0.001261804834970592 0.006577449780128229 -0.020850210412191088; -0.00030921657032255824 -0.0007240655268790624 -0.0015486667165316732; 0.0002422191047584371 0.0008158723402133597 -0.0023563911171887433; -0.0017979979271656537 0.0013993947754676185 -0.002259915505171407; 0.0005693667440481132 0.00018573253299630505 -0.001416782461989711; -0.0014069410982389733 -0.0005488165144751369 -0.0014543451227162414; 0.00011893889715382494 0.000686667936025758 -0.0016844201339796373; 0.0011082565647115641 0.0017754209374383583 0.00041579779313696006; 0.000949110497844373 -0.0021177169571417144 4.22922611666716e-5; -0.0008461303724775401 0.001319741844363678 -0.0046182885114118295; 0.0010872382118177868 -0.0029656732016637706 0.005845705876551845] %
+
+Mass Used: 100.56390447175045 kg
+Launch C3: 94.33682039050692 km²/s²
+||V∞_in||: 0.0002081680710103333 km/s
diff --git a/archive/ES_0.5578848532055836 b/archive/ES_0.5578848532055836
new file mode 100644
index 0000000..12c89a3
--- /dev/null
+++ b/archive/ES_0.5578848532055836
@@ -0,0 +1,22 @@
+archive/ES_0.5578848532055836---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T13:42:24.320
+Launch V∞: [7.94328411984221, -5.762808784056582, -0.09155417403100533] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.389613154612235e-6, 3.139007245426577e-5, 8.589409893173765e-5] km/s
+ V∞_out: [8.261477402463717e-5, 1.0217705396080628e-5, -3.8920882640101314e-5] km/s
+ time of flight: 1.8534071823760107e8 seconds
+ arrival date: 2030-03-28T17:14:22.320
+ thrust profile: [0.3255634302568498 -0.0012878490452704482 -0.10273499560250099; 0.08274661994361635 0.04947208244985847 -0.09104735421124846; 0.05635005118132995 0.05576976676629488 -0.11354943752377313; 0.02281523026366272 0.02957454710695329 -0.06890507298635054; 0.04276611465133112 0.07244640647937957 -0.1743440545581028; 0.016835462221885773 0.032478782863011216 -0.08896188961394584; 0.01159911417271791 0.02558908341339088 -0.07512960151019399; 0.0049953597426000695 0.01302342731642394 -0.04065615662258128; 0.002118672059401553 0.00659619407606207 -0.02241398258358557; 0.002104754948633265 0.01142728180945489 -0.0383195382265198; 0.000402862113049375 0.0015649616223409675 -0.009115233374065428; -4.998657481169587e-6 0.0004194136205095952 -0.0007677774669173224; 0.0019765910916375346 0.0002453764378029181 -0.002338802022190796; 0.0013146039333977763 0.0008054208685289797 -0.00148147675463363; 5.165583857499043e-5 -0.0017462629599894236 -0.0021887419692505866; -0.00022159719146816112 0.0023305448078886713 -0.0015867889098421894; 0.0009355801501741625 0.003950390780609883 -0.0037739182572579027; -0.0005906680663616886 0.002709490925156003 -0.003526126461272754; 0.002098226751601079 -0.0018028007791525947 0.0038285274714898072; -0.0018732961336156164 0.0027321863762952226 -0.0004770102810012402] %
+
+Mass Used: 89.03335457448293 kg
+Launch C3: 96.31410985691963 km²/s²
+||V∞_in||: 9.19309399232514e-5 km/s
diff --git a/archive/ES_0.5578897748378324 b/archive/ES_0.5578897748378324
new file mode 100644
index 0000000..5625fd2
--- /dev/null
+++ b/archive/ES_0.5578897748378324
@@ -0,0 +1,22 @@
+archive/ES_0.5578897748378324---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T20:45:43.974
+Launch V∞: [7.961275844747766, -5.660402924176248, -0.17885064845153978] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1848673854856167e-7, 3.866698744825616e-7, 1.0892675428855392e-6] km/s
+ V∞_out: [1.0587839515786047e-6, 1.267476273512234e-7, -4.898162505291244e-7] km/s
+ time of flight: 1.8749577787354344e8 seconds
+ arrival date: 2030-04-21T22:55:20.974
+ thrust profile: [0.35800159015733257 0.015216201139191404 -0.10709461252531606; 0.11794544912302647 0.07954903826404743 -0.12621176300559453; 0.06402435748106464 0.0687437855598571 -0.12657886502481386; 0.05044567306302037 0.07839055611921113 -0.15187147840503468; 0.02255684325166863 0.04338759473504945 -0.09925507194130344; 0.015293715342994271 0.03729793593631663 -0.09073927929046631; 0.006747306437479793 0.01873507633071038 -0.051294877711458936; 0.0029283773721735453 0.010122984998181261 -0.02923577357752761; 0.0014436305138415318 0.00547864080879674 -0.0170684288562098; 0.0008741334568711003 0.004056377900877193 -0.013750057786815638; 0.00043156250678986265 0.0021446572431102263 -0.00796954512087398; 0.00030888138209501085 0.001874739736840653 -0.006777884052554072; 4.794735146675734e-5 0.001804639287908472 -0.002730677873841906; -0.0004569765469637717 6.234991151898863e-5 0.0008332001971364941; 0.00046110292710471485 -0.00024972055686497084 0.0002504995924271621; -6.4856174744417e-5 -0.0010679612142002349 0.0018181459371030906; 0.0008433190557500367 0.0023155344693682645 -0.0005924256579209137; -0.0016907346165773683 -0.0009480249768067149 -0.0016965024334600416; 0.0010958641566621938 0.0009120614452634522 0.0011523987977775586; 0.0017942683182072272 -0.0007148092836441091 -0.0011777537029237792] %
+
+Mass Used: 94.05604292541148 kg
+Launch C3: 95.4540618946388 km²/s²
+||V∞_in||: 1.1619193083119563e-6 km/s
diff --git a/archive/ES_0.5578946701862005 b/archive/ES_0.5578946701862005
new file mode 100644
index 0000000..31f1510
--- /dev/null
+++ b/archive/ES_0.5578946701862005
@@ -0,0 +1,22 @@
+archive/ES_0.5578946701862005---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:10:15.949
+Launch V∞: [7.950286494891662, -5.918751762486953, 0.07390764549870203] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6322995730500666e-9, -1.1077732529982117e-8, -6.568123201262873e-9] km/s
+ V∞_out: [-7.0598128132092835e-9, 5.979065346853017e-9, 4.056841783433682e-9] km/s
+ time of flight: 1.8106532381654483e8 seconds
+ arrival date: 2030-02-07T08:05:38.949
+ thrust profile: [0.14340871503405347 -0.009653406901043852 -0.05154378684929445; 0.09991390111169197 0.04606441083955706 -0.11688190474170486; 0.07350147149982864 0.05458604604378318 -0.15201397190878255; 0.05942125387458901 0.05652929186701904 -0.17789329057807127; 0.036114661426072156 0.04073614966906394 -0.14391484684953235; 0.01454906942674182 0.018886376066940287 -0.07439281814855034; 0.008155141247621287 0.01210695851423404 -0.05078266112933165; 0.006369833563302631 0.01026565195270941 -0.045786670445280626; 0.002683251119045106 0.004820991017808717 -0.023721697514426453; 0.0006614602999839384 0.00047982302562656217 -0.0076660470255773385; -9.14475084632816e-5 0.0005775964280227747 -0.0026610990660537186; 6.63135638854329e-5 -0.00019097037920998757 -0.003113301647301941; -0.0011810159012940683 -0.001881854086761828 -0.0012813318179015706; 0.0005276910639250912 -0.00017142601875328297 0.0004144763569658369; -0.0005485620305448103 -0.0011013078602130117 0.0022646676785210746; 0.0013696736319246086 0.0009214516013200194 0.0025597995480682798; -0.0023086310772202703 0.0029935378318709143 0.0014325693062947; -0.0015812350396254885 -0.0021659642926626266 0.0032001759544716896; 0.00011552557561968851 -0.0025636333249035486 0.003366362852491615; 0.00033480462423396526 0.0008300904538583749 0.00016899284271263727] %
+
+Mass Used: 77.7862978688704 kg
+Launch C3: 98.24414011686233 km²/s²
+||V∞_in||: 1.2981556235250498e-8 km/s
diff --git a/archive/ES_0.5578972210077474 b/archive/ES_0.5578972210077474
new file mode 100644
index 0000000..74654e3
--- /dev/null
+++ b/archive/ES_0.5578972210077474
@@ -0,0 +1,22 @@
+archive/ES_0.5578972210077474---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T03:22:58.192
+Launch V∞: [7.974310459366733, -5.669380101542432, 0.18172229098579887] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.317741507115638e-10, -2.3287328604154163e-9, -1.0903658156622767e-10] km/s
+ V∞_out: [-6.437981500521791e-10, -1.3063641140027098e-9, -3.337425035462917e-11] km/s
+ time of flight: 1.826340377862072e8 seconds
+ arrival date: 2030-02-22T23:03:35.192
+ thrust profile: [0.4323618892440017 -0.012404976220525334 -0.11267943787576087; 0.03566723108526887 0.020170702526168243 -0.03679145946609485; 0.03845026128247992 0.036762485577795885 -0.07190269842400417; 0.0293747416031891 0.035888583215865286 -0.07898646319821073; 0.03863066168572842 0.05948090630340335 -0.14184213952514044; 0.02157889545392796 0.04093281599085822 -0.10420598472858664; 0.035168210590852116 0.07199820182612843 -0.19577427986012158; 0.008536410910647663 0.017278336675784146 -0.05152055315412298; 0.0022041046518649714 0.005981075102230982 -0.019357203494961783; 0.001013071357037275 0.003730188173894801 -0.012850771667747831; 0.0006913005251164522 0.0025048509716685905 -0.008727318306088588; 0.00011222217776346435 5.7621335594823194e-5 -8.436836089762651e-5; -9.3280643370784e-5 0.0002623770086550046 -0.001144291319828704; -3.5491948672861583e-5 8.609644431513927e-5 -0.00026447958193349393; -7.619616395619904e-5 -0.000281927212149151 -0.00023649328139786454; -0.00013260730074636458 -0.00017921617606509826 -0.0001705616920034637; -4.262526336016931e-5 0.0003935863813378717 1.161605772040115e-5; 6.545687399758644e-5 0.00023720155972338107 1.3690971076933044e-5; 6.44618348426447e-8 6.193433536984944e-6 -3.7236750422077364e-5; 0.00046114582570795914 3.5438069949509775e-5 0.00011985658614094612] %
+
+Mass Used: 92.25371850553483 kg
+Launch C3: 95.76452102917207 km²/s²
+||V∞_in||: 2.47522401998085e-9 km/s
diff --git a/archive/ES_0.557899087625678 b/archive/ES_0.557899087625678
new file mode 100644
index 0000000..0071901
--- /dev/null
+++ b/archive/ES_0.557899087625678
@@ -0,0 +1,22 @@
+archive/ES_0.557899087625678---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:00:26.633
+Launch V∞: [7.867980448543319, -5.664442401412237, 0.17864182575906365] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.0049559343207354e-6, 2.642588461691586e-6, -1.9778292130465554e-6] km/s
+ V∞_out: [5.481643162285813e-7, 4.441633368994617e-6, -1.7899743168683623e-7] km/s
+ time of flight: 1.859393953065312e8 seconds
+ arrival date: 2030-04-03T15:50:21.633
+ thrust profile: [0.5195325537540987 -0.006866119651192578 -0.15398060385582787; 0.10169892112689949 0.05709529957430543 -0.10526989095558953; 0.07023896720696932 0.06728353812677898 -0.13576274660212684; 0.02567787857046763 0.03164544021122456 -0.07848261764535383; 0.021080203615912712 0.03229068690720902 -0.08678838701699595; 0.016291465986833564 0.029176892442333062 -0.08438130824585519; 0.008107381822867767 0.015607041117265524 -0.04332012380459912; 0.008848679816409246 0.020441058610588318 -0.06774387807447439; 0.007469461194847777 0.019968680909879147 -0.06903507453051759; 0.0004699183194756255 0.00334921347036156 -0.01008396644908596; 0.001460315877464644 0.004474991136485024 -0.016144472538113408; -3.874016193102508e-5 0.00012141840202549025 -0.0025639720021131407; 0.0019783597781536325 0.0013896130012395365 -0.0039939639551595145; -7.37953818837246e-5 0.0007777254486239573 -0.0028279761767810137; 0.0001745577064121691 0.0008858097698264414 -0.002471716087788859; 0.00041629976628910256 -0.00012423269928445104 0.00012403273700613065; 9.644287697839135e-5 -0.000330883190078183 0.001073743994757148; 0.0005275192663362749 -0.00044912431156837133 -0.0029633094048185124; 0.002515780981748046 -0.0002125591596597035 0.004217903459999086; -0.0004461347709661336 -0.0024480387785132856 0.0015786346212393896] %
+
+Mass Used: 102.41513663294836 kg
+Launch C3: 94.0229369594873 km²/s²
+||V∞_in||: 4.463725164148804e-6 km/s
diff --git a/archive/ES_0.5579079308627815 b/archive/ES_0.5579079308627815
new file mode 100644
index 0000000..e3ea17f
--- /dev/null
+++ b/archive/ES_0.5579079308627815
@@ -0,0 +1,22 @@
+archive/ES_0.5579079308627815---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T13:23:22.894
+Launch V∞: [7.801153048590762, -5.633417892905768, 0.3062146177295675] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012362723245441593, 0.06940643218680666, 0.08779795734788548] km/s
+ V∞_out: [-0.05053229676020144, 0.043076874087259416, -0.0908533870764798] km/s
+ time of flight: 1.874957778700714e8 seconds
+ arrival date: 2030-04-20T15:32:59.894
+ thrust profile: [0.5336664092577796 0.0022882332085486204 -0.12542584284156408; 0.21989033671256947 0.13870297454569427 -0.1955700284844757; 0.06367693130512862 0.06937351644740376 -0.11677473894712324; 0.022782007696430687 0.03351199703503894 -0.06641132406988191; 0.045891443844430835 0.0859447325286344 -0.17099129784325154; 0.013333494822427057 0.030297524940844395 -0.07063944255838642; 0.005699174231039199 0.014931989252050708 -0.03868050257430703; 0.0018633237236997825 0.005827563917872326 -0.016152257490049986; 0.0004723332179803712 0.0015374590343733051 -0.0048757514078019695; 0.0007650598147557042 0.0030183660571014162 -0.009357663898721632; 0.0006554310617922924 0.0031427539231489447 -0.009599435901434925; 0.0003058430060712652 7.075924709253008e-5 -0.0012872239807950599; 0.0003466641456168177 0.000552357193049666 -0.001577836806168461; 0.001272650671728503 0.001578174402400029 -0.000684219045392434; 0.0018349965518059427 -0.0013206571536352226 -0.0015583519334837152; -0.0007992038149063813 -8.140979063048237e-5 -0.001300364287038859; 0.0018959311278763358 9.647160977374245e-5 -1.9746475262808448e-5; -0.0016375789216912825 0.00032829714403420033 -0.0009525741221909688; 0.00042934111089516525 0.0019922193514834664 0.000501722486232235; 7.5395979019110565e-6 0.0005034210996461789 -5.915443187676315e-5] %
+
+Mass Used: 110.2175242979838 kg
+Launch C3: 92.68715343575906 km²/s²
+||V∞_in||: 0.11259916105107662 km/s
diff --git a/archive/ES_0.5579109566730904 b/archive/ES_0.5579109566730904
new file mode 100644
index 0000000..fdff5ac
--- /dev/null
+++ b/archive/ES_0.5579109566730904
@@ -0,0 +1,22 @@
+archive/ES_0.5579109566730904---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:07:22.419
+Launch V∞: [8.073983024576618, -5.711538545396211, 0.15243361729788407] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.3782283251301714e-6, -3.155384085891762e-6, 2.147030545835119e-6] km/s
+ V∞_out: [-6.625669245562563e-7, -5.036263632551625e-6, 2.254054562354775e-7] km/s
+ time of flight: 1.8549229569715405e8 seconds
+ arrival date: 2030-03-31T04:45:37.419
+ thrust profile: [0.22842062058561285 -0.009758992359080428 -0.08120345378511047; 0.054996610865878856 0.02736777688697314 -0.06902604132801729; 0.06641551547098631 0.051144655302353806 -0.1441925930881726; 0.05535002218716302 0.054458148859156084 -0.17447580339223892; 0.020703359528834026 0.024845312771027733 -0.0905982879392891; 0.023027216053797123 0.03255568413610841 -0.12598168002043175; 0.00567379627492303 0.00970776138511699 -0.04069905291040398; 0.002034376854022392 0.0038115676677365953 -0.017197061870642277; 0.00207445544399182 0.003991133606786214 -0.022819523635368006; -0.00012691348397344203 0.00022069435775127523 -0.007612736807064891; 0.001892544762256648 0.0040876462762510675 -0.025133645739559674; 0.0005818424402091406 0.003077387579692369 -0.0021704372815980542; -0.0012227415963262864 -0.0015779994093084889 -0.0016926080793499888; -4.938946461407559e-5 0.0011789487961735407 -0.004970008756906851; -0.00015354223511208204 -3.2209398659438634e-5 0.002923759105075801; 0.0005777332018873694 -0.0014758740292290652 -0.0004107077362761448; -0.0016677554119800056 0.006571873974491225 -0.003611786364779297; -0.0044472150136631305 0.0007927000314460625 -0.006214471827099869; 0.0008776884629850056 -0.00491623007051502 -0.0035600719704168664; 0.004524357356112403 0.009130622439939597 0.0032318312833405903] %
+
+Mass Used: 80.19713852638552 kg
+Launch C3: 97.83411044438057 km²/s²
+||V∞_in||: 5.096922160574933e-6 km/s
diff --git a/archive/ES_0.5579220066351401 b/archive/ES_0.5579220066351401
new file mode 100644
index 0000000..d64ed90
--- /dev/null
+++ b/archive/ES_0.5579220066351401
@@ -0,0 +1,22 @@
+archive/ES_0.5579220066351401---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T02:40:00.516
+Launch V∞: [7.876245688421231, -5.780264376809818, 0.06091622724883032] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7755802824822642e-9, 1.3997870904469536e-9, 3.4688307342430794e-10] km/s
+ V∞_out: [1.597969810340168e-9, -1.4790492070446565e-9, -1.1816791943673663e-9] km/s
+ time of flight: 1.874957778749349e8 seconds
+ arrival date: 2030-04-24T04:49:37.516
+ thrust profile: [0.4419872985588551 -0.0029285265180362496 -0.11867915140857914; 0.04999066676582706 0.029990461308698757 -0.05609005644422793; 0.049728604592932324 0.0486515954469168 -0.09595072340762444; 0.03512432949202107 0.0460279732233678 -0.10272705921915531; 0.01819891764050963 0.027918964439038664 -0.07336077223839725; 0.016138378430823507 0.030422778421105055 -0.08299343130371163; 0.008713977873243522 0.01880897590754412 -0.05658064523622825; 0.0063780030467912915 0.022198750164700725 -0.06696725273266123; 0.01607981764524821 0.03237013433245973 -0.10932542262998214; 0.0022816145662403306 0.008853216566707255 -0.03002469098307853; 0.0008434213959810008 0.00512230638214729 -0.019060670130148134; -0.0005586028245356866 0.0003389617463386374 -0.00040333158222367925; 0.00030855071164940514 0.00022127245800505896 -0.000835982749981441; -0.00041987555050686357 -0.0008799547911302479 0.0011839701293354155; -0.000313399947673035 0.0005136118073734573 0.0005905117826083504; 0.0005002134762893665 -0.000343307526646342 0.001134191902664796; -0.001590678604529723 0.00033889220583285915 -0.004076819589498909; 0.0008665474682130602 0.002276850808195293 -0.005275854397184731; -0.0007385495495649388 0.0011540627119868577 -0.00010317732474523743; 0.0005408883749292231 0.0004825980217758504 0.0004808116994902366] %
+
+Mass Used: 94.11493075888848 kg
+Launch C3: 95.45041319693286 km²/s²
+||V∞_in||: 2.2874477272169608e-9 km/s
diff --git a/archive/ES_0.5579268478630314 b/archive/ES_0.5579268478630314
new file mode 100644
index 0000000..ab2f8b8
--- /dev/null
+++ b/archive/ES_0.5579268478630314
@@ -0,0 +1,22 @@
+archive/ES_0.5579268478630314---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T01:32:27.036
+Launch V∞: [8.002175242599137, -5.594410129659658, 0.1680115328599683] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.064960379220849e-6, -2.6132000814969138e-5, 4.939156866362503e-6] km/s
+ V∞_out: [-3.788132433054868e-6, 1.438364625491229e-5, 2.3008342626420705e-5] km/s
+ time of flight: 1.8592169278773242e8 seconds
+ arrival date: 2030-04-02T22:27:19.036
+ thrust profile: [0.4286002029867508 -0.0013620582316501084 -0.13075098720036424; 0.06278560473408341 0.036661821657415286 -0.07011199386726612; 0.07171365032521586 0.06866815584955463 -0.14172342923696946; 0.042864254660735124 0.054565753029815096 -0.12780583168282048; 0.031214641215208082 0.04914985033391067 -0.12721200874353217; 0.018051318136591353 0.03385270370519706 -0.09619456025762929; 0.008110176065188488 0.017916701267746696 -0.055522291205751924; 0.004450495378444074 0.01164654158314932 -0.03701202901079538; 0.0029177759297442287 0.006675577789681686 -0.02534253429185726; 0.0008203470778132987 0.002427746925811581 -0.009052828280941812; -0.000562279586896313 0.0011255136005968627 -0.003909640442745755; -7.213892049297413e-5 -0.001398564159691344 -0.0055967686719311325; -0.000600154088295776 -0.0001554279388191596 -0.0010382814561101963; 0.0003058384446208483 0.0023451957031973766 -0.00024077113560838376; -0.0001435625360110728 -0.001412591417388261 0.0015805514169284181; -0.0005569181095084969 0.00034204323397000655 -0.0019885120389492653; 0.0031447908013721533 -0.0009252807692230382 0.002109171540248623; -0.0006613696265909729 -0.0005967062402295642 0.0020359067401852496; 0.0033546005307672454 0.0026280117763101563 0.004775550146659996; -0.0006206275751138688 -0.0017175212560561624 0.002931106903722061] %
+
+Mass Used: 94.64529891440861 kg
+Launch C3: 95.36046118727909 km²/s²
+||V∞_in||: 2.6770706364798765e-5 km/s
diff --git a/archive/ES_0.557927430291621 b/archive/ES_0.557927430291621
new file mode 100644
index 0000000..016bb36
--- /dev/null
+++ b/archive/ES_0.557927430291621
@@ -0,0 +1,22 @@
+archive/ES_0.557927430291621---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T23:41:51.375
+Launch V∞: [8.031736790593135, -5.751284909936231, 0.20494633375519317] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008485270423004593, 0.05237401756722299, 0.05303975841569472] km/s
+ V∞_out: [-0.01300126208114039, 0.01097813526052419, -0.073023285342947] km/s
+ time of flight: 1.874957778741704e8 seconds
+ arrival date: 2030-04-25T01:51:28.375
+ thrust profile: [0.30431390098664296 -0.004447346756998066 -0.10157214608328986; 0.021596682949053567 0.01116713328715327 -0.027386746740587588; 0.031062807297653733 0.02609535893662747 -0.06786412378352512; 0.02307073029559897 0.024870285616005516 -0.0745812128614892; 0.04029555685969985 0.05086861190353695 -0.1641585501101144; 0.0218880174771981 0.031968233406563636 -0.11474598665809042; 0.012813528195134517 0.021541835880303187 -0.08434358963049085; 0.00797160236157983 0.014731176448271145 -0.06509146135556286; 0.005049437535708424 0.009238472719458537 -0.04163102704946477; 0.0023854542223194523 0.003137792049720569 -0.01786306490975725; 0.0017028088440903606 0.0018434727441898001 -0.005394643877873065; 0.003282847330161458 0.0035900720532904625 -0.012115350586740296; -0.0012447339976523974 -0.0015378990453332993 -0.003867844072468987; 0.0013082037815657322 0.0025888208208099256 -0.0030967452840661063; 0.00028476194373147883 0.0015486787835202076 0.000268084193508821; -0.003816214847403797 -0.0019434880309972475 0.0011480804930328928; -0.0066681167407130135 0.004463189271493646 -0.0001465482477361669; 7.080124790692904e-5 0.0002546039029005388 0.0019381856459690563; 0.0008566397555169258 0.002468869855281109 -0.008139328075219127; -0.0033068113127370006 0.00315337400116892 0.003643337750065716] %
+
+Mass Used: 81.41821957486582 kg
+Launch C3: 97.6280769883472 km²/s²
+||V∞_in||: 0.0750216868850505 km/s
diff --git a/archive/ES_0.55793175475376 b/archive/ES_0.55793175475376
new file mode 100644
index 0000000..68b735b
--- /dev/null
+++ b/archive/ES_0.55793175475376
@@ -0,0 +1,22 @@
+archive/ES_0.55793175475376---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:11:51.964
+Launch V∞: [7.942698877973461, -5.716610474404426, 0.02071069082943179] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.5262728402224974e-6, 0.00012681760940022388, 2.2987904083800055e-6] km/s
+ V∞_out: [0.0001225837878006309, -1.8398897358021087e-5, 2.6767984813453398e-5] km/s
+ time of flight: 1.85612729173484e8 seconds
+ arrival date: 2030-03-31T06:17:20.964
+ thrust profile: [0.3750332164614023 0.005708753014489498 -0.10345058868664676; 0.07248348207673452 0.044628913655028385 -0.07704854024220474; 0.05270233493788829 0.05316523933186007 -0.1006426015724017; 0.04533193114834566 0.060526084935528315 -0.12607761836983442; 0.023654080491295564 0.03978882599327906 -0.09379752667516632; 0.02561432413426531 0.051677598655057735 -0.12819396595336915; 0.009742591240350486 0.02320798009617909 -0.06389197333052125; 0.006639364821558034 0.018557064261999743 -0.05405927969943119; 0.0013750460440685322 0.003995602108500082 -0.013703419615650643; 0.003723169029502036 0.013560071592244465 -0.04343821653488024; 0.00033515407093091094 0.0007814137043136707 -0.004738976709487414; 0.0004152250608386608 0.0016595851865647201 -0.005879754133397199; 0.0004071759291536495 0.001880970888141399 -0.005880711191473403; 9.362731786659257e-5 -0.0017919917646790524 -0.003401954266885376; -0.001637589909152391 0.001965324093720525 -0.0038176157339144387; 0.0010590650239540216 0.0022120214333754534 -0.0032895177211516476; 0.0004905789845600908 0.004972078715257726 0.002708241833683235; -0.0008211010876047912 0.00033367788442688687 -0.00133606193670195; 0.0019505221213746936 0.0008506271938431929 0.00012795566342369393; 2.054795350135859e-5 0.0012984348737005316 -0.001216812418346184] %
+
+Mass Used: 92.28229054220219 kg
+Launch C3: 95.7665297149459 km²/s²
+||V∞_in||: 0.0001269587735559618 km/s
diff --git a/archive/ES_0.5579333874908491 b/archive/ES_0.5579333874908491
new file mode 100644
index 0000000..3e863fb
--- /dev/null
+++ b/archive/ES_0.5579333874908491
@@ -0,0 +1,22 @@
+archive/ES_0.5579333874908491---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T09:00:05.307
+Launch V∞: [7.8350897314823795, -5.763106987061512, -0.03203350297865192] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.566973436082149e-6, 2.5726407105607123e-6, 2.5142564665912653e-7] km/s
+ V∞_out: [-2.3031133545828318e-7, 1.1165922927279257e-6, 2.7988696986824875e-6] km/s
+ time of flight: 1.85923255259817e8 seconds
+ arrival date: 2030-04-04T06:21:00.307
+ thrust profile: [0.4476722779725153 0.0008106512727952044 -0.13455153617963275; 0.11080949555900507 0.06852181843372737 -0.1178225561286512; 0.065950225155388 0.06627989449664462 -0.1272086012246618; 0.04184826319187302 0.056584033045523424 -0.12225497703267517; 0.019331147861087104 0.0335114426322128 -0.08299564623608295; 0.006550928512205551 0.013116154661331104 -0.037375678367848886; 0.00730076760923557 0.017059169555293255 -0.0513750752577088; 0.0077603629667599905 0.024600707361984275 -0.07206132274282565; 0.010492147914378382 0.024281220884486157 -0.0875254285151062; 0.0018839387582294262 0.00728311866760074 -0.024379309259231263; 4.057231883046499e-5 0.0005528284806419881 -0.0021920188666617324; 0.0005538399497358315 0.0007416797728475404 -0.0006063321910592626; 0.00011325902563539887 -0.00015895514282784483 -2.4714311135510918e-6; -0.0005010978596204925 -0.0010144584679052074 0.00041194288457420576; -0.0008135160772150914 0.000692020896124753 0.0008111163000981371; -0.0013821663716009364 -0.00016922024863595404 0.0009002097429080722; 0.0002698799184277284 -0.000655747165889276 0.0007561765302320144; 0.0007008815978434833 -0.003362007936585869 0.00029327330017809867; -0.0005697272774565544 0.0007341119276173809 0.0012106937143728038; 0.0004876544280488082 -0.0005652654338189726 0.002431763269012787] %
+
+Mass Used: 99.07110563092692 kg
+Launch C3: 94.60305939001093 km²/s²
+||V∞_in||: 3.022763773572024e-6 km/s
diff --git a/archive/ES_0.557935356926101 b/archive/ES_0.557935356926101
new file mode 100644
index 0000000..fcc3dce
--- /dev/null
+++ b/archive/ES_0.557935356926101
@@ -0,0 +1,22 @@
+archive/ES_0.557935356926101---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:49:47.377
+Launch V∞: [7.945701496545313, -5.736791365601548, -0.214699504782922] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010921117827720076, 0.0070861100890934935, 0.0004703216649129304] km/s
+ V∞_out: [-0.009554240174272135, -0.004220757954986261, 0.0077532524086496545] km/s
+ time of flight: 1.8749577787556085e8 seconds
+ arrival date: 2030-04-22T09:59:24.377
+ thrust profile: [0.28802164084533227 0.01431431957416294 -0.07392645803296491; 0.10082550427909272 0.06881047611718788 -0.09733165130847714; 0.07446863885762305 0.0839185500842902 -0.12900462969320547; 0.0615773298748603 0.09818853659097107 -0.16657494783858606; 0.022609135981595224 0.04519274864002445 -0.0885796139744419; 0.019048831545037673 0.04081983646918119 -0.08683074045079911; 0.010166177154171636 0.02950353117451617 -0.06956105501075896; 0.0036005969675457095 0.01359144324995046 -0.03352151572604928; 0.004469382417213494 0.020580478042397727 -0.051255759144548475; 0.0006126264259049385 0.0005130904052235036 -0.0007848742671049292; -2.3820475137712743e-5 4.986975013069196e-5 -0.0004270853604301781; 0.0007190690168191022 -0.00042516344911533514 -0.0015485689781394195; 0.0006400535881936646 0.0005468987405198359 -0.0003487174714898373; -0.0011075425078368156 -0.0022825766021131104 -7.347740235339167e-6; -8.14310247719504e-6 0.0010524772915226602 0.0009224623643710099; -0.001661803197089664 0.00022398257101700133 0.0013343934947232894; -0.0001733638219283226 -7.656243668123438e-5 -0.00024636328639355165; 0.00048037776395873626 0.0004155988340512869 -0.0009596899444138756; -0.0007135577227384529 -0.00028716351102014254 -0.00040308842225824336; 0.000580886156848781 0.002121856875814165 -0.0013750348995601215] %
+
+Mass Used: 90.39349703546895 kg
+Launch C3: 96.09104332199693 km²/s²
+||V∞_in||: 0.013027086138894773 km/s
diff --git a/archive/ES_0.5579525198441861 b/archive/ES_0.5579525198441861
new file mode 100644
index 0000000..33c8955
--- /dev/null
+++ b/archive/ES_0.5579525198441861
@@ -0,0 +1,22 @@
+archive/ES_0.5579525198441861---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T10:30:42.617
+Launch V∞: [7.888341195299436, -5.929648318907001, 0.08921844180425674] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.289667628792672e-6, -1.759289416987318e-6, -1.8966576277261344e-7] km/s
+ V∞_out: [1.5128660342640077e-7, -7.290938697573742e-7, -2.0590049838962994e-6] km/s
+ time of flight: 1.8342093410158557e8 seconds
+ arrival date: 2030-03-08T08:46:16.617
+ thrust profile: [0.29822522286718506 -0.013290858992887114 -0.10643276744336937; 0.05019240379762707 0.02326083690307949 -0.06398208199716822; 0.04320028458243177 0.03181516367204412 -0.09704431383301115; 0.048838228432844334 0.04663444907151248 -0.15772235872405527; 0.021820896647583996 0.023755101379631015 -0.09393306624822077; 0.020524868421435437 0.0254303409728869 -0.10969669591959341; 0.012293348801725893 0.01633604933206293 -0.07782517153418236; 0.009985620822675663 0.0143904491282926 -0.07362947046941319; 0.004198657164589072 0.006952724354900335 -0.03795964455917501; -5.533502646184931e-5 0.0014788823606402153 -0.011177903332329; 0.0014076944205436994 0.00119965905691002 -0.009646803642356977; -0.0004213196654108157 0.00018565677065893098 0.0008530189773882982; 0.0010022469369400718 0.0013579172538624438 -0.002886799952720287; -0.00043167943856546414 0.0012745339706865134 0.0016069834579215624; 0.0007140569743618304 -0.0010016044304475647 0.0020757996414770196; -4.1049296746110194e-5 9.383973529812064e-6 -0.0015347645165758957; -0.0010602897537159502 -0.0014236633943550251 -0.00021659420842701444; 0.00036215721989364837 0.0006671624453128844 -0.001142350121947967; -0.0005575909916736162 -0.0038869848355366746 -0.0030009938925190044; 0.00040339876088247325 -0.001361140098999463 0.000588161624523125] %
+
+Mass Used: 82.80934689477635 kg
+Launch C3: 97.39461592973272 km²/s²
+||V∞_in||: 2.189592415735725e-6 km/s
diff --git a/archive/ES_0.5579540971762518 b/archive/ES_0.5579540971762518
new file mode 100644
index 0000000..d245de2
--- /dev/null
+++ b/archive/ES_0.5579540971762518
@@ -0,0 +1,22 @@
+archive/ES_0.5579540971762518---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T19:55:51.054
+Launch V∞: [7.9704703081790615, -5.692515305608844, 0.03974863843171797] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.360023955800101e-6, -8.72471643782298e-5, -1.4888402173619585e-6] km/s
+ V∞_out: [-8.499786611136771e-5, 1.2270248661866803e-5, -1.7652931157606058e-5] km/s
+ time of flight: 1.8564795401670197e8 seconds
+ arrival date: 2030-03-31T12:48:25.054
+ thrust profile: [0.3436945299928322 -0.001572765752768555 -0.1072410494408209; 0.063439724133125 0.03680852568289646 -0.07232289512958007; 0.10916335565583934 0.10339468292977816 -0.20784367382940558; 0.05413480413256434 0.0727595234261486 -0.16643896170221673; 0.019787058808139434 0.030683134706953014 -0.08391192279350546; 0.010106846742543956 0.01889110488742394 -0.05640436196526551; 0.004090537865594636 0.008424011331313921 -0.028525118500917563; 0.005866116140757708 0.01294601289367893 -0.044996863223633304; 0.0029433255265900547 0.007771658223263708 -0.029186043105279627; 0.0006864200739433275 0.0024379755572177435 -0.011307028253656473; 0.0008365956152359479 0.002522780184516173 -0.010365254394568684; 0.000916988734851971 0.003192249154250427 -0.013438913540236368; -0.0003599549343552235 0.001471614127495342 -0.0032100505791389576; 0.0005952830995334297 -9.068582356748533e-5 -0.0028517525545913233; -0.0008995235001749058 -3.432539185501841e-5 -0.0017099268151287705; -0.0009528260467406412 -0.00030515327447579025 0.001637122405590467; -0.0025473156142316747 0.0007252850771832198 0.002010527794846036; -0.00574310792132249 0.009238740273461658 -0.0028819402296229365; -0.0026611103251928544 0.004323749511789386 -0.00010422875027888112; -0.0005025334913632915 -0.0006077628121326266 0.0001898127293173956] %
+
+Mass Used: 91.32732024988945 kg
+Launch C3: 95.93470739241215 km²/s²
+||V∞_in||: 8.74243341069375e-5 km/s
diff --git a/archive/ES_0.5579570651292369 b/archive/ES_0.5579570651292369
new file mode 100644
index 0000000..5cb7131
--- /dev/null
+++ b/archive/ES_0.5579570651292369
@@ -0,0 +1,22 @@
+archive/ES_0.5579570651292369---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T16:42:38.553
+Launch V∞: [8.08433229484103, -5.575162665407191, 0.1596197286506724] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004982081583189355, 0.00030367864459046704, 1.9931448501620028e-5] km/s
+ V∞_out: [-0.00041170407073461054, -0.00024332807915238445, 0.00032553544155622356] km/s
+ time of flight: 1.8572351601146457e8 seconds
+ arrival date: 2030-03-31T06:34:34.553
+ thrust profile: [0.34281960320404914 0.0007119005918270643 -0.09680146389378985; 0.06014203714758432 0.03678183222535264 -0.06293150571959617; 0.05781432849414902 0.05868191846527074 -0.10860074475585688; 0.040469488874237146 0.05429710478829569 -0.11258039731823904; 0.030588493331400516 0.050758160266505044 -0.1139419546505444; 0.023278226917271144 0.0483564721840311 -0.1224752883895658; 0.010219248113360465 0.024494938221776053 -0.06523087652678894; 0.008933956783375415 0.025187791371912693 -0.07111692918243703; 0.002176925118781653 0.0071173534782366975 -0.021827933120240874; 0.002362473526910239 0.008840059044501707 -0.027818688733753313; 0.00012653424739276906 0.0006902615493430614 -0.0026073470219958915; 0.0004792241572645401 -0.0008634770048450064 4.8584571127433386e-5; -0.0011102953105657427 0.0008309279887691291 -0.0004297829949431498; -0.00010759480707609554 0.00031136560918702767 0.00024174272916805935; 0.0006889987715855107 0.001190412288920094 -0.00043441960565814247; 0.00017731877802452896 0.00033420710609726096 -0.0003900657937867453; 7.773415780085798e-5 0.00016626657706640246 -7.71910163353673e-5; -0.0005187929315051286 -0.0012413094952250132 -0.00013302419195760013; 0.0008140894265830982 0.0008551197624111014 0.0001160599801750175; -0.0035966546791942867 0.00035352762174267684 0.00024128615533785863] %
+
+Mass Used: 88.2412251519927 kg
+Launch C3: 96.46434585693436 km²/s²
+||V∞_in||: 0.0005838059188079729 km/s
diff --git a/archive/ES_0.5579692837660463 b/archive/ES_0.5579692837660463
new file mode 100644
index 0000000..283cc3e
--- /dev/null
+++ b/archive/ES_0.5579692837660463
@@ -0,0 +1,22 @@
+archive/ES_0.5579692837660463---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:36:22.217
+Launch V∞: [7.996699935261514, -5.6676763001761605, 0.3249940348810319] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.709362779299114e-6, -1.986825465250139e-6, -0.0001298172053714385] km/s
+ V∞_out: [0.0001249975762734044, 4.1961786062445204e-5, -4.5775927461352504e-5] km/s
+ time of flight: 1.8749577787430438e8 seconds
+ arrival date: 2030-04-22T07:45:59.217
+ thrust profile: [0.30631881805114086 0.00742238978259029 -0.08595082963599392; 0.11111903902997787 0.07375719216199005 -0.11354400643757628; 0.07420267287041404 0.07922260801279817 -0.13806541208903608; 0.04206360650022831 0.06082026154947645 -0.12037394915947493; 0.024034604884558424 0.044636948444355944 -0.09779554851900714; 0.01589761583260209 0.03409880282408187 -0.08272279213578158; 0.0060311760964697585 0.015161736081884772 -0.0411639249078296; 0.006768860383653574 0.0217518086450572 -0.06117675865271573; 0.001192420934198127 0.007042755400742343 -0.022777173194133537; 0.0020552013769489542 0.008286621956290282 -0.02631677175222075; 0.0017399770744387975 0.0008401292217004784 -0.002736370673415327; -0.0017750574715635881 0.0014109241028949946 0.00012937263545826912; -0.00260052493486215 -0.002962432854453189 0.001095701125218373; 5.708856837369084e-5 -0.0014637569285718707 -0.000570367052376692; 0.00033824458277012867 0.0012176488008862744 -0.002647135063031346; -0.00025387321767873967 4.7315971340617345e-5 0.002692449371918238; -0.0015244048644870254 0.0010658733151736835 0.003343902572498025; -0.0003455205392975738 -0.0004060952715057083 0.0012743620425062713; 0.001232933306468587 0.0020388783776519774 -0.0033344336978628005; 0.0036876489804156982 0.0007830797251362154 -0.004720152086135486] %
+
+Mass Used: 89.94108160514725 kg
+Launch C3: 96.1753856208983 km²/s²
+||V∞_in||: 0.00012986067508121717 km/s
diff --git a/archive/ES_0.557972122220901 b/archive/ES_0.557972122220901
new file mode 100644
index 0000000..1af4fa2
--- /dev/null
+++ b/archive/ES_0.557972122220901
@@ -0,0 +1,22 @@
+archive/ES_0.557972122220901---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T04:10:36.146
+Launch V∞: [7.992123708356855, -5.814012855906283, 0.12449759501951244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.1454639017039396e-7, -4.107485361920637e-6, 8.146077145438095e-7] km/s
+ V∞_out: [-6.498264895144758e-7, 2.4853358504665275e-6, 3.333220166760679e-6] km/s
+ time of flight: 1.8492597915396902e8 seconds
+ arrival date: 2030-03-24T12:30:15.146
+ thrust profile: [0.22309922964280265 0.0010064430951034964 -0.06857400037660741; 0.05782171882325819 0.03461670844931036 -0.06457203801472367; 0.0597458767067167 0.060863787986861026 -0.11846161572706897; 0.03929996877758022 0.05408833362511209 -0.1163411585534494; 0.025281970995827404 0.04286134559515963 -0.1017925138566046; 0.013035065287468011 0.026349374229948028 -0.07166330424548786; 0.01093121762108484 0.027690970742419236 -0.07804562855364287; 0.008218747407342866 0.020429480966110997 -0.06111614050999188; 0.008933146001651236 0.020527574377418693 -0.06405243380111887; 0.004444769100359345 0.014790090220798616 -0.04991766773927727; 0.0007040724597670375 0.0036027749822219604 -0.014057863472408966; 0.0001458043656442432 0.0002092453760783458 -0.0025078984728658803; 2.2551142596742514e-5 -0.0017189639960799637 9.48578789243741e-5; -0.0002709179536872961 -0.000595023188570144 0.0002342988861708255; -0.0008201621966561765 -0.001706635392451706 0.0012852364789697282; -0.0008454074438195849 -0.0025376547515120747 0.00033581338545859486; -0.0007378810612948952 -0.002205414946706446 -0.001857649499438356; -0.00021148174541883356 0.0025181073032297654 -0.003256101485674936; -0.00011177672284406353 9.937909496094592e-5 0.0022386670091200603; 0.00032419634155234555 0.0011216911526794136 -0.0004920148266350236] %
+
+Mass Used: 81.0958046190326 kg
+Launch C3: 97.6922865094889 km²/s²
+||V∞_in||: 4.207953236026977e-6 km/s
diff --git a/archive/ES_0.5579721504778156 b/archive/ES_0.5579721504778156
new file mode 100644
index 0000000..d7bcf90
--- /dev/null
+++ b/archive/ES_0.5579721504778156
@@ -0,0 +1,22 @@
+archive/ES_0.5579721504778156---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T18:45:51.128
+Launch V∞: [7.907537280596833, -5.558190410914146, 0.110362953261877] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0055232155819228265, -0.034252581965187184, -0.035219285769060506] km/s
+ V∞_out: [0.008527675918289408, -0.00798028469409283, 0.04801480433131356] km/s
+ time of flight: 1.8749577784486315e8 seconds
+ arrival date: 2030-04-20T20:55:28.128
+ thrust profile: [0.5504935978609281 0.00922579863385983 -0.15246913324859482; 0.15560351278414297 0.09459282232316203 -0.160446319507374; 0.037646570413461256 0.03935206487461229 -0.0760596744341549; 0.030597738928575882 0.04290205453311279 -0.09270820192176789; 0.014462074052948278 0.02565062271692035 -0.062337635270675935; 0.020792738346670055 0.04403740288449367 -0.11205850408618837; 0.008283958452522548 0.021373619128551975 -0.05994543956852645; 0.005508092274541839 0.016683789350281204 -0.048964344559497885; 0.007075170498741769 0.024133601940832524 -0.0721422324721421; 0.0005337153715978998 0.002435789234648258 -0.008533587475081981; 0.0001523732294825317 0.0006206667603329914 -0.0022576980139575003; 6.683594441300057e-5 5.0937981202110586e-5 -0.0006707827305640154; 7.837382198485655e-5 0.00026698675368006544 -0.0012926194911888212; -0.00018165816927094873 0.0004074483155244811 -0.00034229046272062774; 0.0004391689833683577 0.000253629421311367 0.0001601330645835732; 0.0008903624424749095 -0.0001411491919159287 -0.0023203816236815962; -0.0010417276626713881 -0.0001536915987057293 0.0010711948993870565; -1.4407196354710858e-5 0.0009104293765631395 0.0001427701405269441; -0.00013214765589612715 -0.0005679195117614624 0.0003232998243066789; 0.000332924260020733 -8.144651983676564e-5 -0.0009962008359681034] %
+
+Mass Used: 105.93113781893817 kg
+Launch C3: 93.43480646945942 km²/s²
+||V∞_in||: 0.04943827840579614 km/s
diff --git a/archive/ES_0.5579742015361007 b/archive/ES_0.5579742015361007
new file mode 100644
index 0000000..46e14cf
--- /dev/null
+++ b/archive/ES_0.5579742015361007
@@ -0,0 +1,22 @@
+archive/ES_0.5579742015361007---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T18:37:35.300
+Launch V∞: [7.829809881888154, -5.8507855700338345, 0.073588755543928] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.5201093600753834e-5, -2.1262999434174632e-5, -0.0013355275009632002] km/s
+ V∞_out: [0.001257005586654514, 0.0004282710045048528, -0.0001958345988389249] km/s
+ time of flight: 1.811297817544177e8 seconds
+ arrival date: 2030-02-06T04:27:16.300
+ thrust profile: [0.3671885077599352 -0.007893791718822452 -0.11299040622469989; 0.08534807197560375 0.047723464422800975 -0.09211524696319802; 0.09941730718657477 0.09524973324633973 -0.19031295953561483; 0.03777697274013195 0.04604714524904377 -0.10763443993550817; 0.029838818922420234 0.04526890719024147 -0.11515296984025494; 0.011998211988378745 0.021024741566674828 -0.05990126114186747; 0.015416947404296416 0.0325370317251882 -0.09544505853711574; 0.006679200833244801 0.015321774080593922 -0.049381606020669835; 0.0038887595173968705 0.009825016166720815 -0.033849444800789184; 0.0017445883785681248 0.004939327891312054 -0.017504910056123237; -1.6223180076900112e-6 0.0013803236589063656 -0.004927156235065043; 0.0003099522041489243 0.0010015069651862242 -0.0038551299693012566; -0.001143448603303661 0.0006073706805987772 -0.002374340206506656; -2.1189993293921957e-7 0.00027697390710757267 -0.0008060360013689304; 0.00025390543600888613 -0.00010927166008004702 -0.0008128717064740587; -0.0009883250452407994 -0.0004447006336932192 0.0007793624838475525; 0.0009437745069618845 0.001911708602089676 -0.000738668566704281; 0.0010100405531664194 -0.0018095513891301053 -0.0022264992543374407; 5.972932917698052e-5 3.2317496751725335e-5 -0.00015482138247914956; 0.00017641372850097167 0.001392848748459323 0.0008738951838149914] %
+
+Mass Used: 93.63556083728054 kg
+Launch C3: 95.54302987797203 km²/s²
+||V∞_in||: 0.0013359344729786046 km/s
diff --git a/archive/ES_0.5579835933390838 b/archive/ES_0.5579835933390838
new file mode 100644
index 0000000..8184b6e
--- /dev/null
+++ b/archive/ES_0.5579835933390838
@@ -0,0 +1,22 @@
+archive/ES_0.5579835933390838---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T01:38:37.661
+Launch V∞: [7.863911568388718, -5.665139910575962, 0.11970012837991244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8339533774270415e-6, -1.935891920110652e-5, 2.8843247981302872e-6] km/s
+ V∞_out: [-3.047839731419347e-6, 1.1674220923290858e-5, 1.552449099211633e-5] km/s
+ time of flight: 1.8749577787488282e8 seconds
+ arrival date: 2030-04-22T03:48:14.661
+ thrust profile: [0.5189110269394859 0.013553014672111629 -0.14725362026199412; 0.0927539588930025 0.05823902709549758 -0.09938482121159727; 0.0463995016007647 0.047865931541482026 -0.09376880892158912; 0.06577211497072132 0.09360511518074788 -0.19019313120685427; 0.01779688285074476 0.030164640219808272 -0.07459423135658053; 0.010940979071879402 0.0220442245461392 -0.059651779804582104; 0.007355894294175867 0.017801487231683077 -0.05213903904681325; 0.004386192519137163 0.01248373157359774 -0.03851230314853894; 0.003685812193394689 0.01244370172487657 -0.040990668415847004; 0.0009132648848566368 0.003511692257278036 -0.01217400381874736; 0.0006004919336679937 0.0031126427746287983 -0.010679754371271586; 0.0003166994471537202 0.0011734260795378368 -0.004672771834271598; 0.0017828588852024903 0.0010920908995601401 -0.003677327903195313; -6.450178359003803e-5 0.0015591409058505156 -0.004206571837568707; 0.0036077617617308547 0.001914696051168024 -0.0027799727519118044; -0.0005161370920804496 0.007346570561676593 -0.0020491912817886928; 0.0014531912764704329 0.0030889782676691777 -0.007700553191535564; 0.003033164088727949 -0.00206794272840321 -0.0013913142261268556; 0.0018454679342188951 -0.001261938323048729 -0.0021957764783232764; 0.0008616110744856885 0.0016348056738107412 -0.0019584199319431896] %
+
+Mass Used: 102.94360524725698 kg
+Launch C3: 93.9492434825727 km²/s²
+||V∞_in||: 1.965834344919877e-5 km/s
diff --git a/archive/ES_0.5579864108927577 b/archive/ES_0.5579864108927577
new file mode 100644
index 0000000..6807eef
--- /dev/null
+++ b/archive/ES_0.5579864108927577
@@ -0,0 +1,22 @@
+archive/ES_0.5579864108927577---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T23:44:59.782
+Launch V∞: [7.811942983826804, -5.706686813209137, 0.18766931029810316] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.783596347213593e-10, -9.420891391687493e-10, -1.2132518885883392e-9] km/s
+ V∞_out: [1.1996704726938887e-9, 3.5275213991882847e-10, 4.1302009174844865e-10] km/s
+ time of flight: 1.858489712157486e8 seconds
+ arrival date: 2030-04-02T00:27:50.782
+ thrust profile: [0.513955243647707 0.002641559906381318 -0.12829922118812917; 0.11334793344582843 0.07355001365743971 -0.11417663447310467; 0.06755615163366281 0.07209438292459354 -0.12499045497338937; 0.05103719426116072 0.0748097633835615 -0.14354650628110194; 0.02984875792452331 0.05393234400603973 -0.11597589075348366; 0.017197497286527134 0.03736709979794793 -0.0864709712906453; 0.009295358320865402 0.025632713816334706 -0.06336199222631295; 0.003969030308131214 0.012168335290567116 -0.0335288201248422; 0.0020103768173953636 0.007408889539314115 -0.021113793726720474; 0.00022984183054401477 0.0007665447561262622 -0.003086329418403614; 0.00020404605474105998 0.0007202499996179655 -0.0038594809278434178; -7.558828784375433e-5 0.0007417396636410322 -0.0005963664853742953; -0.00014942443345106315 -0.00024569915594337415 0.0008320113416281922; 0.0005714702465121441 -0.0017345447982178679 0.0018274025700060652; -0.000285085876311757 -0.0002219891236137919 0.0013429285301564974; 0.0005868853409488518 -0.0003091513983386648 0.0029552457559069885; -0.002653440284942788 0.0006977129086818067 0.0019563819396855326; 0.0010129339728936668 -0.00040920389216052224 -0.0005815267456197372; -0.00010940487331689623 0.0018805974824447312 0.00254039902081896; 0.0003491224741528156 0.0025691720278506252 0.0001420259249406429] %
+
+Mass Used: 104.82111991112924 kg
+Launch C3: 93.62794733664366 km²/s²
+||V∞_in||: 1.6791914379611943e-9 km/s
diff --git a/archive/ES_0.5579870845809648 b/archive/ES_0.5579870845809648
new file mode 100644
index 0000000..09a3045
--- /dev/null
+++ b/archive/ES_0.5579870845809648
@@ -0,0 +1,22 @@
+archive/ES_0.5579870845809648---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T13:35:09.227
+Launch V∞: [8.165946181530103, -5.61722389346617, 0.16057721026952965] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003224979231473671, -0.0001651019911185545, -1.3316453562673955e-5] km/s
+ V∞_out: [0.0002659219547495078, 0.00016013095647526832, -0.00020277389530272798] km/s
+ time of flight: 1.8749577788641068e8 seconds
+ arrival date: 2030-04-23T15:44:46.227
+ thrust profile: [0.19208850536007435 -0.0042129009348028145 -0.06431996915579873; 0.10972022421736911 0.05789266450869254 -0.13167716580608405; 0.0328807615548204 0.027955621314729756 -0.07192119922183828; 0.017363611656906138 0.01896977226281961 -0.05666506328334201; 0.014762226114880834 0.019317813804849055 -0.06408199200636021; 0.020669103864335892 0.03142409103386109 -0.11188683825144616; 0.0047925348307282095 0.008252111877034136 -0.03319292495680655; 0.0037198392853274084 0.007586466390243844 -0.032352716980852986; 0.010802814053621407 0.04437292085166349 -0.18245737268442977; 0.0033623942300622517 0.007355682650433965 -0.030240956125887817; -0.0007324166910470801 0.001332069211932551 -0.014926960276605563; -0.0005891197226975054 0.0017538276208137731 -0.005433993791966234; 0.00010906891267679467 0.00047037329211281577 -0.00012876609941057915; 0.0007345194929457113 -0.0012708070508780952 -0.0023738833580131975; 0.00018020224538471108 0.00028010291317193516 -0.001099382188482598; 0.0006177881285270128 0.0005031057457147306 0.0006367618316693441; 0.0019232852519654136 0.000441385287260464 0.0007647810278181705; -0.0008354482802337738 -0.002428008257989337 0.002004930308834329; -0.002591288796669773 -0.002824404598334141 0.0009566051856562132; 0.0021698668534988847 -0.0013086584871755515 0.0013229660663126692] %
+
+Mass Used: 77.79187830611 kg
+Launch C3: 98.26166634943124 km²/s²
+||V∞_in||: 0.00036254779800898415 km/s
diff --git a/archive/ES_0.5579910747170208 b/archive/ES_0.5579910747170208
new file mode 100644
index 0000000..73cfa4e
--- /dev/null
+++ b/archive/ES_0.5579910747170208
@@ -0,0 +1,22 @@
+archive/ES_0.5579910747170208---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:36:23.747
+Launch V∞: [8.041203831321196, -5.673853308063105, 0.2950483295376322] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.142729974273452e-10, -8.095936463284019e-10, -1.2403687906154064e-9] km/s
+ V∞_out: [1.0477854809566773e-9, -9.446750777553148e-10, 3.566115482061257e-10] km/s
+ time of flight: 1.874957778738007e8 seconds
+ arrival date: 2030-04-23T09:46:00.747
+ thrust profile: [0.28889745263402705 0.002954564464735834 -0.062233333034393025; 0.08734058543746966 0.051191516608512254 -0.09884671162464682; 0.04153795270103336 0.03890001292179963 -0.08703483828960289; 0.0393624599729841 0.0484497374739119 -0.12219410512289189; 0.0324116237174953 0.0487014674603607 -0.13686742929573487; 0.019595114715587534 0.034301601465897696 -0.10491232713465837; 0.011955344729711449 0.02554546517394314 -0.0801723175099141; 0.004174436524443034 0.00933641137297031 -0.034096384088418634; 0.0008595606701938094 0.0020833452393010246 -0.010598207357115273; 0.0015489355146432252 0.004024348332895961 -0.017572411999913197; 0.001039202962864555 0.002915599773427537 -0.014829030164294375; 6.296074537711537e-5 0.00020968180528877162 -0.0037901722402374095; -0.002278638812643493 -0.0020535787600647268 0.000496206766169779; -0.0003464392903055831 0.0005597489213421021 0.003644095243113132; 0.004230922193378595 0.007493500270265562 -0.0011341362017075105; 0.0008894951403538396 -0.003231104760142332 0.00091501053992828; -0.0033262305779926706 -0.0007374369562096431 0.0039225356901119125; 0.0006036027101392254 -0.0009724291056757649 0.0033323465108887848; 0.006870305954634327 0.002995500501874228 0.0010925125664119548; -0.002217245316914965 0.0003802493598940328 -0.0006436405031613221] %
+
+Mass Used: 85.5026142154793 kg
+Launch C3: 96.94062393503627 km²/s²
+||V∞_in||: 1.6035235964202144e-9 km/s
diff --git a/archive/ES_0.5579924762725468 b/archive/ES_0.5579924762725468
new file mode 100644
index 0000000..e50cfe9
--- /dev/null
+++ b/archive/ES_0.5579924762725468
@@ -0,0 +1,22 @@
+archive/ES_0.5579924762725468---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T16:39:42.587
+Launch V∞: [7.9397687647059305, -5.584710911930495, 0.15934418912504567] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6329827175668092e-5, -1.4092247490415426e-5, 9.870158241122893e-6] km/s
+ V∞_out: [-3.13423413964694e-6, -2.3240994138821233e-5, 1.1220336072057134e-6] km/s
+ time of flight: 1.8749577787637228e8 seconds
+ arrival date: 2030-04-21T18:49:19.587
+ thrust profile: [0.5317113059700266 -0.014336324288032005 -0.1298660039126587; 0.03191442996220416 0.0194138924849592 -0.03608270930973039; 0.07466443991474174 0.07379230865611776 -0.1411375880875747; 0.053060155470312335 0.07305617089013446 -0.14717121506845554; 0.028009512807130328 0.043976946519013856 -0.11803768083259059; 0.01077715691480663 0.023328628867827095 -0.06427951865200485; 0.007296854612971479 0.01841775276843737 -0.05717126169559014; 0.005108179955262722 0.012872249233647593 -0.0415026981043131; 0.0042278741179159795 0.00984803008616226 -0.03345536105831749; 0.002888476694382911 0.007269175677339106 -0.0203767389392125; 0.0010228220138745095 0.0029157373372679907 -0.010144205832466665; 4.045533628821234e-5 0.0010863810547956094 -0.005040535085452429; -0.0008601291212626335 0.0008423907998359915 -0.002958112807632773; -0.0033415389758263622 0.00048002712271294815 0.002764357216635107; -0.0011422521406882773 0.000393388905307864 -0.0012320150195961397; -0.0013259473569698233 0.0001808805885112144 -0.0015283992991297524; -0.0003799086388137805 -0.0006194493558027052 -4.303151705417271e-5; 0.0051154215377979435 0.0010369384427461313 -0.005054448769561654; -0.005333354089704843 -0.004702227217729872 0.0001485396065989855; 0.0022689734583556456 0.0021868093030082345 -0.004467150085523208] %
+
+Mass Used: 101.17438728288471 kg
+Launch C3: 94.25431457744341 km²/s²
+||V∞_in||: 2.3720765557273106e-5 km/s
diff --git a/archive/ES_0.5580003426955271 b/archive/ES_0.5580003426955271
new file mode 100644
index 0000000..42a2bf7
--- /dev/null
+++ b/archive/ES_0.5580003426955271
@@ -0,0 +1,22 @@
+archive/ES_0.5580003426955271---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:38:13.457
+Launch V∞: [7.71805770052733, -5.742970691312375, 0.41907877012189615] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.870829305123059e-10, -8.587176798050595e-10, -1.2857878319189027e-9] km/s
+ V∞_out: [1.1147733718853208e-9, -9.85409121764542e-10, 5.014855532776613e-10] km/s
+ time of flight: 1.8749577787489814e8 seconds
+ arrival date: 2030-04-23T21:47:50.457
+ thrust profile: [0.717934323104759 -0.013471036726563473 -0.2080746970669401; 0.056626993169836055 0.03099226914678527 -0.06917864071699362; 0.023328209107715457 0.020694886015130556 -0.05244530650012631; 0.024976537138179215 0.02726236821865304 -0.07819744830058134; 0.0239395523366526 0.031800417215707755 -0.09880505014192684; 0.0222196033029608 0.03417097148434119 -0.111703623788035; 0.007881301910253307 0.01515935644106103 -0.05910527731593039; 0.011190119174775087 0.021314218314256606 -0.08073409001026867; 0.00582210892653087 0.012241903977660715 -0.04801569314828091; 0.003119289499894062 0.008425684913944884 -0.03409893496918177; 0.001364125308003873 -0.0007002562166305516 -0.0012685710174953858; -0.00013935682851654778 -0.0010258245329638675 -0.0005144231023635665; 0.00022756868827746287 0.001103453415395622 -0.007539326816034423; 3.363226110967622e-5 -0.00022541967519052884 -0.002387831756867094; 0.0004147538025109424 0.00011864327140745335 0.00020294122100734426; -0.000865639759943099 -0.00027105631770641466 0.0014407695703522795; -0.0005458560307631272 1.793624106581506e-5 -0.0011479297816184286; -0.0004847191492986777 -0.001589544943674174 -0.0029989820226423145; 0.000938312554798395 -0.0025078624331877747 -0.002320729276139891; -0.0018666198717207914 0.001181983179732636 0.0045135085294501645] %
+
+Mass Used: 110.10016787931227 kg
+Launch C3: 92.72575404550903 km²/s²
+||V∞_in||: 1.6210787098463026e-9 km/s
diff --git a/archive/ES_0.5580006653721187 b/archive/ES_0.5580006653721187
new file mode 100644
index 0000000..55789f6
--- /dev/null
+++ b/archive/ES_0.5580006653721187
@@ -0,0 +1,22 @@
+archive/ES_0.5580006653721187---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T00:11:44.215
+Launch V∞: [7.880336712961675, -5.69555919793861, 0.1923203050666751] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.8188597184160405e-5, 4.094271230839846e-5, 0.0029112994072893247] km/s
+ V∞_out: [-0.0026152100677445935, -0.0008453724363208596, 0.0009579163723892344] km/s
+ time of flight: 1.8749577787488237e8 seconds
+ arrival date: 2030-04-22T02:21:21.215
+ thrust profile: [0.43241971212156205 0.012962505199096296 -0.11855238217199886; 0.10967985033485594 0.07146979894451135 -0.11089441037303324; 0.0617822464494258 0.06606158709394676 -0.11507081405474338; 0.05701603976400959 0.08383553203716443 -0.1590104153282754; 0.03270213237974334 0.06079926870985558 -0.12846069475783384; 0.018447145398978265 0.041565723434450495 -0.09675474299182141; 0.003625824487642004 0.0098203292647272 -0.02558295138285159; 0.0031797072160807136 0.009936099545343172 -0.027190829858242612; 0.0012547843713395467 0.005774848088098009 -0.016066818737071706; -1.0745265726597728e-5 0.0010766927384770286 -0.004617939564411504; 0.000493800199229068 0.001896657439075472 -0.00623976927734624; 0.0008852534956069742 6.884732087340147e-5 -0.0008846482261251745; -0.0020613413352682576 -0.0031435482391406868 -0.0027091451319459746; -0.0014327371261987892 -0.0004016890138802993 -0.00027519798619583466; -0.0002498976215933339 -0.0008782359941769442 0.00026388733596333113; -0.0028230159943986952 0.004742507981990768 0.00041136193026826916; 0.006964789740954639 0.0036671954250516877 0.0012661254429590608; -0.0019593420620970846 -0.00019220990824460972 2.332105614322698e-6; -0.0007239159048461178 -0.001132562500246221 0.004180664949032631; -0.0003538921213890756 -0.0014739863966677226 -0.008802455507428022] %
+
+Mass Used: 99.30692734554714 kg
+Launch C3: 94.57608838661565 km²/s²
+||V∞_in||: 0.0029121686862914726 km/s
diff --git a/archive/ES_0.5580112607197478 b/archive/ES_0.5580112607197478
new file mode 100644
index 0000000..b100607
--- /dev/null
+++ b/archive/ES_0.5580112607197478
@@ -0,0 +1,22 @@
+archive/ES_0.5580112607197478---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T01:36:00.739
+Launch V∞: [8.029638088020931, -5.808609828582066, 0.18627611544201172] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.489376416708524e-7, 2.8068858261651945e-6, -6.920982854900964e-5] km/s
+ V∞_out: [-2.9345200785590077e-6, 6.920003753795822e-5, -5.397078768541076e-7] km/s
+ time of flight: 1.8203098439803156e8 seconds
+ arrival date: 2030-02-18T21:45:44.739
+ thrust profile: [0.2265260510265123 -0.022631413732256647 -0.08049361912205966; 0.05318430625799469 0.022242007694472467 -0.07348875240507227; 0.0384559098060428 0.02617222753468199 -0.09544876096703403; 0.03364571838463772 0.02841242647049283 -0.11866368002850597; 0.02650541215567618 0.026040702825297853 -0.12246174460730991; 0.019668763002813387 0.02211012185641821 -0.11430918688585065; 0.012168097791951335 0.015983545261268 -0.08833957367942889; 0.006195583964015215 0.00885600343959466 -0.050776841628071; 0.004239208633196926 0.0041470190820581485 -0.03186316334503501; 0.0018962371394640883 0.002677073075450032 -0.018919188538721942; 0.003351147904692759 0.0029679323070507485 -0.02903378053280686; 0.0023985553613604187 0.0030470724665322283 -0.025625698273297165; 0.0019599886442748966 -0.0003942176857746205 0.0001847596777583381; 0.00014084138492915152 0.0007466992927193784 0.000891477741490392; -0.00023656807008890933 -0.002162358272951767 0.0006574296521193224; -0.0007168311439346342 0.0005517697581273011 -0.0012248623221998269; -0.0009788724043218483 -0.0010923391711459415 -0.00034660848718466965; 0.00015268443627091205 -0.00077802171838521 -0.0014746629390872711; 0.000598050065925103 -3.44380840746517e-5 -0.00039459212934124326; 3.3090606832879353e-6 0.0004057035087341745 -0.00048497261132769134] %
+
+Mass Used: 77.88968476023456 kg
+Launch C3: 98.24973475648079 km²/s²
+||V∞_in||: 6.926817826989926e-5 km/s
diff --git a/archive/ES_0.5580230003087602 b/archive/ES_0.5580230003087602
new file mode 100644
index 0000000..c842410
--- /dev/null
+++ b/archive/ES_0.5580230003087602
@@ -0,0 +1,22 @@
+archive/ES_0.5580230003087602---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:33:12.795
+Launch V∞: [7.905970076486293, -5.746141685628589, 0.0557166279907141] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.952373096125046e-7, -6.265874276895671e-7, -5.909104944291496e-8] km/s
+ V∞_out: [5.0539765317365076e-8, -2.5868619548590057e-7, -6.965904660787388e-7] km/s
+ time of flight: 1.8749577787370914e8 seconds
+ arrival date: 2030-04-23T19:42:49.795
+ thrust profile: [0.4273640932772292 0.006857277441951136 -0.11937852455618535; 0.07090565441587787 0.04398923723094339 -0.0806046737707436; 0.03693940164971571 0.03580467792449022 -0.07665903023402658; 0.02462083423168634 0.0325239893622199 -0.07690985235194582; 0.016903571024417724 0.028145881805666878 -0.07196292384147736; 0.025569653629203368 0.05066307590075793 -0.13737073070705497; 0.012925252423518913 0.03096222178727998 -0.09286292797272704; 0.0031239238862216224 0.008270617229519548 -0.027898985475637225; 0.009818806659536206 0.036584363354415256 -0.11701997392196314; 0.0001354989113704182 0.001625782519655326 -0.005097168810363315; 0.0005679416992760464 0.0018840910952826141 -0.007823002787515094; 0.003434326869401676 0.00022999305674940027 -0.0022368593775527195; 0.0004929813671275767 -0.0014280311953344515 0.0005248073961282647; 0.0002239471113883994 -0.0008501962494143863 0.0021687245229689766; -0.001490062458259354 -0.001075307661596601 0.0034722524838794715; -0.0006045354461268406 0.00021023992556562976 -0.0011079112744671517; 7.12437864031854e-5 0.0025889333061142232 0.0029183062203487235; -0.0024207887151821215 0.0007784665938766391 0.001024718735934536; -0.0018707975956222126 -0.0003750693146996713 -0.00022344890367137672; -0.0018354055018641124 0.000317885032069208 -0.00255092577894363] %
+
+Mass Used: 93.79410015209578 kg
+Launch C3: 95.52561146424989 km²/s²
+||V∞_in||: 7.431797141826628e-7 km/s
diff --git a/archive/ES_0.5580270263508513 b/archive/ES_0.5580270263508513
new file mode 100644
index 0000000..df55be5
--- /dev/null
+++ b/archive/ES_0.5580270263508513
@@ -0,0 +1,22 @@
+archive/ES_0.5580270263508513---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:39:03.297
+Launch V∞: [7.991051971953029, -5.739385092551873, 0.14504496349085155] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6262763671040854e-9, -1.2047259156638477e-9, -1.674313322755702e-9] km/s
+ V∞_out: [3.692435029099801e-10, 7.246183938332884e-10, 1.719426895485267e-11] km/s
+ time of flight: 1.8356139192957187e8 seconds
+ arrival date: 2030-03-07T12:55:34.297
+ thrust profile: [0.3208901375896938 -0.009548111588901556 -0.10461163846308306; 0.04860294646347258 0.026256590362818275 -0.05575374257516875; 0.040689435942531785 0.0357286754917556 -0.0829673920723796; 0.0483547144510236 0.055518372828884346 -0.1425781566466011; 0.031454267328791634 0.04410230682067446 -0.12555723583547423; 0.029583200612399746 0.04996636029270051 -0.15167969895104028; 0.0065751944722600465 0.012199099444058604 -0.042706465671879044; 0.0034848205137397734 0.007441820101841853 -0.02766986782082856; 0.0011418437311996683 0.0027708616539821166 -0.012116261527171292; 0.004692601208926962 0.011745684345385561 -0.046312358678953995; 0.005132208415640435 0.010365466700027274 -0.04487508925619904; 4.9690931705599764e-5 -0.0008711661838220147 -0.0006935290451327005; -0.00015682635940007938 0.0008737986723983575 -0.00138575143603855; 0.0001246324489706708 -0.0005552866858292669 -0.0002951214645509259; -0.00036167893279021664 0.0004157251382829136 -0.001378757704944992; -0.0032918655298450443 -0.0002763985420604682 0.0005527218890626362; 0.0019256339273302993 -0.0004945702914805736 -0.00048666455616861977; 0.005318847892187124 -0.004551690655764375 -0.002545913167370856; 0.0010438508868655285 -9.611663752447244e-5 -0.0012350660429239586; 0.004765342723624219 -0.002351269540348987 -0.00042620176698725113] %
+
+Mass Used: 86.2570004897716 kg
+Launch C3: 96.81849090049514 km²/s²
+||V∞_in||: 2.626683166434543e-9 km/s
diff --git a/archive/ES_0.5580271658943081 b/archive/ES_0.5580271658943081
new file mode 100644
index 0000000..4a17958
--- /dev/null
+++ b/archive/ES_0.5580271658943081
@@ -0,0 +1,22 @@
+archive/ES_0.5580271658943081---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:23:01.596
+Launch V∞: [7.965699192345318, -5.751051612369484, 0.1766170245430839] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.753056422982728e-9, 2.329376391568534e-8, -4.523289433349598e-9] km/s
+ V∞_out: [1.1093471582803819e-8, 2.268147374631063e-8, 5.977346914254566e-10] km/s
+ time of flight: 1.8749577787493256e8 seconds
+ arrival date: 2030-04-24T00:32:38.596
+ thrust profile: [0.3075325150087347 0.0028566494335152087 -0.09545795301968364; 0.10779559850534745 0.06315044247302623 -0.1183949010293882; 0.041773753302249306 0.03825855892867975 -0.08494898543702559; 0.03479563136069729 0.04198259684162534 -0.10342272621668368; 0.02837418429561319 0.042359432104691154 -0.11438914715112279; 0.019010668622141392 0.03357201331993005 -0.09890612275154025; 0.011898437589840227 0.026003890430013974 -0.08446794210682361; 0.003269877156010057 0.007620453312157388 -0.025627281509836935; 0.0029625190084792935 0.0076005678948078605 -0.027345788317218928; 0.001667990983858612 0.004686087931604185 -0.018187102539610086; 0.002208332199322067 0.004575746011788279 -0.018556518791084296; 0.0007198981126258821 0.0011704944814742706 -0.0024740656212168567; -0.0009991172596141976 -0.0007819964396805017 -0.0034694339953820763; -0.00208499962113069 0.00034825329309584596 -0.0016433008087045372; 0.00019198513823167436 0.0011622286011222784 -0.00026537634581336785; -0.0004518384252574564 -0.0003266644549603099 -0.0028176619109654523; 0.004074567436835334 0.00039441353338184984 -0.0028400513237189927; 0.007033649487808898 0.011180721570942978 -0.012567411763340084; -0.0006029237137421429 0.0023499734040111193 -0.006968779032341048; 0.00017443438379979121 -0.0032560523411350227 -0.0031133313712631227] %
+
+Mass Used: 87.77580778420224 kg
+Launch C3: 96.55815184442696 km²/s²
+||V∞_in||: 2.441633147840927e-8 km/s
diff --git a/archive/ES_0.5580424180879292 b/archive/ES_0.5580424180879292
new file mode 100644
index 0000000..9d06542
--- /dev/null
+++ b/archive/ES_0.5580424180879292
@@ -0,0 +1,22 @@
+archive/ES_0.5580424180879292---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:17:49.393
+Launch V∞: [7.713479255696925, -5.84480215486476, 0.31264595096460523] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.135773077838423e-8, 5.044983049376632e-7, -1.107770554105055e-5] km/s
+ V∞_out: [-4.6765815065139465e-7, 1.1071081997524066e-5, -1.325416734179067e-7] km/s
+ time of flight: 1.8103504374759898e8 seconds
+ arrival date: 2030-02-05T21:48:32.393
+ thrust profile: [0.6161965674267843 -0.043989576699878526 -0.20045343179810665; 0.040384988055687715 0.019259440655971523 -0.04791192394049947; 0.03970874981877588 0.030984420351116166 -0.08251281305029175; 0.03552571331035219 0.03617027981624334 -0.10717350714869757; 0.028632771030996266 0.03498456072963107 -0.11442925294555016; 0.024437904210895933 0.03438022159692365 -0.1214856634454686; 0.013237374932320717 0.020398267705256618 -0.0805974685273887; 0.008908013591018291 0.014738902745460294 -0.06396765279920595; 0.002412784353109332 0.0042883166296995125 -0.020047191819372444; 0.00632846124878553 0.012386987949246375 -0.0575549444731886; 0.0010180533245961892 0.00268022934273711 -0.013385989451694625; 0.00039643607165173295 0.001482204824832791 -0.008560428747565966; -0.0009091391059266726 9.720219115211135e-5 2.5645350667677e-5; -0.0001622216823975497 0.00041759158326396006 -0.0007900747636909909; 0.00024580763404551126 0.0004052774261277796 -0.0008387919113463332; -0.0007423940991388507 0.0011332762081997553 -0.0020327433405804077; 0.0001988343866928693 -4.341157387008441e-5 -0.0008901243304089268; 5.893222399053959e-5 -4.581793296678637e-5 -0.00023075724184693945; -0.0013001634903975978 0.0011296771556421085 0.00015768931065471238; -0.0010878335675833062 0.0006801443196660982 -0.0013573640063793166] %
+
+Mass Used: 104.13235973789097 kg
+Launch C3: 93.75722194823311 km²/s²
+||V∞_in||: 1.1089417050487769e-5 km/s
diff --git a/archive/ES_0.5580456078383099 b/archive/ES_0.5580456078383099
new file mode 100644
index 0000000..18709d6
--- /dev/null
+++ b/archive/ES_0.5580456078383099
@@ -0,0 +1,22 @@
+archive/ES_0.5580456078383099---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T17:38:59.873
+Launch V∞: [8.020105637163196, -5.75818975416202, 0.09175250908961656] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0927299424523265e-6, 1.7450910174349154e-6, 0.0001115772277003256] km/s
+ V∞_out: [-9.68445711819351e-5, -3.278665153268311e-5, 3.732136722555154e-5] km/s
+ time of flight: 1.8749577787367907e8 seconds
+ arrival date: 2030-04-24T19:48:36.873
+ thrust profile: [0.29908062703529903 0.004808994712065468 -0.09760669148852065; 0.031850364754051785 0.01878842370357479 -0.038606563108708414; 0.029604678451998268 0.027807737657272725 -0.06556987994274155; 0.03994438135880161 0.04765581217301736 -0.1253388165274495; 0.026175164356320245 0.040610005941889654 -0.11726649110184312; 0.014200264644265487 0.024037000101944903 -0.07971649487397503; 0.010350307420990575 0.024097557147262718 -0.08184168444667386; 0.009587642408205338 0.0230549689702055 -0.08609461069345498; 0.003696349710556295 0.009657207749073705 -0.036836750469384116; 0.00237942396394682 0.00720850585009964 -0.028871822077863353; 0.000995674180165483 0.0027105667367940153 -0.011640708236166974; 0.002246012883935693 -0.0014704789706955427 -0.006845247194945711; -0.0010104856835506382 0.0010953819156044914 -0.006326475547760308; 0.000322367755684149 0.0018286411363520085 -0.003923272485615758; 0.000920023968908941 -0.0004860350421093001 -0.0009499858656931513; 0.000786691865008341 -0.0007322390533440071 -0.001408676872224551; 0.0012064894052810644 -0.005726717427013597 -0.004909163047581407; 0.006062272465668145 0.0037961995468536874 -0.0027395776395946272; -0.0010617781974510071 -0.00044108746113420173 -0.010338053982036766; -0.0010429056438788621 -0.0012034425750328342 -0.003861773441368719] %
+
+Mass Used: 82.37751298317562 kg
+Launch C3: 97.48726219911758 km²/s²
+||V∞_in||: 0.00011161049503770456 km/s
diff --git a/archive/ES_0.5580510297498422 b/archive/ES_0.5580510297498422
new file mode 100644
index 0000000..36407b9
--- /dev/null
+++ b/archive/ES_0.5580510297498422
@@ -0,0 +1,22 @@
+archive/ES_0.5580510297498422---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T02:50:24.430
+Launch V∞: [7.886025920488019, -5.589897037331865, 0.28239569084077576] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.618039050349674e-6, 8.50194335253798e-5, 1.4504251125326513e-6] km/s
+ V∞_out: [8.226373952260167e-5, -1.220567818940407e-5, 1.7695936312574178e-5] km/s
+ time of flight: 1.8749577787414804e8 seconds
+ arrival date: 2030-04-22T05:00:01.430
+ thrust profile: [0.6198903027731456 -0.004168684252786197 -0.18283075986651598; 0.055943584557704505 0.03111820830225946 -0.0624889831175348; 0.03927324264408837 0.035420066736617 -0.07984052000705023; 0.028698751344788002 0.03507196132860299 -0.08948696444030275; 0.031373196097356275 0.047332689404177994 -0.13240183808403783; 0.019528178226655306 0.03556156447717467 -0.1109496545857423; 0.009800899266700892 0.019816736485167213 -0.06687301142145892; 0.007119443189292849 0.016261706226903896 -0.05880058930322013; 0.0021832741084802654 0.006327426215215178 -0.02339257952107398; 0.001446697286048406 0.0024055415343346557 -0.01191739542884261; -4.77209690550215e-5 0.006709479349282551 -0.01670744181636484; -0.0002584134387516406 -0.001157022888849361 -0.0031254627920095494; 0.00011971961709350293 -0.0004902210157690008 0.002836753175093521; 0.0004325582882695159 0.0001921839064166019 -0.0007353403355955142; 0.001742444057164642 -0.005347102408701456 -0.0003321303231990881; -0.0010899507358010953 -0.004121709031842821 0.002704869924627636; -0.0002767021595053195 -0.0047690952184783735 0.0011583723379315443; 0.00455363153997341 0.0020448319493213385 0.006090274458890847; 0.0011733010341044164 0.0005894523416825715 0.0009961090268186365; 2.6858252365623454e-5 -0.0006414791202746799 0.0008366173187920716] %
+
+Mass Used: 105.5489453502314 kg
+Launch C3: 93.51610103278591 km²/s²
+||V∞_in||: 8.51087423039102e-5 km/s
diff --git a/archive/ES_0.558054737547109 b/archive/ES_0.558054737547109
new file mode 100644
index 0000000..825cd06
--- /dev/null
+++ b/archive/ES_0.558054737547109
@@ -0,0 +1,22 @@
+archive/ES_0.558054737547109---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T15:21:53.619
+Launch V∞: [8.006143519517488, -5.795499925856156, 0.11486630669805353] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005301154770484594, -0.03148985181197168, -0.038541479675340405] km/s
+ V∞_out: [0.021842220336819713, -0.0179308383431079, 0.041346904325575584] km/s
+ time of flight: 1.8471238638706675e8 seconds
+ arrival date: 2030-03-22T12:21:39.619
+ thrust profile: [0.24806860343661521 -0.008691120683038001 -0.08508821343840246; 0.060707948989446855 0.031061022762949708 -0.07314239244554917; 0.04816908728419675 0.039556439402697555 -0.10354181507129294; 0.038579667855800207 0.04089117992394399 -0.12165677859221645; 0.024992879899448074 0.031394263517423984 -0.1050828001167689; 0.015720025286719706 0.022319569676009513 -0.0819513280374579; 0.006259019250347976 0.010777662565411664 -0.04234615777271785; 0.01656962173522961 0.03032416606612821 -0.12544388012578442; 0.006595617600998822 0.012210349113546324 -0.055899861382203944; 0.0021781329917162015 0.0037457993542482663 -0.016020003647363414; 0.0001687088152864672 -2.279643539120855e-5 -0.0024809044907931027; -0.002455881195451319 0.0003365044310368454 -0.0016699655925558792; -0.00010586365182024924 0.0001274570935678285 -0.0013858809749344022; -0.0005502930572669161 0.0036424242865165653 -0.0024631953794275584; 0.00017333831016898182 -0.0010250196040804717 -0.00284273486636317; 0.0005878982405387 -0.002546813506789045 0.0006013209573529868; -0.004083263245412507 -0.0023926453734087255 -0.0034007717691602454; 0.00540495857346162 0.005440868214009928 0.000734415965353306; -0.0011542299612224164 0.0013218906522353667 -0.0010974559769383629; 0.0036298913321014194 0.003718701719700443 0.0032579354882347235] %
+
+Mass Used: 81.15099880589787 kg
+Launch C3: 97.69934771412503 km²/s²
+||V∞_in||: 0.05005156006165288 km/s
diff --git a/archive/ES_0.5580569643155511 b/archive/ES_0.5580569643155511
new file mode 100644
index 0000000..80538dd
--- /dev/null
+++ b/archive/ES_0.5580569643155511
@@ -0,0 +1,22 @@
+archive/ES_0.5580569643155511---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T00:42:03.835
+Launch V∞: [7.93675770767678, -5.850443628916433, -0.1948921723221865] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00015076043544489962, -0.00011925259041604496, -7.703857961570504e-5] km/s
+ V∞_out: [-1.4977426596917956e-5, 9.72151862273031e-5, -0.00018212508359379502] km/s
+ time of flight: 1.8749577788569826e8 seconds
+ arrival date: 2030-04-25T02:51:40.835
+ thrust profile: [0.26894962708532233 0.0032460811191390914 -0.09198341332026383; 0.08707552640543934 0.05144180762278976 -0.10168932097529056; 0.04654782962394767 0.043647450514634936 -0.09909032801536634; 0.03640241369455166 0.04600874022150286 -0.11623234141112875; 0.0301411910793354 0.046405802796216165 -0.12987088555157658; 0.019646244837537317 0.036125286469808636 -0.1104390582310791; 0.00981901170548665 0.02121189090011882 -0.07207209264736589; 0.006012486251745484 0.013708159837936483 -0.05052952333799113; 0.0013331538739043732 0.0029798268226046984 -0.012428482708088504; 0.0006897687630671562 0.0014885969016324152 -0.006877426894289792; 0.000793301926839069 -0.0004740189715983017 0.00011204750635637219; 4.588902666073294e-5 0.0006461901143300071 -0.0024121411582085873; -6.215539514714106e-5 0.000915828452130308 -0.0017762605413212268; 0.0010306245013836101 0.0026174820880599543 0.0011186566927659167; -0.0003034787460287344 0.0013054630567763056 -0.0037411142917871745; 0.00027756182665695313 0.0004209915917930205 -0.002938348717474977; -0.005206638984321861 0.003439028364560257 -0.002345164146515555; 0.0006850343391446841 0.005132129775929773 0.0020971480576822714; -0.00251099900688565 -0.0005707719970060984 -0.0033020763137221387; 0.005190090827476181 0.0025827994133854446 -0.002929507105657138] %
+
+Mass Used: 83.72931197622893 kg
+Launch C3: 97.25779652432811 km²/s²
+||V∞_in||: 0.0002070865325550603 km/s
diff --git a/archive/ES_0.5580613003714757 b/archive/ES_0.5580613003714757
new file mode 100644
index 0000000..81c9b8b
--- /dev/null
+++ b/archive/ES_0.5580613003714757
@@ -0,0 +1,22 @@
+archive/ES_0.5580613003714757---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T17:36:56.213
+Launch V∞: [8.162988816878523, -5.552042955564257, 0.12964928313335894] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.783874936681107e-8, -6.026722316592521e-7, 5.22431432249924e-8] km/s
+ V∞_out: [-9.573455361546074e-8, 3.6572541881990114e-7, 4.74767326734839e-7] km/s
+ time of flight: 1.8749577787493858e8 seconds
+ arrival date: 2030-04-21T19:46:33.213
+ thrust profile: [0.2376790464070976 0.001967318666467891 -0.07184678365208909; 0.07858504051469663 0.047857495586641874 -0.08263196876769764; 0.05671847851670796 0.05623406970323058 -0.10832108444586301; 0.046334228410505204 0.06121328594059645 -0.13213175938762245; 0.030563799908846806 0.050404035213669804 -0.1202747833693498; 0.0180016722113168 0.0361225082576103 -0.09369983855406304; 0.00911115747879465 0.022000199084260968 -0.06097895962131769; 0.002298213109996697 0.006305287513491768 -0.019319996221972363; 0.004454859504683526 0.01946935483133039 -0.053028370031927646; 0.002615434048026086 0.009517311191931992 -0.03020128488615614; -0.00044346792131796687 0.00048264499762946657 -0.0023240329116220584; 0.002345384270428343 0.000836643967754219 -0.0007205871596231885; 0.0007366169110606585 0.000234913213172283 -0.002571098459618581; 0.0003446953656438118 0.0021015384639287158 -0.002044948379990347; 0.0012225411504557045 0.0014366784417287272 -0.004434028565393127; -0.0038654623739485467 -0.0012525716615835285 -0.00188834126519533; 0.0013221405673836902 0.005030318624106115 -0.001424850851404433; 0.0004486756964205908 0.0019974292531250992 0.0030619845921252098; 0.001727357362594106 0.002980494870412887 -0.001309255584517153; 0.0008162197988998539 -0.00045266128289764247 -0.0018557000492321748] %
+
+Mass Used: 82.45932177445457 kg
+Launch C3: 97.4763763415315 km²/s²
+||V∞_in||: 6.068209874156883e-7 km/s
diff --git a/archive/ES_0.5580752694488134 b/archive/ES_0.5580752694488134
new file mode 100644
index 0000000..364e1ed
--- /dev/null
+++ b/archive/ES_0.5580752694488134
@@ -0,0 +1,22 @@
+archive/ES_0.5580752694488134---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:28:53.414
+Launch V∞: [7.983677717520839, -5.762047118347824, 0.3349771199332594] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.50830900751041e-5, 2.5509981099322192e-5, 0.002238790117606869] km/s
+ V∞_out: [-0.0019881080010378423, -0.0006864626127812944, 0.0007643857817611048] km/s
+ time of flight: 1.8586415501271877e8 seconds
+ arrival date: 2030-04-05T05:24:48.414
+ thrust profile: [0.34457976959723313 -0.005509751829652309 -0.11022146624880402; 0.036667356546714325 0.01927401904879624 -0.04372204134170654; 0.032909585546722166 0.027828046546774135 -0.0702297701320876; 0.022369512402589734 0.024340590082302816 -0.06998964870657211; 0.03389271647541419 0.0451686694465599 -0.14357705416154848; 0.01322316034774274 0.01979831994829106 -0.06959371655907541; 0.011443400190114347 0.019237223704783795 -0.07254684063159271; 0.007926440968444678 0.013965222319127063 -0.05757185223272792; 0.005870982573769138 0.011901417575569324 -0.05217421794633252; 0.010169555264443146 0.022353912716897087 -0.0981766209707774; 0.0027568667269406034 0.0057417957946208934 -0.02337656083047833; 0.0020987056639081353 -0.0003246922727575698 -0.0016747900871350062; 0.000423052395187118 0.00040808633908653467 -0.002745992239673884; 0.0007096027193183587 0.00042546003238409693 -0.0037072633095432; 0.00017045989762041742 0.0004276790034851022 -0.0026329991336762814; -0.0008951597723249735 -5.4835196525157516e-5 -0.0011060120299366278; 0.0009223231828094508 -3.6962231458426836e-5 -0.0024268679318460735; 0.0007405025454011579 -0.0011639116784528981 0.0001737217894406751; -0.0012716438224397923 0.0006546346238885301 0.004193359046155809; 0.00019138424600451695 9.879408483048745e-5 0.001312854472394349] %
+
+Mass Used: 84.9481927442439 kg
+Launch C3: 97.05250656217801 km²/s²
+||V∞_in||: 0.0022392103012086836 km/s
diff --git a/archive/ES_0.5580852709044943 b/archive/ES_0.5580852709044943
new file mode 100644
index 0000000..16aec43
--- /dev/null
+++ b/archive/ES_0.5580852709044943
@@ -0,0 +1,22 @@
+archive/ES_0.5580852709044943---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T13:12:27.258
+Launch V∞: [7.729762739073607, -5.762945517391794, 0.3443216087160248] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.174225831502965e-10, -7.520617443916373e-10, -8.379263993779445e-10] km/s
+ V∞_out: [2.6726556160597464e-10, -2.0522026066315926e-10, 9.580715929864269e-10] km/s
+ time of flight: 1.8597687668552026e8 seconds
+ arrival date: 2030-04-04T01:27:03.258
+ thrust profile: [0.5637049404498689 0.009991006867674157 -0.13492261653660154; 0.11651511016945613 0.07477550008435287 -0.11540243199868969; 0.07298775808435477 0.07745589311716464 -0.1328816577084828; 0.04529041614539491 0.06479825776994111 -0.12559393062010044; 0.03658920501690018 0.06611890627247026 -0.13872486315178084; 0.008543466878442218 0.017979786440190267 -0.044759747703010534; 0.006049995477214307 0.01322716361069027 -0.035893908614473787; 0.005910794597037032 0.019640460236238687 -0.052738248042575944; 0.005055886684597206 0.012556565120720207 -0.0396743829543218; 0.0006774456138542938 0.002892482328194107 -0.008399697531033604; -0.0003474023083420509 0.0007779778785454278 -0.0017631856440770333; 0.0002245707445651668 0.00010826506009614808 -0.001009191201697213; -0.0006231894221414992 -0.00037114051239625634 -0.005065343735278029; 0.0007823568723483755 -0.00022787385710693715 -0.0033614080668115894; 0.0005192372052672048 0.0024014518462890542 0.0021702483398895077; 0.0013646475453008918 -0.0009439275620961083 0.0007079513337233377; -0.00015711767044926535 0.002698652443863814 0.002720670211535865; 0.0011978255224108544 -0.0001659910437188504 0.0008401520775905819; -0.004762343497300894 0.0016278710611566166 0.0004250767619769861; -9.131822935903682e-5 -0.0007353423663726974 -0.0013255332992229887] %
+
+Mass Used: 108.13672200259361 kg
+Launch C3: 93.07933040902566 km²/s²
+||V∞_in||: 1.3350702906461226e-9 km/s
diff --git a/archive/ES_0.5580892092846502 b/archive/ES_0.5580892092846502
new file mode 100644
index 0000000..8a685ad
--- /dev/null
+++ b/archive/ES_0.5580892092846502
@@ -0,0 +1,22 @@
+archive/ES_0.5580892092846502---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T04:06:14.766
+Launch V∞: [8.001718204268336, -5.771653649575412, 0.2465881187960149] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012570800039215381, 0.076403041435215, 0.07973814920565427] km/s
+ V∞_out: [-0.019780164690685862, 0.017373930265731773, -0.10796475443186176] km/s
+ time of flight: 1.8291693647580773e8 seconds
+ arrival date: 2030-02-28T06:21:50.766
+ thrust profile: [0.2700530127757831 -0.011039098052064255 -0.08986126621372484; 0.046789815015279665 0.0241534803183778 -0.05435458742312733; 0.05910807868210341 0.04915029125437832 -0.12036595327375536; 0.043607702915095914 0.04715670986619333 -0.13016130802899623; 0.031673613601109374 0.04123958266082652 -0.12618668163548638; 0.021088144065807578 0.03177991672436487 -0.10635700726953597; 0.009235499991148446 0.01591847677886382 -0.05776550954061065; 0.0047899370626317776 0.009228035518682528 -0.03486870311925292; 0.006853848008153588 0.01467407033706573 -0.05878107500810277; 0.0032284196386832813 0.007358134456054309 -0.03050753306105891; 0.0008699043354292266 0.002090679149237406 -0.009311471523537911; 0.000986222751280255 0.003634967359718209 -0.01565675345719092; 0.0009017856114011581 0.0007970493768493835 -0.0016411973123504745; -0.001994384404731146 0.001370712985820759 -0.0031121488586201024; 0.00013064219619078035 -0.0017628756754076392 -0.002006164399110376; 0.001980107287073779 -0.001981149296036335 0.0013694504801598432; 0.0035584654887571717 -0.001517910927764651 -0.000835945490060863; 0.0019646844901438183 -0.0018547718784904246 -0.0006742760105905362; 0.0006286148585084629 0.00010680949674537812 8.586814367589042e-5; -0.005331606310492838 0.0014381716192604405 0.0031463897616513903] %
+
+Mass Used: 82.93574383162968 kg
+Launch C3: 97.40028577150782 km²/s²
+||V∞_in||: 0.11114684967609428 km/s
diff --git a/archive/ES_0.5580935002492297 b/archive/ES_0.5580935002492297
new file mode 100644
index 0000000..34f86ec
--- /dev/null
+++ b/archive/ES_0.5580935002492297
@@ -0,0 +1,22 @@
+archive/ES_0.5580935002492297---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T10:21:36.560
+Launch V∞: [7.644409413989886, -6.071685553915882, 0.17296202580629286] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.617294248099623e-9, -8.558966550120637e-8, 1.4713693562837172e-8] km/s
+ V∞_out: [-1.3593985805647999e-8, 5.2022812426536545e-8, 7.069761242893617e-8] km/s
+ time of flight: 1.791270293745139e8 seconds
+ arrival date: 2030-01-15T15:52:05.560
+ thrust profile: [0.41479994368881584 -0.016941632342307163 -0.1352323823948125; 0.11259790019203662 0.0560703810135629 -0.12610358004042976; 0.04528321475707332 0.036200297721115444 -0.0914003299245906; 0.03439870740022377 0.03585743756958218 -0.10112716663280474; 0.04949049268644348 0.06478142999828752 -0.1937264732982147; 0.01962483399569494 0.028426699378079595 -0.09603741592438014; 0.010390299743519963 0.016863173516292875 -0.06275724969822802; 0.009500427774884492 0.017349161790908486 -0.06646448493407005; 0.0011227989679346475 0.002095968380091946 -0.009280037763453463; 0.0009419989807626193 0.002401719447346086 -0.011430878453001309; 0.0019793453915559448 0.004410432269415787 -0.020399889617794834; 6.11842866394608e-6 2.4652560351560122e-5 -0.0005706904392749535; -0.0003817815796935464 0.0004177177368688785 -0.0010869618227211395; 7.219796268213158e-5 0.00033722513276352264 -0.0006167133218756586; 2.875295953074912e-5 0.00010328227366734508 -0.0013827956204996725; -2.0807996481579807e-5 0.00026139630327780337 -0.0008042075132642457; 0.00023495311532730238 -0.00041661228394758996 -0.00032826347874506163; 0.0005316863046795099 5.521404435155264e-6 -0.00024813302132593114; -8.454461694293173e-5 9.064239836953261e-5 0.0001852794176577565; 7.921669109070938e-5 -0.0002589196950167732 -0.00045809389281147104] %
+
+Mass Used: 95.00413669335694 kg
+Launch C3: 95.33227661669902 km²/s²
+||V∞_in||: 8.737606060886472e-8 km/s
diff --git a/archive/ES_0.5580975488820206 b/archive/ES_0.5580975488820206
new file mode 100644
index 0000000..73aa49b
--- /dev/null
+++ b/archive/ES_0.5580975488820206
@@ -0,0 +1,22 @@
+archive/ES_0.5580975488820206---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:43:14.664
+Launch V∞: [7.966738495358473, -5.590555071633886, 0.15441663582387197] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007737800709628736, 0.0494872423541044, 0.04953044358097077] km/s
+ V∞_out: [-0.012134345358824086, 0.011004626032548892, -0.06839801989505441] km/s
+ time of flight: 1.874957778744263e8 seconds
+ arrival date: 2030-04-22T07:52:51.664
+ thrust profile: [0.5239829634924218 0.0019298824598246234 -0.15417829542501785; 0.02629934277472748 0.01620482437245961 -0.031383854306886505; 0.04039905098471974 0.04026778702239612 -0.08451557332948159; 0.04825766279828625 0.0630322056490969 -0.14269897784427; 0.020673229834399714 0.03381090919454402 -0.08770699359398879; 0.012328425351448905 0.024952363910601568 -0.07062016635519827; 0.00519190587618304 0.012316013526804007 -0.038310116288726576; 0.004174134166913651 0.014681684230097327 -0.0464433513900193; 0.005050986140499688 0.015997717379463774 -0.06299916160224671; 0.006448561998771181 0.0242190965013286 -0.07964831167127487; 0.0021066311430815656 0.006068984530649631 -0.028421844281372233; 0.0005861579589162352 -5.866562281523738e-5 -0.004556600113246297; 0.0015869023978736358 0.0026340691708300243 -0.0010888400135572833; 0.001567120914973857 -0.0009155430992822215 0.0005793785309600886; -0.001287848777737442 -0.0017307153107363365 -0.001146393370588826; -0.0005104156136038847 0.00010915450875952841 -0.0004753626096674899; -0.0002414707328071329 -0.0007836691128980994 0.000314881428843818; 0.0020184419051030057 -0.00038512249737436154 0.00042041036181685596; -7.243353108975689e-5 -0.0009189375919174954 0.0006528357608703462; -0.0029994594084993493 0.0013165461671026425 0.005428375691499054] %
+
+Mass Used: 98.42254926342412 kg
+Launch C3: 94.74707275981712 km²/s²
+||V∞_in||: 0.07044235627066661 km/s
diff --git a/archive/ES_0.5581023420875818 b/archive/ES_0.5581023420875818
new file mode 100644
index 0000000..78ac0a2
--- /dev/null
+++ b/archive/ES_0.5581023420875818
@@ -0,0 +1,22 @@
+archive/ES_0.5581023420875818---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T00:50:07.985
+Launch V∞: [8.070243460795798, -5.574719252280255, 0.19859829818964597] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9025514118369745e-5, 1.941526060042971e-5, -1.21286662531044e-5] km/s
+ V∞_out: [3.986710232337341e-6, 3.0019700103913507e-5, -1.426705125040846e-6] km/s
+ time of flight: 1.8749577787546247e8 seconds
+ arrival date: 2030-04-22T02:59:44.985
+ thrust profile: [0.35191703388774964 0.002869534048876236 -0.10150026687372904; 0.07340515077167085 0.043862231883732214 -0.0835511665608257; 0.061831216327351765 0.06096087378858044 -0.12575562860563969; 0.04061075249969587 0.050862923216162426 -0.12092259542489817; 0.02634412759887704 0.04022294127503059 -0.10808958262053356; 0.013335630672653958 0.0267762563812003 -0.0748068481893352; 0.008383119981942945 0.01821910807673449 -0.058110742131704154; 0.00594053594069452 0.014299153744358856 -0.04876550496053782; 0.0025654282947777237 0.007019940449925862 -0.025184748444782638; 0.001278897783296325 0.003721129186986215 -0.015577179700592487; 5.529653984324284e-5 0.0024093676502804015 -0.010330928639182368; 0.002052548986765602 0.006918475247157474 -0.027624884327489656; 0.00022226726467264362 0.0032851636860854448 -0.005221767044421793; 0.0011044671773694213 0.0017241867652968627 -0.0017293235320073174; 0.001254911607697824 -0.0005571525889039768 0.002306485329650617; -0.004418921942738776 0.0005075564321073243 -0.0034967963239383648; -0.0027358068161189492 0.002884673162958497 0.0001080872092044001; -0.000413626470241038 7.367448280485352e-5 -0.001111208867415131; -0.0013392331883389594 0.0008454548041985804 0.0019013528184542384; 0.0018902019302794919 -0.0009569585711028235 0.0071525908215477885] %
+
+Mass Used: 89.68576677206465 kg
+Launch C3: 96.24576554230528 km²/s²
+||V∞_in||: 2.976620695906817e-5 km/s
diff --git a/archive/ES_0.5581158857147868 b/archive/ES_0.5581158857147868
new file mode 100644
index 0000000..e48911c
--- /dev/null
+++ b/archive/ES_0.5581158857147868
@@ -0,0 +1,22 @@
+archive/ES_0.5581158857147868---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:32:03.734
+Launch V∞: [7.921854398520748, -5.649022507645703, 0.2375576988615702] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.478381410035282e-10, -1.2117869856587823e-9, 8.449432771999975e-10] km/s
+ V∞_out: [5.170628983842867e-10, -1.6373677858751555e-9, 2.5863515312194797e-10] km/s
+ time of flight: 1.8749577787318736e8 seconds
+ arrival date: 2030-04-22T09:41:40.734
+ thrust profile: [0.4820761320501541 0.001859138179427003 -0.11536822638134309; 0.06776310602994362 0.042469637375023704 -0.07203263167186826; 0.05659870243553991 0.059855866247777535 -0.10891735266551282; 0.028865742973171106 0.03757911243937135 -0.08493416694560904; 0.019326493547307342 0.034979965917326265 -0.08312913981560387; 0.03136936045456038 0.0619879008901811 -0.14815098746985522; 0.004881262684226857 0.014497391201403687 -0.04263202186152389; 0.0019287058137910861 0.01083522697652702 -0.03367677916922065; 0.003166505464049857 0.015665708009177638 -0.05325064485258057; 0.0051726240051796915 0.011116843320438653 -0.040460291132376806; -0.001718383446892827 0.008914642729515358 -0.022502513484033593; -0.001557614358362091 -0.001866894837435234 -0.0005518715863786559; -0.0001520169981293745 -0.0017587189853146459 0.0021891339277729464; -0.0038378693268074707 0.0007379822642554646 0.0009872286542550067; 0.003469062208411806 0.00044971884760180005 5.83994746568197e-5; 5.369995157105626e-5 0.0008419181806320515 -0.0013033592549260165; 0.0002487579020991782 -0.0003518111591825764 -0.00040311495353146515; 0.00043301425863558356 0.0019448232377574336 -0.002317530824860241; 0.002706580560306735 0.002657800244301264 -0.0027583632391433846; 9.943820317351749e-5 3.356593503594206e-5 0.0018088049570084816] %
+
+Mass Used: 98.58048129660892 kg
+Launch C3: 94.72366606353867 km²/s²
+||V∞_in||: 1.7552076748460547e-9 km/s
diff --git a/archive/ES_0.5581233895075337 b/archive/ES_0.5581233895075337
new file mode 100644
index 0000000..74b97c3
--- /dev/null
+++ b/archive/ES_0.5581233895075337
@@ -0,0 +1,22 @@
+archive/ES_0.5581233895075337---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T12:37:55.978
+Launch V∞: [8.027267035101376, -5.7050756192826775, 0.12939659848640708] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.058494022846335e-6, 0.00016792120292656658, 2.9480589736343768e-6] km/s
+ V∞_out: [0.00016265058453826306, -2.4435356661275572e-5, 3.4698606255840166e-5] km/s
+ time of flight: 1.855765590158225e8 seconds
+ arrival date: 2030-03-31T09:40:34.978
+ thrust profile: [0.29231980858103335 0.0019331489526897615 -0.09372132604443655; 0.06415308654936164 0.037506262144697516 -0.07238105203925793; 0.0371560618161181 0.035071358068326536 -0.07572680648178602; 0.04663447384766437 0.05952299400606272 -0.13923254247219835; 0.029174573411747045 0.045591817289476484 -0.11929801712680901; 0.021518048417110705 0.03989511206281982 -0.11320928218912688; 0.011067163536211698 0.023838608144409423 -0.07355663793027943; 0.006821581117327017 0.017144889730956157 -0.05675998984759398; 0.003345680190408558 0.009038240879108378 -0.03126448940417336; 0.0015751166778798574 0.005218633367681719 -0.0192679552503217; 0.0014713875186436968 0.002797133277301534 -0.011062393575276887; -0.0005809251020404155 0.0014408552131566707 -0.004419877896417904; -0.0002779709907547931 -0.001175036031681027 0.0010680907002788447; 0.00041569769964343577 0.00035586977652281884 0.0022739606591915523; 0.0030214736481296014 -0.0003921632174700518 0.0004562464058283232; -0.0016340361726786697 0.00043915438865322655 -0.003044425975281432; -0.003916372863303489 -0.0050654650676768345 -0.003301267981758375; -0.0018543699104468512 -0.0012933811207079967 -0.00233450248402706; -0.000625433106987584 -0.0012220632739919426 0.005521884112274017; 0.006516178055104259 -0.0024321778511546986 0.002836076977779958] %
+
+Mass Used: 85.30101152561338 kg
+Launch C3: 97.00164735425872 km²/s²
+||V∞_in||: 0.0001680953413449871 km/s
diff --git a/archive/ES_0.558132203222415 b/archive/ES_0.558132203222415
new file mode 100644
index 0000000..cf9498c
--- /dev/null
+++ b/archive/ES_0.558132203222415
@@ -0,0 +1,22 @@
+archive/ES_0.558132203222415---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T13:54:25.090
+Launch V∞: [7.969705787533854, -5.808754144964638, -0.08496338896512523] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009219179695460417, -0.0006365929055301649, -4.006216651263405e-5] km/s
+ V∞_out: [0.0008136893735565351, 0.00035650083611332673, -0.0006839801479211511] km/s
+ time of flight: 1.8450312130861324e8 seconds
+ arrival date: 2030-03-20T00:46:26.090
+ thrust profile: [0.2886408875611252 -0.006281975985375157 -0.0971406715002358; 0.07203133424839007 0.03803007623201065 -0.08726664406459218; 0.0300423966973519 0.02527563905292478 -0.06748522692166976; 0.039203567128685904 0.04353107040479151 -0.12584523763412342; 0.018190033273089126 0.025046210833938078 -0.08240954823976636; 0.017779216980222355 0.028981809142334065 -0.10305012514598029; 0.006855642127833938 0.011727012547035892 -0.04713186237388231; 0.004985759035295423 0.009612992142444095 -0.040456190973752325; 0.011528537248149123 0.026843296139644514 -0.11387143884390163; 0.005303857907738008 0.010946784270652092 -0.05102461012975205; 0.0015147569078683045 0.0036873471509268766 -0.016421636184350934; 0.0013353090238975324 0.0017932625905832003 -0.011818527656384963; 2.7964897752932234e-5 -0.0005770844420070729 -0.00018260675134456814; 0.0001406716330166251 -0.0008803774011565883 0.0006529048564887811; -0.0006046185356003716 0.00031649181506301504 -0.0021891073067602336; 0.0007791672651984635 -0.00017007086652245815 -0.002019560847288011; -5.163794752082704e-5 -0.0011109761188584234 0.0016238882882046333; 0.00024624459594821174 -0.00020498593932669193 -0.0003281669903792959; -0.000675771092055857 0.0007589094362936248 -0.0015719603324985348; -0.0008172529739657508 -0.0013853922931761802 0.0019556234053896143] %
+
+Mass Used: 83.77475639472368 kg
+Launch C3: 97.26505383395893 km²/s²
+||V∞_in||: 0.0011210656747617062 km/s
diff --git a/archive/ES_0.5581399771927356 b/archive/ES_0.5581399771927356
new file mode 100644
index 0000000..18b9cbb
--- /dev/null
+++ b/archive/ES_0.5581399771927356
@@ -0,0 +1,22 @@
+archive/ES_0.5581399771927356---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:18:19.014
+Launch V∞: [7.935674078706518, -5.767896862701248, 0.08943247726973591] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.846788274764876e-6, 1.3124847475212953e-5, 2.7949356998931837e-5] km/s
+ V∞_out: [2.5299106936494998e-5, 2.8058345320866106e-6, -1.1834163232238158e-5] km/s
+ time of flight: 1.8749577787516895e8 seconds
+ arrival date: 2030-04-23T18:27:56.014
+ thrust profile: [0.27915839789487906 0.0012000918439216543 -0.08825004496557198; 0.1628906983796477 0.09435700243149797 -0.17415965590243385; 0.060858803395184034 0.05737203494767959 -0.12073343136767678; 0.027326721128130962 0.03382022732858117 -0.08171542683000499; 0.0321573632465802 0.05085254435428964 -0.12914358150063898; 0.016529505680501957 0.0313546438321591 -0.09049067025673749; 0.0038899698277864727 0.008156748981976816 -0.027070301161710632; 0.0065246600502475455 0.014784950770186083 -0.05051647577612039; 0.002238012358975086 0.0017638431652032022 -0.008943725765432085; 0.002060666051934839 0.005168847784811679 -0.01844790154768898; 0.0013190833418316615 0.004791244929704301 -0.01747762284906296; 0.0023181305356389805 0.002143712825209162 -0.0031850319419844003; 0.002829224264335058 0.0008133664801310674 -0.0021262682760723973; -0.000915169571251589 -0.00018904641027925394 -0.004967438583076793; 6.8295162202390526e-6 0.000564736838645997 -0.0013294834147162776; -0.004072960116285998 0.003963913903303909 -0.0010714865630004717; 0.005144039810830757 -0.006867916381943516 -0.004608876218103181; 0.0002284191837544614 -0.0004946683987628359 -0.0015899686312221381; 0.00484682965433187 -0.00028101000573366565 0.0021007277277284497; 0.0015865812378281442 -0.0034072470072843836 0.006570068213714983] %
+
+Mass Used: 89.69589981533454 kg
+Launch C3: 96.25155547020405 km²/s²
+||V∞_in||: 3.1116329441825435e-5 km/s
diff --git a/archive/ES_0.558144326935172 b/archive/ES_0.558144326935172
new file mode 100644
index 0000000..6c8950e
--- /dev/null
+++ b/archive/ES_0.558144326935172
@@ -0,0 +1,22 @@
+archive/ES_0.558144326935172---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T16:28:06.602
+Launch V∞: [8.063294666891435, -5.824158083245984, -0.040566605268407926] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6824094963756575e-7, -2.6947204238360057e-6, 5.9506977231376945e-5] km/s
+ V∞_out: [2.4905116417851817e-6, -5.950921576604826e-5, 6.967358551045982e-7] km/s
+ time of flight: 1.8749577787451953e8 seconds
+ arrival date: 2030-04-25T18:37:43.602
+ thrust profile: [0.16206611579685504 0.0002211705630622126 -0.057842268437647636; 0.06586059195304965 0.037172202743295 -0.08206286505799704; 0.034509088158836486 0.03206299111146611 -0.08104804710387661; 0.030788183309443804 0.03490904754173005 -0.1012500678633611; 0.03187173594792101 0.044203314027433736 -0.1389651305904949; 0.012908857140387227 0.021094484114401926 -0.07554636032239474; 0.01361804343574926 0.020722998433203202 -0.07717007784615357; 0.005029334805184188 0.00849216436245342 -0.035767803457420394; 0.006544252070353285 0.01689475487378923 -0.07196151252360733; 0.003585333623991895 0.007515966738238983 -0.04143261028600351; 0.00031425261146808667 0.0011617099503765911 -0.0050237542235511325; 0.0019712651894981652 -0.0012596703678974545 -0.0025597978813907936; 0.002448425724721216 -0.001356720054781154 -0.0015867868283672042; -0.0028162004443637047 -0.0006517182711433878 -0.0016661601049744723; -0.002845274321373857 -0.0015881523234017167 -0.004717042190678703; 0.0009212374840067239 -0.002614904532470718 -0.0003599853223866414; -0.00024264178711558304 0.001917529911110048 -0.0007650434720503893; 0.001490836212719548 0.00010933292855863115 -0.005171541376623283; -0.004002685455826317 0.0022163198856193543 -0.0035015677400603144; -0.0009918116266143281 -0.0006306892126203067 0.0019756972126888897] %
+
+Mass Used: 74.02314193057009 kg
+Launch C3: 98.9391839132224 km²/s²
+||V∞_in||: 5.9568563945971664e-5 km/s
diff --git a/archive/ES_0.5581453515108274 b/archive/ES_0.5581453515108274
new file mode 100644
index 0000000..cf150f6
--- /dev/null
+++ b/archive/ES_0.5581453515108274
@@ -0,0 +1,22 @@
+archive/ES_0.5581453515108274---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T13:30:55.537
+Launch V∞: [7.880771917043548, -5.835766957149135, 0.1073730595708207] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.836744392432573e-5, -6.345040581840434e-5, -5.40195465856961e-5] km/s
+ V∞_out: [-1.1680014486130338e-5, 7.99108310659705e-5, -0.0001004180933009648] km/s
+ time of flight: 1.8528445493524805e8 seconds
+ arrival date: 2030-03-30T01:25:09.537
+ thrust profile: [0.4262922916796236 -0.018046082083629983 -0.15403218537466193; 0.03449053573765765 0.01611080523132317 -0.045004149352629245; 0.03957052656640405 0.028556199827462332 -0.09292414384506402; 0.03299208022199361 0.030653091947322922 -0.11044792448528332; 0.02373898513010336 0.02518897714770312 -0.10332533530192302; 0.019552657597033216 0.023485835409658203 -0.10678848600685995; 0.011224089381102599 0.014717976083388054 -0.07364670615013282; 0.00967912839246295 0.018375546285848976 -0.0931585568245355; 0.003940584104858967 0.006107961795668567 -0.03496714365266729; 0.00038968797613606043 0.0012768208882544816 -0.00307727431109564; 0.0013299163231022943 0.002077355649599826 -0.010850560918909262; -0.004500939292622351 0.0015351475372357142 -0.004035635347956785; 0.003334486332077527 0.00060801479285094 -0.0017249602458724931; 0.00014853902577124855 0.002051777725024572 -0.009613470093422307; 0.000285565143331485 0.0011677267044212466 -0.004720882328309669; 0.002626765191614345 -0.003966245830014528 -0.0037985583369996886; 0.0008266511560180787 0.00020249830836933523 0.000638089098926017; -0.0022475183535621375 0.0012444298516448404 -0.0038255742981104; -0.000256196541265695 0.0019563098095027103 -0.004642193800769752; 4.864749089089713e-5 0.00010457028937072921 -0.0019625586581707177] %
+
+Mass Used: 90.15299615949652 kg
+Launch C3: 96.17427096053751 km²/s²
+||V∞_in||: 0.00012891943001754917 km/s
diff --git a/archive/ES_0.5581563123212032 b/archive/ES_0.5581563123212032
new file mode 100644
index 0000000..1c89cc4
--- /dev/null
+++ b/archive/ES_0.5581563123212032
@@ -0,0 +1,22 @@
+archive/ES_0.5581563123212032---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:23:28.982
+Launch V∞: [7.863395802977273, -5.805721499291355, 0.16048469276704477] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006354008698041754, -0.004923262786895028, -0.00024389966508777083] km/s
+ V∞_out: [0.0059038863929795045, 0.0026875500423568354, -0.004747766990454545] km/s
+ time of flight: 1.8749577787480003e8 seconds
+ arrival date: 2030-04-23T19:33:05.982
+ thrust profile: [0.38475746936129307 0.014616284399110594 -0.11215943549861729; 0.09851336589975175 0.06263777099867572 -0.10160146581387464; 0.04729010617882515 0.048595956540672676 -0.08963465784106668; 0.02244835312915734 0.031092912892774716 -0.0653489526966728; 0.03941385432724314 0.06967204706481771 -0.15418363673973884; 0.024294407027949695 0.05143526272130025 -0.12485831214760865; 0.013333439517067737 0.033325003931948725 -0.08762711181784753; 0.002445075113109519 0.005577168609440393 -0.0171556376156752; 0.000748326827806199 0.0041511316075244255 -0.01190609710963075; -4.601769597764474e-5 0.004810596844404441 -0.01586290418398133; 0.00044685174846671705 0.0014231413837706875 -0.005334662582409712; 0.0011806651342468864 0.0038020783108526504 -0.01317984920881778; -0.0013640489219986804 -0.0008804705489940899 -0.0006849531224646505; 0.00020289605971426363 0.0008041384213202196 -0.003332590641953079; -0.0032559129806632135 -0.0019593497569579117 -0.00139448962998931; 0.002414727998153648 0.000964685931384724 -0.0009848969193598065; -0.0032324474320811255 0.004304893577166071 -0.0036599196360798357; 0.0038299549451346416 0.006102303054593564 -0.00791339340032503; 0.001015243909262915 0.0038507146972404024 0.002571454767953985; -0.0004452754101080152 -0.004484263000258549 -0.0021873989913379225] %
+
+Mass Used: 93.71898343507974 kg
+Launch C3: 95.56515101822698 km²/s²
+||V∞_in||: 0.008041854888658809 km/s
diff --git a/archive/ES_0.5581657865917923 b/archive/ES_0.5581657865917923
new file mode 100644
index 0000000..77ec726
--- /dev/null
+++ b/archive/ES_0.5581657865917923
@@ -0,0 +1,22 @@
+archive/ES_0.5581657865917923---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:42:38.320
+Launch V∞: [7.8861392858744646, -5.707049332772097, 0.2963286100154095] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4659522419514936e-8, -1.2397083681107836e-7, 2.2411952451206682e-8] km/s
+ V∞_out: [-1.9413261945484775e-8, 7.203838615001614e-8, 1.039907753096545e-7] km/s
+ time of flight: 1.8204769063300955e8 seconds
+ arrival date: 2030-02-16T07:30:48.320
+ thrust profile: [0.5188826156364824 -0.01826464218000432 -0.13988142306896764; 0.040733218276754815 0.0227611039103899 -0.045332441747195744; 0.043277501524601004 0.040014720568111554 -0.08527923884008483; 0.022202062896624252 0.0267997554549014 -0.06451698304335263; 0.02191124862577996 0.033386425921263 -0.08677733495542682; 0.020121113738686726 0.03495091272869637 -0.09825199599961483; 0.03170083510500489 0.0675356947669256 -0.18529633250180524; 0.010691131267611946 0.026294010904837763 -0.08039434594483919; 0.005244420226607916 0.014071146490723479 -0.04830845422792786; 0.0023953086190120552 0.006839415405990432 -0.02485910054659531; 0.0002113644277974815 0.0006228757163829712 -0.0024939512862419784; 0.0002972624177462142 0.00032544020078136286 -0.0009091300505743219; 5.746513598488168e-5 0.00022263729742524828 -0.000873527054771931; 0.00026934458539716187 -6.69486137563333e-5 -0.00011133140716120343; -0.0004782376971829124 0.0001161540556173633 -0.000389434417925991; 0.0001189486782741924 -7.445014352161519e-5 -0.00034604020797613646; 0.00017690231890606756 0.00015294635090406183 -0.00018012180994048365; 2.1133180795676203e-6 0.00021873269110525301 0.00018563733120598364; -0.00030536066420892247 -0.00047461271052031903 -0.0008618829848725193; -7.43675471603642e-5 -0.0001993340562533178 -9.942560407569403e-5] %
+
+Mass Used: 97.90516021030362 kg
+Launch C3: 94.8494155680207 km²/s²
+||V∞_in||: 1.2683046002393287e-7 km/s
diff --git a/archive/ES_0.5581707031928036 b/archive/ES_0.5581707031928036
new file mode 100644
index 0000000..c9bfd19
--- /dev/null
+++ b/archive/ES_0.5581707031928036
@@ -0,0 +1,22 @@
+archive/ES_0.5581707031928036---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T06:18:26.249
+Launch V∞: [8.013628838335787, -5.8682588367952935, 0.00880945658161277] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.871964867472141e-7, -3.838209855630871e-6, 7.528997983575904e-5] km/s
+ V∞_out: [4.7990221622072265e-6, -7.670160337993343e-5, 1.4322564289073133e-6] km/s
+ time of flight: 1.844133465975779e8 seconds
+ arrival date: 2030-03-19T16:14:12.249
+ thrust profile: [0.18803508751759174 -0.0026711800309385876 -0.06420934079993425; 0.031146331878169103 0.016684137754685156 -0.03858748917566458; 0.03660869325984221 0.03180504671821424 -0.0788057613503763; 0.04044642003891378 0.04524726442154606 -0.12105373495005421; 0.02690743176714073 0.03965864537787692 -0.11745485828736801; 0.025312797848846658 0.04206790024395239 -0.13022852654417355; 0.006031991947524782 0.009836887945525497 -0.03360427311885403; 0.012632926611576492 0.021528554518359135 -0.08766406281364619; 0.007892767895236399 0.01926967430490863 -0.07699164482106789; 0.0019273807606341252 0.0053305299740204 -0.022413412832002717; 0.0025262911171922975 0.006879535772833866 -0.03214695373787087; -9.772838189430074e-5 0.0011463058192378002 -0.0010083252005833156; 1.0782149665867054e-5 -0.0005881942656261881 0.0012661742806285648; -7.255102283586565e-5 0.00046926105129628504 -0.004496928515976582; -0.0009344464368999551 9.451333569536241e-5 0.0029108912065382558; -0.001884857908047494 0.0018354847633055614 -0.0004930422251616152; 0.0019000985788357964 0.00015079231377890544 -0.0028202064035703633; -0.003825682281266736 -0.0027335718686367083 0.00039722690150995825; -5.8164859510284635e-5 0.0007531710134300149 -0.000748216591669417; 0.0005929685220719817 -0.0006629694732646491 -0.0007390314888696906] %
+
+Mass Used: 75.71289890384742 kg
+Launch C3: 98.65478654075831 km²/s²
+||V∞_in||: 7.538932470172129e-5 km/s
diff --git a/archive/ES_0.5581951439888282 b/archive/ES_0.5581951439888282
new file mode 100644
index 0000000..2835e33
--- /dev/null
+++ b/archive/ES_0.5581951439888282
@@ -0,0 +1,22 @@
+archive/ES_0.5581951439888282---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:08:33.675
+Launch V∞: [7.848201733445397, -5.825789751492385, 0.15393494545375092] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.898577354918435e-10, 2.1216159214131797e-9, -1.937414982551155e-9] km/s
+ V∞_out: [1.3072325577081072e-9, 2.638229418398523e-9, 6.794230824190334e-11] km/s
+ time of flight: 1.8200231458186686e8 seconds
+ arrival date: 2030-02-16T21:20:27.675
+ thrust profile: [0.34501293353586404 -0.016253298397085097 -0.11264958151946958; 0.16200050396395574 0.08237532674916825 -0.17649603340569348; 0.05368712797830314 0.0442951592280462 -0.10812087356050465; 0.04218054937765357 0.04551053072316358 -0.12431055264650707; 0.03578212634419933 0.04657934734057511 -0.1398448345283207; 0.019759575044979622 0.029909230691727025 -0.09994742530609248; 0.0047869530633328165 0.007779521989622498 -0.030367747197478003; 0.0029321850023043415 0.005150909192035398 -0.02129460113466693; 0.0017522540317643795 0.003631920771300529 -0.01631110624842072; 0.004672506213005469 0.010611396113547644 -0.04588590119260516; 0.00032089239560696226 0.00015588736528803507 -0.0022063164753176757; -0.00028535455876112464 0.0004170247010238528 -0.004733478975545431; 0.0009816480538786655 -9.017507612715697e-5 -0.0007652801121966259; -0.0011230137111781615 0.0015217008273185754 0.00010750612753542346; -0.004534767898238178 0.0016252411459529918 -0.00467124156766155; -0.00029824275240885646 9.43515115428041e-6 -0.0004920408475845232; 0.004104843818818609 -0.0019745203879542187 -0.0046404296555635416; -1.424130277768258e-5 0.003379743131416512 -0.004639326549159774; -0.0028594225462352575 -0.0005014842299647169 -0.0019874869259265586; 0.00021690041974544967 -3.5555342329577386e-5 -0.0012250255707745641] %
+
+Mass Used: 93.80721089182771 kg
+Launch C3: 95.55779264488089 km²/s²
+||V∞_in||: 2.8994516699766555e-9 km/s
diff --git a/archive/ES_0.5581975098838571 b/archive/ES_0.5581975098838571
new file mode 100644
index 0000000..4935dfb
--- /dev/null
+++ b/archive/ES_0.5581975098838571
@@ -0,0 +1,22 @@
+archive/ES_0.5581975098838571---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T05:23:48.892
+Launch V∞: [8.032915095174499, -5.841558935252221, 0.06521430610840595] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.146925307501396e-6, 4.644533056916648e-6, -3.910400049683574e-6] km/s
+ V∞_out: [1.1606073027487845e-6, 7.859279886228425e-6, -3.8879291414909216e-7] km/s
+ time of flight: 1.8469585837615705e8 seconds
+ arrival date: 2030-03-22T21:48:06.892
+ thrust profile: [0.1890596249387006 -0.002248707288414387 -0.0645220430128487; 0.04575564953847217 0.024845133571861664 -0.054679098316072074; 0.026842094305217362 0.023170153005850534 -0.057145595006830245; 0.026747536298286405 0.030349274213373963 -0.08345683469813275; 0.02674453798266174 0.03749102132553898 -0.11228021797119446; 0.022662763773816336 0.036746371731931154 -0.11933376673090992; 0.008473549629973189 0.014952339652438824 -0.054393427205413715; 0.0184814676750168 0.037534159587763995 -0.13315515625688504; 0.00957967415596306 0.021694317694491077 -0.08562511425469713; 0.001350992450455164 0.0030423572660519416 -0.01383730607370307; 0.00021117671076315925 0.00014251528603675435 -0.0030241974683198588; 0.001339907510199763 0.003687922124076448 -0.017543556043564917; -0.0007547947876170474 0.00025579196470878465 -0.00553949845851388; 0.0003429024522228866 0.0009105376679978997 -0.004699684896661019; -0.00041585042045533087 -0.00015864842080326425 -2.875622490616358e-5; 0.00028900453648658816 0.0002335442256610758 0.001722383899861667; -0.0005332880102102155 0.0016084103421443795 0.0017479505459733241; -0.002692020249111639 0.002993101805689024 -0.0004885587687629218; 0.0007705679715079459 0.0005305192801193312 0.0018395135469712661; 0.0019207245121616204 -0.0034247143103256278 -0.0020450467011037207] %
+
+Mass Used: 75.73832787933316 kg
+Launch C3: 98.65578862602858 km²/s²
+||V∞_in||: 7.959507270324913e-6 km/s
diff --git a/archive/ES_0.5582068649679824 b/archive/ES_0.5582068649679824
new file mode 100644
index 0000000..9ea3fd1
--- /dev/null
+++ b/archive/ES_0.5582068649679824
@@ -0,0 +1,22 @@
+archive/ES_0.5582068649679824---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:42:15.662
+Launch V∞: [7.978933523486594, -5.707833425225684, 0.2464190958993322] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005699759183363692, -0.003893217730658536, -0.0002511824073382641] km/s
+ V∞_out: [0.005021564068507503, 0.0023433743413800515, -0.004121710130531797] km/s
+ time of flight: 1.8568600840351406e8 seconds
+ arrival date: 2030-04-01T12:09:03.662
+ thrust profile: [0.3464071793022672 0.0005424931838206034 -0.10635395621913954; 0.062381965923469285 0.036505217196880754 -0.06844353446450804; 0.04816315254405153 0.04578313506840222 -0.09528950097065822; 0.04090471859838336 0.051081671990641495 -0.11928524330346035; 0.03830877912051289 0.05959433640734556 -0.15127899206745155; 0.026411898774807856 0.048607701373938904 -0.13445867137031897; 0.01124976126156881 0.023455479619025877 -0.07092380555533621; 0.004418759253063395 0.010918280220836093 -0.035659866437558016; 0.001994951293264632 0.003998139815657345 -0.015006829490787535; 0.0005872579992410346 0.0008759527029075888 -0.0033789958056813086; 0.0004293714600884391 0.00028063899978765386 -0.000689575087572335; -1.8719482561920268e-5 0.0007643308266691705 -0.004569875617592771; 0.0005957851991868531 0.0023681820986836428 -0.005507362749941461; -0.002281075927081739 0.0013250099672459446 -0.001709028211110711; 0.0001690688833332301 -0.0015508926733409055 0.004600502725857851; 0.0027389462889406517 -9.562214122056022e-5 -0.0018377843291305302; 0.0014950734045645773 0.0012471297044784708 0.003838775216134434; 0.00017542176651738753 -0.0028879608880329356 -0.000909698172400454; 0.0063049018878269785 -0.009018577780419555 0.014214766040678985; -0.000495736749994338 -0.0011690779381194902 0.0027958700871291813] %
+
+Mass Used: 89.47113023584689 kg
+Launch C3: 96.3034649531656 km²/s²
+||V∞_in||: 0.006907060999325906 km/s
diff --git a/archive/ES_0.5582101190476855 b/archive/ES_0.5582101190476855
new file mode 100644
index 0000000..115b2ad
--- /dev/null
+++ b/archive/ES_0.5582101190476855
@@ -0,0 +1,22 @@
+archive/ES_0.5582101190476855---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T18:15:29.335
+Launch V∞: [7.843971412164019, -5.739437864257198, -0.022567572841253557] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.8289835372950424e-5, -0.00044097737762017407, 0.00842154143120702] km/s
+ V∞_out: [0.0003085055624843951, -0.008422171357115722, 9.440854245571421e-5] km/s
+ time of flight: 1.8749577787106034e8 seconds
+ arrival date: 2030-04-21T20:25:06.335
+ thrust profile: [0.4271491291914258 0.0231103660336776 -0.0998277333065427; 0.04596180331737255 0.03245591692250209 -0.04553963129020564; 0.15918078143783432 0.1725579958869454 -0.25251431773452176; 0.02305912234085363 0.037453591485653255 -0.06310690200534988; 0.04108159391412137 0.08403564504517246 -0.14384612965432228; 0.009449129134457938 0.02594127689252734 -0.051417517385704645; 0.006251795954593411 0.01938690138643968 -0.04191779130636867; 0.0017483668655775342 0.007310882741042563 -0.016893691953748877; 0.004794103030696823 0.024986747923346587 -0.057999996920656875; 0.002136928568737701 0.01257995473280203 -0.031129400235838652; 0.0005989650290993589 0.0006880305241233702 -0.002024406715060892; -7.046667401584003e-6 9.759529803646339e-5 -0.0010679834707776816; -2.8111401466042585e-5 -0.00010249161821604695 -0.0003168400430327257; 0.0004601490897161409 0.0008112224089551546 -0.0008812363787967487; 5.823524271051941e-5 0.0011290059553407514 0.0001281335559933192; 0.0004766964128010223 0.0007101453409329269 -0.00290399255428666; -0.0010839130516075233 5.990740970936669e-5 6.152246897201275e-5; 0.0016149285163262583 0.0007800998508041159 0.0002702965335785436; -0.0005635995674413211 -0.000394548451119631 -0.00023561050552612192; 0.0024239358244793493 0.0015691346172334235 -0.0022337326723290882] %
+
+Mass Used: 100.17280000978553 kg
+Launch C3: 94.46954380785958 km²/s²
+||V∞_in||: 0.008433280431126249 km/s
diff --git a/archive/ES_0.5582120283659332 b/archive/ES_0.5582120283659332
new file mode 100644
index 0000000..876b1c5
--- /dev/null
+++ b/archive/ES_0.5582120283659332
@@ -0,0 +1,22 @@
+archive/ES_0.5582120283659332---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:38:56.699
+Launch V∞: [7.83409766247083, -5.872928144977754, 0.1764988618390731] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.014899819821874298, -0.010354814884433, -0.0006160068606809121] km/s
+ V∞_out: [0.013356463758376635, 0.006058505477377285, -0.010696950540990142] km/s
+ time of flight: 1.8455328762941822e8 seconds
+ arrival date: 2030-03-20T19:27:03.699
+ thrust profile: [0.3974938372180343 -0.008834656859120653 -0.1320985346383793; 0.0688875861929313 0.03557134722007381 -0.08104518289204635; 0.04442954122994716 0.03657914744961939 -0.09376221465586393; 0.05122494753354987 0.05552083857342779 -0.15674530645971327; 0.03363175344268934 0.043473235723804377 -0.1382583064421294; 0.014588426468290377 0.021300127221509788 -0.07638831406637725; 0.00780435369425471 0.01249497840333956 -0.04885214553173043; 0.004006873054995107 0.007246432426913353 -0.02996106672643754; 0.0072380136456546606 0.01421304184907149 -0.0619451901905477; 0.0020901815178563203 0.004068694237458041 -0.015229939876725848; 0.0016678748809441832 0.0015158857858913971 -0.00773059707285078; -8.932288911809967e-5 -0.00080402069363277 -0.0010132263080333869; -0.0015672386277000823 0.0015519894795275884 -0.0038797964043031513; -0.0008665124755849981 0.0016601044206802373 -0.0028000012718294807; -0.0023084568507823464 0.00043930464753129395 -0.0006845658400459094; -0.0006546464372738373 -0.0008054619264408812 0.0015988351365614926; 0.0011337093452688188 -0.000848253015611388 -0.001576050496789931; -0.0024257882498593293 -0.00628449601106172 0.001284029175374843; 0.0012492833396206297 0.00336274873545381 -0.0011601923709610596; 0.0006482267836320202 -0.005343910216452719 0.0074109722164169825] %
+
+Mass Used: 91.85681542189468 kg
+Launch C3: 95.89552302943326 km²/s²
+||V∞_in||: 0.018155062282118432 km/s
diff --git a/archive/ES_0.55821419860973 b/archive/ES_0.55821419860973
new file mode 100644
index 0000000..c7d7540
--- /dev/null
+++ b/archive/ES_0.55821419860973
@@ -0,0 +1,22 @@
+archive/ES_0.55821419860973---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:56:55.823
+Launch V∞: [8.0314927978154, -5.695719073087009, 0.13310714843992572] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.944918673981604e-9, 2.9704975483155755e-8, -5.901172418619111e-9] km/s
+ V∞_out: [1.4492463690698578e-8, 2.8063413316108782e-8, 7.599335166120697e-10] km/s
+ time of flight: 1.874957778732555e8 seconds
+ arrival date: 2030-04-23T17:06:32.823
+ thrust profile: [0.31810146532340616 0.00011960784491788922 -0.0846207710595522; 0.05672318715631209 0.03464593504845271 -0.06402240843966867; 0.03165620374954195 0.03334107201407675 -0.06743636861191658; 0.023473591257235304 0.031529281028248035 -0.07006192426183687; 0.017047979847229923 0.027787734099438067 -0.06894866588559594; 0.012708280515514812 0.03169041621206956 -0.08744074611786724; 0.022662390351496135 0.05340352919224164 -0.14321103522657055; 0.00983856955742177 0.03485366166783799 -0.09892328523954978; 0.005390313501056227 0.017010389367384224 -0.05545073531049443; 0.0026215752729724985 0.009188840236656112 -0.030353661799962257; -0.000157983599159997 0.001424094089488038 -0.0091771820415756; -0.0028497910744903388 0.0009077989901664403 -0.003048065373518732; -8.837583269859749e-8 -0.0021407537266326174 -0.0015238076608435564; -0.0031473115579439045 -0.005092425860951753 0.001396191943937003; 0.0017589371262449294 9.592906755651718e-5 0.0015829282960845856; -0.0016859536841651794 -0.001375286034867675 -0.003268322313163794; 0.001464409700184821 -0.00208640723499666 -0.002607385038848666; 0.00031361794665910655 0.0005599003078044272 -0.0023114755432596876; 0.0014662913275148583 0.0018267169142302773 -0.004122515858525657; 0.0038631206889168388 0.0011377896985500335 1.1080511108063108e-5] %
+
+Mass Used: 85.62767434720581 kg
+Launch C3: 96.96380983385357 km²/s²
+||V∞_in||: 3.1071551293061853e-8 km/s
diff --git a/archive/ES_0.5582197619834167 b/archive/ES_0.5582197619834167
new file mode 100644
index 0000000..a77c87e
--- /dev/null
+++ b/archive/ES_0.5582197619834167
@@ -0,0 +1,22 @@
+archive/ES_0.5582197619834167---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:32:12.323
+Launch V∞: [7.875895271517658, -5.75697847919737, 0.13979139591785267] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0001979844168511949, -0.00017331720905102324, -0.00013957694323562392] km/s
+ V∞_out: [-2.7506600728635602e-5, 0.0001529610290281659, -0.0002473588815028516] km/s
+ time of flight: 1.8749577787521222e8 seconds
+ arrival date: 2030-04-23T10:41:49.323
+ thrust profile: [0.36780553654887194 3.30851289392489e-5 -0.11263723915245542; 0.1791223744638217 0.10539954668474985 -0.19057563848649478; 0.059524225749350214 0.05825496593595629 -0.1187812184762908; 0.024648468531983145 0.03163835257319003 -0.07620905441488703; 0.013690825185799872 0.02143850341601643 -0.05771172650290246; 0.010445730819989327 0.019372349131644366 -0.056873265820853655; 0.008071976047272778 0.017426735791028165 -0.05476865822722756; 0.010307030196690268 0.026590089065005356 -0.08529140207670238; 0.007053085188709126 0.0204795029842572 -0.06962088655541748; 0.0002596764202083596 0.0017578770279734562 -0.010466445689190624; 0.0003313058028560311 0.0009382135212934459 -0.004270261290286473; 5.936913197882939e-5 6.662268562363611e-5 -0.0006876724946657377; -0.0012803451519498034 4.591751117128019e-5 0.001223683798187541; -0.00018446167607869929 -0.00020442626876654533 0.0009117638365398366; 0.0017464051033891394 8.633047965584265e-5 -0.0016195909714339432; 0.00015322436405563252 0.0006553755953849108 -0.001284883442607769; 0.00011392028150863123 -0.0003265134752346525 0.0004628825265766344; -0.0008760283325988853 0.00039801089522474434 0.00200639272794977; -0.0033863969331591136 -0.005479906788479958 -0.008114128806486553; -0.0006834509822778402 -0.0017530977890876265 0.006998005759063569] %
+
+Mass Used: 95.9693188093197 kg
+Launch C3: 95.19206917222853 km²/s²
+||V∞_in||: 0.00029785635355342746 km/s
diff --git a/archive/ES_0.5582204816686285 b/archive/ES_0.5582204816686285
new file mode 100644
index 0000000..bb6ccbd
--- /dev/null
+++ b/archive/ES_0.5582204816686285
@@ -0,0 +1,22 @@
+archive/ES_0.5582204816686285---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T22:44:19.006
+Launch V∞: [7.790416502851873, -5.767524585063807, 0.08730631689308162] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.018542377326411903, 0.11040734336551492, 0.13547232357582562] km/s
+ V∞_out: [-0.07484059923842296, 0.06037419657686663, -0.14699872035089906] km/s
+ time of flight: 1.874957778748909e8 seconds
+ arrival date: 2030-04-22T00:53:56.006
+ thrust profile: [0.43519302863343867 0.013631102893278242 -0.09354896669321308; 0.1595729859100796 0.11116692771969632 -0.14176996511810203; 0.08058342705070004 0.0926180425408089 -0.13628562303649358; 0.025070624309695245 0.041334010404141155 -0.0709266622055407; 0.03291731737918061 0.06831825031240628 -0.12437674895738492; 0.007794607467218093 0.02049926855390385 -0.04213004336438918; 0.00857528496448613 0.02984527437181259 -0.0624218599165083; 0.0062959329062029735 0.025662200809420558 -0.05886957474215523; 0.0044749644763779255 0.021395267062114726 -0.05062202478336823; 0.001550235795405443 0.009263899071991329 -0.02355465771805634; 0.00048045296490886865 0.0038244152421315113 -0.009566151801618574; -0.00017488673915712217 0.00020547134038525976 -0.0006752028822144774; -0.0004351569988650824 0.0003484176110244696 -0.0009586657251297822; 0.00013399461282364016 0.0004245029472580194 -7.734832409696702e-5; -0.0003163655967428148 -0.0002711443405938941 0.0002390714093283195; -0.00039959006738131257 -0.000822527737864102 -0.00044115602518012215; -0.00024937817248992314 -0.0008532511888964851 5.1905080338208564e-5; 0.0002835733427372918 -4.0272760411377606e-5 -0.0011240886879456847; -0.0003301697329192529 -0.00019602463249024263 -0.0001341910062069425; 0.000315647015603444 0.0009742949713198428 0.0014459794033413313] %
+
+Mass Used: 103.14234474561499 kg
+Launch C3: 93.96255152019168 km²/s²
+||V∞_in||: 0.17574513273766343 km/s
diff --git a/archive/ES_0.5582231348491308 b/archive/ES_0.5582231348491308
new file mode 100644
index 0000000..ec68eb7
--- /dev/null
+++ b/archive/ES_0.5582231348491308
@@ -0,0 +1,22 @@
+archive/ES_0.5582231348491308---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T19:44:05.971
+Launch V∞: [7.979432403594191, -5.554316751997275, 0.13227091316130427] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6483146260968461e-9, -1.5911772708279004e-9, -2.008068641605107e-9] km/s
+ V∞_out: [-2.030525289134139e-11, 7.552100235140036e-11, -1.1704994611868727e-11] km/s
+ time of flight: 1.8749577787441722e8 seconds
+ arrival date: 2030-04-20T21:53:42.971
+ thrust profile: [0.48983826356210564 0.012028055479063732 -0.128824123916752; 0.07993352217256873 0.053129680345467056 -0.08275700172461696; 0.046924618613070464 0.051503749130236136 -0.08986311793535409; 0.04991618179149508 0.07573217261230304 -0.14328852813500573; 0.026733233164813897 0.05188879287796231 -0.10923601576869843; 0.012496545543662141 0.029099675373919467 -0.06939318048970453; 0.007182122195775603 0.020016261992486028 -0.05143219309508018; 0.005908790378710313 0.0201621866481484 -0.053722092964141696; 0.0034186673157541032 0.015174613603377766 -0.04277132640806453; 0.0024290507422025025 0.011731521955692005 -0.03563984366823173; 0.00037993024107952386 0.002366639781205545 -0.00766366442888483; 0.00036290301193984975 0.0005841509935518264 -0.0031509634354158086; 0.00017134532501398607 0.0005267489564224764 -0.001272500545828123; 0.0004135208643787021 -0.0004284312082196999 0.00010306082603498659; -9.88618529820975e-5 0.000822695167686274 0.00012240965284266944; -1.2678717806988778e-5 0.00015109401237899692 0.00025949675171498964; -0.001520231816158195 -0.0007944761727219387 0.0004715357238230006; -0.000784794838141614 -0.00029826878787936784 -0.0008053449047667708; -0.002181420345912224 -0.00038862346065448845 -0.000996186562494704; -0.0020697970057516222 0.001545408602341718 0.002346574244459653] %
+
+Mass Used: 99.78123931014807 kg
+Launch C3: 94.53927165951507 km²/s²
+||V∞_in||: 3.046494031374736e-9 km/s
diff --git a/archive/ES_0.5582244620338999 b/archive/ES_0.5582244620338999
new file mode 100644
index 0000000..b20034a
--- /dev/null
+++ b/archive/ES_0.5582244620338999
@@ -0,0 +1,22 @@
+archive/ES_0.5582244620338999---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T18:16:38.365
+Launch V∞: [7.8100666067261395, -5.761494744186853, 0.0698267063815002] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3680102657441417e-5, -0.000923681812620588, -1.6120123844754975e-5] km/s
+ V∞_out: [-0.0008967563440512013, 0.000139057699221996, -0.00017362448318515385] km/s
+ time of flight: 1.8749577787267798e8 seconds
+ arrival date: 2030-04-22T20:26:15.365
+ thrust profile: [0.4551271248732553 0.013611082208449692 -0.13315837875204783; 0.12140508127256246 0.07549393019689721 -0.1253851595387308; 0.088557294666133 0.09050149526075651 -0.1662717813980516; 0.04167127317789033 0.05679264914716499 -0.12050501966061196; 0.02847138700491549 0.04846148594917653 -0.11384313610987802; 0.012411171475195085 0.025768621347263414 -0.06755201572307935; 0.0048940270791303754 0.012215212322271435 -0.035687860664560436; 0.004393578889172479 0.013926136965126321 -0.04306899331316483; 0.0016749622913976542 0.006014911547792062 -0.01991736025147881; 4.553638293816506e-6 0.0015918802158777865 -0.005296034005809247; -0.000548919262531766 0.0006020803278122446 -0.002116840762449819; 0.0003229965432601 -0.00039804560518396444 0.00025524453125450736; -0.0020482401009822987 -9.558807391507901e-5 -6.206296428809413e-5; -0.0017276731156209502 -0.0006636736029907316 -0.002391056101848253; 0.0008409867887897034 0.0003446888671935844 -0.000475523447587168; -0.0007558410665194217 -0.0009648163082666236 0.006854878600811955; -0.003766020776416084 -0.0019641467462073355 -0.004489803566328025; -0.003099227068305929 -0.001195096050435014 0.00019824578814202029; -0.002248180902057021 0.00686920459025804 -0.004528405418143439; 0.003991022264281831 0.0019519937243935716 0.003958684575839283] %
+
+Mass Used: 101.7803182028756 kg
+Launch C3: 94.19683785771558 km²/s²
+||V∞_in||: 0.0009239237493254209 km/s
diff --git a/archive/ES_0.5582254971742153 b/archive/ES_0.5582254971742153
new file mode 100644
index 0000000..09592b7
--- /dev/null
+++ b/archive/ES_0.5582254971742153
@@ -0,0 +1,22 @@
+archive/ES_0.5582254971742153---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:04:47.033
+Launch V∞: [8.087089584056763, -5.629111099788522, 0.3474686498023338] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.03094071739401e-9, -5.039628915146699e-9, -6.112166567595456e-10] km/s
+ V∞_out: [-1.1561267904445608e-9, -2.6248596676136066e-9, -6.774315024711203e-11] km/s
+ time of flight: 1.8749577787295964e8 seconds
+ arrival date: 2030-04-23T21:14:24.033
+ thrust profile: [0.3214284451633336 -0.006144260765433404 -0.11291492182253256; 0.047106571849000085 0.02397004493098545 -0.06042766486142519; 0.04068987300812848 0.032633269199025323 -0.09338333548421947; 0.03608446332728067 0.03706066666752774 -0.12112620216622644; 0.026912732575372144 0.03254471602029311 -0.1198001567408321; 0.01576407533094013 0.021335506020064864 -0.08775536872657766; 0.010199357978886195 0.015086408688876715 -0.06797776781319459; 0.006235131806361638 0.0099818864364713 -0.048709258303367316; 0.003421791376484202 0.005752774037808923 -0.030933406779623616; 0.004791521284498384 0.008692224515330735 -0.04714975979727212; 0.0009771383533200449 0.001992637004683833 -0.011961182217050736; 0.00029248081862633666 0.0006095482577155054 -0.0016852340890213839; 0.00019637672926270378 -0.00031117132095860383 0.001902783532745666; -0.00048324181600647314 -0.0016978793359236758 0.0033259790038892493; 4.1814274935370846e-5 0.0002708953864157339 0.0029204260415965416; 0.0017001739937590782 -0.001913540823819755 0.0006512548220157025; -0.0008729048156074727 -0.0022003134522808124 0.0025135799250299374; -0.00043455731641944064 0.007038617196836233 0.0016259475512468958; -0.005144079836493844 -0.00428749282989447 0.00524625480119404; -0.0005007863313409076 -0.000738784260944445 0.004709546943515195] %
+
+Mass Used: 84.21265567123419 kg
+Launch C3: 97.20864417691719 km²/s²
+||V∞_in||: 5.4677386186111625e-9 km/s
diff --git a/archive/ES_0.5582276644245129 b/archive/ES_0.5582276644245129
new file mode 100644
index 0000000..15fe3a7
--- /dev/null
+++ b/archive/ES_0.5582276644245129
@@ -0,0 +1,22 @@
+archive/ES_0.5582276644245129---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T13:33:14.112
+Launch V∞: [8.013237447543197, -5.642105630418114, 0.08392485597186523] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.4813489854735056e-9, 5.795050576482324e-8, -1.0565655154171939e-8] km/s
+ V∞_out: [8.963093032305165e-9, -3.373353218746987e-8, -4.7261878252806e-8] km/s
+ time of flight: 1.8749577786099967e8 seconds
+ arrival date: 2030-04-21T15:42:51.112
+ thrust profile: [0.32228857323377563 0.014979168936468553 -0.08370646391759846; 0.08755957615812796 0.06008618870589885 -0.08684079676891196; 0.07367292872726271 0.08739466546166592 -0.12954874517796508; 0.0316658874674204 0.050586643760630934 -0.09226673750951737; 0.025702217662966566 0.05428358641062737 -0.10406346845032838; 0.026318260219107235 0.06521313383088193 -0.13163840815696365; 0.005827171622561159 0.01793778521287515 -0.041920167458548555; 0.003036869423654982 0.013474230470712336 -0.03299737204426872; 0.0031212013410722426 0.015044296989890748 -0.03840794408064751; 0.003338656986784153 0.017968523154459508 -0.04612591070399376; 0.0004554121062851539 0.0029639706730536677 -0.008669311026007157; -0.0006720862341322685 0.0004254685987286028 -0.0008353716687336608; 8.667309125409039e-6 -0.0003326848645190549 0.0015113995719943903; 5.899810871318957e-5 0.0004121938567562377 -0.0011471893922910487; 7.155993869049351e-5 0.00030202969507565257 -0.0006596186368895498; -0.00012711436575203012 -0.0013149838025097722 0.0010929992697409213; 0.0004755643748910795 -0.0004599631576103526 0.0009563428381140636; -0.0007265031643431326 -0.0016164039536733519 0.002019739695542525; -0.0005079808097247122 -4.9975026051484925e-5 0.0021474397911394275; 7.655639277561129e-5 -0.00011150738103829014 0.0014687945527865674] %
+
+Mass Used: 90.96009514636489 kg
+Launch C3: 96.0523737169543 km²/s²
+||V∞_in||: 5.9261303326092906e-8 km/s
diff --git a/archive/ES_0.5582300391587557 b/archive/ES_0.5582300391587557
new file mode 100644
index 0000000..606aa21
--- /dev/null
+++ b/archive/ES_0.5582300391587557
@@ -0,0 +1,22 @@
+archive/ES_0.5582300391587557---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T05:26:10.497
+Launch V∞: [8.258789324865175, -5.5925174692549415, 0.15644862348039368] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.427459268012468e-5, 4.603824717415904e-5, 0.003133273064122816] km/s
+ V∞_out: [-0.0027929791612548217, -0.0009620793899384417, 0.0010479803060652586] km/s
+ time of flight: 1.8749577787493154e8 seconds
+ arrival date: 2030-04-24T07:35:47.497
+ thrust profile: [0.13543022577990332 -0.007255017132095456 -0.051671818851327586; 0.051192798919196765 0.024603292652650557 -0.06835122434482947; 0.027568851142183114 0.019765868716159263 -0.06631827704702913; 0.033656073321808616 0.030320450949499624 -0.11129546047099874; 0.01825245016855381 0.018986480507400347 -0.08185224496623579; 0.012378030191939815 0.014400481185460631 -0.06949799130586638; 0.01786904297496395 0.022532869285944054 -0.12058497073453435; 0.012451300625024881 0.018351151020960473 -0.10685123093093707; 0.0059558755494505695 0.008319864004554887 -0.051979662432940284; 0.002421560724685584 0.003367402886783924 -0.023852128866026744; 0.0008460791922515885 0.000899494570218448 -0.0070492866702805326; -0.0011269084511787758 0.0019333810508127564 0.0016352668033363825; 0.0004290166979137671 0.0012212221487144354 -0.008183752371938094; -0.0030238116795602865 -0.0014159659397675142 0.00025767056346826867; 0.0010185685207301288 0.0018383905977893997 -0.005480884997478728; -0.002255019633100661 -0.0009819630327238325 0.0014149523732216044; -0.005968545897689263 0.0014723450167303627 -0.00014734004717429543; 0.0006946426361138529 -0.00041647636534732074 0.0018372658603789602; -0.002199780288920486 -0.003755204599410082 0.004123830115182997; -0.003291938400762009 -0.00563224554898288 0.0024274459790018235] %
+
+Mass Used: 70.8031269372791 kg
+Launch C3: 99.50832892821758 km²/s²
+||V∞_in||: 0.0031342703836498603 km/s
diff --git a/archive/ES_0.5582385111553505 b/archive/ES_0.5582385111553505
new file mode 100644
index 0000000..630c630
--- /dev/null
+++ b/archive/ES_0.5582385111553505
@@ -0,0 +1,22 @@
+archive/ES_0.5582385111553505---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T02:31:47.742
+Launch V∞: [7.8774024807270395, -5.862059090178596, 0.2101816533239587] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.859785848053225e-7, -6.913207974800158e-7, -6.341171505523664e-8] km/s
+ V∞_out: [5.7813127849231905e-8, -2.954215485234778e-7, -7.964007268843853e-7] km/s
+ time of flight: 1.837812875656949e8 seconds
+ arrival date: 2030-03-10T04:53:14.742
+ thrust profile: [0.28623589389640736 0.0020107146992136993 -0.0809524923083333; 0.07078088635367778 0.04558811110295893 -0.07178987487536981; 0.08706826172860835 0.09035489241856363 -0.14969832916228604; 0.037886130599133136 0.053359839633922296 -0.10280604645156818; 0.030893217699051016 0.055842043033024265 -0.1162676232525865; 0.02482884186909009 0.049625058296319316 -0.11146244897026278; 0.014207156047150508 0.03510125034817359 -0.08291545770902795; 0.006674683803683484 0.019219381331320565 -0.05126061741383854; 0.0027987252546384524 0.008057374847148297 -0.021947481832586425; 0.0013272384880022986 0.004695534820583365 -0.015592127022296929; 7.88876695870112e-5 0.002247632398662093 -0.006600780128036748; 0.0014849192022890357 0.0009929926986500552 -0.006767883849638644; 0.0021641610716486752 0.00036756049163183183 -0.0006120847076755524; 0.0009910453768559727 -0.0005856061078448782 -0.0059427556748777866; 0.0023402179213793273 -0.0024993319073937674 -0.0011063909968968074; -0.0020031229952140166 0.0006317813225078724 0.0016357745536532617; -0.0008726747400979774 0.0027123523868270924 -0.003042601786771353; 0.0006112345121948343 2.2978630379946087e-5 -5.718962027173634e-5; -0.004430895482272372 0.0004208440724489476 -0.0005464935681248507; -0.000346138621197969 -0.0018998064315019947 -0.0035697729345717717] %
+
+Mass Used: 88.5868624874688 kg
+Launch C3: 96.46138294750402 km²/s²
+||V∞_in||: 8.474200112836819e-7 km/s
diff --git a/archive/ES_0.558248506312494 b/archive/ES_0.558248506312494
new file mode 100644
index 0000000..af22607
--- /dev/null
+++ b/archive/ES_0.558248506312494
@@ -0,0 +1,22 @@
+archive/ES_0.558248506312494---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T13:03:56.627
+Launch V∞: [8.091743300220907, -5.712143831789252, -0.1477416921479455] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.5695852069964734e-6, -2.9167924558835643e-5, 0.0006997408084478834] km/s
+ V∞_out: [2.950495739289843e-5, -0.0006374492773101078, 5.013742253598073e-6] km/s
+ time of flight: 1.8749577786946008e8 seconds
+ arrival date: 2030-04-24T15:13:33.627
+ thrust profile: [0.21079165872324263 -0.005448175587982283 -0.0729116445080209; 0.08156468180103897 0.042927012806058366 -0.0993122122862645; 0.04699409530421641 0.04106195476703333 -0.10737331099538144; 0.022981963032600614 0.024590546075619703 -0.08108872094676768; 0.01719685755620519 0.022220037833532727 -0.08154471917096803; 0.014611575291561619 0.022555262348389615 -0.08598512332644924; 0.021690073042678597 0.03318676340188037 -0.13589204232772464; 0.0058299141927266864 0.010220206727531763 -0.04859850104544845; 0.005114166746664961 0.011176738637610801 -0.05673089527817289; 0.0013758432349881443 0.003874188484185555 -0.021067928530274255; 0.0003951163153852191 0.0008838504144996261 -0.006657509332377806; 0.0006518508512720715 0.0005633331579506937 -0.004103029168913953; 0.001532673323563456 -0.0002884901455078963 0.0029780933525030044; 0.0013681133175070682 0.0023362338095497177 0.0016916678541916124; 0.000309824689642548 -0.0006255433300370471 0.004372398878857081; -0.0011516636351530556 0.0007093444369725653 0.003993100774666909; -0.00018962243098725147 0.0010759757841427295 0.000635251801926834; 0.0010679141207860748 -0.00034108418423533306 -0.00021525975761515245; 0.0038374997005070017 0.0006026149034240721 -0.00029774707259403095; -0.005032916691349485 0.003355896190986619 -0.001207723264249759] %
+
+Mass Used: 78.88403170189576 kg
+Launch C3: 98.12672439931667 km²/s²
+||V∞_in||: 0.0007003633685019023 km/s
diff --git a/archive/ES_0.558253049116968 b/archive/ES_0.558253049116968
new file mode 100644
index 0000000..aafe577
--- /dev/null
+++ b/archive/ES_0.558253049116968
@@ -0,0 +1,22 @@
+archive/ES_0.558253049116968---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T21:04:54.866
+Launch V∞: [7.636805917365132, -5.8463540331489305, 0.29713852979412275] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008335789557032828, 0.049316695740313575, 0.056501365541600776] km/s
+ V∞_out: [-0.014653471893545328, 0.011967891488997523, -0.07300260589172673] km/s
+ time of flight: 1.8749577520077434e8 seconds
+ arrival date: 2030-04-22T23:14:29.866
+ thrust profile: [0.6112785381257004 -7.643865148100723e-5 -0.09943938295489803; 0.11792109404381462 0.08087038004237534 -0.11296122217201524; 0.037738465057076113 0.04193679202355498 -0.06640256174760308; 0.03838147506222236 0.06198268023178759 -0.10762189483523582; 0.05206219839719662 0.0916579017040095 -0.15099964131545224; 0.010499794287163891 0.025150698475311765 -0.05269112612263994; 0.012926560374230747 0.03787642301792226 -0.08325331636779179; 0.005776853730456011 0.021466960439175023 -0.05074318491480568; 0.0012809525198510358 0.005345248728603577 -0.013268253662287519; 0.0033907136219332628 0.01470330918110475 -0.037661572437432435; 0.0011823355400603789 0.006865895105950754 -0.019657340867394596; -5.0220498961498695e-5 0.00018907038994212623 -0.00029808920969392577; 0.00046490278664043183 0.00048237922397635527 -0.00012143658742278603; 1.7345155541845494e-5 0.00011769406003878812 -0.0004517761670013817; -5.0641562490238285e-6 0.0001245835085947041 -0.00025031382529040866; 0.00021144180032876147 0.0002319842890433825 -9.794507924458745e-5; 3.6201815833806654e-5 -6.858633175432641e-5 0.0004270791075264255; -0.000357068284694605 6.267110319735359e-5 -6.0603369940503485e-5; -0.00010620020962882768 -0.0002474101503173627 -0.00019116637579916847; 3.409448449396051e-5 -0.00028333874498178964 0.0002800895485751084] %
+
+Mass Used: 111.19300743299891 kg
+Launch C3: 92.58895140630808 km²/s²
+||V∞_in||: 0.07545877135461054 km/s
diff --git a/archive/ES_0.558261261306652 b/archive/ES_0.558261261306652
new file mode 100644
index 0000000..6f96cd0
--- /dev/null
+++ b/archive/ES_0.558261261306652
@@ -0,0 +1,22 @@
+archive/ES_0.558261261306652---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:00:44.589
+Launch V∞: [8.079839894943373, -5.609646085866149, 0.23185187431408105] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.932219727488765e-9, 1.5168462828361432e-8, -7.966544505637788e-8] km/s
+ V∞_out: [-1.88715488213426e-8, 7.43425890167493e-8, -1.2023469208501248e-8] km/s
+ time of flight: 1.874957778762703e8 seconds
+ arrival date: 2030-04-22T18:10:21.589
+ thrust profile: [0.31878777820220094 0.0028264899398635713 -0.09453703902013937; 0.06250844309293925 0.03803638503392201 -0.07130639218992066; 0.05017408088637655 0.04966924298279438 -0.1031279612506169; 0.037005782731831374 0.04889752721282012 -0.11394267191744627; 0.016456805539947522 0.026574451990063697 -0.07101528495034569; 0.020430020096895866 0.04093078149543946 -0.11441008330652147; 0.011410319107591414 0.02653081807468239 -0.08253233930133329; 0.0052015294268912505 0.012965388087964437 -0.04457716165089598; 0.0032619544627495423 0.006837274601090199 -0.026573348313151522; 0.0025131911718620217 0.007063995948027518 -0.028094754591300997; 0.0026366733794567577 0.00790671818068812 -0.03190755006447335; 0.0011000214777288908 0.004118909337866688 -0.017992733294431767; -0.003935288205872332 0.0006053369953966241 -0.0020211023406820883; 0.0006436794111557957 0.0006456525954635409 0.003516771218420457; 0.0011374508151838969 -0.0003622739507793879 0.002685630514603172; -0.0002873911396223158 -0.00043929141201210094 0.00017277561581049137; -0.000334673775736007 -0.0001822209941367463 0.0025129923870262257; 0.0008602894560059573 -0.0022421867722852117 -0.0007246168986851022; 0.004175822304510649 0.005030576464869258 -5.8403372054950416e-5; -0.0017499258097415007 0.004270570811626384 -0.0001992475264966077] %
+
+Mass Used: 86.60490435984048 kg
+Launch C3: 96.8056972282149 km²/s²
+||V∞_in||: 8.148365179845162e-8 km/s
diff --git a/archive/ES_0.558267202079036 b/archive/ES_0.558267202079036
new file mode 100644
index 0000000..b8014a8
--- /dev/null
+++ b/archive/ES_0.558267202079036
@@ -0,0 +1,22 @@
+archive/ES_0.558267202079036---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:27:41.587
+Launch V∞: [8.142013280381937, -5.602007383836249, 0.16587551665907177] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.357298886625546e-6, -4.600157469567562e-6, -0.0003154341752319016] km/s
+ V∞_out: [0.00027965402865322395, 9.978915813197946e-5, -0.00010763187437070008] km/s
+ time of flight: 1.853271088313302e8 seconds
+ arrival date: 2030-03-27T14:12:49.587
+ thrust profile: [0.23635992095268035 -0.00687507891030642 -0.07629281201059886; 0.06990445886429286 0.03836200875043833 -0.0787806646660286; 0.055924192797408824 0.04982099140443248 -0.11339343672713345; 0.04457146664353052 0.05216278858305078 -0.13377079840374986; 0.029619847012846978 0.04192249444405475 -0.12001524214723011; 0.018536434739254946 0.03068614953639116 -0.09573952273094258; 0.011117725480623552 0.02101993129043322 -0.0704138636176785; 0.005045405111477938 0.010829878792525656 -0.03881406282266839; 0.0029902538386859887 0.006808594028760152 -0.026714538316034292; 0.0020223740216317038 0.005221911400241879 -0.020747760973055227; 0.0011239233578989648 0.003341162213387654 -0.013708383661821009; 0.00047621663626246785 0.0015734849436252825 -0.007633289012283979; -0.00017617020834650153 4.614030683214418e-5 -0.003597783800536758; 0.00017697343024906465 0.0007196824620351841 -0.003437379068379298; 0.0002583739444063657 0.00022968317947099628 -0.000704710140317952; 0.002458393073994109 0.002456661884452156 -0.008448388928247896; -0.0006194392165185417 0.0018647713139066952 0.00029293230657784393; -0.001734806316733127 -0.005642000462333459 -0.002922646822661022; -0.0029001150523282277 0.005476268969418401 -0.008788756032136243; 0.0001405773009829081 0.00014233914095022285 -0.0007304022719786009] %
+
+Mass Used: 81.38117599680027 kg
+Launch C3: 97.70238167349859 km²/s²
+||V∞_in||: 0.0003155317663914502 km/s
diff --git a/archive/ES_0.5582682439298726 b/archive/ES_0.5582682439298726
new file mode 100644
index 0000000..705ab80
--- /dev/null
+++ b/archive/ES_0.5582682439298726
@@ -0,0 +1,22 @@
+archive/ES_0.5582682439298726---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T10:11:42.260
+Launch V∞: [7.813368580708335, -5.741513641260686, 0.17104545198893714] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.222708289804032e-5, 4.055503187002247e-5, 0.0030086159829206555] km/s
+ V∞_out: [-0.002703351394105764, -0.0008377010144248432, 0.0010192015712120024] km/s
+ time of flight: 1.8556126473212767e8 seconds
+ arrival date: 2030-03-29T02:59:26.260
+ thrust profile: [0.4161084372298065 0.013834769773549919 -0.10358646561788781; 0.1912096517536203 0.13170901183359665 -0.16921738837610092; 0.049696191655111854 0.05503596363863666 -0.0852277476252626; 0.0451002067568834 0.06870157483849795 -0.11562351599545709; 0.038769858435360155 0.07609015765436061 -0.13755240322397555; 0.023152973715301322 0.05640973607479714 -0.11117193754236304; 0.011127202529665493 0.03305058319029588 -0.07109510093695559; 0.0020126835278800295 0.007427444203811826 -0.017664527412477406; 0.0012805755618370113 0.00555063948626631 -0.013881746822832455; 0.0003333537599739536 0.001692892530575228 -0.004761288766206498; -0.0007480411555821339 0.00021708787159477192 -0.0008570903105549971; 0.00018525896217317647 -0.0004945041231330702 -0.00014596932603716956; 0.0007552988971168972 3.250006762255627e-5 -0.0007204666084270016; 0.0002138298447406637 0.00010763002681144466 -0.00028085638637328136; 1.657050430555514e-5 4.369020460816199e-6 0.0005092844791926736; 0.00038210527024260064 0.0013071012976532662 0.0003588791168622411; 0.0003793078129640562 -0.0020699976347331303 -0.00039966919967506913; -0.00015652055898046047 0.0006109365573854933 -0.0014632736396082073; 2.6468318845780678e-5 5.1024880496916905e-5 0.0010818217093087935; -0.0013954532080646916 0.0014043202370921867 -0.0006282841885336667] %
+
+Mass Used: 102.72899448318321 kg
+Launch C3: 94.04296401742882 km²/s²
+||V∞_in||: 0.0030095326968055357 km/s
diff --git a/archive/ES_0.5582772496193174 b/archive/ES_0.5582772496193174
new file mode 100644
index 0000000..812668e
--- /dev/null
+++ b/archive/ES_0.5582772496193174
@@ -0,0 +1,22 @@
+archive/ES_0.5582772496193174---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:53:29.361
+Launch V∞: [7.9185040603679875, -5.646528724743902, 0.13709649317561798] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.12760684199642e-5, 3.761160556350544e-5, 0.002538901725425234] km/s
+ V∞_out: [-0.002246064586564528, -0.0007581952101151132, 0.0009075328501636856] km/s
+ time of flight: 1.858252747152424e8 seconds
+ arrival date: 2030-04-01T22:01:23.361
+ thrust profile: [0.4808556148606809 -0.003937764660488474 -0.11794984036971821; 0.0979901945373992 0.06137795570042542 -0.099115417956501; 0.03843312890632953 0.03973658651455043 -0.07527519404958907; 0.02643960106921228 0.03782841381656204 -0.07784816246603098; 0.022422450068330078 0.03982260332636634 -0.09212226711440827; 0.020058679366255074 0.04495834505408851 -0.11135498458946115; 0.009107885004541946 0.021903591052705215 -0.05885679396434576; 0.015438763645667118 0.04530789074285233 -0.11655922365388363; 0.0035575819052754924 0.012997936509912562 -0.039011802156068594; 0.0018476532394922955 0.007283432394158237 -0.02433805519204044; 0.0011076524355770555 0.00545194250964776 -0.018940761156162285; 4.4797471620300794e-5 -0.00016407184685667377 -0.00021014159567849422; -0.00029108043586519397 -0.0004994600230932712 -3.1246251587478246e-5; 0.0014458847256544694 0.00204882140045412 -0.00020480509086356641; -0.00013439446214662595 -0.0004949001571120455 -2.0393899775564012e-5; -0.00056579962575071 -0.0015124565533563095 0.0006877132111376642; 7.413419414984612e-5 0.002410837947043043 0.00021537739807136027; -2.337063150557021e-5 0.0002265516733533638 -1.0539177723855545e-5; -0.0021615238212965814 0.00135333142581663 -0.0005370736015966342; -0.00017675292732078105 0.0006894815355605596 0.0012696898681837793] %
+
+Mass Used: 99.46219081166737 kg
+Launch C3: 94.60478864186335 km²/s²
+||V∞_in||: 0.0025396979819326754 km/s
diff --git a/archive/ES_0.5582859306532536 b/archive/ES_0.5582859306532536
new file mode 100644
index 0000000..55b2283
--- /dev/null
+++ b/archive/ES_0.5582859306532536
@@ -0,0 +1,22 @@
+archive/ES_0.5582859306532536---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T07:18:07.168
+Launch V∞: [7.6571096602151805, -5.736065578230386, 0.11248530082351331] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.866463293773686e-6, -2.796998355026782e-6, -2.757181328442053e-7] km/s
+ V∞_out: [2.401927386563005e-7, -1.170318946949276e-6, -3.1542631503519947e-6] km/s
+ time of flight: 1.8360334104973936e8 seconds
+ arrival date: 2030-03-06T08:13:48.168
+ thrust profile: [0.7141082051479495 -0.019407926967992446 -0.19962725754195867; 0.11902120627795408 0.06611813501946341 -0.12453166949555622; 0.07166941549905255 0.06572581266050087 -0.1366577582328687; 0.034568147749793804 0.0416932937017992 -0.09843292098632449; 0.03364686258283509 0.05057986545059861 -0.13122327794183603; 0.02183089656008655 0.04064085526735642 -0.11385044467524644; 0.0035363422826558263 0.007704015190644318 -0.023002284589881898; 0.007094685142321074 0.015056323046070106 -0.04920254771831077; 0.0007655999119648594 0.0037590593981467785 -0.014707404543027765; -9.74626816389614e-5 0.0023763817033990472 -0.0096437954111777; 0.00048158662863665645 0.000953170005518501 -0.007615290750561214; -0.0004747642817467363 3.824853420907894e-5 -0.0006786999148474233; 0.0020175495049944052 0.0016081709800050664 -0.0003498122945055325; 0.0008145734478808683 6.581135994074272e-5 -0.0008363058211539229; -6.042070304585758e-5 0.0020036835682165385 0.00016067363782892863; -0.0004973588087302415 -0.001612766635030592 0.0013425611960212489; 0.0009507269839023259 -0.0011219206837421057 -0.0027138835462953755; -0.0008139417806182195 0.0008493113617650957 -0.002922245566518977; -0.0005101162375975695 -0.0012787485329099429 -0.00043479368580340565; -0.0008446167223614526 4.7717832761674415e-5 -0.005052100062583169] %
+
+Mass Used: 117.31274637500383 kg
+Launch C3: 91.54642960922149 km²/s²
+||V∞_in||: 3.3738561785894397e-6 km/s
diff --git a/archive/ES_0.5582866696571323 b/archive/ES_0.5582866696571323
new file mode 100644
index 0000000..874d2f4
--- /dev/null
+++ b/archive/ES_0.5582866696571323
@@ -0,0 +1,22 @@
+archive/ES_0.5582866696571323---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T10:19:22.262
+Launch V∞: [8.072728344317964, -5.605289910777402, 0.31158007008653493] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.154780093742142e-11, -4.862833852433797e-10, -9.706014479569497e-10] km/s
+ V∞_out: [1.6111957985922686e-9, -1.5035594589502462e-9, 5.617384782788469e-10] km/s
+ time of flight: 1.8749577787364632e8 seconds
+ arrival date: 2030-04-22T12:28:59.262
+ thrust profile: [0.31031489532832307 0.002589472113997352 -0.09528327997777654; 0.0874479062642655 0.053118182781571904 -0.09640068498704249; 0.046461338007123855 0.046196301858484126 -0.09490357993622117; 0.039128204693896794 0.05123714051587649 -0.11923676212449098; 0.03421723975298872 0.058050961089347854 -0.1467350546004534; 0.013507598355862521 0.02617808704494831 -0.0753296093514847; 0.005826391156959983 0.011929647035775197 -0.03911625975428397; 0.002702735634785813 0.0066563742725620975 -0.022978171352745085; 0.0040449995080923 0.009291677737851032 -0.03688434987373732; 0.005763355348531194 0.014695174731990213 -0.05007686116454923; 0.0004163860445829137 0.0019937204781959703 -0.004947214600902599; 0.00041840859710318644 0.0016849389410438405 -0.005979751547994361; -0.0016313940271630643 0.0005923641827365833 -0.001000832261885591; 0.004071762072134954 0.0010751259652014042 -0.0012008984734168415; -0.0004576769181410328 -6.93090022348026e-5 -0.00018510557194885077; 0.0015946113591446464 0.004928466898700992 -0.00428586278698647; 0.0007685875428887357 -0.00479558491284532 -0.005726630952193082; 0.0037303409550797023 0.006921668951910218 -0.0012298185718965485; 0.003200589729433186 -0.004652656015905692 -0.007438246620176731; 0.00021197175815764873 -0.00341794513286869 -0.003986973921069292] %
+
+Mass Used: 87.33686433694675 kg
+Launch C3: 96.68530004509272 km²/s²
+||V∞_in||: 1.085819049964186e-9 km/s
diff --git a/archive/ES_0.558292932452159 b/archive/ES_0.558292932452159
new file mode 100644
index 0000000..c720bba
--- /dev/null
+++ b/archive/ES_0.558292932452159
@@ -0,0 +1,22 @@
+archive/ES_0.558292932452159---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T20:21:50.742
+Launch V∞: [7.765537042945469, -5.739099487780317, -0.04553936534075895] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.3417119079251945e-9, 5.26898492513628e-9, 2.5315338338784267e-9] km/s
+ V∞_out: [4.673663444289525e-9, -3.783978429468654e-9, -2.860771756040811e-9] km/s
+ time of flight: 1.874957778740273e8 seconds
+ arrival date: 2030-04-22T22:31:27.742
+ thrust profile: [0.6034287792494042 -0.018732956409098927 -0.14462308284378234; 0.06630920289300116 0.04575993272552387 -0.07348731993978125; 0.03799391719811507 0.04762039511467938 -0.07606311162854466; 0.030779452712014637 0.04915946810092204 -0.0969357854747402; 0.035141270227506974 0.05464072821156992 -0.12242684545328988; 0.00969508608151937 0.027489554969466232 -0.07342581517739644; 0.019991230829026464 0.0439207828343593 -0.11343113178924037; 0.005607373838775056 0.015905061244707225 -0.04169981046021638; 0.006785172901505363 0.019194404894817104 -0.04724766965283797; 0.0009804625985018855 0.005593467373470904 -0.021169118218339406; 0.0012746048699418125 0.004128056007611464 -0.014528160950364535; 0.0011702924902042195 0.0011139384451958547 -0.004791858644373875; 0.001008821557254986 0.0012636343101872258 0.00015622255361861484; -0.0022394674679157224 -0.0023030137061295325 0.0020984107291217246; -0.0023305022437921856 0.0016661216667343732 -0.0013114933795706947; 0.00043432985788077034 -0.0008437090397550068 0.0003832235815784558; 0.0008031773961472556 0.0022733312886636632 -0.0022451692413262133; -0.00041830058643285576 -0.0011812188875472206 0.0022382278050522603; -0.0004930627553042132 -0.0006861116261827622 0.001978547035596706; -0.0006105753514548204 -0.0003428910520640779 0.001369907417390129] %
+
+Mass Used: 107.42482427038613 kg
+Launch C3: 93.24290232979419 km²/s²
+||V∞_in||: 6.7333427188101465e-9 km/s
diff --git a/archive/ES_0.5582949609829231 b/archive/ES_0.5582949609829231
new file mode 100644
index 0000000..d40d745
--- /dev/null
+++ b/archive/ES_0.5582949609829231
@@ -0,0 +1,22 @@
+archive/ES_0.5582949609829231---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:06:50.959
+Launch V∞: [7.633846424380127, -5.981897439643418, 0.05739980987965337] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.835346001838398e-10, 4.814667206387102e-10, -1.700120615910366e-9] km/s
+ V∞_out: [7.883156097595526e-10, 1.5476101491224015e-9, 4.096593963756147e-11] km/s
+ time of flight: 1.8245615155482095e8 seconds
+ arrival date: 2030-02-23T10:22:41.959
+ thrust profile: [0.4872464118265178 -0.016662888811333293 -0.12575818513171408; 0.13523326537946048 0.07288894002270913 -0.139730770445096; 0.08461412690983076 0.0773108088237699 -0.15863674318998036; 0.024002946303936856 0.02843773064358209 -0.07103900970965334; 0.02040035728527239 0.030150239963029884 -0.08131224571756629; 0.007977834389971357 0.01348597181819519 -0.04133035680202386; 0.02282458807502853 0.039362881667192415 -0.12281922009019623; 0.007716901915823591 0.017014544205433982 -0.05726376205645845; 0.004961316424544546 0.012312797620020247 -0.04423402983102171; 0.0037485250490158916 0.010257295778068424 -0.03834284900349501; 0.0005907261377410246 0.0018033479162399837 -0.0072783986711100835; 0.00021944446953736586 0.0006480249423822206 -0.0029111957681366572; 5.064189991918562e-5 0.00010699229000898447 -0.0005999517553627919; -7.582384119473272e-5 7.585234647264862e-5 -0.0005333218183683922; -0.00015606117115717555 0.0003162558819635303 -0.0007010437021333003; 1.8757875271621403e-5 0.0002889397468274777 -0.00032831320022698424; -0.00041347227888990186 0.0005170603590296738 -0.0006326917519229964; -0.0004866977015509791 0.00014707693947513207 -0.0002458139641439931; 0.00032159712929727413 0.000261201407715436 -0.0004502140944552783; -0.00010032813493435701 0.0002662729840399614 -6.8495074284830905e-6] %
+
+Mass Used: 102.64910395236393 kg
+Launch C3: 94.06200294760794 km²/s²
+||V∞_in||: 1.9755641476418965e-9 km/s
diff --git a/archive/ES_0.5582957304859738 b/archive/ES_0.5582957304859738
new file mode 100644
index 0000000..8d0b031
--- /dev/null
+++ b/archive/ES_0.5582957304859738
@@ -0,0 +1,22 @@
+archive/ES_0.5582957304859738---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T04:58:11.790
+Launch V∞: [7.854030286421064, -5.826310572455635, 0.02883911755180979] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.4906508715748877e-6, 0.00023045892060852426, 4.1857490757697825e-6] km/s
+ V∞_out: [0.0002156128323492731, -3.71262142355653e-5, 5.362876045805227e-5] km/s
+ time of flight: 1.851904136432752e8 seconds
+ arrival date: 2030-03-26T14:45:04.790
+ thrust profile: [0.342721372586263 -0.0003435928066858089 -0.09728135644357071; 0.12747125768247394 0.08417405387252107 -0.11758612759260383; 0.043690157699836446 0.049201852831946835 -0.07865935986896438; 0.02172472800089227 0.03155975671058982 -0.05811265282103877; 0.028336157886088478 0.06435120593923786 -0.12044660050043614; 0.01715682095146759 0.043108997114201394 -0.08858067883069858; 0.014652124703501445 0.03666108695114809 -0.08363809461261981; 0.011843442872075722 0.03932337831741849 -0.09207073381494847; 0.004512152330229904 0.021603921595460894 -0.05485021558845186; 0.0027484863535607923 0.012716758184719939 -0.03404703380250881; 0.00025555369170306364 0.002248308034489333 -0.006381674560202713; 0.0005096330333979151 0.0003681736172286526 -0.0014736552689630417; 0.0010333838115120673 -6.593329256856752e-5 -0.0009846980833936544; 0.0015406654922722795 0.0012132391489728075 -0.001287965730285398; 7.984563921190871e-5 -0.00026146595684106813 0.00028223350951504854; -6.841424126113665e-5 -0.0005681252376477965 -3.067969097966046e-5; -0.0009984979052818786 0.00028936863441550323 -0.00048513692454394937; -0.0006104248544909294 0.00029583198946938146 0.00018654368696281363; 0.0002310392226150038 -0.0010661865752295246 0.0015488601011091547; -0.00036643875016370325 -0.0002278635964295514 0.0013387583058433825] %
+
+Mass Used: 93.48866202530144 kg
+Launch C3: 95.6325183214288 km²/s²
+||V∞_in||: 0.00023052335939526523 km/s
diff --git a/archive/ES_0.558306293228093 b/archive/ES_0.558306293228093
new file mode 100644
index 0000000..39d5eec
--- /dev/null
+++ b/archive/ES_0.558306293228093
@@ -0,0 +1,22 @@
+archive/ES_0.558306293228093---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T09:43:41.022
+Launch V∞: [7.957192509335064, -5.781476529201746, -0.09054215821581289] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0015227014307356503, 0.001066660745582195, 0.06329139587435095] km/s
+ V∞_out: [-0.058161246868277984, -0.022612146559955307, 0.010684559366262274] km/s
+ time of flight: 1.8379717806960145e8 seconds
+ arrival date: 2030-03-10T16:29:59.022
+ thrust profile: [0.24689306898596158 -0.012132117599769085 -0.08389399429800552; 0.1998270980889175 0.10042912664389111 -0.21872300862021385; 0.021636255720877896 0.01829004563857777 -0.04812901848530735; 0.024965446175426145 0.027755654254886367 -0.08094166910732413; 0.02223445471517716 0.0279242421986889 -0.09810500523369389; 0.015106062747889878 0.025138026541948525 -0.0920577733346722; 0.007277331511339507 0.010906425558149826 -0.045043308270249285; 0.00861443698694062 0.02130511800179978 -0.0861118979409911; 0.004014697746244017 0.008682910814763044 -0.03540319364194756; 0.0023913875428633173 0.008748409282104339 -0.03684054250600134; 0.0031836006414409576 0.00909498686032319 -0.042871328952143545; 0.00027091213714863213 0.00029548965439908995 -0.00241748192875685; 6.820462481683953e-5 0.000639415206042128 -0.0035152167522261306; -0.00023249596619013977 -0.000605447708416504 -0.0006033402257928336; -0.00023385677896721832 -0.00016941331791687502 -0.0010592086307729192; 3.590723032662967e-5 -0.0008622076498716784 0.0002934876520173465; -0.0009740007879367786 -0.0008571611904442342 -0.00045285647718145143; -4.6681839854470985e-5 6.016546905694437e-5 9.734089321422894e-5; -0.0014705086604535841 0.0012893741999569978 -0.0019796603546777466; -0.0002110456716919103 -0.0007638280189851627 -0.0001633706650712763] %
+
+Mass Used: 86.97895077010708 kg
+Launch C3: 96.7505813707431 km²/s²
+||V∞_in||: 0.06331869531597394 km/s
diff --git a/archive/ES_0.5583127229271572 b/archive/ES_0.5583127229271572
new file mode 100644
index 0000000..8e1355a
--- /dev/null
+++ b/archive/ES_0.5583127229271572
@@ -0,0 +1,22 @@
+archive/ES_0.5583127229271572---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T12:06:55.484
+Launch V∞: [7.939631253568969, -5.971629217712973, 0.1167326296747197] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.090609021620356e-6, 4.110034833080362e-5, -0.0007365970201977876] km/s
+ V∞_out: [-2.7168865654865784e-5, 0.0007372024228560482, -7.111037689671375e-6] km/s
+ time of flight: 1.807601637326267e8 seconds
+ arrival date: 2030-02-05T15:16:18.484
+ thrust profile: [0.20870544662478913 -0.029229985572570102 -0.0835709587958329; 0.04954326688865746 0.015079144099785748 -0.0700010026122573; 0.04263773625139706 0.01986767288344445 -0.10510756089048116; 0.0380029066761596 0.020569491015531606 -0.1316909940238226; 0.03126447112159918 0.018101206729818693 -0.13755063757426586; 0.023495153752582782 0.014100268022230357 -0.12394676560919451; 0.0158351288514827 0.00973276097019951 -0.09675616577579517; 0.008980204040158733 0.005644764089232774 -0.06237648300921817; 0.0035242224217813143 0.0022967010668079072 -0.028261623012063218; -0.00029368889205091194 0.00044679026975432285 -0.0015897067139897473; -0.0008125070923012803 0.0009523456650008508 -0.004655165414815296; 0.0005579283119081472 -0.00031136019461085066 -0.004014800845247988; -0.0009341781994233302 0.0013346809099036869 -0.0026110047313132917; 0.0001304511948602182 -3.50912267487321e-5 -0.0018366228939363848; 0.0002047992420935469 -0.0005660065564154227 -0.0003943697507090408; -0.00044148497803182395 0.0011132348152998526 -0.00036491535897294463; -0.0017938734314801416 -0.0004631340828874309 -0.0006288321874698485; -0.0001675148956519552 -0.0003022988981319169 0.0005468306924134427; 0.0012774477319604917 -0.0005376889094869726 0.0006613405965744515; 0.00018361277974028296 -0.000534997886844439 0.0007473904782654677] %
+
+Mass Used: 75.54643904563136 kg
+Launch C3: 98.71172646332319 km²/s²
+||V∞_in||: 0.0007377541202049238 km/s
diff --git a/archive/ES_0.5583252620456866 b/archive/ES_0.5583252620456866
new file mode 100644
index 0000000..ddb6322
--- /dev/null
+++ b/archive/ES_0.5583252620456866
@@ -0,0 +1,22 @@
+archive/ES_0.5583252620456866---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T00:17:29.151
+Launch V∞: [8.066031835589579, -5.776808303703113, 0.08408529274610413] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3240714108461173e-8, -9.317130244813221e-8, 1.9021509677314238e-6] km/s
+ V∞_out: [8.386053955422675e-8, -1.9089499042732844e-6, 2.2756891294104935e-8] km/s
+ time of flight: 1.8371093533326998e8 seconds
+ arrival date: 2030-03-10T07:06:24.151
+ thrust profile: [0.15500274864290406 -0.0070376797894611464 -0.05705648265372819; 0.12730474206795386 0.0635512337961628 -0.1530007415216608; 0.024146349570332837 0.0189350470106662 -0.05329327579778419; 0.025144992657396347 0.02487521216811354 -0.07992548942704619; 0.026844146838033888 0.0344943689959329 -0.12290369352944364; 0.019128692659785895 0.028921012144064628 -0.11121897014473967; 0.009172365586040196 0.015198837666427977 -0.06330444421123585; 0.004500092941335703 0.008012928505773873 -0.035640603384151676; 0.0038373708991818207 0.007836186176035119 -0.03564329025652791; 0.010519068824685828 0.02146057122080207 -0.10267599231470596; 0.0014930176824871789 0.0030642006074734843 -0.01684114415597706; 0.00019832262303268823 0.00030050146548043794 -0.0019167009014751102; 0.0007600356358552974 0.0013794110549316034 -0.007967462003178445; 0.0008465945813583103 0.0005765616772192921 -0.0013284003593325249; 7.647531557729845e-5 0.00020213425662863 0.0007899027093839386; -0.0017986419188153599 -0.0009138719343634051 7.484100637044147e-6; -0.0020355762795957726 0.0007252404970128818 0.0025250451555315387; -0.0015365089005971067 0.0012604842341510654 0.001056041993363838; -4.545638509255071e-5 0.0004562742037609348 -0.00014944137943859295; 0.00021221560283409718 -0.0011632087826632985 0.0016770488357436073] %
+
+Mass Used: 77.14932354618577 kg
+Launch C3: 98.43945408693403 km²/s²
+||V∞_in||: 1.9044774905867425e-6 km/s
diff --git a/archive/ES_0.5583326892206952 b/archive/ES_0.5583326892206952
new file mode 100644
index 0000000..9e9da8e
--- /dev/null
+++ b/archive/ES_0.5583326892206952
@@ -0,0 +1,22 @@
+archive/ES_0.5583326892206952---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T02:56:46.639
+Launch V∞: [7.970079309270294, -5.779987736306817, -0.4890036313019999] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.029439416309181e-9, -2.6913540507908606e-9, -2.202098375378865e-9] km/s
+ V∞_out: [-9.778131794078748e-10, 8.706681321351485e-10, -3.326968489634116e-10] km/s
+ time of flight: 1.8749577787720206e8 seconds
+ arrival date: 2030-04-24T05:06:23.639
+ thrust profile: [0.27304320395336645 0.001916998120726803 -0.08199966506578386; 0.09201242420290096 0.05817100197899865 -0.10364326983037674; 0.04363484885488664 0.04578604399407639 -0.09222249390149685; 0.0368204285157867 0.04985844293019598 -0.1139595225457395; 0.016938117591971683 0.029488301171058676 -0.07783677239262973; 0.017523496185278205 0.039072098990857715 -0.10647784735047618; 0.014838397980934883 0.035403016728568715 -0.10107029517607062; 0.006113492128224345 0.017466945272131478 -0.05593861656953454; 0.0012680271171973394 0.004717724399029139 -0.015515134071368222; 0.0021816373178023653 0.007593492279513095 -0.026421310388517305; 0.0015536076061313413 0.008762024550965229 -0.0329151079462653; 0.00019823380795216982 0.000608732677529514 -0.002652765905721185; 0.00014439370710207637 0.00019353644608020352 -0.0009293191988155531; -4.2172860780226627e-5 0.0004049052325945288 -0.0003930371446397061; -0.00081429347791648 -0.0004406304966329585 -0.000731798777463704; 7.784318415325815e-5 7.609999475960264e-5 -0.0006187483698241666; 2.8389276936317007e-6 -0.00017657468018241997 0.0008307321618279445; 0.00037454471324264245 0.000699103519794459 -0.0008469646370428061; -8.061307709148017e-5 -0.0011692216226105877 0.00017006355808087278; 0.001705016032208315 0.00043165204138999466 -0.00037467510165254656] %
+
+Mass Used: 84.56578004464836 kg
+Launch C3: 97.16954697934219 km²/s²
+||V∞_in||: 4.611954797983424e-9 km/s
diff --git a/archive/ES_0.5583372292336376 b/archive/ES_0.5583372292336376
new file mode 100644
index 0000000..4c28343
--- /dev/null
+++ b/archive/ES_0.5583372292336376
@@ -0,0 +1,22 @@
+archive/ES_0.5583372292336376---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T16:30:25.189
+Launch V∞: [8.067386284170484, -5.86191177614157, 0.038538272492331514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.917368901462842e-7, -2.8527351346372525e-6, -7.283860048264765e-6] km/s
+ V∞_out: [-7.091479844799993e-6, -8.239120557503596e-7, 3.3494919181640097e-6] km/s
+ time of flight: 1.8749577785440984e8 seconds
+ arrival date: 2030-04-26T18:40:02.189
+ thrust profile: [0.16260025717068727 -0.006310006572412721 -0.06222154898775527; 0.026598270973052947 0.012135810753174813 -0.036402391718175796; 0.06030354031898022 0.04244619990684636 -0.14044209519464187; 0.02867697869108292 0.024464307388052428 -0.09853650639573203; 0.029990218246424106 0.02946831869333513 -0.1327111364794684; 0.02560303723806767 0.02866819604823052 -0.14259259032410748; 0.011954928203796518 0.013623145454530822 -0.0795948261917034; 0.002019082729859717 0.0022745858659346425 -0.015765289527332665; 0.004768615976181711 0.005607928024063496 -0.0398105037345743; 0.0004367813202359852 0.0019596015209023144 -0.0086099730251249; -0.0001110085868800018 -0.0005442642928905207 -0.004406862371962749; 0.0014283179887039487 0.0025671866976321313 -0.002571600454485083; 1.624353874184588e-5 -0.0008109900828574955 -0.002904613818522821; -0.0007996231965653325 -0.000706189335952461 0.004160044260535046; -0.0013100003303644163 -0.0005335827539905682 0.002394074675997302; -0.00012808914902749267 0.0007435936877457282 -0.002462133720468848; 0.0008714744520624937 0.002633943810089269 0.0029757838852605702; 0.0010144558864583063 -0.0003040619032006096 -4.102362305498245e-5; -0.0005068041975068897 0.0011161129692497523 -0.0015027491820419; 0.0024538969805534324 -0.005891300466172582 0.004593885075576409] %
+
+Mass Used: 71.29050552745093 kg
+Launch C3: 99.44621632773594 km²/s²
+||V∞_in||: 7.862541717175173e-6 km/s
diff --git a/archive/ES_0.5583446549832347 b/archive/ES_0.5583446549832347
new file mode 100644
index 0000000..5018cfc
--- /dev/null
+++ b/archive/ES_0.5583446549832347
@@ -0,0 +1,22 @@
+archive/ES_0.5583446549832347---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T06:59:06.786
+Launch V∞: [7.777072247454952, -5.875818629602294, 0.3650718837874344] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7490272374054835e-6, -2.6274736691133118e-6, -2.516952657970682e-7] km/s
+ V∞_out: [2.2343832969260507e-7, -1.114121217009953e-6, -2.9546441683841694e-6] km/s
+ time of flight: 1.8587103698776472e8 seconds
+ arrival date: 2030-04-04T13:49:42.786
+ thrust profile: [0.3973312066170066 0.006559617587153406 -0.10666148543174891; 0.13888713109970316 0.08643870793838439 -0.13519376230811128; 0.041454313215922495 0.04104298342973661 -0.07752651367978904; 0.04354840474920911 0.05834702142285464 -0.12019035344818342; 0.03163540731832969 0.05274010267867477 -0.11948383143664157; 0.01844005951090713 0.03656258928253009 -0.09122287213374276; 0.008022173203374571 0.018558925452895194 -0.05083236598855492; 0.008400715109672252 0.022605757179586704 -0.06454879311145659; 0.0029219452206494744 0.009376122615414326 -0.028001836648536636; 0.0011738378897027159 0.00368542549597398 -0.01189600690362233; 0.0017049797777519613 0.003009308059183291 -0.009100436571085967; 0.0006955250019423176 0.0012762756250050303 -0.003651859465784432; -0.0010355183484639261 0.0015552522539183115 -0.0004173475092677936; 0.001780934948706954 -0.002305746185051108 -0.001780040603990114; -1.4207050904109942e-5 0.000502835792046879 -0.0005668239059510053; 0.0003045377270039153 0.0017709655185806188 -0.0029756722473450897; 0.0005025565866078594 0.0013029934074547307 -0.003581345048059132; -0.0008801912962905879 0.002676540351433723 0.003337308274780764; 0.0024777095290148127 0.000277720621710499 -0.006823366374413827; 0.00017911598119318517 0.001699759099242627 -0.0018795362236955484] %
+
+Mass Used: 96.41074453616329 kg
+Launch C3: 95.14137479044751 km²/s²
+||V∞_in||: 3.166396163763259e-6 km/s
diff --git a/archive/ES_0.5583496238685898 b/archive/ES_0.5583496238685898
new file mode 100644
index 0000000..c7536d7
--- /dev/null
+++ b/archive/ES_0.5583496238685898
@@ -0,0 +1,22 @@
+archive/ES_0.5583496238685898---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T20:11:54.595
+Launch V∞: [7.920536510432081, -5.843782652734491, 0.10672349087364592] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.120125583207666e-7, -2.7417352852876316e-6, -7.953667013035247e-6] km/s
+ V∞_out: [-7.822177753402779e-6, -8.092087089037118e-7, 3.0993804321914236e-6] km/s
+ time of flight: 1.8435797524634933e8 seconds
+ arrival date: 2030-03-18T14:44:49.595
+ thrust profile: [0.3222670101335219 -0.009932286634757622 -0.1090171596859186; 0.07165976467535948 0.03634656918447145 -0.09073477774611041; 0.04320480531429997 0.03523071933128842 -0.09791902157270636; 0.027576788054537112 0.029357754297720567 -0.092541829332739; 0.028648861827854966 0.03617353605337513 -0.12794969874083667; 0.014016133564795492 0.02146150604437871 -0.08524300665118979; 0.008545134856075633 0.01886929035170494 -0.07246820602009073; 0.009467064249940102 0.01727410615282044 -0.07436383455440289; 0.0050801196340568965 0.008527654145430143 -0.04421094245598709; 0.0019288914442990473 0.004623380309387448 -0.021123079802284794; 0.001622349948798115 0.004962038850796599 -0.02408050986631226; 0.00032857812880218647 0.001247251177646695 -0.004576699958716896; 0.0019448447605699985 -0.0011373780541845363 6.577149708966463e-5; 0.00010022022563357599 0.0015744773645006592 -0.001283882652069747; -0.0015222979157312373 -0.003147641571314606 0.00025176835720870693; -0.0013034262310582007 -0.000918414828600273 0.0028371518101843723; -8.490295809813851e-5 -0.0028777077224156466 -0.0005130383607146564; -0.004231519517998452 0.00028323559138790106 -0.000561540695198319; -0.001223669246472502 -0.0008662013074830669 0.004419628604175554; 0.0002495384774130672 -0.0017343926646250722 -0.00125462426716306] %
+
+Mass Used: 86.1807366275657 kg
+Launch C3: 96.89608420899242 km²/s²
+||V∞_in||: 8.452058667786618e-6 km/s
diff --git a/archive/ES_0.558349670214241 b/archive/ES_0.558349670214241
new file mode 100644
index 0000000..89e280f
--- /dev/null
+++ b/archive/ES_0.558349670214241
@@ -0,0 +1,22 @@
+archive/ES_0.558349670214241---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T12:17:49.533
+Launch V∞: [7.789304182139822, -5.62497974549409, 0.11395283173271699] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1835193281376542e-7, 4.028629146219892e-7, 1.08453911753495e-6] km/s
+ V∞_out: [1.05460969736851e-6, 1.1703720646153782e-7, -4.792920833088723e-7] km/s
+ time of flight: 1.8749577787446716e8 seconds
+ arrival date: 2030-04-20T14:27:26.533
+ thrust profile: [0.6315487318642078 0.019091394315287977 -0.15191792938787207; 0.12759531290126114 0.08527458518023902 -0.11824991358089011; 0.04258544080312284 0.0475380573812749 -0.0750946835527686; 0.04057472358964319 0.062120945032148926 -0.10783783405299419; 0.028412133883344088 0.05599506396038193 -0.10606455205363341; 0.017271580039131224 0.04289698788549545 -0.08827016335170813; 0.019220085488717637 0.05739033158787665 -0.12310192065623947; 0.001427196861234505 0.0054423236742666475 -0.013066296193256374; 0.003693366730875926 0.01704076900071076 -0.04220509303541468; 0.00046240345965046126 0.0010998785611398792 -0.0020996135090307405; 0.00013943405690896758 0.0006964477969570724 -0.002731971363676855; 7.104306483986396e-5 0.0004025100971548209 -0.001068187281352109; -0.0009573806048255771 0.0006716939895708722 -0.0009669809323701993; 0.00012342140390882248 -0.0008621477666922786 -6.608445591162432e-5; 6.13882392103758e-5 0.0026938549125629994 -0.0018704134117857965; -0.0012328066879649597 -7.788391872767472e-5 0.000669394517444317; 0.00030620466259662153 0.0010663469230851388 -0.0018474471928533525; -4.491750248359106e-5 0.00028853064285195115 0.0007717276053649929; 0.000213605931134076 -9.155462647364595e-6 0.0011644661273887095; -0.0003902954720638609 1.5004105248547393e-5 0.0006024160727911232] %
+
+Mass Used: 112.83587009256689 kg
+Launch C3: 92.32664202697958 km²/s²
+||V∞_in||: 1.1629835791798467e-6 km/s
diff --git a/archive/ES_0.5583573524463167 b/archive/ES_0.5583573524463167
new file mode 100644
index 0000000..0f84a36
--- /dev/null
+++ b/archive/ES_0.5583573524463167
@@ -0,0 +1,22 @@
+archive/ES_0.5583573524463167---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:05:23.771
+Launch V∞: [7.678296909003271, -6.03133167954783, -0.03707805966013568] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.575410150897075e-6, -1.1545917512275578e-5, -1.0479965602105796e-6] km/s
+ V∞_out: [7.549050715716607e-7, -2.441202772800864e-6, -1.3578846840186245e-5] km/s
+ time of flight: 1.789897255602018e8 seconds
+ arrival date: 2030-01-13T06:27:28.771
+ thrust profile: [0.3664659339156494 -0.02021259252215966 -0.11091071098514235; 0.14181763002888606 0.07316104436630207 -0.15281779300479267; 0.07132320748155518 0.060258397514410464 -0.13749790168307513; 0.040894864309061904 0.04634993919664539 -0.11874402066645409; 0.02439902505384007 0.03338089430973161 -0.0948325111160422; 0.016755036875686146 0.02740469828756039 -0.08493484079070214; 0.013953894063536594 0.025002931913502748 -0.08334646546423782; 0.012183301902034118 0.02543303227217325 -0.08737049246882522; 0.0032527052296695766 0.006346288312375568 -0.02411105851280944; 0.0005150160703906071 0.0014064299488158823 -0.005497889523348607; 0.0021349372090094104 0.004209996371285855 -0.018224868423245243; 2.671260006801734e-5 5.436866946468508e-5 -0.0005837769850528939; 0.00018081537206860896 0.0003366123392727808 -0.0013083720552665662; 9.831358182643343e-6 0.00012576538803064073 -0.0009999843355364695; 0.0001321934060034737 0.00013967764610203195 -4.0547372450073105e-5; -2.735093097355366e-6 0.00017680413899432736 -0.00020296217089674348; -0.00014962821411355107 0.0001916332586275188 -0.00010658101688122836; 0.00018319978485348862 0.00043350454228380025 -0.001356902897238236; 0.00025133672136876237 -0.0004092735242436931 0.0008532630730024686; 0.00026183137163667924 0.001524171029240341 -0.0022192272788708386] %
+
+Mass Used: 95.29852765550095 kg
+Launch C3: 95.3345800340346 km²/s²
+||V∞_in||: 1.3848947503142594e-5 km/s
diff --git a/archive/ES_0.5583733044005168 b/archive/ES_0.5583733044005168
new file mode 100644
index 0000000..94db09f
--- /dev/null
+++ b/archive/ES_0.5583733044005168
@@ -0,0 +1,22 @@
+archive/ES_0.5583733044005168---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T02:16:40.047
+Launch V∞: [7.771803836232901, -5.808398621177326, 0.16676358019806176] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8322094465487835e-6, -2.657354210551862e-6, -2.698901062121693e-7] km/s
+ V∞_out: [2.2546342562921768e-7, -1.4109510911252e-6, -2.905877118504942e-6] km/s
+ time of flight: 1.8598996990010983e8 seconds
+ arrival date: 2030-04-04T18:09:29.047
+ thrust profile: [0.45012130585034954 0.011191574408593313 -0.12475949531197743; 0.10868209402070785 0.06673826433371806 -0.10514916983001375; 0.09089768133769749 0.09377379680184408 -0.15850580693136138; 0.06448277278881742 0.08940119419490848 -0.16840196585829792; 0.023383366848116847 0.039411985436779526 -0.08582111305037132; 0.00996792796401864 0.01982690618303741 -0.04852926814609158; 0.014330535236841198 0.03646196997631215 -0.09286048008451969; 0.0023687674271433124 0.009544118744367542 -0.016764628033755124; 0.0019628534034418017 0.007874035152104431 -0.013503504255014748; 0.0005089074566432057 0.0011102495914266427 -0.006157509654260793; -0.0003328794329819345 0.002153488527735413 -0.0030889505878883413; 0.0010507993434414082 0.0003098309194858953 -0.008856027872468248; 0.00011403994441474596 -0.002545103421709733 -0.005289259789416698; -0.0017360209511894586 0.0022952880075669726 -0.0002458075856807771; -0.0015949400537379078 0.0003574248943732294 -0.005015657396378476; -0.0019049188754693947 -0.004789752964714127 0.0017963244979131497; 0.0024695354102592148 0.0013789623489580073 0.003993693605729142; 0.00026495402426832907 0.0003942390612091055 0.00038968470185640064; 0.00020379132111383457 0.0007537053584921315 -0.0012632376574972966; 0.0025374755713396943 0.00713898073944951 -0.0018364108142718445] %
+
+Mass Used: 102.1324580327555 kg
+Launch C3: 94.16623950305957 km²/s²
+||V∞_in||: 3.2390374381583684e-6 km/s
diff --git a/archive/ES_0.5583748449285668 b/archive/ES_0.5583748449285668
new file mode 100644
index 0000000..cd9c738
--- /dev/null
+++ b/archive/ES_0.5583748449285668
@@ -0,0 +1,22 @@
+archive/ES_0.5583748449285668---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:51:28.429
+Launch V∞: [7.864041495616679, -5.770925120707919, 0.13973882855616399] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0050203112470923e-9, 1.217965655138053e-9, -9.435461969635331e-9] km/s
+ V∞_out: [-2.9591801184906347e-9, 9.636858696799663e-9, -1.6284585711217148e-9] km/s
+ time of flight: 1.821360226987273e8 seconds
+ arrival date: 2030-02-17T08:11:50.429
+ thrust profile: [0.42278489772606365 -0.006699502718325753 -0.11732586461549037; 0.054808553075474484 0.03236583128345804 -0.0585207868617062; 0.09483831603045559 0.09157468289909303 -0.16586609677466752; 0.035124067186293996 0.0468951284498437 -0.10140312822920684; 0.04271079536122595 0.06938688279902472 -0.15498171280981038; 0.014918635001350232 0.029438961677048802 -0.07529541295021128; 0.011751187110214906 0.027415222025362285 -0.07426149185104829; 0.0040591890538080695 0.010850655740922092 -0.03201539779894836; 0.006202613788026079 0.019239656541560696 -0.057880102751649926; 0.0022155173861518325 0.007163092810162333 -0.02353806800843141; 0.000308996844782593 0.0008222416428152469 -0.0032812312600664266; 0.00015975528011821492 -0.00013891068683704488 -0.00045647340454701263; -0.000489789817159601 0.00022672120959889769 0.0004436325474814834; -0.0011274848163994391 0.00014285881435916346 0.00021940631073567255; 0.0008983497340185754 0.00030818987079980694 6.780839573073023e-5; -8.67781135419293e-6 0.0005839265905572369 -0.0002541066775045809; 0.00030031362034786094 0.0003781218308518482 0.0012962058103892916; 0.0015348630862557673 0.001019552568777767 0.0013939598292532105; 0.00279404636692348 0.0018996213464593345 -0.001670212506888807; 0.0008729120379647383 0.0009557104792393691 0.0004301927927046738] %
+
+Mass Used: 96.30084713613223 kg
+Launch C3: 95.16625233380498 km²/s²
+||V∞_in||: 9.722730550932896e-9 km/s
diff --git a/archive/ES_0.5583916528159185 b/archive/ES_0.5583916528159185
new file mode 100644
index 0000000..d16da95
--- /dev/null
+++ b/archive/ES_0.5583916528159185
@@ -0,0 +1,22 @@
+archive/ES_0.5583916528159185---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T12:23:46.743
+Launch V∞: [7.945630047560866, -5.6293974980000305, 0.13933171732698368] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006019814716449832, 0.00047873985563018514, 0.0004061513993455518] km/s
+ V∞_out: [8.108302463413017e-5, -0.0005065990330310839, 0.0007009087270008562] km/s
+ time of flight: 1.8563869028042823e8 seconds
+ arrival date: 2030-03-31T02:41:56.743
+ thrust profile: [0.4890515229657015 -0.005517908028392911 -0.14327029156309992; 0.07632430011183222 0.04421940984382264 -0.08712891598929765; 0.030553653889541146 0.0288034820912114 -0.06484382099802127; 0.026860670133981326 0.033941270820984845 -0.08377487291626345; 0.0379248373995589 0.05820501038850643 -0.15589869492566544; 0.018333332054888383 0.033210444148622946 -0.09952081417919101; 0.007962348212572292 0.015718431169782193 -0.05160992341313609; 0.005898023091046022 0.013410550711487902 -0.047923750686404004; 0.006008069818229144 0.01750384408830084 -0.06243980921084163; 0.003089444192214579 0.007927358901780687 -0.038513709836987035; 0.002104601921153604 0.0029939502950871717 -0.003249216208923442; -0.0002739911674053194 -0.0001920403079988366 -0.0028094005760004757; 0.00035496129751365053 0.000907135982557377 -0.0037958956279327775; 8.084289850224718e-5 0.0002373432773993646 0.00024534491781431304; 0.0024466218892142903 0.0018325284536706032 3.261953696575355e-5; 0.0042176219582493735 -0.0013774924321474022 0.0002936351079835019; 7.435744353241695e-5 0.00039794043132111766 -0.0018822391090977614; -0.0020167558871574966 0.0056520575431706615 0.0007478682544617417; -0.006471595875565209 0.0023511873287781087 -0.0008456673142825761; -0.0004896374301251874 0.0013186791727118293 -0.0022053242959994648] %
+
+Mass Used: 98.20862445647936 kg
+Launch C3: 94.84256637064439 km²/s²
+||V∞_in||: 0.0008697887678988618 km/s
diff --git a/archive/ES_0.558398106278312 b/archive/ES_0.558398106278312
new file mode 100644
index 0000000..e067169
--- /dev/null
+++ b/archive/ES_0.558398106278312
@@ -0,0 +1,22 @@
+archive/ES_0.558398106278312---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T22:45:21.819
+Launch V∞: [7.867832291702536, -5.739414201899007, 0.13520973971981531] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.0672083738371463e-9, -1.8316427153635474e-9, -1.5482070407054929e-9] km/s
+ V∞_out: [-2.4283958175570325e-9, 2.1336000469205015e-9, -8.169795450342905e-10] km/s
+ time of flight: 1.874957778749036e8 seconds
+ arrival date: 2030-04-23T00:54:58.819
+ thrust profile: [0.4352658678251918 0.0112313340893274 -0.12206796156116129; 0.08583850127592281 0.05225207543019397 -0.09106958992409701; 0.06402661643906116 0.06369934542555034 -0.12292986465633844; 0.04637692823707356 0.06137872094784565 -0.1319076688422628; 0.031286547958356045 0.0504714129804852 -0.11952338277410338; 0.021753631162464766 0.042579994078801774 -0.11042847778107548; 0.010184997171635062 0.022029334020572635 -0.06307988439935017; 0.0019423120573132456 0.0055844291880086765 -0.016854940119934072; 0.0011583733697207784 0.001950139741510681 -0.008468484755711965; 0.0009000466556027515 0.0012492449698955077 -0.008945752725466442; -2.816277437581261e-5 0.002165548597659135 -0.0015694224601179587; -0.0006171971212129031 0.0008994525504890049 -0.006935888645926031; -0.0012200133495617101 0.0019251562836826348 -0.004908622191076477; -0.002504597203815908 0.009822834300464541 -0.0036768204609137385; 0.00014504041042958296 0.0016807287540962575 -0.00600610929257033; -0.00027427860342540316 -3.9457730327996984e-5 -0.001963838875564928; 0.0007847257468077826 -0.0004821972128173738 -0.0009897361097001975; 0.012477888693083514 0.014152308138101248 0.012192373514371298; -6.817924588977883e-5 7.573025963202853e-5 -0.00010580854240357018; -0.004464838030546048 0.0010058396574011402 0.003544779809220409] %
+
+Mass Used: 98.10312884534233 kg
+Launch C3: 94.86194202503229 km²/s²
+||V∞_in||: 3.893536603933642e-9 km/s
diff --git a/archive/ES_0.5584021604655229 b/archive/ES_0.5584021604655229
new file mode 100644
index 0000000..0b02303
--- /dev/null
+++ b/archive/ES_0.5584021604655229
@@ -0,0 +1,22 @@
+archive/ES_0.5584021604655229---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T22:51:53.883
+Launch V∞: [8.00997132120609, -5.61617629354202, 0.1860667223538797] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01503630790313779, 0.09102366882284046, 0.11166288470357535] km/s
+ V∞_out: [-0.03966145764781131, 0.06130070332868921, -0.12500019389505732] km/s
+ time of flight: 1.8537930003667226e8 seconds
+ arrival date: 2030-03-27T13:06:53.883
+ thrust profile: [0.3797299352110363 -0.0013463211308080455 -0.10915407559320674; 0.10491084482230209 0.062313971495832274 -0.1122326332976141; 0.059408944305415594 0.0575721173592641 -0.11744600254623935; 0.025580286485652387 0.03226761910044954 -0.07528424174411256; 0.027497314342759725 0.04405167932528669 -0.11149871140226564; 0.020826030645655746 0.03969370977915639 -0.10722085560638049; 0.011248392276736578 0.024282828963883493 -0.072314936283303; 0.006749089147939516 0.016963209632823526 -0.053063490593576415; 0.004396267434731551 0.012710163290088037 -0.041128895830490564; 0.001804987229445652 0.004820587388045733 -0.015082746823034832; 0.00043542788417945844 0.00120013972067643 -0.004630180496876724; -0.0019979326866607504 0.0008623842297554637 -0.003793343908038647; 7.141831515137349e-5 0.001606249056984054 -0.0053889375346403545; 0.00014996807099472952 0.000374608367513016 -0.0024982744587338985; 0.0002970904929165359 6.519934890406568e-5 0.0009216791841590544; 0.0007761350157718182 -0.001276099752883703 -0.002575596373528881; -0.001879943241257467 0.001026780176022459 -0.003136833172994441; 0.0002588238029432523 -0.005277060386749126 -0.003937555386883404; 0.0018626706868919655 -0.0021025599220504715 -0.0036624525765946766; -0.0006020967455784763 0.0006421188745032375 -0.0015032096255138002] %
+
+Mass Used: 93.01095149062303 kg
+Launch C3: 95.73569755185493 km²/s²
+||V∞_in||: 0.1448447398480596 km/s
diff --git a/archive/ES_0.5584072778234828 b/archive/ES_0.5584072778234828
new file mode 100644
index 0000000..a4e07c3
--- /dev/null
+++ b/archive/ES_0.5584072778234828
@@ -0,0 +1,22 @@
+archive/ES_0.5584072778234828---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T04:20:55.445
+Launch V∞: [8.089215775688869, -5.634845007166464, 0.14996553482798738] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00203537994289273, 0.001303617183288147, 8.820168465147944e-5] km/s
+ V∞_out: [-0.0017743059349150595, -0.0008046226121725889, 0.0014577282607330113] km/s
+ time of flight: 1.8749577787478366e8 seconds
+ arrival date: 2030-04-23T06:30:32.445
+ thrust profile: [0.2730087221065171 -0.00034027296224382723 -0.08924477678658817; 0.07442551670156886 0.042070486756309665 -0.08467298548396036; 0.05064014345204702 0.04587676932904794 -0.1029270650477812; 0.03583721720016671 0.041487872327085965 -0.1103018952201258; 0.028574126501608853 0.041452791554393006 -0.12130118338702081; 0.018643191018775034 0.02938681168509092 -0.09533712833018759; 0.015530800982869415 0.02848155056369794 -0.09636668359360537; 0.00424554230477929 0.009431768880712626 -0.03547286612049364; 0.0006728506792719225 0.0025409204606803622 -0.014829069658383874; 0.0019707848663760713 0.0025776818444121167 -0.01407548869314083; 0.002226218299227297 0.0026071629953406013 -0.008222649575123598; 0.002448187362340949 -0.0003433192942656478 -0.008024561811111245; -0.00013363432655545877 0.0035498673716862226 -0.0005557785561134659; 0.002093813501192796 0.004599663371419815 -0.0017335095346105408; -0.00443631448653857 0.006750556217927216 -0.005293854982843309; -0.00022545798018459157 -0.00024304737229406779 -0.006949008370760963; -0.00041468441138296975 -0.011426781380108681 0.0009973162477645266; 0.0028538712350747427 0.0022883978768627427 -0.010394010815438188; 0.004073785066927421 0.003976110737552098 0.0007020269312485205; 0.003937792982439478 0.0016924498479485293 0.0010920470853770649] %
+
+Mass Used: 84.42044206527044 kg
+Launch C3: 97.20937978207876 km²/s²
+||V∞_in||: 0.0024186708766736936 km/s
diff --git a/archive/ES_0.5584252287781932 b/archive/ES_0.5584252287781932
new file mode 100644
index 0000000..4727292
--- /dev/null
+++ b/archive/ES_0.5584252287781932
@@ -0,0 +1,22 @@
+archive/ES_0.5584252287781932---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:13:57.482
+Launch V∞: [8.006921244855537, -5.546909512389449, 0.28362773001216285] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.237254896324794e-6, -5.15434416850075e-6, -1.2252456353209537e-5] km/s
+ V∞_out: [-1.1958088931468583e-5, -1.3330538121731043e-6, 5.773809412573069e-6] km/s
+ time of flight: 1.8749577787379524e8 seconds
+ arrival date: 2030-04-21T11:23:34.482
+ thrust profile: [0.4691890935656721 0.005107083210557144 -0.1358611561266319; 0.0787514221154058 0.04745191740772306 -0.08266207199237954; 0.048103739273308195 0.047304180462252925 -0.0925872154357622; 0.04416880005713875 0.05771521880717995 -0.12565321104259836; 0.024186885963183795 0.03941999902305895 -0.096104355070561; 0.016568577203300097 0.03245658159793145 -0.0862644594382417; 0.007718667703221941 0.018147218131151076 -0.052934054036788705; 0.012405143863473599 0.027907562921237753 -0.08612499706414709; 0.0017433654332755697 0.005847711874577853 -0.021065322648269835; 0.0011294784528886076 0.0032029108435463276 -0.010248713660033331; 0.00027868431349484756 0.0020662847167641227 -0.010291571596019974; -0.0013385523529144342 0.0013522843522333458 -0.003143032029754649; 0.0003608177980012457 -0.0010303394431566198 -0.009155101162639952; -0.0022286600253804806 -0.0021608791691571363 -0.0030972289622118163; -0.0003298289660157352 0.0012977380262817887 0.0017384088988176005; -0.0004031043139709383 0.0007422357452650514 -0.004960428406815989; -0.0010125893143131037 0.000521910926860348 0.0028021093111659937; -0.0002919237918495982 0.001081831958270117 -0.001378225225596462; 0.00794983782537097 -0.0012158570832995225 -0.0036866606990583377; -0.003097905193598022 -0.00029684617847606696 -0.004444435737225035] %
+
+Mass Used: 97.5660472876325 kg
+Launch C3: 94.95943764918735 km²/s²
+||V∞_in||: 1.3349934463252697e-5 km/s
diff --git a/archive/ES_0.5584286952887537 b/archive/ES_0.5584286952887537
new file mode 100644
index 0000000..44accf9
--- /dev/null
+++ b/archive/ES_0.5584286952887537
@@ -0,0 +1,22 @@
+archive/ES_0.5584286952887537---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:50:10.186
+Launch V∞: [7.978107658359546, -5.801558728525525, 0.1500816275842713] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.041807006730396e-5, 5.101311491129701e-5, 0.003524997180600147] km/s
+ V∞_out: [-0.0031660637244629005, -0.0009694287006692223, 0.0012112268765519755] km/s
+ time of flight: 1.8749577787493736e8 seconds
+ arrival date: 2030-04-23T20:59:47.186
+ thrust profile: [0.22822474140730004 0.009121338599636007 -0.06595820526891345; 0.0375245571042352 0.02490528199168406 -0.04009931329657503; 0.12488839621123764 0.1272804133058793 -0.2052125603964398; 0.036379146141416144 0.0539353945615535 -0.10163190097186994; 0.01937123552730271 0.03900058512032008 -0.07965657723779872; 0.009160469908556667 0.023663662500648983 -0.05323607146555729; 0.011885799456597897 0.02830742911036361 -0.07112852997669411; 0.0044026691163229536 0.016934746974118974 -0.04276500584359163; 0.0037404109011064347 0.014789272599143798 -0.040647008299663945; 0.00048238203219164307 0.0031228288507349064 -0.008689867125647933; 0.0048882328881185095 0.028441687430068002 -0.07549851672317877; -0.0005372009946899604 0.00035315134184415363 -0.0011469974884674946; 0.0012810338536667595 -0.0009114825703479758 -0.00181503660961385; -0.000724444570719305 -0.0004248819969232308 -0.0020836300787808125; -0.0012721373292769382 0.0002103983789955135 -0.00237755458345542; -0.0005512014738714042 -0.0007652226238854398 0.00025157411164634133; 0.00034368765876807077 -0.0010097758340148113 0.0016130077150781062; 0.0009022492291245372 0.0022578751351163178 0.000647607176080027; 0.0007127765194765318 -0.003554528081519463 4.53588128590662e-6; -0.0028129450721368905 0.005377251960627165 0.001955274265169827] %
+
+Mass Used: 83.73708626445432 kg
+Launch C3: 97.33080998384428 km²/s²
+||V∞_in||: 0.003525726796409678 km/s
diff --git a/archive/ES_0.5584350267496745 b/archive/ES_0.5584350267496745
new file mode 100644
index 0000000..ec96617
--- /dev/null
+++ b/archive/ES_0.5584350267496745
@@ -0,0 +1,22 @@
+archive/ES_0.5584350267496745---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:47:13.973
+Launch V∞: [7.754474243739079, -5.767230941005468, 0.17597857659134664] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.972748184139512e-8, 4.486664416927092e-7, -8.593956206643307e-6] km/s
+ V∞_out: [-3.102210967700891e-7, 8.554601094856166e-6, -8.19091481611116e-8] km/s
+ time of flight: 1.8749577787421718e8 seconds
+ arrival date: 2030-04-21T16:56:50.973
+ thrust profile: [0.48164665405497287 0.012322311476357362 -0.10820214722038943; 0.12256706111059508 0.08452733128095921 -0.10735586384093991; 0.09979000134661371 0.11882329393870346 -0.15670685697929632; 0.046612573907287846 0.073787574371364 -0.11689208480892903; 0.034532701309462094 0.07055469201862781 -0.1216323609910464; 0.011426399055960653 0.030580592274092832 -0.05878323437694547; 0.011079258221064588 0.03454566425547602 -0.0700126476805703; 0.003481600789975678 0.014048772598806323 -0.030830049592881745; 0.0008580229099888002 0.004127107912993753 -0.00943251158995887; 0.001375704173369039 0.007475431850164601 -0.017888949211800835; 7.60722878215294e-5 0.0005447336364188273 -0.001281110886684619; -0.0003907354928379057 0.000987233793793091 -0.00554046176798445; -0.0001658026578145306 0.0008638151236237972 8.844883357762064e-5; 0.000111097637625384 -0.0019873311562879966 -0.000895513043527345; 0.0021159566662265266 0.0006428007108711917 -0.002074550988270075; 0.0007742663817316406 0.0004728539392912558 -0.005437786902038304; -0.00032046568573198576 -0.00024033995297673832 -0.000979431708754851; 0.00012865846240800254 0.0007273017219003291 -0.000592865866080157; 0.0027118578866213872 -0.0034368798743386482 -0.001468553279334167; 0.002936988879659811 -0.00012468626814492856 -0.0012719431493936604] %
+
+Mass Used: 106.53541130640451 kg
+Launch C3: 93.42379198312268 km²/s²
+||V∞_in||: 8.605867314204381e-6 km/s
diff --git a/archive/ES_0.5584429447437844 b/archive/ES_0.5584429447437844
new file mode 100644
index 0000000..0acddd3
--- /dev/null
+++ b/archive/ES_0.5584429447437844
@@ -0,0 +1,22 @@
+archive/ES_0.5584429447437844---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T02:17:52.324
+Launch V∞: [8.09760431841875, -5.577596394711461, 0.19504763274697234] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.718874063181292e-7, 2.8808312984067874e-6, -7.217577432141387e-5] km/s
+ V∞_out: [-2.352127599197437e-6, 7.219283104182641e-5, -4.1795826454178993e-7] km/s
+ time of flight: 1.874957778749395e8 seconds
+ arrival date: 2030-04-23T04:27:29.324
+ thrust profile: [0.3867438194164464 -0.001476876664611271 -0.12210135984891601; 0.02941897801312988 0.017116098570348952 -0.03821840830910572; 0.019761558851728644 0.016940042009378754 -0.04495942017439206; 0.01418823161351085 0.017821108443595125 -0.049227360294415226; 0.0250494322568418 0.037007313913291005 -0.11209629443500395; 0.017483548598798734 0.030597249208876996 -0.10393325427962968; 0.011805529132073155 0.024787959669289934 -0.08529524721059284; 0.009988884493248988 0.022886854892675595 -0.08772910846022519; 0.005674618346712551 0.01686249304930908 -0.06363435826080682; 0.006158874933405746 0.018182954589950076 -0.07942396286828408; 0.0011273057701149923 0.0036733687037338535 -0.016157160819610487; 0.0002576896195340551 0.001332586963521111 -0.008501319998867577; 0.00030439723175138667 -0.0020220551430987096 0.00048043194225113966; 0.0006063291610861019 -0.00046845612613901467 0.001606007457374475; -0.0009163055798300767 -0.0017464196873902575 0.0015383201597551706; -0.0009329088733031975 -0.0015967948738649976 0.002704466931513382; -0.0010875522684424693 0.0004949211046158193 0.0037308447635007753; 0.0006065214665526556 -3.402361074853876e-5 0.001841810240900569; -0.00018870917482093435 0.0019990674492034594 -0.0008023015091297071; -0.0014233976458744753 -0.004111158921140829 -0.001980063088964559] %
+
+Mass Used: 87.3236474235091 kg
+Launch C3: 96.71882081901246 km²/s²
+||V∞_in||: 7.223478570321771e-5 km/s
diff --git a/archive/ES_0.5584545064603089 b/archive/ES_0.5584545064603089
new file mode 100644
index 0000000..8186081
--- /dev/null
+++ b/archive/ES_0.5584545064603089
@@ -0,0 +1,22 @@
+archive/ES_0.5584545064603089---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T19:25:15.707
+Launch V∞: [7.952580717802071, -5.569033886875723, 0.40738539603143387] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.477361872616778e-5, -0.00018362048120575589, 0.0036633806371636915] km/s
+ V∞_out: [0.00015440699685011601, -0.003785111559870747, 4.8375832709257807e-5] km/s
+ time of flight: 1.8607515542048427e8 seconds
+ arrival date: 2030-04-03T10:57:50.707
+ thrust profile: [0.4454658230972617 0.0050830570392305895 -0.12103115615158908; 0.1708675417972246 0.10566375651357973 -0.16538743111372467; 0.08101044557514815 0.08081822465293254 -0.14839106204053368; 0.03718495151878612 0.04984152409539852 -0.10358402118287627; 0.021850992651583318 0.036691262131606554 -0.084343675965843; 0.01581499034680424 0.03194976168690746 -0.08011532281250225; 0.00710512745762213 0.018489987771909563 -0.04894946178808192; 0.005594213257641363 0.015061407591417829 -0.044526199222177563; 0.0016326631280351705 0.005536203676697457 -0.016303159684928185; 0.0010260471103630837 0.003805240536911574 -0.012300142239488119; -4.8883329482639955e-6 0.00014191994665752825 -0.0003571859475706129; -0.00018249007775540075 0.0021245455194595798 -0.008904131368924404; -0.0002012911869394499 9.275617327094782e-5 -0.0008106366693252129; -0.0004809428080788795 0.0006098310839944965 -0.0006642899096192039; -0.00031329377647931907 0.0006510707133649297 0.0002527049460610165; -2.8114032560030744e-5 -0.00012473605084277608 0.0003433249146360774; 8.06379356126148e-5 0.00018083783995106691 0.0005775210158191788; 0.0008046960906766635 0.00045417270927295035 -7.303267982434276e-5; 3.4821359682178834e-5 -0.0008760086444090794 0.0012848997621455495; 0.0004694228566971653 -0.00046468127044786115 0.0009651296730446655] %
+
+Mass Used: 100.7256828948689 kg
+Launch C3: 94.42364136722712 km²/s²
+||V∞_in||: 0.003668063236375414 km/s
diff --git a/archive/ES_0.5584670032481018 b/archive/ES_0.5584670032481018
new file mode 100644
index 0000000..b119bd1
--- /dev/null
+++ b/archive/ES_0.5584670032481018
@@ -0,0 +1,22 @@
+archive/ES_0.5584670032481018---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T08:38:19.400
+Launch V∞: [7.8494786720522445, -5.8908063752311675, 0.1414490293217759] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.117707778985481e-7, -2.6113237547826558e-6, -7.721777413809493e-6] km/s
+ V∞_out: [-7.425761956788122e-6, -9.100965068768101e-7, 3.3339632767272806e-6] km/s
+ time of flight: 1.8749577787459594e8 seconds
+ arrival date: 2030-04-25T10:47:56.400
+ thrust profile: [0.3640984081177009 0.004479275667173025 -0.11361910286703618; 0.08257316019512846 0.04840120834859516 -0.09784586382334717; 0.05771464885718069 0.05427009429918516 -0.12418517085002921; 0.03503777522570633 0.04392202586660225 -0.11387121530195035; 0.02119844710502112 0.02866660792527748 -0.08804126492808036; 0.0139494756433149 0.02353880218192205 -0.07833295543725675; 0.009852589741396077 0.02103162628434058 -0.07730228606230123; 0.004111300524147762 0.016662782125801925 -0.057565493293324284; 0.002792193342246622 0.005163649786972679 -0.024037165190456348; 0.0012459437758116504 0.003522372585256266 -0.017273706386276073; 0.0003196120154166294 0.0006915238720586956 -0.00418788113694743; 0.001662999990979277 0.0027571083028830714 -0.015082793885178374; -0.0011456100432131555 0.00118087537995764 -0.0005367570665725204; 0.0014476489016596254 0.0011061781182226452 -0.001436410186307531; 0.0005706596295917183 -0.000631312201994996 -0.0029649885463779646; -0.0006294162623324104 -0.0010210348077511818 0.002651316505858984; 0.0011439444620700103 0.003351757899453136 -0.004044871936692712; 0.0017432109643702315 0.0015655213384353401 -0.0010707497725521607; -0.0006368054580436894 0.0009032423165855315 0.003716743976971137; 0.00017122487172190054 0.0025299050731177526 -0.003851273189762241] %
+
+Mass Used: 89.58528628149952 kg
+Launch C3: 96.3359230013633 km²/s²
+||V∞_in||: 8.19169274183063e-6 km/s
diff --git a/archive/ES_0.5584723163603018 b/archive/ES_0.5584723163603018
new file mode 100644
index 0000000..5b27ebf
--- /dev/null
+++ b/archive/ES_0.5584723163603018
@@ -0,0 +1,22 @@
+archive/ES_0.5584723163603018---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T14:27:30.959
+Launch V∞: [7.975294957304531, -5.723030379235525, 0.1596836411822196] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009034531468057814, -0.0005988980923820698, -0.038067557716371395] km/s
+ V∞_out: [0.03578895437349725, 0.011226414956195233, -0.005185145828370377] km/s
+ time of flight: 1.84527614029034e8 seconds
+ arrival date: 2030-03-19T08:07:44.959
+ thrust profile: [0.3665687931371142 -0.013423009314192925 -0.12441529211451485; 0.06076331220899952 0.030898020960612733 -0.07308367710910768; 0.04050534355429195 0.032965082367616035 -0.08747154249036351; 0.03301398967149709 0.03463847060474105 -0.1034544568971146; 0.022097779179364126 0.027756850246487164 -0.09278328537428737; 0.02241031914235077 0.03192368551668352 -0.1166980532832783; 0.025640462643393504 0.04286296843115048 -0.16424329686196887; 0.004160694514463968 0.007189657970275401 -0.03181248479281639; 0.002001751164099895 0.0029915576986296304 -0.01481653421873629; 0.0022480767005768603 0.00495411578917974 -0.024475623906750878; -0.0011328609253549522 -0.00011055914772754535 -0.0038454923843812593; 0.0005241262738305559 -4.4458635643131053e-5 -0.0008186951507326071; -0.0001233864255632163 -0.00019956602736172815 0.0010848917810418804; -0.00264510512456622 -0.0003795166245343554 -0.002453635964454301; -0.0035495283396079318 -0.0019836254731065385 0.0017776593038726948; 0.00033036322826665473 -0.0001703148282584396 -0.0023282101704528756; -0.0003635835403547275 0.0031502570426792504 0.005697097047025522; -0.00850062056544627 0.006243279781498173 0.0017932146600886031; 0.001891371038814093 -0.0007826875063199528 0.0005705424976391843; -0.0014368738062848236 0.006281238599356939 0.006639038311108722] %
+
+Mass Used: 89.31158850331303 kg
+Launch C3: 96.383905242921 km²/s²
+||V∞_in||: 0.038082986450681616 km/s
diff --git a/archive/ES_0.5584775815292277 b/archive/ES_0.5584775815292277
new file mode 100644
index 0000000..33286fe
--- /dev/null
+++ b/archive/ES_0.5584775815292277
@@ -0,0 +1,22 @@
+archive/ES_0.5584775815292277---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:36:44.967
+Launch V∞: [7.949953170336334, -5.737329743337831, 0.02332066146968947] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.166242832824342e-6, 3.7435267594340917e-6, -5.358443974975404e-6] km/s
+ V∞_out: [1.1485663068488632e-6, 7.643820626263731e-6, -5.221967384190088e-7] km/s
+ time of flight: 1.8749577788019592e8 seconds
+ arrival date: 2030-04-23T10:46:21.967
+ thrust profile: [0.34902636492256395 0.010315296679549741 -0.10206913724538103; 0.04559279713967394 0.02821071179605104 -0.05131768905029536; 0.10101050954556759 0.10317592842011347 -0.19170201802491027; 0.02782724984255418 0.037845928617705554 -0.08459741923701468; 0.022650878924764067 0.036190170175078924 -0.08983449022166683; 0.015223878014111576 0.03368189941078706 -0.08673998634868016; 0.005861225105041513 0.01430497985150676 -0.04166591300256554; 0.013211315408924439 0.03764681519968256 -0.1113057657107765; 0.0017002191768959497 0.005350814919074742 -0.01778874365112908; 0.0018315476228195331 0.007545358445863818 -0.025148404193855223; -0.00015283572839826204 -0.0007125349592770049 -0.0008893787626763315; -0.000110106747422758 0.0003938160074581289 -0.001359989897919449; 0.00027692079819545347 -0.0002446717965838756 0.0016299641840787414; -0.0003890406759990478 0.001424896079171468 0.0017658652377512648; -0.0024733445893925184 0.000988063369664866 -0.0005310155024941857; 0.00016077555384225905 -0.0015703500025516877 0.003903813135681139; -0.0035593587330982985 -0.006365212336530609 0.0005224827745472468; -0.00766726346540352 0.002936858904151885 -0.0060139569024902405; -0.0019160635666581295 0.0015063812124338103 -0.0011512277839405452; 0.005308498480507606 -0.003217432840280798 -0.003630457968304138] %
+
+Mass Used: 90.86154267320944 kg
+Launch C3: 96.11925184758105 km²/s²
+||V∞_in||: 7.751418823261295e-6 km/s
diff --git a/archive/ES_0.5584989813598826 b/archive/ES_0.5584989813598826
new file mode 100644
index 0000000..dacb01c
--- /dev/null
+++ b/archive/ES_0.5584989813598826
@@ -0,0 +1,22 @@
+archive/ES_0.5584989813598826---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T22:18:39.286
+Launch V∞: [7.882765416310865, -5.665026300168285, 0.17050617981060798] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.743353037855724e-7, -6.25045958162688e-6, 1.0315899419957184e-6] km/s
+ V∞_out: [-9.412006635140085e-7, 3.671677503815684e-6, 5.109515918966106e-6] km/s
+ time of flight: 1.874957778749175e8 seconds
+ arrival date: 2030-04-23T00:28:16.286
+ thrust profile: [0.5532165609627178 -0.003863444128651798 -0.15696464811169497; 0.03888055258597301 0.022600475200197836 -0.04383465067799713; 0.04727642682568289 0.044445751691845586 -0.09575838369226386; 0.0308565143235048 0.039152094206590604 -0.09094123136203522; 0.027351383339717622 0.036524031519067364 -0.10325519110969318; 0.018996225861995612 0.03685734083318248 -0.09919888211273871; 0.015497713710159594 0.033729201161076985 -0.10551745408835363; 0.006134446757448755 0.01404626409099899 -0.045971961296458995; 0.0021428734722332456 0.008908908446582202 -0.03218863638647238; 0.004243825967647906 0.0031682700138623973 -0.013251230437302877; -0.00024544280355831777 -0.0007325807574486509 -0.001781509881514094; 1.947709506036506e-5 0.0033227101877746773 -0.017547494065825096; 0.005736419052252285 0.00020089592625702863 -0.004205102361615349; 8.317251029210997e-6 -0.0013960104451660946 -0.0015091109175250999; -0.005152532664843248 0.007965594723834894 -0.010554508101647627; -0.0012078724861971052 -0.0008024114857853611 -0.004781946806736285; -0.0023710147756227924 0.0019753116534544208 -0.007958833975372543; -0.002768860621910842 -0.0013066732249405223 -0.0032558340355888474; -0.001857833585804452 -0.0016917564308675658 -0.012286381442431018; 0.0019955243900921966 -0.0005933357203349425 -0.002485847010949725] %
+
+Mass Used: 101.73456022588789 kg
+Launch C3: 94.2595859475386 km²/s²
+||V∞_in||: 6.360997078379495e-6 km/s
diff --git a/archive/ES_0.5585082743022702 b/archive/ES_0.5585082743022702
new file mode 100644
index 0000000..7f10a32
--- /dev/null
+++ b/archive/ES_0.5585082743022702
@@ -0,0 +1,22 @@
+archive/ES_0.5585082743022702---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T04:23:09.866
+Launch V∞: [7.976098995449701, -5.78970528673576, 0.13565363086858692] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.006310376070376e-5, 0.00025289453263566055, 4.663494453510462e-6] km/s
+ V∞_out: [0.0002441982560248025, -3.692483671901782e-5, 5.51676686235927e-5] km/s
+ time of flight: 1.8749577787542742e8 seconds
+ arrival date: 2030-04-24T06:32:46.866
+ thrust profile: [0.23576546190778916 0.00374574097269049 -0.0735270665851806; 0.12528337054984573 0.07519616494140889 -0.13225168564150824; 0.05160625011200384 0.05105830235918718 -0.09999288237249546; 0.03194257150798976 0.04032535516513488 -0.0924236108928809; 0.023255091231218765 0.0365342761547974 -0.09353217665676376; 0.01165015392363013 0.022454329987542324 -0.05996858561897789; 0.019716768308595107 0.04507598170730906 -0.13083333764295882; 0.004703008341400799 0.009348553435522291 -0.03370526896502252; 0.004201693830635864 0.009915264495471207 -0.03129037480036023; 0.0037912153914146833 0.00744900800606177 -0.03269132591152926; 0.0011526028617792935 -0.0002920339997868086 -0.007479797336227648; 0.0009414291113257654 0.0015746299198396525 -0.005817686262840227; -0.00034173468689059237 -0.0002420188886544355 -0.004067282989545572; 0.0019346098627189027 -0.0008698354054912697 0.0004082246267489002; 9.706900378395582e-5 0.0021055846607311145 -0.00044630541519327703; 0.0007598800288129248 0.0027291037502666375 -0.002055112990920021; 0.005061755196919385 0.002257838125620866 0.0019023340835446446; -0.002277128471892277 -0.0018497812818394467 -0.0010957753257246697; 0.0038710358256673137 0.0004980240632763782 -0.0016098003096110297; 0.006423796569955492 0.0105982281256109 0.006782142565190333] %
+
+Mass Used: 84.84239435242944 kg
+Launch C3: 97.15724440003757 km²/s²
+||V∞_in||: 0.0002531376283266196 km/s
diff --git a/archive/ES_0.5585111137264063 b/archive/ES_0.5585111137264063
new file mode 100644
index 0000000..3ef6599
--- /dev/null
+++ b/archive/ES_0.5585111137264063
@@ -0,0 +1,22 @@
+archive/ES_0.5585111137264063---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T01:06:21.759
+Launch V∞: [8.045583171880585, -5.7254483227151765, 0.3136285768521365] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5239076150956624e-9, -1.5109395686127551e-9, -1.57404849003205e-9] km/s
+ V∞_out: [5.859862938405448e-11, -1.9631266810917092e-10, 3.1620664274430214e-11] km/s
+ time of flight: 1.874957778747544e8 seconds
+ arrival date: 2030-04-24T03:15:58.759
+ thrust profile: [0.23454117668087773 0.0016857143482430423 -0.07364437179175531; 0.09697759061445026 0.0557439180909695 -0.110795092109591; 0.05240989158151994 0.0478927591676326 -0.10964268895516806; 0.025345433287429716 0.03025052563364094 -0.07907027205163496; 0.019955233799718596 0.03288907872705326 -0.08581215179793046; 0.01474471339871886 0.03302446297537094 -0.10491655201347812; 0.01021333161386178 0.019680519512622622 -0.07260914926555616; 0.009495885510195395 0.01988602126818377 -0.06367323133236415; 0.00416352931542782 0.009748111311989563 -0.04528356785346237; 0.002409402992882838 0.004954136945135228 -0.023840522076271468; 0.0011677543524128845 0.0003573908620935534 -0.005613135725826867; 0.00032170674602880714 -0.0004281690999831684 -0.00046676128394138386; 0.00019944912554401361 0.002254507826340751 -0.004077979050652633; -0.0018244780418217553 0.001564128781084332 0.00014016092417485108; -0.0003453881329162327 0.0005409089639146535 -0.0004642700205529438; -0.002093225361481535 0.003035647566046777 -0.004345441024026598; 0.0009635078729187485 0.002526099356490612 -0.004789023908117335; -0.0006552876110283233 0.006653763830947653 -0.008225472637744806; -0.0028641497850533217 0.002306990906758931 -0.012318989728570092; 0.00031430653959208866 0.00888702802702902 -0.005566103609559365] %
+
+Mass Used: 82.20154127110845 kg
+Launch C3: 97.61052995594838 km²/s²
+||V∞_in||: 2.6613645838776814e-9 km/s
diff --git a/archive/ES_0.5585187292892567 b/archive/ES_0.5585187292892567
new file mode 100644
index 0000000..771eaaf
--- /dev/null
+++ b/archive/ES_0.5585187292892567
@@ -0,0 +1,22 @@
+archive/ES_0.5585187292892567---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:23:34.253
+Launch V∞: [7.9397825893900285, -5.821159053117629, 0.13939111461233175] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.409372363449379e-6, 6.508198140272833e-5, -0.0012347517550926192] km/s
+ V∞_out: [-5.3758466342218255e-5, 0.00123529989063328, -1.5974918351857853e-5] km/s
+ time of flight: 1.8184106329708174e8 seconds
+ arrival date: 2030-02-15T14:47:57.253
+ thrust profile: [0.29865479798493944 -0.015448844789831809 -0.09759708394063327; 0.05755937345592549 0.029479069532627113 -0.06670197338310713; 0.06194812654532191 0.051916580813296684 -0.1274385135037684; 0.033103597527981934 0.03587943552327029 -0.09991283534898908; 0.020743474613927202 0.027289319415233992 -0.08356932750142765; 0.033447283796955204 0.05024492607926748 -0.16217163345003902; 0.016872812760589398 0.02738479470199199 -0.09804841897072193; 0.007199670691691329 0.014122755822930138 -0.0530801990093513; 0.006233604920762115 0.011396933718968884 -0.045287831593235676; 0.0005964693547512486 0.0034256703359169405 -0.012344365695264311; 0.002235763507381849 -0.0006325258663615095 -0.003086573542624363; -0.002043275588268622 0.0011448283384156883 -0.004164697229595837; 0.0008787687199934222 -0.0028624099872942886 -0.0034443387719983775; 0.00155795629234385 -4.0588739156515466e-5 0.003937744058171208; 0.0016156176636829183 -0.004963066582816832 0.0005787996638246713; 0.0016201219428640576 -7.188868799572402e-5 0.0018980395760665914; 0.0006715936157533756 -0.0006807838754327397 0.0002869515479978716; 0.0033027735001021604 0.0016446001951263005 -0.003576784649639242; -0.00014067879219474224 -0.0003833456136866076 0.0012048059496647546; -0.0018100994418342178 -0.0005985510851111786 0.00449789450238314] %
+
+Mass Used: 86.08994150484068 kg
+Launch C3: 96.94547017130722 km²/s²
+||V∞_in||: 0.0012364943503919278 km/s
diff --git a/archive/ES_0.5585199492799439 b/archive/ES_0.5585199492799439
new file mode 100644
index 0000000..16ae135
--- /dev/null
+++ b/archive/ES_0.5585199492799439
@@ -0,0 +1,22 @@
+archive/ES_0.5585199492799439---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T16:21:44.985
+Launch V∞: [7.838846546874048, -5.66360566090696, 0.33835335403093303] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0001788687454260667, 0.00014368369570958814, 0.00011655323677680784] km/s
+ V∞_out: [2.4617410139805725e-5, -0.00016325701272752838, 0.00019728632199514468] km/s
+ time of flight: 1.8749577786437747e8 seconds
+ arrival date: 2030-04-20T18:31:21.985
+ thrust profile: [0.4862175076940379 0.024922102972784792 -0.1141140125364418; 0.15006213374864277 0.10694254341732166 -0.1339616836603562; 0.064457366213566 0.07733436251569484 -0.11124631136708772; 0.04460401186045826 0.07153585115338167 -0.11777160428312237; 0.029183319133382398 0.06450823403539928 -0.11764742937330122; 0.010304237295103038 0.03141055580420059 -0.061795998690646343; 0.011889740755745856 0.04352427707983442 -0.0883758828543582; 0.0031376425758353533 0.01215283735821474 -0.028907490229156164; 0.002248946404348655 0.009241017243157392 -0.02211711626030574; 0.0006394606828607737 0.002850321403536122 -0.006490375898780988; 0.0010375775393478945 0.0012031089287276786 -0.001144509965639356; -0.0017178709938190549 0.0008565965706196191 -0.0007892514421859882; -2.4741867114297952e-6 -9.589686420087814e-5 -7.8968085195382e-5; -0.0013857877825612355 -0.0003055488105501825 -3.399805119396046e-5; 5.5223149231728005e-5 0.0017447491418039634 -0.00018520826525191274; 0.00033406333508363017 0.0004638454019863377 -0.0003871861106106545; -0.0003161496068389217 -0.0016444065145261853 -0.00035591147378056826; 0.0007333343103858653 0.0029057778304088767 0.0007334075700084672; -0.0007641269530156444 -0.0026903612897052256 -0.0013238927830175498; 5.029521136122758e-5 0.0035133188479505298 -0.0003823737538888209] %
+
+Mass Used: 105.38244847729811 kg
+Launch C3: 93.63842725988053 km²/s²
+||V∞_in||: 0.0002573396384279173 km/s
diff --git a/archive/ES_0.55853810775037 b/archive/ES_0.55853810775037
new file mode 100644
index 0000000..a734a5e
--- /dev/null
+++ b/archive/ES_0.55853810775037
@@ -0,0 +1,22 @@
+archive/ES_0.55853810775037---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T02:57:00.787
+Launch V∞: [7.805268287045216, -5.8665225398298935, 0.1695836851270444] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4608300840308782e-9, -9.545712493238852e-10, -1.1336286673512399e-9] km/s
+ V∞_out: [4.644860927748129e-10, -4.108746567758363e-10, -3.391303331097775e-10] km/s
+ time of flight: 1.8062385756194162e8 seconds
+ arrival date: 2030-01-31T16:14:37.787
+ thrust profile: [0.41151556478552703 -0.016800905945208427 -0.12410346313676072; 0.0880615540609967 0.04556839194148163 -0.09666198040374042; 0.04884905986376552 0.04126191868631873 -0.09620623083562431; 0.031899415299894894 0.03528714917021566 -0.09269948995787831; 0.0507397696124347 0.06835893249089393 -0.18926318541044254; 0.01661120106524823 0.026099219872346223 -0.08232197863190138; 0.02375153986422405 0.042496751948545304 -0.13765285654947682; 0.0071705523179125446 0.014399082721116516 -0.05143916471152534; 0.0006022543041573623 0.0010410749094608954 -0.004377356426819864; 2.0806305852067743e-5 -0.0001181362214158104 -0.0004557609082179411; 0.000992732943342092 0.00025917157582457974 -0.0018617276396692302; 0.0003862872824529929 0.0008081577286536794 -0.0024593510931806483; 0.0002482139638128262 0.0011831635707288402 -0.003105824182345571; 0.0030244778778161265 -0.0001572100257222174 -0.00147872612414116; 0.00054998134922126 0.0030951410886986943 0.00035666526687987404; 0.0010160081821146243 -0.00018529269420650704 -0.0008115794691644237; 0.004651175752213741 -0.0011519668423439896 0.004424762904759814; 0.0004699409129210847 0.00047872436284012625 -0.0005030252501906658; 0.0031505127755234626 0.004885104699840197 0.009486230371639861; 0.002064136984858937 0.0006738320326097214 -0.0002082557483042484] %
+
+Mass Used: 95.3199518875731 kg
+Launch C3: 95.3670583693472 km²/s²
+||V∞_in||: 2.0809480435335174e-9 km/s
diff --git a/archive/ES_0.5585557724152452 b/archive/ES_0.5585557724152452
new file mode 100644
index 0000000..f2e856b
--- /dev/null
+++ b/archive/ES_0.5585557724152452
@@ -0,0 +1,22 @@
+archive/ES_0.5585557724152452---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T10:49:46.200
+Launch V∞: [8.016835745087937, -5.879120639147432, 0.027987152839179557] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.402138699343953e-10, -9.372602981556379e-10, -1.1520515168767392e-9] km/s
+ V∞_out: [-2.4985913069210892e-11, 2.4309936658639974e-11, -9.529896496455885e-12] km/s
+ time of flight: 1.8331713361461288e8 seconds
+ arrival date: 2030-03-06T04:15:19.200
+ thrust profile: [0.1312699990871551 -0.001906767610419957 -0.045520505186322946; 0.042899888491343206 0.024033137326564067 -0.049549929775215176; 0.07478612607880221 0.06720624411472616 -0.14811665211853708; 0.03228441863210448 0.03702365031532089 -0.0942553668165077; 0.03319726061914407 0.04336674890027748 -0.12452275951044524; 0.029890837519470814 0.04580111844750515 -0.1374392659776441; 0.008425385010596708 0.016687080770813083 -0.05601714987502921; 0.008973115953521299 0.017502274999835785 -0.06296716235228722; 0.004608214290571902 0.009970723728730386 -0.03957824350983556; 0.0030709019144189082 0.007886766017450468 -0.03135429489026157; 0.00027611606151400485 0.0010311746933819518 -0.005388894448926845; 0.0011904315842300945 0.003011830384777296 -0.014172496230763922; 0.0025364830096373677 0.002153191571033504 -0.0010165496581793863; -0.004113898239486151 -0.0010510275159412957 -0.00039293304098957267; -0.004087623712948105 -0.0004953458022065588 0.002197647453981887; 0.0002920154322190422 -0.0007398403824465743 0.0004025158696136989; 0.010514126971343378 0.0023690361655201476 -0.0013409123072385281; 0.005654309281307551 0.0007462084638179343 -0.0039665468474478615; 7.323991997770253e-5 -0.00028858938333283017 0.0006105779913317972; 0.0003406367482010255 0.00044578342906228597 0.000366062434220099] %
+
+Mass Used: 75.11382870224361 kg
+Launch C3: 98.83449813409301 km²/s²
+||V∞_in||: 1.659396317122599e-9 km/s
diff --git a/archive/ES_0.5585611978249756 b/archive/ES_0.5585611978249756
new file mode 100644
index 0000000..5a8cca0
--- /dev/null
+++ b/archive/ES_0.5585611978249756
@@ -0,0 +1,22 @@
+archive/ES_0.5585611978249756---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T18:08:23.825
+Launch V∞: [7.6645190855408085, -5.972046355066068, 0.24023092806917992] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2235286226953338e-8, -1.871298578775083e-7, 3.417996400355513e-8] km/s
+ V∞_out: [-3.055710946955356e-8, 1.1115569864942229e-7, 1.5404519893153722e-7] km/s
+ time of flight: 1.7780049445822656e8 seconds
+ arrival date: 2029-12-28T15:09:57.825
+ thrust profile: [0.45671998682975457 -0.030361461938244363 -0.11555731832391933; 0.07765215727962052 0.042366630733820285 -0.0724456484514825; 0.07999198228891494 0.06807849220131092 -0.12351762603847027; 0.02625621316093059 0.03148789392181663 -0.06526930010948878; 0.08724705592448571 0.11037301673460001 -0.2301755863063942; 0.023787852675571566 0.04122707242971307 -0.09704674377986346; 0.027207121491570185 0.05250089609306267 -0.13227743225155078; 0.00666945561297665 0.016847226878136123 -0.045729163666741686; 0.0010851859286487174 0.0033804140339193027 -0.009398220779929752; 0.0005720226316969898 0.0011335467264690059 -0.004191648433569585; 0.00012203787745545785 0.0007761732274608048 -0.0031750410526107543; -7.469821378179361e-5 0.0003674476204432767 -0.0002828937166662073; 0.0003069831909864791 0.0001631643147238351 -9.312522662136046e-5; -3.681114280292008e-5 0.0001093137710398551 -0.0003017769772154359; -0.00012156587988031061 -0.00017713103666418218 -0.00032254142131281377; -0.0004319353771210294 -0.0001485662080625399 0.00031723267205696024; -8.215236999136073e-5 1.5781564847854623e-5 -0.00011632399128960845; -0.000639747702338302 -0.00021704152672370205 -0.0006423146521273581; -6.761980185737002e-5 0.00011069738527310168 0.0007421429370180342; 0.0003745099319654711 -0.0009715531743701808 -0.0012302891997025406] %
+
+Mass Used: 100.59197275468205 kg
+Launch C3: 94.4679013784782 km²/s²
+||V∞_in||: 1.9152091687890208e-7 km/s
diff --git a/archive/ES_0.5585621186956828 b/archive/ES_0.5585621186956828
new file mode 100644
index 0000000..a46c10e
--- /dev/null
+++ b/archive/ES_0.5585621186956828
@@ -0,0 +1,22 @@
+archive/ES_0.5585621186956828---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T10:57:37.745
+Launch V∞: [7.7113007988953415, -5.605806768462785, 0.1932706953451506] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1411864102662826e-5, 9.051585126262427e-5, -0.0016679131362233827] km/s
+ V∞_out: [-6.68595874944899e-5, 0.001662250780865691, -2.1548398303339808e-5] km/s
+ time of flight: 1.8613596856291556e8 seconds
+ arrival date: 2030-04-03T19:23:45.745
+ thrust profile: [0.7402394396290365 0.007313648807831413 -0.1915042985819171; 0.16688788375067967 0.10526517728515357 -0.16298297270796833; 0.05466021418921908 0.05646644021696119 -0.1021929079782081; 0.055282482641853425 0.07831288266348123 -0.15353720657173264; 0.02237453837658505 0.03943440081479446 -0.08861616019278573; 0.01082854286905821 0.023021439915342636 -0.05703336260139691; 0.007385369873612948 0.01836471605855119 -0.0485939102651073; 0.0029104026521122543 0.009330692581304641 -0.025757820932020406; 0.004253850247424283 0.015112186644098637 -0.043977896258259284; 0.0006487829818609162 0.0026732737247633213 -0.008254833191440247; 6.257456928790427e-5 0.0002803842930589409 -0.0004002872710795796; -0.0004025601497931761 -0.00013742760390172168 -0.0009143125121511924; 3.6060942983300796e-5 -0.00042685800339301944 -0.000445919925552993; 0.0004506196092027391 0.0005666965969065017 -0.0008471816739502754; 0.00011084064029776942 0.00029059370629232396 -6.827649948367321e-5; 4.191812129374984e-5 0.00016953221944507497 -0.0008248951712044076; 9.732603880424325e-6 0.0003003513851289949 -0.0006944969669168055; -0.0007627268981069426 1.9847347307027296e-5 -0.000989569507108837; -0.00015049812264010808 0.000938883428826455 0.00014381419463695426; 7.672476342965084e-5 -0.00016985640738025043 0.0006356804524977268] %
+
+Mass Used: 121.25073707290994 kg
+Launch C3: 90.9265830980663 km²/s²
+||V∞_in||: 0.0016704064116132382 km/s
diff --git a/archive/ES_0.5585671165809374 b/archive/ES_0.5585671165809374
new file mode 100644
index 0000000..28bf322
--- /dev/null
+++ b/archive/ES_0.5585671165809374
@@ -0,0 +1,22 @@
+archive/ES_0.5585671165809374---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T17:27:13.475
+Launch V∞: [7.982237703080925, -5.746671144663916, 0.10550083812656431] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.932767220271572e-9, -4.89128528421792e-9, -2.399595685650172e-9] km/s
+ V∞_out: [-6.0548362985248816e-9, 5.942603194470389e-9, -2.1282070986571065e-9] km/s
+ time of flight: 1.8181630781170997e8 seconds
+ arrival date: 2030-02-14T01:59:00.475
+ thrust profile: [0.3034384749220337 -0.008740482776214127 -0.09383366896596035; 0.08348315211159117 0.04632523169284882 -0.0909597711230732; 0.051308407039000824 0.04654332745316881 -0.10120956029798726; 0.03742545385374795 0.044812065766126445 -0.10867320625940222; 0.028309830713959205 0.042120109034543406 -0.11117973792597663; 0.016132548671185444 0.028142599550354957 -0.08300410234399279; 0.008487313936647504 0.01953371553087707 -0.06078615107891013; 0.018452792179542606 0.039641830354586155 -0.1273425827323439; 0.006781909322270083 0.012423912690635815 -0.04694884219137327; 0.00275666843756808 0.008866507307142361 -0.032565348646131934; 0.0005068344259699245 0.0008980547365479434 -0.0007310300713182233; 0.00035227796061685393 0.0005120188539515583 -0.0036584653660679672; -0.00027046440292540923 -0.0003775338373197077 -0.0023822848847338467; -7.601175235210153e-5 -0.0005490258485495032 0.0006672194555065836; 0.0004857616039093773 -0.00030497410561921407 -0.00034996787095981704; 0.0009212999547986149 -0.0001575076078414112 0.0003369255558531714; -0.001221308947011134 -0.0005809508974149376 0.000369134131473315; -0.000954794233926378 -0.0025912634920698357 0.00017665017488859046; 0.000713227847708183 -0.0006864735089641539 0.0009060491674650606; -0.00027245883085132974 -0.0010564333718842312 0.0004902999423026572] %
+
+Mass Used: 87.27801189299817 kg
+Launch C3: 96.75147842024494 km²/s²
+||V∞_in||: 8.81736879781433e-9 km/s
diff --git a/archive/ES_0.5585711995701728 b/archive/ES_0.5585711995701728
new file mode 100644
index 0000000..a83266d
--- /dev/null
+++ b/archive/ES_0.5585711995701728
@@ -0,0 +1,22 @@
+archive/ES_0.5585711995701728---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:35:24.376
+Launch V∞: [7.807565101456977, -5.852125460804644, 0.1760603014825804] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0816760326441687e-10, 3.2284018908403263e-9, -1.62014727419302e-9] km/s
+ V∞_out: [1.3947347556492824e-9, 2.820002871766852e-9, 7.36602266016087e-11] km/s
+ time of flight: 1.808358672337401e8 seconds
+ arrival date: 2030-02-03T09:46:31.376
+ thrust profile: [0.449651858648135 -0.01915974946756109 -0.14044587411043563; 0.07450244359969128 0.03404626087789216 -0.08724940254533554; 0.0356311994809208 0.029067686496246293 -0.0727307653640732; 0.041145669122825856 0.04774139462457197 -0.12442996797392201; 0.030221188455605917 0.04337480315509651 -0.12855725673501406; 0.027455274758155367 0.04294601262919656 -0.13434857949977777; 0.008394190979269888 0.015089060009546055 -0.05598045019542322; 0.007482668477983526 0.018069263280919432 -0.06728211502702905; 0.0003160802196002008 0.001614796823131498 -0.007429198685007082; 0.008221767751918402 0.012009327424402543 -0.06100481265808517; 0.0005318579538164223 0.0012069526637422077 -0.0041072996785625985; 0.0009630220346913986 0.0017209238700034825 -0.00822890403834469; 0.0008012731780658809 -0.0005915024385286411 -0.00207499136333879; -3.427280536588976e-5 -0.0003018598385486177 -0.0024862842375355534; -0.0004757728702067158 -0.0007317837104971413 -0.0009936669027894153; 0.0015647017380972252 -0.0013176962937867444 0.0011136262795625736; 1.6696256860175027e-5 0.004169042244792524 0.00028162222936181235; 0.0030080401465136276 -0.003674532617423152 -0.0005239905561799656; 0.0007065405326642854 -0.0008750846650121318 -0.003610676255910327; 0.00038200767026348205 -0.0007198715940680179 0.00242846709217064] %
+
+Mass Used: 96.12048519377231 kg
+Launch C3: 95.23644245224502 km²/s²
+||V∞_in||: 3.6181196373123595e-9 km/s
diff --git a/archive/ES_0.5585751446149586 b/archive/ES_0.5585751446149586
new file mode 100644
index 0000000..74c9a60
--- /dev/null
+++ b/archive/ES_0.5585751446149586
@@ -0,0 +1,22 @@
+archive/ES_0.5585751446149586---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:52:06.699
+Launch V∞: [8.051937603459269, -5.725446015935759, 0.18089526445676088] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.345582912063002e-5, 4.9344881006613536e-5, 0.0028112057071315744] km/s
+ V∞_out: [-0.0025082353356540884, -0.0008512772564817079, 0.0009457841950175752] km/s
+ time of flight: 1.8749577787493622e8 seconds
+ arrival date: 2030-04-23T20:01:43.699
+ thrust profile: [0.20339430032352954 0.005448553524634146 -0.06413052807018581; 0.11080826227115805 0.06682500538171174 -0.11454068993754203; 0.053269294966682465 0.05083856799381777 -0.10272382502361575; 0.03543207118935839 0.043879169456650206 -0.10355337642821329; 0.022614890581699423 0.03426339480700573 -0.08972245336305497; 0.022086299992226166 0.03595171117547331 -0.08715893478443844; 0.00955960507110546 0.019089478707389283 -0.05590535797599775; 0.0012136434526058017 0.015010409212935203 -0.05985369855343283; 0.004273261339142271 0.010721904003147247 -0.030618268137078374; 0.0012928576217712292 0.008347451862233077 -0.029219326150789725; 0.0012336362348624595 0.006347302689477075 -0.02818873266687299; 0.0010545550501252178 0.0036971615341947757 -0.030080795623289136; -0.0015010996180894248 0.00038468754981136493 0.0009850493140530119; -0.0004105753066065976 -0.0020595509437835 0.0004371064061685333; -0.0011260225103946508 -0.0012698339424248315 -0.0026453601565189716; -4.4728443570139315e-5 0.001372052843146039 0.0004576585706519353; 0.0021932171826151577 -0.003201277438248048 -0.0002294989467387903; 0.001439758468911781 -0.0032044726688317815 0.0030232977737704282; -0.004342437330754705 0.0004893613720161167 -0.0021582878600904026; -0.005193398513687029 -0.0017887705663642225 -0.004803174052119474] %
+
+Mass Used: 82.06260168687459 kg
+Launch C3: 97.64715434809894 km²/s²
+||V∞_in||: 0.002812598123430095 km/s
diff --git a/archive/ES_0.5585781048910213 b/archive/ES_0.5585781048910213
new file mode 100644
index 0000000..f948a38
--- /dev/null
+++ b/archive/ES_0.5585781048910213
@@ -0,0 +1,22 @@
+archive/ES_0.5585781048910213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T15:42:05.262
+Launch V∞: [8.009386832158851, -5.902161648887774, 0.12147659332926092] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.064097386565781e-10, 3.5417790788337986e-10, 8.981677930780354e-10] km/s
+ V∞_out: [7.612101366303801e-10, -1.8169974524506463e-9, 2.7872143111707573e-10] km/s
+ time of flight: 1.8530670418568638e8 seconds
+ arrival date: 2030-03-31T09:47:09.262
+ thrust profile: [0.11743147826849115 -0.006985565694192339 -0.04613615801161532; 0.1799502131295248 0.07246590852485128 -0.22522731848781857; 0.016741991199429172 0.01059120471136338 -0.04158215819949416; 0.018195192106768964 0.01455060693092832 -0.06412969624000607; 0.01571229667045086 0.014133828372718558 -0.07133682161984352; 0.028241483602298296 0.024858733326595092 -0.14828443448261944; 0.00877446289257597 0.00856381472990172 -0.05415261423373764; 0.006306099487374712 0.007442801284009273 -0.04844319018730402; 0.003913484212666624 0.004975548771765046 -0.039195604687727245; 0.010074997493273632 0.010912249543575293 -0.08415185539095942; 0.000159927489905663 0.0002398856620493872 -0.00163551549046545; 0.0003251975959190583 -9.338402190967862e-5 -0.0011877796931224352; -0.00010174504294941733 -2.8761107936899766e-5 -5.871677423273391e-5; 0.0004244309037233113 -0.00021492636994978003 -0.0007219813735801295; 0.00047427465058276676 -0.0002576054721611019 0.00034567477780583094; -0.0004862950313936126 -0.0006077226713804892 0.0009247674850223658; 0.0002834771158764019 -1.8039811656320545e-5 0.0001438361443062855; -0.00023158951144589338 -0.000227667821395076 -0.000780471989149799; -0.0005395059988600056 -0.00127296733668917 0.00037314492256666277; -0.000788068178351327 -0.001157057309823202 0.0005034786430718822] %
+
+Mass Used: 74.17127000917753 kg
+Launch C3: 99.00054611948812 km²/s²
+||V∞_in||: 1.324283198295139e-9 km/s
diff --git a/archive/ES_0.558583018328003 b/archive/ES_0.558583018328003
new file mode 100644
index 0000000..ecea2e4
--- /dev/null
+++ b/archive/ES_0.558583018328003
@@ -0,0 +1,22 @@
+archive/ES_0.558583018328003---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T03:35:05.158
+Launch V∞: [8.068249273928444, -5.622796795184108, 0.058482473512082134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0077268957768432895, -0.04868658326802686, -0.0506279591446379] km/s
+ V∞_out: [0.012854301069732125, -0.010206038309666656, 0.06885190520044461] km/s
+ time of flight: 1.8548109303980342e8 seconds
+ arrival date: 2030-03-29T22:06:38.158
+ thrust profile: [0.35915339967008786 -0.0065057523195638615 -0.11575579615299025; 0.042208989467874734 0.0230601901108691 -0.049915239764377166; 0.03492142329497505 0.03089817682080598 -0.0741386613130564; 0.02856472405036442 0.03311514255996554 -0.089226916501282; 0.018842765513980137 0.026745641559829766 -0.08032862249337613; 0.01567136006533991 0.025735825880172692 -0.08404421933116932; 0.016506654453679635 0.030952618500766797 -0.1069618116378423; 0.018535748393592195 0.03991010285538752 -0.1424846374759693; 0.003899473349772998 0.009086558041255612 -0.03660585205236979; 0.001780734303186685 0.005102982303208122 -0.02139519039750911; 0.0011231250682683497 0.0026666127339624985 -0.01441779978577391; -0.0003382989765060412 -5.9538035649728596e-5 0.00032220700684230507; -0.0006979947255258081 -0.0026714196525123596 -0.0018151852656768603; -0.0012267741691225614 -0.0008423570320654529 -0.003323662064029322; 0.0007640992215366814 0.0019377262114184434 -0.010521364195345474; 0.0008859774613520547 0.0009718726231285013 -0.003694178767668277; -0.0010022766759581686 0.0013083782295937622 -0.000765347108018929; -0.0029802938563192657 -0.0032688504142086346 -0.00015617348639308977; -0.006364150932627827 0.0004412382047496638 0.0023256935005597787; 0.0017803908798300694 0.0021121640276738603 -0.002324572896383524] %
+
+Mass Used: 87.5040443649923 kg
+Launch C3: 96.71591034588764 km²/s²
+||V∞_in||: 0.07066313434749294 km/s
diff --git a/archive/ES_0.5585832639300607 b/archive/ES_0.5585832639300607
new file mode 100644
index 0000000..f699f6d
--- /dev/null
+++ b/archive/ES_0.5585832639300607
@@ -0,0 +1,22 @@
+archive/ES_0.5585832639300607---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T08:42:55.036
+Launch V∞: [7.572234079129795, -5.943632696384549, 0.16144877721068254] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7239979731744276e-9, -2.2798791560673193e-9, -1.4828740997896514e-9] km/s
+ V∞_out: [-2.3763444167828687e-9, 2.1892381197247557e-9, -8.067527653246678e-10] km/s
+ time of flight: 1.819102215010775e8 seconds
+ arrival date: 2030-02-14T19:19:56.036
+ thrust profile: [0.48611642040377084 -0.0015695919529295046 -0.13265769686626033; 0.22852082616417674 0.13806535067471015 -0.20797833672766236; 0.09836897478059708 0.09775226245064364 -0.1658806227495376; 0.0635826599106953 0.0852323055621186 -0.16126122875234955; 0.025373529163404004 0.041921394276843764 -0.09005766140071352; 0.01688277116731403 0.03381731353662564 -0.07844570846486759; 0.002957650150026095 0.009207667667792 -0.026156429463345558; 0.001206372355413675 0.002828126842311451 -0.009388078231907468; 0.0018810898568145276 0.002134290043790999 -0.008044654535296257; 0.0019690673235943368 0.0071859537531987 -0.021216432510159; 0.0013242985627038527 0.002838304091945457 -0.006883076281345428; 0.0002168408905208856 0.00044295896024647974 -0.001646375731389008; -7.931861558580866e-5 0.0007001897812575025 -0.004382712445216406; -5.933149451636745e-5 0.0006191541517184683 -0.00018728697942341807; -0.00031403492937696995 0.000957070467222325 -0.000584592240008809; 0.0003494383202586629 -0.00044994366863199695 0.0015844079057942488; -0.0001102009898080528 -0.00014985582754857357 0.00012983503229846167; -0.00080279452087519 0.001982994199696505 -0.0010289782433369253; -6.816172780680823e-5 0.00012748122414263103 0.0009322915294257028; -0.0008515138147305446 0.0009099924302637768 0.00024659620539636547] %
+
+Mass Used: 110.97968291481857 kg
+Launch C3: 92.69156428632895 km²/s²
+||V∞_in||: 3.8492764930510764e-9 km/s
diff --git a/archive/ES_0.5585843660980615 b/archive/ES_0.5585843660980615
new file mode 100644
index 0000000..4c30a5d
--- /dev/null
+++ b/archive/ES_0.5585843660980615
@@ -0,0 +1,22 @@
+archive/ES_0.5585843660980615---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:53:03.404
+Launch V∞: [8.057795001497805, -5.678969711925309, 0.13905686580820872] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0074286472698503895, -0.004693066262468983, -0.00030258422984996914] km/s
+ V∞_out: [0.0065274476543889315, 0.0027825984996801656, -0.005191141494336472] km/s
+ time of flight: 1.8749577787493953e8 seconds
+ arrival date: 2030-04-23T22:02:40.404
+ thrust profile: [0.3103422843935112 0.0004926085999494498 -0.1015051614505432; 0.03702099303132507 0.021016993998396693 -0.04379480582749894; 0.025689329118266935 0.023332612306183543 -0.054869392332614064; 0.02688622058791934 0.031850513948692254 -0.0839887073474161; 0.053917851488067936 0.07850088856111409 -0.21855618855567757; 0.02817912612972062 0.04774092289482126 -0.14821172149400644; 0.006337159561286533 0.012401135491951862 -0.043589685272335185; 0.0031960438227422437 0.007488511683768465 -0.028348523924108655; 0.0027550381013478876 0.007003646992187598 -0.02754629443097765; 8.20592219252553e-6 0.0030854293022819852 -0.014615391876239118; -0.0003291983573591124 0.0003038459809138179 -0.004054061331060062; -0.0020250441646354426 0.0016898778027283814 -0.005818909774592627; 0.005413513213245569 -0.001784015550962176 -0.0038242151700176768; -0.0013623710881100564 -0.0008691189559016654 -0.004057180296085778; -0.002313947934685865 0.001961861585141246 0.003609095945107791; -0.0002476811942103024 0.0008034183401878863 0.002355347539557123; 0.0003663253890205561 -0.0019022197013167496 -0.003969148773204123; 0.0038786531919142307 -0.007792126821654179 -0.010757777260760054; 0.007035267435697969 0.0011969267572957624 0.01101589625423901; 0.002868041819978289 0.008465284806734492 0.008632689967011891] %
+
+Mass Used: 84.69287827324251 kg
+Launch C3: 97.19809408705645 km²/s²
+||V∞_in||: 0.008792111715619527 km/s
diff --git a/archive/ES_0.5585847800199137 b/archive/ES_0.5585847800199137
new file mode 100644
index 0000000..7c1a101
--- /dev/null
+++ b/archive/ES_0.5585847800199137
@@ -0,0 +1,22 @@
+archive/ES_0.5585847800199137---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:08:24.101
+Launch V∞: [7.999578023145296, -5.603665155793254, 0.19659065351245758] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8837080032774074e-7, 1.2094497428515856e-6, -2.9308873767037495e-5] km/s
+ V∞_out: [-1.2131080637015667e-6, 2.9257630973026067e-5, -2.2168829121124842e-7] km/s
+ time of flight: 1.8749577787453115e8 seconds
+ arrival date: 2030-04-22T09:18:01.101
+ thrust profile: [0.44078327062848643 0.005312960398245033 -0.1296452258088183; 0.05249478358578657 0.03164049756069438 -0.059715294236344967; 0.04239505811439647 0.041730062884394716 -0.08753353935929882; 0.03937287350596021 0.05206311472183555 -0.11929240450687996; 0.0328670741361379 0.055298583575603126 -0.13846254372098593; 0.013280017248911674 0.025510721468374714 -0.07193342443175646; 0.010353048607031777 0.023101365306317873 -0.07024483808114643; 0.009025261692574534 0.02355004929214919 -0.07378273247532283; 0.001848466577718323 0.005635191940802973 -0.020230565881029255; 5.871402277713984e-5 0.0026187520353397513 -0.008727702786377682; -0.0014162635297345304 0.0025327810133628555 -0.005265371526353663; 0.0009124496462800842 0.0009840829493734367 -0.006680629414327091; 0.002972765502210076 0.0013385587683988705 -0.00215879846230084; 0.005071125297388906 -0.0030121066790358337 -0.006606376925190454; 0.0006122242633619388 0.0020321795933032887 -0.010608811271855065; 1.367124225664599e-5 -0.00043855818308271514 -0.0007670443665234172; 0.002876719639517661 0.005499447085624101 -0.005133101031126944; -0.00012438088590423137 0.002507391181328411 -0.008232351738086419; -0.00016292211158748594 -0.0015832851327876587 0.006062505335993494; 0.012196036304742832 0.0009907835417596838 -3.38929221951585e-5] %
+
+Mass Used: 94.98997895504635 kg
+Launch C3: 95.4329596116891 km²/s²
+||V∞_in||: 2.9334422335049288e-5 km/s
diff --git a/archive/ES_0.5585854166141828 b/archive/ES_0.5585854166141828
new file mode 100644
index 0000000..869060d
--- /dev/null
+++ b/archive/ES_0.5585854166141828
@@ -0,0 +1,22 @@
+archive/ES_0.5585854166141828---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T12:12:03.598
+Launch V∞: [7.895231319942336, -5.7345161439021775, 0.23029675214545983] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.2457025733011545e-6, -3.027749951166111e-6, 2.0867001636163187e-6] km/s
+ V∞_out: [-6.028590468389397e-7, -4.8481256803173555e-6, 2.1955579032406262e-7] km/s
+ time of flight: 1.8576167281921375e8 seconds
+ arrival date: 2030-04-01T12:39:55.598
+ thrust profile: [0.353786998301117 0.0039041030090489434 -0.0951112859488846; 0.1564044693345203 0.10687044431327318 -0.15308845617377073; 0.06266833746281324 0.06699823372098998 -0.11656052926747561; 0.03387754811658979 0.048424787712188395 -0.09715692197782268; 0.018364769862268416 0.03274596679142432 -0.06569187254388405; 0.013076151977198195 0.029207582072174682 -0.06506481467140332; 0.013208345569952878 0.043324408280810724 -0.09999824079417885; 0.007354354050814455 0.02048378528849501 -0.05227920620459652; 0.002414582591346908 0.008579957386922646 -0.02372774502201987; 0.001729793283435625 0.009893720967636323 -0.03269369119744391; 0.004170099132544403 0.010567962252643413 -0.03152954532763919; -1.4544377230526928e-5 -0.00039982609368441964 -0.000917373226376095; -0.0015332596782348415 -0.00021250700721755882 -0.000619535749608638; 0.0011940919828643762 4.696446375799775e-5 -0.0018972197023302646; -0.0013357575246257204 -0.001663932735806097 0.0003128494444726166; -0.0011241049029633572 -0.00019337187410499215 0.0008639623935755331; -0.0007730968146068989 -0.0010065229767128173 -0.0003143455909214554; -0.0018255036271876061 -0.0015364123960948089 2.9627640644024002e-5; 0.0011028457901186492 0.001463233515958508 -0.0002774483377152516; 0.0023025738786517968 0.001494330420536056 0.001652832953277854] %
+
+Mass Used: 95.92738008416927 kg
+Launch C3: 95.27238959412185 km²/s²
+||V∞_in||: 4.9047092201226874e-6 km/s
diff --git a/archive/ES_0.5585855884953234 b/archive/ES_0.5585855884953234
new file mode 100644
index 0000000..9f62acc
--- /dev/null
+++ b/archive/ES_0.5585855884953234
@@ -0,0 +1,22 @@
+archive/ES_0.5585855884953234---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T19:25:08.515
+Launch V∞: [7.944684312925982, -5.641428375080976, 0.16236916208267363] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5687617377275243e-5, 1.3524162205296303e-5, -9.817734697501399e-6] km/s
+ V∞_out: [2.9471736044248847e-6, 2.2646565467703074e-5, -1.0750326381407518e-6] km/s
+ time of flight: 1.854997322915216e8 seconds
+ arrival date: 2030-03-28T19:07:20.515
+ thrust profile: [0.4531930626865335 -0.00035501966694936914 -0.11605957071822168; 0.0744169942643639 0.04790474829930389 -0.07879894951710499; 0.044518647617487465 0.0468835842676103 -0.08402750521097618; 0.04974490972982047 0.07072617445572575 -0.13590152001567524; 0.020807028872723267 0.03711037838417176 -0.08080117522255795; 0.023758319539851358 0.049541450699376495 -0.11560333414616449; 0.009007903818632475 0.023962340119456492 -0.06051170386179882; 0.006461971798893509 0.017026643780399742 -0.048120070445272944; 0.007755373617096528 0.02763587806955486 -0.0737798461492513; 0.0016602649419281447 0.00727478072468318 -0.021432035903198518; 0.000400574054489793 0.0017558915563589568 -0.005856804216816559; 0.0010237993801377012 0.003703128288854168 -0.005415070681458518; -0.0006227960959674588 -0.0010308295700339842 0.00033485300795873304; 0.0014876826770957227 -9.184989763584464e-5 -0.003912908453059037; 0.0001314812158630936 0.0017372062003940007 -0.0013541854255032645; 0.00156269643251387 0.0023926231624646047 0.0006495151853242614; -0.0008107744433151825 -0.001903757676818244 0.0004190268175726657; -8.630086087515728e-5 0.001814047600484738 0.0023663832294260594; 9.852795727807522e-5 -0.000690940366420984 6.359634108393688e-5; 0.000511847014396028 0.0015174305515444236 -0.0005489955303930498] %
+
+Mass Used: 97.69101423111488 kg
+Launch C3: 94.9700866880164 km²/s²
+||V∞_in||: 2.2921435751747226e-5 km/s
diff --git a/archive/ES_0.5585875205778762 b/archive/ES_0.5585875205778762
new file mode 100644
index 0000000..72d731f
--- /dev/null
+++ b/archive/ES_0.5585875205778762
@@ -0,0 +1,22 @@
+archive/ES_0.5585875205778762---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T17:14:10.657
+Launch V∞: [7.804421343407136, -5.792507063579736, -0.18295274205616988] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.004697956263317e-5, 0.0026873841548795984, 5.365320056795047e-5] km/s
+ V∞_out: [0.0027714876742202447, -0.0004538984447459206, 0.0006170167925928807] km/s
+ time of flight: 1.8642505417974496e8 seconds
+ arrival date: 2030-04-10T09:58:24.657
+ thrust profile: [0.4697899490495666 0.006612594970391782 -0.1364161340006616; 0.08102628117573046 0.050634883549767314 -0.08546302231875952; 0.05599889730471419 0.057871609025681184 -0.10888825845398999; 0.06538042416153796 0.09169941164263955 -0.18398241423896114; 0.020399117598904306 0.0354570353089625 -0.08352722535459853; 0.010713833161619129 0.022783162121634785 -0.059029794947570956; 0.011999797416244726 0.0390652930848275 -0.09902937190070464; 0.005201455787441812 0.015497106786250816 -0.04510098678940783; -0.00034662624255440196 0.005111375144699679 -0.015395910464892842; 0.0009814352180099436 0.003192022414744741 -0.010335964896124901; -0.002733384980563246 0.00031226387627956965 -0.0050157026224795795; -0.0010289165131025448 0.0007649146962419194 -0.0074064390993632415; -0.0018357496485812718 0.001695534963165974 -0.001454624175761184; -0.0015568615896753824 0.0009057552910243083 -0.0022482306141058776; -0.0014843733795900879 -0.0002673036612171783 -0.002456902671700995; -0.0013052671252011664 0.0008923922112983184 0.0005562705046215956; 0.0002362816557610998 -0.0004949094944223858 0.002195326842560585; -0.0014565331177949393 -0.00533822126586644 -0.0021523085206022812; 0.0009845083258155443 -0.0061452238928867385 -0.004669927133461697; 0.004659294634069149 -0.0034159907394898407 0.0007700194012301598] %
+
+Mass Used: 100.46109396574639 kg
+Launch C3: 94.49560229287586 km²/s²
+||V∞_in||: 0.0026882180012791387 km/s
diff --git a/archive/ES_0.5586053441148139 b/archive/ES_0.5586053441148139
new file mode 100644
index 0000000..1751540
--- /dev/null
+++ b/archive/ES_0.5586053441148139
@@ -0,0 +1,22 @@
+archive/ES_0.5586053441148139---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T02:34:31.390
+Launch V∞: [8.058827652448207, -5.840557898848283, 0.47212547102953606] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.960529328300668e-5, -6.55394891470949e-5, -0.004452821150242591] km/s
+ V∞_out: [0.00425543234892623, 0.000891970495920396, -0.0009653863185611214] km/s
+ time of flight: 1.8573112783415443e8 seconds
+ arrival date: 2030-04-05T18:33:18.390
+ thrust profile: [0.18594033030812315 -0.019364719116423915 -0.07416201761763497; 0.05829904357486814 0.018710959745419666 -0.08160961604563002; 0.040172408387585595 0.018823324175209464 -0.09887636718236445; 0.03840698685831581 0.020233193186512604 -0.13248445278554147; 0.02979538166705459 0.016617081941020642 -0.13105479183161356; 0.019176169477630355 0.010662930059824563 -0.09903860455674976; 0.010049587247266147 0.0056183578642874646 -0.05942720887321053; 0.003228145465330148 0.0016187736761890982 -0.02145252591299337; 0.008720793346398465 0.0050469058984568636 -0.06257490061292043; 0.0018996937051517925 0.0008047904521003844 -0.014028846800698649; 0.0004225497767852386 0.0008856330134996438 -0.006407822400711318; 0.0019987208601675486 0.000683289198007571 -0.014971417272661366; 0.0005497275138941863 0.0004453847888671647 -0.003042883290381524; 0.00012370402611770184 5.790493294844355e-5 -0.0012980801280014524; 0.00031240145574388606 -4.210893948627958e-5 -0.0010360941632663156; -8.831250507929241e-5 -2.9294346788481416e-5 -0.001648513571184649; 2.4871204796982852e-5 0.0004951529464734775 -0.0005264342602982917; -0.00018289838612690668 0.0006747493233550854 -0.0008227935007041887; -0.00013128156762720004 -0.00043757537584653613 -0.00158793538920112; 0.0009140116338973811 0.0006358691021311003 0.0009334960710307442] %
+
+Mass Used: 72.57452218861226 kg
+Launch C3: 99.27972216205782 km²/s²
+||V∞_in||: 0.004454204836923168 km/s
diff --git a/archive/ES_0.5586060779124284 b/archive/ES_0.5586060779124284
new file mode 100644
index 0000000..7811ff5
--- /dev/null
+++ b/archive/ES_0.5586060779124284
@@ -0,0 +1,22 @@
+archive/ES_0.5586060779124284---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:21:39.599
+Launch V∞: [7.869197081229218, -5.766324910066236, 0.15407092185052634] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6569314506520709e-9, -2.0792191989068762e-11, -5.877674973810985e-10] km/s
+ V∞_out: [9.151450874838396e-10, -8.432213184805141e-10, -6.312260366897618e-10] km/s
+ time of flight: 1.8749577787424687e8 seconds
+ arrival date: 2030-04-23T18:31:16.599
+ thrust profile: [0.4495135366325253 0.0009390775330834469 -0.11470535728233892; 0.06356304405477682 0.039908794260055745 -0.07018441951667896; 0.03793854945237771 0.03899364746388548 -0.07738339218564406; 0.03840971835195292 0.052276368069237925 -0.11321844278693544; 0.02635905845020675 0.046032737813555456 -0.11013607241492425; 0.0184761388413525 0.03882761128814125 -0.10155638498586944; 0.012198514333304957 0.02974080757627175 -0.08365976169363325; 0.0078032865168009375 0.022094450316460578 -0.06768850117369767; 0.004523351326087076 0.009369374237272368 -0.026823866635531858; 0.0014324306322107206 0.005834324009273351 -0.021638194201553638; 0.00381183886318322 0.0010162144107901407 -0.008040905659886986; -0.0012054334976463364 0.005613579687454372 -0.0034441833972976618; -0.00019720461441078004 -1.0768013985489933e-5 -0.0004210612208211044; -0.003409433204553515 0.0018702960373244816 0.0003519334738869657; 2.921724403758116e-5 0.0003582712111109933 -0.002942291120000092; -0.0008888544226687589 -0.006440831559018976 0.002513821775083249; -0.0011294190881880506 0.00025437552389731766 -0.0007426859263850746; -0.0017233413792653125 0.0025077940617885927 -0.0007583576687248479; -0.010261138995643859 -0.009042280630483297 -0.006527075282875734; 0.001041520417158454 0.0017450381171901905 0.0041067108533980965] %
+
+Mass Used: 96.3824870274525 kg
+Launch C3: 95.19850352063669 km²/s²
+||V∞_in||: 1.7582163627908045e-9 km/s
diff --git a/archive/ES_0.5586111327064651 b/archive/ES_0.5586111327064651
new file mode 100644
index 0000000..3a04da3
--- /dev/null
+++ b/archive/ES_0.5586111327064651
@@ -0,0 +1,22 @@
+archive/ES_0.5586111327064651---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T06:42:20.760
+Launch V∞: [8.13793147403687, -5.654472016475777, 0.14042984744458714] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.096585873983077e-6, 7.054130711935255e-5, 1.2603781097502047e-6] km/s
+ V∞_out: [6.764911752799155e-5, -1.0120381627999836e-5, 1.778244558103774e-5] km/s
+ time of flight: 1.8598698576090127e8 seconds
+ arrival date: 2030-04-05T21:45:25.760
+ thrust profile: [0.23839562979704212 -0.005272501608167607 -0.08288445147975164; 0.028778689558376928 0.015170447868288667 -0.03480115639568807; 0.03845451473875269 0.03240036569534326 -0.08366756015786637; 0.028684227231290348 0.031190375058000926 -0.09168794022939174; 0.02593761402355531 0.03382296813469767 -0.11045667044702494; 0.011154763702239851 0.016542956004874466 -0.05961266312467192; 0.025812041397534347 0.04434828949535225 -0.1656777202151882; 0.00835511558096657 0.015477134140394555 -0.0635519772916384; 0.005450049861133666 0.01100229816713158 -0.049157441203087085; 0.0034297228431824636 0.007097443976602405 -0.032996229389576574; 0.0005389302431742123 0.0013597029126672525 -0.005322665989408339; 0.0008111508802348051 -0.002769745284621523 -0.002457129690651072; -0.00046217541593983943 0.0009731475225605117 -0.003031605954839356; -0.00025557468896029827 0.0013253893556965358 -0.003664563708469271; -0.0003922575959024732 -0.004116008648756567 -0.008967322872064186; -0.0027393563271108185 -0.0009649838119566052 -0.00249490913801681; -0.006140016740805334 0.004797453735628881 -0.0014528160940390463; 0.0010614740337726246 -0.000188099164426004 0.0009406546492228525; 0.008362840666160012 -0.0006977913352678829 0.0007383695938575259; -0.009813403829420071 0.0042356472498022045 -0.00492558264428898] %
+
+Mass Used: 78.77055397173763 kg
+Launch C3: 98.21870300328087 km²/s²
+||V∞_in||: 7.062048857917444e-5 km/s
diff --git a/archive/ES_0.5586202116931135 b/archive/ES_0.5586202116931135
new file mode 100644
index 0000000..630e8aa
--- /dev/null
+++ b/archive/ES_0.5586202116931135
@@ -0,0 +1,22 @@
+archive/ES_0.5586202116931135---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T11:53:12.527
+Launch V∞: [8.02073907573326, -5.727674751791698, 0.13757663491616887] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.869008743302532e-5, -3.161461475176141e-5, -2.551455587137972e-5] km/s
+ V∞_out: [-4.870140331528554e-6, 3.5967315088922696e-5, -4.2705216737593014e-5] km/s
+ time of flight: 1.8233548898947784e8 seconds
+ arrival date: 2030-02-20T20:38:00.527
+ thrust profile: [0.3040470657478295 -0.016747547170641527 -0.1019174569813772; 0.03752795323181071 0.01835903360756266 -0.04392491555226821; 0.04546855657972723 0.036552272350450304 -0.0942257742110924; 0.04946192627771061 0.05145085341678835 -0.14730069509865548; 0.03815680034242113 0.047543343258360314 -0.15093379825999317; 0.024292427122517075 0.034900598535708434 -0.12190957619235449; 0.009135433255222064 0.014256777469789489 -0.05565785298672905; 0.0019272521173059115 0.0032802304012299575 -0.015701483848062983; 0.0049004216213168455 0.01096273017865989 -0.044194441410618714; 0.002129652293531386 0.006230420886809377 -0.030098402362619958; 0.0011746691679984903 0.003935027944136591 -0.01819257479674364; 0.0012562970684026598 0.0023197953598742414 -0.012420379161298813; 0.0008463413133335645 0.00297517688466667 -0.0040231002298680915; 0.004328610308833746 0.004887438503166417 -0.006369879386650576; 0.00026427914400539666 -0.00023765670249498074 -0.005264787245798467; 0.003914077956163553 -0.0017366201823977227 -0.00010391150323592465; -0.0011205584053170718 -0.004659651405494927 -0.005150703770086035; -0.001203461925251715 0.003623522326023019 -0.0037408738971982537; 7.942819537221763e-6 0.001286601913508997 0.00011158300231716659; 0.000134154705015509 -0.0008695218399213622 0.002338518961893655] %
+
+Mass Used: 84.97184281157433 kg
+Launch C3: 97.15744071378138 km²/s²
+||V∞_in||: 5.610168707615834e-5 km/s
diff --git a/archive/ES_0.5586208214620029 b/archive/ES_0.5586208214620029
new file mode 100644
index 0000000..6527db4
--- /dev/null
+++ b/archive/ES_0.5586208214620029
@@ -0,0 +1,22 @@
+archive/ES_0.5586208214620029---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T19:15:57.836
+Launch V∞: [8.100229922423306, -5.634753906988842, 0.130479501426792] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0011291627945462844, 0.000646248288069691, 4.888413149628452e-5] km/s
+ V∞_out: [-0.0009242618916395169, -0.0005506481616420763, 0.0007205867597639019] km/s
+ time of flight: 1.851872230714554e8 seconds
+ arrival date: 2030-03-25T04:09:40.836
+ thrust profile: [0.23205661226814683 0.004598532401932398 -0.06485585865193512; 0.08666192062342028 0.055847155473951055 -0.08806402451514747; 0.05838683380429052 0.06219769300549162 -0.10722189884987356; 0.039895420260873164 0.05743754547991262 -0.11060580099076577; 0.030988931045742824 0.05894331436624714 -0.1249607724066645; 0.02335773936734141 0.05473336220919971 -0.1264941536722735; 0.008799456412998247 0.023923220909605223 -0.060341804938178346; 0.004747083470868185 0.015242674839860741 -0.04086221103111075; 0.005126254876684573 0.019670340894658505 -0.05603350647854012; 0.0006322149702079798 0.002818315081531084 -0.007292578643900588; 0.0005373197856082981 0.0018009330974766255 -0.0061805568579336705; 4.67153060905712e-5 0.0006668576665123098 -0.0019911665156292324; 0.0004252645696872198 0.0005822863058131795 -0.0008521629929608632; 0.00011605282235914484 0.0016358944912472277 -0.001269272311520665; -0.0003901037857195966 0.001130368214079398 -0.0001662717091013299; -0.0007429841032624795 2.971768165165717e-5 -0.0020121292139729813; -0.0006239357451718001 -0.0006230571898916887 -0.0060367721055648695; -1.1929162475872532e-5 0.000574805520277797 -0.001949104624182883; 0.0006929759679547006 -0.00268224624708475 -0.004782355269863396; 0.0016157262274176182 -0.0014428572674326837 0.002339809123146132] %
+
+Mass Used: 83.66728418801722 kg
+Launch C3: 97.38120128874048 km²/s²
+||V∞_in||: 0.001301935146131606 km/s
diff --git a/archive/ES_0.5586539852688239 b/archive/ES_0.5586539852688239
new file mode 100644
index 0000000..15fd95f
--- /dev/null
+++ b/archive/ES_0.5586539852688239
@@ -0,0 +1,22 @@
+archive/ES_0.5586539852688239---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:36:46.207
+Launch V∞: [7.671044187672711, -5.802989844069069, 0.14860268211028393] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007137942234052485, 0.0004991231457277686, 0.03358029264277876] km/s
+ V∞_out: [-0.031069518635101562, -0.011365994899507962, 0.005712827964287216] km/s
+ time of flight: 1.8005494000818858e8 seconds
+ arrival date: 2030-01-23T02:52:26.207
+ thrust profile: [0.5865211983275639 -0.03137452233153673 -0.17968226901901202; 0.20459048064614022 0.10690196195385612 -0.21435456760413601; 0.05318311492323662 0.044576231398419375 -0.10483414931170457; 0.04755953274556988 0.05279342120805165 -0.13695217130335582; 0.032612696234593515 0.044275630222102395 -0.12619602460316387; 0.022034189656455556 0.03475771175042785 -0.1073424091612227; 0.006773910204728074 0.01171131393973844 -0.03909992736276186; 0.003125520414800308 0.00632355489795137 -0.022622682669659378; 0.0011739768027736247 0.0027549921273992226 -0.010708339708158723; 0.0002709339738900622 0.0008847785579798304 -0.004151735767099365; -0.00023495191362875377 -4.7402366709444756e-5 -0.001681779128565098; 0.000215638497004045 0.0001834513666178337 -0.0008768811250519342; -0.00013826095215523055 0.00046896123317666835 -0.0026424864090688984; 0.0004830937122822612 0.0006806993252863453 -0.0027318164625949495; -9.960274500498312e-5 0.0007118894305741771 -0.0017432115720973356; -3.868693761040123e-5 0.00021623541372634274 -0.0006366499975960841; 0.0005752649205545702 0.0016326104903974419 -0.00172213757671583; 0.0006957536907825045 -0.0019664854974371653 -0.002044651724953627; -0.000120155590091045 0.00022126600435928655 -0.0007846969620483794; 0.00021013860021420731 0.0002401509026176015 -0.0020129107431222162] %
+
+Mass Used: 111.93644138272384 kg
+Launch C3: 92.54169281672641 km²/s²
+||V∞_in||: 0.03359158644783882 km/s
diff --git a/archive/ES_0.5586546490119624 b/archive/ES_0.5586546490119624
new file mode 100644
index 0000000..0f28bfc
--- /dev/null
+++ b/archive/ES_0.5586546490119624
@@ -0,0 +1,22 @@
+archive/ES_0.5586546490119624---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T08:33:09.646
+Launch V∞: [7.8252310649201, -5.655430657089764, 0.16089886998828223] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7346920528621014e-5, 1.5496897357637608e-5, -1.1280148107513118e-5] km/s
+ V∞_out: [3.3813144494120078e-6, 2.557200681277749e-5, -1.1836736237751219e-6] km/s
+ time of flight: 1.8449482911314738e8 seconds
+ arrival date: 2030-03-16T17:06:58.646
+ thrust profile: [0.5852041983306665 -0.010154136383474024 -0.16994415436994445; 0.0752442810528456 0.042138449719093585 -0.08194972027138474; 0.10867397337200951 0.09846770008054709 -0.20639589665738006; 0.03492967845197824 0.04281333882469416 -0.10295133342044267; 0.03865122920892918 0.05822336088853159 -0.15080285812865696; 0.0070066870207543255 0.012631500864822518 -0.04040149998076588; 0.004366961916034835 0.009682246741536733 -0.03252982399113449; 0.003974216964068528 0.009511859049729517 -0.030818872826244383; 0.0026086134409493283 0.008889770916355939 -0.03100304380149146; 0.0028202136615296685 0.0033686300261593196 -0.013638620526465504; 0.001634070320055578 0.004157661507622914 -0.014169354360329916; 0.0020019855965575793 -0.0004388185538466169 -0.0017584677066860835; 0.001196163482924315 -0.0012432272221394875 -0.0027434943630678483; 0.005966324681240226 0.003214616595291149 0.0010516423263516245; 0.000550286518612927 0.0018972366257035598 -0.005439871862111253; -1.5837036509495315e-5 6.903720916868203e-5 -0.0009222392986482824; -0.001643833651156125 -0.0034193793872699637 0.0006634137834693914; -0.000450209591687809 0.00023506331189560243 -0.0010102549584748224; -0.001195773432235228 -0.003664890224724234 -0.0005487403116002665; -3.2384791936574824e-5 -0.001786737006564809 0.0032437450599489643] %
+
+Mass Used: 107.84027461367805 kg
+Launch C3: 93.24402558290483 km²/s²
+||V∞_in||: 2.58517160139686e-5 km/s
diff --git a/archive/ES_0.5586655086733114 b/archive/ES_0.5586655086733114
new file mode 100644
index 0000000..d6e0a2e
--- /dev/null
+++ b/archive/ES_0.5586655086733114
@@ -0,0 +1,22 @@
+archive/ES_0.5586655086733114---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:05:15.014
+Launch V∞: [7.969977116270676, -5.701107896541114, 0.10089481850744492] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8141298673312896e-9, -3.5267691706134798e-9, -1.09983348802602e-9] km/s
+ V∞_out: [-5.695409755120194e-10, -1.042820259413411e-9, -5.328893017499418e-11] km/s
+ time of flight: 1.839527272144261e8 seconds
+ arrival date: 2030-03-11T05:04:02.014
+ thrust profile: [0.3687768248338884 -0.004720745783986622 -0.1041289498412877; 0.07006234880088298 0.04104334416072016 -0.07665239604722121; 0.04296025366167338 0.04242279490135187 -0.08211682933488676; 0.03195816829043173 0.0439849141067128 -0.09600799048469168; 0.044743100561702255 0.06872392585606978 -0.16293534447196034; 0.01854831454036515 0.035858464770638025 -0.09434591153158337; 0.012707347605593543 0.028748132408620546 -0.08096290315515063; 0.0066983686107732095 0.017410670582969766 -0.05180477286452883; 0.003334465963029601 0.01040008761153573 -0.030831271183791628; 0.002306541614665746 0.009931050168873497 -0.033636023905756374; 0.0024586497005587506 0.000805100458007438 -0.01040077709792639; 0.00048426869658482806 0.002955837087004646 -0.004326386504004409; -0.0008613166106316203 0.0021459441380270033 -0.005079440606410674; 0.0006878539980277193 -0.00038019557270135764 -0.004215996382037688; 0.00044617882381515686 0.00037404730477498375 0.0021054951784229953; -1.5171996522256404e-5 -0.0015367364432596381 0.0008232098918527844; 0.002603725867549796 0.0009546747769050574 -0.010274907538670473; 0.0005987882787445446 0.0004236481749197511 -0.0014012550057621379; -0.0017873720613397963 -0.0021856190125770763 -0.0024063418087204337; -0.0022876430655850303 -0.0010307962256099982 -0.0008229776883952082] %
+
+Mass Used: 91.58190701554395 kg
+Launch C3: 96.03334624628333 km²/s²
+||V∞_in||: 4.1156775456438055e-9 km/s
diff --git a/archive/ES_0.5586720632871995 b/archive/ES_0.5586720632871995
new file mode 100644
index 0000000..3c56e49
--- /dev/null
+++ b/archive/ES_0.5586720632871995
@@ -0,0 +1,22 @@
+archive/ES_0.5586720632871995---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:10:58.393
+Launch V∞: [7.9653758780667445, -5.824695755090763, -0.285895363064297] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1808159646697628e-6, 1.0449283193755218e-6, -7.342774538662169e-7] km/s
+ V∞_out: [2.2520972115684182e-7, 1.7142789622196587e-6, -8.163606007539498e-8] km/s
+ time of flight: 1.8539802786655682e8 seconds
+ arrival date: 2030-03-30T14:38:05.393
+ thrust profile: [0.2689774202358437 -0.0013608400525846574 -0.08405707479142882; 0.05783602425768303 0.03414932643143678 -0.06928369619226177; 0.036439434222372176 0.03536901574790501 -0.0783624817451575; 0.029567975560701867 0.0375998669122696 -0.09458201736889042; 0.044727636539814465 0.0677561787294254 -0.1803241445613722; 0.010841509154692118 0.02275368502146639 -0.07174793918254249; 0.010031617343785118 0.02280087357632486 -0.06973851504158866; 0.006292106166172296 0.01713361174543219 -0.05792523774567408; 0.0066614426980429785 0.01636300642964886 -0.06028680086338033; 0.001830262811562556 0.008935369227041587 -0.03291709297686496; 0.0008322165038630396 0.0038422578811002804 -0.014512268029742136; 0.0005853165493269359 0.0005034677592948426 -0.0023330999528217776; -1.1515444237023714e-7 0.0006101776837932264 -0.0003663087797463266; 4.978272702262897e-5 -0.0006911063147929913 0.001086767740704589; -0.003105481743131964 0.0034215692610577563 -0.0026906395742861797; -0.00016681184523800784 -0.00026543421577593374 -0.0008670857359510903; 0.0029607415007997114 -2.844022634799901e-5 0.0013028294273197385; -0.0038898311770512966 0.0015877640788545758 -0.002154483001706308; 0.0020095546209404048 -0.005171855076133478 0.0004350812803642275; 0.0027951352119346415 -0.004413443439820266 0.002299824564539357] %
+
+Mass Used: 83.29056738659028 kg
+Launch C3: 97.45602967688158 km²/s²
+||V∞_in||: 1.7393576154167346e-6 km/s
diff --git a/archive/ES_0.5586873593381654 b/archive/ES_0.5586873593381654
new file mode 100644
index 0000000..713ee1e
--- /dev/null
+++ b/archive/ES_0.5586873593381654
@@ -0,0 +1,22 @@
+archive/ES_0.5586873593381654---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T20:46:23.173
+Launch V∞: [7.955726414434782, -5.566462200244662, 0.2397723403489861] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.646926608189835e-7, 2.6899834525178524e-6, -5.547487230724731e-5] km/s
+ V∞_out: [-2.05873172810824e-6, 5.547128200330183e-5, -5.971052412335821e-7] km/s
+ time of flight: 1.874957778748474e8 seconds
+ arrival date: 2030-04-20T22:56:00.173
+ thrust profile: [0.5171491552986296 0.008436152898796397 -0.13430458184630453; 0.055771999871542084 0.03661176202177402 -0.05617054620276673; 0.06937768566546719 0.07529025906397341 -0.12588316829441998; 0.026923919856326316 0.0403455858245523 -0.07679289392948369; 0.016732805823938966 0.03184104136902151 -0.06687898345712912; 0.037679913241064004 0.08154522640323617 -0.15408816820193613; 0.005996347301969908 0.017095634617839934 -0.04293084199091381; 0.009073572099276322 0.028271918751516 -0.07141776269947049; 0.004363049718348303 0.020152080979534522 -0.05296316580267582; 0.0012080867178032252 0.003718668593562351 -0.00998363626770835; 0.0002571045604735988 0.005938122600096499 -0.01664152376227132; 0.0006920465345117503 4.768413009621124e-6 -0.0009954026016270002; -5.982826769216647e-5 0.0006680122841174015 -0.0015988634705020124; 0.001486246029451647 0.00016936921219783978 0.00018628537989361072; -0.0018016425165655386 0.0014772669848239506 -0.00041861408622335516; 0.0024918241674443398 -0.0001341757818710081 -0.0013311630370400102; -0.0028957896991754395 0.0009044701352139831 0.0012880434093359068; -0.0032659575708137174 0.002621551143763045 -0.0008140125210983183; -0.000903321338774354 -0.0007261700722765666 0.0027687829856738637; 0.0008233179900363434 -0.00010030905160897708 -0.0009078404618981116] %
+
+Mass Used: 101.50523182536745 kg
+Launch C3: 94.33657498328438 km²/s²
+||V∞_in||: 5.554125015893205e-5 km/s
diff --git a/archive/ES_0.5586995986951158 b/archive/ES_0.5586995986951158
new file mode 100644
index 0000000..3611a40
--- /dev/null
+++ b/archive/ES_0.5586995986951158
@@ -0,0 +1,22 @@
+archive/ES_0.5586995986951158---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T17:37:04.055
+Launch V∞: [8.138296422993552, -5.69781711392224, -0.1507728988280994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.016528539051392257, 0.10286458301258379, 0.10579245120115] km/s
+ V∞_out: [-0.025726343993842934, 0.024195511005251143, -0.14229124807352342] km/s
+ time of flight: 1.8749577786806974e8 seconds
+ arrival date: 2030-04-24T19:46:41.055
+ thrust profile: [0.20318612667422659 -0.003406962416817689 -0.07342141527117159; 0.026326806877041795 0.013577087914948122 -0.032712358776862516; 0.026604917420179043 0.0219420196678246 -0.060148088187410194; 0.03246767356973338 0.034375581661159595 -0.10560843453191618; 0.02615967137513783 0.03326132883487845 -0.11260934963071996; 0.038400062518451544 0.057941022315234465 -0.21272630154592004; 0.007666665512582307 0.012022977686777946 -0.05209831086367285; 0.0027766037762687458 0.0045473546773341375 -0.020952625059426223; 0.006000933939981697 0.011534567875066619 -0.05271953984849967; 0.002422892331738758 0.00437990025877645 -0.021546241199146162; -0.0020808740406805647 0.0016811226281306807 -0.016445406688058602; 0.0032711050854094563 0.0011096674255090305 0.0012484317954761983; -0.0012919717024108147 -0.002324249164261215 -0.00373334330927789; 0.0032208615554467812 0.00738548351543455 -0.0021893990535976782; -0.00027555367394707653 0.0015611647737353608 -0.008271258352478206; 0.00028435905473567956 0.0019348254299285821 -0.0025685097521686087; 0.004055531916526625 -0.000851857636320577 -0.007270862992814546; -0.005360928288387121 -0.007736064466860617 0.0003179815727789286; -0.006642089107113936 -0.0026077410238618693 0.00735020433837499; 0.0028562510618011204 -0.000801995484938083 1.1802958755351145e-5] %
+
+Mass Used: 75.95115931542614 kg
+Launch C3: 98.71972099923583 km²/s²
+||V∞_in||: 0.14848015952535154 km/s
diff --git a/archive/ES_0.558701862471938 b/archive/ES_0.558701862471938
new file mode 100644
index 0000000..0d44f8a
--- /dev/null
+++ b/archive/ES_0.558701862471938
@@ -0,0 +1,22 @@
+archive/ES_0.558701862471938---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T00:00:28.594
+Launch V∞: [8.0754668906268, -5.636333968484601, 0.1402806649331551] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5408556829617355e-9, -1.5515904900370529e-9, -1.4445070056198186e-9] km/s
+ V∞_out: [6.578451815562285e-11, -5.97343056490628e-10, 7.377175533945727e-11] km/s
+ time of flight: 1.8749577788777578e8 seconds
+ arrival date: 2030-04-23T02:10:05.594
+ thrust profile: [0.3135439425595627 0.004420084615840651 -0.09312483814952104; 0.05838374878548017 0.03689620875271934 -0.06847640210562374; 0.02796496726866946 0.029427081724782554 -0.06152966768885796; 0.036219419320411284 0.05312675992276213 -0.12078426463377297; 0.017281017401649983 0.028991629678455748 -0.0754617227452703; 0.0075079822385893955 0.015055990092712518 -0.045539301881337646; 0.010877903181708625 0.024418443281808266 -0.0722099950032776; 0.01941845098964724 0.054038302975506526 -0.15632497246512694; 0.005678583886191217 0.018775967114698092 -0.0646375632615347; 0.0017521978964704973 0.005140538753022506 -0.022318575002308084; 0.0007330166511982227 0.0022894792774171757 -0.011657059490971663; 0.0003844110850582444 0.002084175537289484 -0.00773692772424385; 0.0013028448367216122 -0.00010180424237028057 0.00019590082822141803; -0.0004989921171779033 0.00262900082491816 0.0017487352257359754; -0.0019675282637246615 0.0030636804276982163 0.001300957619064496; -0.0015048396286365892 -0.0029808883105994404 0.0004541423563207978; -0.0018499405917138554 0.005818765731515111 0.0035715937107509282; -0.0001514804424470039 1.3975998427308631e-5 -0.0005836196688823502; -0.001610326981843362 0.0005103951620679327 0.002383706086235613; 0.00039289058643365447 -0.0075486958121279025 0.0051759533850211335] %
+
+Mass Used: 85.97906172059447 kg
+Launch C3: 97.00110477085713 km²/s²
+||V∞_in||: 2.6207384023922784e-9 km/s
diff --git a/archive/ES_0.558711582866176 b/archive/ES_0.558711582866176
new file mode 100644
index 0000000..c08bf15
--- /dev/null
+++ b/archive/ES_0.558711582866176
@@ -0,0 +1,22 @@
+archive/ES_0.558711582866176---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T07:34:46.041
+Launch V∞: [7.968296745643684, -5.666291125309124, -0.0007466171110208315] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00013381913255957896, 0.00010029445369738057, 0.006693581572650291] km/s
+ V∞_out: [-0.005944881249746429, -0.0020975196736489434, 0.0022425175769304126] km/s
+ time of flight: 1.8489716688079086e8 seconds
+ arrival date: 2030-03-22T07:54:12.041
+ thrust profile: [0.39785143252275984 -0.0027289509914422273 -0.12447537213218395; 0.0793787284014512 0.04632827660658573 -0.08929824213785859; 0.0628534864616092 0.06023742455872421 -0.12744856477884534; 0.03083189304693497 0.038965201643551106 -0.09479389763252205; 0.03458390709343804 0.054708743221292475 -0.14206798435236634; 0.012534792759239174 0.022724747296073978 -0.06723866032639314; 0.009855084011141487 0.020589023134323422 -0.06411223037743122; 0.00504302509964534 0.012096299859676063 -0.041957238599110054; 0.005306568490892055 0.014385984813502145 -0.04656842668545516; 0.002409710074927079 0.00821027233434992 -0.030727269019200868; 0.0011760943471080735 0.0036090931268321514 -0.015230911813118418; 0.0016345051926716027 0.000998224998081913 -0.007327725857003281; -0.000993297048708169 0.0014492596345972327 0.00011762067943660044; 0.0005260712564099938 0.0003447616691541395 -0.0031956226010387127; 3.750977809328904e-5 0.0006920428717109598 -0.0030855713477183143; 0.00018560069180413634 0.004669047418760183 0.003886043807527003; -0.00021684090367480105 -0.0011127413853496224 -0.0003625385700688397; -0.0004324887608230663 0.0026331169673181574 -0.0012478853387147871; 0.0045723666372089996 0.0021250475535799784 -0.007603194476365834; -0.0002463232560336963 0.00014259233008544257 0.000546481154556218] %
+
+Mass Used: 94.1599625890317 kg
+Launch C3: 95.60060870082977 km²/s²
+||V∞_in||: 0.006695670303069365 km/s
diff --git a/archive/ES_0.5587165689306142 b/archive/ES_0.5587165689306142
new file mode 100644
index 0000000..9fe2478
--- /dev/null
+++ b/archive/ES_0.5587165689306142
@@ -0,0 +1,22 @@
+archive/ES_0.5587165689306142---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T21:25:40.777
+Launch V∞: [7.962126767333948, -5.981068164263589, -0.017246855167084994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.510124853846178e-8, 8.36190984157894e-8, 2.408766562031707e-7] km/s
+ V∞_out: [2.515451066415335e-7, 3.107738982650985e-8, -1.1052914589995417e-7] km/s
+ time of flight: 1.824744382494759e8 seconds
+ arrival date: 2030-02-25T20:46:18.777
+ thrust profile: [0.16708547280994804 -0.009383487181469311 -0.06273383741317942; 0.021877347897553096 0.009640692992556859 -0.028274473349073466; 0.03771248359283781 0.026392545800942382 -0.08440310744112256; 0.04867092365881285 0.04417994433043837 -0.15514907341625286; 0.035617189240063477 0.03698492131833689 -0.14877927636533333; 0.023525054919038262 0.027422117549481616 -0.11914060427970372; 0.013263187511066539 0.01644023116177449 -0.08044540693464007; 0.007411874140434877 0.009753347746324909 -0.05230955507974693; 0.005295619625149243 0.0077558184733821575 -0.04444101042438704; 0.002079190523564848 0.0014833363392201307 -0.0066153349395874535; 0.0014009894917699469 0.002344723584101051 -0.011617303705625158; 0.0026084295419736346 -8.562229544104889e-5 -0.005173384435394277; 0.0002489900099434218 7.643189861527807e-5 -0.001668979248707135; 0.0036912853783519946 0.0006388932495326765 -0.005420990749281675; 0.0009438343685808218 -0.0032229785442126303 -0.005401528451149691; 0.0045986186728002865 0.0028468009191685343 -0.011984415624200533; 0.0011664052254338358 0.0039818035236003375 -0.005409393952681596; -0.0004932111231867232 -0.0012347022575658125 -0.001948887202202629; 0.00021192064360095746 0.00024420213707021044 -0.0019677331856254084; -0.00023377761493431723 -0.001081725050224614 -0.0002590450480295745] %
+
+Mass Used: 73.35053417677136 kg
+Launch C3: 99.16893649867632 km²/s²
+||V∞_in||: 2.5621044046189765e-7 km/s
diff --git a/archive/ES_0.5587191421323559 b/archive/ES_0.5587191421323559
new file mode 100644
index 0000000..12542c9
--- /dev/null
+++ b/archive/ES_0.5587191421323559
@@ -0,0 +1,22 @@
+archive/ES_0.5587191421323559---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T00:14:40.888
+Launch V∞: [8.07191402113441, -5.888797477470527, -0.019099030706463307] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.957695134834066e-7, -7.689786263791185e-7, 5.600513473800032e-7] km/s
+ V∞_out: [-1.712693786911562e-7, -1.291076014492157e-6, 6.314821266572805e-8] km/s
+ time of flight: 1.858948967013069e8 seconds
+ arrival date: 2030-04-07T13:42:56.888
+ thrust profile: [0.120174954832482 -0.006136502430901625 -0.04365805562401687; 0.03647939128338108 0.017474114141270904 -0.047799012567287816; 0.041555940352619974 0.0292968682046251 -0.09184299542894553; 0.020102496443651544 0.018432173892449475 -0.06738897202284576; 0.03215206765381304 0.02985672801626768 -0.12837921096610447; 0.022806811631121002 0.023688098078874075 -0.11312963774140068; 0.008584495180483223 0.011995680986813403 -0.0578203661147515; 0.004998530987433279 0.006872138911970093 -0.03731730098861223; 0.019084291354259708 0.04178568292999783 -0.14967740952062197; 0.0005423599114201906 0.0018013846027746376 -0.008558021805671136; 0.0022185150926685086 0.0037009318760669067 -0.025818360324876163; 0.0012426685508656198 0.0005593507393509163 -0.006957010432191566; 0.0012345947187352507 0.0013492289100300926 -0.003086939517595578; -0.0014440635356215304 0.0018973597317149533 -0.0015340501152172174; 0.001632881112015124 -0.0004794309145654313 -0.0003965701317983489; -0.000694897252692399 0.0018263663054661325 -0.00202580569275726; 0.001147149691543121 0.0009236874016698694 -0.00235942912998855; -0.003093126807422534 0.0014638147538828862 0.0008898950678258069; -0.0006719956971232249 0.0003694193148799925 0.0023379444773690607; 4.576582517709879e-5 0.0003886815381447771 0.0002607894079589599] %
+
+Mass Used: 69.4734364231117 kg
+Launch C3: 99.83409646822345 km²/s²
+||V∞_in||: 1.306670831088064e-6 km/s
diff --git a/archive/ES_0.5587199593773109 b/archive/ES_0.5587199593773109
new file mode 100644
index 0000000..3b1f9e8
--- /dev/null
+++ b/archive/ES_0.5587199593773109
@@ -0,0 +1,22 @@
+archive/ES_0.5587199593773109---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T01:41:30.416
+Launch V∞: [7.565812903949794, -5.940407824187746, 0.028617729545849024] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00024412979782694865, -0.00019875332121081622, -0.00016578847083511625] km/s
+ V∞_out: [-3.534383916194474e-5, 0.0002217976487915621, -0.00027507763847841986] km/s
+ time of flight: 1.8540233206889987e8 seconds
+ arrival date: 2030-03-29T22:20:22.416
+ thrust profile: [0.5982177269354307 0.0056748187022684065 -0.16845604326454242; 0.1664312374095709 0.10002404501515162 -0.17006830888883964; 0.05278958320979118 0.051286386808336935 -0.10276507146864626; 0.04710138501306585 0.06169184924025577 -0.1360143015309248; 0.031718714944501535 0.051582254318170276 -0.12588729436503826; 0.012033906654512622 0.02332164968328359 -0.06409683435800292; 0.009119256836362296 0.020058575990145575 -0.0577459769922098; 0.004128087139752802 0.01151245887139821 -0.034284087828072296; 0.00043847439526424836 0.0016876510579877852 -0.006054983543550661; 0.0012065281453279837 0.0010519907043614913 -0.0024741137662263176; 0.0003112402943840093 0.001126265301584001 -0.002864593064564292; -0.0015569023392716845 -0.001608131868653303 -0.0038980875070938103; 0.0008633367958258623 0.002585776255155346 -0.0004396483308994484; 0.001624434194870437 0.000131294362031019 -0.004041891223628885; -0.0020657763012795743 0.001109715936295498 -0.0027008019806173773; 0.00017491161687749356 0.0011510498592219019 -0.004826022853802063; 0.002771714695851585 0.004888745178745769 -0.004675122731148756; 0.0001533439022232077 -0.002061321526192954 -0.002461900941259724; 0.0006476747056970188 0.0007276711892223941 0.0027265400623846937; 0.0016846208646642091 -5.850225933004037e-5 -0.001732647401004721] %
+
+Mass Used: 112.07701683367941 kg
+Launch C3: 92.53078898968856 km²/s²
+||V∞_in||: 0.0003557921555363509 km/s
diff --git a/archive/ES_0.558720927129951 b/archive/ES_0.558720927129951
new file mode 100644
index 0000000..0825327
--- /dev/null
+++ b/archive/ES_0.558720927129951
@@ -0,0 +1,22 @@
+archive/ES_0.558720927129951---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T09:05:32.470
+Launch V∞: [7.8134164609221, -5.85269820646695, -0.06322862405226795] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0771734186284035e-5, -7.87140502821809e-6, 6.554758017438998e-6] km/s
+ V∞_out: [-2.2485345884861785e-6, -1.467533762524075e-5, 7.292225649454396e-7] km/s
+ time of flight: 1.8749577787511733e8 seconds
+ arrival date: 2030-04-23T11:15:09.470
+ thrust profile: [0.31927801601151967 0.011410950340326005 -0.08927585011409161; 0.1793343868417437 0.12077545196356462 -0.1727057622509466; 0.06494999748041524 0.07108932602130129 -0.1203816350277851; 0.03243296811281488 0.0477362426748705 -0.09198268423534982; 0.039084416679837815 0.07329343834936775 -0.14990979542706165; 0.013783238699675043 0.032824088416112916 -0.07560288953465592; 0.008670833611231195 0.024193425071975503 -0.06065788209108842; 0.004845457700311455 0.015309082086784286 -0.040295964926174724; 0.0007588393591442957 0.0028138833673948785 -0.00797928458872517; 0.0004558023946902994 0.000772654687778807 -0.0026950447032823175; 0.0008371724412927295 0.00038820134976949366 -0.0023102635138880106; -0.0023210658554924345 0.00010232802541012415 -0.001376819438257972; 0.00030772296050140657 0.00041103002124591274 -0.0008835113510354559; 0.0009462524352417071 -0.0011708764021018325 -0.001151202510266864; -3.687691630696816e-5 0.0008998971313294128 -0.0029779376089473196; 0.0023288444972413315 -0.0008131996906574511 0.0014387122570800066; 0.002022508524006584 -0.0015639566478404822 0.002602532667825461; 0.001529736018053009 0.0013261473115123218 0.002441803419787678; 0.0023639073877247145 -0.008069106142822675 0.00015200830224788332; -0.005469673875964341 0.0048194674571455974 0.0037852151455445137] %
+
+Mass Used: 95.8803677959213 kg
+Launch C3: 95.30755094668942 km²/s²
+||V∞_in||: 1.4864525796856018e-5 km/s
diff --git a/archive/ES_0.5587221734185861 b/archive/ES_0.5587221734185861
new file mode 100644
index 0000000..c3fd0ea
--- /dev/null
+++ b/archive/ES_0.5587221734185861
@@ -0,0 +1,22 @@
+archive/ES_0.5587221734185861---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:19:48.239
+Launch V∞: [7.697216136680507, -5.790055511671956, 0.27330608396400735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3027071852522255e-7, 1.6394561325215083e-6, -3.535891075924034e-5] km/s
+ V∞_out: [-1.485167297192224e-6, 3.5468909426019496e-5, -4.2051229063940335e-7] km/s
+ time of flight: 1.8255501307263255e8 seconds
+ arrival date: 2030-02-22T04:03:21.239
+ thrust profile: [0.6218256253357669 -0.005030172560280967 -0.1545241931415564; 0.09837131487742368 0.05960543305334933 -0.09706569618316513; 0.056727674449741264 0.056379316159757005 -0.10219755946166878; 0.038627034758544045 0.051632603673407995 -0.10447834059593686; 0.015655852864454336 0.026220443249891538 -0.05874766909362762; 0.017116995492910177 0.03420546791734909 -0.08127655528462739; 0.025896211395051796 0.05699956776077374 -0.14294267903372182; 0.007130730890043262 0.02027253837329818 -0.05667774576284353; 0.005917450707461054 0.014300490940986033 -0.04013496048423003; 0.0032665689253195216 0.012636272248153025 -0.03576211526180839; -8.603474387987417e-5 0.0005737383909297184 -0.001109106123741902; 0.00017348697257428257 0.0004762880405029651 -0.0018833049228426043; 0.00019683342176928127 0.0006849572486941132 -0.0025351756069930615; 0.00018023120984658053 0.0019085761744350768 -0.007049142064685676; 0.00046996173429554046 -0.00038930771309777525 -0.0006045773020606779; 5.829743908313998e-5 7.1605054957461e-5 -0.0005123518188043432; 8.770189515982884e-5 0.0006207203180848006 -0.0012000529848620216; -1.4868726750718301e-5 5.3008008253086885e-5 -8.986497636905314e-6; -3.909529225822869e-5 0.0003656881370920318 -0.00010415780784301092; -0.0025437455217541087 -0.0005162067436061648 5.886955398070714e-5] %
+
+Mass Used: 110.23751308014607 kg
+Launch C3: 92.84657529854933 km²/s²
+||V∞_in||: 3.539764697115042e-5 km/s
diff --git a/archive/ES_0.5587244390727587 b/archive/ES_0.5587244390727587
new file mode 100644
index 0000000..dd95393
--- /dev/null
+++ b/archive/ES_0.5587244390727587
@@ -0,0 +1,22 @@
+archive/ES_0.5587244390727587---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T19:47:51.434
+Launch V∞: [8.002465466164045, -5.657210104303127, -0.049991157893097] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8365538027891605e-5, 4.464798552024165e-5, 0.00012749580487371836] km/s
+ V∞_out: [0.00012496565202323583, 1.5355373717446117e-5, -5.313428018643216e-5] km/s
+ time of flight: 1.874957778742165e8 seconds
+ arrival date: 2030-04-21T21:57:28.434
+ thrust profile: [0.3004894903132625 0.01072022897804432 -0.0830834571603529; 0.13552126083888127 0.09156943191849345 -0.1321042525678859; 0.057542570930538404 0.06710771226592917 -0.11200531586709023; 0.026014451429757775 0.04025145413554136 -0.07594318477721428; 0.029993334974555072 0.054863573730748925 -0.11404144781421806; 0.016477809979247676 0.040170667321271725 -0.09011567956095516; 0.01207709910663128 0.04373721788704591 -0.09570158598364947; 0.004479641173877394 0.017251238820044413 -0.04522709515167066; 0.0016266428994519198 0.008837299202829153 -0.02261238856450601; 0.00015417741180126553 0.004181059071521284 -0.01109304539493355; 0.0012797172649453303 0.008923573800362091 -0.02563102150006355; 0.0015053441514855793 0.0006068334904067134 6.729581598813273e-5; -0.00034268107207830796 -0.002361156816246863 -0.0016270284725133299; 0.0022280794797543487 -0.001156491802525918 0.00012107363539965929; 5.233119600666148e-5 0.0002596229499650881 0.0008397813662767627; 0.0006456371337077129 -0.0004287075703536601 -0.0015644555891739186; -0.0021455228107371124 -0.0030318237656366846 -0.00081635682521392; -0.00014089048860417477 0.0013827996981448354 -0.0012734723396406163; -0.0011537714895161555 -0.0008941556101968022 0.000994870530997347; -0.006440361277445533 -2.0580468322232966e-5 0.0023109159486168367] %
+
+Mass Used: 91.57696915095585 kg
+Launch C3: 96.04597881724503 km²/s²
+||V∞_in||: 0.00013633017222341835 km/s
diff --git a/archive/ES_0.5587277033316588 b/archive/ES_0.5587277033316588
new file mode 100644
index 0000000..fa32eaa
--- /dev/null
+++ b/archive/ES_0.5587277033316588
@@ -0,0 +1,22 @@
+archive/ES_0.5587277033316588---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:37:54.562
+Launch V∞: [7.764546419027637, -5.9235852418461885, 0.3270437765400666] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.860815923445804e-10, -1.2395512105155305e-9, 5.752876460130583e-10] km/s
+ V∞_out: [4.700225522088963e-10, -1.4887110350926691e-9, 2.4654620638375435e-10] km/s
+ time of flight: 1.8593489626103568e8 seconds
+ arrival date: 2030-04-04T20:12:50.562
+ thrust profile: [0.33714013473651017 0.021037870094774338 -0.07533716536791689; 0.1382662878358586 0.09775603593391832 -0.11640946453880999; 0.039344023286603816 0.04522031909418114 -0.06585370921419387; 0.032307740864941474 0.05203085402444831 -0.08310547908648692; 0.047501564135628414 0.09993452695181454 -0.1592224600576338; 0.01606273148083701 0.04239889707882017 -0.07899832158942034; 0.013506517563040181 0.03899839734671459 -0.07580312803550791; 0.010724180456528815 0.041130997820595615 -0.08394945856853672; 0.0030512788444200896 0.01457416888970462 -0.03259719306742375; 0.0013740537177861069 0.007896460854177736 -0.01889954378904183; 0.00028940830513603895 0.0015165434277183572 -0.0032183149739248335; 0.0002793129738510313 3.324218236045134e-5 -0.0012643449548382748; -6.256151671311873e-5 -2.3325138341770478e-5 -0.0008581980241874758; 0.00015470680474397386 0.0009151759072957285 -0.0014290070521593135; -0.000164785441157203 0.0017142108456024807 -0.00028538336387558575; -0.0006351232381913798 0.0007397752502305654 -0.001166080932767388; -0.0007389400024149797 0.0005717076307196047 -9.400994746713203e-5; 0.0003600064457571734 -0.0008531028249867002 0.0010595576617056103; 0.0011018031521823973 0.0010673019347794445 0.0009162738569698; -0.0004690628854016914 -0.0006245699739450567 -4.8021492809162056e-5] %
+
+Mass Used: 94.85898230611429 kg
+Launch C3: 95.48400084242644 km²/s²
+||V∞_in||: 1.6851706103260247e-9 km/s
diff --git a/archive/ES_0.5587350625304599 b/archive/ES_0.5587350625304599
new file mode 100644
index 0000000..7900dfc
--- /dev/null
+++ b/archive/ES_0.5587350625304599
@@ -0,0 +1,22 @@
+archive/ES_0.5587350625304599---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T01:57:41.110
+Launch V∞: [8.00235731470902, -5.705343986870514, 0.10054220622999013] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9884502770460224e-7, -6.474098893816488e-7, -1.8897885624170874e-6] km/s
+ V∞_out: [-1.847440833869188e-6, -2.2564956352585673e-7, 7.846697599998949e-7] km/s
+ time of flight: 1.834341558544522e8 seconds
+ arrival date: 2030-03-05T03:53:36.110
+ thrust profile: [0.32144656687020107 -0.005686395454508751 -0.09768926654240323; 0.05981989307051661 0.03409034538755253 -0.06630192920684855; 0.06380400586530999 0.059211616725391755 -0.12433520315678165; 0.04937200231655414 0.06118881629534971 -0.14155311866377207; 0.02006630083413281 0.03217227544864284 -0.08312841311423073; 0.0190213523452368 0.034827390307998286 -0.09732796081582383; 0.014840551460754404 0.03437937196850779 -0.09817653488720686; 0.006889317591317258 0.017077518011741174 -0.056118174981050865; 0.002702165569387325 0.009334276932272257 -0.03357704807493624; 0.002814455387901626 0.009317642561045779 -0.034933983593578466; -3.9384469221349005e-5 0.00047224053263129244 -0.002437986212380226; -0.0023095755983701754 0.00015209433222707243 -0.0036799200895273557; -0.0011116834993707076 -0.0016855016361806967 -0.002829444352647104; -0.002964406725089305 -0.0008949397052070788 0.002461449076096603; -0.002062083707587533 0.0005188436076797558 0.002178648922654564; 9.640256825893196e-5 4.9601694270806726e-5 -0.00040269878714780717; -0.0015257940569766287 -0.0030891491767603 -0.002472201510480593; 0.002455245357668077 2.6599224678949267e-5 -0.0039660150910170635; 0.00017576440922466524 0.0007934219372700898 0.003965205638597732; -0.0011232695391028458 -0.0005878594584839152 -0.0015192817308430076] %
+
+Mass Used: 88.364681825361 kg
+Launch C3: 96.59878133603009 km²/s²
+||V∞_in||: 2.007480939026432e-6 km/s
diff --git a/archive/ES_0.5587391469107693 b/archive/ES_0.5587391469107693
new file mode 100644
index 0000000..6a9d6c0
--- /dev/null
+++ b/archive/ES_0.5587391469107693
@@ -0,0 +1,22 @@
+archive/ES_0.5587391469107693---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:52:16.224
+Launch V∞: [8.042390324475003, -5.679978382966862, 0.20627995417274878] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8375924923255244e-7, 2.227048853786632e-6, -4.688121868205233e-5] km/s
+ V∞_out: [-1.7293010586667214e-6, 4.741585896546342e-5, -4.843164082810143e-7] km/s
+ time of flight: 1.8215424187434998e8 seconds
+ arrival date: 2030-02-17T13:16:17.224
+ thrust profile: [0.28095388346232997 -0.011762083916596017 -0.08948478059711201; 0.10008576859781843 0.05306072130619436 -0.1103218646959829; 0.05866841153380244 0.05090580440904973 -0.1165332911698337; 0.04992189264579364 0.057093616402165086 -0.14537785904250886; 0.0192564917497604 0.02697083345213898 -0.0769673065924517; 0.0146599301904194 0.02385424207906706 -0.07328650986049755; 0.014762182986836203 0.027370483272716795 -0.09035092248537867; 0.009510781647334753 0.01876396980777254 -0.06702321143959361; 0.002370542626665603 0.005622222730973514 -0.02106122036893254; 0.006383117075924256 0.01625934497445729 -0.06290998375090859; 0.00014929737540589472 0.0010708222805475222 -0.0017993140475900454; 0.0007435510280058421 0.0004573619319388107 -0.0013697873041253993; -0.0001331974473472538 0.0005355097184053073 -0.0020402678556008247; -7.557766380286179e-6 0.0004008583715756002 -0.0006190989741944302; 0.0012546559613564798 -8.468583838851725e-5 -0.001234933619424498; 0.000551592046554838 -0.001227775714331196 0.0006594802894180219; 0.0003039223567267244 -0.0003210980277894488 -0.0006346525587296217; -0.0005222125155937994 -0.0017799655350481227 -0.0005454228110114972; -0.0009195190759278542 -0.0016262466395459082 0.00021841584942894056; 2.218993758851395e-5 3.824473743038711e-5 -0.0003741782602690025] %
+
+Mass Used: 86.11797483613555 kg
+Launch C3: 96.9847479816735 km²/s²
+||V∞_in||: 4.693494360306711e-5 km/s
diff --git a/archive/ES_0.558747142540957 b/archive/ES_0.558747142540957
new file mode 100644
index 0000000..7c311f7
--- /dev/null
+++ b/archive/ES_0.558747142540957
@@ -0,0 +1,22 @@
+archive/ES_0.558747142540957---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T18:22:45.232
+Launch V∞: [7.839591971331136, -5.798881381776378, 0.12161904484035195] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.464615039856191e-6, -3.3845543160721105e-6, -2.4144576133198526e-7] km/s
+ V∞_out: [2.969031295078514e-7, -1.440994156124623e-6, -3.928214963635209e-6] km/s
+ time of flight: 1.8749577787492132e8 seconds
+ arrival date: 2030-04-24T20:32:22.232
+ thrust profile: [0.4746916134302762 -0.007830418579170396 -0.1655008405888; 0.08839710536528597 0.04514410248799113 -0.10981878780553503; 0.03543550178852803 0.02854926285332808 -0.08089300989745424; 0.0374166149040405 0.03846188425612507 -0.12435758922073072; 0.02910251379035863 0.035460335598572944 -0.12890935723312374; 0.018930658867346198 0.026419544969654728 -0.10625359578697248; 0.01077847255258741 0.01691451040148772 -0.0743617412855498; 0.0028976793784204233 0.005450648905434844 -0.02650619544876367; 0.0008666395989332368 0.003026778546666032 -0.013157875596883823; 0.001346941988353472 0.002488354120525758 -0.011126199963225553; 2.5140583786240154e-5 4.010873695877077e-5 -0.0006233956564219308; 9.894634516989588e-5 0.0004331582992315652 -0.002358629502326991; 0.0021936008787873788 -0.002820817659484417 -0.00015513518665216403; -0.0003878874251069695 -0.001041150327902286 -0.0005228266936236994; 0.0034458673992765077 0.001211057452104499 0.004002967830400449; -0.0025332392140515877 -0.003239578668484735 0.0054891210355199165; 0.0013282982809335584 4.882762194875152e-5 0.004596313171795988; -0.004967852277245656 0.0028777481216330993 0.0013502841197603828; -7.231762043078771e-5 -0.0010988310619823053 0.002624495572946469; -0.008805602142604247 -0.005726347004246388 0.002944945232206522] %
+
+Mass Used: 97.11572359563206 kg
+Launch C3: 95.1010187489402 km²/s²
+||V∞_in||: 4.193784838161451e-6 km/s
diff --git a/archive/ES_0.5587474924398192 b/archive/ES_0.5587474924398192
new file mode 100644
index 0000000..abe46c9
--- /dev/null
+++ b/archive/ES_0.5587474924398192
@@ -0,0 +1,22 @@
+archive/ES_0.5587474924398192---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T00:25:27.963
+Launch V∞: [8.06760401100903, -5.53445082198219, 0.1917191500867182] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013547178210165585, -0.08713176020749772, -0.09846309683352489] km/s
+ V∞_out: [0.05594073145472333, -0.048280189530269996, 0.12157390262007788] km/s
+ time of flight: 1.8749577786951125e8 seconds
+ arrival date: 2030-04-22T02:35:04.963
+ thrust profile: [0.4463647986470767 0.0009304804157011568 -0.13008594480619706; 0.045010673265225086 0.026887384822647013 -0.05295099379416093; 0.031247285917309266 0.030139208383201034 -0.06650337260826142; 0.02655343895160451 0.03370479119314929 -0.08327455574929307; 0.021168617079303356 0.03325520079774216 -0.09055867970668394; 0.012023994007546895 0.02259686751232733 -0.06735410926704546; 0.01370955278587255 0.029955654893196116 -0.09484909291427938; 0.013044664233299218 0.032518951410414006 -0.10760692299400193; 0.0021938947799593892 0.006911744589163485 -0.024073071528775327; 0.00586767711739955 0.018785890339301826 -0.06921239216436999; 0.0017542379529720633 0.006811989593081703 -0.026597656473907026; 0.0025744530606734706 -0.00037795435441441796 -0.004922713225815588; -0.0012122972052014073 -0.0001303147694736973 -0.0003599313989554936; 0.0036092854747407322 0.0015103818777938672 -0.0007818789489493277; 0.0004566081540085101 0.000389952848017796 -0.0005498282481670647; -0.00015856887950175088 -0.0014590590349447842 0.005143611169332891; -0.0011518711357040266 0.002027374172655242 0.0021590326136354376; -0.0010573085987876912 -0.000801260472501807 -0.001027095779683749; -0.00043279264907391483 -0.0011937177947211977 0.005070264754588546; -6.27524151122381e-5 -0.0007768425270604433 0.0009288602045740205] %
+
+Mass Used: 93.31211094371565 kg
+Launch C3: 95.7531366118983 km²/s²
+||V∞_in||: 0.13217583407099412 km/s
diff --git a/archive/ES_0.5587507793900826 b/archive/ES_0.5587507793900826
new file mode 100644
index 0000000..459ff43
--- /dev/null
+++ b/archive/ES_0.5587507793900826
@@ -0,0 +1,22 @@
+archive/ES_0.5587507793900826---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:17:31.526
+Launch V∞: [7.888351147421434, -5.7637449026365815, 0.02976484820921783] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7485537676140207e-9, 1.7168714195766566e-9, 5.318862441755089e-10] km/s
+ V∞_out: [1.6681939929842757e-9, -1.6098268288683499e-9, -1.271637107019049e-9] km/s
+ time of flight: 1.8577481074575782e8 seconds
+ arrival date: 2030-04-04T03:24:21.526
+ thrust profile: [0.47333420053030967 -0.007689519326425106 -0.1547799446716066; 0.05580078479749361 0.024818686861186642 -0.07315326284756458; 0.037699264975044215 0.027815115992480478 -0.08956293660192043; 0.02482379230196914 0.024082807600696175 -0.08478965377615216; 0.022939799052176774 0.025548450850194002 -0.10790044766380498; 0.011595509602460722 0.013978051838307113 -0.062131928061886006; 0.009091813808974341 0.010537773436787953 -0.05338625473896399; 0.017475610664934055 0.02181141965652373 -0.13382161599017356; 0.007270129092857564 0.00707239026257609 -0.05003138446171932; 0.0019067529791851638 0.003793972378922121 -0.019339160679166797; 0.0017648263255166075 0.002826116501203679 -0.01936816489682419; -0.0006828992080500113 0.0017444635603255847 -0.002478181163656008; -0.00030209048601997023 0.0005676273725985857 -0.003620478113924714; 0.0008853897944946451 0.000755504162276368 -0.0031269757824460803; -0.0015377528302845203 0.0029459348082758194 0.0004482742922981321; -0.00014657262576589896 0.0008976962103056985 0.0028232981113554033; 0.0019374907069357752 -0.0002184956795599195 -0.0028199669924341532; 0.00022154060507219674 0.0033454348303288014 0.0017024816335855395; -0.003159387325663066 -0.0007019872653289392 -0.00767195500128572; -0.0025270363366263916 -0.0037974934026470237 0.005642781350226245] %
+
+Mass Used: 95.09751302411132 kg
+Launch C3: 95.44772507388315 km²/s²
+||V∞_in||: 2.507586633865215e-9 km/s
diff --git a/archive/ES_0.558753041195733 b/archive/ES_0.558753041195733
new file mode 100644
index 0000000..ef28e79
--- /dev/null
+++ b/archive/ES_0.558753041195733
@@ -0,0 +1,22 @@
+archive/ES_0.558753041195733---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T11:23:46.294
+Launch V∞: [7.528657652893246, -6.07398273110035, 0.1306272088078759] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.049585989841489e-5, 2.4683433548110092e-5, 7.058993597071642e-5] km/s
+ V∞_out: [6.900190996744635e-5, 8.524808873050791e-6, -2.9398491831246837e-5] km/s
+ time of flight: 1.7754091418261304e8 seconds
+ arrival date: 2029-12-27T08:19:00.294
+ thrust profile: [0.567366727914776 -0.037270679949559495 -0.17383263423796452; 0.1064094283162648 0.0494839635863306 -0.11933203045904774; 0.05880974803591438 0.0451085262519171 -0.11794551957837768; 0.0496320192630911 0.04956704951122265 -0.14487641642387422; 0.02474497651222834 0.029363231689491197 -0.09569151571027233; 0.023638949614294514 0.0325100859511581 -0.11325917676735528; 0.018183049064057374 0.027715290986109538 -0.10426819995841051; 0.009991161468496358 0.01662266215140658 -0.0676013682599092; 0.001153272062555916 0.0028427342511839386 -0.01154928198996816; 0.00041841519236712434 0.0003122696978237589 -0.0017279232520486271; 0.00028034122226335744 0.00042459114158694517 -0.003226537410562856; -0.00010544186691325072 0.00047089029796895324 0.00034952552857798634; 0.00014313414598759273 0.00032365474300000857 -0.005224682952866144; 0.0005410110326574008 0.0006552123817589796 0.0005091361696369567; 0.0002247848112966174 -0.0007155483991693225 -2.9658253448191802e-5; 5.073269358858132e-5 0.0003971578003716893 -0.0002445200872133503; -0.0006866471255711332 -0.0026816683658526202 -0.0009921588150666395; -0.0019412119569727673 0.0007401427780779267 -0.0005130766009852801; -0.0011093489606828419 -0.0009791207910954912 0.00215477746813576; 0.00016823301979396155 0.0002424763983291985 -0.00031731557882379345] %
+
+Mass Used: 105.93095624587204 kg
+Launch C3: 93.59101573985424 km²/s²
+||V∞_in||: 7.55140650943979e-5 km/s
diff --git a/archive/ES_0.5587636801033686 b/archive/ES_0.5587636801033686
new file mode 100644
index 0000000..cd10377
--- /dev/null
+++ b/archive/ES_0.5587636801033686
@@ -0,0 +1,22 @@
+archive/ES_0.5587636801033686---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T20:18:48.757
+Launch V∞: [8.074190712794165, -5.675343029225616, 0.12329668946320853] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004284901037094592, -0.002910418413077858, -0.000160692013547942] km/s
+ V∞_out: [0.003673130037857531, 0.0018072151277379435, -0.0031771330585641396] km/s
+ time of flight: 1.8749577787428167e8 seconds
+ arrival date: 2030-04-22T22:28:25.757
+ thrust profile: [0.21578493922534106 0.006146414805154422 -0.06091191838543678; 0.1185195407052222 0.078122952037376 -0.12088657519478796; 0.035344559840532586 0.03774409653330186 -0.06922647571053307; 0.031820496928493404 0.046206965494794076 -0.09554601814350007; 0.02924230214235439 0.054500088396010817 -0.11933577267259685; 0.010934430867480253 0.02789038593149842 -0.0685947305529272; 0.013082232247486454 0.03649620654392221 -0.09416667425076698; 0.005898423297046168 0.017537417558785323 -0.049356120422882496; 0.006087313228236579 0.020618680532718404 -0.06267905154337614; 0.0014655173917230639 0.007888153307477806 -0.024834540802102355; -0.001605366110704512 0.0038366408536491476 -0.009237324899880953; 0.003694360407961979 0.0008354302621861162 -0.006270270702697437; 0.0038163062092667756 0.0005556543680532633 -0.005216413390156559; -0.003461916267240178 -0.0021708268055396296 -0.0012571316430200936; -0.001241939881641139 -0.0007403344910085571 -0.0007592363467887292; 0.0008433194231371301 0.0021009027632661 0.002565991488237539; 0.00025687504167933945 -0.0026666017681557658 -0.0007769945422276122; -0.0008631032096807766 0.0028227536565845197 -0.0004893414449911558; 0.003410772308766429 -0.006075430754848788 0.00197321881855437; -0.002899265803158616 0.002590169428163868 -0.008828965350932179] %
+
+Mass Used: 83.62351538969051 kg
+Launch C3: 97.41727623958393 km²/s²
+||V∞_in||: 0.005182348324851875 km/s
diff --git a/archive/ES_0.5587689412433672 b/archive/ES_0.5587689412433672
new file mode 100644
index 0000000..e6b3967
--- /dev/null
+++ b/archive/ES_0.5587689412433672
@@ -0,0 +1,22 @@
+archive/ES_0.5587689412433672---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T05:09:16.396
+Launch V∞: [7.982943729288649, -5.78594542282345, 0.3168071723821733] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.831632411132422e-7, 3.189694694177835e-6, -7.519411903063628e-5] km/s
+ V∞_out: [-3.4272931737917495e-6, 7.480207880328977e-5, -6.763864133805042e-7] km/s
+ time of flight: 1.8749577801623422e8 seconds
+ arrival date: 2030-04-25T07:18:54.396
+ thrust profile: [0.32099444318222 0.0010519331483024074 -0.10311417598637057; 0.057068838920568965 0.03204462854735927 -0.07353127432642326; 0.03579641824971347 0.031150912524136917 -0.08334446271034951; 0.026932991902503648 0.028466780134042968 -0.08970990951829594; 0.024321088508953047 0.03284726073988079 -0.1110807476623301; 0.013315857508769234 0.016970737354744032 -0.07061343930724852; 0.009857371389605801 0.01596855130125764 -0.06944696564394662; 0.00752644598133804 0.013193262990961432 -0.0608298029786669; 0.005240873641879363 0.009387928060897971 -0.04816071630680281; 0.004094143514565533 0.007243174085607734 -0.039723638712703804; 0.0022446750985363334 0.006373848903695103 -0.036207161310393594; 0.0015838777361306526 0.0026817023453632816 -0.01806463120811223; -0.0007989593541300262 0.0006654392676600106 -0.0014545809473638224; 0.0003202004306734424 -0.0026456071422672873 -0.0010981081674054866; 0.0032499758091406174 0.002429656576870516 0.0006805093692523927; -0.000889029192132266 0.0007024220469681161 -0.0013439429804657644; -0.0023405276065976924 0.0016595150476954774 -0.003502884151782567; 0.0026927369329189034 0.002134627627574227 0.0011080219876158735; -0.0013528022674995563 0.0006620338238643208 0.0021307076209779894; 0.0019904416056122716 -0.002131869568416474 -0.005608179680592849] %
+
+Mass Used: 84.28505425270032 kg
+Launch C3: 97.30492180535337 km²/s²
+||V∞_in||: 7.526329208686747e-5 km/s
diff --git a/archive/ES_0.5587707765785971 b/archive/ES_0.5587707765785971
new file mode 100644
index 0000000..770aac9
--- /dev/null
+++ b/archive/ES_0.5587707765785971
@@ -0,0 +1,22 @@
+archive/ES_0.5587707765785971---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T04:42:24.690
+Launch V∞: [7.840933913156971, -5.565581324280756, 0.47277073362856514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.649768664278259e-6, 9.872636258542551e-5, 1.9399321533817733e-6] km/s
+ V∞_out: [9.086610416461272e-5, -3.193641712726663e-5, 2.1241830062516838e-5] km/s
+ time of flight: 1.874957778350806e8 seconds
+ arrival date: 2030-04-20T06:52:01.690
+ thrust profile: [0.6186992472498574 0.012359106423459769 -0.14875409978391832; 0.15461322060699056 0.10384429256094442 -0.14361915363641273; 0.045011776863626514 0.05021572631544526 -0.08319384786493374; 0.018544474637450115 0.026411500871124014 -0.05209988045271731; 0.03803685178713879 0.07414485282685275 -0.14310978440280486; 0.013517292595923856 0.03358494405516704 -0.07017963059923697; 0.009585637303487113 0.022396146194497805 -0.05956817869228962; 0.008579682622618488 0.03077470713805591 -0.08023755292107858; 0.001210942906401381 0.004908918604855506 -0.01359750121010707; 0.0011765969765901766 0.008189626440893527 -0.021958010145257417; 0.00010791162703277607 0.0005608919121565894 -0.0016337889213996746; 4.959641017836891e-5 -0.0002534349724288582 0.000177723196016651; -4.960317759191718e-6 -0.0001003024236061464 -0.00012088373469858475; -2.970996306855234e-5 4.9459483616147415e-5 -0.0002600861681205972; -0.0021769086016341925 -0.0010548413856498776 -0.0015436870459633492; -0.0011395602133882853 0.0003005748714538424 -0.0002163774409775647; -0.00024735917826519373 -0.0002707378374896366 -0.0003750393746460559; 0.0018706261030034881 4.076872270857891e-5 -0.00016284049672209654; -0.0005909575259318043 0.0038533569951014514 -0.0016414784636119045; -0.0006133809926320941 0.002848491635414536 0.002606329534930972] %
+
+Mass Used: 111.2691010752178 kg
+Launch C3: 92.67945227425352 km²/s²
+||V∞_in||: 9.885483475652538e-5 km/s
diff --git a/archive/ES_0.5587714650274966 b/archive/ES_0.5587714650274966
new file mode 100644
index 0000000..53f7a63
--- /dev/null
+++ b/archive/ES_0.5587714650274966
@@ -0,0 +1,22 @@
+archive/ES_0.5587714650274966---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T19:33:36.263
+Launch V∞: [8.09733475231708, -5.700158918852573, 0.057481080572208305] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00762499120225341, 0.004189700930497877, 0.00030505496886642895] km/s
+ V∞_out: [-0.0060213988037930545, -0.003813022514394302, 0.00499761601113192] km/s
+ time of flight: 1.8749577787484112e8 seconds
+ arrival date: 2030-04-24T21:43:13.263
+ thrust profile: [0.250615964520233 -0.008524192396754332 -0.0943716561500044; 0.04602540693083635 0.023528150882714774 -0.06436492832821747; 0.030430626463049074 0.023874858399546346 -0.07471620918209673; 0.03338730641276625 0.032324850385692196 -0.11882650851588063; 0.029922733494690545 0.03338591497522797 -0.13941434895405405; 0.02083307323005636 0.026879639971608787 -0.12021382336354074; 0.012537860366037622 0.018629579336371146 -0.09054919260210882; 0.0035519840882336858 0.006369499055851295 -0.03542756929549248; 0.004471192286618939 0.0057589273896590295 -0.023587370449121466; 0.00020097065775576345 0.0004915638944819637 -0.012111188948686742; 0.0016083189782319799 -0.0003366787591459028 -0.006969979673431849; 0.002372457590659939 0.0005613071423776445 -0.006570782161937446; 0.0010847796609559292 0.004018587751086276 -0.00046239086386944107; -0.00116072194558725 0.0009555751560402313 -0.0024124816406804464; 0.0012114657422540574 -0.0001807435014337079 -0.0027300678700257802; 0.008099093446216081 0.0027460158583039827 0.004031840540313022; 0.00023815669347967007 0.0009308053187280366 -0.0020423618002655087; 0.0036342237532914962 -0.0031107258978736595 0.004673474561888254; -0.0027272709133712002 0.0129675299963316 0.012369993736358624; -0.005747110612642086 -0.0029652006278938206 0.006607698151927227] %
+
+Mass Used: 79.87202498111174 kg
+Launch C3: 98.06194586588018 km²/s²
+||V∞_in||: 0.008705581155528146 km/s
diff --git a/archive/ES_0.5587729648930216 b/archive/ES_0.5587729648930216
new file mode 100644
index 0000000..495403d
--- /dev/null
+++ b/archive/ES_0.5587729648930216
@@ -0,0 +1,22 @@
+archive/ES_0.5587729648930216---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:06:07.686
+Launch V∞: [7.741962754001648, -5.88551471115743, 0.15776147359974504] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6324175183495678e-9, 1.5247597558247472e-10, -4.4613402031116064e-10] km/s
+ V∞_out: [9.62097247372642e-10, -9.102658353667606e-10, -7.466787681048997e-10] km/s
+ time of flight: 1.799106204259999e8 seconds
+ arrival date: 2030-01-23T11:16:27.686
+ thrust profile: [0.5053632249837021 -0.02917409737683107 -0.16579998555164885; 0.05986021721378798 0.030334520498056367 -0.07140446927865142; 0.061205094331930374 0.05014649012217088 -0.1260072854608908; 0.03480690844725419 0.03765505820531755 -0.10665172177422749; 0.03741252851237048 0.04853169833701074 -0.14924677403325923; 0.015111406813815197 0.022978189955248536 -0.07912333604257252; 0.0108184162210408 0.019904317622831957 -0.07432883310381447; 0.01182937324485935 0.024181771680530522 -0.09662773844065155; 0.0022004750939859626 0.005132823602345632 -0.021367591929345228; 0.0030407158869749378 0.00508021129629686 -0.022512452146777173; 0.0003417401955695913 0.0009611338902740887 -0.0051611603100764165; 0.0023371648686597527 -0.0002456810984398387 -0.0026579590756257913; 0.0009309009835693942 -0.0005371842973114143 -0.0003608829705313368; -0.0003868504420610025 -0.00016189040159813388 -0.0007706811796632611; -0.00019566343916724725 0.00031861436577624593 0.0020524880236294342; 0.0007153653011436804 -0.002289337070920299 0.001382262601013496; -0.00040638567384583676 -0.0031568704649502363 0.0011313204746489325; 0.00018153051664912307 0.0011436577050971514 0.0033727674969402854; -0.0048227123902015775 -0.0019541702517678135 0.003761518022913143; 0.0008916109470723775 0.000914085490333691 0.000496086359161509] %
+
+Mass Used: 100.05586264597378 kg
+Launch C3: 94.60215938215167 km²/s²
+||V∞_in||: 1.699138440923337e-9 km/s
diff --git a/archive/ES_0.5587774376544872 b/archive/ES_0.5587774376544872
new file mode 100644
index 0000000..cdff7a6
--- /dev/null
+++ b/archive/ES_0.5587774376544872
@@ -0,0 +1,22 @@
+archive/ES_0.5587774376544872---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T12:28:40.897
+Launch V∞: [7.850399937104646, -5.704271628257535, 0.1760886733398072] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012539982343123142, 0.0009500618006886897, 0.050180419729637854] km/s
+ V∞_out: [-0.046163316569797996, -0.017958641959408907, 0.008021776193713822] km/s
+ time of flight: 1.8536742218306443e8 seconds
+ arrival date: 2030-03-27T23:25:42.897
+ thrust profile: [0.48602539115663806 -0.0044800814238166505 -0.1397581318532929; 0.1504502332715992 0.08887751688062412 -0.15371175485373975; 0.03821107466853328 0.038131017219150486 -0.07824486775998607; 0.01985570818285282 0.026309436028265867 -0.06273188575403571; 0.017952873350674286 0.030172005470149598 -0.07745781728245071; 0.01783070442608624 0.03638853966339486 -0.098796766027529; 0.00707360238804568 0.011290460571161832 -0.037841692838551225; 0.021761909151057465 0.051346710924490696 -0.14923567238953084; 0.0017034935474577466 0.006821273201010523 -0.021246616564450094; 0.0005745198917610131 0.009898698814977607 -0.03563153661339885; -0.0002086438774445066 0.0003962556715265469 -0.0032873524042388567; -0.0008689678730142225 -0.0004287267383840821 -0.0021175813099041166; 0.00012923037576875152 0.0025822786335077032 -0.00026212812372297233; -0.0007732696837619456 0.0023138232277792113 -0.004993472326646909; 0.0011649381560460074 -0.001483781841909131 0.0033578822023807705; -0.004025896045440645 -0.001161820299793204 -0.0029410541673137924; -0.000458505510848092 0.0005826478701090613 -0.0010305524012198383; 0.001050226533734605 -0.0007824100481961934 0.000664463231287867; -0.002857826014997078 -0.0010218346147792975 0.0008019135038557432; -0.0005572067934317816 -0.002999234203262545 0.0023679805705847314] %
+
+Mass Used: 102.41575358339696 kg
+Launch C3: 94.19850120231509 km²/s²
+||V∞_in||: 0.05020507597085592 km/s
diff --git a/archive/ES_0.5587944243813137 b/archive/ES_0.5587944243813137
new file mode 100644
index 0000000..3e74317
--- /dev/null
+++ b/archive/ES_0.5587944243813137
@@ -0,0 +1,22 @@
+archive/ES_0.5587944243813137---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T02:36:27.407
+Launch V∞: [8.01660796722145, -5.643854173291441, -0.11289950373913923] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.647826444367826e-10, -7.943109469127204e-10, -9.662328937278707e-10] km/s
+ V∞_out: [-2.190021094381571e-11, -4.21315232468232e-11, -1.0950170433728295e-12] km/s
+ time of flight: 1.8558110395216912e8 seconds
+ arrival date: 2030-03-30T00:54:50.407
+ thrust profile: [0.3100228736483169 -0.002307549729111939 -0.0928181528123879; 0.1173781509001383 0.06889940285213837 -0.12486886914700895; 0.08362724192229053 0.08101745744408233 -0.16146649172038283; 0.027550490475142516 0.04094875410100602 -0.09295211059507451; 0.03707396702933819 0.06192689827912401 -0.1512200727054019; 0.013076129151492684 0.028461878854774487 -0.08239960927153557; 0.005515920334297529 0.012404811938834338 -0.037919984690309945; 0.004772685689990938 0.013195820068001013 -0.04193729700379983; 0.002834362884748168 0.009428278185800594 -0.03312245751064804; 0.001743609527265977 0.004928763648939476 -0.017984285745426133; 0.0018780678446768018 0.001044034896263737 -0.0005665597290755162; -0.0007477715492808143 0.00018692844584716333 0.0013086745059049801; 0.0011547383894228384 0.0019083330603573698 0.001129419741205028; 0.0034702425395594337 -0.0006464783855875088 -0.0009288547788319568; -0.0007461508758904592 0.002594735152032522 0.0004040334688043386; -8.690688224539044e-5 0.0006761816306942325 0.0006933689553124832; -0.001474084232271613 0.0001144063862067969 -0.0034174765160592735; -0.0008158301027234979 0.00033318120116845504 -0.0005595238583091752; -0.0030641354426230796 -0.0009889486770720205 -0.0011630454440637455; -0.00028911961656854194 0.0023402038789130763 0.0051411238682122495] %
+
+Mass Used: 91.15776453478657 kg
+Launch C3: 96.13183952744218 km²/s²
+||V∞_in||: 1.579664975972294e-9 km/s
diff --git a/archive/ES_0.5587996819490205 b/archive/ES_0.5587996819490205
new file mode 100644
index 0000000..10d8cde
--- /dev/null
+++ b/archive/ES_0.5587996819490205
@@ -0,0 +1,22 @@
+archive/ES_0.5587996819490205---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:17:22.428
+Launch V∞: [7.675485625105917, -5.996728960411707, 0.5330313911610433] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.801120621757737e-10, 1.498319505990795e-9, -1.7953346743542057e-9] km/s
+ V∞_out: [1.1504521808211898e-9, 2.1760887200949613e-9, 5.343273735282061e-11] km/s
+ time of flight: 1.832280998891993e8 seconds
+ arrival date: 2030-03-04T00:59:01.428
+ thrust profile: [0.3946020460568218 0.008155785284189938 -0.0928452521240498; 0.10600038783306132 0.06950961058390584 -0.09657983932412928; 0.06826086008686072 0.07588376106099566 -0.11486778823996376; 0.04239340243703908 0.06443716713488684 -0.10972379320962411; 0.03546399768122596 0.07207794857890328 -0.12894148721653675; 0.019976725228771006 0.04782978277923481 -0.09827681951445844; 0.009996756391881507 0.03527749281709128 -0.07616535480153473; 0.006237284207016486 0.018882447709266423 -0.04350332124639369; 0.004681565697763073 0.01755088606770228 -0.04245230369667058; 0.0020799505905321866 0.007492411730993483 -0.018886923431186284; 0.00043691164169171236 0.0027119896399952427 -0.007389812060644166; 3.1436852839036115e-5 0.00012840539410025235 -0.0002641861504486227; -0.00013358198580733967 -1.5702749430150973e-5 -0.0006959364008216948; -2.9191251422197703e-5 0.00017200684474477797 -0.00030732041666844934; -0.00016065136918184963 5.589635808035158e-5 -0.0001688168497299528; -2.834856940028607e-5 -0.00012508842318821129 -0.00024260709210215733; 0.0005237911619869318 0.0006259216595918761 -0.0014203223398140032; 8.314344703005746e-5 0.0003420960335515314 -0.00011491445460767329; 0.00018641543721833066 0.00029407019812886104 -0.0008281452840809888; -7.104823084563077e-5 -3.2627995137953023e-5 8.783130194768454e-5] %
+
+Mass Used: 96.8448606999591 kg
+Launch C3: 95.15796026981111 km²/s²
+||V∞_in||: 2.4092982255530035e-9 km/s
diff --git a/archive/ES_0.5588014176447007 b/archive/ES_0.5588014176447007
new file mode 100644
index 0000000..32b8233
--- /dev/null
+++ b/archive/ES_0.5588014176447007
@@ -0,0 +1,22 @@
+archive/ES_0.5588014176447007---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:40:45.722
+Launch V∞: [7.950321598162736, -5.817082421123899, 0.012486496725362787] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.658344076820791e-6, 3.8988622951315796e-5, -0.0006950888987675985] km/s
+ V∞_out: [-2.714678410554682e-5, 0.0006951222139815507, -9.257735327527016e-6] km/s
+ time of flight: 1.8143055722063816e8 seconds
+ arrival date: 2030-02-10T21:03:22.722
+ thrust profile: [0.2934698729286004 -0.028193143456816377 -0.09905704977896936; 0.06581681483341663 0.030431386937090098 -0.07818518833779536; 0.05173704603322096 0.03963173230238472 -0.10931644269437696; 0.039157242673689585 0.038869753801416745 -0.12059590696077946; 0.02781524955794396 0.033068401947587214 -0.11355361153021226; 0.017885701067144096 0.024890550761828376 -0.09230794489393754; 0.011568139743953296 0.020199537978001496 -0.07647163030677981; 0.009067633863041998 0.01710170460963522 -0.06952582733663963; 0.0080722023052466 0.016203631328128593 -0.07142043179764455; 0.0020984706014270053 0.004835199005708823 -0.02250907866136503; 0.0007885298127174133 0.00129127000830494 -0.011669278727732213; 0.0006158243530793905 0.001522779404221283 -0.008025361560879027; -0.00021327855133719407 0.0012428983400737431 0.0004100962613811884; -0.0006252365286990299 -3.311606493880165e-6 0.0014790497268565312; 0.0020705813497622857 -0.0028074393011835895 -0.0009520484857098003; 0.0007502468118533073 0.0005648443183145476 0.0011410458356960447; 0.00023861455058852578 0.00037512957822888457 0.002044007582804741; -0.0016372289063501754 -0.006651704348998963 0.000985106430242813; 0.00022149269267341553 0.004486838117451042 0.002108269643394457; -0.0008748080231358545 8.635203743272169e-5 0.00028610593519677455] %
+
+Mass Used: 85.83205287987221 kg
+Launch C3: 97.04621732096204 km²/s²
+||V∞_in||: 0.0006961970914038141 km/s
diff --git a/archive/ES_0.5588021017563061 b/archive/ES_0.5588021017563061
new file mode 100644
index 0000000..c59caa7
--- /dev/null
+++ b/archive/ES_0.5588021017563061
@@ -0,0 +1,22 @@
+archive/ES_0.5588021017563061---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T13:53:12.145
+Launch V∞: [7.952704916148978, -5.733105420457298, 0.19060327802997531] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.643609141629268e-8, 7.437444823681484e-7, -1.3491291883572062e-7] km/s
+ V∞_out: [1.1960792542041526e-7, -4.519048730598605e-7, -6.175536780568358e-7] km/s
+ time of flight: 1.874957778441945e8 seconds
+ arrival date: 2030-04-22T16:02:49.145
+ thrust profile: [0.28600594696998677 0.011661542553678178 -0.08015629710700684; 0.12803816188369738 0.08412393709436303 -0.12288564840319599; 0.061656787582003596 0.06483259769430363 -0.1079659351980073; 0.04009149317475288 0.05846630508898851 -0.10920656108627197; 0.031543260897046836 0.06106411144903992 -0.12347534870999495; 0.02248407304938586 0.04885705545130323 -0.10650972176105696; 0.012489044318967935 0.03310802589139271 -0.07971320695652541; 0.0022699787397279817 0.007331062965275252 -0.02078053657113701; 0.002004049012112713 0.007715761979579366 -0.022772314814276613; 0.0002852352104050469 0.004408028914435712 -0.01241759188194816; 0.00022208032754828202 0.0010694044890233764 -0.0036515434099789958; -0.0029325498908545035 0.0006773916989435351 -0.0024386435425083576; -0.002846450471068838 -0.0011121016184520677 -0.00015238476212779022; -0.003079978838634897 -0.001595539107680504 0.0006271198367211109; -0.0011761736954957283 -0.0006532206405868761 0.0008182990915734875; -0.002933690150481026 0.002286919900560442 0.004957260482000604; -0.0011317400938134102 0.006799525228670564 0.0019021663069363776; 0.0007103324598457848 -0.00011738477039346918 -0.0037148674526928742; 0.001345103545641099 -0.002256888341149521 -0.00018365459367325606; 0.0075630256614639515 0.008905132282052263 -0.004913572119455006] %
+
+Mass Used: 91.05878539478272 kg
+Launch C3: 96.15034285501274 km²/s²
+||V∞_in||: 7.597366825373372e-7 km/s
diff --git a/archive/ES_0.5588046626027996 b/archive/ES_0.5588046626027996
new file mode 100644
index 0000000..1ca9adb
--- /dev/null
+++ b/archive/ES_0.5588046626027996
@@ -0,0 +1,22 @@
+archive/ES_0.5588046626027996---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T10:18:02.619
+Launch V∞: [7.958821379957036, -5.719768037591398, 0.13832121072908513] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.465779190351388e-6, 3.886219816597226e-5, -0.0020801571231717987] km/s
+ V∞_out: [-7.738599937743662e-5, 0.002078956524453706, -2.2222204490201087e-5] km/s
+ time of flight: 1.8749577787493646e8 seconds
+ arrival date: 2030-04-24T12:27:39.619
+ thrust profile: [0.4248062773599429 -0.00760764339649726 -0.13468045771985296; 0.03819035204082516 0.019633848935897983 -0.04681468284780133; 0.03272824335457814 0.02648298299650783 -0.0727057534767043; 0.030507741066901753 0.032016058025813664 -0.10014747145233983; 0.02899463080361726 0.036377264197957164 -0.12683345707003293; 0.013798760451550816 0.019411117399265872 -0.07520520899939544; 0.01649439175005884 0.02661883799844625 -0.10806123902726265; 0.006075241878163673 0.010323698779347783 -0.04591269529066259; 0.006586455901848309 0.012366748475215102 -0.05460140219052505; 0.0023005715100402058 0.00305839773884344 -0.02967730946252653; -0.0039025249032664717 -0.0023191827098841726 -0.00013666025556387327; 0.0012128763123036984 0.0017657915485755583 -0.005710328258016809; -0.00027492432805134614 0.0070943428763764116 -0.0022887512662095716; 0.0003841745037302216 0.0006628285216988931 -0.0035409611795939374; -0.0013751748624237143 1.739420343966052e-5 -0.0056448070084449695; -0.005601300465746141 -0.004109735020096669 0.0016153845009169087; 6.287474419605247e-5 -0.0016243818518577825 0.0012826199451695334; 0.004565691384985337 0.000681769565871091 -0.00914661779109345; 0.0003174148207354114 0.0013854934899883574 -0.004532509054956766; 0.004359550077884376 0.005419927944128716 -0.008109292277786274] %
+
+Mass Used: 91.48542434096908 kg
+Launch C3: 96.07771691925092 km²/s²
+||V∞_in||: 0.0020805249026898094 km/s
diff --git a/archive/ES_0.5588055645482355 b/archive/ES_0.5588055645482355
new file mode 100644
index 0000000..6e6fed1
--- /dev/null
+++ b/archive/ES_0.5588055645482355
@@ -0,0 +1,22 @@
+archive/ES_0.5588055645482355---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T11:13:09.526
+Launch V∞: [8.221522620210072, -5.627317218380497, 0.1465909467944107] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.309519548042712e-7, 6.316614563020096e-6, -0.0001250659645091571] km/s
+ V∞_out: [-4.267929227709084e-6, 0.00012511214507132147, -1.2323493955206595e-6] km/s
+ time of flight: 1.8749577787577102e8 seconds
+ arrival date: 2030-04-24T13:22:46.526
+ thrust profile: [0.16659339807957807 -0.005551643877467228 -0.05899772503420953; 0.03703410754469554 0.019456266953934168 -0.05030689410009305; 0.024182707764736 0.018389468415740295 -0.06119904843699577; 0.02241971160282061 0.023231457270892413 -0.07832011129925211; 0.013829401075188529 0.016057239689129373 -0.06284056417503477; 0.013216474053757662 0.019379681582132366 -0.08274768889748796; 0.01332649474682851 0.020708902712351897 -0.09348192327233139; 0.01703420817524224 0.02931020274292188 -0.12998286377728013; 0.002852001431365661 0.00802687664554379 -0.03378092705264636; 0.008942633911813536 0.015519470303443996 -0.08325716494026857; 0.002216106026825358 0.004027046723066656 -0.011999741857283907; 0.0020527815974048422 0.005916399188682573 -0.027451751690298787; 0.004125988760640692 -0.0016328344851183922 -0.005253517192115265; 0.0012567131538977557 0.001718185488157048 -0.0005228734803981953; 0.0006543233763876748 -0.0018654300890262987 0.00016340435586953243; 0.004655637814488042 0.0026010489762623647 -0.001059176405864508; -0.002937828272586426 -0.0027253392579712895 -0.0027760896196528818; 9.795266560956302e-5 0.00012434632312043233 -0.0019304267799432522; -0.0025368548929682114 0.0049744117533096635 -0.004396188628561292; -0.0027647289468122455 -0.003932112908478553 0.001482816309783734] %
+
+Mass Used: 72.79702927616881 kg
+Launch C3: 99.28162217658958 km²/s²
+||V∞_in||: 0.00012522813413644193 km/s
diff --git a/archive/ES_0.5588087454579168 b/archive/ES_0.5588087454579168
new file mode 100644
index 0000000..71aa516
--- /dev/null
+++ b/archive/ES_0.5588087454579168
@@ -0,0 +1,22 @@
+archive/ES_0.5588087454579168---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:21:28.925
+Launch V∞: [7.872400137919027, -5.800814131573705, 0.26267784593725624] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.250851259808818e-7, -8.315972273199503e-6, 1.2758796046799926e-6] km/s
+ V∞_out: [-1.304169200385787e-6, 5.001533897607869e-6, 6.702143380413511e-6] km/s
+ time of flight: 1.8318926149921015e8 seconds
+ arrival date: 2030-03-02T16:15:49.925
+ thrust profile: [0.3686188131466555 -0.002277662391250332 -0.10377683817198366; 0.09844427231009498 0.05911417876252619 -0.10569258599176995; 0.05375239578273386 0.053370706105133316 -0.10753392520870893; 0.042296046551777815 0.05722817180371986 -0.1267233458663427; 0.030082274456885168 0.051163760947366146 -0.12428865834859783; 0.01891084521333291 0.03943865461730483 -0.10403281912034294; 0.011633105673828427 0.02935406178895188 -0.08300365066528033; 0.005045826026513766 0.015921573897176904 -0.0480822171269262; 0.002164185661940934 0.008632835930089677 -0.027256571211412346; 0.00011425956875042937 0.001580606585224803 -0.005310142774670349; 0.0003734646573939866 0.0020130310563997817 -0.007669865678803416; -0.0004144677400994462 -0.00024235302449384787 0.0011445955158475973; -0.0018985935354908763 0.0003941152461757022 -0.0030068416144511606; -0.0012842537967805358 0.0019772534201966986 -0.003602162327354222; -0.00047718896184528416 1.4190506059742612e-5 0.001168599015314178; 0.00017436036632871154 -0.001968374736508626 0.002186951256814402; 0.0040173452720932284 -0.0003048735431640248 0.003860476785208511; 0.006393249929068199 -0.005124668654124527 0.0009875942077143228; -0.00038147580278991055 0.00042826345912364434 0.0004411214629902268; 0.006341801962265494 -0.003439166062285029 0.004994573731317968] %
+
+Mass Used: 93.73362203487568 kg
+Launch C3: 95.69312817131896 km²/s²
+||V∞_in||: 8.463985237733603e-6 km/s
diff --git a/archive/ES_0.5588101958021864 b/archive/ES_0.5588101958021864
new file mode 100644
index 0000000..aadf55e
--- /dev/null
+++ b/archive/ES_0.5588101958021864
@@ -0,0 +1,22 @@
+archive/ES_0.5588101958021864---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T04:40:40.580
+Launch V∞: [7.95591557408727, -5.647706801250439, 0.06124605923320903] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.023411221569867e-6, -2.023616957750107e-5, 0.00039487851649050784] km/s
+ V∞_out: [1.557629069397654e-5, -0.0003950395982321852, 4.218101152671444e-6] km/s
+ time of flight: 1.8749577787428534e8 seconds
+ arrival date: 2030-04-22T06:50:17.580
+ thrust profile: [0.34989483218059947 -0.00031813275163839047 -0.10286416920062263; 0.21669689201810338 0.12788510943465015 -0.21455046974556524; 0.029698117377240783 0.02771416591607286 -0.05975353302462546; 0.022872497980184793 0.02820255792953584 -0.06902146848895796; 0.020438851226159054 0.030849039253346987 -0.08365234888354994; 0.02414546479356999 0.04378085394559947 -0.1268781383316894; 0.010671833346956823 0.02218609026278453 -0.06963519410742106; 0.007500927975357225 0.017910023680743712 -0.059669736355799766; 0.001982173217032859 0.004226866462241944 -0.014594180330246072; 0.0007194038258032839 0.005661554939066411 -0.015224068548501501; -0.00021763033327970908 0.0014507372814696704 -0.004140141869342651; -0.0006058426528510607 0.0003804805533685699 -0.0021931010978863703; 0.002132281733207247 0.002175964264591999 -0.006688703779383357; 0.0035370318467320716 -0.001968337828198905 -8.808735904501132e-5; 0.011016252350818786 0.0007895679216566659 -0.0023121149641526203; 0.002310676320258599 0.002304892809575614 -0.00017248671893628931; 0.002566665497418005 0.0020784495709859283 -0.004581623192264534; 0.0007568064326752052 -0.0003097685836382664 -0.0021983148452198306; -0.004131050015254116 -0.000731671736717638 -0.0027178013546801695; 0.0012788757648146299 0.002784620382352254 0.006276689101828476] %
+
+Mass Used: 96.62976951699648 kg
+Launch C3: 95.19693581466645 km²/s²
+||V∞_in||: 0.00039540187093371884 km/s
diff --git a/archive/ES_0.5588130466713077 b/archive/ES_0.5588130466713077
new file mode 100644
index 0000000..7a63de5
--- /dev/null
+++ b/archive/ES_0.5588130466713077
@@ -0,0 +1,22 @@
+archive/ES_0.5588130466713077---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T07:10:31.811
+Launch V∞: [8.046676287827427, -5.4814589322396685, 0.674311266395684] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000876101962521491, 0.06147559894860381, 0.0011857306609950285] km/s
+ V∞_out: [0.00015053250450043374, -3.105583475820916e-5, 4.589757020859995e-5] km/s
+ time of flight: 1.8749577783958146e8 seconds
+ arrival date: 2030-04-20T09:20:08.811
+ thrust profile: [0.49771450507513004 0.005558584305865718 -0.11357916229681377; 0.053436212405025385 0.03559799048443589 -0.05305699020778607; 0.04206757149109146 0.0461277971421476 -0.07621189854003256; 0.039319920336500704 0.058594386691458465 -0.1072153781177898; 0.027703471501575993 0.05100350602172969 -0.10122446590879632; 0.017657488291035237 0.04114791251207461 -0.08692852843614265; 0.013952629533945729 0.03946637611445803 -0.08909980691075535; 0.004515536765316049 0.01438291773622079 -0.035842353856087826; 0.007971527241579072 0.033053491871070644 -0.08167920360493063; 0.001713991714712536 0.007752548138701803 -0.02151232441838661; 0.0001437798391083101 0.0003148641480022205 -0.0008366824122612958; -2.941127603143475e-5 -0.00021932611429717605 0.0006241782171338673; -9.785005383942431e-5 0.00015814930621362713 0.0006660022229192416; -6.686616258699688e-5 -5.956468237354943e-5 2.964582254290875e-5; 0.00028767367833791764 0.00044755011097399487 -0.000364532243216012; -0.00011718931335837575 -0.0006187056243873468 -9.10162377673277e-5; -0.00030773119224149697 -8.294684184383192e-6 0.0002511395215991186; -0.0004475437120431351 -0.00026240662479165604 -9.300594092159022e-6; -0.0005304219046691288 0.00023123174078093045 -0.0004637102361889733; 0.0007186241865390933 -0.0003028882589550298 -0.0005909108106918699] %
+
+Mass Used: 96.32304700292843 kg
+Launch C3: 95.25008699090237 km²/s²
+||V∞_in||: 0.06149327424961803 km/s
diff --git a/archive/ES_0.5588191907596151 b/archive/ES_0.5588191907596151
new file mode 100644
index 0000000..b52c3d6
--- /dev/null
+++ b/archive/ES_0.5588191907596151
@@ -0,0 +1,22 @@
+archive/ES_0.5588191907596151---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:10:07.474
+Launch V∞: [7.766499866896131, -6.074001464303365, 0.33133129515766324] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00029571736870550246, -0.00016064618983675685, -1.1325156120098014e-5] km/s
+ V∞_out: [0.00021744360037141594, 9.662660343518185e-5, -0.0001711517249156455] km/s
+ time of flight: 1.7902273464577442e8 seconds
+ arrival date: 2030-01-14T19:42:21.474
+ thrust profile: [0.2670198891848331 -0.011675297663911772 -0.08462743859418254; 0.08472784206909903 0.04359094459304644 -0.09554677066908626; 0.03387677864624352 0.027682105094802643 -0.06848081451084281; 0.04556238753440798 0.04996862940479063 -0.1301063590851836; 0.02422849583998401 0.03146873685244752 -0.09912028418614806; 0.031393775591188895 0.047992904179810024 -0.1497046308533919; 0.00817661752175536 0.014092457252345673 -0.04772539662982386; 0.013110534101909327 0.028327739793865776 -0.08596454716053775; 0.011914177337175457 0.023632078497044427 -0.09252212887271193; 0.0025795601046729707 0.004908987350350089 -0.018438308385898477; 0.0011599879599393328 0.0022750609774304345 -0.011751658947160806; 9.148866105094567e-5 0.00012064989785543379 -0.0002396871061290979; -3.0531123468693314e-5 -6.337956694954039e-5 -0.00011571273492751554; 0.00011827129128689153 0.0002989359104021582 -0.00048620231393902357; -0.00015897839705811414 3.325510865431049e-5 -0.00022055929058918198; -9.762418183192488e-5 3.867148742775316e-5 -8.681173756622785e-5; 0.00012872696200696466 -0.00012710345833055972 -0.00015270592649667503; -3.438664641240187e-5 9.928394453979266e-5 2.1895550605475465e-5; -0.00010695229103331691 -4.9402642289792355e-6 0.00010241079825448393; -0.0001144007083739157 2.0166254265916274e-5 -0.00019341500306011572] %
+
+Mass Used: 84.24525523117154 kg
+Launch C3: 97.3217943980079 km²/s²
+||V∞_in||: 0.00033672573353445677 km/s
diff --git a/archive/ES_0.5588240823441882 b/archive/ES_0.5588240823441882
new file mode 100644
index 0000000..0329d2c
--- /dev/null
+++ b/archive/ES_0.5588240823441882
@@ -0,0 +1,22 @@
+archive/ES_0.5588240823441882---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T14:12:09.904
+Launch V∞: [7.9818301410935515, -5.598151466766008, 0.09766152121451802] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.530656591038604e-5, 3.7956963979169573e-5, 2.943631699597826e-5] km/s
+ V∞_out: [6.094573867289961e-6, -4.30191737679165e-5, 4.927284126176147e-5] km/s
+ time of flight: 1.8749577790032744e8 seconds
+ arrival date: 2030-04-22T16:21:46.904
+ thrust profile: [0.4508660035676925 -0.011408448029244058 -0.13818465452581521; 0.12229882121051443 0.06698542046247592 -0.13858190168312126; 0.021192532529690732 0.01906329364611849 -0.048135479386771374; 0.03258000073132101 0.03704298896926664 -0.10463125477811787; 0.01862427632172916 0.025239366010619626 -0.08204328275599833; 0.012777959408180578 0.020447001312462576 -0.0741280368304055; 0.009508301304414017 0.01707837004604697 -0.0667004931739776; 0.006681136864039872 0.013335298710345738 -0.05584530354732957; 0.003575812987000244 0.008613951224405988 -0.038835419335973516; 0.006287134648761402 0.01463634232061558 -0.06532086539691777; 0.0007976237165039158 0.002983742274688419 -0.013430532481401048; 0.003329731961596049 0.001315740797282346 -0.007825948108394327; 0.0003654627072014263 0.0010116178342509828 -0.007304464255540998; 0.004103672016849438 0.006334414917457061 -0.0038587881812884427; -0.001635114068125508 0.001047887142210162 -0.0013590764145795953; -0.0007329762872764665 0.00291374037059785 -0.005127875749450226; 0.002263867785611039 -0.0008855630570882198 0.004899729112494037; -0.0007657605150591703 0.00019407089850592376 -0.0020592352770376528; 0.0007670824397604283 0.004345487765682537 -0.004339854728739643; -0.002117338892636707 0.002321624312963404 0.0035025057568192535] %
+
+Mass Used: 97.45380429159559 kg
+Launch C3: 95.05845001884984 km²/s²
+||V∞_in||: 6.602963567517126e-5 km/s
diff --git a/archive/ES_0.5588289593453516 b/archive/ES_0.5588289593453516
new file mode 100644
index 0000000..58a8c5a
--- /dev/null
+++ b/archive/ES_0.5588289593453516
@@ -0,0 +1,22 @@
+archive/ES_0.5588289593453516---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T06:34:29.550
+Launch V∞: [8.040720885288884, -5.9198402616325785, 0.01221287024400045] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1562895726433096e-9, -3.720365462060327e-9, -1.1641825621206384e-9] km/s
+ V∞_out: [-4.882241663193561e-10, -1.0435007125446322e-9, -2.699841516111986e-11] km/s
+ time of flight: 1.874957778173417e8 seconds
+ arrival date: 2030-04-27T08:44:06.550
+ thrust profile: [0.16387684070309969 -0.0029797269514147888 -0.06544398746385562; 0.04742747795169463 0.02273548532958549 -0.06550365911674896; 0.021791412125248273 0.01647439038451195 -0.05216839184162745; 0.02157627162582679 0.01993959233426198 -0.0776378882436312; 0.03721022949962665 0.04140339979600627 -0.17098533293182236; 0.0172042739512073 0.020472438728788955 -0.09996486068187882; 0.011961226496700901 0.015127516403848316 -0.08031317689729939; 0.006275004744547775 0.008387582758799614 -0.04914408574541896; 0.0027332451067426356 0.0038427298466513554 -0.02507230577689309; 0.0044569378898162105 0.0080045787448286 -0.05248611010048786; 0.0032078914601825917 0.004110785957159934 -0.029185983866925985; 0.00029224214466773895 -0.0007654992721167227 -0.0010494247245609292; 0.00020823280753578735 0.0004594528386465343 -0.003766521247253395; -0.0003760858713089104 0.0006810949799039877 -0.0030636898665360275; 0.00013373675372051284 0.00040661882363744295 -0.0006746305750676816; 0.0009827731940403345 -0.0009000825725125047 -0.0003411845117580177; 4.0091773337174774e-5 0.000801203739545387 -0.0003086635006234027; -4.2071817366366076e-5 0.00037696941583515104 -0.0012601416573182278; -0.0011499595454642054 0.0003165350664729506 -0.0014514175142279916; -0.00012039142368073282 0.0004296595097449938 0.0013365298110427] %
+
+Mass Used: 70.39632621293867 kg
+Launch C3: 99.69785023256654 km²/s²
+||V∞_in||: 4.4548877573208725e-9 km/s
diff --git a/archive/ES_0.5588344360124219 b/archive/ES_0.5588344360124219
new file mode 100644
index 0000000..84a29b7
--- /dev/null
+++ b/archive/ES_0.5588344360124219
@@ -0,0 +1,22 @@
+archive/ES_0.5588344360124219---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T18:28:08.930
+Launch V∞: [7.873023278826192, -5.5827272911297765, 0.17402651066559371] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0025279924878807386, -0.0017004210205947823, -0.00010967585301600008] km/s
+ V∞_out: [0.002198382515294629, 0.0010209789320769123, -0.0018454698147552747] km/s
+ time of flight: 1.859064486695292e8 seconds
+ arrival date: 2030-04-02T11:08:56.930
+ thrust profile: [0.6514171865508986 -0.01066645926579501 -0.18727028023952055; 0.046221148075380296 0.027519319870425992 -0.05120385416727061; 0.031014295692032182 0.030493386023725918 -0.06313535689975368; 0.061808378446719436 0.07782111734932448 -0.17375801484900238; 0.019209561783682653 0.032245400759935545 -0.0817961187317163; 0.008100346871379624 0.015509889525945458 -0.044381999152055235; 0.00593757363906799 0.013762931738183702 -0.04191822943035364; 0.00791347331929956 0.021238732276036353 -0.06676121640304994; 0.002276556309726828 0.009784911961570152 -0.03389535202128187; 0.013370884192437826 0.03485444212916615 -0.10604805233030819; 0.0010608333794179246 0.004123222946410805 -0.01587946084656603; -0.000171694550136091 0.0007813930116545263 -0.00014634331810597548; -0.00013917002483989152 0.0006802083543031453 -0.0024191679757880227; 0.0005402704498899501 -0.00037211491375137816 -0.001803686767375192; 0.000858525414240807 0.0006842128650696383 -0.0031184813993838214; 0.00012735942104183384 -0.0008910720157607477 -0.001311006462073444; 0.00013094204764578675 0.0034306372128685043 0.00011761972185294505; 0.0012905178002473366 -0.0006293918351961082 -0.0011085374250088256; 0.00047268511209994763 0.002346129458294994 0.0005610594143225613; -1.3852091845422397e-5 -0.0007281935104317138 0.00017507877744503072] %
+
+Mass Used: 108.41403078336589 kg
+Launch C3: 93.18162478247879 km²/s²
+||V∞_in||: 0.003048640099912883 km/s
diff --git a/archive/ES_0.5588395949424341 b/archive/ES_0.5588395949424341
new file mode 100644
index 0000000..9144762
--- /dev/null
+++ b/archive/ES_0.5588395949424341
@@ -0,0 +1,22 @@
+archive/ES_0.5588395949424341---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T11:35:07.130
+Launch V∞: [7.829916283328417, -5.856738445444002, -0.22850365962488783] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3312781947645995e-7, 1.4966291833815037e-6, -3.619006805533125e-5] km/s
+ V∞_out: [-1.59911387479599e-6, 3.617267319335555e-5, -2.7576909625747604e-7] km/s
+ time of flight: 1.8243469605091453e8 seconds
+ arrival date: 2030-02-22T23:53:23.130
+ thrust profile: [0.4019494503790443 -0.02056396674760107 -0.13613848074652138; 0.09115568321142399 0.04599211316869166 -0.11115730596979512; 0.05089510945452156 0.04166801605568178 -0.1120724805116091; 0.03233778609435474 0.0345016525361199 -0.10561276999173382; 0.021748411370694404 0.02791677691252868 -0.0951015024762534; 0.022259436595758242 0.0333045451976174 -0.12188294506583784; 0.01120824742937238 0.01854897473036889 -0.07488120734127035; 0.005555058772604287 0.01020745745805579 -0.04426849655861909; 0.008740355346714905 0.018157903718975004 -0.08093554087086044; 0.00040631460961964357 0.0005971907283466015 -0.0028077833953307485; 0.0001416579106104525 0.001209140084015331 -0.007631915487936793; -0.0009438726917712934 -0.00027945097463098273 -0.0017281274142781898; 0.00026563194683096016 -0.00023261378082140713 0.00021114696022692865; -0.0012473013937658003 0.0003162534582238941 0.002146096902637927; -0.0022663213672029087 -0.00029137903651157705 0.00260957873414796; -0.00024169870197769197 0.0013312816746869204 7.147671376536667e-5; 0.001272083965193123 -0.003794280181630151 0.0026394103114810424; -0.0007157947554400982 0.003157069886652652 -0.00012038420247177602; -0.0025041887119270035 0.001127239337453632 0.0016714595875767305; -0.0020245892212052653 -1.0659136212444912e-5 -0.002737005308535883] %
+
+Mass Used: 93.95592992188404 kg
+Launch C3: 95.66118814473528 km²/s²
+||V∞_in||: 3.622175138424798e-5 km/s
diff --git a/archive/ES_0.5588486761788221 b/archive/ES_0.5588486761788221
new file mode 100644
index 0000000..34e1662
--- /dev/null
+++ b/archive/ES_0.5588486761788221
@@ -0,0 +1,22 @@
+archive/ES_0.5588486761788221---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:10:51.190
+Launch V∞: [7.945818240259221, -5.94120966383693, 0.14055523392790287] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.19180925543054e-5, 3.066085716229282e-5, 0.003639471658116584] km/s
+ V∞_out: [-0.0032274867045952683, -0.0011174100611226578, 0.0011884663006676013] km/s
+ time of flight: 1.8067508360903051e8 seconds
+ arrival date: 2030-02-03T02:42:14.190
+ thrust profile: [0.18027111685608754 -0.007555062069803527 -0.06757364987517711; 0.059951404473054484 0.02806633246373559 -0.07256816657881933; 0.040164723951288256 0.0316129485022682 -0.088119049637832; 0.0415355375876353 0.04477575017148388 -0.13693184457517904; 0.030864646606964995 0.03765041680163678 -0.12709549817436255; 0.023598726129945135 0.03346754735503853 -0.12642263686481517; 0.014349184407556524 0.02271962448787188 -0.09187189232560022; 0.013054359574389844 0.023410782187195292 -0.10212391349582903; 0.0030391810833061738 0.005243951664745183 -0.026639824843772596; 0.0007087899375410638 0.00042284200239300234 -0.004769294548267208; -0.0006057668727108835 0.0011942228536248921 -0.0013796547480841269; 0.00013463446244313328 0.0002353961720520471 -0.0004479954090462297; -0.0015382981334556337 0.0008565953589744302 -0.0013056426629369318; -0.000342216044433621 -0.0015052387795204624 0.00489287845045105; -0.0005577458618024368 -0.0017162725438144791 0.0035811762748534973; -0.0006013073581787394 0.0014807344875693758 -0.0019052270904409833; 0.0027143195830435615 -0.00068069806400609 0.0010108564106548763; -0.004169664410209965 0.0016109393293785885 -0.0029727210744340832; 0.0002220837984547933 -0.0007234780901428193 0.000455381909054299; -0.0014515020640882485 -0.004204209240990379 -0.00787983880144715] %
+
+Mass Used: 77.67654816293407 kg
+Launch C3: 98.45375555068999 km²/s²
+||V∞_in||: 0.0036398421895570132 km/s
diff --git a/archive/ES_0.5588516721450503 b/archive/ES_0.5588516721450503
new file mode 100644
index 0000000..8dff2e1
--- /dev/null
+++ b/archive/ES_0.5588516721450503
@@ -0,0 +1,22 @@
+archive/ES_0.5588516721450503---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T09:47:48.712
+Launch V∞: [8.023841305461639, -5.81075737692453, 0.03412358471346602] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8649088444675455e-9, 1.7990171340744319e-9, 3.4181138477529447e-10] km/s
+ V∞_out: [1.6334897754530076e-9, -1.4604949804202372e-9, -1.5746024351060182e-9] km/s
+ time of flight: 1.8516680767722374e8 seconds
+ arrival date: 2030-03-28T13:01:15.712
+ thrust profile: [0.23265701072565184 -0.00665254775012458 -0.08479171099020387; 0.050571550246716376 0.02509555467292095 -0.06534857693418947; 0.04475266619035231 0.03613988934729791 -0.10378263576739567; 0.03211904978978145 0.03296742316931209 -0.1079534029814409; 0.021367802126634267 0.025452828182604446 -0.09511934519438711; 0.014334722863571616 0.01945611109751742 -0.07949861543374542; 0.008967208726247476 0.012078712382294313 -0.058253671338504134; 0.004332109118866667 0.006181672744591456 -0.032814794558703536; 0.006077873472509287 0.010436440321531733 -0.04934239182912339; 0.012463533529419906 0.02487468334910312 -0.1233788876733138; 0.0022034629937681765 0.004438601702513752 -0.02532362714275995; 5.730676852814696e-5 0.0011283172855942123 -0.005824443443816763; 0.0023714059684091576 0.00019554527774851878 -0.0016025485957744875; 0.000982229432115081 0.0004816370438964323 3.8753054997435195e-5; -0.0005810720406576184 5.5190220728816184e-5 0.002145331338273564; -0.00040080154121318186 -0.0002727847596819406 0.0006812844400579542; -3.697326730032905e-5 0.00042927808456060955 -0.000122498084717834; 0.0005881419892922731 0.00521254025118555 0.003937532771791909; -0.001133101257449029 0.0006063235299903076 -0.0006944951622621356; -0.0018160123890400115 -0.004859493980104813 0.0016913705631145819] %
+
+Mass Used: 79.46306329069012 kg
+Launch C3: 98.14809500774889 km²/s²
+||V∞_in||: 2.6136531272586007e-9 km/s
diff --git a/archive/ES_0.5588555292398782 b/archive/ES_0.5588555292398782
new file mode 100644
index 0000000..56864bb
--- /dev/null
+++ b/archive/ES_0.5588555292398782
@@ -0,0 +1,22 @@
+archive/ES_0.5588555292398782---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T21:44:02.573
+Launch V∞: [7.710548800606863, -5.730769630551915, 0.3023114034516619] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9806684425982213e-10, -4.2244916427719815e-9, -3.1886770809329067e-9] km/s
+ V∞_out: [-1.716056653324844e-9, 1.608063399491991e-9, 1.3135263079388556e-9] km/s
+ time of flight: 1.860046861154913e8 seconds
+ arrival date: 2030-04-04T17:42:08.573
+ thrust profile: [0.6536541108679387 -0.0019354722753802118 -0.18292893695890222; 0.13629478572084094 0.08043794951681452 -0.13967072518370802; 0.05097171979150894 0.049490715566265255 -0.09813795116617892; 0.028078338393249944 0.036519010523677724 -0.0825970898083785; 0.012569308167351044 0.020224862764522657 -0.05235276471758425; 0.0074154649008921995 0.013751231708146953 -0.041473984736026266; 0.009931535621749777 0.02185714883619165 -0.06645087564558634; 0.0061990115019440505 0.022439571431421137 -0.06753487650453623; 0.009688165901006535 0.018714796032277364 -0.07996354344549846; 0.005205925186465357 0.013427464449406765 -0.04596418991445679; 0.002465922654156774 0.0019582297647917075 -0.011903979833203186; 0.0015315862516894095 0.004780450342766442 -0.016995830844214504; 0.0002795108889757996 0.0010055085212243224 -0.0018046998092062212; -2.7510240899575366e-5 -0.0002893969658905866 -0.00014362139808820132; -0.00021594909654348984 0.00046845988710556767 0.0019776591305558453; 0.0002091389620655932 0.0007988491081477634 0.0005077386115228334; -0.0002525549640245875 -0.0009960278052345967 -0.001109868958442537; -1.3512234635166984e-5 0.0004211124129132127 -0.0032947711626276437; -8.726523530264065e-5 -0.0003124491344595852 0.0013264598002819656; 0.002227665867605909 -0.0025355853196947337 0.0033603192384882036] %
+
+Mass Used: 113.0816767402157 kg
+Launch C3: 92.38567554965297 km²/s²
+||V∞_in||: 5.3012107117114414e-9 km/s
diff --git a/archive/ES_0.5588608290973311 b/archive/ES_0.5588608290973311
new file mode 100644
index 0000000..7f71f9d
--- /dev/null
+++ b/archive/ES_0.5588608290973311
@@ -0,0 +1,22 @@
+archive/ES_0.5588608290973311---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T19:54:09.680
+Launch V∞: [7.935871426657628, -5.824400902909408, 0.11049305335605247] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.014574179496892532, 0.10562688242534478, 0.09857795412872768] km/s
+ V∞_out: [-0.02205805101228427, 0.01993845531028958, -0.14212035669325104] km/s
+ time of flight: 1.8063314984371436e8 seconds
+ arrival date: 2030-01-31T11:46:38.680
+ thrust profile: [0.24765793912474454 -0.009792198215552154 -0.0828562144701432; 0.14369936630022728 0.07598741120432884 -0.15838473339239936; 0.03560447069915167 0.03008157275318403 -0.0718223228860479; 0.041461961979152306 0.04651776007832339 -0.12152747999039047; 0.03733149751157822 0.05137581389171884 -0.14583463034249497; 0.01949335186016433 0.030958680848494704 -0.09736730557232659; 0.013087149384969491 0.023555906265289417 -0.07987325834504767; 0.008563494570680489 0.01718995061392166 -0.06223481618934985; 0.00022623765622460673 0.000912819697463776 -0.004935794620274154; 0.004604363947438456 0.011141480044020612 -0.04450824362365107; -0.00019820407525394332 0.0022762088547965704 -0.006512535166021779; 0.0004559988725805406 0.000864873644549004 -0.0006368048140844712; -0.0003875510538971496 -0.0007437664410919143 -0.0029727420852555626; -2.6355962708160343e-5 -0.0003133114247114235 0.0013433092808960321; 0.0012798983078969697 0.00145216864283645 -0.0009239670220974152; -0.0009777732372466329 -0.0004993349056129056 0.0016964632714140423; 0.00027546551516993034 -0.0001035035344858872 -0.0007425086554183414; 0.0005638183272620772 -0.0002161060249480088 0.0007460596997451475; -0.0002401044412486719 0.002058715786781463 -0.0026439434950937778; 0.007112034720486633 -0.003103387682177431 -0.004716936186996098] %
+
+Mass Used: 86.67315957051142 kg
+Launch C3: 96.91390989309285 km²/s²
+||V∞_in||: 0.1452138355636638 km/s
diff --git a/archive/ES_0.5588706678362498 b/archive/ES_0.5588706678362498
new file mode 100644
index 0000000..650b749
--- /dev/null
+++ b/archive/ES_0.5588706678362498
@@ -0,0 +1,22 @@
+archive/ES_0.5588706678362498---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T01:40:36.630
+Launch V∞: [7.877759711691267, -5.73966265254082, 0.11021387228050483] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.862385358670791e-10, -1.1145576546254635e-9, -1.3054989120089934e-9] km/s
+ V∞_out: [7.317070809116222e-10, -6.637578630989436e-10, 2.498900689425632e-10] km/s
+ time of flight: 1.843317578988845e8 seconds
+ arrival date: 2030-03-15T12:56:33.630
+ thrust profile: [0.4479690882087824 -0.010332042690570635 -0.1026926052509393; 0.03959963251275885 0.025436751081687897 -0.042851897589933276; 0.056815237359446005 0.06048973460812036 -0.10075939236958548; 0.05789057105458099 0.0882860567936614 -0.15875668254758443; 0.030641138597128702 0.058240652810967915 -0.12266468481748558; 0.015551199091524989 0.036561988692423254 -0.0816359134176157; 0.012390382842546184 0.03168798954361495 -0.0763779013629974; 0.006323518104461141 0.021919778292993096 -0.05573852620668071; 0.004264505894080717 0.01752927365122099 -0.04516658303863781; 0.0029747580178675096 0.0074134984866347795 -0.023065264486403093; 0.0008556593368252164 0.0036126177523492994 -0.010884298369552356; 4.4208150254422844e-5 0.00012005061263606023 -0.0015303106786437877; -0.0013181359116643512 0.0019692501397725374 -0.0021612431585651833; -0.00035034958127346834 -0.002557029348657006 -0.0032245705737926475; -0.0002988685756197726 -0.0011143274049539658 0.0016748824111805086; 0.00015066996313580758 0.00031046819552585906 0.0008306435447877946; -0.0038142591562314913 -0.000785734943384271 -0.0006270473568359325; -0.002950234643832614 -0.001207224414437635 0.00041019089573959616; 0.000985023570184723 -7.0001165056008015e-6 0.0032157578327662688; 0.0035006899518980586 -0.0005811296205324866 -0.005641162640063277] %
+
+Mass Used: 97.76177267201865 kg
+Launch C3: 95.01497253776105 km²/s²
+||V∞_in||: 1.9318345988196564e-9 km/s
diff --git a/archive/ES_0.5588728715158031 b/archive/ES_0.5588728715158031
new file mode 100644
index 0000000..18e80bd
--- /dev/null
+++ b/archive/ES_0.5588728715158031
@@ -0,0 +1,22 @@
+archive/ES_0.5588728715158031---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:48:15.670
+Launch V∞: [7.8227329241866626, -5.8072266814198645, 0.2995538994067874] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005294164102029635, 0.002969990835248354, 0.00023423638281365404] km/s
+ V∞_out: [-0.004286093078536087, -0.0024442329348520345, 0.003536962802621822] km/s
+ time of flight: 1.8749577787488812e8 seconds
+ arrival date: 2030-04-23T10:57:52.670
+ thrust profile: [0.43592596035152753 0.015377993149977554 -0.11334195537744618; 0.09432007399123134 0.06362884987511093 -0.09264592968646317; 0.03466874062097284 0.03797919778988427 -0.06431122023245686; 0.031626186143448885 0.04739114498285958 -0.08696130621636931; 0.020838330278458717 0.040064816170669114 -0.0810740587011781; 0.040986175076097704 0.09637000663836887 -0.19088379357159693; 0.007852178918122123 0.018082606390774084 -0.04583530730842208; 0.006117153522461644 0.01830585191729132 -0.047937358855170295; 0.004193264803456961 0.014775834941286042 -0.04070530083032563; -0.00033768830649438916 0.003132167496219985 -0.009793340998670564; 6.267535194043707e-5 0.0041703012218975875 -0.011471797286539678; -0.00048825513496297476 0.0026774118440738414 -0.01112463005158176; -0.0003226346464991236 0.002007757015179588 0.0019471296553140323; -0.0006978320986077974 -0.0009218983116961533 -0.0029563745157101624; 0.00031535132792727026 0.0015815112130827679 -0.00463990253238129; 0.0003494907016503275 0.002926482196865842 -0.0023923101074006937; 0.005036162551098959 0.0031831121104274134 0.0006106866424968615; 0.0019958980202469385 -0.006214375704241812 -0.0003449466020589366; 0.0020076141910205835 0.00703895321878069 -0.0021457172292740512; -0.0014438111750295678 0.0011482784357302622 -7.548405579535272e-5] %
+
+Mass Used: 97.80055618644519 kg
+Launch C3: 95.00876467119859 km²/s²
+||V∞_in||: 0.006074856852940001 km/s
diff --git a/archive/ES_0.5588837529909769 b/archive/ES_0.5588837529909769
new file mode 100644
index 0000000..3a77359
--- /dev/null
+++ b/archive/ES_0.5588837529909769
@@ -0,0 +1,22 @@
+archive/ES_0.5588837529909769---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:46:21.034
+Launch V∞: [7.908992125575889, -5.624722854544211, 0.2270888485376351] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.02018252029643191, 0.12323785824831945, 0.14565041394386474] km/s
+ V∞_out: [-0.08580043993121282, 0.05970483726506385, -0.16076546083328752] km/s
+ time of flight: 1.8749577787485224e8 seconds
+ arrival date: 2030-04-21T06:55:58.034
+ thrust profile: [0.44898856898422357 0.011048992624314847 -0.12639738196130362; 0.1472975044947421 0.09519514516902108 -0.14772523454840833; 0.06924766236399998 0.07374423664926046 -0.1300056160254951; 0.03835903490199312 0.055714636779129315 -0.11056106739369005; 0.03250708752759102 0.059800721065952946 -0.13123590783216552; 0.01430266393615751 0.03228847199348319 -0.07715227470574146; 0.005066660035224964 0.0142978318214365 -0.03709454889417231; 0.0032314897950328166 0.011677682786523886 -0.032502831769432965; 0.0013817386021533077 0.00807952345365238 -0.023945816817229147; -1.759551406265226e-5 0.0013024804049547015 -0.003923100042019195; -0.0005281679716502199 0.0010057653386096816 -0.0069302325764774245; -0.0006650845585108898 -0.00036440096141588003 -0.005115402503674276; -1.618692418062879e-5 -0.0006396669950961824 0.0018902173489606332; -0.0012373377527891314 -0.0019669656296586974 0.000163985279023044; 0.0016320254647854517 -0.0004121321314859844 0.004407288059561514; -2.5263283085640722e-5 -0.0013093463108561096 0.002923548904448259; 0.00034107677678345147 -0.0024359636268814835 0.0035609315442883226; -0.0006426624900229448 0.0009839322037649158 0.0013993510627364047; -0.00043191485267083263 0.002001351971982829 0.001420421486417843; -0.001815267114978057 -0.0097229838307935 0.0004812130102311978] %
+
+Mass Used: 102.29051945123592 kg
+Launch C3: 94.24123297798353 km²/s²
+||V∞_in||: 0.19185657901976652 km/s
diff --git a/archive/ES_0.5588919446246942 b/archive/ES_0.5588919446246942
new file mode 100644
index 0000000..732abba
--- /dev/null
+++ b/archive/ES_0.5588919446246942
@@ -0,0 +1,22 @@
+archive/ES_0.5588919446246942---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:37:16.991
+Launch V∞: [8.02316659655846, -5.732079328628842, -0.01727887392857708] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.698997596174517e-10, 9.654009824279457e-10, -2.3292376527320274e-10] km/s
+ V∞_out: [6.656954171374522e-11, -2.681106922163552e-10, -3.5365154602626047e-10] km/s
+ time of flight: 1.863545171552871e8 seconds
+ arrival date: 2030-04-10T20:45:53.991
+ thrust profile: [0.3028358419908613 -0.008684870904046698 -0.10592678707375203; 0.04446342232609345 0.02247740464324755 -0.05326838812824649; 0.036866936431306174 0.02931158103020805 -0.07903481432157412; 0.04122157909071438 0.041788743242672115 -0.12935921235012496; 0.0369323694740832 0.044585290267043616 -0.1541523618624301; 0.023025135595961112 0.03139957379071668 -0.1200207741988831; 0.008916405664003813 0.014029237661154275 -0.057548797508571; 0.004575162842198393 0.00826983087467789 -0.03630251454108754; 0.002468792837078784 0.0022943598220245684 -0.019663194657251568; 0.0020710261733288293 0.004266132960145807 -0.01977609491092958; 0.0016907333467246959 0.0021566358978729275 -0.013647653995284224; 0.0012725437023400421 0.003554735337025035 -0.01779093475031409; 0.0014874599413085914 0.002605006047070999 -0.005743265426470666; -0.0008872716693125798 0.0002009044844913863 6.731868547960431e-5; 0.0004845699043514455 -0.000472802612935645 0.002318604472526171; 0.00474257703390741 0.003928372796054123 -0.005709285304301782; -0.0006326290243801765 0.001176726479967046 0.00595897539858693; -0.0029016314320141692 0.006693835478507916 0.004743255493142117; 0.00435147280691704 0.002880070867296534 -0.0071943740732879225; -0.00015575051643505096 0.012265771633660657 -0.005179343001009483] %
+
+Mass Used: 84.87590241450289 kg
+Launch C3: 97.22823422530976 km²/s²
+||V∞_in||: 1.0075308757650838e-9 km/s
diff --git a/archive/ES_0.558896149436322 b/archive/ES_0.558896149436322
new file mode 100644
index 0000000..3db928f
--- /dev/null
+++ b/archive/ES_0.558896149436322
@@ -0,0 +1,22 @@
+archive/ES_0.558896149436322---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T02:41:11.006
+Launch V∞: [7.9311743609353895, -5.690051685221918, 0.007577593086526759] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1305109415278341e-8, 6.609213725914213e-9, -9.701897518211869e-9] km/s
+ V∞_out: [7.010486238538744e-9, 1.39875984097548e-8, 4.3872663678852837e-10] km/s
+ time of flight: 1.8710192315295434e8 seconds
+ arrival date: 2030-04-17T15:26:34.006
+ thrust profile: [0.3988138342328143 0.011699519427602967 -0.1120158682812046; 0.09342794400107553 0.061494188393404356 -0.0941130449621049; 0.04800331994512504 0.05202934359209592 -0.08936448778589919; 0.0466381111650456 0.06846028030056907 -0.12929382459331362; 0.014783622334560823 0.02745570768430989 -0.05878806777330534; 0.0269845181042185 0.06174253346551572 -0.13559914913758306; 0.008645625048484812 0.024729055960109946 -0.06006965941000491; 0.00437630366936149 0.015199445050599093 -0.039406049316602784; 0.004475270874064562 0.016264440701414293 -0.04286581492141841; 0.003417024641340824 0.015145178830356048 -0.042621782664971165; 0.000822298323555791 0.0010272771949418227 -0.003757222686318681; 0.0011441052246532772 0.00195393160464346 -0.007029713664415666; -0.0017804756111190374 -0.0007451956227522158 -0.004549296484395505; 0.0011046508416162112 0.002431850989862796 -0.0055489149441156635; 0.0024501978494887926 -0.0005823731828376791 -0.0001459107206021014; -0.0017730336670342996 -0.0038030596038755166 -0.001127535148852019; -0.002635270012281676 -0.002052373626635051 -0.0013015174422829302; 0.000916129963311923 -0.0021512501932970766 0.002054611421810344; -0.003981562319805587 0.0005178132158977335 0.008917479426732171; -0.0003297736044009826 -0.00018346557715063138 0.0002964132406789626] %
+
+Mass Used: 96.24391900253522 kg
+Launch C3: 95.28027234397265 km²/s²
+||V∞_in||: 1.629766917139115e-8 km/s
diff --git a/archive/ES_0.5589008280325164 b/archive/ES_0.5589008280325164
new file mode 100644
index 0000000..e16093c
--- /dev/null
+++ b/archive/ES_0.5589008280325164
@@ -0,0 +1,22 @@
+archive/ES_0.5589008280325164---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T23:21:58.169
+Launch V∞: [7.632470503620281, -5.767157425576644, 0.5776576145741553] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.019099626356181967, -0.12008216057726374, -0.15813648569762] km/s
+ V∞_out: [0.10279226753331526, -0.073794036384957, 0.1541085737768173] km/s
+ time of flight: 1.852012435276079e8 seconds
+ arrival date: 2030-03-25T12:09:21.169
+ thrust profile: [0.7016256191773028 -0.0018077761030526282 -0.16686002227198823; 0.1115420598430141 0.07369553674634152 -0.10930060861353885; 0.06335009893683931 0.07077445676365489 -0.11522604707269711; 0.03545635845382738 0.05471331119961648 -0.09922347689843304; 0.020336847531959374 0.04009114099437008 -0.08380359580536306; 0.02777769689254406 0.05821020509706263 -0.1282975812796982; 0.006813998103047715 0.01907252804412974 -0.046952091512994766; 0.003740697710180555 0.011995743239608501 -0.032995218174793194; 0.003063722039465347 0.011763010426978644 -0.035538053533948066; 0.00011592279314568581 0.0011132653496349408 -0.003121957292889464; 0.0013706895344107648 0.008342057525230921 -0.024896990241393895; -0.0005308966335835723 0.0011054213362052534 -0.0029860635503817555; 0.0009552629085204248 0.0011151842879339611 -0.0006306968116032399; -0.0002524781113374334 0.00010832200247279616 0.00018718333742778412; 0.0007552157536803892 -7.274084047734415e-5 -0.002194644657405274; 0.0004558472592084686 0.0015714292979139973 -0.0028908595628367876; 3.0224995823062168e-5 0.0003393341642309656 0.0015389804864171146; -0.00374881923521285 -0.0002782059857620759 0.0029324532819077725; 0.0007446519134694988 0.001168801546498986 -1.282188217343206e-6; -4.8272019488580794e-5 -0.0024947725641814365 -0.002929138480206512] %
+
+Mass Used: 116.26863807306017 kg
+Launch C3: 91.84839907969297 km²/s²
+||V∞_in||: 0.1994784928874366 km/s
diff --git a/archive/ES_0.5589027719564661 b/archive/ES_0.5589027719564661
new file mode 100644
index 0000000..0345aec
--- /dev/null
+++ b/archive/ES_0.5589027719564661
@@ -0,0 +1,22 @@
+archive/ES_0.5589027719564661---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T20:16:28.865
+Launch V∞: [7.933824808551773, -5.7439694609233864, 0.12256627030067242] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.76047759327457e-6, 0.00023467527141308499, 4.18253698499919e-6] km/s
+ V∞_out: [0.00022902030211431368, -2.900067770165627e-5, 4.31650817066854e-5] km/s
+ time of flight: 1.8566547808956227e8 seconds
+ arrival date: 2030-04-01T18:01:06.865
+ thrust profile: [0.38318250638045404 0.00036458654931880157 -0.1156908952680443; 0.06589239645719819 0.03753237740085945 -0.07370933323978093; 0.04500818829740486 0.04377671824532854 -0.09267171311048898; 0.03279194833302376 0.04290823566836019 -0.10118423113339847; 0.029817299306122258 0.047069967066096216 -0.1207102739329363; 0.013458633736584019 0.025929327721948038 -0.07419915148476326; 0.015349935970630437 0.029851262187562413 -0.08980076918978105; 0.012474787907200488 0.03012991737392049 -0.09787512187924952; 0.004264708552570237 0.008354236794231102 -0.03237002099396295; 0.0005343463898225054 0.0004411038155214848 -0.0002984157940245236; 0.007161122007634383 -0.0062466253638756245 -0.005715439499875824; 0.0015547070918422489 0.0011423686516327505 0.0004825704154823301; -0.001523108426894826 0.002073330689615272 -0.00707111451905393; 0.002041150047024606 9.608742054971649e-6 -0.010526883522378993; -0.0033414675148965827 0.0023234279888480363 -0.008301011869597866; -0.0022945700762907824 -0.005224088181044214 -0.0011803372259209016; 0.0003450192704775512 0.0011680124534864528 -0.001825279924452099; -0.0018082581335331018 0.003079094468034093 -0.008151222285398607; -0.00625993148378007 0.006030639161060825 0.0024451255755383473; -0.0032795156075417 -0.0006717609654439458 0.0007422946580905477] %
+
+Mass Used: 92.32282873255008 kg
+Launch C3: 95.9537837514275 km²/s²
+||V∞_in||: 0.00023491539658201377 km/s
diff --git a/archive/ES_0.5589082788497237 b/archive/ES_0.5589082788497237
new file mode 100644
index 0000000..09eed7d
--- /dev/null
+++ b/archive/ES_0.5589082788497237
@@ -0,0 +1,22 @@
+archive/ES_0.5589082788497237---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T02:24:19.695
+Launch V∞: [8.082976521693553, -5.7278427033039065, 0.05691649551411135] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0021820574755982165, -0.0013641723847027133, -9.229966863398752e-5] km/s
+ V∞_out: [0.001879760714035645, 0.000852305455489393, -0.0015348165110913982] km/s
+ time of flight: 1.8586539848748222e8 seconds
+ arrival date: 2030-04-05T07:40:57.695
+ thrust profile: [0.2391330216452412 -0.007587686571890055 -0.08418543876834968; 0.053977582993764546 0.02599472929292651 -0.07098964136540459; 0.03301980653956835 0.026062191724432977 -0.07755083440205982; 0.02358685081958448 0.02491193856610094 -0.08076040552852887; 0.017761905462248845 0.02269448598351535 -0.08351240125182235; 0.013611764692037412 0.02079552598120195 -0.08114800728138132; 0.012023248493284145 0.018334163059884324 -0.07953257655491133; 0.007481681954179524 0.013152061491358348 -0.06874340160242498; 0.01038017129482331 0.02142242439320497 -0.10030466367285047; 0.007835485582092393 0.014372240880218053 -0.06723295417568557; 0.0018822512416454536 0.003153714561077349 -0.017091604024800422; 0.00040753134486904417 0.0005791998860951184 -0.0054854281283784855; 0.0023988732599732375 0.000411347184484738 -0.0039113699430908325; 0.0029594032466857714 0.000599879607073209 -0.0005399803723635764; 0.0015298783365620427 -0.002060419658226665 -0.0008561758699198555; -0.0015171777360193826 -0.0010206938213559217 0.005608934022607558; -0.0005513664957733954 0.003739315335456867 0.0032841119393499027; 0.0010479357861524763 0.0007714442465418193 -0.003272509859457899; 0.0021757917021959098 -0.0006544087511018387 -0.000467454906599597; -0.0027862683146069305 0.0012842593817697272 0.002104965392642828] %
+
+Mass Used: 79.54172799091248 kg
+Launch C3: 98.14593097150261 km²/s²
+||V∞_in||: 0.0025750456987846822 km/s
diff --git a/archive/ES_0.5589242185811312 b/archive/ES_0.5589242185811312
new file mode 100644
index 0000000..52335b0
--- /dev/null
+++ b/archive/ES_0.5589242185811312
@@ -0,0 +1,22 @@
+archive/ES_0.5589242185811312---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:07:19.671
+Launch V∞: [7.728685570579666, -5.7792261495067105, 0.2156552918068296] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.07754725653451996, -0.44268819428603867, -0.6405477545232795] km/s
+ V∞_out: [0.33481763272328174, 0.15914039343352784, 0.6885834960480645] km/s
+ time of flight: 1.841807229846551e8 seconds
+ arrival date: 2030-03-12T23:26:01.671
+ thrust profile: [0.5150434592312306 0.003645514858358353 -0.12468356040152485; 0.1869753317868984 0.120316458507851 -0.16300237737969006; 0.0417517204323041 0.045062059611664526 -0.07294597233987189; 0.02744217151788338 0.03943495374500119 -0.07222407967415895; 0.028717317090825964 0.056238595403451504 -0.10676639913110977; 0.03413984157255523 0.07885456221314993 -0.1567465961348576; 0.013783935631017902 0.036476450411204224 -0.0826210404235288; 0.006108854938174416 0.020747095736963893 -0.04918717935990979; 0.0012367544427133754 0.005754204056422212 -0.013713163116784612; 0.0008632095343847066 0.003628621968725169 -0.010647512593448812; 7.137905239831553e-5 0.0006950847766475539 -0.001107913344465886; 0.00024748809425791313 0.00036090341828721464 -0.0018473799239923055; 9.11632490002281e-5 -0.00016166271180565362 0.0004873260190136556; -0.00035193174937943046 0.0005727682207522177 -0.0005356209248846633; -1.0890626177853363e-5 -0.0006754304160792631 -0.0006983794652851366; -8.433848487500242e-5 -0.00032124304569903595 -0.001023367669028189; 0.0005323620724780574 0.001924646261608525 0.0027608856760679; 0.0011160472678325465 0.0004512445158302769 0.0012500763711584524; 0.0010712611814912738 -0.0011757990690148654 -0.002701605641069247; 0.001119094554187083 -0.002264099284977592 0.0019442458692963823] %
+
+Mass Used: 108.5367556893284 kg
+Launch C3: 93.17854274091279 km²/s²
+||V∞_in||: 0.7824882364490087 km/s
diff --git a/archive/ES_0.5589284294025506 b/archive/ES_0.5589284294025506
new file mode 100644
index 0000000..785bdc2
--- /dev/null
+++ b/archive/ES_0.5589284294025506
@@ -0,0 +1,22 @@
+archive/ES_0.5589284294025506---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T10:49:29.663
+Launch V∞: [7.964863740810984, -5.771714646413308, 0.05734645885389462] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003245638022559665, 0.0018926719430010018, 0.00013797458770523346] km/s
+ V∞_out: [-0.0025914817547177523, -0.0016328798512384819, 0.0021898169785148055] km/s
+ time of flight: 1.8334301322301048e8 seconds
+ arrival date: 2030-03-05T11:26:22.663
+ thrust profile: [0.3301367210859228 -0.015847791804535577 -0.11415934752113548; 0.017431486442167663 0.008664453798936623 -0.023187020300121472; 0.08865827388856036 0.0703402206850493 -0.18507700408219724; 0.04321142478869749 0.044156637043359294 -0.13396084154551793; 0.03441599737749218 0.04195062122735892 -0.14157472504091967; 0.0188818926538359 0.0264994581712852 -0.09914937729438966; 0.006735343207588022 0.01076133626287276 -0.045479838049103626; 0.002932790454422007 0.004772417605103378 -0.02257789781887915; 0.0008498274412983627 0.0018466863621720536 -0.010263677132785008; 0.003955035315459733 0.007969442427502527 -0.03729020116106175; 0.001967123592320507 0.004187737219908904 -0.021762444159228435; 0.00029807840838721333 0.003082839040272887 -0.011935404476604851; 0.0027471800018356134 0.0010120362064672183 -0.0062461451114730155; 0.0039105596472797065 0.004114337142852007 0.0001567508187524545; -0.001750043259072843 0.00031290200782235094 0.002207839463928769; 0.0002936100245313298 0.0011804392139777948 0.0010333581568604836; 0.002093985784228381 0.0018063667903506569 0.0004333257475744399; 0.0034670593526131654 -0.009786115131257976 -0.0015299058514691539; 0.0015547626191040201 -0.0001981374569595462 0.004969311858916652; 0.000636916316692169 0.006179928446906114 -0.009366039638313872] %
+
+Mass Used: 87.67880855334761 kg
+Launch C3: 96.75503298565053 km²/s²
+||V∞_in||: 0.0037597087977874867 km/s
diff --git a/archive/ES_0.5589293122617244 b/archive/ES_0.5589293122617244
new file mode 100644
index 0000000..ca6d4cf
--- /dev/null
+++ b/archive/ES_0.5589293122617244
@@ -0,0 +1,22 @@
+archive/ES_0.5589293122617244---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T02:11:45.296
+Launch V∞: [7.86658471201367, -5.947921232096535, 0.08503665997886452] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.015419743958908686, 0.09254034969306903, 0.08689809234830687] km/s
+ V∞_out: [-0.022442465100024678, 0.021211166997729902, -0.12408681735962102] km/s
+ time of flight: 1.8391671044466826e8 seconds
+ arrival date: 2030-03-13T18:10:15.296
+ thrust profile: [0.2164741236793693 -0.006955517737750107 -0.07610409951751984; 0.15594093668972422 0.08004615970145787 -0.1784761787535521; 0.05654735001263477 0.04601593673630158 -0.1191551252573043; 0.03993065305542302 0.04194789547419334 -0.12359944861399225; 0.02668100990227465 0.033460569123255866 -0.11063643580974629; 0.010108424133767302 0.014629178740885655 -0.055290481335894065; 0.016944703264273813 0.02753691497347923 -0.10712628124662785; 0.003956872188318645 0.007080317995265397 -0.03138859473466647; 0.002095252070051917 0.004044575585157252 -0.020164282056398364; 0.001843225765243442 0.0029115771330439195 -0.012476885975808538; 0.00029058231111739 -4.875213146394568e-5 -0.002037082021847355; -0.0005858165659392719 0.0015870234313180194 -0.006511486877572909; -0.00019361501999192658 0.0008203896324001234 -0.006056608058995362; -0.0011496891729844503 -0.0004940658750560663 0.0007670444090523993; -0.00038784228280569195 0.0027380772707447636 0.00013781093445128928; -0.00017528916724067652 0.0003238832442071957 0.002508166906503996; -0.002393986554010766 -0.0014444602572808328 0.001674536564549585; -0.004254714239993559 -0.003073641484890732 -0.004460062559294131; 0.007640309528119114 -0.0010958525254915312 0.0028079812942301565; 0.000893887117912621 0.00044960514806850597 0.005716982423318264] %
+
+Mass Used: 84.68663702504 kg
+Launch C3: 97.26815324805231 km²/s²
+||V∞_in||: 0.1278779233442922 km/s
diff --git a/archive/ES_0.5589349545430271 b/archive/ES_0.5589349545430271
new file mode 100644
index 0000000..3e73620
--- /dev/null
+++ b/archive/ES_0.5589349545430271
@@ -0,0 +1,22 @@
+archive/ES_0.5589349545430271---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:27:54.085
+Launch V∞: [8.10274629139003, -5.698086762933311, 0.22672936896161053] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.85337301585209e-5, 5.759710839609408e-5, 0.0037809832450948467] km/s
+ V∞_out: [-0.0034492571074146933, -0.001158778126098134, 0.0010319482196792457] km/s
+ time of flight: 1.8749577787320295e8 seconds
+ arrival date: 2030-04-23T20:37:31.085
+ thrust profile: [0.17844847579836484 0.001499208754078939 -0.05761372375911134; 0.0800352457037786 0.04677792686421258 -0.08966722513879966; 0.05677702833683778 0.05310902849242068 -0.11426001314839408; 0.03847394044080408 0.04723633920615317 -0.11607168431362296; 0.02786376005489981 0.04172922104646419 -0.11389593363289549; 0.018444261010621684 0.03261124724341364 -0.09786580353293263; 0.012329520981823152 0.025202733826105758 -0.08181831900261952; 0.005306349850561732 0.013073045415837694 -0.04623688473146658; 0.001457876583898566 0.0032261705747728955 -0.012360714108669714; 0.0014729217146094331 0.003562685732087282 -0.014246896589198397; 0.001875970494651171 0.0017912257849549416 -0.005877593716429638; -0.00034438413511044636 0.00500997922649003 -0.008703589913203458; -0.0016674440290298251 0.00029931210564111514 -0.006603254638713848; 0.00047672702260913736 0.0005995886124249037 -0.001525810897013639; -0.0005536734740632463 0.0005284380817498672 -0.005413357971179278; 0.015525900909333933 0.0037472641581932785 -0.0015740601038491397; -0.0011557542497809018 0.007658095720145448 0.0011326506657061393; 0.002623266279186694 0.004849048917080014 -0.015773578498666698; 0.00010251556756322995 4.5949960977495485e-7 4.864115975510008e-5; -0.012041969661085422 -0.008876748358004057 7.65651981984583e-5] %
+
+Mass Used: 79.40855114094575 kg
+Launch C3: 98.17409642730044 km²/s²
+||V∞_in||: 0.003782237336994621 km/s
diff --git a/archive/ES_0.5589365779303144 b/archive/ES_0.5589365779303144
new file mode 100644
index 0000000..b2454c9
--- /dev/null
+++ b/archive/ES_0.5589365779303144
@@ -0,0 +1,22 @@
+archive/ES_0.5589365779303144---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T09:58:45.336
+Launch V∞: [8.047934594907773, -5.764833847777766, 0.2470060104604119] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0019177414527515673, 0.0013136135313490944, 8.015866898682351e-5] km/s
+ V∞_out: [-0.0017559698420753166, -0.0007943185930656321, 0.0013330539603767357] km/s
+ time of flight: 1.8749577785416132e8 seconds
+ arrival date: 2030-04-24T12:08:22.336
+ thrust profile: [0.21208171374573484 0.004172376605904584 -0.06655818339789187; 0.06914360818827421 0.04477227675099509 -0.08039449676581012; 0.04621805160409795 0.04619470062834698 -0.09448094338583762; 0.02392522430816121 0.03223015313633933 -0.07509417681320639; 0.020904819362065556 0.03765999433082216 -0.0920770716981032; 0.015311063605244183 0.03337571958675499 -0.08807391298450523; 0.013335191613068419 0.03191000124809535 -0.09084704591351161; 0.00753713021695016 0.021328191393020206 -0.06461135867278081; 0.003476864044267827 0.0134995612419052 -0.045162658366385715; 0.005398843028466997 0.019902741102348756 -0.06877155695134783; 0.0013516281090471792 0.00166612852862552 -0.0012333714254938498; 0.0005713184183724891 0.0036360640385663117 -0.011489933299944499; 0.0015982012046939931 0.0022573390814844417 -0.000663632808017062; -0.0023275937075857367 -0.0047324067047400204 0.0024965950585486402; 0.0024375344044887245 -0.005505447083985257 -0.0020029207589056055; 0.0017072904621249453 -0.002077978846097622 -0.00389685651778889; -0.006007368123397407 -0.00505792539894061 -0.007056585626044466; 0.0017925101067636077 -0.0010840428762857901 0.0003933692925485446; 0.00319604836193652 0.0005094517198679222 -0.001061140391365892; 5.4787900322133295e-5 0.002372550594259061 0.0011383777652156555] %
+
+Mass Used: 80.05516796936035 kg
+Launch C3: 98.0635725056011 km²/s²
+||V∞_in||: 0.002325884391271172 km/s
diff --git a/archive/ES_0.5589368089442182 b/archive/ES_0.5589368089442182
new file mode 100644
index 0000000..b597d9c
--- /dev/null
+++ b/archive/ES_0.5589368089442182
@@ -0,0 +1,22 @@
+archive/ES_0.5589368089442182---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T06:19:13.453
+Launch V∞: [7.866587693901174, -5.687991227786578, 0.004040471782859926] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.200810220500803e-7, 6.94511265093905e-6, -1.5677259951544956e-6] km/s
+ V∞_out: [1.0293344049581805e-6, -3.975170451034373e-6, -5.7278781164779016e-6] km/s
+ time of flight: 1.8749577787483254e8 seconds
+ arrival date: 2030-04-22T08:28:50.453
+ thrust profile: [0.4899066245796822 0.007803831107287775 -0.11886277957371347; 0.11377907628852527 0.0756131617047392 -0.11099549806120579; 0.04259463929047493 0.046835793391893914 -0.08477907401195854; 0.025579309841299948 0.03881937839538876 -0.07706693879471181; 0.0151655194878253 0.032556701079899095 -0.07108075222862359; 0.012412112860240713 0.027773740534846107 -0.06723537108536518; 0.003645859887901288 0.01042042065921198 -0.029678729067812746; 0.033019233741312846 0.08751866414098722 -0.22296754129269733; 0.00107580237194017 0.0038838058468163546 -0.012102850413527216; 0.0009783367352355125 0.004346224594994331 -0.011166496349748253; 0.0012379077983868884 0.005258169518545216 -0.01880196224219231; 0.00011000787902761184 -0.00037709281191097334 -0.00026761351682513985; 0.0003332231816713842 0.0003826147160697638 -0.0012371418873280441; 0.0002987319870444704 0.000545855395866699 -0.0007434011077091843; -0.0005296210555058914 -0.0035572110124950642 -0.00024387752517154447; -0.0025399955256063577 -0.0008825527001485048 0.001610526678758518; -0.00423379577602419 0.0005049957735851013 0.0011019613512061092; 5.595460572924691e-5 -0.0017115806229865917 0.002509346639668404; -0.001889992605632978 -0.0027624849587187415 -0.004068871821199946; -0.0014884918963878968 -0.001053043965805379 2.279364592215231e-5] %
+
+Mass Used: 102.38024597626554 kg
+Launch C3: 94.23646247862668 km²/s²
+||V∞_in||: 7.1669301247356595e-6 km/s
diff --git a/archive/ES_0.558941838206383 b/archive/ES_0.558941838206383
new file mode 100644
index 0000000..255fb9b
--- /dev/null
+++ b/archive/ES_0.558941838206383
@@ -0,0 +1,22 @@
+archive/ES_0.558941838206383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:55:39.871
+Launch V∞: [8.04599126330741, -5.767317503521621, 0.09400031040637756] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2637159192593738e-5, -2.0864654362604635e-5, -9.211709167177464e-5] km/s
+ V∞_out: [-8.701000416723068e-5, -1.01719855467747e-5, 3.7055378887156685e-5] km/s
+ time of flight: 1.8430278841463128e8 seconds
+ arrival date: 2030-03-17T09:08:47.871
+ thrust profile: [0.22576753198430755 -0.0061779037583529605 -0.07801235330633721; 0.06119943136321726 0.03136178471005857 -0.07727930771858418; 0.039480785975172225 0.031983752623796255 -0.08831022580725328; 0.04099395647191182 0.04181005588108715 -0.12631454594425917; 0.021551207118390092 0.02816092951158314 -0.09446159721944089; 0.013132498467546381 0.018762206722224742 -0.07163659137935709; 0.01495775801608952 0.025915868472215362 -0.10242804542591533; 0.011362080126795016 0.022444731354361952 -0.09569558458798368; 0.004524600317872273 0.008935968592034087 -0.04231563304776098; 0.0035658995906446894 0.00762867726032972 -0.03680518764146798; 0.0016654554762708807 -0.0017096853927092554 -0.0018155389618796742; 0.000256340108319981 0.00020959033584054223 0.0005547429925850107; -0.0012033820892899019 -0.000928078608651623 -0.0039452951671670854; -0.0008950116015354408 -0.00015317157138851518 0.004464734210440708; -0.0019607037074129887 0.0031468469367218763 -0.0030318780952586655; -0.007050832456289248 0.0029859913385736807 0.0010229301093829944; 0.00027935054778924825 -3.4431290077954735e-5 -0.0010062441026700056; 0.00395214529509437 -0.00023529941702122204 -0.008948747918483418; 0.0016177982470324188 0.006622191208513514 -0.009356047704624565; -1.777510973605535e-5 0.0002152674852928838 -0.001421582423847557] %
+
+Mass Used: 80.38102909243207 kg
+Launch C3: 98.00876265400252 km²/s²
+||V∞_in||: 9.529213069396678e-5 km/s
diff --git a/archive/ES_0.5589504560976121 b/archive/ES_0.5589504560976121
new file mode 100644
index 0000000..2eb056f
--- /dev/null
+++ b/archive/ES_0.5589504560976121
@@ -0,0 +1,22 @@
+archive/ES_0.5589504560976121---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T20:38:23.209
+Launch V∞: [7.903620961425289, -5.850318253953609, 0.10256722855685513] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.024453649671534e-10, -1.0365280044227882e-9, -1.275423832810138e-9] km/s
+ V∞_out: [7.893386870942031e-10, -8.137237713645259e-10, 2.8316005873423534e-10] km/s
+ time of flight: 1.8749577787495843e8 seconds
+ arrival date: 2030-04-24T22:48:00.209
+ thrust profile: [0.2888526358210569 -0.0005373546496685555 -0.08971009486965338; 0.1360139872403782 0.07848857201850125 -0.14523886425128726; 0.041972566716924446 0.037783154948083666 -0.08604882962843756; 0.027349926953994633 0.03351607022834982 -0.08440467456615053; 0.024447247243818634 0.03631385495383325 -0.09935787125167334; 0.016542668726504544 0.029076490759520283 -0.08693058990802366; 0.01883948027850248 0.0413695314648145 -0.12848079164500625; 0.0017226907803103233 0.007937063436026678 -0.0290016599135613; -0.00032190953883436796 0.004989177657634665 -0.020757744077341427; 0.0009799211888358412 0.006261986506388767 -0.022417151176556696; -0.0011330904348328314 0.0008140756682266129 -0.0038378728158882797; -0.0001320294591466425 0.0006999464786034088 -0.0007558257003652106; -0.0010292777340131065 0.0006565785669090714 -0.0016039949077480782; 0.003270939614833216 1.2754847905998553e-5 -0.0016123889608420394; -0.0011771266170388969 0.002166071581185637 -0.004755959510287873; 0.0028690744717566868 -0.0033412645174758426 -0.0017200894293460385; 0.0024497050507189663 -0.0030256812031589247 -0.0032750505423920578; -0.0028614151690396464 -0.005255201420233107 0.004510953575777009; 0.0002053366527658994 -0.003009641309917369 -0.013555125424758426; -0.003582687812435013 -0.000802187267392331 0.0025674063235639004] %
+
+Mass Used: 88.00238538422673 kg
+Launch C3: 96.70396801079784 km²/s²
+||V∞_in||: 1.828938167628982e-9 km/s
diff --git a/archive/ES_0.5589571144623874 b/archive/ES_0.5589571144623874
new file mode 100644
index 0000000..8c7e77a
--- /dev/null
+++ b/archive/ES_0.5589571144623874
@@ -0,0 +1,22 @@
+archive/ES_0.5589571144623874---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:53:00.961
+Launch V∞: [7.889120724029373, -5.539277399182598, 0.23969621201924673] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5024954029142182e-5, 1.2778831752409643e-5, -9.936454090690457e-6] km/s
+ V∞_out: [2.657304053408322e-6, 2.1897126432058278e-5, -1.0084811990162523e-6] km/s
+ time of flight: 1.8749577787313774e8 seconds
+ arrival date: 2030-04-19T18:02:37.961
+ thrust profile: [0.5733957452800882 0.011116717223096593 -0.14061425193175908; 0.1427971302479441 0.09515394334634908 -0.1328003899552773; 0.0650141493994011 0.07233350653194665 -0.11544930562220036; 0.04875404826343558 0.07358816805416507 -0.1300077989296011; 0.025199441984912686 0.04839253286108897 -0.09562727214206876; 0.008781962941988424 0.02041795316814828 -0.04600353369184571; 0.01668023835617847 0.04864888006011975 -0.1083833722190599; 0.0038781334942367372 0.013580654346097454 -0.03409892941978885; 0.0006085846667919137 0.0028393909368822808 -0.007573625101830415; 0.0014767045385383542 0.0056209559026949695 -0.014320185842308668; 8.373404668662787e-5 0.0005831788753070403 -0.0021674121311544537; 0.0005950226751944436 0.0012001186296550484 0.00020657750931966804; 0.0004956918592115057 -0.001342575472508976 -0.0007109471302934307; 1.993146997107163e-5 -0.00010663423577756632 -0.0004090368759956258; 0.00015938913772241498 -0.00023605944274105155 5.674567681216672e-5; -0.0004504228114102208 0.0004043555409869343 -0.00043381290445783556; 0.00038257078511666834 -8.067726892087724e-5 -0.00018127120431954522; -0.001087218136198074 -0.00012271214358581067 0.0017502721314254014; 0.0012301783978130709 -0.0003219919571663404 0.001872344197347061; 0.0003635301051156092 0.0011519186204206118 -0.0002431308329082539] %
+
+Mass Used: 109.73753417092803 kg
+Launch C3: 92.97927417746124 km²/s²
+||V∞_in||: 2.208576248243714e-5 km/s
diff --git a/archive/ES_0.5589639432310278 b/archive/ES_0.5589639432310278
new file mode 100644
index 0000000..0246625
--- /dev/null
+++ b/archive/ES_0.5589639432310278
@@ -0,0 +1,22 @@
+archive/ES_0.5589639432310278---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:50:12.234
+Launch V∞: [7.73848214472318, -5.790862015338701, 0.1900342661566474] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.21583621122313623, 1.2421318959800773, 1.5664579157288203] km/s
+ V∞_out: [-0.8280599905248214, 0.6828420176849515, -1.6985742934563246] km/s
+ time of flight: 1.8749577787597638e8 seconds
+ arrival date: 2030-04-22T01:59:49.234
+ thrust profile: [0.46819629761756704 0.019401180820143263 -0.11011069436687823; 0.18832887464086215 0.13368414084382185 -0.16432052307044245; 0.05819044555292632 0.07111426271951755 -0.10899042434973938; 0.03816845330192307 0.06403220414262088 -0.10928403868065326; 0.025761436386223302 0.0538716567875177 -0.10108911353625787; 0.013934071830270605 0.03596047869067594 -0.07270666060409316; 0.007192239034198304 0.02323351903748884 -0.050860782483427666; 0.0035896228167109773 0.015068125569606398 -0.03487719722129253; 0.0015154678023804782 0.0067968377453410484 -0.01723511777061543; 0.0017090409050014934 0.007112869417910717 -0.01880902769736296; 0.0011807000768851465 0.01213980283548589 -0.03150978016920786; -5.201046917903125e-5 0.0014205784523971734 -0.0022481385819395055; -0.0001711449380369963 0.001027037754072087 -0.00390695465315678; 0.0005604488191233485 0.00081849611491927 -0.0021627113667981564; 0.00038035362214679735 0.00161850894336229 2.1112547550948806e-5; 0.003697865315431351 0.0013889233771603924 0.002336815229253988; -0.0001355709462354573 0.00030915076983272817 -0.0017762068358974192; 0.0010362901207673228 0.0010913443762282505 -0.0018236068947194266; -0.00034017595283651733 -0.0035451338919448416 -0.004285571644841365; 0.000367192011113233 0.0006269326699446203 0.001083131396627161] %
+
+Mass Used: 106.9745065608322 kg
+Launch C3: 93.45430180720577 km²/s²
+||V∞_in||: 2.010787735897477 km/s
diff --git a/archive/ES_0.5589741701430776 b/archive/ES_0.5589741701430776
new file mode 100644
index 0000000..da45415
--- /dev/null
+++ b/archive/ES_0.5589741701430776
@@ -0,0 +1,22 @@
+archive/ES_0.5589741701430776---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:34:00.450
+Launch V∞: [7.706584345063749, -5.607946746114325, 0.11470836977223903] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.3926767445062054e-5, -4.218715341341307e-5, -3.4656351099008416e-5] km/s
+ V∞_out: [-6.460103372613171e-6, 5.092835304811674e-5, -5.694466007698775e-5] km/s
+ time of flight: 1.8749577787491214e8 seconds
+ arrival date: 2030-04-21T06:43:37.450
+ thrust profile: [0.8371531211853754 0.009093657973709751 -0.19359816781071781; 0.06160990729497251 0.039843600584054555 -0.06885812958804038; 0.052601388555201065 0.05822712775057972 -0.10908696443170372; 0.00957635647122439 0.013524714750424277 -0.03026936243764026; 0.020569998190123985 0.037092596223030724 -0.0893012738115427; 0.01633315769224249 0.03704838999867346 -0.09646925255872088; 0.007107919070951149 0.018582057136324173 -0.05188165308403462; 0.0073795999836665125 0.02274610494072671 -0.06636818787519601; 0.006501518629262976 0.027579918628479798 -0.08250205051268984; 0.004235107425877455 0.022921967807175526 -0.0698623476570584; 0.00011642489561288833 0.001266297170976236 -0.0044358613386594435; -0.0005685506685738222 -0.00031222921894955155 5.148631825463174e-5; -3.5764503044981543e-5 -0.0001728450517926183 -0.0014192042698739208; -0.0012609647323665774 -0.00013527004158715277 0.0017429322390465042; -0.0003393601326364899 4.767895390173798e-5 0.0003553285841278968; 0.0005760153281980377 -0.00010580578515166498 3.608084273170459e-5; -0.00012567943887877725 -0.0011994257084433206 0.000535580028205874; 0.0005480204319886236 0.001234926996659707 -0.0005680781930679808; -4.593309759186187e-5 -0.00116247143829295 0.0020784385971356935; -0.0005603530293099978 -0.0011978267186673885 -0.0012488633895884995] %
+
+Mass Used: 122.15680775482224 kg
+Launch C3: 90.8536669849317 km²/s²
+||V∞_in||: 7.673926525383467e-5 km/s
diff --git a/archive/ES_0.5589768095883447 b/archive/ES_0.5589768095883447
new file mode 100644
index 0000000..0053bad
--- /dev/null
+++ b/archive/ES_0.5589768095883447
@@ -0,0 +1,22 @@
+archive/ES_0.5589768095883447---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T03:12:56.306
+Launch V∞: [8.141613916731448, -5.656673964431375, 0.18507509243854808] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.583217237785586e-5, 4.961977919548045e-5, 0.0034447621638249238] km/s
+ V∞_out: [-0.0030118348212156173, -0.0010716617480531125, 0.0012862130340086863] km/s
+ time of flight: 1.8749577787493384e8 seconds
+ arrival date: 2030-04-24T05:22:33.306
+ thrust profile: [0.20714769814657977 -0.0046068924088454085 -0.07425359508598285; 0.0697346475937824 0.037163849875491047 -0.08743755698421252; 0.038514356597302256 0.03258614396980743 -0.08811481453126291; 0.03171938641223917 0.034654287364795026 -0.10623793949252998; 0.018379490371431707 0.023668769546481207 -0.08242124426918544; 0.014881466760627578 0.02253314272964586 -0.0849948563400417; 0.010175165857851947 0.016953172466898862 -0.07038670130451348; 0.007667238062809397 0.014404623709862103 -0.0632496085194292; 0.005748984647650053 0.011159977422283586 -0.05273376320827757; 0.0033634756228621697 0.006895481123703621 -0.03520538607909666; -0.0015794204120048003 0.0015611607250271297 -0.009026945831600096; 0.0020399534378579254 0.005159935134291221 -0.0295148034895612; 0.0015784502314092068 0.003016840752940046 -0.004577399518887139; -0.0020521870678313556 0.002631261787297854 -0.005408956300373702; 0.0013622181321106216 8.510227671339968e-5 -0.0032041733849761424; 0.006639141344046633 -0.0011963359340870304 -0.0012132233880109721; 0.00047414953523998253 0.0005785258755256831 0.005628701172319517; -0.004313893391608596 -0.005824565997042371 -0.0036082505895568173; 0.0008122721935064916 0.004179289770898154 -0.015195927612959542; 0.00031370749464191975 -0.0001391657332284388 -0.00040803313793166644] %
+
+Mass Used: 78.61741777654834 kg
+Launch C3: 98.31809029883209 km²/s²
+||V∞_in||: 0.0034457484473953068 km/s
diff --git a/archive/ES_0.558977318121217 b/archive/ES_0.558977318121217
new file mode 100644
index 0000000..50cb01f
--- /dev/null
+++ b/archive/ES_0.558977318121217
@@ -0,0 +1,22 @@
+archive/ES_0.558977318121217---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T09:03:55.510
+Launch V∞: [8.078446386985439, -5.700194372025823, 0.20021704234368015] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00017919993678709175, -0.00034990772664865406, -0.00013343985673278645] km/s
+ V∞_out: [-6.428869013503352e-5, 0.00028228478678775544, -0.0002975338388958939] km/s
+ time of flight: 1.8590064540913838e8 seconds
+ arrival date: 2030-04-05T00:08:00.510
+ thrust profile: [0.2404553602490086 -0.004323740731348109 -0.08058210642230432; 0.0836922214600989 0.04505677795818852 -0.1001122617637755; 0.032819832296740174 0.0283083215680217 -0.07342399679996219; 0.025878326929473186 0.0288772750500337 -0.08444587861065785; 0.020865709016667493 0.028213186428637984 -0.09115622987297253; 0.0172094846827765 0.027123128773564584 -0.09529893821469428; 0.010719595218815586 0.01968045610333938 -0.07407595728531347; 0.009849670772565548 0.01916533101442378 -0.0790081287586337; 0.011058928091073046 0.023047529108827035 -0.09729251794237892; 0.0019043248853065674 0.00236275048005089 -0.019851937907657765; 0.0005589014963999282 0.0008982231173597602 -0.0036316538249816185; 0.0008289099899205711 0.0026230196501365625 -0.013668476300885081; 0.0005887200006780811 0.000758570314360511 -0.0034278023035180204; -0.0028203913888539475 -0.003707814267338309 0.0036646793076936003; -0.0033150671790774756 -0.0018634615749756715 0.0005352629044164416; -0.0021783115111424535 0.0010287029132591326 0.0016840404435356836; 0.0035323331344497546 0.004237746393630917 0.0023820137245761123; -0.006385780872608679 -0.0008545842184638497 -0.0010042460967072616; -0.0015666170603596745 -0.0016337980121307952 0.0027527728104811758; -0.004274694674899371 0.0002165750334994793 0.0030133523232180764] %
+
+Mass Used: 81.67754498123259 kg
+Launch C3: 97.79359877031781 km²/s²
+||V∞_in||: 0.0004151556694515847 km/s
diff --git a/archive/ES_0.5589787491869315 b/archive/ES_0.5589787491869315
new file mode 100644
index 0000000..4e4335b
--- /dev/null
+++ b/archive/ES_0.5589787491869315
@@ -0,0 +1,22 @@
+archive/ES_0.5589787491869315---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T14:39:58.494
+Launch V∞: [7.871651409823729, -6.0137538713659024, -0.09035505398931842] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4018118359382844e-5, 1.6038181542537623e-5, 0.0009984204200525263] km/s
+ V∞_out: [-0.000935939508819003, -0.00031317681461024034, 0.00014274614274991678] km/s
+ time of flight: 1.7785541057337126e8 seconds
+ arrival date: 2030-01-01T02:56:48.494
+ thrust profile: [0.22296606500092708 -0.0230861287861524 -0.086161594343638; 0.054701230206136875 0.022212797712659653 -0.070838186102142; 0.043921636244298616 0.029102541148500298 -0.09978098393643642; 0.03066802492708533 0.025736568169072122 -0.10017057811934306; 0.03465669125282398 0.03395753511308025 -0.14655702115902652; 0.018942472269439008 0.020727579733084076 -0.09908890810033823; 0.02123487312447607 0.025322846262660893 -0.13004321229490876; 0.011964714140148701 0.014247784151646636 -0.08319205859782662; 0.006975324631099479 0.009192778494173033 -0.0557778697384778; 0.0010273705987412728 0.0017623299777443295 -0.010239302516442639; 0.001493826977193633 -0.0002826339493728155 -0.0013086505613595513; 0.000664140869768049 0.0009982098273935806 -0.00782043893063626; -9.647700090587056e-6 4.885494505273124e-5 -0.0005921631320694298; -0.00010490207071801272 0.0003207345097831424 -0.0008954740712925504; 0.0012461842539951834 0.0011184084172016031 -0.00011765026115697838; 0.00025917706538375557 0.0017095607210513126 0.0006304625061786908; 0.0020142134219107715 0.0006008575566477575 0.00015120501840810475; 0.0009118543992553709 0.0016386275069611073 -0.004843222895303462; 0.000807995508328278 -0.0005884617737531287 -0.0045548123696624865; -8.336719858027241e-5 -0.0006447165208413796 0.0005945346884422397] %
+
+Mass Used: 79.68014984099682 kg
+Launch C3: 98.13629557892969 km²/s²
+||V∞_in||: 0.0009988380391507824 km/s
diff --git a/archive/ES_0.5589797182489422 b/archive/ES_0.5589797182489422
new file mode 100644
index 0000000..26ae87b
--- /dev/null
+++ b/archive/ES_0.5589797182489422
@@ -0,0 +1,22 @@
+archive/ES_0.5589797182489422---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T05:36:24.593
+Launch V∞: [7.8567213610072235, -5.7850277815677655, 0.06940728111226295] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.303901178040455e-6, -7.419350557998765e-6, -2.1444650619083725e-5] km/s
+ V∞_out: [-2.0884205662567274e-5, -5.786092108703382e-8, 8.994223707202387e-6] km/s
+ time of flight: 1.8257241399218634e8 seconds
+ arrival date: 2030-02-23T08:09:57.593
+ thrust profile: [0.42817766872272733 -0.011265394845990616 -0.13278812880775695; 0.08793884986949874 0.048586996465084194 -0.09501135634905881; 0.04940096098394912 0.044947922121490985 -0.09706202847703323; 0.03137915336534901 0.03796117991143844 -0.0919142814918253; 0.03823064401978845 0.05665557999658698 -0.1479637086169064; 0.021428559150006982 0.037751293647994795 -0.10765694665969337; 0.011635050499925643 0.024042380676221532 -0.07393096286548088; 0.005139132105690378 0.012208657051704278 -0.04085832376233685; 0.004088331111815106 0.010757977003922583 -0.037850893557600136; 0.00047129909393931455 0.003697077264123184 -0.019879065003685706; -0.0010528645046842368 0.0024011555300631105 -0.009980952679108788; 0.0017624072756254367 0.00317509103442634 -0.018085578744865684; 9.192838499800223e-5 0.0010815065884168733 -0.002082694867555907; 0.000370075191750621 0.0011398202122948735 -0.004800495659922489; 0.0016071536069270998 0.00027637613731370993 -0.0004921198818632067; -0.0031334865848822507 -0.00011732709588909394 -0.00022815294845207265; 0.00011336169615563615 0.0002960968630393891 -0.003931723541776231; 0.001450763913757228 0.004863246607140199 0.0021940099589138795; 0.0008440909160970646 -0.009579275729883492 -0.0008304403406869593; -0.0010449503115072204 -0.002172446782345504 -0.0003721403911563807] %
+
+Mass Used: 96.8129709230775 kg
+Launch C3: 95.19943434868945 km²/s²
+||V∞_in||: 2.2808502000684324e-5 km/s
diff --git a/archive/ES_0.5589866850116092 b/archive/ES_0.5589866850116092
new file mode 100644
index 0000000..2702af4
--- /dev/null
+++ b/archive/ES_0.5589866850116092
@@ -0,0 +1,22 @@
+archive/ES_0.5589866850116092---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T06:32:29.328
+Launch V∞: [8.015705463212925, -5.694641809904868, 0.19785760350969475] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.064688409533968e-9, -4.4004313078380864e-10, -1.0855092874781092e-9] km/s
+ V∞_out: [-1.4079465213247278e-10, -2.871147760411587e-10, -7.640177620739982e-12] km/s
+ time of flight: 1.8552766468799746e8 seconds
+ arrival date: 2030-03-30T14:00:13.328
+ thrust profile: [0.30029969383376676 -0.006151316839868422 -0.09069906883316357; 0.06969721952933149 0.040742667598431266 -0.07529073071475856; 0.0721074455216705 0.06713403677569085 -0.13802397437249728; 0.04124897400701979 0.05109085219170572 -0.11841518014631608; 0.024406314579260457 0.03741617293624384 -0.09622745718829216; 0.02266563193634918 0.04116808091632249 -0.11375561952718528; 0.008012587795885562 0.013499938625792043 -0.041089020613872186; 0.008193601070818577 0.01617700750740553 -0.051902431439673644; 0.0058916490652947285 0.015286473335970286 -0.05127359331912535; 0.00226871259797063 0.0028465827236193717 -0.0029214486542975533; -0.0048748247185496415 -0.004074877177715267 -0.013664741460293305; -0.007599070291479545 -0.0014734331870206053 -0.0012991921417806666; -0.0003654069181813856 -0.0004944297094640808 -0.001502689308175136; 2.4985018806385098e-5 -0.0014584061926795964 -0.0016556062193015405; -0.005406342099960073 -0.00139313054097906 -0.014779268019143624; -0.002115135962130081 -0.006120204708505066 -0.016009269264263413; 0.0004681773735779346 -0.002238232468078076 -9.43754968601634e-5; 0.00047496020669182367 0.0033428967658338197 -0.00030060160904642235; -0.0002409547170344851 -0.0011813926484833916 -0.0049759410286317075; -0.0003153941583804233 0.0028860449306335086 -0.0030142958094638733] %
+
+Mass Used: 87.95330807058326 kg
+Launch C3: 96.71962704736472 km²/s²
+||V∞_in||: 1.5828865340090613e-9 km/s
diff --git a/archive/ES_0.5589889228350816 b/archive/ES_0.5589889228350816
new file mode 100644
index 0000000..8123895
--- /dev/null
+++ b/archive/ES_0.5589889228350816
@@ -0,0 +1,22 @@
+archive/ES_0.5589889228350816---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T07:03:33.187
+Launch V∞: [7.74377416371284, -5.851864480063201, 0.15271406828737977] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4031943416841808e-6, -1.3207923440553583e-5, 0.00026896089064252935] km/s
+ V∞_out: [8.650547767790177e-6, -0.0002688856395963675, 2.2386007459368588e-6] km/s
+ time of flight: 1.8064409704102558e8 seconds
+ arrival date: 2030-01-31T01:58:30.187
+ thrust profile: [0.5354989335715507 -0.01572613055408758 -0.12138496424602102; 0.031369823780513076 0.01800205238915891 -0.03314019335247947; 0.05206138624105476 0.051765839233897847 -0.10070277430112154; 0.04206799029437624 0.06417215497067116 -0.1259087389272972; 0.05112520332916633 0.09288160140893664 -0.19780157625158568; 0.018512326774965577 0.03625800331600992 -0.09486842485423692; 0.0059573443430889815 0.01297744147784982 -0.03445186268823429; 0.0035711071319132256 0.009705141593017878 -0.028243013084725904; 0.010009240173618887 0.03085107436493833 -0.0879999082491443; 0.002354959847463978 0.007819602978092033 -0.02489153200757105; 0.0016073209245738545 0.007997131952399582 -0.024441974332639695; -0.001197695855121774 -0.00021015601127409816 -0.0011497698364905115; 1.2289351731993537e-5 -0.00015385475347834323 -0.0002021276163345476; 0.0001611059557370317 0.00015901634358356855 -0.0011324005902502506; 0.00044722680931958195 -0.0005366392626023393 0.0013613678627200211; -0.000546186992281686 0.00036937322255475977 -0.000553718462288079; -0.001536188025326813 -0.000856250441729662 -0.00040699770008013035; 0.0005090589507217008 -0.0004759430752096528 0.0012212735961179841; -0.001017038437196476 -0.00032272141555848285 0.0017154748972843096; -4.013737131593195e-5 0.0014443418265724698 -0.0019976917981460738] %
+
+Mass Used: 102.45728960105089 kg
+Launch C3: 94.23367777826473 km²/s²
+||V∞_in||: 0.0002692886534765152 km/s
diff --git a/archive/ES_0.5589910455235303 b/archive/ES_0.5589910455235303
new file mode 100644
index 0000000..909b799
--- /dev/null
+++ b/archive/ES_0.5589910455235303
@@ -0,0 +1,22 @@
+archive/ES_0.5589910455235303---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:48:14.163
+Launch V∞: [8.164628387180585, -5.56058343024508, 0.39790858604592905] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.313181838811602e-9, 6.135385259511882e-9, -4.040022327301815e-8] km/s
+ V∞_out: [-9.863595433742136e-9, 3.266950234787265e-8, -5.289728409493458e-9] km/s
+ time of flight: 1.874957778777175e8 seconds
+ arrival date: 2030-04-22T07:57:51.163
+ thrust profile: [0.23062792212860947 0.0012041568618894605 -0.07159786790873447; 0.08320659868742819 0.0491065777963912 -0.09214183754962621; 0.05116187606261832 0.04861098981994369 -0.10328699122340328; 0.05296595086192578 0.0668532560428785 -0.15664978557219938; 0.02133300058108366 0.03236102354665687 -0.08850358832752722; 0.017676006567821798 0.031730342274584655 -0.09290956596989917; 0.009904901762999362 0.0195075802280215 -0.06175912520960391; 0.0048646477004050176 0.011337552129674364 -0.04161398673461159; 0.0017640540411204898 0.00493302006118446 -0.01822468455077348; 0.0019311557650226801 0.00557535240125692 -0.02200899693897547; 0.0013014459836186176 0.0041562614114106 -0.018545575779213928; 0.0005373403025612803 -0.006436037600623086 -0.004546460249739504; 0.0003940840489825112 -0.0011946107678812376 0.0004958187840221275; -0.0008617053495981565 -0.0011430138460987297 -0.002328128521381127; -0.006582046214435373 0.007327942205670745 -0.0028677637558733654; 0.0001532249775299937 0.0021190843379222707 -0.0031952370470079887; -0.006771682954559613 0.008399102600056399 -0.0003633118157374514; -9.208058357673194e-5 0.0009144881671281883 0.005309725878066013; -0.00018431175526696566 -0.001315487311243528 0.0025334873152183385; -0.00497065770188752 -0.00680445091892011 -0.0023989104850341246] %
+
+Mass Used: 82.00869294558379 kg
+Launch C3: 97.73957602832026 km²/s²
+||V∞_in||: 4.134824370783182e-8 km/s
diff --git a/archive/ES_0.5589927899471794 b/archive/ES_0.5589927899471794
new file mode 100644
index 0000000..8f38d64
--- /dev/null
+++ b/archive/ES_0.5589927899471794
@@ -0,0 +1,22 @@
+archive/ES_0.5589927899471794---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T20:45:42.150
+Launch V∞: [7.889577638668852, -5.897896115087495, 0.15599476640378668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0498902644154937e-6, -1.368391592431377e-6, -1.663639315928869e-7] km/s
+ V∞_out: [1.26770897467911e-7, -6.186876905433344e-7, -1.608360755309804e-6] km/s
+ time of flight: 1.8547582351468506e8 seconds
+ arrival date: 2030-04-01T13:49:25.150
+ thrust profile: [0.33235714398683214 -0.0051405642112215275 -0.10509366673939927; 0.050968284320684586 0.027912093297151247 -0.06203500807897621; 0.03760797536455235 0.0317405834437771 -0.08189819692353206; 0.028375970227755284 0.032000432490527635 -0.09000750965244915; 0.03031241579483526 0.041128383724469336 -0.12592616630072126; 0.016602239046821267 0.02569664925795554 -0.09020591288873192; 0.01734198011193918 0.030683331474866616 -0.11138758898873731; 0.0064283029713678485 0.011480145499240497 -0.04894164008734564; 0.003250432239777219 0.0066615444757626594 -0.029135924247646664; 0.004589926960265444 0.010815692210954873 -0.04742858439585832; 0.0007427301240361308 0.0017387560804122556 -0.012440542409189606; 0.0003278340370196922 0.00037084540909333307 -0.005042190243565848; -0.00044774498163898204 -0.0007349120470996442 -0.005410653573208104; -0.0013024222565634948 0.002572304199391895 -0.002488549855297051; 0.0003730211629739107 -0.00016934066523405017 -0.0028615065524572256; -0.0023828587964698704 0.002505891458505614 -0.004235456506891685; 0.0015339921166208994 0.008000008105238357 -0.004810503864092583; -0.0007027605607404346 0.0026298479491783685 -0.002032847145336138; -0.00019153841179382275 -0.00017603500122383977 0.006099869105632527; -0.0012833270475910204 -0.003603913652155317 0.00042300520432622636] %
+
+Mass Used: 86.00439004116606 kg
+Launch C3: 97.05494826809311 km²/s²
+||V∞_in||: 1.732755630574132e-6 km/s
diff --git a/archive/ES_0.5589934856528042 b/archive/ES_0.5589934856528042
new file mode 100644
index 0000000..0e49db1
--- /dev/null
+++ b/archive/ES_0.5589934856528042
@@ -0,0 +1,22 @@
+archive/ES_0.5589934856528042---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:59:55.770
+Launch V∞: [8.096498956986682, -5.736609052266357, 0.121119216651923] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.020846814157593506, 0.11926566242216377, 0.1454998771469698] km/s
+ V∞_out: [-0.06508293098579142, 0.06532093419879839, -0.16530570381027573] km/s
+ time of flight: 1.8475461432376125e8 seconds
+ arrival date: 2030-03-22T20:43:29.770
+ thrust profile: [0.20049194515805344 -0.007443974119619802 -0.07050748052621686; 0.04142396115949159 0.020011689208418282 -0.052431923312878916; 0.05337303144906463 0.042749616553349794 -0.11659755902961377; 0.03505836246664015 0.036181994070592666 -0.1137533407708648; 0.01310542592658052 0.015594336065542416 -0.05802386718404165; 0.01531468206051107 0.022127692322777837 -0.08559187911721114; 0.01730306182765334 0.026783620120278774 -0.11081376143171401; 0.011757672332789583 0.014978057690038713 -0.08570367051431525; 0.005935029471292956 0.010601086060392706 -0.05363892751218363; 0.003438388394280922 0.005755026630907649 -0.03295101077341894; 0.0020479257795293017 0.004882261577427713 -0.02853817399225889; -0.0004400657778771673 0.0021335910172949014 -0.009451725460491141; -0.0010980806835971628 -0.00011456523755249478 0.0005818432537233013; -0.0009534446764629763 0.0009949850746970757 0.0023157271615006285; 0.003162738542968073 -0.0028871080540512485 0.0011129663420991155; 0.005430922896213664 0.0036253415810638657 0.001521821736661853; 0.004671957472117257 0.0018649215188766438 -0.0006392343550810954; -0.0028238127508705725 0.00026240543129559836 0.006447575734442171; -0.0005540494522404313 0.0027414830921899695 -0.0002056258323786162; 3.739726386507453e-5 0.0005764340052582695 -0.0026162909174099096] %
+
+Mass Used: 77.71194950684503 kg
+Launch C3: 98.47664864367312 km²/s²
+||V∞_in||: 0.1892857684647794 km/s
diff --git a/archive/ES_0.5589949285497567 b/archive/ES_0.5589949285497567
new file mode 100644
index 0000000..11f052d
--- /dev/null
+++ b/archive/ES_0.5589949285497567
@@ -0,0 +1,22 @@
+archive/ES_0.5589949285497567---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:34:46.381
+Launch V∞: [8.046801761914043, -5.605781056753002, 0.06443621628357701] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00012682680751763926, -9.067529635222766e-5, -0.005670180662809119] km/s
+ V∞_out: [0.004992794637065796, 0.001692690977627951, -0.002064762610751346] km/s
+ time of flight: 1.8749577793307102e8 seconds
+ arrival date: 2030-04-23T01:44:23.381
+ thrust profile: [0.4067452420435872 -0.0018797242392952702 -0.1200511023517477; 0.03771442726017833 0.021939372061380868 -0.04739138316323629; 0.031892850318834286 0.03027638698084453 -0.07200016870413235; 0.027538039771909318 0.03414728293452427 -0.09122201124637876; 0.02500211641380177 0.03809701836774202 -0.1109949912681709; 0.01499766313669995 0.02690362133889457 -0.08718040541277462; 0.00980670953487758 0.01857759575336114 -0.06661243518359906; 0.00912593010876728 0.020549890791396287 -0.07524802305454584; 0.007402025446860375 0.018789902425081932 -0.07385210353650415; 0.003954342133279265 0.009480943227693057 -0.03978418907637421; -0.0014957148558805576 0.0020096518050089986 -0.012726331111857987; 0.003513866594251368 0.002790911991678786 -0.009087579763731308; -0.004292302547662302 0.0009544652935513454 -0.0038005280778841428; 0.0001611391572085528 0.0018523154957454948 -0.005311763015737201; -0.0033381093066561685 0.004035791312252748 -0.001229397074944149; 0.00015679736104530332 -0.0017550492131406536 0.002384118825009094; -0.0016017055916884378 0.001160125518932771 0.0066314021289425595; -0.002678019889956101 0.00299960016520365 0.00022314292590521357; 0.0007950329940505582 -0.0007734912728162618 -0.0014812406106144826; 0.0018792375283379905 -0.0076303115270289655 -0.009187255079239069] %
+
+Mass Used: 91.1110306877672 kg
+Launch C3: 96.17995187776269 km²/s²
+||V∞_in||: 0.0056723236682481495 km/s
diff --git a/archive/ES_0.5589993851577921 b/archive/ES_0.5589993851577921
new file mode 100644
index 0000000..fd10569
--- /dev/null
+++ b/archive/ES_0.5589993851577921
@@ -0,0 +1,22 @@
+archive/ES_0.5589993851577921---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T07:02:48.005
+Launch V∞: [7.685223926378427, -5.723958490642677, 0.0782887687332875] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012934558466736919, -0.0009172916988563028, -6.406485492143489e-5] km/s
+ V∞_out: [0.0011134286913327682, 0.0005351540151095628, -0.0010010004418284613] km/s
+ time of flight: 1.850532016408435e8 seconds
+ arrival date: 2030-03-23T02:42:49.005
+ thrust profile: [0.6531966444699214 0.004190861655175436 -0.16108070931215418; 0.16469136303228035 0.10473458816551712 -0.15588989184232488; 0.05371397367916581 0.057160850958166164 -0.09937592038431697; 0.02564761633365313 0.03697376662724706 -0.0728296658376733; 0.03140568521723891 0.058233518336258325 -0.1212054317833506; 0.016153198495148215 0.03651514279097617 -0.08388598526748148; 0.006531545556379967 0.017962190847412126 -0.04491221888698447; 0.0096242433616029 0.031170879233946215 -0.07971644421578629; 0.005036706149204498 0.016752262597506874 -0.04903551890397671; 0.0015542774504068158 0.0019129447917606165 -0.006565133798598012; -0.00023020595913371476 0.00023808792604630827 -0.0011106187275014756; 0.000314051078271087 0.00032174012136489604 -0.0007100644082529476; 0.0005258974691967652 -0.00018335913410765805 -0.0005246222433979725; 0.0014130701879214737 -0.00028276953691609003 -0.0003508256910594691; -6.417716733360084e-5 0.0021431973442814665 -0.0003699316103538625; 0.0002647878545587772 0.002665491352486592 -0.007991393661304576; 0.0001646628495578573 -0.0010983632657612951 -0.0002280694437593511; 0.001113180629695525 -0.0007526342075433565 0.0005514971674198087; -2.9012146154473858e-5 0.00023224461516976967 -0.0015255062903329316; -0.00017419330154133192 -0.0019113447006031425 -0.00023013668087921036] %
+
+Mass Used: 116.47638507790134 kg
+Launch C3: 91.83249673248962 km²/s²
+||V∞_in||: 0.0015869960282625612 km/s
diff --git a/archive/ES_0.5590054902343401 b/archive/ES_0.5590054902343401
new file mode 100644
index 0000000..5bf29a5
--- /dev/null
+++ b/archive/ES_0.5590054902343401
@@ -0,0 +1,22 @@
+archive/ES_0.5590054902343401---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T21:59:55.947
+Launch V∞: [7.822840276754077, -5.896114439644522, 0.1739881288715414] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3037289056516827e-9, -1.3779712295151955e-9, -7.7591239774648e-10] km/s
+ V∞_out: [1.7543386708974268e-10, -5.37167558477117e-10, 8.488186599495897e-11] km/s
+ time of flight: 1.830655386052243e8 seconds
+ arrival date: 2030-03-01T17:32:13.947
+ thrust profile: [0.26366125542102287 -0.0040598655557803984 -0.07824262950883233; 0.20060332383716858 0.11788997001598198 -0.1867195528082287; 0.03495685539592698 0.0331962185109453 -0.0663585996939747; 0.055720187438106875 0.07303476963670015 -0.15272084844556927; 0.023537510775175838 0.0376824145207032 -0.08921755130370568; 0.02346614626136491 0.046553000453152096 -0.12035634509004198; 0.01312208560327619 0.029585343605430556 -0.08210578867670427; 0.004380599870461758 0.011814925166776654 -0.03643699459442134; 0.0014924145718726608 0.005363011928158724 -0.016954579365704946; 0.0002825534884154677 0.002061932986594595 -0.008447857867478311; 0.001338756981745645 0.0020090037153909805 -0.009223418723651598; -0.0008531153709313568 0.0011456741541247262 -0.0053419029974740295; -0.00019343569612663536 0.0009268357801638878 -0.0018394494056895596; 0.0005718470655186393 0.00012516281761184038 0.0001766604486166586; 0.002282352387931832 0.0016504500989185421 0.004589750620369399; -0.00036250126922681336 -0.0038421718886419787 0.0033342916246413413; -0.0005293162327676975 0.002017081693198551 -0.0007363084812819381; -0.0067949064042035 0.0021738714922202133 -0.001972076471730758; -0.0024550729400029322 0.0049927619546905255 -0.006298635477529664; 0.0003079232914922853 0.0003374679356525221 -0.0010000398299502501] %
+
+Mass Used: 92.22401239852115 kg
+Launch C3: 95.99126734997867 km²/s²
+||V∞_in||: 2.0495252664409986e-9 km/s
diff --git a/archive/ES_0.5590180373292251 b/archive/ES_0.5590180373292251
new file mode 100644
index 0000000..48b5398
--- /dev/null
+++ b/archive/ES_0.5590180373292251
@@ -0,0 +1,22 @@
+archive/ES_0.5590180373292251---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:59:35.956
+Launch V∞: [7.844926875210658, -5.768185469981527, -0.03178245577008296] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.505997746624563e-6, 3.714806795093105e-6, -3.0373168392013646e-6] km/s
+ V∞_out: [9.050205137633675e-7, 6.508458235125324e-6, -3.178531106635333e-7] km/s
+ time of flight: 1.855539822393921e8 seconds
+ arrival date: 2030-03-31T07:45:57.956
+ thrust profile: [0.4917442645205169 -0.016856366234926472 -0.11032457491208617; 0.04944358719691445 0.03074171300508088 -0.053882629622494176; 0.03246482143438352 0.03265842340819968 -0.06465509389716562; 0.026706190785759004 0.0356739352561011 -0.07801392215036407; 0.023498486978099947 0.03854360991092406 -0.08917160443822332; 0.027980450765273678 0.058184330528171395 -0.1463918469128345; 0.023908095703448443 0.054222170099218835 -0.14934566002352392; 0.006455602792916071 0.017462531710856165 -0.05361521927503512; 0.0019720570598142522 0.007610694063368143 -0.031156787256437033; 0.0009676315042320192 0.0035819035352955414 -0.011809233926841942; 0.004285496512191884 0.0060493900429849905 -0.025588523780761194; 0.00026304559661582884 0.0014774702496652974 -0.003903128024288505; 0.0004341722119060086 -0.00100652759122265 -0.0024070847692698465; 1.3987117416293187e-5 0.0029316559626094835 -0.0012613574481871576; 8.775189766047683e-5 -0.0001191331101881558 0.0034891745177716375; -0.00017902222572574214 0.0013166092982878801 -0.0017575872198842292; 0.007578064532943901 0.004595685926163278 -0.00015147912366258965; 0.0009992934635530333 -0.0003527615188167277 -0.0030708217889819124; -0.0020227190838966137 -0.0028158376906973555 0.009591929500236858; 0.0017170507525232199 -0.0006626687399560677 8.946742398407547e-5] %
+
+Mass Used: 99.09524361241029 kg
+Launch C3: 94.81585141800325 km²/s²
+||V∞_in||: 6.5824842422258566e-6 km/s
diff --git a/archive/ES_0.5590184380570378 b/archive/ES_0.5590184380570378
new file mode 100644
index 0000000..2637bf3
--- /dev/null
+++ b/archive/ES_0.5590184380570378
@@ -0,0 +1,22 @@
+archive/ES_0.5590184380570378---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T00:10:00.220
+Launch V∞: [7.884466109747633, -5.776809017461274, 0.37053617638401815] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.853553579578233e-7, 1.1843891404210512e-6, -2.8245671128050243e-5] km/s
+ V∞_out: [-1.2077096342420933e-6, 2.822397701773426e-5, -2.1928182271083548e-7] km/s
+ time of flight: 1.8749577787335098e8 seconds
+ arrival date: 2030-04-25T02:19:37.220
+ thrust profile: [0.4717955708912244 -0.0073054093484506335 -0.15539999184491488; 0.04125307066697511 0.020376652039680837 -0.05235789492859641; 0.042474850165251425 0.03245671184265558 -0.09524619466106066; 0.0285830109773747 0.027422440046690276 -0.0933670576343072; 0.030073739113151497 0.03347734563474444 -0.12487757400459287; 0.0232650003684628 0.02908427006078896 -0.12054748314396739; 0.011002936576589054 0.015556992670812403 -0.07169218122242657; 0.008981313843475829 0.013789439053850943 -0.06866038663072997; 0.0010170497317890186 0.001596400589479078 -0.01233147681596235; 0.0011255124733437509 0.0021854631885672112 -0.011959911470438617; 0.0005839118598197578 0.0012806140658872533 -0.0077368067928773356; -0.0007328385537024708 -0.0016815693238887682 -0.0023585601380545934; -0.0012070005368726114 -0.0010041366797153143 0.0021442331416284825; 0.0010485007979266843 0.003976942455444823 0.0005744961907557982; 0.003488276447440224 -0.0042616695561997694 0.001797247683417171; -0.002142681919656108 -0.0031557699170320134 3.00338682353385e-5; 0.0009317710979474745 -0.00025100526323942944 0.0004414098658230639; 0.009444517536181724 -0.011425239717667037 -0.001659815665861988; 0.0002246744440027158 -0.001586186110762945 -0.0005097681719301605; 0.004945650029498405 -0.0008022103335063901 -0.00848268164388363] %
+
+Mass Used: 94.09203004493475 kg
+Launch C3: 95.67362531799016 km²/s²
+||V∞_in||: 2.8271099584534064e-5 km/s
diff --git a/archive/ES_0.5590238668028642 b/archive/ES_0.5590238668028642
new file mode 100644
index 0000000..1bacdf6
--- /dev/null
+++ b/archive/ES_0.5590238668028642
@@ -0,0 +1,22 @@
+archive/ES_0.5590238668028642---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T04:53:38.169
+Launch V∞: [7.911415909261552, -5.596181878700654, 0.19009521573846946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.637826179002197e-9, 1.104709611254386e-8, 8.133481231803442e-9] km/s
+ V∞_out: [-1.1445134939159769e-9, 1.1840632579593208e-9, 7.284099864931096e-10] km/s
+ time of flight: 1.874957778707042e8 seconds
+ arrival date: 2030-04-22T07:03:15.169
+ thrust profile: [0.5608758081592018 -0.016104260324261946 -0.16169630490759523; 0.06919119172162685 0.039379291347838595 -0.07901837541348769; 0.050661072245517295 0.046323166490867616 -0.10504043327213938; 0.03910256019223778 0.04736458808041017 -0.12049648442266672; 0.024950141975897643 0.036679294028283446 -0.10487689193412415; 0.016774064886490414 0.029386214586517644 -0.09179089193490202; 0.00947643202070239 0.019002351041875355 -0.06498993729212549; 0.005116866201751182 0.011546928765121428 -0.04243242972911256; 0.0016693071931310202 0.005510985872829123 -0.02325185737179859; 0.00032883380118367046 0.0013378875322727622 -0.011214947834038763; 0.0011759313801250214 0.00414969489188105 -0.012973145258341482; -0.0031071582916076495 0.001601680770255404 -0.00297990109767098; 0.0003801091004102362 0.0005288125257275247 -0.004573657857208554; -0.0062214750991810746 -0.0005958545955195892 0.0005262349512825124; 0.0009570658390528307 0.0007628481939588076 -0.005446923386340799; 0.0009716691605400763 0.000750405988959075 -0.001014022786653695; 0.0050207945924894875 -0.011647542247507619 -0.009363169578246452; 0.0016126477386919178 0.0007697242829211435 -0.003751471897901753; -0.0038173967159704295 0.005472120330443505 -0.010234636000445376; 0.0027837447544877105 -0.010016955289745 0.002144746046633435] %
+
+Mass Used: 104.18848918748563 kg
+Launch C3: 93.94388949986102 km²/s²
+||V∞_in||: 1.4481066298257136e-8 km/s
diff --git a/archive/ES_0.5590304780389233 b/archive/ES_0.5590304780389233
new file mode 100644
index 0000000..14c6b86
--- /dev/null
+++ b/archive/ES_0.5590304780389233
@@ -0,0 +1,22 @@
+archive/ES_0.5590304780389233---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:28:48.429
+Launch V∞: [8.043699148629083, -5.5706089834803425, 0.1651314960650474] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.028125133069365826, -0.09949034131059241, -0.0012071264040366453] km/s
+ V∞_out: [0.07609262305530294, 0.03189854480215937, -0.06186542782847392] km/s
+ time of flight: 1.874957778745208e8 seconds
+ arrival date: 2030-04-22T07:38:25.429
+ thrust profile: [0.42073896769928526 -0.002210991752762236 -0.12387827553853988; 0.05295689428272037 0.030073774315634905 -0.060963421905371705; 0.06000584683549534 0.056984721452622795 -0.12163266247527424; 0.02189239473012498 0.027613859693594672 -0.07001067697814198; 0.024638348440402084 0.03866616602463896 -0.10350683258089749; 0.008857997006400433 0.017181739860440585 -0.05136838908689954; 0.011947116145647297 0.02946833445836609 -0.0858234267435756; 0.004787511171590307 0.013133678755628925 -0.04491700507003088; 0.008675526023138792 0.026023876622185717 -0.09269114417476322; 0.0004168910383171296 0.00682788137630576 -0.023923802287927978; 0.000737020820279134 0.005929897452651084 -0.021674937718289454; 0.0008064278510238241 0.0023175275219591593 -0.019151426698627502; -0.0001255971926183209 0.00028841495597328607 -0.002337293146056551; 0.0007507523923975166 -0.0013852658710684545 -0.0032355585666510303; 0.0008996335643215213 -0.00029709365049131143 0.0040687328744191675; -0.00014269973365541022 -0.0005950301255807239 0.004926039831686643; 0.001001825144461218 0.003090289963607663 -0.002797992409481529; -0.0006168745205842082 -0.0010012795099409665 0.0010357756700736655; -0.0009551994452516636 0.00044376479601469917 -0.004689119835712195; -0.006441718780902413 0.004088603175893468 0.0010511685035491337] %
+
+Mass Used: 93.60193941177249 kg
+Launch C3: 95.76004885148079 km²/s²
+||V∞_in||: 0.10339636491880663 km/s
diff --git a/archive/ES_0.5590353486612525 b/archive/ES_0.5590353486612525
new file mode 100644
index 0000000..d99d218
--- /dev/null
+++ b/archive/ES_0.5590353486612525
@@ -0,0 +1,22 @@
+archive/ES_0.5590353486612525---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:45:45.999
+Launch V∞: [7.726754359217655, -5.752102685786414, 0.2217600507553585] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1490876198602064e-6, -1.992314119295581e-6, 1.4715189482024317e-6] km/s
+ V∞_out: [-4.6858823608295194e-7, -3.2413195142517696e-6, 1.5662248880274735e-7] km/s
+ time of flight: 1.8749577787398487e8 seconds
+ arrival date: 2030-04-23T07:55:22.999
+ thrust profile: [0.6373489789508759 0.0050558219293998 -0.18807076957452054; 0.0891945566000146 0.049648849374522325 -0.09916873564874376; 0.045698155283245265 0.04075904909065958 -0.0922821472498525; 0.06024757713915616 0.07119607958359211 -0.17990112396872807; 0.019797370546913905 0.027526328513597535 -0.07967905244677971; 0.019317088062851182 0.0313694805423982 -0.09904364329884564; 0.0075368405713883025 0.013662150303235369 -0.04766715715412755; 0.000713476689865627 0.0019581517038542023 -0.00899201346979169; 0.0009747136871587833 0.0026799132497232637 -0.007890485513624352; 0.0013624705973776655 0.003644981579566653 -0.014908960949411635; 4.397438691929105e-5 -0.001899622408813946 -0.0035712377501532105; 0.0009155278787299056 0.005368555865915436 -0.0016620898982905496; 0.005051819473374224 0.006317642728900032 -0.019485101901631725; 5.3474739466156246e-5 0.002393037013466826 -0.0029160731878573615; 0.0001744574195530102 0.001050228528796924 -0.004105640465170195; 0.003381433273937592 -0.005809142337458476 -0.008719336040983666; -0.0005313766850319306 0.0014644150703146928 -0.006400555534406645; -0.0036139278022852203 0.01379699606831933 -0.016557840974662435; -0.0007496681269630488 0.001298774814725968 0.00027135209001671965; 0.00025419750285117276 -0.0016733670809078085 -0.006315428868210054] %
+
+Mass Used: 110.64943153027843 kg
+Launch C3: 92.83859575563133 km²/s²
+||V∞_in||: 3.2792165470886067e-6 km/s
diff --git a/archive/ES_0.5590386529824736 b/archive/ES_0.5590386529824736
new file mode 100644
index 0000000..a77bf88
--- /dev/null
+++ b/archive/ES_0.5590386529824736
@@ -0,0 +1,22 @@
+archive/ES_0.5590386529824736---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T06:49:32.681
+Launch V∞: [8.08594822179885, -5.780885944421541, 0.044151783537562855] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.955260589220421e-10, 2.0597542208394124e-9, -1.7254096278182573e-9] km/s
+ V∞_out: [1.4138413707749107e-9, 2.7205979262787597e-9, 6.983285492425257e-11] km/s
+ time of flight: 1.8533450937464043e8 seconds
+ arrival date: 2030-03-30T08:38:01.681
+ thrust profile: [0.17416515233384552 -0.003984064216533338 -0.06463274129025426; 0.05177914697453345 0.02657500205854089 -0.06591932292540671; 0.027657599316768075 0.022573144588468513 -0.06235665082517698; 0.043277041071251 0.04616781198230408 -0.14221991691172675; 0.028590749295116825 0.03558685832140585 -0.12405427526508592; 0.01287265433201409 0.018875892240575495 -0.06995569064140188; 0.008721543915763848 0.013102962569930437 -0.0597249777442727; 0.0061214042583576855 0.01005648577032301 -0.05572363295980803; 0.009372162603931908 0.019524288757641197 -0.08880705941784772; 0.002659797280651972 0.0064136105117658685 -0.031735688421215706; 0.0029057924001953932 0.0017514408661822927 -0.023151233711935046; 0.001325381933034184 0.0028685663612397884 -0.016222384944080934; -0.00011837448739952265 0.0036378769445640975 -0.002873287583905827; -0.00028596510001404555 0.0002381858187939289 0.00232498835255535; 0.005126988647992016 -0.003893977312127004 -0.0038970687373933487; 0.002317871916238907 0.0010600779548792364 -0.0010394725020670906; 0.0039848988289664655 0.0017447362856999969 0.004351990890064373; -0.0010444127082668876 0.001911391326704871 -0.0020560965757589907; -0.008492996278573178 -0.005106782006236404 0.002532932338695456; 0.00015531362408721926 -0.0016913717918816712 -0.00014080639431757587] %
+
+Mass Used: 75.86005156614874 kg
+Launch C3: 98.80315032801207 km²/s²
+||V∞_in||: 2.775496772232557e-9 km/s
diff --git a/archive/ES_0.5590429255871971 b/archive/ES_0.5590429255871971
new file mode 100644
index 0000000..2ced10f
--- /dev/null
+++ b/archive/ES_0.5590429255871971
@@ -0,0 +1,22 @@
+archive/ES_0.5590429255871971---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T08:14:09.928
+Launch V∞: [7.766622704275168, -5.821558712057231, 0.1300247022314995] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.03824802698142781, -0.22654323083442277, -0.2725138974335386] km/s
+ V∞_out: [0.014229020782875497, -0.01569731361263148, -0.35579126089206053] km/s
+ time of flight: 1.8294058307362247e8 seconds
+ arrival date: 2030-02-26T17:03:52.928
+ thrust profile: [0.4479824898668148 -0.008695460782419239 -0.09991924774529463; 0.11026994665668768 0.07100343840514708 -0.10187715863962984; 0.07559920544910127 0.08273163429453613 -0.1325518667688349; 0.03950664906720002 0.058193627800264935 -0.10305039207138483; 0.05261748343109257 0.09294518986501565 -0.16745625997440014; 0.011225472960397581 0.02591688938550322 -0.05513056950787085; 0.006796312904210276 0.019054639881605544 -0.043682910185725614; 0.01024891179623818 0.03407387811676661 -0.07885519305214762; 0.003798234089605909 0.015043939067670608 -0.037938704726022884; 0.001483537769832437 0.007134589175431454 -0.01906332801907925; 0.0009933102509687534 0.004898308671918328 -0.014239551964696454; 0.0001397277696908335 0.0012548679081589432 -0.00275675080569636; -0.0003128802466175266 -0.0004994742110235174 -0.0003775076277364325; 0.0007101975545010172 -0.0009052342179285877 0.0005580847328879708; -1.3902664011072055e-5 -0.00030865066860190723 0.0010658229633142646; 0.0009758438113587234 -0.0008167968026997079 0.001398670522326305; 0.0003167500244500621 -0.0006796169631340637 0.0012526974336971833; 0.0005005821947014412 0.001212102452064018 0.0009792526587077649; 0.0003690412809839313 0.00022475646994408365 0.000482333716310665; 0.000432791904446217 -0.0004922537085382441 -0.000598432633597299] %
+
+Mass Used: 102.5541103169162 kg
+Launch C3: 94.22788049168236 km²/s²
+||V∞_in||: 0.35643873428583456 km/s
diff --git a/archive/ES_0.5590615415164136 b/archive/ES_0.5590615415164136
new file mode 100644
index 0000000..eb7ffa5
--- /dev/null
+++ b/archive/ES_0.5590615415164136
@@ -0,0 +1,22 @@
+archive/ES_0.5590615415164136---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T06:05:29.837
+Launch V∞: [7.98394502533542, -5.5669072029798095, 0.2172875312034434] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.05687164761651427, 0.33674131141326824, 0.40771187707254325] km/s
+ V∞_out: [-0.21813027841484636, 0.19039398078414774, -0.4511721367157423] km/s
+ time of flight: 1.8749577785018104e8 seconds
+ arrival date: 2030-04-21T08:15:06.837
+ thrust profile: [0.45051733963446866 0.002948281098333791 -0.12911765148320425; 0.09004109571519946 0.0542949720384471 -0.09576884656130717; 0.08376763465631797 0.08278260856425515 -0.15978196923500157; 0.045135898057483234 0.060714816472729784 -0.13218501988432557; 0.016433665349461415 0.0265856026253485 -0.06610805686286853; 0.021624834112670334 0.04290172236793897 -0.11355823559045249; 0.0066014722884366024 0.014142203905397725 -0.042506722713588914; 0.0037571351135761186 0.009795466919673151 -0.029316615893595018; 0.002356672168858601 0.003834607765986535 -0.014023203271296114; 0.0016666794794902512 0.004465952394813144 -0.01597643978546734; -0.0005879638083051921 0.0034869903501415986 -0.002786316813665494; 0.0008509332519672415 0.00418698999074916 -0.007999393086397336; -0.0005899699597717543 -0.003223598205363816 -0.004741324854433696; 0.0007030480159493603 0.0016359934250068987 -0.001684417805587355; -0.004962820366378373 0.0018302515006640328 -0.00032948200933892403; 0.002146730427890173 -0.0007662359359390394 0.0004808301213405364; -0.0015633924368061614 0.002286530200460198 -0.007408066381612585; -0.0005056227226763444 0.0023591619904606994 -0.009355474321168452; -0.005519654560335704 -0.005066535872011391 -0.007806811309939241; 0.00045086523233833846 0.004158704698598449 -0.00557037925438336] %
+
+Mass Used: 99.34901933774745 kg
+Launch C3: 94.78104784538317 km²/s²
+||V∞_in||: 0.5318440277195573 km/s
diff --git a/archive/ES_0.5590630808655538 b/archive/ES_0.5590630808655538
new file mode 100644
index 0000000..4df658c
--- /dev/null
+++ b/archive/ES_0.5590630808655538
@@ -0,0 +1,22 @@
+archive/ES_0.5590630808655538---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T11:56:10.523
+Launch V∞: [7.927148551947161, -5.858039455772568, -0.07012929393266096] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.690178599110196e-10, 2.4571536997447497e-9, -2.157270101363996e-9] km/s
+ V∞_out: [1.536480407915342e-9, 3.1245592306732815e-9, 8.228443347814088e-11] km/s
+ time of flight: 1.839390500993466e8 seconds
+ arrival date: 2030-03-12T10:07:00.523
+ thrust profile: [0.21855441648012028 0.0015071574061498471 -0.06655460353748704; 0.11555126755994749 0.07202051092322388 -0.11838763022175526; 0.060279122941795514 0.06275295309684882 -0.11575903558818357; 0.03722567862073283 0.05119859323479287 -0.10839843746254882; 0.01952328718599368 0.03717100584580267 -0.08378024974752506; 0.013137196123088123 0.028339940922977574 -0.07143074170777919; 0.015711694753415627 0.04111185006076438 -0.10872412247529487; 0.008882746568174135 0.026770660665334158 -0.0749682668374536; 0.005090063637147027 0.01966983912034694 -0.058700980826925625; 0.000595033047494975 0.0037776857137989087 -0.011684864358218446; 0.0001511954909951456 0.0021344838234245676 -0.007333163773316808; 0.0005865270208769799 0.000866599310881211 -0.004915912513799596; -0.00047155688792399294 -6.841552136089917e-5 -0.001474684161184069; 0.0007814875286495666 -0.0006112108486982131 0.0019024187088254232; 0.0025994721900689365 1.1559632592541245e-5 -0.0054423942302817; -0.002059124158995844 -0.0006031785131164181 0.00018411143978473124; 0.0001993374625819575 0.0005447396330755471 -0.00011583619320195142; 0.0006967990814345197 0.0005681562638154574 0.001525154052293515; 0.0015943031278721253 0.001706432676919408 -0.0017754098324820468; 0.0005012319336341951 -0.011664166419079943 -0.008308596621732472] %
+
+Mass Used: 85.46642781376659 kg
+Launch C3: 97.16122854789363 km²/s²
+||V∞_in||: 3.3189154733596415e-9 km/s
diff --git a/archive/ES_0.5590653572123191 b/archive/ES_0.5590653572123191
new file mode 100644
index 0000000..6f2dea9
--- /dev/null
+++ b/archive/ES_0.5590653572123191
@@ -0,0 +1,22 @@
+archive/ES_0.5590653572123191---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:27:31.932
+Launch V∞: [7.709112024453563, -5.893511482544447, 0.12647043630582475] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1263210259758237e-6, -1.952256367082667e-5, 0.0004642410759175342] km/s
+ V∞_out: [1.839660254403635e-5, -0.00046417702401829015, 4.794631130200443e-6] km/s
+ time of flight: 1.8312185089673734e8 seconds
+ arrival date: 2030-03-02T18:38:21.932
+ thrust profile: [0.5228862287041272 -0.00614738736989348 -0.15936459997395488; 0.08870463774472251 0.052687928034085806 -0.09699137770872479; 0.045622073221395644 0.042294272070390625 -0.08642576210177026; 0.02794550703026744 0.03425073804237963 -0.08215006498020318; 0.021009286856826254 0.032108976158029386 -0.0845720020974858; 0.02218205630671919 0.04998671649324326 -0.1197423022572621; 0.018016221050320937 0.039808634779946915 -0.11307869365192288; 0.0036096649652670515 0.009881583023996436 -0.029686683121369857; 0.0033836465750719537 0.009069696327661676 -0.029663132069073034; 0.0017858611687173631 0.006918529851142733 -0.024456054961316847; 0.0015679243156932821 0.0020360113225321276 -0.013278888469622411; 0.00294243486146392 0.01655096447536 -0.05415280330640087; -0.0013148445455307507 0.0003906718461260851 -0.0020360462727318476; 0.0007690305716582102 -8.431947015115999e-5 -0.002639719175385775; -0.0009938598099307342 0.002783275160431468 -0.0013647364389985082; -0.0012982453146701063 -0.00035503604811998356 -0.0006407981314917107; -0.0015538983343233196 0.0013404632031499006 -0.0016695797805611522; 0.0012192981114749414 -0.002028873428299623 0.0014111516921857842; 0.00031164335055107397 4.6704279926528414e-5 -0.000562194242505989; -0.0016990287275065407 0.00033076689918020395 0.001741328463278099] %
+
+Mass Used: 102.86028007935556 kg
+Launch C3: 94.17988057171715 km²/s²
+||V∞_in||: 0.0004646562474587604 km/s
diff --git a/archive/ES_0.5590727750891238 b/archive/ES_0.5590727750891238
new file mode 100644
index 0000000..1da1db1
--- /dev/null
+++ b/archive/ES_0.5590727750891238
@@ -0,0 +1,22 @@
+archive/ES_0.5590727750891238---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:23:05.361
+Launch V∞: [8.058798370733799, -5.664092597407848, 0.641319639445587] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.04336037770181584, 0.2682848921054265, 0.27136829063823836] km/s
+ V∞_out: [-0.0645163866311401, 0.06226822992815729, -0.3738149718420198] km/s
+ time of flight: 1.8749577787115765e8 seconds
+ arrival date: 2030-04-24T00:32:42.361
+ thrust profile: [0.3024451379280253 -0.005356873154635282 -0.10125772560555663; 0.06008463797958302 0.031019193668489008 -0.07207121192480131; 0.04516762060937244 0.036573592551877525 -0.0968445011766846; 0.03624502651995864 0.03738521336310042 -0.11337532081513657; 0.029829761986304795 0.03635066108773556 -0.12342467611334798; 0.025166378257800742 0.034743750840259206 -0.12966540022766548; 0.011233208100516427 0.017415568886077173 -0.07056514122831103; 0.00495595759635792 0.008392754644341584 -0.03512311463357052; 0.0019433607636408269 0.003285341389566211 -0.015977464743574404; 0.0011891774028152807 0.0021998216394298288 -0.01125959523970976; 0.000794542202564106 0.001047337565768697 -0.007400929918211928; -4.5634041058395904e-5 0.0006291266967622854 -0.0004251595173555738; -0.00013868790239703914 0.0032562992137579808 0.0015799767277308906; -0.0025865240558218235 0.0018016651467942467 0.0009711990175341224; -0.0007082446535857972 -0.003697221155398593 -0.0026009965711328133; 0.000748441514889031 -0.007437459021339597 0.002812658819614197; -0.006062456167580747 -0.004367421229308305 0.0028412683262035547; 0.0022968967219796953 0.00595331593781554 -0.0013433334958902806; 0.002363042311108869 0.001900489614780768 -0.003959723297726512; 0.011326135463688658 0.007669707346341911 0.0026098151783113797] %
+
+Mass Used: 83.86634670011517 kg
+Launch C3: 97.43746701209072 km²/s²
+||V∞_in||: 0.38405423425654855 km/s
diff --git a/archive/ES_0.5590727938116964 b/archive/ES_0.5590727938116964
new file mode 100644
index 0000000..1503de9
--- /dev/null
+++ b/archive/ES_0.5590727938116964
@@ -0,0 +1,22 @@
+archive/ES_0.5590727938116964---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T00:41:23.439
+Launch V∞: [8.043305772061222, -5.899796267076807, 0.12427958829635194] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.68614383813471e-6, -3.829028172228055e-5, 0.0006790854994286309] km/s
+ V∞_out: [2.744046902279885e-5, -0.0006809225575325621, 9.09832505987437e-6] km/s
+ time of flight: 1.8749577787400967e8 seconds
+ arrival date: 2030-04-27T02:51:00.439
+ thrust profile: [0.15626937519931453 -0.0044811759488521735 -0.06049490272344524; 0.06415066463902236 0.030081864500616947 -0.08587984384458591; 0.03461550611865766 0.024722884190145056 -0.08330946000756498; 0.031160629267154485 0.027591962301299924 -0.10884146310951637; 0.026195759497753737 0.0269901929225214 -0.12177243123768812; 0.018419387614686377 0.02082624324894296 -0.10570580914780663; 0.00945970825115949 0.011419190889834051 -0.06507431008664706; 0.006533221344193563 0.010089559218887406 -0.05389616156496072; 0.004409985128686662 0.003953481306121377 -0.028156965686378384; 0.002226863902748846 0.005027918207037112 -0.03541090033041392; 0.0006428921996911921 0.0011224456686388406 -0.015979010695998726; 0.0017413127558764756 0.0003006099335503653 -0.008855107652463317; 0.002403625460546274 -0.0010921419364152084 -0.0006659299077316763; 0.0014845579403633632 -0.0016767999756181992 -0.00200123966373443; 0.0003685761461080602 0.0010570574033976746 -0.0015819759222086604; 0.0007565832854240439 0.000588570469648337 -0.003138379631762389; -0.0019608149515314764 -0.0005316238702083067 -0.0011584380175211017; 0.0017229973566544583 0.00013303851626230323 6.755124683964324e-6; -0.003476767645231386 0.00262813236344015 0.0006710632325314336; 0.0017764730228363194 0.0035065983210861265 -0.0003049836040456351] %
+
+Mass Used: 71.73103939391467 kg
+Launch C3: 99.51780915195391 km²/s²
+||V∞_in||: 0.0006801802857718506 km/s
diff --git a/archive/ES_0.5590763252058891 b/archive/ES_0.5590763252058891
new file mode 100644
index 0000000..1b85aac
--- /dev/null
+++ b/archive/ES_0.5590763252058891
@@ -0,0 +1,22 @@
+archive/ES_0.5590763252058891---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T16:59:47.595
+Launch V∞: [7.945333539989612, -5.66705696951981, 0.005616058949671385] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.897607049931995e-9, -1.3800041801807833e-8, 2.7651358326396277e-9] km/s
+ V∞_out: [-5.5183442392974284e-9, -1.0697077720645447e-8, -2.7758671875981e-10] km/s
+ time of flight: 1.8749577779907453e8 seconds
+ arrival date: 2030-04-21T19:09:24.595
+ thrust profile: [0.36921835258799046 0.01651937096443451 -0.09859273743933632; 0.1288290434449125 0.08849780822873207 -0.12651166469101432; 0.0684253996851831 0.07764795311700873 -0.12718815310746023; 0.025526686675202793 0.03926648382162931 -0.07536175440734175; 0.02316475712972108 0.04544837008368432 -0.09462073741323969; 0.017281751467596383 0.04207455652931017 -0.093717542617397; 0.010454135140531411 0.030895726254733226 -0.07326808491478282; 0.007884912604211891 0.03349637816427468 -0.08222517442834602; 0.002038760678978414 0.010200074427979981 -0.02777367463298412; 0.0014477171093319502 0.006951800278034221 -0.01811138943656302; -0.0006948149120520983 -0.0007955973154868096 -0.00032502022881245886; -0.0006955609149481525 0.0010619495402220693 0.0004347203962689315; 0.00026501239743267793 -0.0007085581476906264 0.0012501838694275263; 0.0015358365496732631 -0.0009281198315094894 0.0008880718024233711; -0.0006900198203010485 0.0013920380856930071 -0.0020870881852627244; 0.0008682473174843035 -0.002037554816461659 0.0014557843578257425; -0.00224441314488133 -0.0008389644005982558 0.0033432614959403683; 0.003048077479714198 0.00014918306423710963 0.005422979646529079; -0.0007642785390706013 0.0008695498868113798 -0.00041535373484342594; -0.0004933838284356558 0.004967956716802426 0.002597768692753838] %
+
+Mass Used: 96.66634683762459 kg
+Launch C3: 95.24389129758504 km²/s²
+||V∞_in||: 1.4902136917909955e-8 km/s
diff --git a/archive/ES_0.5590853931092332 b/archive/ES_0.5590853931092332
new file mode 100644
index 0000000..28ce6b0
--- /dev/null
+++ b/archive/ES_0.5590853931092332
@@ -0,0 +1,22 @@
+archive/ES_0.5590853931092332---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T03:09:06.165
+Launch V∞: [8.090517627110012, -5.6299974083563455, 0.3310575047229668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.974440909039003e-7, 8.90456904334183e-6, -0.00018741872187090023] km/s
+ V∞_out: [-7.521261308122424e-6, 0.0001905637173813942, -3.2780733869860804e-6] km/s
+ time of flight: 1.8713756316444254e8 seconds
+ arrival date: 2030-04-19T01:48:29.165
+ thrust profile: [0.3084664424967537 0.0029712841117369693 -0.0937365196994249; 0.05785664938672707 0.03396033370094407 -0.06661818361825321; 0.02528764600978114 0.023980580686659494 -0.05425535248479294; 0.030235044810571255 0.03753810214842792 -0.09355724722589731; 0.024910693055591158 0.03796171077415384 -0.10332297617781312; 0.012928369951252374 0.023111177939166283 -0.07058532773898502; 0.007083611766232259 0.014799202300987208 -0.04865808682330675; 0.007500762756217629 0.017629399041550226 -0.061653729022275644; 0.009075366350372567 0.02578624153779068 -0.09217107421846685; 0.0016690305043186155 0.004860983017264024 -0.019702670163399483; 0.008957823104081816 0.026054237946831572 -0.09995649699397653; -0.0003355910861454726 -0.0007545516142037534 -0.002005701861294032; 0.0004285384105894185 9.575279836211703e-5 0.0003594158067775112; 0.002060020655393492 0.001426965455466726 -0.0034871617886117357; -0.001256291245599493 -0.000319332463672755 0.0001073005119506744; -0.001309453485795298 -0.0033082449192264243 0.002330216545125891; 0.0029225188160215717 0.0016250540517900726 0.00029625045690121507; -0.0009116124178509016 -0.0016322778454465143 0.0021968885742100603; -0.0009570460775604258 -0.004741407224840451 -0.0006651910960586891; 0.0004788184163202758 -0.003057129343738884 -0.0034025528389380706] %
+
+Mass Used: 84.89911067012827 kg
+Launch C3: 97.26294536411038 km²/s²
+||V∞_in||: 0.0001876322841716366 km/s
diff --git a/archive/ES_0.5590882724093249 b/archive/ES_0.5590882724093249
new file mode 100644
index 0000000..1a8d0ef
--- /dev/null
+++ b/archive/ES_0.5590882724093249
@@ -0,0 +1,22 @@
+archive/ES_0.5590882724093249---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T03:13:02.223
+Launch V∞: [8.005883771735034, -5.902650970949108, 0.08701989613519921] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.423215940821355e-5, 5.110406237217132e-5, 0.003509526665397896] km/s
+ V∞_out: [-0.0031147074403920327, -0.001186002555933269, 0.0011025226200048462] km/s
+ time of flight: 1.8425402983623484e8 seconds
+ arrival date: 2030-03-18T16:53:31.223
+ thrust profile: [0.1843393440150439 -0.009836806729550899 -0.07064825544700455; 0.02930563430357018 0.013094881257607835 -0.03848906089739787; 0.04285358248911719 0.030281293561756437 -0.09816438904735685; 0.044153008585800284 0.03905311440083149 -0.14498829987237105; 0.033094590327099674 0.03362061141454112 -0.14206791216669903; 0.02648403684528507 0.029593809317185114 -0.13858057347291264; 0.012262045627725789 0.015122678955000805 -0.0777034359994379; 0.004550114007496143 0.0060837369239010565 -0.033668218157134965; 0.003292550810445449 0.004735746798977688 -0.027358394452567245; -0.00010781403740294827 -0.0006306536885763099 -0.00519061269336375; 0.00304182660657319 0.0019595959419477947 -0.00776949126117267; -0.001987331320953648 -4.649699390884903e-5 -0.0014005494322347988; 0.0005583743265207646 0.0003117706164752665 -0.0035564320571179735; -0.0002965781259881248 -0.006373233783390586 -0.0044181206154130645; -0.0006877893395176703 0.0048294452084446035 -0.001809215301078142; 0.005436279140197594 -0.001568757780834862 -0.006656981634768947; -0.00040061323543829144 0.0010956588095184074 -0.006322835983464531; -0.008676687954857928 -0.003849982364358748 -0.003910783483890378; 0.0026025590353062384 0.004752463668232791 -0.0010128558128361755; -0.0016403467623270413 0.006059267623893997 -0.004704039752448118] %
+
+Mass Used: 75.10194164762788 kg
+Launch C3: 98.9430359137002 km²/s²
+||V∞_in||: 0.003510683616308969 km/s
diff --git a/archive/ES_0.5590926010085676 b/archive/ES_0.5590926010085676
new file mode 100644
index 0000000..8a766a3
--- /dev/null
+++ b/archive/ES_0.5590926010085676
@@ -0,0 +1,22 @@
+archive/ES_0.5590926010085676---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T15:23:18.102
+Launch V∞: [7.987142808098617, -5.62760560368367, 0.07802208598230424] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8726517384567137e-5, 2.5142738583420766e-5, -1.9271132722336087e-5] km/s
+ V∞_out: [6.383903800441171e-6, 4.2331975003916124e-5, -1.933855632158849e-6] km/s
+ time of flight: 1.855415032781355e8 seconds
+ arrival date: 2030-03-29T02:41:41.102
+ thrust profile: [0.4096434747092699 0.006436691318163344 -0.10884631063602794; 0.08372249772688349 0.055952731978148776 -0.08724067343239678; 0.04308420110867305 0.0490838612328076 -0.08465670318083521; 0.02875464172419043 0.043154476342007565 -0.08311264112088046; 0.0322374916874482 0.06269433047700697 -0.12710822031867539; 0.019331854856482433 0.048304753131312994 -0.10641721157318978; 0.00917681919262174 0.024219913214989036 -0.059776657324025075; 0.009869756721773282 0.02965892598642382 -0.07595856642652665; 0.006313565968435064 0.021053027771978563 -0.05845248471821262; 0.0005938083334897739 0.003008684362163146 -0.009209579175583514; 0.0003821758020110806 0.010363655056657666 -0.030429812708281857; 0.00016000598368632257 0.0003249990571190977 -0.00035456668053182117; 0.00039607196168249667 -0.0003061913453085023 0.00013795790299143094; -0.001271343905587384 -0.0006244074186601699 0.00030982047353599095; 0.0015762369759475298 -0.00018566019722323122 0.00010924090820121197; 0.00029232813642033955 -0.0006675384912884861 0.0022235322501183235; 0.0002191152448127142 -0.001360089255904951 0.0015683954853620197; 0.0009444100018686669 -0.002070789978027908 -0.00011472928997803501; 0.0007945603473219442 -0.0012141438582031156 0.0009670363058326612; -0.0005115566201268572 -9.678003322196652e-5 -0.0006583183726929002] %
+
+Mass Used: 95.36355318139522 kg
+Launch C3: 95.47048251347434 km²/s²
+||V∞_in||: 4.27638475925865e-5 km/s
diff --git a/archive/ES_0.5590956397432519 b/archive/ES_0.5590956397432519
new file mode 100644
index 0000000..8e68848
--- /dev/null
+++ b/archive/ES_0.5590956397432519
@@ -0,0 +1,22 @@
+archive/ES_0.5590956397432519---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T21:28:09.594
+Launch V∞: [7.660321662192601, -5.970272328994087, 0.13474117837824268] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3347102424139626e-7, 1.3968767198886338e-6, -3.8030966551739165e-5] km/s
+ V∞_out: [-1.5718854172580713e-6, 3.800225468731313e-5, -2.9363174597336245e-7] km/s
+ time of flight: 1.790665401419603e8 seconds
+ arrival date: 2030-01-13T10:10:29.594
+ thrust profile: [0.47952424197590793 -0.022302087389525414 -0.13195158372453386; 0.10497312815848478 0.05601938094866379 -0.11061897757622594; 0.058172312696924286 0.05009524771938647 -0.10861729497730198; 0.045109526834707696 0.05149430633267891 -0.12362048033824143; 0.03605791999114776 0.05033864243591565 -0.13005493954020747; 0.014770991979128524 0.02336535580059945 -0.0678681838183577; 0.018471218155123658 0.0349608322626088 -0.10563281319477572; 0.0150701384338594 0.03336922811551264 -0.10703012508397958; 0.0004970331675266376 0.0011364003635421626 -0.004658595602191562; 0.002620325204462028 0.002844944003891334 -0.014180737656346285; 0.0009968645447899383 0.0007685172524976291 -0.0017968245536104767; 0.0003389271228562323 0.0008779100932656772 -0.0031622658118521303; -0.00069988593885781 0.0005824960887682072 -0.0012701884275687493; 0.001020101873055537 -0.001171589489490191 -0.004071326336353124; -0.0005954492945202388 0.0036482344695543227 -0.0004383492530407218; 0.0005167058442274472 -0.00342649313196755 -0.0019138169254815374; 0.005307155189497238 0.0016138161959539737 0.000425521380242895; 0.0024149811016501025 0.0024733909795415002 0.00046805780685287425; -0.0005715118179959715 0.001367640219981335 -0.0027734986676369736; 0.0002939166680668769 0.0009963159033409613 0.0002843187200824379] %
+
+Mass Used: 101.94504315852464 kg
+Launch C3: 94.34283483576044 km²/s²
+||V∞_in||: 3.805732768008325e-5 km/s
diff --git a/archive/ES_0.5590975080072035 b/archive/ES_0.5590975080072035
new file mode 100644
index 0000000..d901b3d
--- /dev/null
+++ b/archive/ES_0.5590975080072035
@@ -0,0 +1,22 @@
+archive/ES_0.5590975080072035---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T14:52:56.121
+Launch V∞: [8.072518173453508, -5.831730425933822, 0.09584490005440607] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0461122874855896e-6, -9.067485184924221e-6, 0.0001794971225712157] km/s
+ V∞_out: [6.3352119149713254e-6, -0.000179100109462777, 1.8401541926655394e-6] km/s
+ time of flight: 1.8524623168337333e8 seconds
+ arrival date: 2030-03-29T16:10:07.121
+ thrust profile: [0.11717098268170827 -0.003974520411409332 -0.04283543455578055; 0.06925798604043731 0.03418486653570566 -0.08428156129218403; 0.05953052007810014 0.047008330868805466 -0.12934394525311563; 0.02551688788144415 0.025266163808985023 -0.08232766265865023; 0.034255582360729425 0.04043797346562564 -0.1435802396167452; 0.02382076032765613 0.032029584777816665 -0.12473243279571947; 0.011605996416981311 0.01625365677763313 -0.07113920249714945; 0.006660214031932906 0.010824479644483818 -0.050616194473038875; 0.003302515212526192 0.0031673555006713257 -0.012394140697699375; 0.0020778654037118833 0.0036834033539545536 -0.020164706656769622; 0.006652630383625702 0.001343475497661042 -0.01846408064426289; -0.004454079446589999 0.003467140372697148 -0.0061405761163761076; -0.0005484893335878417 0.0012484002593508392 -0.004086459319963795; -0.0013777934229539318 -0.0015955653649430313 -0.0021943447883130598; -0.0015287890986250149 0.0015307805936296667 -0.00021171199157335322; -0.00012938126292587416 -0.0071996145953635345 0.0006898888463313166; 0.0002860012018939689 0.00023868232361069856 -0.0013101501531601102; -0.0010527769714863743 0.003346015682625659 0.003821028580116423; 0.0013416101526361871 0.0006401805263494409 -0.005123806538908192; -0.003895135874093166 -0.0004329457702771944 0.019400210489683156] %
+
+Mass Used: 73.70816795460314 kg
+Launch C3: 99.18381566636587 km²/s²
+||V∞_in||: 0.00017972904787441255 km/s
diff --git a/archive/ES_0.5591001869278887 b/archive/ES_0.5591001869278887
new file mode 100644
index 0000000..181b0d6
--- /dev/null
+++ b/archive/ES_0.5591001869278887
@@ -0,0 +1,22 @@
+archive/ES_0.5591001869278887---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T01:15:46.891
+Launch V∞: [8.0503342501567, -5.710268166309256, 0.15130430977225054] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.38824212391832e-7, 8.533759406329629e-7, -2.079813943212524e-5] km/s
+ V∞_out: [-9.446902677594962e-7, 2.07928696582257e-5, -2.508478339700837e-7] km/s
+ time of flight: 1.8749577787493393e8 seconds
+ arrival date: 2030-04-25T03:25:23.891
+ thrust profile: [0.33309402395582083 -0.005856324704721741 -0.11550923747000598; 0.0316993033841911 0.01469306982092588 -0.04354993879065942; 0.026920995941371203 0.019625515480867883 -0.06540957990494227; 0.026106693904981455 0.02340396103210875 -0.08944554544242546; 0.019755730355901505 0.020641102666654542 -0.0891140784657623; 0.0187993503167118 0.021534916548244045 -0.10279294926743925; 0.013521373574719288 0.016005091072537954 -0.08868627705597877; 0.007429196487410106 0.010270878731625523 -0.0686355630569617; 0.002352280862150242 0.004535015254035295 -0.026675947495953898; 0.004387991737477275 0.007017952565088675 -0.04371557635370267; 0.007922644169974865 0.01095390089547627 -0.07687603350965613; -0.00042260122513377023 0.00032331427079231425 -0.006256549583417095; -9.287918042476343e-5 0.001833452182016635 0.002744622520430659; -0.00034093385186790057 -0.0022499582447111336 0.0032264847398771413; -0.0021096624640105717 -0.00086663844286747 0.0008322649938094855; 0.0022352948171309815 0.0010555777252738647 -5.4009456904453336e-5; -0.0005448204321158313 0.005174905611712478 0.00288615470131916; 0.00285885885361526 0.0002534161968304966 0.00041749976931923917; -0.0033245173270379774 0.005063076461087352 -0.0013220365950805618; -0.0005182105925172773 -0.0002992483364500859 0.0012823413593137365] %
+
+Mass Used: 83.89558520589844 kg
+Launch C3: 97.43793706456657 km²/s²
+||V∞_in||: 2.0816102576998418e-5 km/s
diff --git a/archive/ES_0.5591015965644661 b/archive/ES_0.5591015965644661
new file mode 100644
index 0000000..16c474c
--- /dev/null
+++ b/archive/ES_0.5591015965644661
@@ -0,0 +1,22 @@
+archive/ES_0.5591015965644661---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T12:15:27.316
+Launch V∞: [7.846909384770033, -5.901574957731044, 0.0713337604825376] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0010569288574070934, -0.000725426165238938, -0.0428527020534814] km/s
+ V∞_out: [0.03820931788483934, 0.01747794222321807, -0.008523353651918529] km/s
+ time of flight: 1.801168436289526e8 seconds
+ arrival date: 2030-01-26T04:42:50.316
+ thrust profile: [0.27987631152950454 -0.01680500051261107 -0.09477210047731892; 0.17167787476969892 0.08212190542028253 -0.18567990798923245; 0.039211665808318294 0.030540768544990042 -0.08204589087320158; 0.034414747737070296 0.03529104791363199 -0.10495148999019628; 0.01898728326034085 0.023457907245099947 -0.07784725726326484; 0.02024544060612833 0.02858347348208293 -0.10271337730950485; 0.020491648347633992 0.03288160710492584 -0.1253788033217463; 0.007616714197197251 0.013083282955519977 -0.0555844937340011; 0.004603159100239627 0.00857021282584722 -0.03882975883358092; 0.0021305676207429933 0.004280065836889343 -0.020407942742707637; -5.508510043272319e-5 0.00023603293877342717 -0.0017047507794211133; 0.0010303644206570875 0.0013833392018587774 -0.007740628148002049; -0.0003472938348156449 0.0009976257825556102 -0.0011664158151241874; 0.000268476914894888 0.0007516382630753876 -0.0014750329186264764; 0.0009630555865799476 0.0009111100326696406 -0.0022258032256042117; 4.72977399844644e-5 0.0013218061222341664 0.0010192946419317027; 0.003093681258467887 0.0004194980940042844 -0.0013643072782259554; 0.0010952566670476803 0.006283952739479957 -0.004061895479174443; -0.0021823057511413226 -0.0044049504138940765 0.0005017574472371007; 0.00044890893139318635 -0.00227390387554891 0.0043498562241801805] %
+
+Mass Used: 89.90716544249108 kg
+Launch C3: 96.40766237989476 km²/s²
+||V∞_in||: 0.042871872072668835 km/s
diff --git a/archive/ES_0.559113248360976 b/archive/ES_0.559113248360976
new file mode 100644
index 0000000..50c425e
--- /dev/null
+++ b/archive/ES_0.559113248360976
@@ -0,0 +1,22 @@
+archive/ES_0.559113248360976---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T15:48:15.219
+Launch V∞: [7.942420577700226, -5.856646668515265, 0.3214450514599138] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.895025903768771e-5, 1.9711829182926244e-5, 0.00138803419995162] km/s
+ V∞_out: [-0.0012398069623974855, -0.0004202292439609665, 0.0004814663048145262] km/s
+ time of flight: 1.8584152651952314e8 seconds
+ arrival date: 2030-04-05T14:27:01.219
+ thrust profile: [0.2891353191018947 -0.0031355302315698506 -0.0925233056906119; 0.042087920412326674 0.02315112517316813 -0.0521010725573201; 0.05645570566751917 0.05040411660907987 -0.1208029218729849; 0.021993202445333815 0.024917825791832417 -0.07093149023566632; 0.037357260783821 0.05165118678234891 -0.15406947412184566; 0.015373458452472432 0.02452372634414184 -0.08362316417643735; 0.015368965052511122 0.028452948232279396 -0.10147505602198326; 0.007353469839855173 0.01439645225722635 -0.05855966000383456; 0.0035935989920301246 0.006798943967894126 -0.031313232568349864; 0.0017935860171264758 0.0029823448389833464 -0.015721714985052784; 0.0023862732419761244 0.005483531431770156 -0.025890434368456082; 0.0017063374802508686 0.00021977071944114386 0.002047528453949313; 0.0027331511933384543 0.003178029400605864 6.190339925305714e-5; -0.0028197045170709105 -0.0008475002598726715 -0.0012900103680358543; 0.0008102159660781907 0.0017005247831508104 0.0005464998377893962; 0.0004301785803593422 0.004361336537674808 0.0005940903406136131; -0.0006620744868718906 -0.0028432822290890966 0.006931041228979296; 0.0005431784119633238 -0.0012039761076405291 0.003097853091636223; -0.00022436123054919794 -0.0009309990652092569 0.005467754646183315; -0.0009761021988405361 0.0024754230546871927 -0.003647286450832711] %
+
+Mass Used: 83.63231285605116 kg
+Launch C3: 97.485681754015 km²/s²
+||V∞_in||: 0.0013884760040934882 km/s
diff --git a/archive/ES_0.5591223761021502 b/archive/ES_0.5591223761021502
new file mode 100644
index 0000000..4a217ed
--- /dev/null
+++ b/archive/ES_0.5591223761021502
@@ -0,0 +1,22 @@
+archive/ES_0.5591223761021502---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T16:50:52.926
+Launch V∞: [7.960109400843555, -5.566384650061473, 0.28405685643984185] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.371764957862641e-10, 2.075179690534501e-9, -2.076081194906843e-9] km/s
+ V∞_out: [1.7405289143618078e-9, 3.181054104183071e-9, 8.972928204099919e-11] km/s
+ time of flight: 1.8749577785222417e8 seconds
+ arrival date: 2030-04-20T19:00:29.926
+ thrust profile: [0.47567809810379036 0.011326974493132212 -0.11891904196547373; 0.13888466722413476 0.09469448823019538 -0.13342346906839192; 0.02849662180675522 0.03237342444877543 -0.05496678945039215; 0.03493965596138767 0.053873863796943054 -0.0995915696237253; 0.015977168418565023 0.03099402290947448 -0.06341058675147594; 0.020586065242794126 0.05134843488994801 -0.10970822691720213; 0.009383526247436035 0.028102910159133274 -0.06514998083209053; 0.006287439771191652 0.02288648598764084 -0.05568183917860841; 0.006737082620600399 0.028390858286468947 -0.07296107102034485; 0.0020649158624402157 0.011771605908068508 -0.030082940789779817; 0.0004586048481906657 0.0031520638109395938 -0.011027908320784688; 0.0008993593757453753 0.0007565297657936231 -0.0015296061745331616; -0.000982296375117245 -0.0007775683645744422 -0.0011085136258141752; 0.0007508033645317597 -0.001286440532939554 0.00023539407493639616; -0.0004342821013677523 0.0010245023777203052 0.001361154760021961; -0.001099014673636675 -0.0014572028223965821 0.0008053565647180168; 0.0010112632458920015 -0.0006255274934698584 0.0016228680439288065; -0.002892207577425165 0.0007702153506890954 8.65634250817942e-5; 0.00024426157078100125 0.00044513592492344603 -0.0005668806136792355; 0.0007362876563143342 0.0010869972595567937 -0.00039406792568339464] %
+
+Mass Used: 101.4755418652594 kg
+Launch C3: 94.42866804352842 km²/s²
+||V∞_in||: 3.026534827454065e-9 km/s
diff --git a/archive/ES_0.5591255737389962 b/archive/ES_0.5591255737389962
new file mode 100644
index 0000000..253a1d6
--- /dev/null
+++ b/archive/ES_0.5591255737389962
@@ -0,0 +1,22 @@
+archive/ES_0.5591255737389962---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T17:32:59.333
+Launch V∞: [7.918419622978759, -5.885287437969329, 0.11916580452977898] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.712171556053025e-5, 3.826131521766802e-5, 0.00270402592362838] km/s
+ V∞_out: [-0.002561123575757956, -0.000814398242085282, 0.0003732067371911131] km/s
+ time of flight: 1.8110833219408208e8 seconds
+ arrival date: 2030-02-07T21:25:11.333
+ thrust profile: [0.2982818630830107 -0.019644150774660783 -0.09412579431984003; 0.04059895775014474 0.020789202368681238 -0.04807454209411865; 0.03767803952502041 0.029543331085182922 -0.08547086171724246; 0.02909629919118133 0.02955845433003741 -0.09639038404264533; 0.019550491267592368 0.02250280171794553 -0.08336426534176022; 0.040299241786395885 0.048783266117244276 -0.17924308655017618; 0.013163316067294706 0.01982525932153663 -0.08918763458638637; 0.00953680042318693 0.014346053265430323 -0.06651023041543352; 0.009805953214385791 0.015381825239116149 -0.06819819180479254; 0.001769476083858948 0.002948414470196621 -0.017211955694236253; 0.0024437777852011904 0.004834903527360775 -0.0318912392395312; 0.00014283855886567407 0.0009379859417732434 -0.0009207644059078049; 0.0004706077357866879 1.1478260569768332e-5 -0.001860050159258833; -3.571042668652721e-5 0.00012724234215442807 0.0012497835548845669; -0.000698770959925517 -0.00017789861303480712 0.0012611586305108853; -0.0019633273176587938 -0.0002653058008441901 0.003511111805669046; -0.0011061829057160885 0.0009367511706530119 0.005138323079079068; 0.00012082784985850865 -8.836127735034843e-5 -0.0017427816628923993; 0.00016733439593413514 0.00271353934451311 -0.004696344872237696; -0.0010586452889067184 0.0035367221700403225 0.004081638990627479] %
+
+Mass Used: 84.4254641167895 kg
+Launch C3: 97.3521780420639 km²/s²
+||V∞_in||: 0.002704899815942372 km/s
diff --git a/archive/ES_0.559132422658741 b/archive/ES_0.559132422658741
new file mode 100644
index 0000000..ed689d6
--- /dev/null
+++ b/archive/ES_0.559132422658741
@@ -0,0 +1,22 @@
+archive/ES_0.559132422658741---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:21:59.996
+Launch V∞: [7.83137572922902, -5.69898297535263, 0.40932901263877103] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0046861323185856275, 0.002366029283790581, 0.00020459761275283474] km/s
+ V∞_out: [-0.00350263978957366, -0.002370032760850909, 0.003111809289241098] km/s
+ time of flight: 1.8749577787473112e8 seconds
+ arrival date: 2030-04-21T11:31:36.996
+ thrust profile: [0.457558383212383 0.012640527463407799 -0.1043321976963303; 0.13979296224474827 0.09386798500197852 -0.1256846889524545; 0.07411806139737996 0.08205676631445241 -0.12568348116252803; 0.05809778648720754 0.08709807889503329 -0.14487367059149134; 0.0223045427130996 0.046437999733405635 -0.08452456869492442; 0.014930813575107553 0.03789696854913079 -0.07325048081080965; 0.011971130957232769 0.030336318454899633 -0.06578209027506235; 0.002254759521761372 0.008751803618381624 -0.01933449302205777; 0.0019193215810550414 0.010632211635018282 -0.03017334260616061; 0.0018206952522375529 0.004986732575196764 -0.018245341789475896; 0.0001163435608454544 0.0016598902772169868 -0.004708778069304699; -0.0027255196319326547 0.0003282425116501544 0.0005151693367653897; 0.0006070681599377359 0.0014919167829855649 -0.0005120694622984256; 0.00030961962188294327 -0.0003652705004350195 0.0015695053194356684; -0.0014251478565237507 -0.0009354325222741594 -0.0026482074693615666; 0.0006562253249217193 0.0011359313901323697 0.00022132694991615614; 0.0009255641515388109 -0.005285058883896716 -0.005165152362708073; 0.0008933993388544174 0.0012745579916680037 -0.002643653415840136; -0.0023918787493834716 -0.002259488492329772 0.002568900088835936; -0.005005617197609643 0.004506928423325265 0.007441246545533205] %
+
+Mass Used: 104.12547556508935 kg
+Launch C3: 93.9764030063043 km²/s²
+||V∞_in||: 0.005253550310237015 km/s
diff --git a/archive/ES_0.5591517161010692 b/archive/ES_0.5591517161010692
new file mode 100644
index 0000000..8573240
--- /dev/null
+++ b/archive/ES_0.5591517161010692
@@ -0,0 +1,22 @@
+archive/ES_0.5591517161010692---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T17:34:57.285
+Launch V∞: [7.576996702672796, -5.8342896661354615, 0.22626168982012046] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7933321896948425e-6, -4.781243495153424e-6, -1.2758089963721867e-5] km/s
+ V∞_out: [-1.2638421997231841e-5, -1.4081665374171792e-6, 5.124927962241741e-6] km/s
+ time of flight: 1.8556836855601722e8 seconds
+ arrival date: 2030-03-30T12:21:05.285
+ thrust profile: [0.7057030920868201 0.015110196027611628 -0.16932834003611266; 0.105738442337943 0.0664416837698034 -0.1032149328893404; 0.07878167066118814 0.08210511208782267 -0.13926140345296611; 0.03869185961976151 0.053580333128455414 -0.10391776481167966; 0.03473675416395673 0.06134307871090222 -0.12865290043855548; 0.015009494074865369 0.031407409615589306 -0.07272412733915154; 0.007994288604892362 0.019486352151301616 -0.0486409502195103; 0.0061092125613843124 0.01773614276883973 -0.046252080649018236; 0.0021384801601208553 0.007183365594706161 -0.019175136451686836; -1.161110202157231e-5 0.002027419611716001 -0.00335306055473439; 0.000966832167588032 0.004174448999598176 -0.012070889383927016; 0.0006201386791079219 0.0006097518827567433 -0.0033698227228844383; 4.531730772603304e-5 0.0002151905433761831 -0.002343607230302726; -0.00034291125795572037 0.0012093969288103942 -0.0034892933013982333; 0.004847894624391267 -0.0012625316616039872 -0.005413047015109706; 0.003854761434035017 -0.0013326938328889143 -0.010483477433531771; -0.002008384265145428 -0.0012870400110940592 0.001156304771094731; 0.0001257648365572869 0.0050545409140075465 -0.006764168927637203; 0.0017599040212021477 -0.00227676547138212 -0.0044818914512407175; 0.0005780262581169737 -0.00013297302177690362 -0.0017474310693637429] %
+
+Mass Used: 118.58778124225728 kg
+Launch C3: 91.50100929296973 km²/s²
+||V∞_in||: 1.3742095517968257e-5 km/s
diff --git a/archive/ES_0.5591580595461509 b/archive/ES_0.5591580595461509
new file mode 100644
index 0000000..66eedd5
--- /dev/null
+++ b/archive/ES_0.5591580595461509
@@ -0,0 +1,22 @@
+archive/ES_0.5591580595461509---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:45:04.948
+Launch V∞: [7.99922753094915, -5.520559209091305, 0.7107823677285222] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.006428398913349e-7, -2.745386711728288e-6, 5.416541819691074e-5] km/s
+ V∞_out: [2.171812349832689e-6, -5.414890026306697e-5, 6.10943263583267e-7] km/s
+ time of flight: 1.8749577787456098e8 seconds
+ arrival date: 2030-04-21T06:54:41.948
+ thrust profile: [0.5162280813765016 0.008869571155255449 -0.13927212968893854; 0.07301710595768034 0.045838827488127384 -0.07835542368092403; 0.043021665438833304 0.04375307677589343 -0.08443606061307102; 0.032459611267393176 0.04411676812962187 -0.09527903873350811; 0.01790965495738106 0.03003001737873939 -0.0725087058149848; 0.01315116621152908 0.026324439825188315 -0.06865228471679048; 0.015723125191174515 0.037772849624733186 -0.10357023215282914; 0.004854738311624418 0.013039194126060942 -0.03947940025008682; 0.004475076604690311 0.013557063003191858 -0.04263687335316479; 0.004453914111874324 0.01486953209173079 -0.04920949097472437; 0.0018339416842844372 0.007479161625087101 -0.026747561584490962; 0.0001387684690863793 0.00027158720085327086 -0.0013809863218187837; -5.050281799906807e-5 -0.00042251649304286636 -0.0003210498548899037; 0.0015025850791614787 2.0299042024343576e-5 0.002018612711974613; 0.002298088885250738 0.0017735348456962457 -0.00015381624395427343; 0.0020642700951995566 -0.0014856267491849418 -0.000524235253154955; -0.0002857105008183859 -0.001298671102501616 0.0036514427347495463; -7.285502161969874e-5 -0.0030092567704185736 0.001897830412179763; 0.0004848300426282524 -0.0008983163784383303 0.00020462271257407484; 0.0005505632563064208 -1.5746186675122525e-5 -0.00042491135917323666] %
+
+Mass Used: 98.36274736154292 kg
+Launch C3: 94.9694266472514 km²/s²
+||V∞_in||: 5.423578212545977e-5 km/s
diff --git a/archive/ES_0.5591591739434812 b/archive/ES_0.5591591739434812
new file mode 100644
index 0000000..163ab7f
--- /dev/null
+++ b/archive/ES_0.5591591739434812
@@ -0,0 +1,22 @@
+archive/ES_0.5591591739434812---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T05:34:49.890
+Launch V∞: [7.906955196844013, -5.728924223623509, 0.019665168779156056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0140386867511961, -0.008782336837163006, -0.0005637685652589615] km/s
+ V∞_out: [0.012312314094828846, 0.005204133259437067, -0.009835038073397221] km/s
+ time of flight: 1.8041971644442546e8 seconds
+ arrival date: 2030-01-27T10:10:05.890
+ thrust profile: [0.43275796308005354 -0.019111210788804362 -0.13120268886944356; 0.06339601736906268 0.03645636252543214 -0.07121505122293696; 0.07276240388727236 0.06590244932251536 -0.1361857349774072; 0.047929501589600555 0.056701384797779246 -0.13250647110676284; 0.037431689845481814 0.05577173316948346 -0.1382041026133042; 0.01730930398093252 0.031990630622241924 -0.08926803197015284; 0.010820935842034439 0.0222771465449321 -0.06839647325301179; 0.00794767666018845 0.01890568687094977 -0.05562370518578125; 0.0030079829738086697 0.008362198335991378 -0.03165911380239266; 0.0014032154014394845 0.007868553973404203 -0.02901193990522148; 0.0004447176974283271 0.0015776827399158044 -0.005634356396916214; 0.00036394128120801293 0.0027816415515139552 -0.010949121958049146; 5.8357484450519804e-5 0.00021877068104749978 -0.000696258523440477; -7.760841420810863e-5 1.5775260231069106e-7 -0.00024702922561635314; 0.00013152842006652253 9.726171574848536e-5 -0.00021241314920649292; -0.00013582869832218486 0.00021724131455663024 -5.183463010449243e-5; -8.64334304035059e-5 7.108038385010166e-5 -0.00010236379314709006; 2.487588792450629e-5 0.0001123125730288133 -0.00016212122953476472; -0.0001869936834435898 1.6093530629365415e-5 0.00021337158299636962; -0.00013768149700092112 9.30941814340271e-6 0.00010928547107773144] %
+
+Mass Used: 96.19711981200044 kg
+Launch C3: 95.3408999637819 km²/s²
+||V∞_in||: 0.01656900724288493 km/s
diff --git a/archive/ES_0.5591602932961567 b/archive/ES_0.5591602932961567
new file mode 100644
index 0000000..0b0f421
--- /dev/null
+++ b/archive/ES_0.5591602932961567
@@ -0,0 +1,22 @@
+archive/ES_0.5591602932961567---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:04:19.896
+Launch V∞: [7.826674897351051, -5.84370360166713, 0.10009121809289988] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.192862862213971e-5, -5.6303228665368466e-5, 4.214909596495661e-5] km/s
+ V∞_out: [-1.4559756120364109e-5, -9.944371056302013e-5, 4.502435509292896e-6] km/s
+ time of flight: 1.8307757893180215e8 seconds
+ arrival date: 2030-03-01T01:57:17.896
+ thrust profile: [0.3668863571586155 -0.0007259301328571245 -0.09139450957146186; 0.10230474240104724 0.0665130179551613 -0.09528001347616119; 0.06592133825545068 0.07163641188081574 -0.11367352844967209; 0.03625405657379082 0.05409199669541553 -0.09603397095775261; 0.02092642154859947 0.039056635621715144 -0.07745803524417778; 0.01773153792980873 0.0418615669366127 -0.08801139306163897; 0.009609766292180145 0.02651004518468963 -0.06099978229844554; 0.012623288895803704 0.0425626016510604 -0.09935167941526936; 0.0033440047518273515 0.012858682168880059 -0.03220485665943673; 0.008630630722254805 0.03794348022256078 -0.0924388499354312; 0.00038376464038718136 0.002274079423190914 -0.006216500315715358; 0.00010612840584493104 0.0006729774071595273 -0.0016845266554693836; 3.067598511196589e-5 -0.00020252271455119958 -0.00044955204861348334; 9.76373592286519e-6 -0.00015104710438707404 -0.0004354768719607834; -0.0009757575427676401 -2.8328727869944646e-5 0.0002578753477554877; -0.0002538381127882434 -0.0008684938623125362 -0.0010793517427050996; 0.00021826467778170684 0.00027827788258448906 -0.0006736748261313465; 0.0003199888555822858 -0.00025378020248382425 -0.0005072654882948909; 0.00021028953859641167 -0.0007824567825112296 0.0012429671395382163; 7.110417967180348e-5 -0.00044570791940651473 0.000701452823937165] %
+
+Mass Used: 95.76191726692241 kg
+Launch C3: 95.41572998490177 km²/s²
+||V∞_in||: 0.00010059983829146838 km/s
diff --git a/archive/ES_0.5591618840392426 b/archive/ES_0.5591618840392426
new file mode 100644
index 0000000..934b4dc
--- /dev/null
+++ b/archive/ES_0.5591618840392426
@@ -0,0 +1,22 @@
+archive/ES_0.5591618840392426---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T10:12:54.708
+Launch V∞: [7.975764906504826, -5.80612066588757, 0.17505141343693817] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00015002238042382786, -0.00027326722835101474, 0.005281048972498487] km/s
+ V∞_out: [0.00021647294482355451, -0.004943804521915084, 6.164564818695516e-5] km/s
+ time of flight: 1.844860278628058e8 seconds
+ arrival date: 2030-03-19T16:20:01.708
+ thrust profile: [0.29803143096065904 -0.004343020266308911 -0.0958414844157298; 0.03594615018015115 0.01992460179970625 -0.04336895922826621; 0.04767107807108386 0.04518025869978705 -0.10294177180420012; 0.017575186652677877 0.020713760904933036 -0.05646282094824163; 0.022662602285353325 0.03322810567608062 -0.09562784974047943; 0.02381661910922183 0.0427967363889495 -0.12873103589742502; 0.012298449203912995 0.02251235457423008 -0.07848263723135578; 0.009973278023807774 0.02180157546763615 -0.07505527526335896; 0.006361202116690616 0.014289672688929927 -0.057761186217875536; 0.003998728384084994 0.012832071386661708 -0.053612617738731216; 0.0017025373118381866 0.003133021610892479 -0.009297278943954277; 0.0023425574919966182 0.007000335345317095 -0.034408727043360045; -0.00017810672159317354 0.0014290264969217797 -0.0024941666880050496; 0.001468546926413091 -0.0025094784049999362 0.0019528125718661705; 0.0015979901247090088 0.0013967532345172445 -0.0006166258115767945; -0.0028555777981649337 0.0020378508812093337 0.0019465847997719929; -0.0037501374698871086 -0.0006429212793521756 0.003486197904126332; 0.0007964347610313002 0.0003284354969153115 -0.004466176942628722; 0.0008783494941461079 -0.0011189674071013572 0.0020331444772716542; 0.0007817293601355072 0.00043846419236178455 -0.004052935767844226] %
+
+Mass Used: 84.45424621562597 kg
+Launch C3: 97.35450602802693 km²/s²
+||V∞_in||: 0.00529024195501926 km/s
diff --git a/archive/ES_0.5591720103004051 b/archive/ES_0.5591720103004051
new file mode 100644
index 0000000..af77435
--- /dev/null
+++ b/archive/ES_0.5591720103004051
@@ -0,0 +1,22 @@
+archive/ES_0.5591720103004051---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T17:59:57.478
+Launch V∞: [8.026349737713224, -5.732343797189083, 0.33142264516436115] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0033446552517916624, -0.0019625157040512402, -0.0001387422892207932] km/s
+ V∞_out: [0.0027679053749968467, 0.0014079990730987593, -0.0023191301354554437] km/s
+ time of flight: 1.8749577787124434e8 seconds
+ arrival date: 2030-04-24T20:09:34.478
+ thrust profile: [0.3181294159269611 -0.007391833953783253 -0.10629862703769685; 0.02585996297786951 0.013749492031966315 -0.032023082461897896; 0.046432708021973974 0.03878646530427863 -0.09973523082878863; 0.03288903541931046 0.035457281027553036 -0.10447852220324988; 0.030392676086355597 0.03869487507721043 -0.12691800168617204; 0.011922028576020465 0.0174546943333071 -0.06436691609510471; 0.010236497114503293 0.01483174621643055 -0.06208136444752061; 0.012059456522778483 0.01697215217366049 -0.09001593076729332; 0.006809109927096935 0.016627373956995723 -0.06780400063351734; 0.001890893390876943 0.0022804579573704894 -0.01276837489558173; -4.015066443619985e-5 0.0008824146463982802 -0.004290357049807709; 0.0008332287660614429 0.0037001159921372416 -0.02104354958325653; -0.001692795405032168 0.0009930600521315704 0.00011707421181999297; 0.0010196807093748358 -0.0010954195941999575 0.003748296981354994; -9.068750672846441e-5 -0.002235532554418666 -0.002698859045114484; -0.0010053189905129076 0.0013611506531543745 -0.0037490885760108512; 0.0005230262180043183 0.001201133228224402 0.0027354798641833224; -0.003030682258775987 -0.0019325213253842384 0.0023869043961860293; -0.006797003913483073 0.012474872017833295 -0.0027433219479469; 0.005016613507423134 0.010040319725388915 -0.005269296690921988] %
+
+Mass Used: 84.24794915303664 kg
+Launch C3: 97.39189649098903 km²/s²
+||V∞_in||: 0.003880391225740455 km/s
diff --git a/archive/ES_0.5591745717149611 b/archive/ES_0.5591745717149611
new file mode 100644
index 0000000..5642de0
--- /dev/null
+++ b/archive/ES_0.5591745717149611
@@ -0,0 +1,22 @@
+archive/ES_0.5591745717149611---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T17:57:43.218
+Launch V∞: [7.825013144560418, -5.697464734510945, 0.13480729732710492] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7852732247755848e-9, 1.7578834606987418e-10, -4.72632800398755e-10] km/s
+ V∞_out: [1.2527936043810634e-9, -1.1316009167357473e-9, -9.412373816479448e-10] km/s
+ time of flight: 1.8749577784957525e8 seconds
+ arrival date: 2030-04-20T20:07:20.218
+ thrust profile: [0.4989464172029878 0.026169164120752382 -0.1055411922965082; 0.0868856779606476 0.06596889606046043 -0.07801270099152452; 0.057914417786400704 0.07402062807110188 -0.0951624385752758; 0.05568105074914253 0.10215966432125452 -0.1387643760081443; 0.03385079032295114 0.07806460086958357 -0.12003854285629621; 0.018619847921069643 0.05668516316957505 -0.09447218341761325; 0.009603640936684551 0.036968232043887404 -0.06828611228778933; 0.0044378296354850005 0.018825830931033467 -0.03716727056510345; 0.0017453615926743618 0.01236055566936713 -0.02508870434507977; 0.0020171026141728755 0.013330375447800559 -0.02970856358968342; -0.0009594779922030099 -0.0002528400208523281 -0.004347822268403343; 0.0003427873190835604 0.0010064004324128154 -0.0007965080082934872; -9.885738854423771e-5 0.0006277584316620051 3.3209144460982646e-5; 0.0003330401887829582 0.000542193954755996 -0.0007021102325801955; -0.00012822446202468123 0.0009969710422301056 -0.001377084075131096; -0.0003769053207027786 -0.0005017026228740463 0.000953558548866691; 0.0001377471541094865 -0.000990395886265377 0.001569651149745045; 0.0004976338764970697 -0.0011475333563775326 0.0007411397631466806; -9.759420350351938e-6 8.811238312427211e-5 -0.00047085829296418286; -0.0003947811936763308 -0.00282833954275989 -0.00017105896517923225] %
+
+Mass Used: 105.7280362952356 kg
+Launch C3: 93.71010812095183 km²/s²
+||V∞_in||: 1.8551236599556826e-9 km/s
diff --git a/archive/ES_0.5591784475484177 b/archive/ES_0.5591784475484177
new file mode 100644
index 0000000..c7064ee
--- /dev/null
+++ b/archive/ES_0.5591784475484177
@@ -0,0 +1,22 @@
+archive/ES_0.5591784475484177---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:39:26.394
+Launch V∞: [8.017551936970808, -5.687905804192632, 0.1433190802387331] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.720017743600037e-7, -1.42034031043978e-6, -1.4294897867497874e-7] km/s
+ V∞_out: [1.2416113179098387e-7, -5.639553859975814e-7, -1.6271540549583895e-6] km/s
+ time of flight: 1.8486871048384443e8 seconds
+ arrival date: 2030-03-22T16:04:36.394
+ thrust profile: [0.3277954510764798 -0.003949298192494021 -0.09695507614855713; 0.07341087032037072 0.04249722470631526 -0.08077491055930697; 0.05026596405843437 0.04741633447469449 -0.10099354305672174; 0.020206245266428502 0.025082412346113154 -0.0613119930284584; 0.015870616621796126 0.024027016536070818 -0.06490749490345886; 0.011166246333268319 0.01985906941660979 -0.058288661364473505; 0.02281547911786278 0.0498895108381997 -0.14220205222804808; 0.013483372193650913 0.032623460030710594 -0.1046362955276171; 0.00898113201201489 0.02715008131744296 -0.08758569708676406; 0.0008427871938944194 0.002553006266621829 -0.013440443199746738; -0.0005016454365156266 0.004053656310567421 -0.011387517673998575; 0.0007575323172381643 0.00041384838183887874 -0.002290932392949079; -0.00037985547433845254 -0.0005090240406613997 0.0005101327759053521; -0.002881609739342612 2.3390454197535788e-5 -0.0023765247323866583; 0.00282318719407269 -0.00014352787264977867 -0.005119885636948564; 0.003153267620712414 -0.0008435875434100032 0.0008102143319151725; -0.00010514684697001306 -0.003455449771483641 -0.002925814375602658; 0.0021038910552321766 0.005620655496555683 -0.0012317069444306883; 5.366528951776506e-6 -0.008223818524596487 -0.0012600095765421587; 0.0009422120315219103 -0.00229625929518562 0.0014415309882807844] %
+
+Mass Used: 88.56013630059442 kg
+Launch C3: 96.65395185815306 km²/s²
+||V∞_in||: 1.7270172139626707e-6 km/s
diff --git a/archive/ES_0.5591815707364995 b/archive/ES_0.5591815707364995
new file mode 100644
index 0000000..0f2b65e
--- /dev/null
+++ b/archive/ES_0.5591815707364995
@@ -0,0 +1,22 @@
+archive/ES_0.5591815707364995---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:13:27.142
+Launch V∞: [7.648408579934272, -6.1833417478180195, -0.24277256162771801] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2992935929493686e-9, -1.3982463343941e-9, -1.4815905018901087e-9] km/s
+ V∞_out: [4.13253975715014e-10, -3.738367899698172e-10, 1.365452001017404e-10] km/s
+ time of flight: 1.7828686744127375e8 seconds
+ arrival date: 2030-01-07T02:21:14.142
+ thrust profile: [0.3029014718380257 -0.022666419017422806 -0.11056426527392954; 0.12139162572434989 0.0542525274228301 -0.1461260760477033; 0.05355386667215124 0.03930186346816372 -0.11688522103912054; 0.04187398309763066 0.03957914471179054 -0.1310904831159089; 0.0423178505345414 0.04776200072439813 -0.17348930074602015; 0.016845933343234764 0.020353049747776512 -0.08842779239072047; 0.010758394657603533 0.014616455625015325 -0.06635217170826402; 0.005692803691222595 0.00815881723136041 -0.04139136606076457; 0.0029774552855221467 0.004523324069851735 -0.0244237548364791; 0.0010547977164910222 0.001799296378063179 -0.010253836122443849; 0.000369197259341948 0.000575329300570523 -0.0038726480106828485; -5.088245243912637e-6 6.0907063795105176e-5 -0.001827808069857286; 0.00021593229100776477 0.00018581275432970272 -0.0007485366657392506; 0.0005214186728461023 0.0009654728169060348 -0.0011904360315032644; -0.0001801197271279127 -0.0008106106042890537 -0.0008381578857327111; -0.0006288484089560424 0.0003198457812575939 -0.00029902909086246764; -0.00015379001633062094 -0.0002001656184699896 0.0010789496793801741; 0.0004106404532900172 0.000526983501766283 -0.00020206051646272846; -0.00013628147471236114 6.569036796283615e-5 -0.0005878953443557468; 1.3993527519400096e-5 0.0012881438175762414 0.0001588998610644135] %
+
+Mass Used: 87.7654554857454 kg
+Launch C3: 96.79080749260069 km²/s²
+||V∞_in||: 2.4162713149844744e-9 km/s
diff --git a/archive/ES_0.5591886732978449 b/archive/ES_0.5591886732978449
new file mode 100644
index 0000000..5497d03
--- /dev/null
+++ b/archive/ES_0.5591886732978449
@@ -0,0 +1,22 @@
+archive/ES_0.5591886732978449---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T21:26:43.449
+Launch V∞: [7.841001723289415, -5.784788915482485, 0.0975128831673417] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.752330265125132e-6, -0.0004564794180718647, -8.761592085917482e-6] km/s
+ V∞_out: [-0.00043968234964827983, 6.818542184584412e-5, -0.00010481634036985594] km/s
+ time of flight: 1.813159204916822e8 seconds
+ arrival date: 2030-02-07T10:58:43.449
+ thrust profile: [0.40332659133308657 -0.00526978697479912 -0.11202217731583004; 0.15064550196111193 0.08716012558665306 -0.14472787699936487; 0.05630169056337342 0.05372411732277327 -0.0960318603967372; 0.030112221448684917 0.03779452084178358 -0.07844350216316436; 0.02514744439623931 0.038675684053563225 -0.109557398514223; 0.029224074017063534 0.05629031388178292 -0.13964702101076484; 0.016418291099001447 0.03196639486302129 -0.102548993847396; 0.007071713732761343 0.011297369925397335 -0.040161229345829635; 0.002211984889898862 0.00690040038091169 -0.027967862071585185; 0.0025368207038233828 0.0041763980681435746 -0.013929098884040444; 0.002207381715777916 0.007024993546185321 -0.016386496719220673; 0.00016892598886628644 0.001482413045540428 -0.0027643377587489157; 0.00023098457128626306 0.0001592625365764764 0.000654647665521775; 0.0003472616140583818 -0.0019002293589722833 -0.0002078276128396325; -2.0233999182386445e-5 0.0011605615421701816 -0.0024655117025440985; 0.00014542195593007242 0.00030720681505467303 -0.001251357387635515; -0.0002526992513470505 0.0015613216909406763 -0.0012809011900443115; -0.0008377603628096917 0.003407176486207057 -0.001687377329952387; 0.0012514772968412542 0.0003176677152420305 6.10199253573309e-5; 0.00017416127213047193 -0.00027543857815340756 0.0014464842735067494] %
+
+Mass Used: 98.48495460923459 kg
+Launch C3: 94.9545995837002 km²/s²
+||V∞_in||: 0.0004566134235686874 km/s
diff --git a/archive/ES_0.5591929738712642 b/archive/ES_0.5591929738712642
new file mode 100644
index 0000000..16418b9
--- /dev/null
+++ b/archive/ES_0.5591929738712642
@@ -0,0 +1,22 @@
+archive/ES_0.5591929738712642---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T04:28:28.801
+Launch V∞: [7.882983071983007, -5.844817602504056, 0.19590814995695643] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004188781367755915, 0.002400478390887329, 0.0001811457283250084] km/s
+ V∞_out: [-0.0033421669505160423, -0.0020386900224302717, 0.002825135884886305] km/s
+ time of flight: 1.8556503176146555e8 seconds
+ arrival date: 2030-04-01T22:18:59.801
+ thrust profile: [0.3489439916852445 -0.00888303767411587 -0.11649813835808116; 0.11415721430964595 0.05869569874768407 -0.1342751953299948; 0.02587961358636833 0.0204175421102558 -0.054928465042918706; 0.025049935382484626 0.02590058098864609 -0.07857037684789442; 0.026132696870451742 0.03337058144206555 -0.10942010122046607; 0.026390413850696834 0.03763670892351129 -0.12937993293819813; 0.016078814561586715 0.027385536577475448 -0.10052319039240744; 0.009485815189086895 0.015080443657976292 -0.06490542955966223; 0.003679776674941903 0.0067557154822240235 -0.032258627912847726; 1.8804083626564405e-5 0.001275420179781721 -0.0007120730673977008; 0.0008183831269209939 0.002323486684191904 -0.008937304524020896; -0.0004512117990430346 0.0013181227689587865 -0.002252772033089429; 0.0008955904575676085 0.0014147463016651442 -0.006607853341166625; 0.0016104144248258179 0.0005512371541247494 -0.0007389060926769673; -0.006314206453638584 -0.002261615575298398 0.00535320447251057; -0.0008149765700473841 0.001625222924215553 -0.0015657392456131201; 0.0018974133076827273 0.0001629522800376522 0.0006931677534144885; -0.0002976431578220173 -0.004634773255331677 0.013012666383098982; 0.00030332986549103054 0.0027184908783552276 -0.0023495594424225324; -0.002936503153916672 0.0008458036383975731 0.005342829281675496] %
+
+Mass Used: 90.39858246604126 kg
+Launch C3: 96.34169492293148 km²/s²
+||V∞_in||: 0.004831252386997241 km/s
diff --git a/archive/ES_0.5591937301009369 b/archive/ES_0.5591937301009369
new file mode 100644
index 0000000..0705a0e
--- /dev/null
+++ b/archive/ES_0.5591937301009369
@@ -0,0 +1,22 @@
+archive/ES_0.5591937301009369---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:18:42.612
+Launch V∞: [7.622833667448883, -5.753265831956483, 0.04356405749160138] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005211058959450843, 0.028891677657142862, 0.030326831334502227] km/s
+ V∞_out: [-0.007850450639527674, 0.006546682458733423, -0.040688577600590664] km/s
+ time of flight: 1.874957778665776e8 seconds
+ arrival date: 2030-04-22T21:28:19.612
+ thrust profile: [0.7940667897477646 0.0028040630332909545 -0.2132123305027833; 0.06141446816388004 0.0383664017808364 -0.06690087470471107; 0.0650816026975904 0.0651013226768044 -0.122214895822592; 0.028977209701942876 0.04055667904683914 -0.08581615836234056; 0.01353966309841526 0.02489331690124839 -0.0639929544592398; 0.008288633087434674 0.01984393301893977 -0.054521200349437; 0.005580730413958491 0.012855557131749488 -0.0382283145910354; 0.011205590773118588 0.029774186382118834 -0.08507723439646962; 0.007835548567306524 0.015884543393662524 -0.05320613677486505; 0.006676412986850514 0.022733231539470426 -0.08050635881181037; 0.0006569299398003953 0.004442403755489796 -0.015380971535872538; -0.00020251836000220822 0.001642129083852893 -0.003950928927276218; 0.0016670495759934902 6.0072155300018305e-6 0.00047399736631191503; 0.0012448725562562862 -0.0034186557210033578 -0.0006112822424774085; 0.001297344665988253 -0.000202762081699454 -0.0001586329386900783; -0.002798976362893733 -0.0010113859128532284 0.0023096047900447465; 0.0013571507009370474 0.0002054700614253749 -0.002024683510330912; -0.000985999045803499 0.0016381334355106527 -0.002503091651591496; 0.0002660080149700283 0.0004309608008878044 -0.0010801327013731687; 0.0004533881043880658 -0.0008558936962726827 0.00038125786488709345] %
+
+Mass Used: 120.33692614027086 kg
+Launch C3: 91.20955868185523 km²/s²
+||V∞_in||: 0.04220901410971911 km/s
diff --git a/archive/ES_0.5591940029574614 b/archive/ES_0.5591940029574614
new file mode 100644
index 0000000..c358bb4
--- /dev/null
+++ b/archive/ES_0.5591940029574614
@@ -0,0 +1,22 @@
+archive/ES_0.5591940029574614---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:02:41.445
+Launch V∞: [7.8721009362370715, -5.776477749849678, 0.16305115007104518] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7950648111474253e-6, 4.1727426745721905e-6, 3.8351604016171544e-7] km/s
+ V∞_out: [-3.6781642160525825e-7, 1.0256248799665331e-6, 4.915006477996918e-6] km/s
+ time of flight: 1.874957778193709e8 seconds
+ arrival date: 2030-04-22T21:12:18.445
+ thrust profile: [0.3086560617504458 0.012767915135516306 -0.08125889569994621; 0.21062739326978858 0.13879321692407642 -0.19157994308767035; 0.04891180450249142 0.050289237098209136 -0.09164586677990784; 0.04557301231593274 0.06352822596828218 -0.1265323696460861; 0.017539502701023543 0.030373685310138364 -0.07097832579277405; 0.015009029082877249 0.032200020755906306 -0.07996316124777997; 0.004362633467726555 0.012035700850257068 -0.031223960469928935; 0.009133737944387595 0.022701602137306907 -0.06714362841036985; 0.002902808791468994 0.009727061117301861 -0.02615458930325433; 0.00040888599988076044 0.010042894402468147 -0.024663190648972634; 0.0008339279985970075 0.0028000078298702326 -0.005998889175300663; -0.0005824658806248195 0.0022917163183682606 -0.014077970805865533; 4.6412832185136355e-6 -0.00042615817225654653 0.0011167887540267014; -0.0026555052184820916 -0.003059820830936301 -0.001094132678664127; -0.0003355216135393404 0.004025900259201212 -0.0021643024602129232; -0.0002774291436391493 1.6825695217595558e-5 -0.005038197402300506; -0.0082246782048622 -0.0008827307887234626 -0.003774743260331329; -4.312091681871454e-5 0.003919154383678189 -0.004047014274813123; -0.002258765483916596 0.0005310899435413117 -0.0016159619516714601; -0.0034960303617329515 0.0014126446475294895 -0.00563785989417785] %
+
+Mass Used: 96.10152165331556 kg
+Launch C3: 95.36425402235247 km²/s²
+||V∞_in||: 5.036988512968021e-6 km/s
diff --git a/archive/ES_0.5591980627895994 b/archive/ES_0.5591980627895994
new file mode 100644
index 0000000..fd3f663
--- /dev/null
+++ b/archive/ES_0.5591980627895994
@@ -0,0 +1,22 @@
+archive/ES_0.5591980627895994---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T07:39:37.358
+Launch V∞: [7.795753820377827, -5.940025395361047, 0.11901088369757255] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01478679618397674, 0.09136942464816697, 0.0973511411158228] km/s
+ V∞_out: [-0.022306408502659445, 0.02023851836357439, -0.1309007377562585] km/s
+ time of flight: 1.859934849252122e8 seconds
+ arrival date: 2030-04-07T00:31:01.358
+ thrust profile: [0.35179177008706913 0.011607335648205194 -0.0979976653066796; 0.10595857701357823 0.06836102479569942 -0.10718538000443484; 0.045564744778052946 0.048998444198001236 -0.09229168835757663; 0.023118019588589816 0.03613942204111807 -0.07515623741594743; 0.027570512404252165 0.04904223768853061 -0.11041588841047453; 0.016060757968216773 0.03259518247428856 -0.08654022827621832; 0.015971970726298884 0.04482884605668521 -0.11418111125252753; 0.007333667376491036 0.027255754681343235 -0.07748993743413485; 0.0018088924009586646 0.0057349727889916486 -0.020682725371505662; 0.0009945918994318482 0.0027523637067915748 -0.009661272437102016; 0.0005462448164150369 0.0009256056225290163 -0.0052390619825043675; 0.0019050140773807197 0.005375553488797192 -0.02304884253898304; -0.0005631902631626935 -0.0012862310270684246 0.0009121141356240425; 0.0021124163506783212 -0.0023508739464447484 0.0010897806824492037; 0.0010489165195883702 -0.0006004299787364246 -0.0002709893941871197; 0.0009901664384217002 0.0006033127335812569 -0.0027668999591462327; -0.0008321401960607372 -0.0012326750412931789 0.004523314690008464; -0.0003684522654518914 0.0030402754187617937 -0.007133760304993316; -0.000360501528072824 0.0012743587812455502 -0.003300008328197544; -0.0003345981161035597 0.0001526205987231594 0.00036101100772468163] %
+
+Mass Used: 91.97865624506858 kg
+Launch C3: 96.07184291590812 km²/s²
+||V∞_in||: 0.1343289461675196 km/s
diff --git a/archive/ES_0.5592067082089581 b/archive/ES_0.5592067082089581
new file mode 100644
index 0000000..f7bee37
--- /dev/null
+++ b/archive/ES_0.5592067082089581
@@ -0,0 +1,22 @@
+archive/ES_0.5592067082089581---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T18:46:07.718
+Launch V∞: [7.82093066436902, -5.5691018736507445, 0.18552752938183711] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.129017716500804e-9, 1.6157607909812199e-9, 4.544263679577737e-10] km/s
+ V∞_out: [1.5786215709442573e-9, -2.10732944946574e-9, -1.90155693930627e-9] km/s
+ time of flight: 1.874957778695518e8 seconds
+ arrival date: 2030-04-20T20:55:44.718
+ thrust profile: [0.6718861314152129 0.0036247736910967492 -0.19044676304241798; 0.1168256031553986 0.0717466358553682 -0.12231459108594579; 0.04663126906927759 0.04663061857384722 -0.0906094979293521; 0.041736249747301654 0.056354221082617346 -0.12201954085075511; 0.025309289523868676 0.04226167796177433 -0.10129866560606879; 0.01383458839362932 0.02771557513310835 -0.07267581163800396; 0.012243242131020704 0.028733778911942953 -0.08041227119853306; 0.0040291646962101555 0.011075412032073063 -0.0330881367889942; 0.002006177978389352 0.006305288117031731 -0.01992398231152219; -0.00047969490856047844 -0.0007503704335607006 -0.0014146030116501539; 0.0009451840299159861 0.0035577574314185926 -0.013098253293187437; -0.0003947274278910571 0.0008886560349788374 -0.002380386679801881; -0.0038922902422768996 0.000862118593643405 -0.004526950959612055; 0.0016321509453455472 -0.00041445225120178165 -0.0039501831765983535; -7.50104062142258e-5 -7.605848245758814e-5 -0.0037504807024409097; -0.00032978298381453747 0.001619066930617344 -0.0012463169039226938; -0.0032150350617317267 0.0008874342432204892 -0.001938138048406741; 0.0012338571061336115 0.00039647151464672397 -0.0011272060229869166; 0.00803571189469847 0.00558603078538652 -0.0008192467053692639; 0.006756357932197549 0.0028685538683956434 -0.013136633778319702] %
+
+Mass Used: 114.4795694097138 kg
+Launch C3: 92.2162726001264 km²/s²
+||V∞_in||: 2.7110703964932095e-9 km/s
diff --git a/archive/ES_0.559211681071346 b/archive/ES_0.559211681071346
new file mode 100644
index 0000000..0f81109
--- /dev/null
+++ b/archive/ES_0.559211681071346
@@ -0,0 +1,22 @@
+archive/ES_0.559211681071346---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T08:31:30.518
+Launch V∞: [7.7524319355968, -5.910511281728595, -0.04799343501515631] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9116564035197787e-8, 1.668828547111482e-7, -3.101864606802704e-8] km/s
+ V∞_out: [4.25067883731953e-8, -1.589302091441212e-7, -4.312704050949359e-8] km/s
+ time of flight: 1.77448056003878e8 seconds
+ arrival date: 2029-12-24T03:39:06.518
+ thrust profile: [0.38590243594550955 -0.022536915572817603 -0.12348503680062936; 0.1511196670906645 0.07955057833991365 -0.16209813696825962; 0.09221757604039947 0.07989808088491283 -0.17527659045064506; 0.030756558535300068 0.03494378447389875 -0.0899706501996986; 0.018797431227513033 0.025739593556094377 -0.07347443980846288; 0.029671039480565365 0.04700328884386673 -0.14573962743561325; 0.01067904232256255 0.019606802939529443 -0.06332400023929927; 0.006517883011250692 0.01375714316873263 -0.047993059471473316; 0.005386601539968931 0.01358168094070773 -0.05066267918839916; 0.002028462286395143 0.004984183110260687 -0.019442640132261022; -7.733580928233653e-5 4.0022620184514364e-5 -3.2877922095934565e-5; 6.768532712209452e-5 0.0004311153950732801 -0.001633799126717395; 0.00020734223024851595 -0.00011058913358583152 4.953640258838767e-5; 0.00043698939780268764 0.0002884432834900553 4.445630132469058e-5; 0.00031294123127568096 -8.393297959462687e-5 -0.00023097320589018276; -0.00023075125078417794 5.860056843912193e-5 -0.0003048183723822471; 0.00023116119821324775 0.0001080958892124426 -0.00025801052435204066; -0.00011065998821704548 -0.00023677055105630006 -1.520331080478055e-5; -0.0006449462582447165 0.00029295836892528817 -0.00037701238299729233; 4.250858207741168e-6 3.265652651197487e-5 -6.662844377512515e-5] %
+
+Mass Used: 98.03318184894806 kg
+Launch C3: 95.03664789730668 km²/s²
+||V∞_in||: 1.7081418741119704e-7 km/s
diff --git a/archive/ES_0.5592186658047181 b/archive/ES_0.5592186658047181
new file mode 100644
index 0000000..e315daa
--- /dev/null
+++ b/archive/ES_0.5592186658047181
@@ -0,0 +1,22 @@
+archive/ES_0.5592186658047181---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:49:47.229
+Launch V∞: [7.835056420243145, -5.897395562751835, 0.10751736403460409] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.547193352001276e-10, -1.0041424976300953e-9, -1.2620918219964914e-9] km/s
+ V∞_out: [8.585603062562945e-10, -7.784125209962522e-10, 3.151865133480135e-10] km/s
+ time of flight: 1.8387125243718034e8 seconds
+ arrival date: 2030-03-12T18:10:39.229
+ thrust profile: [0.3413457213173033 -0.020877747337084997 -0.09281931244160425; 0.12498578885207408 0.06192459088120485 -0.13645044006892668; 0.037197599020577336 0.03362727109106814 -0.08087755968306763; 0.02965058172308108 0.03382436066834206 -0.09287725011519962; 0.029855065749621136 0.03666252614113272 -0.118353023673469; 0.013636704016778191 0.021740258972963177 -0.07480470812205442; 0.012127641341781507 0.019699726430548313 -0.07379924374643013; 0.0061604379574490215 0.01163654201225121 -0.046944427826391556; 0.013036527242287207 0.02774870238271448 -0.11627211786418523; 0.0018662448729362719 0.004488574849166517 -0.021717868199729363; -0.0008979203877849781 -0.00017677173108495702 0.0011464452128838235; -0.0003764433613556193 -0.0005574850512665422 0.0022969726769601546; -0.0006843385854621921 0.0007000192677966869 0.0009708883524121464; 0.00015450113868640798 0.0003937890299540841 -0.000180836781657891; -1.1909570214953973e-5 -0.0010593431901784933 0.0022163213765773017; 0.00038965442927415883 0.0002941272021008736 -4.9426308948815286e-5; -0.0014929700416642618 -0.0036013893576040843 0.010159380502137057; 0.00023815684629138295 -0.0017867906035421077 -0.0001502547588329772; 0.0025033064239241417 1.8032593500296163e-5 0.0012421045808640471; 0.0008272047060282635 -0.0003149118517818237 -0.0003743854578670908] %
+
+Mass Used: 91.37793959826195 kg
+Launch C3: 96.1789435155273 km²/s²
+||V∞_in||: 1.7806681885242269e-9 km/s
diff --git a/archive/ES_0.5592265929003932 b/archive/ES_0.5592265929003932
new file mode 100644
index 0000000..cd8be1c
--- /dev/null
+++ b/archive/ES_0.5592265929003932
@@ -0,0 +1,22 @@
+archive/ES_0.5592265929003932---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:10:55.736
+Launch V∞: [7.628304799846212, -6.031507410168833, 0.6034482609632436] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0875972533778235e-6, -1.9140557124305e-5, 3.4168720891482627e-6] km/s
+ V∞_out: [-3.022435721585168e-6, 1.159780385806925e-5, 1.5449529433821925e-5] km/s
+ time of flight: 1.816717227341278e8 seconds
+ arrival date: 2030-02-14T07:32:57.736
+ thrust profile: [0.4359114104593332 -0.00958001283120508 -0.10743150898971957; 0.12384502185700882 0.0672092658755478 -0.12402213863678857; 0.0816713473127001 0.0828982908550845 -0.1538195911980114; 0.017454877002193586 0.021484891234577422 -0.048896517523906; 0.046610270416361135 0.06957932852053415 -0.16785186152918072; 0.019666857619702594 0.03336307481886982 -0.08626461846696115; 0.007946747094936738 0.015358889493984824 -0.04326724847802068; 0.006522665051376493 0.014480502182595967 -0.04305943813456654; 0.0074177760633653165 0.014884112552863543 -0.056314236987670976; 0.0015538021481390485 0.005913641914142075 -0.020559475577306547; 0.0010040201341684405 0.004757020074244374 -0.018211790564352008; 8.518297992871039e-5 2.5466538807543046e-5 -0.00032544758290966984; 0.0001658794301797428 0.00015827694140566008 -0.0005174823439653654; 0.00020241628427676006 -0.0002799347841022941 -0.00042064257066313517; 9.15161595724173e-5 4.2111133484984355e-5 -0.00010047408398183692; -7.619238575584822e-5 -0.0005600102159745813 -0.0006784009174751886; 0.00021353788773314958 0.0007252402821098636 -0.00011614694452725084; 0.00018614360096682076 0.00024459434324729457 1.7144797423878987e-5; 8.991264843682541e-5 0.00027737518990172873 -7.80284981019096e-5; 0.00024150743066965718 -0.00021495643506060894 -7.423440252456648e-5] %
+
+Mass Used: 98.64780927248785 kg
+Launch C3: 94.93426556193786 km²/s²
+||V∞_in||: 1.9554897192127957e-5 km/s
diff --git a/archive/ES_0.5592288394811683 b/archive/ES_0.5592288394811683
new file mode 100644
index 0000000..cdaf894
--- /dev/null
+++ b/archive/ES_0.5592288394811683
@@ -0,0 +1,22 @@
+archive/ES_0.5592288394811683---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T05:51:27.764
+Launch V∞: [7.62314439769262, -5.946000999280755, 0.10456757764604137] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.655631850232519e-9, 9.40797803616904e-10, 8.484573357545428e-11] km/s
+ V∞_out: [1.317938556371939e-9, -1.238978543535269e-9, -1.011288739780987e-9] km/s
+ time of flight: 1.7876214033505633e8 seconds
+ arrival date: 2030-01-09T06:00:27.764
+ thrust profile: [0.5790583661228802 -0.023996649492273446 -0.16691019434192947; 0.07687338221489615 0.0432147744908329 -0.08150272073166562; 0.05422478565131992 0.049382937032400785 -0.09839736580958859; 0.03810922026727666 0.04684502441256764 -0.10372167186189837; 0.03276681622401257 0.05244302044564323 -0.12209110855872947; 0.01685463256607372 0.030921005120536086 -0.08086174579883411; 0.01263280886658708 0.026830431755497437 -0.07451309428022417; 0.023681860847946948 0.0574239787682266 -0.15697703309098482; 0.0034774471862069863 0.009465683957562919 -0.030283563479114487; 0.0013896540176380457 0.0037975563872869825 -0.012492454980845705; 0.00035547178851172043 0.0011754997431858273 -0.004055415320748961; 0.0001422265679016874 0.0012910211186779115 -0.0025625667797394944; 1.773576678375374e-5 0.00010778212533028942 -0.0008211874264374135; 0.0010424827047380326 -0.000734327819200532 0.00014985318215775722; -0.00010202181860219527 -0.0009395878322764558 0.00038161055929410484; 0.0006437732521273527 -0.00011203940485315499 4.592550409569991e-5; 0.0005312195695767633 -0.0017766230555770813 -0.0001524137526711725; -0.0007573630148999332 0.0013433552768341885 -0.0012013547366409964; 0.00020211122608621018 0.0007489080352155986 -0.00344026101598966; -0.00038679431725050704 0.0004136963490155647 0.0018431263405310275] %
+
+Mass Used: 107.1441882374429 kg
+Launch C3: 93.47819276981488 km²/s²
+||V∞_in||: 1.9061521789460307e-9 km/s
diff --git a/archive/ES_0.5592506413520684 b/archive/ES_0.5592506413520684
new file mode 100644
index 0000000..83d8def
--- /dev/null
+++ b/archive/ES_0.5592506413520684
@@ -0,0 +1,22 @@
+archive/ES_0.5592506413520684---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:06:29.814
+Launch V∞: [7.835798455425541, -5.7528441095359275, -0.019929843183993174] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7100311518408306e-5, -0.0018172520279710301, -2.71253486660066e-5] km/s
+ V∞_out: [-0.001753706991317378, 0.0002813082225767223, -0.0003808698351240768] km/s
+ time of flight: 1.849125597030797e8 seconds
+ arrival date: 2030-03-22T07:42:28.814
+ thrust profile: [0.47500726050270586 0.0030613221906884767 -0.11064208236940856; 0.0581093092819559 0.04022593480565114 -0.059554448361755274; 0.07253110211004198 0.07958608665933097 -0.13163719358349768; 0.03580648276577725 0.05572351629930886 -0.1006470107231921; 0.025987279165847213 0.05489446930891728 -0.10387380755659502; 0.016917678772732314 0.03951731737942892 -0.08385388386540688; 0.014511635520956573 0.04434158729954264 -0.09512768461253919; 0.003087102298206094 0.011546680848405298 -0.028348963367092347; 0.004152189031426685 0.03342540837084032 -0.08409766775438529; 0.001783597056860029 0.007442299224156826 -0.02218982280600159; 0.0007783643913260297 0.005361943054000052 -0.016930970538923916; 0.0014679683875155418 0.0006625859047427455 -0.0007582812789367207; -0.0005272143463476991 0.0002388025426433701 0.0003468446403744627; 0.0005436811553860982 0.001055653955232895 -0.0015393827799054564; 0.0011047941260201243 0.00030556898143944863 0.0004893145069939586; 0.000637820146374295 0.0002572385100725177 -0.0014791808137475525; -0.0022264601505415584 0.0001930388969617578 0.0016927556099200526; -0.0007142634006094278 0.0008819570424019559 -0.00017554586725648238; 8.198800309576717e-5 0.0015953795413101422 -0.002973740814628852; 0.0018106745191497984 -0.004736220404220191 0.004058784679087209] %
+
+Mass Used: 101.23620668637477 kg
+Launch C3: 94.49534998132086 km²/s²
+||V∞_in||: 0.0018176564979636468 km/s
diff --git a/archive/ES_0.5592508302419151 b/archive/ES_0.5592508302419151
new file mode 100644
index 0000000..ec162e5
--- /dev/null
+++ b/archive/ES_0.5592508302419151
@@ -0,0 +1,22 @@
+archive/ES_0.5592508302419151---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T21:29:06.817
+Launch V∞: [7.751052846167995, -5.640979573344344, 0.14745553135101755] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9894380050400517e-8, -2.1097029754511796e-7, 4.436645327632119e-6] km/s
+ V∞_out: [1.9660696717853913e-7, -4.460931520072164e-6, 5.64597901988441e-8] km/s
+ time of flight: 1.827053563584333e8 seconds
+ arrival date: 2030-02-22T12:58:22.817
+ thrust profile: [0.7490606400033559 -0.019905765963447074 -0.17464438131516863; 0.06562661110569944 0.03797841226550716 -0.07111132477556384; 0.038211365082452584 0.03680810834770242 -0.07407497232670152; 0.06927744737675208 0.0915672509993267 -0.19468217374068686; 0.022801212177837888 0.03783065767488792 -0.09196924661686087; 0.015198065833682708 0.030568113042635653 -0.08290469493303564; 0.01085016020442871 0.024732661395982805 -0.07139936707152734; 0.007862664390082683 0.020035857637154215 -0.06290249162448482; 0.004230372004145673 0.011337224914700616 -0.03695003428607581; 0.001348245031093821 0.0036795140894983263 -0.014405723737453304; 0.0009261413431771413 0.0029520493642183417 -0.011053844701066913; 5.9154881520604935e-5 0.0005946962960482169 -0.0007762931368274096; 2.5949972731073253e-6 0.0003600146670638367 -0.00039444816806104906; 8.010352796894644e-5 0.00027387831554936504 -0.0009285142018137461; -1.3109422828730334e-5 0.00019450200510895237 -0.0006198148784749401; 5.825070180322917e-5 0.00021793117479822725 -0.0006268150464133458; -0.0005858588539927405 0.0006089812381424515 -0.0008889383004558038; 1.679648585643868e-5 -1.1066853104378053e-6 -0.00046430178395088085; 0.0007338891384963018 0.0007290897240172984 3.592790927115278e-5; -0.00015921399742618348 -0.00021051616100825122 0.0010866499165830337] %
+
+Mass Used: 116.25222083813287 kg
+Launch C3: 91.92121390470311 km²/s²
+||V∞_in||: 4.441759100131927e-6 km/s
diff --git a/archive/ES_0.5592626467892583 b/archive/ES_0.5592626467892583
new file mode 100644
index 0000000..1b23cc2
--- /dev/null
+++ b/archive/ES_0.5592626467892583
@@ -0,0 +1,22 @@
+archive/ES_0.5592626467892583---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T05:55:14.314
+Launch V∞: [7.8575774317328415, -5.966875235331324, 0.14143132514726095] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7993318228139443e-7, 1.1230982399791237e-6, -2.7092771661142988e-5] km/s
+ V∞_out: [-9.54010679960433e-7, 2.7082443084216113e-5, -1.8932839894424607e-7] km/s
+ time of flight: 1.83464131442766e8 seconds
+ arrival date: 2030-03-08T16:10:45.314
+ thrust profile: [0.25168641404900643 -0.01046712298562203 -0.0821691038862054; 0.09557870634457247 0.04765189513901902 -0.10599551008871527; 0.06455226150216901 0.05218016936944876 -0.12901853078122574; 0.04157219904719486 0.04333785434963071 -0.12190977624482296; 0.02332882633399856 0.02978436035210357 -0.09522971783191223; 0.0091372673956326 0.013494755444510141 -0.04850976601237639; 0.014379396370925997 0.026700767167311942 -0.09829838312689834; 0.003424599820585164 0.007739004113404664 -0.03014588275264129; 0.00498616658109888 0.011498743161614353 -0.0479981687690069; 0.005744309758133331 0.014185922061328281 -0.059969210135740685; 0.0012273468898272837 0.002716558372035038 -0.012004920759260553; 0.00066183434742141 0.002564251939458358 -0.012217659793203038; -0.0004692834927583719 0.0006662782422413632 -0.0012438743858128206; 0.0009989771800838565 -0.0003080095623191005 0.0002218273963419861; 0.0004035973321975231 -0.00034389112142706635 -0.001901855144380108; 0.004590981224999778 -0.0004930404711256688 -0.0032467042995696477; 0.004680417864851357 -0.0003837548541332764 -0.002555389762842798; -0.002480952652671952 0.000343327791188837 -0.004194299920605682; 0.0005222071135596051 -0.0011499065171481494 -0.0009046309374596989; -0.0007920935614060729 -0.005861740435988815 9.683949255483984e-5] %
+
+Mass Used: 84.50985298251544 kg
+Launch C3: 97.36512598942043 km²/s²
+||V∞_in||: 2.7116636994464536e-5 km/s
diff --git a/archive/ES_0.5592700414088685 b/archive/ES_0.5592700414088685
new file mode 100644
index 0000000..cd53176
--- /dev/null
+++ b/archive/ES_0.5592700414088685
@@ -0,0 +1,22 @@
+archive/ES_0.5592700414088685---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T14:26:35.992
+Launch V∞: [8.03371350672608, -5.471294468674302, 0.2529869915231228] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01108632353032437, 0.06501534754907481, 0.07965418668848954] km/s
+ V∞_out: [-0.030276276928744184, 0.034071692220608484, -0.09255581725001864] km/s
+ time of flight: 1.8749577787297595e8 seconds
+ arrival date: 2030-04-20T16:36:12.992
+ thrust profile: [0.5112221824896165 -0.0009234292903318921 -0.15032177388792234; 0.09440892088087616 0.054973137436968224 -0.10571138314758223; 0.054476269016423086 0.05138910058776488 -0.1114275199231372; 0.042851278609536206 0.05370665500317019 -0.13113082076772595; 0.021360603544254137 0.03209924045904968 -0.08752660875106259; 0.013864057312806306 0.02640719373479496 -0.07427639840704446; 0.010956344312452026 0.023123308520272546 -0.07191987342446417; 0.005019470487310105 0.014430677931819569 -0.04475070747464066; 0.0025380852353163617 0.0053761246432940234 -0.023904095693168502; 0.0010022801176079032 0.0034368359945249997 -0.013436704600975199; -0.0006191076122296969 0.00429642474971136 -0.013428125753850762; -0.0006654253654527471 -0.0007599506097702086 -0.0004169514126764098; -0.001192662789042489 -0.002159842142239771 -0.0003296514769657829; -0.004153308664638627 0.000514335618529271 -0.0022713852951456288; -0.00275705430544606 0.0002001376621609697 -0.002917479727225985; 0.00023921192094449704 -0.0025835480079874104 -0.00041792156922509146; -0.0006627096641018379 -0.004435920950241218 0.005225292474420252; 0.00036226832795043505 0.001952928883827872 0.0010613383203278964; 0.0003075696853579058 0.0008808445172815486 -0.0006052733049659254; 0.004295285678140425 -0.005575556307868002 0.004667757524676892] %
+
+Mass Used: 101.00060829130234 kg
+Launch C3: 94.539618288979 km²/s²
+||V∞_in||: 0.10341514126737321 km/s
diff --git a/archive/ES_0.5592717350738583 b/archive/ES_0.5592717350738583
new file mode 100644
index 0000000..a0bf263
--- /dev/null
+++ b/archive/ES_0.5592717350738583
@@ -0,0 +1,22 @@
+archive/ES_0.5592717350738583---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T01:29:08.653
+Launch V∞: [7.823031364280662, -5.713517271461867, 0.23392590646235537] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004567595986524988, -0.0027364349914782873, -0.00019567681129488445] km/s
+ V∞_out: [0.003702191612647156, 0.002140379638938354, -0.0031733952465336545] km/s
+ time of flight: 1.8387335348671618e8 seconds
+ arrival date: 2030-03-09T05:25:01.653
+ thrust profile: [0.5026031089448129 0.0025055569814187465 -0.12688795829874847; 0.11801175337920859 0.07507735272721212 -0.11922849268435362; 0.07027269662461978 0.07346177710191783 -0.12537885426860948; 0.05055383524042758 0.07216472712443621 -0.14002160435472386; 0.02424716311606827 0.041852987342948365 -0.10511837625197022; 0.014497823641052447 0.03339478326633748 -0.0788139373616507; 0.007801589075980663 0.02010532315682969 -0.050220248605484276; 0.006674746180727291 0.020200087675548616 -0.058739792848483255; 0.002427292317412934 0.008060641169423628 -0.02288429392526868; 0.0026670655169442137 0.009434166552995536 -0.02801455528223001; -0.00046431182859192345 -0.00026206583149932113 0.0002584315323855802; 0.0004307996994350193 -0.0012967209440764716 -0.002749725185770214; -0.0008913018209132592 0.0004555460527590285 -0.0017368465142633181; -0.0016449467320847737 0.0017968663688861983 0.00011130775855894845; 0.0013009033030656962 -0.00023435805322504988 0.001446348230297915; -0.0019432888326989884 0.0016291394832574544 8.331964342616488e-7; -0.002520216536050167 0.0010747090438740698 -0.00017848346112117738; 4.300475029042443e-5 2.0812491182969775e-5 0.0006034855343307088; 0.004820725980830004 -0.0007947755362729934 -0.003012503004643595; -0.0009014576826958986 -0.004906939766816509 0.0035474295077655878] %
+
+Mass Used: 104.74057035893156 kg
+Launch C3: 93.89882066752624 km²/s²
+||V∞_in||: 0.005328160937245092 km/s
diff --git a/archive/ES_0.5592739794091608 b/archive/ES_0.5592739794091608
new file mode 100644
index 0000000..742a4e9
--- /dev/null
+++ b/archive/ES_0.5592739794091608
@@ -0,0 +1,22 @@
+archive/ES_0.5592739794091608---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T10:59:22.483
+Launch V∞: [7.884769391851066, -5.922110131443762, -0.01048394613500921] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.601246062517178e-7, 1.9181808625948907e-6, 5.185665050667303e-6] km/s
+ V∞_out: [4.983668437087599e-6, 6.009781864900703e-7, -2.412762126867413e-6] km/s
+ time of flight: 1.842122351184661e8 seconds
+ arrival date: 2030-03-17T13:03:17.483
+ thrust profile: [0.29186334051203083 -0.011256222424372249 -0.09854158042176767; 0.05342551183728227 0.026059903380105703 -0.06197191058939047; 0.07454770685448434 0.06060954627335754 -0.1509629626897045; 0.0265754147169481 0.026081932149701243 -0.08111937480826101; 0.021958843886783683 0.025825799776436533 -0.08850230910482301; 0.030387511207113044 0.039052092912544474 -0.14662413578595596; 0.01074541135181506 0.015301524706070968 -0.06336315378027974; 0.0062554922572147795 0.010048421613939703 -0.043125948390970885; 0.0016873595420598933 0.004074698661723733 -0.013711743862433836; 0.0036276679386073223 0.005755300296298652 -0.03272914501465041; 0.0012473869290462207 0.006506599948568785 -0.027880915916260043; 0.0006849009863067571 0.003869663137260787 -0.017189749383571283; -0.0026723532877673596 0.002150737011500893 -0.0018900148767863213; 0.00042697776425368664 0.0028173173034322894 -0.0042629580848199435; 0.0012950771357933036 -0.0011531921371791334 -0.013454049856346045; 0.0004186405233849022 0.0013662671743040135 -0.006573666535696014; 0.002970198147680014 0.0034419824500337695 -0.00286002389392478; -0.000799860851162222 -0.004133934036787028 -0.0011971404643217646; 0.0013945856387186854 -0.0015125060358879218 0.004657472334174998; 0.0006596897685921224 -4.073329410338938e-5 0.0010393077720219385] %
+
+Mass Used: 85.24663698299764 kg
+Launch C3: 97.24108668474683 km²/s²
+||V∞_in||: 5.557362631128748e-6 km/s
diff --git a/archive/ES_0.5592803607959682 b/archive/ES_0.5592803607959682
new file mode 100644
index 0000000..acb8de0
--- /dev/null
+++ b/archive/ES_0.5592803607959682
@@ -0,0 +1,22 @@
+archive/ES_0.5592803607959682---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T12:52:31.604
+Launch V∞: [7.946843451545427, -5.68920470660413, 0.5592442644578861] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.082422780460397e-5, 0.008608897254512924, 6.8190847412590854e-6] km/s
+ V∞_out: [-8.417421872161397e-6, 0.0003766101527094051, 0.007003735246779829] km/s
+ time of flight: 1.858112742866179e8 seconds
+ arrival date: 2030-04-02T03:07:05.604
+ thrust profile: [0.38427460520388523 0.00972597221109478 -0.09671670490485997; 0.10118045061230801 0.06711482068360737 -0.09937428134173543; 0.0444528742176101 0.048680707937060495 -0.08169153613906484; 0.029828056944168076 0.04363204291823553 -0.08039292440936112; 0.013805751446938805 0.025428778858599524 -0.052877899318282615; 0.011869662226170974 0.028536282663100054 -0.062267055650499746; 0.015079193835955271 0.03629352509310644 -0.08603502223088544; 0.012937218244993593 0.042466719165013794 -0.10024824433168966; 0.0035155794498001316 0.0121260921723642 -0.03321408741146624; 0.006808702132726272 0.03836329627247357 -0.09910383061284635; 0.0013947893576579807 0.006866043667692807 -0.019954201874348758; 1.0435887837637492e-5 0.00042130759067705127 -0.0014453637904162618; -0.00032224196484967294 0.0003649164477472774 -0.001484685314624424; -0.000390935200230511 -0.0003477442853453412 0.0007255392423024128; 0.0015439478468378099 0.0009259138196282748 0.00014855679776873908; -0.00025086132889466347 0.0010415266991759301 -0.0017541823670971031; 2.1683094464277535e-5 -3.153452530214922e-5 0.0005756046462022784; -7.16657367613087e-7 0.000139549334016115 0.00026954059523871614; 0.00020506694118312737 0.00019833728557065472 -0.00016614855651601396; -0.0025645261743263083 0.00035157591262587485 -0.0006425016845224229] %
+
+Mass Used: 93.4730240199442 kg
+Launch C3: 95.83212518434607 km²/s²
+||V∞_in||: 0.008609114822405664 km/s
diff --git a/archive/ES_0.5592964279436405 b/archive/ES_0.5592964279436405
new file mode 100644
index 0000000..fbd9c8b
--- /dev/null
+++ b/archive/ES_0.5592964279436405
@@ -0,0 +1,22 @@
+archive/ES_0.5592964279436405---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T21:02:08.204
+Launch V∞: [7.998006147242351, -5.636250997133124, 0.1304989873068134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.480562779768748e-9, 4.92422523569435e-9, 2.2282411760224624e-9] km/s
+ V∞_out: [4.1015025659112595e-9, -4.079940933981875e-9, -2.376265294124911e-9] km/s
+ time of flight: 1.8749577787493548e8 seconds
+ arrival date: 2030-04-21T23:11:45.204
+ thrust profile: [0.3325540316577712 0.002214384308901568 -0.08895507092433798; 0.11322370003941329 0.06966771767269717 -0.11364201748168606; 0.07269285745311141 0.07372782167891886 -0.13331481698611974; 0.054131765684652174 0.07419215388047837 -0.14998089436191833; 0.028479843074532198 0.04925148470127126 -0.11022559378486327; 0.01590328660492611 0.03438695433702035 -0.08377992266409412; 0.008302860931331188 0.021046857875775135 -0.05564728993633893; 0.003857799144934988 0.011479932528856311 -0.032352450098804816; 0.00188829571645205 0.0033614030487717464 -0.009839092985253872; 0.0006224588220877101 0.003065235359090141 -0.009833905763601089; 0.000973516914469148 0.00045005629476941927 -0.003224885961393761; -0.0009768031535154983 -8.30995380948895e-5 -0.0011935877820468204; -0.0006567334199403755 0.0017442129418770952 -0.0014346899739679734; -0.0026094283443667547 0.0011544371257953454 -0.0002959015531314973; 0.0006764738524280137 -0.005438923661097864 0.004202088460930391; 0.009111975261732567 -0.0025102450909934015 -0.00901389484101904; -0.002284345873823029 -0.005900809930636146 -0.009317455306537766; -0.007462130800744716 0.00592111965865867 -0.0005668745911433092; -0.0009209194403932157 -0.003955939669325099 0.0034834885758953152; 0.001803893671691574 0.00330280556740311 0.005762467949357683] %
+
+Mass Used: 93.95649648600511 kg
+Launch C3: 95.75245761969866 km²/s²
+||V∞_in||: 5.946952548553344e-9 km/s
diff --git a/archive/ES_0.5593039030059357 b/archive/ES_0.5593039030059357
new file mode 100644
index 0000000..b33a716
--- /dev/null
+++ b/archive/ES_0.5593039030059357
@@ -0,0 +1,22 @@
+archive/ES_0.5593039030059357---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T02:31:13.116
+Launch V∞: [7.774352820063127, -5.64089247637929, 0.10358108924296568] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.553516503228638e-7, 2.594887329050573e-6, -5.106539634927624e-5] km/s
+ V∞_out: [-2.14960602062829e-6, 5.134421606363209e-5, -6.208140415701136e-7] km/s
+ time of flight: 1.8744893721587193e8 seconds
+ arrival date: 2030-04-20T15:40:10.116
+ thrust profile: [0.678784433913801 0.011071609234985933 -0.15364135391143954; 0.08091109962176929 0.05451262700194639 -0.07936630061423171; 0.025179811481305957 0.027794952770830633 -0.047260931953073675; 0.0265420480086587 0.04100427317130899 -0.07495067562663094; 0.02830134263098452 0.05524011305470956 -0.1080695167367095; 0.051260059352351686 0.10751273252042873 -0.2047673642148955; 0.010308249771651517 0.030841257451801548 -0.0708245264313403; 0.00428098401740344 0.015385852606707082 -0.03877625953580764; 0.0014556746232925453 0.007625923069999503 -0.020011579841437723; 0.002743875671569351 0.0035007318306405264 -0.007664175905950388; 0.0010417638208086474 0.0027121809408151587 -0.009073525617282113; 8.15227296057623e-5 0.001911961315398801 -0.005284940233722031; -0.000415063416234971 0.000506247839773888 -0.000996879712510359; -0.0018539486896982514 -0.00023876813198878236 0.00047490290624861643; -0.0001616042738657559 0.0009270590805106828 -0.001751789930259377; 0.0009318971324986126 -0.004672520619025316 -0.005730114853852565; -0.004207841903112684 -0.0022880186233725968 0.002746402056407916; 0.0004574756504269119 -0.0022736394737560054 0.0025313686072313854; 0.0016096975817342448 -0.0030459870959929558 0.00391014389968883; -0.0025097993849086285 -0.0040863224136638045 0.0032661093219910403] %
+
+Mass Used: 114.27396083974736 kg
+Launch C3: 92.27095874294474 km²/s²
+||V∞_in||: 5.1132518218395324e-5 km/s
diff --git a/archive/ES_0.5593133477748964 b/archive/ES_0.5593133477748964
new file mode 100644
index 0000000..a4006d2
--- /dev/null
+++ b/archive/ES_0.5593133477748964
@@ -0,0 +1,22 @@
+archive/ES_0.5593133477748964---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T00:48:01.701
+Launch V∞: [7.7823562132547375, -5.960995611632541, -0.017077451301021934] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0013812255387238867, -0.0009050462427486497, -0.055688102233191865] km/s
+ V∞_out: [0.022207366077478866, 0.04664230529095811, -0.023993585421327904] km/s
+ time of flight: 1.7654420128079456e8 seconds
+ arrival date: 2029-12-14T08:51:22.701
+ thrust profile: [0.3435484659157275 -0.025776594468999294 -0.1151095715025513; 0.06073800932854741 0.028764338161765293 -0.06806570625144696; 0.093847098435004 0.07450726038889975 -0.17888584078810782; 0.04820032613017215 0.050377691873933136 -0.13602149178257722; 0.04198687480647455 0.053108166006195376 -0.15609312990394753; 0.021731896829705947 0.03180289606466461 -0.10334186651440443; 0.008354251527992412 0.01364740409768998 -0.04985053460411937; 0.007843133576194466 0.014691001325560718 -0.05413828415047413; 0.005520662825615024 0.010864847316038491 -0.044248094974608285; 0.002669850903177991 0.005619282475246163 -0.02459422410684747; -0.0002713408060738557 -0.00042679501483286085 -0.004789716808799091; 4.058885199533852e-6 0.00028634562811257174 0.0002946734101520799; -0.0003954835572510324 0.0008597681227083407 0.0001846686458188032; 0.0002859859037857546 0.0005300686486727158 0.0006078716652574093; -0.00038633820931462646 -0.0011463949369085143 0.001552301252125711; 4.07654329699205e-6 -0.00033709432743283233 0.001300576756832142; -0.00012929572252532887 0.0015930170513121737 -0.0010277222531409416; -0.00015514865118484463 0.001143596857058541 0.00019442584713442817; 0.0019540576908918706 0.00023073870058060218 0.003025081254635019; -0.0028196923264261755 0.0016932915603111113 -0.0002879283430500492] %
+
+Mass Used: 91.95573918853779 kg
+Launch C3: 96.09882855122996 km²/s²
+||V∞_in||: 0.055712580473576745 km/s
diff --git a/archive/ES_0.5593138813153915 b/archive/ES_0.5593138813153915
new file mode 100644
index 0000000..9ed5e92
--- /dev/null
+++ b/archive/ES_0.5593138813153915
@@ -0,0 +1,22 @@
+archive/ES_0.5593138813153915---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:28:41.314
+Launch V∞: [7.840644313832482, -5.802021066374984, 0.0483702899622631] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.414923581597622e-7, 1.958963711670469e-6, -3.7391998826967984e-7] km/s
+ V∞_out: [2.9948872983007645e-7, -1.1338369843027376e-6, -1.5989880567253375e-6] km/s
+ time of flight: 1.8254795581260332e8 seconds
+ arrival date: 2030-02-23T06:14:36.314
+ thrust profile: [0.47172642620012384 -0.00039878780076271645 -0.14053792066036358; 0.05197473484249501 0.03035607914923335 -0.05693341787222671; 0.03642565301188819 0.035053081648007765 -0.07167944736821869; 0.027297049074247366 0.03523721750254447 -0.08003620545439781; 0.019064037894545128 0.030533978094349584 -0.07648509503845274; 0.01271219227198635 0.02409305378192856 -0.06591188322877943; 0.008480791900310997 0.018066142942772763 -0.05315441861836145; 0.0246210923661965 0.06339726863952938 -0.17525647452247645; 0.016449741383413572 0.04808054792645228 -0.14436254081482464; 0.0012079385469066656 0.003965613392929158 -0.013859861083469234; -0.0003478378161026178 0.0005949369037025721 -0.0005389729041389043; 0.0007069661729390414 0.00045950270611772563 -0.00027238176035041493; 9.305119001125265e-5 7.427177348974607e-5 -0.0004465090192906612; -0.0006401019041305206 -0.0017309410246502772 0.0009906480943043968; -5.1075008818572915e-5 0.0009352848488699476 -0.002565799472320344; -0.0005160425371663129 -0.0002033212516586232 -0.0004476672140165433; -0.002688276859750356 -0.002416721182577361 -0.0004728006066712254; -0.0009070020942657929 -0.0017970237394073405 0.0018380397260459734; -0.0005368170289797152 0.0037364405681344984 -0.002147506355131189; -0.0007230533704893787 0.00013424481838445677 -0.0005122285370302667] %
+
+Mass Used: 97.54082839336797 kg
+Launch C3: 95.14149139564378 km²/s²
+||V∞_in||: 2.0088985888588058e-6 km/s
diff --git a/archive/ES_0.5593154667417125 b/archive/ES_0.5593154667417125
new file mode 100644
index 0000000..da2f77b
--- /dev/null
+++ b/archive/ES_0.5593154667417125
@@ -0,0 +1,22 @@
+archive/ES_0.5593154667417125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:00:15.301
+Launch V∞: [7.661571924009417, -5.868813150241897, -0.046626949010829276] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.203404810018797e-5, -6.707515793981747e-5, -5.533564741080626e-5] km/s
+ V∞_out: [-1.0669026719355722e-5, 7.5518039300461e-5, -9.091010874926805e-5] km/s
+ time of flight: 1.822939531522335e8 seconds
+ arrival date: 2030-02-20T11:12:48.301
+ thrust profile: [0.6063759444561523 -0.015449698866928931 -0.18539567194676182; 0.07960797042733037 0.042537331161758334 -0.08811382433852998; 0.06877213989400029 0.059453636367917596 -0.13445920511248613; 0.03734429979553476 0.04616544742518225 -0.11362243033787219; 0.023944781023695013 0.03463001735320411 -0.09801266017098186; 0.01993651583218196 0.03636320678388689 -0.10903741814567008; 0.013017833799960538 0.025729550622790774 -0.08438323334924865; 0.00634119978175763 0.012748068240200725 -0.04813080707492147; 0.0020693176402605718 0.005253541083476825 -0.021511547015411282; 0.0017252798933071129 0.005756160482784622 -0.02398275701732289; 0.0006987191291149034 7.830782289890256e-5 -0.003075589924511858; -0.0017966198174650101 0.0007247053823726277 -0.001528022317518653; 0.0004330718202686466 0.0002783303708565826 -0.0025171150473292316; 0.0003067226631105165 -0.0005202548992686963 -0.0008372238824838223; -0.004654671671139781 0.002811262471508903 -0.0005508097011886451; 0.004621188980151566 0.003224694798575173 0.0015639839267687877; 0.00014163196172483947 -0.0023339742053282383 0.0034034449360487726; -0.0011237090531743517 -0.004401504937532737 -0.0005863911462084897; -0.00269757478617769 0.005280682084848821 -0.009965046842664173; -0.0007148839865844319 -0.0025552175426149606 -0.0009608784137855183] %
+
+Mass Used: 109.18989163102333 kg
+Launch C3: 93.14482621159564 km²/s²
+||V∞_in||: 0.00011954369801343975 km/s
diff --git a/archive/ES_0.559316679408488 b/archive/ES_0.559316679408488
new file mode 100644
index 0000000..5d43677
--- /dev/null
+++ b/archive/ES_0.559316679408488
@@ -0,0 +1,22 @@
+archive/ES_0.559316679408488---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:03:49.401
+Launch V∞: [7.7252818086672495, -5.942013625968739, 0.17943380830816408] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.727062703623636e-5, -7.641579243628148e-5, -6.306290472927552e-5] km/s
+ V∞_out: [-1.2797942410996657e-5, 8.869308925920873e-5, -0.0001059847505192407] km/s
+ time of flight: 1.7963653997869366e8 seconds
+ arrival date: 2030-01-20T17:06:08.401
+ thrust profile: [0.432372374813613 -0.02802717735094289 -0.14230456362232732; 0.11344949088259283 0.05406949798436557 -0.1269424892492953; 0.0650193985384188 0.05032057891385575 -0.1297352620667606; 0.04333027086880266 0.04331549153835245 -0.12605415917167181; 0.022083137587373694 0.025926666260087966 -0.08658054616703507; 0.016620848630248215 0.022340778326631363 -0.08200672773271707; 0.013951353580541849 0.021184477671395294 -0.08281763315492442; 0.00547391725998021 0.008888416657199753 -0.03974277642189151; 0.006475085214427023 0.011149916596883365 -0.056923738629324296; 0.0009664698182417606 0.0017119399861457362 -0.005199177817553543; 0.0012401810018382675 0.0023310805043851284 -0.012139775461302158; 0.002846807879001531 0.006377816423907603 -0.03457630203481961; -0.0001717820453181045 0.000905485907322234 -0.005757520534694894; -0.0018547885993865372 -0.00040522358095947206 -0.0008215480749857599; 0.000843326792193941 -0.0023532921715947288 -0.001385108949414984; -0.001377246514173651 0.0017916700855385471 -0.0043517030159237685; -0.0009367845989925802 0.002002813621909596 0.0013819858908230946; 0.0007069555642913255 -0.00055281506249026 -0.0005077011702666625; 0.000701402927502889 -0.0003722154628827735 0.0009862723935714474; 0.005580836376019012 2.322537646493966e-5 0.0009127720686269965] %
+
+Mass Used: 98.25453420772692 kg
+Launch C3: 95.01970144608727 km²/s²
+||V∞_in||: 0.0001388447988603863 km/s
diff --git a/archive/ES_0.5593204725966611 b/archive/ES_0.5593204725966611
new file mode 100644
index 0000000..318ff8d
--- /dev/null
+++ b/archive/ES_0.5593204725966611
@@ -0,0 +1,22 @@
+archive/ES_0.5593204725966611---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T00:19:48.378
+Launch V∞: [7.823560196995155, -5.7559851091055645, 0.11358170168219066] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.773326829663266e-6, 0.0001257249405719497, 2.227104144999612e-6] km/s
+ V∞_out: [0.00012201852492751759, -1.8203570577855544e-5, 2.4804056158649283e-5] km/s
+ time of flight: 1.852990461330137e8 seconds
+ arrival date: 2030-03-27T16:17:14.378
+ thrust profile: [0.48551515395930406 -7.407291786717493e-5 -0.14046164042629838; 0.08580389424868282 0.05171371387763295 -0.09345121186396368; 0.07506338800776134 0.07366682255528587 -0.1450474165542146; 0.04473340473810005 0.059301461383685146 -0.13176367187336713; 0.017226239225573786 0.029259664024939125 -0.07258634908324009; 0.01032662601353192 0.02206066649374808 -0.05981599495222506; 0.010094105022577326 0.024578983706047147 -0.0701758354254813; 0.004457830860150634 0.01354118743448843 -0.04253082578410222; 0.006417685643977231 0.01796485205369932 -0.06051102614421308; 0.0018949984800572925 0.008118891178787186 -0.028466409067573493; 0.0011910524778317461 0.0015238475024180302 -0.005842162721682141; 0.000826412606587564 0.001655556175674507 -0.005490124445999583; -0.0027587608187198093 -0.005026693033252129 -0.008145844368249232; -0.0002772454442809602 -0.0017806747230470726 0.0011837593004434149; -0.0017178146191895985 -0.0013522727974827054 0.0031059647772938596; 0.00023609228268589686 0.001486884131108251 0.0015847505255201068; 0.003812038898191963 9.824407912383654e-5 0.0030595994857923687; -0.003298648459125529 -0.002639990043430725 -0.005372821390041743; -0.0005335690332324513 0.0020748093799201305 0.0038144400694606383; -0.004255440322659354 -0.00024844458951814123 0.006460551193631584] %
+
+Mass Used: 102.15178740738611 kg
+Launch C3: 94.35235953520889 km²/s²
+||V∞_in||: 0.00012587713047799854 km/s
diff --git a/archive/ES_0.5593217978746752 b/archive/ES_0.5593217978746752
new file mode 100644
index 0000000..65c239e
--- /dev/null
+++ b/archive/ES_0.5593217978746752
@@ -0,0 +1,22 @@
+archive/ES_0.5593217978746752---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:34:57.994
+Launch V∞: [7.930927148416544, -5.767219392952121, -0.07461988658623675] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.280708621058521e-7, -3.0836903475438032e-6, 5.848845711863917e-7] km/s
+ V∞_out: [-4.922064506350584e-7, 1.8204637749638139e-6, 2.5314882919592235e-6] km/s
+ time of flight: 1.856854257382792e8 seconds
+ arrival date: 2030-04-02T17:52:02.994
+ thrust profile: [0.358127289109264 -0.006992455495388805 -0.12076568935952055; 0.10392702611510855 0.053100064883473116 -0.12982746989319743; 0.040442474232876946 0.032559385557551855 -0.09240896608452975; 0.04110098493484239 0.042098279682351865 -0.13548613461363052; 0.023055585856732525 0.027836585785155063 -0.10087667245939581; 0.00981274774583545 0.013897106415357229 -0.056784798326495446; 0.00983253724275336 0.01451203450842123 -0.06576765333110418; 0.004240624097332092 0.007046655347113825 -0.034874388961350394; 0.0038648729196646145 0.007219134505473901 -0.03711711099502482; 0.007483055819451147 0.01410369285452724 -0.0753286002274497; 0.0004313502790034817 0.0013061979770923418 -0.009770818480899477; 0.0033071855544951 0.003649998297199258 -0.0001818387302082898; -0.0008807470153352258 0.0005574446075644332 0.0015855838189739275; -0.00033358296959576963 -0.0037268064736231043 0.0008812659768791978; -0.0005467881998678326 -0.00011537219205519172 0.003500004105695415; 0.0006035296415543691 -9.662168262564359e-5 0.0008563359755749526; -0.006310769018656176 -0.004487194254972102 0.0007955267520635783; -0.0002271002366794672 -0.0009197425059681648 0.004386909688775203; 0.0005292004389779311 -0.00016553862720879384 0.0034455283038276763; 0.0006003560850045952 0.0018740469047408919 -0.00566507061787001] %
+
+Mass Used: 91.57380451057588 kg
+Launch C3: 96.16599308740776 km²/s²
+||V∞_in||: 3.1557671985920614e-6 km/s
diff --git a/archive/ES_0.5593270305153338 b/archive/ES_0.5593270305153338
new file mode 100644
index 0000000..f10d429
--- /dev/null
+++ b/archive/ES_0.5593270305153338
@@ -0,0 +1,22 @@
+archive/ES_0.5593270305153338---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T00:15:46.229
+Launch V∞: [7.976239070784515, -5.975432022011424, 0.08015116077466519] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.778588758738583e-6, -4.7807227993082975e-5, 0.0009016736106300513] km/s
+ V∞_out: [3.636473660916596e-5, -0.0009027415242873094, 1.1846576611424586e-5] km/s
+ time of flight: 1.83818446774511e8 seconds
+ arrival date: 2030-03-14T12:56:32.229
+ thrust profile: [0.18953616876878437 -0.01342856607210278 -0.07666158984544527; 0.014562326919288666 0.00574060837007554 -0.020382968206283488; 0.050554017591673744 0.03080684850757724 -0.12135891648703964; 0.03641030566870778 0.026913987236693467 -0.12511059355710408; 0.022126859452296435 0.01824412465320203 -0.09871499892054611; 0.019058892082071774 0.01692445200523869 -0.10293334076430248; 0.017787125738772877 0.016663974903649664 -0.11174409628025024; 0.014381817762580256 0.014044206615489647 -0.10339925465531041; 0.0011769148484465967 0.0010275831224518248 -0.009692019347589528; 0.0006342791022073512 0.0004887944914799855 -0.005565208622920504; 0.004211520881521221 0.0043154536970823835 -0.03956462776673075; -8.360502184652803e-5 -0.00012340281561942472 0.0008418759482576278; 9.845742547866716e-5 -0.00017008288646478905 -4.305506347067269e-5; 0.00032679514486178994 -6.826664124090506e-5 0.0008234178726947653; -0.0008920857580903994 -0.00034538923764342857 -6.915921713698461e-5; -0.00047000290725259354 -0.0003132393157400706 0.0023550396173672343; 0.00031847506833392096 -7.223356484094211e-5 0.0002792834748352669; -0.00034354432278220644 4.577461877687142e-6 0.0025050712267480836; 0.0004215381219238164 0.0011490097126293454 0.003034279711409774; -0.00012123612672427095 -0.001274978811194512 0.004396559690357971] %
+
+Mass Used: 73.10802526127509 kg
+Launch C3: 99.33260177256247 km²/s²
+||V∞_in||: 0.0009029655477484044 km/s
diff --git a/archive/ES_0.5593301011419318 b/archive/ES_0.5593301011419318
new file mode 100644
index 0000000..2738893
--- /dev/null
+++ b/archive/ES_0.5593301011419318
@@ -0,0 +1,22 @@
+archive/ES_0.5593301011419318---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:42:38.007
+Launch V∞: [8.117634710382866, -5.639337045017684, 0.11027598665670847] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.381356330368787e-6, 4.090073528713957e-6, -5.27497349519701e-6] km/s
+ V∞_out: [1.2451234729770698e-6, 8.474920581341555e-6, -3.9153015953184734e-7] km/s
+ time of flight: 1.8749577787451932e8 seconds
+ arrival date: 2030-04-23T14:52:15.007
+ thrust profile: [0.2575510850519437 -0.0007190397671687425 -0.08122053817194408; 0.05435490118265936 0.030912738248122962 -0.06447207773446478; 0.04325307484057347 0.04218256752134908 -0.10223105751996645; 0.02686349783287257 0.030533847612051145 -0.0792752724624314; 0.02308248969686625 0.040665234413946545 -0.1170931598254555; 0.01118522552287161 0.018487771813702224 -0.05933012001127929; 0.01380186388138076 0.02661901748567766 -0.09010112201695841; 0.01016668716758236 0.021763447315993233 -0.08043965693848158; 0.0019774501306946118 0.0042796849762567445 -0.018991149523322395; 0.0013327285138281307 0.009679681444560342 -0.03376119061442025; 0.004386038974706471 0.010768845191158182 -0.050220074637820855; -0.0008330114480277037 0.0025483352635092046 -0.003988157233443887; 0.002870641165663097 -0.0007647708498633827 -0.006907417057460568; 0.0027461963166482044 0.005821371999172647 -0.004011973300767947; -0.003656993429920376 -0.0012078991908318843 -0.0005954152935094791; -0.0009935850946042994 -0.0005471211216627127 -0.006374689103662923; -0.0035798964808609534 -0.0024467098164428205 0.004355578118616182; 0.002072946947897084 -0.0026763429900887445 -0.006823672501231694; -0.0011011991455013581 0.0026189261421026254 -0.012741274713993743; -0.0016675598320418656 0.005117821037962551 -0.004179923865362607] %
+
+Mass Used: 82.57517238035189 kg
+Launch C3: 97.7102763917546 km²/s²
+||V∞_in||: 8.573974737525053e-6 km/s
diff --git a/archive/ES_0.5593344249733985 b/archive/ES_0.5593344249733985
new file mode 100644
index 0000000..e8e5f5d
--- /dev/null
+++ b/archive/ES_0.5593344249733985
@@ -0,0 +1,22 @@
+archive/ES_0.5593344249733985---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T12:00:54.461
+Launch V∞: [8.102855067235069, -5.903693300503125, 0.2154875840453097] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.314525437058289e-7, 7.654482448382609e-7, -0.0001861118735497496] km/s
+ V∞_out: [-7.134612809350401e-6, 0.0001860832371784216, -2.05097353718208e-6] km/s
+ time of flight: 1.8749577778630182e8 seconds
+ arrival date: 2030-04-27T14:10:31.461
+ thrust profile: [0.10025496489886788 -0.004265035966756486 -0.04132721956872116; 0.022604235579633376 0.009619572361017138 -0.03217831306496848; 0.048709241196467655 0.03354460123038828 -0.122759332411202; 0.034789908892570894 0.029594274601789303 -0.13317134364063346; 0.03019338777701981 0.02359073937414256 -0.1275056177612286; 0.016124647441520753 0.016535786773650214 -0.08753733064989967; 0.012736030766923399 0.010835454989267997 -0.07517634267118052; 0.00606513724013498 0.005903580156064687 -0.046344636890653906; 0.004631285929417672 0.005378694068193614 -0.045581557111521745; 0.0013505937437062777 0.0014968981355181793 -0.01528199873497525; 0.0009730948868593287 0.001028000164730662 -0.009871566809894896; 0.0013035995390488745 0.0018484548815831268 -0.016533893820046074; -0.00041028760486018024 -0.0006762897425730733 0.0006890934548992522; -0.002349314661740785 0.001303932323437776 -0.0010387813210136555; 0.002062161747400496 -0.00024231444625795158 -0.0028775593441180427; -0.0010519124177041537 -0.0023389896653523514 -0.0008155951051073234; 0.0001225881248170537 0.0015774653150396282 -0.0024152499831370175; -0.001001822844305712 -0.0018934694450877573 0.0028095340961565808; -0.002314387778730084 -0.0008437084627747697 0.000274736747191863; 0.0017634767259584235 0.00011833902357565038 -0.0019120697170221987] %
+
+Mass Used: 65.97847240121382 kg
+Launch C3: 100.55628972590019 km²/s²
+||V∞_in||: 0.0001861157784580735 km/s
diff --git a/archive/ES_0.5593472152216766 b/archive/ES_0.5593472152216766
new file mode 100644
index 0000000..f044994
--- /dev/null
+++ b/archive/ES_0.5593472152216766
@@ -0,0 +1,22 @@
+archive/ES_0.5593472152216766---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T13:13:54.228
+Launch V∞: [7.6770244489668205, -5.8273251015778165, 0.26011420906681954] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6197187630005194e-9, 7.166957058180603e-11, -4.987614205833083e-10] km/s
+ V∞_out: [9.680382558592997e-10, -8.579144340967967e-10, -6.858036812010299e-10] km/s
+ time of flight: 1.8749577787472638e8 seconds
+ arrival date: 2030-04-22T15:23:31.228
+ thrust profile: [0.5708830962339988 0.024428925563568085 -0.11568150143654524; 0.09907265679207662 0.06745749342553743 -0.09264770013773986; 0.07778024852156214 0.0891023351581619 -0.13244509449254893; 0.042712237561915396 0.0682661846163897 -0.11498795750787076; 0.030333875658845596 0.062293883691301906 -0.11592060296878057; 0.01453195926747894 0.03740437698793107 -0.07707650788636503; 0.006120097562681272 0.018177134610947037 -0.04143063127863662; 0.005810431276264193 0.022363085743396453 -0.05289727484250628; 0.0034131254075070827 0.015679214651949575 -0.039590601830357834; 0.0021054263039767237 0.008086224876665118 -0.02103220232444771; -0.00021082830991317198 0.0011449915047985625 -0.0024566476411310907; -0.00022898536142903754 -0.0010980293877130302 4.99525508844119e-5; -0.0004251070061498541 0.001062946040340932 -0.001207402195775175; -0.0018959351181602928 0.0003436122341553421 0.00023369433070354853; -0.001334517954042783 -0.0012804074849915555 -1.1306070407972519e-5; -0.001202253459582362 0.0007670121386378995 -0.00034375642504440784; 0.0007074708207245445 0.005150183704537276 0.002736370221797065; 0.001958158642023455 0.0011095430436327586 0.0018208879283336604; 7.05923763414654e-6 -0.000717855837653803 0.004363368212833899; 0.003895969179822966 0.005846635348651134 -0.007423299082348275] %
+
+Mass Used: 110.29294157620461 kg
+Launch C3: 92.96208163127169 km²/s²
+||V∞_in||: 1.6962866365168337e-9 km/s
diff --git a/archive/ES_0.559358725105581 b/archive/ES_0.559358725105581
new file mode 100644
index 0000000..ae29f53
--- /dev/null
+++ b/archive/ES_0.559358725105581
@@ -0,0 +1,22 @@
+archive/ES_0.559358725105581---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:46:49.939
+Launch V∞: [7.710997271621161, -5.7923605027693705, 0.15320237142234577] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3332609922028747e-6, 4.663553009829039e-6, 1.2223538177452088e-5] km/s
+ V∞_out: [1.159098121439848e-5, 1.3195567442697351e-6, -6.063331611607077e-6] km/s
+ time of flight: 1.8197005492346674e8 seconds
+ arrival date: 2030-02-14T15:01:03.939
+ thrust profile: [0.5221813042050395 -0.004398220125917724 -0.1454973562329655; 0.21022759790006687 0.1290913483361146 -0.2057028954213273; 0.05161496966626315 0.049352999924760825 -0.09435795903293688; 0.04014367410000196 0.05246315516478116 -0.11007848790065458; 0.025546307463801213 0.03997274048980851 -0.09408819905018136; 0.0285124331523034 0.05524792724973798 -0.13608936651832856; 0.012199229034409124 0.028275770544199465 -0.07583089139276308; 0.0026172791241456726 0.00704842032381714 -0.02102523311952712; 0.0011328891388329807 0.0024230627539684824 -0.008133962521485159; 0.0007001521477541485 0.002033939491531567 -0.007417759805172856; -0.0009420175595873708 -0.00018650294843866827 -0.0008547141690505968; 0.00021126027406197446 0.0010823466092707533 -0.003753262285700322; -0.00018591001800480063 0.0007174842651845586 -0.0070293344076369675; 0.0008869108760737017 0.0016348653092330347 -0.0004970383704840952; -0.0007214505822236271 -0.00038363135735999056 -0.0014536761050525288; 0.00026806395474718075 0.0027909380661258185 0.0009127474924007332; -0.002513859817382961 -0.0004034227691251358 -0.0008179120408408737; 0.007201577864155658 0.0005638590892682532 -0.00047215192887429614; 0.0008218113922629053 0.0008061317557339247 -0.0015579567414815516; 0.00012606450013243867 8.998012162456684e-5 -0.0003610861846899149] %
+
+Mass Used: 109.88457046883832 kg
+Launch C3: 93.03439008360107 km²/s²
+||V∞_in||: 1.315071089806342e-5 km/s
diff --git a/archive/ES_0.5593604561814962 b/archive/ES_0.5593604561814962
new file mode 100644
index 0000000..e289c68
--- /dev/null
+++ b/archive/ES_0.5593604561814962
@@ -0,0 +1,22 @@
+archive/ES_0.5593604561814962---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T06:17:02.717
+Launch V∞: [7.813449916840554, -6.138335390360884, -0.18307820626903706] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00018912605637051572, -0.00023120817285276801, -0.00011974848129285322] km/s
+ V∞_out: [-2.8773138781589116e-5, 0.00021525233865199754, -0.00023663137224678863] km/s
+ time of flight: 1.805687461686574e8 seconds
+ arrival date: 2030-02-04T04:16:08.717
+ thrust profile: [0.21939785111469595 -0.016417845027022687 -0.08083535215410838; 0.04051391197664174 0.017444973509769594 -0.05292488834850986; 0.038798511083470336 0.0265454895936199 -0.08876529043010205; 0.03517529965504752 0.029926957854055115 -0.11422610197193837; 0.040182613173581544 0.03879742504860827 -0.1599368355466101; 0.019976112956851696 0.02316841936850057 -0.10897698402955552; 0.011864552823122121 0.013293721766951391 -0.07173844228255406; 0.010615869699507409 0.01401592930371677 -0.07773638853005121; 0.007738935713267235 0.011376132065491469 -0.06536620476101582; 0.0024054103612409262 0.0032901227181543653 -0.021614012041672015; 0.000688558496634509 0.0012424292828226372 -0.008044147528619122; 0.00015158602055574872 4.7807574470480895e-5 -0.000382053044663843; 0.0001035736723778548 -0.0003060896470558989 -0.0003347116813244618; 8.668118105363304e-6 0.00016795198027985962 -0.00043158428975731384; 1.077909904766746e-5 0.00013780766580243021 -0.0004367192478484811; 0.00021880559763765036 0.00046916629078590287 1.9025274198141828e-5; -0.0001872940344008933 2.5509478177890936e-5 -0.00029618537396015036; 2.3868657466596867e-5 -2.5074724062182103e-6 -3.292577018123129e-5; -0.00012743447527411683 -7.717339951266273e-5 -0.00039863721404234925; 0.00017597498577304584 -6.880250486926463e-6 -0.00025866811874975817] %
+
+Mass Used: 76.47157372841002 kg
+Launch C3: 98.76267859714325 km²/s²
+||V∞_in||: 0.00032181607039444716 km/s
diff --git a/archive/ES_0.5593626561190457 b/archive/ES_0.5593626561190457
new file mode 100644
index 0000000..2bb3a05
--- /dev/null
+++ b/archive/ES_0.5593626561190457
@@ -0,0 +1,22 @@
+archive/ES_0.5593626561190457---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:16:39.658
+Launch V∞: [7.902717813340605, -5.6351565734461575, 0.22827351173477425] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.691090842935488e-7, -3.2172134335714904e-6, 5.539220115111536e-7] km/s
+ V∞_out: [-4.938121541553285e-7, 1.8608080175994132e-6, 2.663919469142948e-6] km/s
+ time of flight: 1.874957778749177e8 seconds
+ arrival date: 2030-04-21T05:26:16.658
+ thrust profile: [0.4173861143439906 0.004478380057318683 -0.11595525806037822; 0.18118719458332103 0.11141998760423201 -0.17201479481487383; 0.06908524804625148 0.07313249799537444 -0.12717971239560297; 0.04770006171115045 0.06723635449263296 -0.12951583483418816; 0.02543407946858339 0.0459844443050744 -0.09875536285355224; 0.01435582401525812 0.031894362454779134 -0.07491892181808349; 0.008960091221714397 0.023605864689511317 -0.05955868670541283; 0.0008267997928595013 0.002571138712714839 -0.008483288023994886; 0.000939054522257155 0.008375097048948378 -0.018941987296802795; 0.00019284878421780248 0.0017738330239352139 -0.012094836997795923; -0.00024604902507596857 0.003991577612433304 -0.0020370921951360153; -0.00013977149087065273 0.003105342471552571 -0.004925240480809629; 0.0062252818728180895 -0.0014653284863244385 -0.0008928566035649942; 0.0008402924017101628 -0.002040226774495154 -0.0019422757257769507; 0.0010686102615874455 -0.0013585483459899598 -0.0011857162885563419; -0.00015567061014338997 -0.002495578214589111 0.008433538970788539; -0.0037130969474788496 0.002178112496462959 -0.006974559676272538; 0.004127086466683005 0.006749651292732256 0.00018386220979988203; 0.0008108186429749873 0.0006485370498043566 -0.0014948739839962767; 0.003307284992996451 0.001981998476203352 -0.0011652261778832042] %
+
+Mass Used: 102.73948990144618 kg
+Launch C3: 94.26004724070407 km²/s²
+||V∞_in||: 3.285351334042897e-6 km/s
diff --git a/archive/ES_0.5593742050522984 b/archive/ES_0.5593742050522984
new file mode 100644
index 0000000..3c01674
--- /dev/null
+++ b/archive/ES_0.5593742050522984
@@ -0,0 +1,22 @@
+archive/ES_0.5593742050522984---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:04:12.370
+Launch V∞: [7.740643109085416, -5.899124231054655, 0.2440843325004866] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.022303149859219242, -0.158501838556909, -0.16920570134185167] km/s
+ V∞_out: [0.04120319210387117, -0.0341987806754222, 0.22681925997111246] km/s
+ time of flight: 1.8749577787404573e8 seconds
+ arrival date: 2030-04-23T16:13:49.370
+ thrust profile: [0.4249043962850636 0.019246489829171307 -0.09691956153320222; 0.0860238499475132 0.06203683546820436 -0.07920968707543993; 0.07474790345004238 0.08231197428225807 -0.11926555830909327; 0.04501921896811657 0.07301030985750452 -0.11368044147910923; 0.019349712330887836 0.040609265289238305 -0.07125217268857924; 0.02519280618470695 0.06808224070014529 -0.12433506734877388; 0.012513661137886541 0.03555472638141666 -0.07313057333392523; 0.006649972615492512 0.02769167687156549 -0.05438262001771187; 0.004305491622270597 0.019003546607013685 -0.04231958134706408; 0.0034645888764237246 -0.002773030745169487 -0.0034119752245906423; 0.00029052157926145084 0.0015857365400096374 -0.004001410238100219; 0.0013451512776041993 0.0013598941403510432 -0.002719568974399918; 0.0015978633167950968 -0.0007887019337584115 -0.0032265526271674254; -3.453959146069473e-5 0.00018835287735452988 -0.0015438368507441666; 0.0004833501395173855 0.0024175434094733223 -0.0027349772655471836; -0.0005300541289823568 -0.003322158052092603 -0.0048630842215081575; 0.0021608846927259878 0.0007747358205265947 -0.002293642190487474; 0.00033383651966250005 -0.00687876619772732 0.005590082771532725; -0.00036616186792482505 0.0019143829354317772 0.0007034446173899331; 4.578999150367351e-7 0.00044744809444534697 -0.000992170186737989] %
+
+Mass Used: 99.73857491173203 kg
+Launch C3: 94.77679959701992 km²/s²
+||V∞_in||: 0.23291808149250914 km/s
diff --git a/archive/ES_0.5593759233097342 b/archive/ES_0.5593759233097342
new file mode 100644
index 0000000..cd25d4a
--- /dev/null
+++ b/archive/ES_0.5593759233097342
@@ -0,0 +1,22 @@
+archive/ES_0.5593759233097342---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T16:08:26.703
+Launch V∞: [8.106354687330304, -5.722656662975033, 0.022371134286674164] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0351798879549123e-9, 2.487614830196058e-10, 1.3316871560961624e-8] km/s
+ V∞_out: [2.6727252008013414e-9, -9.051605319374544e-9, 1.442094267172873e-9] km/s
+ time of flight: 1.874957778809801e8 seconds
+ arrival date: 2030-04-24T18:18:03.703
+ thrust profile: [0.20953934348086933 -0.0010008504341241862 -0.07250930352850532; 0.03121396710923866 0.017079949082295962 -0.03952339332572118; 0.04844186377412211 0.04271049418987007 -0.10578107439194571; 0.03292323098429748 0.03731674460269774 -0.10578714314995447; 0.022322998085212965 0.030812023184543857 -0.0977814204030149; 0.02053297383828263 0.033443016396021964 -0.11430467597979665; 0.00862019400149694 0.01618424544966075 -0.06032048895999503; 0.010916755061536292 0.02108417545703592 -0.08903122517884872; 0.002381762236082079 0.007799953052763355 -0.028135957324583467; 0.002382906947857043 0.005321052066338956 -0.03027619244730938; 0.0010220473298193306 0.0025996087620922302 -0.014621760255728335; 0.0005376854255162249 0.0038308607943919343 -0.020367479848349423; 0.0007564475685496049 6.496463360696186e-5 -0.004162170308723933; -0.00428857064037832 0.00019070565894744587 -0.007443604934385116; 0.0003142878635769198 -0.0005214183555145992 0.013929321997970076; -0.00517231124513857 0.005865061377644657 0.002544078539942517; -0.0029863878295957325 0.0009100878174762401 -0.004276058666061941; -0.00016946196786624698 -0.0019373587509400967 -0.002973461734485973; -0.0015614514278892476 -0.0017353209797195412 -0.008242328520361575; 0.001979628462715436 -0.002019470253353448 0.0013138866214856054] %
+
+Mass Used: 78.24190847201771 kg
+Launch C3: 98.46228606674381 km²/s²
+||V∞_in||: 1.347378594244835e-8 km/s
diff --git a/archive/ES_0.5593816962292311 b/archive/ES_0.5593816962292311
new file mode 100644
index 0000000..2eefd4d
--- /dev/null
+++ b/archive/ES_0.5593816962292311
@@ -0,0 +1,22 @@
+archive/ES_0.5593816962292311---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T04:20:17.117
+Launch V∞: [7.818083203159423, -5.985619487020531, 0.11941296072262551] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2548678814082753e-7, 7.576110351175323e-7, -1.9935196470037553e-5] km/s
+ V∞_out: [-8.366700932765886e-7, 1.9930979904869704e-5, -2.442240794964283e-7] km/s
+ time of flight: 1.8438246248164397e8 seconds
+ arrival date: 2030-03-20T05:41:19.117
+ thrust profile: [0.3169382015612669 -0.010839984361051404 -0.10809201301357246; 0.08941980866009228 0.04185549497661011 -0.10533483324000008; 0.05583944004358431 0.0409756026968116 -0.11955226325784467; 0.04179058446950667 0.038739314577480366 -0.1310732353665363; 0.030804819094132355 0.03302024675630205 -0.12791132929622454; 0.01841337851410901 0.021769394913235728 -0.09695356241541048; 0.011097758897446313 0.014018254689792975 -0.07121318693719332; 0.002977785813054386 0.004091217501717647 -0.023947119595577777; 0.002584675637346937 0.004008593373505123 -0.023629362922530567; 0.0016361521803515018 0.0026000299614880686 -0.0168377181217847; 0.0016272355779638269 -0.00022651638175445483 -0.004495499131480738; 0.0017639679226623343 0.0032132803622330784 -0.008075396101665354; -0.002399128279467755 0.0009397329633075243 -0.001265677721404874; -0.0006783443404034931 0.00181490934891662 -0.0038066164806439514; -7.363198092194976e-5 -0.0006156090198577929 0.0025533897429266036; -0.00016848268574564925 -8.073785841727888e-5 -0.0036630689150155163; 0.004632400314051728 -0.0027766573173736214 0.0016227718024420155; 0.0006653086056353116 -0.0002755662107995974 -0.0015419370740834635; 0.008834329354208404 -0.0022143300210357075 -0.004434894486046783; -0.00044143300977674395 -0.0003437299274598742 0.0038594439896986136] %
+
+Mass Used: 86.98674935844974 kg
+Launch C3: 96.96432507011197 km²/s²
+||V∞_in||: 1.9949981947699288e-5 km/s
diff --git a/archive/ES_0.5593835100039664 b/archive/ES_0.5593835100039664
new file mode 100644
index 0000000..607fb43
--- /dev/null
+++ b/archive/ES_0.5593835100039664
@@ -0,0 +1,22 @@
+archive/ES_0.5593835100039664---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T12:27:55.152
+Launch V∞: [8.105334070293248, -5.8558610612091675, 0.08754627253355822] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0033081287393901654, 0.0022537435848444523, 0.0001417010537802654] km/s
+ V∞_out: [-0.0029683994467826105, -0.0013112977351965422, 0.0023606663452047246] km/s
+ time of flight: 1.87495777877623e8 seconds
+ arrival date: 2030-04-26T14:37:32.152
+ thrust profile: [0.09170015032048169 -0.003065931052606919 -0.03616564386206694; 0.046801721135328066 0.023320579149417188 -0.061354950003131105; 0.062324911584736596 0.04502742713454671 -0.13744198681295036; 0.04019609665572184 0.037700146098231066 -0.13279807848920674; 0.024957503051377995 0.027618054818758182 -0.11067103960317369; 0.00932715752565309 0.011301893158033526 -0.05118216858940627; 0.015341042129611243 0.021998905972789036 -0.09805908610635156; 0.004875530788184435 0.007483688626309019 -0.039211663494991104; 0.003966336769446717 0.00584124658008226 -0.03255247273404376; 0.002136585539987963 0.00349095272582184 -0.018580960413428767; -0.00029048047975100506 0.00033125413981242033 -0.010065687074995618; 0.0033686451106454676 0.0038772778097043792 -0.03147174409846853; 0.0003368043514143344 -0.0008729032967878804 0.0025716454941793624; -0.004165281901825494 -0.000942836008579814 -0.0009157344722883405; 0.0010308024357409385 -0.0012420005166636047 -0.00719091314170521; 0.0015627585925186967 0.0004016036713349751 -0.0032275236878318275; -0.0028089898394434527 -0.0017869103110906685 0.0004822701437660684; 0.00782113151281644 -0.002203234778220728 -0.0070810962730126995; -0.001090173276897921 0.00469124009055732 -0.005084271860607995; -0.0007954376257185205 -0.0003021431269939058 -0.00227403716235035] %
+
+Mass Used: 69.3086828683463 kg
+Launch C3: 99.99521350907678 km²/s²
+||V∞_in||: 0.00400539075387772 km/s
diff --git a/archive/ES_0.5593865955335697 b/archive/ES_0.5593865955335697
new file mode 100644
index 0000000..88f12ae
--- /dev/null
+++ b/archive/ES_0.5593865955335697
@@ -0,0 +1,22 @@
+archive/ES_0.5593865955335697---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T13:47:52.138
+Launch V∞: [7.830369675215263, -5.851365424215272, 0.07486301145722189] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8678054501508637e-6, 4.519095654316047e-6, 4.236779849675261e-7] km/s
+ V∞_out: [-4.052504119286445e-7, 1.8606456108334682e-6, 5.021899820453955e-6] km/s
+ time of flight: 1.817159862840602e8 seconds
+ arrival date: 2030-02-12T18:27:38.138
+ thrust profile: [0.33846263791480474 -0.0005988406101915504 -0.09545881729099959; 0.13389026802090775 0.08179265298210402 -0.1298451362199706; 0.06712260690570164 0.06951935612296808 -0.12209271736844832; 0.03319164739795512 0.0464629649104981 -0.0958944623574158; 0.03170775283919946 0.05804671653672937 -0.12553840194144608; 0.0188248601025011 0.045913364241185715 -0.1080350462312364; 0.007489169381306832 0.018061700207009184 -0.04834763475240916; 0.008155831011307076 0.03335387862059593 -0.0850824349230547; 0.002133244257298816 0.006153741302922125 -0.01931837712369478; 0.0026626742423888194 0.007222636931820853 -0.02302403116160568; -0.00035353148484285285 0.0026349659005682844 -0.0077341203006127636; 0.002069077182795293 0.003685162834046083 -0.01212533007519175; -0.0016375011623456298 0.0006345219904463329 -0.0027337147300640105; 0.00041203980952793167 -0.0006809489947494022 -0.0007305918961998423; -0.0015930424329568564 0.0012810402351120084 -0.00030964765861919794; -0.000529980560164303 0.0011372647260364695 -0.001108704144909619; 0.0008330494213495979 -0.0013574401512322083 0.0010669516331573892; 0.0002675312475643912 0.0031572855869984205 -0.00010360576545931713; -0.0013402000781039666 -0.0032405341718356523 0.004698351202016785; -0.002129083351571173 -0.0003852798255262336 -0.002803676448699527] %
+
+Mass Used: 95.19153033831435 kg
+Launch C3: 95.5587710487172 km²/s²
+||V∞_in||: 5.368988421268882e-6 km/s
diff --git a/archive/ES_0.559390220620385 b/archive/ES_0.559390220620385
new file mode 100644
index 0000000..6abecb0
--- /dev/null
+++ b/archive/ES_0.559390220620385
@@ -0,0 +1,22 @@
+archive/ES_0.559390220620385---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T15:51:05.584
+Launch V∞: [7.7821266210751965, -5.873757572037381, 0.08683157066282186] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.583254472653991e-7, 2.1937116393848518e-6, -5.3176998123150456e-5] km/s
+ V∞_out: [-2.3168104957654896e-6, 5.316135618411837e-5, -4.008827790501106e-7] km/s
+ time of flight: 1.874957778779194e8 seconds
+ arrival date: 2030-04-24T18:00:42.584
+ thrust profile: [0.46511332485497864 0.007291907181902973 -0.12316917216631663; 0.09215914487017086 0.05837025075130004 -0.10096698567038921; 0.029104318744126296 0.02978607404357724 -0.06412689663277882; 0.020322540320583185 0.03079574042817173 -0.0737300215053481; 0.032782565652986394 0.05693268619011621 -0.13502110369062253; 0.01436723211041562 0.026653285122217266 -0.07716283862378873; 0.017747074120544007 0.04407621525898486 -0.1212232435619339; 0.004377828460062114 0.010865318320821384 -0.028903249960545045; 0.0035196254992356586 0.011531473764819859 -0.03791440364943793; 0.0030748271097296733 0.013530028349426343 -0.04538011377389049; -0.0012751222138679894 0.0008698692133362505 -0.004627877029762741; 0.00022684387326691116 0.0015247307719637186 -0.005522744931924148; 0.0015459059278046337 0.0003331630831102352 -0.001208349260302075; 0.000182244687766673 0.0025513250082145385 0.0015494297800764537; 0.0006328155813505103 -0.00013748107945073945 0.002316373786418748; -0.0007027101407150526 -0.0008350703933367318 -0.00049192010290396; 0.0037569931763077316 -0.0011903371035943038 0.002440222514342067; 0.002343683325132673 -0.008008150101129409 -0.0027344188428321255; -0.0011585399459125949 0.005846374149292645 0.0023780984643338907; 0.0030168063444847015 -0.0020616814771603014 0.00104419791697949] %
+
+Mass Used: 98.0465595719138 kg
+Launch C3: 95.0700624831775 km²/s²
+||V∞_in||: 5.3223433723055465e-5 km/s
diff --git a/archive/ES_0.5593934353364093 b/archive/ES_0.5593934353364093
new file mode 100644
index 0000000..194a0a6
--- /dev/null
+++ b/archive/ES_0.5593934353364093
@@ -0,0 +1,22 @@
+archive/ES_0.5593934353364093---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T01:50:40.159
+Launch V∞: [7.584405457067927, -5.982547902799037, 0.12146371449895577] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3600315292714976e-6, -2.520609063478306e-6, -7.297485980967423e-6] km/s
+ V∞_out: [-7.148517649807644e-6, -8.581721550350803e-7, 3.091265877979956e-6] km/s
+ time of flight: 1.7770987369478285e8 seconds
+ arrival date: 2029-12-26T21:41:53.159
+ thrust profile: [0.5461826002461322 -0.013696959522247637 -0.13937148179847472; 0.08970435303174587 0.05179390613781027 -0.08387942280904749; 0.062294409530700576 0.06039259991550482 -0.10281126141686688; 0.05016101599427686 0.06605008254789364 -0.1220239444798593; 0.07342675113275947 0.12573209799452995 -0.23170708312304025; 0.03150000086487754 0.06347969689665087 -0.13404219148664065; 0.006905085492216385 0.01585725414123004 -0.03819486654813531; 0.0025275360433213087 0.006718069312793166 -0.01710625703968547; 0.002849077239861811 0.008613874722001934 -0.022854587591967707; 0.0015833295394875131 0.005477675257053304 -0.015098545691952821; 0.0011887795860042372 0.004821079940590404 -0.013158885822880695; -0.0001384379051651099 0.00077710808871091 -0.0016952276709498333; -4.762439004283095e-5 0.0003677431940806586 -0.0013183569736572773; 0.0004863044349101241 7.047746224303117e-5 -0.0008825536332294782; 0.0002143281649080685 0.00033551500018208524 -0.0010662947712074243; 0.00012556964528384937 0.0004487960736625239 -0.0003348895725996926; 0.000581245221430686 -0.0002205886187422975 -0.00046755684419912884; -0.00033800674390321644 -0.000395994632920596 0.001067371348162741; -4.721448765360547e-5 -0.0003028754934509086 0.0003587083988693348; 0.0003962528937653026 -8.514062947226231e-5 -0.0009220310727035158] %
+
+Mass Used: 108.20744717332127 kg
+Launch C3: 93.32883898042678 km²/s²
+||V∞_in||: 7.83941690777558e-6 km/s
diff --git a/archive/ES_0.5593993012303666 b/archive/ES_0.5593993012303666
new file mode 100644
index 0000000..239dc26
--- /dev/null
+++ b/archive/ES_0.5593993012303666
@@ -0,0 +1,22 @@
+archive/ES_0.5593993012303666---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:02:42.068
+Launch V∞: [8.053751464275347, -5.796713157860654, 0.10290519156433016] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.276730866690494e-6, -1.8818921941330915e-6, -2.2393653008913888e-7] km/s
+ V∞_out: [1.594502467734806e-7, -7.560680757230502e-7, -2.150661697620645e-6] km/s
+ time of flight: 1.8525851388955477e8 seconds
+ arrival date: 2030-03-29T04:44:35.068
+ thrust profile: [0.16204722183112896 -0.005486350343928599 -0.0566664714471663; 0.07690556774651724 0.038001547726084745 -0.08946306179778718; 0.057270956201025715 0.045123558303532686 -0.11944698380273658; 0.043418403600151194 0.04378986473347458 -0.13239575267745002; 0.03155514492797114 0.03706001255732982 -0.12705264805107253; 0.020988733228677073 0.027690415544708333 -0.1042377272582192; 0.012071067289472851 0.01698922490307589 -0.07052568572481403; 0.004190493517998064 0.005531690775534679 -0.028242322910671656; 0.0005808299207018905 0.004025687087805636 -0.008809577342075235; 0.0024831070641292883 0.002839833079428605 -0.01960451543541032; 0.00040002629076364314 0.0019795918571595297 -0.013807354075431785; -0.00011906345774456728 0.004262266887223984 -0.008407044332029628; 0.0006229191050785374 0.0013196036642591415 -0.004820797250322431; 0.0004854757875421131 0.0016072126749810626 -0.014016355176055048; -0.0007395429414023677 0.0014275009900940575 -0.003785827159569032; -0.0037388540453926365 -0.001738556638473617 -0.005359720782264247; -0.008847845297231071 0.0033575880854886473 -0.0037612682976481127; 0.0015004831217752758 0.004242596756016055 -0.005864149843856838; 0.004978885676447195 -0.01033177419434443 -0.004505468547789329; 0.0045666280071555545 0.0002761779596750716 -0.016116013866396172] %
+
+Mass Used: 78.1927689946101 kg
+Launch C3: 98.47538556128303 km²/s²
+||V∞_in||: 2.285105578700399e-6 km/s
diff --git a/archive/ES_0.559427710075528 b/archive/ES_0.559427710075528
new file mode 100644
index 0000000..4fe2df1
--- /dev/null
+++ b/archive/ES_0.559427710075528
@@ -0,0 +1,22 @@
+archive/ES_0.559427710075528---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T08:50:38.995
+Launch V∞: [8.002873407065277, -5.515009382655391, 0.21546358996516088] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.245843562228415e-10, 1.486871857977842e-9, -1.8713370426912143e-9] km/s
+ V∞_out: [1.099568981460862e-9, 2.2144970890684137e-9, 5.750909472703617e-11] km/s
+ time of flight: 1.8734969348830265e8 seconds
+ arrival date: 2030-04-18T18:25:31.995
+ thrust profile: [0.5181404499156491 0.011707704321716694 -0.1321227810662717; 0.07420377290821646 0.05105342528651822 -0.07717094732472232; 0.04358935422946653 0.04764179418731105 -0.08010662514562919; 0.039062670095608897 0.06056007632807127 -0.1100202282545749; 0.020566468474061527 0.037896523401505275 -0.08459048714372855; 0.009907303169866538 0.026769939614343766 -0.05969560090898431; 0.005935716758227629 0.02491260175946456 -0.06300787390387333; 0.007670181740493238 0.032383460536743076 -0.08396938570641847; 0.006582352071400813 0.03657012490287199 -0.0947818750953326; 0.0030231532111552706 0.010130325059278819 -0.02814439256504706; 0.0003807159389339858 0.0004806747508686736 -0.0023476605582662038; 0.0009460000467835517 0.002724539430784211 -0.0037623251205569585; 0.0010458990881236562 0.0002969424311096854 -0.0010027716397443863; -4.33096393565221e-5 -8.758336936223706e-6 -0.00013899211926842017; 0.00010686262577065838 0.0009427788374238665 0.00020478068485927097; 0.0015603761535931291 5.208494697748667e-5 0.0024986467350744486; -1.007346968151827e-6 -0.00017246715676783237 0.0014904055267283688; 2.0148360870577213e-5 -8.524600360048536e-5 0.00014559926419050275; 0.0006755152172295618 -0.0007529212232986822 0.0016951929515360074; 0.002280920664890583 -0.0007064101401231719 0.0022663860996259364] %
+
+Mass Used: 101.37053614458955 kg
+Launch C3: 94.50773581889027 km²/s²
+||V∞_in||: 2.4703837490222203e-9 km/s
diff --git a/archive/ES_0.5594297755335842 b/archive/ES_0.5594297755335842
new file mode 100644
index 0000000..1970acc
--- /dev/null
+++ b/archive/ES_0.5594297755335842
@@ -0,0 +1,22 @@
+archive/ES_0.5594297755335842---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T02:39:18.774
+Launch V∞: [7.824341825084701, -5.663215388899223, 0.15829124206057124] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.9288240883080463e-5, 3.531560285381823e-5, 0.0023365712735616832] km/s
+ V∞_out: [-0.002056887566080039, -0.000762673601280527, 0.000803400247647952] km/s
+ time of flight: 1.8749577787474898e8 seconds
+ arrival date: 2030-04-21T04:48:55.774
+ thrust profile: [0.5129626440435591 0.01708489376761223 -0.13617348383436012; 0.1588048343357197 0.106615805975745 -0.15399205929351098; 0.059058940961300356 0.06574915732460022 -0.1097502453259143; 0.03978181840753967 0.06082782840534072 -0.11310829345727952; 0.028900300233524523 0.05694482215572099 -0.11588000969358153; 0.018738055569183506 0.04578420759621076 -0.10100455701067253; 0.007156920486600508 0.0212972081057071 -0.05201202404341925; 0.0040396856790410355 0.012702320408288531 -0.034027227008334805; 0.0007840666861014377 0.0026626983876536178 -0.009037854827639292; 0.0012039451836266357 0.0027394680773373406 -0.008938733369062134; -0.00013058116713132923 -0.00015417603758312488 -0.003078217212463226; -1.3359981886472525e-5 0.0004743915382964632 -0.0006018880686912741; 0.0010443362972609946 0.0006648852465334916 3.148845418983015e-5; -0.0006035899936028185 0.0012900802864025942 -0.0007267445151593385; 0.0006586934204738352 -0.001011571049705322 0.005123452965967572; -0.00171552954954281 -0.0016690754727536783 0.002915841406591081; -0.0011888843966151783 0.0006796036714550865 0.003982620128552475; 0.004880460085485379 -0.002629689900233061 0.00463898751860342; 0.0030463867744523585 0.0025405200367440363 -0.0064200832192889586; -0.005553001349775244 0.004675631564257913 0.0009418183491283373] %
+
+Mass Used: 108.31663180665237 kg
+Launch C3: 93.31738965414786 km²/s²
+||V∞_in||: 0.002337357875663875 km/s
diff --git a/archive/ES_0.5594458608374229 b/archive/ES_0.5594458608374229
new file mode 100644
index 0000000..9ca0c5f
--- /dev/null
+++ b/archive/ES_0.5594458608374229
@@ -0,0 +1,22 @@
+archive/ES_0.5594458608374229---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:08:07.672
+Launch V∞: [7.942466890869841, -5.693966758822164, 0.0008204887937681685] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.69149721511683e-9, -1.6030449541226301e-9, -2.3664325398717512e-9] km/s
+ V∞_out: [-5.3961834218116457e-11, 1.8917012937854661e-10, -3.031603293323583e-11] km/s
+ time of flight: 1.8749577785953334e8 seconds
+ arrival date: 2030-04-21T17:17:44.672
+ thrust profile: [0.3108077987909783 0.016810035050266247 -0.0854580498244004; 0.15858472665722306 0.11049077206510473 -0.14854621293912043; 0.07437634494524863 0.08645685795804328 -0.13164131686008693; 0.028023383062989904 0.04435757788360134 -0.0797684099256722; 0.03075770293411073 0.06366117599110602 -0.11948421974639581; 0.010155806960245106 0.026522809333010114 -0.056849283948578785; 0.013194266749101357 0.04228822923432863 -0.09346671589688553; 0.0039214548137022345 0.013676878366367471 -0.03562856959141662; 0.0023118910341491565 0.013851406911807421 -0.037158735187039695; 0.0015231360283065644 0.004943903837646939 -0.013526337426974702; 0.0014070927313881904 0.005266706129318094 -0.008291722099247889; 0.0004697006865361633 0.0038009898476864634 -0.006461663797279847; 0.0023218662582622763 -3.738398963623341e-5 -0.0019664624539926113; 0.0013198015648279533 -0.001092250049869608 0.00031800952230722325; -0.0011807255125007043 0.00010681213818451545 -0.0006606505210641172; 0.0005719781014763362 0.0012697012285259588 0.006750918995889994; -0.0007970197103264673 -0.0009510069725624946 0.0034612504272700773; 0.0014843490064957035 -0.001537523585425206 -0.001454663492723197; 6.719466081608282e-5 -0.0011984340321073792 -0.006736178830407351; -0.0003494910028153597 -0.0006878482401606767 0.0019078799869090344] %
+
+Mass Used: 95.57994676502585 kg
+Launch C3: 95.50403843633728 km²/s²
+||V∞_in||: 3.3212827219991202e-9 km/s
diff --git a/archive/ES_0.5594490698276515 b/archive/ES_0.5594490698276515
new file mode 100644
index 0000000..ea5ee14
--- /dev/null
+++ b/archive/ES_0.5594490698276515
@@ -0,0 +1,22 @@
+archive/ES_0.5594490698276515---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T04:31:25.910
+Launch V∞: [7.751359974240779, -5.624063336078149, 0.2618933566050244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5567590252135393e-6, -5.052272140360822e-6, -1.4326599689461588e-5] km/s
+ V∞_out: [-1.4428724786842859e-5, -1.2648184755843398e-6, 4.840410909187726e-6] km/s
+ time of flight: 1.8749577787438494e8 seconds
+ arrival date: 2030-04-20T06:41:02.910
+ thrust profile: [0.6261963728706869 0.014727863834228564 -0.16129357783203893; 0.17961304984470644 0.11678026519378298 -0.16874058433081127; 0.08916751868508158 0.09643737241880244 -0.15658090318194387; 0.04432540231362824 0.06607188098421274 -0.12165882040247278; 0.024088812975356977 0.045641424986185085 -0.09413444583963658; 0.011373522053092753 0.02673109826890046 -0.060509664865968205; 0.005268722738933908 0.014476275378950635 -0.03556757078790615; 0.002122480481943461 0.007998581405787047 -0.020628196915779863; 0.0007221020939926891 0.0038372655560638996 -0.011004480458753112; 0.001328077399916341 0.004138011683931514 -0.012763981743813472; 0.0005921806483529992 0.0037781122828710206 -0.007239090444035234; -0.0015292024943745395 -0.0007562907445611078 -0.0009888912240064523; 1.2917884443960518e-5 0.0010404958051089736 -0.0011635932250403996; -0.003036134251207473 -0.0014625235054469394 -0.004030702457057878; -0.0012993726650091277 -0.0042429877478472955 -0.000506601533134298; -0.0008358090893867858 -0.0008539122259218462 0.001042679030762844; 0.0010540981013349045 0.002462539176153568 0.003031282420274171; 0.00043506389021700674 -0.0017331674881992363 0.0024404450011774647; 0.0014738871021430615 0.0005188374597726291 -0.008816767336815454; 0.001196925357839768 0.0012896202018587944 -0.0012118777355562868] %
+
+Mass Used: 117.29407653142653 kg
+Launch C3: 91.78225798871432 km²/s²
+||V∞_in||: 1.527090079546491e-5 km/s
diff --git a/archive/ES_0.5594501416161494 b/archive/ES_0.5594501416161494
new file mode 100644
index 0000000..2a94629
--- /dev/null
+++ b/archive/ES_0.5594501416161494
@@ -0,0 +1,22 @@
+archive/ES_0.5594501416161494---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T21:34:35.115
+Launch V∞: [7.8042908365045465, -5.76448868513811, -0.4722798748714231] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.455665982251335e-7, 2.233100471616393e-6, 7.178393206811753e-6] km/s
+ V∞_out: [6.865008860351739e-6, 7.202277776214557e-7, -3.065057905442724e-6] km/s
+ time of flight: 1.87495777795949e8 seconds
+ arrival date: 2030-04-22T23:44:12.115
+ thrust profile: [0.4565231175464 0.009469703530210266 -0.13910753228347628; 0.12870082673738967 0.07974907181083289 -0.13893252496161324; 0.07417851897785237 0.0756900479386174 -0.1482032715349726; 0.044717399104731166 0.061686470903071354 -0.1369761316408321; 0.020947120211034162 0.03645284777623503 -0.09159771463657446; 0.015216570911182718 0.03220028319865238 -0.08742157292412317; 0.006512684520703178 0.016416432662709063 -0.04857616939571797; 0.006275977983215159 0.018549957946483595 -0.05816806813969159; 0.0008508063646635984 0.0029344243761056073 -0.01068585531337047; 3.7446597234649316e-5 0.0009981698164348 -0.004145433176633321; -0.0013315065105558258 0.0008437373097544153 -0.00034377355928246676; -0.0002741727638111825 1.3783060729258712e-5 -0.0009462826493215527; -0.0007252198900247509 -0.00013398466041460768 0.0021070628726850395; 0.0013726118068124022 0.00035185653176939593 0.0024227837317018696; -0.0005594608326078092 -0.0010857543246208241 0.0031830833975168326; -0.001080165368056447 -0.0004623279138823321 0.0014176804615962612; -0.0007439672513649561 9.596027885631305e-6 0.004288285374476459; -0.0030649521945873936 -0.004395314209667805 0.0013392422326686223; 0.00010517822691037648 -0.0010557153159548257 -0.0007399418560114477; -0.0002587233880106032 -8.493692220558065e-5 -4.637346711075432e-5] %
+
+Mass Used: 102.26238622359188 kg
+Launch C3: 94.3593335420427 km²/s²
+||V∞_in||: 7.5545970309688575e-6 km/s
diff --git a/archive/ES_0.5594754813276137 b/archive/ES_0.5594754813276137
new file mode 100644
index 0000000..12a3ecc
--- /dev/null
+++ b/archive/ES_0.5594754813276137
@@ -0,0 +1,22 @@
+archive/ES_0.5594754813276137---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T18:21:05.975
+Launch V∞: [7.936400034561741, -5.830707693163598, -0.39036085579951263] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4179498207992023e-9, -1.6395620623913758e-9, -1.2744799637544466e-9] km/s
+ V∞_out: [1.6906039238485318e-10, 3.3702531680697614e-10, 8.775402337283036e-12] km/s
+ time of flight: 1.8749577780942544e8 seconds
+ arrival date: 2030-04-25T20:30:42.975
+ thrust profile: [0.35133575410688994 -0.01028274056321476 -0.13237950601671644; 0.03834541230249723 0.018052145845690044 -0.05005066649785954; 0.0473525394622885 0.03591085226016094 -0.10970383680404952; 0.036172654569132386 0.034691695419559944 -0.12260052840633333; 0.026993950391408714 0.030495428099283482 -0.1224142201184527; 0.021540739358331427 0.027341907976026904 -0.120584020972995; 0.010637913539488267 0.014887532620039239 -0.074394428419627; 0.0021525838494840747 0.003673353298256685 -0.01969247580497182; 0.005452006104896146 0.0067525270851441135 -0.03197846690890696; -3.891186735837087e-8 0.00022424159622493533 -0.004806906280143414; -0.002220900232208731 0.003268385972278457 -0.011553303317050522; 0.0005079439433786952 0.0008941077101590651 -0.006018753984352646; 0.00016920578034160182 -0.00044906896904470684 -0.007818274440772686; 5.109522530749664e-5 0.0010401928096316583 -0.000570541284383884; -3.905174886640196e-5 9.956011783512876e-5 0.001924957184931739; -0.0002776519760780054 -0.0015192335165902507 -0.0037810758482406106; 0.001462430249962779 -0.0014981946051887294 -0.002991503401404907; -0.0006584132324692089 -0.0007243063065563273 -0.006570345908146896; -0.0005037510337997154 0.0014982301135357252 -0.0025537251133859592; 0.012820499297821357 0.011220321958470463 -0.008210793353195824] %
+
+Mass Used: 86.09484891042848 kg
+Launch C3: 97.1359793094493 km²/s²
+||V∞_in||: 2.5145664892281307e-9 km/s
diff --git a/archive/ES_0.5594837003663802 b/archive/ES_0.5594837003663802
new file mode 100644
index 0000000..fa02a12
--- /dev/null
+++ b/archive/ES_0.5594837003663802
@@ -0,0 +1,22 @@
+archive/ES_0.5594837003663802---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T18:57:48.136
+Launch V∞: [7.556213857167881, -5.857354403344505, 0.29182561204832586] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.0830801234307356e-5, -3.576846526398046e-5, -1.4025935381937877e-5] km/s
+ V∞_out: [-7.608159742557626e-6, 4.646011673219497e-5, -4.284850478871583e-5] km/s
+ time of flight: 1.874957778745517e8 seconds
+ arrival date: 2030-04-21T21:07:25.136
+ thrust profile: [0.5582679064078062 0.023955307109912106 -0.12845396020467087; 0.3109297745241928 0.21401776664670671 -0.24734197095868163; 0.05694778832670707 0.06319421945141572 -0.10077824982463077; 0.03213506660322676 0.05126631183735215 -0.0940997361723391; 0.019513428134254166 0.03883291435786982 -0.07967998770059401; 0.01475884102962074 0.03805923179276296 -0.08001895712975284; 0.01082406912405938 0.026969352001014617 -0.06228424853965321; 0.002951209089937249 0.010405110106398538 -0.025904676137431637; 0.002015508573473901 0.008939598755771865 -0.022859586682796196; 0.0001450306991048083 0.00011204183665096683 -0.0012262007043555485; 0.00015817112770589173 -6.969912380714498e-5 -0.002745792109488998; -0.00014149842719079933 0.00019608959090716734 -0.0011824383003953738; 0.00027431025036539074 -3.2884590390345775e-5 0.0009255512100343123; 0.0002745319439125832 0.0002642080991727912 -0.0025891655536678295; 0.0006425286143440821 0.002477730010355542 0.00010797732741218632; -0.0018796255817648668 -0.000936474294207507 -0.000355703455274921; -0.0009639972469831023 0.0008289110363079524 0.003965257896525392; 0.0005557737406087606 -0.003687251206505646 0.0016973959293767652; 0.0001182183969612138 -0.001433860228474647 -6.666707297121703e-5; 0.0006434522009497796 0.0004837594717549425 -0.0002254670842392096] %
+
+Mass Used: 119.03855497212862 kg
+Launch C3: 91.49013064948255 km²/s²
+||V∞_in||: 6.3717190182874e-5 km/s
diff --git a/archive/ES_0.5594914850696805 b/archive/ES_0.5594914850696805
new file mode 100644
index 0000000..581090a
--- /dev/null
+++ b/archive/ES_0.5594914850696805
@@ -0,0 +1,22 @@
+archive/ES_0.5594914850696805---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T02:41:23.553
+Launch V∞: [7.8388854969087305, -5.743618589746484, 0.21908346450751706] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9000002571476476e-5, 1.6945135144626448e-5, 0.001447732836835496] km/s
+ V∞_out: [-0.0012819494447415152, -0.00044497974046518995, 0.000499170451392003] km/s
+ time of flight: 1.8461193079328907e8 seconds
+ arrival date: 2030-03-18T19:46:53.553
+ thrust profile: [0.4329545716895648 -0.002770330629582656 -0.12253578748637321; 0.13246643178336356 0.08067518488415848 -0.1345524348947818; 0.09412158853849194 0.09211226396232805 -0.1696756067587716; 0.03313549563511783 0.04445013399849786 -0.09535149633636032; 0.015086959304773708 0.02512402857088667 -0.060196407047058476; 0.0150533272385874 0.03008901424078432 -0.07605075265460864; 0.01365674733135764 0.032216334294215006 -0.08672464141652715; 0.002817237791657182 0.008801008150175352 -0.027062112209456653; 0.004944114501948654 0.015737609203773227 -0.04792481936598539; 0.0023337236713482515 0.0067744683167899715 -0.02653866641691426; -0.0021884476798975623 0.004561362184793232 -0.005936591026768574; 0.0009143036684276218 0.0022734694090929004 -0.006096868880620122; 0.00010931562883047783 -0.00034050286318815584 0.0019069629419001411; -7.857022470445711e-5 0.0006570809426366549 -0.002603596088465985; -0.0014251438429987938 0.0010508760162841703 -0.0002999316791725585; -0.0008302336521636795 -0.006692007835461399 -0.002778224981884284; 0.00370385633520264 0.0005617327117092409 -0.002278776677660972; 0.002365253509802265 -0.0018587474850077345 0.0015681153111662535; 0.00023425545683061186 -0.00159058929112692 -0.004186241562230978; -0.009131027582131693 0.004015419337253797 0.0037401247780300354] %
+
+Mass Used: 101.57594481643036 kg
+Launch C3: 94.48527790254803 km²/s²
+||V∞_in||: 0.0014481224066376325 km/s
diff --git a/archive/ES_0.5594968715221014 b/archive/ES_0.5594968715221014
new file mode 100644
index 0000000..f6a186d
--- /dev/null
+++ b/archive/ES_0.5594968715221014
@@ -0,0 +1,22 @@
+archive/ES_0.5594968715221014---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T05:08:40.707
+Launch V∞: [7.917197514273394, -5.694840119406399, 0.10249352496086837] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.461424883687592e-7, 4.312541088544484e-6, -9.631917065960804e-5] km/s
+ V∞_out: [-3.877901420919217e-6, 9.63002587970373e-5, -1.0284584107114932e-6] km/s
+ time of flight: 1.8286587849547967e8 seconds
+ arrival date: 2030-02-25T17:13:18.707
+ thrust profile: [0.42495398592267947 -0.01191797719118164 -0.12701978892275456; 0.10811810895562848 0.06179269361795465 -0.11636248731165165; 0.062012596246056574 0.057636322302678976 -0.12059966101234366; 0.040328884883011284 0.05007144450185853 -0.11747764713960854; 0.02363041164643408 0.03827567902363185 -0.09823635734757914; 0.009418784522570984 0.01769550589332659 -0.05174322828622478; 0.017143234846863815 0.037639640670233426 -0.11359423861725368; 0.008584782469556339 0.02180985029478031 -0.07138829582226246; 0.002529895530847597 0.006909323814229346 -0.02478621338464756; 0.0016472805675369665 0.004515823259967815 -0.017403481735744283; 0.0012891894400014381 0.0030355976836349044 -0.012915055861064128; 0.0004782001986108283 0.0016419683184645637 -0.007210451681577332; 0.0014341364588838332 0.0004678429870883642 -0.0018472106257396968; -0.0003050289418853736 -0.0006423417219163905 0.002374302082252219; -0.0008087953647392572 -0.0010466486095248924 0.001113956580805298; -0.002698494910612246 0.001403096713810957 0.00272251433492484; -0.0009355936055035697 0.0014241397476187792 -0.0023503384258977736; 9.331972630147558e-5 0.002822588815410971 -0.002071607794138448; -6.528126436435499e-5 -0.0009738507203650685 -0.000731681400610681; -0.0016818943321174882 -0.004408409678478471 0.0037190822329761066] %
+
+Mass Used: 97.8579520108392 kg
+Launch C3: 95.12372538827641 km²/s²
+||V∞_in||: 9.641721277247483e-5 km/s
diff --git a/archive/ES_0.5594972111692459 b/archive/ES_0.5594972111692459
new file mode 100644
index 0000000..ca0b755
--- /dev/null
+++ b/archive/ES_0.5594972111692459
@@ -0,0 +1,22 @@
+archive/ES_0.5594972111692459---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T19:12:52.475
+Launch V∞: [8.010510748435083, -5.804548496761168, 0.36850564295483135] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9912406318739745e-6, -7.318151255744294e-5, -1.2313630880739285e-6] km/s
+ V∞_out: [-7.110535801451378e-5, 1.0280634909181444e-5, -1.582324756250131e-5] km/s
+ time of flight: 1.874957778480893e8 seconds
+ arrival date: 2030-04-25T21:22:29.475
+ thrust profile: [0.2948140442670635 -0.007006073735573494 -0.08649580957991782; 0.021592909039488233 0.010663595396357022 -0.027867300521980488; 0.04327842019778191 0.03591253591880295 -0.09796291550215133; 0.027313447420797474 0.025962794240563733 -0.09131945284407827; 0.0233904741193157 0.026767156998633582 -0.10552710908580017; 0.011926607637877267 0.015226417174483538 -0.06420080144904373; 0.018973882413910986 0.020741950655028155 -0.09327956142791638; 0.006387160616881484 0.010392457419129985 -0.054777447011663254; 0.008835406541616698 0.017050542094665257 -0.07297554258076486; 0.004007390767603585 0.008411130868454825 -0.04574661298800571; 7.437473118067676e-6 0.0005352969707860043 -0.0031299973565384713; 0.0028301072315152272 0.004677591855521957 -0.042929699842749636; 0.0001505600581872816 -0.0002667245775966101 -0.00033719431231020626; -0.0016017441854979796 0.004508842137090947 -0.0004800591107983422; -0.0018377579580302124 0.002683454573223168 -0.002324755092964739; 0.0015483332671162586 -0.003366518153662899 -0.0007542133442413783; -0.00020693178808980778 -0.0005930390273367303 -0.0005029089540513507; 0.0026864632079922723 -0.00221636621560026 -0.0014240796859225806; -0.0015854762358756668 -0.0029268154751692327 0.0004817623376939184; 0.007867254519427333 -0.000516358117008271 -0.003979775200751292] %
+
+Mass Used: 81.0983840503277 kg
+Launch C3: 97.99686211093587 km²/s²
+||V∞_in||: 7.325296960374797e-5 km/s
diff --git a/archive/ES_0.5595206250137768 b/archive/ES_0.5595206250137768
new file mode 100644
index 0000000..c3c3004
--- /dev/null
+++ b/archive/ES_0.5595206250137768
@@ -0,0 +1,22 @@
+archive/ES_0.5595206250137768---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T15:23:06.271
+Launch V∞: [7.9144295260030555, -5.92086027038597, 0.06926768009478912] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1000800419831542e-5, 0.000160868030785286, -0.0028868201183990406] km/s
+ V∞_out: [-0.00027667374934613507, 0.0028925516279740054, -3.71845980884123e-5] km/s
+ time of flight: 1.840202009565851e8 seconds
+ arrival date: 2030-03-15T12:06:26.271
+ thrust profile: [0.26127169454801635 -0.009419746301471176 -0.09206387803525955; 0.07184867462313006 0.03691585348970368 -0.09601292557623456; 0.046594218979505636 0.03816334107970516 -0.11269414996133048; 0.031465547241469737 0.03293426896050871 -0.11258658904779371; 0.02340914886110083 0.027890963514734385 -0.10764648914226475; 0.016071033728294642 0.02091473538351316 -0.09029270906634462; 0.010487668396991716 0.013185959879505925 -0.06280647553126795; 0.0077147367074237 0.012072729321634402 -0.06654588130869112; 0.003615311922915776 0.006025329286772417 -0.03317612098207195; 0.000930167196101616 0.004256796475549029 -0.01959711016425056; 0.003872359261794779 0.0070511697841658914 -0.043022778529544545; 0.0006095641411637888 0.0005393761738294604 -0.0057840190711693695; 0.0013811859941086583 0.0009037700360983447 -0.0030365573157633847; 0.0008144068491453091 4.75734178450103e-5 -0.001032968611019678; 0.004940427177403235 0.0005172279892609419 -0.00015200646570077796; 0.004288580330855426 0.002228899461584154 -0.0028531814938654717; -0.0033483509259734827 0.002459218944358259 0.004687080358650264; 0.001153367415058285 -0.0003959440934571461 0.007754503827610391; -0.0008616418949228006 0.0022305262695595336 -0.0011778509703982446; 0.0017607173065299132 -0.0012649838071432146 0.0010079559623368084] %
+
+Mass Used: 82.85985124518311 kg
+Launch C3: 97.69957907500968 km²/s²
+||V∞_in||: 0.0028913750972401455 km/s
diff --git a/archive/ES_0.5595343351181956 b/archive/ES_0.5595343351181956
new file mode 100644
index 0000000..9055845
--- /dev/null
+++ b/archive/ES_0.5595343351181956
@@ -0,0 +1,22 @@
+archive/ES_0.5595343351181956---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T08:43:51.933
+Launch V∞: [7.839363459800086, -5.495167717078827, 0.41292618986744073] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8514103035216931e-9, -1.6194363719524026e-9, -1.3819723876269756e-9] km/s
+ V∞_out: [-9.802442458629809e-10, 9.163439871146422e-10, -3.3794318558824427e-10] km/s
+ time of flight: 1.8749577787468886e8 seconds
+ arrival date: 2030-04-19T10:53:28.933
+ thrust profile: [0.7103604904750775 0.013021485474621447 -0.18122621761632496; 0.13897166092789806 0.08834322463212221 -0.13459893567579734; 0.05075533865098167 0.05291952145644776 -0.0924473483288444; 0.051837508622697814 0.07350700905175718 -0.1409872892396794; 0.017926813842953616 0.03177904369868192 -0.06881067580954169; 0.015557423558885326 0.033538325306211855 -0.0782867750684514; 0.008833544111574318 0.022745892016046394 -0.05690731794544143; 0.006700550576970491 0.020956025004851813 -0.05528685324615177; 0.0012107202810360727 0.00437306830718111 -0.012769752294260325; 0.0011968941966324768 0.002428869074149822 -0.007888624356476298; 0.0008974778039163903 0.001576694433302677 -0.0048155539171806875; -7.716089107376363e-5 -0.0015728984418026354 -0.003953659478389724; -0.0011720442855192464 0.0002652933999484055 -0.002395523648975823; -0.0011040179187917793 0.0005823083667879929 -0.0032862308162201733; -0.0003106461065512245 0.004695727571565772 0.0011587313456062642; 0.0006513315838840488 0.0004469474921271849 -0.0008528616362925274; -0.0007962918482250824 0.0009837681722623171 -0.0006593404987457405; 0.0010272939587450548 1.185146154286925e-5 -0.0023201900094045134; -5.4003866673994674e-5 -8.487590407076561e-5 0.0006160314962912663; -0.0010735606489521983 0.0028976829413202157 0.002687168746831012] %
+
+Mass Used: 117.15591586817163 kg
+Launch C3: 91.82299573195255 km²/s²
+||V∞_in||: 2.821372353120384e-9 km/s
diff --git a/archive/ES_0.5595495442092232 b/archive/ES_0.5595495442092232
new file mode 100644
index 0000000..3eba807
--- /dev/null
+++ b/archive/ES_0.5595495442092232
@@ -0,0 +1,22 @@
+archive/ES_0.5595495442092232---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T11:06:09.434
+Launch V∞: [7.502658693117302, -5.974751603284414, 0.08975167352345041] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.083470022845631e-5, 2.9239953373205304e-5, 0.0020516781106113724] km/s
+ V∞_out: [-0.0018313233629768636, -0.0006352565442578267, 0.000670578371240166] km/s
+ time of flight: 1.7961585933205637e8 seconds
+ arrival date: 2030-01-19T08:23:48.434
+ thrust profile: [0.6815976051980281 -0.011627674016592074 -0.1719462473107301; 0.1267492438803145 0.07425027812318793 -0.1283259282580054; 0.041615245005085524 0.038947557440476004 -0.07902631324194016; 0.03473557594311067 0.04406647474183048 -0.09666595388914395; 0.04081964452768727 0.06803852711628684 -0.15829985917727207; 0.016425884840059093 0.031171211783668076 -0.08252371059576127; 0.014428089710882571 0.03549886403161587 -0.10105042420209003; 0.006645942614852586 0.018258638421512114 -0.05333622507107863; 0.002454682151009857 0.007037390184786389 -0.02304083294819719; 0.003990214952059047 0.010365711098525984 -0.03533098225014074; 0.00010037675244706633 0.0002738469578477309 -0.0023592899375405076; 0.0003714049131303927 -0.00013992938898386162 -0.00019541782883853256; -0.0012224512558888729 0.00020931191927284546 -0.001953409732096989; 8.117828002555233e-5 6.475527897776916e-5 -0.0010525228714815768; 0.001480245804238837 0.002940279129890362 -0.00022452610949104802; 0.0009889669144911109 -0.0008799441661122207 0.0004258540618425487; -0.0008382809033791454 0.001493182271450052 -0.0005387668557811385; -0.00021171838472757213 -0.00365412617081766 -0.005076794819494749; -0.002046995769947501 -0.0017339564929909697 -0.000631490724990493; -0.0008677490969593941 0.0014623878132980865 -0.001598476776509491] %
+
+Mass Used: 116.1668042067522 kg
+Launch C3: 91.99559954925856 km²/s²
+||V∞_in||: 0.0020522927464613487 km/s
diff --git a/archive/ES_0.5595573754674337 b/archive/ES_0.5595573754674337
new file mode 100644
index 0000000..225a41a
--- /dev/null
+++ b/archive/ES_0.5595573754674337
@@ -0,0 +1,22 @@
+archive/ES_0.5595573754674337---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T05:42:17.783
+Launch V∞: [7.954998939465207, -5.851240710030373, 0.14850862495618214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4409329274947652e-6, 1.3086887312481836e-5, 2.1105088119132385e-7] km/s
+ V∞_out: [-9.269684760526803e-7, 4.7152400991820164e-6, 1.2307808735298357e-5] km/s
+ time of flight: 1.85218019726765e8 seconds
+ arrival date: 2030-03-28T23:09:16.783
+ thrust profile: [0.25226659505512866 -0.005876178475925868 -0.08674693133733195; 0.04646023416603918 0.02335956446870083 -0.05595769801348164; 0.10060354240896127 0.0837758745738173 -0.20814615269901335; 0.029157285638532416 0.03192180934796044 -0.09420000070637014; 0.024056776509271217 0.03008105688870556 -0.10280138486634006; 0.01599680765943204 0.022163499985065317 -0.08542805377870234; 0.009941486220635001 0.016639788697091398 -0.06891249995000281; 0.007604353621153168 0.015110517545894556 -0.07498418406789431; 0.0024182880568154965 0.003850007657415338 -0.021958761202249998; 0.0013602026513690772 0.0038027169719884687 -0.01993783697677025; -0.0017287854928441718 0.00034347607901229226 -0.002956712476634615; -0.0026300954857646744 0.0006919656771183252 0.00018298986481095824; 0.0007435395363626725 -0.0006764054883483452 0.0015016706534359036; -0.002291518921482715 0.0004607472679712892 0.003697848812200797; 0.0010599058009489442 -0.003143407389256403 0.0002654245031861106; -0.0015538262010443967 0.004390114868688245 0.0021348953607256294; -0.0001511325040951718 0.004572117400132347 0.008027460531016474; 0.0004818408379697429 -0.002616767940643864 0.0038364604863646247; 0.0003356653257271185 0.004300214451903853 0.00528636280652809; 0.009725829407433714 0.004963305597674814 -0.003969976872133373] %
+
+Mass Used: 83.8273001311145 kg
+Launch C3: 97.54108078529568 km²/s²
+||V∞_in||: 1.3167666828469967e-5 km/s
diff --git a/archive/ES_0.5595640685731474 b/archive/ES_0.5595640685731474
new file mode 100644
index 0000000..ea5ab59
--- /dev/null
+++ b/archive/ES_0.5595640685731474
@@ -0,0 +1,22 @@
+archive/ES_0.5595640685731474---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T19:21:24.674
+Launch V∞: [7.730445844585785, -5.963372955560695, 0.08590745791317539] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3065466108609976e-6, -1.2438676269372377e-5, 0.0002465803708557319] km/s
+ V∞_out: [1.0330657638131907e-5, -0.000246421837987675, 2.7656838298817212e-6] km/s
+ time of flight: 1.8335372949401963e8 seconds
+ arrival date: 2030-03-04T22:56:53.674
+ thrust profile: [0.2832089093892908 0.005759172540837859 -0.07669106213359515; 0.2132220148505066 0.13409616528009638 -0.17891327831032494; 0.0671579993347187 0.07381237167427385 -0.11646112105939044; 0.041188585699292984 0.06485089874640572 -0.11130145920379951; 0.022235349818189944 0.043596937610677254 -0.08502570332298365; 0.01112223425279468 0.023910554314557363 -0.05267643465627843; 0.012673650226514847 0.0446080572624104 -0.09587609332645423; 0.008743971338159883 0.03633945093867687 -0.08563635609216096; 0.0020642409588176973 0.01821713219581626 -0.045318966254382; 0.0005223565913772585 0.0019007578809976159 -0.00550637777031983; 6.118652751976411e-6 -8.163157133422676e-5 0.00032320178610259834; 8.617025717168867e-5 0.00012958001589958646 -0.0011377083069110793; 0.0014128584073697173 -0.0013831986800624972 -0.0008213910399756363; 0.0014137774568775039 0.0015427240599323476 0.001867246400529313; -0.00028275146999633106 0.002384208885411652 -0.0019577909442191777; 0.0004613559378058359 -1.354252027422763e-6 -0.0007986551741249119; -0.00021477868047363837 -0.0009332393470350259 0.0021023709675582264; 0.0005760298280742414 0.0019552668086724057 0.002984274492840726; -0.0007170643550548178 -0.004159911094735328 -0.0021804685814123576; 0.0006562557998844136 -0.0009004354441262722 -0.00035872141650557796] %
+
+Mass Used: 96.73897135068864 kg
+Launch C3: 95.32899005451144 km²/s²
+||V∞_in||: 0.0002468973613118028 km/s
diff --git a/archive/ES_0.5595645530816489 b/archive/ES_0.5595645530816489
new file mode 100644
index 0000000..9b64f77
--- /dev/null
+++ b/archive/ES_0.5595645530816489
@@ -0,0 +1,22 @@
+archive/ES_0.5595645530816489---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T09:23:38.398
+Launch V∞: [7.998569643886006, -5.5196346078612, 0.23451445453491593] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0254232701308298e-5, 8.164742838709994e-5, -0.0015011830367514765] km/s
+ V∞_out: [-6.061625803589008e-5, 0.0015020978583684338, -1.8126029964159567e-5] km/s
+ time of flight: 1.8749577787493202e8 seconds
+ arrival date: 2030-04-20T11:33:15.398
+ thrust profile: [0.4689544436191143 0.007579615837107996 -0.12639493495452486; 0.12090490904830473 0.07605599990729661 -0.12165888253916003; 0.07393794871013971 0.0764022434754641 -0.1371025091600815; 0.037930843303995446 0.05193498477252336 -0.10558389341704155; 0.01652643461657885 0.02756603396685532 -0.061902546055776636; 0.01782322139646831 0.036418551134244956 -0.08826841004055577; 0.008649338089515136 0.019638268895768713 -0.05114084719580754; 0.010445292235839863 0.029632084590893483 -0.08094518924748693; 0.0037018964517368876 0.003014733846381627 -0.009650135776453342; 0.0015034726432250271 0.004846799019006541 -0.012280060174171725; -0.0010267010281730265 0.0030700749472875517 -0.006813916856886908; -0.0001643178579812584 0.001395251472591742 -0.005853455731097742; 0.0005159501959381527 0.0023234584843275195 -0.0075865585889403645; 0.00020749050918727907 0.0005387935405750743 -0.003573251935953866; 0.0006791380596095867 0.002918909601518911 -0.007946200678142772; 0.0003337865161927063 0.00293201565754409 -0.006622582945583006; -0.00016981432384667513 0.00023581454588072028 0.0009949498228064822; 0.0009038406619059297 0.00015426621457264754 -0.0047912044497413955; -0.0012963717555003543 -0.0074726908514181935 0.0015298171597394813; 6.491677917157181e-5 0.0006034695785850275 -0.002306653281867523] %
+
+Mass Used: 101.58418103487611 kg
+Launch C3: 94.49847958177958 km²/s²
+||V∞_in||: 0.0015034367168859832 km/s
diff --git a/archive/ES_0.5595798018332236 b/archive/ES_0.5595798018332236
new file mode 100644
index 0000000..daaff1a
--- /dev/null
+++ b/archive/ES_0.5595798018332236
@@ -0,0 +1,22 @@
+archive/ES_0.5595798018332236---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:21:04.238
+Launch V∞: [7.57081801406411, -6.138721812413219, -0.03330767210463297] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005928589870120388, -0.00040635622820826036, -0.023335104110309837] km/s
+ V∞_out: [0.007765864725072535, 0.020417154528450856, -0.008200091719622188] km/s
+ time of flight: 1.7081990111798406e8 seconds
+ arrival date: 2029-10-08T13:19:25.238
+ thrust profile: [0.48327109713252936 -0.06659481921011674 -0.1738286543421779; 0.036058729142546014 0.013552506793236475 -0.042975722298424855; 0.08223080393732368 0.053384524374638496 -0.1656115902340077; 0.04884230008267179 0.04088707661811254 -0.1420433418189934; 0.057003374572133544 0.05616784678711674 -0.21053625472714158; 0.021599380405198588 0.024007671222566404 -0.10090006445722571; 0.016416286569206042 0.02012872896347688 -0.09096033100110493; 0.010667404565541739 0.014169502412325388 -0.06858516662565504; 0.002784102712746129 0.00395012514217933 -0.020311411891643795; 0.0006322006470609569 0.000948123866681847 -0.0053241506538364534; 9.8803617696145e-5 9.294120326358714e-5 -0.0005648163938641304; -7.66343667851635e-5 0.00026566156907189816 -0.0007990085191387817; 3.3087157008560426e-5 3.7830698916785485e-5 -0.00018377621587495005; -2.3579514209246552e-5 0.00023578847908884259 -0.00037975462769748454; -1.1740355711053866e-5 2.790550068857301e-5 -0.00020620460869849185; 7.527415135785732e-5 0.00022854567168850918 -0.00014156218017639488; 2.6815443145260057e-5 6.747543268896606e-5 -0.00029726900416236985; 0.00022277754805017342 -0.000258600862324162 0.0002852557408214764; 3.294257028154838e-5 -2.9967063709206848e-5 -5.046968748072223e-5; 0.0002961268350465164 -0.0001266871725403711 -0.0003770199044793631] %
+
+Mass Used: 98.66301709453137 kg
+Launch C3: 95.0023002932965 km²/s²
+||V∞_in||: 0.02334617079954834 km/s
diff --git a/archive/ES_0.5595837465359279 b/archive/ES_0.5595837465359279
new file mode 100644
index 0000000..48bd229
--- /dev/null
+++ b/archive/ES_0.5595837465359279
@@ -0,0 +1,22 @@
+archive/ES_0.5595837465359279---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T10:31:47.053
+Launch V∞: [7.689941681256413, -5.632927350267179, 0.2780728312427783] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.581240678217267e-10, -1.0890647384052888e-9, 1.493857991568509e-9] km/s
+ V∞_out: [5.989714977815994e-10, -2.0327823087558007e-9, 4.672435860441751e-10] km/s
+ time of flight: 1.8749577787478885e8 seconds
+ arrival date: 2030-04-19T12:41:24.053
+ thrust profile: [0.6938266425450348 0.03304985057102924 -0.15653803312583428; 0.18157455915785536 0.13034111186540143 -0.15896343073973815; 0.08185162930188516 0.09949487085572545 -0.14053687681356908; 0.04098982041923515 0.06911151768719018 -0.11239111652789538; 0.02133021782799126 0.04542607229738138 -0.08306445298960115; 0.017862363239655107 0.04905133706866673 -0.09293401719811989; 0.007099093025442955 0.0191734069428069 -0.04178997942140551; 0.002596592034858303 0.01092143475216756 -0.025769346088103013; 0.002146998504251895 0.010169684161667344 -0.024204297276680938; 0.0004348803062678063 0.0023655317025216673 -0.006514574253970585; 7.825686245472076e-5 -0.0005335628808149275 -0.0006795152637522164; -0.0005466730228793557 0.0004034757347289394 8.137790552885534e-5; -0.0014311550887454226 0.0011344496157121885 -0.0008534713236185901; -0.0003840233662709635 0.0007319041442851089 0.0008114176762784973; -0.00020971111780183828 1.9422552265676175e-5 -0.00035616801483567264; -9.90034846350408e-5 0.001087186604072402 0.0003049829071044602; 0.0003821155113934181 -0.0011626613738186663 0.00030718010870390655; 0.00022566028511109058 0.0015975184822521653 0.0020344178423724758; -2.538315800662792e-5 -0.0002674568393938773 0.0014098809676282129; 0.00015396476996756012 -0.0003097342314869489 0.0004126394760824916] %
+
+Mass Used: 122.35038207698517 kg
+Launch C3: 90.94239809398812 km²/s²
+||V∞_in||: 1.998105554174114e-9 km/s
diff --git a/archive/ES_0.559583896723922 b/archive/ES_0.559583896723922
new file mode 100644
index 0000000..70fb6b2
--- /dev/null
+++ b/archive/ES_0.559583896723922
@@ -0,0 +1,22 @@
+archive/ES_0.559583896723922---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T20:41:47.511
+Launch V∞: [7.9299027210239785, -5.82887827418213, 0.24127445819634663] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2803081726774161e-6, -8.162876289968025e-5, -1.507895249455176e-6] km/s
+ V∞_out: [-7.895135854912326e-5, 1.1762184794307776e-5, -1.7100366052675312e-5] km/s
+ time of flight: 1.8143833758084804e8 seconds
+ arrival date: 2030-02-09T20:14:04.511
+ thrust profile: [0.2739375078495971 -0.002974642937519898 -0.08076457487898257; 0.07831793857073369 0.04637786566979289 -0.0786596019847; 0.05566333118847766 0.054409549688199575 -0.09920778646491654; 0.044224398350015966 0.05806997354416346 -0.11577601208627876; 0.020347137441684728 0.03334539540651693 -0.07510254303745699; 0.014217601716740393 0.028024601387056577 -0.06835741305488105; 0.011856632549537043 0.027572461783381807 -0.07157156691357279; 0.02330487048768056 0.07532944555509437 -0.18273426340159413; 0.005927868105340211 0.019469642996952644 -0.055628058519300604; 0.0008282376258038316 0.0033320454886708014 -0.012020780381995099; 0.00013677991618896623 0.004144150376923262 -0.014749704570889255; 0.0002995137839820376 -0.0008699397256238151 -0.0015996081275352434; -0.001082381751564024 -1.2034319537700933e-5 0.0005018650421155486; 0.0008907299603673196 -0.0008286586619004142 0.0009083827799599706; 0.0007907123104449699 0.0006677644551017626 0.00036959319147559914; 0.0003108309864458936 0.00038407626392094956 0.0004205644577983973; 0.0023276628798811743 -0.0021271329646933286 0.0004937573676266195; 0.0013596224777879004 0.0003082995480954482 0.002378562016565066; 0.00025820997067449534 -0.002162223225191256 0.0022078831042608646; 0.0030262233596757056 0.0010617819432624344 0.000623374163584438] %
+
+Mass Used: 87.49642346941118 kg
+Launch C3: 96.91739246431389 km²/s²
+||V∞_in||: 8.165272726389835e-5 km/s
diff --git a/archive/ES_0.5595839106211138 b/archive/ES_0.5595839106211138
new file mode 100644
index 0000000..48cd584
--- /dev/null
+++ b/archive/ES_0.5595839106211138
@@ -0,0 +1,22 @@
+archive/ES_0.5595839106211138---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:25:55.100
+Launch V∞: [7.993660523952878, -5.7614257430302835, 0.15311100582805356] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.468321381538498e-10, 1.2203914937102878e-9, -1.6651783969428514e-9] km/s
+ V∞_out: [1.0790536009663101e-9, 2.142347846680039e-9, 5.791045754355504e-11] km/s
+ time of flight: 1.8572888074847904e8 seconds
+ arrival date: 2030-04-03T10:47:15.100
+ thrust profile: [0.3198370527054708 -0.007077513921379055 -0.10423376300063203; 0.02831170392970004 0.014295631045314741 -0.03350131946959531; 0.04787554360854214 0.03966362911633808 -0.09964502512453972; 0.04526917169014249 0.04833337051867903 -0.13697695778761584; 0.03025982995376 0.03844680357118768 -0.12181308071816348; 0.011206624972554325 0.01591517979741145 -0.057637243934391354; 0.010039102076746763 0.01657499493407944 -0.06335867464453654; 0.006952118073643904 0.01196033485820696 -0.048432350692708875; 0.008657812895689355 0.016988121225776313 -0.07306755935743653; 0.0036931243716395836 0.007258202694560126 -0.034742557210909096; 0.0014215741119003589 0.0041698088569482724 -0.02012140032947434; 0.000424511927422895 0.0013634664538784435 -0.00696420690543257; 0.00027292402998479613 0.0018875687203230135 -0.006414132967126912; 0.0006108266465031507 0.0045579681286689756 -0.010597584725527279; -0.00043195964600363035 -0.001453136679257623 -0.00077905351156194; -0.0028022011052686083 0.01111237107844057 -0.004659571311697662; 0.00355785431136814 -0.004253864765086794 -0.008464716954356206; -0.006654991336987447 0.0006846852030613045 0.0019686182371408912; -0.0009803174123423062 -0.0024417369258488697 -0.0019463609976719679; 0.008976409702252398 -0.00693152155112802 0.009671660202835193] %
+
+Mass Used: 86.33743988019751 kg
+Launch C3: 97.11607814476034 km²/s²
+||V∞_in||: 2.23143432835829e-9 km/s
diff --git a/archive/ES_0.5596046585337457 b/archive/ES_0.5596046585337457
new file mode 100644
index 0000000..916faef
--- /dev/null
+++ b/archive/ES_0.5596046585337457
@@ -0,0 +1,22 @@
+archive/ES_0.5596046585337457---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T11:05:45.951
+Launch V∞: [7.786957183486338, -5.995522740880131, 0.17549715792302384] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.581632362906358e-10, -1.1954524886337302e-9, -1.3228328764294322e-9] km/s
+ V∞_out: [6.494690853048693e-10, -6.075609851362393e-10, 2.2530952737179865e-10] km/s
+ time of flight: 1.830335288477833e8 seconds
+ arrival date: 2030-03-01T21:44:33.951
+ thrust profile: [0.19756069833291423 0.005980886350835358 -0.05753270943031741; 0.18635082745837991 0.12104947408210323 -0.1632735977336407; 0.06907653888777472 0.07271133466522679 -0.11858103015650508; 0.03839824639654239 0.05794952729158759 -0.10671906891393505; 0.020643566614322525 0.03676496586558217 -0.07652194413583742; 0.01972720295641814 0.04417860645366872 -0.09647850357323069; 0.015613216893669742 0.040671336787102365 -0.09464289222435514; 0.006409825010537805 0.019438922521066052 -0.04961174710336046; 0.004321309352220335 0.016622122684327535 -0.043856158042781854; 0.0026058726842614127 0.01077093187332535 -0.027321510075969686; 0.0005884885360002898 0.0016050974780974971 -0.004710071954418568; 0.00028008879379938544 -3.6734495339947625e-5 -0.0016350509605019196; -0.0020251323216687947 -0.0011582740517469454 0.0001322027905482743; -0.00045879726014343787 0.0005840239250252734 -0.002204974039586427; 0.002977035912009175 -0.001319647336066299 -0.001431344406342936; -0.0011580513869981802 0.00032801501841858927 -0.0004930048975362982; -0.0009333500033916854 0.0001098599687183762 0.002369161938131539; 0.003905376673944861 0.003789187569935709 0.001203303596400126; -0.0006444419742411306 0.0005259834954672901 0.0026397033421076623; -0.0013889262604527073 0.0036514248629168095 0.001090190500073146] %
+
+Mass Used: 89.29163448595727 kg
+Launch C3: 96.61379436629933 km²/s²
+||V∞_in||: 1.978746474832984e-9 km/s
diff --git a/archive/ES_0.5596058056317821 b/archive/ES_0.5596058056317821
new file mode 100644
index 0000000..6fdf613
--- /dev/null
+++ b/archive/ES_0.5596058056317821
@@ -0,0 +1,22 @@
+archive/ES_0.5596058056317821---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T00:36:49.732
+Launch V∞: [7.851278972378895, -5.663107501156068, 0.08610387317629462] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.951043251188485e-5, -1.2899596598835194e-5, -1.0499244093934986e-5] km/s
+ V∞_out: [-2.2985573642937585e-6, 1.560411620579324e-5, -1.9853202152333723e-5] km/s
+ time of flight: 1.8571741902187568e8 seconds
+ arrival date: 2030-03-30T12:47:08.732
+ thrust profile: [0.5145454802018247 0.011799078698723027 -0.12348807356909312; 0.11269597035336336 0.07878602897829289 -0.10226119934157106; 0.05798264522628116 0.06872169007341514 -0.0999702199951737; 0.04503889053533251 0.07333639523631125 -0.1189096368214999; 0.020332013221603162 0.039257513627009 -0.07701001757936494; 0.0157453860718481 0.03730936047463394 -0.072209581357088; 0.012337811867730501 0.032503594457764774 -0.06996990928171362; 0.010951428625724485 0.04478879056486241 -0.09629413002851159; 0.0036597735961975573 0.016532546576224865 -0.03660707353535636; 0.0023717328001812052 0.014583572992049721 -0.03534424386454307; 1.3548128794040482e-5 0.00013314135727864176 -0.00025146646210568693; 0.00046258780211192254 0.003789055808153613 -0.011124261642289992; -0.0002274958516515312 -0.00019596510961372758 0.0005516813629494292; 0.0007076514644702409 0.0005490199770593023 -0.0006296989459337717; -0.0004994973439972194 -0.001090666134372715 5.829736178976087e-5; 0.00039385902599687987 -0.0004092529468057765 -0.00014139140241422015; 0.0011315636889967875 0.00036214293526539923 5.4296716860844675e-5; -0.0003673013547971243 0.0004476876777865249 -0.00019798400200579067; 0.00021846640271728541 -0.0008200975932103403 -0.0004970171060486182; -0.00010114569172289909 9.121423799614783e-5 -0.0002768740077913625] %
+
+Mass Used: 106.16887853606613 kg
+Launch C3: 93.72078194874508 km²/s²
+||V∞_in||: 2.563768116966748e-5 km/s
diff --git a/archive/ES_0.5596071617682398 b/archive/ES_0.5596071617682398
new file mode 100644
index 0000000..20e269c
--- /dev/null
+++ b/archive/ES_0.5596071617682398
@@ -0,0 +1,22 @@
+archive/ES_0.5596071617682398---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T22:52:53.829
+Launch V∞: [8.039935846098508, -5.745505153677705, 0.09437637585829514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.6864742540781453e-6, 0.0002545965890849049, 4.599622436541765e-6] km/s
+ V∞_out: [0.00024589580221122127, -3.658549569269029e-5, 5.520592415763193e-5] km/s
+ time of flight: 1.8749577787493154e8 seconds
+ arrival date: 2030-04-25T01:02:30.829
+ thrust profile: [0.2789258727063349 -0.005402200711282249 -0.10185252796926636; 0.052278618412432386 0.027214066250778973 -0.06757127097011027; 0.03719884096292918 0.030451097026271964 -0.08601895069975839; 0.03423887838989183 0.03587135569314986 -0.114963293634596; 0.020635500693364207 0.025594461174539455 -0.09330888462130106; 0.016100592248540265 0.022835402051044243 -0.09174758290122093; 0.016919710110364118 0.0274617642445569 -0.11921541048158096; 0.005127672999164007 0.008392998629469656 -0.041112033087461634; 0.00397092324605801 0.006677924282287231 -0.035593058639225024; 0.0034955587103662243 0.005416304038267746 -0.03147495109983511; 0.0013387152146240781 0.0008288913898122602 -0.0080277620700813; 0.0056779091804618 0.0009774155923177098 -0.0015878807794607146; 0.00018239509763799905 -0.0018668710014606942 -0.0031485826862321046; -0.001159950500890379 -0.0028090912056719206 0.0019832457114950792; -0.008734766215637377 0.005268928928565116 -0.004584244962232269; -0.002303196253794587 0.01007424519937534 -0.0039109412973131405; -0.0010059174861849463 0.003369492341962064 0.004102657372107656; -0.001620880258492838 -0.000935880886726827 -0.0015688642465817412; 0.004863496406263457 -0.0072610096777208834 0.0006593144279022579; 0.007326775925668085 -0.011081786527572537 0.005559762514741258] %
+
+Mass Used: 83.18991084256413 kg
+Launch C3: 97.66030478063695 km²/s²
+||V∞_in||: 0.00025466481852162584 km/s
diff --git a/archive/ES_0.559613536414808 b/archive/ES_0.559613536414808
new file mode 100644
index 0000000..7b157df
--- /dev/null
+++ b/archive/ES_0.559613536414808
@@ -0,0 +1,22 @@
+archive/ES_0.559613536414808---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T17:11:04.661
+Launch V∞: [7.879212222925542, -5.91097169559082, 0.12245999937741818] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4434036437552566e-7, -1.0348132115926984e-6, 2.2452362424119234e-5] km/s
+ V∞_out: [8.624199862241233e-7, -2.2496383019375096e-5, 2.285128285299213e-7] km/s
+ time of flight: 1.8544157269757456e8 seconds
+ arrival date: 2030-03-30T00:43:56.661
+ thrust profile: [0.18620873704729546 0.011095442257547373 -0.049520907596103794; 0.14222111571241158 0.10275553466642083 -0.12487641499418597; 0.044800548263775684 0.0544925057947765 -0.07711351551612716; 0.05490737643853521 0.091569698590194 -0.1413112531500165; 0.019070073100218465 0.04189394002591274 -0.07324353174933605; 0.014618619958609812 0.04381434894653689 -0.08149844068852223; 0.010571838941446702 0.03957441624916268 -0.07640352880947025; 0.010606634041128672 0.037808036787266096 -0.07207119350176518; 0.003799629528590788 0.01772384074866935 -0.040645061615019254; 0.0027594445214276847 0.022627292580209544 -0.05157874176616605; -0.0001315064752250171 0.005272210511374139 -0.013633288917364352; -0.0002753411778693627 0.00019822937634941373 -0.0021004505003194107; 0.0010990424270040614 -0.0007663316597578574 -0.0016535127924958244; -0.0004597775041492077 0.0022392047591002985 -0.001509803442177523; -0.0006655347778555089 -0.00024052103847531982 -7.089457793763021e-5; 0.00014610770939549106 0.002334143917908106 -0.0007868787409611065; 0.0018609507609066262 0.0013856479535576554 0.0027680604732123444; -7.954993575931822e-5 0.0002113332269876358 -0.0014778346339130175; -0.0016681877997668597 -0.0007952167771587701 0.003997681692433625; 5.388707624560602e-5 -0.001835572358880847 -0.00022132558805464716] %
+
+Mass Used: 86.83581195064426 kg
+Launch C3: 97.03656809142258 km²/s²
+||V∞_in||: 2.2476660137744578e-5 km/s
diff --git a/archive/ES_0.5596264673122331 b/archive/ES_0.5596264673122331
new file mode 100644
index 0000000..42c1a8d
--- /dev/null
+++ b/archive/ES_0.5596264673122331
@@ -0,0 +1,22 @@
+archive/ES_0.5596264673122331---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T10:08:24.058
+Launch V∞: [7.787198609517974, -5.8945650176115425, -0.46005875851022493] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01914261023247605, -0.11391497686045343, -0.15104269918994168] km/s
+ V∞_out: [0.07134603610832803, -0.057962117269911975, 0.16641786812238854] km/s
+ time of flight: 1.8749577779197675e8 seconds
+ arrival date: 2030-04-24T12:18:01.058
+ thrust profile: [0.3606105377214992 0.009106777838823039 -0.11489745873223367; 0.14497690324336482 0.09259462004506294 -0.15537617264259165; 0.07104238325324617 0.0749947415986732 -0.14333431522529097; 0.03641654263818623 0.05203195565967241 -0.11504776381031709; 0.01500970946953203 0.026573667871599014 -0.06756958291632055; 0.011609789408707464 0.026417882459100324 -0.07311415758314892; 0.008409859615147475 0.02063357584209022 -0.06098256214306126; 0.002768614108260679 0.009856850600062259 -0.030264639847580262; 0.00171879641772574 0.005359842010816854 -0.01970999976491692; 0.0037378535451541278 0.015933610574168106 -0.05451192485216922; 2.4954726826945952e-5 0.002037309319731311 -0.011522172967595334; -1.1957624427588677e-5 0.0007984204867557225 -0.0031274499135258817; 0.00031966791446824303 2.2320621473155967e-5 -0.0004738131688097921; 0.0010888082558949777 0.0010843803314958384 0.000806372171256928; -0.00043617788777140163 -0.0008425451892482732 0.0007154404054414963; 0.0004975894108170688 0.0007024553882737126 -0.000844523422450525; -0.0009240460429052539 -7.406409637264794e-5 0.00020768445600294024; -0.0010323444528466926 -0.000930834980627626 -0.0019678608562766044; 0.00044994894909448614 0.0031601784226650688 -0.0004981691067363809; -5.358725089202416e-5 -0.00015425775001673978 0.003959858057713308] %
+
+Mass Used: 95.24246940971125 kg
+Launch C3: 95.5980129922104 km²/s²
+||V∞_in||: 0.19014983160185375 km/s
diff --git a/archive/ES_0.5596265460008246 b/archive/ES_0.5596265460008246
new file mode 100644
index 0000000..1273bc9
--- /dev/null
+++ b/archive/ES_0.5596265460008246
@@ -0,0 +1,22 @@
+archive/ES_0.5596265460008246---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:06:22.745
+Launch V∞: [8.149252355786823, -5.550323440565346, 0.37563256249293514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.34184920633258e-5, -2.5498186871311447e-5, -2.093581179246648e-5] km/s
+ V∞_out: [-4.9796183412862405e-6, 2.4317142227269317e-5, -3.985523480759593e-5] km/s
+ time of flight: 1.8749577787442914e8 seconds
+ arrival date: 2030-04-22T10:15:59.745
+ thrust profile: [0.2761701916856174 -0.004354597462266766 -0.08830514539648121; 0.06574262702274997 0.035913437809265036 -0.07247715075877693; 0.05197702344130953 0.04543471575839025 -0.10427917017603741; 0.055229678963602376 0.0621947138040691 -0.16363467178848437; 0.024951035523938948 0.033863542638018884 -0.09839587238555841; 0.01979157444387606 0.031164190390549507 -0.09899817789768318; 0.0066633688746532945 0.012033440688341928 -0.039619192189759324; 0.0019175738461932668 0.003986891382020537 -0.014493595747480454; 0.001969163981968995 0.007043634811438432 -0.02431621352146759; 0.00894623488034175 0.011980293706089148 -0.030357075678054617; 0.0017272106816465323 0.0034148187223219948 -0.016457685880751544; -0.00048726838038099657 0.003420232752731962 -0.01698385103279878; 1.2041725636465007e-5 -0.0029944449332687194 0.0002838310467086205; -0.0031717893142701728 0.0024753759278608707 -0.0015208679592937958; -0.00023714012964878915 0.002639715908843968 -0.010917057386694712; 0.0018121329108589364 0.008548159045492769 -0.023945988721649984; -0.0012624292193579036 0.0012570618538947993 -0.0006699079885253991; 0.007587559274767135 0.00535410287346781 0.00022240993839535818; -0.00013062907498170287 0.0006521578941112711 -0.003877935196818458; 0.005124737043624895 -0.0035489449178819684 0.011420983658691956] %
+
+Mass Used: 84.97886322901331 kg
+Launch C3: 97.35750407519122 km²/s²
+||V∞_in||: 4.696021040115203e-5 km/s
diff --git a/archive/ES_0.5596266683690578 b/archive/ES_0.5596266683690578
new file mode 100644
index 0000000..3a70d62
--- /dev/null
+++ b/archive/ES_0.5596266683690578
@@ -0,0 +1,22 @@
+archive/ES_0.5596266683690578---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:38:02.844
+Launch V∞: [7.834766314849169, -5.941143825524813, -0.02378880119773723] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4771665813386887e-9, -1.4933917992683311e-9, -1.5100683831643994e-9] km/s
+ V∞_out: [1.3778566389921143e-10, -1.2529240264597834e-10, 4.6845062480080135e-11] km/s
+ time of flight: 1.7842965698093492e8 seconds
+ arrival date: 2030-01-06T04:25:38.844
+ thrust profile: [0.2777693184683224 -0.020652550763749826 -0.09536096717616234; 0.08712702344152222 0.041195127336214464 -0.09863170376398142; 0.08457290194901113 0.06542234569438445 -0.16712457293767777; 0.05924026837930077 0.05981324315236719 -0.1710699325912923; 0.029080691287236348 0.03582596880216814 -0.113011854127048; 0.022739803981976312 0.031230958444739984 -0.10798229800040916; 0.00886310898685958 0.013927499348933312 -0.05297324421443856; 0.0048888100060527195 0.009012096711007509 -0.03660197674803309; 0.0009850946419272912 0.0018924170572606565 -0.008356070601731384; -0.0012149636787927342 0.0007621851489772928 -0.01256791436965033; -0.0007869921087617371 0.0006903075381559968 -0.0027095073450466812; 0.0020611697186525163 0.005309554959455935 -0.023859783691816617; 0.002989679239823801 0.0036803517745242808 -0.021501820934011113; -0.0005485570358689912 0.0010248621967240315 -0.00359284680436233; -0.0005635483890553403 -0.0012404089657858026 -0.001237280744440578; -0.0006505940110465569 0.002673273727235667 0.0030977604755068923; -0.0008080509241784307 -0.0011598391719756023 0.0010327465555030084; 0.0007424566525494129 0.0025232878646320525 -0.010452581091399644; -0.000856611189680996 -0.0049317670426261605 -0.0002996873587358473; -0.00044742852060880133 0.0009490799867259662 0.0016147488231193583] %
+
+Mass Used: 88.9234185168134 kg
+Launch C3: 96.68131907092926 km²/s²
+||V∞_in||: 2.58699568940083e-9 km/s
diff --git a/archive/ES_0.5596268984185068 b/archive/ES_0.5596268984185068
new file mode 100644
index 0000000..aa330db
--- /dev/null
+++ b/archive/ES_0.5596268984185068
@@ -0,0 +1,22 @@
+archive/ES_0.5596268984185068---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T05:47:45.433
+Launch V∞: [7.7703496367713365, -5.652765542540899, 0.28142117466297856] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4001316774072683e-5, 1.3101050124718228e-5, -8.960573613179004e-6] km/s
+ V∞_out: [2.7792653929056765e-6, 2.0907601130954264e-5, -9.946942258673858e-7] km/s
+ time of flight: 1.8414879108296075e8 seconds
+ arrival date: 2030-03-11T14:14:16.433
+ thrust profile: [0.6093932926584144 -0.022055630637477446 -0.15095868876942264; 0.13214791285973151 0.07465456367980801 -0.1271923256652865; 0.1161377439083467 0.11091889937732641 -0.19968459323046495; 0.05572684851613322 0.07266852398964128 -0.14374840567904976; 0.02251422595004365 0.034577902754504064 -0.08214524609654081; 0.011720465930384368 0.022080623070292165 -0.057082240853945684; 0.0070193146150239055 0.015387354397244223 -0.04284350105176595; 0.001986450687023567 0.004954237682871785 -0.015551940847876502; 0.004095131275416628 0.011476811276248715 -0.035931534075851694; 0.0006166533468201419 0.0008699168604951321 -0.005601918176443775; 0.0021087201110491123 9.406642729241355e-5 -0.003352562994850872; -0.0023581025062315913 0.0024456570553317 -0.004346431590773452; 0.001072422355538735 0.002681913723901366 -0.004431878604205074; -0.001451662663139696 0.0037737750202145397 -0.002215197319304802; 0.0032016118595014245 0.00025403526097600307 -0.000914665053063208; -0.0032600115061546574 0.0020530915757766286 -0.0007314729961232602; -0.004200911417247594 0.00021744913567054634 -0.00190982173776037; -0.0012706951217279318 3.4059259359794784e-5 -0.0011932529325484797; -0.0015386956506191 -0.0006345942314421602 -0.004359462943131293; 0.00030259472255801624 4.981261892677419e-5 -0.0013960793000618046] %
+
+Mass Used: 113.83219195566471 kg
+Launch C3: 92.41128963415883 km²/s²
+||V∞_in||: 2.1165213565081464e-5 km/s
diff --git a/archive/ES_0.559629242204508 b/archive/ES_0.559629242204508
new file mode 100644
index 0000000..51e053a
--- /dev/null
+++ b/archive/ES_0.559629242204508
@@ -0,0 +1,22 @@
+archive/ES_0.559629242204508---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T05:37:31.709
+Launch V∞: [7.614699637182138, -5.867694432809597, 0.09678679250082847] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.023728231534818e-10, 1.7967485287865218e-9, -1.8086723542417442e-9] km/s
+ V∞_out: [1.2389923994625795e-9, 2.5332704007426237e-9, 6.62105989870759e-11] km/s
+ time of flight: 1.801397140006561e8 seconds
+ arrival date: 2030-01-24T04:26:05.709
+ thrust profile: [0.5896256005945677 -0.017969775172517424 -0.16232635062736683; 0.15369202081221317 0.08686278854848106 -0.14830886295405726; 0.07692438235746724 0.0724928874997124 -0.13611353826000616; 0.07089617401173959 0.09027344277359875 -0.18284991653556815; 0.02906824105068697 0.04540082300704545 -0.1048297919663724; 0.01858456357275598 0.0344948391891469 -0.08649850883305112; 0.009238251011557666 0.019616176561576614 -0.05280355369884151; 0.0051560667480190095 0.012453742006322316 -0.03530584666169642; 0.0004666726252538328 0.0016130645177351317 -0.004309254502928234; -0.0004216851512356636 0.0029247259935331845 -0.0016793818619856504; 0.001209046342869728 0.0014532680617904978 -0.00752450289035532; -0.00031330640246590615 0.0011437835527487953 -0.004709172337021386; -0.0023136135169375014 0.000582491022173354 -0.0007602691871707525; -0.0011891748394595556 -0.001428204958248781 -0.002679610062101362; 0.0018218697029396083 0.002343051002561 -0.0040942450509561515; 0.000954309077022646 0.00013128785645389598 -0.0019656283081671607; 0.0005364701343879476 0.0005173284487254523 -0.003179810475821105; 0.001224557032846636 -0.004343963527791817 -0.00017298266724134607; 6.0872129554027766e-5 -3.0265590153866553e-6 -1.693924436687623e-5; -0.002663129618409446 0.0018665728858136264 0.005305614691188887] %
+
+Mass Used: 113.76745471217282 kg
+Launch C3: 92.42285620452913 km²/s²
+||V∞_in||: 2.6444145937049084e-9 km/s
diff --git a/archive/ES_0.5596322486099483 b/archive/ES_0.5596322486099483
new file mode 100644
index 0000000..ae78099
--- /dev/null
+++ b/archive/ES_0.5596322486099483
@@ -0,0 +1,22 @@
+archive/ES_0.5596322486099483---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T02:41:29.580
+Launch V∞: [8.025154703949166, -5.883671004882501, 0.21657321369510946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.400227544820904e-7, -1.1028448617171174e-6, -3.239391762318676e-6] km/s
+ V∞_out: [-3.086084062734637e-6, -4.3242092729436743e-7, 1.4192699798234924e-6] km/s
+ time of flight: 1.8250280203686887e8 seconds
+ arrival date: 2030-02-25T09:54:51.580
+ thrust profile: [0.1515874289278483 -0.011907117061099832 -0.057230490608955076; 0.06584179254040708 0.027231028674008097 -0.08483475064207431; 0.03703156400340408 0.023513790421956945 -0.08176939536353917; 0.03077111608863818 0.02399127723354494 -0.09727090406160822; 0.02177688189846801 0.019395729402066655 -0.08837904077346194; 0.03131850037766497 0.030727831918124872 -0.15930931679774066; 0.01937899064540146 0.020662556310211536 -0.11740504578469922; 0.0045341958442245015 0.005735079575105704 -0.02605476028823668; 0.00975958082008779 0.011198943155710033 -0.06814673809196495; 0.00020957638596794202 0.0003908312982174365 -0.001429392989801018; 0.007639570311956006 0.004662740665206025 -0.027729455424914718; 0.0022220264024919245 0.002368955548891453 -0.01742071430268089; 2.2847213808437907e-5 0.00046946214437555293 -0.0028055736855313908; -0.0016661462791229195 -0.0010995691758948515 0.0044427160089068165; 0.0009533756387059697 0.00011074717381194787 -0.0031582610247531213; -0.00016262698650426803 -0.0023863675064505463 -0.0020161954559545455; 0.001541835735202621 -0.002755801938673837 -0.00262611984523634; -0.010345756325464342 0.007652320427818665 0.00043084728881184883; -0.001551457657860445 0.0010154756434123564 0.0012188605482585336; -0.0007798993849617907 -0.0010804790038240007 0.0034995168838565464] %
+
+Mass Used: 75.00997728634047 kg
+Launch C3: 99.06759647290272 km²/s²
+||V∞_in||: 3.430384337281045e-6 km/s
diff --git a/archive/ES_0.5596330814714019 b/archive/ES_0.5596330814714019
new file mode 100644
index 0000000..f77840c
--- /dev/null
+++ b/archive/ES_0.5596330814714019
@@ -0,0 +1,22 @@
+archive/ES_0.5596330814714019---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T21:52:28.484
+Launch V∞: [7.8244972500747245, -5.73523811049797, 0.13929781892889911] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0030896880984332183, 0.0022176817557256704, 0.00015763269406947304] km/s
+ V∞_out: [-0.0026428010022157434, -0.0016821440925883743, 0.0021572162186115377] km/s
+ time of flight: 1.8749577787451375e8 seconds
+ arrival date: 2030-04-22T00:02:05.484
+ thrust profile: [0.4635076561166512 0.017105563444143313 -0.11334029789952864; 0.08330361755599038 0.055939349458353355 -0.08026542581121618; 0.08963771968720498 0.10067056782662691 -0.15243386747569143; 0.05365977891553966 0.0822037916251671 -0.14103568421145501; 0.0233841933917489 0.04452755154111374 -0.08757532523943846; 0.02001930219023084 0.049231073159985754 -0.1029047134124384; 0.010987440497679673 0.03210357555611321 -0.07193358296655435; 0.004388197380119329 0.014933207704132326 -0.03708159151512417; 0.00023767803707912933 0.0024418684135845197 -0.007213760904227149; 0.0019081376804411135 0.0014403232831919298 -0.0020646217506197577; 0.0005562927409808792 0.0015778443231733216 -0.0040182674660772175; -0.003947797621693213 0.0012771279167769288 0.0004492893566478808; -0.0039541989883554035 0.0004832218155384233 -0.002242482745978841; 0.004648283030797631 0.0035973914272581734 -0.000790489545654897; 0.0030112165445306547 0.010490980043455406 -0.0032094817439948103; -0.003509640882587068 -0.0033575734023720944 0.003531057838223231; 0.007126327009056619 0.002838742577702012 0.0024607803126605785; 0.00024341598991602445 0.0038029585062594263 -0.012323496677419495; 0.00014449578337328065 0.001460564324918857 -7.638260421396165e-5; 0.0005033404806864954 0.0016280918347021814 0.002021309131792602] %
+
+Mass Used: 103.78374423308969 kg
+Launch C3: 94.13511728289359 km²/s²
+||V∞_in||: 0.0038064593760498704 km/s
diff --git a/archive/ES_0.5596348073524652 b/archive/ES_0.5596348073524652
new file mode 100644
index 0000000..b0bef2a
--- /dev/null
+++ b/archive/ES_0.5596348073524652
@@ -0,0 +1,22 @@
+archive/ES_0.5596348073524652---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T09:43:23.218
+Launch V∞: [7.943993638403631, -5.959335732677266, 0.28969200924717864] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.692934122114895e-6, -3.2544717860691427e-6, 2.365078657088344e-6] km/s
+ V∞_out: [-7.23800159918308e-7, -5.437371403836811e-6, 2.461187037260707e-7] km/s
+ time of flight: 1.8567901023110062e8 seconds
+ arrival date: 2030-04-05T11:13:33.218
+ thrust profile: [0.23649400239807994 -0.009617979052892111 -0.08822301712674524; 0.038815676624015125 0.01755229387081843 -0.0504997509298611; 0.03614748443708302 0.025300027388801223 -0.08301524500590336; 0.04064217865368856 0.035371554382802955 -0.13330760554106832; 0.030250655927570983 0.03021067446277262 -0.1293664671868639; 0.026427514077926026 0.029240907808299823 -0.13835860023161475; 0.010280178008454563 0.011991795710988637 -0.06437472349640942; 0.005383335026761078 0.006672205267173846 -0.038822438318077176; 0.003926182954648456 0.005441677225613706 -0.03251155187377988; 0.0031606879055871115 0.004137676851797352 -0.028464840107598994; 0.0002621433731226691 0.0003728815420054279 -0.0036224282939496897; 0.0005313026903291231 0.0006301650462093016 -0.0064225451656602485; -0.0009175853374767035 -0.000566031751202299 -0.0005403414031011512; 0.0007230583953900436 -0.00025951299881165973 -0.0039087769468159755; -0.00017829436723705507 -0.0001841900412496134 -0.0003562871796337697; 3.325581985379403e-5 -7.893257403723163e-5 -0.0009165776194182669; -0.00047016731515557927 -0.0008036768810328566 0.002552797396564643; 0.0021524498080343194 -0.008178330787537165 0.0006126503076271071; -0.0013081354152337753 0.00039412547881947306 -5.0098911207268e-5; -0.0009938376592118906 -2.4898600618488732e-5 0.009167567916276282] %
+
+Mass Used: 77.13021579964106 kg
+Launch C3: 98.70463876198313 km²/s²
+||V∞_in||: 5.461038920463339e-6 km/s
diff --git a/archive/ES_0.5596362590977764 b/archive/ES_0.5596362590977764
new file mode 100644
index 0000000..f7676af
--- /dev/null
+++ b/archive/ES_0.5596362590977764
@@ -0,0 +1,22 @@
+archive/ES_0.5596362590977764---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T22:06:47.957
+Launch V∞: [8.106160826226507, -5.6572870623333, 0.13808053260920344] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00010442423051267807, -0.00026864722338386073, -7.22138480645108e-5] km/s
+ V∞_out: [-3.254479861716549e-5, 0.00018150589008000524, -0.0002330077940826744] km/s
+ time of flight: 1.8749577787493291e8 seconds
+ arrival date: 2030-04-23T00:16:24.957
+ thrust profile: [0.21959208184216217 0.00782445492870396 -0.06654822602301513; 0.08088265680002883 0.05227252985087917 -0.08566620289188154; 0.03869527898925498 0.04047319903982088 -0.07642006944128185; 0.028601298619446193 0.03882861349523653 -0.08213413401528846; 0.02668705003485986 0.0477960817415732 -0.10833606273156313; 0.018423890082843238 0.042913196634323164 -0.10322858308755266; 0.013063264660779433 0.0333175027715807 -0.08740831855301039; 0.0075916786623444355 0.021688141567932324 -0.06148638293366478; 0.003805907776408805 0.01872732480784046 -0.05109446952406178; 0.003164875300619329 0.009558122639208088 -0.03896104958216061; 0.001126297765197238 0.0019589444408809704 -0.005671464061020471; -0.0016268546006733544 0.003448182845695576 -0.002622865282432764; -0.0012643586533142757 4.3038011105608204e-5 -0.014114206365545537; -0.0011546609639227633 -0.0027463916745662817 -0.002567782062715532; 0.003969993806642769 0.0002803718609378109 0.0035044512992342958; 0.0019346268508329918 0.004136663897299541 7.342526065163722e-5; -0.010464514977911283 0.006565783947183641 -0.0038599946447207237; -0.00890304331070179 -0.0016738203025952565 0.004204185063622227; -0.0003074220781731327 0.001214367648648934 -0.0016053987575701933; 0.003794900496093094 0.0020144807240844256 0.005869672716110027] %
+
+Mass Used: 82.79509781536399 kg
+Launch C3: 97.73380647977858 km²/s²
+||V∞_in||: 0.00029713732583152045 km/s
diff --git a/archive/ES_0.5596404681599977 b/archive/ES_0.5596404681599977
new file mode 100644
index 0000000..c143a16
--- /dev/null
+++ b/archive/ES_0.5596404681599977
@@ -0,0 +1,22 @@
+archive/ES_0.5596404681599977---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T16:35:23.065
+Launch V∞: [7.817173955011902, -5.7103560868768835, 0.20015329972824067] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009064194901477087, 0.055995463167729395, 0.058173919990296204] km/s
+ V∞_out: [-0.01463899939398504, 0.013014304648962936, -0.07880862334134595] km/s
+ time of flight: 1.843243439060215e8 seconds
+ arrival date: 2030-03-14T01:47:46.065
+ thrust profile: [0.4885565841957628 0.012877246786569436 -0.11691687825051435; 0.15223954252289434 0.09969296045529666 -0.1380265225229728; 0.05233687684574188 0.0560936176003305 -0.0891507754826905; 0.0459976134573573 0.06700948840455022 -0.11672817722757858; 0.02895079184051366 0.05464539628691994 -0.10552770417403778; 0.022258558547551828 0.05140008584072966 -0.10470359776621455; 0.01640580410327059 0.0459932338811511 -0.09918955092284115; 0.005104855938475139 0.01647639342100626 -0.038227066899488536; 0.0016023055616767804 0.006436880629536869 -0.01556671379796614; 0.00046697002298844376 0.0031399597235419814 -0.007667518923567211; -0.00010475949118228552 -0.0001850275744171596 -0.0024061555717667486; 0.00028456103723334007 0.0011249275059155516 -0.005153407305910272; -0.00048298527483306495 0.0010189298400824238 -0.0033736776521212618; 0.00040971157517827957 0.001471472391500075 -0.0038049082091775204; 0.00024736319398485754 0.0002473552721481789 -0.004958248104482189; 0.00015133532236559868 -0.0005593944783743126 -0.00165668166440828; 0.0009429160618565719 0.004813221778020816 -0.0004785316179969581; -0.0008530053924518742 0.00036349542107622025 0.0009759520689000504; -0.0013190990155831784 2.597658689029416e-5 -0.0003832221853582869; 0.0014379018268111195 -0.0029442782703830717 0.0037249174356772637] %
+
+Mass Used: 106.0013325394284 kg
+Launch C3: 93.75643662524038 km²/s²
+||V∞_in||: 0.0812518091590451 km/s
diff --git a/archive/ES_0.5596587982069638 b/archive/ES_0.5596587982069638
new file mode 100644
index 0000000..b44c802
--- /dev/null
+++ b/archive/ES_0.5596587982069638
@@ -0,0 +1,22 @@
+archive/ES_0.5596587982069638---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T13:42:04.076
+Launch V∞: [7.904816739152363, -5.93556198718807, -0.1841055282733766] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1822340086909082e-8, 1.0950437494214206e-7, 3.307890700029365e-7] km/s
+ V∞_out: [3.172706850430088e-7, 3.791879107684927e-8, -1.583456293294442e-7] km/s
+ time of flight: 1.7995197541522858e8 seconds
+ arrival date: 2030-01-25T08:21:39.076
+ thrust profile: [0.24711163430159744 -0.01693288972166776 -0.09279359848687714; 0.039833361027517944 0.018165414197376807 -0.04980325169843405; 0.053003442186927666 0.03960962779384503 -0.11581556612822937; 0.04601254808387393 0.04427421707864791 -0.1449957480604312; 0.03578555128478809 0.04098287592532304 -0.14888394154598378; 0.024075636799000495 0.03108095062885841 -0.12507570433222903; 0.011439320434110112 0.016490680013251297 -0.07244485132522487; 0.007263974921463021 0.01182751965420492 -0.054767536055072626; 0.005061887537735818 0.0090715584380794 -0.045013436668265724; 0.0005070286026279554 0.0014230102807809702 -0.007505367857121219; 0.0005670079670223918 0.00107561665574501 -0.008031482257512768; 0.0023893626801441805 -0.000351499190418965 -0.0017863740074100375; 0.0014900401814809667 0.0020733033165972383 -0.005542258502441476; 0.0024759573093553738 0.002942455377659565 -0.0003315526076936256; 0.00042789755967970514 -0.0014784819661465734 -0.00012955940282178635; 0.006663224028040446 0.00038657925495648514 -0.00030060974877506395; 0.0018846801552919459 -0.001878829762500455 0.003173161682474574; 0.008506111887728755 -0.0023163445855980775 0.00460938611373711; -0.0023267151257704496 -0.004613172341071335 -0.0025939312191822317; 0.0017863972482128295 -0.004267822764871393 -0.00587122987321693] %
+
+Mass Used: 82.72157257301342 kg
+Launch C3: 97.75091862887619 km²/s²
+||V∞_in||: 3.4864363566542753e-7 km/s
diff --git a/archive/ES_0.559660245578363 b/archive/ES_0.559660245578363
new file mode 100644
index 0000000..ff97495
--- /dev/null
+++ b/archive/ES_0.559660245578363
@@ -0,0 +1,22 @@
+archive/ES_0.559660245578363---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T20:36:31.519
+Launch V∞: [7.894280996567412, -5.787709890444664, 0.10910994788095287] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1844836790069356e-9, 7.507357516690568e-9, -1.8770829644835473e-7] km/s
+ V∞_out: [8.986314776864334e-10, -2.7718172337443817e-8, 2.080424950502512e-10] km/s
+ time of flight: 1.8489636947001728e8 seconds
+ arrival date: 2030-03-23T20:42:40.519
+ thrust profile: [0.4039493350828735 -0.0040827914515872655 -0.11173889580123933; 0.054153599311379794 0.029675879852611557 -0.05971341147932687; 0.049437511131093154 0.04499212966516701 -0.09820244911569005; 0.032346878481528785 0.03841049868074166 -0.09278942215865876; 0.016409101076417038 0.022774323719092642 -0.06594025725013573; 0.01391661258578053 0.022383281061387577 -0.06904055769309499; 0.024820711748959508 0.045013966742370425 -0.1345762709206098; 0.014817152679282344 0.03495792756044539 -0.11117700783652264; 0.001883906138606784 0.008737049228118927 -0.03363903457000553; 0.00437079721643127 0.01053588560074123 -0.03523745596099624; -0.002344174351712412 0.00757681755129979 -0.004881947627118735; -0.001136289140203574 0.007660250511697359 -0.0074269746064000094; -0.0028876894430875104 -0.0026709281156225757 -0.004545595023842489; 0.003327362933995593 0.0015493420607172429 -0.0019216022616961753; -0.00029204719108606237 0.002026292870009732 -0.001945756266473338; 0.0015531063620836604 0.003697195851677891 -0.005109161737441781; -0.003650304236277553 -0.0012171988265874997 0.006087899657054875; 0.00226750126461911 0.0007331826228479884 -0.0036497271324962117; 0.0042832907879510815 -0.006531261398123822 -0.01261059732098207; 0.0003316738985002588 -0.0004007033139375023 -0.0015675891183858865] %
+
+Mass Used: 93.93350111967311 kg
+Launch C3: 95.82916320944294 km²/s²
+||V∞_in||: 1.878620982902423e-7 km/s
diff --git a/archive/ES_0.5596636167122055 b/archive/ES_0.5596636167122055
new file mode 100644
index 0000000..de3dc6d
--- /dev/null
+++ b/archive/ES_0.5596636167122055
@@ -0,0 +1,22 @@
+archive/ES_0.5596636167122055---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T20:22:37.175
+Launch V∞: [7.965190460328733, -5.622653511103036, 0.0101282892367901] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.782423658195696e-9, 5.40622209358256e-9, 2.943405525873186e-9] km/s
+ V∞_out: [4.936408393870634e-9, -4.7701421454792045e-9, -2.847349721626374e-9] km/s
+ time of flight: 1.873184671347415e8 seconds
+ arrival date: 2030-04-19T21:17:04.175
+ thrust profile: [0.4471499071901701 0.010543968340600347 -0.12440716012301897; 0.06659668691191227 0.04309259588116524 -0.07177642151525607; 0.06333421049979894 0.06765133805425526 -0.12118119011354384; 0.03277686434289246 0.04758712377190952 -0.09672496661307102; 0.01603843582096584 0.02938921528227259 -0.06679687241883515; 0.012701384333523242 0.028668699884011325 -0.07202106161919423; 0.011076654000790092 0.03063054034988422 -0.08218470102807356; 0.012830988243824708 0.03981178253415083 -0.10655720971283322; 0.005511380989898838 0.02687212836538729 -0.07336976783964312; 2.9818842239592988e-5 0.0010362379061746975 -0.005734712972967346; 0.00038582566317230853 -6.420708633914161e-5 7.816118542539724e-5; 0.0009955799842781563 -0.0009733208240890431 -0.0014490970765884158; 0.0008553906889067525 -0.00026312102303960717 0.0002741674001525109; -0.0003973792866319458 0.000996014116898926 0.0005693624308721807; -0.004595931935174298 -0.0038135443712606332 -0.001100374724233598; 0.008822537553335012 -0.004183459956757467 -0.00020164845467261858; 0.0016028639669512733 -0.0007455909112100562 0.003549011848314632; -0.004825432702531668 -0.004050925561105311 -0.002133835845858946; -0.0012801895584931503 -0.0019300519232302916 0.0019003249142780939; 0.004320033820435045 -0.006250149680080806 0.004645613392965233] %
+
+Mass Used: 98.43242024564142 kg
+Launch C3: 95.05859415747402 km²/s²
+||V∞_in||: 6.755202056827621e-9 km/s
diff --git a/archive/ES_0.5596672973221287 b/archive/ES_0.5596672973221287
new file mode 100644
index 0000000..360ff15
--- /dev/null
+++ b/archive/ES_0.5596672973221287
@@ -0,0 +1,22 @@
+archive/ES_0.5596672973221287---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T14:56:18.418
+Launch V∞: [7.926198080879866, -5.668933003399541, 0.16447872328301608] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7424015653009442e-9, 1.80888290155066e-9, 6.377879246913645e-10] km/s
+ V∞_out: [1.7056450075209206e-9, -1.6846248315448772e-9, -1.4174906776297294e-9] km/s
+ time of flight: 1.858953834831958e8 seconds
+ arrival date: 2030-04-04T04:32:41.418
+ thrust profile: [0.4992620209316415 -0.021065551145644873 -0.14928616274016251; 0.060202764485398026 0.03334912318795923 -0.07078224365367629; 0.03235360878926621 0.030067000074813447 -0.06736815540067384; 0.022723572560095447 0.02530273178228815 -0.0689947732699604; 0.0140007814085367 0.017931279175256554 -0.05485657852326556; 0.012432323903746788 0.01920430503300704 -0.06890510761686561; 0.017880650875425466 0.033652036678437 -0.11281735036961135; 0.019423562700722492 0.04566097966196607 -0.1861254389477076; 0.004402979410446289 0.009964684006225943 -0.041881168965991214; 0.0014777660555287005 0.002163326942511935 -0.009744341659809527; 0.0007199820089605147 0.001385131043926656 -0.010402654718815477; 0.0006202010002584312 -0.0004231489624639908 -0.0034840361906865965; 1.1343624182068475e-5 0.000733253110582496 -0.0023250681602702715; -0.00010282411189703851 -1.0314818014471247e-6 -0.0006674936985174278; -0.0036559155891925303 -0.004662621887246824 0.002969693842297805; -0.005692381813043119 0.0018542206979998937 0.0009651056697135953; 0.0014807563864768565 -0.002389067235873437 0.0030937246370274533; 0.0015319360765216434 0.004621301728993456 0.0030502560197516893; 0.0024989512026588555 0.0013632880034254939 -0.002372482301244004; 0.01462703744033758 0.006925701691327902 0.00536054378250265] %
+
+Mass Used: 98.84576799788101 kg
+Launch C3: 94.988470664789 km²/s²
+||V∞_in||: 2.591291956373815e-9 km/s
diff --git a/archive/ES_0.5596683345043234 b/archive/ES_0.5596683345043234
new file mode 100644
index 0000000..b15fb69
--- /dev/null
+++ b/archive/ES_0.5596683345043234
@@ -0,0 +1,22 @@
+archive/ES_0.5596683345043234---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T06:26:46.939
+Launch V∞: [7.70450087500372, -6.1463604776143175, -0.44829028076802685] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002964146207651177, 0.00020381177361696859, 0.012590881371579985] km/s
+ V∞_out: [-0.011859250705254586, -0.0038176937894590897, 0.001771383107071188] km/s
+ time of flight: 1.7546483776924625e8 seconds
+ arrival date: 2029-12-04T02:40:43.939
+ thrust profile: [0.2968997291457884 -0.029797833783903452 -0.11399042453259779; 0.04794934938915434 0.01981232708665571 -0.06112445807977777; 0.06618083860045032 0.04557675169674873 -0.14683696869283272; 0.037748619359240454 0.03377768424281518 -0.12049963217506976; 0.033833813563484236 0.03627597769983314 -0.14133650622217378; 0.021007926414505336 0.025160180732350657 -0.10956003279556897; 0.02113661757163946 0.028061505830065985 -0.12885560912177849; 0.007648287652409841 0.010661842026061824 -0.0569818151040032; 0.004560375430503601 0.006847884523433342 -0.0380214621981178; 0.0015604428520339024 0.0023163678538288823 -0.014371745630953878; 0.0002017572779547709 -0.00010460235117434148 -0.0006692262914261582; -0.00010531716108655789 0.000249202075374123 -0.00033936242771626216; 0.00046016672096069384 0.00010412937129995536 -0.001030457900803726; 1.1767836776696e-5 0.00017113532207793555 -0.0006527584369130923; -1.9028534323501776e-5 -0.00016374339460444091 -0.0006810925450642843; -0.0003772649952363536 0.0003855966712197678 0.0004846704901721186; -0.0004007116649372665 -0.0003092125501400929 -0.0005666335779941668; -0.0006044740053481796 -4.44595338668e-5 0.0013927957302689912; -0.0006889730655338917 0.0011224318214339583 -0.0005661654878309512; -0.0030671779848313076 0.0002925260895621402 -0.00018150950036659936] %
+
+Mass Used: 85.14112758270721 kg
+Launch C3: 97.33804502954345 km²/s²
+||V∞_in||: 0.012596018997273232 km/s
diff --git a/archive/ES_0.5596712940660458 b/archive/ES_0.5596712940660458
new file mode 100644
index 0000000..3d0bfb1
--- /dev/null
+++ b/archive/ES_0.5596712940660458
@@ -0,0 +1,22 @@
+archive/ES_0.5596712940660458---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:01:08.494
+Launch V∞: [7.851824891492575, -5.696010570041577, 0.33870696974789083] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.327674778491068e-6, 0.00021618907768202516, 3.70938635731184e-6] km/s
+ V∞_out: [0.00020845999278614805, -3.209959990655396e-5, 4.809558351310174e-5] km/s
+ time of flight: 1.8749577787486404e8 seconds
+ arrival date: 2030-04-21T06:10:45.494
+ thrust profile: [0.44383597931397806 0.027725428664781348 -0.11073172849207245; 0.11674935446920667 0.08218053246852092 -0.10659540066516798; 0.0699175730146296 0.08115683693125192 -0.11733428327944521; 0.06047716459001331 0.09814569914833254 -0.1538420002901199; 0.037985596178038185 0.07893513494413885 -0.13700743839176976; 0.013888939867591793 0.0349534845533726 -0.06901783692572339; 0.0070455264951944045 0.02157542858609407 -0.045557378657999324; 0.0017537401995379998 0.008929350039629465 -0.020033208072425538; 0.0005850647602607393 0.005157014588548658 -0.007007960611008987; 0.0025834251695156718 0.004334824053304135 -0.01802619570329917; -0.0004128822358650452 0.0006427900344893366 -0.001866616471570765; 0.0004288905474134278 0.0022559437301501754 -0.007303956644430673; -0.0003090751409902169 0.0010855081686864784 -0.0029932044874385884; 0.0015363991857231059 -0.00040645362375858784 -0.002537848528259501; -0.0024381940604584207 0.0006227695627615596 -0.004381322770552259; -0.001530873678818948 0.0042152913792609294 0.00045442504810105835; -0.004371385870118952 -0.004984534320315851 0.001483924023603911; 0.001190305554133312 -0.0026434771174796575 -0.0017321442261796147; -0.00038640453887468036 -0.0017081484251193482 0.006742638367337329; 0.0025486603231170374 0.006831160589736126 -0.010901479887643666] %
+
+Mass Used: 103.38910085679936 kg
+Launch C3: 94.21041295204355 km²/s²
+||V∞_in||: 0.00021642200066750565 km/s
diff --git a/archive/ES_0.5596723235813869 b/archive/ES_0.5596723235813869
new file mode 100644
index 0000000..09dcbba
--- /dev/null
+++ b/archive/ES_0.5596723235813869
@@ -0,0 +1,22 @@
+archive/ES_0.5596723235813869---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T08:25:44.899
+Launch V∞: [8.121992246044536, -5.946159705422405, 0.0019966035843321803] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.009478319445403118, -0.06590734125173679, -0.08021632129159388] km/s
+ V∞_out: [0.04188929913974553, -0.03656490821187927, 0.08857554968895362] km/s
+ time of flight: 1.8749577779666457e8 seconds
+ arrival date: 2030-04-28T10:35:21.899
+ thrust profile: [0.07054953261797813 -0.004895470253450498 -0.030178965140287096; 0.016188181737412558 0.005622037944265613 -0.023811799379385726; 0.027976806182599966 0.014934175312673475 -0.07136556177891278; 0.04125178600383884 0.026096002575230905 -0.14753970859652896; 0.03394253643115941 0.023023489234555456 -0.15472969971719777; 0.01955487496147183 0.013555290283625102 -0.10767031836107945; 0.013093219573431727 0.008989832442138178 -0.0829716069171957; 0.0066416902022498805 0.0042449496836065165 -0.046901810255125534; 0.006493833115786172 0.004132872691514298 -0.05014250316353534; 0.0012560372328326928 0.0008248663163232463 -0.009823233218103382; -0.00017042349913919173 0.0006438224340738325 -0.0023528353846151862; -0.00022179226904132473 0.001249239270501546 -0.0019061757176626508; 0.00020869029572793848 -3.4614009080830032e-6 -0.00222197194058786; 0.0007708521768431377 0.0008992181629652171 -0.00665706340481736; -8.993860514232776e-5 0.0006058199773425871 0.0007310021226783854; 0.0016356912356428588 0.00022616553187818642 0.0005008418787647403; -0.0004364079077956085 0.00013652888696056198 0.0015813485803208576; 0.00026025824335622815 0.0004726640173788671 -0.0019948025587667394; -0.0017530172593130545 0.0037038769463421635 -0.0030181632802242547; -0.0006646280833589953 -0.0006524846440344012 0.0005431225866277923] %
+
+Mass Used: 61.89684341548673 kg
+Launch C3: 101.3235772736225 km²/s²
+||V∞_in||: 0.10425101616741302 km/s
diff --git a/archive/ES_0.5596776267452113 b/archive/ES_0.5596776267452113
new file mode 100644
index 0000000..7d7b43a
--- /dev/null
+++ b/archive/ES_0.5596776267452113
@@ -0,0 +1,22 @@
+archive/ES_0.5596776267452113---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T12:55:32.436
+Launch V∞: [7.8066715930412505, -5.980119416534833, -0.05528924643933837] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1327674150720261e-8, -1.3056606859832392e-7, 2.1179537756791003e-8] km/s
+ V∞_out: [-1.914295206317062e-8, 8.4007866807243e-8, 1.0422194753460758e-7] km/s
+ time of flight: 1.7753818007852232e8 seconds
+ arrival date: 2029-12-27T09:05:12.436
+ thrust profile: [0.3336416192378598 -0.027731626692470892 -0.12074129823013126; 0.04564927009890168 0.019714713761862176 -0.054913385882168396; 0.055966922261038755 0.04019969420092968 -0.11820300747363859; 0.04557527218410512 0.04235519641524863 -0.13897852893426912; 0.026802840830245322 0.02917149750124264 -0.10739334369804679; 0.031231959125433476 0.038996147861623 -0.15470355047855694; 0.01471277416847248 0.020110832236116465 -0.08739679006920072; 0.009957171187167872 0.014623462354812768 -0.06806795060820944; 0.0007829552287447586 0.0015718117212347475 -0.008156502104159946; 0.005264086414084837 0.008846653651392871 -0.0459925314417126; 0.0007231075454075679 0.0014236535055844254 -0.003033438750951167; 0.0004970093740015884 0.0007788169357384098 -0.002872812397782108; -0.0013436847198783936 -0.001528720288661732 -0.0009898563705461089; -0.0030248769090385763 -0.0007086855339795504 -0.005460672660075054; -0.0032873852057607508 -0.0026340518736989197 -0.004628417917219626; 0.001461179072501737 0.005976940149408845 0.0027103245778116675; -0.0025333885957456626 0.0008325816805765419 0.0001853988398837019; 0.003089808291326524 0.0009081707706737755 -0.006718302827593754; 0.002192292584173177 0.001689662829338009 0.002328827495606911; -0.00020152907944158608 0.0009429577133823596 0.001651149764308006] %
+
+Mass Used: 88.82135996216175 kg
+Launch C3: 96.70900649838595 km²/s²
+||V∞_in||: 1.3275687285590325e-7 km/s
diff --git a/archive/ES_0.559683081596785 b/archive/ES_0.559683081596785
new file mode 100644
index 0000000..a05378f
--- /dev/null
+++ b/archive/ES_0.559683081596785
@@ -0,0 +1,22 @@
+archive/ES_0.559683081596785---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T12:54:08.463
+Launch V∞: [7.994106247552423, -5.787092090732551, 0.04629021020338142] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00027186741664513573, -0.0002203847848533244, -0.00017163627789805615] km/s
+ V∞_out: [-3.5587994826696434e-5, 0.0002480098589183635, -0.00029910169398683617] km/s
+ time of flight: 1.8387907562929076e8 seconds
+ arrival date: 2030-03-11T18:25:23.463
+ thrust profile: [0.22418138278523467 -0.0048181686356646445 -0.07655952622532573; 0.12737941671090972 0.07133752624079015 -0.14296218995816162; 0.03895643641738765 0.03442679233525894 -0.08302452218562666; 0.02916025225269243 0.03428698611737133 -0.09151847907723111; 0.015588881368854427 0.024357902278793864 -0.07497186620110685; 0.023080738937372888 0.03988683910165937 -0.1261768726154983; 0.01571517353955957 0.030876240789243278 -0.10591828100633055; 0.0030987830406717233 0.01025136326659877 -0.04010268961245004; 0.007101938469065031 0.016291477779196296 -0.06608770391087797; 0.002081712974860907 0.006407922464497872 -0.028541520236952254; 0.0008704622754380372 0.003696482832629817 -0.012674153066449402; 0.0005340591581939112 -0.00051718868671236 0.0010067562290515736; -0.0005275412827210376 -0.0015387832560014667 0.004905291788571745; -0.0033968218262786475 0.002004035551805275 0.002998023414941599; -0.00043169272590085235 0.002108805486081327 0.002602614559199434; -0.002377236411590503 0.0012093538299591084 0.00048774423440406986; 0.004186980182544613 -0.0014244071387706926 0.0005824820591463639; 0.006318059750000588 -0.005208797067958834 -9.694586205418674e-5; 0.0001908471943444337 -6.164807306027847e-5 0.0003036566025955878; 0.0031270703499801478 -0.0026258723374664 0.006805616156201971] %
+
+Mass Used: 84.80677317011896 kg
+Launch C3: 97.39831234733661 km²/s²
+||V∞_in||: 0.0003897952764193592 km/s
diff --git a/archive/ES_0.5596858105605593 b/archive/ES_0.5596858105605593
new file mode 100644
index 0000000..2eb9f33
--- /dev/null
+++ b/archive/ES_0.5596858105605593
@@ -0,0 +1,22 @@
+archive/ES_0.5596858105605593---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T02:24:44.634
+Launch V∞: [7.960616452260264, -5.95052844454942, 0.028221467109377136] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.7473593756630353e-10, 2.344143416610769e-9, -1.8520621763805487e-9] km/s
+ V∞_out: [1.3875506600951575e-9, 2.729481811074717e-9, 6.50296764112395e-11] km/s
+ time of flight: 1.7947506554458568e8 seconds
+ arrival date: 2030-01-20T08:35:49.634
+ thrust profile: [0.18106902927712548 -0.01827501192414253 -0.07070733629418689; 0.022517182488445454 0.008715888053078947 -0.02965049436782695; 0.06937619587557681 0.04392084771700747 -0.15703483387626135; 0.03281390865228707 0.02606352818773926 -0.10947250855728748; 0.027471372431663837 0.02586881129469757 -0.12149139635296961; 0.022122696962951105 0.023516251477962893 -0.12210410650107281; 0.01562623221866588 0.01764803750750416 -0.10109090448212671; 0.01022789593764915 0.011453968126107961 -0.07255568631968785; 0.002176720304819515 0.0025493261573583496 -0.017471889981438154; 0.0018931900112814089 0.0029658676767281614 -0.02093110099642471; 0.004474523825828373 0.005552379242710508 -0.040935546202768534; -0.0014625648996837222 0.0006717790566099385 -0.0015275724901358894; 0.0002186158563580432 0.0012270589660251028 -0.0005099262221814516; 0.0001376283071412728 -0.0002225941169199821 0.0007923694695198736; 0.0055541558465467605 -0.0003418091855326554 0.0008751633603292885; -0.0016609953609748676 -0.0029870087956912917 0.0005867287823295478; -0.00012008767992277558 5.5687639859384956e-5 -0.00036582622244230164; 0.00343735926362706 0.0031897133051696455 -0.0028941751756723037; -0.00249501786825276 0.0008415500109828794 0.005880499360103823; -0.0010816481286788538 -0.003954141460959439 0.00695011846682642] %
+
+Mass Used: 76.74428178385233 kg
+Launch C3: 98.78099952059432 km²/s²
+||V∞_in||: 3.0109084485787273e-9 km/s
diff --git a/archive/ES_0.5596864679887905 b/archive/ES_0.5596864679887905
new file mode 100644
index 0000000..fd1296f
--- /dev/null
+++ b/archive/ES_0.5596864679887905
@@ -0,0 +1,22 @@
+archive/ES_0.5596864679887905---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T13:52:07.614
+Launch V∞: [8.00831225476594, -5.707767182621977, -0.22277639077051398] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.324729751939084e-7, -1.6935703075109594e-6, -1.5764425019031863e-7] km/s
+ V∞_out: [1.350986194649308e-7, -6.563968270425782e-7, -1.820646817348335e-6] km/s
+ time of flight: 1.87495777874936e8 seconds
+ arrival date: 2030-04-23T16:01:44.614
+ thrust profile: [0.31726689753345816 0.0061860042333379715 -0.10081218556299282; 0.05750718816796097 0.03625359330118858 -0.0670200660738883; 0.048785865130481804 0.050933235168388435 -0.10804199487870024; 0.045470690886863445 0.0637242942676384 -0.14832069276732684; 0.01878306819223038 0.03519757131471987 -0.09322166324287741; 0.00984947277397724 0.018822391752509847 -0.06091754829814532; 0.012548661459833764 0.026013957168131208 -0.07376514488873798; 0.005456808118580157 0.01241732287076511 -0.03774496038404377; 0.004349004227613269 0.012872555992168295 -0.04879466665409069; 0.0005582386451507505 0.005624286849057574 -0.015352651841380818; 0.007517751650373878 0.006949464928096397 -0.05038981077571563; 0.0007316173775214968 0.0021009015840515077 -0.01007589319221914; 0.00360672917387739 0.0014949163579930657 -0.0031308901551013765; 0.0016315282095439093 0.005413187703402222 9.682198187178134e-5; -0.0009016951507910451 -0.0028858188475952957 -0.001088038047990029; -0.006355958306737884 0.0002841610399021014 0.000937196057794216; 0.00033285431700969133 -0.0051971127061122245 -0.001537751511606444; 0.003268355379560082 0.003967919017088429 -0.003357698733779708; 0.005699307028251994 0.01193070011236447 -0.00021606862768587423; 0.00014282703663059276 -0.0013950917478128821 0.000539119508434709] %
+
+Mass Used: 88.52662523029858 kg
+Launch C3: 96.7613007011355 km²/s²
+||V∞_in||: 1.9397262553174386e-6 km/s
diff --git a/archive/ES_0.5596894287095442 b/archive/ES_0.5596894287095442
new file mode 100644
index 0000000..10f91cf
--- /dev/null
+++ b/archive/ES_0.5596894287095442
@@ -0,0 +1,22 @@
+archive/ES_0.5596894287095442---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T06:34:12.696
+Launch V∞: [7.633198285548728, -5.9808040639524815, 0.09521899892256427] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.69896331731306e-9, 6.561530716371881e-10, -1.0693728882481992e-10] km/s
+ V∞_out: [1.2263855147178492e-9, -1.1095772083387763e-9, -9.292674079850666e-10] km/s
+ time of flight: 1.7681647535489866e8 seconds
+ arrival date: 2029-12-16T18:15:27.696
+ thrust profile: [0.4396399164409478 -0.027666293909192497 -0.13366564889272373; 0.1768234586499306 0.0893862379538039 -0.17517791494993395; 0.08399015512540603 0.07000125301506493 -0.14818342445811306; 0.047638420899796474 0.05307185377331457 -0.12468226146131449; 0.04412893860421057 0.06063061013507708 -0.15396602255307437; 0.027219829679695908 0.04347354029788425 -0.12023787451132192; 0.0058519428041999 0.010545939195607364 -0.03208741977332458; 0.0039986077600944634 0.008321735756005866 -0.026542421054913872; 0.002167332922153837 0.005615165801098953 -0.02256175501030119; 0.0021346474047477014 0.004530139157210394 -0.015682690123456487; -5.327208847449936e-5 -0.0003433778709924486 0.00020790434690509023; 0.0022455946681974835 0.0012801211371139332 -0.005624448344351373; -0.0019506943667012828 -0.0004192060412114147 0.0006607459225295156; -0.00014912232315200322 2.2332096488471038e-5 0.00010492816622207192; -0.0006997365930545524 0.0010201831473956775 -0.0007385150551242306; -0.0006066557712092009 -0.0003662992727685157 -0.0025184559702206505; -0.0006465242002769744 -0.00019420140324723836 0.0011899031639600662; 0.00014232673184947308 0.000451912115228082 -0.001843170206105896; -0.003530725006473256 0.0016263538692984762 -0.004692109164063142; -0.0013527546923580193 -0.0021261718198715123 -0.002282238164991319] %
+
+Mass Used: 104.37633363650775 kg
+Launch C3: 94.04479997565038 km²/s²
+||V∞_in||: 1.8244036808600001e-9 km/s
diff --git a/archive/ES_0.5596933568989974 b/archive/ES_0.5596933568989974
new file mode 100644
index 0000000..cd8e514
--- /dev/null
+++ b/archive/ES_0.5596933568989974
@@ -0,0 +1,22 @@
+archive/ES_0.5596933568989974---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:05:36.532
+Launch V∞: [7.6004734939183525, -5.786659644005218, 0.29564171905803954] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.039085445517108e-5, -0.0005371279092750845, 0.009523999322699131] km/s
+ V∞_out: [0.0010035363934735014, -0.009476634429202374, 0.00012001006447318338] km/s
+ time of flight: 1.813671551560034e8 seconds
+ arrival date: 2030-02-07T14:51:31.532
+ thrust profile: [0.7494831966278114 -0.022456180299124613 -0.19879218778323754; 0.10275621002710936 0.05561066814726715 -0.09866050197659224; 0.06979480113193912 0.06151040433001807 -0.12387387930659856; 0.051060914915044116 0.05881255708355425 -0.13158002113360387; 0.03858010455751347 0.052343083331235635 -0.12807513617749383; 0.01429791564146973 0.028882140181868396 -0.07411189075007944; 0.00966561832567772 0.02196507511392651 -0.06124906747660609; 0.006019137780943562 0.013738302825031232 -0.04076373277071664; 0.00236858593728661 0.007240928643271926 -0.023614478276490554; 0.0015820348273000713 0.00482245752623899 -0.015817518153408983; 0.0012392957116182466 0.005427134091693398 -0.01700600777114593; 0.0013227412704535672 0.0033741002544540434 -0.010930662433171963; -0.0018011639407166356 -0.0018373852738653657 -0.0005326486388288491; -0.00038951689458683724 0.0008138629644496118 -0.0020005630285791437; 0.00023159443509236915 -0.0003828333481096964 -0.00010345758546774118; 0.0028621540664418104 -0.0013482589705443942 0.0002932751704675107; 0.003284805611870995 0.0011179732422091793 -0.0005556004797855794; 0.0010933787453198947 0.00016034672401401127 0.003149099972709618; -3.926101495235182e-5 0.0017464221211803497 -0.0010130490593850288; 0.0005581849532365704 0.000419574719596324 0.0054707842097562] %
+
+Mass Used: 120.15873442088741 kg
+Launch C3: 91.34003119336164 km²/s²
+||V∞_in||: 0.009539393291089673 km/s
diff --git a/archive/ES_0.5596950799035383 b/archive/ES_0.5596950799035383
new file mode 100644
index 0000000..c066597
--- /dev/null
+++ b/archive/ES_0.5596950799035383
@@ -0,0 +1,22 @@
+archive/ES_0.5596950799035383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T17:22:20.558
+Launch V∞: [7.739672665131806, -6.112178885180287, -0.016436841102874005] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.573693976962875e-6, -2.3241788510542878e-6, -2.2059573785414363e-7] km/s
+ V∞_out: [1.7835362660106133e-7, -9.901105832189284e-7, -2.6293865599615487e-6] km/s
+ time of flight: 1.7383903330143312e8 seconds
+ arrival date: 2029-11-13T17:59:33.558
+ thrust profile: [0.27411189602341907 -0.024147484930544326 -0.09562712320991183; 0.04220705703318699 0.01840385508172864 -0.04870539177880203; 0.06132350061430597 0.0455955581042685 -0.12141518114396431; 0.0425251994882335 0.04101997955222786 -0.1210860366236958; 0.041337102095048046 0.04849702731827198 -0.15443255207990556; 0.03696022769640443 0.04925455773398441 -0.16843475585676335; 0.01637715069935884 0.024029689992383675 -0.09139340721309828; 0.008064098380508875 0.012800256279231023 -0.05277596114290269; 0.004666869653531675 0.007921308831898215 -0.03491303254147606; 0.005299635841951282 0.00974169253265655 -0.04401095763454915; 0.0005976375144858129 0.0008403089109158021 -0.003358255269202754; 0.0002753683860537854 0.000744573887343158 -0.003414522082475186; -0.00047430956362917796 7.97519021043679e-5 -0.0014316664109841211; 0.0006367683087369656 -0.0004143836593108691 -0.0009549445692547332; -0.00028243743931772713 0.0002879515275423147 -0.001910923308846803; -0.001214389040389339 0.0012453436079259373 -0.0003672847286600811; -0.0009083938897119451 0.00010928074812990423 -0.000998531640433638; 9.978999094676581e-5 0.00027808343567578076 -0.0010895439722922323; 0.00017144395955026647 3.559220752822993e-5 0.0005513843357116862; 0.00012033305860232139 0.002374328160917979 -0.004521908831160429] %
+
+Mass Used: 85.61864571825845 kg
+Launch C3: 97.26153385757765 km²/s²
+||V∞_in||: 2.8154897521349057e-6 km/s
diff --git a/archive/ES_0.559703989317581 b/archive/ES_0.559703989317581
new file mode 100644
index 0000000..e100776
--- /dev/null
+++ b/archive/ES_0.559703989317581
@@ -0,0 +1,22 @@
+archive/ES_0.559703989317581---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T10:08:41.828
+Launch V∞: [7.758475175083148, -6.06836909836606, -0.01604180582410006] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.321302069697895e-8, -2.0241403511659903e-7, 3.9187821190025475e-8] km/s
+ V∞_out: [-3.268884338254884e-8, 1.234697869781016e-7, 1.6456165973190295e-7] km/s
+ time of flight: 1.7413950809189242e8 seconds
+ arrival date: 2029-11-16T22:13:49.828
+ thrust profile: [0.2772787342637195 -0.02493712449493098 -0.09959850007152919; 0.08123484589092854 0.03534436047018769 -0.09575726258120916; 0.058588878032346414 0.042547343070675286 -0.12036295901258935; 0.041117801570940575 0.03861926412220207 -0.12192606088695523; 0.032795369654221154 0.03745337673022934 -0.130123167963953; 0.028512071461896677 0.03783778748086062 -0.14047037443843363; 0.02036604206909992 0.029865620375264735 -0.12000595867066385; 0.010450258900535886 0.01606355231442694 -0.06947654099984603; 0.003757834813051995 0.006025656265777117 -0.02644061312369056; 0.001286017495026074 0.0025550001355698643 -0.011316594624299155; 0.0009482945341898148 0.00194918918863788 -0.009404228906939996; 6.603347508413762e-5 0.000627017446008917 -0.0007943508236949007; 0.0005270540413633659 -0.0007506590466300029 -0.003565085495211601; 0.0005706113344292598 -0.00010628058937101103 -0.0012708742904148592; -0.00029119251038812327 0.002317550025542587 -0.0023454392515112913; -3.08263385627943e-5 0.00010864732090960636 -0.0007801179612755263; 0.0021914658817689826 0.0023297128549587148 -0.0023413862351478595; 0.0011545831440250573 0.0004857764809274184 0.0011401406844492087; 0.0003250667706413083 0.0004024183575718984 -0.0006821206144353512; 0.001964977603915363 0.0002615094562668641 0.0034387087754473127] %
+
+Mass Used: 87.04208314431298 kg
+Launch C3: 97.01929789591969 km²/s²
+||V∞_in||: 2.0747523050157954e-7 km/s
diff --git a/archive/ES_0.5597125597010606 b/archive/ES_0.5597125597010606
new file mode 100644
index 0000000..95aa1cc
--- /dev/null
+++ b/archive/ES_0.5597125597010606
@@ -0,0 +1,22 @@
+archive/ES_0.5597125597010606---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T01:48:03.099
+Launch V∞: [7.91176562090022, -5.713221605287271, 0.039227005119136786] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6621545234948362e-9, -1.0563725623005413e-10, -6.348720295136376e-10] km/s
+ V∞_out: [8.843446769727096e-10, -7.799086380551139e-10, -6.156768890446027e-10] km/s
+ time of flight: 1.8588953222179615e8 seconds
+ arrival date: 2030-04-04T13:46:55.099
+ thrust profile: [0.481693356957099 -0.01109525406154133 -0.16150511527220215; 0.03671818976458049 0.02009446509094109 -0.045063173044984105; 0.029200439035900812 0.025576628490531418 -0.0642276825104449; 0.03910643179608285 0.0447504693816472 -0.12490164262839408; 0.027542072215162992 0.03800020109317591 -0.11862516876283258; 0.015816494439566058 0.02553472814690416 -0.08739771909577836; 0.023949821927899146 0.04368599698317816 -0.15829329580438378; 0.004503387314898983 0.008512743224006811 -0.03596037691945338; 0.0008488807604745689 0.005405086193641515 -0.016531844347097816; 0.0034304912089592634 0.005663578463747108 -0.025549269950051016; -0.001031552492975573 -0.0021378971635925507 -0.0015684551171384453; 0.00016146809909661948 0.0004573605791801474 -0.0020988256573396826; -0.0017919421157554039 -0.005108695795303408 0.002061287936705298; -0.0019345353604172414 0.008548344694191913 -0.0014697157442718468; 0.005316755483076211 -0.0020538047608910995 0.004663406435231307; -0.0014199358597715038 -0.0013846245077502816 -0.0040199735540368394; 0.009467392596125326 -0.008641057632010141 -0.0010397448124562843; -0.002708217070075195 0.006581241240390355 0.004561884409324483; 0.0067081778024484316 -0.006543872305977504 3.4817545100722077e-6; -0.003220792594833065 -0.002679504134649999 0.0001913399221669313] %
+
+Mass Used: 97.44021484809264 kg
+Launch C3: 95.23847510911052 km²/s²
+||V∞_in||: 1.7824083100504567e-9 km/s
diff --git a/archive/ES_0.5597152208325529 b/archive/ES_0.5597152208325529
new file mode 100644
index 0000000..8628078
--- /dev/null
+++ b/archive/ES_0.5597152208325529
@@ -0,0 +1,22 @@
+archive/ES_0.5597152208325529---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T22:10:54.781
+Launch V∞: [7.945999115410295, -5.542630446300323, 0.12770164781342994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2883543971906036e-5, -1.088470624384102e-5, 8.267446807108453e-6] km/s
+ V∞_out: [-3.0878296724755518e-6, -1.8415452581269278e-5, 1.017247826457355e-6] km/s
+ time of flight: 1.874957778745955e8 seconds
+ arrival date: 2030-04-21T00:20:31.781
+ thrust profile: [0.5496632639006216 0.0111548586653341 -0.14489488962155503; 0.10243017393312458 0.06473289110256832 -0.10886551161184213; 0.03669308957976266 0.03716931076498816 -0.07522317148555271; 0.0366644176853556 0.05186954343974663 -0.11276503114281496; 0.02624966770615412 0.04712204703246439 -0.11206195495695011; 0.014604157863937749 0.031785174511726 -0.0826022723250011; 0.008562787427870963 0.022511553895681012 -0.06381350508390209; 0.005116743454784507 0.012738298729852505 -0.03892614420255071; 0.005698774413598972 0.018566015214451982 -0.056083945873059496; 0.001418073674498062 0.0055813606233803045 -0.018461384219598455; 0.0009836447945487598 0.0038761008556366045 -0.01465620296754074; 0.00043078013165041157 -0.0011268157077181239 0.0023876806311918263; 0.0012558803991594525 -0.0016410787130475154 -0.0005051097873702202; 0.0009668600776744982 0.0018825900770520953 -0.0029163385451863887; -0.00314032482169264 -0.0006023670203746045 0.0025364499487385474; -0.00034303242482904776 0.0006468636687052971 -0.001963309078001997; -0.00035136072386121185 -0.0053699621815128645 -0.006991110649690415; -1.3833679604628366e-5 0.00320203207412933 -0.006170702584976412; -0.003657472951053046 0.004418313839464753 -0.002526987811123577; -0.00056264570033593 -0.004890938099298454 0.0014375336845740654] %
+
+Mass Used: 105.39131312091558 kg
+Launch C3: 93.87596191721077 km²/s²
+||V∞_in||: 1.8783322709231075e-5 km/s
diff --git a/archive/ES_0.5597304547142955 b/archive/ES_0.5597304547142955
new file mode 100644
index 0000000..766611f
--- /dev/null
+++ b/archive/ES_0.5597304547142955
@@ -0,0 +1,22 @@
+archive/ES_0.5597304547142955---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T09:02:37.089
+Launch V∞: [7.6610084453737075, -5.573288408614878, 0.1914662916623075] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.572598484494263e-6, -9.238033661255725e-5, 0.0018285960312919266] km/s
+ V∞_out: [8.303627747671086e-5, -0.0020525684258457986, 2.1418943603854057e-5] km/s
+ time of flight: 1.8749577787130165e8 seconds
+ arrival date: 2030-04-19T11:12:14.089
+ thrust profile: [0.8143297223889787 0.014436672556447643 -0.19869391017399485; 0.21000896195187332 0.13750456824267684 -0.1922288945731289; 0.05577950640241673 0.06064880520971405 -0.10278372880977886; 0.02505183616269956 0.037355322740690304 -0.07237867246572749; 0.022720357792233276 0.04360801170421763 -0.09208084594249444; 0.010392443009803435 0.02452283182079604 -0.056633759463489614; 0.009696335334048052 0.028075511367341995 -0.06779711500511024; 0.006273546968425524 0.022177194904396295 -0.057255188924929985; 0.002188987684383878 0.009161270932969 -0.02521424839190911; 0.00043616178404544555 0.0014395314298232809 -0.004458282100617343; 0.0003835955429677265 0.003651728245150717 -0.009852847500849023; -3.590875212139893e-5 0.0005488056905278791 -0.0005870239883437528; -0.0005250790728816932 3.042660332940733e-5 -0.0014403863013761685; 9.427688726434125e-5 -4.7646215659152683e-5 -0.0013989029437152497; -0.00035090569892745757 -0.0003157830592218549 -0.0008190217550042131; 0.0001137847234193301 0.0002169865891387913 -0.0012127444218266762; 0.0005386474584295477 -0.001033321511264216 -0.0006605520337278619; 0.001964754241741564 -0.00033664840134090446 -0.003559952999577378; 0.0002478319156238851 -0.000330038558642049 0.001395711935026133; -0.001971256917197926 -0.0006098494415821866 0.00017802382662278815] %
+
+Mass Used: 129.24821884524636 kg
+Launch C3: 89.78925342653115 km²/s²
+||V∞_in||: 0.0018309481318961522 km/s
diff --git a/archive/ES_0.5597320565487625 b/archive/ES_0.5597320565487625
new file mode 100644
index 0000000..35f060e
--- /dev/null
+++ b/archive/ES_0.5597320565487625
@@ -0,0 +1,22 @@
+archive/ES_0.5597320565487625---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T04:53:09.382
+Launch V∞: [7.682195696195466, -5.850626185133351, 0.09533499237932311] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.820817167667537e-9, -1.4495653086292626e-8, -8.632303760670487e-9] km/s
+ V∞_out: [-1.3618011678765515e-8, 1.1826430876311726e-8, 7.816553181926044e-9] km/s
+ time of flight: 1.8283555808543533e8 seconds
+ arrival date: 2030-02-25T08:32:27.382
+ thrust profile: [0.45659939216256434 -0.0004798873242829923 -0.12448451913618291; 0.22130226998005553 0.1354578301579232 -0.20209096532128187; 0.0807416219804491 0.08155474345710238 -0.1419790409014901; 0.057045660828130874 0.07784272038557305 -0.14997229595721223; 0.03108255619810334 0.05326136651710568 -0.11592222509641388; 0.008740658103506181 0.01898280773604064 -0.045520973704388526; 0.003962702478230561 0.011062912734929601 -0.02869357343121477; 0.004639379289663418 0.011149742434662211 -0.029440388129597768; 0.0013948338966724083 0.00813103209658967 -0.02176579497133426; 0.001971801636056139 0.007868676283226106 -0.02335661674133065; -0.00024364860791769265 0.0013157473999536656 -0.0023869316015914374; 0.00031531200971466234 0.0026880506602542297 -0.006405272103937373; -0.0030282832086134513 -0.001771755932086931 -0.0036025345187598286; 0.0011005561364286738 -0.0002913722865824325 6.756527809492416e-5; 0.0003071534697888382 0.0008246244587168648 -0.002052314998582574; -0.004438071290170392 -0.005578224156906408 -0.006814015113463837; 0.008957402877004476 0.0008574280344998273 -0.0024476672808053223; 0.0012476163721239926 0.0005839420809359741 -0.0006455930853701191; 0.000409904892876045 0.0017890348136220494 0.0017723935822918984; -0.00015327356982257389 0.0007905681479910845 0.0006116369359077574] %
+
+Mass Used: 109.03296294431539 kg
+Launch C3: 93.25504623358412 km²/s²
+||V∞_in||: 1.729853376570898e-8 km/s
diff --git a/archive/ES_0.5597335025356085 b/archive/ES_0.5597335025356085
new file mode 100644
index 0000000..8d2cca3
--- /dev/null
+++ b/archive/ES_0.5597335025356085
@@ -0,0 +1,22 @@
+archive/ES_0.5597335025356085---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T05:58:44.443
+Launch V∞: [7.659730319879518, -5.823748615316184, 0.12029703493381451] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00011869500049616149, 0.007594451950886833, 0.0001197147215536342] km/s
+ V∞_out: [0.007348663272501162, -0.0011747987899023995, 0.0015328994401329005] km/s
+ time of flight: 1.874957778745149e8 seconds
+ arrival date: 2030-04-21T08:08:21.443
+ thrust profile: [0.5044528424381831 0.014825702627816548 -0.10171638741615713; 0.1362193104730322 0.09977202634066268 -0.11466414130979768; 0.1414096939204998 0.1711372311977998 -0.20362043977056146; 0.05245172373754574 0.09159447673459183 -0.12972077843027133; 0.017770886859894527 0.039776047837832215 -0.06448376598385698; 0.010909219918950934 0.031144183473670553 -0.05439956035235881; 0.009084937638370445 0.03190545062361315 -0.05909284424128369; 0.006112043849341584 0.028241082409455633 -0.05450217680320925; 0.0012734270344286899 0.006520978713300568 -0.014083975801239799; 0.0008932726004142184 0.0044305858629153485 -0.009659511746701039; -0.00029938479961689796 0.002146283704457129 -0.004649352321985626; -0.0006261065227326568 0.0002658188592105363 -0.0007939811820744656; -0.00034999459864237375 0.002700789323613252 -0.002814065313840702; -0.00020814820989651934 0.000802827180816838 -0.0011294357050821526; -0.002026957791274343 -0.0004255613262449827 -0.002291068133365739; 0.0006469477743274569 0.0010473458180083072 0.0007635949966352498; 0.00036651820386185473 0.0005406383499495344 -0.0002743269733442745; -0.000172316660699453 0.004866415965611648 0.0006657223563064816; 0.0010620048109152732 -0.0015077928810582242 -0.0008917602612383375; 0.0025685043527238893 -0.0009287119409585793 0.0017033419438864054] %
+
+Mass Used: 112.84415696650285 kg
+Launch C3: 92.60198788429263 km²/s²
+||V∞_in||: 0.007596322830951056 km/s
diff --git a/archive/ES_0.5597482092789612 b/archive/ES_0.5597482092789612
new file mode 100644
index 0000000..4c2df79
--- /dev/null
+++ b/archive/ES_0.5597482092789612
@@ -0,0 +1,22 @@
+archive/ES_0.5597482092789612---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T02:43:23.423
+Launch V∞: [7.832964184241166, -5.555979142722331, 0.2080733729127222] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8482380997196286e-6, -3.261071239479274e-6, -2.686710575731239e-7] km/s
+ V∞_out: [2.776691790265379e-7, -1.3237987874931772e-6, -3.5046849649626197e-6] km/s
+ time of flight: 1.8749577787470925e8 seconds
+ arrival date: 2030-04-20T04:53:00.423
+ thrust profile: [0.6304292481136522 0.004277964582114222 -0.16853865736692322; 0.1406331884053673 0.08912507125406421 -0.13810186150315226; 0.08860633253585751 0.09424055231967159 -0.1629561354084334; 0.04229299119530725 0.06404794845698229 -0.12646649299677828; 0.012273007067991929 0.02394001216684167 -0.054201859438823954; 0.007650859659591255 0.01895881417306696 -0.04665142476872148; 0.007725133421670857 0.02270783820639302 -0.06675533256756676; 0.0053601508974977586 0.01392356884432286 -0.04768208765870935; 0.0017080086456003033 0.007885693440195268 -0.019739842643561427; 0.0019213050737847462 0.0016975848235719815 -0.003948007613932728; 0.0018642883888699887 0.008397977180387435 -0.024816181084324734; 0.00013589019420389196 0.0004145534431366596 0.0003241740944801596; -0.0001527199985579728 -2.0245882382429717e-5 -0.00020702241352373962; 0.0013967006937307752 -0.0005738383686175747 0.00245720119747349; 0.001726922845543675 0.0005884986842320718 -0.0024476904826875936; 0.0028382194889992815 -0.0005694542138611927 0.0013691902757957464; 0.003468065246608482 0.0004438488539743582 -0.0006993742605386779; -4.540220982369425e-5 0.0006685651638648947 -0.0005813300063300217; 0.00024031492097430332 -0.004164311738075283 0.0027416597862680156; -0.0002367627732712224 -0.005694112050131489 0.006846567138154329] %
+
+Mass Used: 114.81233855762139 kg
+Launch C3: 92.26752667448571 km²/s²
+||V∞_in||: 3.7580252579501875e-6 km/s
diff --git a/archive/ES_0.5597493993182734 b/archive/ES_0.5597493993182734
new file mode 100644
index 0000000..2cec9a8
--- /dev/null
+++ b/archive/ES_0.5597493993182734
@@ -0,0 +1,22 @@
+archive/ES_0.5597493993182734---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T21:25:38.170
+Launch V∞: [7.722722201959541, -5.908637605969162, 0.36027524561091234] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.755928589700062e-6, 4.3764552833964265e-5, -0.0008025126418298496] km/s
+ V∞_out: [-3.1041107748301515e-5, 0.0008026338939586902, -1.0147252724748792e-5] km/s
+ time of flight: 1.777079731271757e8 seconds
+ arrival date: 2029-12-26T16:45:11.170
+ thrust profile: [0.371109973077507 -0.02011584802040713 -0.10956636535352506; 0.23389093981359108 0.1309671093095967 -0.22655858567641463; 0.07411521634809362 0.06704018872135686 -0.1385355211808703; 0.0432920309485588 0.05154101513898701 -0.11968967048470383; 0.021856025201641937 0.03033872857462336 -0.08180828948284136; 0.015489371375971391 0.026318756831711573 -0.07673807509947228; 0.005299113496048973 0.010011865361005068 -0.031224363561559727; 0.014854892686976498 0.03515744210590677 -0.10842588478164106; 0.004179542845450196 0.010069987091412628 -0.03446838907388707; 0.001518817350417895 0.003848616964237054 -0.014078967737376878; 5.623901047592345e-5 0.00014173099435970762 -0.0007085111686238155; 7.597158169602794e-5 0.00017773219819202776 -0.0005025950964809981; -9.629840682122744e-5 0.0004229011473729019 -0.0006521491217501144; -0.00013832789252418397 -0.0001521422260707168 -0.0004339473278329636; 0.00027745733965016454 0.00035532418411693466 8.213187751358354e-5; -0.0002625617885384259 -0.0005064002255284508 4.503395582000297e-5; 0.0006838650044428792 -0.0001004257190839535 0.00032674070616956256; 0.00016775448920410146 0.00012671076581204137 0.0001290085559021268; 8.38542049427458e-5 0.0002064175376583265 5.750563444272127e-5; 0.0005613149602986886 -2.3709776346320956e-5 8.902090165953435e-5] %
+
+Mass Used: 100.72792942183332 kg
+Launch C3: 94.68223481991181 km²/s²
+||V∞_in||: 0.0008037257038912038 km/s
diff --git a/archive/ES_0.5597496416166479 b/archive/ES_0.5597496416166479
new file mode 100644
index 0000000..5728a0b
--- /dev/null
+++ b/archive/ES_0.5597496416166479
@@ -0,0 +1,22 @@
+archive/ES_0.5597496416166479---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:41:36.093
+Launch V∞: [7.8840310562712395, -5.733544232417308, 0.15634081447329548] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00021410885639010148, 0.00014723887876839315, 0.011332661540594945] km/s
+ V∞_out: [-0.010490163336915251, -0.0037505543285747977, 0.0020811145245563547] km/s
+ time of flight: 1.8423856092762756e8 seconds
+ arrival date: 2030-03-15T01:04:16.093
+ thrust profile: [0.43758653950572324 -0.015305749827964314 -0.1273055725541487; 0.10245839670053246 0.05780079568368976 -0.10744944154687347; 0.040891784279381796 0.03725350424689431 -0.0783356457359106; 0.023919937622706382 0.029074752921554658 -0.07021783713664971; 0.04337014984644565 0.06461922143878432 -0.1587866385442489; 0.01400451643948311 0.024373328479842426 -0.07066361035797063; 0.012983620612783735 0.023816709715947907 -0.07228345493939366; 0.013894208374361212 0.027295762511525334 -0.09148347608833578; 0.003198477423745152 0.006599721385792746 -0.030039000469140823; 0.002895182842795072 0.007915402547927781 -0.032309198772686364; -0.00018947364602062773 0.0009839540966150064 -0.008178989491928208; 0.0010939351810445607 0.0011541090067866112 -0.002302552595442083; -0.0007178165877852566 -0.003793036936317277 -0.003091908392333807; -0.003791643225084683 0.0010774296106729028 -0.003370183231420269; 0.003086722115450116 0.0018233724483872474 -0.00030133610677563426; -0.004435990870301356 -0.0007256879206985986 -0.006464946558961793; 0.0006669344842592422 0.004749541047378951 0.003325071008173374; 0.000848689344568592 -0.0007692721154864634 -0.0028933439490118765; -0.00947480491323493 -0.0005177783022937811 0.013379266287708184; 0.0016745672977449872 -0.0007605374468376087 0.0030558391450292957] %
+
+Mass Used: 98.54839581839133 kg
+Launch C3: 95.05591761160535 km²/s²
+||V∞_in||: 0.011335640232624069 km/s
diff --git a/archive/ES_0.5597524006355007 b/archive/ES_0.5597524006355007
new file mode 100644
index 0000000..8c116c4
--- /dev/null
+++ b/archive/ES_0.5597524006355007
@@ -0,0 +1,22 @@
+archive/ES_0.5597524006355007---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:04:51.926
+Launch V∞: [7.818402569750738, -5.793864915730448, 0.26270009451962406] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.456304827825882e-6, 3.064911952970007e-6, -2.272671435217384e-6] km/s
+ V∞_out: [6.779500652025884e-7, 5.0961687670938685e-6, -2.2782996637112791e-7] km/s
+ time of flight: 1.8749577811078268e8 seconds
+ arrival date: 2030-04-23T14:14:29.926
+ thrust profile: [0.4581381774981543 0.00655547841240613 -0.12245181680544123; 0.08971657397777281 0.0572444138543489 -0.09344647162657288; 0.04432428443083987 0.046426723110599116 -0.08537294947964733; 0.052444681281425015 0.07493706384601642 -0.14934056007757007; 0.020354566258298307 0.03601175067357017 -0.08315882810015907; 0.022708179644811925 0.04939600316507097 -0.11916293807825405; 0.0044778015920602385 0.011443862256348462 -0.030488235319191367; 0.0045547751376390395 0.013781325359552463 -0.038366308081943655; 0.003993506209393695 0.014412523597458742 -0.04279912802472346; 0.003826921482429955 -0.00029010546237266286 -0.0072113195703643; -4.883918623644918e-5 0.007527355066474836 -0.02849249579531812; 0.002252491000563297 -0.0011124829404114515 -0.002674416437502714; 0.0029531178162760896 0.0014865288930201212 -0.0012836224588575551; 0.003579071497831377 0.004796710463084402 -0.003908817345271589; -0.0010079968732700493 -0.000832263422666873 -0.00336011537887598; -0.004881501624221005 0.005108972902826514 -0.0032652620321534406; 0.00013318305675430158 0.0037054551264675342 0.0020827055762572435; -0.003552384908711227 -0.004068826687665149 -0.005401023722658417; -0.002293769889835191 0.005905475242567152 -0.011502212723282746; 0.0013440038127701542 0.008237648362385604 -0.010480966295985411] %
+
+Mass Used: 100.24687973429718 kg
+Launch C3: 94.76530074407776 km²/s²
+||V∞_in||: 5.148277750351467e-6 km/s
diff --git a/archive/ES_0.5597679012143206 b/archive/ES_0.5597679012143206
new file mode 100644
index 0000000..bf3ddff
--- /dev/null
+++ b/archive/ES_0.5597679012143206
@@ -0,0 +1,22 @@
+archive/ES_0.5597679012143206---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T10:43:52.258
+Launch V∞: [7.900390815667956, -6.130805513643686, -0.046011824766339166] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00045366636038716805, 0.0012106112297257487, 0.0029441582417213054] km/s
+ V∞_out: [0.002934084958429451, 0.00036395594592610725, -0.001264036778090069] km/s
+ time of flight: 1.7795458713383102e8 seconds
+ arrival date: 2030-01-04T02:33:39.258
+ thrust profile: [0.10260481666404907 -0.012898938321765112 -0.041500115072255164; 0.025069335457497136 0.008386955222448408 -0.03363482577739858; 0.044316190588893856 0.023116281192959276 -0.10085810371029083; 0.04655217394267721 0.029368257709714397 -0.14963318540946166; 0.04271408849028717 0.029860144034148592 -0.17527276054439123; 0.022939788922425382 0.017134481108984547 -0.11380384186062095; 0.015410382764641989 0.011994717778444138 -0.08885240169107989; 0.01708634475895888 0.013523121348406138 -0.10937647000920493; 0.0008883048817039086 0.0006591087773449002 -0.0053545326256101864; 0.0013858031682110591 0.0027933863562483938 -0.01623196905157304; 0.0006269485342459578 1.2265202939788257e-5 -0.002939249855915137; 0.001029755326689856 0.00023750926191715057 -0.005147374135416839; 0.00066499590988358 0.000316370422694661 -0.0047086712965237155; -0.0008540432678102569 -7.003955905192437e-5 -0.0015239610698734572; 8.26046757542205e-5 0.002317555280577972 -0.002957070374935585; -0.00030756207102117955 0.004229757908336868 -0.0061838526530795645; 0.0014906909312744207 -0.0009004608668563314 0.0014918138177251912; -0.0018334505504200406 -9.300483157904731e-5 0.00048669658409296584; -0.00019064837092233405 0.0007028659374120224 -5.602107518522443e-5; 0.0006735879359290268 -3.571859529563745e-5 0.0016282317888362213] %
+
+Mass Used: 69.69965256584965 kg
+Launch C3: 100.00506837443274 km²/s²
+||V∞_in||: 0.003215503143892184 km/s
diff --git a/archive/ES_0.5597711039256236 b/archive/ES_0.5597711039256236
new file mode 100644
index 0000000..1d59935
--- /dev/null
+++ b/archive/ES_0.5597711039256236
@@ -0,0 +1,22 @@
+archive/ES_0.5597711039256236---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:03:16.327
+Launch V∞: [7.588669656676181, -6.113602193455124, -0.23439294850488668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.177694150528942e-5, -4.5976823558520115e-5, -0.0030672493675025594] km/s
+ V∞_out: [0.0027149032318230146, 0.0009702490900948819, -0.0010554829258864649] km/s
+ time of flight: 1.8106874088378856e8 seconds
+ arrival date: 2030-02-06T02:55:36.327
+ thrust profile: [0.29409778967916805 0.007780130161532008 -0.07718584839447239; 0.18090565286044183 0.11846315980280162 -0.14769333205195506; 0.08609298674065798 0.09201540962480799 -0.13211405197782805; 0.06182405042110743 0.09109692283086067 -0.1423275085167709; 0.044763625042384764 0.0847451955350136 -0.14298141924903116; 0.028354561093282535 0.06818065735112015 -0.12589608530571914; 0.010142828066923005 0.028161974681601247 -0.05995873987050633; 0.003459572236401828 0.01235702137038653 -0.026128197054052938; 0.0016204732091931419 0.006164708610540146 -0.01623738619486959; 0.00025944073679655313 0.0012208167329443905 -0.0035497098439504233; 1.7011229751003579e-6 -6.403998591271616e-6 0.00013716195448696842; 2.951308581574106e-5 -0.00016123249670958002 -0.00031484376868858737; -2.201639002997564e-5 -0.00019528074121890495 0.0004288905047531899; -7.935136360984012e-5 0.00016855371660894042 0.0006213290239176343; 3.3025500509406025e-5 -0.0008024057965437174 0.0001291511064920775; 0.00043614434322975545 -0.00046301800794025603 0.000806061115873944; -2.0798196865664307e-5 -0.0002657378930336955 0.0008814383792450263; -5.1269326857800625e-5 0.0006576904547552641 -0.00018331974817391587; -6.158909049332134e-5 0.00033762204150345756 -0.00024982982248593225; 3.601029300166509e-5 0.0007199077507181982 -0.00013791450519290714] %
+
+Mass Used: 98.78891045822638 kg
+Launch C3: 95.01897899228591 km²/s²
+||V∞_in||: 0.003068215921549709 km/s
diff --git a/archive/ES_0.5597776354518231 b/archive/ES_0.5597776354518231
new file mode 100644
index 0000000..d58e2ef
--- /dev/null
+++ b/archive/ES_0.5597776354518231
@@ -0,0 +1,22 @@
+archive/ES_0.5597776354518231---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T19:42:37.614
+Launch V∞: [7.937715254450271, -5.617833352435844, 0.13119927373391588] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2993699785482122e-5, 0.00031437532973342886, 5.438191512956176e-6] km/s
+ V∞_out: [0.00030534533979937445, -4.575119833437914e-5, 6.33930064898023e-5] km/s
+ time of flight: 1.874957778723105e8 seconds
+ arrival date: 2030-04-21T21:52:14.614
+ thrust profile: [0.5129849711701233 -0.006263654037786428 -0.1209824692325215; 0.04258114092337822 0.02783764427539357 -0.0426261088527531; 0.034998159643185686 0.037811312690198995 -0.06333887578612361; 0.03806920831320648 0.05639748100458064 -0.10357101403333974; 0.02021771601453654 0.036986624684382886 -0.07636208794171055; 0.012270288044536686 0.03071697934802113 -0.06662912099899916; 0.005120260145267866 0.013483445461455966 -0.03350995394624795; 0.01971228846027515 0.06447380084374488 -0.1426093168579974; 0.01700980181876717 0.05539731223959693 -0.1373438230256448; 0.0014079636205194014 0.0035750048566115613 -0.01257697423915868; -0.0018413925228137889 0.000933091140469027 -0.003096427845773735; 0.001824715092390832 0.00028658128696697915 -0.001781946184182192; -0.0034289947319435174 0.001376601324679613 -0.0014137397536651444; -0.0008752562228650751 0.0016117290786037827 0.0018611004049614724; 0.000807807290412239 0.0009817946176309197 -0.004235430564681985; -0.0021026022682013572 -0.0014416983885970525 0.0006876523165561086; -0.0020203075698984824 -0.002930573565737502 0.002652132493720521; 0.0030111043390293286 -0.0017424704374964127 -0.0017535221982280182; -4.9859943060837184e-5 0.005051876960220532 -0.005084734860272173; 0.0007563297872928889 0.00015790887537202314 -0.004664011534547885] %
+
+Mass Used: 101.33047635936873 kg
+Launch C3: 94.5845882859014 km²/s²
+||V∞_in||: 0.0003146907340644922 km/s
diff --git a/archive/ES_0.5597910024657058 b/archive/ES_0.5597910024657058
new file mode 100644
index 0000000..fe9e195
--- /dev/null
+++ b/archive/ES_0.5597910024657058
@@ -0,0 +1,22 @@
+archive/ES_0.5597910024657058---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T09:44:47.383
+Launch V∞: [7.86744104861468, -5.492917082215979, 0.580408127526444] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.211381889647801e-9, -4.148839293843542e-8, 6.780393446823378e-9] km/s
+ V∞_out: [-6.734088188946858e-9, 2.53959947998615e-8, 3.5286042527782903e-8] km/s
+ time of flight: 1.8749577787445295e8 seconds
+ arrival date: 2030-04-19T11:54:24.383
+ thrust profile: [0.6763107864804849 0.01447033654371285 -0.16015353202967053; 0.1470916798689738 0.09638734531682075 -0.13756450031883646; 0.040816769392516675 0.042966880998734434 -0.07236714983754608; 0.0276029643597681 0.03930316947090025 -0.07352671260172029; 0.029020569796940114 0.05268360831561398 -0.10662264519067899; 0.01398775195032704 0.03033533105606409 -0.06763504196513674; 0.01798673291018522 0.05065196748478016 -0.1160289311018433; 0.005753590139709728 0.017299882707821936 -0.04420815486359637; 0.0013790915599025608 0.005413002507225277 -0.014965044735752496; 0.0005255081589804616 0.003720551271121185 -0.006852830751724798; 0.00043391991454861105 0.002587564950921279 -0.0069960028484586404; -0.00026791481164229375 0.0016822786755030592 -0.0013141171442951865; -0.0014484040029237397 0.0014913252137606484 -0.001993046690341401; 0.0005238496220045071 0.0006509566788765175 -0.003636888507281782; -0.0001698917324707474 0.0011158677149750414 -0.0033469600882360243; -0.00010699759895530262 -0.00016209454938119353 -0.0009551217071508064; -0.0008930543848504422 -0.0012439783179760931 -0.0005297229933877374; 4.23008983542627e-5 0.0005492563099726362 -9.841220626824292e-5; 0.00023994793396302618 -0.0013768414602238661 0.0007045098972127128; -0.002516584455313331 -0.0029838588784484458 -0.004660810963125681] %
+
+Mass Used: 114.05660100983778 kg
+Launch C3: 92.40564032002611 km²/s²
+||V∞_in||: 4.2249215629739174e-8 km/s
diff --git a/archive/ES_0.55982781382513 b/archive/ES_0.55982781382513
new file mode 100644
index 0000000..8245141
--- /dev/null
+++ b/archive/ES_0.55982781382513
@@ -0,0 +1,22 @@
+archive/ES_0.55982781382513---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T21:55:47.959
+Launch V∞: [7.828199980718763, -5.966214866018369, 0.025194065639041748] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9176577679481894e-8, -2.5810812404950547e-7, 4.824692611357479e-8] km/s
+ V∞_out: [-1.848913715271719e-8, 1.5573630473449234e-7, 2.1313822274573212e-7] km/s
+ time of flight: 1.8181198200324404e8 seconds
+ arrival date: 2030-02-16T05:15:29.959
+ thrust profile: [0.3051862882720383 -0.0036165853301262938 -0.09832178435064433; 0.046522558266602516 0.025250532607452067 -0.051367671942706424; 0.04698864449296434 0.043024659858526694 -0.09310853638670044; 0.05199703398087316 0.06600391018581211 -0.14857640627149177; 0.02993015833438498 0.044637181874884656 -0.11685924840737068; 0.017700756027484867 0.029655548126622234 -0.08648826832072742; 0.015311478648432523 0.030762376088170645 -0.09366887988181402; 0.009393307420457546 0.022531252585828276 -0.07243780859145975; 0.006778129753463886 0.016873058279086098 -0.05820584875454555; 0.0015836396986214176 0.0014099371993585843 -0.012447680654683404; 0.001003037408209222 0.0010309761208017625 -0.007202356688995392; -0.001712766138798397 0.0029688875664989475 -0.0032412292282615576; -0.0028754261820546083 0.0012085620575210587 -0.0047036307505859375; -0.00024775471630993984 -0.0005907335798309237 -0.0030553849202906718; -0.0027851874243131824 0.0030576409282282667 -0.008201109621098093; -0.00019346472465014102 0.013093988387472177 -0.0034067502894810533; -0.0005705525203458482 -0.0028114572629347225 2.2890498430122933e-5; 0.005824600076304782 0.00876716104959263 -0.0013228423104816004; 0.0009599671276473722 -0.0018490927009600987 -0.0014861764195962875; 0.0006293882532079559 0.005908939980813925 0.003062755038679129] %
+
+Mass Used: 88.0162106743428 kg
+Launch C3: 96.87706950656725 km²/s²
+||V∞_in||: 2.641947052172895e-7 km/s
diff --git a/archive/ES_0.5598283117055515 b/archive/ES_0.5598283117055515
new file mode 100644
index 0000000..215b35a
--- /dev/null
+++ b/archive/ES_0.5598283117055515
@@ -0,0 +1,22 @@
+archive/ES_0.5598283117055515---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T10:49:58.763
+Launch V∞: [8.071811003080748, -5.621284491434999, 0.40300301874311517] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0002842028619481504, -0.00022636894639907145, -0.0001777823676433647] km/s
+ V∞_out: [-5.377332991848296e-5, 0.0003334785997721969, -0.00044397829588626925] km/s
+ time of flight: 1.8749577787754774e8 seconds
+ arrival date: 2030-04-23T12:59:35.763
+ thrust profile: [0.3502007467664072 -0.0006717111256672418 -0.11027425431942657; 0.0517431870857496 0.028306053962482123 -0.06220205081628871; 0.03381181408426332 0.029489214112624736 -0.07339575881855943; 0.02177451120096763 0.02417208121692296 -0.07086491082598018; 0.02021094643703764 0.027482619327982637 -0.08646765612725524; 0.018220574631899362 0.028276788110864717 -0.09749133620516241; 0.012702911027689652 0.02142837596918759 -0.08338442402811151; 0.011979864107759593 0.024540884688964423 -0.09506759009915712; 0.005534562835036779 0.011692846889501219 -0.05139298739039676; 0.006406552171912928 0.014312127602493011 -0.06054937608096984; 0.0002857318108602695 0.001344268827476194 -0.00039671942712023265; 0.0003514120862047963 -0.0007545523021657446 -0.00575394840910977; 0.0013771654688754117 0.003584383213425425 0.00016017644297778785; -0.0034492154110132797 -0.0019230516324664465 0.002870644450694724; -0.0003151856323565839 -0.0007834538016285287 0.0034368920963589577; 0.006843214617927327 0.0017882500645555913 -0.003568737907356614; 0.0017995931446862096 0.00023269642442932947 0.003193275438074263; -0.009637534038090294 -0.0012126728421129316 0.0001474186484981025; 0.008716471502563553 0.005110142965340025 -0.009274227526771789; 0.0036316401562266074 -0.004254147798057897 0.004129861110524578] %
+
+Mass Used: 87.7932924451984 kg
+Launch C3: 96.91538363621913 km²/s²
+||V∞_in||: 0.000404500601826778 km/s
diff --git a/archive/ES_0.5598294708225682 b/archive/ES_0.5598294708225682
new file mode 100644
index 0000000..2236553
--- /dev/null
+++ b/archive/ES_0.5598294708225682
@@ -0,0 +1,22 @@
+archive/ES_0.5598294708225682---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:17:03.088
+Launch V∞: [7.95046238878219, -5.701614674596901, -0.0611506900108716] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.20049881005902e-11, -8.967284237259495e-9, -1.031840905261019e-8] km/s
+ V∞_out: [1.5068011114524394e-9, 5.798093892040974e-9, 4.707809338878246e-9] km/s
+ time of flight: 1.8749577780268925e8 seconds
+ arrival date: 2030-04-23T20:26:40.088
+ thrust profile: [0.4194887779915663 0.0008269165266830672 -0.13217470492917038; 0.08370050518411379 0.04796277496512415 -0.10061507645004047; 0.022376535568792443 0.020464239354877508 -0.05129940368975572; 0.021015038764182932 0.02538039625115323 -0.07058462377358864; 0.023108299358709367 0.03404909537022749 -0.10304916822904088; 0.012056603886046426 0.020980023436618964 -0.07076742672742425; 0.019738163511155073 0.03868746204151403 -0.13428929742057547; 0.010838124379493845 0.023726793554512914 -0.09074889927452455; 0.005027138674604424 0.011170181332397897 -0.048378158048909436; 0.0016500765346294192 0.0026360987811195153 -0.016131957464936786; 0.0006615338812803019 0.0014242810656377382 -0.006707683088470184; 0.0006027656665566138 0.0017235874784725482 -0.002309164644429408; -0.00019508235974763512 0.0006028160188631829 -0.0028391442714427737; -0.00042347876182840453 -0.003296909171240933 -0.005077976587798683; -0.0010294459443111682 0.0005036905906247115 0.008769106422793639; -0.004422475383438119 0.003973761156511951 0.003837263068398666; 0.0011847089565404124 -7.982564245540718e-5 -0.005459363201042131; 0.005460676686728515 0.000503867427179093 0.0033771855943203685; 0.008138131155637864 0.005327821269939328 0.0119282457914506; -0.00023596804668342582 -0.0005698559044876154 0.0026162483432286615] %
+
+Mass Used: 94.75604054353425 kg
+Launch C3: 95.72200149990776 km²/s²
+||V∞_in||: 1.3670487781651825e-8 km/s
diff --git a/archive/ES_0.5598566386179695 b/archive/ES_0.5598566386179695
new file mode 100644
index 0000000..890d8d5
--- /dev/null
+++ b/archive/ES_0.5598566386179695
@@ -0,0 +1,22 @@
+archive/ES_0.5598566386179695---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:56:47.433
+Launch V∞: [8.068344217879686, -5.704903172697638, 0.22923374437872548] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.3249601870378315, 1.0634337567980658, 2.1489383633407333] km/s
+ V∞_out: [2.2248536447746194, 0.33458448106320277, -1.315585916771688] km/s
+ time of flight: 1.874957779051003e8 seconds
+ arrival date: 2030-04-24T02:06:24.433
+ thrust profile: [0.26032835280792693 0.0025471487796692063 -0.08112148680297913; 0.05822541080094439 0.035759470403081715 -0.06745260695766957; 0.04207839928839011 0.04167949762677083 -0.08771482198828105; 0.023006515805217155 0.03003049622935273 -0.07283630387996613; 0.013075494117180404 0.020916201519225724 -0.05658671344944076; 0.014370238452005246 0.026042823300055317 -0.07518167532247291; 0.008244926513316706 0.01822176746707867 -0.0577066612350002; 0.00944896933440393 0.022893330668234423 -0.0778093043641353; 0.007408577542658356 0.020275101499870357 -0.06765693161244168; 0.010558113074212132 0.04156410881122364 -0.13883031826139947; 0.0016767782464534838 0.004535817271323699 -0.02101353744104058; 0.0005834617723676884 -0.0017210213381562557 -0.002615041631345821; -0.003909428093668839 -0.0006657034547848861 0.0011973053063409561; -0.003678923122102852 0.004275204925085232 0.0032846871144868338; -0.0003566008335700373 -0.0007892539558618065 0.000694664635969308; 0.0003335238366666747 -0.0002729702418942053 -0.0017112894844999622; 0.0006940302972324912 0.002523466037082733 0.004668727988695729; 0.0006958925635185603 -0.0015841239049615829 -0.0005513752202349624; -0.0025845846868168248 0.0016094318074288962 0.0042841765514896645; -0.004356155384065237 -0.004349883669963592 -0.001606335306235159] %
+
+Mass Used: 83.26897241823917 kg
+Launch C3: 97.69664673761004 km²/s²
+||V∞_in||: 2.4195922316983207 km/s
diff --git a/archive/ES_0.5598573849841976 b/archive/ES_0.5598573849841976
new file mode 100644
index 0000000..770549b
--- /dev/null
+++ b/archive/ES_0.5598573849841976
@@ -0,0 +1,22 @@
+archive/ES_0.5598573849841976---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T12:20:07.671
+Launch V∞: [8.066775855665611, -5.535334637029113, 0.18386817072062078] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8619065014641073e-5, 0.00041916930604574327, 7.371175880118734e-6] km/s
+ V∞_out: [0.00040442732257906845, -6.466274869001795e-5, 8.973530193460574e-5] km/s
+ time of flight: 1.8749577787445244e8 seconds
+ arrival date: 2030-04-21T14:29:44.671
+ thrust profile: [0.4184560068922459 0.004608994743693074 -0.11984922190906105; 0.05700853073319756 0.03701564010449497 -0.06721133649657879; 0.039098161976179574 0.03960141519996633 -0.07875096954329248; 0.04656797901887521 0.06275985883224944 -0.13942156349838772; 0.03041473379688232 0.04927207637013283 -0.12087290281653228; 0.013954935647386094 0.029005086913640243 -0.0768298493641642; 0.006076633903674968 0.016014164946195723 -0.04598027577770168; 0.009391996930426652 0.029685308949853502 -0.08985807621129736; 0.0013851279751869899 0.004918213870480697 -0.019842775390864285; 0.004194988715915113 0.009483633232999226 -0.03572273519916788; 0.00020127998385346935 0.0015621685595364329 -0.008727062362387579; 0.0014519029254191453 -0.002786018184943356 -0.0033426440999314937; 0.0008732618442284413 0.0005624785519187314 -0.0022258193594692152; -0.0003712132078920632 -6.709096285022317e-5 -0.0014384515087415236; -0.004428293726183161 0.0043733078216473585 0.0042791844239143196; 0.0007381340739563459 -0.0021588960555894293 0.0009250537279854205; -0.007887294666702556 -0.0046244530918831935 -0.0017112937947610831; -0.002540121956435634 0.0014806113744613562 0.007077300587063424; 0.00042194444701012444 0.0009894168313785033 -0.0002646045266169756; -0.0001864917187461565 -0.0076654324937982105 0.013900170610450156] %
+
+Mass Used: 94.645058918617 kg
+Launch C3: 95.74660975364803 km²/s²
+||V∞_in||: 0.00041964736499440226 km/s
diff --git a/archive/ES_0.5598611339033338 b/archive/ES_0.5598611339033338
new file mode 100644
index 0000000..1003af4
--- /dev/null
+++ b/archive/ES_0.5598611339033338
@@ -0,0 +1,22 @@
+archive/ES_0.5598611339033338---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:28:39.970
+Launch V∞: [8.120161463660216, -5.594232167479871, 0.14564615782388654] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0013892251770636656, -0.0007942461129330255, -6.005890182695324e-5] km/s
+ V∞_out: [0.0011080639972542872, 0.0006835776361317141, -0.0009330883220336016] km/s
+ time of flight: 1.8749577784070572e8 seconds
+ arrival date: 2030-04-22T18:38:16.970
+ thrust profile: [0.27225125560989855 -0.0009044875768498123 -0.08686920869402891; 0.08564696440590897 0.04861144038226037 -0.09700572431818716; 0.032710348956665365 0.029719936582531834 -0.06909548160173494; 0.036261104872206844 0.04285391098646136 -0.10837872596611003; 0.02637732544667067 0.03976708179438691 -0.11258492559393185; 0.023119903285363303 0.03951078847938013 -0.12291041671607315; 0.018218378887311232 0.03456158809119631 -0.11600036543248117; 0.0023402822119385587 0.007406355026471275 -0.027905729700426075; -6.327477530758104e-5 0.0030961315149886934 -0.012657472376046275; -0.0009432883523110502 0.006201629695310675 -0.020847286585516586; 0.003605868835215041 -0.0006810949062850719 -0.01032099933236467; -0.00307534818921411 0.003325032622515892 -0.002183198256215377; 0.0005227982787486065 0.0010770498477418167 -0.007488343320620491; 0.00031059443632909056 0.0005522445209589247 -0.0004154760837881185; -0.0019704780601214975 0.009748644334762545 0.001288264870752839; -0.00038374583217308154 -0.002820537783807873 0.0034643775073894788; -0.0031946073792604745 0.001112773986012304 0.007044078462687066; 0.0028058986869343976 0.0012899999760587815 0.0021253669654968652; -0.006869498134120589 0.003717285697597202 0.007901152864870952; -0.0020959200748106167 0.00435530976536333 -0.020230891943845426] %
+
+Mass Used: 85.85825638716051 kg
+Launch C3: 97.25366854286781 km²/s²
+||V∞_in||: 0.0016013683374493993 km/s
diff --git a/archive/ES_0.5598623584127563 b/archive/ES_0.5598623584127563
new file mode 100644
index 0000000..4eb0626
--- /dev/null
+++ b/archive/ES_0.5598623584127563
@@ -0,0 +1,22 @@
+archive/ES_0.5598623584127563---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T10:21:42.266
+Launch V∞: [7.849142605980651, -5.760968944003777, 0.07361170220609226] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.203809556319305e-9, 8.775961718568146e-9, 5.053338368914473e-9] km/s
+ V∞_out: [6.349123511845658e-9, -6.0828567366132634e-9, -3.787453859606257e-9] km/s
+ time of flight: 1.845476182063592e8 seconds
+ arrival date: 2030-03-17T09:35:20.266
+ thrust profile: [0.403729099699749 0.007946637069551475 -0.10050511469735532; 0.09065918670868053 0.05948562435826825 -0.08115159292981873; 0.053215158321511004 0.058542556030964525 -0.0878664657922842; 0.0982296584552326 0.14770250196075588 -0.22278736450221073; 0.021299933197391718 0.04125180645437631 -0.07589839761860778; 0.014909935405160718 0.035385162651306354 -0.06941258459851354; 0.006237928997860883 0.018442185316054165 -0.039684549133806465; 0.016828045262211575 0.04792643488177859 -0.10273027965543058; 0.003341456429636233 0.011566081990617233 -0.028141247096378257; 0.0018690180431957806 0.00826147457898175 -0.020732340564543362; -0.0013596599138783027 -0.0006261276690167528 -0.00219254325881725; 0.0003980272344964053 -0.00042980362344930334 0.0002958889001155609; -0.002489874428288927 0.00015917152520613775 -0.0015652139644203884; -0.002003431508737323 -0.00027138739548753 -0.00045249463423568254; 1.5735971912262623e-5 0.0003073804513427108 0.00036474682261858696; 0.001729889589622897 -0.0026412340019750804 -0.0005320291584999803; -0.005263674753874315 0.0007887648614720393 -0.0002814835739660598; -0.0029819933834098105 0.005928082261530224 0.0006422491936156073; 0.0009819114986270117 0.00019941012435828134 0.0019526300482982856; -7.643327828624373e-5 -0.0001632761248277953 0.0020229752888712618] %
+
+Mass Used: 100.15395936614186 kg
+Launch C3: 94.80322150549839 km²/s²
+||V∞_in||: 1.0964750227083072e-8 km/s
diff --git a/archive/ES_0.5598709441135493 b/archive/ES_0.5598709441135493
new file mode 100644
index 0000000..7f4a3ca
--- /dev/null
+++ b/archive/ES_0.5598709441135493
@@ -0,0 +1,22 @@
+archive/ES_0.5598709441135493---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T02:53:14.089
+Launch V∞: [8.03686573191209, -5.696671787170443, -0.0010230640788776368] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.952459652299012e-9, -2.881605882987309e-9, -1.5615931108041262e-9] km/s
+ V∞_out: [7.731446284001235e-12, 1.5592203100201373e-11, 5.088670918569264e-13] km/s
+ time of flight: 1.8749577787453e8 seconds
+ arrival date: 2030-04-23T05:02:51.089
+ thrust profile: [0.2579636261196402 0.006469272292398611 -0.08023455839741296; 0.08116398638470634 0.05135210524705131 -0.08755261553647227; 0.05388478206661951 0.055591443653045566 -0.10603605286287823; 0.03814131239022727 0.05296458235841868 -0.11327090043329338; 0.04201885242928686 0.0752745011575095 -0.16865602713946232; 0.015848317977216326 0.03373808524348577 -0.08628328144550076; 0.004543726151045845 0.012050193835417689 -0.031343423298062514; 0.0035872359469066063 0.011777124000471643 -0.03286960024259138; 0.004159366614204971 0.015135020510583524 -0.044864947766997156; 0.0020566294592168524 0.009944566752666015 -0.030706534785450088; -0.0018711603515243573 0.0035644300885298696 -0.0019637281718795987; -0.000561580430873857 0.0010696131153485678 -0.002431972158444636; 0.0013189397659499973 -0.0010647205664509867 -5.2861206539419323e-5; 0.005200479609531818 -0.0050390801135995235 -0.005421620467739234; -0.00012841897538725446 -0.002588301745650941 0.0031228519091620176; 0.0008989178175003174 -0.014009751534170129 -0.005262112866490419; -0.000589105599989664 -0.000659319751866335 0.0018166595365793517; -0.0010731281716601223 1.1617345352887137e-5 -0.004356878708367611; 0.004808308919115533 -0.0041746380861180255 -0.011156394637814319; -0.006139230804194025 -0.0054785838177772925 0.013464780098810924] %
+
+Mass Used: 87.09696060638544 kg
+Launch C3: 97.04328129018664 km²/s²
+||V∞_in||: 3.815013001607407e-9 km/s
diff --git a/archive/ES_0.5598744391937565 b/archive/ES_0.5598744391937565
new file mode 100644
index 0000000..cda99bf
--- /dev/null
+++ b/archive/ES_0.5598744391937565
@@ -0,0 +1,22 @@
+archive/ES_0.5598744391937565---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T18:49:14.484
+Launch V∞: [7.832895146307034, -5.763702236801839, 0.1788813052402495] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9125190580689514e-8, -1.7542451319425738e-7, 3.023517870821773e-8] km/s
+ V∞_out: [-2.769914145489349e-8, 1.0777557566418177e-7, 1.4147995340029293e-7] km/s
+ time of flight: 1.857286972843168e8 seconds
+ arrival date: 2030-04-01T10:07:31.484
+ thrust profile: [0.398877787699839 0.0054073186235701984 -0.11451542606358768; 0.16189277408338082 0.09968330690790934 -0.15975004651568245; 0.060487337737354784 0.05997943335463063 -0.1100592256994222; 0.05464859433029786 0.07285680683755005 -0.1484942898881423; 0.021799035395156343 0.03579712018398958 -0.08224986038939117; 0.019442194558552717 0.038790586678018775 -0.09583418742854075; 0.008585729212238664 0.019729285563066395 -0.05269546777718816; 0.005108228354877476 0.013205843423837547 -0.03562455349465325; 0.002398769296249324 0.004986067349068661 -0.011596619158437531; 0.0006368098793241386 0.0020585334472773944 -0.002202045691191447; 0.0014525445577032578 0.0027797483100723682 -0.0038929353859937506; 0.003531535826204926 0.008032557290795777 -0.008492800193941295; -0.0010170694891005363 0.002029127744466461 -0.003976599726289617; 0.004322061694818035 -0.0020972572939372378 -0.009957632746921932; 0.002117430421704009 0.004499096163525077 0.00011508419951810462; 0.005417659838718457 -0.006218652354872798 -0.007664500805604364; -0.00075039163180782 -0.005696612442620855 -0.007552203277097699; 0.003612129065545627 0.0010092063733317226 -0.004041913271539164; -0.00207442981183424 -0.004862270626108431 -0.011501663287179418; 0.002139375795743565 0.0016944834220865642 0.007299607844351557] %
+
+Mass Used: 101.31554690735356 kg
+Launch C3: 94.60650836891926 km²/s²
+||V∞_in||: 1.7903546792663106e-7 km/s
diff --git a/archive/ES_0.559874910749675 b/archive/ES_0.559874910749675
new file mode 100644
index 0000000..de995b4
--- /dev/null
+++ b/archive/ES_0.559874910749675
@@ -0,0 +1,22 @@
+archive/ES_0.559874910749675---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T23:11:55.113
+Launch V∞: [7.840791828077982, -6.046728262695704, 0.03077148114847642] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.8085966735205897e-7, 2.8410272676307836e-6, -6.38687086283996e-5] km/s
+ V∞_out: [-2.2763813480843637e-6, 6.390564951076043e-5, -6.598864669640551e-7] km/s
+ time of flight: 1.7503098544091472e8 seconds
+ arrival date: 2029-11-27T18:55:00.113
+ thrust profile: [0.1756112988387399 -0.019218178082941177 -0.06589805024527051; 0.08936156508603696 0.03635789421227068 -0.10649040564892856; 0.07040780954296057 0.047328068358420086 -0.1461199034742696; 0.05154870066131477 0.04425479875031452 -0.15387237957409688; 0.035281815688488885 0.03554486908525942 -0.13841380858070534; 0.020761856015555753 0.0237432933555221 -0.10205233884267091; 0.010825138565962301 0.013031606458376345 -0.06023836032144129; 0.014122097997745168 0.017231108224195796 -0.08572062629364167; 0.004932830078105381 0.00676791639971302 -0.03487509065106786; 0.0017055288808172334 0.0023028174563996307 -0.013633813525705215; 0.001078315036322658 0.0012720923641709944 -0.00904453970078778; 0.0006772017319966379 0.0009469314751175388 -0.0047436078363713614; 0.00022903679470872413 -4.780331978654654e-6 -0.000832806484856725; 0.0009728664444502432 0.000834724456426853 -0.0009835825027269527; 0.00020000769567222023 0.0010409815553972602 -0.004509146370578433; -0.0008848365580141568 0.001727630619638744 -8.842994295478305e-5; 0.002686131478273621 -0.001331588411584756 -0.004056484680230875; 0.00026700257749197407 1.3529650210151371e-5 -0.005391534613404985; 0.004494666651350497 0.0025725315440921297 -0.001565778175703553; -0.0007880111993728604 0.0013195449814225782 0.0023528183298806727] %
+
+Mass Used: 81.27639386851524 kg
+Launch C3: 98.04188605818953 km²/s²
+||V∞_in||: 6.393299955329049e-5 km/s
diff --git a/archive/ES_0.5598808468450195 b/archive/ES_0.5598808468450195
new file mode 100644
index 0000000..34bfd61
--- /dev/null
+++ b/archive/ES_0.5598808468450195
@@ -0,0 +1,22 @@
+archive/ES_0.5598808468450195---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:18:22.110
+Launch V∞: [7.9218676986897965, -5.513580474352832, 0.26945982624154013] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0007299788080369901, -0.0006110050577566313, -0.00047583179004590507] km/s
+ V∞_out: [-8.652098201195162e-5, 0.0007406424887657192, -0.0007593063749529875] km/s
+ time of flight: 1.87495777871284e8 seconds
+ arrival date: 2030-04-20T08:27:59.110
+ thrust profile: [0.6026098628807347 0.005801186823196963 -0.1603726241913364; 0.09304125874783249 0.05680820391551765 -0.09415875918380552; 0.07230348260374932 0.0743483601644425 -0.13589984277499223; 0.030980884856768285 0.04306722978176345 -0.08969850811837485; 0.023094938510277177 0.038288377101831146 -0.09256039044554802; 0.023651909109725085 0.04977702725096504 -0.12470715308776041; 0.008985813224379791 0.020930792847942796 -0.05662996345044275; 0.001998103947159613 0.005231144438828989 -0.016168205417078352; 0.002015228164712144 0.006404946517312587 -0.020742849377071725; -1.9935961962920567e-5 0.004175250752947092 -0.013802172871142139; 0.0009564999847332871 0.002918438453392652 -0.012169492283987287; 0.001033888493577405 0.0001976143550285375 -0.003482110291778747; -0.00023326098892881026 0.0059745336601696895 -0.013031905758466931; -0.0010517787588934994 0.0023785372564030572 0.00022884576849888007; 0.003620416749161955 0.00020100632230159914 -0.0018822723242239619; 0.00295383975563569 0.005341364292139837 0.001703512997747997; 0.003915463996759174 0.004617270965172012 -0.0068319200995193554; 0.0014622710816089533 0.0005707762349419516 -0.001541422632975203; -0.00013465702783643847 0.007949957940332545 0.0012598543816996796; -0.005334189677687561 -0.0005731768300595102 -0.0014822223559556897] %
+
+Mass Used: 109.36335251529454 kg
+Launch C3: 93.22816608066769 km²/s²
+||V∞_in||: 0.0010642425161614148 km/s
diff --git a/archive/ES_0.5598811264346004 b/archive/ES_0.5598811264346004
new file mode 100644
index 0000000..d7719fa
--- /dev/null
+++ b/archive/ES_0.5598811264346004
@@ -0,0 +1,22 @@
+archive/ES_0.5598811264346004---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T00:09:59.570
+Launch V∞: [7.908599252552935, -5.594938639114463, 0.20965152484459595] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7015023504088579e-9, 7.678882580059368e-10, 1.4772157294583814e-11] km/s
+ V∞_out: [1.229779853111933e-9, -1.2138560363238953e-9, -9.476958468769325e-10] km/s
+ time of flight: 1.8582813334146202e8 seconds
+ arrival date: 2030-03-31T19:05:32.570
+ thrust profile: [0.548945379309276 0.007081542632833341 -0.13744696142865495; 0.0761725982707832 0.052293517642453456 -0.08097813761142908; 0.060238960252667714 0.0730231330600485 -0.12630422825478652; 0.038662706440791374 0.061401834256549735 -0.11697024431363993; 0.024722723692606325 0.04648988157590646 -0.09450903467874866; 0.01509482572376385 0.04426651684227712 -0.0998472475153455; 0.00725209798685596 0.021050698683472747 -0.053092824816105125; 0.009289163203096452 0.04254563154381272 -0.10937600880209489; 0.00046258138915817974 0.0019132447930240062 -0.005353296289294306; 0.00044016951249953155 0.002080512212756558 -0.00604721733293988; -0.0011882974583598707 0.0015690579757977902 -0.004273552346275775; 0.00023364141407926798 -0.0011391356589933834 -3.0544208064435877e-5; 0.0006533614308674783 0.0007857003525616492 -0.0018503275659589025; 0.00017960351179221372 -0.0004257257647082463 0.0007291327872211758; 0.0004755308648073304 -0.0003554425126484455 0.001190265343449177; 0.003694018680648507 -0.0032174735151865846 0.002688506027185824; -0.0008653378217209362 -0.0008859254069598431 0.0021109915643347478; -0.00029371586945439303 -0.005440974849416522 0.0034403441330765; -0.0008808517546429333 0.0015385630376860576 -0.0038058268273665767; 0.00033869192489287806 0.0007579870695782268 0.006508810952383939] %
+
+Mass Used: 105.48411423732932 kg
+Launch C3: 93.89323427480649 km²/s²
+||V∞_in||: 1.8668103390171683e-9 km/s
diff --git a/archive/ES_0.559883820180167 b/archive/ES_0.559883820180167
new file mode 100644
index 0000000..102ddbf
--- /dev/null
+++ b/archive/ES_0.559883820180167
@@ -0,0 +1,22 @@
+archive/ES_0.559883820180167---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:51:54.169
+Launch V∞: [8.120400070769005, -5.6715214522607145, 0.13112399599997043] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3130151047562714e-6, -1.9808643867154342e-6, -1.9317624216586548e-7] km/s
+ V∞_out: [1.6595138519065097e-7, -8.058861005271341e-7, -2.237808128095425e-6] km/s
+ time of flight: 1.8749577787493914e8 seconds
+ arrival date: 2030-04-23T22:01:31.169
+ thrust profile: [0.2095522392810666 0.0002769206310369308 -0.07117599289648668; 0.07688238233798023 0.044572417425899014 -0.09016554457835503; 0.02581141394565386 0.02351594815928243 -0.06064741016694387; 0.026341489831641376 0.028964490191335065 -0.07630933615553262; 0.016661227265912716 0.022986999153377118 -0.07025624000069271; 0.04808748561428828 0.08192813940682504 -0.24129323258967866; 0.00930362237927172 0.019865434946007576 -0.07063328042342899; 0.003068329487000079 0.0016587706300370169 -0.020676906287557036; 0.00023592471744590627 0.001609575762489308 -0.03218630789628429; 0.004055292172140562 0.0068574008797005655 -0.013370130626344755; -0.0022367181963514633 0.007407194601325646 -0.012163435683330653; 0.00489710939753734 0.007516264510937114 -0.004453024626259986; 0.0004363260500374489 0.000966073357875285 -0.0026309861342429276; -0.0007217848777801876 0.0008288354287490159 -0.002963738652049088; 0.0008188903201173489 0.005207937383299858 -0.007209363946435788; -0.011405250415591102 0.002864194354742576 -0.005012601864907712; -0.00041158209477672853 0.002454165778884249 0.0014008782748522394; 0.00477113243251855 -0.00855604231185943 0.005347238431908172; 0.0035028271719794134 -0.002333731066843857 -0.031949624826169136; 0.00021932406964017006 0.00020058892712767002 -0.0024603846563910265] %
+
+Mass Used: 80.80635290529472 kg
+Launch C3: 98.12424639512575 km²/s²
+||V∞_in||: 2.3843551422581664e-6 km/s
diff --git a/archive/ES_0.5598899725300617 b/archive/ES_0.5598899725300617
new file mode 100644
index 0000000..c0f8bda
--- /dev/null
+++ b/archive/ES_0.5598899725300617
@@ -0,0 +1,22 @@
+archive/ES_0.5598899725300617---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T23:25:08.261
+Launch V∞: [8.148410586867266, -5.697536664455089, 0.010655461947644917] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.211072165300207e-7, 2.5271749652123578e-6, 0.0015451341712935777] km/s
+ V∞_out: [-1.51435723096424e-5, 0.001541726170401626, -4.689693752818365e-6] km/s
+ time of flight: 1.8749577787483364e8 seconds
+ arrival date: 2030-04-25T01:34:45.261
+ thrust profile: [0.1852127678638699 -0.006493452761969191 -0.06894566704764651; 0.04255931275887102 0.020563802570297524 -0.055248151584787256; 0.03745438442984872 0.02933762474173911 -0.09192264989786401; 0.03598494924521741 0.03374610833512606 -0.12208493014277191; 0.03146394309817811 0.03437354954361447 -0.142875860925305; 0.011608847905225851 0.014490849428700889 -0.07052804217058502; 0.007347229819483703 0.011487442985970847 -0.0597298311158888; 0.006326869595988499 0.009189913357829626 -0.05380228276779864; 0.010060374983336432 0.012739917686524695 -0.05529052139322171; 0.0051398062390401525 0.0011994431856721236 -0.031581085858616645; 0.0009178686296765017 0.004889023678753578 -0.01754160989093452; -0.0018623562922508849 -0.0019185441203934447 -0.002362956607564844; 3.895512050042628e-5 -0.004093888084856726 -0.002315327406164332; -0.008563920144485213 0.0014516199784295294 -0.00474554526651382; -0.0054652363320022304 0.0017101634263427179 -0.003815147647628328; -0.0010897909248265925 0.004642203631847903 0.003676547426629033; 0.00183056666559006 -0.002716554635912292 -0.0038642148186315145; -0.0011641836592988127 0.0036499548559758522 -0.005531858251677342; -0.0011778463161832187 0.0037736473948054923 0.010211689911066833; 0.004971460444245077 0.011859937750779183 -0.013031514477655786] %
+
+Mass Used: 76.52961068761442 kg
+Launch C3: 98.85863267384987 km²/s²
+||V∞_in||: 0.0015451362713438063 km/s
diff --git a/archive/ES_0.5598929902332835 b/archive/ES_0.5598929902332835
new file mode 100644
index 0000000..01998d2
--- /dev/null
+++ b/archive/ES_0.5598929902332835
@@ -0,0 +1,22 @@
+archive/ES_0.5598929902332835---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:44:51.410
+Launch V∞: [7.682671676352912, -5.855815685079899, 0.09696102853832729] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0020108806527824844, -0.0013578417561671433, -8.067080735052702e-5] km/s
+ V∞_out: [0.0017350305113879218, 0.0008240993786536206, -0.0014872439034538307] km/s
+ time of flight: 1.827223186575323e8 seconds
+ arrival date: 2030-02-25T06:56:49.410
+ thrust profile: [0.5741946552423172 -0.009759043580702679 -0.1641192780188129; 0.11275667630286305 0.06512320814997678 -0.11529769985395392; 0.0521642101089926 0.04968615454684441 -0.09999260031536406; 0.04414233712864797 0.05500618908997023 -0.1219018263179663; 0.010761343006456649 0.017103703693014824 -0.04392681994924872; 0.01171495251934575 0.01998708637990012 -0.05757076735148316; 0.00610646279578791 0.016317845081046212 -0.046800912786380905; 0.006042055542409318 0.016804003734328745 -0.05028596294839251; 0.002834777574901648 0.00814053576116458 -0.026701816957446937; 0.017842297071875863 0.05825838707420264 -0.17391508761884047; 0.0008064312272586137 0.003123422806534567 -0.011078951898438914; 0.00037216691640616325 0.0020758790655930805 -0.007903676886038108; 0.0006880499850331216 0.0014659195596634915 -0.0014983088270234806; 0.00041468369662100784 0.0009736227527450544 -0.0016349201330924336; 0.0016603474189497982 0.00028984173682589727 -0.0010312030139112227; 9.022448924636081e-6 0.00014836742686674448 -0.0006184337329629124; -0.000479045013398084 -0.002001660977808777 -0.0012268370371936845; 0.0005673781041134751 0.0002460631900361253 0.00044380325194884676; 0.001284888056337049 -0.0032351152615066906 -0.0019140144012267568; 7.86688070422046e-5 0.0006086636591700841 0.000401824883763081] %
+
+Mass Used: 108.82185522447435 kg
+Launch C3: 93.32342286531824 km²/s²
+||V∞_in||: 0.0024277320720550214 km/s
diff --git a/archive/ES_0.5598946570857316 b/archive/ES_0.5598946570857316
new file mode 100644
index 0000000..a0de0ce
--- /dev/null
+++ b/archive/ES_0.5598946570857316
@@ -0,0 +1,22 @@
+archive/ES_0.5598946570857316---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T07:41:15.326
+Launch V∞: [7.910361443980569, -5.8211127593883365, 0.09051284287402817] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.741314138835844e-9, -1.6181056957738598e-9, -2.4698750387139132e-9] km/s
+ V∞_out: [-6.131056300222261e-11, 2.0072438217008642e-10, -3.239619166133486e-11] km/s
+ time of flight: 1.8580091554808328e8 seconds
+ arrival date: 2030-04-04T19:03:10.326
+ thrust profile: [0.39300651550274873 -0.004003351417261991 -0.12252096232101974; 0.035730105417447 0.017592384488226184 -0.04338133006299266; 0.02778028484543772 0.02233977866626202 -0.05886804843546905; 0.03336958887544979 0.03789704273351734 -0.10691760973067099; 0.016421629262888 0.021743054720557084 -0.0713140558473542; 0.0188592351172839 0.030208730287002234 -0.10381401970459088; 0.01556046210861458 0.029693882879450417 -0.10716953168656726; 0.008176583952948775 0.016279059114357917 -0.06586696023982473; 0.008023162227269226 0.019413810274662196 -0.07929320161668613; 0.003440734054409636 0.008406453975348773 -0.0388028809647125; 6.410889779352507e-5 0.000798930534512131 -0.011673153193131214; -0.0008004486800498431 0.0036637614324579377 -0.0050568994961437295; 0.0019157148924420515 0.0030497170029450027 -0.002192715278606954; 0.0017160912507419527 0.002338696616854226 -0.002866558632516892; 0.00421676255973163 0.0027631294746252753 0.0030580694471102187; -0.009641032915115895 0.007535633865323639 -0.010363229818654632; -0.002267340177253321 0.002376543912596386 -0.005462170470823786; 0.005641703773325541 0.005870845614560533 -0.00838275739519161; 0.0014874644369347384 0.0015469071673322008 -0.004396636484346443; 0.004660040439796248 0.002098163105103292 -0.0023040467599910333] %
+
+Mass Used: 90.48414031121001 kg
+Launch C3: 96.46736450665318 km²/s²
+||V∞_in||: 3.4279328581037696e-9 km/s
diff --git a/archive/ES_0.5598953658881787 b/archive/ES_0.5598953658881787
new file mode 100644
index 0000000..8b13dd5
--- /dev/null
+++ b/archive/ES_0.5598953658881787
@@ -0,0 +1,22 @@
+archive/ES_0.5598953658881787---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T20:14:21.573
+Launch V∞: [7.908546270141891, -5.9533147245708316, 0.1459216188872242] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3628055964286368e-9, 2.9937599404980114e-10, -1.2818624388902275e-9] km/s
+ V∞_out: [1.7319221712336275e-9, -1.6590129598799513e-9, 6.009414395480002e-10] km/s
+ time of flight: 1.7968335376081702e8 seconds
+ arrival date: 2030-01-22T12:16:54.573
+ thrust profile: [0.24584757451990033 -0.019058124999522107 -0.0838488037946853; 0.03545588672495544 0.015737482615664006 -0.044455228098217635; 0.03585459054114455 0.02567777169037057 -0.07417340678608228; 0.037115566039383145 0.03367336357758257 -0.11403828130580376; 0.017197201332178638 0.018664122298682875 -0.07157993900843397; 0.04153623301926938 0.04950947556460381 -0.1938152230951588; 0.019419782869386393 0.022224635228102925 -0.10198151360377121; 0.009024700055455923 0.011918891140575972 -0.058898937482335004; 0.010268152058797412 0.016644086318738233 -0.08339655858414113; 0.002223229733475224 0.00269298639967064 -0.018336681131149033; 0.0010305072875583042 0.0017430073164449826 -0.010836370813143061; 0.0007175278905196367 0.0014132403505670312 -0.007713523760017391; -0.0002692774944626499 0.005345150933060389 -0.003632027046013879; 0.0018678966318318995 -0.00011383816028013102 0.004052179853752433; -0.0032065565472624573 0.0016355157624233355 -0.004700042568050299; 4.6812996462788393e-5 -0.002033290002364108 0.0013781845605912958; 0.0023541098554683546 0.0002751376464463903 -0.004879539766934976; 0.0007921629172804436 -0.002309861682056119 0.003145575824782301; 0.0010838963170429839 -0.004550149961678654 0.002610708118915039; -0.0020018372718101345 0.0025479119220221795 0.0027415917956967423] %
+
+Mass Used: 81.49586516172485 kg
+Launch C3: 98.00835343562576 km²/s²
+||V∞_in||: 1.8947391355297757e-9 km/s
diff --git a/archive/ES_0.5599003393515565 b/archive/ES_0.5599003393515565
new file mode 100644
index 0000000..ece3763
--- /dev/null
+++ b/archive/ES_0.5599003393515565
@@ -0,0 +1,22 @@
+archive/ES_0.5599003393515565---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T07:39:01.480
+Launch V∞: [8.074493217366086, -5.691101291770024, 0.09033004836977088] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0068593578402113e-6, -1.749708913310951e-6, -1.38347535599466e-7] km/s
+ V∞_out: [1.434518899115499e-7, -7.169173791657859e-7, -1.8869545917837164e-6] km/s
+ time of flight: 1.874957778749356e8 seconds
+ arrival date: 2030-04-24T09:48:38.480
+ thrust profile: [0.29287161872111994 -6.055079627278334e-5 -0.09813712711423095; 0.03604478227775285 0.01976676228863474 -0.04366740597914984; 0.030809371822090495 0.026921709526118266 -0.0667274857804933; 0.026094935393443673 0.029612127904012412 -0.08309975704468689; 0.023017616683851494 0.03139952502970215 -0.09833034554744673; 0.018128201001330894 0.028597772370972375 -0.09696092017910497; 0.013950262778913307 0.02503756923961814 -0.09204595005978904; 0.006727925040074278 0.013687592583395988 -0.05528049779585132; 0.01276847055332012 0.02856576701383411 -0.11520011774038423; 0.0023494908997235228 0.005689999715005604 -0.025729291258601836; -0.00022940839263453487 0.0006228622468817788 -0.009067442806357446; -0.00013182256516155067 0.002205478767107344 -0.00411879502104049; 0.0029581215389197332 -0.0018122934643584237 -0.006566099483652246; -0.0025247805034789555 -0.007698327502713905 -0.00013410407785421127; 0.000573445946915376 0.00022324127508208417 -0.0020300746715997907; -0.0007629321000878712 0.0028180999542542465 -0.004507296781944893; -0.007782958868723927 0.001898792815643654 0.004468398871000152; -0.0033618202371278757 0.005061734201928462 0.011078321947695391; 0.0010321688854505935 -0.003396263256296425 -0.0019385368488250747; -0.0006129151221820679 0.003965721637731209 -0.013630899395360413] %
+
+Mass Used: 83.9173633794735 kg
+Launch C3: 97.59423414811585 km²/s²
+||V∞_in||: 2.0234591887153637e-6 km/s
diff --git a/archive/ES_0.5599048989820288 b/archive/ES_0.5599048989820288
new file mode 100644
index 0000000..0d6fb48
--- /dev/null
+++ b/archive/ES_0.5599048989820288
@@ -0,0 +1,22 @@
+archive/ES_0.5599048989820288---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T04:55:14.102
+Launch V∞: [7.771691642764029, -5.86174791734037, 0.12852868771778758] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.287758987035163e-6, 7.285247214582585e-6, -5.291252070126382e-6] km/s
+ V∞_out: [1.6794679261124166e-6, 1.2045056650525471e-5, -5.400859030380413e-7] km/s
+ time of flight: 1.8548863775943276e8 seconds
+ arrival date: 2030-03-30T01:32:31.102
+ thrust profile: [0.3559302462779251 0.007142272437233222 -0.10065836653075706; 0.16889152735547108 0.10651847228338787 -0.15961819924059908; 0.08493431193241896 0.0876325396463655 -0.14710810060900853; 0.0561089512713329 0.07823241580464717 -0.1466747914165205; 0.02723785054163575 0.04747712848369264 -0.09930871849052576; 0.01320385347479879 0.02866455187469156 -0.06502709595426462; 0.006191717389101547 0.016667871089403465 -0.0404278768807236; 0.0019109130465952005 0.007620912547185106 -0.019688090450485016; 0.0003121897912565213 0.004084364293620002 -0.017649783012662353; 0.003412738834635065 0.005333117153399414 -0.01635428448813792; 4.373859230059649e-5 0.00034768420789662983 -0.0014483725232563856; 0.0012009068046575423 0.009958943410745125 -0.025910431770287755; 0.0015636767746360998 -7.842855892491174e-5 -0.005660008295956559; -0.0014663818194451585 0.0002695222379206618 0.0009518451668840662; 0.0005908776409989119 0.001138790663903146 -0.0008459911066103098; -0.0010941657553247327 -0.00235556938363668 -0.0033257011522702085; -0.00879736652896085 0.010459264005517943 -0.007238497335336055; -0.005379108068691662 0.0018014856107110059 0.001238790271103427; -0.0051740381514837 0.0031008790319565728 -0.0033256980234711206; 0.006461491642085111 0.0004974368087659374 0.006433925102681222] %
+
+Mass Used: 100.36355312775686 kg
+Launch C3: 94.77579926021888 km²/s²
+||V∞_in||: 1.223761106075782e-5 km/s
diff --git a/archive/ES_0.5599059415560108 b/archive/ES_0.5599059415560108
new file mode 100644
index 0000000..0e1b389
--- /dev/null
+++ b/archive/ES_0.5599059415560108
@@ -0,0 +1,22 @@
+archive/ES_0.5599059415560108---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T12:55:18.096
+Launch V∞: [7.713481012038095, -5.990076906495114, 0.22242672859613932] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.8350463605258904e-7, 2.2780403654391314e-6, -5.709211427325233e-5] km/s
+ V∞_out: [-2.5345200470609707e-6, 5.704803187426355e-5, -4.370891442511127e-7] km/s
+ time of flight: 1.7624898217081678e8 seconds
+ arrival date: 2029-12-10T10:58:20.096
+ thrust profile: [0.3882222750536482 -0.01879288309322783 -0.11623751300609167; 0.0872195125169261 0.045261212543003415 -0.08975931487115422; 0.0586533431920494 0.05035890713657215 -0.10647442714895683; 0.06426423948419391 0.07799604040090807 -0.17103717303084962; 0.04443487666042735 0.06338766702528077 -0.15562500508709645; 0.024034956604011677 0.04019093162345686 -0.10831760841176069; 0.014057859803609405 0.026645136687271666 -0.07783167873717807; 0.009789906308402195 0.020547514113916105 -0.06427408605759824; 0.002852817467459685 0.006886956731251549 -0.022005582596972113; 0.0004627323584442165 0.0016808347615466517 -0.006406014745410274; 0.000156235250552555 0.0010001106541396225 -0.003658557263460754; 0.0010639417330166867 0.0017688841995981365 -0.007571903693110901; -0.0005471471561669873 0.00035294704564344664 -0.0002190954336919843; -0.00104805245939364 0.00029243716609481053 0.00031269192444662367; 0.00016770671494607578 3.6098124222092064e-5 0.0004714796849135508; 0.0012293912667718098 -0.001122531535696111 -0.00016016225941006143; 0.00013601156041863444 0.002299694295998511 0.002669198969116907; 0.001321282837311248 0.0046945037903508655 -0.002049601558348894; 0.0034676322220692415 0.0006958428682937007 -0.0028602398977178923; -9.064391153822556e-5 0.003825244764226141 0.002368741434819645] %
+
+Mass Used: 96.55860662472423 kg
+Launch C3: 95.42828431839229 km²/s²
+||V∞_in||: 5.7138831418769376e-5 km/s
diff --git a/archive/ES_0.5599092513341924 b/archive/ES_0.5599092513341924
new file mode 100644
index 0000000..5ccf394
--- /dev/null
+++ b/archive/ES_0.5599092513341924
@@ -0,0 +1,22 @@
+archive/ES_0.5599092513341924---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T15:34:54.157
+Launch V∞: [7.724167206839574, -5.721064884464875, 0.25338305590864957] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.524554866084096e-5, -1.3111130791750352e-5, 9.81449744240045e-6] km/s
+ V∞_out: [-3.0765087323059072e-6, -2.2132830367262483e-5, 1.0361375731261689e-6] km/s
+ time of flight: 1.8043922828664973e8 seconds
+ arrival date: 2030-01-27T01:35:22.157
+ thrust profile: [0.6413357579989176 -0.03637201565811807 -0.19099143429959473; 0.16127053291500135 0.0835369581803525 -0.1704964017390493; 0.06867985592735086 0.05879370638962442 -0.13253968860579862; 0.03532619920431165 0.039876884991500064 -0.1012631835384621; 0.024298733240554784 0.03351817853318683 -0.09367173698963409; 0.016997825349286077 0.027767166800849504 -0.08386328499172775; 0.01206120519181689 0.022394693225117116 -0.07269341028802982; 0.0058741117341335435 0.01221739188062207 -0.042466738898105115; 0.0011408043062858854 0.002903844489777703 -0.010286206303287379; 0.003588379868627062 0.009127571392473171 -0.034788923038721185; 0.000833807692861506 0.0024994294632032284 -0.009243438727618788; 0.00030731113084670836 0.0004893533603433594 -0.004436032420099385; 0.00019367249033275567 0.0002591794799947274 -0.0012715693501053338; 5.967064803057522e-5 0.0006366239545654116 -0.0013955724647686375; 0.0002558707958069731 7.989896597682036e-5 -0.0020165995492243682; 0.0006895955267717721 0.0026776395495859296 -0.003312157256699804; -0.0002921866341278464 0.0005611105072445902 0.00012856598192838992; 0.0007494611801653764 0.0008688105517252751 0.0005066717732170202; 0.000585371825608977 0.0002614270537199393 -0.004088753727256323; 0.00042263627364090236 0.00057903507531182 -0.0004416461932020806] %
+
+Mass Used: 113.89177824700619 kg
+Launch C3: 92.45754542449457 km²/s²
+||V∞_in||: 2.2375273510179462e-5 km/s
diff --git a/archive/ES_0.5599100432117264 b/archive/ES_0.5599100432117264
new file mode 100644
index 0000000..a3a64b9
--- /dev/null
+++ b/archive/ES_0.5599100432117264
@@ -0,0 +1,22 @@
+archive/ES_0.5599100432117264---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:52:42.677
+Launch V∞: [7.911314179951788, -6.017759094668733, -0.026727635718284952] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.734319515696769e-11, -1.7191781619209153e-9, 5.045858781514892e-9] km/s
+ V∞_out: [7.999424448958911e-10, -2.7870710691424813e-9, 4.394504371976355e-10] km/s
+ time of flight: 1.7931176563400415e8 seconds
+ arrival date: 2030-01-19T01:42:07.677
+ thrust profile: [0.19828012283781588 -0.018348856936976448 -0.07654176979961007; 0.01744768008944485 0.006793959315272022 -0.02391698285352558; 0.03723525712745567 0.02342900896497454 -0.08467395081482401; 0.03640438585162595 0.028837617597223267 -0.11661666685946372; 0.03886399907702176 0.035762825266528936 -0.16335642492918503; 0.039359370473024256 0.037713024545934434 -0.20010169576123693; 0.014016175525634271 0.015098000245766447 -0.08457933252426612; 0.00755859257693244 0.007878385456149497 -0.04860702085168923; 0.001889748504684778 0.00169388557247563 -0.01726461009245456; -0.002716030600035756 0.0030658577073599098 -0.011463668454906472; 0.0010209961440107852 0.0004528983205559365 -0.004975469587983238; 0.0008693946029690992 0.0006724524960897867 -0.006772652938218986; -0.0022123343627331133 0.0008270326025869437 -2.3270242774960006e-5; 0.0006455924999834977 0.001011783557433324 -0.0038828263741713725; 0.0041627143238447345 -0.00011917173076896699 -0.00612531554212716; 0.00712066006385075 0.006920776899068598 -0.006292374901276541; 0.0025323442612339656 0.001981613377068885 -0.005226274292232807; -0.008270180371416438 -0.0036416903909828667 -0.00787017195131429; 0.001651959491212113 -0.0007117993768947528 -0.0038274095513745497; 0.002341826080739862 0.005573536835959769 -0.0026287620858661724] %
+
+Mass Used: 76.87736991934844 kg
+Launch C3: 98.80303094188557 km²/s²
+||V∞_in||: 5.33157951202644e-9 km/s
diff --git a/archive/ES_0.55991595813749 b/archive/ES_0.55991595813749
new file mode 100644
index 0000000..162fe85
--- /dev/null
+++ b/archive/ES_0.55991595813749
@@ -0,0 +1,22 @@
+archive/ES_0.55991595813749---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T19:48:58.963
+Launch V∞: [8.151482371911767, -5.7950685460335025, 0.15844213735062435] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.07865607694059e-5, 5.6681071227602865e-5, 2.060604618408218e-5] km/s
+ V∞_out: [7.273714022238043e-6, -4.80252397241813e-5, 4.880553625995793e-5] km/s
+ time of flight: 1.8749577787498447e8 seconds
+ arrival date: 2030-04-25T21:58:35.963
+ thrust profile: [0.09896841712351243 -9.803061296428204e-5 -0.03606745814983202; 0.03774712401090365 0.0219986111222685 -0.047381230085720566; 0.03180576044592639 0.02827951685704246 -0.07370173011711399; 0.02008623621869195 0.024537475390307675 -0.0669172083647478; 0.024094831274658605 0.029745499372930893 -0.10096712874849707; 0.015242240234162615 0.023185133520987736 -0.08998809005027479; 0.00770971181490044 0.014117353138799693 -0.057927326194086894; 0.005082245452992044 0.014772117508040012 -0.056316702482362174; 0.005537942693030587 0.014693533184022604 -0.0586862511099391; 0.003115786290700296 0.013003064643974539 -0.051916484504428845; 0.0013242998152393883 0.0030547714788129745 -0.01486393339056398; 0.012417768856851238 0.037584442546837134 -0.13450618648947613; 0.0004501633052043527 -0.0009724334641064835 -0.001503371037191807; -0.0005300257501559063 0.00032303894647857975 -0.00024672994315440137; 0.0003608378697574027 -0.0005264129752923906 -0.0015710979827896815; 0.0003430497639317433 0.0007214057329867304 -0.0010087041837086078; -0.001124645297572167 0.0006005124590718811 -0.000689213687196388; -7.210335877251927e-5 -0.00021840169116631142 0.0022991044308083002; -7.42458587836422e-5 -0.00029585687131688143 -0.0011964749259460049; -0.0002996790472770434 -1.2207287382566312e-5 0.002046276585678687] %
+
+Mass Used: 69.5835198554687 kg
+Launch C3: 100.05458822370336 km²/s²
+||V∞_in||: 6.771384864898346e-5 km/s
diff --git a/archive/ES_0.5599172251759453 b/archive/ES_0.5599172251759453
new file mode 100644
index 0000000..4f1d592
--- /dev/null
+++ b/archive/ES_0.5599172251759453
@@ -0,0 +1,22 @@
+archive/ES_0.5599172251759453---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T16:31:57.237
+Launch V∞: [8.06391056743193, -5.890598182306734, 0.11466060750944033] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.958075298767442e-6, -0.0006065455033292531, -1.1865526783890715e-5] km/s
+ V∞_out: [-0.0005849147686052108, 9.448230701567541e-5, -0.00013066663167767413] km/s
+ time of flight: 1.8749577787474155e8 seconds
+ arrival date: 2030-04-26T18:41:34.237
+ thrust profile: [0.12000351336599396 -0.003270287509282913 -0.04295092691704553; 0.028489799507071006 0.01388873620981342 -0.03379557645307247; 0.08597617321850509 0.06312281478250173 -0.17217298876742554; 0.03502640858702259 0.03310084272057829 -0.110385879601037; 0.017263802378259214 0.02060304638913103 -0.07351164819880456; 0.008687950083865794 0.011610368155371417 -0.0508923441120004; 0.026094112797612905 0.03323937361422019 -0.15035867215700185; 0.009133013036588568 0.011488982521255919 -0.059306156934289374; 0.002225274302462399 0.005826748617067204 -0.02210990673621536; -0.0017549501049068652 0.0013206628252868961 -0.0068733309549386425; 0.00487293517418935 0.001233763797296606 -0.016698093860636705; 0.0027952704259914182 -0.0004285035145541573 -0.010837773876763773; -0.0010755239351509052 -0.0017166271112429377 0.000874522654499508; 0.0008313464701455286 0.0009757425689765368 -0.007164797505020036; 0.00028675344062924733 0.0033199932732616228 -0.005276557474616524; 9.236644995211114e-5 -0.00024076480053667783 -0.007736330446627768; -0.005749460378679613 -0.003180035503355689 -0.001894004179916517; 0.000316078284161777 0.0017448867097437492 -0.003410394028119458; 0.0011346324830316303 0.0034381949620345626 0.00645646456814427; 0.006318553117535292 0.004650185163308907 -0.007764240396545706] %
+
+Mass Used: 71.42623480614338 kg
+Launch C3: 99.7389476398502 km²/s²
+||V∞_in||: 0.0006067432748687472 km/s
diff --git a/archive/ES_0.5599196135566241 b/archive/ES_0.5599196135566241
new file mode 100644
index 0000000..cd23de4
--- /dev/null
+++ b/archive/ES_0.5599196135566241
@@ -0,0 +1,22 @@
+archive/ES_0.5599196135566241---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T13:31:48.464
+Launch V∞: [7.986547000273277, -5.783402503718661, 0.18617231323910974] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.8532507817620485e-6, -3.3758261648580884e-6, 2.4511944643181627e-6] km/s
+ V∞_out: [-6.8147969748353e-7, -5.631079591084003e-6, 2.469090476720785e-7] km/s
+ time of flight: 1.8311592254639262e8 seconds
+ arrival date: 2030-03-02T23:03:50.464
+ thrust profile: [0.2987216471660606 -0.008723672636707846 -0.09520726959993266; 0.05804576627379025 0.03080932936433805 -0.07077256096824498; 0.03351332241813943 0.0255769895021095 -0.07171664934324688; 0.027944546863296605 0.030925903405947332 -0.08408458754448363; 0.02309973990954944 0.030856079175444775 -0.09756348389114895; 0.011372595672128366 0.021606854583638264 -0.0687323131043911; 0.012836350110480397 0.021269251293255725 -0.08560401372856696; 0.011659704932575343 0.017943448552647463 -0.07033310681654743; 0.014807133894878645 0.039459874342325986 -0.14531332463185206; 0.0011794439087214658 0.0024251056385748474 -0.010607756237861374; 0.0033185071545887845 0.007891089601654817 -0.03863917438975731; 0.002466944950978868 0.002429831831832815 -0.0076731077923113174; 0.00028164419890740915 -0.0007679942988063878 -0.0024685259275590357; -0.0008479398825606442 0.0005225372644430415 -0.006483340854533196; -0.0017929421871729612 0.0018463894334692177 0.0010253040097461972; -0.0006817599859295733 0.00015605361137693586 0.0011158813628757845; -0.002902686354273155 0.004717395139556362 0.0025168812559978253; 0.007616675753432197 -0.0025029231476573757 -0.0006251552726411781; 0.0007583426619647785 -0.000623558815863629 -0.005441093543740677; -0.0001357479722690954 0.0030735948309231573 -0.005669845770213298] %
+
+Mass Used: 85.84674626216884 kg
+Launch C3: 97.26733763781017 km²/s²
+||V∞_in||: 5.679093077630822e-6 km/s
diff --git a/archive/ES_0.559921470729198 b/archive/ES_0.559921470729198
new file mode 100644
index 0000000..21c1e5f
--- /dev/null
+++ b/archive/ES_0.559921470729198
@@ -0,0 +1,22 @@
+archive/ES_0.559921470729198---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:34:31.382
+Launch V∞: [7.959093251537516, -5.650777714427139, 0.17148011266225893] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.463467704214573e-5, 3.738431908984377e-5, -2.7204401391178486e-5] km/s
+ V∞_out: [9.272542898423925e-6, 6.292690948880335e-5, -2.8238730538462915e-6] km/s
+ time of flight: 1.874957778743462e8 seconds
+ arrival date: 2030-04-23T13:44:08.382
+ thrust profile: [0.48388725832216645 -0.0018808039764308866 -0.1512677541713091; 0.0436694324416731 0.023539787018164584 -0.055232420540408105; 0.03349930328025003 0.031285917330808495 -0.08027575151144728; 0.030029902149308188 0.033184424366283556 -0.09680980352387841; 0.015067711768338222 0.019949343046743517 -0.06853938812170236; 0.012734159431317282 0.020082023711825204 -0.08289180721002223; 0.014512785507115716 0.028827794352646773 -0.10729279387337286; 0.01435612330005058 0.02918588723678914 -0.11221197053445167; 0.00589260195398946 0.009494675546212394 -0.04254113418640382; 0.001206650325952146 0.002863654091424345 -0.010214834858603023; 0.0009996225861099214 -0.0004949590729754344 -0.01312277259222976; 0.0013991921713223015 0.0026842714617829225 -0.0026798521761736815; -1.5446997564529206e-5 0.004388166769896247 -0.002546835623675601; 0.0005028634027319494 -0.001702228730523381 -0.00036204717108320023; 0.001928542881912233 -0.0004753167801081096 -0.007150515542598648; 0.0010924767877137796 -0.00976858127353845 0.0018321368450699704; 0.002658534752814608 0.01191411868092979 0.009715188008367518; -0.0006919745754463614 -0.004180070757813344 0.009846603851416239; 0.0022804901453009627 -0.0021923819949660178 -0.002300011090741352; 0.0008293891728696901 0.004817658453888167 0.006563318546096571] %
+
+Mass Used: 97.27920155487618 kg
+Launch C3: 95.3078595935751 km²/s²
+||V∞_in||: 6.426446267977553e-5 km/s
diff --git a/archive/ES_0.5599248162909279 b/archive/ES_0.5599248162909279
new file mode 100644
index 0000000..850cf8a
--- /dev/null
+++ b/archive/ES_0.5599248162909279
@@ -0,0 +1,22 @@
+archive/ES_0.5599248162909279---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T21:57:22.933
+Launch V∞: [7.974177468692256, -5.711232820581853, 0.1333470293751383] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.430283583452618e-6, 6.5093899534734204e-6, 1.3237423278628631e-5] km/s
+ V∞_out: [1.2260591147731624e-5, 1.820246052223427e-6, -8.116087498075938e-6] km/s
+ time of flight: 1.874957778749441e8 seconds
+ arrival date: 2030-04-24T00:06:59.933
+ thrust profile: [0.376814030592999 -0.0020788117424942643 -0.12317960288305818; 0.053306726488533546 0.028572934194478542 -0.06183561077312488; 0.04475909854560108 0.03840048279029617 -0.09541745848802724; 0.03545614378982817 0.03857808786884789 -0.10885339313866037; 0.03790627970602467 0.05245461496367921 -0.15941853787349317; 0.020305453011564903 0.031375802471907854 -0.10386545806068272; 0.01341610840433826 0.02188450369594643 -0.07881954913339347; 0.005286868532637393 0.006252122250953916 -0.033445215534895635; 0.002585762825712673 0.004584877377504514 -0.021205723922245446; -0.0015570060454685062 0.005006805660523647 -0.005827999923587877; 0.000620794915776159 0.0030762633152648226 -0.0038381252315231786; 0.00017186616610517433 0.0025399995996457894 -0.002685502497261948; 0.0009222100974099436 0.003802518435996957 -1.8572683871142994e-5; -0.0056546339899940555 -0.007280925765740031 -0.004855193457111957; -0.0004603439607563664 0.0016158375793468038 -0.0033712794020858126; 0.005277437302454202 -0.00012525329408114363 -0.0017677832593229695; 0.001440745056637509 -0.0009567981479541461 0.004782290240696296; -0.00674682449370282 -0.0013156703735641056 0.013238424372915093; -0.0022237319320500453 -0.0016308877073920847 -0.01286860528855708; -0.016437495862873724 0.008919889243123322 0.008715331738280431] %
+
+Mass Used: 91.94205530330237 kg
+Launch C3: 96.22346806333375 km²/s²
+||V∞_in||: 1.4820500792923764e-5 km/s
diff --git a/archive/ES_0.5599268174953772 b/archive/ES_0.5599268174953772
new file mode 100644
index 0000000..669fb5c
--- /dev/null
+++ b/archive/ES_0.5599268174953772
@@ -0,0 +1,22 @@
+archive/ES_0.5599268174953772---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T13:33:17.871
+Launch V∞: [7.838505367040118, -5.552129658095689, 0.19497700276897992] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7119354479566693e-9, -1.6243113788003198e-9, -2.212275595421855e-9] km/s
+ V∞_out: [-5.933415161101341e-11, 2.2089757965300707e-10, -3.5132800648274965e-11] km/s
+ time of flight: 1.8749577787414142e8 seconds
+ arrival date: 2030-04-19T15:42:54.871
+ thrust profile: [0.6033921787018819 0.011778088988494053 -0.15266955801049978; 0.1827464835340827 0.11884142487686405 -0.1687241229567753; 0.06362550823180739 0.06918926420005336 -0.11430347249705171; 0.04674454457916485 0.06946660345721992 -0.12742336341326788; 0.022754284271643343 0.043457468212954 -0.08920593090788888; 0.007041409464842238 0.017477662633285956 -0.03999876412233613; 0.015076104319713957 0.03591381679969066 -0.07444516184328576; 0.003046678429530025 0.012826746047533907 -0.0324280164048329; 0.0030734387005746963 0.01737878635793189 -0.044505559276320474; 0.00020779304176290643 0.0010333473247381715 -0.002905732348465883; 0.0005179470940825895 0.000627030934369373 -0.002557737009963972; 0.0005179586138297025 0.0013242004937793705 -0.004354590639574515; 2.2669060490550885e-5 -0.000641251219625781 0.0002535929302903184; -0.0002020088133721074 -0.0005243774260255316 0.001182412572113192; -0.0010084823844623847 -0.001060462814569633 0.0010290557053527312; 0.0008479151687394102 0.00036723599818473185 0.00016720097993027283; -0.0008155706346473173 -0.0010378526989031581 0.0024527292786533576; -0.0007932784886321522 0.00023555961917710188 0.001745340345193996; 0.0002289231639398647 -0.0014359248737831345 0.005109700182783195; 0.0008453740570493457 0.00034215200303615084 4.648107613319536e-5] %
+
+Mass Used: 114.79438447192433 kg
+Launch C3: 92.30632616103127 km²/s²
+||V∞_in||: 3.234698400681263e-9 km/s
diff --git a/archive/ES_0.5599332747050478 b/archive/ES_0.5599332747050478
new file mode 100644
index 0000000..6eea5e6
--- /dev/null
+++ b/archive/ES_0.5599332747050478
@@ -0,0 +1,22 @@
+archive/ES_0.5599332747050478---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T19:33:27.176
+Launch V∞: [8.069930946745488, -5.477217276860312, 0.2031081321696416] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.553486091438842e-7, 1.0840056317806735e-6, 1.1066405398505559e-7] km/s
+ V∞_out: [-9.70127193042063e-8, 4.7498093870019994e-7, 1.2339460577352113e-6] km/s
+ time of flight: 1.87495777874208e8 seconds
+ arrival date: 2030-04-20T21:43:04.176
+ thrust profile: [0.48889446674819137 0.0005344241722814273 -0.12782781673036653; 0.05264649766687992 0.03165451968832183 -0.05595331252274616; 0.044835336321088784 0.045328977568643576 -0.08686935776761286; 0.02664923094271903 0.03634676466879029 -0.07991091895248358; 0.023857459786144494 0.04225187179840019 -0.09611496920868284; 0.023593035298760348 0.04891384079023071 -0.1266878597599132; 0.009112902330574853 0.021647303725832186 -0.0604390949206566; 0.007178344616086762 0.022626544078396656 -0.07106617512880815; 0.005159315293649882 0.013083949916582543 -0.04492236631406134; 0.00028114100977828815 0.0023288249929179577 -0.010148721851370326; 0.0014313822272225725 0.012364860571763583 -0.027971649339698736; 0.0006809063097082055 0.002969203092509224 -0.010187719018139302; 0.0011425261049826485 -0.004223822842322988 -0.003220674513846197; -0.0013460992361714625 0.0010228959530954912 -0.0021250114080852544; -0.0036271276368089935 0.002164718064695129 -0.0024582011925901506; -0.001335210903257031 0.00032676062518670497 -0.0032102699611463743; 0.0003210322352822384 0.001543734659379882 -0.008179175858286179; -0.000776751859665486 -0.005671673865112251 -0.008145524467796117; 0.0011668711301878096 0.003362839645359843 0.0035619896810709707; -4.242998784186885e-5 -0.0019827046941467592 -0.0015967566247817627] %
+
+Mass Used: 98.12662675945785 kg
+Launch C3: 95.16494749653107 km²/s²
+||V∞_in||: 1.3258454902107654e-6 km/s
diff --git a/archive/ES_0.5599427635500015 b/archive/ES_0.5599427635500015
new file mode 100644
index 0000000..907055e
--- /dev/null
+++ b/archive/ES_0.5599427635500015
@@ -0,0 +1,22 @@
+archive/ES_0.5599427635500015---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T15:44:15.531
+Launch V∞: [7.751435368186276, -5.968794676850366, -0.04372141971457738] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.248032099178321e-5, 6.699295781736044e-5, -4.900531248627313e-5] km/s
+ V∞_out: [1.6764774743165093e-5, 0.00011613282776536268, -5.535718027177049e-6] km/s
+ time of flight: 1.7714972301629332e8 seconds
+ arrival date: 2029-12-21T23:59:38.531
+ thrust profile: [0.3672536335985959 -0.025799743121964123 -0.1234991127930607; 0.11018963657477064 0.04918432755634746 -0.1260143104985985; 0.06672703328555873 0.048716855343336925 -0.13472568514865088; 0.04432307953879051 0.04169155918735879 -0.12900515214159824; 0.03167098261295587 0.03541671842073142 -0.12097866039842695; 0.026766314924542012 0.03425443567115284 -0.1283275551646832; 0.011819357470362859 0.016845211827460637 -0.06579774984446263; 0.0049615281984539345 0.008328506725956152 -0.03231636617444928; 0.004660095031127458 0.007964810341005334 -0.03346028866430397; 0.00156218743848411 0.0037354641343644857 -0.014142844801404101; 0.0007080991689474904 0.0025670335211354037 -0.01268601397130003; 0.0006993698684746632 0.0012409430738666858 -0.00796489869492218; 0.0006970511546891456 0.0013643714603389907 -0.007183759982318948; 0.0007228256351365784 -0.0017118755158357524 -0.004400280249477788; -2.1429137942574302e-5 0.002268471600888171 -0.0006483893018316151; 0.0032992843885765637 -0.0047187791576320335 -0.004972985057936466; -0.0002224086054725234 -0.0022102358953217686 -0.009774764270600996; 0.0015592783215374918 0.002193192568310837 -0.005213247486142555; -0.0011973776760262657 0.00036697952273028215 -0.0004555476958610523; 0.003401719983212444 0.0009436755973765798 -0.0028076937196730043] %
+
+Mass Used: 94.9397224177037 kg
+Launch C3: 95.71317172410824 km²/s²
+||V∞_in||: 0.00011701529985392297 km/s
diff --git a/archive/ES_0.559953893138373 b/archive/ES_0.559953893138373
new file mode 100644
index 0000000..c26e032
--- /dev/null
+++ b/archive/ES_0.559953893138373
@@ -0,0 +1,22 @@
+archive/ES_0.559953893138373---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T22:28:40.470
+Launch V∞: [7.825698578001556, -5.842497128584222, 0.16084298556185872] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006542003711666928, 0.039240308194552403, 0.042245506250138995] km/s
+ V∞_out: [-0.010327538967106423, 0.010348838132052122, -0.05605781060498207] km/s
+ time of flight: 1.788311991970306e8 seconds
+ arrival date: 2030-01-08T17:48:39.470
+ thrust profile: [0.3965484249392587 -0.011419424190678016 -0.10521668474882803; 0.06636514678479756 0.03726012531603384 -0.06475683138166415; 0.07690924353552135 0.07280767551032151 -0.1296282702328527; 0.07014236711598675 0.09013452715824191 -0.17233418658191227; 0.017583504229407746 0.027587692753956325 -0.061567169578955784; 0.04035819946385313 0.07700081306911363 -0.17089948629735535; 0.012511773670102429 0.027618325260604145 -0.06978915650192238; 0.011903708299768886 0.03027459090462784 -0.07973483469905984; 0.0022501123052507104 0.0065583014703080094 -0.019248430263548954; 0.001342746151278714 0.0012544870842299363 -0.007139978421048496; 0.00016033070898975414 0.002435273337525387 -0.0019928016217108393; 0.00035087641844251433 0.0014652533861722714 -0.005394338759302623; -0.00011774653329634318 0.0002960977287704781 -0.00026652902286388347; 7.81573388318547e-7 0.00030475743203367935 -0.0004822102558938255; -0.0008847052130715697 0.0008677540338704289 -0.001722412603836422; 0.0011974473701497068 -0.0019101590567753906 0.0011126191263299914; -0.0003439215223171659 0.002664111237399732 -0.0013124234432208975; -0.0010872995691403966 -0.002507358982096306 0.0009373902870980205; -0.00036955945497280925 0.0020102429654688717 -0.0007059226750003223; 0.00032048448274500814 0.0003224502874649497 -0.00022216921148060476] %
+
+Mass Used: 96.76670051078145 kg
+Launch C3: 95.40220139725491 km²/s²
+||V∞_in||: 0.05802828963615465 km/s
diff --git a/archive/ES_0.559954893000161 b/archive/ES_0.559954893000161
new file mode 100644
index 0000000..9298b2a
--- /dev/null
+++ b/archive/ES_0.559954893000161
@@ -0,0 +1,22 @@
+archive/ES_0.559954893000161---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:18:54.066
+Launch V∞: [7.96661992892456, -5.534070237532715, 0.039340749171803635] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.500225357048097e-7, 2.929256213762391e-6, -7.26026571690188e-5] km/s
+ V∞_out: [-3.0060745910892143e-6, 7.250287820509177e-5, -5.311746608349074e-7] km/s
+ time of flight: 1.8749577787491006e8 seconds
+ arrival date: 2030-04-21T12:28:31.066
+ thrust profile: [0.5748161381065026 -0.0014577487224469922 -0.17384165159359471; 0.034775688960957805 0.02062452094558 -0.039417783810619465; 0.03580357553266859 0.03455536726339021 -0.07303398556545235; 0.055444896199353486 0.07120244174920777 -0.16438044202998248; 0.026132884979049437 0.041589979947782 -0.10820042583187182; 0.01202074664723695 0.022879343947527796 -0.06580744159896883; 0.008616198795073533 0.019203013730450403 -0.059318624600290214; 0.007009171380817531 0.017942965861281402 -0.058603275285271796; 0.00473902450646554 0.013840148798557729 -0.04774061868423193; 0.002158934086617346 0.005460647157186811 -0.01817904101890477; 0.0007082435704583646 0.00284211411914226 -0.010974278892932818; 0.00013064746980396994 0.0010050189886555087 -0.0016441955966052437; -0.0032485439643916347 0.001974324358055855 -0.012721067498451706; 0.003330175434651917 -0.0009944948568030442 -0.0002259714919944189; -0.001026919760658847 -0.0018140679370466403 -0.003623901383052963; -0.0015110426015378254 0.0010536589309109142 -0.00441896969304873; 0.007449619903176904 0.003928215923281452 -0.009105079936131532; 0.0021803251847405613 0.006735339560926054 0.0016953475204173143; 0.0018836187149906419 0.004073998759528317 -0.010091435122372006; 0.0003072540150999164 0.002833655277050098 -0.012141207051885379] %
+
+Mass Used: 104.3960424476868 kg
+Launch C3: 94.09451418042876 km²/s²
+||V∞_in||: 7.266311918883323e-5 km/s
diff --git a/archive/ES_0.5599550696003058 b/archive/ES_0.5599550696003058
new file mode 100644
index 0000000..bbe1e7d
--- /dev/null
+++ b/archive/ES_0.5599550696003058
@@ -0,0 +1,22 @@
+archive/ES_0.5599550696003058---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T07:17:30.202
+Launch V∞: [7.669610231377511, -5.750858631671818, 0.1489037084085173] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.845507225505409e-6, -2.6202111257342932e-6, 1.8315224001987812e-6] km/s
+ V∞_out: [-5.547417232835971e-7, -4.2370125652386735e-6, 1.9082348502894844e-7] km/s
+ time of flight: 1.846909790297193e8 seconds
+ arrival date: 2030-03-17T22:20:29.202
+ thrust profile: [0.5828797177198765 0.018112300620691676 -0.1347897648025577; 0.20782144603295385 0.1392856350862457 -0.1740186310359761; 0.0735973096368548 0.08086370614823127 -0.1185018162538162; 0.047474764589553735 0.07085169988949708 -0.11715403523322208; 0.03351269872985459 0.06567969620432114 -0.11654018335032096; 0.016519521924707802 0.03982365744148439 -0.07798355848246846; 0.00484751286144145 0.014621913306405956 -0.03138795734947115; 0.008692020755739301 0.03168976210328491 -0.06841322014791797; 0.0022861627946694197 0.010486100444986173 -0.024770800113846622; 0.0006482416243627525 0.0007291185300435047 -0.000859514047827886; 0.0004390684102222271 0.001024394030179343 -0.0021520083750238006; 0.0001701596366512711 0.0003053315863925798 -0.0008502125422577681; -1.117602923180671e-5 0.00024199902538549962 -0.0001963547199850665; -7.382463364102438e-5 -0.0004433748276320555 -0.0017715154521581473; -0.00016738677223483464 -0.0010648402947969343 8.66729435319444e-5; 0.0008554988429353517 -0.0007736740969721867 0.0006537063680457271; -0.00018566802809900053 0.0005175119883202979 -0.0010726464922583496; 0.00025905634859273776 0.0021221455866172823 0.00020589723579372506; 0.0012771029806037462 -0.0009101676545413654 -0.0021793387382602466; -3.931033470975835e-5 0.001838944358734311 -0.001961534447966551] %
+
+Mass Used: 117.09568210059115 kg
+Launch C3: 91.91746841710268 km²/s²
+||V∞_in||: 4.279823830048985e-6 km/s
diff --git a/archive/ES_0.5599650606154125 b/archive/ES_0.5599650606154125
new file mode 100644
index 0000000..9a72430
--- /dev/null
+++ b/archive/ES_0.5599650606154125
@@ -0,0 +1,22 @@
+archive/ES_0.5599650606154125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T01:10:31.686
+Launch V∞: [7.8771034277692475, -5.820225267993084, 0.2564559511899599] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0026950109318406e-9, -1.1658685273514379e-9, -1.2520110839454215e-9] km/s
+ V∞_out: [6.242012413609072e-10, -5.659638328933177e-10, 2.156737506586749e-10] km/s
+ time of flight: 1.841215351865021e8 seconds
+ arrival date: 2030-03-15T02:02:46.686
+ thrust profile: [0.4040550482474197 -0.011927442295584218 -0.12123232829918702; 0.04197137278360009 0.021983885287187987 -0.047104512998925506; 0.03999513899189928 0.033961328324860235 -0.07932860692760892; 0.04004932005128981 0.04350361498979314 -0.11347323367069306; 0.031622521188568994 0.04132392117618764 -0.11885117925401309; 0.033284447662552334 0.0506305125977313 -0.1540616030390414; 0.009953743261259224 0.016783725307606447 -0.06085481279240907; 0.009004806343484837 0.013836296643551382 -0.05501806659819448; 0.00430604255155535 0.006512268214697726 -0.033946914025634295; 0.00023829199574896577 0.004725596995181843 -0.01728530389663191; 0.002894721642542951 0.004258312769828579 -0.01176585731737973; 0.002420415652049536 -0.0008024871862408163 -0.00870590672359215; 0.00393820715217928 0.0017187455013228288 -0.007284435186137254; 0.0006763835531051108 0.00047662361396283296 0.0021919997038276164; -0.008924017326547906 0.004956410218822942 -0.009091583380807436; -0.002221632090708251 0.004297409270838349 0.002677170740610427; 0.002104365922487932 0.002048147637926092 -0.010047046793313252; -0.0005630366122918549 0.003001036920764326 0.004444711644107452; 0.002384423076112683 -0.004844818671501815 -0.010630752444639248; 0.0022829722915833897 0.00535159306278083 -0.010865373976235895] %
+
+Mass Used: 93.3535276696316 kg
+Launch C3: 95.98955023685994 km²/s²
+||V∞_in||: 1.9829721284824966e-9 km/s
diff --git a/archive/ES_0.5599696876894416 b/archive/ES_0.5599696876894416
new file mode 100644
index 0000000..072d279
--- /dev/null
+++ b/archive/ES_0.5599696876894416
@@ -0,0 +1,22 @@
+archive/ES_0.5599696876894416---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:49:06.684
+Launch V∞: [7.732315989347829, -5.835304117159599, -0.23485720326158935] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.903544526279417e-9, 3.3273367529621754e-8, -6.532864299459939e-9] km/s
+ V∞_out: [1.1844381387378015e-8, 2.4935887760191185e-8, 6.147005374025829e-10] km/s
+ time of flight: 1.8586239633569118e8 seconds
+ arrival date: 2030-04-02T14:15:42.684
+ thrust profile: [0.4336598232973445 0.01961164071423834 -0.11310099277669493; 0.15672435045976016 0.10832501959237723 -0.14083935884808088; 0.05661342526185334 0.065057343717179 -0.0973119094943638; 0.07085452623884393 0.11468031590664493 -0.1788479254103737; 0.01743641638827611 0.036195666730247725 -0.06683550415846187; 0.02538626836516477 0.06753133815025698 -0.1271706843647804; 0.009521585524072037 0.030217583130539658 -0.06291305632433769; 0.0024937072118230755 0.008831320059132902 -0.019249538735545836; 0.002395624721780991 0.012379304451921204 -0.028757072741814542; -0.0014544420137485995 4.607298704803952e-5 -0.002607526098372892; -0.00044415358895187476 0.0032701598408734584 -0.005639533893784467; 4.7614548015226645e-5 0.0016320096402062873 -0.003033230880191469; 0.0020214796209980183 -0.0007349006720515404 -0.0012742041824181172; 0.0013459584449659113 -0.0009710237529448945 0.0009482800824531; -0.0025478927354947944 -0.002284986185936511 -0.0014529584062174137; -0.00016225745438111223 -0.0010411721270718564 0.0004706107364408022; 0.0007835904719863447 0.0009458345422398184 -0.003960086243288574; 0.0015254022755165518 -0.0009099782843719084 -0.007661042574360159; 0.002502945118460313 0.003462739692984566 0.0013128777623232788; 0.0005113036564237547 -0.0005570068888192744 0.0006350363143744623] %
+
+Mass Used: 105.5792204430868 kg
+Launch C3: 93.89464260478772 km²/s²
+||V∞_in||: 3.413257919620332e-8 km/s
diff --git a/archive/ES_0.5599849355811296 b/archive/ES_0.5599849355811296
new file mode 100644
index 0000000..80d0ad7
--- /dev/null
+++ b/archive/ES_0.5599849355811296
@@ -0,0 +1,22 @@
+archive/ES_0.5599849355811296---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T14:32:59.970
+Launch V∞: [7.6611097328929185, -5.6743661431122465, 0.1765986452305636] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9939009267161533e-7, -2.3330449025464065e-6, 3.842516513746634e-5] km/s
+ V∞_out: [1.2999341405237527e-6, -3.90343474150814e-5, 3.555617633050724e-7] km/s
+ time of flight: 1.8749577805060646e8 seconds
+ arrival date: 2030-04-19T16:42:37.970
+ thrust profile: [0.6113096384122355 0.020714901793575567 -0.14918273122412445; 0.2897035135157394 0.19938583708425112 -0.24611356415769117; 0.07652038785498312 0.08878841584680212 -0.1314781483562864; 0.0467981146287114 0.07543963575288236 -0.12495216234541796; 0.015165518600889473 0.030433760829224565 -0.057990400319192725; 0.011009288807147863 0.02784479780557618 -0.057125409933124746; 0.005771785205948972 0.018249920580218692 -0.039958323314752145; 0.002793540437124111 0.010640768309543379 -0.02497916917267584; 0.00036412756914605055 0.0014462647542553143 -0.0038935638721721367; 0.00189770488021537 0.01057258608458752 -0.026495335084788213; 7.96276575812632e-5 0.0008392132201218967 -0.002452178450443563; 0.00032973972623307705 0.0010426878647550608 -0.0042487364165019114; 0.0006359084495944256 0.0012896971765256023 -0.0008730664692014041; -0.0003935868433849951 0.00010587907787989537 -0.0013504809109196755; 0.000729137598058217 0.0007030581225011649 -0.001097106609758015; -0.002630100828347684 -0.0012417904305967206 -0.002364709105847027; -0.0017213029825511568 -0.0007797140863735688 -0.001127581540535036; -0.0013460332649659458 0.0021268802592642366 -0.00044782143154856527; -0.0014339015050606986 -0.0011312291936568012 0.00017202283838042409; -0.00014439903361710305 -0.00013119605648117765 0.0003362284769671659] %
+
+Mass Used: 122.93613832035362 kg
+Launch C3: 90.92222054702243 km²/s²
+||V∞_in||: 3.849709143281407e-5 km/s
diff --git a/archive/ES_0.5599869331175109 b/archive/ES_0.5599869331175109
new file mode 100644
index 0000000..120bf63
--- /dev/null
+++ b/archive/ES_0.5599869331175109
@@ -0,0 +1,22 @@
+archive/ES_0.5599869331175109---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:23:56.701
+Launch V∞: [7.719858429536628, -5.884518918633172, 0.2785875024651324] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0030988111858265086, -0.017863859169018982, -0.01868489827080551] km/s
+ V∞_out: [0.004725498693439909, -0.0008875335551693932, 0.025626759043605646] km/s
+ time of flight: 1.8557577096763578e8 seconds
+ arrival date: 2030-04-01T11:13:26.701
+ thrust profile: [0.45499072018617265 -0.02064120851729164 -0.12637565468320858; 0.18811561870344629 0.09936175106904468 -0.19391192195659437; 0.04274404567901756 0.036444880604083386 -0.08558710392098592; 0.04210289171534549 0.046949764999678414 -0.12284104872646921; 0.022460890849718553 0.029134464217730357 -0.08792030706541683; 0.013528076939179038 0.021174885065317915 -0.06716249584833445; 0.010568584725519699 0.019614853728930567 -0.0683217872291317; 0.005007373827796174 0.009457668149278156 -0.03173340333733281; 0.003078725720953061 0.0045358997203127464 -0.013907266721948617; 0.000547556210475122 0.006291460810464326 -0.018386809230273728; 0.014071869297447557 0.00584741964518499 -0.022484280842645935; -0.0012337304223165532 0.006609534361058043 -0.0060589517793280066; -0.001344069254313537 -0.0037256461546745275 -0.008374194137854661; -0.008187630603293397 -0.004509505356814691 -0.0032182315336238875; 0.0007909323148137895 0.008883278451788417 -0.01299175888887652; 0.0006009524158537209 0.00041777189293883414 -0.002375695167958089; -0.0001764535718535204 -0.002137877105817509 0.001891730017080965; 0.00014472135012710168 0.0002614663243051007 0.00020481078469779344; -0.006672513978395587 0.008398749349707638 -0.0045809328554849305; 0.00041783500586104784 -0.0004609599500921441 -0.00035246172629163636] %
+
+Mass Used: 103.22665821494229 kg
+Launch C3: 94.3013880723692 km²/s²
+||V∞_in||: 0.026035466551730883 km/s
diff --git a/archive/ES_0.5600005437372004 b/archive/ES_0.5600005437372004
new file mode 100644
index 0000000..6f6a42a
--- /dev/null
+++ b/archive/ES_0.5600005437372004
@@ -0,0 +1,22 @@
+archive/ES_0.5600005437372004---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T23:21:27.522
+Launch V∞: [7.844928685606438, -5.618616271782927, 0.17585150760707197] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01701446094941096, 0.009526715687596459, 0.0006931568589143391] km/s
+ V∞_out: [-0.012818470362200372, -0.008345448975670196, 0.01217416989282566] km/s
+ time of flight: 1.87495777875214e8 seconds
+ arrival date: 2030-04-20T01:31:04.522
+ thrust profile: [0.5469825940041941 0.03228879504109832 -0.12184732103678539; 0.11860033306281227 0.08436896303888752 -0.1054976937783428; 0.07121909700351305 0.08430478055659038 -0.11638522340935602; 0.041379381487196464 0.06737870219335566 -0.10432327579905122; 0.027448771687977276 0.05811009710378207 -0.09840293444206905; 0.019453960910849638 0.051795894743187604 -0.09398258420061181; 0.01855583540983942 0.0629367901407297 -0.11778193090688485; 0.0013593150526123392 0.006048770583830084 -0.013010679418553233; 0.001159373273398182 0.006454580659344217 -0.014410198921822494; 0.0011636916919448455 0.009304261435816273 -0.02175774925173087; 0.00030090308445538446 -7.768423710002186e-5 -0.0008453281894284217; 0.0020383575423810517 0.0015554351490585836 -0.002360457190815079; -0.00020971783620356442 -0.0005063657474026669 0.0004250957229655662; 9.096925595980866e-5 -0.0004677538844474749 0.0013295964780742832; 0.0012276921077163628 -0.0005534807390787548 -0.000568053262775333; -0.000268678441049578 -0.00017558472740215381 0.0005767424125725264; -0.0022521329832361848 0.00514460471197009 -0.0033680880334286062; 0.0017243953793143062 -0.0007021531531857805 -0.002306516623553399; 0.00028839969056297416 -0.002010273272725376 -0.001889254630775077; -0.0003957524680167075 -5.5796281303119e-5 -0.00474529725380292] %
+
+Mass Used: 110.00167560035379 kg
+Launch C3: 93.1426786445223 km²/s²
+||V∞_in||: 0.01951232071339509 km/s
diff --git a/archive/ES_0.5600070126940064 b/archive/ES_0.5600070126940064
new file mode 100644
index 0000000..e89c594
--- /dev/null
+++ b/archive/ES_0.5600070126940064
@@ -0,0 +1,22 @@
+archive/ES_0.5600070126940064---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T07:05:42.336
+Launch V∞: [7.9744692034576445, -5.6506999552754165, 0.1498341891142979] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.737106076543374e-6, 8.022830333576302e-6, -5.617974117303346e-6] km/s
+ V∞_out: [1.5831679632552342e-6, 1.301533623551505e-5, -6.028047983504623e-7] km/s
+ time of flight: 1.8749577787647316e8 seconds
+ arrival date: 2030-04-21T09:15:19.336
+ thrust profile: [0.3009347198490458 0.009995485072657203 -0.08119822559913245; 0.17938225553331702 0.12033655132427098 -0.16532657748264992; 0.08108357086294357 0.09141493518443426 -0.14455465559701894; 0.0337024104879598 0.051148746960542474 -0.09615789592036028; 0.019007196829257694 0.03661194300377513 -0.0764239300715536; 0.011794619542177677 0.02954542259020778 -0.06683282521028966; 0.013461798595313023 0.038689473034890585 -0.08929498330347929; 0.0027066566684510918 0.012839079803462671 -0.03440361766291639; 0.0028989988054827338 0.011282079636036054 -0.03087232115419639; -0.00017077449308101 0.003876226274171608 -0.007079091616376059; 0.00102257665308274 0.005744224237774407 -0.017497166728275004; 0.0004723215541585268 0.0032845640505053705 -0.004422856854750586; 0.0008709194543814996 -0.0007427516561307086 -0.00024553231847938546; -0.0006397910157900521 0.0010890475854166157 -0.002821570626618682; -0.00024215557358055683 0.00025520542683592185 0.0001947163286819309; -0.002877853047362282 -0.0024675700226793854 0.004780881401556096; -0.0014051077529198843 -0.002547711131372807 0.005522897673600969; -0.0040478883785546515 -0.0015805580557802274 -0.0016907593577549786; -0.0007850539848072037 -0.006340831159477838 0.004073323886625231; 0.008021715976497194 -0.0005555254438513384 0.002442092312023119] %
+
+Mass Used: 95.99556862659028 kg
+Launch C3: 95.54501934567153 km²/s²
+||V∞_in||: 1.312495570799435e-5 km/s
diff --git a/archive/ES_0.5600152936704055 b/archive/ES_0.5600152936704055
new file mode 100644
index 0000000..61c657c
--- /dev/null
+++ b/archive/ES_0.5600152936704055
@@ -0,0 +1,22 @@
+archive/ES_0.5600152936704055---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:20:23.119
+Launch V∞: [7.956732759833716, -5.582668797787937, 0.1898722211164827] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6404902831304344e-9, -7.786738976715708e-11, -5.682680582146815e-10] km/s
+ V∞_out: [9.76805179062555e-10, -7.139096496153755e-10, -5.93870478067325e-10] km/s
+ time of flight: 1.8749577787471613e8 seconds
+ arrival date: 2030-04-19T17:30:00.119
+ thrust profile: [0.4046349609505755 0.01905847768378913 -0.09651277475646815; 0.15774731110147558 0.11274980470654986 -0.1354628377212629; 0.067120306892142 0.08070627876854986 -0.11174034246212965; 0.054334514579795615 0.09101037977643722 -0.13692486653330577; 0.036802124910846536 0.08016707773363897 -0.1323999848796748; 0.010728513328168059 0.030763878029976124 -0.059132981023344855; 0.007852706010007565 0.02989037267087798 -0.058793088589345226; 0.0047833270087636265 0.019647762806647765 -0.044722633750739926; 0.0025097555859229853 0.011649203831070775 -0.02509125519060137; 9.810714885539143e-5 0.00021197715888701836 -0.0013260872417469186; 9.695363033138217e-5 4.708698866122602e-6 6.747331460415585e-5; 0.00016364517052377045 0.00014635494913496427 0.00029165710210131445; -0.00020841135175774775 -0.0007150467002401085 -0.0005531551858579472; -5.4819110324114595e-5 0.0006799585543226308 -0.0014583744634044306; 0.001160777686659555 -0.000974817112103091 0.0006537003418269156; -0.0007984034990295971 0.0007798871556691706 0.0016131919940809468; -0.0004258032119940583 -0.0017078044778460705 -0.0004748922867346216; -0.00027135797846957463 0.000635116825881635 -0.00016309196048702387; -0.0012474297044015679 -0.000644132967680312 0.002793529145154105; -0.002830292906502924 0.0012045899668355507 0.002039142570176561] %
+
+Mass Used: 102.0321175797194 kg
+Launch C3: 94.51183857755777 km²/s²
+||V∞_in||: 1.7378723443974842e-9 km/s
diff --git a/archive/ES_0.5600313368869642 b/archive/ES_0.5600313368869642
new file mode 100644
index 0000000..2c249ec
--- /dev/null
+++ b/archive/ES_0.5600313368869642
@@ -0,0 +1,22 @@
+archive/ES_0.5600313368869642---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T22:22:32.192
+Launch V∞: [7.788812193379987, -5.536643699715765, 0.2354264010943612] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.94061388219021e-5, -1.7430546576661028e-5, 1.3116636684335466e-5] km/s
+ V∞_out: [-4.008896788397077e-6, -2.8858506220041878e-5, 1.425970963919916e-6] km/s
+ time of flight: 1.8572778376606703e8 seconds
+ arrival date: 2030-03-29T13:25:35.192
+ thrust profile: [0.7845346284861022 -0.014788070663948338 -0.17963073221592385; 0.0636839841292947 0.04016696325662747 -0.06326119150778466; 0.07199374721916964 0.07538212727064984 -0.12973319366530953; 0.03199372287058275 0.045934650357997965 -0.0886969094249771; 0.042429893274381555 0.07724710499139825 -0.15933613573859667; 0.013951657614369476 0.031127365690492143 -0.07086063068159036; 0.01016267705321994 0.02633896870580275 -0.06358329107568067; 0.00653289908080568 0.021354218237701825 -0.05699609580804924; 0.0022923524492233223 0.007160811207256218 -0.017255720676606398; 0.001126470531959106 0.005118713633828507 -0.014733040566537483; 0.0005439104120379572 0.0012342136565331669 -0.004676174413331489; 0.0001829538984220047 0.0013693773964581113 -0.004910922806571325; 0.0002874587821226061 0.0011902398178714527 -0.0002772056072177693; 0.0002306270641863965 -0.0008186566683732463 -0.0001650719784206335; -0.0003975972875089891 0.0012424657486584988 0.0007198886735435069; -0.0008611746742799452 -0.0003176994627010128 -0.00017509639123714491; -0.0001571307227098568 -0.000673580182007816 0.0021026007067950223; -0.0007417438346474362 0.00014187326746782148 -0.002732564046401764; 0.0005591120670589954 0.00015748522067174684 0.0036856527132743877; -0.0006696783111766504 -0.0010468209438973814 -0.003169021309379362] %
+
+Mass Used: 120.34646718332897 kg
+Launch C3: 91.37544443167928 km²/s²
+||V∞_in||: 2.9197060397323222e-5 km/s
diff --git a/archive/ES_0.5600396446680661 b/archive/ES_0.5600396446680661
new file mode 100644
index 0000000..121d98f
--- /dev/null
+++ b/archive/ES_0.5600396446680661
@@ -0,0 +1,22 @@
+archive/ES_0.5600396446680661---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T17:20:29.218
+Launch V∞: [7.971700528415906, -5.842591802096005, -0.12332839055951829] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.849409789403285e-9, 1.986102373301159e-9, 8.113216054707976e-10] km/s
+ V∞_out: [1.8294145594700012e-9, -1.7133647276574294e-9, -1.4631117271962397e-9] km/s
+ time of flight: 1.8562765478514493e8 seconds
+ arrival date: 2030-04-03T04:34:43.218
+ thrust profile: [0.23949714139401568 -0.010460865912826967 -0.08721254946499404; 0.11573931354048868 0.05607164725307729 -0.14065015680215764; 0.03061049156788385 0.024659511186986786 -0.07142005831802682; 0.02540702302377544 0.02582894856549493 -0.08480808653918392; 0.021518654506148673 0.024836816530296863 -0.09311812461628316; 0.016956937609448657 0.023293268849772703 -0.0963065816612169; 0.013178454775373662 0.018928216770066692 -0.08408500489051485; 0.007830471762718645 0.013382516562408622 -0.06401194304586054; 0.0057600097280943625 0.010180613441406191 -0.0525251566123857; 0.001881185645772929 0.00403546875444719 -0.02126999499661127; 0.0016864383089297496 0.005118399994095751 -0.031025578732172047; -0.00011609021130545688 -0.000647707937508528 -0.0015876285385581076; -0.0009439770807728955 0.0001934929868720471 -0.001402526359680602; -0.005967922558099161 0.0008364973057112194 -0.008100486704765309; -0.004628969188365092 -0.0029771088852978797 -0.002503875602572957; -0.0007589612868985739 -0.0005307735157486088 0.0024560883516418462; -0.0006636837539894721 0.0003937387299088251 0.0001715928901486317; 0.0006979690562153344 0.0008765533639857972 0.006154889480629502; 0.010037079489686053 -0.004850541992367499 0.00022403684905817375; -0.0025519329620106667 -0.0032302354164662032 0.009195649670692745] %
+
+Mass Used: 83.46817943933775 kg
+Launch C3: 97.69909817258389 km²/s²
+||V∞_in||: 2.8325186590518536e-9 km/s
diff --git a/archive/ES_0.560048198423917 b/archive/ES_0.560048198423917
new file mode 100644
index 0000000..7d8a16e
--- /dev/null
+++ b/archive/ES_0.560048198423917
@@ -0,0 +1,22 @@
+archive/ES_0.560048198423917---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T01:31:23.355
+Launch V∞: [7.764752292738126, -5.872460610410894, 0.13050352141436758] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.20683959679729e-5, -7.460071576207518e-5, 5.2982742962159644e-5] km/s
+ V∞_out: [-1.842777053523895e-5, -0.00012835788604853167, 5.791814171148922e-6] km/s
+ time of flight: 1.794683409746658e8 seconds
+ arrival date: 2030-01-18T05:50:23.355
+ thrust profile: [0.5064899185611248 -0.037929886617600814 -0.16241985299669273; 0.06290937960096708 0.03242175007285211 -0.07609539402120752; 0.036698683689235095 0.02951847977788158 -0.07658006271029122; 0.03439567430919545 0.03755925897388711 -0.10615990508428663; 0.02105825404191154 0.02680108201322074 -0.08534031308273432; 0.016392618535681868 0.024205901001627055 -0.08329956211903868; 0.017806217227473144 0.02901323541815886 -0.1062422335235759; 0.010723382841902338 0.019732506766531602 -0.07877916446485991; 0.009089687637000068 0.01881400356386889 -0.06478382975195038; 0.002200066581366656 0.004119866087298839 -0.025026546939994284; 0.003224978045941032 0.007854131417527438 -0.03980414367728962; 0.0007703021643782208 0.005715031166476213 -0.03403821091746323; -0.0011295089028132115 -0.0009133273827582608 -0.00011194831944591021; -0.00040441699964136415 0.00012767132656130755 0.00029317140968064927; 5.996437254299753e-5 -0.00116607950325506 0.000510421949691817; -0.0005233575170341049 0.000263009694971736 -3.210975276326882e-5; -0.000728878512919079 -0.0005948195688898687 -0.001018299951047107; -0.0009606679039373384 -0.0019328559726577465 0.0012649465123182287; 0.001971174032414237 -0.00028224048789312413 -0.005837104844406121; 9.910966214158885e-6 -0.00018775886281350044 -0.00414390089836649] %
+
+Mass Used: 100.42338090908879 kg
+Launch C3: 94.79420295751103 km²/s²
+||V∞_in||: 0.00012980380341162448 km/s
diff --git a/archive/ES_0.5600495599584965 b/archive/ES_0.5600495599584965
new file mode 100644
index 0000000..a5044fb
--- /dev/null
+++ b/archive/ES_0.5600495599584965
@@ -0,0 +1,22 @@
+archive/ES_0.5600495599584965---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:06:23.210
+Launch V∞: [7.954283648231266, -5.706977047477625, -0.020214836251404467] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.192728599333535e-5, 0.0002786538727556626, 4.876511509594836e-6] km/s
+ V∞_out: [0.00026927345674796594, -4.016474067586459e-5, 5.8641691979176206e-5] km/s
+ time of flight: 1.8560020463597783e8 seconds
+ arrival date: 2030-03-31T10:43:07.210
+ thrust profile: [0.36156275632285256 -0.00637804201161269 -0.11360930539230282; 0.08880716509214011 0.048668437491401484 -0.09574465471757251; 0.07088287490422104 0.06315479548066537 -0.13704207907453203; 0.03650307389183995 0.042590773930680705 -0.10619706949743947; 0.03833862829704991 0.05159124041680382 -0.14216409024230378; 0.009082889367759563 0.015188842315898548 -0.048562810136778996; 0.005825612387352574 0.011394835889773278 -0.03895732288266549; 0.00479211783583992 0.010560190500027895 -0.03797255926464988; 0.008707251389428794 0.025342921660672688 -0.09448628880007083; 0.0006075419751366712 0.0016833119093314472 -0.0064921345146628775; -0.0003063709528075588 0.0022149357135466414 -0.0081639395268461; 0.0003776300881720967 0.0013253199684103332 -0.0053858786235813395; 0.0020144992411154595 -0.0021146444103786652 -0.0015808035124075142; 0.004330916261613568 0.000673393744354267 -0.005670536200635337; -0.008517220381511216 0.007498346994795058 -0.0035551708072628753; -0.00039061641376248563 -0.005405405346266002 0.0008059766939781821; 0.00431889450326444 -0.0001247467737275056 -0.0034432235562791118; 0.003710198992995256 0.00617227423793455 0.004789716256128897; -0.007475801613643054 -0.006393401497151915 -0.006744604061066353; -0.006202886862514105 0.00634302261393269 -0.0038885842779052375] %
+
+Mass Used: 94.32084652164349 kg
+Launch C3: 95.84062401656041 km²/s²
+||V∞_in||: 0.0002789516469164487 km/s
diff --git a/archive/ES_0.560051810073991 b/archive/ES_0.560051810073991
new file mode 100644
index 0000000..0b92e05
--- /dev/null
+++ b/archive/ES_0.560051810073991
@@ -0,0 +1,22 @@
+archive/ES_0.560051810073991---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T06:53:03.685
+Launch V∞: [7.9797406971470535, -5.694531968800053, 0.11431256970246105] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.615547997989251e-9, 1.4173092244691447e-9, 4.006296531500781e-10] km/s
+ V∞_out: [1.5604124224373065e-9, -1.4440431090576261e-9, -1.1397874422742963e-9] km/s
+ time of flight: 1.8749577787536147e8 seconds
+ arrival date: 2030-04-23T09:02:40.685
+ thrust profile: [0.3812667412142468 0.0047845066304434206 -0.10276513383536134; 0.05068112898046015 0.03200185424741312 -0.06062903191785272; 0.03640793511851451 0.03813756263734713 -0.07664551518577585; 0.04267027411612299 0.06123160411490191 -0.1265123260675793; 0.021029163556794073 0.03908359000709373 -0.09202549159201712; 0.012723621214240338 0.02626822098124996 -0.07098946399510972; 0.006300986182373295 0.016337679113171456 -0.04787184237498146; 0.013536947134111563 0.0332557338499632 -0.10799728353732915; 0.0030015693955865634 0.014079479754620238 -0.04460314218382954; 0.004145198455753949 0.01396579375555113 -0.0451706622035749; 0.0011012699076015933 0.003416193773564723 -0.012842395707196875; 0.0006475990845799275 0.004224405015670006 -0.009918244520590591; 0.0014393505841442007 0.0006838500373901418 0.0027200559519191215; -0.0006673997331973123 0.0010762270454789246 -0.0016282619158964075; -0.006104819771518334 -0.0036053138399335443 -0.00014403476099703223; 0.0004382732451813417 5.1465350019508273e-5 -0.0017302977235482443; 0.008972155107436989 0.004751421217430241 -0.007094258099933424; -0.005235147660052498 -0.005762573582425606 -0.0043768220862520635; 0.0032676773885940325 0.0014453240338183936 -0.007168004277435949; 0.012269680629817044 -0.009286596003210124 0.004831776622147727] %
+
+Mass Used: 92.71114249725679 kg
+Launch C3: 96.11702330098274 km²/s²
+||V∞_in||: 2.1861529888266185e-9 km/s
diff --git a/archive/ES_0.5600733396559847 b/archive/ES_0.5600733396559847
new file mode 100644
index 0000000..99ccd1c
--- /dev/null
+++ b/archive/ES_0.5600733396559847
@@ -0,0 +1,22 @@
+archive/ES_0.5600733396559847---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:31:08.846
+Launch V∞: [7.911814048280214, -5.7569868522975876, 0.1631171890662192] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.28081909711072e-5, 4.962144896644834e-5, 0.0036156984135953672] km/s
+ V∞_out: [-0.003214917342845347, -0.0011097529447498388, 0.0012298415913522176] km/s
+ time of flight: 1.8749577787493706e8 seconds
+ arrival date: 2030-04-23T19:40:45.846
+ thrust profile: [0.3797427289952564 0.00791012487192792 -0.1086345129096796; 0.09841130913893315 0.05974536954743021 -0.10798423484395064; 0.04338599818665364 0.042175709995897134 -0.09181165293244803; 0.03522910356280417 0.04581267151055399 -0.11169513138580899; 0.03014597434877977 0.04799343747243084 -0.13118401826269452; 0.011343434443372952 0.020272276171630865 -0.06200919566260056; 0.010245676537671427 0.023718677815996233 -0.07709814180182878; 0.0061211819558970315 0.014345368866555835 -0.04950064975194238; 0.003063481316245783 0.00745590899078626 -0.027766431684158238; 0.0016824926844361966 0.0035909288995763892 -0.01422200522502803; 0.00026488625636723407 0.0013439405266299199 -0.004993090411412851; 0.00020198862263334324 0.0015195854584761936 -0.0026021885458146054; 0.0009782672122658613 0.0023367921202012464 -0.0042814773860610535; -0.005009486155245751 -0.0035594949694420187 -0.007118701970470173; 0.0026131751463814986 0.012352872747680944 -0.004874616947339992; 0.0005340361141399669 6.348411501509287e-5 -0.003461459466258746; 0.0010696626658998737 0.016165493339325647 -0.010846052761274538; 0.006317249144296134 -0.0004987054076785809 0.0023665796823844516; 0.0027219751963965685 0.0046286300820058265 -0.020680730201222446; -0.004693929395652651 0.005919223143118046 0.001289900185997829] %
+
+Mass Used: 94.78210911013048 kg
+Launch C3: 95.7663063694603 km²/s²
+||V∞_in||: 0.0036167718118435494 km/s
diff --git a/archive/ES_0.5600753421610118 b/archive/ES_0.5600753421610118
new file mode 100644
index 0000000..0af616c
--- /dev/null
+++ b/archive/ES_0.5600753421610118
@@ -0,0 +1,22 @@
+archive/ES_0.5600753421610118---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:58:05.248
+Launch V∞: [7.691056981574655, -5.913440940279386, 0.06465546710353338] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.217485948878005e-9, 1.1600046165234211e-9, -1.0243542009853293e-8] km/s
+ V∞_out: [-4.042072227395005e-9, 1.0068467041531443e-8, -1.5072071072839127e-9] km/s
+ time of flight: 1.790106498869232e8 seconds
+ arrival date: 2030-01-11T13:08:54.248
+ thrust profile: [0.45811389469812164 -0.022322775003301817 -0.12092375992704811; 0.14895397725602566 0.08335227046480943 -0.142547633106586; 0.06999857085469322 0.0647376001475901 -0.12162167784199615; 0.03865797840211822 0.04780987248358547 -0.1013317310852347; 0.0200936289289443 0.030411913393782655 -0.07113692766186859; 0.026874889510819056 0.04948284356282135 -0.12149103836874828; 0.010246408097541822 0.021735317129398978 -0.0581837198766806; 0.023125250418650586 0.057323044763131645 -0.15048406096083083; 0.002313219153162344 0.006515635261835425 -0.01966875116755698; -5.033901435934568e-6 -0.000463307937353057 -0.00488592933094346; 0.00013714904884219584 0.0016504393874408815 -0.003357516785430589; 0.00019818572033730258 0.0016252666710510548 -0.0054907179898854375; 0.0013928709340725312 -0.00018864113867420723 -0.00198915667195383; -0.0020243911904684717 0.0020131121287727573 -0.0008917535017736221; -0.0017000258073269223 -0.0010349955625506633 -0.0004754810532302939; 0.00018663078794739886 0.0005704165830610606 0.0013428089189338802; 0.0016912664358921842 0.0008933530134839563 0.0003593851675002661; -0.00244792288168304 0.0003544665024395971 0.0024549868569258846; -0.00084005985914096 0.002284285155421899 0.002697646831826614; 1.3542308683081686e-5 0.0008274040424523579 -0.0013021426832589902] %
+
+Mass Used: 104.35685665285655 kg
+Launch C3: 94.12532157742697 km²/s²
+||V∞_in||: 1.0544809507594544e-8 km/s
diff --git a/archive/ES_0.5600886631544241 b/archive/ES_0.5600886631544241
new file mode 100644
index 0000000..d80debb
--- /dev/null
+++ b/archive/ES_0.5600886631544241
@@ -0,0 +1,22 @@
+archive/ES_0.5600886631544241---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T05:59:43.781
+Launch V∞: [8.017658993270093, -5.639893580229773, 0.49099026972602267] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.909173570876192e-7, 4.895161244833186e-7, 4.8171971799450226e-8] km/s
+ V∞_out: [-1.647487147862218e-8, 6.45297976083814e-7, 2.017622804168756e-7] km/s
+ time of flight: 1.846048452334011e8 seconds
+ arrival date: 2030-03-18T21:07:08.781
+ thrust profile: [0.3394239828158611 -0.0075815793534088766 -0.10010702914885167; 0.1336841958554286 0.07783583273131128 -0.1403437886990211; 0.04953954623333943 0.04346013601783999 -0.10212683819812748; 0.020945382221218493 0.025225819132890934 -0.06476958704998192; 0.01534255069570109 0.020035043617629925 -0.061346232601535086; 0.02270339275968656 0.036370554463396564 -0.11655009665140095; 0.009976707255649496 0.017972977234958144 -0.06027647029129435; 0.008706947553298384 0.017300349095257368 -0.06716386245110201; 0.004340752755150432 0.009079177587478681 -0.036011849583943566; 0.004512482066164094 0.011018136128406113 -0.04548616296063453; 0.0016570740282040109 0.003087880433847145 -0.013443458826848465; 0.0024090901264926766 0.0075058424382079755 -0.03257712570130807; -0.001565124675901069 -0.0005868817113202766 0.0006364541320457726; 0.002570443310654664 -0.0010206200076838957 -0.001973337402622649; -0.0019758672378679884 -0.0008729851896118301 0.003612462221058999; 0.0001846453149713569 0.003160626035832349 -0.0038762862763096354; -0.0013980952555156497 -0.0024030678042775387 -0.0038116469750931986; -0.00249915397196093 -0.0007105301742894592 0.0009984755613479139; -0.0003784161970983213 -0.0019282630726424614 -0.0037012492265160353; -0.0022465039983800695 0.0024743531141734392 0.004683232487340412] %
+
+Mass Used: 91.49820083388477 kg
+Launch C3: 96.33232677364742 km²/s²
+||V∞_in||: 6.949434699931412e-7 km/s
diff --git a/archive/ES_0.5600930846535346 b/archive/ES_0.5600930846535346
new file mode 100644
index 0000000..70f3c52
--- /dev/null
+++ b/archive/ES_0.5600930846535346
@@ -0,0 +1,22 @@
+archive/ES_0.5600930846535346---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T14:18:12.292
+Launch V∞: [8.090006533074147, -5.824623529870846, 0.0031629427099133614] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4756478224051947e-9, 1.9187310374144267e-9, 6.776946087512993e-10] km/s
+ V∞_out: [1.6709084931425105e-9, -1.5844070079887406e-9, -1.2619888950061075e-9] km/s
+ time of flight: 1.8480771744614208e8 seconds
+ arrival date: 2030-03-24T13:46:49.292
+ thrust profile: [0.13630887086006926 -0.004665749282731014 -0.051689805204641844; 0.03512755240565545 0.017328288182475376 -0.04566318079683608; 0.036054869528773396 0.028319844642083508 -0.08257188312973386; 0.04042856171992436 0.04081918811661607 -0.13304470282820097; 0.019301703602047263 0.02325579665820151 -0.08720757257386347; 0.027718668957236223 0.0374621342455511 -0.14967715701912604; 0.015415116947010938 0.02300072898474899 -0.10129648219789104; 0.0055637754380623424 0.009209016044557506 -0.04453020057039961; 0.004768320983705842 0.008733367487093609 -0.043462667744465215; 0.0027020219596239443 0.003622420900714776 -0.023966048847061782; 0.0012581878032128084 0.0021690284960899464 -0.012711046436128788; -0.0002889794546330573 0.0007143524813283631 -0.003542256341400162; -0.0009849789219417912 0.003205687517822524 -0.009225882056482535; 5.1668559890545975e-5 -0.00051114887490292 -0.0015303282401555656; -0.0055262228779289916 -0.010088355208995627 -0.004528834905755466; 0.003965021060477228 0.010585462888502943 0.0005862615811261067; 0.0026355691618928493 -0.00043061715621806827 0.00022770738908900207; -0.0032995210912893473 -0.0032274793609130153 -0.007805600701036855; 0.002635559190142868 0.007998061057562037 0.008879383834923045; -0.00714350918859822 -0.01008272059049151 0.0006751425505222694] %
+
+Mass Used: 73.75761141345811 kg
+Launch C3: 99.37445497411409 km²/s²
+||V∞_in||: 2.513629899654524e-9 km/s
diff --git a/archive/ES_0.5601034520792892 b/archive/ES_0.5601034520792892
new file mode 100644
index 0000000..8987743
--- /dev/null
+++ b/archive/ES_0.5601034520792892
@@ -0,0 +1,22 @@
+archive/ES_0.5601034520792892---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T22:19:18.135
+Launch V∞: [7.828774235395592, -6.0654924273158715, 0.053241078070394715] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0988075606626456e-6, 3.1379312674616652e-6, 9.843785973589171e-6] km/s
+ V∞_out: [8.955771048591048e-6, 1.130828332848714e-6, -5.138776650395659e-6] km/s
+ time of flight: 1.7754682276738843e8 seconds
+ arrival date: 2029-12-27T20:53:00.135
+ thrust profile: [0.18834893088445506 -0.008617401133991452 -0.0626124713571887; 0.05283249985915532 0.027747879762809104 -0.05821879606073194; 0.04717667557597328 0.040628111398479376 -0.09023852810576824; 0.05590490931107049 0.06188945190743587 -0.15183996617824683; 0.028158382630419497 0.03835252058167789 -0.1041595038454156; 0.02680676354228887 0.04290625375655984 -0.12392919342698505; 0.02058152011160482 0.033611013158910005 -0.10308043678294598; 0.010130333061433594 0.022939564219307082 -0.07424454008595616; 0.007133213478962911 0.015621576136896196 -0.055016910114401824; 0.0033360690139668677 0.0070665540471103626 -0.028500780566426357; 0.0023441183529575886 0.002870736197722059 -0.013474184091350276; 0.00045068606308951967 0.0016517125950486868 -0.005641150037949348; 8.52265737998222e-6 -0.0005774320474902718 -0.004949931174320008; 0.005261870354084387 0.001941896879888665 -0.0017539817558299346; 0.0005018065849018778 0.0032195616265478064 -0.00900409246971587; 0.004259290446521735 0.0018716943608928019 -0.0015315913552229913; -0.0003256417815560694 0.0022973630197789495 -0.0061355034244039135; 0.0031510546670721873 0.0013680000502790184 -0.005460160771538602; -0.0003275779948063613 -0.00018644421706362144 -0.0010606755723266627; -0.00038922854069936195 -0.00015338457084008636 -0.0014469771549995149] %
+
+Mass Used: 81.30471643492183 kg
+Launch C3: 98.08273902701411 km²/s²
+||V∞_in||: 1.0390096870987964e-5 km/s
diff --git a/archive/ES_0.5601053284232422 b/archive/ES_0.5601053284232422
new file mode 100644
index 0000000..7c74cf2
--- /dev/null
+++ b/archive/ES_0.5601053284232422
@@ -0,0 +1,22 @@
+archive/ES_0.5601053284232422---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T13:05:10.102
+Launch V∞: [7.674714306571231, -6.013734106756503, 0.0056394642611274325] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.70880398126339e-10, -1.8515658457460911e-9, -1.571101635557064e-9] km/s
+ V∞_out: [-3.6793829576568253e-9, 2.852177997942969e-9, 2.0538815259214184e-9] km/s
+ time of flight: 1.825937337566871e8 seconds
+ arrival date: 2030-02-25T21:34:03.102
+ thrust profile: [0.4609587274693095 -0.018621318774157753 -0.12044216231854117; 0.07552515540186583 0.04327235540321104 -0.0878722551782157; 0.06663578703728022 0.06510734211936826 -0.135215559901146; 0.029140431916059445 0.036629062642035665 -0.09102069997022047; 0.019232019091256387 0.029344712700110617 -0.08059813919212434; 0.013394992082066026 0.025068127567770552 -0.07423239105693015; 0.013033408555517836 0.028029427287103607 -0.08095722470180108; 0.005485744718925089 0.013438932214049298 -0.04651177791748746; 0.008206287728904057 0.02325792467811531 -0.08034354361040381; 0.005022393780606013 0.01649966804262205 -0.06357111363487292; 0.0005588912104434608 0.0012174839866099256 -0.004942192966698465; 0.0005385106062652252 0.001421035712640482 -0.0024982068815134267; -0.0004434701869965676 -0.00023931097990737308 -0.0013884104639172844; -0.00014837827108566776 9.441900884675982e-5 -0.003680014903637654; -0.002419802193647462 -0.00342138512964707 -0.003019445537081227; -0.002988554448405345 -0.0002858501123549639 -0.008903375264521937; 0.002559505907388231 -0.0010752933871574044 -0.000642838055845947; -0.0003742117585363294 -0.0008009456145316998 -0.0009012161557354275; 0.002035778667404846 -0.003598633995828141 -0.0032442898431030943; 0.0010029702282087207 -0.002558315004166785 -0.0020627737858351907] %
+
+Mass Used: 98.90297833987506 kg
+Launch C3: 95.06626939781272 km²/s²
+||V∞_in||: 2.473536896778202e-9 km/s
diff --git a/archive/ES_0.560109028203875 b/archive/ES_0.560109028203875
new file mode 100644
index 0000000..2acbe97
--- /dev/null
+++ b/archive/ES_0.560109028203875
@@ -0,0 +1,22 @@
+archive/ES_0.560109028203875---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T09:10:51.654
+Launch V∞: [7.935268825875223, -5.546861659889794, 0.3663528721888927] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.5171769749216365e-9, -1.0018842284747545e-9, 3.035382932266895e-11] km/s
+ V∞_out: [-4.6243674129060965e-9, 3.815338421713558e-9, 2.7393827108926027e-9] km/s
+ time of flight: 1.8404216497071472e8 seconds
+ arrival date: 2030-03-10T12:00:15.654
+ thrust profile: [0.6188688116408496 -0.017790437918495897 -0.1769945747729446; 0.0589000749272526 0.03455284475603954 -0.06362781563818815; 0.04061579648671674 0.03920347530392667 -0.07937691219564307; 0.0322824081663429 0.04193901010359652 -0.09384498401369158; 0.022967992193640634 0.036960917030771395 -0.09105157464806314; 0.016987545147450354 0.032575710120989455 -0.08678868515152098; 0.00747622594771613 0.016195291130020526 -0.04728130283498117; 0.004974108712515794 0.01334221080015305 -0.041444300431592966; 0.006465023723992533 0.018934042095743224 -0.060184302778094535; 0.012736781006214752 0.04190960760487328 -0.12997975994829167; 0.0003102033262612787 0.0007706042586846291 -0.003183092158927885; 3.917666930249855e-5 0.001241094614859521 -0.005152685782189705; 1.0934846327633748e-5 6.47506461593826e-5 -0.0005635929799866938; 0.0001554276459673324 0.00039865499457989253 -0.00042346038581778144; 4.9068663215014576e-5 0.00013261430448398542 -0.0005870112903617171; -5.961127786542671e-5 0.00047111011790244866 -0.00024694976010299324; 7.644078739635568e-5 0.00018586451838574177 0.00011529895041280115; 0.00020371952823576778 0.0001670946605684512 -0.00030675107982278826; -1.8351183515511599e-6 2.0284131741775188e-5 -0.0001408823708152207; 0.0004186686324569861 0.0004541855801805529 -0.00021508146181522275] %
+
+Mass Used: 105.88331600555011 kg
+Launch C3: 93.87038003982356 km²/s²
+||V∞_in||: 3.6572157763987506e-9 km/s
diff --git a/archive/ES_0.560112027904094 b/archive/ES_0.560112027904094
new file mode 100644
index 0000000..fd0e61a
--- /dev/null
+++ b/archive/ES_0.560112027904094
@@ -0,0 +1,22 @@
+archive/ES_0.560112027904094---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T13:42:26.294
+Launch V∞: [7.97128445884716, -6.039189852305846, -0.011076760865192142] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005018020724001508, 0.00139067970483264, 0.003171195995761545] km/s
+ V∞_out: [0.00320224452339908, 0.0003835118422356357, -0.0013452814108584465] km/s
+ time of flight: 1.8050344377548072e8 seconds
+ arrival date: 2030-02-02T17:33:09.294
+ thrust profile: [0.09345238076678467 -0.006233315176459761 -0.03717149894926537; 0.03698003211676286 0.016071643316568296 -0.04784717773732191; 0.0275016927928309 0.019248400271576836 -0.06274703044118016; 0.043743880077415725 0.03907807879633793 -0.13957895180076885; 0.03240544634683999 0.033826930232982506 -0.13549574385377708; 0.012192898206894428 0.014166713477045489 -0.06418731907703487; 0.012883539338095381 0.016968617613634825 -0.08455971092663146; 0.00842685470284598 0.012934195702177503 -0.07250701772835554; 0.0063691807744748665 0.009133667324857975 -0.0519618316881585; 0.011740028887172568 0.019583701616838138 -0.12506805232780957; 0.0019698270607186176 0.0029911376698540416 -0.019437415358726312; 0.0005063064013769137 0.0011678798476265223 -0.0008607694858120752; 0.0001820565462460775 -9.586275354528135e-5 0.00035906741847539683; -0.0001948771102976477 -6.453795290699266e-5 0.00010963215031004015; -0.0008447638460168324 -0.00041425337648411055 -0.0004907568475172162; -0.0003985201981213632 0.0018870522788175287 -0.0023246425177014356; -9.271223119133713e-5 -0.002720397310256125 0.0012952819077787555; 8.70958838849762e-6 -0.00020119594321347037 -0.0013362950841379684; -0.002439844244307262 -0.0023861325010015046 0.0005234402114534301; 0.0029763824916962753 -0.0007591777854959055 0.00010168249422386482] %
+
+Mass Used: 70.05304185912291 kg
+Launch C3: 100.01331269068342 km²/s²
+||V∞_in||: 0.0034988968839953748 km/s
diff --git a/archive/ES_0.5601273205179945 b/archive/ES_0.5601273205179945
new file mode 100644
index 0000000..40a7099
--- /dev/null
+++ b/archive/ES_0.5601273205179945
@@ -0,0 +1,22 @@
+archive/ES_0.5601273205179945---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T22:47:06.155
+Launch V∞: [7.788543624015196, -5.719598583939361, 0.04940286487674511] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3476740135678966e-7, -1.048340873342889e-6, 2.0500153176256046e-5] km/s
+ V∞_out: [7.684853021994701e-7, -2.05113923300679e-5, 2.2305614917924508e-7] km/s
+ time of flight: 1.8749577787619856e8 seconds
+ arrival date: 2030-04-23T00:56:43.155
+ thrust profile: [0.5512621491454823 -0.0013796034982037678 -0.1748573566001959; 0.15884300106024968 0.09166046732885276 -0.18005386234927268; 0.04086353291808486 0.038736072149116826 -0.08838110893402626; 0.02468469585138617 0.031018219973700443 -0.08037770838961236; 0.015267106153240768 0.02405036103121122 -0.06877877334605301; 0.020363075892398497 0.03845945613122809 -0.11904851917608383; 0.009139132629135906 0.019988290720503666 -0.06695440367565468; 0.00022566311569345294 0.004559160876121177 -0.020348885243538933; 0.0009759053240507754 0.009216305565584905 -0.035970633983784236; -0.0014726094409122752 0.0007950404255218746 -0.009666688780205632; 0.0011053198869888118 0.002969835631166658 -0.013433823491570667; 0.0038095374735727305 -0.0001290946898827505 -0.0063826575376092435; -0.0007450604500527095 -0.0026343467596262665 -8.130696905410666e-5; 0.0013670720583867147 0.004621734858750814 -0.0110751675913798; 0.006636967050586742 -0.0002466616141275017 -0.0028398784828184325; 0.0024001300341019946 0.0036229429748809473 0.0005192880714093304; 0.002241663070243544 0.0029413806313157266 -0.00627914814769279; 0.00471230224654172 0.005103417760535437 0.002031915370432854; 0.008867808247076187 -0.002902713528313482 0.01160991192892114; -0.0009170594170528344 0.009307368945824332 -0.005208891034632063] %
+
+Mass Used: 108.77885500971979 kg
+Launch C3: 93.37766038764694 km²/s²
+||V∞_in||: 2.052738320120591e-5 km/s
diff --git a/archive/ES_0.5601348390998118 b/archive/ES_0.5601348390998118
new file mode 100644
index 0000000..4bffe60
--- /dev/null
+++ b/archive/ES_0.5601348390998118
@@ -0,0 +1,22 @@
+archive/ES_0.5601348390998118---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T15:10:18.816
+Launch V∞: [7.7045524853921, -5.691933128964909, 0.2534026751589257] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.0436599465046786e-5, 0.0010283156749142858, 1.64500149610387e-5] km/s
+ V∞_out: [0.0009995932322968686, -0.00013275932713873866, 0.00019779334647918945] km/s
+ time of flight: 1.874957778727611e8 seconds
+ arrival date: 2030-04-20T17:19:55.816
+ thrust profile: [0.5718785480606324 0.014772276683911872 -0.13102432446663495; 0.28256585473835893 0.1871826185863458 -0.22278529254737978; 0.04638111178402934 0.05075795575227058 -0.08193825817042483; 0.01942627983797845 0.02958584415635057 -0.054685879147867475; 0.014497577873608804 0.02892597972394356 -0.05823735194806244; 0.01806211806840167 0.04203291865616089 -0.08964909092104655; 0.006101909841230631 0.018556248869633772 -0.04301472352712454; 0.008003666403912405 0.027588175891366088 -0.06676965739642776; 0.004401202895298834 0.019536346954337824 -0.046600368213758736; 0.0018992861279112942 0.010349212890115886 -0.028020105566821645; 0.0011484156128551161 0.008178210174541447 -0.02275217336209247; 0.0007908935619961245 0.0035290147465945154 -0.007745514806842269; 0.0003816157874177862 0.0003406256524158646 0.0004737988061863604; 0.00012790509808648884 0.0005650670795919281 8.12021534231204e-6; 0.0013621041670920384 -0.0015608549777782392 0.0014572978993796209; 0.0005117515770689468 -0.0009207869616129141 -0.0015805420022430195; 0.0001979573612959436 -0.0020694128452485596 0.0003460714415078655; -0.0004891116054225695 -0.0006821229407982814 0.0016845983114540863; 6.932065672806046e-5 0.0008961165526562794 -0.001489872283644207; -0.0005919990789822545 -0.0009061967646723425 -0.001690077058156504] %
+
+Mass Used: 117.85971842991967 kg
+Launch C3: 91.82244466054755 km²/s²
+||V∞_in||: 0.0010292418806300773 km/s
diff --git a/archive/ES_0.56015008448963 b/archive/ES_0.56015008448963
new file mode 100644
index 0000000..4054577
--- /dev/null
+++ b/archive/ES_0.56015008448963
@@ -0,0 +1,22 @@
+archive/ES_0.56015008448963---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T00:31:20.401
+Launch V∞: [7.739586967611511, -5.81694516772151, 0.1656871023210437] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.984956769822344e-8, 1.053112476240227e-7, -1.467406006554363e-8] km/s
+ V∞_out: [3.2308832548078255e-8, 6.425995417585346e-8, 1.5836415408430052e-9] km/s
+ time of flight: 1.8735229396593234e8 seconds
+ arrival date: 2030-04-20T10:49:33.401
+ thrust profile: [0.4088730297211385 0.01422038467959477 -0.099817717834136; 0.23886723820231034 0.16545714120752594 -0.19412857388508722; 0.044899886386895974 0.0517295099456061 -0.07827562358062098; 0.034946165682723164 0.059106831577206795 -0.09622591657502039; 0.02127466907425809 0.044964210937194965 -0.08466894706693895; 0.012855064022270667 0.03652362946310989 -0.07080651007861932; 0.016038692071298155 0.05386048037379311 -0.10856788147942699; 0.0065449534078038454 0.02587647773913631 -0.055959103612853583; 0.00046400710283102246 0.0036198479901024603 -0.008545138766712628; -0.0003186635252487766 0.00015883317735548448 -0.000414704409304814; -0.0004695589454897695 0.0005133188851025941 -0.0023255036986977594; 0.0007954358275000411 0.0025300563841010345 -0.003210107449297748; -0.0014723415048132078 0.004751746126128662 -0.003368777490346894; 0.006503111734937828 0.005647577718409438 -0.012290063972093326; 3.136276653229532e-5 -4.9667334002895854e-5 -0.00229268178241992; 0.006157277508586682 -0.0025135456961985136 -0.007159902706785126; 0.002291396215495209 0.0001347783037447996 -0.0004171336250216027; -0.001430998368702404 0.002575388598243115 -0.012476363977754526; -0.004012561843802845 0.0038185006803433323 -0.004447948594051887; -0.00012699111396066048 9.136227650836633e-5 -0.0004006433187695004] %
+
+Mass Used: 106.54295848320771 kg
+Launch C3: 93.7655097293761 km²/s²
+||V∞_in||: 1.1043904928378474e-7 km/s
diff --git a/archive/ES_0.5601646966859536 b/archive/ES_0.5601646966859536
new file mode 100644
index 0000000..6d9b368
--- /dev/null
+++ b/archive/ES_0.5601646966859536
@@ -0,0 +1,22 @@
+archive/ES_0.5601646966859536---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:55:37.408
+Launch V∞: [7.887136340730376, -5.848498475451559, 0.13466972793515022] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1060487096330113e-6, -1.7002911285822727e-6, -1.6589842547164512e-7] km/s
+ V∞_out: [1.4718869426387873e-7, -6.87415083111488e-7, -1.909905195597053e-6] km/s
+ time of flight: 1.8040486031293818e8 seconds
+ arrival date: 2030-01-29T15:23:17.408
+ thrust profile: [0.3654373048893859 -0.020699789553618224 -0.12154922182724612; 0.060174388454772666 0.030265388807007694 -0.07287149845664932; 0.03956693840070796 0.03226042078754414 -0.0858031728190137; 0.032121233846767 0.03375388720509507 -0.09983786053524754; 0.024208649722024942 0.028310110185495493 -0.09758468762303985; 0.012166595899480773 0.017162919436066792 -0.0638944238260235; 0.0070730396814188525 0.009973121297132452 -0.036179897898855985; 0.017293483316449382 0.029491244568445627 -0.11580167855695768; 0.013694088416924004 0.02683966893961156 -0.11119870664331752; 0.004300151860251488 0.014459658319168792 -0.06211601080893223; 0.0007459013003409168 0.0030253984896746336 -0.009883650254451383; 0.0034892381764399004 0.007919770723736706 -0.031636646762530335; -0.0008251910764791655 -0.0008348326273321853 0.0008509781556971718; -0.0012356336390787674 -0.0006151348941653116 0.001001783315201238; -0.0011510129141069055 -0.00026963867839440087 0.0014021161932385718; -0.0001615427148157723 0.00019929740100437486 -0.0016209842596178756; -0.003148631578927739 0.0010440341631802992 8.964265148313265e-5; -0.0012168512870231413 0.001329960671013187 0.0005257534746476392; 0.0019927924462699994 -0.0018145717383095832 -0.0016054460489374825; -0.003119647118980243 -0.0002840400417416339 -0.002772849349305686] %
+
+Mass Used: 91.0172044071478 kg
+Launch C3: 96.42999001025109 km²/s²
+||V∞_in||: 2.035155020530475e-6 km/s
diff --git a/archive/ES_0.5601753456000009 b/archive/ES_0.5601753456000009
new file mode 100644
index 0000000..98e4f05
--- /dev/null
+++ b/archive/ES_0.5601753456000009
@@ -0,0 +1,22 @@
+archive/ES_0.5601753456000009---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T00:49:09.766
+Launch V∞: [7.886224632069779, -5.522410508495716, 0.31594102103672583] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.925307363768685e-6, 0.00026926761780851296, 3.0145550562290016e-6] km/s
+ V∞_out: [0.0002605163365460388, -3.9817126487737177e-5, 5.455117358946792e-5] km/s
+ time of flight: 1.8749577787475526e8 seconds
+ arrival date: 2030-04-20T02:58:46.766
+ thrust profile: [0.613148211807805 0.010372002239303858 -0.1649026493714667; 0.14926216364808484 0.09452576711617056 -0.14966560004884774; 0.04636169629472894 0.0476071779705597 -0.08746192166728395; 0.040290554743841175 0.056121861917410226 -0.11411787898128961; 0.021712308291028905 0.03741544767808018 -0.0850225503323438; 0.018600172076803614 0.03954425319895364 -0.09673872995320514; 0.005318944416244116 0.013050730466082844 -0.03637238674886697; 0.009195294268496319 0.027008478231240737 -0.07488286677897862; 0.0007328627502300472 0.0025961769206593777 -0.003688425230246364; -0.002208274786158761 0.002445953601151544 -0.003770547850453926; 0.0004907399220236307 0.0018493554799082557 -0.006138849579293786; 0.002595867223085018 0.0021944890701647572 -0.005605882839846164; -0.00023118638636590648 0.003851551624844289 -0.005036108027300049; -0.0006951148211526941 0.00125714772428589 -0.005669498800873623; 0.0023829743633664315 -0.0013657557391021876 -0.008968315507536809; 8.756973292680822e-5 -0.0005299860324324895 -0.008299149692256712; -0.00020377224340013995 -0.0005460036501254694 0.0017916778541524864; 0.00099123524145437 0.002399861292357271 0.002021150804748543; -0.0005012948643197403 -0.0006977661485225886 0.004562053196574667; -0.0073067546882663705 -0.004295612117772657 -0.0069402518364970935] %
+
+Mass Used: 112.26654611327422 kg
+Launch C3: 92.78937550058176 km²/s²
+||V∞_in||: 0.00026940109138470216 km/s
diff --git a/archive/ES_0.5601770171356165 b/archive/ES_0.5601770171356165
new file mode 100644
index 0000000..91bf633
--- /dev/null
+++ b/archive/ES_0.5601770171356165
@@ -0,0 +1,22 @@
+archive/ES_0.5601770171356165---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T20:00:14.573
+Launch V∞: [7.851635249969939, -5.610453680592776, 0.11455513993297013] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.57777786978847e-7, -4.660144920822145e-6, 9.835506111930302e-5] km/s
+ V∞_out: [4.42969816981417e-6, -9.835671833338318e-5, 1.2414819270579848e-6] km/s
+ time of flight: 1.8749577782862395e8 seconds
+ arrival date: 2030-04-20T22:09:51.573
+ thrust profile: [0.5099394449554686 0.003133419590758368 -0.1496229268438883; 0.19109796621337505 0.11751447801425412 -0.196715924462079; 0.07482577425463306 0.07505414957671773 -0.1449735632949836; 0.06108818090619487 0.0828237101892815 -0.1779975103865217; 0.014482547791837474 0.02387636943685797 -0.06035863486993344; 0.008258508106329084 0.016316131451357102 -0.045585201680953445; 0.004889368064485714 0.010834549397268441 -0.03289076876539092; 0.003965428994001751 0.009114411737430867 -0.030831373773215022; -0.0002600307919277731 0.0012673259815434502 -0.0032535739358751036; 0.0003118348049761143 0.0001868162021711104 -0.0029054377356959823; -0.0032365901937762478 0.002708185775747321 -0.010291623740207211; 0.000386587579264979 0.0011044436431503334 -0.0024838235432699703; -0.0056886569116660094 -0.0001411827555485804 -0.003146227561881905; 0.0043608150224333985 -0.0005646460196358084 -0.0007642563365479783; 0.0054001889143497645 0.006013930556030145 0.00016088313134805972; -0.0004109317902908111 -0.00016059668195067154 -0.004345741635977245; 0.001126587879859305 -0.0011686928231090187 0.005850589041483893; -0.00590403435235121 0.004064131217020804 -0.004694630247580876; 0.0013895264246769142 -0.001917427029384511 -0.010794790490540385; 0.004729030311918048 0.007735792311955427 0.0002152989186910419] %
+
+Mass Used: 110.23199802061254 kg
+Launch C3: 93.13848948073259 km²/s²
+||V∞_in||: 9.846759705650351e-5 km/s
diff --git a/archive/ES_0.560177933664376 b/archive/ES_0.560177933664376
new file mode 100644
index 0000000..5dae6c4
--- /dev/null
+++ b/archive/ES_0.560177933664376
@@ -0,0 +1,22 @@
+archive/ES_0.560177933664376---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T21:01:22.365
+Launch V∞: [7.918477972844496, -5.752398763757548, 0.23825099821794263] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.5757673047742625e-9, -1.3803819195348427e-8, -8.583594189532169e-9] km/s
+ V∞_out: [-9.826134439808897e-9, 9.353864006646155e-9, 5.986525001536194e-9] km/s
+ time of flight: 1.8256531202181676e8 seconds
+ arrival date: 2030-02-22T21:36:34.365
+ thrust profile: [0.36949323852491406 -0.00940615221129667 -0.10928927739421543; 0.08162208646784323 0.044620984095594916 -0.08718371641609898; 0.06226570246573436 0.058875611044447954 -0.12439484497566465; 0.04208318781282637 0.04900465432383952 -0.12094677842405965; 0.033207432693217145 0.0473631107493107 -0.12136459589722513; 0.024055422257757 0.04210253350842033 -0.11616307622922512; 0.010988035658412535 0.022683332841134357 -0.070059163063438; 0.007769485707933486 0.017892702632980297 -0.05893886827007358; 0.0014451723194701218 0.00666378411311002 -0.02183309998338327; 0.0009384822148651973 0.001859091448318835 -0.007282650483098056; 0.00238722744850608 0.003804987461764361 -0.016438908742725827; -0.0035029907588867383 8.539018734608002e-5 0.0008798679511999737; 0.0019094706237434453 0.0007745030798589575 0.0004686989495006665; 0.005466075075347255 0.0029818983299024935 0.0011340029685497736; -0.0001938639423030656 -0.0015392093377041337 0.003431589564239125; -5.893278119523419e-5 0.0025392034440031228 0.0013218006516146946; 0.009572650442316519 -0.0001772183474028157 -0.0062818878613559925; -0.0007129224041408232 0.008815061401710376 -0.002333569640364158; 0.0037266434983680365 -0.007254798482716062 -0.0016527862372050632; 0.0038022278736320305 -0.004329868754718774 0.0006829065947740699] %
+
+Mass Used: 94.42088979761957 kg
+Launch C3: 95.84914848185468 km²/s²
+||V∞_in||: 1.6886715489279767e-8 km/s
diff --git a/archive/ES_0.5601911451244612 b/archive/ES_0.5601911451244612
new file mode 100644
index 0000000..32f5d49
--- /dev/null
+++ b/archive/ES_0.5601911451244612
@@ -0,0 +1,22 @@
+archive/ES_0.5601911451244612---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:21:42.976
+Launch V∞: [7.801024095637435, -5.889453168042649, 0.15188451903981673] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1945310348664523e-9, -1.3577976388183004e-9, -2.180077432473684e-10] km/s
+ V∞_out: [2.6583183970938444e-10, -1.026907388877996e-9, 1.542308042344775e-10] km/s
+ time of flight: 1.813890486575831e8 seconds
+ arrival date: 2030-02-09T13:12:30.976
+ thrust profile: [0.3646610661361156 -0.008844609141151401 -0.10023046332261552; 0.09698111651467616 0.05835583774849936 -0.09975943837082159; 0.07512806066948662 0.07508073634187254 -0.1351616658559787; 0.021980003776627618 0.027149288651722576 -0.0609422219975849; 0.027752049913767545 0.04294403617560875 -0.10225589364235946; 0.034906146162678335 0.07265801835869021 -0.16992115116028417; 0.011667022670361987 0.024838971242235903 -0.06648626494157324; 0.007058502592023749 0.017767068009903183 -0.05384220019379548; 0.0073833302432173105 0.02104952606058219 -0.06275326106376881; 0.000725800306546831 0.0015164053178864834 -0.005418350196902981; 0.0013020730744684364 0.00041734221145109054 -0.0006723227314127458; 0.0002999444232372971 0.002764167915241072 -0.009391094497219813; -0.0004917977679674386 -0.000739412236124534 0.0013395251966015955; 0.00025402255778914 0.00106921893899832 -0.0017931446461127722; -4.510837149852083e-5 -0.0003846904103826007 0.0009110627598620099; -0.003962881091716336 0.002974404435047214 -0.004836116636734562; 0.000873550239933892 0.00738454184948097 0.0060468281903276085; 0.0018929910203485337 0.00011533266285063744 -0.0019422534839535805; -0.0012047942796958497 -0.0020018567081877305 -0.011741819857306712; 0.0060710218102325315 -0.0037915700296233482 0.004011343077324392] %
+
+Mass Used: 96.09555992449486 kg
+Launch C3: 95.5647044664074 km²/s²
+||V∞_in||: 1.8215504926725144e-9 km/s
diff --git a/archive/ES_0.5601962119561941 b/archive/ES_0.5601962119561941
new file mode 100644
index 0000000..afb3321
--- /dev/null
+++ b/archive/ES_0.5601962119561941
@@ -0,0 +1,22 @@
+archive/ES_0.5601962119561941---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T10:55:27.622
+Launch V∞: [8.081766079635731, -5.877570386667416, 0.06796524073399662] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.024064294226755e-5, 1.6156659530849994e-5, -1.2844293124200135e-5] km/s
+ V∞_out: [4.270930722937318e-6, 2.8530232856018443e-5, -1.3821368641941062e-6] km/s
+ time of flight: 1.861720781146942e8 seconds
+ arrival date: 2030-04-11T05:23:25.622
+ thrust profile: [0.13187444975255894 -0.007590036424381059 -0.05386614551548289; 0.04569960800328174 0.018923529598819846 -0.06025147419155559; 0.026976734449080216 0.016538195714416698 -0.06265193542864204; 0.03694794149186058 0.02875598234895544 -0.12732615468540906; 0.026631061198844303 0.022657285598313835 -0.11668083157258141; 0.01751857771912978 0.015738061545899594 -0.0925886837265248; 0.017101340940077814 0.017022845838557222 -0.10852884325737047; 0.010112725577869876 0.008841207040117774 -0.06258885039121123; 0.002872017371931751 0.0033513051098649897 -0.03386170920376252; 0.0041202592061827395 0.0008071556430445659 -0.014327872610851767; 0.0019806542743509292 0.0019544526712058597 -0.013158595662103843; 0.0019293134242888183 -9.548056371100691e-5 -0.01660435101835138; 0.0005690109052957683 0.0006569692392500925 -0.0028387852336698126; 0.0007088019246543095 0.0009783520756794194 -0.00644056072087178; -0.004099802420881812 0.0017413363419950157 -0.007103410838114076; -0.0065267056483321075 -0.0028557812245937012 -0.012624619875742382; -0.0008744842174607358 0.0009989637301796358 0.0021840337803842877; -0.000258007030652672 0.0022278744913426865 -0.010080965922042183; -0.003085678965488053 0.001979495481119047 -0.0044153204740704196; -0.0005554736367812479 0.007997168574162342 -0.003323582913587869] %
+
+Mass Used: 71.01410458981036 kg
+Launch C3: 99.86539589012847 km²/s²
+||V∞_in||: 2.8908426795184584e-5 km/s
diff --git a/archive/ES_0.5602013795584084 b/archive/ES_0.5602013795584084
new file mode 100644
index 0000000..0920193
--- /dev/null
+++ b/archive/ES_0.5602013795584084
@@ -0,0 +1,22 @@
+archive/ES_0.5602013795584084---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T18:17:57.652
+Launch V∞: [7.287899959571731, -5.990602424130751, -0.05153958214777408] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.524188043697825e-6, 6.0117153549199786e-6, -4.582380004179431e-6] km/s
+ V∞_out: [1.4329967930871368e-6, 1.0556392926866459e-5, -4.971824142307446e-7] km/s
+ time of flight: 1.832277883462162e8 seconds
+ arrival date: 2030-03-03T10:54:25.652
+ thrust profile: [0.940135568347544 -0.01609778109461962 -0.21309930895921925; 0.14446132773369108 0.09237244716521174 -0.13982408141905514; 0.0419417482402761 0.04149218639050848 -0.07764227970629879; 0.033862450851342416 0.045474154768750004 -0.09383839704331373; 0.027168351990631535 0.045226704219328444 -0.10061472900060006; 0.009433043087445865 0.019607076275026867 -0.050770651636996914; 0.018041126462935615 0.04462650668293425 -0.10895018960352812; 0.00726513331744417 0.02099318992145052 -0.05885977600875432; 0.0032695903184772643 0.016529855633131557 -0.05298821183750083; 0.0029325004615631755 0.008177905453862279 -0.02579942334513145; 0.0006052347057979424 0.002419157642608944 -0.008157676052398768; 0.00023706559086618634 0.0003510130936610597 -0.0008762265497055765; 0.00038961454415916677 0.00022116881536728117 -0.0005203909536545181; 0.0007031392000778736 0.0002920612949759108 -0.0008829998091450707; -3.9006301084399775e-5 0.0008014743875968376 -0.00015094376191914074; 0.00025539523033738995 9.823464484768615e-5 -0.00033279602012134557; -1.546409951408954e-5 -3.0313719478823625e-5 -0.00012786328994039177; -0.000967981777917801 -0.0008587598071053286 -0.0002961648129706392; -0.00028218419113336656 -0.00047066615031065434 -0.00016531728957816391; -0.0006908134885927305 -0.0006822494165206278 -0.00027650923169008734] %
+
+Mass Used: 134.38142875749008 kg
+Launch C3: 89.00345955325483 km²/s²
+||V∞_in||: 1.0665473910155583e-5 km/s
diff --git a/archive/ES_0.5602150007021635 b/archive/ES_0.5602150007021635
new file mode 100644
index 0000000..4b0f475
--- /dev/null
+++ b/archive/ES_0.5602150007021635
@@ -0,0 +1,22 @@
+archive/ES_0.5602150007021635---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:53:24.708
+Launch V∞: [7.913060737310488, -5.707417171572108, 0.1932874648702295] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000812191122355703, -0.0017273216316738922, -0.0006019347959317397] km/s
+ V∞_out: [-0.000706065434891513, 0.0010890993810571826, -0.0015249255615944353] km/s
+ time of flight: 1.856560104124226e8 seconds
+ arrival date: 2030-03-31T19:00:14.708
+ thrust profile: [0.38523321231843716 -0.005612010079108196 -0.12176987001005472; 0.13415595054095072 0.0752151864293685 -0.1467214394558678; 0.07166445346949103 0.06537776514538626 -0.1428555382846403; 0.03232203983258972 0.038959076334505106 -0.09796573807936337; 0.026721117047062096 0.0395330003610682 -0.10924778286626452; 0.0156172851541218 0.027376469397923892 -0.0832183340721821; 0.013147028283125889 0.026464194562382297 -0.08565389244764861; 0.00271795212143608 0.005854460796022389 -0.020809735264755384; 0.001159976830675361 0.002448246062996409 -0.012062012586559418; -0.0002577395847712144 0.003974873788911739 -0.015874030104583645; -0.0005573375834428615 0.0016030286139029537 -0.004236754429799601; 0.002021355364384824 0.002791159553123317 -0.0041031327428517755; -0.0006765463630925412 0.00022748748578549176 0.0029041333925229674; -0.0011734018419877882 -0.00030108281312101197 0.004332469590549167; -0.0033840798580448295 0.005292643137150701 -0.0013989276127286646; 0.012319888919936694 -0.009020966297279073 -0.0071003639569624626; -0.0001440485029025648 -0.0020110097733935543 0.003723038280169827; 0.004765182403395449 0.002673226708382247 -0.000884799744161838; 0.002554078413430072 0.0070195330136798234 -0.014271431030629448; 0.008601050768906342 -0.003669320017205091 -0.006389861506215505] %
+
+Mass Used: 98.08457804620866 kg
+Launch C3: 95.22850104679692 km²/s²
+||V∞_in||: 0.0020014044911100203 km/s
diff --git a/archive/ES_0.5602239913379634 b/archive/ES_0.5602239913379634
new file mode 100644
index 0000000..1b61528
--- /dev/null
+++ b/archive/ES_0.5602239913379634
@@ -0,0 +1,22 @@
+archive/ES_0.5602239913379634---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T02:27:30.943
+Launch V∞: [7.619735434202342, -5.887643026581721, 0.40021291050220187] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.981469649298933e-6, 0.00013485559511668436, 2.5117213722214026e-6] km/s
+ V∞_out: [0.00013013270876083678, -1.983506611498139e-5, 2.830381228465501e-5] km/s
+ time of flight: 1.8039772462627047e8 seconds
+ arrival date: 2030-01-28T00:56:14.943
+ thrust profile: [0.621233146572962 -0.015403910809371401 -0.15084413867591073; 0.08470480432496305 0.05022174612338314 -0.08682647170992067; 0.08345132041600342 0.08236966327387907 -0.14642807441973296; 0.03262574212641838 0.0426528745910009 -0.08905227552151779; 0.024364694603532293 0.04005707532561455 -0.09058688601764357; 0.019981737741343743 0.039638999534551835 -0.09570018629551443; 0.01646063181743757 0.03962158165377137 -0.10094261115894075; 0.008791108529411827 0.021500586156654154 -0.06081921846691291; 0.003469910723972119 0.009959986930508395 -0.02957072847138892; 0.00023342528337094506 0.0009093462533422041 -0.0028086032274675745; 0.0023618416529060334 0.00827022181363212 -0.026990299577088213; 0.001885584571012489 0.006791123753962206 -0.02272689234161296; -0.0009150635893919208 -6.293706009147346e-5 -0.0008094119501255254; 0.0004883532838505763 0.0014073450859400333 -0.003397699995993473; -0.0010759267882442967 -0.0012160371278433543 0.0001713157541449546; 0.0003950699215821089 -0.000690575466415659 0.0014201405888435187; 0.00030296267664921327 -0.0018949911320275674 -0.004148607062873686; -0.0010849636137197976 0.0034465472416881048 -0.0018192330155277765; -0.0016409944296881319 -0.003906972412514557 -0.0005143191895330856; -0.0004061859251687301 -0.0010651280942732524 0.003570599281994959] %
+
+Mass Used: 111.76619648929545 kg
+Launch C3: 92.88487886942775 km²/s²
+||V∞_in||: 0.00013489353765283891 km/s
diff --git a/archive/ES_0.5602471039772234 b/archive/ES_0.5602471039772234
new file mode 100644
index 0000000..8e35924
--- /dev/null
+++ b/archive/ES_0.5602471039772234
@@ -0,0 +1,22 @@
+archive/ES_0.5602471039772234---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T06:30:17.589
+Launch V∞: [7.992289145071185, -5.563170890992921, 0.20806238426204568] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2932967589836213e-6, -3.3986357724910903e-6, -3.523632634007841e-7] km/s
+ V∞_out: [3.204599701382064e-7, -1.78282787426015e-6, -3.6931924680475404e-6] km/s
+ time of flight: 1.8749577787477145e8 seconds
+ arrival date: 2030-04-21T08:39:54.589
+ thrust profile: [0.4688601167281144 0.009730061720296179 -0.13199104846905588; 0.08455431738958574 0.054775720862727806 -0.08892642514286177; 0.056254430913342125 0.059737237579409984 -0.10768009006011482; 0.03154909420663783 0.0466483878740275 -0.09516857556915433; 0.01665865931225893 0.03142664414754251 -0.0715962470013333; 0.008933289922798413 0.021540302556349016 -0.052285913884602554; 0.009628547419327426 0.025338234498964406 -0.06330782221278416; 0.0076106412946060605 0.0226965866243789 -0.06308951868010441; 0.00652333295307003 0.02732110760379602 -0.07520291375041564; 0.0028170622604916317 0.013796670470296847 -0.04215440273758565; 0.0009836100583223057 0.005098507107277665 -0.0205331137443883; -0.0006368848098227849 0.003815717738876969 -0.016131881791570962; -0.0007679472333287254 0.0030216038001908848 -0.004555420803208745; 0.005271022619963366 0.0009591237840104554 -0.0005917301773864479; 0.00041619877127149676 -0.0011500668096997833 0.0032308690326157056; -0.002484216288315968 -0.005055836938624469 0.0017884394425239335; -0.003759819904218352 0.0025036890124876814 -0.0018366277943136044; -0.0029768788484600983 -0.001093447126676815 -0.00276927413090804; 0.001480039403722713 -0.0006374927348555231 -0.0014659964143784385; 0.0002461446137860771 0.004115803493999768 -0.00599223222902246] %
+
+Mass Used: 100.22001907683625 kg
+Launch C3: 94.86884609655847 km²/s²
+||V∞_in||: 4.115105710454512e-6 km/s
diff --git a/archive/ES_0.5602706357271601 b/archive/ES_0.5602706357271601
new file mode 100644
index 0000000..9c70c02
--- /dev/null
+++ b/archive/ES_0.5602706357271601
@@ -0,0 +1,22 @@
+archive/ES_0.5602706357271601---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:52:52.114
+Launch V∞: [7.978631070773277, -5.664552120261628, 0.14598222361277147] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.649459515169164e-8, -2.315661712760691e-7, 4.1874393689080286e-8] km/s
+ V∞_out: [-3.521729098517736e-8, 1.3971345962262983e-7, 1.8628648302998484e-7] km/s
+ time of flight: 1.8651782472834563e8 seconds
+ arrival date: 2030-04-11T11:23:16.114
+ thrust profile: [0.4034029717778815 -0.004247939650995248 -0.12801405489905068; 0.0706249998165195 0.03937874539303828 -0.08073691376448182; 0.047276239871801115 0.04245758862122554 -0.09770393656115549; 0.034197698215366196 0.040247939514260624 -0.10492238169527587; 0.018683683736410377 0.026614056943226102 -0.07776696241768297; 0.024924149215746195 0.042151650038331843 -0.13125437755414193; 0.008417343818844155 0.016022692042504578 -0.05502770278053207; 0.005011334306993617 0.010786116637995748 -0.03986345259691634; 0.0100861925344487 0.024518063632296354 -0.0929324765747352; 0.0023643351950602097 0.0022048444800429304 -0.011357109332033434; 0.0007966021020971968 0.001798084127680363 -0.0034538503055504544; 0.004827528571642191 0.003113400682289589 -0.005307186905353414; 0.0027512678980048362 -0.00028431382459869067 -0.0014390938318534709; -0.002898798512045139 0.0017657743936165976 -0.001755326716823392; 0.004368038665588414 -0.003161668052839517 -0.004339964542437812; -0.0019826913760762318 -0.000846189266156707 0.0029129832855926937; -0.004884694193961979 -0.0013872386825630554 0.00630268448962306; -0.0017103007816765907 -0.005227554803843441 0.00606629070520965; 0.00010661356209575622 0.0003221339670933836 -0.0012287078261182822; 0.007964952934753581 0.001239765757260469 0.02734171834118519] %
+
+Mass Used: 95.00815245338572 kg
+Launch C3: 95.76701529628016 km²/s²
+||V∞_in||: 2.368086149162186e-7 km/s
diff --git a/archive/ES_0.5602840402871143 b/archive/ES_0.5602840402871143
new file mode 100644
index 0000000..0dff928
--- /dev/null
+++ b/archive/ES_0.5602840402871143
@@ -0,0 +1,22 @@
+archive/ES_0.5602840402871143---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:51:34.706
+Launch V∞: [7.632486446825971, -5.9057747751131915, 0.07489157065550289] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8633293919894465e-6, -2.7214528854699476e-6, 1.1737191042384804e-6] km/s
+ V∞_out: [-5.354145147200028e-7, -4.079683385801476e-6, 1.8204302397553456e-7] km/s
+ time of flight: 1.8749577787475288e8 seconds
+ arrival date: 2030-04-21T03:01:11.706
+ thrust profile: [0.38716187179731004 0.037613571417675545 -0.08263316305003639; 0.21112439358434518 0.16800772783228918 -0.15901040679148715; 0.1124381041719422 0.1521767114030072 -0.16063316718091145; 0.05934993070901889 0.1146251587811897 -0.13774662818373412; 0.02886600456239436 0.0720299167922246 -0.10004877674507533; 0.014698690180335495 0.04872280440670634 -0.07354855474225594; 0.006403258897349658 0.02399920223088754 -0.039518856310241685; 0.004659436361721921 0.02677077815264689 -0.04704446954427099; 0.0003082543321883931 0.0030703056731545306 -0.006032265780377368; 0.00024823356232264656 0.0018496782035220525 -0.0036706098269276384; 0.00013426624900581336 1.8660307085668405e-5 4.94179378615766e-6; 6.395573082398891e-5 3.6105283897595164e-5 -5.645411096511326e-5; 8.206570221574503e-6 5.101364007377407e-5 0.00014430530143510478; 0.00015403099031949016 0.0001433995864261373 0.0002918413329102381; 0.00020302378832338268 1.0994958226081378e-5 -0.00017521034986209668; -0.0001002946006552211 -0.00034098554529313777 6.967500028744476e-5; 0.0001369258607608913 -0.0001096251382392308 8.572542607462961e-7; -0.00018533829694241774 -0.0001370339925789442 -0.0002007018437846025; 0.00017206969314855346 0.00023694859296927737 9.988295493295842e-5; 9.445878197133722e-5 1.665220175190382e-5 -0.0001706247856170215] %
+
+Mass Used: 110.35601648587954 kg
+Launch C3: 93.13863380270065 km²/s²
+||V∞_in||: 4.1209923016814456e-6 km/s
diff --git a/archive/ES_0.5602863319860043 b/archive/ES_0.5602863319860043
new file mode 100644
index 0000000..8903ebb
--- /dev/null
+++ b/archive/ES_0.5602863319860043
@@ -0,0 +1,22 @@
+archive/ES_0.5602863319860043---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T16:52:58.359
+Launch V∞: [7.94641617487281, -5.71453544854656, 0.1375447735516621] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0001285258645900992, 8.596432089903681e-5, 0.005449770262124062] km/s
+ V∞_out: [-0.005108168884482949, -0.001683523599602654, 0.0007653632460284164] km/s
+ time of flight: 1.8431468819243166e8 seconds
+ arrival date: 2030-03-15T23:24:26.359
+ thrust profile: [0.3803785835414188 -0.009816260631174783 -0.11839616899722605; 0.08096756275563037 0.04514160443856629 -0.09096232634856391; 0.04287608264248488 0.038507049891461205 -0.08698414736872058; 0.05176588737404817 0.062286137354082144 -0.15219623663707688; 0.030589692621936417 0.044744372904934236 -0.12345806399602983; 0.014689643592279972 0.02532389088751724 -0.077712080449026; 0.014492095202470124 0.028919808893806482 -0.09297944667308788; 0.008067528136268313 0.009829146272825712 -0.044909787920999575; 0.002688531443160863 0.006114746460961267 -0.018319267718314432; 0.002801267359364274 0.007623849752820992 -0.029659905738675538; 0.0001797563370097988 0.0015148022735122814 0.0006189721123504737; 0.001483419588455851 -0.0007542262065511353 -0.005554075641374742; -0.00031478763029959075 -0.002566514211626523 0.0011879166319975877; 0.0020953281907271472 0.0006092643392155747 -0.0022588896819162145; -0.005357829070665692 0.001779041573465537 -0.00044510734300545643; -0.003060287574795834 0.002029752796619444 0.004303125457296781; 0.005706863049673148 -7.636217718069401e-5 -0.0023117495282245497; -0.005829197017407933 0.011971323737445016 -0.0017486944041932725; -0.000899952162659943 9.565332628924556e-5 -0.015871556741890787; 0.00791398926862151 -0.0012860468378826416 0.008832039819684868] %
+
+Mass Used: 94.71526409038188 kg
+Launch C3: 95.82036398170682 km²/s²
+||V∞_in||: 0.005451963377744574 km/s
diff --git a/archive/ES_0.5602893001843319 b/archive/ES_0.5602893001843319
new file mode 100644
index 0000000..f921446
--- /dev/null
+++ b/archive/ES_0.5602893001843319
@@ -0,0 +1,22 @@
+archive/ES_0.5602893001843319---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T16:08:54.303
+Launch V∞: [7.766038914286816, -5.768332185965305, 0.008935352800472668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.05985060321553861, -0.36534623738466115, -0.4388494697647462] km/s
+ V∞_out: [0.23078624681503015, -0.20309677524904368, 0.4843237000579602] km/s
+ time of flight: 1.8503580027717608e8 seconds
+ arrival date: 2030-03-24T06:58:54.303
+ thrust profile: [0.5491473997275427 0.001580730255236155 -0.15314135794676492; 0.10642997052623608 0.06582161699092284 -0.10741174320891123; 0.051393955674012816 0.052947136570024166 -0.09721042947132394; 0.03624307166402106 0.050765233215872375 -0.10362562962566363; 0.01647576164544909 0.028230542322812423 -0.06581783144679257; 0.01420382361314306 0.030108536034417384 -0.07481815751989356; 0.004200513082265933 0.017496965559860383 -0.06882599121125269; 0.01632355685374144 0.04808568816824779 -0.12716298056368774; 0.003755278330531995 0.016161461501883388 -0.046389803289531156; -0.0007614001839579075 0.0016717888309674383 -0.007765248589276399; -0.000510488504258967 0.005158187643560651 -0.003634434616855379; -0.002033258788261047 0.0007219213397132157 -0.006513951244957558; 0.0007526049697700044 -0.002300075526748413 4.364068118915799e-5; 0.000253037223051843 0.003019384870330221 -0.011994071966958168; -0.003088788135767322 -0.003805502944876934 0.0028412850496300213; 0.0011372935623226279 -0.0008478815730583642 0.0042789522293075815; -0.00014531483587366934 0.005453776088297281 -0.004337147708121006; -0.0032258805301382813 -0.0008988051224941454 -0.009822375592373414; 0.0005442240304894541 -0.002225880464874282 -0.0021421240019847683; 0.000845055879610435 0.00041957437932087964 -0.005088279258840656] %
+
+Mass Used: 107.75778749444498 kg
+Launch C3: 93.58509646639008 km²/s²
+||V∞_in||: 0.5741505246790182 km/s
diff --git a/archive/ES_0.5602915703693883 b/archive/ES_0.5602915703693883
new file mode 100644
index 0000000..c347fa2
--- /dev/null
+++ b/archive/ES_0.5602915703693883
@@ -0,0 +1,22 @@
+archive/ES_0.5602915703693883---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T11:17:59.270
+Launch V∞: [7.975300388758037, -5.7772861309600625, 0.12825005107759682] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.988287971489267e-6, -3.6695309099208057e-6, 4.140060364847344e-6] km/s
+ V∞_out: [-9.283665107145392e-7, -6.746443709196796e-6, 3.281930114025115e-7] km/s
+ time of flight: 1.8383349594062707e8 seconds
+ arrival date: 2030-03-11T04:09:34.270
+ thrust profile: [0.28312639447075094 -0.009031978707666425 -0.08879448006911039; 0.0854983568966706 0.0466662097359928 -0.095594137422729; 0.05057863431326616 0.04332012176128479 -0.10089279792428235; 0.02488724287661211 0.028558702349435187 -0.07445880283797617; 0.029118675749501555 0.04029454474070736 -0.11629791481891816; 0.013656638934819373 0.022458008338511637 -0.07222278144029823; 0.013835062190620397 0.023798041459955514 -0.08044293791604831; 0.017319837133265178 0.03387094239552642 -0.11945052683042527; 0.0024831949693541475 0.0054136233309117435 -0.019233016885536487; 0.004995068070976288 0.012414636553810495 -0.049643335431397324; 0.0013510091761966961 0.002156757443833777 -0.01038593874025474; -0.004030345043266496 0.004392227128949013 -0.002140265504176434; 0.0011088799220586774 0.0005128922314119174 -0.0023318937191060198; 0.0010035821313909513 -0.0028687612044025097 0.0005649291616982542; 0.00019521687144049936 0.0021732131360404096 -0.008396622204964867; 0.0011605246371752843 -0.001748938433507497 -0.004376601514817772; 0.003502312267936468 0.010864282964202294 0.0030372320008047226; -0.005650066291225378 -0.0022445121873297166 -0.01229005797349112; -0.0009636632538147455 -1.532187035159331e-5 -0.0009764225015789028; -0.011691924299779714 -0.0011678680909887366 0.007358622304729818] %
+
+Mass Used: 87.84658556548402 kg
+Launch C3: 96.99889940550898 km²/s²
+||V∞_in||: 6.81997051804259e-6 km/s
diff --git a/archive/ES_0.5602922998132391 b/archive/ES_0.5602922998132391
new file mode 100644
index 0000000..00c1905
--- /dev/null
+++ b/archive/ES_0.5602922998132391
@@ -0,0 +1,22 @@
+archive/ES_0.5602922998132391---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:22:21.892
+Launch V∞: [7.7031299846095616, -5.878940082607888, 0.15704982229220185] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9275671298815518e-9, -6.439711541691215e-9, -8.444253221191209e-10] km/s
+ V∞_out: [-1.599789298781557e-9, -3.0774534701506154e-9, -8.177815181262618e-11] km/s
+ time of flight: 1.8337229330955863e8 seconds
+ arrival date: 2030-03-04T13:07:14.892
+ thrust profile: [0.5002064037717421 0.0011218618059782733 -0.11168884840017412; 0.08572009425458746 0.057301371926719254 -0.08135433283379094; 0.05029913256315154 0.05574338546462779 -0.08677527505529779; 0.06216020863310165 0.0937564365350225 -0.15216532916815678; 0.029831836453365325 0.05941390404163906 -0.11007710683072146; 0.012993995483451254 0.030393699017002278 -0.06314892890742747; 0.009521340540653992 0.023234587226624304 -0.05245566210105477; 0.012496427136382188 0.04314731210032568 -0.09440427107930759; 0.0019765585537100385 0.008926636056775092 -0.020286487040057005; 0.003753731093606236 0.018191476874524704 -0.044399742727949484; 0.0016069189574570214 0.010321099757923379 -0.023882293820913822; -0.0015549329927749696 0.0010165771126700565 -0.0018672386115976152; -0.0016783167141453475 0.003934582005779732 -0.006107672905726691; 0.004619776583707318 0.0009360498246600633 -0.006078947738375325; -0.0005301635795394771 0.0005424531203632376 0.0006860403603132306; 0.0005095283503370079 -0.002555387579138429 -0.00012437897974829234; 0.001626836240673158 0.006826826825491048 -0.0061331427663210095; 2.1184526521279205e-5 -0.0010803650139344263 -0.0033032588262675447; 0.00019850184881444998 0.00222740759700879 -0.0011989878135896439; 0.002223353446998616 0.0008784670217356939 -0.004484565637857204] %
+
+Mass Used: 105.77960902414088 kg
+Launch C3: 93.92481270136655 km²/s²
+||V∞_in||: 7.124155259733601e-9 km/s
diff --git a/archive/ES_0.5602987636834301 b/archive/ES_0.5602987636834301
new file mode 100644
index 0000000..3a56e9c
--- /dev/null
+++ b/archive/ES_0.5602987636834301
@@ -0,0 +1,22 @@
+archive/ES_0.5602987636834301---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T20:29:54.604
+Launch V∞: [7.860939742849362, -5.618987500749103, -0.007490092567396749] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2451040553735311e-9, -1.3803812736638359e-9, -4.127170562657816e-10] km/s
+ V∞_out: [2.6676101461745517e-10, -9.039405177622951e-10, 1.3936525516110347e-10] km/s
+ time of flight: 1.8434996502499637e8 seconds
+ arrival date: 2030-03-14T12:49:19.604
+ thrust profile: [0.6323141466194392 -0.007468058329721813 -0.1673280405140423; 0.04485557055244832 0.0272344821995042 -0.047809079586365724; 0.03384118106043711 0.034327987356386654 -0.06556401726900302; 0.02444286696927571 0.03362186080276007 -0.07081038053031145; 0.020304920967857958 0.03509854659918862 -0.0809899083029256; 0.06597378853360053 0.11976352505936458 -0.2620179832282035; 0.010061117577508945 0.02348129230573662 -0.06434796190149564; 0.005064675549030203 0.014511629707290304 -0.04188208485784791; 0.004192052425732327 0.013923579483409143 -0.04187572610346683; 0.00011214675868046462 0.0023880002394760748 -0.007296598532123348; 0.0002568777791219761 0.0031759691314737753 -0.008828283579117233; -0.0009803442676545823 8.781524508809347e-6 0.0016195488303556405; 0.0005542064915762332 0.0012907332443078726 -0.004622890495791879; 0.002830579416194066 0.00046538933917884937 -0.0014636047859697167; -0.0047625055656028295 -0.0021425284705344854 -0.0029800181489869604; -0.0018477522659886367 0.0026317306327773146 0.0009807131702881224; 0.0042758008288029965 -0.00026120521800365227 0.0006407746985726279; -0.00751961690867411 -0.0015319594353878218 0.002458701920670504; 0.001501344798556807 -0.0001779501784035456 -0.0006983372383695546; 0.002055483519648668 7.625113633989891e-5 0.00025400499924520335] %
+
+Mass Used: 109.03843102201063 kg
+Launch C3: 93.36745027576991 km²/s²
+||V∞_in||: 1.9042247603479217e-9 km/s
diff --git a/archive/ES_0.5602992440801475 b/archive/ES_0.5602992440801475
new file mode 100644
index 0000000..5cbf24f
--- /dev/null
+++ b/archive/ES_0.5602992440801475
@@ -0,0 +1,22 @@
+archive/ES_0.5602992440801475---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T22:39:38.818
+Launch V∞: [7.714499934271329, -5.952264437517146, 0.06275744515669916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.81970205395515e-5, -3.686572908899052e-5, -3.050406112977239e-5] km/s
+ V∞_out: [-6.438296147304297e-6, 4.081800499791373e-5, -5.385036821248056e-5] km/s
+ time of flight: 1.7803456489132538e8 seconds
+ arrival date: 2029-12-31T12:42:22.818
+ thrust profile: [0.43120573614098895 -0.013483477963340602 -0.12147562004547598; 0.07150236907657424 0.0395564216158033 -0.07546620882705406; 0.08427037174807153 0.08101134777422794 -0.15500823546679457; 0.050212130504123265 0.0634664920611228 -0.13658281772582045; 0.02658547396029834 0.040030536876401096 -0.09759559874829384; 0.023932083522385305 0.04330217549117928 -0.11142021191927164; 0.011853065940183987 0.024331640536970234 -0.06886610889011152; 0.010985686459463228 0.027009258444631947 -0.07932962576724915; 0.0010280984120198434 0.0029260303391276474 -0.009400268780011203; 0.0043819246780825456 0.012667224905752221 -0.041095260347973325; 0.0019289312168915026 0.006160440586262819 -0.021544208025410825; 0.0003872805634393378 0.0006334703167931799 -0.0014431212438394403; -9.831059580050019e-5 0.00014888692927262688 -0.0033882787521952746; -0.0005568115499661095 0.0003601532021066211 0.00032675305076950833; -0.0005062154804728769 0.0012686735937134023 -0.0036779407739120262; -0.0017404317009397626 0.0001911389663038325 0.0010088905854155417; -0.0049446196735204746 -0.00021104915134081666 -0.0018113168884188347; -0.0004943852509467313 -0.00399682721767056 -0.00010970545009608095; 0.005650422679498647 0.003465319325130367 0.0021369263851532877; -0.0013097342251393728 0.002267570338105515 -0.0015238445437101983] %
+
+Mass Used: 99.82553670310244 kg
+Launch C3: 94.94689966692623 km²/s²
+||V∞_in||: 6.791562791848193e-5 km/s
diff --git a/archive/ES_0.5603242981349826 b/archive/ES_0.5603242981349826
new file mode 100644
index 0000000..3e6f693
--- /dev/null
+++ b/archive/ES_0.5603242981349826
@@ -0,0 +1,22 @@
+archive/ES_0.5603242981349826---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T09:56:09.716
+Launch V∞: [7.8088896350332195, -5.6242508853256625, 0.009643988461029297] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.113236609934206e-11, -8.076414636570552e-10, 5.0404914248673565e-9] km/s
+ V∞_out: [1.4032443967644015e-9, -4.394615986090624e-9, 7.036574053309837e-10] km/s
+ time of flight: 1.8749577787493792e8 seconds
+ arrival date: 2030-04-20T12:05:46.716
+ thrust profile: [0.5851545837904677 0.019755232981916972 -0.14555972558150537; 0.15267662195540121 0.10674012175614458 -0.14494740215090562; 0.05704678740871782 0.06777956366778262 -0.10710342646181466; 0.02705549626539993 0.042217083591984 -0.07731355458914838; 0.030715536396199148 0.06651381852224672 -0.12549128140032206; 0.016155201094264753 0.04265834808019787 -0.09018235308997524; 0.007230035071199039 0.022236361348663632 -0.051538529984642825; 0.004519772951471086 0.017525564838475092 -0.04153260985475818; 0.0028524593826671973 0.01304247854235184 -0.034208998387441035; 0.0015398379332365215 0.009460041664688933 -0.02545618022028263; 0.0016750563180056735 0.0010166177745357607 -0.006472421895249981; 0.0007607208474963179 0.0040835337490039356 -0.003306717208740187; 0.0001422128853136381 -0.00021202782185437117 0.0009995588636986107; -8.108490166812131e-5 -0.0017877389495923781 0.003546888371943428; -0.00018941843971426997 0.0005895229796712894 0.0014440209376519128; 0.0017604926042562642 -0.00021875919810621417 -0.0013129552854794719; -0.0013067087906121603 0.0005646651161265055 -0.0023148731552930786; 0.0005708388882899283 -0.002114934899223272 0.0017856804444942316; 0.0005766919648651013 0.00017588530372218908 0.007194592652600158; -0.0027087269468395276 0.0016494929651241965 -0.0018605739248370471] %
+
+Mass Used: 113.48056572572614 kg
+Launch C3: 92.61104835972918 km²/s²
+||V∞_in||: 5.105151878657908e-9 km/s
diff --git a/archive/ES_0.5603254614679557 b/archive/ES_0.5603254614679557
new file mode 100644
index 0000000..f0329d7
--- /dev/null
+++ b/archive/ES_0.5603254614679557
@@ -0,0 +1,22 @@
+archive/ES_0.5603254614679557---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T20:10:24.341
+Launch V∞: [7.8238594714128356, -5.726934012330708, 0.05704331342187244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.951905561811064e-10, 8.963869207261442e-10, -1.4537673449061447e-9] km/s
+ V∞_out: [4.828795776091796e-10, 6.854648750352835e-10, 1.8178773743630296e-11] km/s
+ time of flight: 1.8749577787441736e8 seconds
+ arrival date: 2030-04-20T22:20:01.341
+ thrust profile: [0.407009253331721 0.021275156582901727 -0.09651358753994983; 0.13645513321830768 0.09792950533297119 -0.1187970410118603; 0.10769991651894044 0.13246538375069336 -0.16641835828755358; 0.05747806537988653 0.09670309917357496 -0.14391210473494317; 0.029689755498221823 0.06492799303827111 -0.10772442423096519; 0.011242431079950215 0.030383751766051976 -0.05521037975469588; 0.0056423189536639416 0.019221772821552484 -0.037389735022560724; 0.005086837741873012 0.023474517431206834 -0.047250578378868854; 0.0013073113033896125 0.006893237201501671 -0.014702662079587465; 0.0006012816227057333 0.0052936852031661786 -0.009273725681243523; 0.0015736460422904536 0.0013435506185832814 -0.00471696903967827; 0.0015234262031581238 0.0014555056883686906 -0.003046433573539364; -0.0016177518311598568 0.00031348647312795877 -0.0035522789545659747; -0.0020528199244797245 -0.0033532926611402293 -0.0026695652554974978; 0.004725656820306021 0.0008380885570308301 -0.0018712089035535168; -0.00632568518417859 -0.0008136968139231943 -0.001866596076016227; -0.0014969179086602694 0.0032324275750512783 -0.006154209381813435; 0.003715563683944859 0.005952154558694215 3.1024858875139134e-5; -0.0002452973028699796 0.0018713909236655172 -0.002648316824142502; 0.0018378515463245895 -0.0014479702224763436 0.000549565460627008] %
+
+Mass Used: 105.29918083987377 kg
+Launch C3: 94.01380414961278 km²/s²
+||V∞_in||: 1.883952500835405e-9 km/s
diff --git a/archive/ES_0.56032895143903 b/archive/ES_0.56032895143903
new file mode 100644
index 0000000..f8ac3d6
--- /dev/null
+++ b/archive/ES_0.56032895143903
@@ -0,0 +1,22 @@
+archive/ES_0.56032895143903---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T14:00:28.442
+Launch V∞: [8.102719035581494, -5.835410973239287, 0.3011873881368503] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.440781117178352e-6, 5.3963026042871146e-5, -0.001065548511621904] km/s
+ V∞_out: [-4.390238540417937e-5, 0.0010695531374559802, -1.2409687641223669e-5] km/s
+ time of flight: 1.8706541066479704e8 seconds
+ arrival date: 2030-04-20T16:37:18.442
+ thrust profile: [0.08092395818104162 -0.000292923292609924 -0.0286675851315478; 0.07742738159230124 0.04258373238564331 -0.08816443518069403; 0.04736931034341432 0.04028839819256975 -0.09798096455357626; 0.022863390520473117 0.024867533700738246 -0.07138200488687779; 0.018039383319022644 0.023278127965873596 -0.07450920021171442; 0.021633560842027746 0.03289808848178339 -0.11386094439307902; 0.019940232337110265 0.03495595712128842 -0.1251569354949235; 0.008453267489506026 0.015181067723105898 -0.06125239754965482; 0.00680284486379065 0.012963678007671049 -0.05592403844004439; 0.00046738771922514525 0.001091303637598407 -0.005953021426565956; -0.00014325612841146958 -0.0005266315111787463 -0.0005582759788089319; 3.5536674159596115e-5 -0.00011740845655378761 0.00019004016046931561; -0.005988471140339478 0.004040969600309437 -0.007571171162693827; -0.007497602736142212 0.0035298215517888362 -0.019824027262981447; 0.002336338950150325 -0.003319860675938326 -0.00669393620493808; 0.006087217450633799 0.01517430721803128 -0.017030831827917127; 0.0052910406967254155 0.007621841832480988 -0.015261867195401289; -0.0006707861512216344 0.001834033021805938 -0.0003032160351428713; 0.0035175121923105524 -0.0007649180478209645 -0.005830562252700781; 0.0016013953249399424 -0.001496164575397235 -0.003844632600876087] %
+
+Mass Used: 71.56916345166655 kg
+Launch C3: 99.79679083894888 km²/s²
+||V∞_in||: 0.0010669279455045328 km/s
diff --git a/archive/ES_0.5603309774720404 b/archive/ES_0.5603309774720404
new file mode 100644
index 0000000..40f6556
--- /dev/null
+++ b/archive/ES_0.5603309774720404
@@ -0,0 +1,22 @@
+archive/ES_0.5603309774720404---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T12:32:11.324
+Launch V∞: [7.941952931912107, -5.718867414866672, 0.13746848175982537] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.30880679578526e-7, 2.828463953917032e-6, -6.678627249604418e-5] km/s
+ V∞_out: [-2.81404632246236e-6, 6.67802273580505e-5, -5.898379925466394e-7] km/s
+ time of flight: 1.8561796058860648e8 seconds
+ arrival date: 2030-03-31T21:04:51.324
+ thrust profile: [0.38722300414830163 -0.004142442204133084 -0.12166315001542527; 0.07920936754201052 0.04565170628990136 -0.08973699726875273; 0.0500256976355068 0.04690440573597548 -0.10276245985221044; 0.04304398431077701 0.053602506132827445 -0.1323824038197051; 0.01903157506963506 0.03155553910932557 -0.08518315918914733; 0.01935427265119439 0.03677031771552448 -0.10793890224243373; 0.007817300272028786 0.01502007249577431 -0.05217143035685404; 0.005486668357296791 0.011435258429677497 -0.04349177196931983; 0.0036882390776938547 0.011877362692192616 -0.046259418282753866; 0.0028299894991856336 0.009525956089599658 -0.04547259713022202; -0.0010392462833565593 0.004587460514030276 -0.008176953469286014; 0.0013625459074273203 0.002140836093639555 0.0003623993761588378; -0.0032818638650699743 -0.0034041380604077336 0.004909725537126422; -0.00014198182743298677 -0.0037864188323656887 0.001436135214097376; -0.009687144599611012 -0.001769157670374654 -0.0037067667272633713; 0.010888058255537205 -0.0008450963816762548 -0.0013829712713471511; -0.005891140237630512 -0.0052441041854144384 -0.004828665466881601; -0.011433262596841316 0.0032909609892346216 -0.003729230135559307; 0.00026366214779420744 0.0006972579131035979 -0.0036717420525834614; 0.0017951972921280367 0.002665516842566604 -0.0027192823264967823] %
+
+Mass Used: 94.89221600483097 kg
+Launch C3: 95.79895846500848 km²/s²
+||V∞_in||: 6.684752845404615e-5 km/s
diff --git a/archive/ES_0.5603579702988791 b/archive/ES_0.5603579702988791
new file mode 100644
index 0000000..a96e19d
--- /dev/null
+++ b/archive/ES_0.5603579702988791
@@ -0,0 +1,22 @@
+archive/ES_0.5603579702988791---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T13:53:05.002
+Launch V∞: [8.011851449058566, -5.775476535582745, 0.11403846731863763] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.405805114757155e-5, 4.583293340510882e-5, 0.0031923889388430255] km/s
+ V∞_out: [-0.002862217988001292, -0.000956963186555737, 0.0010390233802837394] km/s
+ time of flight: 1.855227490452584e8 seconds
+ arrival date: 2030-03-31T19:58:54.002
+ thrust profile: [0.25734879857826004 -0.003164770623032367 -0.08115305257140021; 0.060186662893844174 0.03385475806272327 -0.065880253800961; 0.03752898625253003 0.030238236066654805 -0.07695168622705911; 0.036273394704112935 0.04133245915413833 -0.10048739330181168; 0.027900464995217072 0.039458837205503396 -0.1043759423068929; 0.020150577092110114 0.0328012190771901 -0.0940468357107415; 0.023392977609118945 0.04379977468862967 -0.14428418226188294; 0.006238967544105335 0.014041791314202457 -0.05254122314088444; 0.0007393482796325909 0.008507655816469794 -0.01794694455178264; 0.00275036876853984 0.006289194949262074 -0.02619340990631265; -0.0030260406800431128 0.002197674514234399 -0.02238355108046488; -0.00195869392847644 -0.006073477935805519 -0.010303626664011547; -0.0026530878878062276 -0.0003058298773575788 -0.0026812733801619944; 0.0009628413641766949 -0.004336228396645125 0.005382715619439119; -0.005585599827180725 0.0067653726490128265 0.0014951508738261115; -3.659366742859993e-5 0.0014207582253710814 -0.01059724114616491; 0.0017142116935909002 0.0013605760973035821 -0.010559939945163705; 0.0006216623497057981 0.0026975883761662257 -0.012482560707447464; -0.004913253815519113 0.003927771869270961 0.0025599126998467666; 0.002686952229354762 0.0012869218651853434 -0.008359546200480234] %
+
+Mass Used: 84.65739585857591 kg
+Launch C3: 97.5588976268771 km²/s²
+||V∞_in||: 0.003193360491480509 km/s
diff --git a/archive/ES_0.5603972316887321 b/archive/ES_0.5603972316887321
new file mode 100644
index 0000000..3b9fd13
--- /dev/null
+++ b/archive/ES_0.5603972316887321
@@ -0,0 +1,22 @@
+archive/ES_0.5603972316887321---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T20:10:20.648
+Launch V∞: [7.82147084174267, -6.051905872930394, 0.04244106176468869] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002978104519759197, 0.00019848212607685492, 0.01221512854348886] km/s
+ V∞_out: [-0.011483987350819909, -0.0037763561181648458, 0.0017788532438091026] km/s
+ time of flight: 1.7788632565225708e8 seconds
+ arrival date: 2030-01-01T17:02:25.648
+ thrust profile: [0.2448453912795824 -0.023557394513250614 -0.08920262535263623; 0.06716147543392152 0.027513361837433564 -0.08323496113156308; 0.03319068250879252 0.022077706920288615 -0.0731256902300908; 0.031071923970491605 0.0262101006251084 -0.09736267137345349; 0.059205079068792923 0.05579504152254539 -0.22278767920455694; 0.019582712033063658 0.021448625457653803 -0.09879490387135116; 0.008273742185554395 0.010063600749085844 -0.05099410738009529; 0.013311904924123092 0.0167515329765397 -0.09013643477623423; 0.008058120971694819 0.01131491115689128 -0.065390732860607; 0.0017252188382960664 0.0027416618191702224 -0.015278615114347001; 0.0012110727412316718 0.0002458960803193935 -0.003492004366770414; 0.0004703522726493448 0.0009984045764672436 -0.006242603452404065; -0.0005852297137520707 0.0008574984480024397 -0.0008449926603921416; 0.00039392562706743817 0.0009561045735235425 0.00218713826801914; 0.0001993490293430854 0.000569176102434681 -0.002363626062428984; -0.0005354572555597524 -0.00210864618130004 7.087452243686315e-5; 0.004337473442385025 -0.0035512488687109165 -0.0017931553294643408; 0.0034278446633235985 -0.0032942327873341473 0.007006893224353468; -0.008448715491330402 -0.0046034278692354234 0.004000561065395924; 0.002960762808387783 0.0011524422507545999 -0.002038179909017734] %
+
+Mass Used: 83.28059991406462 kg
+Launch C3: 97.80277206676391 km²/s²
+||V∞_in||: 0.012220370352556192 km/s
diff --git a/archive/ES_0.5604124930927892 b/archive/ES_0.5604124930927892
new file mode 100644
index 0000000..2bc9307
--- /dev/null
+++ b/archive/ES_0.5604124930927892
@@ -0,0 +1,22 @@
+archive/ES_0.5604124930927892---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T11:15:26.597
+Launch V∞: [7.7823474213211075, -5.701661352561651, 0.15832413733449796] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.359298467553369e-8, -1.0320168203255678e-7, 2.3168855693386472e-8] km/s
+ V∞_out: [-1.835978759491671e-8, 6.270270608692083e-8, 8.632333481559821e-8] km/s
+ time of flight: 1.808605310617213e8 seconds
+ arrival date: 2030-01-31T18:17:37.597
+ thrust profile: [0.5820008448111614 -0.02665956631445329 -0.1702922093764402; 0.15054270347699406 0.08155968571375616 -0.15298110799747133; 0.06566560031586754 0.059167671079237365 -0.12212293121122662; 0.05845430118134402 0.07046450482671286 -0.15989867530674357; 0.02261120313930792 0.03402519330206719 -0.08606784769945211; 0.01243140428380554 0.023084930749564195 -0.06221850998187286; 0.004340687420509976 0.012130325764695778 -0.03064951493898402; 0.010893846353406894 0.027430829519646222 -0.08596299051750399; 0.006321731896882183 0.005200901452873962 -0.031616680020479966; 0.0011742913937072762 0.00413978787662985 -0.013629018492637071; -0.0006141528444320336 0.0010690587631155875 -0.0045728500952458215; 0.0008236190348599165 0.003033044612931262 -0.009686916510180115; -0.0003599784932857259 0.0014810958920029376 -0.00433828404668195; -0.0002722709271414034 -0.00018549599459690563 -0.0010376862585614642; -0.0008448094572882554 0.0006208860256162987 -0.0036381876236983904; 0.00010076154552219615 0.0005812021931083052 -0.0011343902507180248; -0.0001232686671130201 0.0020256616730028537 0.001242492897860173; -1.0104022983976684e-5 -0.0003102797771705095 0.0007115036613404965; 0.00017500333317864493 0.0009242415892183142 -0.00045084057490035073; -0.0008124952801865279 -2.4650495704380514e-5 0.0021604272746700882] %
+
+Mass Used: 110.73742470383058 kg
+Launch C3: 93.09894009790116 km²/s²
+||V∞_in||: 1.0664029388968888e-7 km/s
diff --git a/archive/ES_0.5604195705327268 b/archive/ES_0.5604195705327268
new file mode 100644
index 0000000..0d831b1
--- /dev/null
+++ b/archive/ES_0.5604195705327268
@@ -0,0 +1,22 @@
+archive/ES_0.5604195705327268---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:23:10.641
+Launch V∞: [8.097945511938502, -5.677143621694586, 0.06813534418839208] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.7053456589119566e-7, -3.587863988839486e-5, -5.691942177132988e-7] km/s
+ V∞_out: [-3.484028573378259e-5, 5.219037867107104e-6, -7.500234586029123e-6] km/s
+ time of flight: 1.8749577785800332e8 seconds
+ arrival date: 2030-04-23T20:32:47.641
+ thrust profile: [0.22674277487316272 9.030082476870328e-5 -0.07633936166803786; 0.05765082403718509 0.0320617952565917 -0.06865020012790214; 0.06519962078633584 0.06007514842226691 -0.13968088213883703; 0.04566387742543459 0.055703933342909566 -0.14460303576444858; 0.01781293089061038 0.025440295387905532 -0.07838409894374132; 0.010111623879184756 0.018143045912150706 -0.06206045179210094; 0.008374121876075414 0.01556703342129642 -0.057795150834831124; 0.005358074243232599 0.014045169965199951 -0.05642652688128872; 0.004010319325134157 0.007093058373343671 -0.04053386494314167; 0.0030688616747854345 0.011498609732772383 -0.029507720308914125; 0.0034291836522373775 0.00319210189233986 -0.021847728099358657; 0.0009788447406157293 0.005496346013695768 -0.0026777522150433944; 0.0023389219593847425 0.0012219900973071828 -0.0054995624915636695; 0.012643226042009029 -0.003016962021599444 -0.004031325852548137; -0.00847570594066013 0.00856049005809054 -0.003589690710635594; -0.0008857947310777558 -0.0021941296642448635 -0.003426783904623134; -0.0034205206217436147 0.0013449371041492973 -0.01413640467974833; -0.006718812462381461 0.004654137079225277 -0.003213101939454509; -0.008789026198372067 -0.007427417147036954 0.006772813636152442; -0.00014782555856167096 -0.006805823693568846 0.007652271192743083] %
+
+Mass Used: 83.25677771684741 kg
+Launch C3: 97.8113236408001 km²/s²
+||V∞_in||: 3.5886239494774254e-5 km/s
diff --git a/archive/ES_0.560435214748318 b/archive/ES_0.560435214748318
new file mode 100644
index 0000000..94022ef
--- /dev/null
+++ b/archive/ES_0.560435214748318
@@ -0,0 +1,22 @@
+archive/ES_0.560435214748318---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:29:53.646
+Launch V∞: [7.802837211928767, -5.8471332534133085, -0.035640765739772554] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0669485530348471e-7, -9.8634915288157e-7, 1.7054658943116128e-7] km/s
+ V∞_out: [-1.6250952295610975e-7, 6.182590351586972e-7, 7.801615757717201e-7] km/s
+ time of flight: 1.8347206787390974e8 seconds
+ arrival date: 2030-03-06T20:57:40.646
+ thrust profile: [0.4482214721894321 -0.007165490464115699 -0.12837813006526289; 0.05802757216897871 0.033193316817769825 -0.06704393493824785; 0.06131978721670937 0.055981963598821294 -0.12037731886847731; 0.03634037913095832 0.04336843032839886 -0.10535657752757348; 0.03312332714556019 0.048322784204118625 -0.13114497262124988; 0.02681310963560094 0.04647072279397378 -0.1352954789463009; 0.008822711463772842 0.018721187003969107 -0.05651235698733448; 0.006515152173255411 0.014799159390212847 -0.05085985985148953; 0.006126985989675349 0.015433796610045203 -0.05274421327834683; -4.910247510478373e-6 0.004208797793493856 -0.002342007362853725; 0.0005668877448363484 0.0028082841421635577 -0.009016881126563951; -0.003700683371348536 -0.0002002060715796198 0.0007604188489292638; -0.00047878824708823026 -0.00012417997617753345 0.00018744304336148327; 0.0015553316429570622 -0.0005935233892543014 -0.0012584653841131116; 0.0014287163344558031 -0.0012081295516744208 0.00025488302880441276; 0.0011867357626821446 -0.005203497902342018 0.00336976789054787; 0.006140979675764156 -0.0018764563491276112 0.012275742091567851; 0.005907926255620096 -0.00020776610560255314 -0.00647212049872274; 0.007422798678821962 0.0024791463057372 -0.009986612441731187; 0.003259602578083117 0.008785730158738174 0.00036490002055836684] %
+
+Mass Used: 99.23979827095309 kg
+Launch C3: 95.07450610321452 km²/s²
+||V∞_in||: 1.0066551458692414e-6 km/s
diff --git a/archive/ES_0.5604436234499486 b/archive/ES_0.5604436234499486
new file mode 100644
index 0000000..7ca3706
--- /dev/null
+++ b/archive/ES_0.5604436234499486
@@ -0,0 +1,22 @@
+archive/ES_0.5604436234499486---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:14:22.131
+Launch V∞: [7.686606180102379, -5.848898908236648, 0.3225677790021946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005322426370027463, -0.001441320736404476, -0.0026002199227137834] km/s
+ V∞_out: [-0.002754330065727727, -0.0003062313761001442, 0.0011976092504386202] km/s
+ time of flight: 1.7901297026543286e8 seconds
+ arrival date: 2030-01-11T09:03:52.131
+ thrust profile: [0.5625815901780028 -0.03230221554217143 -0.16057463214700793; 0.136359955238718 0.06620782723555711 -0.13368722151370874; 0.05772682037000736 0.04837276870452309 -0.10412764213132185; 0.04091045429927127 0.04499576057477086 -0.10717254413891858; 0.030923980224643335 0.0434001420170797 -0.11176920346694151; 0.02580644872075558 0.041668255060330964 -0.11815894651797368; 0.011806694381375455 0.023125815227737784 -0.07152272105319325; 0.006544862232636263 0.014704453460796525 -0.050263816642793994; 0.002659575449025224 0.004671547005468727 -0.018718249016018988; 0.005464298937259038 0.013101941067147762 -0.0471886780495132; 0.00013467995405298943 0.0020376580856286373 -0.0035977103380043325; 0.0011057776793465838 0.0004449726174653105 -0.0033720955820519326; 0.0006053973924096072 -0.00165240244547643 -0.0020552957032214736; -0.0015617818642025768 0.0003795643723597616 0.0007253970775523968; 0.0004051874907735071 -0.0004519063312737612 -0.0015758863078927402; -0.0012692866792270159 -0.0018965815920790278 -0.0028655901974829947; -0.0003313723741231573 -0.0032708364199769387 -0.0014940103292999168; 0.0012465099441902395 -0.00456169235232995 -0.00537128345939617; 0.0032159808826815904 0.0017713250770305011 0.004869707797947216; 0.002033568830494316 0.00531285960758888 -0.0020411987182177927] %
+
+Mass Used: 109.03165998187978 kg
+Launch C3: 93.39758297881033 km²/s²
+||V∞_in||: 0.0030202369669134993 km/s
diff --git a/archive/ES_0.5604460667694166 b/archive/ES_0.5604460667694166
new file mode 100644
index 0000000..0876a1f
--- /dev/null
+++ b/archive/ES_0.5604460667694166
@@ -0,0 +1,22 @@
+archive/ES_0.5604460667694166---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T12:26:24.193
+Launch V∞: [7.515616335337876, -5.978135747521793, -0.16065166613312146] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.496271697123151e-6, -2.0026332687526122e-5, 0.00036432980018779085] km/s
+ V∞_out: [1.5948295683415758e-5, -0.00036591258212692926, 5.187322589292722e-6] km/s
+ time of flight: 1.7929448558699346e8 seconds
+ arrival date: 2030-01-14T16:27:49.193
+ thrust profile: [0.5621001722554453 -0.024131219282594502 -0.134085960927171; 0.20363790877046473 0.11810269617898823 -0.18060139699799785; 0.08367123816928788 0.08345579097353763 -0.14336853101165736; 0.03648269354976632 0.048242522717687204 -0.0939206871621318; 0.040483379105384965 0.0689386723091246 -0.14071443375489362; 0.01722049505207575 0.03548018046435248 -0.08144407290780535; 0.007473646553992051 0.01815880849556709 -0.045558688453822306; 0.007830334423429423 0.02189859152331127 -0.0572361522696736; 0.0025979518327562574 0.008089834546171393 -0.02196323413668658; 0.00221140951404768 0.006646789220322664 -0.021876225774251207; 0.0022609519111521704 0.009014867102860251 -0.026717481289855623; 0.0019767231769528197 0.0011283808499841126 -0.0003251050784044337; 4.047832636954363e-5 0.0006691536184686357 -0.000454868986074657; 0.0002225615945793457 0.00024538602204800627 1.2903263286285008e-5; 0.0012527479317595615 -0.0003082618155202721 -0.0008561665048979012; -0.00021612323786100555 0.000745090532900584 0.0006978816607586442; 0.00020801999907959053 0.00019246291464030822 0.00011997820213975683; 0.00024199857201992567 0.00044856478557125294 -0.0005303251076506402; 0.0008802673928997347 0.00030839433458781804 -0.0010157391043873118; 9.545354272144126e-5 -0.00010327503929354379 0.0015539240886710637] %
+
+Mass Used: 115.7380494681629 kg
+Launch C3: 92.24840487362681 km²/s²
+||V∞_in||: 0.0003648883235706138 km/s
diff --git a/archive/ES_0.560449361391246 b/archive/ES_0.560449361391246
new file mode 100644
index 0000000..7c25012
--- /dev/null
+++ b/archive/ES_0.560449361391246
@@ -0,0 +1,22 @@
+archive/ES_0.560449361391246---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T17:54:07.884
+Launch V∞: [7.883692927347965, -6.038200469054075, 0.06194856876371028] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4856868284200241e-5, -1.019827124567188e-5, -0.0006305099214339629] km/s
+ V∞_out: [0.0005972461421541554, 0.0001979395481335423, -8.334221934888827e-5] km/s
+ time of flight: 1.773626116755818e8 seconds
+ arrival date: 2029-12-26T13:17:38.884
+ thrust profile: [0.1830323523268635 -0.02035164656308752 -0.07245400180620885; 0.04449143848295977 0.01646644793037659 -0.05937704318096972; 0.05292876464156119 0.03228598701926376 -0.12302154275788833; 0.048156383691892485 0.03719427788432975 -0.1589785874047124; 0.035416566296087186 0.031472066077240214 -0.1530613311677869; 0.01935732052687998 0.019168048986524567 -0.1039522284792685; 0.011056741413825868 0.011522183557179913 -0.07072050399882286; 0.011241342858874678 0.011676088352862359 -0.07967941921385216; 0.005553978391128788 0.005990406389864586 -0.04319272094534689; 0.0010748244407475854 0.0010097525599348828 -0.008587766946311554; 0.0001158492244003644 0.0006202422413447145 -0.006917363115472707; 0.001499493268366196 4.690728096101639e-5 -0.005258145530456697; 0.0004621482801661996 0.0003291354921637424 -0.005871113443248054; 0.0001692324081825159 -0.00017401341519550416 0.0014113845558476204; 0.00017543261218570152 0.001895732482042554 -0.0020814450219176286; 0.0001415643001149246 -0.0005888150330412966 0.0009637904630461387; -0.00469187867033582 0.004311027802323915 0.0005565931213688533; -0.004009970622071292 0.009275503468451601 -0.0004761263286335756; 0.0007217263197840148 0.00034685871764534535 0.004658122534287337; 0.00893211973025692 0.0077150196320370755 0.0012548994280534454] %
+
+Mass Used: 78.59574085927761 kg
+Launch C3: 98.61631670237304 km²/s²
+||V∞_in||: 0.00063076738366713 km/s
diff --git a/archive/ES_0.5604661146796245 b/archive/ES_0.5604661146796245
new file mode 100644
index 0000000..7a02d80
--- /dev/null
+++ b/archive/ES_0.5604661146796245
@@ -0,0 +1,22 @@
+archive/ES_0.5604661146796245---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T21:15:40.794
+Launch V∞: [7.941837198301744, -5.663236337882532, 0.08481765664028622] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.004220813612007e-9, -8.923086054401729e-9, 3.829244203247697e-8] km/s
+ V∞_out: [1.3861325665833494e-8, -4.379103996491843e-8, 7.108409024207354e-9] km/s
+ time of flight: 1.8749577787199524e8 seconds
+ arrival date: 2030-04-22T23:25:17.794
+ thrust profile: [0.41008614956265643 -0.00836756191833312 -0.12649499451323537; 0.14565234898828922 0.08147861953693647 -0.15757397988790675; 0.045280181952888486 0.04403660992531146 -0.09390266521287065; 0.023206784803077293 0.02827376462017803 -0.07326332529245637; 0.019526215706376606 0.029066082179590877 -0.08410788413775495; 0.00750965942140561 0.013847321284027414 -0.044671652199892886; 0.009594690586972173 0.021604468206121465 -0.0708729397342461; 0.005254012511627462 0.008607220247515887 -0.04030527897409758; 0.007171216305179236 0.015656264588599422 -0.06365209981222437; 0.002436372479367694 0.004774812730261241 -0.021593093376192727; 0.002569680748801724 0.013799885391255954 -0.05285468554362184; -6.083038916596985e-7 0.0027866084597697174 -0.01244533136511244; 0.0029347747242884515 0.001332816248979419 -0.00496340695042255; -0.0023513203050136468 0.000568792059449468 -0.0020128080037060984; -0.0019161223728623418 -0.0003360285182344479 -0.0018018409445318172; -0.010028782366364621 -0.0006425373075504837 -0.0031021478876401025; -0.003531853531253489 0.0017186690921243827 -0.0020506952078808705; 3.1591889259228756e-5 -0.0035309730467927977 -0.0029921195014465524; -0.006980736595638285 0.0033324383433485415 -0.006924012943134488; -0.00016733109377894658 -0.010630412741570134 0.014272163298489179] %
+
+Mass Used: 98.82252915502613 kg
+Launch C3: 95.15221793792041 km²/s²
+||V∞_in||: 3.952172017851742e-8 km/s
diff --git a/archive/ES_0.5604754185754757 b/archive/ES_0.5604754185754757
new file mode 100644
index 0000000..6a24be5
--- /dev/null
+++ b/archive/ES_0.5604754185754757
@@ -0,0 +1,22 @@
+archive/ES_0.5604754185754757---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T16:42:27.963
+Launch V∞: [7.755647389003335, -5.938445172643009, 0.7997723949517398] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.772988186710378e-10, -1.1624543336922353e-9, -1.3452881424694309e-9] km/s
+ V∞_out: [6.806452794687537e-10, -5.872983923962558e-10, 2.1557298681822723e-10] km/s
+ time of flight: 1.874957778750119e8 seconds
+ arrival date: 2030-04-25T18:52:04.963
+ thrust profile: [0.4537366780228177 -0.015355461438615147 -0.11019133691638477; 0.04574602148386118 0.025004229569704894 -0.04916978290992069; 0.0502812575473861 0.04406653868643969 -0.09398959848088302; 0.07030848228443365 0.07228232163708352 -0.15860374110313116; 0.02275803777509816 0.038157047027354375 -0.09566935888745179; 0.014048332258797756 0.02738172444495737 -0.07937152584635483; 0.008314514776614558 0.01687754895358622 -0.05318849635021953; 0.012278372380163202 0.023910189766605406 -0.08090767761504968; 0.003461293500309875 0.007530212306411708 -0.02829453619888833; 0.002722118546589062 0.007480690108896227 -0.03018761112546484; -0.00017042193747687675 0.00047739242517713546 -0.0014579859331243224; 0.00010776768969497175 -0.00016934838762809753 -0.0011537254669377408; 6.543655296688668e-5 0.0002262312521387692 -0.0010291288574263901; 0.0003085271938195694 0.0004905124146200829 -0.0007408439257363301; -0.00019250621443768555 5.7564698641119315e-5 -0.0002992705476984863; -0.0003175405069196103 -0.00037919920287422413 -0.00012481995179643894; -0.00016462303000182635 4.1326209299825196e-5 4.0507163821095534e-5; 0.0028324580700289812 -0.000479462344488319 -0.0009551918207854241; 0.0036639015402480887 -0.001820093548678539 -0.005430097049951336; 0.0009815152479402491 -0.0019925097244416342 0.001300198681375057] %
+
+Mass Used: 93.56812698524072 kg
+Launch C3: 96.05483337476815 km²/s²
+||V∞_in||: 2.0288452984800286e-9 km/s
diff --git a/archive/ES_0.5604777694357372 b/archive/ES_0.5604777694357372
new file mode 100644
index 0000000..e374aa5
--- /dev/null
+++ b/archive/ES_0.5604777694357372
@@ -0,0 +1,22 @@
+archive/ES_0.5604777694357372---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T19:49:12.229
+Launch V∞: [7.839379851410603, -5.733228526501382, 0.36776974046034483] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6819000618533987e-9, -3.089593010556553e-9, -1.0966050963873661e-9] km/s
+ V∞_out: [-1.9840250095324576e-10, -4.687426052827086e-10, -1.2083555583972978e-11] km/s
+ time of flight: 1.838956489104109e8 seconds
+ arrival date: 2030-03-09T05:56:40.229
+ thrust profile: [0.4160602379796077 0.005288852122422231 -0.10457493617077923; 0.15523696243364962 0.09996332200060853 -0.1403683536519619; 0.08144710177379708 0.08561773729400632 -0.13743064741063468; 0.04215141483367418 0.061719056225820745 -0.11154786621623945; 0.03309474293242375 0.06115890045008714 -0.11996661352710938; 0.017968211696638012 0.0410560192520296 -0.08889662011099; 0.007931889808009629 0.020918102125826156 -0.05042748360105083; 0.0039012512195399835 0.012345706548267305 -0.03190856760510122; 0.0034435368755404237 0.009993130973222932 -0.029100558088228447; 0.003075756300397474 0.008490026742536657 -0.02799349381115982; 0.00044017653216605604 0.001052584759516065 -0.0035619611183650896; 0.0029112848226328933 0.004126118937846649 -0.001026667476817344; -0.0003531897899761883 -0.0009276719016680019 0.0004086956109365233; 0.002022841571368011 0.00024338429484237867 -0.0014563816359545543; 0.0027652580290887397 0.006923224911099055 0.0007230545034351788; 0.0013675345257191016 0.0024924816201398604 0.0012424803275985197; -0.0011889978667792658 0.005239210038744559 0.00363702558895325; -0.0009677933777877672 0.00241959006134895 0.005445626924604192; -7.433360878069035e-5 -0.002598538790144536 0.0031116532263337506; -1.0762364519199157e-5 0.0004436683551132393 0.00018592992370434786] %
+
+Mass Used: 102.8679954945851 kg
+Launch C3: 94.46104037379 km²/s²
+||V∞_in||: 3.684686625259347e-9 km/s
diff --git a/archive/ES_0.5604797137700692 b/archive/ES_0.5604797137700692
new file mode 100644
index 0000000..64236f9
--- /dev/null
+++ b/archive/ES_0.5604797137700692
@@ -0,0 +1,22 @@
+archive/ES_0.5604797137700692---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T03:08:25.731
+Launch V∞: [8.021663901436122, -5.606022575664781, 0.09831232180526593] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008436768219189388, -0.053384239856198626, -0.05258381463586014] km/s
+ V∞_out: [0.012620130291918908, -0.011526882145122373, 0.07361724293805506] km/s
+ time of flight: 1.849447004334103e8 seconds
+ arrival date: 2030-03-21T16:40:05.731
+ thrust profile: [0.40229722454488864 0.006151417593767349 -0.10400769698567813; 0.054878914342588334 0.03602796696734168 -0.057716083091169476; 0.06588727476387521 0.07084798046485666 -0.12006961772566999; 0.03424653161567215 0.05175277046493739 -0.09709003166471185; 0.0220975656344624 0.040519009335916484 -0.08632692952287178; 0.016683740119224615 0.0417054633870693 -0.09066306722361397; 0.011715622512329483 0.03487927894794743 -0.08883605746252318; 0.007334498392327768 0.024566551215054747 -0.062391473345088724; 0.005273700395205662 0.022768244809784753 -0.05779497306433188; 0.0052850877382973616 0.021380158767125092 -0.06142649533876608; 0.000996658434608962 0.0023156424575743193 -0.006431535749721171; 0.0006300444562223533 -0.00014966496606142366 -0.0006404340856017237; -0.00016255490679351054 -0.00030129882866225635 0.00036457085902323887; 0.00074374762982592 0.0010696025333174232 0.0008754255621701004; -0.0009089574116773306 0.00024354757832755662 -0.0003631506395160401; 0.0013950857845367278 0.002377097945978101 0.0019007800276865982; -0.003110648808623257 -0.0011840219508041311 0.00018434041641779246; -0.0003638206478631865 -0.004502634516550169 0.005183648491666951; 0.00015984926276213567 0.002854193470268328 -0.00024057759606436351; 0.0012348962122574292 0.001262530472696964 0.0010465197528640334] %
+
+Mass Used: 95.15156335374968 kg
+Launch C3: 95.78424617908532 km²/s²
+||V∞_in||: 0.07540632390368178 km/s
diff --git a/archive/ES_0.5604800896218233 b/archive/ES_0.5604800896218233
new file mode 100644
index 0000000..457237f
--- /dev/null
+++ b/archive/ES_0.5604800896218233
@@ -0,0 +1,22 @@
+archive/ES_0.5604800896218233---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:00:48.066
+Launch V∞: [8.032108621992899, -5.629193468545033, 0.1765200030261357] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0266474672491524e-9, 1.5723372220090614e-9, -2.1337769146786482e-9] km/s
+ V∞_out: [1.3825698813517432e-9, 2.7114389438338297e-9, 6.913873338797434e-11] km/s
+ time of flight: 1.848953686460739e8 seconds
+ arrival date: 2030-03-22T13:50:16.066
+ thrust profile: [0.37353213384209366 -0.013605227512889641 -0.12071945307778578; 0.05856977685565662 0.03125321879804887 -0.06725802743038424; 0.056901231316425896 0.048325539906199394 -0.11499138521393923; 0.03451800041219738 0.038521597283750354 -0.10420200711979238; 0.03333580333014237 0.044445545312349184 -0.13347946197590196; 0.014436139121692577 0.023428626937400266 -0.0758895918965025; 0.015480140991031285 0.027687392212320278 -0.096652643398706; 0.003493092700899298 0.008345215177896027 -0.030286941073872795; 0.0032689766670568475 0.008768292730919308 -0.033660921026236315; 0.0020408782232989426 0.004850595528515268 -0.024391213758049618; 0.002039218361610141 0.0051626161452372815 -0.02487506548843998; 0.0012308759628953784 0.004545380597300532 -0.020275323007080112; -0.001144057266555646 0.0047858968748421575 0.0018631760889205335; -0.0010924387531297567 3.1013880418311805e-5 0.0039772847924499245; -0.004961335967770724 -0.007064373551951742 0.0042749493882926265; 0.00019411577218715734 4.889718371651015e-5 -0.0018284104079958486; 0.0015776354274731606 -0.004853038399273323 0.0014758124302238244; 0.013492843363878225 -0.0037178324682018747 -0.0026584571777745116; 0.004836951639184593 0.0009471700498394855 0.005964981686875526; 0.0010137650972189844 -0.0029096417944673193 0.0001499998835558184] %
+
+Mass Used: 92.52991178137927 kg
+Launch C3: 96.23374733327107 km²/s²
+||V∞_in||: 2.8424027306734354e-9 km/s
diff --git a/archive/ES_0.5604813103810956 b/archive/ES_0.5604813103810956
new file mode 100644
index 0000000..f51dd6e
--- /dev/null
+++ b/archive/ES_0.5604813103810956
@@ -0,0 +1,22 @@
+archive/ES_0.5604813103810956---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:26:10.303
+Launch V∞: [7.86586145126251, -6.026566670034078, 0.093148818514249] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.060877906111634e-5, -0.00039823137783029475, 0.006815496225404231] km/s
+ V∞_out: [0.0007059947616333972, -0.00678998548283126, 8.287972268632665e-5] km/s
+ time of flight: 1.79034006544541e8 seconds
+ arrival date: 2030-01-15T03:06:16.303
+ thrust profile: [0.18583165597640502 -0.01519074269052968 -0.06708723787760915; 0.08551699823459524 0.036960413326273936 -0.10138087997898503; 0.04515032776300946 0.031619707521598255 -0.09605010501410084; 0.04586668208347554 0.040731373912582365 -0.13814819981212137; 0.04158860321359826 0.04321950144952022 -0.16204405101887331; 0.019600809886506438 0.023478374309474807 -0.09642157490219541; 0.011303641068443048 0.015279614196406627 -0.06816340716049059; 0.006600666629154375 0.007963023893977812 -0.04214379692805423; 0.008908097321475433 0.01341484951024588 -0.07096954786173466; 0.0006789291135548065 0.0024374618452696396 -0.012187618872986443; 0.0021669509350638223 0.0033643025299078064 -0.02175869805958046; 0.001453604774646337 -0.0006066375838362603 0.0004459822619551383; -0.003335470164158003 -0.000447373842860297 -0.00547543418803093; 1.5935100861304757e-7 -0.0015131985797301852 0.0014586450703113546; -0.00507603267716146 -0.002230783033669459 -0.0017813560791265922; 0.0003189486231810684 -0.0006314528117163742 0.0036204162146410293; -0.006115862639810536 0.004436509736468053 0.005541692700922474; -0.006070252059724919 -0.006660465047395849 -7.08809461609412e-5; -0.00029282559694241426 0.003203498902423018 -0.0010157964872795958; 7.862321126124931e-5 0.0024537233988695425 0.00013232824532727165] %
+
+Mass Used: 81.06176852086446 kg
+Launch C3: 98.19995890121379 km²/s²
+||V∞_in||: 0.0068273082746647664 km/s
diff --git a/archive/ES_0.5604836013510789 b/archive/ES_0.5604836013510789
new file mode 100644
index 0000000..362805d
--- /dev/null
+++ b/archive/ES_0.5604836013510789
@@ -0,0 +1,22 @@
+archive/ES_0.5604836013510789---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:43:31.020
+Launch V∞: [7.694783728191287, -5.717176288374444, 0.5819068798802134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.43342828294381e-8, -1.2799489570239335e-7, 2.3240652997518426e-8] km/s
+ V∞_out: [-2.0794519257904523e-8, 6.945965027801902e-8, 1.1042695701200986e-7] km/s
+ time of flight: 1.8749577787472397e8 seconds
+ arrival date: 2030-04-19T17:53:08.020
+ thrust profile: [0.5406314390090866 0.025298330072389862 -0.09590024194290303; 0.20871004310176328 0.1523634031129578 -0.15009246679935076; 0.06481381760141115 0.0791339183408428 -0.09474999431915161; 0.08081273902568609 0.1387233110119409 -0.1730871416069591; 0.02303964317850747 0.051426729298393856 -0.07528368751386454; 0.012770077657664244 0.03625668272532286 -0.057537671882789264; 0.018407972297705067 0.06619817025281399 -0.10653298608851722; 0.0013016869194058308 0.006412927615775936 -0.011935880115878069; 0.0008083920411999756 0.004777031818532067 -0.009316017827292624; 0.0006824488322949591 0.0003138775943246491 -0.0014900507679733565; -0.000138239190353156 0.0019227107564720515 -0.0032003322895003514; 7.728087780787594e-5 -0.0004383768768840698 -0.0012575193244231402; -0.0005987222763326814 0.00024443825792812274 0.0006624315854341576; -0.00010078988283900885 -0.0003344043906047741 0.0008703146262734609; -0.0008846500639587221 4.069522366257451e-5 0.0008763760928179932; -7.721102709261997e-5 -0.0005562196454510416 -5.9913879491962094e-5; -0.00024435050619683266 0.00021257863315109996 0.0008089514832868828; -0.0011356869127682164 0.0001389770854321145 -0.00037888702250623457; -0.00013169470230192852 0.00022168340958404845 0.0005857656537055908; -0.0004848755846178132 -0.0004420232110504442 -1.1120371048535581e-5] %
+
+Mass Used: 115.86343601802355 kg
+Launch C3: 92.2344169528403 km²/s²
+||V∞_in||: 1.3087510436233448e-7 km/s
diff --git a/archive/ES_0.5604966036883228 b/archive/ES_0.5604966036883228
new file mode 100644
index 0000000..de956e2
--- /dev/null
+++ b/archive/ES_0.5604966036883228
@@ -0,0 +1,22 @@
+archive/ES_0.5604966036883228---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:24:50.866
+Launch V∞: [7.7474800432725806, -5.843254336662468, 0.12882286925596115] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2486584014607495e-9, -3.6966462424804407e-9, -2.9318153233234013e-9] km/s
+ V∞_out: [-8.67623294970076e-10, 7.941213845938633e-10, 6.689664069993425e-10] km/s
+ time of flight: 1.8243338895899418e8 seconds
+ arrival date: 2030-02-20T18:21:18.866
+ thrust profile: [0.39076819355981335 0.0004603255854276681 -0.10511051045880493; 0.23391264942365003 0.13947350218084578 -0.20018451099410223; 0.07656360012329018 0.07644399886619117 -0.1307775182543322; 0.020438767173763674 0.028399709673315503 -0.05744263570105733; 0.02035209557392681 0.03745019596032939 -0.08218288808055058; 0.010728136514716402 0.021858300071105514 -0.051134294843876264; 0.0180054065331144 0.03975833762357811 -0.1020447801155409; 0.00448573003596708 0.013280496903781068 -0.03509869645207003; 0.003328991729161959 0.012037554892039587 -0.03299190124923841; 0.0027664784473215237 0.012788518336083889 -0.03569603071549883; 0.004504868346878199 0.022603833462043924 -0.06428068581030122; -0.000649632836154219 0.0003423639313337095 -0.0013749196625308091; 0.0019120552520856102 0.0006508901370667838 -0.0038726274734177052; 0.00030104229891868837 2.9009052991907174e-5 0.0011319146080048747; 0.0001318301124326051 0.000498466436174146 -0.00110840472822692; 0.0009529234355976482 -0.0008714877251472234 0.0007960554929342489; -0.0005141799077030881 0.00024052388957799295 -0.0009336117204072364; 0.0001579716745361468 -0.0004135966345565978 -0.0035201434894703678; -0.0004898075579535085 0.001704183241948332 0.0018563937207353065; -5.286452494592843e-5 0.0012066078173702884 -0.002048171536798181] %
+
+Mass Used: 104.50799999610581 kg
+Launch C3: 94.183663595475 km²/s²
+||V∞_in||: 4.880561682394474e-9 km/s
diff --git a/archive/ES_0.560503911357954 b/archive/ES_0.560503911357954
new file mode 100644
index 0000000..6a4258a
--- /dev/null
+++ b/archive/ES_0.560503911357954
@@ -0,0 +1,22 @@
+archive/ES_0.560503911357954---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T21:38:22.798
+Launch V∞: [7.779909238996482, -5.651771067154111, 0.11934867048392492] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00022052772082609154, -0.0001681163447680424, -0.00013792191714014635] km/s
+ V∞_out: [-2.767951428964847e-5, 0.0001923806127671547, -0.00024063104248480316] km/s
+ time of flight: 1.874957778734689e8 seconds
+ arrival date: 2030-04-20T23:47:59.798
+ thrust profile: [0.6139092894441169 0.01633113401499588 -0.15334643132699735; 0.10693868597951503 0.07143304162889585 -0.10097660017432637; 0.08287118744724284 0.09325643899413939 -0.14364880354937212; 0.03138179116671288 0.04643688104602213 -0.08346746810051985; 0.028858167053756236 0.0578350112750328 -0.11052531525910596; 0.013381174766893319 0.03133589978573221 -0.06735798270788827; 0.008023823554297737 0.02394600191074901 -0.05439635760307381; 0.004500394622004058 0.0165971310117559 -0.041570902972978524; 0.0026227194304466097 0.011717544918421712 -0.02989323198320195; 0.0036391554445180637 0.017556493989804918 -0.04530095706125475; 0.0007299968137081008 0.004098825989097279 -0.011118759319745933; 0.00014401939171412544 0.0011428474014832323 -0.0007780996825447516; -0.0012484523702630686 0.0009669845086488884 -0.0006816567174626103; 0.0017146846795897356 0.0018335339335997867 -0.0024646257188652137; 0.002013062098094048 -0.0019207469474727163 0.00012735751952735097; 0.000812757448020909 -0.00025428854403020975 -0.000597458125415107; -0.004445587506270686 0.002486936021242627 0.006178747474193027; -8.166042047491666e-5 -0.004236849993957347 -0.005146525784073739; 0.0026745089067611023 -0.007251985564001608 -0.0025216102066811467; 0.0036232247564682617 -0.0011108984381647522 0.010217573711699826] %
+
+Mass Used: 114.43269952275796 kg
+Launch C3: 92.48374806768942 km²/s²
+||V∞_in||: 0.00030970637103316305 km/s
diff --git a/archive/ES_0.5605103064071406 b/archive/ES_0.5605103064071406
new file mode 100644
index 0000000..dc97f23
--- /dev/null
+++ b/archive/ES_0.5605103064071406
@@ -0,0 +1,22 @@
+archive/ES_0.5605103064071406---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T17:02:42.266
+Launch V∞: [7.687961426348146, -6.151412456409376, -0.009086601392458465] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.399287372093932e-6, 4.1100002053789684e-5, -0.000761159198558424] km/s
+ V∞_out: [-3.18277023662244e-5, 0.0007614705732644763, -9.888469769108583e-6] km/s
+ time of flight: 1.7423875189642152e8 seconds
+ arrival date: 2029-11-19T08:41:53.266
+ thrust profile: [0.32037752614307374 -0.0371946916555408 -0.11779122381067607; 0.055634963077052374 0.022438373550020988 -0.06881357374692475; 0.05146054608820199 0.034525358611021406 -0.10980099759641941; 0.03969608917948535 0.03430498375368968 -0.1214256608021897; 0.030054431993681015 0.030653204761091794 -0.11999297009593413; 0.02394282586735389 0.02760908516212124 -0.11750897727485478; 0.02098310322528961 0.026503542348257695 -0.11963089501790657; 0.015203137892279206 0.02105709081068778 -0.10495753272005237; 0.0030446902813379075 0.004148323316325172 -0.022568261624111262; 0.0038804360393721745 0.006165115591249812 -0.03452789542014471; 0.0002454386080964754 0.0003791243477057921 -0.0025076834022246157; 0.0005914485782788608 0.0010881256912490987 -0.00724436886777883; 0.00015107551933816663 0.00039478563818136467 -0.0018355456671425253; -0.0003102257685173889 -0.0005174307194561869 -0.0009121822583492318; -0.0012731904275733934 0.0013936537365969223 -0.011041179293432426; -0.00011805123016987208 0.0011779700516317579 -0.00198498820206047; -0.0029960589599429144 0.002894376034689322 -0.005636770100470131; -0.0005267517128444957 0.00013481595347373108 -0.0010028271031811817; 0.0005144173615160409 0.001346792431914423 -0.00018937691154476827; 0.0024021548293243745 -0.0024516745510251587 -0.0020853465616255343] %
+
+Mass Used: 88.41789024377067 kg
+Launch C3: 96.9447086682103 km²/s²
+||V∞_in||: 0.0007622871427638343 km/s
diff --git a/archive/ES_0.5605108158233039 b/archive/ES_0.5605108158233039
new file mode 100644
index 0000000..ca4310d
--- /dev/null
+++ b/archive/ES_0.5605108158233039
@@ -0,0 +1,22 @@
+archive/ES_0.5605108158233039---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:15:27.952
+Launch V∞: [7.9654814471114666, -5.518492102428302, 0.46223986982590726] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3036965044764122e-9, 1.3940470778816707e-8, -3.979697157253006e-9] km/s
+ V∞_out: [5.379653653721303e-9, 1.0898476155302767e-8, 2.7984702414502204e-10] km/s
+ time of flight: 1.874957778759394e8 seconds
+ arrival date: 2030-04-21T11:25:04.952
+ thrust profile: [0.5933869278120549 -0.0030450745573757775 -0.17071835794009996; 0.04343168130410916 0.026198320751936587 -0.050191989926075216; 0.03758874722921305 0.036869632141761234 -0.07815325603895763; 0.03704866764842258 0.0477495932264504 -0.11182106150450864; 0.01704189500454068 0.027379400566396612 -0.07309414773074442; 0.02219722986972402 0.041702962495197476 -0.11696491948099881; 0.010815994765358924 0.024013909044662454 -0.07338357952493356; 0.005673791536354656 0.013397837680783222 -0.04379449966242699; 0.002709187411290651 0.004799237867782588 -0.019930834868697445; 0.0030839706642505323 0.011187739237038209 -0.04048032577075634; 0.0032430943994679884 0.008666440360015785 -0.035005687473132985; 0.001812209916467857 -0.0016991433768247812 -0.004918157663437242; 0.00012184291496519084 -0.0011070610130370078 -0.0007395870517055412; -0.00037589817077644415 0.006674776866997665 -0.004306335499148927; 0.0028829455242452757 0.0026320559302904123 0.00804677731431069; 0.0026686811253546832 0.002491882071952664 0.0012864940579184535; -0.009211929284749835 -0.003399673982308177 -0.013634788182672714; 0.010386755388390196 0.004337905533074389 -0.003144184503249515; 0.0002629733971575458 -0.00010470018968561194 -0.006820813065175365; -0.0020349092889506383 -0.0019494393238813031 -0.0011443783872092147] %
+
+Mass Used: 104.91744490828751 kg
+Launch C3: 94.11631546609719 km²/s²
+||V∞_in||: 1.4555903942190406e-8 km/s
diff --git a/archive/ES_0.5605113212597677 b/archive/ES_0.5605113212597677
new file mode 100644
index 0000000..e7abcad
--- /dev/null
+++ b/archive/ES_0.5605113212597677
@@ -0,0 +1,22 @@
+archive/ES_0.5605113212597677---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:53:19.332
+Launch V∞: [7.960189258994187, -5.519709321631737, 0.24656987948092762] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.596638291920855e-6, 6.285110503796999e-5, -0.001123566524474759] km/s
+ V∞_out: [-4.413334389206254e-5, 0.0011245238507433613, -1.4482430120208245e-5] km/s
+ time of flight: 1.874957778749143e8 seconds
+ arrival date: 2030-04-21T03:02:56.332
+ thrust profile: [0.5928878614234527 0.004906221729143483 -0.17274347370140866; 0.04182888442688013 0.025935602406449657 -0.046096021866478494; 0.058421198174751006 0.05958895019771961 -0.1158207759231991; 0.034800159816373424 0.047761842734742224 -0.10514256602948283; 0.01774010742008684 0.027623186792923828 -0.07116556215107585; 0.011542889577333224 0.022782463525937005 -0.05677703556835133; 0.012280724644339928 0.02844770109488923 -0.0848828142926247; 0.005260560311588177 0.01499349971153594 -0.04628203813877349; 0.009284603685276688 0.030905576110790686 -0.09164698851836663; 0.001427948970101729 0.005324858581656452 -0.018054548003631717; 3.171886212020424e-5 0.0028708604723693193 -0.009644535367628486; -0.0004730965096567516 0.003530716791002411 -0.007256152608647203; 0.0015769332730927905 0.003394216146659918 -0.012371874927030197; -0.0023353564006190763 -0.001125911564369468 -0.000302453969801616; 0.0011765316376647545 0.0004398411897915686 -0.002593657892730864; -0.0032184074404114985 -0.005234958776014191 -0.0022364359203095293; -0.0006167403356519037 0.00010544984933189006 0.004862911935590681; -0.0070418041361997785 -0.003627937829536421 -0.012705366366431851; -0.0032434996592838835 0.005131399728454812 0.001613397375638587; 0.0023342182927492032 0.00443762315413 0.007705518519064355] %
+
+Mass Used: 106.22303715433418 kg
+Launch C3: 93.89260073978195 km²/s²
+||V∞_in||: 0.0011253487038416676 km/s
diff --git a/archive/ES_0.5605134595415643 b/archive/ES_0.5605134595415643
new file mode 100644
index 0000000..78072c8
--- /dev/null
+++ b/archive/ES_0.5605134595415643
@@ -0,0 +1,22 @@
+archive/ES_0.5605134595415643---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T21:11:46.835
+Launch V∞: [7.630822922458928, -6.20225310732044, -0.47112407087355457] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.541793827087891e-7, 2.8906344516703563e-6, 8.089039040171862e-6] km/s
+ V∞_out: [7.690321275559442e-6, 9.401714296094812e-7, -3.7323150280310333e-6] km/s
+ time of flight: 1.751126128407362e8 seconds
+ arrival date: 2029-11-29T15:35:18.835
+ thrust profile: [0.2826405398141655 -0.01995371497805463 -0.09992937592199526; 0.0960178953315689 0.045393014318355185 -0.11041867337794062; 0.0701267022154886 0.05565631244795547 -0.1408727433160025; 0.05205577300765252 0.054607103798674894 -0.152327366013317; 0.033672595405932385 0.04280936440325236 -0.1332426829455717; 0.019729390662332907 0.029003292861183666 -0.10093822886354623; 0.010039659785612737 0.01628957315491127 -0.06274578945991684; 0.004748465635870057 0.008240407820660213 -0.0357057030971433; 0.010414963715948357 0.021294763237371797 -0.08663105820113626; 0.0022923621416929886 0.004475462935840413 -0.02176050351758433; 0.00044241869393675797 0.0010623968165037944 -0.00493516016756914; 7.506141970248679e-5 8.954716909817414e-5 6.710813278188463e-5; -0.00022251183557867062 9.951612681784945e-5 0.00048648720848014143; -2.7240182991787417e-5 -0.0002465368749729577 0.00109321015274528; -0.00020298442859775334 -0.001284168567161412 0.0003308504257153326; 5.697351316554606e-6 -0.002513891552365707 0.0005052535945068788; -4.398199791823892e-5 -0.001073951758114724 0.0006189066742754135; 2.1486524094612825e-5 0.0005381843042281969 -0.0002498622138907044; -8.113879979785755e-5 -2.0682293358396334e-5 0.0009081737079326973; 0.00019183228336018716 0.0005934946094447447 9.132594469164014e-5] %
+
+Mass Used: 88.5694362989666 kg
+Launch C3: 96.91935997134715 km²/s²
+||V∞_in||: 8.597311391460944e-6 km/s
diff --git a/archive/ES_0.5605139576423932 b/archive/ES_0.5605139576423932
new file mode 100644
index 0000000..81a6af4
--- /dev/null
+++ b/archive/ES_0.5605139576423932
@@ -0,0 +1,22 @@
+archive/ES_0.5605139576423932---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T18:16:48.736
+Launch V∞: [7.434238598358346, -5.933521765627251, 0.32522610065822943] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.21438616798795e-5, 8.705880350250296e-5, 0.00023771000796101187] km/s
+ V∞_out: [0.00023418504743583638, 2.7522886576570484e-5, -9.549932961836217e-5] km/s
+ time of flight: 1.7791101462638006e8 seconds
+ arrival date: 2029-12-27T22:00:22.736
+ thrust profile: [0.7504719725208537 -0.040959988155545995 -0.15509799737985513; 0.1185191714130535 0.0679961039417579 -0.10300058085330145; 0.1264374506334153 0.12250173205599602 -0.18766229033667772; 0.06662731543720393 0.08835459588522226 -0.15139498980584856; 0.04804751449256496 0.08042386328852101 -0.14890566327178625; 0.018075750289813855 0.035886408474172224 -0.07456631297148755; 0.013603804004789034 0.03240409118552923 -0.07113169491021608; 0.0028299772216219526 0.007852807993993145 -0.018732950225302913; 0.000674414139204634 0.0021682519400228286 -0.0054687146482979305; 0.0006945373563929057 0.0025920919536835847 -0.006790687638876995; 0.0004280404311632695 0.0017327790941959686 -0.004571926177987283; 8.845922417174818e-5 0.0006457546304282601 -0.0015085396926954315; -6.721970042502124e-5 0.00044831034406358453 -0.001138951077275381; 0.000989557326982761 0.000420097644898213 -0.0006913040585871419; 0.0002566333864609722 -0.0002749875296690779 -0.0011938250306982553; 0.0005318056111716727 -6.719438268357268e-5 -0.0011189304372628303; -3.366775003612991e-5 0.0007284202866357904 -0.0017591850600389108; 8.538360184565119e-5 -0.00010361173948359459 -0.0005325340568649297; 0.0004636653513718765 0.0003428922462141754 0.00015379844652323548; 7.976485708870439e-5 -0.0005145049735409311 0.00010768004417480886] %
+
+Mass Used: 125.54754001670926 kg
+Launch C3: 90.58035609704275 km²/s²
+||V∞_in||: 0.0002551832890214541 km/s
diff --git a/archive/ES_0.560525852490877 b/archive/ES_0.560525852490877
new file mode 100644
index 0000000..5744c5e
--- /dev/null
+++ b/archive/ES_0.560525852490877
@@ -0,0 +1,22 @@
+archive/ES_0.560525852490877---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T08:09:42.648
+Launch V∞: [7.914347179318701, -6.019872097810366, -0.03999692365348044] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.092884330266422e-6, -3.638962837026846e-6, -1.0275666551097795e-5] km/s
+ V∞_out: [-9.966552360640912e-6, -1.0248116654586006e-6, 4.4580437320214775e-6] km/s
+ time of flight: 1.874957777798284e8 seconds
+ arrival date: 2030-04-27T10:19:19.648
+ thrust profile: [0.2230507609050875 0.0004292056256291622 -0.07568953440590867; 0.0416233620151584 0.022711983076455635 -0.051216469703687525; 0.04978001118478353 0.04395121330475413 -0.11045737143279427; 0.03223807166592525 0.03687122512896524 -0.10638486898220866; 0.03300739227317162 0.04790590795615277 -0.13976187707662327; 0.011096130326921064 0.01597673974139551 -0.06051968255797275; 0.011675626775582704 0.022011437971001933 -0.08481877927259673; 0.008050329417921939 0.01964334406747146 -0.08109538888950071; 0.0033687012223005135 0.0076246514176061585 -0.03045221084044534; 0.0009445361071728339 0.0030399125053542373 -0.012041997691621027; 0.001930306810481272 0.004654395224346136 -0.024611935594622075; -9.038834874895573e-6 0.00023982780278542876 -0.0006376709664880693; -0.0019282566168357153 -0.0008544872438367508 -0.0006969533291311136; -0.00204638251794161 -0.0009876722326605848 -0.0015300774594088412; 0.0004478780843060866 -7.889597502095617e-6 -0.0006831162105905538; 0.0001787903223300494 -0.0003785984272296096 0.0022044606658822704; -0.004134556796206276 -0.003908075684170739 0.001298992457965057; 0.0005580853024708231 -0.0022467557212176767 0.000542510531275689; 0.001344680652537415 -0.0024508279562628515 -0.00341737020354285; 0.002745266773451587 0.0025862357555927256 0.0024941847510948642] %
+
+Mass Used: 77.16227980701342 kg
+Launch C3: 98.8773511026874 km²/s²
+||V∞_in||: 1.0955627310106639e-5 km/s
diff --git a/archive/ES_0.5605398123924059 b/archive/ES_0.5605398123924059
new file mode 100644
index 0000000..81f247e
--- /dev/null
+++ b/archive/ES_0.5605398123924059
@@ -0,0 +1,22 @@
+archive/ES_0.5605398123924059---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T02:35:57.590
+Launch V∞: [8.106796656982329, -5.4431809499173225, 0.1246460907827672] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.42241261355907e-8, 1.340631893783489e-7, 1.3124870954334356e-8] km/s
+ V∞_out: [-1.18372390945845e-8, 5.567050053149551e-8, 1.4685119697713214e-7] km/s
+ time of flight: 1.874957778742571e8 seconds
+ arrival date: 2030-04-19T04:45:34.590
+ thrust profile: [0.39254578456563705 0.004013162957435715 -0.10779583031259748; 0.0968354885820319 0.06151982467062676 -0.09584338340598986; 0.14760482711150563 0.15755498983476296 -0.2588999588137617; 0.0391050272185553 0.055886001522326194 -0.108192122851439; 0.021862870074163876 0.03918318351828549 -0.08391981538115173; 0.011641126163430325 0.024881754480944634 -0.058223744880120144; 0.005944900031541212 0.014960814997380003 -0.03812762528912587; 0.005267112692456217 0.015786207741323045 -0.04185942141679803; 0.001468404596471547 0.0018959873054923309 -0.006708635471338643; 0.0004744684810444558 0.0018130611725044482 -0.007480437040600608; 0.0002944050960212141 0.002463413589110109 -0.006784396593699946; 0.0002330234175182454 0.001150750755282379 -0.0031866969330164013; 0.0015423361692916593 0.0012090200523365026 -0.0024200438706724445; -0.0004203810582970184 0.0005561886023993778 -0.0013441526658257103; -0.0018642733133999478 0.001281924256822401 0.0001381204954491082; 0.0014364109239796443 0.0013332129694757593 0.0011553029045365923; 0.0006269363417225537 -0.0001650005016144679 -0.0008550368088605157; -0.000229441823870973 0.0006681879709973051 -0.0004714698834603036; 0.0022098904442953474 0.001235861781124479 0.0006473008151698655; 0.0014179685738559046 0.00016899529055666658 -0.0005611529640944682] %
+
+Mass Used: 97.67365381276431 kg
+Launch C3: 95.36390753915015 km²/s²
+||V∞_in||: 1.588675687708692e-7 km/s
diff --git a/archive/ES_0.5605466906430266 b/archive/ES_0.5605466906430266
new file mode 100644
index 0000000..0aef0cf
--- /dev/null
+++ b/archive/ES_0.5605466906430266
@@ -0,0 +1,22 @@
+archive/ES_0.5605466906430266---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T17:53:40.378
+Launch V∞: [7.779425808264831, -5.648714469114391, 0.10556342907673492] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7075365544482405e-7, 1.7535988844970525e-6, -2.7146455267681116e-5] km/s
+ V∞_out: [-1.0076378897385287e-6, 2.7158583449498858e-5, -2.6913755063895374e-7] km/s
+ time of flight: 1.874957778725044e8 seconds
+ arrival date: 2030-04-19T20:03:17.378
+ thrust profile: [0.5514014383682518 0.021875956426971762 -0.12582954825244805; 0.1630778035520793 0.11424727241900542 -0.13856168661314125; 0.08934262578046565 0.10513293447383362 -0.14115898014712458; 0.04890590468066156 0.07990382456997852 -0.12088800908206605; 0.03401630625935578 0.07212495412656855 -0.11890117488834691; 0.019859282148507927 0.05324668736460771 -0.09529178307139326; 0.0032408555117868234 0.010320716449345756 -0.021845970772218178; 0.0028348646723201356 0.010119616286293978 -0.020418245578643992; 0.002177253731648617 0.01224728699487096 -0.02709308605503622; 0.0004552401780050724 0.006043600631971371 -0.014293448134924107; -0.0006130771303735716 0.0014999501008424272 -0.002955451045730943; 0.001024515937276606 0.0013144664181838663 -0.003100222179030508; -0.00015379829193096545 0.0012679112804950062 -9.558846072641684e-5; 0.0007407116104364462 0.0016177931826319132 0.0002963947625608996; -0.002621579994480367 0.0010045652623390214 -0.0014240208386886977; 0.00422146258807389 -0.0019349417453388821 0.0023523144155437586; 0.0006838156552705844 -0.0002419800663030796 -0.00023492343138010368; 0.00018105685339233648 -0.000640221884852191 -0.004748438072535154; 0.0008877695551654936 0.0014743777088313012 0.002358680095242145; -0.004412687863162709 -0.0001457142988513652 -0.00031674572514974614] %
+
+Mass Used: 114.74606168181163 kg
+Launch C3: 92.43858469743762 km²/s²
+||V∞_in||: 2.7203571446756194e-5 km/s
diff --git a/archive/ES_0.5605472272782301 b/archive/ES_0.5605472272782301
new file mode 100644
index 0000000..9146371
--- /dev/null
+++ b/archive/ES_0.5605472272782301
@@ -0,0 +1,22 @@
+archive/ES_0.5605472272782301---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T07:35:22.261
+Launch V∞: [7.892926426677194, -5.680227447296816, 0.12006163243606052] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6954168992149495e-9, -1.6720733270774625e-9, -1.943894190854001e-9] km/s
+ V∞_out: [1.1410256689162797e-11, -3.535262733873365e-11, 6.092222950458916e-12] km/s
+ time of flight: 1.859758693100561e8 seconds
+ arrival date: 2030-04-02T19:33:11.261
+ thrust profile: [0.4343258857613348 0.01289125781793145 -0.10007648991848643; 0.12340184279912034 0.08795208245524054 -0.10797740818028384; 0.047878439902197964 0.059480392338645015 -0.08636379001824729; 0.037522391707089764 0.06357768206139447 -0.09782725040420531; 0.015096539092754793 0.03632562743617328 -0.06190935397280046; 0.027177531319125942 0.0771619834096038 -0.1324194522827905; 0.0074216568823389575 0.02744154659806753 -0.05250783986869373; 0.006525547408933895 0.030726805705565897 -0.061278205944576294; 0.00400311754529153 0.02136872840315104 -0.04667923074456893; 0.0016656793938261817 0.011363055904259222 -0.02796840902223478; 0.0012084862587956487 0.014642812084872317 -0.04129999299550627; 0.0005142276979811721 0.006090568267924427 -0.016352848725427194; -0.00012508289161780432 -0.00036840726162654195 -0.0002036426716727127; 5.010806593898827e-5 2.350226848404338e-5 0.0011283291993822498; -0.0028489288974432136 0.0012750610961193187 0.000149039025779185; 0.0001979861332168749 0.00010472695493748816 0.00048329599670917723; 0.0002529669750614495 -0.0015023976260849698 -0.00032857844813086157; 0.0004460439793345531 -0.0002852498533702395 0.0014947132757420073; -0.0014004877962048874 -0.0006969783590175587 -0.0006625001835830904; -0.00025871449021075714 -0.00018452542941653982 -0.0004381667394975433] %
+
+Mass Used: 102.26859550891368 kg
+Launch C3: 94.57768622554653 km²/s²
+||V∞_in||: 3.0739213227575395e-9 km/s
diff --git a/archive/ES_0.5605512737671 b/archive/ES_0.5605512737671
new file mode 100644
index 0000000..aedeec7
--- /dev/null
+++ b/archive/ES_0.5605512737671
@@ -0,0 +1,22 @@
+archive/ES_0.5605512737671---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:04:39.941
+Launch V∞: [8.10848147960195, -5.6223907393441745, 0.3016859374601588] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.570054488298924e-9, -1.87112657957448e-9, -1.4323193603604362e-9] km/s
+ V∞_out: [5.3846458723174145e-11, 1.1110002449831549e-10, 3.448720751600767e-12] km/s
+ time of flight: 1.874957778746973e8 seconds
+ arrival date: 2030-04-23T09:14:16.941
+ thrust profile: [0.28525403256943616 -0.0017398496364819667 -0.08894655819400202; 0.04096887765342367 0.023140403194381366 -0.04880168246868594; 0.04894999927397314 0.044436861540198797 -0.10306568942860779; 0.04258782224941888 0.050683909568876695 -0.1313026760350788; 0.027950212599970787 0.040211507841122235 -0.11744813266819637; 0.012234017627986026 0.020305832565101017 -0.06510403593348249; 0.005923098342632106 0.010768627508074101 -0.035829867345974244; 0.007928421721222696 0.01448364607386947 -0.05682346522597859; 0.0014120811914589992 0.0031880891082687723 -0.014580358670418195; 0.011219476832807074 0.02777830866544456 -0.11271617040168265; 0.005052970015963835 0.006688598673109452 -0.01576587969095995; 0.00018149374973683896 0.0013026520049094874 -0.0050741790244163; -0.0018616594985696633 -0.0022263948916976086 0.003962368163547152; -0.004783949212169683 0.0009807642971753 -0.00015270232640373325; 0.0013974412481287427 0.003513023371461023 -0.0033868309486382465; -0.005333940141208555 0.006417103514606974 -0.000950166633834286; -0.0020490233866964722 -0.015496678513362604 0.0030661773412357244; -0.0036093751055073036 -0.008490276078514398 0.010591470348906763; 0.0006726050964454059 0.000135569240673527 0.004740659391834923; 0.001565743579837564 -0.0008835770401257188 -0.002444207661133787] %
+
+Mass Used: 85.51952976961229 kg
+Launch C3: 97.44976393577218 km²/s²
+||V∞_in||: 2.8315586737839317e-9 km/s
diff --git a/archive/ES_0.5605545447934291 b/archive/ES_0.5605545447934291
new file mode 100644
index 0000000..e36a34f
--- /dev/null
+++ b/archive/ES_0.5605545447934291
@@ -0,0 +1,22 @@
+archive/ES_0.5605545447934291---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T01:55:47.733
+Launch V∞: [7.667988496954263, -5.845509016894701, 0.12113132416473962] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.885120590595384e-7, 4.427307559774436e-6, -9.201271886376565e-5] km/s
+ V∞_out: [-3.2703663644585557e-6, 9.198636755155051e-5, -8.615562474548311e-7] km/s
+ time of flight: 1.781356949816778e8 seconds
+ arrival date: 2029-12-31T20:04:01.733
+ thrust profile: [0.6254460157638881 -0.03741209038402995 -0.17854322362588176; 0.11824364242905043 0.06208954318457052 -0.12789535815317488; 0.041721910252055336 0.03574736492614221 -0.08135042623244662; 0.03589045736057186 0.04188822548735886 -0.10344691252124126; 0.031224311062623855 0.04044222873867942 -0.11180671983656616; 0.014530442209380144 0.025559603269409408 -0.07629903227807285; 0.012401231316568333 0.0219446815435703 -0.06760608527775412; 0.00958079072632338 0.020447948776017726 -0.06351100782065394; 0.01462508288963389 0.034452558043809915 -0.11382077771235728; 0.00025404176378972563 0.004376658117167984 -0.023983688647861122; 0.0003929111388141185 0.0008773759013922309 -0.006311087668411459; 0.001091228605059464 0.0027444610928404663 -0.015987153239202863; 0.0005475372471031847 0.0003899751060430361 0.00043561108200779143; 0.0010970140506603668 -0.0004036588207149309 -0.0001715652155575868; 0.00041642433306773375 -0.0005688737270794618 -0.0005397015876987584; 0.000727267927678084 -0.00019661448523122603 0.0009592523599380258; -0.0009743589691712159 -0.0003053404043213069 0.0005547027471789718; -0.00013279226613244923 -0.000992163666619164 0.0026414573739105534; 0.00024025614723250456 0.00011535324576554095 -0.00033374065869609887; -0.0007112144915584096 -0.0004038920584570121 0.001438458097233761] %
+
+Mass Used: 111.58124194566881 kg
+Launch C3: 92.98269605371404 km²/s²
+||V∞_in||: 9.212104988207022e-5 km/s
diff --git a/archive/ES_0.5605551386966175 b/archive/ES_0.5605551386966175
new file mode 100644
index 0000000..d0fecc4
--- /dev/null
+++ b/archive/ES_0.5605551386966175
@@ -0,0 +1,22 @@
+archive/ES_0.5605551386966175---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T22:46:23.596
+Launch V∞: [7.731846053312578, -5.548124650746553, 0.1948544631472007] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5158071212684684e-9, 1.2996704482438287e-10, -4.1423405155300283e-10] km/s
+ V∞_out: [1.2110294961702207e-9, -1.2063536366071532e-9, -7.038432806030836e-10] km/s
+ time of flight: 1.874957778727539e8 seconds
+ arrival date: 2030-04-20T00:56:00.596
+ thrust profile: [0.8055942412003732 0.002623353299615579 -0.21549011571427495; 0.12104175330697305 0.0772807914730329 -0.12118241868743695; 0.07596674684824105 0.08063556906349756 -0.14068025789514288; 0.023479875853465816 0.033380581068586726 -0.06858681575144912; 0.011673713168750604 0.020832408973987155 -0.04767931833769099; 0.016659280511858297 0.03725233259869584 -0.08921531886925471; 0.01144968501278348 0.031589311479001486 -0.08023083646131873; 0.004593861685720196 0.013692887317603744 -0.03875849223871649; 0.0011983278910728608 0.004119649754413704 -0.011573317215651689; 0.0006734903422007884 0.004198471634134449 -0.013143022437058288; 0.0034659329111219024 0.01845453936399833 -0.05603760331476128; 0.001158614693666763 -0.001513566311937284 -0.0013890523166964325; -0.0006513943411064015 0.0009185328527096274 -0.0034110058740469155; 0.0005291245155752175 0.0008070051684486406 -0.0024782862760015247; 0.0004962498896774528 0.0011940831345011711 -0.002443801913883885; -0.004061042036328972 0.0012867967061994177 0.001995996693615382; 0.004776297730968944 0.001584717579185197 0.00048298376992737357; -0.00023607725431822816 0.0005507576502192063 -0.0011581785533542278; -0.000692160432936839 -0.004035391654933834 0.0007257270258030849; 0.0073272716021985495 0.00334010135431859 -0.0020262238871486806] %
+
+Mass Used: 125.47458551348154 kg
+Launch C3: 90.60109879415525 km²/s²
+||V∞_in||: 1.5767537889900885e-9 km/s
diff --git a/archive/ES_0.560555371216558 b/archive/ES_0.560555371216558
new file mode 100644
index 0000000..5726297
--- /dev/null
+++ b/archive/ES_0.560555371216558
@@ -0,0 +1,22 @@
+archive/ES_0.560555371216558---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T11:01:01.772
+Launch V∞: [7.876073300792127, -5.895917327179075, 0.18572496413833905] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4703950429902945e-6, -1.1329546921445017e-5, 0.0002412650171541302] km/s
+ V∞_out: [6.985406876698545e-6, -0.00024135293997750188, 2.0679290918457928e-6] km/s
+ time of flight: 1.8058317023117346e8 seconds
+ arrival date: 2030-02-01T13:00:31.772
+ thrust profile: [0.318254942388526 -0.024380380039505562 -0.11339162435360815; 0.06690331747191823 0.027629828074023467 -0.07829809261905049; 0.05742581092976307 0.04106628688890943 -0.12117727702527552; 0.03299651509567735 0.02912961257389185 -0.09863140688216916; 0.03199972941293014 0.03442986042486597 -0.13186242491458297; 0.024226963858975832 0.026847860354277966 -0.11465111903248858; 0.020696659568103622 0.024644865403392623 -0.11310585750430131; 0.009298834364961175 0.01317214181194572 -0.06169104955532103; 0.003367260449450212 0.0057532618074814905 -0.027497155378426015; -0.0008191082081321011 -0.0015413597716630034 -0.0029335253850045714; 8.957017520836545e-5 -0.00187368965234177 -0.0033220404464039126; 0.00247483094593852 0.002171515649515344 -0.004110326159445076; -0.0020067766326440383 0.0009244155410753164 -0.00027851105396733576; 0.0022686076118480472 -0.0005411401888600386 -0.005104953654909627; -0.0006344479954893221 0.0012584701507358056 -0.0023614335779776996; -0.009294508611592367 -0.006705574115557843 0.0010258624899281764; -0.008087449739518974 -0.00258821915644617 0.0061161072951166915; 0.0001925258609482184 0.0020121637395355057 -0.00635553277131594; -0.0013258487406043254 -0.013029343585556491 -0.008962809232254544; 0.0055346125057583115 -0.005049763774691699 -0.004392240520426374] %
+
+Mass Used: 89.1462174903204 kg
+Launch C3: 96.82886553068523 km²/s²
+||V∞_in||: 0.00024153535806877306 km/s
diff --git a/archive/ES_0.5605558174924449 b/archive/ES_0.5605558174924449
new file mode 100644
index 0000000..c0a001d
--- /dev/null
+++ b/archive/ES_0.5605558174924449
@@ -0,0 +1,22 @@
+archive/ES_0.5605558174924449---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:12:50.851
+Launch V∞: [7.894576058397994, -5.607629171661403, 0.17244424444346496] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003223586277638431, 0.018061908215392285, 0.016922690684439246] km/s
+ V∞_out: [-0.004211786970466736, 0.003745415993653439, -0.024079782483893027] km/s
+ time of flight: 1.8501444160938874e8 seconds
+ arrival date: 2030-03-21T20:06:51.851
+ thrust profile: [0.5156710389451795 0.000637378768089417 -0.13882964070812942; 0.13711778395218563 0.08479350565471534 -0.13453953465681873; 0.05303522334809231 0.05597737725159066 -0.0973731935663952; 0.04211314967233336 0.06024112283147212 -0.11039492416619878; 0.04555109075880431 0.08058844328202129 -0.170594827275901; 0.011705428958664735 0.02500335968996189 -0.06075612126031062; 0.011040015510733029 0.02533035275398526 -0.06684373353582072; 0.002919489110719593 0.009318757653609592 -0.02666386271512514; 0.0016772431035065151 0.006239292686897031 -0.013649709273984392; 0.001364826567744411 0.0038779914191935027 -0.01708035952471396; 0.0005911556836503357 0.0025684836361990334 -0.0104340750835017; 0.0015773043522911516 0.0026249937584722416 -0.00782232739989169; -0.0015407946005748508 1.847462094273797e-5 -0.0022819142210206453; -0.0010015726564704436 0.0007449711916516972 0.0009409686595681322; 0.0030314824110191626 -9.185014547930128e-5 -0.0006057956830282777; 0.00019227256989423836 0.001367442008040056 -0.0033110568822101506; -0.003326562581218436 0.006071457774375677 -0.0026161018745691107; -4.039414953917689e-5 0.001786855202829756 0.003105133276734647; -0.00048734685237448875 0.0006952614202329537 -0.0014984289635799615; -0.0033040754056467116 -0.006593073485272811 0.00945621093774281] %
+
+Mass Used: 106.81761073869984 kg
+Launch C3: 93.79957308614043 km²/s²
+||V∞_in||: 0.024959997934131343 km/s
diff --git a/archive/ES_0.5605662063953228 b/archive/ES_0.5605662063953228
new file mode 100644
index 0000000..cb2cf1c
--- /dev/null
+++ b/archive/ES_0.5605662063953228
@@ -0,0 +1,22 @@
+archive/ES_0.5605662063953228---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T19:03:21.764
+Launch V∞: [7.8571762300439785, -5.937479374439788, 0.19565387604291243] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.461864873001606e-5, 2.4061751490111817e-5, 0.0017246943423384988] km/s
+ V∞_out: [-0.0015556001957462138, -0.0004985622731922913, 0.0005515129191246438] km/s
+ time of flight: 1.8469108991613457e8 seconds
+ arrival date: 2030-03-23T10:08:10.764
+ thrust profile: [0.33150278627434976 -0.00792679402406436 -0.11051868364040121; 0.032968955938627476 0.016431563751683535 -0.03701109983066754; 0.072130136517514 0.0581221063637242 -0.14436388402381198; 0.032927831950169094 0.035038000511364215 -0.0997424376833938; 0.020811329336170394 0.026203365501176273 -0.08353423389302074; 0.0212381858239223 0.031019094071849225 -0.1070672551014627; 0.014208629347036794 0.02338512401605343 -0.08444669861477974; 0.00779680379859416 0.014011980625894633 -0.05481003860148421; 0.006940101192276925 0.00805398487772255 -0.03604565794542195; 0.0038944430495050047 0.008263830936122598 -0.036104778371584274; 0.0031549933009670825 0.0013366098223483876 -0.007774688353683695; -0.0017972298940241984 0.0030595938341690023 -0.006125574021821901; 0.0037641583309392284 -0.0036530061800900786 -0.01015298166605797; 0.0003751191551465481 0.0042914883984256184 -0.012420824821811227; -0.0026072560465836385 -0.000635791015323987 -0.002611445398938428; 0.0035095401439399617 -0.00010636845016023788 -0.005379226388122331; 0.0008371449595735339 0.001765098266204546 -0.008521341305371114; 0.0013733441422579388 0.009736379802538535 0.0011060024397244687; 0.0017740150620453351 0.011471337111302294 -0.00916002726965102; 0.00036540637870791754 -0.0010079710416410442 -0.004588031755023099] %
+
+Mass Used: 88.00214037992964 kg
+Launch C3: 97.02716007107662 km²/s²
+||V∞_in||: 0.001725209550523962 km/s
diff --git a/archive/ES_0.5605777034585179 b/archive/ES_0.5605777034585179
new file mode 100644
index 0000000..ae18a73
--- /dev/null
+++ b/archive/ES_0.5605777034585179
@@ -0,0 +1,22 @@
+archive/ES_0.5605777034585179---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:50:41.968
+Launch V∞: [7.945120792823161, -5.755999927951525, 0.018495863218769133] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1584304043243901e-7, 4.0757744517630196e-7, 1.1038278205684186e-6] km/s
+ V∞_out: [1.0532161923067113e-6, 1.2416469206514334e-7, -5.110573896861227e-7] km/s
+ time of flight: 1.8444282418879202e8 seconds
+ arrival date: 2030-03-18T02:57:45.968
+ thrust profile: [0.36322749643839 -0.006668897066301312 -0.1131121327910936; 0.06320101184288371 0.036282047832610916 -0.06993973585800331; 0.029205599510396724 0.025330084764315426 -0.05837402528562854; 0.043009105315597665 0.0529133326049812 -0.12366458325677752; 0.023002287307707345 0.034853888363493686 -0.09339512101870256; 0.014182315929716404 0.02491592595899837 -0.07220678458827347; 0.023348436851553706 0.04481907855216551 -0.1345020933250744; 0.00670668038723999 0.013999845613246464 -0.04788382886064736; 0.0078020618362738105 0.022966826549823682 -0.07459319665998358; 0.004590539622636824 0.00886433063991608 -0.039193537147393966; -2.391699168491628e-5 0.00228792866812439 -0.0034328671662771887; 0.0013657368405044531 -0.0030876959520878 -0.004057263880708886; 0.0032365862425754806 0.00461746462123141 -0.006000650115042824; -0.004716288031778491 6.945758662449657e-5 -0.001734141168085207; 0.002963777900227983 -0.001556700573841453 0.004059590163714624; -0.002670496356225889 0.001110509977286095 -0.0020753793300098584; -0.00558506830476937 0.00772918319421524 -0.0037332250480712906; -0.011636804694904634 0.008065708306463604 -0.0047226051366362305; 0.01152459170249396 0.007905767129922303 0.00117648591511774; 7.748563994313643e-5 -8.256038222878353e-5 -0.0032909216215328725] %
+
+Mass Used: 92.50919423444111 kg
+Launch C3: 96.2568216800851 km²/s²
+||V∞_in||: 1.182359861164907e-6 km/s
diff --git a/archive/ES_0.560587462080823 b/archive/ES_0.560587462080823
new file mode 100644
index 0000000..d375a24
--- /dev/null
+++ b/archive/ES_0.560587462080823
@@ -0,0 +1,22 @@
+archive/ES_0.560587462080823---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:01:25.027
+Launch V∞: [8.003751874906147, -5.607664325744749, 0.11356495548789142] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1015544401492596e-10, -1.866387726409428e-8, -1.2521994525885533e-8] km/s
+ V∞_out: [-3.9339813796521325e-9, 9.867072618539632e-9, 2.877730364975335e-9] km/s
+ time of flight: 1.874957778734459e8 seconds
+ arrival date: 2030-04-21T12:11:02.027
+ thrust profile: [0.3799411618174131 0.011730334887114627 -0.0995046726440378; 0.08714136377820914 0.05673635326706746 -0.08737974128125528; 0.056853917083944876 0.06272407047914155 -0.10507444522635374; 0.0704339438068374 0.10374268544422796 -0.18865001307586268; 0.015246854228616965 0.030148555710414145 -0.06244945385336699; 0.009805522854999688 0.019334975633016324 -0.04575961947376304; 0.007727264307893347 0.02637273063444681 -0.06474644507486683; 0.003821161597157341 0.014784766025120813 -0.03875735245072567; 0.001431207971365462 0.010909195940836324 -0.03140614115994522; 0.002322638924318695 0.01431455061726185 -0.04041971472978759; 0.0005665815521451429 0.0031275924130025994 -0.010942548619886168; -0.0007285081066898433 0.006412385933144317 -0.03289594021831353; 0.00016775925616930259 0.0021958336729882132 0.0008238634335097908; 0.0022707041290405384 -0.001273635257306068 6.872307466414956e-5; 0.004101195774385083 0.0009288659566181929 -0.002305612052162824; -0.0007900176114388579 0.00594150067325995 -0.0036121526593048603; 0.0003754812244423575 0.0006067976196959202 -0.005051875881747283; -0.0004034238751309681 -0.003736443335595716 -0.0030481603149666373; 0.00014943465610110757 0.008620525287496184 -0.00958368519060546; -0.0017194665611052974 0.011923320889522082 -0.0026765580362997344] %
+
+Mass Used: 96.82547088524143 kg
+Launch C3: 95.51884026440894 km²/s²
+||V∞_in||: 2.2476317019167794e-8 km/s
diff --git a/archive/ES_0.5605953518578017 b/archive/ES_0.5605953518578017
new file mode 100644
index 0000000..b76d11f
--- /dev/null
+++ b/archive/ES_0.5605953518578017
@@ -0,0 +1,22 @@
+archive/ES_0.5605953518578017---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T21:54:24.881
+Launch V∞: [7.588278995592454, -5.591898336177637, 0.15503011622801893] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2208655882313754e-6, 0.00010917034461592424, 1.9221404300982746e-6] km/s
+ V∞_out: [0.00010527830028284219, -1.550390086090648e-5, 2.4194064994441313e-5] km/s
+ time of flight: 1.8547499951785228e8 seconds
+ arrival date: 2030-03-26T14:44:23.881
+ thrust profile: [1.0 -0.0005180646004906117 -0.23706744782148645; 0.075992603339261 0.04967195244454376 -0.07857557673472763; 0.05616460892473131 0.062007558413052645 -0.10641693738971572; 0.03302899755176997 0.04908584744894745 -0.0917898725698546; 0.021755727617168732 0.04085531326630162 -0.08355226364435323; 0.01690333727368644 0.041319467809587736 -0.09533703441749329; 0.00900569800507472 0.02734110220991755 -0.06563396231205446; 0.005702810768937286 0.01695833048078519 -0.044326604645587436; 0.003402183166089262 0.012855480340758622 -0.0347908595606899; 0.0030536331364367604 0.012074197567070368 -0.034584518030552285; 0.0020432376123306383 0.011218759977448835 -0.033374156956348315; -7.801847358658001e-6 0.0008581854922348549 -0.002514390374689006; -0.0002690787480756506 -2.1974407520916064e-5 -0.001131614122425741; -0.0004405972191133872 0.0001592837986571475 -0.0010757860208235313; 0.0008239319879153984 0.0006795126284285876 0.0007706616594124727; 0.0014031332373560523 -0.0011631692162667492 -0.0009225408314707164; 0.0005428253663964849 -0.0016381632771960454 -0.0006325851111294019; -0.00028432300199323 -0.001350749799702338 -0.0003696645097366381; 0.0007972148975824115 0.000453442526335594 0.00040139878415202486; 0.00021190420363925233 -0.00016784697205597015 0.0013527302620835076] %
+
+Mass Used: 135.5884303522398 kg
+Launch C3: 88.87533945403352 km²/s²
+||V∞_in||: 0.00010919408995077163 km/s
diff --git a/archive/ES_0.5606221339219126 b/archive/ES_0.5606221339219126
new file mode 100644
index 0000000..36edec9
--- /dev/null
+++ b/archive/ES_0.5606221339219126
@@ -0,0 +1,22 @@
+archive/ES_0.5606221339219126---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T06:57:28.265
+Launch V∞: [7.958292117002565, -5.8223237469339875, 0.10428005410656628] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4516446735711684e-7, -4.80700580109947e-7, -1.3539282463042261e-6] km/s
+ V∞_out: [-1.3133016377235193e-6, -1.5292151887189214e-7, 5.87800395520054e-7] km/s
+ time of flight: 1.8749577782527533e8 seconds
+ arrival date: 2030-04-25T09:07:05.265
+ thrust profile: [0.29551481648039174 -0.0021807018019970262 -0.09862125881564379; 0.07267493024107474 0.03899923733635375 -0.08898125406691838; 0.05005314475494472 0.04475480427868125 -0.1104170701240799; 0.02976998606708005 0.03395027229641525 -0.09881821150171437; 0.023567042432580346 0.02903984692372342 -0.0952625088841699; 0.012152335629970267 0.023005747141735977 -0.07554381509852659; 0.011856783575334312 0.021061428312176823 -0.07183162449775343; 0.016508641708947523 0.027556893434304366 -0.116360045825007; 0.002684114163766403 0.006274634418122718 -0.02384132136742881; -0.0006300627125895137 0.0006373118164338402 -0.0047872804869952814; 0.0013308207822469728 0.004760420403814744 -0.009319957594943551; 0.00031714206369789816 0.0013182853790828955 -0.003549432275774607; 0.0006394868218582562 -0.0038159639734139557 0.002274187611977195; -0.0028273659647391407 -0.00210406989101264 -0.002289178183128966; -0.0014283726831819132 -0.011806224005545707 -0.004548026781288916; 0.009903242835299168 0.0012746636532753074 0.0018572214547849114; -0.004569149501093732 -0.002135522839163419 -0.004416241200532338; 0.0008706809050771417 -0.004099707388897818 0.006344256736915829; 0.009874146080442308 0.0023911085182566853 -0.009944416905896114; 0.007639497535233258 0.004322446510713097 -0.0019166777334822813] %
+
+Mass Used: 86.79816378940859 kg
+Launch C3: 97.24474156334107 km²/s²
+||V∞_in||: 1.4440455209035315e-6 km/s
diff --git a/archive/ES_0.5606246863057148 b/archive/ES_0.5606246863057148
new file mode 100644
index 0000000..c5ffe5e
--- /dev/null
+++ b/archive/ES_0.5606246863057148
@@ -0,0 +1,22 @@
+archive/ES_0.5606246863057148---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T15:52:17.586
+Launch V∞: [7.918303129237071, -5.825701756333751, -0.06181537363804937] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1228528614701572e-9, -1.3220120708646413e-9, 1.0933873108697993e-10] km/s
+ V∞_out: [3.738060397896915e-10, -1.209414222895762e-9, 2.0012896539900797e-10] km/s
+ time of flight: 1.8442265421140176e8 seconds
+ arrival date: 2030-03-19T04:23:11.586
+ thrust profile: [0.3459149591113012 -0.010982304126268579 -0.11684262432962528; 0.06635802673393978 0.03487227811443402 -0.08231083809904295; 0.031222773097939322 0.024857214660042468 -0.06789663356194373; 0.03150180308424844 0.03332292472003028 -0.10244172982466032; 0.03351362514756029 0.042213550111180616 -0.14207330044613453; 0.020181271617200403 0.029288227110843206 -0.10845437417176265; 0.01322950492309142 0.020866027660502717 -0.08559685555748509; 0.007576724706615395 0.013521294601555035 -0.057901248301180666; 0.006233691008407047 0.009377399625897996 -0.04249732605057851; 0.002230929725572648 0.0027841531091858805 -0.0054054725118422575; 0.000915922620858516 0.005234234400480984 -0.0168651666062519; -0.0005449361518053944 0.0015564479448662606 -0.004860093330587215; -0.00647637740210055 -0.008243807987746724 -0.006040211328919428; 0.004107507468085712 0.0014653308158438115 0.0031804576964004653; -0.0010246034617845314 -0.0017355954552424203 -0.0044922552605496085; -0.00020074617571598844 -0.00010802681759117662 -0.0003495227025264876; -0.0013760850246922164 0.0011377211950794528 0.0032544335627600804; 0.0005164129791574287 0.003932053701849158 -0.0061848035056115604; -0.005171956913224425 -0.01483730837179169 -0.018177359472385916; -0.0036572553930002117 0.00031337044802182113 -0.015539346098537344] %
+
+Mass Used: 90.31627920285382 kg
+Launch C3: 96.64214654065374 km²/s²
+||V∞_in||: 1.7379497754938859e-9 km/s
diff --git a/archive/ES_0.5606282902243162 b/archive/ES_0.5606282902243162
new file mode 100644
index 0000000..be9f571
--- /dev/null
+++ b/archive/ES_0.5606282902243162
@@ -0,0 +1,22 @@
+archive/ES_0.5606282902243162---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:26:25.206
+Launch V∞: [7.909165252093375, -5.848944500052827, 0.13784692615595157] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.018399119641074e-5, 4.994687662448562e-5, 0.0034676079338719283] km/s
+ V∞_out: [-0.003097359825405365, -0.0009997805776167895, 0.0011991551178041784] km/s
+ time of flight: 1.8527616364716235e8 seconds
+ arrival date: 2030-03-29T00:02:28.206
+ thrust profile: [0.29693076345469976 0.000838029845265851 -0.09057131623262049; 0.0878127018221771 0.05499648722148134 -0.10124502174165208; 0.04575173944653623 0.04499027240423471 -0.0949886499000217; 0.03559394335219234 0.0442056406866973 -0.10377273138002333; 0.015542986288124953 0.02810648598516632 -0.08592732539407016; 0.019207471586130946 0.04048656136535986 -0.10880240058244564; 0.014937452373867439 0.028614536229107052 -0.07915704216929308; 0.008626019611072074 0.024749931891933058 -0.07191584912073105; 0.0034702927466685792 0.015070415443565731 -0.04395710245373305; 0.001483594212520048 0.003706904937973029 -0.01592677255323652; 0.0008608777508919557 0.006665430884333326 -0.015362243491316228; 0.002409252180316148 0.004199543393438457 -0.001427618982140021; 0.0018323638162432354 -0.0014918563530157904 -0.0013226694007850367; -0.0023904851294727957 -0.0008681892143006414 -0.010033926977590528; 0.008380465419206784 0.0019293330511383894 -0.00203367126188734; -0.0015274184749089865 -0.0015825684028066716 0.001664725903692527; -0.0029075143005533395 -0.001403362265178459 -0.0024234532017959115; 0.007125510797141342 -0.010121823650624084 -0.004577380070692159; -0.003894193420039196 0.004034048012684376 0.007155699672544217; -0.01015359986954081 -0.009297220357694052 -0.010944566387252278] %
+
+Mass Used: 89.49272220112653 kg
+Launch C3: 96.78404852467011 km²/s²
+||V∞_in||: 0.0034686777403149377 km/s
diff --git a/archive/ES_0.5606359899439339 b/archive/ES_0.5606359899439339
new file mode 100644
index 0000000..255533f
--- /dev/null
+++ b/archive/ES_0.5606359899439339
@@ -0,0 +1,22 @@
+archive/ES_0.5606359899439339---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:54:15.504
+Launch V∞: [7.960571840336577, -5.86037902971746, 0.3422990421812846] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.778968985118717e-5, -7.304935490560097e-5, -0.00019248612798158316] km/s
+ V∞_out: [-0.00018977148495204094, -2.5976943231403502e-5, 8.051743587242314e-5] km/s
+ time of flight: 1.8516189250146922e8 seconds
+ arrival date: 2030-03-27T14:45:47.504
+ thrust profile: [0.18997646554796904 0.0026423584499857987 -0.059110128431544194; 0.09542589760245643 0.05736689629202108 -0.099176687308847; 0.06374346302317256 0.06374790809631388 -0.12104546578341321; 0.03275864612981749 0.044317419571098325 -0.09703845416592112; 0.03013836856960901 0.046327253233469194 -0.11483990094855538; 0.01515321052763947 0.029551226963753358 -0.08023529941444804; 0.009979793407884541 0.022137515148922614 -0.06297025268633616; 0.01171754483839349 0.03073874583012853 -0.08988354062516912; 0.0008765885261013454 0.004557974122678285 -0.02019117995386654; 0.0021171283786651654 0.004531112122591545 -0.022047459407784048; 0.00034330449416909974 0.005047741685768997 -0.0154708836643964; -0.0022406547607288748 0.002661542595713228 -0.004799751665873662; -0.0047100576854509435 0.00629815172119277 -0.0034728666660262496; 0.0007458858303874996 0.002295959067419079 -0.0016169435078431408; 0.010419404098202757 0.009478878698565011 -0.004783956535229678; -0.0029337756573978905 0.0005107926891517005 -0.008565260910906137; 0.0054850569158807205 0.0034074814184008803 -0.007327697664354701; -0.0005421453118149228 0.006120834680698736 -0.013448854054111448; -0.008779103162370811 0.001103913815124487 -0.0022310344858875062; -0.00047870728095311183 -0.005872304367812742 0.0057879294084041445] %
+
+Mass Used: 83.38915058481416 kg
+Launch C3: 97.83191503139007 km²/s²
+||V∞_in||: 0.0002077483684159566 km/s
diff --git a/archive/ES_0.5606392728542628 b/archive/ES_0.5606392728542628
new file mode 100644
index 0000000..0cf6a0d
--- /dev/null
+++ b/archive/ES_0.5606392728542628
@@ -0,0 +1,22 @@
+archive/ES_0.5606392728542628---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T05:56:01.940
+Launch V∞: [7.883870910088355, -6.1046655479483025, 0.08916243925459687] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.330834933636189e-6, -6.353837337389955e-5, 0.001173598147892607] km/s
+ V∞_out: [4.8616753226518196e-5, -0.0011748016322134284, 2.2630886725562807e-5] km/s
+ time of flight: 1.8419109695959112e8 seconds
+ arrival date: 2030-03-20T02:07:37.940
+ thrust profile: [0.21008542797465665 -0.014398694030474475 -0.07909858149259764; 0.04165081266505539 0.01644035679823626 -0.06029479977616454; 0.038324300784625454 0.02564549243933937 -0.09788800263118551; 0.031288942031311565 0.022252514240205322 -0.10960368978726837; 0.030620158924168063 0.02914547997559333 -0.14291986031030182; 0.01732561982002231 0.015242187588862295 -0.0934228502390341; 0.014584247236507834 0.016182550085494084 -0.10645462653620051; 0.006650704860329358 0.006584443651425916 -0.04874863629896994; 0.003177547319827286 0.0026910172706963455 -0.024171080942469173; 0.003191040430887668 0.002887345297039186 -0.029065839536899073; 0.0007100312217510295 0.0010340096744614299 -0.009972084017789127; 0.001148133239444164 0.001466292032939342 -0.012181873699171002; 0.00023619306791280601 1.1047655437770117e-5 -0.0008591942301751053; 3.70410240713754e-5 0.00013109851388721518 -0.0006901031369148114; -1.7958902692845504e-5 0.000509524243909815 -0.0006981968617880034; -2.7475093770048045e-5 8.865460923649727e-5 -0.0005042092417528747; 0.0004733545327795859 -0.0005455859400339267 -0.0008712888765763439; -0.00026355334566069064 0.00032137565990058366 -0.0010274478307226165; 4.5361672288025e-5 -4.613015080857115e-5 -6.224935817891611e-5; -0.00014094039277459235 -0.00020086963115112974 0.0002529291442898102] %
+
+Mass Used: 74.06899879770071 kg
+Launch C3: 99.43031191981815 km²/s²
+||V∞_in||: 0.0011753463916814694 km/s
diff --git a/archive/ES_0.5606415604367481 b/archive/ES_0.5606415604367481
new file mode 100644
index 0000000..7537eec
--- /dev/null
+++ b/archive/ES_0.5606415604367481
@@ -0,0 +1,22 @@
+archive/ES_0.5606415604367481---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T00:43:38.934
+Launch V∞: [7.754929172135357, -6.084689621468404, 0.30510776390118677] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.615353595454984e-6, 1.758144961982311e-5, 4.30266145031949e-5] km/s
+ V∞_out: [3.989357030641408e-5, 6.694525180779326e-6, -2.406577103219387e-5] km/s
+ time of flight: 1.7635150570637712e8 seconds
+ arrival date: 2029-12-14T03:15:23.934
+ thrust profile: [0.27496555713525717 -0.025304636674319682 -0.09956751031224323; 0.06845222318765247 0.028078319849676996 -0.08153028444001328; 0.06298930195322987 0.04202159289458482 -0.12897195154250135; 0.05089177139276519 0.0427633159257794 -0.14856035082898994; 0.032941908988573514 0.03198194830196141 -0.12826998911245496; 0.02850040361894859 0.03397275412990294 -0.1367813040566968; 0.015852415207725977 0.018347405446324683 -0.09138105159804659; 0.006427615419029497 0.008958239345983167 -0.046180260273142745; 0.002272303642932582 0.005560584307973425 -0.026391769583483812; 0.0018141741963347395 0.0030871345996612634 -0.016864247355228363; 0.001005514540111178 0.0009210441047667801 -0.0030550389799378097; 0.001631547756106779 -0.0003546721178249659 -0.0067685558863372144; 0.0029721099064621997 0.001455300733272206 -0.010588907691991984; 0.001053237009133936 -0.00039514356350233543 -0.000979893394454582; 0.002746222056038513 0.002880590771527264 0.0009898248095278387; 0.002777902108984867 -0.006238477163958758 0.0015229369877837414; 0.0007119660290836647 0.004315810530984631 0.003388600657835204; 0.004077623555325966 0.00030902555067296544 -0.0019756581313889513; -0.00437794688898076 -0.00022232469745011682 0.0033881495876056642; 0.001051800874826109 0.0031566719506708777 -0.0013286686855279411] %
+
+Mass Used: 86.75827466434066 kg
+Launch C3: 97.25546500203407 km²/s²
+||V∞_in||: 4.694848058812787e-5 km/s
diff --git a/archive/ES_0.560645507942724 b/archive/ES_0.560645507942724
new file mode 100644
index 0000000..2547223
--- /dev/null
+++ b/archive/ES_0.560645507942724
@@ -0,0 +1,22 @@
+archive/ES_0.560645507942724---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T03:10:21.583
+Launch V∞: [7.705767318603757, -5.799769714103521, 0.14331903553887382] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7414769512451527e-9, 2.4063256383082116e-8, -4.7173050703254355e-9] km/s
+ V∞_out: [3.2839256686495435e-9, -1.2411789592671806e-8, -1.7701783378888752e-8] km/s
+ time of flight: 1.8206735651740262e8 seconds
+ arrival date: 2030-02-16T09:26:17.583
+ thrust profile: [0.5469730059200613 -0.030902229972362107 -0.12230568642753319; 0.17168611062714187 0.09302427847673053 -0.15404295708977664; 0.05931618813974853 0.056425225447403214 -0.10858804742753052; 0.041078556103062734 0.04459392120739016 -0.10219468083957944; 0.020563021840733185 0.031930515369101534 -0.0766495693644096; 0.022719221051481636 0.04246494135727474 -0.10672781555830776; 0.009127401646341102 0.01773913280862187 -0.05113724117911996; 0.010534211918785914 0.027481741171169992 -0.08014774876759113; 0.003006276113672357 0.008661365209651174 -0.026981860050449773; 0.0037258477986679803 0.009084381461518187 -0.03292847967280148; 0.0021299781924678926 0.010180981062335344 -0.03151914234287381; -0.00028437519409111364 -0.0016594552600493109 -0.0005956822723171165; -0.002172733597294764 0.0016823844482114659 0.0001807544153860593; 0.0026719450285583803 -0.0006559687554347356 -0.0011154881177231329; -0.0004670240486484217 0.0008385127850261195 0.002942165826841649; 0.004029770264543301 -0.003562124269150725 -0.002826990537515316; -0.0027306920600606117 0.0038898941375415455 0.0013647614497417047; 0.0017612883924069643 0.0039633270872805205 0.003245532267416784; 7.353318851450671e-5 0.002981507187025117 -0.0003815236705529692; -0.0002568166626944461 0.002340477740545733 -5.3589834686963554e-5] %
+
+Mass Used: 111.37223146876659 kg
+Launch C3: 93.03671905104197 km²/s²
+||V∞_in||: 2.4674054607191512e-8 km/s
diff --git a/archive/ES_0.5606573889001436 b/archive/ES_0.5606573889001436
new file mode 100644
index 0000000..c001df4
--- /dev/null
+++ b/archive/ES_0.5606573889001436
@@ -0,0 +1,22 @@
+archive/ES_0.5606573889001436---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T22:24:16.435
+Launch V∞: [6.640098203867051, -7.333698017696634, 0.10701632473973499] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0236572517495217e-6, 0.0003413844414062404, -0.00023490054824434824] km/s
+ V∞_out: [-0.00020989426627460224, -0.0003497602751367781, 7.298331215752471e-5] km/s
+ time of flight: 1.8749577787493473e8 seconds
+ arrival date: 2029-04-09T00:33:53.435
+ thrust profile: [0.20057215005753742 -0.05202262901232035 -0.07285440949237439; 0.06594160085005146 0.017210955716817546 -0.07299711266992709; 0.07495003066747104 0.03821566002308577 -0.13855179377944174; 0.06932262612532025 0.04746182816727281 -0.17906133842462127; 0.046129042959062706 0.037924776463611004 -0.15401191325128774; 0.03257033656354852 0.030688590514421618 -0.13327570442293582; 0.016279244062875158 0.017058822423030844 -0.07982928734758538; 0.0019235162079628398 0.0022292900600939455 -0.011143325495814038; 0.0018699412788243566 0.002317982801508553 -0.011897578471859757; 0.0003555784455213778 0.00042250582929329885 -0.002360030331964979; 0.0005939774858975397 0.0006778143427615777 -0.004248169325289196; 0.0010108635139420832 0.0011742516912770892 -0.007091776771608708; 3.105977665045895e-5 5.731607298792296e-5 -0.0006101452697746034; -0.0004275230571542969 6.830620027633525e-5 -0.0011494140366099114; -0.0006297383034933471 -0.00010299437853287152 -0.0007095832333635607; 9.699018407319674e-5 2.4845917624465437e-5 1.205789749480937e-5; -0.0004640918174925639 0.0003039306825343551 -0.0006978648976432915; 0.0012776477631140151 0.00011555681126660945 -0.0023577350793599575; -3.797800640402047e-5 -1.7254143741626506e-5 0.00015592239724208413; 0.00014905441187313087 -0.0001666161440633966 -3.434710782561381e-5] %
+
+Mass Used: 83.10163466792801 kg
+Launch C3: 97.88548326552679 km²/s²
+||V∞_in||: 0.0004143943197896362 km/s
diff --git a/archive/ES_0.5606584454984362 b/archive/ES_0.5606584454984362
new file mode 100644
index 0000000..9957ab5
--- /dev/null
+++ b/archive/ES_0.5606584454984362
@@ -0,0 +1,22 @@
+archive/ES_0.5606584454984362---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T22:06:19.890
+Launch V∞: [7.834593170496187, -5.614624504258389, 0.05169408597369839] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2983711921975094e-9, -2.3979413752794002e-9, -2.0525350537732196e-9] km/s
+ V∞_out: [-3.142178136125051e-10, 2.810095933318556e-10, 2.4172308126314583e-10] km/s
+ time of flight: 1.8749577783410287e8 seconds
+ arrival date: 2030-04-21T00:15:56.890
+ thrust profile: [0.6176192547485465 0.002909637848447406 -0.1518066020238458; 0.10466895061307879 0.069188336578597 -0.09362335572624904; 0.026367251215544053 0.030723674166227673 -0.04614477126889657; 0.020620138059936323 0.03131316388802188 -0.05373203094483476; 0.01758568834075463 0.036971650091906304 -0.068375723065348; 0.012198023025791578 0.0337687250776722 -0.06763637852523632; 0.020733511915552914 0.0682369181639096 -0.13351516450135603; 0.021828480279235233 0.06559158817148743 -0.1368589532292758; 0.008790135275811801 0.020765483876406393 -0.05211781553956089; 0.00019246267009526575 0.0026527151763276304 -0.008150302481568936; 3.935343591871074e-5 0.005851521792201666 -0.01655247464047483; 0.00012489395282939958 0.0017986168568473525 -0.006131405084670192; -0.000766578266096674 0.00029597796088494583 -0.0014518976162411741; 0.00032708631176954684 0.0027027009235419184 -0.0082509325864623; -0.0038186122200490136 0.0021034861553485967 0.0017481413827258926; -0.0008943159288533787 -0.0005871547270447649 0.0021034858877375297; 0.00450701357512881 -0.004498763688812975 0.0017329976804963654; 0.0021882554730862733 -0.0014522328405474673 0.002891986284582308; 0.00029338391518465487 0.00020696102382143818 -0.0006060822988319431; -0.0006757948759767903 -0.0025385173536135227 -0.002570086312189282] %
+
+Mass Used: 112.1409237092571 kg
+Launch C3: 92.9075307495289 km²/s²
+||V∞_in||: 3.413032484312606e-9 km/s
diff --git a/archive/ES_0.5606666490040322 b/archive/ES_0.5606666490040322
new file mode 100644
index 0000000..d4803a1
--- /dev/null
+++ b/archive/ES_0.5606666490040322
@@ -0,0 +1,22 @@
+archive/ES_0.5606666490040322---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T20:35:40.212
+Launch V∞: [7.883357658053592, -5.54892557307183, 0.21088859251889272] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0301318149538505e-7, 7.279988299455304e-7, -1.5821715676763918e-5] km/s
+ V∞_out: [-6.595094534398601e-7, 1.5814529392261217e-5, -1.95129767307992e-7] km/s
+ time of flight: 1.874957778717258e8 seconds
+ arrival date: 2030-04-20T22:45:17.212
+ thrust profile: [0.6392295870250958 0.007893606868335097 -0.17897958649626963; 0.06982120311459825 0.04399273862937147 -0.0756497704056489; 0.04596972183163725 0.04765451019934172 -0.09031886409798849; 0.04956197390486102 0.0693054222095135 -0.14767408662509326; 0.02660121714723795 0.047256101720754846 -0.10987566952487045; 0.013368274105458645 0.029294286744680403 -0.07427865491811866; 0.010962125097063558 0.028791281529641912 -0.07929947419692458; 0.004178269467191105 0.010334357957078745 -0.02660815604877016; 0.0034789311247067087 0.007674626985381531 -0.025361567353476965; 0.0013764828470368552 0.006146189955911096 -0.012957718527783041; 0.0012097562760566584 0.0049426134366607165 -0.01834717678566367; -0.0018254201638876924 -0.000273250939740226 -0.0011714319623214696; 0.0013630503444365927 -0.0035571900979496102 0.0015750022737528518; -0.006102383836929448 0.0006199302066052161 0.0051758395107167725; 0.0005409204659567198 -0.00018594130592318892 -0.004304240803283642; 0.0024916087129009763 -0.006973205958456961 0.00578050778021039; 0.0071957499506461325 -0.004850211895222133 -0.009380047981154115; -0.005189330451967982 -0.005580879285251257 -0.005641546875255925; 8.969286885629534e-5 -0.007004806342831479 0.0011075242172490624; 0.0010563790216807536 0.0013805437795735764 0.002473745387123801] %
+
+Mass Used: 111.71389146206957 kg
+Launch C3: 92.98237697873736 km²/s²
+||V∞_in||: 1.583879038842048e-5 km/s
diff --git a/archive/ES_0.5606690950660596 b/archive/ES_0.5606690950660596
new file mode 100644
index 0000000..0f9057f
--- /dev/null
+++ b/archive/ES_0.5606690950660596
@@ -0,0 +1,22 @@
+archive/ES_0.5606690950660596---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T14:30:58.908
+Launch V∞: [7.591266546366568, -6.10582777398141, 0.12772450618688583] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2148506034934793e-9, 1.6020841242326065e-9, -1.1781663155347423e-8] km/s
+ V∞_out: [-3.678370406271765e-9, 1.2045437178310094e-8, -1.954414087897832e-9] km/s
+ time of flight: 1.7143536219899735e8 seconds
+ arrival date: 2029-10-14T19:27:00.908
+ thrust profile: [0.44927775241799883 -0.04930439647415313 -0.13706178826934448; 0.08414709397256191 0.037854039262653225 -0.08792417208892374; 0.04804461748151418 0.03646810121975047 -0.08798058891898448; 0.08595107814418483 0.08950142722003626 -0.22422433760215818; 0.0421054352629727 0.05113599073249006 -0.14216937051096376; 0.02570497623173448 0.036239606861991715 -0.10956981056188249; 0.017098995957729887 0.026887444231439312 -0.0873519001688877; 0.006374709168777627 0.010816043872350061 -0.03827996991119513; 0.008515525378537376 0.01645012127529261 -0.05931912502132699; 0.003224542591407839 0.006629108045423277 -0.02527987638525045; 0.0005511251102246203 0.0009889789597311625 -0.0038298220492181444; 2.809458623556196e-5 0.0004959135357873803 -0.002089195662293559; 0.0002169199545087691 -0.00014556814692532905 0.0001471915751419555; -5.601022476016927e-5 -0.00030933204803791376 -0.0001090687383632034; -5.601751919333419e-5 -0.00018231223036098643 0.0009696661021448627; 2.7296457420889636e-5 9.562860182896007e-5 -0.00017357897505302543; -6.27786613341696e-5 -6.133562063354641e-5 0.0001556474997619333; -0.0005669395589826705 -0.0004739758161897526 6.362594304408682e-5; -0.00023972284898389728 -0.0014349541493446577 0.0004231753242047059; -0.00026711128775937286 0.00044187777961281476 -0.00037996490784425344] %
+
+Mass Used: 100.38609513464144 kg
+Launch C3: 94.92477413298766 km²/s²
+||V∞_in||: 1.2094619607204875e-8 km/s
diff --git a/archive/ES_0.5606699209482972 b/archive/ES_0.5606699209482972
new file mode 100644
index 0000000..1140e06
--- /dev/null
+++ b/archive/ES_0.5606699209482972
@@ -0,0 +1,22 @@
+archive/ES_0.5606699209482972---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T21:35:10.049
+Launch V∞: [8.116051096237344, -5.6231707181778, 0.16957105200460332] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.35542467098234e-10, -1.0989449679034772e-9, -1.3006039897630957e-9] km/s
+ V∞_out: [9.44971522961582e-10, -7.882340423384882e-10, 2.951651527886405e-10] km/s
+ time of flight: 1.8749577787584573e8 seconds
+ arrival date: 2030-04-22T23:44:47.049
+ thrust profile: [0.252818114116282 0.0031838222771745596 -0.07554816337229; 0.07019742750613245 0.0430656599326158 -0.07634273716197516; 0.05264944815971209 0.0530262291458666 -0.10153776524983689; 0.025945570579645322 0.035356181163222485 -0.07977342045704154; 0.015535052419107114 0.02531616735397216 -0.06611149633582973; 0.020191920452489527 0.04360745168536853 -0.1108728769139619; 0.007987704346701452 0.021928294144430264 -0.06465619366597711; 0.004088005335196501 0.009510925474749138 -0.03260419178485145; 0.007427794103314085 0.023131641550631583 -0.07891641805518547; 0.003004949089474842 0.008048915607173156 -0.0359756531604835; 0.005030385663355072 0.020256304552318284 -0.0699863648954532; 0.0010456451138831755 0.002250207829422644 -0.011398399359359313; -0.0025101520258903973 0.0008756504445762929 -0.0030126264440309596; 0.0019895190003314453 -0.0029609716307640232 0.0025931694888247964; -0.00018167992681136823 -0.005560160730882694 0.0038927455658608096; 0.00042295160955949074 -0.0006362837391282144 -7.96169645227282e-6; -0.0008668709782778197 0.004154650685281952 0.006096774095010861; -0.003859417965684777 0.00034120660672925986 0.0012512751825065533; -0.002292585140948653 0.0011070296346945216 0.00022656858847702136; 0.011198831195310718 -0.013733495686133171 0.0034991500334296934] %
+
+Mass Used: 85.2535572319307 kg
+Launch C3: 97.51908866418559 km²/s²
+||V∞_in||: 1.8966765657308736e-9 km/s
diff --git a/archive/ES_0.5606760348236438 b/archive/ES_0.5606760348236438
new file mode 100644
index 0000000..be88105
--- /dev/null
+++ b/archive/ES_0.5606760348236438
@@ -0,0 +1,22 @@
+archive/ES_0.5606760348236438---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:35:11.816
+Launch V∞: [7.880037921159134, -6.054166410240781, 0.024095392063297437] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9371445663421605e-9, -2.266728509182285e-9, -1.5962190961484473e-9] km/s
+ V∞_out: [-2.1019515780515357e-9, 2.000867038549646e-9, -7.59237565976755e-10] km/s
+ time of flight: 1.7658915265185052e8 seconds
+ arrival date: 2029-12-17T02:07:43.816
+ thrust profile: [0.14860068521423614 -0.016346932996121496 -0.05532959144494984; 0.05948257316053707 0.026333007523625974 -0.08035083836086207; 0.05907152364490304 0.0374812413022041 -0.12502223336605622; 0.04868129651259839 0.039626223940976694 -0.1478231269782712; 0.02340453678074528 0.022101382895479183 -0.09293988964599854; 0.028719511199637636 0.029199827190009856 -0.13399978820808597; 0.015721045588319722 0.018338698470585068 -0.08384348277521368; 0.011291687650281153 0.012846361592246799 -0.060290456395909145; 0.003847553706117688 0.0028387825892518424 -0.015316532809685783; 0.0014405803259238468 0.0033181057948365226 -0.025795897959824; 0.00565145575996553 0.017028844948604734 -0.07045139267450712; 0.0003428975099586418 -0.0022538017455873195 -0.00926758910723448; -0.0023413646877185742 0.003863521800447204 -0.006871463508408084; -0.0004761846872442354 0.000806546184857207 0.00023020303484472563; -0.003772923003267597 -0.005386753269432341 -0.0024711472095749172; 0.0012397407922073306 0.000911612719540265 -0.0015691970063484617; 0.00012902014934572143 0.0002955365361525604 0.0016619548781965912; 0.0005467681941850086 0.00038667816907511946 -0.004139146595265757; 0.004114795604096666 0.002491039911166674 0.0012815313046560073; 0.0014109181437009857 0.0011622568704191907 -0.00042887699463313553] %
+
+Mass Used: 78.08907058759542 kg
+Launch C3: 98.7485091497124 km²/s²
+||V∞_in||: 4.03890972179894e-9 km/s
diff --git a/archive/ES_0.5606966555843502 b/archive/ES_0.5606966555843502
new file mode 100644
index 0000000..df4124c
--- /dev/null
+++ b/archive/ES_0.5606966555843502
@@ -0,0 +1,22 @@
+archive/ES_0.5606966555843502---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T11:07:23.035
+Launch V∞: [7.911125438234521, -5.559757824627121, 0.12572213908393534] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.28948014339797e-6, 2.8923785066310996e-5, 8.583331033867563e-5] km/s
+ V∞_out: [6.89126517065845e-5, 7.560483848668639e-6, -5.876544800101555e-5] km/s
+ time of flight: 1.8749577787524617e8 seconds
+ arrival date: 2030-04-20T13:17:00.035
+ thrust profile: [0.5712077458399585 0.006075231889640321 -0.140898163578636; 0.08253937341788671 0.057680117176392556 -0.08502480071674641; 0.054905100351702596 0.059958647076807446 -0.10189824814330252; 0.03623123077200874 0.054925936054934274 -0.09929321871263763; 0.01853398586520048 0.036754457829397714 -0.07316962326558374; 0.030430458490537365 0.0732955775071908 -0.1484763381613546; 0.009151625758066499 0.02839910875910528 -0.06425370490092908; 0.007304791463821124 0.028159535507009104 -0.06623673190383005; 0.0020004664315053894 0.007768991634611523 -0.019559289305362666; -0.0032950961279253417 0.0016809202025733923 -0.007122131049837853; 0.0011225834466281068 0.0013462803874762057 -0.009011333123872294; -0.0010032152229294575 -0.003932396675299859 -0.0016890053564733933; -0.001856768810350659 0.003639489354540523 0.0013498572222899897; 0.0029141207852471126 0.004674881366413197 -0.008053257550413325; -0.008435753711452793 -0.004441795710889594 -0.0012394156221873834; 0.0015015967562993296 -0.0012509793724210503 -0.0025410086055521848; -0.000620682898932288 -0.0009823915198324926 -0.0035627228791425686; 0.0063972267781367345 0.001682403897406815 0.007454020680974718; -0.0004105625361618053 2.461987408608826e-5 0.004280877933060569; 0.002188568088808966 0.000993916624382968 0.00100188168140734] %
+
+Mass Used: 108.65582170701055 kg
+Launch C3: 93.51261882423967 km²/s²
+||V∞_in||: 9.09541532163614e-5 km/s
diff --git a/archive/ES_0.5607045007980515 b/archive/ES_0.5607045007980515
new file mode 100644
index 0000000..a037a8f
--- /dev/null
+++ b/archive/ES_0.5607045007980515
@@ -0,0 +1,22 @@
+archive/ES_0.5607045007980515---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T02:39:23.507
+Launch V∞: [7.720694930960081, -5.9084802738901665, -0.006004593321957555] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.490038111122676e-5, 9.698080501366903e-5, 0.0002231606625862932] km/s
+ V∞_out: [0.00022563065525294925, 2.5864577295881182e-5, -9.335069288105364e-5] km/s
+ time of flight: 1.7887776032715887e8 seconds
+ arrival date: 2030-01-09T10:55:23.507
+ thrust profile: [0.4052921225939519 -0.0078584294749661 -0.11306772133605349; 0.16448822160587917 0.09895969573288055 -0.15371874069590255; 0.055636600946296286 0.05560027149719186 -0.09922613990687466; 0.05903655503157897 0.07835268194889859 -0.14887316670513015; 0.03335004838279503 0.05966702780175499 -0.12582777782283275; 0.018035552979540743 0.03891108394310309 -0.08888230058312815; 0.01159016417456027 0.03080766934412326 -0.07511393477829792; 0.011078870115830211 0.033804722096007225 -0.08378310773324234; 0.002339853157665579 0.008098775363278254 -0.02266885470591297; 0.00034732636810081335 0.002541087328978842 -0.007537763368129967; 0.0004421961569929644 0.0019372574604703762 -0.004761996849992181; 0.0005445638484108469 -0.0015302964248294082 0.0010455291548551067; -1.2649332322434403e-5 -0.0014165944470159691 0.004010565115237327; 0.001017294552817034 -0.0007147617421235533 -0.0011749710454081169; -0.0009880539932492988 -0.0016242639131348361 0.000766828122287714; -0.0003443993602740392 0.001352548317949616 0.0006458722119904908; 0.00034727608623667014 -0.00024925826488393643 0.0001925544591802394; 0.00010795498880519007 -2.5643737728093564e-5 -0.0003816448607760658; 0.00016090969510454376 8.813048918972356e-5 0.005187756832696328; 0.0012347789577109906 0.0009052161289202571 -0.00078014438993553] %
+
+Mass Used: 102.79263598664329 kg
+Launch C3: 94.51930541904288 km²/s²
+||V∞_in||: 0.00024581292575607486 km/s
diff --git a/archive/ES_0.5607138328015497 b/archive/ES_0.5607138328015497
new file mode 100644
index 0000000..7aae55b
--- /dev/null
+++ b/archive/ES_0.5607138328015497
@@ -0,0 +1,22 @@
+archive/ES_0.5607138328015497---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T14:33:52.561
+Launch V∞: [7.58225786226119, -5.818988120009192, 0.43287024910510236] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2037675909722417e-9, -1.3864559907082216e-9, -9.91323122726983e-11] km/s
+ V∞_out: [3.348041111288764e-10, -1.167070519376657e-9, 1.9774511207646808e-10] km/s
+ time of flight: 1.7809277607935762e8 seconds
+ arrival date: 2029-12-29T20:46:48.561
+ thrust profile: [0.7133982890795075 -0.03704137180660401 -0.1856128303907778; 0.1638512482341229 0.08796353003194136 -0.15329153571340867; 0.07529522642802627 0.06734924646570203 -0.12772347424691455; 0.04933196718092222 0.058979583285548025 -0.1237097207580432; 0.02913342695823782 0.042883334350474374 -0.09896632896242961; 0.026564320989266848 0.046605949404938805 -0.11444807963697026; 0.015843379657932193 0.031993090777889956 -0.08433058993228079; 0.0028134416867896827 0.007662185523115387 -0.02085335760766168; 0.0036101744792413353 0.008509178549375806 -0.025836308937524366; 0.0007501670161170366 0.001887426960855431 -0.006246096959898343; 0.0004227196333863216 0.001291107514847122 -0.004744137311538256; 0.0006636998673162487 0.002100037786806589 -0.0069159326214904325; -0.0005188333227232689 0.0004776565335448537 -0.0005964399528551699; -0.0003000359792913841 0.00027790349544825667 -0.0007789297414052123; 0.00022748419596844115 0.00033016890029525327 -0.0017908747418823188; -0.00018464586745902545 -0.00022391065858478015 -0.0005215988411300838; 0.0016956481584641842 0.00042047435430511915 -0.0017763511300306096; -0.0002280272340614759 -0.000246237592317137 0.0004695847388033105; -0.00014650338405058666 -0.0007141737938725641 -0.0007092270044827833; -0.0005310955350314897 0.0001694539465634984 -0.00035349459721547747] %
+
+Mass Used: 120.19077511653268 kg
+Launch C3: 91.53863368319006 km²/s²
+||V∞_in||: 1.8387886889423598e-9 km/s
diff --git a/archive/ES_0.5607211494268683 b/archive/ES_0.5607211494268683
new file mode 100644
index 0000000..e7001d2
--- /dev/null
+++ b/archive/ES_0.5607211494268683
@@ -0,0 +1,22 @@
+archive/ES_0.5607211494268683---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T18:15:45.807
+Launch V∞: [7.856239157426329, -5.633757012514352, 0.20711632539361918] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8644366023432432e-7, -1.4399818897651592e-6, 2.9113075210049262e-5] km/s
+ V∞_out: [1.0594441687158035e-6, -2.9270213135286366e-5, 2.98869047500508e-7] km/s
+ time of flight: 1.847547453885483e8 seconds
+ arrival date: 2030-03-20T03:01:30.807
+ thrust profile: [0.5900438758306266 -0.01764472092175104 -0.1787489491850284; 0.08383316749371275 0.04599789522929075 -0.09591350684402769; 0.05617894416037773 0.050436121851059425 -0.11351873048761675; 0.03560042108489331 0.041832850663824785 -0.10801982387721162; 0.03783683206898406 0.054429052128948344 -0.15203981091873034; 0.013149097517123669 0.02244762904906753 -0.06888917047428883; 0.008958469152507005 0.018565142405034853 -0.05995542977732667; 0.002987495627640024 0.007661750065443092 -0.026928098941915547; 0.004420662331321838 0.010116814941543113 -0.03522198946687589; 0.0005182963719536481 0.0035072272029060664 -0.01534129501496824; -0.0002668188022671355 4.496513321225557e-5 -0.007599648354912237; 0.0005206686315447806 0.0005525622139699029 -0.003512712463063771; 0.0016249279342809499 -0.001020470760739172 -0.007928613804871391; -0.0022239112213577805 0.002991981263077946 -0.0018407037168545349; 0.002909081113846831 -0.0036250456999482143 0.003132157381674697; -0.001823837526656889 -0.000903739464666238 -0.005719569707360983; 0.0011626090559582866 0.00010421439084941884 -0.007028319165196029; 0.015349394519280897 0.005845231510118802 0.0008038765912448042; 0.0008950100168709014 0.00188079254799605 0.0014740516583527513; -0.008437482579275568 -0.01619261553733762 -0.014603002835385431] %
+
+Mass Used: 108.74278880730844 kg
+Launch C3: 93.50260894697794 km²/s²
+||V∞_in||: 2.914926169334788e-5 km/s
diff --git a/archive/ES_0.5607220886356743 b/archive/ES_0.5607220886356743
new file mode 100644
index 0000000..595d191
--- /dev/null
+++ b/archive/ES_0.5607220886356743
@@ -0,0 +1,22 @@
+archive/ES_0.5607220886356743---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T12:58:58.302
+Launch V∞: [7.728365985817934, -5.793406038664955, 0.5098916663608258] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.72162344719778e-7, -1.955608391568761e-6, -6.3784741964032936e-6] km/s
+ V∞_out: [-5.489884814439423e-6, -6.069324185758273e-7, 3.7799931887148e-6] km/s
+ time of flight: 1.8088021668376046e8 seconds
+ arrival date: 2030-02-02T01:29:14.302
+ thrust profile: [0.5486947776323133 -0.027355380773924923 -0.13887614459433528; 0.0995825120765841 0.053998069839248077 -0.09701754373646451; 0.12479212309798282 0.11159497088513116 -0.20764448451396; 0.0216035448532328 0.02576981613319774 -0.06125712272444029; 0.025391994928014885 0.03780843942400175 -0.08934887674825107; 0.03315680045421173 0.05451560118849448 -0.13478048744098922; 0.007764617783942706 0.017262369905735073 -0.04936621881299695; 0.005269705396201126 0.013210359542475287 -0.0380127883410386; 0.001756563769102353 0.011209561013089921 -0.034112427513044746; 0.0022781210013356635 0.007776991366065494 -0.026187651837041078; -0.00022861154982969033 0.0011709558961051159 -0.004301669603932528; 0.0022581929617103676 -0.0006107203941500103 -0.002829385508710576; 0.0003644252803495929 0.0032042328683053204 -0.007371525983559501; -0.0018854882477625289 -0.0019476064645309907 0.004019422667786614; -0.0005762784464225686 0.00020212955105683748 0.00047199544048892204; -0.0008662664937482943 -0.0006386101111260445 -0.0008021646132482562; 0.002736013953908001 -0.0012034796366279157 -0.0012013430401973217; -0.0011677276191271416 -0.002655880709837216 -0.00355690638905072; 0.0018289189348541749 -0.0038780058848420862 -0.005153419244451769; -0.0013572496959509993 -0.002343997639648948 0.009189069478193337] %
+
+Mass Used: 108.46053094405352 kg
+Launch C3: 93.5511838510114 km²/s²
+||V∞_in||: 6.6960217296594874e-6 km/s
diff --git a/archive/ES_0.560736879257194 b/archive/ES_0.560736879257194
new file mode 100644
index 0000000..0045eec
--- /dev/null
+++ b/archive/ES_0.560736879257194
@@ -0,0 +1,22 @@
+archive/ES_0.560736879257194---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:03:54.992
+Launch V∞: [7.928302519864188, -5.692283733298168, 0.13599242817689766] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.017207432757856772, 0.012151034208203517, 0.0008174215933029234] km/s
+ V∞_out: [-0.015370154565120852, -0.006632663298956461, 0.012784303976622821] km/s
+ time of flight: 1.874957778742193e8 seconds
+ arrival date: 2030-04-23T01:13:31.992
+ thrust profile: [0.4122296145335936 0.0006951989611858873 -0.12276610926548089; 0.11700027372122648 0.07059732801222936 -0.12496268854504561; 0.032953169888826905 0.03302856340012432 -0.06866524133157019; 0.025232350636274672 0.03410693713330397 -0.07869043848976184; 0.01419668273730142 0.024406356646686625 -0.061294710483553255; 0.026219871391989735 0.051829204773868764 -0.1320295172448382; 0.013375771055397357 0.03141645072441252 -0.09228782733826914; 0.009904621575509092 0.026758307205792406 -0.08434388854688409; 0.0016522073151957017 0.005705808032281866 -0.019842653839922363; -0.0007316698493259155 0.0044201468574443185 -0.015459144316620283; 0.0009632871037922423 0.0034604302340398283 -0.013237290513384495; 0.0031608915362172038 0.0055925103562292425 -0.002945885810740673; -7.091669470961728e-5 -0.003420037819502558 -0.0017343028137573463; 0.0077286033685079174 -0.0003184669482670702 -0.005259693225217027; 0.006154238964664081 0.003577937833365253 -0.00539971045842406; 0.004316098057483025 0.01089174558285202 -0.0003761202292407754; -0.005960775149993245 0.0008845057603501449 0.0033683467102067505; 0.000477970682111351 -0.005974068378187758 0.007973870893043935; 0.010472743893368584 -0.00810047419375682 0.0006957812992171716; -0.0006267352128258669 0.004619963880917794 0.00834424383127886] %
+
+Mass Used: 98.40137395702595 kg
+Launch C3: 95.2785688873772 km²/s²
+||V∞_in||: 0.021081070952546323 km/s
diff --git a/archive/ES_0.5607376500283833 b/archive/ES_0.5607376500283833
new file mode 100644
index 0000000..fbdb9e7
--- /dev/null
+++ b/archive/ES_0.5607376500283833
@@ -0,0 +1,22 @@
+archive/ES_0.5607376500283833---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T20:22:57.812
+Launch V∞: [7.924057837050348, -5.821605063823833, 0.02523747142143523] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009409117482816966, -0.0007010590126272751, -0.03915203591519071] km/s
+ V∞_out: [0.0359491657606658, 0.013970367728847483, -0.006909522136004733] km/s
+ time of flight: 1.8749577780955845e8 seconds
+ arrival date: 2030-04-24T22:32:34.812
+ thrust profile: [0.3272232933262711 0.0005806559426689409 -0.10882049405807308; 0.07401236960631856 0.040766745723505554 -0.08743147921036987; 0.032062394649021206 0.027651432205600356 -0.07000329057900813; 0.05789186733439873 0.06684892975793202 -0.17931894602424645; 0.039151628839992826 0.054709084302380424 -0.16459404621686624; 0.014346314076009892 0.022287928513240216 -0.07885437119448482; 0.008486054977121056 0.014474231445835522 -0.057727473149885355; 0.0026761808717229215 0.004067535397950649 -0.02365756130220372; 0.0022121499140376932 0.0032090524736739807 -0.020788758348708764; 0.0031889314371170937 0.0009378903727629241 -0.0026769037927589926; -0.0015167926850457778 0.003452565486282467 -0.00882852930094245; -0.002678449618371914 0.0007857388294088425 -0.0023272793653949025; 0.003007653556428751 0.0026441850636838957 0.0006773706655172633; -0.002196821612478743 0.012790354346220298 -0.0009977328129828025; -0.005158655114991512 0.0005597578878630933 0.003593865189621033; -0.008961269322044644 0.0020748588591458107 0.006607724276557569; -0.0007388796325848951 -0.006878376382220081 0.009918407441257193; 0.0034129979927096264 -0.0019054130894267465 0.004162420587623188; 0.006160997289084792 -0.0014348674556535997 -0.021407242259200474; -5.9099039981235944e-5 0.0006155139687213211 0.001240802134597156] %
+
+Mass Used: 90.2131705513184 kg
+Launch C3: 96.68241505402207 km²/s²
+||V∞_in||: 0.03916961468998162 km/s
diff --git a/archive/ES_0.5607514035910232 b/archive/ES_0.5607514035910232
new file mode 100644
index 0000000..e4a41a7
--- /dev/null
+++ b/archive/ES_0.5607514035910232
@@ -0,0 +1,22 @@
+archive/ES_0.5607514035910232---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T09:37:42.425
+Launch V∞: [7.8416045804201655, -5.901533709041922, 0.003096858343571841] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.125842640903035e-10, -9.936031980775871e-10, -1.18501823035427e-9] km/s
+ V∞_out: [1.955806609280468e-11, -1.4679724077776843e-11, 5.5942600581249885e-12] km/s
+ time of flight: 1.8219593476567462e8 seconds
+ arrival date: 2030-02-21T03:36:36.425
+ thrust profile: [0.38709183383454776 -0.02697316428015214 -0.13735265733563673; 0.03964865852373402 0.017765769244048324 -0.049105130143740225; 0.043335757103209145 0.031001206067701896 -0.0931220778789483; 0.03600936704902571 0.03296728864160759 -0.11129782368697856; 0.036998080884847934 0.0395534505949213 -0.14979398980908873; 0.027569164657523945 0.03292004372149467 -0.13813036405008267; 0.010963639512390728 0.014535593165864375 -0.06795242338292304; 0.009803455675752071 0.01332772141419537 -0.0665883025189392; 0.001114839112528734 0.0034653489850963743 -0.017814777863962954; 0.0035211999286455156 0.005383959392345733 -0.030326535597021212; 0.0035221026851802745 0.0014084863439041177 -0.0007375500491543364; 0.0016845907316512475 -0.00025307047946147084 -0.0016453247988882035; 0.0003797591670104478 0.0012870635685600764 -0.003981568015413105; 0.006785923533767449 0.005273927372088267 0.00020319549597035244; 0.001798279864497092 -0.005543605092594286 -0.004710366864775686; 0.0015215913030013862 0.002316217634165839 0.0013573682406344864; -0.0015148724915825874 -0.001315693206380608 0.004103964730762151; -0.004015857045982434 -0.005881187812958363 0.00837309069172201; 0.014411145925844445 0.005919566550602282 -0.010465156536656276; -0.004991737143292408 0.0033281561978657204 -0.009104424385306927] %
+
+Mass Used: 92.34988357611564 kg
+Launch C3: 96.31887210515623 km²/s²
+||V∞_in||: 1.7469426744312918e-9 km/s
diff --git a/archive/ES_0.5607627057169039 b/archive/ES_0.5607627057169039
new file mode 100644
index 0000000..60d129a
--- /dev/null
+++ b/archive/ES_0.5607627057169039
@@ -0,0 +1,22 @@
+archive/ES_0.5607627057169039---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:49:10.088
+Launch V∞: [7.897988366369244, -5.849167263362824, 0.3260673144162767] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.018788083206793656, 0.10932093332857602, 0.13701711775726041] km/s
+ V∞_out: [-0.07014773936088217, 0.06075149237590188, -0.14985275584131533] km/s
+ time of flight: 1.8093324574131525e8 seconds
+ arrival date: 2030-02-05T03:03:15.088
+ thrust profile: [0.3389816227202647 -0.01764947099667643 -0.11107771502383595; 0.07443049127617138 0.03655674679631231 -0.08603762877388127; 0.03892367147430814 0.03077588475575531 -0.08086565488772123; 0.02669850928930631 0.027227593405179808 -0.08086853285689215; 0.027667749592106636 0.03398415817257811 -0.1097979410930807; 0.017074476988236085 0.02384926073424513 -0.0851836522736317; 0.009029887832250243 0.013825004379368202 -0.054072049228095095; 0.010424793968793087 0.017628657730802726 -0.07220037586969219; 0.003366772572044045 0.006401275855314966 -0.028602451980903908; 0.0288831190039067 0.03925221142956677 -0.17733367483896875; 0.0005150554951136678 0.001030419518461804 -0.0012353037419764058; -0.0003315768036017479 -0.00020263886459366467 0.0015821413345942564; -0.0017103952297900435 -0.000341834922511476 0.002377847218338843; -0.00031759846611094004 7.428143772779893e-7 -0.003461059772531818; -0.004164554683851339 -0.0033750938129741637 -0.0002523191697025686; -0.0005469905092649708 0.000112106305471627 -0.003077459114751319; 0.0001670265054085779 -0.0012939876539682536 -0.0011979396314637017; 0.0015000522286676365 -0.004773642049033222 -0.005285788149660884; -0.0007568813278918643 -0.0036946184721663887 -0.004856983271935801; 0.0006986759941354926 -0.003239469883500658 -0.0016141731640895325] %
+
+Mass Used: 90.15558614854672 kg
+Launch C3: 96.69729780362991 km²/s²
+||V∞_in||: 0.176288822938164 km/s
diff --git a/archive/ES_0.5607692152333923 b/archive/ES_0.5607692152333923
new file mode 100644
index 0000000..3165f83
--- /dev/null
+++ b/archive/ES_0.5607692152333923
@@ -0,0 +1,22 @@
+archive/ES_0.5607692152333923---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:12:05.562
+Launch V∞: [7.573326491396061, -6.265747744730003, -0.09623294973406434] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7476919284538095e-6, 2.589533099060004e-6, 2.4812208024096865e-7] km/s
+ V∞_out: [-2.1040046651064808e-7, 9.74587243365498e-7, 2.9791607941254495e-6] km/s
+ time of flight: 1.7221647258703893e8 seconds
+ arrival date: 2029-10-26T06:06:37.562
+ thrust profile: [0.28391275820025785 -0.026256068983924335 -0.1004526029219305; 0.10412635551459114 0.04752852416235016 -0.1186159732560821; 0.07624813070379562 0.0567697992464339 -0.14742906720199986; 0.050414272661946063 0.047530697801217534 -0.13687549642010421; 0.038809156394488696 0.045055724164390826 -0.14374747309034336; 0.03246869396280766 0.03705645769936438 -0.13777812446093818; 0.017373262921246645 0.02701900824518621 -0.09335685351541985; 0.00618964334759234 0.009706572904401712 -0.04328708858446387; 0.007214552759749939 0.015030014470900303 -0.054903607259249816; 0.0005748254951122127 0.0008669637448006584 -0.003910518364589583; 0.00012615898038715164 0.00044590461433890603 -0.001963781575574966; 0.00012574374665302445 0.00035991319978348333 -0.0013734645591182318; -0.0002737706883402017 -0.0006576694304464898 0.003055011438340683; -0.00024747501876675967 0.0006599830666776765 0.0011310310486851722; -0.00018209285153315623 -0.0020536642040541345 -2.347648786279349e-6; 0.0007230874174349142 -0.00019475130984765207 0.001718358034901587; 0.0008132965417519823 -0.0014018141928438554 0.002179824414841402; -0.0001408774655306673 -0.0007225315017399857 0.0018557479132864326; 0.0012188856931849288 -0.00017298776999448168 0.000445681863198373; 0.00016639844293788526 0.0002579081507207042 -0.00019453010504939295] %
+
+Mass Used: 90.58999436779504 kg
+Launch C3: 96.62412972648502 km²/s²
+||V∞_in||: 3.1339548999009237e-6 km/s
diff --git a/archive/ES_0.5607779313877133 b/archive/ES_0.5607779313877133
new file mode 100644
index 0000000..1194a21
--- /dev/null
+++ b/archive/ES_0.5607779313877133
@@ -0,0 +1,22 @@
+archive/ES_0.5607779313877133---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T07:47:04.126
+Launch V∞: [7.677767704136876, -5.855504546550413, 0.2212041023137796] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.209350939953166e-7, 7.780693662583096e-7, 7.761395180326279e-8] km/s
+ V∞_out: [-7.18093485852765e-8, 3.63040700966509e-7, 9.38614124123851e-7] km/s
+ time of flight: 1.8591151363457352e8 seconds
+ arrival date: 2030-04-03T01:52:17.126
+ thrust profile: [0.4418099842871788 0.0146742486139159 -0.10906122611426941; 0.1818352114293936 0.1221446780891269 -0.15676133448606708; 0.1278966992390346 0.1427970308323828 -0.19945999780760343; 0.0488135356127534 0.07473242638476557 -0.12402333343926354; 0.02119457261696682 0.04163500002944664 -0.07783164705806817; 0.012875005831151639 0.031221379744833865 -0.06285395963957285; 0.006225990566981591 0.01969487904238696 -0.0423290191478858; 0.0030238437648271066 0.010236657004356891 -0.025499735152929307; 0.0018662218713960687 0.00779947536175059 -0.018642282955054167; 0.002391293897949953 0.006238775900583475 -0.014323994832676086; 0.00023423112723877477 0.000860854751677321 -0.007928301187135814; 0.0022425973753089218 -0.00011524583655186634 -0.0012089151961495654; 0.0014463585464729069 -0.002841957694633096 -0.0008022367383158971; -0.005862522925024537 0.0050453171501570375 -0.002679429961139232; -2.2229989042627806e-5 -0.001991743567061495 0.0021694154493386852; 0.0040041728851503595 0.004625082274206908 -0.0017894580075915162; -0.009260547196192594 0.001988054496533444 -0.0009336621155240563; -0.002197778912173654 0.00031206251406626644 -0.0031659554193248438; 0.0049666150164327134 0.0036561114134151854 -0.0005048139670954838; -0.00046070784965286893 -0.009024129086774751 0.000775065269642901] %
+
+Mass Used: 110.08436022093065 kg
+Launch C3: 93.28398166824024 km²/s²
+||V∞_in||: 9.39568643782899e-7 km/s
diff --git a/archive/ES_0.5607806065079883 b/archive/ES_0.5607806065079883
new file mode 100644
index 0000000..9eeec0b
--- /dev/null
+++ b/archive/ES_0.5607806065079883
@@ -0,0 +1,22 @@
+archive/ES_0.5607806065079883---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T01:21:18.326
+Launch V∞: [8.061234568612187, -5.96304173138033, 0.2747005129913337] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.171405285905931e-5, -8.736184541658575e-6, -0.000567324863467057] km/s
+ V∞_out: [0.0005178876891377556, 0.00017109032207643666, -0.00019796477372975474] km/s
+ time of flight: 1.8749577777142987e8 seconds
+ arrival date: 2030-04-28T03:30:55.326
+ thrust profile: [0.07679713119540961 -0.004636510734291467 -0.0317281214209199; 0.11215643481330981 0.04048604663606088 -0.13845340601739892; 0.022777493898915455 0.012806753411716677 -0.056105158087469575; 0.024074236585449816 0.016469050581385786 -0.08534160003114066; 0.024271397944618103 0.016008281075685468 -0.10360667065537403; 0.015427586902915066 0.011429277975247489 -0.08179051513706888; 0.020644494665028542 0.01668201030265217 -0.12587306116927965; 0.01186266669497488 0.009267047766046796 -0.0811485495443629; 0.005024917637118108 0.004075532028125168 -0.03950910815382059; 0.0024212465881983144 0.001847124728772745 -0.019906709180377027; 0.00016812058445149887 0.0002005386601965514 -0.0012938009849862461; -0.00018394994047552177 9.661883042020289e-5 -0.001453879734974635; -0.0005047482988871986 -5.497568306255722e-5 -0.0003013000731179349; 0.000985930037124363 0.0007608197469379521 -9.10981960369982e-5; 0.00014000960816187667 0.0002525867191861272 -0.001068273037043932; 0.000956412318991484 2.209172880634974e-6 0.0011750804077693593; 0.0015050287183334741 0.0013161438143988362 0.0002852357843889954; -0.0007027019478612498 -0.001938242074382267 0.0006349304631204607; -0.0010270084582766027 0.003045943125473987 -0.0015155352995298774; 0.0035983901266399936 -0.004299795038121057 0.0004237819275860118] %
+
+Mass Used: 67.31253357143305 kg
+Launch C3: 100.61682983220915 km²/s²
+||V∞_in||: 0.0005675130312712172 km/s
diff --git a/archive/ES_0.560804926861521 b/archive/ES_0.560804926861521
new file mode 100644
index 0000000..55f9f41
--- /dev/null
+++ b/archive/ES_0.560804926861521
@@ -0,0 +1,22 @@
+archive/ES_0.560804926861521---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T07:16:15.216
+Launch V∞: [7.562093004931958, -5.878946153351896, 0.10285884754003934] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.202720348529652e-9, -2.5312242474625155e-9, -7.446253786834328e-9] km/s
+ V∞_out: [-7.91675850979502e-10, 2.5734166218399427e-9, -4.225963976643967e-10] km/s
+ time of flight: 1.8371663104172304e8 seconds
+ arrival date: 2030-03-06T15:40:06.216
+ thrust profile: [0.534774727778683 0.010966576327945388 -0.1168478936591338; 0.20517548334669128 0.13807730081598787 -0.16226654116841185; 0.13201995544493927 0.1474758604027944 -0.19136293564945978; 0.06683169593313937 0.10614981734637126 -0.15225729321271636; 0.02804905274252161 0.05671625376116336 -0.09218292761735365; 0.015438533857198284 0.039103421024093164 -0.0681313091203359; 0.0041696891670289634 0.014981503964834452 -0.028375496481227315; 0.004676019416514897 0.018248041956862388 -0.03711259791662048; 0.0013005395863929293 0.0071133387329147795 -0.013843530108989142; 8.875932782223612e-5 0.0022343756405436626 -0.007286104409686491; 0.0002986448200422957 0.0019813017515310258 -0.004166192951768219; 0.00048182164378885025 0.00026134107203163457 -0.0008945654471478821; 0.0006213397905878738 0.00035529766890382726 -9.320130949771717e-5; 2.737050282708382e-5 0.0004976890933210044 -0.00203371758605286; 0.0007746606356010926 0.00039915452280665396 0.0001486173857178281; 0.00019968759559436011 0.0016660285696261292 0.0007568787081048709; 0.00012966674819917461 -0.0031076329365760285 0.00235393054223605; 0.0006803560843474008 -0.0005497909416789094 0.0005885648954683572; -0.0008801986562494089 0.0013493021251612784 -0.001115455948213889; -0.003747319407113575 -0.0007275313142609187 0.0005695714449632521] %
+
+Mass Used: 119.01835715312109 kg
+Launch C3: 91.75783843176916 km²/s²
+||V∞_in||: 8.491831915421585e-9 km/s
diff --git a/archive/ES_0.5608059122454162 b/archive/ES_0.5608059122454162
new file mode 100644
index 0000000..f2d794f
--- /dev/null
+++ b/archive/ES_0.5608059122454162
@@ -0,0 +1,22 @@
+archive/ES_0.5608059122454162---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T18:57:11.075
+Launch V∞: [7.953114220537983, -5.46079759896621, 0.33150953884717765] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.004520334492478e-5, 0.00023469682991613584, 4.02606833367963e-6] km/s
+ V∞_out: [0.000226975642886781, -3.411763395904069e-5, 5.0744222692920765e-5] km/s
+ time of flight: 1.874957778500917e8 seconds
+ arrival date: 2030-04-19T21:06:48.075
+ thrust profile: [0.5588316008517806 -0.013622463554216516 -0.14695315670244338; 0.22134905976841784 0.12787003981742523 -0.23964222583590394; 0.043412671605852535 0.04036494598197442 -0.086770001600984; 0.02870708590313993 0.0354326798134296 -0.08636985672376501; 0.014806291568552635 0.0226084127165427 -0.06219956728611128; 0.011859904687045971 0.02087290719738432 -0.06284931017876719; 0.009839083257031124 0.020183361433703192 -0.06483946552001245; 0.004692631104722661 0.010884117920480002 -0.038864281111831656; 0.0019610954205005683 0.008326215100111145 -0.03196961957398098; 0.002207083891213046 0.005864658809273824 -0.019786961699021378; 0.003283908117349434 0.0033916240593751326 -0.014768128985046172; 0.001542669552574853 0.0012164660167264876 -0.0007041546925089766; -0.0007595376516565222 7.962608245143691e-5 -0.00044835027965428446; 0.0011614942823650438 -0.00029059315837756634 -0.0007706577347468271; 0.000689883785350024 0.004616267686238777 -0.0011566058269028411; 0.00015958732758306364 -0.0004745575417393238 0.0004294707493563534; -0.0010516412160350215 0.01016238551607396 0.004132474177343226; -0.00029389578512947605 0.0007757284696233216 0.0003524059356753567; 0.0011793681911990157 0.0026002627074507745 -0.008047546817442118; -0.001975274834994791 0.004907024093936382 -0.005621720720328077] %
+
+Mass Used: 110.71052797547145 kg
+Launch C3: 93.18223479614528 km²/s²
+||V∞_in||: 0.0002349462008825679 km/s
diff --git a/archive/ES_0.5608193074565263 b/archive/ES_0.5608193074565263
new file mode 100644
index 0000000..ced30a8
--- /dev/null
+++ b/archive/ES_0.5608193074565263
@@ -0,0 +1,22 @@
+archive/ES_0.5608193074565263---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T11:50:14.562
+Launch V∞: [7.682892132904044, -5.7391066066872165, -0.15656438919077056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.818335215549831e-9, 4.5757115574727774e-10, -7.77215818596932e-9] km/s
+ V∞_out: [-2.216466812763963e-9, 7.705673449546783e-9, -1.2100069978973209e-9] km/s
+ time of flight: 1.8749577787405252e8 seconds
+ arrival date: 2030-04-21T13:59:51.562
+ thrust profile: [0.6055531171791639 0.009940581029551693 -0.15607550437611248; 0.15408299968139255 0.10034165951983504 -0.14908203754550092; 0.0856331096995925 0.09252786236364145 -0.15375239899041138; 0.04568766736227129 0.06644023707247322 -0.12522096354367931; 0.03533187185051686 0.06466606928269276 -0.13254107690503583; 0.016611085964923902 0.038302551545965256 -0.08517037253217058; 0.0025969293051812978 0.0068427859019419305 -0.016763652834971533; 0.0026610992148892614 0.009379266036008152 -0.02381632701078415; -6.430670849669851e-5 0.0026811456637617654 -0.005580906002781098; -0.0020550179257941385 0.004363964500795439 -0.004367865978446302; 0.0005824915675150409 0.00488233536961994 -0.003192024250073591; -0.0003527667765986684 -0.0011756802192785549 0.00047551611528000087; -0.0010048972713341115 -0.003215159605089682 6.099780695412692e-5; -0.0036938597258378437 -0.0013443544309307966 -0.0017399462359844247; 0.002611538052309158 0.0005137499637192944 -0.00716241755997622; -0.0030341474302762513 -0.00637983390792094 -0.0048884646439492484; -0.007058662259049064 -0.0030504792443708114 -0.003372491544696462; 0.0040746088737070585 -0.006337631054572368 -0.0017741310867085197; 0.0037722704895713707 0.0013351444147329835 0.006621611528100219; -0.0056520366562304285 0.0058175056447690885 0.0015546051042160003] %
+
+Mass Used: 117.68850866840012 kg
+Launch C3: 91.98868857672238 km²/s²
+||V∞_in||: 7.995133343879292e-9 km/s
diff --git a/archive/ES_0.5608232374895321 b/archive/ES_0.5608232374895321
new file mode 100644
index 0000000..e5ec528
--- /dev/null
+++ b/archive/ES_0.5608232374895321
@@ -0,0 +1,22 @@
+archive/ES_0.5608232374895321---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T16:45:10.549
+Launch V∞: [8.045873396887568, -5.901166607081959, 0.3076587892546292] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.085825266544724e-9, 5.320012635589451e-10, -1.6719340922356749e-9] km/s
+ V∞_out: [6.381682575628777e-10, 1.246272428779425e-9, 3.2472519582021746e-11] km/s
+ time of flight: 1.8450670833171514e8 seconds
+ arrival date: 2030-03-22T04:36:58.549
+ thrust profile: [0.15586584535438866 -0.009296417802421499 -0.057443004201327405; 0.035937694191768274 0.015146128958700145 -0.04478516565557419; 0.023810725352474662 0.015230206178666574 -0.052738010154892934; 0.025254944514234424 0.02009932100389899 -0.0794129759571259; 0.01648740784121383 0.015090447108531609 -0.06788289594824598; 0.013730052491849202 0.013459812653204907 -0.06796714849674867; 0.021094889332060832 0.021432629041558657 -0.11552317133645197; 0.03660764224185368 0.03816674033485702 -0.22655515019808767; 0.007365499558514847 0.009036490634176952 -0.05505484327407391; 0.002610913112954591 0.0017776592325502744 -0.004576099970706146; 0.0031013275232057943 -0.0004482925204059092 -0.0051528293867881296; -0.0027945672584486535 0.000455166264405983 -0.01071779463294548; -0.0020753858365704517 0.002977238502472379 -0.0065260937125199096; -0.0006038120514811824 -0.0004585841654870356 0.002735921655986427; 0.0003760492832316092 8.095371704369491e-5 -0.00107754134083364; 0.0006855476276543078 0.003633994259884068 -0.003113845735132773; 0.002154566025353053 0.0023345818896151785 -0.009852829229374586; 0.0031412608103802125 -0.009572511285253459 -0.008133214008884528; 0.003580917761126989 0.0011861515903028531 -0.0032875130712629345; 0.003361001590971772 -0.001975096050347796 -0.001841817642533234] %
+
+Mass Used: 72.97586055677448 kg
+Launch C3: 99.65449997388794 km²/s²
+||V∞_in||: 2.0633481196044367e-9 km/s
diff --git a/archive/ES_0.560834254103596 b/archive/ES_0.560834254103596
new file mode 100644
index 0000000..8eda83b
--- /dev/null
+++ b/archive/ES_0.560834254103596
@@ -0,0 +1,22 @@
+archive/ES_0.560834254103596---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:07:23.470
+Launch V∞: [7.989806352592002, -5.659197832231158, 0.20523794962756434] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.5684268185208165e-6, 1.1661727819041047e-5, 3.30882557196164e-5] km/s
+ V∞_out: [3.1396067698106184e-5, 3.7828751728178048e-6, -1.5420876148565165e-5] km/s
+ time of flight: 1.843670960159372e8 seconds
+ arrival date: 2030-03-16T01:12:19.470
+ thrust profile: [0.3726736208055964 -0.009548486365452795 -0.11756586466547585; 0.092854383907645 0.050389205208188466 -0.10354253361857267; 0.04405849872060487 0.038587847779191047 -0.089654317689524; 0.053714843689102974 0.06276492400079346 -0.1600943553064597; 0.031342972241425675 0.0443362017624905 -0.12774437268714248; 0.016689316657061512 0.02712832949322404 -0.08588927376934083; 0.013181077273306066 0.02428295113026741 -0.0820129487071116; 0.005047336990197809 0.010039728008722538 -0.03728538463234817; -0.0011769598197557774 0.0022668506186035407 -0.006882822767452438; -0.000606019167214678 0.0019102325340764831 -0.0017780775129614924; 0.00032618591090068956 0.0009865041112282452 3.75967960874698e-5; 0.0011780581366107078 0.0033091573772111227 -0.011675100509803528; 0.0006805064465919803 0.007408090805927591 -0.007174177249201609; 0.004421357563083392 0.0003426441484536044 0.001031730927436904; -0.0016114143481248439 -0.002758213083186356 -0.010434799795975091; -0.002912575427180028 -0.003364450704262761 0.002076879034840922; 0.0008780296380204945 -0.003365700145847596 -0.004594930311558573; 0.010979765829257257 0.012942911373387012 -0.01929428056005212; 0.002687762367933444 0.00038441153435610307 0.0013028083400163173; 0.005341835508324298 -0.013456999445413568 -0.01617126730895228] %
+
+Mass Used: 94.85701486626476 kg
+Launch C3: 95.90564827221667 km²/s²
+||V∞_in||: 3.526417774812369e-5 km/s
diff --git a/archive/ES_0.56086339364598 b/archive/ES_0.56086339364598
new file mode 100644
index 0000000..fc923dc
--- /dev/null
+++ b/archive/ES_0.56086339364598
@@ -0,0 +1,22 @@
+archive/ES_0.56086339364598---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T22:42:30.534
+Launch V∞: [7.7445677435467895, -5.570703142521764, 0.18775103200208393] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.239016247723188e-9, 3.4379659890133857e-9, 1.9199993112186062e-9] km/s
+ V∞_out: [3.2228358628432768e-9, -3.035416735692201e-9, -2.2564277371657464e-9] km/s
+ time of flight: 1.8540822961868113e8 seconds
+ arrival date: 2030-03-25T20:59:39.534
+ thrust profile: [0.7746238248086367 -0.0012996398910242201 -0.19880932019617986; 0.14792069752419493 0.09355477609553832 -0.1431183018602192; 0.04767810244046263 0.052108821853920184 -0.0928716828890652; 0.030003039022738084 0.04421280904385299 -0.08823357174176898; 0.015533373557818647 0.029276589168568193 -0.06728184667411093; 0.014307950093149257 0.02781448004102504 -0.06780565437229831; 0.004982209079075696 0.013124935039581615 -0.03541182747105957; 0.0031547952314873048 0.011860451399987402 -0.033068874918080825; 0.015477541826107569 0.05878986877003309 -0.1455844322368351; 0.002092474221727028 0.008199891779875922 -0.026876411202996633; 0.0002532624613706552 0.001915604215409319 -0.005441498289071466; -0.0003074084856678903 0.0005712886183980804 0.00013946397803281475; -0.0003105091274530195 -0.0009969581592045172 0.00032764963155040367; -0.0003733303821526475 0.00017551188778565033 0.0010496704404343287; -0.0001840910534593915 0.0002924118251210493 -0.000146621648292855; -1.4381404285741532e-5 -0.0004934408301085853 0.00011026090575692617; 0.0007551827061998829 -0.0007455617558807075 0.000916496351542528; 0.0007098680158583153 0.0001082060659595923 0.0016439048021531396; -0.0003842178273198359 2.1118263295746998e-5 0.0007793512714393051; -0.00036900708818068847 0.00015752542056796876 0.0009287695980334052] %
+
+Mass Used: 123.23713058236353 kg
+Launch C3: 91.04631348650511 km²/s²
+||V∞_in||: 4.529812496589802e-9 km/s
diff --git a/archive/ES_0.5608827185946298 b/archive/ES_0.5608827185946298
new file mode 100644
index 0000000..0a4e66e
--- /dev/null
+++ b/archive/ES_0.5608827185946298
@@ -0,0 +1,22 @@
+archive/ES_0.5608827185946298---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T21:45:12.630
+Launch V∞: [7.945684354816495, -6.076890381227974, -0.017968986569187537] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.086641623607469e-9, 8.207257755037323e-10, -1.260318841679686e-9] km/s
+ V∞_out: [3.2069683033506965e-9, -3.2064597404372814e-9, 1.1692078514526684e-9] km/s
+ time of flight: 1.826687222322337e8 seconds
+ arrival date: 2030-03-02T03:03:54.630
+ thrust profile: [0.15619713427012635 -0.020906350422898026 -0.06862101912542598; 0.03581469057946025 0.009916043839735536 -0.05243365065269433; 0.03862310412443996 0.015694109717324704 -0.0987213923684343; 0.03527146676254012 0.015983579736510035 -0.12673979503661678; 0.02962398084561481 0.013686342589089998 -0.13409299051863754; 0.02310898519712669 0.010423651493588303 -0.12343732201254837; 0.016424731843286893 0.007044850141430873 -0.09931074860227726; 0.009863065321625907 0.003993375247348204 -0.066344693845581; 0.004139991587467092 0.0016652179318935576 -0.03142556294933725; 0.0012269072758902375 3.7274937503183276e-5 -0.004814251641997193; -0.0005336789811215462 0.0011489803698017773 -0.005193361363781783; 0.0002713649539489958 -0.0003759330256091789 -0.0017871445870474758; -0.00018974749513837148 0.0004627640023866338 -0.0013159176940686903; 0.001811901401559279 -0.0008958810728709244 -0.0013167069465002056; -0.0008309374880012524 -0.00012883379493028844 0.0013725304124738856; -0.0020807152400197197 -0.0006331370982016833 -0.0025574089914359496; -0.0007830031565675777 0.001843335681916001 -0.0012705031001721478; 0.0006039470858224595 -0.0002776595902325512 -0.002313812351648192; 0.0009336632242688198 0.0010514477603364432 -0.00268277203990633; -0.0005402712854385707 0.002116204985497817 -0.0021154323906336326] %
+
+Mass Used: 70.6633915318971 kg
+Launch C3: 100.06281945631503 km²/s²
+||V∞_in||: 4.354610676176473e-9 km/s
diff --git a/archive/ES_0.5609004587807164 b/archive/ES_0.5609004587807164
new file mode 100644
index 0000000..1770e5b
--- /dev/null
+++ b/archive/ES_0.5609004587807164
@@ -0,0 +1,22 @@
+archive/ES_0.5609004587807164---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T05:17:38.836
+Launch V∞: [7.619016986403004, -5.835530157410833, 0.42215842887275423] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.467264289653342e-6, 9.628664825173522e-5, 1.6733749117473656e-6] km/s
+ V∞_out: [9.260461029771823e-5, -1.4214333552525003e-5, 2.2088952592710438e-5] km/s
+ time of flight: 1.8085750582450318e8 seconds
+ arrival date: 2030-02-02T11:29:23.836
+ thrust profile: [0.6737648241375929 -0.022845623304087233 -0.16580702839212003; 0.1515037035120958 0.08051466499001189 -0.14556694038551687; 0.032235386101083195 0.028475390425443226 -0.06488345836679212; 0.034644711629809755 0.041209327930212064 -0.09912205133413642; 0.02055690212315161 0.02959814002026289 -0.08076450286129938; 0.01320967018105144 0.021169410500257224 -0.06357963274068648; 0.012830028304450099 0.02267319866046682 -0.07511782401553142; 0.009929180087330736 0.020467697586620964 -0.07307177896502864; 0.004154763728826278 0.010759075589630735 -0.03578692819038383; 0.0063261379600251695 0.023506609507268628 -0.08248959384126235; 0.001187360526113816 0.0061168403298509375 -0.019708784536508234; 0.00060790111204623 0.0019394695161558816 -0.007084324601285627; 0.003502295433858629 0.005670376500953285 -0.016783571875892595; -0.00013311918132383026 0.0015284392310645648 -0.0016999329678167407; 0.0026013698615187 -0.004332331507000483 0.000998635586435699; 0.001272011142111968 0.0007824342981340882 -0.001604314570595157; 0.00025837429009168875 0.00025277767737276957 -8.138893004023477e-5; 8.189191359605043e-5 0.0004923702076931349 0.002180861518167968; -0.0032373826520913796 0.001124134084509242 0.0006834500067956945; 0.0011541849199593148 -0.0013759092226028773 -0.0032707127129020432] %
+
+Mass Used: 116.07774476623581 kg
+Launch C3: 92.28104979621713 km²/s²
+||V∞_in||: 9.63123651440683e-5 km/s
diff --git a/archive/ES_0.5609009591372146 b/archive/ES_0.5609009591372146
new file mode 100644
index 0000000..cbe642a
--- /dev/null
+++ b/archive/ES_0.5609009591372146
@@ -0,0 +1,22 @@
+archive/ES_0.5609009591372146---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T00:04:36.616
+Launch V∞: [8.085991396306817, -5.828809860508292, -0.587189737589191] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.088742576892365e-6, -5.11270122273352e-6, -4.54397732014813e-6] km/s
+ V∞_out: [-8.972777173805637e-7, 6.273621469072147e-6, -7.316123042652528e-6] km/s
+ time of flight: 1.8749577784650216e8 seconds
+ arrival date: 2030-04-26T02:14:13.616
+ thrust profile: [0.148040244271376 -0.000805437980618621 -0.05570343911941068; 0.04223202691847635 0.025137795268310614 -0.056324594493266884; 0.02235718306758092 0.01913460764920122 -0.05312034178149206; 0.03021151607332453 0.03597504805575534 -0.10362153120288176; 0.017539798616948293 0.026005920071289233 -0.08494434105944347; 0.014368925350103482 0.02470234248951357 -0.08832753961312372; 0.013323830272717517 0.026096427713786938 -0.0973984226938248; 0.020201842064754342 0.043251738707852434 -0.164453981581734; 0.004434655137409128 0.00912459110060031 -0.04373237915247838; 0.0016558790870368197 0.0034399633930753204 -0.013829299802688082; 0.0014991855125877627 -0.0010088869770734678 -0.005147391671243058; -0.0001344392536219162 0.0005999238665168763 -0.008457703418813523; 0.006503065326115668 0.002557188472505103 -0.0031021427360697082; -0.0028510648096369837 -0.0010131610605232369 0.0010425153334377222; -0.001089234476100375 -0.0011550010584391941 0.006420154772707779; -0.0008161791293769944 -0.003287412619364361 -0.0012046990202392754; -0.0012441718575895433 -0.0009009329514552984 0.001970453297284273; 0.0019743568283496693 -0.0022508442012163575 0.002130204935015148; -0.001661046222090426 0.0037830337505992354 0.0011426617515090756; 0.0023103474637590805 0.0036331947290139566 -0.004758740617194661] %
+
+Mass Used: 72.78319293237018 kg
+Launch C3: 99.70307303903661 km²/s²
+||V∞_in||: 9.850772304769206e-6 km/s
diff --git a/archive/ES_0.5609046531134404 b/archive/ES_0.5609046531134404
new file mode 100644
index 0000000..00ebd74
--- /dev/null
+++ b/archive/ES_0.5609046531134404
@@ -0,0 +1,22 @@
+archive/ES_0.5609046531134404---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T08:22:54.978
+Launch V∞: [7.987839283649908, -5.551082201038648, 0.2590706080772451] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005945084821624036, 0.004185721554772492, 0.0002551909433159116] km/s
+ V∞_out: [-0.005248801338560595, -0.0024096522515491365, 0.00441164825258226] km/s
+ time of flight: 1.8749577787425315e8 seconds
+ arrival date: 2030-04-21T10:32:31.978
+ thrust profile: [0.4796301954565681 -0.00019266043665075805 -0.1453045116905358; 0.07673652625298306 0.04484348966886215 -0.08396965905889019; 0.06808946681716663 0.06481545933155573 -0.13471390091861613; 0.0423439801570718 0.053300950299645294 -0.12576080617350233; 0.03503546888314006 0.05447531114084954 -0.14157753498853873; 0.01761997672478007 0.032210485786916335 -0.09229537877102477; 0.006311349495207357 0.013524721040632019 -0.04224982239875592; 0.002458715313190598 0.005790487194117301 -0.024748291304620702; 0.00012581739087401004 0.003972567498364952 -0.01615077913323886; 0.0016420736315259777 0.004034793625831686 -0.013603181578471043; -0.002990376324409726 0.002309604232283132 -0.0009332584360683838; -0.0009793136837686393 0.005941054945221431 -0.002807361799428101; 0.006267769432975949 -0.003751618864453976 -0.0008757042943138855; 0.00026563351332591886 -0.0018424081128784037 0.005928511370205582; -0.00042443186778608655 -0.00027934029600825295 0.003306453432483122; 0.008101811421047964 0.003940358554847983 -0.001185278960612201; -0.005876150121139102 0.0022179535239957265 0.0051416002225868115; -0.0026610854197260895 0.0032646464651408325 -0.008900897023989357; -0.0010095213148172675 -0.009140422454741856 0.010754390937398805; -0.003027228841878241 0.0021111075148996508 0.010575964208361937] %
+
+Mass Used: 102.04671760855717 kg
+Launch C3: 94.68720760407827 km²/s²
+||V∞_in||: 0.007275260881091619 km/s
diff --git a/archive/ES_0.5609066431708594 b/archive/ES_0.5609066431708594
new file mode 100644
index 0000000..dc7c1f4
--- /dev/null
+++ b/archive/ES_0.5609066431708594
@@ -0,0 +1,22 @@
+archive/ES_0.5609066431708594---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T17:47:33.366
+Launch V∞: [7.512417032064546, -5.595008123423014, 0.283181838139495] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00010299993193037878, 7.189047156276608e-5, 0.004848683342024516] km/s
+ V∞_out: [-0.00452740593162754, -0.00153911069687329, 0.0007814085037352958] km/s
+ time of flight: 1.8749577787447062e8 seconds
+ arrival date: 2030-04-18T19:57:10.366
+ thrust profile: [0.9653305426486692 0.016507665199558 -0.20903905262805425; 0.2308036051679776 0.15342829025607965 -0.1950840765289312; 0.05048966542559865 0.05584654294890476 -0.08785606866317974; 0.03759798244089454 0.05738225801460802 -0.09993043050123367; 0.018744544713652375 0.036600685055476395 -0.07069598688921384; 0.02093596996538955 0.051334063827302136 -0.10445231614485016; 0.004192679108688182 0.012830981355672552 -0.02938411931250297; 0.007494118757484614 0.027092070420728972 -0.06316807694958133; 0.000491888625740943 0.0022055482572191907 -0.006145456665923669; 0.0006476044236562575 0.002599550718169636 -0.008060584297894859; 0.00019148244658009949 0.0005971347198971304 -0.0023811901423271315; 0.0002454399426623498 0.0004117889062253263 -0.0013406836205792257; 0.0004935577507986337 -0.0003962489847360274 -0.0017754123939094535; 0.0004799536161404958 0.0016298996699138815 -0.0028581485199562417; -0.0004886125874412233 3.529858983441838e-5 0.0003008191799468837; 0.00045979054550417825 0.00180397757921306 -0.0003324832074279939; 0.0005562315408117785 -0.0013703270143164438 7.930800968817056e-5; -4.1256187173042296e-5 0.000965540215937577 0.00100623778298531; -0.003694115339741527 -0.004894669735587797 0.0022535653225893124; -0.00015148509787337504 -0.0021540194355450125 5.148862917713978e-5] %
+
+Mass Used: 142.10356484273143 kg
+Launch C3: 87.82071751827506 km²/s²
+||V∞_in||: 0.004850310028967757 km/s
diff --git a/archive/ES_0.560918479652911 b/archive/ES_0.560918479652911
new file mode 100644
index 0000000..282a577
--- /dev/null
+++ b/archive/ES_0.560918479652911
@@ -0,0 +1,22 @@
+archive/ES_0.560918479652911---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T13:50:54.886
+Launch V∞: [7.723696218997763, -6.059547961965199, -0.17311050756556165] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.379863133253021e-6, -1.3587597436616452e-5, -3.776132636481566e-5] km/s
+ V∞_out: [-3.7208206644535746e-5, -4.439860758155949e-6, 1.5356147631161636e-5] km/s
+ time of flight: 1.820766044354834e8 seconds
+ arrival date: 2030-02-19T22:40:58.886
+ thrust profile: [0.311354553959053 -0.007866414599258029 -0.10145826310508095; 0.10892333614861269 0.058780239245694546 -0.11520836103164889; 0.045002724319959615 0.042246697432453545 -0.08620266921501388; 0.06411568389900382 0.08655402485255229 -0.19878486340468363; 0.021048226198870704 0.0342988687797825 -0.08423415026256441; 0.013019809816506462 0.023658902794228765 -0.0650434276126879; 0.008677522270633096 0.017626629082937797 -0.05584898607262335; 0.011495090601012734 0.029560588690180495 -0.08336275360539463; 0.005332863290249275 0.00855072729041276 -0.030053837160310515; 0.003367545982565368 0.013228009243399202 -0.04043482369620558; 0.0002575769557353778 -0.0035792846921616486 -0.005136323056083209; 0.0008045978560130866 0.001798157871465397 -0.001936979022669648; 0.0009842561151925415 -0.0026255646247989204 -0.004893562789053946; -0.00513679811861602 0.0015783611326148847 -0.000606464578522958; 0.000667106366019764 -0.001270217139149302 0.0036894378530976726; -0.0018275792956512237 0.004804148050569332 -0.0012593832209836886; 0.0012682975208121788 0.0027741433052738693 -0.001507959560177415; 0.0038060397581488915 -0.006080229561450157 -0.004260443822726475; -0.0024178320095543247 0.0024263323345418693 -0.0053723296288272085; -0.0022205575163046277 -0.0004587231358808503 0.006492768461862649] %
+
+Mass Used: 92.05072272687448 kg
+Launch C3: 96.40357203454656 km²/s²
+||V∞_in||: 4.049053593448972e-5 km/s
diff --git a/archive/ES_0.5609188880343434 b/archive/ES_0.5609188880343434
new file mode 100644
index 0000000..381f5f2
--- /dev/null
+++ b/archive/ES_0.5609188880343434
@@ -0,0 +1,22 @@
+archive/ES_0.5609188880343434---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T06:17:55.485
+Launch V∞: [7.687726524227514, -5.711823911425465, 0.2188409501594542] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.536547920497277e-7, -5.501943755828381e-6, 0.00011361940154799535] km/s
+ V∞_out: [6.049514618534085e-6, -0.00011438281732601881, 1.3521068242024948e-6] km/s
+ time of flight: 1.8749577780585393e8 seconds
+ arrival date: 2030-04-21T08:27:32.485
+ thrust profile: [0.6712949080510628 0.0242532114511065 -0.15587884623765028; 0.11161690679535273 0.07616357146418055 -0.10614532622385783; 0.05537002725576984 0.06040045979330157 -0.09733799087277122; 0.027064741806914046 0.03992043424541252 -0.07305581077146703; 0.07048877163476701 0.12151971303140795 -0.21423872011909326; 0.01698406709659713 0.04163734645929678 -0.08720385970731138; 0.003903029394189079 0.013751104668634107 -0.030346401163139386; 0.0027756928910192633 0.00997612013078907 -0.023068202699989312; 0.0018530132347337365 0.004543737675134656 -0.011223910362683465; 0.002754240670420634 0.0012008973486901723 -0.002710209100425643; 0.002722542672876663 0.007047904408011814 -0.018958739412096796; -0.0013991015973625273 0.0016265150822882975 -0.0024439445128408392; -0.0019710571950654907 0.000707615962461744 -0.0034396849676733526; 0.005123766809614192 0.005300944465653255 0.0015217302926373573; 0.011885453043664326 0.0038748008149534718 -0.0018196235861612322; -0.00966085009750308 -0.004638742661924473 -0.0012240651293595466; 0.000962336888113158 -0.012699819509955666 -0.00837009550746316; -0.0028449631741826716 0.003379644607138719 0.000913635990728709; 0.0031503098726320426 0.006574614725903263 -0.003812246382835402; 0.00027227098276816954 0.002428522618756526 3.202806294072343e-5] %
+
+Mass Used: 119.05725264392777 kg
+Launch C3: 91.77396286790965 km²/s²
+||V∞_in||: 0.0001137550341249234 km/s
diff --git a/archive/ES_0.5609203029886916 b/archive/ES_0.5609203029886916
new file mode 100644
index 0000000..edde28e
--- /dev/null
+++ b/archive/ES_0.5609203029886916
@@ -0,0 +1,22 @@
+archive/ES_0.5609203029886916---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T18:37:53.376
+Launch V∞: [8.245736520954294, -5.535834027237761, 0.3488872737079204] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7764188758842281e-7, 1.1075367743652694e-6, -2.672810444827693e-5] km/s
+ V∞_out: [-3.2159577296369163e-6, 2.6540393633199458e-5, -3.2658194015875843e-7] km/s
+ time of flight: 1.8519900936264795e8 seconds
+ arrival date: 2030-03-29T06:48:02.376
+ thrust profile: [0.2845344378589719 -0.09022676202443282 -0.12471390151070887; 0.021797190381411813 0.0013221254733468764 -0.033296509126960284; 0.01576052190631502 -0.0012131732472497646 -0.046271443802678246; 0.02341772008618174 -0.007010502966442249 -0.09546330488001195; 0.029010371198511773 -0.013932183003397854 -0.14251674262485808; 0.022515859590458365 -0.012828073362709956 -0.12357337488296155; 0.01977634149520766 -0.012422689915795006 -0.11754606293105616; 0.012484411586394158 -0.0076455633248900656 -0.07720437901318448; 0.006236704143860163 -0.0034246290541526106 -0.03919903557669422; 0.0019205251737865578 0.0017089149826678058 -0.005944729986257445; -4.3639312071254194e-5 0.00043357476959866577 -0.0017162722969883814; 0.0014970439109932734 -0.0005372028850054038 -0.002230300213744207; -0.0005841653183019588 0.00013149955968928774 -0.0023328327667457337; 0.00014649952468044234 -0.00023862992033460423 -0.0010753847824058627; -0.0004939282174850165 -0.0027421303378811317 -0.0011793547289693802; -0.0006802385133753476 -0.001715463612475723 0.0016056380184219965; -0.003452722966729563 -0.003017402460567966 0.002112559267365016; -0.0021224374299200453 -0.0073786116690116275 -0.0026251801085191676; -0.001207429419171608 0.0005507481821830358 0.0045792914118976645; -0.001292904676287655 0.0016299141209683518 0.0015923724308080202] %
+
+Mass Used: 78.3108031875172 kg
+Launch C3: 98.7593514798782 km²/s²
+||V∞_in||: 2.6751631010927136e-5 km/s
diff --git a/archive/ES_0.5609371364465403 b/archive/ES_0.5609371364465403
new file mode 100644
index 0000000..6fc66e7
--- /dev/null
+++ b/archive/ES_0.5609371364465403
@@ -0,0 +1,22 @@
+archive/ES_0.5609371364465403---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:04:10.891
+Launch V∞: [7.970885675126989, -5.693812895027635, 0.1488916349018422] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.836264451049388e-5, 4.135207625936406e-5, 0.0028577832889405755] km/s
+ V∞_out: [-0.0025769442387426934, -0.0008180349233863982, 0.0009244141407076424] km/s
+ time of flight: 1.8749577787488887e8 seconds
+ arrival date: 2030-04-22T21:13:47.891
+ thrust profile: [0.35538268225288183 0.014826872309548456 -0.09794527919728098; 0.08468231785930952 0.05556277268392417 -0.09588237728345811; 0.054401528663957616 0.05883222854571767 -0.11091327460423839; 0.037873682690353495 0.05523610016887103 -0.11910268708213739; 0.026631487113041325 0.04779605125495594 -0.11404191876847909; 0.015264091680532974 0.03087745369127412 -0.08079146026377712; 0.009174498865021804 0.022455188833346018 -0.06460372965907381; 0.003706403707510062 0.01285283095120517 -0.038275423251318844; -0.00015756271088317636 0.007289894313745314 -0.015069849081682199; 0.00188415132871318 0.0015618650312070144 -0.00529741608025354; 0.0005777275068013888 -0.0019413645298701696 -0.0005683236781681726; 0.005943650644219704 0.016481889502649564 -0.03159739379250419; 0.00041647611224613783 -0.0010634181617428127 -0.0038893451681204865; -0.014009900926239327 0.004152130546855514 -0.0142198287381576; -0.008091252432531192 0.0040216464556205155 -0.010210408953730725; -0.00566552033964929 -0.0012569025568953094 -0.006431674357561777; 0.006210204013141882 0.003660649184479058 -0.013556136382106787; -0.007613409511142745 -0.0003147448788340992 -0.022712461476801588; 0.002626863759244574 0.00041896635930458554 -0.003172058170553801; 9.337622735483043e-5 -0.0066516357320525596 -0.007266280358813127] %
+
+Mass Used: 94.56261990488065 kg
+Launch C3: 95.97669244847137 km²/s²
+||V∞_in||: 0.002858678281834672 km/s
diff --git a/archive/ES_0.5609548029065529 b/archive/ES_0.5609548029065529
new file mode 100644
index 0000000..b95a03c
--- /dev/null
+++ b/archive/ES_0.5609548029065529
@@ -0,0 +1,22 @@
+archive/ES_0.5609548029065529---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T17:47:34.143
+Launch V∞: [7.857046133459666, -5.6230265899823655, -0.06180998845358579] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1873330046818177e-8, 1.002613187004485e-7, -1.9514216097901512e-8] km/s
+ V∞_out: [1.563699846951459e-8, -5.690481224240065e-8, -8.073741697988112e-8] km/s
+ time of flight: 1.8614493357983667e8 seconds
+ arrival date: 2030-04-04T04:43:07.143
+ thrust profile: [0.507777436957459 0.005892776512183744 -0.1368545870989423; 0.14814503431068032 0.09484736142446346 -0.13969775589662123; 0.08467667269268098 0.09075054373374176 -0.14791944922411968; 0.0686293786197485 0.10085731630685102 -0.18076358400541678; 0.014179713699421946 0.02673501173884335 -0.05385259583537429; 0.015510640731106749 0.035332498235998655 -0.07687821974953674; 0.007851775447301982 0.022320573697568052 -0.05143015450386647; 0.0010876072293413285 0.0035894367195267746 -0.00977781135787732; 0.002926825436201759 0.008836670033846849 -0.026599402716448138; 0.0015079018394588924 0.006050801169336787 -0.01807494439736619; 0.0002676489113698013 0.0010623649159711402 -0.005730540723343575; 0.0007607724564897879 0.00039696133311009933 -0.0064651418037270664; 0.002014792577262081 0.0014428826827351277 0.00032435986322012144; -0.0023959940178643665 0.0022626545379514874 -0.007450107046343719; 0.00012891547112201928 0.0005135541394141675 -0.0028593307969500695; 0.002057177101954578 0.005357652671521303 -0.015936747266979974; 0.0009481363782086218 -0.00045011979313860223 -0.0009023501019640705; -0.0008672484775304563 0.002403070197281462 -0.004712351798629992; -0.00016355142894461882 -0.005008021894263226 0.005581369498658078; 0.000833667869378418 0.0002879412212884935 0.0010256311360664302] %
+
+Mass Used: 109.87397243477517 kg
+Launch C3: 93.35542244963483 km²/s²
+||V∞_in||: 1.0283050434510752e-7 km/s
diff --git a/archive/ES_0.5609671394506508 b/archive/ES_0.5609671394506508
new file mode 100644
index 0000000..6012b71
--- /dev/null
+++ b/archive/ES_0.5609671394506508
@@ -0,0 +1,22 @@
+archive/ES_0.5609671394506508---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T01:05:55.274
+Launch V∞: [7.7075730480583164, -5.613914414744297, 0.2797042904043993] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.5279985624118265e-6, 5.625702471652119e-6, -3.5508828999594127e-6] km/s
+ V∞_out: [1.2237537303421311e-6, 8.547047945969755e-6, -4.292029186839454e-7] km/s
+ time of flight: 1.8568456623036322e8 seconds
+ arrival date: 2030-03-30T04:08:41.274
+ thrust profile: [0.8257399106657709 -0.023829202585305864 -0.19312211136464813; 0.058188061394524766 0.038092614486410464 -0.06001080333638526; 0.04782091577839875 0.052296078318446876 -0.08905677990316814; 0.030332330461748498 0.04478289866490333 -0.08636185199768409; 0.017459569683060196 0.030637199757775214 -0.06743967524754155; 0.010457237115960761 0.024622730892364504 -0.05942312006958133; 0.014310085103007266 0.03930167819685842 -0.09359755773850849; 0.01631453092797641 0.05664978781470976 -0.1337842688378566; 0.005041668217484328 0.01631505483921272 -0.04236165034045815; 0.00024220735599328697 0.0019503000242272774 -0.0036798590896016557; 0.0005555973444073679 0.0071470468973989405 -0.019253650998614584; 0.0003636844815633804 0.002078692467835518 -0.007376440361292961; 0.002808187828881176 0.000604441953045554 -0.004448964419864113; -0.0004773448111396665 0.0011750525964607092 -0.004304339349528079; 0.003408816325844875 0.0015451908857575854 -0.004229581208956345; -0.005130117155690463 0.004416401008964584 0.0020453547510787097; 0.005434886090697567 -0.003507428573269504 -0.0027680031567981836; -0.0004866034538778827 0.00839164326239881 -0.0038363421794644524; -0.0003786086603123754 0.005558277525414507 -0.0066158340099227945; -0.00011328145026346498 5.113650402615417e-5 0.0005652883850017654] %
+
+Mass Used: 123.62277697484615 kg
+Launch C3: 91.0009518372994 km²/s²
+||V∞_in||: 8.649628071472446e-6 km/s
diff --git a/archive/ES_0.5609704635329639 b/archive/ES_0.5609704635329639
new file mode 100644
index 0000000..e7a3ea2
--- /dev/null
+++ b/archive/ES_0.5609704635329639
@@ -0,0 +1,22 @@
+archive/ES_0.5609704635329639---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:05:49.577
+Launch V∞: [7.847332030864472, -5.676006188358551, 0.29734210498670927] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.576340581934769e-9, -1.5116333373254991e-9, -1.4571683796496264e-9] km/s
+ V∞_out: [-2.9324482941493554e-10, 1.3250585155583314e-10, -5.072531418244643e-11] km/s
+ time of flight: 1.848419133650943e8 seconds
+ arrival date: 2030-03-21T09:04:22.577
+ thrust profile: [0.5427569360713562 -0.009322971380365409 -0.15482932274503694; 0.0672684587743577 0.03772050214278905 -0.07070572532546508; 0.08107295119658621 0.07429259664446716 -0.1501952373754978; 0.05003258306907654 0.06005775299791076 -0.13880132845419077; 0.02751680290209932 0.04084793936850476 -0.10416503331144131; 0.021335978979530407 0.037340833614257496 -0.10311146488738747; 0.008174368266967763 0.017177980497674016 -0.05044535377258048; 0.0019675128385022453 0.006737539772183497 -0.021230498077659008; -0.002362426343116345 -0.0012473753163105305 -0.012042214236481406; 0.006249393753298086 0.0032741210247851766 -0.00487218468467447; 0.0011942776189222998 0.002273899258636766 -0.008043733099117371; 0.0016518413620876004 0.00974531432502299 -0.005194701475186904; 0.0032300625027835866 -0.0006471307612196926 -0.0011792716624805044; -0.0021345419869139683 -0.0020509963764148184 -0.0018306041538730515; 0.0024678066150368573 0.005420052993470379 -0.013817986129902454; -0.0002651805473985675 -0.006148768105679081 -0.024662189841351292; 0.013135044523253847 0.004806923083398626 -0.019651021878877985; 0.0010620542195314882 0.0004690116425213149 -0.002212628785866913; 0.004538210006575685 -0.005183758721957293 -0.002317752657557565; -0.001140281174935501 -0.004706056524975348 -0.01028541146553277] %
+
+Mass Used: 106.79674906995933 kg
+Launch C3: 93.88607858031402 km²/s²
+||V∞_in||: 2.625495127289135e-9 km/s
diff --git a/archive/ES_0.5609747990118304 b/archive/ES_0.5609747990118304
new file mode 100644
index 0000000..eb5debf
--- /dev/null
+++ b/archive/ES_0.5609747990118304
@@ -0,0 +1,22 @@
+archive/ES_0.5609747990118304---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:57:56.612
+Launch V∞: [6.405474755176122, -7.3900240973677365, 0.06380150742647996] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.845477174913946e-6, 1.1595633238974296e-6, -2.53958525884217e-8] km/s
+ V∞_out: [-1.7215228302243153e-6, 3.8729325339638874e-8, 8.733327905166755e-6] km/s
+ time of flight: 1.8749577788724747e8 seconds
+ arrival date: 2029-04-08T22:07:33.612
+ thrust profile: [0.3532736189291979 -0.07957696996168889 -0.11573193739758812; 0.0739878629979336 0.02295380224798903 -0.07498400660525116; 0.09168090432856428 0.05432801353413295 -0.15285608888607036; 0.08574086950319204 0.06910585053670845 -0.19999338233636935; 0.0400414422201257 0.03875100333070956 -0.12229237709629778; 0.03258259202158226 0.03713578481743383 -0.12353513268560726; 0.012417336611257972 0.01556828980981476 -0.057033084437855104; 0.0025701620442923167 0.003718201910167825 -0.01419424338655812; 0.004068375950339169 0.006413323665496442 -0.025558683158119714; 0.0010610872645670296 0.0018118064020934408 -0.0073979852498836755; 0.0007915074644420847 0.0014371710977416085 -0.006142894293848515; 0.00011693650669376116 0.00022769271601352848 -0.0003328552699521106; 2.4353713923558043e-5 0.00010628016125793987 -0.0005927137301198118; 0.0001354521898069056 0.00010303580217391736 -0.00039219057300311604; 0.00016523814905179804 -0.00016691610666035386 -0.0002590759639041915; 0.0001266361254982333 0.00015828576308795974 -0.0006156867198432335; 0.00023176672580329702 -5.9645489892740295e-6 7.850577957903819e-5; 0.0010552143660857304 0.0008665606653972042 -0.00030929641961722186; -0.0006290351415415637 -8.118343507894017e-5 0.0010639985232273105; -0.0009023532414626753 -5.706217596898628e-5 0.0012658257422519792] %
+
+Mass Used: 96.5319026649936 kg
+Launch C3: 95.64663363122433 km²/s²
+||V∞_in||: 8.921193782413896e-6 km/s
diff --git a/archive/ES_0.5609781308310098 b/archive/ES_0.5609781308310098
new file mode 100644
index 0000000..8a57809
--- /dev/null
+++ b/archive/ES_0.5609781308310098
@@ -0,0 +1,22 @@
+archive/ES_0.5609781308310098---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T13:34:42.558
+Launch V∞: [7.839362975360478, -5.727752365110895, 0.30337478740804874] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.79855331682481e-6, -2.8474281808304992e-5, -8.12201651934151e-5] km/s
+ V∞_out: [-7.850569215485003e-5, -9.119621666143978e-6, 3.461204363246925e-5] km/s
+ time of flight: 1.8749577787303102e8 seconds
+ arrival date: 2030-04-21T15:44:19.558
+ thrust profile: [0.37643395601080826 0.014607017315100753 -0.09279851953763135; 0.2158424792379076 0.14542674195378147 -0.18273817502444029; 0.06943020914107115 0.07573103725121244 -0.11553437004649683; 0.03705146389670356 0.057545730747055476 -0.09950061369208725; 0.014976091479994668 0.028129390339837794 -0.055066819809049976; 0.01717863402996447 0.04214247646018349 -0.08733990655381564; 0.005570845268910926 0.017313719712722164 -0.03962133438213712; 0.00624961840675544 0.020645197156378674 -0.0496277716295866; 0.005837952714882869 0.023061101351993754 -0.05797324926384226; 0.003812885988973502 0.009562303288741554 -0.022243381775182154; 0.0008989463212325538 0.0017386259462444447 -0.002673874034110103; 0.002075308245718376 0.0012318773722096409 -0.006019405283142544; 0.0007193344100509176 0.0015377862593359203 -0.0060312571474007435; -0.0014447356211157445 0.0030535613516519365 0.0033993128661457587; 0.0018655349334158497 0.00214620977109605 -0.005732053535312424; -0.0006748794980476066 0.0006783543344697165 -0.0004066378291263349; -0.0003688631622710774 5.4248912352907266e-5 -0.003475258388410599; -0.004188644695120731 0.0066470760882842905 0.008145663593302495; 8.604889218298464e-5 0.006253783466331069 -0.002497767862296234; -0.004567768029588918 -0.013725612980685422 -0.006250131601069309] %
+
+Mass Used: 104.07151351963876 kg
+Launch C3: 94.35479527712101 km²/s²
+||V∞_in||: 8.651540035747055e-5 km/s
diff --git a/archive/ES_0.5609797840873102 b/archive/ES_0.5609797840873102
new file mode 100644
index 0000000..71ea518
--- /dev/null
+++ b/archive/ES_0.5609797840873102
@@ -0,0 +1,22 @@
+archive/ES_0.5609797840873102---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T09:58:08.376
+Launch V∞: [6.72661061934486, -7.35067406592036, 0.21350086954160785] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.971620674617177e-7, 5.020538426544748e-6, -2.9918139379942666e-7] km/s
+ V∞_out: [1.8246254894902827e-6, -4.138842078326719e-6, 2.312732094458332e-6] km/s
+ time of flight: 1.8749577787482584e8 seconds
+ arrival date: 2029-04-09T12:07:45.376
+ thrust profile: [0.11333045965936353 -0.028509230546927895 -0.042134643190145565; 0.036199162531555015 0.009754848875968615 -0.04203969637909838; 0.06351212930017365 0.0324590792465889 -0.11859745289069228; 0.06267461884183001 0.04325803328519412 -0.1622609572708251; 0.050504061695481925 0.04141807634294482 -0.1670100092517844; 0.0245660773054297 0.022922172981296677 -0.10213803798911684; 0.013993159631296721 0.014930674050424341 -0.07069065111197509; 0.011913802587013985 0.012338673648136643 -0.06139476630862729; 0.007242120051228139 0.009354245005740591 -0.04855618054949354; 0.0026736280443165005 0.00346987224424503 -0.019451236639616395; 0.0005922591186080129 0.0007732528312563678 -0.004566701325284932; 0.0006749463041344435 0.0009140931663192054 -0.005554048650517448; -9.069647277049699e-6 0.00018837348633583438 -0.0002919546578439595; 0.00012872102379120568 -2.8395359922882827e-5 -0.0006122560430978535; 5.09288201973876e-5 6.034017007999868e-5 -0.0002341275174972736; 6.305593933352409e-5 7.803904750101627e-5 -0.0001432791057571648; 0.00046320448105812177 -6.999959014145877e-6 1.6155939316238354e-5; -0.00010231603481971389 4.947394644400297e-5 -0.00033256078510191195; -0.00045017403632459607 -0.00018181350353889414 0.00014215581806676617; 0.00012566632977409922 0.00024243821304283542 -3.54262015218975e-5] %
+
+Mass Used: 75.0789348661906 kg
+Launch C3: 99.32528226897223 km²/s²
+||V∞_in||: 5.077533904083328e-6 km/s
diff --git a/archive/ES_0.5609899984989183 b/archive/ES_0.5609899984989183
new file mode 100644
index 0000000..8417e8f
--- /dev/null
+++ b/archive/ES_0.5609899984989183
@@ -0,0 +1,22 @@
+archive/ES_0.5609899984989183---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T01:44:35.698
+Launch V∞: [6.608844678565036, -7.403816546282876, 0.11973014581868334] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.2806833282695344e-8, 6.718103548187066e-8, 4.621946168306628e-8] km/s
+ V∞_out: [-2.254222476570193e-8, 4.9526258995618804e-8, -7.437345998173085e-8] km/s
+ time of flight: 1.8749577787493962e8 seconds
+ arrival date: 2029-04-10T03:54:12.698
+ thrust profile: [0.15689523784499304 -0.0417770131959493 -0.05786179096009741; 0.061030925221712905 0.014867180452599016 -0.06827677911120629; 0.0727844342324335 0.03442047339462571 -0.1360434555634558; 0.06361819550152391 0.040004891522761196 -0.1663662012306975; 0.04809155289389082 0.036175004616244094 -0.16132594269167863; 0.029701788647169484 0.02555467667365533 -0.12181531377885903; 0.012623114140236725 0.011741651662764477 -0.06195035354666626; 0.006133808611304652 0.00620740210643768 -0.03496410835439696; 0.001858364972576621 0.0020255231146364505 -0.011779224806376706; 0.005221379142393782 0.004489940706102881 -0.03173075250518316; 0.0009883413535638553 0.0014308231751944428 -0.008240371949255455; 0.00022006039381131698 0.0004894925774721267 -9.914577050029299e-5; 9.685764561988145e-5 -0.000360761617330505 -0.0006782453971228554; 0.0006713834117794484 -0.0004377010967662465 -0.0014663919604776506; 0.0007033113561662618 0.0004399244103978076 -0.0006570694933378726; -0.0016217515162340042 0.0005501991718333374 -0.00040251673416549024; 0.000695373673181766 0.0001287640283618082 5.828984326857194e-5; 0.00065526509438711 -0.0015985980859482161 0.00042475533459243695; 0.00017015416088582988 0.00015825622154067595 -0.0009314611295490097; -0.00041423990181681936 -0.0008339332544224036 0.0006895889418884358] %
+
+Mass Used: 79.86029890741247 kg
+Launch C3: 98.50766274422725 km²/s²
+||V∞_in||: 9.209753059871514e-8 km/s
diff --git a/archive/ES_0.5609969845183885 b/archive/ES_0.5609969845183885
new file mode 100644
index 0000000..9015fc1
--- /dev/null
+++ b/archive/ES_0.5609969845183885
@@ -0,0 +1,22 @@
+archive/ES_0.5609969845183885---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:29:53.124
+Launch V∞: [8.064790315924254, -5.682898255274521, 0.22356443736155024] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4102226916453895e-10, -8.471646081035525e-10, 4.140360832005251e-9] km/s
+ V∞_out: [1.0629466834255142e-9, -3.748802769330215e-9, 5.638125230062341e-10] km/s
+ time of flight: 1.8543552998377004e8 seconds
+ arrival date: 2030-03-30T01:22:02.124
+ thrust profile: [0.2649617719253558 -0.00537307416033548 -0.09097329326710436; 0.09815241439283602 0.05300482874769117 -0.1200153585332395; 0.027786467724474736 0.02299580292908589 -0.06297057812280454; 0.03920392055565557 0.044979294365258 -0.13394149376368758; 0.020309750834962177 0.02697106920798448 -0.09130317724269929; 0.010768630696471852 0.015136932485292225 -0.05960720460471883; 0.009503736759949458 0.016958028784741824 -0.06973803128605943; 0.011636787264411431 0.02278281509384117 -0.10057420849448018; 0.004702227829315759 0.00800457553555968 -0.039850582459083836; 0.0037918161791822558 0.004424797558776003 -0.01999162392227058; 0.002630502098729577 0.004120157921062742 -0.022890674387720966; 0.0018023670556370811 0.0002692502629023487 -0.012525751767174603; -9.61451857151446e-5 0.0007441848684636356 -0.002212317223663843; -0.006131467566233344 0.003925418084816211 -0.001860532864188442; -0.0010342064469276548 0.0006585393140018199 -0.0045271423509858424; 0.0016045874590636178 0.001981636060547203 -0.0009003284403654556; 0.007526409923189323 0.005700443544752042 0.003547156936394764; 0.0015861246635577465 0.00783575198496869 0.0030540109285692634; 0.0024307653867055657 0.00892531014224168 0.0011693634155402295; 0.012314641975450154 -0.00962135565598985 0.023285360416798274] %
+
+Mass Used: 86.41056915398303 kg
+Launch C3: 97.38615647728062 km²/s²
+||V∞_in||: 4.22849417320478e-9 km/s
diff --git a/archive/ES_0.5610189608962259 b/archive/ES_0.5610189608962259
new file mode 100644
index 0000000..cf0abc2
--- /dev/null
+++ b/archive/ES_0.5610189608962259
@@ -0,0 +1,22 @@
+archive/ES_0.5610189608962259---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T19:29:41.270
+Launch V∞: [7.5025877382927595, -5.817631518651463, 0.1477053308359528] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.030558109286659044, -0.18780295000823027, -0.20263578755818076] km/s
+ V∞_out: [0.049426099988884226, -0.04157971090700031, 0.26979042224464655] km/s
+ time of flight: 1.8503054618885458e8 seconds
+ arrival date: 2030-03-22T08:52:07.270
+ thrust profile: [0.7196389760797386 0.00036305949120331445 -0.15031513827721185; 0.20185838097433456 0.1320098630038782 -0.1644541157549628; 0.08077329017530754 0.08595169991101846 -0.12329622580320679; 0.06835635884696437 0.10036375142141492 -0.15789056388380676; 0.022230154303430734 0.04245317599766419 -0.07542131053398442; 0.018378114575228997 0.04361257478040304 -0.07849485299780821; 0.006120002792913877 0.02010665975967696 -0.04125861387664869; 0.0028424751346771983 0.010828567586298753 -0.021961578070419183; 0.0026165250764375357 0.009959464046373991 -0.024611605873353874; 0.0022208069747995385 0.012860169044456778 -0.030803456683569208; 0.0002810008380681692 0.0009970903127996895 -0.002257574991851635; 0.0003123675022114914 0.0011208103466627398 -0.0028884737000716395; 0.00022806824013773148 0.00017463625013051844 -0.00027272406853457365; -0.0007063896890754161 -0.0010698348090739673 -8.137615253581663e-6; -0.0022795505700764214 0.00297489788251455 0.0013174244578366176; -0.0009755058489439736 0.006992226952848307 -0.004216407561254794; 0.00044648518906711845 0.0019860623062412336 -0.002335997660333595; -0.0024997209065373543 -0.0007480802811472304 -0.003743442834940946; 0.0024908682982581996 -0.0037104153629172972 -0.0027188645878578888; 0.0023955158907958156 -0.002648931837937238 0.002356269938937412] %
+
+Mass Used: 128.6151769985836 kg
+Launch C3: 90.15547612234515 km²/s²
+||V∞_in||: 0.27796584048097245 km/s
diff --git a/archive/ES_0.5610198298090611 b/archive/ES_0.5610198298090611
new file mode 100644
index 0000000..8cbd127
--- /dev/null
+++ b/archive/ES_0.5610198298090611
@@ -0,0 +1,22 @@
+archive/ES_0.5610198298090611---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T10:17:30.462
+Launch V∞: [7.9168327161524275, -5.547347046806188, 0.2372102733708973] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3276585611682197e-9, -2.024357919033174e-9, -1.889672152668861e-9] km/s
+ V∞_out: [-7.355977542185897e-10, 6.846381351651918e-10, -2.5498215533339976e-10] km/s
+ time of flight: 1.8749577787301365e8 seconds
+ arrival date: 2030-04-20T12:27:07.462
+ thrust profile: [0.5277638235305323 0.0025263775872495318 -0.1378158132122663; 0.18300575660282156 0.11428176147763712 -0.17386695468059213; 0.03402820763139337 0.03549095637737396 -0.06432675855692317; 0.02987339938426268 0.04209617855169702 -0.08508477662740818; 0.022329010422685844 0.03973704921347807 -0.08812822077966712; 0.016407259419088566 0.035490936021032864 -0.08363340388035144; 0.016499919675498572 0.04112786269323465 -0.10531098439774535; 0.0024461652490467426 0.006684555910208611 -0.02029554344083188; 0.003613616380598044 0.013326835465910314 -0.038378835174712404; -0.0011740902407687288 0.0025195753738280627 -0.0025325861969394585; 0.001223223199149508 0.0026702574531221853 -0.011991336946991858; -0.0026428993661798354 -0.004772048963880886 -0.008462937207805632; 0.0007198714141308481 0.001327132499976673 -0.008024643006454633; -0.004488156806914532 0.001385340050016698 -0.005838085581802094; -7.75058499088029e-5 0.0012310000975930238 -0.005888046262871084; 0.0002471442483429594 0.004426438574638083 -0.001837201922497918; 0.0026312510787977073 0.011602451810351406 -0.0036326500504362536; 0.007739079959725841 -0.0037600204910572367 -0.0075007841020336315; 0.0020739803776552474 0.004922519135838445 -0.005145088935087508; -0.003870754609853252 -0.004455450148300581 0.000258356648308743] %
+
+Mass Used: 109.07398678615118 kg
+Launch C3: 93.50556822704344 km²/s²
+||V∞_in||: 3.6175793296490673e-9 km/s
diff --git a/archive/ES_0.5610289441029624 b/archive/ES_0.5610289441029624
new file mode 100644
index 0000000..e58b1de
--- /dev/null
+++ b/archive/ES_0.5610289441029624
@@ -0,0 +1,22 @@
+archive/ES_0.5610289441029624---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T23:42:11.486
+Launch V∞: [7.776658489387393, -5.724422820415517, 0.09843676765195286] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.845514325428208e-7, -3.953201889710893e-6, 7.173129214155417e-7] km/s
+ V∞_out: [-6.306417982770846e-7, 2.411090406347783e-6, 3.1904562427845982e-6] km/s
+ time of flight: 1.8749577787494323e8 seconds
+ arrival date: 2030-04-21T01:51:48.486
+ thrust profile: [0.5217759344305138 0.0295552493314181 -0.1135097300694061; 0.11383282484165111 0.08513855781756452 -0.10241262531540335; 0.06333516949950145 0.07764055822991153 -0.10007820213022274; 0.042869811915740096 0.07921059277629412 -0.1153420394762654; 0.025596209363025438 0.058015000854610414 -0.09700232934438828; 0.020391034458118316 0.05344646822451963 -0.09847231413328907; 0.015679055782356233 0.056280492580224155 -0.09566559249154344; 0.006372804692687417 0.021843026675215253 -0.04273954988910381; 0.0014498192757156836 0.006075189700101307 -0.014464344581333959; 0.0015790493628885017 0.010630603649715782 -0.02356055876359325; 0.000230449519306744 0.0023483208912882217 -0.0037063792135704765; 0.00014308420061051442 1.493849624634809e-5 -0.0006101323432710084; -0.0007778408692359254 -0.0018873127989811308 0.0011668234162644604; -0.00030678995081006346 -3.0324352157960646e-5 0.0020787309994226514; -0.0005847185479246907 0.003092233680772187 -0.004331646124250323; 0.005245858000986163 0.00563751189842168 0.0023689363805993176; 0.00016602139231445612 0.0021850756610377665 -0.00640654550031305; 0.006111435712088461 0.002095856301127914 -0.00413423556743858; 0.00042920692561966003 -0.0030719531953118185 0.001041159642425364; -0.008706014786521735 -0.005275001425138396 -0.00028241642866989967] %
+
+Mass Used: 110.54554662615192 kg
+Launch C3: 93.25512368468073 km²/s²
+||V∞_in||: 4.046867072047558e-6 km/s
diff --git a/archive/ES_0.5610307214077203 b/archive/ES_0.5610307214077203
new file mode 100644
index 0000000..360e939
--- /dev/null
+++ b/archive/ES_0.5610307214077203
@@ -0,0 +1,22 @@
+archive/ES_0.5610307214077203---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T02:43:45.533
+Launch V∞: [7.7871211646515, -5.6615586019083874, 0.2682979035676364] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.2794644690212054e-5, 0.0007559651730885059, 1.3290810823202658e-5] km/s
+ V∞_out: [0.0007281270760389515, -0.00011225654894901098, 0.00016563576485229903] km/s
+ time of flight: 1.8749577787572467e8 seconds
+ arrival date: 2030-04-22T04:53:22.533
+ thrust profile: [0.6067719651135867 0.0027535099397175346 -0.16757594423971875; 0.1569872416562115 0.09053995880114965 -0.1584743393711473; 0.03931382215891726 0.03581325968895636 -0.08118160870487034; 0.03391888303043071 0.040362354832816874 -0.10237534025262195; 0.01843598937810507 0.027392230496343678 -0.07799008696847257; 0.013476779983962735 0.02519457948349817 -0.07352236662715717; 0.01116560559066477 0.025336748801584673 -0.0782498056761686; 0.004672912601184932 0.013927554752837922 -0.038882634326514974; 0.007753094004996894 0.006247091084995344 -0.04520375694715647; -0.0002991879645167653 0.0037548087294762243 -0.01100835222208012; -0.003249004142141629 0.012529344788974184 -0.008475843050656408; 0.00021770323806862208 0.002890409923835824 -0.008797492614721198; 9.946486797398409e-5 -0.00015782845828913282 -0.0032427478812665253; 0.0004715632319048865 0.0014668848374069874 -0.004845543068111686; -0.005551429196057283 -0.0063146493321311024 0.001141216243009174; -0.0020771491336174157 -0.0010968384698475978 -0.0007991864442273423; 0.0009692336219299707 -0.009487661438656153 0.002748790509870175; 0.01159783767252593 -0.00031999465590452203 0.0030149188421218645; -0.0034395088235005854 -0.01912726615288906 0.010225081891535138; -0.0024650029614718323 -0.0008881127496810676 0.00020211222510646944] %
+
+Mass Used: 113.40967563729464 kg
+Launch C3: 92.76448560086497 km²/s²
+||V∞_in||: 0.0007567928893002564 km/s
diff --git a/archive/ES_0.5610554755992169 b/archive/ES_0.5610554755992169
new file mode 100644
index 0000000..4b00c3b
--- /dev/null
+++ b/archive/ES_0.5610554755992169
@@ -0,0 +1,22 @@
+archive/ES_0.5610554755992169---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T14:48:58.429
+Launch V∞: [7.815185331143583, -5.553206050562554, 0.14862680495161013] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0015154967058424516, 0.0008024117223634404, 2.9727333678692548e-5] km/s
+ V∞_out: [-0.0011933703338282804, -0.0007485334859462644, 0.0009691215573560789] km/s
+ time of flight: 1.8749577784600505e8 seconds
+ arrival date: 2030-04-20T16:58:35.429
+ thrust profile: [0.73185945976845 0.0037531157640370546 -0.17757755024233687; 0.06961672237581816 0.04221663493851715 -0.07071399103470717; 0.04512168797576037 0.044750295563469066 -0.08541024465951674; 0.03938627518762957 0.05167786971250915 -0.10767841067545428; 0.021948363355356267 0.03581158948146664 -0.0839958594312382; 0.006960885611411665 0.015965218373809317 -0.03996376587700251; 0.012914591656550787 0.03849036587855657 -0.09930648114188868; 0.020769387682558774 0.05792033106829796 -0.14381951345233376; 0.00046141755816530514 0.0010778912827344254 -0.00708381316890246; -0.0015901002937092415 0.008774632210740214 -0.021848231643855735; 0.0018503816565108083 -0.0002278650759646616 -0.0011281072558345024; 0.0038564381091438804 0.001572565856663671 -0.0020452799589859984; 0.005253630636680497 0.004892614709743774 -0.0038361641736634703; -0.001475120344875059 -0.0012636361886578407 0.0041540251922380575; 8.170397686288773e-5 -0.0004893148384447788 0.002344920598169937; -0.004625721240854392 0.001951680825842918 -0.0020517577732430074; 0.0036380494698949654 0.0034911961382358024 0.001844203738634911; 0.0005780948370422635 -0.0003963452699439685 -0.004699172194271562; -0.012314262677099355 -0.001185284673219816 -0.005403879622889954; -0.0006949744119967415 0.005003373375917828 0.0060758828035286025] %
+
+Mass Used: 118.26375162330669 kg
+Launch C3: 91.9373091272765 km²/s²
+||V∞_in||: 0.0017150739202650216 km/s
diff --git a/archive/ES_0.561060961310179 b/archive/ES_0.561060961310179
new file mode 100644
index 0000000..ea48f00
--- /dev/null
+++ b/archive/ES_0.561060961310179
@@ -0,0 +1,22 @@
+archive/ES_0.561060961310179---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T16:04:28.408
+Launch V∞: [7.563046071141931, -6.099813579018164, 0.0636306863563402] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.513972497503229e-6, 3.547209804544255e-5, -0.0006882247543054853] km/s
+ V∞_out: [-2.8773667354903544e-5, 0.0006881476003402243, -9.121342607930186e-6] km/s
+ time of flight: 1.7244529445276076e8 seconds
+ arrival date: 2029-10-26T13:32:42.408
+ thrust profile: [0.4409431663628527 -0.04437845274249227 -0.13699459541552603; 0.13288575693427143 0.05952501323991215 -0.13225702398148118; 0.0919901357969289 0.06977016317092463 -0.1595321270819143; 0.0505141235052251 0.04999294455827674 -0.12624070658599448; 0.05460098601237423 0.06646275284556682 -0.18003512847016617; 0.028573357411657105 0.03952498791240628 -0.11676290709300631; 0.013012348211570716 0.019701386505874847 -0.0623065642369622; 0.007051473743666633 0.011495294760998651 -0.03813687885915426; 0.005191261370733672 0.00397260635555834 -0.019514236881989767; 0.00015287475628599704 0.001147557423206032 -0.0023457584474268454; 0.0029096417907085222 0.003230683386659706 -0.015817761836793134; 0.00310604496119539 0.0025740477015254574 -0.011199913218700779; 0.0006221085365245669 0.003019757081144026 -0.00936874244479337; 0.0004236104350136856 -0.0001702927804298959 0.0007036982640935786; 0.0023360437966619 0.001288866685332549 0.0003857833649827053; -0.00024087992141638305 0.000463197118692138 -0.0004172786656073122; 0.0009078510215749418 0.002146660097779581 -0.0012231873340732271; -0.0014372372508723676 0.003457772921755106 0.0016545172049423841; 0.0002539461546544469 0.0005036236026534002 -0.0018367216547308437; -0.0020403432967595054 0.0003790824479585614 -0.001354140155075562] %
+
+Mass Used: 103.83771897799897 kg
+Launch C3: 94.41144043723597 km²/s²
+||V∞_in||: 0.0006891530730732464 km/s
diff --git a/archive/ES_0.5610683534878737 b/archive/ES_0.5610683534878737
new file mode 100644
index 0000000..bf8331e
--- /dev/null
+++ b/archive/ES_0.5610683534878737
@@ -0,0 +1,22 @@
+archive/ES_0.5610683534878737---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:33:18.344
+Launch V∞: [7.8554398754206645, -5.52030893436798, 0.241078222017215] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0015948729627688122, 0.0010561615396192194, 6.90621900943264e-5] km/s
+ V∞_out: [-0.0014064528924375942, -0.0006450212605259983, 0.0011322512810522994] km/s
+ time of flight: 1.857097332720652e8 seconds
+ arrival date: 2030-03-29T21:35:31.344
+ thrust profile: [0.7614499724818957 -0.011573455295189258 -0.20274492979831055; 0.033802402574858115 0.02322617042221718 -0.035353426965674895; 0.03333393577179894 0.0364278018688652 -0.06497811342120698; 0.03848882109174918 0.059414725571568495 -0.11309916273394947; 0.02149002842553709 0.04146637442325444 -0.08655555020050504; 0.01248860227293785 0.029382008519653034 -0.06822727450275287; 0.010014280208680539 0.03239492021320309 -0.08946899320760407; 0.009123591332101628 0.02545925885973366 -0.0744429947531303; 0.009653128166262072 0.03761927468597242 -0.10196985898549936; 0.0015736492326924177 0.006714238024975384 -0.021724414611355287; -0.00035103931099571045 -0.0022114645686075757 -0.00114460381397122; 0.0017909108082957651 0.002889686038216448 -0.009283793332561859; -0.0007934326990595658 -0.0005556568474537785 -1.6094675320293093e-5; 0.00027203776079814517 0.0006594867968220555 -0.0012161156106755503; 0.0010262140831297708 0.001527551355981254 0.0021872318588119803; -0.0025231230514824116 0.0020360211272394593 0.00049529971035293; 0.0010075538735201954 -0.004557193013313501 0.004508969861268295; 6.02555792668908e-5 0.00025712652637027266 -0.0006729876748753376; 0.0006878654524003736 0.0003603889175460292 0.002433663251666949; -0.000489587776471706 -0.0015926680219793235 0.007021260547267446] %
+
+Mass Used: 116.51386612385204 kg
+Launch C3: 92.23986507634295 km²/s²
+||V∞_in||: 0.0019141229195750293 km/s
diff --git a/archive/ES_0.5610837256729171 b/archive/ES_0.5610837256729171
new file mode 100644
index 0000000..0415d9b
--- /dev/null
+++ b/archive/ES_0.5610837256729171
@@ -0,0 +1,22 @@
+archive/ES_0.5610837256729171---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T19:58:23.044
+Launch V∞: [7.776817020259242, -5.913807589039489, -0.33429530393703666] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1528334720817864e-8, -4.436859772104286e-8, 1.441028974660011e-8] km/s
+ V∞_out: [-3.963775817280486e-10, 1.5988836003440299e-9, 2.112776848270061e-9] km/s
+ time of flight: 1.7836135127398497e8 seconds
+ arrival date: 2030-01-04T04:47:34.044
+ thrust profile: [0.33087924414286946 -0.019427811316401963 -0.10518202476776813; 0.17278610909321157 0.09027038491026028 -0.17739046934756741; 0.06299638263930314 0.05411317707106309 -0.11889013761405402; 0.03822344701331486 0.04466169064784559 -0.10660418376181634; 0.02852813531828745 0.041044298108911796 -0.10660757584969803; 0.022826473899722012 0.0394307296252714 -0.10938661862816398; 0.015642831520400514 0.03006587274517433 -0.09110428834700936; 0.008598990988143153 0.01896561182307056 -0.06122645871527598; 0.005026742264423572 0.011939813020058795 -0.04211108208667383; 0.0011327109168654701 0.004683440456571682 -0.014784525234912497; 0.0013848139560828153 0.0010615242592847034 -0.005801255396712523; 0.0001222292666299326 4.811501935600723e-5 -0.0002579296847794015; 0.0002058694781941201 -0.0001614133157029809 -0.000546991457789101; -0.00032543029027848265 0.0013978872393025509 -0.0006408742876052811; -5.985067806177531e-5 0.0002479411071574332 -0.0016887705852703264; 0.001425797803283584 -0.0026900388840765824 0.0007500892240537993; 0.0007482528745288012 -0.003743737456228249 0.0010737428796274988; -3.4678427140889996e-5 -0.0009620918208493906 0.004671181456883446; -0.0021958565080217258 0.0006174235445167742 -0.000663468947652525; -0.0028115800470384453 -0.000333941431298702 0.006952287995954155] %
+
+Mass Used: 97.14243360251612 kg
+Launch C3: 95.56375651700924 km²/s²
+||V∞_in||: 4.80534225185669e-8 km/s
diff --git a/archive/ES_0.5610938553677335 b/archive/ES_0.5610938553677335
new file mode 100644
index 0000000..187fde3
--- /dev/null
+++ b/archive/ES_0.5610938553677335
@@ -0,0 +1,22 @@
+archive/ES_0.5610938553677335---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T13:58:04.522
+Launch V∞: [7.875333530171959, -5.661497253623082, 0.0277799025589171] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0025289025241620254, 0.0013960350067601796, 0.00010369583984781887] km/s
+ V∞_out: [-0.001780074331057618, -0.001031322976456321, 0.001762072989165802] km/s
+ time of flight: 1.8481475573484582e8 seconds
+ arrival date: 2030-03-20T15:23:59.522
+ thrust profile: [0.5254479448231886 -0.004991337193622902 -0.14831080311358796; 0.07017162252567749 0.043241526747033326 -0.07524303354869323; 0.0618892846045328 0.06232970785666024 -0.11774089485818516; 0.05599662957310939 0.07544707932337094 -0.1583415689717432; 0.022700372510945473 0.03745434904743251 -0.08540153916178858; 0.013946428122551424 0.029155444392908406 -0.0720516335322199; 0.01348922893624646 0.03007734316697339 -0.08444371331793692; 0.007316455350256306 0.021232445162044332 -0.060406799446179146; 0.001056662059168653 0.002556688136082012 -0.01017010206527681; 0.0026330712611205348 0.011455101055521002 -0.041334919120461; 0.000709714871802357 3.0501786092886258e-5 -0.002127048550021143; -0.0027480487509949233 -0.0007510903019408099 -0.0015535310333492543; -0.003016440512040127 0.00662106648247596 -0.0060509600970223235; -0.0003843613185682151 -0.0006048305781936913 0.0025808076437349786; -0.004740768784555739 -0.0007628899516810359 -0.004506643102120015; 0.0038942679998221776 -0.0028376996790098717 -0.0001600703408414935; -0.002369595697381892 -0.0026635054064592534 0.004683278745637983; -0.0004525436747078936 -0.004462596940644437 0.0004999346229512956; 0.003051260954146426 -0.009301705635327331 -0.0105155621590345; -0.008940309003855841 0.0007431690532260673 0.008385768149681349] %
+
+Mass Used: 105.84332492024714 kg
+Launch C3: 94.07420108721861 km²/s²
+||V∞_in||: 0.0028905042023866187 km/s
diff --git a/archive/ES_0.5611091355624334 b/archive/ES_0.5611091355624334
new file mode 100644
index 0000000..bbc1f5b
--- /dev/null
+++ b/archive/ES_0.5611091355624334
@@ -0,0 +1,22 @@
+archive/ES_0.5611091355624334---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T17:31:30.696
+Launch V∞: [7.948632920528229, -5.464734352335939, 0.15382224081164278] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.02203636279932107, -0.141272980312589, -0.1620157081219726] km/s
+ V∞_out: [0.03535991821547132, -0.03245044034514357, 0.21070182101967702] km/s
+ time of flight: 1.8749577787347555e8 seconds
+ arrival date: 2030-04-19T19:41:07.696
+ thrust profile: [0.6437785992848165 0.0038802719520227864 -0.17356645355404815; 0.073573196796642 0.04763080653176024 -0.0777117048669988; 0.06272422616026992 0.06632961083283331 -0.12053230908098413; 0.04097832452675942 0.059452718101955467 -0.11840145209540039; 0.018701304164353613 0.03453507260853017 -0.07807691091876495; 0.00732901028850889 0.016026936203851913 -0.040800545374254135; 0.012382357643731256 0.03420598218762923 -0.0890037407033925; 0.006763563774574907 0.021828292362669068 -0.061033376511784025; 0.0070737095175843045 0.027418288880385448 -0.0791442351432284; 0.0006745866407321251 0.0025844247774297747 -0.009384426377296546; 0.0002151661505997929 0.0007580437301690796 -0.0032266906080771957; 0.0006280163199925981 0.000555268575470467 0.0013817521119168729; -0.001351569849703342 -0.000288328035044508 0.0003353047300484794; -0.0008768150175124609 -0.00012285708713509103 0.005102163681390422; -0.0029452657944013024 -0.0024379779796889624 -0.0005386714717855946; -0.0007074206478570723 -0.0008021914862653147 0.0007579003655951838; 0.0040969372736634636 0.0008314983007655677 0.00272923779958754; 0.0043358382912914 0.002694004265966512 0.0019405757723148568; -0.0030034341749939856 0.003286562857534219 -0.0032090522055722723; 0.0007974866633039168 -0.0007293543856386246 -0.0029456881610870622] %
+
+Mass Used: 111.73212740557437 kg
+Launch C3: 93.06774812867393 km²/s²
+||V∞_in||: 0.21608504328177988 km/s
diff --git a/archive/ES_0.561133318565157 b/archive/ES_0.561133318565157
new file mode 100644
index 0000000..6f55a6a
--- /dev/null
+++ b/archive/ES_0.561133318565157
@@ -0,0 +1,22 @@
+archive/ES_0.561133318565157---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T10:46:16.512
+Launch V∞: [7.79294304027814, -6.051809165732526, -0.0381347339756948] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0012689891630081726, -0.0008555708308386466, -0.05270120605765135] km/s
+ V∞_out: [0.016214725628574792, 0.043567400338081236, -0.024664995083197274] km/s
+ time of flight: 1.8016281745929152e8 seconds
+ arrival date: 2030-01-28T15:59:53.512
+ thrust profile: [0.25911144777016465 -0.01588710865151455 -0.0891480713697633; 0.07519663425988189 0.03577439335821633 -0.0836202619387748; 0.06394396949390391 0.04829973432844219 -0.12619483118487482; 0.039198093583039086 0.03752970119559871 -0.11063296844214009; 0.04883237547443791 0.056060114525041775 -0.17834247874940287; 0.02039837365292272 0.026382638535365502 -0.09293224879927842; 0.010974968620486822 0.016703048467588005 -0.06734047006789749; -0.0018171822315665013 0.0023692173136784043 -0.028965800059821377; 0.0008212943715455031 -0.0025891897140881484 -0.02603000553346069; 0.00030278400133715213 0.01158075362498648 -0.02757501268352368; -0.004415323084168577 -0.005009330087633469 -0.0178553153591067; 0.0017490878444903568 0.004740009379649925 -0.0057393333061035055; 0.00859603135581825 -0.004877698772001999 -0.009600479592324773; -0.002697296898520697 0.00363842950012961 -0.011563280588269536; 0.0005743073026597597 0.0006709992471376968 -0.011711135353717615; 0.0018087906313489087 1.6766677193932314e-5 -0.0006570551087201463; -0.0013581398780314366 0.0032948707498975504 -0.007834857618552238; 0.0017095641661689824 0.010892840298160109 0.0011529402270921973; 0.0001923186036653507 -0.0012717045119570239 0.006219942779869795; 0.000579048641230842 -8.237073062057555e-5 0.003929684724158859] %
+
+Mass Used: 86.74664861118845 kg
+Launch C3: 97.35580966539911 km²/s²
+||V∞_in||: 0.05272342415732728 km/s
diff --git a/archive/ES_0.5611471780042292 b/archive/ES_0.5611471780042292
new file mode 100644
index 0000000..c9ad5e2
--- /dev/null
+++ b/archive/ES_0.5611471780042292
@@ -0,0 +1,22 @@
+archive/ES_0.5611471780042292---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T16:29:23.594
+Launch V∞: [7.333131174582843, -6.2699527950094565, -0.25527185620033377] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00024124548625241551, -0.00018873118155079762, 0.00014420514564341273] km/s
+ V∞_out: [-5.3094414841751e-5, -0.00033340659139513296, 1.493695055739923e-5] km/s
+ time of flight: 1.71676753825712e8 seconds
+ arrival date: 2029-10-19T16:28:36.594
+ thrust profile: [0.6119364115206972 -0.07568384096768445 -0.22119007494856682; 0.11257643057111084 0.043033509377541225 -0.13314617615523344; 0.08356754827441759 0.05444895419839254 -0.17172970906732304; 0.06576161611079938 0.05571421165561471 -0.19380935531979165; 0.042854510210100547 0.04295340286090564 -0.16659458233878707; 0.0196770313704378 0.022193747072460912 -0.09675356304729368; 0.005717381313747648 0.00716810921776735 -0.03491242271166623; 0.0028414654205422166 0.004068934314551793 -0.020612420911570017; 0.002084138935811308 0.002784869325734411 -0.015633878240240612; -0.000689720793327501 0.0005073365132347814 -0.002115658241012226; 0.0005800087234767141 0.0013150113037869635 -0.0051578973072843445; -7.642764216757157e-5 -0.0007242451595548346 -0.001709203659791054; -0.00028819895310798265 -0.0001476547584136265 0.0012679426754341019; -0.0015117475679676119 -0.0008829049794022417 0.0002213194310644363; -0.0035365285546371684 -0.0001431926725058152 0.0016765949742237676; -0.0005218702337396535 -0.0007488396893150157 0.0012922997123426402; 0.00015607954019991767 -0.0006534203802004439 0.0023725681403561384; -0.00018102077801770695 7.416372328316866e-5 -0.007418124922261026; -0.0002571320077287538 -2.263221274099043e-5 -0.00135641237632686; 0.0010686988156984256 0.00027574668253350487 -0.0008406805389119083] %
+
+Mass Used: 111.28338086245458 kg
+Launch C3: 93.15228459585362 km²/s²
+||V∞_in||: 0.0003385468469159954 km/s
diff --git a/archive/ES_0.5611554412617799 b/archive/ES_0.5611554412617799
new file mode 100644
index 0000000..bc27c16
--- /dev/null
+++ b/archive/ES_0.5611554412617799
@@ -0,0 +1,22 @@
+archive/ES_0.5611554412617799---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T23:21:09.110
+Launch V∞: [7.933598533929637, -5.653636650886397, 0.08737287230938505] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3032944230104345e-6, -3.484575307991461e-6, -9.53403597066159e-6] km/s
+ V∞_out: [-9.266900616662555e-6, -1.182196436967969e-6, 4.102983873497727e-6] km/s
+ time of flight: 1.8283445493816403e8 seconds
+ arrival date: 2030-02-24T02:42:03.110
+ thrust profile: [0.4082163606714314 -0.0038897757631065643 -0.11431530777889631; 0.17878028172591112 0.10831181880329517 -0.1722820248493504; 0.051455867190345915 0.05104736877178653 -0.09475739461870769; 0.036416899414105613 0.04895877331170511 -0.10034408275454822; 0.022685103841696662 0.03804349655726385 -0.08575015069348679; 0.01402136465056794 0.028321048665098592 -0.06871337845157674; 0.011272912819588183 0.027928910361336275 -0.07165185663389582; 0.005430524493095392 0.015549353684452368 -0.04296839530446531; 0.012895243704896297 0.04257228650743716 -0.11753535231458241; 0.0009555873127769591 0.003250400578452697 -0.009686995285507007; 0.00017173528727843597 0.00033507127679171535 -0.001310901984624674; -0.0008976604340197093 0.0005040272869045071 -0.002034808521762946; 7.051400358097583e-5 0.0010651308509705484 -0.0037050908165032915; -0.0004989575636866965 0.0011158825282574136 -0.003021412290816164; 0.003400797014561552 -0.00017178170365913636 -0.0010686877425890374; 0.0014391709726851542 0.0010551759006196728 0.00011740980646422696; 0.0002462660464615221 -0.0006130322589004186 -3.8677742892982356e-5; 0.00014014661708702884 0.0011564666067145767 0.00028165868419923764; -0.002311513096362263 0.0006099774913023529 0.001386262496811313; -0.0010665768655592944 0.003243781025097263 0.0006430418710144212] %
+
+Mass Used: 101.02085674172304 kg
+Launch C3: 94.91322709663203 km²/s²
+||V∞_in||: 1.0234191874299747e-5 km/s
diff --git a/archive/ES_0.5611690023015958 b/archive/ES_0.5611690023015958
new file mode 100644
index 0000000..dcf1047
--- /dev/null
+++ b/archive/ES_0.5611690023015958
@@ -0,0 +1,22 @@
+archive/ES_0.5611690023015958---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T18:52:00.023
+Launch V∞: [7.672265854499277, -5.739820186552676, 0.2764432200348706] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.078551966322262e-6, 1.7404977386752727e-5, 4.7392349819224284e-5] km/s
+ V∞_out: [4.67581485183301e-5, 5.596148800890982e-6, -1.939504495426992e-5] km/s
+ time of flight: 1.829034947061373e8 seconds
+ arrival date: 2030-02-24T17:23:34.023
+ thrust profile: [0.6157087823226236 -0.004033020163919954 -0.15425633207782583; 0.2123400139834324 0.12939126600865886 -0.18899325610982573; 0.06106753543833527 0.061548433976710414 -0.10178649702311175; 0.040458424782430724 0.055805641466321186 -0.10179104727721705; 0.0472459758547892 0.08089448557176995 -0.15799541692570446; 0.017501808687610792 0.037474012999202465 -0.08083878259457561; 0.006396183047343296 0.016306194257957828 -0.03746672413091154; 0.0023631257029003323 0.006456123850167417 -0.01639246836506228; 0.0020862623398571456 0.005444775279543753 -0.01632207818091339; 0.000991941989696331 0.004070045105414412 -0.011358986191716124; 0.002268024909373107 0.010095064781537613 -0.026146089847334363; 0.0005629554194989071 8.503662007629535e-5 -0.00436411764850089; -0.0010430304824602232 -6.004859222584827e-5 -0.004132855041572863; -0.003061763228038783 -0.001147513673719609 0.00047557583519560387; -0.00021854214468685056 -0.0007024723165835857 0.0012516976007843979; 0.0002289168369472808 -0.0011542695731813182 -0.0003627112484934022; -9.104986706727798e-5 -0.0019037026144478407 -0.0008651593286966622; 0.0013306339635661133 -0.002934297393823357 0.005113797644345299; 6.223428194482639e-5 0.0001121191978986245 -0.004931297358642797; -0.0020396660554491703 0.006851476412024489 -0.0004183448373412666] %
+
+Mass Used: 118.69771952699966 kg
+Launch C3: 91.88561996997637 km²/s²
+||V∞_in||: 5.098111373009643e-5 km/s
diff --git a/archive/ES_0.5611788772880952 b/archive/ES_0.5611788772880952
new file mode 100644
index 0000000..7c3ada9
--- /dev/null
+++ b/archive/ES_0.5611788772880952
@@ -0,0 +1,22 @@
+archive/ES_0.5611788772880952---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:57:52.478
+Launch V∞: [7.689398437418138, -5.83268562465223, -0.03917844363715963] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.199890016222236e-9, 3.3798814523541512e-9, 1.2492248752724248e-9] km/s
+ V∞_out: [5.526704946423203e-9, -4.654243375699347e-9, 1.7390077239413549e-9] km/s
+ time of flight: 1.8749577787662956e8 seconds
+ arrival date: 2030-04-21T12:07:29.478
+ thrust profile: [0.479778141126 0.03372475410452455 -0.09966387791086746; 0.1408363387938589 0.10614539975484187 -0.11246960439188736; 0.06204071315456847 0.07891366116506549 -0.09744815880883663; 0.08506461220041169 0.13376062084727888 -0.17849794784668724; 0.022966528027036023 0.05270680218574986 -0.07907665629755266; 0.01621585116218435 0.050529572546904156 -0.0794723794340188; 0.009239255511204697 0.036285432671928526 -0.06114290490629318; 0.004632727128965724 0.01856034184502039 -0.03590625498411395; 0.004335194323239565 0.03151180857100427 -0.058529820555149444; 0.00047196145228289887 0.0025006062594050004 -0.004654864844285423; -0.00028459319147730973 0.0014951879566006312 -0.0006393989934572328; -0.0014356128921861088 0.00010853100079595747 -0.002089157622416577; -0.0036760563030311653 -0.00017072827519350338 -0.0025051640584256678; -0.0004275937219179521 -0.0008188956011382748 -0.0018892364561315742; 0.0034801547564306803 0.0021253989724335618 0.00019463387431113016; 9.107803334585751e-5 -0.0006175529931110103 0.0022523508220220374; -0.001943115879131539 -0.0023665551816662847 0.0019391429351223446; 0.006330907220952885 0.0024673437108095196 -0.0022860357345533397; 0.0015210562434074294 -0.0035921765772691868 -0.004500849043404063; 0.00046894947916855626 -0.00066611166625054 -9.797762624497435e-5] %
+
+Mass Used: 111.34182839371624 kg
+Launch C3: 93.14860487583911 km²/s²
+||V∞_in||: 6.326374759826887e-9 km/s
diff --git a/archive/ES_0.5611835773551617 b/archive/ES_0.5611835773551617
new file mode 100644
index 0000000..bb689bc
--- /dev/null
+++ b/archive/ES_0.5611835773551617
@@ -0,0 +1,22 @@
+archive/ES_0.5611835773551617---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T22:14:53.324
+Launch V∞: [7.7995499032664215, -5.653689303264736, 0.10345304195151313] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.62418473430583e-6, 2.3034403152675194e-5, -0.0005607241409405805] km/s
+ V∞_out: [-2.3370266277031184e-5, 0.0005602407146718625, -4.147195439857385e-6] km/s
+ time of flight: 1.8749577787335476e8 seconds
+ arrival date: 2030-04-20T00:24:30.324
+ thrust profile: [0.49351359112354576 0.012218700743313144 -0.1141679185243084; 0.21694604249031502 0.15157999993339577 -0.1805970199127479; 0.08995247751043525 0.10722453510235644 -0.1468822631861622; 0.029122679745164755 0.04792257894690705 -0.07823328843470914; 0.028798483313274618 0.060284756721816 -0.10232019512194707; 0.007476167753015407 0.019807864587603738 -0.03986979904453458; 0.010991279873661856 0.03752661066353654 -0.07657107137527487; 0.003412287216617859 0.013711752845460898 -0.03195036354384926; 0.0038390233789674863 0.018976569716328686 -0.04315456470237803; -0.0002555198231115317 0.004404757108480233 -0.012005553832125936; 0.001517602418862474 -0.0007926203462554284 -0.003882996849823246; -0.0007980584706246341 0.0019029689421709588 -0.006263609622538503; -0.001681402996792021 0.002145295951983749 -0.0008257468333276968; -0.004236398488606082 0.0018957821482220962 -0.00389216884341214; -0.0009327193924266187 0.00199823221777955 -0.0012568682449657304; -0.00011410299620769068 0.0048312321947637845 -0.001335013055720063; -0.00018799767101738518 -0.0003500011918830524 0.0018390396535873563; 0.0009547183919222164 0.0065816221354851896 0.004635450486496424; 0.0004381467668821937 0.0005657392415835999 -0.001168355237486221; -3.18370816302876e-6 0.0027763376833478846 -0.003908383200348184] %
+
+Mass Used: 113.3348504618748 kg
+Launch C3: 92.80788396328236 km²/s²
+||V∞_in||: 0.0005612087674628225 km/s
diff --git a/archive/ES_0.5612030297404386 b/archive/ES_0.5612030297404386
new file mode 100644
index 0000000..865eb37
--- /dev/null
+++ b/archive/ES_0.5612030297404386
@@ -0,0 +1,22 @@
+archive/ES_0.5612030297404386---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T22:00:15.845
+Launch V∞: [7.928869506712229, -5.656209431135643, 0.20171927144346136] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8694845976604066e-9, -5.8808346690874185e-9, -1.1334596973725347e-9] km/s
+ V∞_out: [-9.62626509512577e-10, -1.9829818974820518e-9, -5.0724785166392405e-11] km/s
+ time of flight: 1.8749577787261415e8 seconds
+ arrival date: 2030-04-23T00:09:52.845
+ thrust profile: [0.4832703129529122 -0.00562348462023709 -0.13627819587976786; 0.06530032530421911 0.037800305919773264 -0.07313966139997725; 0.04419833889779137 0.045302292720343834 -0.09434908799998436; 0.03310400162925833 0.038853169282986384 -0.1018897578582718; 0.025159179716150726 0.030330793588196087 -0.09319962084423421; 0.017997706608303233 0.02884493947920189 -0.091863627543295; 0.012248889131022442 0.01953693677353006 -0.061012665602949746; 0.005307771995031715 0.005925854599651679 -0.0354847274680138; -0.011539374904900954 0.015453549291254812 -0.019921668033290672; 0.010148838463991448 0.02167885285373994 -0.08737647056946946; 0.000904906208134576 0.0010408743994092578 -0.00029410666574478876; 3.6489540813976754e-5 0.0009867510438957446 -0.0054088334327354656; 0.00318152916804119 0.00082647055691305 -0.003092382438355292; 0.006645382493542405 0.018864263318515685 -0.02273436281072958; -0.00028401708189524624 -0.0014172872672680986 -0.000415668305766257; -0.004502261366301982 0.00039770661620445785 -0.014871084447926496; 0.00625737810269357 0.003257181333491984 0.009931730635762033; -0.0012847269519301549 0.0026651160591287686 -0.003036358547202217; 0.0019241657453866713 -0.01203105396192942 -0.015175779464638967; 0.0006550276048889581 -0.0008109058365967884 -0.006266951050995634] %
+
+Mass Used: 101.15139125161704 kg
+Launch C3: 94.90036744781051 km²/s²
+||V∞_in||: 6.641000613380387e-9 km/s
diff --git a/archive/ES_0.5612268380056118 b/archive/ES_0.5612268380056118
new file mode 100644
index 0000000..8f5240c
--- /dev/null
+++ b/archive/ES_0.5612268380056118
@@ -0,0 +1,22 @@
+archive/ES_0.5612268380056118---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T16:17:45.543
+Launch V∞: [8.013121779824807, -6.0172185263656734, -0.17681675482067494] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009757395144164304, -0.0006823349197040974, -0.0405241900760167] km/s
+ V∞_out: [0.03720090209712555, 0.014581350068638942, -0.007005759065945883] km/s
+ time of flight: 1.8749577782030386e8 seconds
+ arrival date: 2030-04-28T18:27:22.543
+ thrust profile: [0.1285151630399959 -0.009904576538955613 -0.05450274725574373; 0.09297045033014303 0.03302393374700351 -0.132530249068955; 0.028235350874008393 0.014716186125186981 -0.07239697542412227; 0.022700372501844698 0.013486987560689463 -0.08271033069297509; 0.021085982561719827 0.013222000635869213 -0.0974539965674859; 0.01384457067254355 0.008980405217265173 -0.07746819982279078; 0.015128254258218154 0.009779728380927697 -0.09623153199961905; 0.0127705830170056 0.007976075967424067 -0.09047451294284199; 0.0052246826079958425 0.003338909570521058 -0.04210683101021927; 0.0017102612512031106 0.0012134049832180826 -0.016795104185458914; 0.0013923709741324973 0.000815775757865198 -0.013439144422090998; 0.00034035562011293206 0.00032351008262842255 -0.004331602089396786; 3.2873635607019486e-5 -3.502346350283856e-6 -0.00017751994281256717; -5.06642856714442e-5 -0.0001555015432706741 -5.4201568512471507e-5; -0.0002422448279209092 0.00015836819193768895 -0.00022518026819974595; -0.0007780257838489193 0.0006498128560187928 -6.483254268057508e-6; 6.459862096695556e-5 -0.0009784712282238759 -0.00018403252427713743; 0.0001868583694660524 -0.00016586308999283218 0.0001484817237193555; 0.0003924918458321785 0.0004854991681937159 0.0003600176027503372; 6.970530224243132e-5 0.00010484757237867932 2.2891373179693237e-5] %
+
+Mass Used: 68.81620657331041 kg
+Launch C3: 100.44830361712629 km²/s²
+||V∞_in||: 0.040541677689259134 km/s
diff --git a/archive/ES_0.5612414762719368 b/archive/ES_0.5612414762719368
new file mode 100644
index 0000000..8149614
--- /dev/null
+++ b/archive/ES_0.5612414762719368
@@ -0,0 +1,22 @@
+archive/ES_0.5612414762719368---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T05:17:48.496
+Launch V∞: [7.81565360668869, -5.558301801152713, 0.3055616725414567] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.675577787470174e-5, 4.128384074174775e-5, -3.015905751978002e-5] km/s
+ V∞_out: [9.600818092227445e-6, 6.835058676937667e-5, -3.337703722971491e-6] km/s
+ time of flight: 1.8552571377233168e8 seconds
+ arrival date: 2030-03-27T12:13:01.496
+ thrust profile: [0.7275982717441395 -0.029078422666548948 -0.14316771247876367; 0.08111204433778861 0.05440561758138317 -0.07766257614785108; 0.04122498376482661 0.04514091604211822 -0.07304551712242648; 0.03260121907585506 0.048851777050731585 -0.08665059151318771; 0.01978273562843847 0.03764282004929246 -0.0728438325691646; 0.015671635488247106 0.037095844654446514 -0.07545655054307199; 0.01703048084599216 0.04980100581158084 -0.10712102147277118; 0.010548476041795464 0.040116252227873093 -0.09152225344198404; 0.0045052304996342244 0.018244726252817377 -0.04528855813683173; 0.0020188369486346235 0.010053760227676818 -0.02692335085078451; 0.0017801376854335372 0.0127137424698455 -0.03406988282978265; 0.00014109839366727243 0.00076108007320379 -0.0025177620658589995; 0.0007034951315244098 0.0017110418692413182 -0.0018735827151935068; -0.0007134576180137891 -7.794627903424402e-5 0.001417382630086889; -0.0006565915153645322 -0.0009888396193350683 -0.00206141460264801; -0.0006458687168081503 -0.0029573229913869934 -1.6463948693310523e-5; -0.00014390017802012292 0.0003479864173318646 -0.00018400523818262325; -0.0016785804282662118 0.0004980812074535585 -0.000127504719962628; -0.004997027965490343 0.0032302647815782297 -0.0006104449860612923; 0.00027683725371165763 0.0018755460926412183 0.00027935083747616615] %
+
+Mass Used: 117.69197478626938 kg
+Launch C3: 92.07252814816975 km²/s²
+||V∞_in||: 6.928222731364689e-5 km/s
diff --git a/archive/ES_0.5612450710214788 b/archive/ES_0.5612450710214788
new file mode 100644
index 0000000..7ebe5e9
--- /dev/null
+++ b/archive/ES_0.5612450710214788
@@ -0,0 +1,22 @@
+archive/ES_0.5612450710214788---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T11:40:41.648
+Launch V∞: [8.021909703077354, -5.749151157124916, 0.11902775093900021] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3316682097336525e-5, -0.0010029826523570576, -1.6561290482246377e-5] km/s
+ V∞_out: [-0.0009667817282817482, 0.00014861606757605157, -0.0002216379055435342] km/s
+ time of flight: 1.8749577787363833e8 seconds
+ arrival date: 2030-04-24T13:50:18.648
+ thrust profile: [0.25898531295065824 -0.00040690788571314364 -0.08896190851570146; 0.08135582119724258 0.04577799421254492 -0.09866815612569588; 0.047493770915380595 0.042511322543608315 -0.10515002442165951; 0.0462783567246968 0.054219841566489825 -0.14915519421386064; 0.022333510722506146 0.0313708144696423 -0.09978175634840003; 0.011358868559776619 0.01844052870025684 -0.06546816391541554; 0.007141857739476762 0.013471605960071121 -0.05400046037034536; 0.003928021619223811 0.011738555456816197 -0.03964312200838907; 0.0024333104079123317 0.006316481961933044 -0.03157875973538905; 0.003538727865920152 0.009324637793772227 -0.045378666913846386; 0.0014782979455162284 0.0024539947929646177 -0.009862640269862888; 0.00033347322992988604 0.0021792535753370782 -0.013858673149924158; -0.0004670299324331761 -0.00121886043940949 -0.0008905378306694398; -0.005921292157185904 -0.0036544651990440425 -0.005163985591909229; 0.00044397176555433676 -0.004167114433582173 0.005045310230716602; 0.017115788027416964 0.009210518313671992 -0.006188484553223383; -0.003431487903855754 -0.0009323367699462815 -0.004157301541212065; -0.0008328726348185562 0.0005077556019957499 0.008159394452316171; 0.012464408286538768 -0.0031460884291330217 0.003024551585243364; -0.010234932971081252 -0.0039636952289608665 0.01688539310188163] %
+
+Mass Used: 86.51458834086134 kg
+Launch C3: 97.41794191729096 km²/s²
+||V∞_in||: 0.0010032077607822405 km/s
diff --git a/archive/ES_0.5612476183334613 b/archive/ES_0.5612476183334613
new file mode 100644
index 0000000..ad2578e
--- /dev/null
+++ b/archive/ES_0.5612476183334613
@@ -0,0 +1,22 @@
+archive/ES_0.5612476183334613---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T17:00:21.100
+Launch V∞: [6.664262983790661, -7.344522902046671, 0.16804842512112148] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.83775547983834e-7, 4.558007661999583e-6, -2.6300981049768863e-7] km/s
+ V∞_out: [1.8333643266984958e-6, -3.6474695464784822e-6, 2.1263154524022843e-6] km/s
+ time of flight: 1.8749577787493443e8 seconds
+ arrival date: 2029-04-09T19:09:58.100
+ thrust profile: [0.1792777910385135 -0.05476960637682528 -0.0687192741989405; 0.08105471909031452 0.018196967755568342 -0.09503998511451248; 0.05250374700923679 0.023350642575045506 -0.10496974701946378; 0.04605454054708346 0.027198424669003025 -0.12971083279759046; 0.03775011379314542 0.02646295454447432 -0.13673656205172244; 0.027665623076809497 0.02189271272321796 -0.12235681596611563; 0.01771503280029928 0.015279825183135481 -0.09263056459876824; 0.009262317127297073 0.008126319147288705 -0.05561135382982659; 0.004464112952479174 0.0037023292581723037 -0.029418311380249404; 0.002161858318043488 0.0021018106584896105 -0.016063391801829727; 0.002194931642863591 0.001959059629160967 -0.017154299432629878; 0.0007631123703179057 0.000732589139330605 -0.006438030671761263; -9.431276844849828e-5 0.00031735871555442713 5.17289744987861e-6; 0.00016083870302570867 0.0002019171742012875 -0.00022614605619955243; 0.0003699703273950668 0.00017326137279939082 -0.0002069629285224096; 7.865994693312349e-5 9.144186343824794e-5 -8.784788816777285e-5; -5.608673850194507e-5 -3.676878383878786e-5 0.0003123577845933724; 8.347041614400313e-5 0.0002639229452356108 -0.00033537672961694864; -0.0004981786495110963 -0.0005242235909199463 -4.2744426378065385e-5; 0.00023820532703633832 -0.0003700108682297731 -5.034360009589209e-5] %
+
+Mass Used: 80.89004943656073 kg
+Launch C3: 98.38265804899613 km²/s²
+||V∞_in||: 4.602760247687115e-6 km/s
diff --git a/archive/ES_0.5612477417558898 b/archive/ES_0.5612477417558898
new file mode 100644
index 0000000..5416127
--- /dev/null
+++ b/archive/ES_0.5612477417558898
@@ -0,0 +1,22 @@
+archive/ES_0.5612477417558898---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T10:42:53.737
+Launch V∞: [6.471151295328684, -7.370093125495227, 0.1471444087176648] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0011016712208284018, 0.001193317665709545, 0.0011284459950617813] km/s
+ V∞_out: [-0.0013212882247491697, -0.0006402618783858693, 0.0013249649980667188] km/s
+ time of flight: 1.8586551451242688e8 seconds
+ arrival date: 2029-03-20T16:01:27.737
+ thrust profile: [0.34816593202635143 -0.09016300532970822 -0.11984880840754134; 0.060934867329879086 0.015900377772554663 -0.06439542879673578; 0.05633720205505469 0.028914725747037226 -0.0996495075588441; 0.06330666013244533 0.04409491325404843 -0.15633154563783136; 0.0394194911156743 0.03303344724606148 -0.1252177975024216; 0.03234762325404856 0.03136698447248268 -0.12511375359960542; 0.03154342715128428 0.034121568693792986 -0.1437825111683027; 0.008289385990413433 0.009595068731611724 -0.04427632783857093; 0.002136247718622523 0.001470160769050456 -0.012444247342867514; 0.0018093799205720644 0.002089387539433632 -0.010912883437983656; 0.0002760205068699395 0.0002984621041452654 -0.002059210160487663; 0.0004273343871331427 0.0006087053409058076 -0.003795471399462705; -0.0001799331844267571 0.00012037796986719939 -0.00024659503854662103; 0.00013990951839967919 -0.00029575557397248453 -0.00011257990744582862; -0.000614150557542183 0.0008502168982850079 -0.0003376355670288909; -0.0008804534336335694 -8.269349664778052e-5 -0.000632456517603454; -0.0008316974334143153 0.0003135027300336823 -0.0004726228836000578; 0.0005727975202778207 0.00044876254245158876 -0.0005711028042968798; 3.62608887044046e-5 0.000582228987042213 -0.0015471075290508958; -0.00015234799294315781 -0.00025744481686610667 -2.9842734467018593e-5] %
+
+Mass Used: 93.53064646715393 kg
+Launch C3: 96.21572324252298 km²/s²
+||V∞_in||: 0.001977644278900276 km/s
diff --git a/archive/ES_0.5612541120432365 b/archive/ES_0.5612541120432365
new file mode 100644
index 0000000..31cb53c
--- /dev/null
+++ b/archive/ES_0.5612541120432365
@@ -0,0 +1,22 @@
+archive/ES_0.5612541120432365---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T20:51:36.452
+Launch V∞: [7.577098264214638, -6.005686891936312, -0.0009564576001615653] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004871356552202434, -0.00024445987740937805, -1.8654037331972608e-5] km/s
+ V∞_out: [0.0003775741498129123, 0.00023329537538207702, -0.0003195919381828237] km/s
+ time of flight: 1.7445589527859962e8 seconds
+ arrival date: 2029-11-19T00:49:51.452
+ thrust profile: [0.5739859327030883 -0.051346604227448925 -0.17070060713135132; 0.060822879620475535 0.028878203309361864 -0.06862878547750073; 0.107172515910154 0.0855163681865687 -0.19366509808420887; 0.07462188135710307 0.07898028511932073 -0.1970789313085863; 0.020286823226723632 0.02589519930974493 -0.08010337287845562; 0.01367956275409854 0.02030355626948925 -0.06849422951987066; 0.008354988641608364 0.014813827555274087 -0.05183330435915249; 0.013730557473557435 0.026651283360004288 -0.0927912881568965; 0.0021640854983911734 0.005196730737432242 -0.019329660896732527; 0.002970347448695498 0.005237280139193988 -0.0297370318735117; 0.0017087373039777036 0.009608248623387676 -0.03331897928397889; 0.00042781501532400596 -0.0006265537755635558 0.0010664981704238486; -0.0009052357628460011 -0.000804890013591107 0.001648390778659348; -0.0006950579753043557 0.00034749315990702636 0.002566455695107869; 3.932621877513869e-6 0.00043584793124682255 0.0011232067128064383; -0.0007634442673489007 -7.939688965694167e-5 4.371324624500737e-5; -0.0008273441502888057 0.0024620658904769524 -0.0013034252420285539; -0.0017145500379974542 -0.003742409526018683 -0.0010764785464556232; -0.0004610807583605336 -0.00011953620905286644 0.0026153594426586483; 0.0016883913118147399 -0.0010710804974979444 0.0010542322118738973] %
+
+Mass Used: 109.49241534172688 kg
+Launch C3: 93.48069406435125 km²/s²
+||V∞_in||: 0.0005453528686627096 km/s
diff --git a/archive/ES_0.5612632040896416 b/archive/ES_0.5612632040896416
new file mode 100644
index 0000000..24aa355
--- /dev/null
+++ b/archive/ES_0.5612632040896416
@@ -0,0 +1,22 @@
+archive/ES_0.5612632040896416---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T02:48:03.796
+Launch V∞: [7.810194132216086, -5.790537689877883, 0.019584828269074137] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.561304126943658e-9, 1.3917524246853858e-9, -1.2840428079334497e-9] km/s
+ V∞_out: [5.2726664358610455e-9, -4.000619584694079e-9, 1.8706481490594474e-9] km/s
+ time of flight: 1.798091338250366e8 seconds
+ arrival date: 2030-01-20T05:46:56.796
+ thrust profile: [0.46120722138803794 -0.022829972059187933 -0.13943148802066854; 0.09016063720663561 0.04910940051812725 -0.09344493012902226; 0.08895969256489594 0.08047034454696456 -0.16186315216437294; 0.06326683605723826 0.07659238353671208 -0.1703396516307227; 0.028933886178827056 0.04368831702121759 -0.1075140593987801; 0.019283709583966736 0.034710259878845295 -0.09218158324032714; 0.016216785466506456 0.0325655370044601 -0.09146230296557521; 0.0026677015773174315 0.006818570053837758 -0.020461461028482907; 0.0019183311161027757 0.005725980767823809 -0.017811522941360614; 0.0010736611498520473 0.00390950721305171 -0.012674312497231352; -0.0008528639028310231 0.0006223512477447075 -0.0011581827455519884; 0.0008424640142014741 0.0007754504514128706 -0.0030806170779619363; 0.0002579913685310418 -0.0014357852755293465 -2.6830837329668667e-5; -0.0011830619518851408 -0.0028983775753938083 -0.0036517529039580476; 0.0009929782884657607 7.940029418299131e-5 -0.005597177395661945; -0.004948180797630331 -0.00369368531242667 0.001599949404975226; -0.0017010366745103308 -0.0020454144531517025 0.0028537135954788016; 0.007539117365080338 -0.0018823545363914954 0.00584258446684524; -0.007302581336846646 -0.0013693616879899314 -0.00011299111515479477; -0.0010855509956951086 0.0017511368029067944 -0.0073044058608272245] %
+
+Mass Used: 103.38298910118147 kg
+Launch C3: 94.5298426862972 km²/s²
+||V∞_in||: 5.874848452222732e-9 km/s
diff --git a/archive/ES_0.5612669797750184 b/archive/ES_0.5612669797750184
new file mode 100644
index 0000000..82d7954
--- /dev/null
+++ b/archive/ES_0.5612669797750184
@@ -0,0 +1,22 @@
+archive/ES_0.5612669797750184---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:27:20.097
+Launch V∞: [7.821331866500227, -6.1204233293900945, 0.034400096854240586] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.365743390250978e-7, 7.712435856873236e-7, -5.676160278791791e-7] km/s
+ V∞_out: [2.14784245893454e-7, 1.3216834708467447e-6, -5.601202474068488e-8] km/s
+ time of flight: 1.7320136561367488e8 seconds
+ arrival date: 2029-11-06T15:56:45.097
+ thrust profile: [0.10627426421692147 -0.01476221137456193 -0.04041687504780763; 0.1321761734327293 0.0490032522053677 -0.14544547024504376; 0.04871063241066917 0.029873190025023276 -0.10195585929010792; 0.044393607141882334 0.03029903637043568 -0.12266356234565812; 0.06671291566855735 0.043485104894607 -0.20930430165547667; 0.015820896461761658 0.014338066449215264 -0.07370412754402864; 0.021011675647853202 0.02106416019205108 -0.11242191926155404; 0.009849159878588932 0.012136580491029919 -0.06476912357644395; 0.003550059481110555 0.004344704472841511 -0.027088475192138195; 0.002957697842662454 0.0038397520536160106 -0.023838974243921746; 0.0010361878783727227 0.0013617803809254359 -0.009091584126289094; 0.0035031050784376542 0.0020095366638069054 -0.0021903600889626286; 0.0004572201625433071 0.0016030300208503831 -0.0028086537580785543; -0.003236294098024164 0.0008511388395064589 -0.003174013540730299; 0.004764762706978154 -0.0016219563365723803 0.0011425211609543406; -0.002122547907206944 0.00024394207989838416 -0.00019230177251342798; -4.649251023895661e-5 -0.0004248182743246296 0.0009509523251082809; 0.0005479844727860317 -0.00668620467536012 -0.0029051495579745733; 0.0014808718001929073 -0.005719662459800564 -0.006049492261438813; 0.0018432722338602146 0.0013165749931552393 -0.0010989167641670184] %
+
+Mass Used: 79.44649236688292 kg
+Launch C3: 98.63399726353803 km²/s²
+||V∞_in||: 1.3394685946633747e-6 km/s
diff --git a/archive/ES_0.561270906704743 b/archive/ES_0.561270906704743
new file mode 100644
index 0000000..fed3bdf
--- /dev/null
+++ b/archive/ES_0.561270906704743
@@ -0,0 +1,22 @@
+archive/ES_0.561270906704743---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T17:46:14.887
+Launch V∞: [7.985620621591096, -6.002778127700482, -0.10645075692962713] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.12816733646823e-10, -2.569254754380807e-9, -2.064158166861553e-9] km/s
+ V∞_out: [3.3802651683211094e-11, -2.6051388551791462e-11, -1.9679452598169292e-11] km/s
+ time of flight: 1.874957778259478e8 seconds
+ arrival date: 2030-04-28T19:55:51.887
+ thrust profile: [0.24032001561559502 -0.01742555803668506 -0.10097120906036079; 0.013001188668806252 0.0045175898344425635 -0.019452907060154238; 0.013520180879680115 0.006735191843464414 -0.03523277180657515; 0.03323793595358911 0.019679937414184202 -0.12251457749947613; 0.03221599978994569 0.020455166510295678 -0.15072565846401076; 0.02460649849800145 0.0160161895802751 -0.1388133971115955; 0.00961433198232068 0.00588900324173035 -0.062193559227743465; 0.0065896176432069815 0.0036040927819217974 -0.0472916488655522; 0.009539741941763285 0.005806692765805915 -0.07571647415916007; 0.0008071897527081371 0.0004554115812677957 -0.006552128420991439; 0.0014836194717575539 0.0008172684251449181 -0.013373744070779459; 0.0002547133716838852 0.0008469251674863115 -0.0003093720554120789; -0.00028702869790199774 -9.467249004279095e-5 0.0003780111627447795; 0.00025343123620644593 0.0004725547051616955 3.912097876667558e-5; -0.00012584221855379575 -0.00010513435286659013 -6.645407157116151e-5; 0.00032546342833734797 0.00027607456322179414 -0.001008234677104845; 0.00032561366583379987 -0.001582848659132509 -0.002895862140901491; 0.0010562045737489772 -0.0023548656665896136 -0.0016965289974637259; -0.0035520959764781396 -0.0024685281742773202 -2.9136674427861892e-5; 0.0005663569044125423 -9.370904376929397e-6 -0.0008208218524736492] %
+
+Mass Used: 72.56297775368512 kg
+Launch C3: 99.81481372603115 km²/s²
+||V∞_in||: 3.3944793375753397e-9 km/s
diff --git a/archive/ES_0.5612734464235005 b/archive/ES_0.5612734464235005
new file mode 100644
index 0000000..2bdcdf5
--- /dev/null
+++ b/archive/ES_0.5612734464235005
@@ -0,0 +1,22 @@
+archive/ES_0.5612734464235005---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T10:15:24.452
+Launch V∞: [7.588725323723072, -5.995060589735059, 0.4719400074476] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005262060839263121, -0.0003783514340298964, -0.02178661655830846] km/s
+ V∞_out: [0.019810613869823968, 0.00807114029226692, -0.004107249538226135] km/s
+ time of flight: 1.772881938573638e8 seconds
+ arrival date: 2029-12-22T08:58:37.452
+ thrust profile: [0.46430119958513943 -0.019974566732832114 -0.1318348960528592; 0.20950030686193044 0.1126260906122501 -0.1988289632621495; 0.07088773599537615 0.05983163502481097 -0.11872379440704448; 0.05132578627940275 0.061621830912634054 -0.13532650376040417; 0.02929258199211634 0.03846635545288199 -0.09757326225728842; 0.02135681024887217 0.038995186175965715 -0.10244459666181532; 0.013613328140339283 0.028329545232746618 -0.07830636793444248; 0.006756862594089762 0.014979927012040234 -0.044931541653267175; 0.0007452135570604037 0.0021318711585204247 -0.009575564182859967; 1.976782944698843e-5 0.002330000057762856 -0.00720321102549676; 0.002756230018251321 0.006998422776153484 -0.025414906865523997; 0.000709138323227442 0.00039086231484585903 -0.001408803101177083; -0.0005296532427715361 0.0008951738212388753 -0.0013127409798678637; 8.043714408661822e-5 -0.0017960927893806147 0.0006556828821191695; 3.4265038195429334e-5 0.00015246016238228222 0.0036449777626925846; 0.00015787795203183697 -0.0033175410130317105 0.0027331665366995663; 0.0006496755389598716 -0.00348303506464982 -0.0038192521470291787; 0.00037643582211337813 -0.0010250216587467773 0.002142063865314821; -0.0014595671427105957 -0.0022965437835938156 0.004453274076119645; -0.0006332269952593325 -0.0013340474199865378 0.0049150980324344645] %
+
+Mass Used: 107.93100733660094 kg
+Launch C3: 93.75223088413995 km²/s²
+||V∞_in||: 0.02179625435044182 km/s
diff --git a/archive/ES_0.5612773561160955 b/archive/ES_0.5612773561160955
new file mode 100644
index 0000000..e240b55
--- /dev/null
+++ b/archive/ES_0.5612773561160955
@@ -0,0 +1,22 @@
+archive/ES_0.5612773561160955---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T17:59:09.796
+Launch V∞: [7.906275705932641, -5.707203787874224, 0.20669274961335057] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.136118777224617e-7, -6.251331566369675e-6, 1.1314765267085946e-6] km/s
+ V∞_out: [-9.725380791614176e-7, 3.788683389325875e-6, 5.05684748788803e-6] km/s
+ time of flight: 1.8349880560966197e8 seconds
+ arrival date: 2030-03-06T13:52:34.796
+ thrust profile: [0.39741404988240053 -0.036845058231917464 -0.1286227621157885; 0.19992055976865508 0.07021629201526511 -0.20574861001333467; 0.04999159918186401 0.035688398744709166 -0.11172754227141407; 0.024713902084756992 0.022667156955859257 -0.08170611716315583; 0.015509335946637264 0.016612309016350257 -0.06808784245816933; 0.009674414569939895 0.01126007869382885 -0.05270909320152547; 0.012459869655711253 0.014969010621991574 -0.07687981370801904; 0.009104677308890658 0.015556357723680374 -0.06659959438064458; 0.003329052821889757 0.007325394437262008 -0.04500176294218505; 0.003688603552558504 0.006815422006400143 -0.03682723152231558; -0.0018209850828941067 0.0028282957154599337 -0.004304592542627456; -0.0010355444146127146 0.0010311339035557862 -0.007198645235326026; 0.0008935539954780317 -0.008595282164465444 -0.005071621928906292; -0.0014871130182969173 -0.0015069293913622208 -0.0021633157657973768; 0.0007323071548113136 -0.001434759240646371 -0.004812859595792045; -0.0005955357320921662 -0.005236157651460153 0.005320240888195692; -0.01232377807964937 -0.0006500033849837906 5.906022747230802e-5; 0.0005240467013258311 -0.0006539230289867987 -0.006696364064178943; 0.0005910857609952368 -0.007703924495999439 -0.009260307044970141; -0.007219139920643024 -0.005658892232202479 0.0021375031752256758] %
+
+Mass Used: 99.93304250959045 kg
+Launch C3: 95.1240925072893 km²/s²
+||V∞_in||: 6.392857529713067e-6 km/s
diff --git a/archive/ES_0.5612814695869 b/archive/ES_0.5612814695869
new file mode 100644
index 0000000..2f05248
--- /dev/null
+++ b/archive/ES_0.5612814695869
@@ -0,0 +1,22 @@
+archive/ES_0.5612814695869---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T10:28:20.086
+Launch V∞: [6.525643637453546, -7.341747248223848, 0.19617295521083714] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9908329616146595e-5, -3.0894012398771085e-6, 5.379707293897202e-8] km/s
+ V∞_out: [3.954431226521701e-6, -8.870787409803779e-8, -1.9751711913239214e-5] km/s
+ time of flight: 1.8749577787679365e8 seconds
+ arrival date: 2029-04-09T12:37:57.086
+ thrust profile: [0.35519366750765835 -0.09261442541962438 -0.12504017266773768; 0.04188709400011693 0.010849401712440523 -0.04788488006595195; 0.044186878909567615 0.022367159679345393 -0.08416435334226091; 0.038312906091964964 0.0259193843368806 -0.10185660003928082; 0.04880701897238113 0.039760265461538206 -0.16407728159181834; 0.03960170571352935 0.036582633186766196 -0.1609252518709735; 0.010486120727827794 0.010969012410403104 -0.05315086827034674; 0.009951314298323934 0.010942297909975212 -0.05500623839618144; 0.007200529742184581 0.008792770431310142 -0.04700281046251429; 0.006002770959786328 0.007801595470081208 -0.04377644621861866; 0.0012891931141075332 0.0020672423829326265 -0.011807782639091909; 0.0001348166264522854 0.00017680413832646906 -0.0010990883560265236; -5.499728802707409e-6 3.0136604243835933e-6 1.3841608638961826e-5; -0.00023488591615495423 -0.0003043045995310283 -0.00010900301508116298; 0.00034603445461044277 -0.0004512402019376611 -0.0006827173112733179; -1.876531279304472e-5 -0.0004893486981423073 -0.00011634585968078984; -3.317505118863375e-5 0.00018318790512336433 -0.00022461711321885232; -9.372539855705906e-6 3.368435419973706e-5 -5.609284584938923e-5; -0.0001750315436812305 0.0001456288072352899 0.0006518703070747631; -0.00016948332265502792 4.193309363582955e-5 0.00039992819724874725] %
+
+Mass Used: 91.77310653690347 kg
+Launch C3: 96.52376136819653 km²/s²
+||V∞_in||: 2.014668415028018e-5 km/s
diff --git a/archive/ES_0.5612825352740443 b/archive/ES_0.5612825352740443
new file mode 100644
index 0000000..6bd92eb
--- /dev/null
+++ b/archive/ES_0.5612825352740443
@@ -0,0 +1,22 @@
+archive/ES_0.5612825352740443---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T07:03:31.750
+Launch V∞: [6.633160625916447, -7.3523941462185585, 0.17271649734767225] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.986852843544168e-9, 4.7725013393499016e-11, -6.27003021704346e-9] km/s
+ V∞_out: [-1.3449769708338861e-9, 3.0245512861438887e-9, 4.227064298676334e-9] km/s
+ time of flight: 1.8749577782851025e8 seconds
+ arrival date: 2029-04-09T09:13:08.750
+ thrust profile: [0.2029035819744154 -0.050018101195083015 -0.07229202026344783; 0.06876390659471135 0.018974346337829254 -0.07486764315229118; 0.044571033207712614 0.023560051333292028 -0.0820414892379114; 0.059123640197756615 0.042027476391831166 -0.15048573987666536; 0.02770957902279115 0.023660583458086675 -0.09218486756699501; 0.03703134414059198 0.03646023183128374 -0.1491733335927776; 0.022074101985198314 0.023921105803861847 -0.10203216538055712; 0.010119910841586414 0.012128587886464114 -0.05598876545724416; 0.009314824768890242 0.011818869899801288 -0.05810047719078047; 0.003640391352745244 0.0051281013240613025 -0.026454301309386904; 0.0006548375521852913 0.0009422730898261038 -0.005264195895983459; 0.00012657462731327252 1.6541932004560757e-5 -0.0007068107115693134; 0.0001323798437235601 -4.5506350692431794e-5 -0.00022542689308715702; 0.0003280291601138397 0.0003724502159764658 -0.0005586525539554609; -0.0003109073166149979 3.1814138835088395e-5 -0.00028042209235218054; 3.246353657783345e-5 -7.811280580734031e-5 -0.00028131228142637296; -0.0001937924015503994 6.423926718109442e-5 -0.00016127290341593208; 0.000438536865577547 4.616106046846221e-5 -0.0005096607081368451; -0.00018493599846128398 2.3438430076408712e-5 -0.0003520828333911732; 0.0004722862692902772 5.6539147082608254e-5 -0.00023345644057592578] %
+
+Mass Used: 82.65924622547436 kg
+Launch C3: 98.08635055901325 km²/s²
+||V∞_in||: 9.387846891427378e-9 km/s
diff --git a/archive/ES_0.5612906322463044 b/archive/ES_0.5612906322463044
new file mode 100644
index 0000000..68689b1
--- /dev/null
+++ b/archive/ES_0.5612906322463044
@@ -0,0 +1,22 @@
+archive/ES_0.5612906322463044---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T14:21:54.319
+Launch V∞: [8.15140510421563, -5.567199481932842, 0.21243582505565134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.801911037307224e-7, -6.247664197848807e-6, 1.102713842434147e-6] km/s
+ V∞_out: [-9.414421210029029e-7, 3.759678656449228e-6, 5.068823988076482e-6] km/s
+ time of flight: 1.874957778749254e8 seconds
+ arrival date: 2030-04-22T16:31:31.319
+ thrust profile: [0.25891655662574325 -0.0008025775000522008 -0.08395746186803056; 0.06716024088700238 0.03745142568493563 -0.0783932152908554; 0.06413250939776508 0.05964784259254372 -0.12790600870586522; 0.038997570966467235 0.04602308371973431 -0.11349441340070004; 0.02014556144180279 0.030069033370389797 -0.08640491507124624; 0.009625747750431509 0.016694120671665643 -0.05419558263663091; 0.009840159727881917 0.017658598920104296 -0.06171464957292162; 0.007745043054445966 0.019078709697893707 -0.06545835537194734; 0.0042863820701938395 0.01180995921338695 -0.044960464985275686; 0.0029919688583569626 0.011206301259349781 -0.03615190644938681; 0.0025534213280137977 0.005105313971746104 -0.028944309223416197; 0.0005819446676040417 0.001514898090834735 -0.009009382666956927; 0.0016821557438536092 -0.00043642813500587886 -0.0011857571818985908; -0.002086837039334769 -0.008255049129700903 -0.001335595031796752; 0.0021106354276710293 -0.0008752927762820579 -0.0018380809741763426; 0.0007444565686025199 -0.0007706862182908709 -0.011116318929432871; 0.00026688573629920435 -0.0044917445141600745 0.0045934825826234905; 0.013829369804898349 0.00033141208400726263 -0.008959543427143266; -0.00048417481956125803 0.0005317769717350625 0.006222590827134013; 0.011674004907360976 0.02320925765088163 0.006211063766029208] %
+
+Mass Used: 86.18097964482922 kg
+Launch C3: 97.484244224433 km²/s²
+||V∞_in||: 6.3805913272181965e-6 km/s
diff --git a/archive/ES_0.5612984256283743 b/archive/ES_0.5612984256283743
new file mode 100644
index 0000000..f883c98
--- /dev/null
+++ b/archive/ES_0.5612984256283743
@@ -0,0 +1,22 @@
+archive/ES_0.5612984256283743---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T02:56:13.053
+Launch V∞: [7.819646008743582, -5.721473025242478, 0.08191454278680957] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5016014767829784e-6, 0.00010273353538652214, 1.8125716960684151e-6] km/s
+ V∞_out: [0.00010023471805191748, -4.441985362231005e-6, 2.1847860048486367e-5] km/s
+ time of flight: 1.843424161798726e8 seconds
+ arrival date: 2030-03-14T17:09:49.053
+ thrust profile: [0.4793593530914014 0.006355480391018176 -0.1305177134399487; 0.12811741934709442 0.08267505857855412 -0.12419651449070014; 0.08119915923757098 0.08682876252231514 -0.14332763501507448; 0.04830478135028917 0.07042281074720648 -0.12901271917442747; 0.03294314388681349 0.06023085171344599 -0.12253472707788551; 0.007968049276829892 0.0182157999530257 -0.045327506047083015; 0.00542804141667261 0.012228199434551522 -0.03492021548978574; 0.0052068043155403705 0.0231852413433747 -0.06339261081583025; 0.004428551933266659 0.014616620375758858 -0.034856950242913756; -0.0018936553627852582 0.009477902329635756 -0.019314923804243107; 0.0027375366696159283 0.007306642662256625 -0.014685729963167277; 0.0005285272152255757 0.0008072359622583395 -0.0008917557081549203; -0.0007280818928390772 0.00027386866936908536 -0.0039028862254342723; 0.003557801751856539 -0.005914275242531209 -0.001039327669052318; 0.00277408871619249 -0.008366015562415733 -0.005522628950552879; -0.0066075776680786825 0.0036960476505571273 -0.001909550223209714; -0.001513414253932219 -0.00037255605063118356 -0.0031214534482337498; -0.009705929155815703 0.0023078840070373786 0.008895857841408714; -0.00024050232452535328 0.0014626359639242715 -0.004987488452683862; 0.00042010514355886276 -0.00018205206972231954 0.0015469805206357286] %
+
+Mass Used: 107.16333747418912 kg
+Launch C3: 93.88882727295672 km²/s²
+||V∞_in||: 0.00010276049589293671 km/s
diff --git a/archive/ES_0.5613056771959524 b/archive/ES_0.5613056771959524
new file mode 100644
index 0000000..c415cd0
--- /dev/null
+++ b/archive/ES_0.5613056771959524
@@ -0,0 +1,22 @@
+archive/ES_0.5613056771959524---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T02:50:17.231
+Launch V∞: [7.771503010496741, -6.227810693659398, -0.10323568137963884] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0003718702225888224, 0.0009664846870266405, 0.0022717659085734867] km/s
+ V∞_out: [0.002270294812669682, 0.0002850423412771802, -0.0009987402614703815] km/s
+ time of flight: 1.7573860765395343e8 seconds
+ arrival date: 2029-12-09T03:07:04.231
+ thrust profile: [0.17838923017576766 -0.02494310779443815 -0.07381391499918419; 0.04011305237918386 0.012579665153037725 -0.05358838640065495; 0.03692843763190418 0.01881576620632722 -0.08518480712539073; 0.04377469613000552 0.026791298841815275 -0.14313640691350224; 0.03456158316248592 0.02343599413762694 -0.14427602158660763; 0.025440955027414454 0.01863293162254924 -0.12700850211892503; 0.02002073539347737 0.014747529316016552 -0.11389651605996094; 0.013806691688016964 0.010059530794191836 -0.08424570876253461; 0.004883623621235826 0.008355092289184034 -0.04424855986373671; 0.0010457387300742465 0.0011367346722858268 -0.008170522911686373; 0.0016795188271766636 0.002838538319710647 -0.011909112583114759; 0.0013092806982682142 0.0005015774324157308 -0.004425964786759645; 0.00024101859664710993 0.0029731231319003334 -0.0023545579898298394; 0.0006242283460045473 -0.0009637189900731759 -0.003378342649914458; -0.00033184767672034396 -0.00010635549597538124 -0.0029278667027344265; 0.001407292938292939 0.000475001224784444 -0.004495113121124022; 0.0010166725264723218 0.0006008891359493195 0.00020237844578403948; 0.0006103789226633602 5.0325859480355854e-5 -0.0020896526844015207; -0.0007905049059294721 0.0014103562942270045 0.0030681764291032145; 0.00364814637786797 0.0003398783452749206 0.0006957757146214145] %
+
+Mass Used: 76.23345773786332 kg
+Launch C3: 99.19254268412818 km²/s²
+||V∞_in||: 0.002496657857228732 km/s
diff --git a/archive/ES_0.5613118172282401 b/archive/ES_0.5613118172282401
new file mode 100644
index 0000000..7448f12
--- /dev/null
+++ b/archive/ES_0.5613118172282401
@@ -0,0 +1,22 @@
+archive/ES_0.5613118172282401---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:49:11.641
+Launch V∞: [7.911444940769104, -5.559033413896193, 0.11372938158859452] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3722791654586005e-6, 9.979105754680606e-6, -0.00020691061198641698] km/s
+ V∞_out: [-7.734950993664812e-6, 0.00020679362451446145, -2.223644840706123e-6] km/s
+ time of flight: 1.87495777873979e8 seconds
+ arrival date: 2030-04-19T17:58:48.641
+ thrust profile: [0.5165712590284339 0.01581571407605048 -0.12835780807491895; 0.1437361054873046 0.09740979337237583 -0.12919502963431678; 0.055636516953251766 0.05938254864112668 -0.0901000937311913; 0.04388223284207637 0.062211617037534 -0.10308925586780686; 0.04681313122010739 0.09358247653541234 -0.16414466162122646; 0.01452306207658122 0.03641712619910495 -0.0661602932610068; 0.005189403439654199 0.016138980576510302 -0.0349289759988138; 0.00881592965525211 0.034593071907319084 -0.07327879020845646; 0.0009683414774979736 0.001808886126679827 -0.007940817022306918; 0.0009256061003384325 0.005038395409935836 -0.011203552946751093; 0.0002867143151921406 0.0041286462666503595 -0.00717859473034916; 0.0008755586589001263 0.0015108689600332684 -0.0035428309266825725; 0.0002363164837569185 0.0016540723048615652 -0.002511941687044739; 0.0004380008366112693 0.0009569663150597015 -0.0010454465395495155; -0.0002258050764834098 0.0007596100784444967 -0.001885267873986604; -3.075445912914499e-5 0.0014137708770561774 0.0040352223206894825; -0.0012561234085751649 0.002314768490380589 -0.010600164071394623; 0.00084985560285915 0.0013466468199459978 -0.006655185563396613; 0.004414245060878734 -0.0028595317896114567 0.004744306741245707; 0.002462446625550242 -0.0040830846707474765 -0.004565993888345991] %
+
+Mass Used: 109.4077572336937 kg
+Launch C3: 93.50674791987194 km²/s²
+||V∞_in||: 0.00020715565899671835 km/s
diff --git a/archive/ES_0.5613146487472538 b/archive/ES_0.5613146487472538
new file mode 100644
index 0000000..b2635df
--- /dev/null
+++ b/archive/ES_0.5613146487472538
@@ -0,0 +1,22 @@
+archive/ES_0.5613146487472538---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T14:04:46.984
+Launch V∞: [7.729360662817471, -5.778129393013928, 0.1546884785272056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8077502312193913e-6, -1.443518783839218e-5, 0.0002798824061281545] km/s
+ V∞_out: [1.112932741205979e-5, -0.0002819488427572256, 2.8289387994268906e-6] km/s
+ time of flight: 1.804096217217609e8 seconds
+ arrival date: 2030-01-26T15:51:47.984
+ thrust profile: [0.5665714322068502 -0.016482366029665733 -0.15122164938950577; 0.14104258426842428 0.08223510150046501 -0.1308023239974767; 0.06569930210433395 0.06475553659862497 -0.11333730347305739; 0.036206497392138666 0.04767775461957468 -0.09436906557185352; 0.02980975487342592 0.04858979168798525 -0.10586788050291043; 0.015644374214026757 0.03025350754401171 -0.06829524365855091; 0.029020176223693142 0.06093013296798592 -0.137663776824868; 0.003619410243951558 0.014579878028644841 -0.03862147319138042; 0.0040063629557307075 0.015989219274893426 -0.045499087886144506; 0.0013789610601948315 0.004291757427355947 -0.01180714787528602; 0.0005577233854635604 0.003592814703377969 -0.017894435607047655; -0.0004154355949689414 0.0018555017105196126 -0.00486749551065313; -0.0015479552524792308 0.0013448561202383056 0.0012151623224846294; -0.0004765848143108081 -0.001014675709051725 0.00016053788193725726; 5.121993274768825e-5 6.353847365216602e-5 -0.0012922038285945387; -0.000988456186885403 0.0028816149454222494 -0.0009858730241830173; -0.000805155932154475 -0.0020486901128341844 -7.270481449739926e-5; -0.00433945559758615 0.0034109678868182993 0.0022632111816893066; 0.0001100655586271477 0.0007493953157178402 -0.001410241278186016; 0.00017552999520863686 0.002644987276697053 -0.0034659996052548944] %
+
+Mass Used: 111.47036650015025 kg
+Launch C3: 93.15372406371071 km²/s²
+||V∞_in||: 0.00028026024311149334 km/s
diff --git a/archive/ES_0.5613172547173693 b/archive/ES_0.5613172547173693
new file mode 100644
index 0000000..eb9764a
--- /dev/null
+++ b/archive/ES_0.5613172547173693
@@ -0,0 +1,22 @@
+archive/ES_0.5613172547173693---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:08:45.082
+Launch V∞: [6.460844861364786, -7.36295285761794, 0.08271071227512232] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.15983008199971e-6, 0.00037293697378642084, -0.0002581064906453192] km/s
+ V∞_out: [-0.00020994996235361603, -0.000393709991789011, 8.136380027641613e-5] km/s
+ time of flight: 1.8749577787475038e8 seconds
+ arrival date: 2029-04-08T17:18:22.082
+ thrust profile: [0.32858398676074557 -0.0761112726799356 -0.1075245938668002; 0.07933450497126598 0.02374479313864837 -0.08007362199552463; 0.0940398680221414 0.05447257727664404 -0.1579816523751028; 0.07998508563067622 0.0628620102899419 -0.1886127725549361; 0.031100086061783206 0.029113998531545688 -0.09632529714495379; 0.03181893321877087 0.034787889568700034 -0.12058298064733834; 0.021099485647621003 0.025825071974352045 -0.09528400593267394; 0.004042866292759361 0.005332797337166559 -0.02254139803396082; 0.0017732067066894416 0.001530369864835522 -0.00783702941161682; 0.0018458847881764476 0.002525005813919907 -0.00862197298147423; 0.0003070679227824539 0.0005905579861152637 -0.002695074298249317; 0.0007584860963766205 0.00033397555086178655 -0.004697919657949216; -5.400109999651229e-6 0.0003890585592751137 -0.0013451199628846944; 0.0010007942831291262 0.001519538521461581 -0.0035747633346216415; 0.0004780204295270154 -0.0019326524357172624 -0.0007318117852959963; 0.0010400881149267938 -0.0006262856397030157 -0.002275015563704567; 0.00040063147892120264 -8.71721969303559e-5 -7.132158004960717e-5; -5.015467030326017e-5 -7.441086242020119e-5 0.0005206058692160582; 0.0011800852563328234 -0.00017791785490049803 0.0005947299862332951; -0.0006362348251930307 0.000789592712012025 -0.001541075217774847] %
+
+Mass Used: 95.08927618995494 kg
+Launch C3: 95.96243216805301 km²/s²
+||V∞_in||: 0.00045354414574111184 km/s
diff --git a/archive/ES_0.5613240925547274 b/archive/ES_0.5613240925547274
new file mode 100644
index 0000000..e997320
--- /dev/null
+++ b/archive/ES_0.5613240925547274
@@ -0,0 +1,22 @@
+archive/ES_0.5613240925547274---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T13:25:34.591
+Launch V∞: [7.875250994421366, -5.752384907380634, 0.19514720339605535] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.323032930750776e-6, 0.00012031237383954391, 1.958121046374027e-6] km/s
+ V∞_out: [0.00011592588521563945, -1.7974393220613966e-5, 2.6842217814057106e-5] km/s
+ time of flight: 1.8579941923304394e8 seconds
+ arrival date: 2030-04-02T00:22:33.591
+ thrust profile: [0.3832557833189578 0.01156343717296216 -0.10119020003958479; 0.09857992308230934 0.06308750919178623 -0.09460514077758247; 0.07940714894499883 0.08755590673686582 -0.1386882439801804; 0.0467849420848769 0.06749837520248714 -0.1275604060823704; 0.021470133047249818 0.04146250697517972 -0.08399326904903244; 0.02499266934314478 0.05269546390557194 -0.10995866319871445; 0.009185002136255341 0.02252555849764129 -0.053649783670907975; 0.00559144606483465 0.022418317388736456 -0.05503261585461777; 0.0022042909636787343 0.006312493412804711 -0.019219780408949585; 0.0011628607174714199 0.004229345204662947 -0.015300282781191056; -0.0026815553463427014 -0.0018566937334481557 -0.002744167415094009; 0.0007664764687581025 0.0009008161512427549 -0.004543721908562958; -0.004019682282149876 0.01260938251332917 -0.009446232135260142; -0.0015683412309856724 0.0009475796910401102 -0.004246658865146252; 0.005221687059670875 0.000553264044834786 -0.0002688359568770952; 0.0006114254298674512 9.233194891827053e-5 -0.0028749993372713706; -0.008981972276003274 0.009387028594852666 -0.0050356364394698785; 0.003301686945950218 0.0024171758485675345 0.009595474246792721; 0.005414278426652325 -0.0010007394432678712 -0.013481346001353022; 0.002970286653051555 0.012621442902554599 -0.00978942970532361] %
+
+Mass Used: 99.85048343758217 kg
+Launch C3: 95.14759277878852 km²/s²
+||V∞_in||: 0.00012044598879381696 km/s
diff --git a/archive/ES_0.5613348598328413 b/archive/ES_0.5613348598328413
new file mode 100644
index 0000000..abd2218
--- /dev/null
+++ b/archive/ES_0.5613348598328413
@@ -0,0 +1,22 @@
+archive/ES_0.5613348598328413---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:52:18.530
+Launch V∞: [8.068883310958466, -5.572940836511872, 0.16966813171813333] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.5283471862712863e-9, -2.9230462234950845e-8, 5.701039473091575e-9] km/s
+ V∞_out: [-5.281571073467449e-9, 1.9971768418567747e-8, 2.830646484072479e-8] km/s
+ time of flight: 1.8749577787456036e8 seconds
+ arrival date: 2030-04-22T10:01:55.530
+ thrust profile: [0.3644770643970211 -0.002022078551169134 -0.1152604830912522; 0.07676854146597314 0.04359173380233317 -0.08893296336501687; 0.05082385635922584 0.04713927803297262 -0.1089546100037289; 0.04147099253705485 0.04984929403655934 -0.1326101044963793; 0.020186964098514247 0.029126721085583805 -0.08940554048676229; 0.013465871212582376 0.02129030096140202 -0.07267915575089075; 0.013845379308295307 0.025542086504484224 -0.0902320452282695; 0.008493632520462467 0.014676650984398933 -0.06101852938252988; 0.0025649015212426533 0.007113697093120448 -0.021605629530834593; 0.0012151487424118797 0.0028650340906674976 -0.01013676813523734; 0.0012336339067043271 0.002229013060652839 -0.005362868435793438; 0.0007065651706635768 0.0019797514487272998 -0.0063334354196661145; 0.00042038869230288304 0.00028519967018456104 -0.0008400144585131728; -0.0009677853581890427 -0.001605855567928794 -0.0008553268510263414; 0.00043958884843309015 0.0024785459434695325 -0.005221063848656322; -0.0011305575379052702 -0.0022363456904293698 -0.008545766127484578; 0.006367971250377752 0.025923091135504346 0.0011213210505379174; -0.000175248220011484 -0.0013406910281635368 0.002434808656863641; -0.011221794098230832 -0.0017894409878878208 0.010881513774242716; 0.0012503391867120213 -0.029811818217274858 -0.009259133157799837] %
+
+Mass Used: 93.76288389137744 kg
+Launch C3: 96.19333472804641 km²/s²
+||V∞_in||: 2.9989514957889936e-8 km/s
diff --git a/archive/ES_0.5613643909537877 b/archive/ES_0.5613643909537877
new file mode 100644
index 0000000..abb790f
--- /dev/null
+++ b/archive/ES_0.5613643909537877
@@ -0,0 +1,22 @@
+archive/ES_0.5613643909537877---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:52:35.561
+Launch V∞: [7.752891852547246, -6.245647433997948, 0.01387875594707576] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.357728380145798e-8, 2.3823085373845934e-8, 1.2074357940852043e-8] km/s
+ V∞_out: [1.9030513143519377e-8, -1.731958730426685e-8, -1.1005204179255128e-8] km/s
+ time of flight: 1.7481279093494716e8 seconds
+ arrival date: 2029-11-27T19:59:05.561
+ thrust profile: [0.15754222892537292 -0.01754321720659731 -0.06580775765380177; 0.06633092538785844 0.024002242292225365 -0.0875702551603984; 0.03907985011748081 0.022286462575498826 -0.08708309705476565; 0.034480568880870276 0.02488605756851304 -0.10886141679243845; 0.030377084560483672 0.025523401320510414 -0.12352462639457071; 0.025017926719387983 0.021804336116338353 -0.12295106697916684; 0.027791017510561775 0.02704128593231932 -0.17002730621361914; 0.010655920516349629 0.010581293275696171 -0.07000284372762512; 0.00467415381637527 0.004661302885171883 -0.034350126694589186; -0.0009713748045339717 0.0006716135484659955 -0.005124750270285626; 0.003052958786455018 0.006612117352120581 -0.03876735411882688; 0.0007240686031410529 0.0008396923225787462 -0.0072703268262216455; 0.002038974899291402 0.00021146060065423329 -0.0005210964065935032; 0.00035096632606330274 -0.00121330776994218 -0.002184900268087413; -0.0015631203501871196 0.0006173092229716849 0.0009370067784261081; 0.0005356621632473409 0.00017714245224082327 0.00012361985399562308; 0.00010113804412335522 0.0002589991499644743 -0.000668097133650705; 0.001147232554260381 -0.002448404859620074 -0.001435049171724339; 0.0007614171131082428 0.0008079798280967334 0.001821054063504251; -0.0001849577184859113 4.329312849001173e-5 0.0004115281469313607] %
+
+Mass Used: 76.75057613878835 kg
+Launch C3: 99.11563656696525 km²/s²
+||V∞_in||: 2.996117741075444e-8 km/s
diff --git a/archive/ES_0.561369946967653 b/archive/ES_0.561369946967653
new file mode 100644
index 0000000..94c761e
--- /dev/null
+++ b/archive/ES_0.561369946967653
@@ -0,0 +1,22 @@
+archive/ES_0.561369946967653---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T16:18:44.234
+Launch V∞: [6.471224072705012, -7.367911074592437, 0.256825043848056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.109838126537048e-6, 4.823672299146864e-6, 5.472874686129661e-6] km/s
+ V∞_out: [7.506878448965651e-6, 4.788244161707253e-6, 1.511871452308835e-7] km/s
+ time of flight: 1.8749577787331054e8 seconds
+ arrival date: 2029-04-08T18:28:21.234
+ thrust profile: [0.2951031424863178 -0.06999482328318381 -0.09766126789759616; 0.09867330385643464 0.028976155817983885 -0.09996554637002816; 0.12155510006454341 0.06897904764891209 -0.203847117403003; 0.04726355494600957 0.035593688410583545 -0.11393733285558112; 0.04692551684862384 0.04317332817318713 -0.1454883411465076; 0.03065164179456707 0.0324862981928849 -0.11659376454919478; 0.009651683538434637 0.011264172659499479 -0.04473628758847469; 0.00814945723896439 0.01045468295646396 -0.042661219112629184; 0.0016596501327981455 0.002915976490920868 -0.012800020242549713; 0.0011006848365314877 0.002463388602811265 -0.009476691917253394; 0.0010189733309492856 0.0013327598763412175 -0.0005433946000298336; -0.0004359736749076761 0.00033162207656461907 -0.002217792706712587; 0.0002298615066661927 -0.00016966309465644438 0.00019411263448369798; -0.0002040153285278232 0.000254608320587434 -0.0031277224112474405; 0.000160660810697728 -7.970650977264171e-5 1.4970110865043166e-6; -0.0001601446015605944 0.00036762782256399883 -0.0017034717661216794; -0.0003708096770135733 -0.00026638753957750766 0.0008347117529643817; 6.905773391386994e-5 0.0005032547331915274 -0.0027957052245648054; -0.001791523969648891 0.0009867726709345166 0.0017509856629097328; 0.0012589540423724086 -0.0004856230066743555 -0.0007018939866754526] %
+
+Mass Used: 93.59685818072512 kg
+Launch C3: 96.2288137054063 km²/s²
+||V∞_in||: 8.906773684059075e-6 km/s
diff --git a/archive/ES_0.56136998267924 b/archive/ES_0.56136998267924
new file mode 100644
index 0000000..bb09fb5
--- /dev/null
+++ b/archive/ES_0.56136998267924
@@ -0,0 +1,22 @@
+archive/ES_0.56136998267924---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:27:48.110
+Launch V∞: [7.4007561349465085, -6.068087536181799, 0.35043303498792727] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1561351158241293e-9, -5.432593965305505e-10, -2.343449053486046e-9] km/s
+ V∞_out: [-8.66351998832966e-10, 2.7778686439361292e-9, -4.429133685430984e-10] km/s
+ time of flight: 1.8749577787449795e8 seconds
+ arrival date: 2030-04-23T13:37:25.110
+ thrust profile: [0.6510895389887235 0.05373733196089762 -0.16335928010350545; 0.1483760128635155 0.11498933844020838 -0.12871644081729983; 0.08072568937300513 0.10448364833588564 -0.1342995951475294; 0.050324813535597375 0.09194130664222307 -0.1280091368103711; 0.03019148905588411 0.06860807888711835 -0.10533640696285337; 0.013039728704392479 0.037419068357025645 -0.06528966371089859; 0.007905573337765506 0.027999513389647974 -0.051844894767263054; 0.004495806037658923 0.019377805746172674 -0.038607684043668745; 0.001365677629914807 0.00724097238000661 -0.015490399133068046; 0.00012907632884100038 0.0014743466200299788 -0.005355546360987224; -0.0007650237885126023 0.000990785287442853 -0.0019039631344437815; -0.00037606128947594817 -6.594999994460757e-6 0.00033901295178824867; -6.379633892923117e-5 0.002406875224307156 -0.0019802696998186633; 0.0018401666977067273 -0.0008904389612343342 -0.0011032766295841386; -0.0024621239199355285 -0.000593881553539779 0.0002133479317712266; -0.0011106695786570135 0.002321821732614142 0.0014661895588370698; -0.0013282545490768487 0.0003139338502212848 -0.0015666981640433996; -0.0014323602947234814 0.0021073549227986575 -0.002059814044870963; 0.0002511120439200187 0.0001105196561569557 -0.0009606100188019065; -3.3255953758741166e-6 -4.7986136048303995e-5 0.00013508621112994943] %
+
+Mass Used: 119.92350713072256 kg
+Launch C3: 91.71568102772413 km²/s²
+||V∞_in||: 2.6689946879387105e-9 km/s
diff --git a/archive/ES_0.5613822081311345 b/archive/ES_0.5613822081311345
new file mode 100644
index 0000000..2ecd83d
--- /dev/null
+++ b/archive/ES_0.5613822081311345
@@ -0,0 +1,22 @@
+archive/ES_0.5613822081311345---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:03:36.945
+Launch V∞: [7.784359111448898, -5.7874881933943705, 0.004300334917825836] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03859261495915336, 0.24621825999303523, 0.25996811318019] km/s
+ V∞_out: [-0.06186775925855679, 0.05478005431353128, -0.3487891651037608] km/s
+ time of flight: 1.8749577787412062e8 seconds
+ arrival date: 2030-04-22T10:13:13.945
+ thrust profile: [0.4271974511651585 0.02022192341368151 -0.11644460372729899; 0.17256809963617356 0.118924886595958 -0.16100697735235658; 0.05829408623223128 0.06606102843422383 -0.10553051287789768; 0.04331126535812094 0.06685701649210284 -0.1186854701317342; 0.022530600945686752 0.04532135848821401 -0.08877127382158347; 0.013861322330033335 0.03434087243326146 -0.0736605194239373; 0.007751874663057866 0.023219534041108266 -0.053316642781311395; 0.005528228024953827 0.017708133036723486 -0.04290989826062801; -6.128170054924605e-5 0.014178728408213114 -0.0384091464028432; 0.0021417777054072856 0.0043092156016895705 -0.01922463530096798; 0.0013272721289907408 0.0069231596772513105 -0.006656789495563101; -0.0027170599455412356 0.0006423208799758474 -0.0024372423183575192; 0.0016951945821000625 0.005475243850870231 -0.0018992813038772294; 0.0012004400537293336 -0.0002799608497559326 -0.0033171455591608275; 0.0007474103621773834 -0.001736324665408251 0.005122329536014632; -0.001393482789149588 0.00018887610672357435 -0.006187591706190401; -0.0017514436131396338 -0.0004819706692913747 -0.0023889843052725666; -0.005737765550549439 0.003654518701289308 -0.009312355742411222; -0.004266755278506106 -0.0038813029174131946 -0.005675029075541006; 0.012336041380638126 -0.002764361553081955 -0.021219243415723187] %
+
+Mass Used: 106.08008115057373 kg
+Launch C3: 94.09128485755713 km²/s²
+||V∞_in||: 0.3601336437405584 km/s
diff --git a/archive/ES_0.561389256831013 b/archive/ES_0.561389256831013
new file mode 100644
index 0000000..2849fa4
--- /dev/null
+++ b/archive/ES_0.561389256831013
@@ -0,0 +1,22 @@
+archive/ES_0.561389256831013---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T15:04:45.268
+Launch V∞: [7.998499983349984, -5.71729752481969, 0.2335219431559877] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2435397673879399e-9, -3.3681655516577696e-10, -1.5989392913599282e-9] km/s
+ V∞_out: [7.667702114570904e-10, 1.5213174656903795e-9, 3.993944702217392e-11] km/s
+ time of flight: 1.817545989222141e8 seconds
+ arrival date: 2030-02-13T06:28:03.268
+ thrust profile: [0.32926383429072964 -0.013877709346147092 -0.09975386756075093; 0.07584057459679842 0.03967092762859838 -0.08183866480531363; 0.03942098391955241 0.03387766847465679 -0.0772621422303295; 0.04188219628895246 0.0472762641780104 -0.11784429528207359; 0.02042428431018451 0.027336948960409342 -0.07714373830935597; 0.01805304809852783 0.030485219917891316 -0.0901509621659495; 0.015226349647243039 0.027972635364228077 -0.08884669321209313; 0.006062558927324724 0.012482539629047846 -0.04272952701908191; 0.01821104598761666 0.040920144152128 -0.14597617048625372; -3.766505013867423e-5 0.00010227235854517785 -0.0048798929146920255; 0.0031840994063848937 0.007184587961864359 -0.028847325833628246; 0.0008819181183369871 0.0019480514558704687 -0.010108665438587032; -0.000515335627103605 0.0007426167438141908 -0.0009296631898071017; -0.0014287776572567104 0.0007376651115991405 0.0022526454785102715; 6.47263151462024e-5 -4.357186503009883e-5 0.0013655200457310622; 0.0034366795289543514 -0.0010533606715841448 0.0009525335418673121; -0.0012552765516555449 0.0027927135656483815 -0.0027571290736310107; 0.002128135282718324 0.0009072243050127623 -0.0008619537632020649; -0.002362641880733386 -0.00850443382012537 -0.011489692387170895; -0.009038765267480646 0.006442442040929306 -0.011543255367714902] %
+
+Mass Used: 90.7656510676311 kg
+Launch C3: 96.71802546889441 km²/s²
+||V∞_in||: 2.053398013626092e-9 km/s
diff --git a/archive/ES_0.5614044193796155 b/archive/ES_0.5614044193796155
new file mode 100644
index 0000000..f0b67c5
--- /dev/null
+++ b/archive/ES_0.5614044193796155
@@ -0,0 +1,22 @@
+archive/ES_0.5614044193796155---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T20:39:48.535
+Launch V∞: [7.459671623866581, -6.056109643500519, -0.08943442486272365] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.073144882292895e-7, -4.598755920431363e-7, -6.119636267540692e-8] km/s
+ V∞_out: [-1.4418848768730761e-7, 6.987212006189842e-7, 1.8637901036634562e-6] km/s
+ time of flight: 1.8749577780629265e8 seconds
+ arrival date: 2030-04-25T22:49:25.535
+ thrust profile: [0.7219843274930875 0.006232222724557881 -0.21301827062170006; 0.1427854141783336 0.0800141095350859 -0.16503117234481385; 0.04628952020744049 0.04019478156294604 -0.09968624973945929; 0.028049105342127807 0.031744432701439236 -0.09029431643515391; 0.030776563851988063 0.0426816668135916 -0.13260100894941754; 0.017429175325579985 0.027475310300184096 -0.09549680969303843; 0.0036195750330001992 0.0059279404972093115 -0.023540568044118474; 0.003363318296588318 0.006326365391650723 -0.02641930766756247; 0.0023172596743107846 0.004844025455586771 -0.021142600271700788; 2.2471442096660755e-5 0.0009448319860539921 -0.004548949899850038; -0.00032820008680992975 0.0015280264126993075 -0.005805635234189059; 0.00044166221686503613 0.0008985250201176524 -0.0035724954823007794; -0.0002667124647536878 0.0006073697495856513 -0.00429308025197689; -0.00027699150057714037 0.0003955477317123496 -0.0017628000233808018; 0.0007050170511732213 -0.0011561501874298259 -0.0017255923976044825; 0.0012143333051144204 0.003079360243499448 -0.003219612534335262; 9.438396997251081e-5 -0.001304551578800927 0.00043184496384943497; -0.001088020378046337 0.0019869881608027967 -0.0007086339723491264; 0.0011719780749516948 -0.0007990895835511067 0.00048635136662727443; -0.00010801899953754568 -0.0003286289116629815 0.006862145797997787] %
+
+Mass Used: 116.37337022238853 kg
+Launch C3: 92.33116326637078 km²/s²
+||V∞_in||: 5.564824791827278e-7 km/s
diff --git a/archive/ES_0.561405153666095 b/archive/ES_0.561405153666095
new file mode 100644
index 0000000..e4298d2
--- /dev/null
+++ b/archive/ES_0.561405153666095
@@ -0,0 +1,22 @@
+archive/ES_0.561405153666095---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T07:09:00.008
+Launch V∞: [6.629682295098582, -7.35169223951311, 0.21235550018225513] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.033157923756986e-7, -0.00024064192253700655, 0.00016269640646655645] km/s
+ V∞_out: [0.0001495645444969765, 0.00024390254349346713, -4.934495396400101e-5] km/s
+ time of flight: 1.8749577786871368e8 seconds
+ arrival date: 2029-04-09T09:18:37.008
+ thrust profile: [0.1905337515558702 -0.05016160204275559 -0.06764835758845034; 0.09511651754062003 0.024768332805403814 -0.10109048863146046; 0.046209065284258874 0.02337772349515146 -0.08759915711782178; 0.054886165056937414 0.03662384958559283 -0.1419930851708108; 0.03856912863300944 0.0315129334511786 -0.13102601985881698; 0.02821838059876461 0.025982836215980083 -0.11134969034892316; 0.024844933502978322 0.025548987087522894 -0.11820613341442132; 0.012912596130026552 0.013512479505176023 -0.0683627844290011; 0.004641993839566011 0.005932597309747751 -0.03005066656795482; 0.00017959861309509422 0.0005669595323481605 -0.0018408808448745386; 0.0013319321444805264 0.001955991927246213 -0.01026328006093897; 0.00012307101433594434 2.8791221917340043e-5 0.0003152828421318144; -0.0003786044489317069 0.0004942606498722408 0.00017661088314654077; -0.00027603786231395627 -0.0005188626509555309 -0.00038090878067880806; -0.0007509799101727417 -0.0003679418763713505 5.911659210533092e-5; -0.0003792594079492605 -4.299827828578557e-5 0.0006706394098323068; -0.0008530946510208804 -0.0010223360975655151 -1.1689888938853032e-5; -0.00025385020981790477 -0.0008171949607071676 0.00037121651056523403; -0.000600104817163577 0.0001314536802426319 0.0005725086979042213; 0.0023498722292722637 9.974392243410649e-5 -0.0008911480817822135] %
+
+Mass Used: 83.04257357841925 kg
+Launch C3: 98.04516097691855 km²/s²
+||V∞_in||: 0.0002904808947461802 km/s
diff --git a/archive/ES_0.5614105796247171 b/archive/ES_0.5614105796247171
new file mode 100644
index 0000000..46369e7
--- /dev/null
+++ b/archive/ES_0.5614105796247171
@@ -0,0 +1,22 @@
+archive/ES_0.5614105796247171---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T17:21:36.630
+Launch V∞: [6.501602173357481, -7.392899170805159, 0.14273308435239987] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4122702962620605e-5, 2.2644628350553926e-6, -3.7989949702433324e-8] km/s
+ V∞_out: [-2.810165222677223e-6, 5.938470767773716e-8, 1.4028004392375303e-5] km/s
+ time of flight: 1.8749577787979934e8 seconds
+ arrival date: 2029-04-09T19:31:13.630
+ thrust profile: [0.27677404007044176 -0.06925045049947859 -0.09757388874690057; 0.10137804303055874 0.026916766819126966 -0.10891749837947971; 0.04557777366261379 0.02287175965811797 -0.08491212848741488; 0.03992560672250762 0.027279841192434203 -0.10442508996632968; 0.04100519136816155 0.03399969183070234 -0.13564054605181025; 0.04818974469596258 0.04594936113989062 -0.1899052712677755; 0.011877551425670718 0.012213872978520765 -0.058274638960574394; 0.009707330438445795 0.01093993203615308 -0.055083811355110056; 0.006767940238826525 0.007813133403103918 -0.04323869928099383; 0.00039895249471021653 0.0007720794944228782 -0.00391734195995929; 0.0011709942536115912 0.0014025238066560472 -0.00790856065869337; 0.00025069544073832165 0.00022349954921941205 -0.00035074711664173067; 0.00013713647696457542 4.207234556612258e-5 -0.0005440598283115406; -0.00033302134572432555 0.0004745260695789924 -0.0002818079109380832; 0.0010921297549528592 0.0008262288488508839 0.0007158740727496431; -0.0007310153118346478 -0.0006216766424141918 0.0008588024500398141; -9.174655362282038e-5 -0.0014980602330797736 0.0013504089772664255; -0.00033053734389804226 0.0005332717733148426 -0.00021298059157895356; 0.00023353566661028714 0.00016815798341826622 0.0001322539623203878; -0.0005138994059198205 -0.001425157373834696 -0.0021055538955060053] %
+
+Mass Used: 89.45973295744534 kg
+Launch C3: 96.94616170366707 km²/s²
+||V∞_in||: 1.4303145602909812e-5 km/s
diff --git a/archive/ES_0.5614113528660407 b/archive/ES_0.5614113528660407
new file mode 100644
index 0000000..70a88ac
--- /dev/null
+++ b/archive/ES_0.5614113528660407
@@ -0,0 +1,22 @@
+archive/ES_0.5614113528660407---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T14:03:54.752
+Launch V∞: [7.714175321659197, -6.200940577010186, -0.47122668234363513] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.272355663037883e-9, 3.3212064148536273e-9, -1.899995258885872e-8] km/s
+ V∞_out: [-4.3047222371756824e-9, 1.3399575261467665e-8, -2.1385458764991442e-9] km/s
+ time of flight: 1.742279906851488e8 seconds
+ arrival date: 2029-11-20T02:43:44.752
+ thrust profile: [0.261212198413969 -0.029974875673914613 -0.10146937022480397; 0.0330301172101947 0.012774171815117981 -0.04263061265169068; 0.03852029541530665 0.025043162299467722 -0.08608724039984317; 0.03227152457549078 0.026899843523107994 -0.10321730996341812; 0.017355255062381895 0.01666672358763349 -0.072178438550762; 0.03359353929701807 0.03756321572051713 -0.167066555962843; 0.027575036498571723 0.03385824535435807 -0.16386504373723068; 0.006330699562520869 0.008069093624339014 -0.044603639054874994; 0.016903782138560603 0.023416668347702452 -0.11859660203341257; 0.0017109872657454308 0.0024077117770834456 -0.015123644038400379; 0.00193055998434041 0.002679227334778811 -0.019088194613467536; 2.855669497003029e-5 0.00018789623234003692 -0.00010891579574527963; -7.989676197004283e-5 0.0009251867637718263 -0.0012581208429462947; -0.0009328656515889102 0.0014349345812554788 -0.003748697409667388; 0.0014897661132323332 0.001452150604530445 -0.0004228411798635124; 7.400774895703188e-5 0.00013576807745467454 -0.001306371173725037; 0.00036287044617613396 -0.00047873210349457906 0.0009938085600850097; -0.00042213324754648406 0.00030320272496911407 -0.0015666860022877389; 0.0011945161784807446 -0.00030064712326005345 -0.00021201158996613748; -0.000664399245335403 0.001435802720456585 0.0026906308141597737] %
+
+Mass Used: 82.25029781586545 kg
+Launch C3: 98.18221951905979 km²/s²
+||V∞_in||: 1.9563663307631323e-8 km/s
diff --git a/archive/ES_0.5614166837532146 b/archive/ES_0.5614166837532146
new file mode 100644
index 0000000..7917947
--- /dev/null
+++ b/archive/ES_0.5614166837532146
@@ -0,0 +1,22 @@
+archive/ES_0.5614166837532146---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T01:00:02.374
+Launch V∞: [7.790317918314969, -5.9500897493660885, 0.13719960022063987] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.009366257139200515, -0.05786930448173061, -0.0641622087797754] km/s
+ V∞_out: [0.03638555102241052, -0.03003691534449773, 0.07284763199147253] km/s
+ time of flight: 1.7845513164907214e8 seconds
+ arrival date: 2030-01-06T11:52:13.374
+ thrust profile: [0.32753221038458097 -0.023497876019773108 -0.10913596629494508; 0.0990804769884894 0.047280851865787406 -0.1120137635294815; 0.08218925300119027 0.06359394281548378 -0.1611050439825179; 0.040758600505845004 0.041585369603670104 -0.12077451821671341; 0.03449854010436392 0.042477526043447164 -0.13476032039599756; 0.020735059065074363 0.02964626215726604 -0.10333185056198928; 0.009452769014024209 0.012354111786258296 -0.05378457456631989; 0.00676555358146304 0.012643390799810219 -0.04550407264722295; 0.005328767694519617 0.010706594448375423 -0.04095757931746758; 0.001300638493571516 0.002202922894172382 -0.018441149334874007; 0.0029645110585337863 0.0039571684176121285 -0.015212559055966864; 9.399814962601739e-5 0.002229053235140499 -0.003984830214136492; 0.0012211471899263818 -0.0002386498353808944 -0.0006453262756074118; -0.000634414720154948 0.004857609419546542 -3.3271114663753834e-5; -0.0009949716603610283 -0.0021599372543812004 0.0025266747412174407; -0.0008965823771695544 0.0007585053369082537 -0.0025812632123922313; 0.011799718673539529 -0.0033966071125829753 0.0020666691901420706; -0.0022092154345665616 0.011844549199147233 0.008713057999618901; -0.006734101559067859 -0.011227486321354875 0.00805142289989395; -0.002717710533177181 -0.0011210139747568097 0.0010676873035240172] %
+
+Mass Used: 94.33603507073394 kg
+Launch C3: 96.11144502423139 km²/s²
+||V∞_in||: 0.08691013870369992 km/s
diff --git a/archive/ES_0.5614250474257166 b/archive/ES_0.5614250474257166
new file mode 100644
index 0000000..93c2939
--- /dev/null
+++ b/archive/ES_0.5614250474257166
@@ -0,0 +1,22 @@
+archive/ES_0.5614250474257166---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T21:23:32.744
+Launch V∞: [7.8962797938606855, -5.884512281331019, 0.1437887257165153] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0012765974628042073, 0.0007317419052527399, 5.403422307068579e-5] km/s
+ V∞_out: [-0.0010305960036395899, -0.0006304915155847621, 0.0008393666188156111] km/s
+ time of flight: 1.7948893642322105e8 seconds
+ arrival date: 2030-01-18T07:25:48.744
+ thrust profile: [0.2663181138829427 -0.011780249869745655 -0.08527836317175982; 0.08953789925391446 0.04682587561206363 -0.0958508509614467; 0.04635832782885325 0.04011659243769857 -0.09014227397273625; 0.04379123076503116 0.05135142436044374 -0.12561583372568236; 0.03723982973635352 0.05412961543933425 -0.14453717256322177; 0.023200480960234325 0.0337837734438254 -0.09960440724724406; 0.009015230391477207 0.018781353429803204 -0.060855619273130386; 0.014665236561788942 0.029330592487425006 -0.0983771429599319; 0.00791049713598941 0.01747029277424615 -0.06277455292852636; 0.0008078554141463248 0.0018289801969479092 -0.007983472525902646; 0.00332988874215912 0.002545986784801389 -0.00718769325073397; 0.001235305897462418 0.0007991099595283982 -0.004024925021786302; 0.0003976229322883708 0.0015474579314997176 -0.0037826287611766166; 0.00044957817239661165 -0.00044541060328947174 0.0037638048152259873; -0.001074496367043147 -0.0038613554410191577 0.0011580405066934996; 0.004076184646319802 -0.002254611989842792 0.003928773962398003; -0.010536164211857263 0.004047791930678125 0.006959223953670401; -0.003446699460578151 -0.01073355278812257 -0.0018194452745431547; 0.00027166852564701406 -0.0010912909560922546 -0.0009750782584608494; 0.0031055126003639603 0.006684505093421706 -0.00881136758730828] %
+
+Mass Used: 89.16608700668667 kg
+Launch C3: 96.99939456971133 km²/s²
+||V∞_in||: 0.0014724357355089905 km/s
diff --git a/archive/ES_0.5614324384288749 b/archive/ES_0.5614324384288749
new file mode 100644
index 0000000..8868a5b
--- /dev/null
+++ b/archive/ES_0.5614324384288749
@@ -0,0 +1,22 @@
+archive/ES_0.5614324384288749---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:05:27.182
+Launch V∞: [6.322215622110724, -7.48155026199349, 0.12120204885248864] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001245990912493123, 0.0014450671293471933, 0.001284107004311757] km/s
+ V∞_out: [-0.00151941223290993, -0.0007763486788489948, 0.0016525824934393166] km/s
+ time of flight: 1.8387932561838162e8 seconds
+ arrival date: 2029-02-26T09:40:52.182
+ thrust profile: [0.3389444147622153 -0.10650385139299191 -0.13086849978061518; 0.10572660301173956 0.019505163771372583 -0.12342532780043836; 0.0790028900268037 0.03106530967400336 -0.15473291401118236; 0.07379083296301135 0.039246060551136226 -0.20221904346688227; 0.03678272833624071 0.02302692818458682 -0.12985258842237382; 0.022570744462548916 0.015886650170136893 -0.09703812263500461; 0.012392883005871509 0.009456654530537626 -0.06291390137579125; 0.0033894827400006555 0.002907008367244311 -0.02023430975165057; 0.0014334301786191762 0.001262398528136701 -0.008956105521605784; 0.0026025519024518913 0.0027267196016186176 -0.019033681245407903; 0.0004405789025496289 0.0006527932560737314 -0.0054308799139568265; 4.7170969642468014e-5 8.876482469051665e-5 -0.0015266194287180043; 0.00017642336053594844 -1.5027368669499426e-5 -0.0006835496737384908; 9.746561757625395e-5 -0.00016609351997022 -0.000671427209784514; 6.7972837290069e-5 5.882136606606239e-5 -0.0006828087856612167; -0.00016007770328007597 -0.0002694763447911642 0.00026726244639038276; 0.0001342725841393851 0.0001010938601519783 0.0009480429419948947; -0.0004650095958560654 -0.0001023803712074016 -0.00020214961918213156; 0.0001841927187534046 0.0001230262266811445 -7.134460864611196e-5; -2.1984200704137105e-5 3.5247035565344896e-5 -8.233026868180779e-5] %
+
+Mass Used: 95.24545948127707 kg
+Launch C3: 95.95869463184178 km²/s²
+||V∞_in||: 0.0022999224249651766 km/s
diff --git a/archive/ES_0.5614382670581557 b/archive/ES_0.5614382670581557
new file mode 100644
index 0000000..d31d41c
--- /dev/null
+++ b/archive/ES_0.5614382670581557
@@ -0,0 +1,22 @@
+archive/ES_0.5614382670581557---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:00:47.188
+Launch V∞: [6.597886244498757, -7.452833398926626, -0.048838130327974585] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012600732386899792, -0.00037929788368652756, 0.008590345773111898] km/s
+ V∞_out: [-0.014635515507315542, 0.00014735281675678366, 0.0042995895992665465] km/s
+ time of flight: 1.874957778323897e8 seconds
+ arrival date: 2029-04-10T20:10:24.188
+ thrust profile: [0.1350273943194193 -0.03400071449608859 -0.05248063935401373; 0.03261594505312212 0.008242511703023741 -0.03747643050940521; 0.06498047643633872 0.032571505159717185 -0.12588839929384127; 0.05457951985792811 0.03667189193126539 -0.1477539552721157; 0.04816371784185692 0.0398516224836475 -0.17054564135901723; 0.03302136392727921 0.030356680389873037 -0.14066178491585607; 0.01813720374063363 0.01805766748191109 -0.09146050476351897; 0.005263289627859271 0.00541834595622668 -0.029853028997139885; 0.004493647375760012 0.005218736871108048 -0.0294089456639274; 0.0010321131455472178 0.0012560262144915688 -0.0069810298176680545; 0.0007564538854811497 0.001040228812365263 -0.0065881637572428675; 0.00015104540848029233 0.00034535483608893764 -0.002504625307285132; -0.0008125582115943953 0.00134420939421088 -0.0029880269017964795; -0.0003401812476103909 0.001202422280862607 -0.0079151565220563; 0.0002931232415200695 0.0005896423455098285 -0.003142442498145513; -0.00047430184870546615 0.000963927450636088 -0.0006831006414681714; -0.0007859510974083308 -0.0026720718850768432 -0.000718983632528494; 0.00020307557458540136 0.0013555749552976444 -0.0008773340011629218; -0.00045671866750204404 0.00021919353958114085 -0.0028480000331982773; -0.00020509752033235837 -0.00021612843204846677 -0.0007654677806404788] %
+
+Mass Used: 77.04923147340469 kg
+Launch C3: 99.07921373047606 km²/s²
+||V∞_in||: 0.015255043889561767 km/s
diff --git a/archive/ES_0.5614479998810871 b/archive/ES_0.5614479998810871
new file mode 100644
index 0000000..a36c1d0
--- /dev/null
+++ b/archive/ES_0.5614479998810871
@@ -0,0 +1,22 @@
+archive/ES_0.5614479998810871---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T13:38:06.424
+Launch V∞: [7.632297933831604, -6.292896872560629, -0.1267217684517193] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0006083556925524957, -0.0004020207696409516, -0.025434686613703787] km/s
+ V∞_out: [0.010661230317281686, 0.01967371635061699, -0.012155031633092978] km/s
+ time of flight: 1.7070864400739148e8 seconds
+ arrival date: 2029-10-09T08:42:10.424
+ thrust profile: [0.22051068602849294 -0.031083099600603344 -0.08726190381709714; 0.09385717226603475 0.03405097028421969 -0.11197154167809101; 0.051312597144593936 0.028236278423946257 -0.11612517426949923; 0.061211980273853724 0.04227324889893182 -0.1727027582830044; 0.038474794618481904 0.03299260826629206 -0.15473530309845773; 0.017763330361716366 0.01706761568707877 -0.08831206938852797; 0.008123095462330546 0.007533363792610952 -0.04459873374571003; 0.01374438020997188 0.014701716107766643 -0.09536093073213835; 0.006626703963129587 0.006991935521137207 -0.052732025072988804; 0.004790575785145864 0.005731752564540648 -0.03475060896628992; 0.004403315322565295 0.0041687959620220925 -0.03521071511722496; 0.00044384789012586075 0.0005113013066737852 -0.004064479671453652; -6.79050583516515e-5 9.514556983007295e-5 8.681925779611748e-5; -0.0003273856069072326 -6.3855096841764e-5 -0.0004317852784017558; 0.0001424846121674184 -0.00019662228739020753 0.00038717523030303014; 5.065496291115113e-5 -1.634536160730277e-5 -0.0005439209346787107; 0.00014976038268481925 -0.00013215187031786482 -0.00022733564130094326; 3.6434702714185944e-5 -0.00020868109059674915 -6.528372713372592e-6; -0.00026615842220563174 0.00022442947825363619 -0.0003718818715562482; -0.00010126253926221211 0.0003951563861089147 -0.00046500750852506204] %
+
+Mass Used: 84.12260949262554 kg
+Launch C3: 97.86858120605304 km²/s²
+||V∞_in||: 0.02544513706949142 km/s
diff --git a/archive/ES_0.5614526850132676 b/archive/ES_0.5614526850132676
new file mode 100644
index 0000000..09d4ed7
--- /dev/null
+++ b/archive/ES_0.5614526850132676
@@ -0,0 +1,22 @@
+archive/ES_0.5614526850132676---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T14:03:40.557
+Launch V∞: [7.77166783058293, -5.8272176438950165, 0.11070159981345169] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.013404374913118572, 0.08253264284210929, 0.08521061152370382] km/s
+ V∞_out: [-0.02153133639986631, 0.019145736030571837, -0.11591594197121274] km/s
+ time of flight: 1.794558313776187e8 seconds
+ arrival date: 2030-01-17T14:54:11.557
+ thrust profile: [0.547757882978732 -0.04367866278464742 -0.17124244150392764; 0.031352565120609174 0.013774922092886721 -0.036294403271853265; 0.06961045844041368 0.05258253268846404 -0.14527840168284614; 0.039731729811263265 0.03856109551868557 -0.12011051292029473; 0.02663446150768696 0.030348907013105317 -0.10569807497088499; 0.0271158642710463 0.035524727903896776 -0.13519616759927794; 0.014677525113392688 0.02138820738450211 -0.08936317498777935; 0.0075858018467104184 0.011053737509231639 -0.049874551571926884; 0.0041004120352031385 0.006735341997341644 -0.031488088978444906; -0.00207268962555722 0.0027049933524128005 -0.004088801558146374; 0.0005952244067653155 0.0016447632497520325 -0.005751468404854507; 0.002101585906947467 0.0023358797482143402 -0.011350029587743145; 0.0005967946339244788 0.003199439917876152 -0.004694411410020136; 0.002046774028666014 -0.002374831553148554 -0.0017410326905588653; -0.0014092347724482936 0.00012560243741484376 -0.00028631638441779317; 0.010126701583986594 -0.0016630919507054811 -0.024075972042980846; 0.0007001759456369332 0.012098497946499531 -0.0027204588730618514; -0.00012935053612373425 0.00018063162075725647 0.0007462649441869213; -0.006370999544719102 0.0025712599675763604 1.4521801605112128e-5; -0.016620722616154434 0.003951707354674422 0.015618137556222818] %
+
+Mass Used: 104.55080895124411 kg
+Launch C3: 94.36754118244023 km²/s²
+||V∞_in||: 0.11938242214647088 km/s
diff --git a/archive/ES_0.5614576148211343 b/archive/ES_0.5614576148211343
new file mode 100644
index 0000000..2096b44
--- /dev/null
+++ b/archive/ES_0.5614576148211343
@@ -0,0 +1,22 @@
+archive/ES_0.5614576148211343---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:50:41.346
+Launch V∞: [7.747779548093915, -5.807875102821627, 0.04739762650859157] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.318323958392241e-6, 1.4778378108554525e-5, 4.135957093734828e-5] km/s
+ V∞_out: [3.9844373266699606e-5, 4.703620622985593e-6, -1.8331648368206168e-5] km/s
+ time of flight: 1.7837341823875973e8 seconds
+ arrival date: 2030-01-02T08:00:59.346
+ thrust profile: [0.5241662327083759 -0.02452288297961407 -0.13602061589986114; 0.1399008967714387 0.0806039129314648 -0.12944646305204763; 0.04667446626340531 0.04561718989499869 -0.0817844747400532; 0.05563469328909224 0.07236823911272539 -0.13581535162099254; 0.03404077944941046 0.05719716413894948 -0.11781699745714734; 0.014922865696769786 0.029933174718298622 -0.06838520734474779; 0.022080957697013185 0.05383577030352392 -0.12501592939679929; 0.008567596933774074 0.023604352182657648 -0.059795921115663626; 0.005133483300420903 0.016838589739684603 -0.04421093707848422; 0.002035900041683951 0.007218933364885959 -0.020618569620449893; 0.0010898884292033205 0.004843857261907759 -0.014606542933306611; -0.0001363934729043518 5.8315628000633185e-5 -0.0005646662204146057; 0.0004036626521290945 0.00017955125550630772 -0.00022241609549524097; 0.0003342038504483922 -7.642480290927798e-5 -0.0013226910867839778; 0.00020026670753858224 4.6194561623612523e-5 -0.000591174963451329; -0.00012836682259645808 0.0002501425881974785 -0.0003832367426315807; -3.7796099355124946e-5 0.00019603444854224524 -0.0004444276645820161; -0.00026738906759554996 1.8742589035659798e-5 -0.000520596623051274; -0.00014560568872071662 1.066519847674587e-5 0.00021421016181788564; -1.2656207144724112e-6 -6.36058711219067e-5 -0.0004986159531164755] %
+
+Mass Used: 108.0903558781115 kg
+Launch C3: 93.76174767083631 km²/s²
+||V∞_in||: 4.413232930007856e-5 km/s
diff --git a/archive/ES_0.561459720592286 b/archive/ES_0.561459720592286
new file mode 100644
index 0000000..5f4261f
--- /dev/null
+++ b/archive/ES_0.561459720592286
@@ -0,0 +1,22 @@
+archive/ES_0.561459720592286---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:53:11.732
+Launch V∞: [7.81636801842851, -5.614618293354957, 0.20904519601366514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2441396326227288e-8, 3.709200934511149e-8, -5.218359858453038e-9] km/s
+ V∞_out: [1.9661960853626773e-8, 4.312658828479017e-8, 1.2055973332640623e-9] km/s
+ time of flight: 1.874957778731489e8 seconds
+ arrival date: 2030-04-21T12:02:48.732
+ thrust profile: [0.6231488622829593 0.00035018279180946987 -0.1781053165242552; 0.12464756734591659 0.07458319538245979 -0.1284797443490362; 0.041440661349194316 0.04062881419266846 -0.08225098340612563; 0.05983868962651467 0.07782596037407333 -0.16955978226377844; 0.018575380883324555 0.030223963564580406 -0.07697052728970553; 0.009439142802559333 0.016519503521653045 -0.04659734178580329; 0.011275392762599153 0.01884157892995495 -0.06280256005586395; 0.0031362018070799124 0.005107212392962992 -0.018971158818248915; 0.0014860905660172574 0.0031354150805790724 -0.01600393672307157; 0.0019581881006814038 0.013211618629323314 -0.04206437044780435; -0.002701288498663606 0.007053235735301864 -0.018196120431743693; -0.00033491845075548217 0.001695372833620476 -0.006822016349139589; -0.005103175670191193 0.003197708104233033 -0.0040811182219137165; 0.004298031504432388 0.0064300386831151165 -0.008769362915797727; 5.8953717797330325e-5 -0.006795799020846643 8.814154854615893e-5; -0.0005903486251868579 0.007467791551343096 -0.006499618392021143; -0.004704937131093214 0.01474181657324814 -0.002435979442546199; 0.0021403586736494767 -0.006227142928167591 -0.0005614205911661048; 0.005106966713323356 -0.008597189991015289 -0.005906890789408804; 0.0012466801797919708 0.005157923428926169 -0.015835281979412554] %
+
+Mass Used: 114.50073042854046 kg
+Launch C3: 92.66324747356455 km²/s²
+||V∞_in||: 3.946944108315209e-8 km/s
diff --git a/archive/ES_0.5614608961885532 b/archive/ES_0.5614608961885532
new file mode 100644
index 0000000..a9c5370
--- /dev/null
+++ b/archive/ES_0.5614608961885532
@@ -0,0 +1,22 @@
+archive/ES_0.5614608961885532---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:40:20.228
+Launch V∞: [7.864483067658958, -5.974872526801592, 0.16036249202376568] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009535707929193492, 0.0006957847904599901, 0.040207687524084434] km/s
+ V∞_out: [-0.03743534779283364, -0.013258244718051116, 0.0062480586680111845] km/s
+ time of flight: 1.812172701667921e8 seconds
+ arrival date: 2030-02-09T17:48:10.228
+ thrust profile: [0.22287493876829714 -0.012347534662237508 -0.07568611169450046; 0.10892613767767129 0.05265398806698712 -0.1284023726381088; 0.06272123324130995 0.048023707759845866 -0.13051178683645204; 0.031201968791871842 0.03006794263700194 -0.09504753302137954; 0.022960395487553683 0.028037504240320844 -0.09338511509766534; 0.013404351298524507 0.019396098528240927 -0.07229853959850994; 0.012641942980063785 0.017345690263914235 -0.07528191242917842; 0.019378797463869845 0.031625428739002884 -0.13542690825106596; 0.002768189088927419 0.007225357767934706 -0.04600438777730141; 0.003080937847615102 0.0032714591389976957 -0.015437164536230433; 0.003074686582232716 0.00020869771963046176 -0.0023835602029459576; -0.0011852915336412078 0.0030038014175936554 -0.0012012474369562653; 0.00014641400494971564 9.719661673115814e-5 -0.000889322188238598; 0.0026054626856251506 -0.0013892121622620258 0.0014332831251515528; 0.008615577059132535 -0.003284121211657498 -0.000977122627997986; -0.002986608822690303 -0.0030788609361262105 0.003312326562161034; -0.0013268377815343698 -0.00014457500082940204 -0.0013844950356199158; -0.0002852464147096158 -0.0038099176187281784 0.009222001191824612; -0.0028634713927664325 0.0031446054227571626 0.012133957828215303; 0.0030262013908753096 -0.0009485781830451149 0.011555072690742227] %
+
+Mass Used: 85.85072694239807 kg
+Launch C3: 97.57491176187098 km²/s²
+||V∞_in||: 0.04022501149491643 km/s
diff --git a/archive/ES_0.5614687340958586 b/archive/ES_0.5614687340958586
new file mode 100644
index 0000000..7388350
--- /dev/null
+++ b/archive/ES_0.5614687340958586
@@ -0,0 +1,22 @@
+archive/ES_0.5614687340958586---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T10:37:10.041
+Launch V∞: [8.0030579532713, -5.549546602667367, 0.08590361300954108] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.913175986933657e-7, -5.138174478963414e-6, 9.273149853035128e-7] km/s
+ V∞_out: [-7.109139198077547e-7, 2.8550204814148046e-6, 4.318177380329509e-6] km/s
+ time of flight: 1.8749577783679882e8 seconds
+ arrival date: 2030-04-19T12:46:47.041
+ thrust profile: [0.3781040548473894 0.019197378010033857 -0.09028541454091026; 0.14352525702567082 0.09432293878001174 -0.12535932691749135; 0.11743469521557719 0.1300831159146008 -0.1800044480281703; 0.03837638349673106 0.0631802166778748 -0.1035737999056608; 0.027087493619361244 0.058771474558190345 -0.10076488296588974; 0.0156614549286831 0.04191456225030813 -0.08101276112417818; 0.005004853699870046 0.017931573928163403 -0.03597642937569976; 0.006465184371527864 0.029058109698521496 -0.06158595257350754; -0.0002712680772862812 0.006137224418128583 -0.015158205150232279; 0.0002487861015250756 0.005251645642147462 -0.008631307067803077; 0.0009961612752937372 2.527023403774294e-5 -0.0028370864917238283; 0.0014800338430213933 -0.00042745732060745075 -0.0007917658614868335; 0.0003241261910803301 -3.192216530258432e-5 0.00010787771340109876; 2.280644907537194e-5 -0.0004240260556768067 -0.0009605103777238768; 0.0018490439294374997 -0.0010725399509246571 0.0010071595157740074; -0.0034879054583141287 0.002372885898044076 -0.0010967553413251622; 0.0011058564668276192 -0.006889943348802995 -0.0015897634593512577; 0.0005514490916645408 0.0003485275207663507 -0.009837517975703654; 0.0005331339220343974 -0.002777760622212732 -0.0013402958548325429; 0.00029202022310064 0.0016209086832611607 6.697988683405953e-5] %
+
+Mass Used: 101.73311919077832 kg
+Launch C3: 94.85378352932402 km²/s²
+||V∞_in||: 5.254560548777023e-6 km/s
diff --git a/archive/ES_0.5614766066662187 b/archive/ES_0.5614766066662187
new file mode 100644
index 0000000..267212e
--- /dev/null
+++ b/archive/ES_0.5614766066662187
@@ -0,0 +1,22 @@
+archive/ES_0.5614766066662187---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T03:54:34.029
+Launch V∞: [7.9880904249913804, -5.463789851817148, 0.26644266510932485] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.491988592900184e-5, 0.0005781553499868175, 1.0597071804915467e-5] km/s
+ V∞_out: [0.0005603097391212574, -8.356686052460125e-5, 0.00012150358694046585] km/s
+ time of flight: 1.874957778747683e8 seconds
+ arrival date: 2030-04-20T06:04:11.029
+ thrust profile: [0.617634092968524 0.012410093452039724 -0.16043683869787392; 0.059411969806967356 0.03818294703602487 -0.06147732535765154; 0.048577152468645746 0.051568428307841 -0.09168208555642146; 0.020043603142862205 0.02874167306381917 -0.05827383370986951; 0.01643586269879027 0.029819838895712724 -0.06605900686272753; 0.007997004902806764 0.015786500713561497 -0.0393664030415973; 0.014019094579195698 0.04417565240839177 -0.10728154944005874; 0.006863043234233338 0.027202540956652584 -0.07487207919422569; 0.01548575302386218 0.048650695573416426 -0.13383251414425268; 0.003958606185569034 0.006643269528306023 -0.02662777799533216; -0.00012207582999677771 0.003023640511061587 -0.009974647463996884; -0.0007748692482632321 -0.0007504162839628933 0.0007441829730079916; 3.720660975670983e-5 0.00020809577755136058 -0.00038791988067589617; -0.001152052190216992 0.0008773443123035094 -0.0025995214451094836; 0.0025698893098110203 0.0010834895163037376 -0.002114495275900358; 0.0065117813508321735 -0.0038477076701227938 0.004385083064757798; 0.0056998795272228675 -0.0033751173194538787 -0.004303843252416591; -0.0016277289968419247 0.004056572935971564 -0.0004646416838702458; 0.00016460500330154823 0.0015800945878896452 -0.00041042527547571024; -0.004791750997046027 0.00561791300460265 -0.0029137485532845587] %
+
+Mass Used: 108.27682516463256 kg
+Launch C3: 93.73357987644958 km²/s²
+||V∞_in||: 0.0005787891735026948 km/s
diff --git a/archive/ES_0.5614851671179151 b/archive/ES_0.5614851671179151
new file mode 100644
index 0000000..ff7c31d
--- /dev/null
+++ b/archive/ES_0.5614851671179151
@@ -0,0 +1,22 @@
+archive/ES_0.5614851671179151---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:38:55.233
+Launch V∞: [7.861352339066267, -5.6335614125740525, 0.16193601646599587] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011992708472225602, 0.07661367917351526, 0.0968012569231967] km/s
+ V∞_out: [-0.04479481718698607, 0.05248947233332753, -0.10464449280630929] km/s
+ time of flight: 1.8749577787396753e8 seconds
+ arrival date: 2030-04-19T13:48:32.233
+ thrust profile: [0.4811268528172327 0.029906143389745073 -0.10291401552968554; 0.156042541769728 0.12251759874589699 -0.12914684381363087; 0.05601288612076127 0.07095231575434288 -0.08604405186164395; 0.046832421624640866 0.08685226224858125 -0.11416352125353404; 0.02621473749848897 0.06438726507902647 -0.09300959164694649; 0.016018911451301025 0.04948148607852122 -0.07804205905864302; 0.005198153287462788 0.019720795872752446 -0.03387956745501242; 0.0032565545484757297 0.01579690933577747 -0.028769541586475645; 0.009089165281829851 0.06671140260787002 -0.11410758646478686; 0.00150987762436131 0.015869668718182708 -0.03162851599721927; -0.00015732886469377243 0.00042907303424185987 -0.0010144316194503791; 0.0003665600541197506 0.0006322762941283657 -0.00102668236706653; 0.00029048187261859266 4.657017354606045e-5 -0.0004036534258709641; -0.00011571398687641103 -3.9479380231876996e-5 -0.000505248108756654; 0.0001059029634556132 0.00041364442728778763 -0.0011316240146450316; 0.00025419935678115907 0.00011710685299146553 0.00042973697210026254; 2.617011745203725e-5 -0.0012207201498340729 0.0005049362460902429; -0.00045360769058850866 -0.0001468207967525617 9.563893163431429e-6; 0.0007736588723686247 -0.0001420790992124934 1.008741469970295e-5; -4.687916040865603e-5 0.00024209506631962574 0.00013130027040077284] %
+
+Mass Used: 109.27545627814743 kg
+Launch C3: 93.56409806161489 km²/s²
+||V∞_in||: 0.1240321096930664 km/s
diff --git a/archive/ES_0.5614936806981767 b/archive/ES_0.5614936806981767
new file mode 100644
index 0000000..f7227c8
--- /dev/null
+++ b/archive/ES_0.5614936806981767
@@ -0,0 +1,22 @@
+archive/ES_0.5614936806981767---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:17:47.977
+Launch V∞: [6.515994996743471, -7.3130164271715214, 0.12196386762735013] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.197905813107159e-10, 3.0523812326188667e-9, -2.6784359997682476e-10] km/s
+ V∞_out: [-9.376265561283721e-9, 2.2558959940192593e-8, -1.2899114028420894e-8] km/s
+ time of flight: 1.8749577787473306e8 seconds
+ arrival date: 2029-04-08T17:27:24.977
+ thrust profile: [0.36869595501921154 -0.0926013792322371 -0.12508046932709754; 0.06377623253763297 0.01731407639709199 -0.06963564570421252; 0.07817298469293141 0.04137291733713278 -0.1398056318335245; 0.046642444966980806 0.032972049462289155 -0.11898644914365507; 0.04755913893210655 0.040735916151302516 -0.15378811960931002; 0.01950179915005531 0.01920342531011251 -0.08069256434712652; 0.00885168731762276 0.009789337995412453 -0.04574754187599064; 0.009616873362539914 0.01228164965617625 -0.05365001425828682; 0.016494219864813142 0.02196769886694644 -0.10338982442558131; 0.0015829121319408223 0.0023671753238689924 -0.011602583807120476; 0.0006606165041291313 0.0010215411165427142 -0.005559339865818544; 0.00012979980879684218 0.00010146829813644103 -0.0007535338224245521; 2.0413726832976695e-5 0.0001173468391328448 -0.000489655114344122; 1.4366670894404014e-5 4.518276336798443e-5 -0.0002138643667431709; 0.0007212454005462274 0.0005403803122483586 -0.0007859183183330971; 0.00011013315596860413 0.00024934603696915463 -0.00023043001330408662; 0.00031754467285935667 0.00017698267817225862 -0.00020148364137234051; 0.0002587142700248901 0.00045539272935066005 -0.0002222801826294754; -1.941152202661274e-5 5.447337541792849e-5 -4.182486087741686e-5; 1.263984558341794e-5 1.8608362222498342e-5 3.562096184989963e-5] %
+
+Mass Used: 95.34852187561319 kg
+Launch C3: 95.95327524667309 km²/s²
+||V∞_in||: 3.0807527325618757e-9 km/s
diff --git a/archive/ES_0.5614943345055619 b/archive/ES_0.5614943345055619
new file mode 100644
index 0000000..1aaa243
--- /dev/null
+++ b/archive/ES_0.5614943345055619
@@ -0,0 +1,22 @@
+archive/ES_0.5614943345055619---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:52:43.350
+Launch V∞: [7.802867831404563, -5.874189653315048, 0.15294011386126002] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0018004460646538962, -0.0011968615054000391, -7.527820534944191e-5] km/s
+ V∞_out: [0.0015666589530437206, 0.0007132186501688284, -0.0013061742384653753] km/s
+ time of flight: 1.8186213337589222e8 seconds
+ arrival date: 2030-02-15T13:08:16.350
+ thrust profile: [0.4030176839482635 -0.0031520133051162673 -0.12068452797779912; 0.08612094210805453 0.04824766245423653 -0.09509863144183023; 0.06660026558539842 0.061388858923434576 -0.13010769556687976; 0.03444086368471491 0.040514081203371924 -0.09974349282215021; 0.024713787225984395 0.03692061335706092 -0.09715930244771408; 0.015080587280347512 0.026252429640282255 -0.07719328173761408; 0.012729921726470165 0.02549056318395764 -0.08060767003049041; 0.008128843861743914 0.018041647693963415 -0.0615322934085763; 0.00909016724553595 0.023611734633510247 -0.08117586231741546; 0.0009242796214219086 0.005462367248945267 -0.020374332953053537; 0.0010602394288817092 0.003995578846398167 -0.009738977555472844; 0.0005620761398477432 0.0006768283468669502 -0.00190385389891612; -0.00041152715372799395 -0.00023413121428113304 -0.0006279968708263314; 0.0009376102397730128 0.004888051401767468 0.000937573499089293; 0.004291137925101801 0.002733723758468181 -0.002952451601635247; 0.00014578448508925705 0.015562883082622828 -0.0013557788628688608; 0.006487544306976014 -0.007122252248792147 -0.008247784048994122; -0.012233964521491192 -0.0005936816934418352 0.0015247930508155549; 0.0019340073128745355 -0.0032201434274565423 -0.0040364219530553795; 0.0039925845853564165 -0.007403641975237981 -0.011400930794095982] %
+
+Mass Used: 98.4936501803495 kg
+Launch C3: 95.41424115590961 km²/s²
+||V∞_in||: 0.002163273053277552 km/s
diff --git a/archive/ES_0.5615204119681672 b/archive/ES_0.5615204119681672
new file mode 100644
index 0000000..776f084
--- /dev/null
+++ b/archive/ES_0.5615204119681672
@@ -0,0 +1,22 @@
+archive/ES_0.5615204119681672---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T19:41:46.815
+Launch V∞: [6.577267245812723, -7.4457070183313805, -0.37505424366429646] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.799932578168244e-9, -2.3851729817266175e-9, 4.068480734156189e-9] km/s
+ V∞_out: [1.6435166821070069e-9, -3.745191723617186e-9, -5.205638362335402e-9] km/s
+ time of flight: 1.874957777853782e8 seconds
+ arrival date: 2029-04-10T21:51:23.815
+ thrust profile: [0.15168037997906955 -0.0416829298142705 -0.061164498892178364; 0.05540036981179399 0.01259413124660642 -0.06690842478897573; 0.06780192211845396 0.03081690600709517 -0.13763593089789128; 0.058577528933964895 0.03558234878029463 -0.16685665574158312; 0.041080595792650325 0.02990910001232707 -0.15121947712646952; 0.029667359099704586 0.02447100252316168 -0.13325155914235054; 0.01641653798778911 0.014845666961776109 -0.08706469266985066; 0.00515517539676448 0.004678214866493596 -0.03026825680716001; 0.0032295927570035435 0.002913793242831561 -0.020158992162418742; 0.0007860837774972755 0.0007853083224423965 -0.0055300121131258585; 0.0005760024180826301 0.0006153207873763697 -0.0039804278426732185; 0.00019000601220638266 0.0003493170283887072 -0.0022676968263409527; 0.00018175933993639634 0.00017073623960641148 -0.0016938649720805825; 0.0001426220640475331 0.00013078793660087096 -0.001367514372971463; 0.0005513633855649439 0.00012669917381516623 -0.0014826559325244774; -0.00025495605530773526 0.0003497564455810715 -0.0004252257804586077; 1.3691569084866174e-5 -2.0638594594446502e-7 -0.00015844749131749736; -0.00046412956144755574 7.431517306934893e-5 0.00019627485274348718; -0.0001458976797830227 0.00033038922041598185 -0.00020678938095057347; 0.00041297714450575515 -0.00010737477810653898 0.00018853342547945717] %
+
+Mass Used: 78.54244581325793 kg
+Launch C3: 98.83966311136065 km²/s²
+||V∞_in||: 6.729111263155007e-9 km/s
diff --git a/archive/ES_0.5615217095372178 b/archive/ES_0.5615217095372178
new file mode 100644
index 0000000..8a0b703
--- /dev/null
+++ b/archive/ES_0.5615217095372178
@@ -0,0 +1,22 @@
+archive/ES_0.5615217095372178---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T03:50:25.411
+Launch V∞: [7.841740512652765, -5.665921411843768, 0.0642347895226198] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3178698801380523e-9, 1.819082850796035e-9, -1.1702346754585653e-8] km/s
+ V∞_out: [-3.563263728614808e-9, 1.2331724475133583e-8, -1.8387140224282529e-9] km/s
+ time of flight: 1.8163190007630998e8 seconds
+ arrival date: 2030-02-09T09:08:45.411
+ thrust profile: [0.5372531908888514 -0.016026657720510946 -0.1480938815494134; 0.13206868928905224 0.07610180762426855 -0.12897357397876352; 0.09098079069888015 0.08765839118017557 -0.15996979124088748; 0.049270965031711085 0.0639107854019743 -0.1305357262275298; 0.026577714386263662 0.042471306660552814 -0.09691433580687714; 0.010785203022555997 0.021787530403159346 -0.052057336913861045; 0.01599218172803367 0.036061094291841435 -0.09288174217764994; 0.007924238416222779 0.02158917087529485 -0.058649776995725246; 0.0010562084909270697 0.0034186985988978458 -0.01026034857203276; 0.0014168946243340807 0.003918961115742957 -0.012579211884121007; 0.0009626140788889237 0.003799567309518063 -0.011402041351130958; 0.0002028277005760576 0.0007125859049203504 -0.0027724095719874977; 3.3513664800992826e-6 0.0003112917888131721 -0.0016654338776952366; -3.668125489690046e-5 -0.0008853133358925113 -0.0035762890936271506; 0.00022407810507003877 -0.00032514534325388635 -0.0018255915067729792; 0.0006497335351899167 0.0005379509951753787 -0.00493599757364908; 0.0018296537579236528 0.0024474361819283624 -0.0009646068685483738; 0.0025343964086834824 -0.0023038241013564006 0.002440534361846266; -0.0025875202122154772 1.2630403115251702e-5 -0.00023179485815818471; 0.0003382057509495383 -0.0019335784986813103 0.0013184533312725335] %
+
+Mass Used: 109.11049383668706 kg
+Launch C3: 93.59968582115435 km²/s²
+||V∞_in||: 1.1915987705750484e-8 km/s
diff --git a/archive/ES_0.5615275168562678 b/archive/ES_0.5615275168562678
new file mode 100644
index 0000000..02c0199
--- /dev/null
+++ b/archive/ES_0.5615275168562678
@@ -0,0 +1,22 @@
+archive/ES_0.5615275168562678---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T11:58:00.372
+Launch V∞: [6.407550544755948, -7.462420397850944, 0.12425560825604294] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.970798267768748e-7, 0.00027170542086416927, -0.00016771421512815069] km/s
+ V∞_out: [-0.0001616430864191193, -0.00026933694195594116, 5.691544616158799e-5] km/s
+ time of flight: 1.836035399318017e8 seconds
+ arrival date: 2029-02-22T12:56:59.372
+ thrust profile: [0.2791283698279082 -0.07972007015990712 -0.10196123488079063; 0.09698819868081966 0.021830999975540392 -0.10586772692124036; 0.058731890933438405 0.026467476464824488 -0.10668668012585505; 0.06131144436597621 0.03784393642836661 -0.1557433437820221; 0.04675524677888891 0.03475331503857098 -0.15273043098189495; 0.032042305434468676 0.027399401053145422 -0.12871025771140968; 0.018810826273672844 0.017431782458820294 -0.08744185661568775; 0.012823764303145822 0.012660545889358176 -0.06868381006685177; 0.0008498537884332382 0.0008736908119670894 -0.005418713140885607; 0.0018039038597608354 0.002219188028585353 -0.013531388489220288; 0.00028662082095169954 0.0002888686683208746 -0.0020246665038952502; 0.0003085259067197407 0.0005418149907611294 -0.0028276038672205546; -7.971418778018619e-5 6.244381293284182e-5 -0.0004884580675799952; -0.0003185265441205046 1.8150618999667774e-5 -0.0011319206416049647; 0.000733241383450044 0.0007847854084158674 0.0004243409783974662; -0.0005938016622022957 0.00019944590100803004 -6.408263571180321e-5; -5.839822727542838e-5 -9.677355151067104e-5 -0.00014280509577836232; 0.0005493173760434908 -0.0003242234249067304 0.00020410100251906107; 0.0001688474708043868 -2.0524638526527763e-5 0.0008734656741628925; 0.00015611536579490727 0.0004350346010340442 -0.00047140584372229455] %
+
+Mass Used: 90.6829101337039 kg
+Launch C3: 96.75986163404717 km²/s²
+||V∞_in||: 0.00031930006110127384 km/s
diff --git a/archive/ES_0.5615327620235092 b/archive/ES_0.5615327620235092
new file mode 100644
index 0000000..87d113d
--- /dev/null
+++ b/archive/ES_0.5615327620235092
@@ -0,0 +1,22 @@
+archive/ES_0.5615327620235092---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T15:55:41.909
+Launch V∞: [6.615219610273601, -7.259765370724737, 0.3406965593353335] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.8000455431661516e-7, 0.00012312425626416495, -8.523509241455209e-5] km/s
+ V∞_out: [-7.668849890614786e-5, -0.00012569870683896343, 2.690533588016126e-5] km/s
+ time of flight: 1.87495777874344e8 seconds
+ arrival date: 2029-04-07T18:05:18.909
+ thrust profile: [0.3204654586923912 -0.0792003959457973 -0.10572368762151295; 0.049558892482636244 0.013845880990938633 -0.050708127762968944; 0.09767751518836042 0.05309791827951288 -0.1675731781009663; 0.05612988605404799 0.04084209521183964 -0.1356747185201303; 0.059391430278514956 0.052580939346230766 -0.18438036351074322; 0.03552044518347006 0.03598285662623748 -0.13524010321089835; 0.012641246956105029 0.01414358391146339 -0.05653070332497724; 0.0026180694301501314 0.003178087778180101 -0.013359051450936294; 0.0006931991342149923 0.0011532264295430943 -0.004692201022383159; 0.0009443065479150597 0.0006819788288289161 -0.0041199227978987825; 0.00034642905912473634 0.000630548435643885 -0.003592395237695034; 0.0007083032840662471 0.000946617239960984 -0.005287472504550753; 0.0003409870095984746 0.0026784415274946397 -0.006726122176871822; 0.000993417849438463 -0.0001979606117797994 -0.0023920457343759647; 0.0005033244066958535 -0.0005258410350876136 -0.0012815617916559522; 0.0001958465614271353 0.00037980334799286094 -0.0018056425976281827; 0.00011607105800685814 0.0012244214808809402 -0.0028231067982298946; -0.0003970652867434654 0.00047240303571951235 -0.0007459108314096952; 4.982388338617763e-5 -0.0001815556299808686 0.0006160855215619886; 0.0009950322860348328 2.5957884772164614e-5 0.0010725683515363151] %
+
+Mass Used: 91.73006808604578 kg
+Launch C3: 96.58139787566543 km²/s²
+||V∞_in||: 0.00014974894945535443 km/s
diff --git a/archive/ES_0.5615464531929273 b/archive/ES_0.5615464531929273
new file mode 100644
index 0000000..22d69a1
--- /dev/null
+++ b/archive/ES_0.5615464531929273
@@ -0,0 +1,22 @@
+archive/ES_0.5615464531929273---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T21:42:57.256
+Launch V∞: [7.5846097550981995, -6.3220874113566, -0.07244335823019693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005162842789883797, 0.00033501073627440197, -0.00016572052041179683] km/s
+ V∞_out: [-0.00025796008625689546, -0.0005025847486811427, 0.00029516234857622915] km/s
+ time of flight: 1.6929591682850966e8 seconds
+ arrival date: 2029-09-22T08:21:33.256
+ thrust profile: [0.22195148498314274 -0.03572829215405371 -0.08442331392446248; 0.12896607396544 0.04392985107276203 -0.15149642469282634; 0.056360823262788254 0.032618839837332735 -0.11617208410056172; 0.04951587501567428 0.03670572464987528 -0.14412523472566932; 0.03838002823229521 0.03320394758018536 -0.14404539529007976; 0.029811022948689897 0.028791039626656755 -0.13635950306338795; 0.0159687629312017 0.016789756571681247 -0.08677872617220729; 0.017805035203144113 0.018932500292052127 -0.1080916601779779; 0.004058537822088559 0.004644065298101291 -0.02854485811927804; 0.0006778055052861175 0.0006642449770498614 -0.005079156839242796; 0.0005223156020847036 0.00017902555211152073 -0.0016148424867509614; 0.0002917062226554874 -2.220721861227406e-5 -0.0007953550963425999; -0.001634287147248161 0.0003948342870456801 -0.0012736831409392337; 0.00037575939176021935 6.094559171585906e-5 -0.0020121993628792333; 0.00018502272110399657 0.00014608429512133524 -0.001574118981634106; -0.00017836110424175648 0.0014435780590552109 -0.00050928465849916; 9.77529294658943e-5 0.00018313565311791615 -0.0003145824504168686; 0.0004119377550584637 -0.001596513474465847 0.0011369487625414354; 0.00048536545927819227 -0.0003635654907220195 0.0013435598464413662; 0.00010053189721483783 0.00035980594965287537 -0.0033157921074507316] %
+
+Mass Used: 86.385531309405 kg
+Launch C3: 97.50034241411603 km²/s²
+||V∞_in||: 0.0006373734706082649 km/s
diff --git a/archive/ES_0.5615491174746481 b/archive/ES_0.5615491174746481
new file mode 100644
index 0000000..9d4d09b
--- /dev/null
+++ b/archive/ES_0.5615491174746481
@@ -0,0 +1,22 @@
+archive/ES_0.5615491174746481---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T22:38:07.460
+Launch V∞: [7.900313110648631, -5.637496007833328, 0.14406288945171183] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.5351458506936888e-8, -1.5904057190788888e-7, 3.828509533820059e-6] km/s
+ V∞_out: [3.591095974226324e-7, -3.8653460309234315e-6, 3.8365893809169565e-8] km/s
+ time of flight: 1.8749577787395522e8 seconds
+ arrival date: 2030-04-21T00:47:44.460
+ thrust profile: [0.5095409193379863 0.0032020186505539194 -0.10583107531557423; 0.06311083701772728 0.04785120984482972 -0.05812112188259042; 0.038800729162493414 0.051002047032716484 -0.06741654129404921; 0.017408896957172813 0.030543420611642186 -0.04600304863986735; 0.03504938135122507 0.07948133637108579 -0.12071704383756741; 0.030637895883198905 0.08181791083837482 -0.1316605381973212; 0.013530452250276152 0.04929823931971433 -0.08764221752551371; 0.0030719630167346814 0.02079884754250327 -0.04364484426205927; 0.00397887869082519 0.019244062729785412 -0.03671662971765345; 0.0016842224494471793 0.021710595241218024 -0.043344828541675574; 0.002435989779471872 0.022117007462717244 -0.05296735651140909; 0.0003509261641910983 0.00025185240291280804 -0.002900899593207115; 0.0005314282641454669 0.003382594993125758 -0.0004163159693142504; 0.0004571040015236682 -0.0007658810066370118 -0.0029094664676665508; 0.0036591833265848567 -0.004000441208135047 -0.0013250020050223727; 0.0011386892156312954 0.001171904842260033 0.0002325543994653352; -0.0007979009249783868 -0.007370554848554579 -0.000819923515854336; -0.001958878783545115 -7.212412494864281e-5 -0.0013851856225030525; -0.008159348686762399 -0.007241597225027464 -0.0035413847806384734; -0.0007310468222201264 0.001678377676777318 0.0001323654959510404] %
+
+Mass Used: 105.541105216103 kg
+Launch C3: 94.21706260074053 km²/s²
+||V∞_in||: 3.831895333971468e-6 km/s
diff --git a/archive/ES_0.5615507243687177 b/archive/ES_0.5615507243687177
new file mode 100644
index 0000000..b87054b
--- /dev/null
+++ b/archive/ES_0.5615507243687177
@@ -0,0 +1,22 @@
+archive/ES_0.5615507243687177---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T04:02:57.031
+Launch V∞: [7.907333875537846, -5.883545659903843, 0.057515723313920374] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5561795749265715e-6, -1.58009660803727e-5, 0.0002969635067273582] km/s
+ V∞_out: [1.1636334501339564e-5, -0.000297038439203047, 1.3144468121839542e-6] km/s
+ time of flight: 1.8749577787487337e8 seconds
+ arrival date: 2030-04-26T06:12:34.031
+ thrust profile: [0.34845092069720407 -0.0038133035230106804 -0.12645836844353586; 0.05318030681638757 0.026222786827341076 -0.06690682705900527; 0.0333017240883277 0.025430967363640186 -0.07531025544465775; 0.03038649579004989 0.029517771193264618 -0.0997107795055094; 0.026706975466378707 0.030588131855532975 -0.11551935581239352; 0.02808967934198171 0.03718297576337985 -0.15109540206168387; 0.013663645322720719 0.019016953952687002 -0.08860666489666677; 0.003940595032041031 0.00618877042078859 -0.031862439466449795; 0.0018551147021004862 0.0036921577342418016 -0.017369163524059573; 0.0007273401386823714 0.0017776695976390916 -0.008540002598584687; -0.0009074255563307635 0.0006950420510232957 -0.01881723394924797; 0.002579564463731569 0.004892614902617165 -0.012975168043712626; 0.006132809849313621 0.0072900860774463925 -0.002097278327504457; -0.005256664540034135 -0.0024035022542911446 0.0013964286771757498; 0.0031570307309988646 0.0014399177183253241 0.0048939214654318995; -0.00017810415931751827 0.004822430093701293 0.007522485974255178; -0.0007452952927254805 -0.01301115942659815 -0.003923125902651764; 0.00015073794456576807 -0.008390329433824754 0.0038189129426883426; 0.0001514123407319636 -0.0019201058645463534 -0.0011175381754819757; 0.0027397780044332238 -0.0035808624854596176 0.00900850302858071] %
+
+Mass Used: 88.46132320616198 kg
+Launch C3: 97.14534660983004 km²/s²
+||V∞_in||: 0.00029738765366395465 km/s
diff --git a/archive/ES_0.5615564695306077 b/archive/ES_0.5615564695306077
new file mode 100644
index 0000000..1368e47
--- /dev/null
+++ b/archive/ES_0.5615564695306077
@@ -0,0 +1,22 @@
+archive/ES_0.5615564695306077---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:31:59.139
+Launch V∞: [7.477820011938685, -5.637557868274533, 0.4864774770180737] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7209163866175786e-9, -1.8910195091821053e-8, -1.2243456031948992e-8] km/s
+ V∞_out: [-1.0063197431059587e-8, 9.26446413728765e-9, 6.5429566113960215e-9] km/s
+ time of flight: 1.858820471180518e8 seconds
+ arrival date: 2030-03-29T21:26:06.139
+ thrust profile: [0.9537303460498971 0.024089547945618243 -0.19368598733600678; 0.20217566155212502 0.13630884055936113 -0.16244317326722993; 0.10990331598895584 0.1245687244049518 -0.16455189368447348; 0.041480618342442564 0.06427878347256069 -0.09814418318514997; 0.04051608781144699 0.08154807672447473 -0.1330826476568412; 0.009939435387945136 0.024907220320062203 -0.04655799825227639; 0.006809706259464927 0.021296490333533705 -0.04247935988237973; 0.0009314782006950336 0.0036608172963327372 -0.008059284807197961; 0.0004238096160225633 0.002687446499375409 -0.0058270583622988086; 0.0003689390022042123 0.002245322801390814 -0.005575967202121823; 0.00042651298419622624 0.0015927712055848417 -0.004331646504677135; 4.970465200335151e-5 0.000655052662859345 -0.0018746857133179972; 0.0004158734358285602 0.0006071133403689009 1.924295026361838e-5; 6.603654596498191e-5 0.00036602680794662197 -0.0007818851778401361; -4.9155555496547476e-5 0.00029037325550268153 -0.00040523350343340343; -0.00021319624480415267 0.0005198052995193205 -0.0004314456378656453; 1.2885496097132974e-5 0.0001853189064031684 -0.00019939225473894386; -2.230022122299683e-5 4.628844211461083e-5 0.00015027691765917583; 0.00021480028486114782 0.00030188701474194153 0.00019833962632412967; 2.8632176221529542e-5 0.0016151940337160611 -0.00025470122165796084] %
+
+Mass Used: 142.18623254138856 kg
+Launch C3: 87.93651118474064 km²/s²
+||V∞_in||: 2.2691431863149694e-8 km/s
diff --git a/archive/ES_0.561559966143001 b/archive/ES_0.561559966143001
new file mode 100644
index 0000000..e34bd63
--- /dev/null
+++ b/archive/ES_0.561559966143001
@@ -0,0 +1,22 @@
+archive/ES_0.561559966143001---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T01:18:04.990
+Launch V∞: [6.524125949665607, -7.392792099526822, 0.128272621829947] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001038608852724532, 0.0012528650079436912, 0.0010880768871117583] km/s
+ V∞_out: [-0.001233134289626525, -0.0006319091218759016, 0.0013829136522869251] km/s
+ time of flight: 1.862121887880807e8 seconds
+ arrival date: 2029-03-25T06:54:32.990
+ thrust profile: [0.2818126699701756 -0.07166065495235727 -0.0990884986032664; 0.03270667542781237 0.008819679623161518 -0.03610193784805627; 0.0504224067442851 0.026443372720795888 -0.09135132500434223; 0.07131117563189467 0.05011996893546487 -0.17796094032012225; 0.04974628064853178 0.041800099778486026 -0.1586700539300977; 0.023462434417036056 0.022831026700503826 -0.09351753423614843; 0.018402968785075056 0.02007477899968494 -0.0866418733390633; 0.013420893518561818 0.01599768151924441 -0.07298182115447761; 0.00674286181655363 0.008709773737041276 -0.04189689408154245; 0.0029600858749259775 0.004360258454514771 -0.022427721516630604; 0.0006192428295054316 0.0015853462203709557 -0.006098879787688853; -5.446055944244516e-5 0.00026510465291356425 -0.001729980287498074; 0.0012429676992013617 0.00024429320848522266 -0.0017091444537675033; 0.0001464856933083276 0.0008219515372904848 -0.0015412247556130907; 0.0003978482832334776 0.00040750084651704406 -0.0002905198625971886; 0.00011900726749189004 -0.0005976146064845655 -0.0011997893064225294; 0.00014739999166051118 0.0002854559783258064 0.00031879638059543114; -0.0005962524759392991 0.0018539638547007966 -0.000898556662067063; 0.0004188228207625556 0.00038463326362763806 0.000942787543557533; 0.00021805421624428186 0.00042551409481461747 -0.002370729171514017] %
+
+Mass Used: 87.95467875344912 kg
+Launch C3: 97.23404829943749 km²/s²
+||V∞_in||: 0.001957623658764454 km/s
diff --git a/archive/ES_0.5615627532512949 b/archive/ES_0.5615627532512949
new file mode 100644
index 0000000..e8d0c4d
--- /dev/null
+++ b/archive/ES_0.5615627532512949
@@ -0,0 +1,22 @@
+archive/ES_0.5615627532512949---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T13:48:17.808
+Launch V∞: [7.97248237802291, -5.692067584811518, 0.11416565495886939] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1804652197913077e-8, 1.0397597022368552e-7, -1.8721767226046064e-8] km/s
+ V∞_out: [1.5875872815331483e-8, -6.10988004864242e-8, -8.163267376790846e-8] km/s
+ time of flight: 1.826700373806432e8 seconds
+ arrival date: 2030-02-22T19:28:54.808
+ thrust profile: [0.32933597505948 -0.00047591482384499567 -0.09388560292696796; 0.14183372309903117 0.08821839052256922 -0.1374300374626349; 0.058138501823543125 0.060037240979707224 -0.10660448673951695; 0.03497065993949181 0.047897832163800544 -0.09469351536619854; 0.017328633763586142 0.029867569981807528 -0.0654209939613919; 0.014647368768141662 0.0321104857282561 -0.07491656719825035; 0.015025131859614136 0.04047522584678127 -0.09489445662784554; 0.009137131783620975 0.028866647736002966 -0.07521357284273406; 0.0024881723953669925 0.010425063924228446 -0.02900786213418893; 0.0033462447226763905 0.021236343601631597 -0.059918175512760616; 0.0017534929831540488 0.007427028670386247 -0.02263196007046389; 0.0008223071190922124 0.004149063204141611 -0.012274746053267456; 0.0007691992621512542 0.0015262694677426378 -0.003180225159122756; 0.0031369336245783783 0.0016784427821581926 -0.0031175767996226055; 0.0020505551496579934 0.0015370347473524666 -0.0005653144805621907; 0.0032351177765546774 0.00019417670602346658 -0.004979046648094698; 0.0009073767967910252 -0.0027872828563800115 -0.003256961168089268; 0.0009104723698289835 -0.002335024168419785 0.0010045970615642033; 0.001296763756032661 -0.0016360834940760678 0.003916716788543631; -0.0019220659983452326 -0.0003936391692873748 -0.0014255641177140005] %
+
+Mass Used: 95.31321447397704 kg
+Launch C3: 95.97314245472006 km²/s²
+||V∞_in||: 1.063054879370613e-7 km/s
diff --git a/archive/ES_0.5615662945255806 b/archive/ES_0.5615662945255806
new file mode 100644
index 0000000..808104b
--- /dev/null
+++ b/archive/ES_0.5615662945255806
@@ -0,0 +1,22 @@
+archive/ES_0.5615662945255806---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:57:58.989
+Launch V∞: [7.7117174990978, -6.0023514793145845, 0.10886733566214579] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.853851250724084e-8, -2.454441252181821e-7, 4.628160333863468e-8] km/s
+ V∞_out: [-3.8009940986716795e-8, 1.4437289700858964e-7, 2.0286346904227948e-7] km/s
+ time of flight: 1.80959493420339e8 seconds
+ arrival date: 2030-02-04T20:29:31.989
+ thrust profile: [0.27925678304863044 2.9236242961425964e-5 -0.08849432086207476; 0.18964887338089273 0.11357773320213277 -0.17178022679865226; 0.0795980310986028 0.0778936062407663 -0.13622367742067784; 0.06981509499106625 0.0928329983463249 -0.1802051165557478; 0.023291394070810892 0.037753677150775156 -0.07909147714758884; 0.012884197708759596 0.021570592379770645 -0.04615609354793618; 0.017847199858599887 0.041375321522117744 -0.09987288632579287; 0.0016779457687189237 0.005791729347786124 -0.022599692983885852; 0.006047967658625966 -0.009005807985921457 -0.025788255738521008; -0.011012540500815793 -0.002190891245702671 -0.019058794529262135; -0.0004936977899657921 -0.001225335335333417 0.0015031070100800954; 0.001540131422598215 0.00031280987887164586 -0.0004893607536453895; -0.0027382437549537384 0.0005935652440136727 -0.0031511837157117005; -0.0007228652920907035 0.0014179413155044397 -0.00145798290243676; 0.009188438318290578 0.015433568851382461 -0.017475799222505403; -0.0005649639274814273 0.0015602746795349075 0.0010209413143412865; 0.0021964231224657887 0.0017901599758727346 -0.010471009047901908; 0.0018277919227303895 0.0037833847567889448 -0.00981345280816546; 2.342417115568877e-6 0.0007846986148787357 -0.0017207638371080844; 0.0013774175211493495 -0.0036467018429998626 -0.00950352570647821] %
+
+Mass Used: 98.0151476571209 kg
+Launch C3: 95.51066216389539 km²/s²
+||V∞_in||: 2.513946143174896e-7 km/s
diff --git a/archive/ES_0.5615694670114753 b/archive/ES_0.5615694670114753
new file mode 100644
index 0000000..d462a3e
--- /dev/null
+++ b/archive/ES_0.5615694670114753
@@ -0,0 +1,22 @@
+archive/ES_0.5615694670114753---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T10:44:28.792
+Launch V∞: [7.844661454020912, -5.6909087448039095, 0.15767808602060332] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.015483491087450644, 0.09471673999179088, 0.10651368884109146] km/s
+ V∞_out: [-0.025141410845321288, 0.02269958976808768, -0.13845443929081358] km/s
+ time of flight: 1.8567462138489923e8 seconds
+ arrival date: 2030-03-30T11:01:29.792
+ thrust profile: [0.5062037123909506 0.0081029757987142 -0.11405248892431187; 0.09839188298227933 0.06709963053427395 -0.09110086402584693; 0.03885287638069906 0.04287561446902559 -0.06607955158776771; 0.03652066598629889 0.05526439266547468 -0.0929039814518637; 0.04021096253146943 0.08303082258395482 -0.14599315174224556; 0.0200832135235289 0.04822968161697605 -0.0928373228818802; 0.025295677147666312 0.07570066917127952 -0.14707353429750927; 0.002724183665640806 0.007838848269990978 -0.019441211627627228; 0.002027121821884564 0.007671924381216499 -0.01948567639128092; -0.00022021116909203274 0.0004314759205596912 -0.0012652799911163446; 0.003616424678720348 0.009429377690513264 -0.024962908225282306; 0.0006148263877549787 -0.00033852630958116584 -0.002048060257396566; 0.003321357580241864 0.0007031747276162112 -0.0016348713064738996; 0.0007098750285055327 0.003602984200464812 0.003173055058216831; -0.0005770981836989347 0.000951703015845928 0.0011213900215094217; -0.0020580156951127138 0.001000962589267828 -0.002547485001888515; -0.008947116023380601 0.004717562073635735 -0.00895538396397645; -0.0026284849355865036 -0.0033091187356391618 0.0006295317820117696; 0.0028625423186091044 -0.0016151973674184545 -0.0060130377309251856; -0.010343577412981935 -0.0020622445250154226 0.017714543151954795] %
+
+Mass Used: 107.1226062293149 kg
+Launch C3: 93.95001804869821 km²/s²
+||V∞_in||: 0.14337421400469658 km/s
diff --git a/archive/ES_0.5615750397095417 b/archive/ES_0.5615750397095417
new file mode 100644
index 0000000..11fab6f
--- /dev/null
+++ b/archive/ES_0.5615750397095417
@@ -0,0 +1,22 @@
+archive/ES_0.5615750397095417---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T08:59:22.518
+Launch V∞: [7.644721250817105, -6.075995917456105, -0.1491073100245943] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.027191073970551e-11, -1.899804283263217e-9, 5.119852269361768e-9] km/s
+ V∞_out: [1.1274750079931356e-9, -3.591547383656503e-9, 5.724665788834821e-10] km/s
+ time of flight: 1.7254975587767795e8 seconds
+ arrival date: 2029-10-28T11:28:37.518
+ thrust profile: [0.39171493551549635 -0.05020486070228044 -0.14175274357257306; 0.10710695354002676 0.04236799567849916 -0.12387233530875057; 0.08903711183211994 0.060261470145979025 -0.17996422065520495; 0.06252010738841868 0.05466988415199996 -0.18197103180677915; 0.03870765463781365 0.04029359860990948 -0.14863783325581678; 0.021526715401718036 0.025306299312874543 -0.10252164846523763; 0.008303265934961597 0.010870905930277865 -0.046626041006617165; 0.0033291562097267236 0.005174207550898082 -0.022518492184918172; 0.0035723047872025034 0.005486344549981702 -0.027590875837098468; 0.000488401855562366 0.001109126353806875 -0.010938184913146387; 0.002976752920262263 0.004715986854478925 -0.009002064324640388; 0.0016054387852583595 0.0036550838535365573 -0.010960206144008233; -0.004453991431072906 -0.0012205747454166961 -0.0013020965535130605; -0.003143279657828044 0.0009461861230570669 0.001376995021910553; 0.0002504425409268847 0.0009722111602169913 -0.005161355812543048; 0.0022419375920836463 -0.005896994988236021 -0.005993535426442201; 0.0016885696373068878 -0.0033432895880769597 -0.0028265136403767058; -0.0005985417507985108 0.0012447496313873832 -0.00021647330779450864; -0.0026052439182246596 -0.0038794546144347974 0.002060785860219176; -0.00552544329048158 -0.0001382828911515088 0.0010138647542063547] %
+
+Mass Used: 98.7774991021447 kg
+Launch C3: 95.38172238154068 km²/s²
+||V∞_in||: 5.4610493463595385e-9 km/s
diff --git a/archive/ES_0.5615837118723275 b/archive/ES_0.5615837118723275
new file mode 100644
index 0000000..847b127
--- /dev/null
+++ b/archive/ES_0.5615837118723275
@@ -0,0 +1,22 @@
+archive/ES_0.5615837118723275---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T12:16:43.781
+Launch V∞: [7.623667843051135, -6.078044251670945, -0.015358080143340084] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00011308086965916281, 0.0003124471928701258, 0.0006951241759893837] km/s
+ V∞_out: [0.0007048488456958416, 8.232033620287102e-5, -0.00028749551015887063] km/s
+ time of flight: 1.773149468390198e8 seconds
+ arrival date: 2029-12-23T18:25:49.781
+ thrust profile: [0.34877520095433484 -0.01821175442408776 -0.10093472269343554; 0.13914833427170673 0.07219694317829292 -0.13447570303586592; 0.12697968482380567 0.11160643480050726 -0.20842989995882905; 0.03146871673556012 0.03901351477714358 -0.08383925542910221; 0.03386015318830593 0.05257130140256062 -0.12367817614493334; 0.016982966901967055 0.03177253052731721 -0.0802803145114415; 0.009799787894623949 0.01910406004856635 -0.0533336179992734; 0.00496420704922453 0.014168550126246493 -0.040284729772343326; 0.008047906329918043 0.021451397514043707 -0.063746035971924; 0.003951022641138774 0.009944780761100891 -0.03639208221356116; 0.00046755186290087155 0.0001865200384254129 -0.0018480061790198889; 6.317515468692424e-5 0.0019140851845729037 -0.001891520381785947; 0.0011694277230848893 0.0031574460007708543 -0.011361045004578097; 0.0017032659991875038 0.0006786110315137744 -0.004455220610718386; 0.005393967163102849 -0.0013259634017812535 0.0005232212619782775; 0.0016133110026163488 -0.0018453819757353693 0.003780425688196731; 0.0013141575760901758 0.006855260970487904 -0.0024940736116617025; -0.001957783218761577 0.0005744927460392998 -0.0028413950769704856; -0.0024899130670835786 -0.0027277122579533104 0.004617397498960572; -0.006155526707455718 0.005684478176700467 0.000860960544556951] %
+
+Mass Used: 100.6458436514863 kg
+Launch C3: 95.06316917706785 km²/s²
+||V∞_in||: 0.0007704597013862658 km/s
diff --git a/archive/ES_0.5615843786131913 b/archive/ES_0.5615843786131913
new file mode 100644
index 0000000..df5582e
--- /dev/null
+++ b/archive/ES_0.5615843786131913
@@ -0,0 +1,22 @@
+archive/ES_0.5615843786131913---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T00:38:33.183
+Launch V∞: [6.636200438798753, -7.369414729998704, 0.16179212446187827] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.036525452115037e-8, 3.171376270270306e-8, 2.231955301736216e-8] km/s
+ V∞_out: [-1.5942748648320164e-8, 2.0469253952109238e-8, -3.6612030709707896e-8] km/s
+ time of flight: 1.8749577787482578e8 seconds
+ arrival date: 2029-04-10T02:48:10.183
+ thrust profile: [0.18426192615029993 -0.052356463079106755 -0.07397174412121667; 0.07253574615291716 0.016830554547415374 -0.09142617821977805; 0.051132086836576045 0.020633162161587906 -0.10585211184159636; 0.04535211853116829 0.025455249462818044 -0.13014261804102709; 0.040673530170051445 0.025949941649352246 -0.15187631317402808; 0.04506287890325733 0.039558227866422296 -0.19793430816151597; 0.010120205269408955 0.008411038550768697 -0.0549764081534296; 0.008283176044582192 0.007102560058232472 -0.050325076342973056; 0.0008304095422892719 0.0007125923534590143 -0.007216571388289696; 0.0011426002495032147 0.0009949160276423597 -0.007707138189445046; 2.2062167485417753e-5 0.00012299400221407557 7.417478882428821e-5; -0.000638851318567572 -0.0005106303653528179 -0.00019954211372855515; -0.00038609542187504904 0.0004095387235946784 0.0008114404191197052; 0.0006175652371971313 -0.0004162304193818732 0.0010795762208583167; 0.0007789830040275893 -0.002090107801701462 0.0006979541109474254; -8.679944706529625e-5 0.00033133095185106093 0.0011129509380957748; 0.000806397139992111 -0.00024216381888853488 0.0038042501111258072; -0.0030116305486977647 0.0028977074511043143 0.0035724995580364966; 0.00023732295471590883 0.00011133881612081153 -0.00039508177657050835; 1.224609167006026e-5 -0.0006504511721636486 0.0001393439007793927] %
+
+Mass Used: 81.33573760938361 kg
+Launch C3: 98.37360641817251 km²/s²
+||V∞_in||: 4.3802611604440154e-8 km/s
diff --git a/archive/ES_0.5615862993918079 b/archive/ES_0.5615862993918079
new file mode 100644
index 0000000..119663f
--- /dev/null
+++ b/archive/ES_0.5615862993918079
@@ -0,0 +1,22 @@
+archive/ES_0.5615862993918079---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T01:15:15.044
+Launch V∞: [6.556791787943603, -7.4530926228409236, 0.16276087211884435] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2355648738594498e-6, -1.2060112615392024e-6, -1.3709471547369996e-6] km/s
+ V∞_out: [-1.8876374211450815e-6, -1.1524387572038201e-6, -3.687632581047293e-8] km/s
+ time of flight: 1.8749577787451938e8 seconds
+ arrival date: 2029-04-11T03:24:52.044
+ thrust profile: [0.1874487462186156 -0.05025709789895657 -0.07189024405306939; 0.029461223519520525 0.0063593031288274576 -0.03555044002122536; 0.07459860200819265 0.033157514252389476 -0.1467627456946039; 0.05539946245459744 0.03259790020442657 -0.1539951481035546; 0.04263289596600154 0.02917524413023067 -0.15013820260995658; 0.022266453776392456 0.01715953720358823 -0.09916753956247631; 0.015315060625422637 0.012724769354866192 -0.07702283256955356; 0.01492770519275035 0.01334700673788787 -0.0868827098974223; 0.0010230862679779585 0.0009710742434438268 -0.007169115223407539; 0.00252397386544019 0.002498091553907622 -0.01767384697527024; 0.000550347446510956 0.00023163945068979672 -0.00473166785240996; 0.0007486304743684612 0.0009857103712289535 -0.008355644075050555; 0.0014567774417216304 0.0004549671519154658 -0.00986536545020606; -0.0005103036353091883 0.00022122041863672533 0.0003403180438464882; -9.644482575259618e-5 -0.00024368419036183234 0.0015674872647874875; 0.000257686321351961 -0.00019368325581236104 -8.994272610311836e-5; 0.00014608312837523192 4.2137496656255e-5 0.000342347995625331; 0.00010040800492701885 0.0003754897892972411 0.0006508498352879289; 0.00024305005996024646 0.001392874568966278 0.0010759598057257446; -0.0013610681992816745 0.00040059512324123526 3.1913361498154196e-5] %
+
+Mass Used: 80.2121867270398 kg
+Launch C3: 98.56659929658335 km²/s²
+||V∞_in||: 2.204672270782252e-6 km/s
diff --git a/archive/ES_0.5615908019778746 b/archive/ES_0.5615908019778746
new file mode 100644
index 0000000..3757388
--- /dev/null
+++ b/archive/ES_0.5615908019778746
@@ -0,0 +1,22 @@
+archive/ES_0.5615908019778746---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:10:29.440
+Launch V∞: [6.453663470598279, -7.395584151240041, 0.1296855664410273] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0011237836196387426, -0.00725368904353465, 0.009835531172247225] km/s
+ V∞_out: [-0.008506167718191024, -0.006962971415823595, -0.005478921642287927] km/s
+ time of flight: 1.8749577789693737e8 seconds
+ arrival date: 2029-04-09T13:20:06.440
+ thrust profile: [0.2909453694977255 -0.07531671405083593 -0.1024999780405687; 0.12128284456098411 0.03183664769807001 -0.13013524266025878; 0.07052259716047854 0.03598648174995286 -0.1286473315357983; 0.07147478760179991 0.04896881214093355 -0.18143074920301158; 0.04396008145416268 0.03629876205421145 -0.14501606737685166; 0.0183347452585934 0.017522235197261513 -0.07551652464493751; 0.012450871689090278 0.013256866066996243 -0.0608429502858693; 0.0061657798623076104 0.007150662803858549 -0.0352536097744158; 0.0040644368295690994 0.005239749016947242 -0.026786239474443682; 0.0008279144515413902 0.0007495225056191287 -0.005308572496344337; 0.0011043704388628217 0.0019216504138235416 -0.010747256395613759; 3.753966062747182e-5 8.05314116629168e-5 -0.0008401658071541056; 0.0004101178904176077 0.00045146919244658907 0.00081504476437372; 6.105565152957251e-5 -2.2495250290090717e-5 -0.0006076422015691815; -0.00070669706863031 0.0010451322450053782 0.00013595646101138403; -0.0007399974209859338 0.001321255822069288 -5.953358446899318e-5; 0.0007733490861168 0.001036157014265336 -0.0033635773452089786; -0.0010277511512937175 -0.0028369826002064436 -0.0018510271777986795; -2.4183274859729536e-5 9.388133314453762e-5 -0.00026582099805647633; 0.002946046779837013 0.0025397034230009883 0.0016803329672244467] %
+
+Mass Used: 93.0819453644749 kg
+Launch C3: 96.36125547595064 km²/s²
+||V∞_in||: 0.01227259417581751 km/s
diff --git a/archive/ES_0.5615916287042645 b/archive/ES_0.5615916287042645
new file mode 100644
index 0000000..236f094
--- /dev/null
+++ b/archive/ES_0.5615916287042645
@@ -0,0 +1,22 @@
+archive/ES_0.5615916287042645---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:09:52.653
+Launch V∞: [7.727639243697412, -5.972734508385189, -0.04599751430206521] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.2048282407778075e-7, 1.2065229435824877e-6, 3.967290957102574e-6] km/s
+ V∞_out: [3.7204526137512227e-6, 4.2700495978188345e-7, -1.8230816439375077e-6] km/s
+ time of flight: 1.8211996936912766e8 seconds
+ arrival date: 2030-02-18T20:02:41.653
+ thrust profile: [0.32545275919322586 -0.0018903615495845087 -0.09491266357967573; 0.16018179166770696 0.0921343434887502 -0.14742493096951112; 0.0721701205168522 0.07198314577695847 -0.12846493163731698; 0.023240317590614557 0.02675556262367648 -0.058082197520589275; 0.05926061323670405 0.10227153239764553 -0.22632775134383504; 0.01287970423437192 0.02423739553834229 -0.0560852296743008; 0.008138516058110558 0.017459426369758765 -0.04146709890379745; 0.008267198028108573 0.0230066536174719 -0.06329044559348714; -0.002342848167128565 0.010995863338228145 -0.030641229100398324; 0.001873273066281485 -0.0008460287795440801 -0.008362562573669881; 0.0031270272851957903 0.0004572390225745658 -0.0012923708966491058; 0.0008255682854577855 0.0008867432624412755 -0.004425851939494061; 0.0002443990853646113 0.0016463341079865513 -0.00624801723902556; -0.0015043701734487637 -0.0082805842141664 0.0022411850898394594; 0.0033305619927761283 -0.0012612999803184224 -0.004264509400048023; 0.0028428070485311987 0.005997087566674308 -0.0035861071360491995; -0.0032749859886774552 -0.0005631477843104682 -0.000376052441755881; 0.0029222003553884056 0.00805143494454522 -0.000754473345133437; 0.004691654796418582 0.01383399429844567 -0.02661137171786745; 0.00029744271152318605 -0.001313547881919952 0.0025922072272816093] %
+
+Mass Used: 98.73642439000287 kg
+Launch C3: 95.39208155970955 km²/s²
+||V∞_in||: 4.167961247065912e-6 km/s
diff --git a/archive/ES_0.561595651578885 b/archive/ES_0.561595651578885
new file mode 100644
index 0000000..34f9d34
--- /dev/null
+++ b/archive/ES_0.561595651578885
@@ -0,0 +1,22 @@
+archive/ES_0.561595651578885---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T21:10:33.498
+Launch V∞: [8.168941223832476, -5.628946642745985, 0.15003508333220264] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.329080385509782e-6, -1.939730403223405e-6, -1.9470013068662964e-7] km/s
+ V∞_out: [1.5852690157994259e-7, -7.851957897259244e-7, -2.2193936070028194e-6] km/s
+ time of flight: 1.874957778749387e8 seconds
+ arrival date: 2030-04-23T23:20:10.498
+ thrust profile: [0.20697546595249544 -0.0036612754015666873 -0.07254879491337198; 0.047213649118334824 0.02346579065658286 -0.05553257024802689; 0.03253886314562879 0.02612766310531572 -0.0682941175891139; 0.03573963153517263 0.03811385878390813 -0.11288111574992878; 0.03136881199751282 0.03991897110705816 -0.13211534664533792; 0.02507373210379954 0.03631769174726763 -0.13249100307620032; 0.012722131983687573 0.020467832757757945 -0.08137030395099368; 0.005506951544842256 0.008685137561537357 -0.03781118913421742; 0.0035028649646160707 0.005572068256267199 -0.027515265641755146; -0.0024193960220556324 0.009907875976193182 -0.006640454593006529; 0.0025207584594402863 -0.0067819083955944605 -0.008564024949907222; 0.003993650884425361 0.0040368348717473995 -0.018423481785920993; -0.0007671135626293276 -0.007800033029030654 -0.004528600509874014; -0.00960471108465531 0.015670102641461372 -0.0063277839097345846; -0.003467778817540997 -6.621738961416594e-5 -0.004199663008855919; 0.0020207073240876357 -0.004914710739394307 -0.004211107231211542; 0.0011601005327634738 0.0026759418096032207 -0.006682638249067226; 0.0016282789090369505 -0.006615176854962731 -0.023416385388674393; 0.0019169302400999372 -0.00034298655441697325 0.0005635279755608364; 0.0045840161374905266 -0.01645224125865978 0.02885372861083199] %
+
+Mass Used: 80.9665427913742 kg
+Launch C3: 98.43915155154143 km²/s²
+||V∞_in||: 2.3594314673720564e-6 km/s
diff --git a/archive/ES_0.5616024561320379 b/archive/ES_0.5616024561320379
new file mode 100644
index 0000000..a025152
--- /dev/null
+++ b/archive/ES_0.5616024561320379
@@ -0,0 +1,22 @@
+archive/ES_0.5616024561320379---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T07:11:37.724
+Launch V∞: [8.102818309153806, -5.750207936962939, 0.051037700105153634] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007522790964166132, -0.04586089455295685, -0.05051807589635774] km/s
+ V∞_out: [0.012223411325272647, -0.01108772342783014, 0.06717928987527806] km/s
+ time of flight: 1.8591834319871905e8 seconds
+ arrival date: 2030-04-06T03:10:40.724
+ thrust profile: [0.18476000353509808 -0.005123523193045235 -0.06734023713359298; 0.035275104080317025 0.01819143816957595 -0.045946128886920796; 0.034442699762847764 0.028004404420534305 -0.07908147717575587; 0.04530400616714809 0.046566531658650406 -0.14748246615316235; 0.03407328924057466 0.041676205921833784 -0.14856101926260423; 0.014228401512661118 0.019790257390861 -0.08019993087662938; 0.015253603847013344 0.023991423635133013 -0.10461899052016246; 0.0060184774810079986 0.0120664238396891 -0.05768609011958731; 0.004396381435425114 0.013109307709435095 -0.037777221151997754; 0.0019051472887022668 0.005413042089767966 -0.02144660969817089; 0.0006698187636155269 0.0028204122009946493 0.0004355027501628285; -0.0006319612561521517 -0.0007433000265927204 0.0072437801564579195; 0.0019361781123242887 0.0008165265858626938 -0.0071690075875176975; 0.0077753754796568535 -0.0077353030795183075 0.002210948237375018; -0.001005191362328575 -0.00044905245779509537 -0.0030971027122956574; -0.009064850236379637 -0.004958793665552174 0.005957417278940066; -0.0029654724489629504 -0.0028220528395283386 0.012516209977346314; 0.00628202110425801 -0.002687636625171834 -0.0009600631993628867; 0.012549986890253051 -0.005772112416625951 0.009024072330688485; -0.006166395681807707 -0.0034043960924273293 -0.006426273354359768] %
+
+Mass Used: 79.3177613089506 kg
+Launch C3: 98.72316071630175 km²/s²
+||V∞_in||: 0.06864320815170376 km/s
diff --git a/archive/ES_0.5616082453553877 b/archive/ES_0.5616082453553877
new file mode 100644
index 0000000..2b6b7bd
--- /dev/null
+++ b/archive/ES_0.5616082453553877
@@ -0,0 +1,22 @@
+archive/ES_0.5616082453553877---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T23:02:06.728
+Launch V∞: [6.569644251652669, -7.422419491728459, 0.11900276484082448] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.532961896287247e-8, 8.77472042784933e-8, 4.807657050128388e-8] km/s
+ V∞_out: [-2.785147542039075e-8, 5.565505368944101e-8, -8.693166897342102e-8] km/s
+ time of flight: 1.8749577783334818e8 seconds
+ arrival date: 2029-04-10T01:11:43.728
+ thrust profile: [0.14236675176802613 -0.03627230902101409 -0.05251339962717462; 0.11520894376105541 0.030370476395167923 -0.12617777657108128; 0.07951328997866915 0.04122464111453804 -0.1479605094097381; 0.05521133488134849 0.03761103719375082 -0.14559669639788034; 0.03704669585119124 0.030144383619048396 -0.12648716778464494; 0.021686444313465118 0.02070760838261716 -0.09072074091778386; 0.015224792839132719 0.015938679885938833 -0.0756975564856244; 0.007666877785594566 0.00868582144076839 -0.04454335063671424; 0.0051799250554522055 0.006636248641426538 -0.033144791580664204; 0.0022532148413510113 0.002936255311313964 -0.016598700259242666; 0.001011060080424179 0.0016108396007849756 -0.008374848739326392; 0.0001971893367590634 0.0012631454734582765 -0.00579243027986893; -1.908529589896604e-5 0.0001454799632798036 -0.002807921229378312; -7.699213318741266e-5 0.0010394449730883359 -0.0012080743176104917; 0.00038791802665680974 -0.0005941074106530016 -0.0005056190817582401; 0.00024788837584680977 -0.0004584045147245236 -0.0007312550851099904; 0.0010913036150350473 -0.0018147238103149554 -0.0021755711019561526; -0.0005965017860157511 0.0011071391695327056 -0.00032750631087955905; -0.002971418694283072 0.0002180652424703694 -0.0004685695926981133; 0.0001565611024313023 4.4561217076578496e-5 -0.0005544925275651445] %
+
+Mass Used: 81.9872124666831 kg
+Launch C3: 98.26669836250328 km²/s²
+||V∞_in||: 1.0984399321390205e-7 km/s
diff --git a/archive/ES_0.5616315701098538 b/archive/ES_0.5616315701098538
new file mode 100644
index 0000000..fd87a6b
--- /dev/null
+++ b/archive/ES_0.5616315701098538
@@ -0,0 +1,22 @@
+archive/ES_0.5616315701098538---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T01:18:19.219
+Launch V∞: [7.64009890589003, -5.8674597555688734, 0.11069536292940474] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.990819487555541e-6, -3.048723240602398e-5, 0.0005853661871907642] km/s
+ V∞_out: [2.6503895425093766e-5, -0.0005852601297545545, 6.143082426151367e-6] km/s
+ time of flight: 1.838684530460926e8 seconds
+ arrival date: 2030-03-09T03:52:32.219
+ thrust profile: [0.48077599099232243 0.018798134397867382 -0.11199586102676387; 0.24004632480387075 0.166802365970691 -0.1914801559306148; 0.056751897831774686 0.06518995384543576 -0.09365903534198998; 0.040536519973912465 0.0643512336070592 -0.10166498968132927; 0.023549766898993928 0.04800021364905611 -0.08367177387520973; 0.02005927986091268 0.050396402014563364 -0.0923567522663937; 0.0069319879027451735 0.022870089515269955 -0.045921305212804374; 0.006387723384307605 0.0232468960026616 -0.049228538416018215; 0.0063093547930881495 0.029656177000412412 -0.06464290539243704; 0.004466374155938362 0.018210192869044253 -0.03942662997469684; -9.628182658986669e-5 0.0006166752180248235 -0.0011614810537827524; 0.00035915954941116756 -0.000211875726344307 0.0006403088391884468; -0.0007839526450718222 -0.0010391324226304414 0.0007413830560264322; -0.000157472360873764 0.00023379797689360713 -0.0008221497866940616; 0.00022757402084120325 -0.0016857332843742431 0.000995294528319229; 0.00018122520654914815 0.00026796673729576254 -0.0007857525790035107; -0.004620232053482153 0.0039056154420650667 -0.0024660633362213647; -1.6579167362178415e-5 -0.0008785836572999339 0.002114697292578694; -0.003641801045553987 0.003384061299827986 -0.003449807915086954; 0.00035044999864662613 0.004577048972167546 0.005107130307203493] %
+
+Mass Used: 113.84254748763351 kg
+Launch C3: 92.81044873837644 km²/s²
+||V∞_in||: 0.00058616720263696 km/s
diff --git a/archive/ES_0.5616333310026245 b/archive/ES_0.5616333310026245
new file mode 100644
index 0000000..7520149
--- /dev/null
+++ b/archive/ES_0.5616333310026245
@@ -0,0 +1,22 @@
+archive/ES_0.5616333310026245---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T08:33:52.662
+Launch V∞: [7.956963166203762, -5.643496058164867, -0.016823206468983977] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.026515005454245066, 0.018766811772296606, 0.0011851071923754915] km/s
+ V∞_out: [-0.023933820441957607, -0.010776949448247742, 0.019315210696629934] km/s
+ time of flight: 1.874957778001112e8 seconds
+ arrival date: 2030-04-22T10:43:29.662
+ thrust profile: [0.4092323841440779 0.00333378792135316 -0.12590644815217308; 0.12043456646386692 0.07190157361434713 -0.1296032050202849; 0.0545436937771766 0.05342763257878854 -0.10941829028130386; 0.028788368899656157 0.03750601124422271 -0.08778311522073651; 0.023285446283090268 0.03768023013374068 -0.09706198169062387; 0.015427711071670163 0.029764672193755316 -0.08376717426054574; 0.0049505711289255456 0.012258540256500378 -0.038276394936604494; 0.006766172299455826 0.018283533308749378 -0.05819213469779922; 0.00642409202594487 0.015204083856242251 -0.0557801890875591; 0.0006098578690423875 0.00670028274992798 -0.01902044253248061; 0.0005824341441120662 0.005810269014616488 -0.004465982086609603; 0.0016093403404575566 0.006293451598868586 -0.01614125528171786; -0.0007767981970994767 0.0005802797784489921 -0.0035884127139995505; -0.0036576480245078305 -0.005248375227976576 -0.002496594656352883; -0.002832857079982689 0.004202147654453273 -0.008029127120208975; 0.0003550613797171876 0.0031416640354852885 -0.007354435639634898; -0.0011160479934591693 0.0020847532314513025 -0.008818169904428855; 0.007829606297871933 -0.013478930767047148 -0.0017529829991849131; 0.014122625817425755 0.0017064838643463297 0.005171773031529129; -0.017112621357100108 6.853435826965383e-5 0.007978495813986273] %
+
+Mass Used: 100.12375679485194 kg
+Launch C3: 95.16259360712169 km²/s²
+||V∞_in||: 0.03250604893543471 km/s
diff --git a/archive/ES_0.5616520536051469 b/archive/ES_0.5616520536051469
new file mode 100644
index 0000000..6ffce77
--- /dev/null
+++ b/archive/ES_0.5616520536051469
@@ -0,0 +1,22 @@
+archive/ES_0.5616520536051469---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T05:30:41.641
+Launch V∞: [7.822271555315889, -5.827453340361265, 0.0732785385546183] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0028105379039113977, 0.001903361951547906, 0.11545952402128255] km/s
+ V∞_out: [-0.1074966009692615, -0.03814268914817087, 0.01757502666849639] km/s
+ time of flight: 1.8078011765712273e8 seconds
+ arrival date: 2030-02-01T14:12:38.641
+ thrust profile: [0.3768648384059129 -0.01585025002908052 -0.11695648554722411; 0.13313615751360547 0.07036740880803806 -0.1386565759698351; 0.08396852112744947 0.07277662202630729 -0.15553003575491037; 0.039696189022818476 0.04639860880927312 -0.11284318639214179; 0.04562374149056144 0.06719567705621717 -0.1717964814155304; 0.01605986810283878 0.02753762379064343 -0.07808866981815984; 0.010140668385577102 0.019540474054199723 -0.06059397953846552; 0.0022452181054934753 0.007045474563652964 -0.01829677800531339; 0.00030729057264815567 0.004491287720672511 -0.01355002224339383; -1.1032380613337518e-5 0.00029501769751120923 -0.0019399407082337826; 0.006234733357520242 0.007303034118560078 -0.0237550171748707; -0.0005486054179699737 -0.0004896229206001784 -0.0014860965840700767; -3.519843603010486e-5 -0.002702671515842671 0.0014061004843067986; -0.00029545433292382876 -0.00015925448443631892 0.003919263696771618; 9.082843183211091e-5 -0.0004129038121111848 -0.0015551074556038366; -0.014067798740543005 0.006054203336132703 -0.005201860403025411; -0.004113170551349338 -0.010717577932812968 -0.0029765314232230227; 0.0021857451206768255 0.0007269389418141997 -0.007650923840370064; -0.01225102967869281 -0.01152773130107946 -0.014356395686183604; -3.374942573591087e-5 0.00048742364656497486 -0.004094166193922694] %
+
+Mass Used: 100.20439483614564 kg
+Launch C3: 95.15251446340442 km²/s²
+||V∞_in||: 0.11550940912864652 km/s
diff --git a/archive/ES_0.5616572287831966 b/archive/ES_0.5616572287831966
new file mode 100644
index 0000000..5b6b47d
--- /dev/null
+++ b/archive/ES_0.5616572287831966
@@ -0,0 +1,22 @@
+archive/ES_0.5616572287831966---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T16:42:26.484
+Launch V∞: [7.848809337890496, -5.996026168254406, -0.11553738859916562] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4016964762945162e-8, -2.157115254573501e-7, 3.971742017731957e-8] km/s
+ V∞_out: [-3.495871129973071e-8, 1.2755536757898475e-7, 1.7763540656614515e-7] km/s
+ time of flight: 1.8234231356714144e8 seconds
+ arrival date: 2030-02-24T03:20:59.484
+ thrust profile: [0.29540205839851674 -0.011445070133681422 -0.10185505479872173; 0.05617913124303913 0.025425185251692767 -0.073681435235676; 0.04287546766766836 0.0296358426293616 -0.09981974129603005; 0.033275769691519706 0.027752742173221327 -0.1120127013536551; 0.029297094414154016 0.02749257541422043 -0.12592824614277495; 0.02305853601734668 0.02309466033506777 -0.11947706782975859; 0.017520985985539788 0.01761842863440915 -0.10347259562030785; 0.010766987311671534 0.011229940098353893 -0.07237718489475313; 0.004298626630521663 0.005070302132448547 -0.03500940308897162; -6.413175400563683e-5 0.0010886297521483157 -0.0073606616944338656; -0.002524074985531913 0.0012827295566339015 -0.006082649106152512; -0.0009778433715726914 -0.00016950041555617844 0.001729361578016412; -0.0017170836817659678 -6.136031754639743e-5 0.0036902163861814033; -9.478981381316309e-5 -0.0007534721285717068 -0.0030046873438744634; 0.0076399857158762 -0.0014107527730492892 0.0006829182896675673; -0.007065651226843801 0.003532371569098224 0.004134246612708227; -0.001552748738788764 -0.0002033797518312975 0.004882297324840898; 0.0023192708214421834 -0.0053801197030443944 0.010057707400696761; 0.0004622654942723895 -0.0004457827260210713 0.0007388251598116321; 0.0020618673741021783 0.009391245253429015 0.011032929623073303] %
+
+Mass Used: 86.111427707237 kg
+Launch C3: 97.56948672111297 km²/s²
+||V∞_in||: 2.2064847671602743e-7 km/s
diff --git a/archive/ES_0.5616630164145636 b/archive/ES_0.5616630164145636
new file mode 100644
index 0000000..1450f85
--- /dev/null
+++ b/archive/ES_0.5616630164145636
@@ -0,0 +1,22 @@
+archive/ES_0.5616630164145636---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T02:23:05.191
+Launch V∞: [6.679104032179418, -7.367297157644906, 0.1483701657601054] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.695418471960882e-5, -2.6546248391102388e-6, 4.6243183565185164e-8] km/s
+ V∞_out: [3.3130463161251074e-6, -7.858648753861664e-8, -1.6837860092440626e-5] km/s
+ time of flight: 1.874957778749266e8 seconds
+ arrival date: 2029-04-10T04:32:42.191
+ thrust profile: [0.15584451074305736 -0.04234108628181614 -0.06075168388880647; 0.055713172049788894 0.012219251591620212 -0.06609444924670636; 0.04954935153621759 0.021838867312219845 -0.09982144715729357; 0.04347852062750848 0.025773812479018603 -0.12390995788662094; 0.035612135848848835 0.02537114864556981 -0.1314672216750078; 0.028119627325282323 0.02264276584331035 -0.12629930094714978; 0.020071230467362186 0.016689863007702737 -0.10091296892879123; 0.01408390284356485 0.012154499489687878 -0.07956992533734822; 0.007187035804986383 0.006294311151018347 -0.04521742332120637; 0.002178967728780688 0.0021333524249767507 -0.016306425573893994; 0.00016624626398403547 0.0005181455786684485 -0.0033725288453044693; 0.0007150050125346524 0.0007562206910728404 -0.0063610884428721825; -0.00010182134429864828 -0.00043105066165459677 -0.0017986087356582734; -0.0006447986194407025 0.00040221319878781136 -7.137677201979786e-5; -0.0005303000065823611 0.0005566527063688047 -0.001106727844285792; -0.0007978276055884551 0.00031843834312162263 -0.00018829710885871623; -0.00043330917785021784 0.0006515950486031968 -0.00013283478320158786; 0.0007038436893659912 -0.0027605014127653604 -0.0013202156659911594; 0.0012748348330533419 0.0007621334662928725 -0.0012820782850904218; -0.0006999952797994875 0.0015755632952369233 -0.0015146397525218826] %
+
+Mass Used: 78.30136705479072 kg
+Launch C3: 98.90951178780574 km²/s²
+||V∞_in||: 1.716081440302483e-5 km/s
diff --git a/archive/ES_0.5616637651703231 b/archive/ES_0.5616637651703231
new file mode 100644
index 0000000..27a0508
--- /dev/null
+++ b/archive/ES_0.5616637651703231
@@ -0,0 +1,22 @@
+archive/ES_0.5616637651703231---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:53:34.537
+Launch V∞: [7.649255062614012, -6.1312320546717105, 0.02399445166225512] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1389561473882547e-5, 1.6836819899023365e-5, 1.5532857152635397e-6] km/s
+ V∞_out: [-9.406375825815033e-7, 2.977345024474483e-6, 1.7079699417086822e-5] km/s
+ time of flight: 1.713749856218944e8 seconds
+ arrival date: 2029-10-15T04:03:19.537
+ thrust profile: [0.36447878751436547 -0.04610388290446515 -0.12914920102636832; 0.07231001734934182 0.02865514108515483 -0.08442732499546213; 0.07580518342158943 0.05073044989563947 -0.15004939680157992; 0.048118136100398716 0.042251512971207376 -0.1393679910196626; 0.039320350433472685 0.04073140246589399 -0.1466450893344135; 0.020444436472133048 0.020701773549289954 -0.08351714471653367; 0.012654996911430428 0.0157855046982901 -0.0654435337193948; 0.012777247055432503 0.027631690829867418 -0.11844755214443341; 0.0044546183538492126 0.010640389179748026 -0.050599224160208414; 0.0029066932102058828 0.0040571993584171675 -0.021177617521346757; 0.0008891865447644664 0.0019618301478851533 -0.008376467341614773; 0.00042738375044313465 0.0022112648165275475 -0.005044780039134796; -0.0008192545050852615 0.0005564491561715426 -0.0026819366838261166; 0.0018495043881136108 -0.0033714708281061866 -0.003706790596202424; -0.0015837774731918706 0.0010806718649889878 -0.00026196422994673326; -0.001485829304139803 -0.005195060986496845 -0.0016340799352036672; -0.0005815589198409749 -0.0021650645487926667 -0.0042918087824464195; 0.0011666848920604833 0.0025184867762207508 -0.002892992312540657; 0.001220800539812146 0.002887183697196721 -0.0013232618345841855; -6.901985586409476e-5 0.0006662387520859402 0.001692605354222045] %
+
+Mass Used: 94.66956204529879 kg
+Launch C3: 96.10368525487056 km²/s²
+||V∞_in||: 2.03865963660622e-5 km/s
diff --git a/archive/ES_0.5616667954786101 b/archive/ES_0.5616667954786101
new file mode 100644
index 0000000..ad9470d
--- /dev/null
+++ b/archive/ES_0.5616667954786101
@@ -0,0 +1,22 @@
+archive/ES_0.5616667954786101---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T09:33:34.104
+Launch V∞: [6.420136593668321, -7.385476174039658, 0.09660535655230447] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.437160178033988e-7, -0.00018170939793327935, 0.000141992295188627] km/s
+ V∞_out: [0.0001145027816578118, 0.0001959196804874977, -4.101565641172842e-5] km/s
+ time of flight: 1.874957778726342e8 seconds
+ arrival date: 2029-04-09T11:43:11.104
+ thrust profile: [0.38680091129430744 -0.09377938624054409 -0.12932574225511817; 0.051499950057715384 0.015359797781765239 -0.05605404111511005; 0.07681011317368391 0.04318964057407233 -0.13590263330955646; 0.05806674001425953 0.04399150160519474 -0.14452395456052505; 0.03085173018529834 0.028638909136949813 -0.101051037085651; 0.019446203553212166 0.020930007337262285 -0.07911760590890657; 0.012896181489023939 0.015542642097371438 -0.06286329202839323; 0.016773580313449932 0.022827410304841998 -0.09126224213916784; 0.012911286079678242 0.020109478727253136 -0.08311434821647112; 0.002899042716913238 0.004905906729959417 -0.022956956063777238; 0.0004334934981516164 0.0005985267957625475 -0.0032535598881540204; 0.0001807432902585227 0.0003762854515592661 -0.0012544900270618324; -2.8282293279659006e-5 -0.0001955855928949312 -0.0007162589014506051; 0.0001374578115213015 1.7910715366760898e-5 -0.0003835109298428112; 0.00015500607916699508 0.00015121214137702143 -0.00015249884233363867; -2.156851738941516e-5 0.0004182696274150316 -0.00010128078073696507; -0.0006861848406907781 0.00031879128141934314 -0.0002811170115663126; 8.591296612364381e-5 -0.00011706976220366425 2.666005412326649e-5; -0.0005079400662179919 0.0003319406355111655 0.0007890012692601332; 1.0039149938711197e-5 0.0001690957495047015 -0.00011505719362929357] %
+
+Mass Used: 96.60358342915515 kg
+Launch C3: 95.77274479358114 km²/s²
+||V∞_in||: 0.00023060878738096055 km/s
diff --git a/archive/ES_0.5616759842430369 b/archive/ES_0.5616759842430369
new file mode 100644
index 0000000..3b496c9
--- /dev/null
+++ b/archive/ES_0.5616759842430369
@@ -0,0 +1,22 @@
+archive/ES_0.5616759842430369---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T00:25:40.197
+Launch V∞: [7.811383889858835, -5.726617034981442, 0.09841829151141207] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.181399592168353e-7, 8.346283295178137e-7, -1.7992941100713224e-5] km/s
+ V∞_out: [-6.877498102894592e-7, 1.807761045150112e-5, -1.9772702751730938e-7] km/s
+ time of flight: 1.8477508277785334e8 seconds
+ arrival date: 2030-03-19T14:50:22.197
+ thrust profile: [0.47251852525710364 -0.015961305418201024 -0.09982917439689283; 0.07232911432166197 0.0464462152936388 -0.059767600680314864; 0.16241137938489913 0.17627044402979877 -0.2676256483018932; 0.029103485307908978 0.042760923899894776 -0.06877466765728861; 0.014352403389575323 0.026785450513829846 -0.0500489875210452; 0.013217071906115981 0.030530089134578744 -0.05833554741440287; 0.03085653520462286 0.05814677892277451 -0.10198186331822033; 0.0022108161561143107 0.010728464641938365 -0.023086016141159023; 0.007888551201826603 0.02374877009740309 -0.052205074559318165; 0.0016764740629459 0.01207380795417373 -0.027782789928241746; -0.0012175830786706598 0.00932370273707475 -0.018794104999860135; 0.0010703971811389006 0.0017652001133507374 -0.007757861665847339; 0.0020573607739470794 0.0014843272776033098 -0.0036479547216745484; 0.004236429920785099 0.0014208785431110934 -0.0007400380309583528; -0.0028440132000032386 -0.0015314147596955344 -0.005194507394169811; 0.0002362700302926703 0.004379217833735894 -0.0055140294727845625; 0.0009877161554486722 0.004444539199241958 -0.000257678368766254; 0.0016572646437217342 -0.005236804378490089 -0.0010406299035981136; -0.0028453431106016916 0.004840999489641907 0.004130924737623933; 0.000565725148749257 0.004033792434952451 0.003581041093213529] %
+
+Mass Used: 107.99629019910253 kg
+Launch C3: 93.8215471001898 km²/s²
+||V∞_in||: 1.801267584097745e-5 km/s
diff --git a/archive/ES_0.5616803414712792 b/archive/ES_0.5616803414712792
new file mode 100644
index 0000000..28c11e0
--- /dev/null
+++ b/archive/ES_0.5616803414712792
@@ -0,0 +1,22 @@
+archive/ES_0.5616803414712792---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T02:11:30.190
+Launch V∞: [6.3333763058707895, -7.441109895366478, 0.20995842164598735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.10188688427281e-6, -7.746227952308795e-7, 1.7308421434416494e-8] km/s
+ V∞_out: [1.2140597671641738e-6, -2.7799737121672944e-8, -5.980850657425173e-6] km/s
+ time of flight: 1.8749577787463108e8 seconds
+ arrival date: 2029-04-10T04:21:07.190
+ thrust profile: [0.39039004875660654 -0.09908288771038061 -0.1305232453816079; 0.08645860703019795 0.02301698725885414 -0.09078745114264888; 0.06082687449274203 0.03139889482331818 -0.10798778983332123; 0.08275505137351302 0.056947239083217464 -0.20262156713836774; 0.037531861245740636 0.031070742952678237 -0.12028233668808047; 0.025584653532375344 0.024427309043780532 -0.10081173117488797; 0.007922191687084322 0.00857058265656062 -0.03882296796908712; 0.00651102726349056 0.0077222726136616055 -0.03675401887384677; 0.01005843009690357 0.0123427146962943 -0.05633287308684155; 0.002196844764386715 0.0027222250351753947 -0.014983298572505162; 0.00020296340224452053 0.0006108849149142305 -0.003326864966370817; 9.447644250720213e-5 0.0010382717060320287 -0.006771224302807961; 0.00017591997774459836 0.001024359172995808 -0.0007863242342924171; 0.0005104479078893934 -0.0002662174072926426 -0.00024601465875446083; 0.00024558557985894405 -8.10009876139847e-5 -0.0005353499595006916; 9.106802455709735e-5 0.0001393392517515681 -0.0007225758955430147; -0.0011342765669713998 -0.0003575193479440335 0.00033774887607250807; -0.0007646727335131613 -0.000869566997632068 -0.0016510381692903444; -1.8032872246127017e-5 0.0009701731592667897 -0.0004626148969233406; 0.001474605861393493 0.00016751484605615995 -0.00039841035858358717] %
+
+Mass Used: 98.05958078437106 kg
+Launch C3: 95.52585444550652 km²/s²
+||V∞_in||: 6.150883156490976e-6 km/s
diff --git a/archive/ES_0.5617225763209203 b/archive/ES_0.5617225763209203
new file mode 100644
index 0000000..4afc63c
--- /dev/null
+++ b/archive/ES_0.5617225763209203
@@ -0,0 +1,22 @@
+archive/ES_0.5617225763209203---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:36:30.808
+Launch V∞: [7.872650151003987, -5.780692312597404, 0.1109054237546959] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.242657831280583e-6, -1.865080114551735e-6, -1.8267807827002921e-7] km/s
+ V∞_out: [1.4500246548205898e-7, -7.800994610416661e-7, -2.1036212901784267e-6] km/s
+ time of flight: 1.8749577787493688e8 seconds
+ arrival date: 2030-04-23T19:46:07.808
+ thrust profile: [0.37637155202118594 0.006116077829648151 -0.11634791842980846; 0.16182225240117742 0.10044968754539534 -0.1737351666600906; 0.023272096617942977 0.022758806860744357 -0.04892438289346934; 0.034516446430133844 0.040558551326664714 -0.09831820114934296; 0.01858439756437428 0.032509093609145064 -0.0809596809738342; 0.015209849357922618 0.031935166290870974 -0.08997581551851375; 0.010671270311315066 0.030155060039627816 -0.0864775392289097; 0.004599592693166423 0.012321575442783788 -0.040933106178675446; 0.0030621098106193077 0.010079642885765312 -0.034637933971557795; 0.0032617926164209875 0.008943449703091461 -0.027492637193934945; -0.0015211329031220482 0.004200691009083862 -0.01599218490507619; 0.0012752147951602716 0.0018489594870988086 -0.0119587869233004; 0.008529720991802155 0.0007595193263191641 -0.006737067721924184; -0.0017963010781835644 0.0011729145691233942 -0.004276521830275675; -0.0015033981694381987 -0.006325636578843788 0.0017132145117041107; 0.005869775330104824 -0.001392435135800226 0.008049169540583182; 0.0009309261438583622 0.0032201822640199012 -0.010970648195625878; 0.0019747239995427475 0.0023025004745924776 -9.913404340466448e-5; 0.012259654869772763 0.005324549259604985 -0.0019517158545175005; 6.699382200086207e-5 0.020604743687419262 -0.014777678206422496] %
+
+Mass Used: 98.80028222248347 kg
+Launch C3: 95.40732402604402 km²/s²
+||V∞_in||: 2.2485759047939e-6 km/s
diff --git a/archive/ES_0.5617244933368994 b/archive/ES_0.5617244933368994
new file mode 100644
index 0000000..378aee6
--- /dev/null
+++ b/archive/ES_0.5617244933368994
@@ -0,0 +1,22 @@
+archive/ES_0.5617244933368994---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T01:51:47.672
+Launch V∞: [7.699501051380695, -6.095413394921789, 0.1730001811302655] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000168334724429747, 0.0001071244401294841, 0.007147688361475149] km/s
+ V∞_out: [-0.006681730962872101, -0.0023219438074623525, 0.001014789177618125] km/s
+ time of flight: 1.7632264826911068e8 seconds
+ arrival date: 2029-12-13T20:22:35.672
+ thrust profile: [0.3707591806971487 -0.032972391413416395 -0.12805211364926444; 0.038541820324880446 0.017038051007758473 -0.04864773506756675; 0.06480456768228196 0.04647521085468123 -0.14424168286088082; 0.034723428662400774 0.03307396607555667 -0.11149139973488163; 0.037144780631247536 0.03958566862120367 -0.1354667350747784; 0.012743584844450238 0.016164994729177293 -0.06775367867269849; 0.011285433338534103 0.016050591800011078 -0.06907749745417177; 0.015346889552463952 0.016744484892117068 -0.08159628945511552; 0.005350831153988637 0.013528267034655563 -0.06315129283724624; 0.004176050616686303 0.010295038210568704 -0.049871564573255214; 0.0021421660070787035 0.004708477069076775 -0.025139816697800632; 0.001416184364560975 0.004150151435406536 -0.028214604030640477; -0.0010510434286141674 -0.00016549257807088136 -0.000292959982291193; -0.0003273145523385139 0.0012094834764817333 -0.0023737053742407415; 0.004123787835917183 -0.002535725935073835 0.003616098852013592; 0.0023757318015915447 0.00361731385979009 0.004481819901435683; 0.003548438204126531 -0.002421096184955892 -0.001817281314834367; -0.0008631457244284461 0.003220018918859265 -0.001114694408451061; -0.001124924415496581 -0.004835278883409268 -0.001148323696987101; 0.0001480940220375702 0.0005853404691948654 -0.0022861189835440606] %
+
+Mass Used: 92.62510080544234 kg
+Launch C3: 96.4663099578755 km²/s²
+||V∞_in||: 0.007150472791213823 km/s
diff --git a/archive/ES_0.5617254077033653 b/archive/ES_0.5617254077033653
new file mode 100644
index 0000000..f48764c
--- /dev/null
+++ b/archive/ES_0.5617254077033653
@@ -0,0 +1,22 @@
+archive/ES_0.5617254077033653---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T18:01:17.512
+Launch V∞: [7.969272595592697, -5.678495810267767, 0.06799270241035842] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7550568503024976e-8, -8.351582427968234e-8, -2.676091184158461e-7] km/s
+ V∞_out: [-2.302924635170385e-7, -2.483019691185042e-8, 1.5134418811805855e-7] km/s
+ time of flight: 1.841931338082578e8 seconds
+ arrival date: 2030-03-14T14:46:50.512
+ thrust profile: [0.4219602404216275 -0.014848547545712373 -0.13069746173632987; 0.059916949387869935 0.03151240149473512 -0.07481759061985357; 0.04062201630899039 0.034371785385602496 -0.08881199298962547; 0.033135729958656816 0.03650479053308196 -0.10514478577895013; 0.0317942606093217 0.04425713828885161 -0.13390593847661522; 0.015342563365833888 0.025367979968775458 -0.08683156327960408; 0.008235247050082814 0.012262948295190361 -0.04980973070486767; 0.004555821286985246 0.012420408824187436 -0.04962754790326971; 0.0075291470652128056 0.014007416887062281 -0.061993978523894; 0.0028797016366879057 0.005007973130355269 -0.02551322946040331; 0.0012519814809122951 0.009060276696102394 -0.0233784953287485; 0.0014127137104924148 0.003979769339776647 -0.021380316627405013; -0.0009706132469890598 0.00510895345766503 -0.004045811783511243; 0.0016676878440538513 -0.0007990761907508157 -0.0004540956217446313; -0.001572059013786766 -0.0031637970875469314 -0.00035797222505778385; -0.00807756206666694 -0.013587361855757788 -0.0056672945172094695; -0.0011881650736914485 -0.0004275371752093052 -0.0026945716025852866; -0.0007065203592023235 0.018442200433085344 -0.012646254625735803; -0.006604886291709006 -0.0005095256936654339 0.0051219148296727315; 0.002049663579675601 -0.0008915232045403399 -0.01718896055845362] %
+
+Mass Used: 96.7507226174921 kg
+Launch C3: 95.75924337767442 km²/s²
+||V∞_in||: 2.81688776825171e-7 km/s
diff --git a/archive/ES_0.5617325425887106 b/archive/ES_0.5617325425887106
new file mode 100644
index 0000000..1b970e9
--- /dev/null
+++ b/archive/ES_0.5617325425887106
@@ -0,0 +1,22 @@
+archive/ES_0.5617325425887106---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:42:27.591
+Launch V∞: [7.701325720482706, -6.022011069803702, 0.02348395972479487] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.987377317011803e-5, 7.64020910084839e-5, -6.88721060415521e-5] km/s
+ V∞_out: [2.1443457886404934e-5, 0.00012822062529846732, -5.914324566385967e-6] km/s
+ time of flight: 1.7405082386233526e8 seconds
+ arrival date: 2029-11-15T03:09:30.591
+ thrust profile: [0.42212693939685336 -0.0389279562659377 -0.1386481891135198; 0.05092145800643458 0.022390166894735157 -0.05873952726917025; 0.07236531122689227 0.05326324400161566 -0.14131890235316777; 0.04652801064559364 0.04486265210375283 -0.13451103386780777; 0.030780517587964035 0.03351937896084788 -0.10765458304798438; 0.029117773624628085 0.03719324207369548 -0.12899969527173058; 0.01358571893066665 0.01961636351164634 -0.07636814950831856; 0.0061995758366312995 0.0097411285226637 -0.0443159716033006; 0.012832870511381227 0.024632395014475134 -0.10302073584485927; 0.0012790622907464465 0.0036537589550551326 -0.01601754593544785; -0.0008421804284287628 0.0027303676104276087 -0.004708232708649038; 0.0019798005874307398 0.002516418168088951 -0.018376299813257693; -0.0005206603758285675 0.0023639465991575825 -0.002070180006844694; 0.002759207655190429 0.0007988386122865864 -0.0039956487127501; 0.0005733129003586137 0.003549662160926636 -0.0016365061307970965; 0.002943362938577866 0.0015796701889620552 -0.002697876526001181; -0.006676888695488516 0.0041575676055754145 0.001312924019689126; -0.0021688062049813922 -0.004631319043044402 -0.004497946304203849; 0.002377647259025344 -3.601524201316084e-5 -0.0031858647150869463; -0.0019461506057624253 0.003959600852955088 -0.003219260658440945] %
+
+Mass Used: 97.8303774208307 kg
+Launch C3: 95.57558667417115 km²/s²
+||V∞_in||: 0.0001302323544342915 km/s
diff --git a/archive/ES_0.5617519699180564 b/archive/ES_0.5617519699180564
new file mode 100644
index 0000000..47ec20f
--- /dev/null
+++ b/archive/ES_0.5617519699180564
@@ -0,0 +1,22 @@
+archive/ES_0.5617519699180564---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T21:50:35.559
+Launch V∞: [7.733342136916357, -5.998282213844955, -0.19816066218534178] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0002840888085154188, 0.000777547681416126, 0.0018781689183645317] km/s
+ V∞_out: [0.001981846204015169, 0.00013622228889414553, -0.0005123894759935226] km/s
+ time of flight: 1.7595780290389994e8 seconds
+ arrival date: 2029-12-06T11:00:37.559
+ thrust profile: [0.25347380738870845 -0.016403309790871172 -0.08001545977874504; 0.17872217315483444 0.09237117259419722 -0.1745884053941415; 0.14528237967913543 0.12678544941126987 -0.25018852945279535; 0.042808360300955556 0.049107454794101495 -0.10980815967356748; 0.024327676001638904 0.03461642091912747 -0.0865518078090474; 0.010987371913498389 0.018298283167717217 -0.049789632678364115; 0.018426139925760553 0.035970507751929136 -0.10079424307681589; 0.0035223397207864286 0.007337492252821914 -0.0225413835584759; 0.007335725897412092 0.016896463618428014 -0.05346104611513102; 0.001763582300076601 0.003916661811658305 -0.011826553420868852; 0.0022713262805453332 0.00413569750810735 -0.014700752966062868; 0.0014862400207916622 0.0006873531975147031 -0.002633491527110275; 0.0036435121927085256 -0.0004645319566588765 -0.003825232450723987; 0.0023832362334653854 0.001530020070898452 -0.0018342014864211934; -0.0004903459491422517 -0.0009289797592837859 -0.0012814692061449478; -0.0023152333861281614 0.0015107583915394856 -0.000739430018364802; 0.0009954884813260815 0.00046102848411766256 0.0015152061682394266; 1.345247046484737e-5 0.0014159411213467608 -0.0032676240056497777; -0.0023912933407436174 -0.002795487514378677 -0.00018164174690251614; -0.006580333042944971 0.0010358893204802083 -0.0007493098152839814] %
+
+Mass Used: 96.40841123689279 kg
+Launch C3: 95.82323777157251 km²/s²
+||V∞_in||: 0.002052511957068679 km/s
diff --git a/archive/ES_0.5617647530993415 b/archive/ES_0.5617647530993415
new file mode 100644
index 0000000..fe48604
--- /dev/null
+++ b/archive/ES_0.5617647530993415
@@ -0,0 +1,22 @@
+archive/ES_0.5617647530993415---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T11:10:29.965
+Launch V∞: [7.651724902231536, -5.896595085749392, 0.1094439769675607] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.802985910585384e-7, -4.543064137273443e-6, 8.443646550601515e-7] km/s
+ V∞_out: [-7.181702941249281e-7, 2.612089569459924e-6, 3.7756389644826663e-6] km/s
+ time of flight: 1.8129845598545155e8 seconds
+ arrival date: 2030-02-09T19:51:24.965
+ thrust profile: [0.5991579720499747 -0.052604399692311156 -0.19595976799167836; 0.1481875484435777 0.04721105890895712 -0.15758911348078597; 0.02608108089184001 0.01772842967827344 -0.05704971869388517; 0.03660279787476913 0.02796535908566907 -0.1151102400700526; 0.027434792026578246 0.02425684599732448 -0.11233958292567364; 0.012230261262505147 0.01257683365962444 -0.0636349094315521; 0.011040509389544982 0.01137281952266432 -0.06446054431455034; 0.009051824454521325 0.012802071240201591 -0.06567233562172772; 0.005720384573432606 0.006497747266968859 -0.04446969006818014; 0.005109243484628099 0.005645311017502704 -0.051029177917506975; 0.0011323923254679476 0.001539745983396562 -0.00902459955670885; 0.00043161313484871137 0.0010288866642772423 -0.005502646549232824; -0.0015941449335661892 0.0030748394346380797 -0.002807139058278448; -0.0004483287128025237 -0.0004693236201583404 0.0031007341204512687; 0.0053414344104176625 -0.003163844162986633 -0.005574438870158035; 0.004126736795850974 -0.002624122119425566 0.0010307261323338813; -0.002424782952987765 0.005905127034410456 0.004336784579971534; -0.0014422868173597989 -0.005668633173195115 -0.012048974632102366; 0.0011643560816843972 0.007315800625351898 -0.004398727726038141; -0.004192434041066236 -0.0013124446041439856 0.012670479294017946] %
+
+Mass Used: 110.96309613118183 kg
+Launch C3: 93.33070556880855 km²/s²
+||V∞_in||: 4.645758297917333e-6 km/s
diff --git a/archive/ES_0.5617652283302288 b/archive/ES_0.5617652283302288
new file mode 100644
index 0000000..9e40bd7
--- /dev/null
+++ b/archive/ES_0.5617652283302288
@@ -0,0 +1,22 @@
+archive/ES_0.5617652283302288---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T09:58:50.096
+Launch V∞: [7.881403475459755, -5.585404301076404, 0.340457923109394] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.76629617801382e-6, 4.015128871988052e-6, 0.00028584230280248894] km/s
+ V∞_out: [-0.000255660299687972, -8.52410518424451e-5, 9.442179150187311e-5] km/s
+ time of flight: 1.874957778739552e8 seconds
+ arrival date: 2030-04-20T12:08:27.096
+ thrust profile: [0.5785881131242848 0.013442353148338887 -0.1195746214754652; 0.058143696072693 0.039797863924838146 -0.05701351549997194; 0.0696247933602016 0.08041651996117398 -0.12195632044803419; 0.030845899150520543 0.04851151893500133 -0.08564501855254678; 0.05478001037240521 0.10779473272260383 -0.1892299613437255; 0.016124262561832928 0.03991181307321502 -0.08113623311055339; 0.008541168804355412 0.025481727446995915 -0.05703891083183072; 0.005896625998947655 0.020598693871803898 -0.051008848745360914; 0.001504967618018986 0.004577867355365864 -0.012648971356730335; 0.0005038917757965156 0.004309847895190764 -0.00860099318215146; -0.00014196359560498682 0.0001572494553086375 -0.0009177250819280064; 8.092908236961973e-5 0.0007569509947625687 0.0011880448627888144; -0.0015821617739780226 0.0037347370936078868 0.003713842689776664; 0.006217369494246095 0.004826046068504371 -0.000547412515800292; 0.003371756636251387 0.00017198781181350159 -0.005687203611655998; 0.00019258672355460167 0.0013518202387460508 -0.0025276919780777463; -0.0006367976694752842 0.0033276093620799693 -0.008992071299192514; 0.011750424663564539 -0.01049913096529279 0.0070108605372084555; -0.0005648821463321448 -0.003087767417774187 0.009438270882611073; -0.008375082555297413 -0.006360581050900336 0.005791536243321617] %
+
+Mass Used: 110.3892540284678 kg
+Launch C3: 93.42917354687985 km²/s²
+||V∞_in||: 0.0002859286510703344 km/s
diff --git a/archive/ES_0.5617681206959867 b/archive/ES_0.5617681206959867
new file mode 100644
index 0000000..8e10e6e
--- /dev/null
+++ b/archive/ES_0.5617681206959867
@@ -0,0 +1,22 @@
+archive/ES_0.5617681206959867---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T18:48:11.072
+Launch V∞: [6.543878103510982, -7.3332140060937325, 0.156276762349057] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01754863162149442, -0.008285834437115494, 0.02002745320280854] km/s
+ V∞_out: [-0.017985878250111907, -0.007303300250320093, -0.020020332699695286] km/s
+ time of flight: 1.8749577787429157e8 seconds
+ arrival date: 2029-04-08T20:57:48.072
+ thrust profile: [0.31482624988508157 -0.08473084843934067 -0.09340493218420329; 0.06799865767537762 0.019941163672324135 -0.07293268099972218; 0.04131701841312066 0.023254486179928945 -0.07483872045354129; 0.057665211954720935 0.04523530847794634 -0.14640566343518718; 0.052657759604669244 0.05149354864247782 -0.17420906802394634; 0.030510441095927095 0.03330937719367249 -0.11841280785964539; 0.014617688507284213 0.017807261293629233 -0.07013443336389852; 0.011337418323945638 0.014811532520359567 -0.061562708361738896; 0.003618545327939562 0.004812736723743004 -0.02167420633999606; 0.005358850324325847 0.008434474481737897 -0.03803520617945716; 0.000864434629349198 0.0009578125920879444 -0.005110495635609125; -0.0003157931166360696 0.0005415694700441126 -0.0011198734010642057; 0.0003827752699628595 -0.000362839299708993 -0.00097825732477409; -0.00010953739259105487 -0.0010012748201224816 -0.0022991718466440726; -0.0012432899360062203 0.0005461741338100005 -0.0013835982820404457; -0.000885147451853733 0.00034313997777878677 -9.569092518491354e-5; -0.002197661027836937 0.0007856987114920389 0.0005593329039770842; 0.001036955317238253 -0.0017753988882959837 0.0017707026826757955; 0.0007375374114226101 -0.0006432195912591123 0.0006317849022303448; 0.00013051054419599916 -0.0002846855627040467 0.0006859849259718421] %
+
+Mass Used: 91.76319494980908 kg
+Launch C3: 96.62279071923008 km²/s²
+||V∞_in||: 0.027887423794550996 km/s
diff --git a/archive/ES_0.5617712792709177 b/archive/ES_0.5617712792709177
new file mode 100644
index 0000000..9c36d29
--- /dev/null
+++ b/archive/ES_0.5617712792709177
@@ -0,0 +1,22 @@
+archive/ES_0.5617712792709177---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T08:28:03.128
+Launch V∞: [6.6032643650383624, -7.403346823435396, 0.11714283069475544] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.304247066340453e-9, 1.3607078342062034e-8, 8.178428702322637e-9] km/s
+ V∞_out: [-3.662112160517798e-9, 8.18533465077569e-9, -1.2757352852253972e-8] km/s
+ time of flight: 1.874957778747637e8 seconds
+ arrival date: 2029-04-10T10:37:40.128
+ thrust profile: [0.19297956342318814 -0.05057831949270097 -0.07260244682488173; 0.049874923140435345 0.011825428627057653 -0.05757514442349563; 0.05072149066472915 0.02375160982303607 -0.098086027488951; 0.0417768498594458 0.026051601480947553 -0.11296730317884501; 0.036343015553142774 0.027051954793452623 -0.12551019659376303; 0.03706500199769059 0.03144633778199332 -0.15417817814487125; 0.024279255650364116 0.02249389971469661 -0.11921286474038452; 0.008016174526820777 0.007825509891503565 -0.04606959110653637; 0.0034611289501051794 0.0036587078776350486 -0.02288175334388373; 0.0059018529834915425 0.0065025488168100835 -0.04159510146918858; 0.00133817713397393 0.0011856911914005272 -0.007147695031436147; 0.0011189075742962845 0.001370260065405973 -0.009498473569222619; 0.0002154636800014448 -0.00013370600842579024 0.0006918679923837009; 3.5603302319335735e-5 0.0013863518060883997 -0.002010004550120012; 5.7938183744205804e-5 0.0009334763067264021 -0.002955022942862061; -0.0017492306916428932 8.634799752154118e-5 0.0004020682343939451; 0.0005723655596392504 -0.001544738579050514 -0.0014310570402281762; 0.0004647509060744582 0.0005803731853045795 -0.0007809596638797779; -0.00030910649991744307 -0.001012376672062075 0.000841991328156087; -4.7339744798503255e-5 -8.404609023070189e-5 -0.0007679866604834681] %
+
+Mass Used: 81.24601886767277 kg
+Launch C3: 98.42636690543964 km²/s²
+||V∞_in||: 1.7916467184822248e-8 km/s
diff --git a/archive/ES_0.5617763039039604 b/archive/ES_0.5617763039039604
new file mode 100644
index 0000000..d548a49
--- /dev/null
+++ b/archive/ES_0.5617763039039604
@@ -0,0 +1,22 @@
+archive/ES_0.5617763039039604---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:44:00.750
+Launch V∞: [6.39391977840088, -7.3399682265415285, 0.20620650160862064] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0449906899559654e-5, -2.9961418382231897e-6, 5.0841932299344274e-8] km/s
+ V∞_out: [3.924444222141304e-6, -9.251625526724872e-8, -2.0291352185167994e-5] km/s
+ time of flight: 1.8749577787495476e8 seconds
+ arrival date: 2029-04-09T02:53:37.750
+ thrust profile: [0.44230292382080166 -0.11963616454030744 -0.14684103487902395; 0.12625809838992594 0.03393173560668498 -0.1373576114960891; 0.05110407503652158 0.02609642879247685 -0.09654055451574356; 0.03550697804633874 0.025264645852354346 -0.09632439914736891; 0.036520528997588474 0.030737723740903868 -0.12322408852450696; 0.023793157900399358 0.022993632139344317 -0.09862508334750977; 0.01908687517090198 0.01962306218775077 -0.08934375314941438; 0.014502002870916995 0.014647919288176676 -0.07261789401524799; 0.005892298551947034 0.008942423715378966 -0.04844700134873109; 0.0020235277481340424 0.0027793410682830488 -0.014697311572633947; 0.0008428491865724091 0.001145814817730508 -0.006732879735199703; 0.00040359877215037003 -0.0001987338702773511 0.000117966779225175; -2.0412872545628883e-5 -0.0001772370437953723 -0.0005244666469883135; -0.0004943627876464108 3.164271518254766e-5 0.00012351456885548412; -0.00029222962254890584 -0.000718611851122384 -6.643935571015052e-6; -4.364065548441079e-5 -0.0003022730501794019 0.0011883727836920197; -8.961399464139171e-5 -0.00013923914866481878 0.0007821836432803353; -0.0006333737179383055 -0.00036474535412263034 0.0007356259980215503; -0.0004468390018662437 0.00020616374631662377 -0.00025253370867148054; -0.00016205005598777513 -0.00014926544840041187 4.609022843139396e-5] %
+
+Mass Used: 102.40647643462398 kg
+Launch C3: 94.79986482057082 km²/s²
+||V∞_in||: 2.06682883427121e-5 km/s
diff --git a/archive/ES_0.5617952053990168 b/archive/ES_0.5617952053990168
new file mode 100644
index 0000000..f1e2ec7
--- /dev/null
+++ b/archive/ES_0.5617952053990168
@@ -0,0 +1,22 @@
+archive/ES_0.5617952053990168---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T10:25:55.079
+Launch V∞: [7.760837443675615, -5.7818005046404775, 0.030505655972798182] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.827049847882643e-11, 6.233265583810111e-9, -1.9738345595511996e-9] km/s
+ V∞_out: [2.8615910645279337e-9, 5.744690007899835e-9, 1.6339533233354638e-10] km/s
+ time of flight: 1.8749577787482587e8 seconds
+ arrival date: 2030-04-21T12:35:32.079
+ thrust profile: [0.4793150288159887 0.022509237710708396 -0.10736754624019357; 0.11652677781990801 0.0883294513858607 -0.09770139801072916; 0.035755021116412364 0.04421690304202643 -0.057911448190527376; 0.05693057624923608 0.09938665475380798 -0.13175569706155907; 0.035319836637106514 0.08138507780436223 -0.12119906444942029; 0.02865389360151892 0.0861223045231669 -0.13296410312458826; 0.005751262957581733 0.0238742335345509 -0.04321136411451484; 0.0060947760543487274 0.0263429305287039 -0.04956950244080788; 0.00260741107254347 0.017428804593224254 -0.0373729208029651; 0.0006780503576814655 0.003636898231034512 -0.008796997002513988; -0.000726893213274022 0.0011432252425137184 -0.004591725981786157; 4.286950159477579e-5 0.00026976963009796865 -0.00014742188418556288; 0.0009192496405403348 0.0014007191946041526 -0.0006602868925465809; 0.006977701386951601 0.0066181090766423084 -0.0030168252874967316; -0.004691787555817284 0.008642073425093124 -0.005470003812030172; 0.0038702873939542677 -0.0020360385330014715 -0.003016817111072682; 0.0007908172156365739 0.0008747189251701426 -0.0027190660727213502; -0.011716965999628355 0.0010772788914518807 -0.012303237811976276; -0.003671547011262196 0.005021682838279028 -0.006697447539003741; -0.005257375345204228 0.0027665746083222675 0.003210762186440603] %
+
+Mass Used: 109.0733908958091 kg
+Launch C3: 93.66074549766466 km²/s²
+||V∞_in||: 6.538675979718893e-9 km/s
diff --git a/archive/ES_0.5618018770965825 b/archive/ES_0.5618018770965825
new file mode 100644
index 0000000..ea54b54
--- /dev/null
+++ b/archive/ES_0.5618018770965825
@@ -0,0 +1,22 @@
+archive/ES_0.5618018770965825---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T16:26:43.459
+Launch V∞: [7.638374610808172, -6.005278842985595, 0.24696367280304232] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.666681852883751e-9, 1.5618662133839934e-9, 4.0458883215389586e-10] km/s
+ V∞_out: [2.9345616509210552e-9, -1.993489591574746e-9, 9.856149932350653e-10] km/s
+ time of flight: 1.790576030852689e8 seconds
+ arrival date: 2030-01-13T02:40:06.459
+ thrust profile: [0.4476576281922343 -0.011569170504161548 -0.11109435854177638; 0.11819531535701844 0.06768328986423605 -0.11241034005250246; 0.04482100202779553 0.04297858284670114 -0.0821826900090279; 0.07061089322341452 0.08797027424973163 -0.17214819753797034; 0.03364481931900227 0.052777402728408675 -0.12102180327127936; 0.013849002349399002 0.025969046595774665 -0.0644021214536465; 0.01437017036204013 0.03139530609264778 -0.08064003953291901; 0.014091121422026846 0.03621787838733196 -0.09844292933943626; 0.0034559891578700716 0.00889352088302895 -0.028337628842275562; 0.0013130386736071652 0.004321216317152764 -0.016021278878930848; 0.00045737068753792733 0.001727302031076768 -0.008131732040350913; -8.460488616100499e-5 -0.0009939274859388223 -0.0009727262899128805; 1.8761812661133678e-5 0.002127662784401118 -0.004173689183536222; 0.005444152998252898 0.0016524359304573234 -0.0015417456349207021; -0.0023794271148861986 -0.00038198889338127433 -0.0028901337165625745; -0.00745414363603732 0.007865106568392632 0.0005854055175614657; -0.004806293542506412 -0.0032733677690982327 0.0030979524211648527; 0.010523494135134027 0.0005840010658236795 -0.0012987467826414772; 0.0014401098271345008 0.005607357045527509 0.0024347073905931615; -0.008341672063401358 -0.0008027858407182789 0.007741346428019686] %
+
+Mass Used: 104.36558817173318 kg
+Launch C3: 94.46913173273366 km²/s²
+||V∞_in||: 3.116778833365246e-9 km/s
diff --git a/archive/ES_0.5618043732713165 b/archive/ES_0.5618043732713165
new file mode 100644
index 0000000..ec17d03
--- /dev/null
+++ b/archive/ES_0.5618043732713165
@@ -0,0 +1,22 @@
+archive/ES_0.5618043732713165---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T21:41:34.727
+Launch V∞: [6.516229528211719, -7.459333204731298, 0.11931659350030589] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.344296622977037e-8, 8.629264473450078e-8, 4.6809919263217207e-8] km/s
+ V∞_out: [-2.2138354300341634e-8, 3.4511516992208104e-8, -9.923039634576456e-8] km/s
+ time of flight: 1.8749577787494022e8 seconds
+ arrival date: 2029-04-09T23:51:11.727
+ thrust profile: [0.15407167199228589 -0.03246194127682307 -0.0567070302508268; 0.09921916458593448 0.033286559781915956 -0.10715080988924386; 0.07427083453882663 0.04625229404658336 -0.13409596553931769; 0.05627230051264533 0.047294839747135116 -0.1425780652873804; 0.04185536355237395 0.043002456000112245 -0.13758918657652738; 0.027923474484789552 0.03357661695154703 -0.11376711693658326; 0.01797752292837985 0.024389169286768736 -0.08788041976613961; 0.009130001389738877 0.013744127472807554 -0.053309653030403276; 0.003173682852153937 0.004864273246739425 -0.019989498573335148; 0.0016946021828501494 0.0018759974179702675 -0.0068425526168496235; 0.0009863811885043733 0.0007693503964057545 -0.0025295460924513917; 0.0028629811628978897 0.0010620242519674501 -0.005714928793837696; 0.0027333087039863443 -9.950696873192163e-5 0.00019156742821342188; 0.00015399522382248453 0.0005635892623278686 -0.00250262376528914; 0.00013919169447705886 -0.0002707183537978574 -0.0008277304816571766; 0.0006840871882266467 -0.00043760012465493266 -0.0006453404505390415; -0.00022827285983446877 0.0003515293788156548 0.0014411776597144732; -0.00013273084247863293 -0.0042154413474257265 -0.0007993678676197847; 0.00035043879042387024 0.0008155847367291816 -0.0035076948023494044; -0.00029408467512988235 0.0002486147485225352 -0.00025246238740221465] %
+
+Mass Used: 83.08847797386261 kg
+Launch C3: 98.11713557302971 km²/s²
+||V∞_in||: 1.0735399569435991e-7 km/s
diff --git a/archive/ES_0.5618073295628598 b/archive/ES_0.5618073295628598
new file mode 100644
index 0000000..bd320e3
--- /dev/null
+++ b/archive/ES_0.5618073295628598
@@ -0,0 +1,22 @@
+archive/ES_0.5618073295628598---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T16:27:34.591
+Launch V∞: [7.954662039822549, -5.94076884479574, 0.050596195866531815] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6665289611328257e-9, -2.3608196301501034e-9, -2.038614713287058e-9] km/s
+ V∞_out: [-6.904478414866797e-10, 6.091594679784111e-10, -2.5475475059717657e-10] km/s
+ time of flight: 1.8529622629833412e8 seconds
+ arrival date: 2030-03-31T07:38:00.591
+ thrust profile: [0.20354632743468032 -0.005117473753633629 -0.07586899551437923; 0.07283824516572966 0.035886944862954975 -0.09365569098649935; 0.03767142417718576 0.029245536198626406 -0.0889535580981113; 0.03324292116875602 0.029641172627976154 -0.10458158653805572; 0.02579849083088167 0.027755539943912513 -0.1086614717888854; 0.017018315875274106 0.021144245044578312 -0.09415432439775398; 0.01271033326849119 0.018162986643276 -0.08560432383035307; 0.006382705261614167 0.011717970875153761 -0.054894205666714616; 0.0026261839324666176 0.006380902031421975 -0.03547716459578998; 0.008434201277210321 0.01231159622560055 -0.07303251721344461; 0.0003477062444801499 0.0004740609353906514 0.00533462830447176; 0.0005020349156961556 0.002233361550939462 -0.00184642455868635; -0.0012771218537908067 0.0008923505947969457 0.003871496735320979; -0.0027289790401322745 0.005320380013018718 0.000504360273647616; -0.002565681912182753 0.0026808923617186358 -0.009452583068018152; -0.0011959098860695498 0.0033968067727557926 0.0009012322598143009; 0.001694591964967817 -0.0027380708337564723 0.0008881520676739425; 0.002168588159587171 -0.0011373286441297061 -0.0001290912772627592; -0.012692187571810929 -0.0033091289710962344 -0.005271444094303773; -0.004209152016187541 -0.006463649797645658 0.010973408309465076] %
+
+Mass Used: 80.43888593093652 kg
+Launch C3: 98.5719426101257 km²/s²
+||V∞_in||: 4.103632046844923e-9 km/s
diff --git a/archive/ES_0.5618074920839555 b/archive/ES_0.5618074920839555
new file mode 100644
index 0000000..4955393
--- /dev/null
+++ b/archive/ES_0.5618074920839555
@@ -0,0 +1,22 @@
+archive/ES_0.5618074920839555---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T09:43:19.730
+Launch V∞: [6.492938492907756, -7.2960825822789115, 0.08117574117236165] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.2556655167613265e-9, -2.281446486197795e-9, 3.385032244639917e-9] km/s
+ V∞_out: [1.4452292134205668e-9, -3.478806405240215e-9, -4.758378537100904e-9] km/s
+ time of flight: 1.8749577787401742e8 seconds
+ arrival date: 2029-04-08T11:52:56.730
+ thrust profile: [0.4206425964214093 -0.1056500975368615 -0.14482375512238757; 0.05058568725845576 0.013753831200102998 -0.05545521058740647; 0.06637099955207104 0.03439038533153343 -0.12048048273755668; 0.05966018046612129 0.042583596303696195 -0.15180586931922896; 0.0495459216231369 0.04283341865918786 -0.1625248119183193; 0.034600075549980396 0.03438759848028706 -0.140598958158434; 0.01355429594687025 0.014429423403836197 -0.06409505403185184; 0.004974808813389592 0.005960617318572703 -0.02789548463383187; 0.00370667858291133 0.0047328433080563205 -0.022464853019549653; 0.0010724463334109843 0.001284847900093056 -0.007307062389716741; 0.0013103252615252105 0.0015744916663223997 -0.008224765011454648; -0.00040986424748856785 0.0010278323665204822 -0.004485884152913117; -1.488509155973022e-5 0.0006124485954464966 -0.001358165687138965; 0.0005950273024140239 -0.0007617528132254082 0.0004541360736035055; -9.332832091284667e-5 0.000518934160422399 -0.0002881013622673225; -0.00089436546824937 0.000956045084161618 0.0014794459955594402; 0.000732223041543207 0.0006751506047703203 -0.001235022858131914; -0.0008035089980524139 0.00036441510997111136 0.003360458636580244; -0.0003611970266810251 -0.0014365184200861847 -0.002130179979208599; -0.0017391044799226327 0.0009228716281265076 -0.00436801352100496] %
+
+Mass Used: 98.9557193083624 kg
+Launch C3: 95.39766082107184 km²/s²
+||V∞_in||: 5.89695941627443e-9 km/s
diff --git a/archive/ES_0.5618084750261633 b/archive/ES_0.5618084750261633
new file mode 100644
index 0000000..871265e
--- /dev/null
+++ b/archive/ES_0.5618084750261633
@@ -0,0 +1,22 @@
+archive/ES_0.5618084750261633---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T18:24:46.737
+Launch V∞: [6.314733629070333, -7.389093038837506, 0.0564136961676937] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007531624826176098, -0.004467832369608986, 0.0061899508465694955] km/s
+ V∞_out: [-0.005381322760976488, -0.004306572867561391, -0.0033789958817911888] km/s
+ time of flight: 1.8749577787468514e8 seconds
+ arrival date: 2029-04-09T20:34:23.737
+ thrust profile: [0.5106360600994654 -0.12280388720756062 -0.17819726765233868; 0.05683722975198537 0.014892003027029818 -0.06578410075105752; 0.049774039013584744 0.0254901324787539 -0.09639931453925268; 0.058474866706798 0.04075640322718208 -0.15503380945694112; 0.048698205124837454 0.040942124109432224 -0.16928871336512588; 0.02115173684923415 0.01992932394402651 -0.09098079889613125; 0.009557591745222542 0.009882712458618804 -0.05015718193189176; 0.00606775244144807 0.006327700833393695 -0.03479634984573709; 0.007960235364919493 0.009632617469939117 -0.052723210626851154; 0.005242626843034082 0.006159079526954547 -0.03314871287549313; 0.0003030256865798373 -3.042923635654518e-5 -0.001980483410729786; 0.0005634523504781156 0.0013105503432758276 -0.007152877938586436; -5.6285428452026456e-5 0.00023853770878672743 -0.0017930385024106416; 5.050731996761841e-5 0.0002629364571458387 -0.0007254756293750779; 8.418773300230385e-5 -0.0001187195357556834 -0.001133757003939181; 0.0001896058666814068 -0.0001775206369395912 0.0006919007622972202; 0.00022398315567080044 0.0005788317238084143 -0.0007202539176467551; 0.0007243857620872101 0.0002481440824807709 -0.0014330619479488533; 0.0018227188423743535 0.0010015085683902324 -0.0021404049274478267; 0.0005060650481037402 -6.807090688571312e-5 -0.00023960094990248439] %
+
+Mass Used: 104.32307525155056 kg
+Launch C3: 94.47773924782398 km²/s²
+||V∞_in||: 0.007671001974389981 km/s
diff --git a/archive/ES_0.5618173409028855 b/archive/ES_0.5618173409028855
new file mode 100644
index 0000000..d90f273
--- /dev/null
+++ b/archive/ES_0.5618173409028855
@@ -0,0 +1,22 @@
+archive/ES_0.5618173409028855---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:13:13.495
+Launch V∞: [6.302213207145994, -7.458362533063383, 0.11517000913658623] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0015438783950462635, 0.0013820590943912495, 0.00161886493110792] km/s
+ V∞_out: [-0.0017953578912598526, -0.0009174697614109243, 0.0016883148169879372] km/s
+ time of flight: 1.8329834360011867e8 seconds
+ arrival date: 2029-02-19T16:25:36.495
+ thrust profile: [0.4431412795479208 -0.1489310387076754 -0.16793161809134644; 0.04748997546914024 0.007189405071981327 -0.05700217100364162; 0.045816628165193336 0.015681148798907776 -0.09265805125273446; 0.0635912376737072 0.028440253293418184 -0.17500339233620113; 0.05641648147765174 0.029250875552064494 -0.19504401487630746; 0.02370131744937129 0.014395833897199036 -0.10278346768205099; 0.015730819713182687 0.010175435768901923 -0.07897907738877695; 0.009019763357737446 0.0063278093325362175 -0.05235278354311539; 0.0020092256702781636 0.001541610537029651 -0.013643940302638035; 0.001869745630045114 0.0015326335502354222 -0.014481042959615897; 0.0011390246751846373 0.0008232510576358273 -0.008298147950542402; 0.00038837857370848554 0.00037260349475237096 -0.0032764393518586506; 0.00022389277015488757 -7.79476521565179e-6 -0.00041024635189926663; -0.000617090194226648 0.00047328363042460506 -0.0009864957392643771; -8.511149798592042e-6 -0.00011976969304527626 -0.0005994616755506403; 0.00021137592026628063 -0.0003642305049193831 -0.0006864332873609858; 0.0008351221184584491 -6.007165902030122e-6 -0.0008131528354183362; 0.00028770242845202075 0.00019662445369238125 -0.0010610524466105802; 0.00029724128843039974 0.0003561371531888803 -0.0016814525329756774; -0.0005123345543069711 -0.0009790303059050382 0.0003783544950813615] %
+
+Mass Used: 99.19665622208731 kg
+Launch C3: 95.35832711393356 km²/s²
+||V∞_in||: 0.0026295192534475267 km/s
diff --git a/archive/ES_0.5618198419009518 b/archive/ES_0.5618198419009518
new file mode 100644
index 0000000..22922c4
--- /dev/null
+++ b/archive/ES_0.5618198419009518
@@ -0,0 +1,22 @@
+archive/ES_0.5618198419009518---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T17:19:13.983
+Launch V∞: [6.57347531476243, -7.329173922706785, 0.1814971607101879] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010677981604606522, 0.0011321021286647187, 0.0010896589197505744] km/s
+ V∞_out: [-0.0012744325331764438, -0.0006225445281727385, 0.0012637985638248577] km/s
+ time of flight: 1.874957778749391e8 seconds
+ arrival date: 2029-04-08T19:28:50.983
+ thrust profile: [0.2586268579093091 -0.06690577468279013 -0.08963782133988447; 0.10178073194595655 0.027300717181880887 -0.10915636155758993; 0.08090818103054996 0.04188447459377707 -0.14585959850841432; 0.05673276841110213 0.039415147995118055 -0.1443723635187975; 0.04076325220119373 0.03429476249452904 -0.13403738275220042; 0.01682849100611772 0.016388339921882707 -0.06953616931831638; 0.02085907249830255 0.0227480406028238 -0.1003127126447082; 0.005325295540751251 0.006298656480272786 -0.0309685079610853; 0.0050888181750382445 0.006509087971831445 -0.033138270770478144; 0.0007268187174946847 0.0008035012308806482 -0.005201906151042346; 0.0040730331957485235 0.005881447040007418 -0.03203638525724174; -2.5045964529674922e-5 5.858967896419718e-5 -0.00033185479743863815; 0.00025739990328081837 -0.00038165098457610823 -0.0006429092395098858; -0.00014743338574246833 0.0002320000869368013 -0.0007970809493779855; -0.0006943205560371632 0.0016559126827697822 -0.0004099645638345565; -0.00032682837407443943 0.0017999305619453342 0.0006440361219725544; 0.0006504452281811613 -6.244157982881487e-5 0.0007097822637718797; -0.0015962130683159644 -0.0007035076781282726 0.00017199034742983372; 0.0005368725784572356 -6.59525392157632e-5 -0.0004675260028216394; -0.0008205538183248925 -0.000927543225896348 0.0014382781025878313] %
+
+Mass Used: 89.85467783698186 kg
+Launch C3: 96.96030932242205 km²/s²
+||V∞_in||: 0.0018997906996830805 km/s
diff --git a/archive/ES_0.5618202396904217 b/archive/ES_0.5618202396904217
new file mode 100644
index 0000000..e37d119
--- /dev/null
+++ b/archive/ES_0.5618202396904217
@@ -0,0 +1,22 @@
+archive/ES_0.5618202396904217---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:00:32.007
+Launch V∞: [6.605402456913733, -7.4342641500914, -0.03933504997399085] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01907081738396003, 0.00029223811704575303, -0.013287939067873218] km/s
+ V∞_out: [0.022310545013291695, -0.0002279462870432513, -0.006516847566516822] km/s
+ time of flight: 1.8749577787492964e8 seconds
+ arrival date: 2029-04-10T20:10:09.007
+ thrust profile: [0.14585674778199925 -0.0365220889240562 -0.06098473534105503; 0.07327763725680189 0.01803501920869538 -0.0941360638589436; 0.051427234215737506 0.025202680402061355 -0.11216195798518437; 0.047645019896644845 0.03524898772363109 -0.1799526730167105; 0.029053658109806493 0.022416309929154086 -0.10964661299231537; 0.022859724398520666 0.020728492071623618 -0.10738885259598237; 0.01504880070745601 0.014504386219543954 -0.08256098798792215; 0.008856132455944953 0.009511786379011844 -0.05573185212242835; 0.0019874865384018705 0.0020759054029325093 -0.013807181295652731; 0.0061662609978296555 0.00651017229897975 -0.04976426573028043; 0.000623915636444613 0.0007781038335612124 -0.00520885458158162; 9.794901162839546e-5 2.524403646698482e-6 -0.00021630060928172598; 0.0004728614789640143 -0.0003773830197866183 -0.00197713021700531; -0.0007901548539067064 -0.00031917913235714255 -0.0013795016379179149; 0.0018112972620310918 0.000980864081487709 -0.0019432922779543263; -0.0007960060810665967 0.0007995380613802627 -0.0007815487547046647; -0.0014767405636444964 -0.0009061192716916301 -0.0022917671166409496; -0.00021635736698780682 -0.0005429536209853496 -0.0008060050750389102; 0.00015703493283996772 -2.829200264368179e-5 -0.0005063229448871577; -0.0005712845490399828 -0.00014735310727948556 0.001197474198866627] %
+
+Mass Used: 78.5334411212848 kg
+Launch C3: 98.90117231729266 km²/s²
+||V∞_in||: 0.023245446940872484 km/s
diff --git a/archive/ES_0.5618259978053788 b/archive/ES_0.5618259978053788
new file mode 100644
index 0000000..1c42e3e
--- /dev/null
+++ b/archive/ES_0.5618259978053788
@@ -0,0 +1,22 @@
+archive/ES_0.5618259978053788---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:30:09.981
+Launch V∞: [7.871066727512772, -5.918333845327766, 0.03424521815574416] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3353279025977228e-5, -0.0016439722026928714, -2.3901519226962333e-5] km/s
+ V∞_out: [-0.0015872632720789633, 0.0002557226443058505, -0.00034467828019714593] km/s
+ time of flight: 1.7775132130986628e8 seconds
+ arrival date: 2029-12-29T21:52:10.981
+ thrust profile: [0.33301034269025537 -0.03631604781839619 -0.12110499088973263; 0.045074891868893074 0.01736871697832938 -0.05692246920715641; 0.04083559825996075 0.02550024130940792 -0.09135457414556779; 0.03493671111953335 0.027565269716846953 -0.11199168126676383; 0.029674442482817195 0.02769045687199389 -0.12586616604162731; 0.019124249250383047 0.019548988742052912 -0.09989316134192658; 0.02018067340105359 0.02184405198548532 -0.12078333975385494; 0.016056491499561495 0.019179981820801138 -0.11230352124882004; 0.004899872171625041 0.005460143504176693 -0.029324326556341856; 0.001742332611381165 0.0024199551043455995 -0.015166660975803836; 0.0008337235414246248 0.001017778762886784 -0.014305542487219033; 0.002054581237128192 0.0014323101017878132 -0.0095840510788486; 0.0006911175446362243 0.0007645495525895368 -0.004920429817425005; 0.0020552490911862754 0.0010451007477186723 -0.004465955767796044; 0.0004969600320431497 0.0007468803425058539 -0.004350657325234393; 0.0008786851141363477 -0.0019229725978495865 -0.002096569060370891; 0.0010586247665384347 0.0032338938612790423 -0.0046444854933840735; 0.007188371224939813 0.00741411653667055 0.006944094209476924; 0.004070995669566159 -0.007566482719763147 0.01384590307889333; -0.0030012290491506707 -0.014622222691549312 0.005868843962896693] %
+
+Mass Used: 89.73801603899119 kg
+Launch C3: 96.98153966867727 km²/s²
+||V∞_in||: 0.001644311789621869 km/s
diff --git a/archive/ES_0.5618388431723023 b/archive/ES_0.5618388431723023
new file mode 100644
index 0000000..321715b
--- /dev/null
+++ b/archive/ES_0.5618388431723023
@@ -0,0 +1,22 @@
+archive/ES_0.5618388431723023---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T03:31:13.421
+Launch V∞: [7.8500277032064405, -5.705995228192062, 0.5398824389881433] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4866884974213415e-6, -3.7286456333787813e-6, -1.364691097684271e-5] km/s
+ V∞_out: [-1.298349417269332e-5, -1.5040397930851318e-6, 5.601190829746404e-6] km/s
+ time of flight: 1.8749577786092106e8 seconds
+ arrival date: 2030-04-20T05:40:50.421
+ thrust profile: [0.39542373240974116 0.025115614436066334 -0.0793306843524165; 0.10757465067190858 0.08146899535882295 -0.08238056594215756; 0.12433971949704205 0.1521835041281337 -0.1602429730893024; 0.03754044737790792 0.06797980710477915 -0.08617366555022712; 0.03852213929811199 0.09578777242422613 -0.12477736563861165; 0.016722096199047614 0.05070480862113984 -0.07377009106163919; 0.01159451552287417 0.047836681269581446 -0.07367941349210506; 0.003642394346543484 0.018382514153119856 -0.032520145685267364; 0.0014533206918249668 0.009665053908018889 -0.016827710464114284; 0.0012429712913939032 0.009065789496548352 -0.015484526327545926; 0.0003096121619883702 0.007161344842923365 -0.013988391381162724; 0.0015001502518427324 -0.00016378097628700906 -0.001140864949425987; 0.00040482609670588294 -0.0012399120599258543 -0.0004440843007898561; -0.003328799143205234 -0.004898636306912693 -0.003259336683882684; -0.0002067785125729218 -0.0023499664097461582 -0.00038015791450046743; 0.002335007137548627 0.0029209162964236616 -0.0005666309097503938; 0.0007173838555150555 0.0015571933535706733 -0.003183328471709564; -0.0019158588732491565 0.00206305809484023 -0.005258460735443871; -0.001022500644166927 0.0060596352199333405 -0.0007945789746356912; 0.001860758769106186 0.0010243016603626804 -0.00014136406878820392] %
+
+Mass Used: 104.38737809076201 kg
+Launch C3: 94.47278953318695 km²/s²
+||V∞_in||: 1.4225020919406398e-5 km/s
diff --git a/archive/ES_0.5618446484976481 b/archive/ES_0.5618446484976481
new file mode 100644
index 0000000..b1ff5fe
--- /dev/null
+++ b/archive/ES_0.5618446484976481
@@ -0,0 +1,22 @@
+archive/ES_0.5618446484976481---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:21:57.948
+Launch V∞: [6.559367131483516, -7.462042149826284, 0.17341398403386107] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.028260043577617e-9, -7.795902003498583e-11, -5.218215321746001e-9] km/s
+ V∞_out: [-4.852903517514499e-10, 1.2041130496792277e-9, 1.6159018635808072e-9] km/s
+ time of flight: 1.852112792301029e8 seconds
+ arrival date: 2029-03-14T05:56:36.948
+ thrust profile: [0.1506627751168479 -0.04038081934318866 -0.057095716866732545; 0.04955745456400364 0.011792891135053812 -0.05655886832785028; 0.08138742209852852 0.039586257108018885 -0.15207660121096142; 0.0377884327241078 0.024177298296958232 -0.10032345253398371; 0.035032793820607463 0.027035701727472505 -0.11864431657509426; 0.030001726390646993 0.02634668219620026 -0.12288712045175851; 0.022500941510681646 0.02182505182261344 -0.1083208221318539; 0.01501417661057009 0.0156364029272068 -0.08315055748522977; 0.005276467886947756 0.005696886822813852 -0.033101460781061694; 0.007104527910111108 0.008285278748172932 -0.04865235830345109; 0.00037283560926527865 0.000545289767966794 -0.0026044254636780908; 0.0002854851776241182 0.00045147510770733644 -0.0026733779401101505; 0.00010234359959029093 -0.0003887051428564346 -0.00046148991806584214; 0.00010301817328567518 0.00033046814553176263 -0.0005307119961967239; -0.00021522359215148042 -1.8769371406730264e-5 -0.0005313226806262153; -5.6624564794180736e-5 0.0004100881015151498 -0.00044024810973973576; 6.384743222062031e-5 3.845627252664543e-5 -0.001083526306943264; 0.0006535295851647414 9.803516921190906e-5 -0.0005870803450655796; 0.00017714276646429845 8.828955688020197e-5 -0.000735042930387307; 0.00011404749331853374 -5.78059280486945e-5 8.870100797179331e-5] %
+
+Mass Used: 79.5170079567547 kg
+Launch C3: 98.73744262122884 km²/s²
+||V∞_in||: 7.2470164770579015e-9 km/s
diff --git a/archive/ES_0.5618499172193101 b/archive/ES_0.5618499172193101
new file mode 100644
index 0000000..790471c
--- /dev/null
+++ b/archive/ES_0.5618499172193101
@@ -0,0 +1,22 @@
+archive/ES_0.5618499172193101---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:39:26.658
+Launch V∞: [7.824466370149646, -5.677285725672265, 0.36036050039620054] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.34861363178562e-8, -6.484436787854909e-7, 1.5691024769157804e-5] km/s
+ V∞_out: [6.822134205229886e-7, -1.571962708396431e-5, 1.8774624691081155e-7] km/s
+ time of flight: 1.874957778723665e8 seconds
+ arrival date: 2030-04-19T17:49:03.658
+ thrust profile: [0.4745265631083513 0.02136118454760956 -0.08503088955033505; 0.1354358858453574 0.09961758912029726 -0.09694474116759869; 0.06579340721208278 0.08771563449056063 -0.09412734711101718; 0.05410306684969992 0.09564505401753422 -0.11365553640095477; 0.017986223924034622 0.04460166632035805 -0.05692334363435577; 0.026952416775145458 0.07217564629243681 -0.09684607873138541; 0.013670544499904376 0.05591725723238035 -0.08316396374279356; 0.010034707629581474 0.05110802333192896 -0.07885756840937416; 0.0030267323632834887 0.017604631036469698 -0.031054949075114982; 0.003347002867570284 0.02490781760330626 -0.04238545282257013; 1.2849308563166105e-5 0.00030905565651841507 -0.0007315809977465356; 5.3676385835341926e-5 -0.0005115478633368454 -0.00047250041144026857; 6.184592951020328e-5 -3.22359672578704e-5 -0.0002219772546534621; -0.00029921629634887083 8.739618885062069e-5 0.0005086642427241596; -0.0008084529835608145 -2.939415577714972e-5 -0.0002201230377790887; 0.00030082645251594347 -0.0005436056333455817 0.0005154103116195206; -0.001162604948915819 -0.0003430259600999095 0.0005473470626844388; 2.9037353378446554e-5 0.000603798506372653 0.0011108689624512373; -0.001616514342684608 0.000316531725496021 0.000924504480089108; -0.0007378453409115306 0.000827422270392122 0.00017372627860807056] %
+
+Mass Used: 109.58661329636652 kg
+Launch C3: 93.58370687877063 km²/s²
+||V∞_in||: 1.5704696022800448e-5 km/s
diff --git a/archive/ES_0.5618606982060548 b/archive/ES_0.5618606982060548
new file mode 100644
index 0000000..5854d40
--- /dev/null
+++ b/archive/ES_0.5618606982060548
@@ -0,0 +1,22 @@
+archive/ES_0.5618606982060548---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T22:54:54.459
+Launch V∞: [6.676389368557941, -7.411162624091364, 0.11255911327948775] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.524229803415302e-8, -5.0232422517530604e-8, -2.909641861795667e-8] km/s
+ V∞_out: [1.625719825664514e-8, -3.6255011207820245e-8, 4.927776425127142e-8] km/s
+ time of flight: 1.874957778746294e8 seconds
+ arrival date: 2029-04-11T01:04:31.459
+ thrust profile: [0.12236153496797673 -0.034895247997824966 -0.05035733204989604; 0.053306715439957235 0.010301542086195629 -0.0680148436250225; 0.028093051476754866 0.010899336481924336 -0.06009298820902078; 0.05402303451898501 0.030093545004776814 -0.17181446572142078; 0.028096684017251794 0.017059041916587393 -0.10822551737632392; 0.028739614080015314 0.02046932917726067 -0.13861949875086835; 0.023436779238217097 0.019085209915042964 -0.1374394515555635; 0.007139216874134618 0.005210335480314201 -0.04268391188882691; 0.006087610782154897 0.0048178414328142165 -0.04113563119517701; 0.0016395441098635477 0.0011838674059347386 -0.013166464698395323; 0.0006823774864126627 0.0005825931637178704 -0.0064679824677556464; 0.00044876380171546433 0.0005097654284719268 -0.005572228738670084; 0.0005308254018998887 0.0008947463316940355 -0.008347287375397342; 3.557569264208923e-5 0.00011499067792474291 -0.004593733182928964; -0.0011593016429442533 0.00011788579479715032 -0.00023293365262399852; 0.0004649507977415536 0.0004435992478191493 -0.003387452561020332; -0.00021791191925243632 -6.705750051880829e-5 -0.001063419740023614; 0.0008572453036830108 0.0004982244777297656 0.00014736467269546236; 0.0006069357490351914 0.00033500812015494505 0.0026069966139623457; 0.00036360164794008165 -0.00014976860233373377 -0.0007776989970246283] %
+
+Mass Used: 75.01645460112059 kg
+Launch C3: 99.51217599530456 km²/s²
+||V∞_in||: 6.330143330459506e-8 km/s
diff --git a/archive/ES_0.561861590803818 b/archive/ES_0.561861590803818
new file mode 100644
index 0000000..1e03711
--- /dev/null
+++ b/archive/ES_0.561861590803818
@@ -0,0 +1,22 @@
+archive/ES_0.561861590803818---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T12:18:01.369
+Launch V∞: [7.64711561109135, -5.918983986277939, 0.10033869373983838] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.769808422956256e-10, -1.2231453504566174e-9, 6.706589699052458e-10] km/s
+ V∞_out: [4.595204370597595e-10, -1.55642518320517e-9, 2.416022621556932e-10] km/s
+ time of flight: 1.7861091273535398e8 seconds
+ arrival date: 2030-01-06T18:26:33.369
+ thrust profile: [0.4878425481848314 -0.02554592093617152 -0.13706264886431935; 0.18777235734995143 0.09972036907261346 -0.19033866132432065; 0.08482784700777435 0.07526261694787864 -0.1567372954435855; 0.029620956384126807 0.03447005845432 -0.08373829778351172; 0.027686426899804804 0.03975485526547229 -0.10449504776864563; 0.01905432625740265 0.03235049184382376 -0.09141458801070931; 0.022055131663695597 0.044424601995340415 -0.1308677626469598; 0.004520485003169818 0.010985365534322673 -0.035226807124765634; 0.0010912599606038608 0.0033212252239488505 -0.01005592616593681; 0.0004402322668439995 0.0017352123984444997 -0.003195689834287209; -0.0008499393219787005 0.002459775470212123 -0.005806812251443998; -0.00034996128726894456 -0.0017245946491559678 0.0024808616757069175; 0.000695098088636853 -0.0006170534085285539 -0.001969070777399439; 0.0076809634089513345 -0.0005618885107666629 0.00020876403217899575; -0.004589197540633142 -0.00409885586473997 0.004476358504960773; -0.00015492755526408917 0.00027051066404010866 0.0015171948488879082; -0.012174183129523161 -0.00037185828019936743 -0.0027100034655502298; -0.00021405154023433441 -0.0003452218555229466 0.0019632997457739907; -0.0015052704146938799 0.0029133672172493227 0.01371768148283107; -0.001198597654750797 -0.0017039880038006517 -6.566591649492066e-5] %
+
+Mass Used: 109.95542663052765 kg
+Launch C3: 93.52281645267314 km²/s²
+||V∞_in||: 1.7030442062585096e-9 km/s
diff --git a/archive/ES_0.5618666778811191 b/archive/ES_0.5618666778811191
new file mode 100644
index 0000000..654c4f3
--- /dev/null
+++ b/archive/ES_0.5618666778811191
@@ -0,0 +1,22 @@
+archive/ES_0.5618666778811191---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:09:39.541
+Launch V∞: [6.424636294663653, -7.508593694910719, 0.11031911695433098] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.827194619173445e-7, 4.43069786744268e-6, -2.573876015023648e-7] km/s
+ V∞_out: [1.6115152547955156e-6, -3.608668366470464e-6, 2.101235060913731e-6] km/s
+ time of flight: 1.8477737510388586e8 seconds
+ arrival date: 2029-03-09T02:12:34.541
+ thrust profile: [0.21208303006223853 -0.05338849039937016 -0.07661305124892123; 0.08393727075304 0.023000548528509537 -0.09181021396370477; 0.06254966510400176 0.03425091429602578 -0.11682231841982864; 0.0515520540463507 0.03931193607943125 -0.13479629376079408; 0.04281040516736549 0.039638115974360934 -0.14345314144230165; 0.03377178083972992 0.03184164934913454 -0.13011906027850761; 0.0197285504794035 0.022125398965828342 -0.09536603995758346; 0.007047945315842613 0.008484534789635293 -0.03875314406403914; 0.002663262970264036 0.0032847272201070427 -0.016461111364096125; 0.007735774906579236 0.010007293434596849 -0.04991379195224129; 0.002067881593342685 0.002641193506021573 -0.014826530939203593; -0.00018206397939945457 9.695381877585275e-5 5.8237888622839475e-5; 7.593675468737378e-5 0.00019614756049421243 -0.0001583843061338556; -3.2588633904970406e-5 -3.610199574404665e-5 -0.0004139892995098765; 0.0006699923051634758 -0.000589421882308458 -0.0001307978351524037; -9.60999836889055e-5 -0.00027926308441839694 -9.585607414091467e-5; 0.0003275096646942441 -0.00014984100545407264 -0.00031305929795266756; 9.886958762441957e-5 -0.0004932164389699874 -0.00036831287708766506; -0.00018351902062250022 0.0007433471601445522 -0.0005879843052704243; 6.213488839163346e-5 0.0002094034585154191 7.505185344047879e-5] %
+
+Mass Used: 85.78636776905842 kg
+Launch C3: 97.66710110152809 km²/s²
+||V∞_in||: 4.476258922500517e-6 km/s
diff --git a/archive/ES_0.5618699940668945 b/archive/ES_0.5618699940668945
new file mode 100644
index 0000000..be6b05b
--- /dev/null
+++ b/archive/ES_0.5618699940668945
@@ -0,0 +1,22 @@
+archive/ES_0.5618699940668945---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T18:55:22.817
+Launch V∞: [7.789152584769955, -5.825048276605989, 0.4633440875169116] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0194556877190765e-9, -1.2556612818429157e-9, 4.5735348676276106e-10] km/s
+ V∞_out: [4.441775947862767e-10, -1.4319707031460727e-9, 2.422468463585446e-10] km/s
+ time of flight: 1.874957778748698e8 seconds
+ arrival date: 2030-04-22T21:04:59.817
+ thrust profile: [0.3864202785172284 0.02170064718664074 -0.09627916679840721; 0.15340222406161344 0.10551064438326432 -0.13542714823796298; 0.0717777322815538 0.08084625787125384 -0.12176589886268124; 0.04139799374335319 0.06402841993839115 -0.11099291669763342; 0.013803270535770625 0.02746831588484035 -0.05359337796753028; 0.028780375757534324 0.06864241156555145 -0.1417923969099652; 0.0030695128334749418 0.011716938879413741 -0.02685731201368898; 0.007640269449693711 0.024398283588639432 -0.05328764500470126; 0.003537085166373202 0.014373771926069309 -0.035953620880280306; -0.0011920714118591553 0.0030352954353889197 -0.003186942441449912; -0.0004773020545860439 0.004879351619744184 -0.0068832817750266555; 0.0031598101206580334 -0.0016071598886787 -0.003999286758485158; -0.005660292194750392 -0.0008457069571346802 -0.001846823923727149; -0.0006735787799273516 0.009768758105506509 -0.003752981780086541; -0.0006910661230125569 -1.648381721859474e-5 -0.00883766405939191; 0.007211266463416396 -0.00042388178072023984 -0.002220224052128236; -0.0026356543363550656 0.0010815269825128811 0.002919482794458192; 0.0010071114576062593 0.005145260854397247 0.008776185418106494; 0.006644507240479736 0.0013236386705080896 -0.012473989581409094; -8.262632875733069e-5 -0.013722974992520367 0.0084283626187058] %
+
+Mass Used: 102.4171496618851 kg
+Launch C3: 94.81677315705574 km²/s²
+||V∞_in||: 1.6808174695059022e-9 km/s
diff --git a/archive/ES_0.5618705554414691 b/archive/ES_0.5618705554414691
new file mode 100644
index 0000000..cdcc527
--- /dev/null
+++ b/archive/ES_0.5618705554414691
@@ -0,0 +1,22 @@
+archive/ES_0.5618705554414691---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T15:48:31.439
+Launch V∞: [7.8174865146303585, -5.875997838464335, 0.3327524116893949] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.022470093371556074, -0.1419336574149141, -0.17165836855096317] km/s
+ V∞_out: [0.038316360430653854, -0.035935299702363525, 0.2177813719541497] km/s
+ time of flight: 1.7737824029807964e8 seconds
+ arrival date: 2029-12-22T15:32:31.439
+ thrust profile: [0.39906644653591533 -0.014312633917919261 -0.10417967324163356; 0.06354764045350389 0.03746913992541377 -0.0622451200128828; 0.05837821086209986 0.05739715620897065 -0.10265339361160956; 0.042228301487864335 0.05894015039283467 -0.11276317454953337; 0.029891855378787142 0.050997337322241876 -0.10317494403325914; 0.01880741558837527 0.03846712789231574 -0.0843894720380338; 0.009311666339792074 0.022210713925107886 -0.050407712626396484; 0.02399005304890282 0.0679152131918716 -0.15142625460309767; 0.009492281104229186 0.026734943160345716 -0.06859801731429352; 0.006027715876990559 0.02179581459566051 -0.05761295536992641; 0.0006605339463497214 0.0036299881627884444 -0.010434370177221264; -0.0005188717239718601 0.0004154403388335615 -0.000495891901205884; 0.00011579297193888829 0.000667763704157571 -0.0019339308770817438; 0.0002134557225249684 -0.0003950804509826581 -5.2783903600018634e-5; 0.0003875386536254887 0.0014178461300407709 -0.002344283136667724; -7.947488080557133e-5 0.00021463358609226992 -0.00020296052049835218; 0.0006988598548566393 0.001261511656650026 -0.0011427163500543646; 0.0004288926384018588 -0.0018409240072907347 0.0005841117499456713; -0.0013800508080594892 -0.0025179093953511134 0.0006842140485425172; 2.669342222370741e-5 5.493248454852646e-5 -0.0008479908215393634] %
+
+Mass Used: 96.96715534767145 kg
+Launch C3: 95.75117017155014 km²/s²
+||V∞_in||: 0.2238675137148732 km/s
diff --git a/archive/ES_0.5618721950310563 b/archive/ES_0.5618721950310563
new file mode 100644
index 0000000..eddabb7
--- /dev/null
+++ b/archive/ES_0.5618721950310563
@@ -0,0 +1,22 @@
+archive/ES_0.5618721950310563---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T08:17:28.362
+Launch V∞: [7.820282159818259, -5.77746922177385, 0.018616123962607766] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3522752422023898e-9, -1.4301436702702132e-9, -1.4714889374869549e-9] km/s
+ V∞_out: [2.805811879961478e-10, -2.5488035455500866e-10, 9.689653604557443e-11] km/s
+ time of flight: 1.8146038512071753e8 seconds
+ arrival date: 2030-02-08T13:57:13.362
+ thrust profile: [0.45501553560101177 -0.003214980404736488 -0.11821354996880774; 0.10902943444140001 0.06635098346788734 -0.10329765566333701; 0.06454387641786365 0.06460957929712073 -0.10789377153109796; 0.03197995767263808 0.04411976730940818 -0.08308266735939554; 0.03495879154750343 0.06061938834271011 -0.12136856345931707; 0.014076627999487088 0.033577051318257 -0.07005677810929566; 0.02368146629622959 0.05904743522754681 -0.13374898621966688; 0.0020492464916443856 0.005160648522676981 -0.014557392122104648; 0.012161886199655894 0.04884755779946665 -0.11591942044485455; -0.0008346053204050778 0.001165185649970525 -0.007920290655602331; 0.001105794829013297 0.00302997010944828 -0.01088144761675141; 0.0016603823457358577 0.0028933641574657998 -0.004431708783208506; -0.002147705689351442 0.0003355008647855629 -0.002165758779412068; -0.00018592925332165802 -0.0012992323274835526 0.0029047110346612738; 4.853899189976576e-5 0.001447671425128363 0.0010044432584509805; -0.0001644641997129382 0.0008950245929359459 0.001143436272622389; -0.00011930145669556292 -0.0002197475963507116 0.00017938972185415941; -0.00017230791281416227 -0.0003800656836724877 0.002266331275416604; 0.0016306402139270896 0.0026293321557091516 0.005961562067161196; 0.011860466546713749 0.0027060336078245893 -0.000782450278702091] %
+
+Mass Used: 104.05575120747335 kg
+Launch C3: 94.53631022778725 km²/s²
+||V∞_in||: 2.4574863054417975e-9 km/s
diff --git a/archive/ES_0.5618819047709153 b/archive/ES_0.5618819047709153
new file mode 100644
index 0000000..71c4730
--- /dev/null
+++ b/archive/ES_0.5618819047709153
@@ -0,0 +1,22 @@
+archive/ES_0.5618819047709153---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T14:45:16.102
+Launch V∞: [7.911314965646446, -5.488326195736625, 0.20782547813420119] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.768064713993662e-8, 4.1335284967127747e-7, -7.4140356080162e-8] km/s
+ V∞_out: [6.770363056642634e-8, -2.4236046737452357e-7, -3.3407499116500607e-7] km/s
+ time of flight: 1.8749577787327367e8 seconds
+ arrival date: 2030-04-18T16:54:53.102
+ thrust profile: [0.630020824961864 0.013590530625153197 -0.14629923897960304; 0.11164788457375392 0.07865573331445175 -0.09859115488573665; 0.05393961578883037 0.06442586982824815 -0.08926804266727985; 0.046481178194241184 0.07600460082253167 -0.11601178741462699; 0.04146745139795316 0.08788220422050277 -0.14110505677595528; 0.012525376449772476 0.03811963470684969 -0.06735424042690924; 0.0028080302058308376 0.009574059583768882 -0.018652353671849645; 0.007468120408321632 0.035839532279959424 -0.07371163325627254; 5.699201571385487e-5 0.0019760062454353437 -0.00476104381097569; 0.00260277045463118 0.011966051775100073 -0.027839442088414042; 0.0022302870824956154 0.018979767008210274 -0.043116994508539404; 1.9402472375748667e-5 0.0010031328257582028 -0.0025945908198023167; 0.0007753583120132521 0.00015276405385699151 -0.0016061233509131415; 0.0003291000720588149 0.0006183380264577304 5.964811803624119e-5; -0.0005805821350806913 -0.001157070322547945 -0.0015551557002299495; -0.0001049131157032676 0.0004878936923596966 -0.0011689168537266199; 0.00030626165676477023 -0.0004033480347116064 -0.00016561269558460227; 6.486710937693646e-5 -0.00015818449825153073 0.0007927774327780816; 0.0015816453246269712 -4.990460163739155e-5 0.0010064028827275746; 0.0010924954691976674 0.00039396499679231515 0.00040970879553723787] %
+
+Mass Used: 114.46493688204782 kg
+Launch C3: 92.753820345832 km²/s²
+||V∞_in||: 4.226473883070166e-7 km/s
diff --git a/archive/ES_0.56188876179609 b/archive/ES_0.56188876179609
new file mode 100644
index 0000000..9fb60f1
--- /dev/null
+++ b/archive/ES_0.56188876179609
@@ -0,0 +1,22 @@
+archive/ES_0.56188876179609---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T06:47:44.061
+Launch V∞: [6.537980553820228, -7.482372051029858, 0.1037140626325487] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4941974578847957e-7, -9.760802160575083e-7, 6.397601567093389e-8] km/s
+ V∞_out: [-3.3128538645592664e-7, 8.779091104523539e-7, -4.4131449716251876e-7] km/s
+ time of flight: 1.8556113377440107e8 seconds
+ arrival date: 2029-03-18T23:33:17.061
+ thrust profile: [0.16724074187806864 -0.04622064017256746 -0.06533577531758337; 0.04085771082256034 0.008881055406495099 -0.048311995786200365; 0.05302014784359945 0.023434646854748428 -0.10417302373908632; 0.048166301324617786 0.028761062192397987 -0.13284329603424885; 0.053793771655053925 0.03836978014522738 -0.18641137163504204; 0.02296508792565788 0.018324626819984962 -0.09805856076523099; 0.012988483110593054 0.01120874904477202 -0.06469521680107616; 0.024142781359299682 0.02303307462836441 -0.13609446579731138; 0.003891639216586948 0.0037417229361239243 -0.02415023694737741; 0.0017707160022610992 0.0016644741344718028 -0.011482306563333367; 0.0004419397238466168 0.0005046395846390632 -0.002700429881596727; 0.0003719876603635967 0.0016298282891593872 -0.0019903584347209556; -0.0004745126406961465 0.0007356439010859283 -0.0015134340984848647; -0.0005317680739701772 0.0007995063144398087 -0.0025686179889809; 0.0003888964292794984 -0.00010285998229418681 -0.0006066247509599572; -0.0004592604648162588 0.00035246622282563604 -0.0020203526706930332; 0.000236244905089702 0.0008894981465779528 -0.0008519528144752813; -0.0006528404307336775 -0.0008126365148679719 0.0009939580902273177; -0.0010133747887171027 -0.0004200337592298346 0.002313082081519596; 5.260622629951165e-5 0.00016935690746934702 0.0021628652604934314] %
+
+Mass Used: 79.54283470155178 kg
+Launch C3: 98.74183783895198 km²/s²
+||V∞_in||: 9.895209847150761e-7 km/s
diff --git a/archive/ES_0.5618954997152742 b/archive/ES_0.5618954997152742
new file mode 100644
index 0000000..929af02
--- /dev/null
+++ b/archive/ES_0.5618954997152742
@@ -0,0 +1,22 @@
+archive/ES_0.5618954997152742---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T23:42:47.630
+Launch V∞: [6.486322083885765, -7.386400260968912, 0.19813244478716355] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012242374820103383, -0.0077841414222494494, 0.010939006536260502] km/s
+ V∞_out: [-0.009143110444250126, -0.007929881690478152, -0.005938192446870983] km/s
+ time of flight: 1.8589705219172955e8 seconds
+ arrival date: 2029-03-21T13:46:59.630
+ thrust profile: [0.32552082351306183 -0.08545188166523236 -0.1181213758317778; 0.04756177036990029 0.011596182518187587 -0.05483329215852841; 0.05397110779832241 0.026206107654915954 -0.10351680306684573; 0.07503635026656462 0.05010846880290445 -0.19620096388522534; 0.035013720854960656 0.0273340185864329 -0.12000398447686718; 0.026361450296267505 0.023527338299777996 -0.11016235131402619; 0.014423442571883518 0.014195469066844395 -0.07168089446646356; 0.015788506036725124 0.01686565556412536 -0.08839421143411903; 0.0011251971641376454 0.0017945299296809733 -0.009008655020284815; 0.0024061953343725473 0.0028405543771380212 -0.01916157452590391; 0.0015801361948578586 0.002378356577738906 -0.010696838367647439; 0.0028039873041745844 0.0010097340279657265 -0.0022256055827075986; 0.0005525185314338057 -0.0006240271796884955 -0.0014470754361148382; 0.0015651539510114366 0.0004959371941650742 -0.0007744850242205799; 0.0008598413599184818 -8.768119641705812e-5 9.528434362029081e-5; 0.0010595549047503112 0.00034782857152613377 -0.004173089913836544; 0.004429975316518288 0.0003715701591011749 -0.006757123827695662; 0.00020514315452959135 -0.00014840857488728518 0.00047178933478215774; -3.9818126086406565e-5 -4.914666321821729e-5 0.0005189112073367107; 0.0006485138882343916 0.0009787646731958598 -0.0004086251246659512] %
+
+Mass Used: 91.63326950301825 kg
+Launch C3: 96.67053945682314 km²/s²
+||V∞_in||: 0.013481597794560134 km/s
diff --git a/archive/ES_0.561901320735432 b/archive/ES_0.561901320735432
new file mode 100644
index 0000000..5e934cb
--- /dev/null
+++ b/archive/ES_0.561901320735432
@@ -0,0 +1,22 @@
+archive/ES_0.561901320735432---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:52:56.018
+Launch V∞: [6.618146487282361, -7.430520486232809, 0.2340604325114654] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1504978694393627e-8, -1.93997954172894e-8, -1.287883707435532e-8] km/s
+ V∞_out: [5.388126489140735e-9, -1.195149682205545e-8, 1.8341048552377724e-8] km/s
+ time of flight: 1.874957778746668e8 seconds
+ arrival date: 2029-04-10T21:02:33.018
+ thrust profile: [0.13945802319815837 -0.03763543676775541 -0.05276261487612758; 0.049750218367708654 0.010888959783096152 -0.05698488573630542; 0.057977508582553454 0.025055219633230694 -0.1118982317536768; 0.054199980593228995 0.03092484528246152 -0.1460855243303229; 0.04358160273519601 0.02935750528567736 -0.14982477545794148; 0.030173924828821606 0.022784074240834833 -0.1254281015799039; 0.01609500385829517 0.013195670259485096 -0.07799251793470213; 0.0056453917213457145 0.004760210382355463 -0.032241503307952044; 0.005354913926670804 0.005209797092875277 -0.03748896875520029; 0.0035704919452711364 0.004140355917390332 -0.030396866157829255; 0.005000228777142226 0.0059008234334553536 -0.03857710611429147; 0.002035250279187096 -0.0002743035286986876 -0.0013446526466575452; -0.00016676610688512244 5.1091502358061903e-5 -0.0003988932062943427; 0.00027957421718171905 0.0001926410923177965 -0.0003863465944079704; -0.00016475164638335595 -0.00013114043873517064 0.0009401596431191802; -3.311318701088329e-5 -0.00044207463008266604 0.0011685784014968349; -0.00044868916838894135 -9.996496614825506e-5 0.0007232779339284854; -0.00045293445776124514 0.001089851532831122 -0.0005965631468305653; -0.0006687085305192549 0.0009599329890262466 -0.0006189725710860395; -0.0004709252701908664 -3.871892349443791e-5 0.00139954587774002] %
+
+Mass Used: 77.65906305246608 kg
+Launch C3: 99.06728190952079 km²/s²
+||V∞_in||: 2.5972697999609577e-8 km/s
diff --git a/archive/ES_0.5619052251970009 b/archive/ES_0.5619052251970009
new file mode 100644
index 0000000..acd0c5b
--- /dev/null
+++ b/archive/ES_0.5619052251970009
@@ -0,0 +1,22 @@
+archive/ES_0.5619052251970009---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T03:26:08.984
+Launch V∞: [7.403287260395285, -6.110152066788512, -0.042990856011479485] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002711165460914655, -0.017205527527497894, -0.017032242813359598] km/s
+ V∞_out: [0.004171645724925333, -0.0038758896513750893, 0.023715354881001353] km/s
+ time of flight: 1.7727329194804052e8 seconds
+ arrival date: 2029-12-22T22:00:59.984
+ thrust profile: [0.63480598680077 -0.018656513928164593 -0.15127668349196577; 0.14672341651161833 0.08644741438858146 -0.1339883112402346; 0.06202301723441563 0.06242239162601386 -0.109160273536101; 0.05350117856180688 0.07494747123774305 -0.14056709131563813; 0.016783296709911244 0.027953073386943125 -0.06195267366308605; 0.017800596579692466 0.035482733415853944 -0.08646166828487785; 0.014742627830951484 0.0319188342368139 -0.08026293041336584; 0.014710399705921692 0.03903690134640407 -0.09962476574705348; 0.005600353720168539 0.0202072277578441 -0.0522281579305141; 0.004533699943006431 0.012141426788749984 -0.03614558775188041; 0.0009181617547107537 0.003933731621636782 -0.013470518040194421; 0.0007709898391100917 -0.00029739975478531525 -0.000962325466083499; 0.0007884862555447916 0.001705311095746469 -0.0006867976822295712; -0.0021933227998266478 -1.9394986001152414e-5 -0.0014239491433180136; 0.0015726029849062507 -0.00018816728640079375 0.0011581917734151453; -0.001233037152980719 -0.0007711419646077639 -0.0008399273202599014; -0.0038343605112268653 0.00024362536156714572 0.0016140213940144888; 0.0006266389824653585 -0.0031575324630366136 0.004173751411709163; -0.0002158906217354221 -0.0002064049094734015 0.0013309689500373072; -0.0022123593937260428 -0.0014864978410961032 0.003844357867250014] %
+
+Mass Used: 118.04669500451655 kg
+Launch C3: 92.14446875291164 km²/s²
+||V∞_in||: 0.024361401661423015 km/s
diff --git a/archive/ES_0.5619054167487083 b/archive/ES_0.5619054167487083
new file mode 100644
index 0000000..835fa00
--- /dev/null
+++ b/archive/ES_0.5619054167487083
@@ -0,0 +1,22 @@
+archive/ES_0.5619054167487083---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T09:23:40.410
+Launch V∞: [7.60248099503317, -6.266120465356939, -0.020723860077924067] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006848865381969703, -0.0018956610022126757, -0.0035837623208860247] km/s
+ V∞_out: [-0.0037352591041126225, -0.0004070914681006953, 0.001669455756062478] km/s
+ time of flight: 1.691670804734858e8 seconds
+ arrival date: 2029-09-20T08:15:00.410
+ thrust profile: [0.2906492873559197 -0.041718097732160765 -0.11170295691884488; 0.10518667411702265 0.038688719057260304 -0.13217052373601268; 0.03806718870317449 0.02328461714040308 -0.07845265607236988; 0.04046800887214125 0.03018296658904207 -0.11736892022892584; 0.030706275344873017 0.031160690512807062 -0.12966605450823712; 0.026680881908480034 0.025057653198898883 -0.12523079066524476; 0.02033549026749662 0.023235720483889652 -0.10372058140086947; 0.01604491937320905 0.017772177909055928 -0.10552039141814346; 0.014939006124617005 0.018657444756742077 -0.10987009086963763; 0.001792257113178271 0.0022517761147056313 -0.014573510270023439; -4.440557967960696e-5 6.48544620463088e-5 -0.00020031479581889835; 0.00021970907945202648 0.0002716263293088004 -0.0018347179745732585; 0.00014084625647827186 0.00033542050007351516 7.07768185196939e-5; -0.0011130312585331207 -0.00035558133469717606 -0.0009818980577362534; 0.00023859513886452166 -0.0002450212329672587 -0.0007833281265357781; 1.7279135513846274e-5 0.0011356116313616447 -0.0008002057262446688; -0.00038073340622173286 -0.0003131834239077709 -0.0001259084067836739; 0.0001518238589786812 0.0010017147144079138 0.0005657306892713574; -0.0011287044826209327 -0.0012114856606240002 0.000539884253874619; -0.00039556682395730595 0.00010836705767216029 0.00013726525994773212] %
+
+Mass Used: 89.35891361343056 kg
+Launch C3: 97.06241244458214 km²/s²
+||V∞_in||: 0.0041116848831246515 km/s
diff --git a/archive/ES_0.5619116111600051 b/archive/ES_0.5619116111600051
new file mode 100644
index 0000000..2802588
--- /dev/null
+++ b/archive/ES_0.5619116111600051
@@ -0,0 +1,22 @@
+archive/ES_0.5619116111600051---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T12:41:23.101
+Launch V∞: [6.348236511666772, -7.4240702749765255, 0.17479780612429185] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012516585238670093, 0.0001956548798712695, -0.008908609984413634] km/s
+ V∞_out: [0.01469623748235905, -0.000146821654840301, -0.0044805145177106535] km/s
+ time of flight: 1.8749577787486738e8 seconds
+ arrival date: 2029-04-10T14:51:00.101
+ thrust profile: [0.45384707792221646 -0.12808365204227615 -0.15256588685172096; 0.031860748893224246 0.008991167081489233 -0.039026531441403334; 0.02555498925060076 0.012560248205110841 -0.05081801237435538; 0.09979063377101596 0.06315120703830367 -0.25049752837893763; 0.015584736472008705 0.012589040346347934 -0.05529801266902425; 0.020558102780196336 0.019987212111301212 -0.0963612989907288; 0.020315648476354187 0.02099172471340323 -0.10142064742994292; 0.009956228451871633 0.00976125278551738 -0.05518681204887601; 0.006183990521857463 0.006949636778614134 -0.03889962350806876; 0.006913821254794156 0.009505269068135607 -0.05453445328413311; 0.002342134616257525 0.0032197815361162366 -0.020269557443822018; 0.00019334789405458014 0.0001715754200766939 -0.000869635054318619; 1.492821979441676e-5 1.5687732634421758e-5 -0.00018493314962304299; 8.142927829808995e-5 0.00013806740118921744 -0.0003295311145255785; 8.508203069580288e-5 1.818013980523544e-5 -0.0004863838812762568; -0.0001122908926348022 0.0001683870650287945 7.266906337872198e-5; -7.840622224535191e-6 -0.0001709699519401609 9.895600759096473e-5; 1.6918067406322125e-5 0.0001472899853559907 -9.488573809233359e-5; -0.00018940868425694642 0.0002317968557081107 0.00010387912229162848; -2.2522800238661657e-5 -2.94312749464802e-5 -2.6261273861743272e-5] %
+
+Mass Used: 98.78657660156841 kg
+Launch C3: 95.44748052887499 km²/s²
+||V∞_in||: 0.015364456343239281 km/s
diff --git a/archive/ES_0.5619218878775014 b/archive/ES_0.5619218878775014
new file mode 100644
index 0000000..c30e329
--- /dev/null
+++ b/archive/ES_0.5619218878775014
@@ -0,0 +1,22 @@
+archive/ES_0.5619218878775014---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T20:39:50.271
+Launch V∞: [7.568343408063777, -6.216713245188173, -0.0385550369321964] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008850656771229237, 0.0006931648789462834, -0.0005420395832421222] km/s
+ V∞_out: [0.00020207407817788322, 0.0012305060254918197, -5.156356386839723e-5] km/s
+ time of flight: 1.699683916284566e8 seconds
+ arrival date: 2029-09-29T02:06:21.271
+ thrust profile: [0.3897050500343743 -0.05342982704846628 -0.13809975050799586; 0.06431536850391364 0.024934193664493804 -0.07563583073001401; 0.06967745394548724 0.04735561004687149 -0.1399623714238835; 0.04934555976903582 0.04359861391967005 -0.14086272708052355; 0.04020075812368056 0.042392358533176265 -0.15191535856642907; 0.022730697900607406 0.026862441252358097 -0.10524672839860748; 0.01526109860172432 0.020302624214842364 -0.08791600520294347; 0.012268135966773123 0.016583263595809954 -0.07689763627206811; 0.006171376345676016 0.00870706269170693 -0.04380554684826718; 0.006414087317995762 0.010144875491808142 -0.05189483080464975; 0.000575428765567142 0.0013949649983897266 -0.01020150532924916; 0.0004863957144246946 0.0008706483348908888 -0.0015577874684164104; 0.0004957957311160057 0.00027824510940385885 -0.003954095578729034; 0.000939412236788881 0.0009479216186336506 3.340015048451618e-5; -0.0008916007597537968 -6.77615527141563e-5 -0.0002054789815081949; 0.00032520980100072085 0.0002722488196247331 -0.0004906687192585606; -0.00020884142045552248 -0.0004900599315733997 -0.009589503139789679; 0.0013788541848984634 0.0020296121037185685 0.0002823407637652755; -0.0005343969177315828 0.0002943082116837039 0.0030136542127887286; -0.0003131530082384441 -0.00019222622060107835 -0.0027492401328451676] %
+
+Mass Used: 95.99068248785716 kg
+Launch C3: 95.92883200615334 km²/s²
+||V∞_in||: 0.0012480487618787052 km/s
diff --git a/archive/ES_0.561930825616757 b/archive/ES_0.561930825616757
new file mode 100644
index 0000000..4ef56f1
--- /dev/null
+++ b/archive/ES_0.561930825616757
@@ -0,0 +1,22 @@
+archive/ES_0.561930825616757---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T01:37:45.701
+Launch V∞: [6.535263056102943, -7.371229163004488, 0.1515639927825825] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009562887272221206, 0.0012336170909602456, 0.00104269904672912] km/s
+ V∞_out: [-0.0011856214460844578, -0.0005940925741871262, 0.0013283033637125688] km/s
+ time of flight: 1.8749577787446436e8 seconds
+ arrival date: 2029-04-09T03:47:22.701
+ thrust profile: [0.26716800919595923 -0.058887510657538444 -0.09020750374402642; 0.08621766001774545 0.02736882656800573 -0.091351596369802; 0.051034777999484575 0.029892449581260912 -0.0912484175333232; 0.047932612167105024 0.03823094616361142 -0.11875164555755445; 0.04492992851349635 0.044072577602465995 -0.14368952152949452; 0.029625361291655803 0.03285207557770451 -0.11550094233954317; 0.0192306251057203 0.023895536481231043 -0.08937198471983271; 0.0077026161026151 0.010468466649493262 -0.04171387243699023; 0.01015542550324261 0.01588062407082438 -0.06305560831543731; 0.0047954587890987384 0.0075948973383141915 -0.032691294513063573; 0.0005982996349565106 -0.00024347268585901222 -0.002776524313451849; -0.00016925831039781662 -0.00029222611519258353 -0.00459335631734259; 0.0004229092847645899 -8.273671921532838e-5 -0.002874280761273713; 0.00010857569989793179 0.0001012900246064565 -0.0011144327602736126; 0.001038559182934759 0.001150650800298052 -0.0004225461242656676; 0.0002805943416546799 -0.00012894864640854232 0.00038198532947208215; -0.000486899378949602 0.00016178342853985343 -0.0012956556628256398; -0.001661384121112276 0.001433344920896381 0.0002458474752564402; -0.00023383500231517697 0.0006939127420907627 0.0005771503639390903; -0.0012662127187458988 0.00014400418535417655 -0.00025521652082825135] %
+
+Mass Used: 89.35798021179971 kg
+Launch C3: 97.06765422990001 km²/s²
+||V∞_in||: 0.0018771043015696112 km/s
diff --git a/archive/ES_0.5619337178973924 b/archive/ES_0.5619337178973924
new file mode 100644
index 0000000..18d6ab0
--- /dev/null
+++ b/archive/ES_0.5619337178973924
@@ -0,0 +1,22 @@
+archive/ES_0.5619337178973924---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T08:25:45.210
+Launch V∞: [8.327542593882416, -5.392704448911285, 0.559531216512948] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.472297973901048e-5, -0.00012528308828208576, -1.099207426392053e-5] km/s
+ V∞_out: [1.0807834632991847e-8, -6.957466611962807e-8, -1.5005699272826556e-7] km/s
+ time of flight: 1.8749577787473872e8 seconds
+ arrival date: 2030-04-21T10:35:22.210
+ thrust profile: [0.2387157955744155 -0.00290582759623063 -0.0794535119743396; 0.03729093285369718 0.019512924981858595 -0.04396787497658348; 0.04028169351089907 0.03551513095524824 -0.09033940445143558; 0.045291542179731865 0.05264967063090179 -0.1465197864590414; 0.027091105069373133 0.03712907264037969 -0.11813845969910579; 0.013417493314420196 0.020265482496637174 -0.0732812411128218; 0.007242008749191334 0.01333803565175509 -0.04932702845431029; 0.0054258101994511315 0.009468788077455676 -0.039134932770233236; 0.008421540695347882 0.017739913125720166 -0.0769346121368751; 0.00302853620268655 0.00818338884967877 -0.035647218850619; -0.00034986956139926805 5.2160595185835826e-5 -0.005588943559361986; 0.0005964184673181949 0.0017605461981999812 -0.01055439323023483; -5.2419885015751765e-5 0.0014981500117645249 -0.0030494474361581936; 0.0022261362678160437 0.0011764741231390893 0.0027902296958610536; -0.0001451176745633217 0.0040449405213461905 0.006880641516862272; -4.173396359545605e-5 -0.004881754000786364 0.005566045950621216; 0.0008012489978293897 -0.0007678446519384435 -0.0008480455943375154; 8.489539800837217e-5 0.00020493264957715748 0.0015048267146028885; 0.0009019381402067513 -0.001143611696940854 0.019426182443849048; 0.01031479451144876 -0.006415801683903846 -0.004030043644012157] %
+
+Mass Used: 79.59257524745681 kg
+Launch C3: 98.7423021084859 km²/s²
+||V∞_in||: 0.00015163990636365225 km/s
diff --git a/archive/ES_0.5619350549485091 b/archive/ES_0.5619350549485091
new file mode 100644
index 0000000..6531687
--- /dev/null
+++ b/archive/ES_0.5619350549485091
@@ -0,0 +1,22 @@
+archive/ES_0.5619350549485091---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T17:34:19.751
+Launch V∞: [7.576129309849439, -5.802549501374631, 0.054432352242211914] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.743686060366899e-9, 1.2486216388690822e-9, 3.1903343146159455e-10] km/s
+ V∞_out: [1.0747517229934916e-9, -9.71664410203887e-10, -8.303070697815774e-10] km/s
+ time of flight: 1.874957778742207e8 seconds
+ arrival date: 2030-04-21T19:43:56.751
+ thrust profile: [0.6544521041065833 0.0216255834767201 -0.16644996194941566; 0.22245518214052434 0.146323527353574 -0.20276300496873237; 0.055274776772598164 0.05900088894856514 -0.09843164031650915; 0.049796132446756784 0.0741158753242258 -0.1348561360232869; 0.028377929163059548 0.05364891150324515 -0.11029321315998956; 0.008356569395296089 0.01909350044222375 -0.04565114285728794; 0.008265237615485452 0.021262920719092936 -0.05554392358982706; 0.001257623359618549 0.004431528734742248 -0.013363065013180948; 0.002625536027558525 0.011963175244420938 -0.0268228115691624; 0.0013107948886806465 0.0026534769035475433 -0.006447987246614809; 0.0009297206288153922 0.003092939636700249 -0.008593643726678868; -0.0030252356994317276 -0.000740473440029696 -0.00652576815099982; 0.00024189765622748926 0.0017087607685401989 -0.00540862643822379; 0.0006510339438186205 -0.0018637596024180497 0.004094874175655898; -0.004775179245836366 0.007870720317468632 0.0022756510445787444; 0.0007552446858228235 -0.005792886461875932 -0.0026437790420040996; 4.889460922916317e-6 -0.00024685077479980744 0.004185959711702812; -0.0031644932451295278 -0.002835762765720122 0.007849182595029041; -0.0001525433766308774 -0.0007499996481964558 -6.896596606822611e-5; 0.01563181114816334 0.011926144598294677 0.011658901388342208] %
+
+Mass Used: 124.34760376073291 kg
+Launch C3: 91.07027891643332 km²/s²
+||V∞_in||: 2.168243391448504e-9 km/s
diff --git a/archive/ES_0.561936917223629 b/archive/ES_0.561936917223629
new file mode 100644
index 0000000..cf1a1d1
--- /dev/null
+++ b/archive/ES_0.561936917223629
@@ -0,0 +1,22 @@
+archive/ES_0.561936917223629---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T18:10:08.456
+Launch V∞: [6.5582609587160405, -7.312334792370772, 0.14752011332134288] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6544049370598798e-5, -4.17034659010149e-6, 7.277514243308347e-8] km/s
+ V∞_out: [5.167696653269538e-6, -1.1638980580838531e-7, -2.636657356823233e-5] km/s
+ time of flight: 1.8749577787484053e8 seconds
+ arrival date: 2029-04-08T20:19:45.456
+ thrust profile: [0.34706271455521454 -0.08776364537206142 -0.10793064782277502; 0.04848481481973471 0.013657083443900875 -0.05269554116007447; 0.046436755743435774 0.025282513868295164 -0.0845701374268251; 0.03796092649845887 0.02753144807536253 -0.0960527199713178; 0.038939846357488456 0.03448167743590526 -0.1268813051671536; 0.04895773450260127 0.04764542899276054 -0.17904558490088052; 0.010598098029606842 0.011375236915728087 -0.049670857930837364; 0.015271125561391454 0.019040512037002476 -0.07865125981801452; 0.015444651459273977 0.02164282392643399 -0.09599903354641007; 0.0021401508604761447 0.00310104526870319 -0.012838828513707616; 0.00042460869257742893 0.000825983711115626 -0.001267411554020346; -0.0003131323141085181 -0.00025227936065108246 -0.0005074691243491183; 3.257720254541211e-5 9.43161168966807e-5 3.814750890680514e-5; -0.0003438457056436514 -0.0014292110299512573 -0.0009502070881619998; 1.0558893930863011e-7 -0.000989136668441728 -0.00037842054523852563; -0.0007110462727320393 0.0021340257848244094 0.0011513641259036562; 0.0014458450245938984 -1.1954895318894409e-5 0.00011897516298244016; -0.0005476964561340823 0.0003106617714528392 -0.0008043438554007458; -0.0001808218295128156 0.00012981320582625805 0.00017527125432612403; -0.000275774772276061 -0.00035468214491511825 0.0010134341880564976] %
+
+Mass Used: 92.66013366491188 kg
+Launch C3: 96.50278910216949 km²/s²
+||V∞_in||: 2.6869753327705e-5 km/s
diff --git a/archive/ES_0.5619516733006431 b/archive/ES_0.5619516733006431
new file mode 100644
index 0000000..5861838
--- /dev/null
+++ b/archive/ES_0.5619516733006431
@@ -0,0 +1,22 @@
+archive/ES_0.5619516733006431---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:57:08.147
+Launch V∞: [6.541437244380679, -7.479479951645376, 0.1324840144436217] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.8440819510640396e-7, -0.00012901196740333062, 0.0001426480687364557] km/s
+ V∞_out: [9.970827713768238e-5, 0.00016182266298166007, -3.79559982422498e-5] km/s
+ time of flight: 1.8598752217251727e8 seconds
+ arrival date: 2029-03-24T03:09:10.147
+ thrust profile: [0.16028702955327964 -0.043125104503696526 -0.06337626010009975; 0.061486270673480364 0.013861320471603922 -0.07292557367957361; 0.062365455604914445 0.02815477751323384 -0.1263095833772454; 0.04164839980882573 0.024681644036817513 -0.11737731708792186; 0.03001526749853396 0.02077053841033217 -0.10686949847969981; 0.02092969671545941 0.016719797953440082 -0.09215608490083281; 0.02758483132080347 0.02648391311239053 -0.14742184504672434; 0.00954458205451251 0.008953250805018884 -0.05660316680074063; 0.008978013681924232 0.008639978473692005 -0.05567328821996606; 0.005663342100627839 0.0065640735670264615 -0.0441106874660072; 0.00018072882443590966 0.0001973024680629731 -0.0017822167554127182; -0.0001352867319512769 8.97161418725915e-5 -0.0004260389478197728; -5.880680998916597e-5 0.00014147718860083844 -0.0006362646234445444; 7.906774430984265e-5 9.808509884127938e-5 -0.0009366744409181282; 5.5984790662998565e-5 8.207951112198202e-5 2.0344564490315108e-5; 0.0005153802822446807 -0.00018222468560689746 -0.0010420799118086783; 0.000529129233457757 0.0003037654727825386 -0.0013969446235763778; 0.00022432945384786283 0.00032580578297486797 -0.000202467881747717; 7.440290629811674e-5 4.32250625877009e-5 -0.0006283280100297185; 0.00028431371880246033 -8.713158901490212e-5 -0.0005537718126311887] %
+
+Mass Used: 79.56527294805664 kg
+Launch C3: 98.75057358331891 km²/s²
+||V∞_in||: 0.0001923348824763181 km/s
diff --git a/archive/ES_0.561952787850474 b/archive/ES_0.561952787850474
new file mode 100644
index 0000000..03b49bc
--- /dev/null
+++ b/archive/ES_0.561952787850474
@@ -0,0 +1,22 @@
+archive/ES_0.561952787850474---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T05:39:43.200
+Launch V∞: [7.6773479833206775, -5.728764462711537, -0.01128815801716515] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3579190364230538e-9, -1.430191991367866e-9, -1.492846978373959e-9] km/s
+ V∞_out: [3.31890499669413e-10, -3.10872685683302e-10, 1.2141420505017956e-10] km/s
+ time of flight: 1.846832628968073e8 seconds
+ arrival date: 2030-03-17T18:34:05.200
+ thrust profile: [0.6587795442422513 0.0005675854949489122 -0.13947262345972722; 0.13006035128892518 0.08554418151536268 -0.09922671049381014; 0.04691692458566871 0.054082031350178854 -0.07182322917438749; 0.021068553801828187 0.0338083771437883 -0.050571966179281794; 0.04537463975442479 0.07634700911534653 -0.12185905699725198; 0.045191459457312184 0.08128997717613187 -0.13387684805746153; 0.02484942069671231 0.07595758092109355 -0.12628865567095923; 0.0079837741615095 0.03293245827511673 -0.05908260447115273; 0.0014439202570012098 0.008352777945509428 -0.016322941590489866; 0.0014074176959674842 0.009870877732894873 -0.019288463649921615; 0.0016617514771669296 0.006400590175063738 -0.014014596202437038; 0.0006253902205587586 0.0018968180912296928 -0.004370148999050007; 0.0015571005677490796 0.00037787199041554916 -0.002012714946177898; 0.0006561528056836216 -0.0009444070986641205 -8.971753349723251e-5; -0.0032902774779825232 0.00037894359372256695 0.0009882326104055658; 0.001133193288619312 0.0009053305853044294 -0.002691445302512391; 0.0023816719392542327 -0.0027098537331900225 -0.004117817376924737; 0.001605949645644533 0.0016595945948968212 0.0028712736917997405; -2.4254009025067588e-5 2.3205548564868164e-5 -0.00021039288314846343; 5.776749646569073e-5 0.0003814755779386332 0.0012083685532737962] %
+
+Mass Used: 120.34175895792578 kg
+Launch C3: 91.7605417487361 km²/s²
+||V∞_in||: 2.4734561533395245e-9 km/s
diff --git a/archive/ES_0.5619534545098605 b/archive/ES_0.5619534545098605
new file mode 100644
index 0000000..f32ab6f
--- /dev/null
+++ b/archive/ES_0.5619534545098605
@@ -0,0 +1,22 @@
+archive/ES_0.5619534545098605---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T20:23:04.545
+Launch V∞: [6.593510027274388, -7.4649905599644555, 0.17021265475698116] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2024247073171937e-7, -2.549005515507381e-7, -1.0911979167666664e-7] km/s
+ V∞_out: [8.047683471043276e-8, -1.521673106079714e-7, 2.44061678421627e-7] km/s
+ time of flight: 1.8749577787452102e8 seconds
+ arrival date: 2029-04-11T22:32:41.545
+ thrust profile: [0.16793283072725337 -0.04935353845218331 -0.07362614012878331; 0.033058585076936785 0.005547586978642191 -0.04527098558365666; 0.03486935732456284 0.01246238140992417 -0.07983594387818309; 0.05528778893607501 0.02656777494617479 -0.17953920280807334; 0.030577473054488616 0.017072402298991235 -0.1271766322667682; 0.023908469002167736 0.013091461143263297 -0.1143284665419921; 0.014681203780478939 0.008817195557178104 -0.08393779517572263; 0.01339186144164583 0.00781863280735602 -0.08275354005290082; 0.003985210609963945 0.002599825480817179 -0.028760077737565594; 0.003077243008691215 0.0021489398454546727 -0.025401812798898114; 0.0030362123954802934 0.0017149442143863344 -0.023492682798311036; 0.0003505948208671793 0.00016514393182421867 -0.0027040562412378195; 4.0889422860206534e-7 0.00012495837285676228 -0.0002798722385949944; 0.00012500374527093117 -0.00018057999699257318 -0.0006119511603078217; -0.00010635344802404799 -5.566299487420856e-6 -0.00030068844388625796; -0.00015916251818696227 0.0005578313058300615 -0.0007319132694588449; 0.00018799459885258387 -0.00011392302943189296 -9.634444184069627e-5; -0.00010440270265796168 -0.00016465745526534744 0.00035322775766082775; 8.740843317742641e-5 -8.854567374373147e-5 -0.00031866166897886333; -0.00030994636587173446 0.0001685068387651817 -0.0004407573861282598] %
+
+Mass Used: 76.77401674837029 kg
+Launch C3: 99.22943088796575 km²/s²
+||V∞_in||: 3.0222453885165914e-7 km/s
diff --git a/archive/ES_0.5619568698930453 b/archive/ES_0.5619568698930453
new file mode 100644
index 0000000..faac95f
--- /dev/null
+++ b/archive/ES_0.5619568698930453
@@ -0,0 +1,22 @@
+archive/ES_0.5619568698930453---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T07:47:33.171
+Launch V∞: [6.523997103920628, -7.389021197975158, 0.11238090820053452] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.361372309778487e-6, 1.0044945740468272e-6, -2.1308315618701124e-8] km/s
+ V∞_out: [-3.0136178154631523e-6, 6.840255417162852e-8, 6.791376943047781e-6] km/s
+ time of flight: 1.849707341883998e8 seconds
+ arrival date: 2029-03-10T04:33:07.171
+ thrust profile: [0.2755998179584433 -0.07177778123265399 -0.09572888759156402; 0.06483347561534818 0.01702544085693852 -0.0727650704610183; 0.04983229525282953 0.025686761557071666 -0.09331436472395291; 0.04181424535786854 0.02959655475538227 -0.11093297729026097; 0.05217631530632207 0.043320077867604105 -0.16839551634491653; 0.04555287702743608 0.04368948248341514 -0.17536808896946895; 0.011411994708463685 0.010815144852502633 -0.05305957168049541; 0.009240421076386632 0.012858547224385687 -0.060955209892910416; 0.006167707221758689 0.005250475730748714 -0.03659892249717102; 0.0037600833630706365 0.004723503321149332 -0.028552215764987388; 0.0015258387428947785 0.0019704000553126943 -0.010860798729359022; 0.0010802639089622639 0.0007263432520688765 -0.0008840059731063075; 0.00013297216663846277 0.00030302626009006653 -0.001256013278399124; -0.00010877049500955844 7.408960190378624e-5 -0.0007887473997524416; 0.00046314666400331213 0.0007668184895400125 -0.0005725452769757831; 0.0006302196589467286 -0.0001880485435004401 -0.00043139114590459563; 0.00032626285289989466 0.0002467927336594746 -0.0004489985793375234; -0.0011667214785614167 0.0019635036619747945 -0.0006980436417902419; 0.0005169877512923942 0.0007447869025392007 -0.0006686115931280497; -0.0010435407535686284 0.0004825717145474486 0.00024066434585158438] %
+
+Mass Used: 88.77500353160895 kg
+Launch C3: 97.17280194461895 km²/s²
+||V∞_in||: 7.429620829946673e-6 km/s
diff --git a/archive/ES_0.5619630160081817 b/archive/ES_0.5619630160081817
new file mode 100644
index 0000000..29a02ec
--- /dev/null
+++ b/archive/ES_0.5619630160081817
@@ -0,0 +1,22 @@
+archive/ES_0.5619630160081817---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T16:43:21.809
+Launch V∞: [6.358573798995708, -7.432269459890283, 0.16159069123769554] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.609878323298452e-9, -4.1921077046776844e-12, -5.532689863613954e-9] km/s
+ V∞_out: [-2.0888567564705363e-9, 4.5908577813337155e-9, 6.42277060980752e-9] km/s
+ time of flight: 1.8749577787480837e8 seconds
+ arrival date: 2029-04-09T18:52:58.809
+ thrust profile: [0.36130561427508573 -0.08400936605997937 -0.11619198721281673; 0.11794556207757888 0.03705804480184642 -0.12155224196782934; 0.05614476634754412 0.031864483583755064 -0.09932941313214347; 0.04812111477448445 0.03718372402768014 -0.11792379104872981; 0.03232562540409379 0.030106067254983156 -0.10392328389873477; 0.03624219530145731 0.039977752101281225 -0.14113897141795012; 0.020466747762673265 0.02454951017685752 -0.09555570207132685; 0.009660173466247812 0.0128025347407399 -0.05318732037668279; 0.005712166364558871 0.008289818334625885 -0.03596398036955635; 0.0021439291476658484 0.003211552303080139 -0.014395780034450342; 0.00075203341230227 0.0008730320631266112 -0.006446963085749143; -0.00019548338630921905 0.001257782146069772 -0.0009220020291910031; -0.0006852347691027601 -8.914357490021142e-5 -0.00039985540987243413; -0.001550121912891285 -0.0005157937879509923 -0.0012463673686071454; -0.0002555159849495095 4.4048789184362495e-5 -0.0008056412466498293; -5.7439714328183915e-5 0.00010786424132799257 0.0015887305848962478; 8.255999514379664e-5 4.078800008772371e-5 -0.00016194803971529515; 2.8487953567973606e-5 0.00013606036575480093 -0.00033407963104098296; -0.0004184761196216323 -0.0007139350167912604 0.0010583071151049296; -0.0031755434951650447 -3.1744754663221725e-5 -0.0012367756475041391] %
+
+Mass Used: 97.39567581595338 kg
+Launch C3: 95.69620163318719 km²/s²
+||V∞_in||: 7.879175686765556e-9 km/s
diff --git a/archive/ES_0.5619864869801362 b/archive/ES_0.5619864869801362
new file mode 100644
index 0000000..dc74d51
--- /dev/null
+++ b/archive/ES_0.5619864869801362
@@ -0,0 +1,22 @@
+archive/ES_0.5619864869801362---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T18:53:49.006
+Launch V∞: [6.505473488545801, -7.375024067312457, 0.13513757185287253] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.948543518873309e-6, 5.037015485640353e-6, 6.261079128760604e-6] km/s
+ V∞_out: [8.523440436081196e-6, 5.222008247972699e-6, 1.7188552435402113e-7] km/s
+ time of flight: 1.874957778750729e8 seconds
+ arrival date: 2029-04-09T21:03:26.006
+ thrust profile: [0.31234098216808515 -0.0895048167977679 -0.08572583333841448; 0.08285856172117928 0.02320344349047564 -0.09213737106162957; 0.04217217211652897 0.0210034638367143 -0.07768516118902408; 0.048154527582280865 0.030293877314771032 -0.12290975532969592; 0.020616462253432045 0.015591937319322301 -0.06880225161082101; 0.030402835951305968 0.02518198449821265 -0.1225305461171178; 0.023879900262626604 0.026960453894560008 -0.12642422023120145; 0.01878108691143307 0.023945760301593573 -0.11912854499064743; 0.006849549092740855 0.007250426108932914 -0.03930034901213372; 0.001766699147137375 0.0022171074154619607 -0.013073835675525903; 0.0016706288953934566 0.0022079900659413005 -0.013678737180417769; 6.274700827729298e-5 -7.216053344238942e-5 -0.000595289119920952; -7.091761692735793e-5 0.00017409772121924493 -0.0014385681948356037; 0.0003663143686890177 0.00042133591531733143 0.0004552948044841893; 7.618384462604243e-6 3.1670556598833674e-5 -0.00097566168764548; 0.00018438435852297276 0.0004544857246708376 4.081949344578173e-7; -3.3725056965003074e-7 0.0009765199624573571 -0.0010066136224454489; 0.00021110324267417224 0.00031950802038822955 -0.0011880707556960544; 0.0004844657892501248 0.000947445183725532 -0.0009198684812024428; -0.002242970237914324 -0.001385948785861406 -0.0011819556451597153] %
+
+Mass Used: 91.39007458636252 kg
+Launch C3: 96.73042746693653 km²/s²
+||V∞_in||: 9.997890120175958e-6 km/s
diff --git a/archive/ES_0.5619916204017649 b/archive/ES_0.5619916204017649
new file mode 100644
index 0000000..ea95a83
--- /dev/null
+++ b/archive/ES_0.5619916204017649
@@ -0,0 +1,22 @@
+archive/ES_0.5619916204017649---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T14:26:50.100
+Launch V∞: [6.627979454331565, -7.422642631492432, 0.18495516017428562] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9583317275110727e-6, -3.9363985635061015e-7, 8.432289930139936e-9] km/s
+ V∞_out: [5.71401917231786e-7, -1.284935574714414e-8, -2.976158162363788e-6] km/s
+ time of flight: 1.8749577787457097e8 seconds
+ arrival date: 2029-04-10T16:36:27.100
+ thrust profile: [0.1435327205219659 -0.03641423359308318 -0.054967743080120916; 0.05613832285124175 0.01394918940168365 -0.0662066042643259; 0.04651312337911089 0.022650364655751983 -0.09133656713903578; 0.035103925135524856 0.022697066985693164 -0.09667130628473736; 0.03822308621519702 0.029725328612540004 -0.13262221304196706; 0.03252638153297821 0.02862286527000582 -0.138041196719003; 0.01767375288573422 0.016966563988957947 -0.08771686479700364; 0.02072461460983802 0.0201887306502678 -0.11403213309137944; 0.004976885414231178 0.005471710008989724 -0.03262424703259674; 0.004101863229000785 0.004687577281061362 -0.029435371859285697; 0.0014463473909882907 0.0018127046903978644 -0.01154408899477487; 0.00012763317034179887 -0.0005127669926424942 -0.001860724559975905; 0.00014894061572731692 0.0005853976308792478 -0.001608548895297943; -2.60770340205874e-5 -0.0007720842760155434 -0.0023486406072294437; 0.00012484351676044755 9.398938269982593e-5 -0.0005688134466138636; -0.0001693970312470947 0.00019270313982070703 -0.0013541337959541925; -0.000768665786300207 -0.0009209240133451702 0.00037892983630436426; -0.0007565462886107758 -0.0002456899772351151 -0.0005166171617551904; -0.0005839087352630305 -0.00041584135166860116 0.0016578242710166453; -0.0011615456290482277 0.0024807457463264303 0.0029132270370276496] %
+
+Mass Used: 77.80721892526117 kg
+Launch C3: 99.05994369316535 km²/s²
+||V∞_in||: 2.984417874564459e-6 km/s
diff --git a/archive/ES_0.5619921037365282 b/archive/ES_0.5619921037365282
new file mode 100644
index 0000000..43a8baf
--- /dev/null
+++ b/archive/ES_0.5619921037365282
@@ -0,0 +1,22 @@
+archive/ES_0.5619921037365282---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T07:42:15.882
+Launch V∞: [8.112513087411893, -5.903027853029376, 0.050883158263066317] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9146638219616535e-8, 1.6011146084952182e-7, -3.00898494794659e-8] km/s
+ V∞_out: [2.4210141066007615e-8, -9.357662683494502e-8, -1.254597939071607e-7] km/s
+ time of flight: 1.867494983361286e8 seconds
+ arrival date: 2030-04-18T18:33:53.882
+ thrust profile: [0.09959374010970921 -0.005419913835889329 -0.042407723525876684; 0.026187749976520798 0.010820098064160852 -0.03828626465348115; 0.020758601934767973 0.01269997205571679 -0.05324437087346508; 0.036160053749241944 0.027367761823330918 -0.13105535070676275; 0.02973142231761697 0.02518354506613794 -0.13889997037378488; 0.015081506194653828 0.013145486483710417 -0.0860122619439027; 0.013741051587853999 0.01409115180600086 -0.09513724417968206; 0.007867830448508311 0.007046639960152152 -0.05894211625552634; 0.0075499700455120555 0.007068634285092677 -0.0628571684715568; 0.002421666405250339 0.002344486841327364 -0.02487660543460761; 0.003929965552662755 0.0031272288607500716 -0.029501526136017184; 0.00019080304426913092 0.0011233106419523391 -0.007015848948304022; -0.0005395750339156132 -3.297902242133429e-5 0.0021351978636468504; -0.00020797347954129298 -0.001255622683471408 0.0025218964157577963; -0.0031506571978146716 0.001976614415639646 0.005003448131941278; -0.007059526719999948 -0.005762608781735962 -0.0031440039963742646; -0.0011033964902585616 -0.0076774644610849985 0.004130751247618242; -0.002540473129655542 -0.007351416502608556 -0.0005112125291468434; -0.0014486143859688888 0.002194280056772434 0.001122754927285713; 0.0024016075498460867 -0.0008784555209126383 -0.011425305218815424] %
+
+Mass Used: 68.46714714257223 kg
+Launch C3: 100.66119552286467 km²/s²
+||V∞_in||: 1.64035583615805e-7 km/s
diff --git a/archive/ES_0.5619981885167372 b/archive/ES_0.5619981885167372
new file mode 100644
index 0000000..c28704c
--- /dev/null
+++ b/archive/ES_0.5619981885167372
@@ -0,0 +1,22 @@
+archive/ES_0.5619981885167372---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T15:03:25.474
+Launch V∞: [7.749355114850255, -5.597220391507831, 0.19977198318927128] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00010050033617768492, -6.839836058766288e-5, -7.073466582204225e-5] km/s
+ V∞_out: [-7.3220124447318985e-6, 0.00012330005706911616, -6.699167054116716e-5] km/s
+ time of flight: 1.8582855897860828e8 seconds
+ arrival date: 2030-03-30T10:06:03.474
+ thrust profile: [0.6960756702383415 0.003750818006303488 -0.16126304172335967; 0.15081980614931811 0.10333057035179774 -0.1350982071873061; 0.07931312054041431 0.0938567518016715 -0.13638798456627782; 0.0421239485789136 0.06862251367600475 -0.11419044564902676; 0.024819725108097282 0.052123416406145165 -0.09546538669855625; 0.011329821509401048 0.03028758314305592 -0.06118897975604306; 0.008305019275059089 0.02890309529475927 -0.062003713632537115; 0.004346154327950877 0.01688903269437423 -0.03838590334097257; 0.0020720478479418036 0.00898755265311241 -0.02092131308014214; 0.0019199724806770486 0.009178393638285395 -0.024399982227943724; 0.0011689093427061257 0.006014552023037247 -0.016598148253795224; -0.0005439259248724631 0.0014098206842591875 -0.0002819761713550011; -0.000616549215664569 0.0005991457816878317 -0.0003737688205969912; 0.0006249422962977247 0.0005522102036208553 -0.0015723684366737067; 0.002084164205097422 -0.003499339760067708 -0.0013286826054958896; 0.0001595169492070547 -0.0005893200889392218 -0.001775134356770629; -0.0003012514203426548 -0.0031586983562930876 0.001079772234885405; 0.003726245240730011 -0.0005081799608346771 0.005521063977115002; -0.0023422103445551196 -0.0012048452967551577 -0.0017793858724817536; -0.0002510031486006866 0.004841835518835677 0.004313764667301763] %
+
+Mass Used: 122.37369696366022 kg
+Launch C3: 91.42128965243427 km²/s²
+||V∞_in||: 0.00014064866246027237 km/s
diff --git a/archive/ES_0.562002676615615 b/archive/ES_0.562002676615615
new file mode 100644
index 0000000..e7ccb3e
--- /dev/null
+++ b/archive/ES_0.562002676615615
@@ -0,0 +1,22 @@
+archive/ES_0.562002676615615---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T16:00:05.934
+Launch V∞: [6.4185594408720785, -7.458229918022389, 0.11126330725801113] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.377231671226879e-9, -1.860192559834646e-9, 1.78563210476846e-9] km/s
+ V∞_out: [1.0239814818920772e-9, -2.3954725999048964e-9, -3.3081762201801874e-9] km/s
+ time of flight: 1.8749577786485574e8 seconds
+ arrival date: 2029-04-09T18:09:42.934
+ thrust profile: [0.24743331535772012 -0.05946303236660233 -0.075853536958838; 0.05953171460282847 0.01913016597224437 -0.06088760053471088; 0.11404065312802357 0.061926915211666815 -0.17111298172567818; 0.11089631645936013 0.07769553313671121 -0.22506040255042906; 0.039772149783329 0.039348170491223404 -0.1203929516274093; 0.014273108301741238 0.016589843198785273 -0.05712846992250035; 0.00925091940804983 0.011758524451368917 -0.04271144714198459; 0.009158098761966549 0.013217236576454343 -0.04815399563713564; 0.0031064714694183935 0.004972830821826051 -0.01955714722738247; 0.002226573481009321 0.003746763146944442 -0.014830797141804814; 0.0068164298810868065 0.010999200640980695 -0.04556245725634041; -8.383281630001006e-5 0.0006352408225227407 -0.0010334595352510583; 0.000527610231901529 0.0011108824365523684 -0.0005728641285967889; -0.0008299336829218991 0.00113267760542173 -0.0009464721000923305; 8.081484959144601e-5 -0.0019973796989133713 -0.0014071752008839222; -0.0007498156267691253 0.00023881625651337173 -0.0003324249810259764; 0.0016029388812954805 -0.001305807990415235 -6.433789479452992e-5; -8.194832560018536e-5 5.1020336672411666e-5 -0.0006557231505757544; -0.0005467082198889848 0.0005568869819342359 -0.0005506726457504381; -0.0009953019553005497 -0.0005012541433188683 -0.000953259523016285] %
+
+Mass Used: 90.79616579535059 kg
+Launch C3: 96.83547832963433 km²/s²
+||V∞_in||: 3.507139688111689e-9 km/s
diff --git a/archive/ES_0.5620056433881425 b/archive/ES_0.5620056433881425
new file mode 100644
index 0000000..3270758
--- /dev/null
+++ b/archive/ES_0.5620056433881425
@@ -0,0 +1,22 @@
+archive/ES_0.5620056433881425---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T15:08:15.168
+Launch V∞: [7.576765319421232, -6.039545412828854, 0.1291093037256109] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008089314261876361, -0.005032741648151981, -0.00032060268506805563] km/s
+ V∞_out: [0.0068307736096468175, 0.0031587087142855024, -0.005860233658198358] km/s
+ time of flight: 1.7315199739381126e8 seconds
+ arrival date: 2029-11-02T16:54:52.168
+ thrust profile: [0.5096598477347638 -0.03537726030154464 -0.13677730024526316; 0.08419027616404792 0.04296591472136536 -0.07740440995926033; 0.07600611718367861 0.06617410645711555 -0.11930614315139319; 0.09038175241280803 0.1050777466112797 -0.2009759794073497; 0.05231310547967187 0.0733985080612903 -0.15701754751539693; 0.024300699613589122 0.04221414958127557 -0.09645117113338658; 0.016904160416247125 0.034290868328858984 -0.08367734778626827; 0.006352108491516963 0.013908870888424157 -0.03931789392449179; 0.003105055211141286 0.009942255466890447 -0.02644029385601608; 0.0035761402582172217 0.011585125327114561 -0.03278145111801494; 0.0013927999635135468 0.0024839678438328223 -0.0086363600103485; 0.0007131115201532863 -0.00020495587426479602 -0.0018256076946936996; 0.0006914334988392514 -0.000163970903975378 -0.0008792261151191412; 0.0005179356812485859 0.00026520284849686167 -0.0024528262514716846; -0.0026620291590690208 0.0018287182245112815 0.0005402069975042273; -0.002370466706826572 3.906419226882737e-5 0.0011143772526683439; 0.0010456856399129444 0.0004833948147098158 -9.728986876068337e-5; 0.0004645757634012657 0.0014451972709250587 -0.0005100641689542392; -6.571084691424032e-5 -0.0010593289171386007 0.0007048506184042752; -0.0008912122960550628 -0.0023657798902175153 0.0007298984847800837] %
+
+Mass Used: 107.92237146899606 kg
+Launch C3: 93.90015071151488 km²/s²
+||V∞_in||: 0.009532485499916202 km/s
diff --git a/archive/ES_0.562008451512372 b/archive/ES_0.562008451512372
new file mode 100644
index 0000000..b28e634
--- /dev/null
+++ b/archive/ES_0.562008451512372
@@ -0,0 +1,22 @@
+archive/ES_0.562008451512372---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T16:55:20.985
+Launch V∞: [7.803715693982091, -5.747288005644767, 0.24044391677353033] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.098023975708159e-10, -1.1474967277563412e-9, 1.1906440184090046e-9] km/s
+ V∞_out: [5.725452782855963e-10, -1.864900309878037e-9, 2.9284943458676977e-10] km/s
+ time of flight: 1.8107719343793994e8 seconds
+ arrival date: 2030-02-03T12:08:33.985
+ thrust profile: [0.5100364648007975 -0.007411412156833753 -0.12646494368558958; 0.11809317158420474 0.07318589302731357 -0.1134508726908361; 0.06363968484022621 0.06555302951167297 -0.1115010158631222; 0.04906312572284183 0.06886644459637949 -0.12631496476228976; 0.021547190371578494 0.0375503709134554 -0.07810070455488798; 0.024316121299753614 0.05158913538763063 -0.11234341705531677; 0.01394195741014505 0.036209033891242845 -0.08864543934985795; 0.01036784935971778 0.03214567498729369 -0.07997154318572539; 0.0013089663724576218 0.0038998641231905284 -0.010682657866828467; 0.003169048654693194 0.012623422996076775 -0.03628563056344561; 5.730211477228425e-5 0.000371806223864791 -0.004125369304901259; -0.0043162702924315136 -0.0006551096774995109 0.0008649258354029813; -0.0003553896391130174 -0.0006594461757860537 0.0016075170520232916; 0.00019682173899075148 0.0008040145922650378 -0.002780583448570527; 0.0020860730566581755 0.0026980190680564882 -4.402116524978954e-5; 0.002400420183931768 -0.0010034537112322034 0.0008858338566147669; -0.006153341788659064 -0.006177141443642605 0.002205328267048507; -0.002158326876657609 0.0015396291706686 0.0008649054508841835; -0.00014244878489140864 -0.006555564974551284 0.005054811539386108; 1.0951130225915321e-6 -0.00028929501068065315 0.00024178206593683765] %
+
+Mass Used: 107.41837734267756 kg
+Launch C3: 93.98711132944398 km²/s²
+||V∞_in||: 1.8412392136536997e-9 km/s
diff --git a/archive/ES_0.5620105386071821 b/archive/ES_0.5620105386071821
new file mode 100644
index 0000000..25b37ef
--- /dev/null
+++ b/archive/ES_0.5620105386071821
@@ -0,0 +1,22 @@
+archive/ES_0.5620105386071821---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T07:47:36.678
+Launch V∞: [7.575483287810218, -6.151859133019012, 0.258666983658136] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00035845139602393416, 0.0010756767004340237, 0.0026907153818415378] km/s
+ V∞_out: [0.0026638622997824267, 0.0003377384587200819, -0.0011464627700154368] km/s
+ time of flight: 1.7945339013027665e8 seconds
+ arrival date: 2030-01-21T07:57:26.678
+ thrust profile: [0.5305609807710493 -0.04087770692809411 -0.19104057342657405; 0.028857558517522145 0.011418901989977727 -0.03768022304499414; 0.042416266075921354 0.026780041044786224 -0.0947552716953513; 0.06058640925200788 0.04769781733031485 -0.18415729848263815; 0.03422431998650675 0.030118581156556436 -0.13656590002408497; 0.019519026977471016 0.019957538726874297 -0.1015544864860905; 0.013533870630009428 0.01425647351420702 -0.07972268774463265; 0.005460027711824864 0.005418667707435451 -0.03486426980747737; 0.002463703202618409 0.003576061940922237 -0.018467372823634944; 0.003479219517894181 0.003002728035713122 -0.022338420997595358; 0.000344981628034965 -0.0003464297747168214 -0.001702080926922619; 0.002339818597775407 0.004368098827026585 -0.02693211101370859; 0.0004652483650505764 0.0002653911139332614 -0.0023300968152587995; 0.0033072973529778673 -0.0014332356328037327 -0.0003863620240149982; -0.0007496388215667639 0.0017644696024869692 -0.0020034264196425343; -0.0012181789889744133 -0.0023754127505072314 0.0007737224292833859; -0.004965679336955995 -0.0022898391349519265 0.0020487321909431226; -0.004595197396927841 0.0028037259780320086 -0.0024536308390156096; -0.0004229976064235319 0.0004346718205288753 -0.0023603938679771863; 0.0009680268288885009 -0.0009703815899566541 0.0111528831084079] %
+
+Mass Used: 99.76097411350156 kg
+Launch C3: 95.30022644483614 km²/s²
+||V∞_in||: 0.002919848803148339 km/s
diff --git a/archive/ES_0.5620196356565648 b/archive/ES_0.5620196356565648
new file mode 100644
index 0000000..ab844ee
--- /dev/null
+++ b/archive/ES_0.5620196356565648
@@ -0,0 +1,22 @@
+archive/ES_0.5620196356565648---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T08:54:11.186
+Launch V∞: [6.624947883959532, -7.312144247365776, 0.2449073633574738] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.3882856477601834e-7, 2.4380554521731574e-6, -1.383331381665912e-7] km/s
+ V∞_out: [8.760390103131661e-7, -2.004017034204817e-6, 1.143495986815741e-6] km/s
+ time of flight: 1.8749577787492222e8 seconds
+ arrival date: 2029-04-09T11:03:48.186
+ thrust profile: [0.30006822872695815 -0.07935720970010528 -0.10487735267052362; 0.03491600926208249 0.008187525087233005 -0.04039641000177201; 0.0340009657681156 0.01585785671366142 -0.06634932887461396; 0.03562827468229964 0.022274968553473933 -0.09609223682633278; 0.02638407740141775 0.01977250646586012 -0.09140727708689965; 0.05646518136325631 0.04702648525489174 -0.22583072181356428; 0.01981376467943303 0.017636745680293785 -0.0945834371604419; 0.017592384357360304 0.017466304819405823 -0.09812090932218892; 0.002623161857518141 0.0026366206990892337 -0.01670986466942544; 0.0012439377444577676 0.0015324230931127048 -0.009199273761162682; 0.0033662078878429784 0.0034544391614695414 -0.03022456215705855; -0.0007471729349284881 0.001167113558510279 -0.0007565314324711358; 4.751575250846096e-5 0.00017370564220956544 -0.0009065220735453952; 0.0004388152172320158 -0.00019258883128762955 -0.0016187530511524587; -0.00016072674044388574 0.00025694297883426583 -0.00169259724024855; -0.00025534473051888146 -0.000833991118109022 0.001155585290300785; -0.0025452918430729408 -0.00021244361314731402 -0.00015533345133773125; 0.0012527693210499322 -0.00039460646892588557 -0.002310236698759324; -0.0011206920384790229 -0.0007252953570370263 0.001662617492455412; -0.000690622029043977 -0.002135015875676864 -0.0003161635024069312] %
+
+Mass Used: 87.4215974054614 kg
+Launch C3: 97.417367576091 km²/s²
+||V∞_in||: 2.4653712177468233e-6 km/s
diff --git a/archive/ES_0.5620203599106682 b/archive/ES_0.5620203599106682
new file mode 100644
index 0000000..7235cea
--- /dev/null
+++ b/archive/ES_0.5620203599106682
@@ -0,0 +1,22 @@
+archive/ES_0.5620203599106682---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:41:36.526
+Launch V∞: [7.9262033593254415, -5.833022572761772, 0.1287194549000792] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.833818930683778e-6, 7.498509869215027e-6, 1.643649917178865e-6] km/s
+ V∞_out: [1.4800242261558854e-6, 1.0856053405735757e-5, -4.998551122972902e-7] km/s
+ time of flight: 1.8454855218851483e8 seconds
+ arrival date: 2030-03-20T23:10:48.526
+ thrust profile: [0.3572656152821156 -0.014367024481396123 -0.12132742267065176; 0.03693086863074137 0.01929988824162425 -0.04541803233686555; 0.02406651246404148 0.020140151850642114 -0.053302536234371346; 0.029809447809244397 0.03219973659884822 -0.09486640968291415; 0.015616779279596149 0.020504926191955552 -0.06788411964944004; 0.016791917383017788 0.02441289554918029 -0.08640860222303966; 0.03934742009463309 0.06321238703433012 -0.22475710863811105; 0.005508945142185385 0.008166798235491284 -0.039732711038491506; 0.0030909998398001744 0.007124617022298895 -0.030663058736035392; 0.004534788738049589 0.009981246638432363 -0.04498918134376196; -0.0003448634044157684 0.0002119401527885625 -0.01516289231705414; -0.007103245911520182 0.0030989402089112066 -0.0022302242720392755; 0.0021366007584150536 0.0028229060533733535 0.0001535946596389632; 0.0006390442610646684 0.0025933901325910134 -0.0027826880380366703; 0.0023158717197507657 -0.005591971788310283 0.0004856782626218581; 0.0004899214789079532 0.0010148089252135489 -0.002417963820793333; 0.0031233256866397266 -0.007512938693725589 -0.0009030211969144838; 0.01782426704753358 0.0018882952495561194 -0.009652788352196169; 0.012465863345507429 0.020208230498399225 -0.01656650657233462; -0.003727691656861246 -0.005663238581160964 0.009170186893463106] %
+
+Mass Used: 90.64213232861266 kg
+Launch C3: 96.86542072580005 km²/s²
+||V∞_in||: 1.096804241182978e-5 km/s
diff --git a/archive/ES_0.5620209894574003 b/archive/ES_0.5620209894574003
new file mode 100644
index 0000000..78e0886
--- /dev/null
+++ b/archive/ES_0.5620209894574003
@@ -0,0 +1,22 @@
+archive/ES_0.5620209894574003---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T10:15:05.408
+Launch V∞: [6.4631121658623725, -7.39551138445389, 0.15204226378513103] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.311903296411386e-7, 0.00023003750492918317, -0.0001624144139694427] km/s
+ V∞_out: [-0.00014262826478397158, -0.0002358531861051039, 5.778415741130242e-5] km/s
+ time of flight: 1.8749577787478015e8 seconds
+ arrival date: 2029-04-09T12:24:42.408
+ thrust profile: [0.33099448599692083 -0.07438735776360136 -0.09960541302727773; 0.06133858316667238 0.019215380927581873 -0.06499542791280846; 0.05238388823859908 0.03094862099049153 -0.09276221904962414; 0.0400641161315736 0.03220963162864082 -0.10070282903222445; 0.04006880853940953 0.03799210511335766 -0.12403023020708238; 0.033814140169014024 0.03639889149582758 -0.12551798305495887; 0.033201655006584424 0.04236620977444869 -0.14548863113014038; 0.011272006127630472 0.016144312932716832 -0.06272457992411308; 0.00601858548603146 0.008719799964526638 -0.036668957953232294; 0.0013665863451100464 0.002138922812876399 -0.009082524620433002; 0.0028738827404006986 0.004653570377199257 -0.022120937390004647; -0.00048256204752543695 -0.00030289857549991857 -0.0017756331105315427; -0.00039313540739112785 -0.00011504986618518924 0.0003008589009935962; -0.00011361637534556744 -0.0002699976633596805 0.0008851835706283125; 8.380685226149363e-5 -0.0010555093558350507 0.000702061748529968; 0.0014218462492188244 0.0006816481101918083 -0.0008715546854260591; 0.0010934997713293708 -0.0003651828268691953 -0.0009512564380237212; -0.0012637102613908095 0.0009067190221264477 0.0004095874583930459; 0.0012868054689877326 0.000281632320245483 -0.0003910030147511596; -0.0009682053159417173 0.00013128476927126248 0.0013759055043244277] %
+
+Mass Used: 92.84142895648756 kg
+Launch C3: 96.4885243560822 km²/s²
+||V∞_in||: 0.00028159586321247626 km/s
diff --git a/archive/ES_0.5620257357008096 b/archive/ES_0.5620257357008096
new file mode 100644
index 0000000..dc59453
--- /dev/null
+++ b/archive/ES_0.5620257357008096
@@ -0,0 +1,22 @@
+archive/ES_0.5620257357008096---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T22:27:19.487
+Launch V∞: [8.000276855853997, -5.524428436279554, 0.148307173303242] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.861321174682988e-10, 1.1482598921434467e-9, -1.7558094558794807e-9] km/s
+ V∞_out: [9.621448274063801e-10, 1.9772307754280122e-9, 4.983881698201095e-11] km/s
+ time of flight: 1.8749577787475583e8 seconds
+ arrival date: 2030-04-20T00:36:56.487
+ thrust profile: [0.46819688924442265 0.016141140737361233 -0.11551368292786679; 0.10304356496665087 0.06967079352932183 -0.10032801977143517; 0.0679957115706983 0.07650704303742831 -0.12085088161053038; 0.04284567667341928 0.066355083743479 -0.1164269759307149; 0.02065160253161757 0.04139251584666671 -0.08587169757959243; 0.025133311751825618 0.06073163653544584 -0.12520982281766818; 0.011261666091483335 0.03188037976120707 -0.07517346100366008; 0.005730727578260555 0.0197585646789434 -0.050610254557941964; 0.0008694019511679321 0.006384237973222682 -0.016806999152147183; 0.00013919717583702384 0.001420683588594288 -0.0026355287064657998; -0.0015143185748454102 -0.002025517558156884 0.0005219296553445134; -0.0015932051039951377 -0.002008244466149805 0.000796986434207364; -0.0007946577466695243 -0.0037469686642665474 0.003860748018554204; -0.0031780271081215576 0.001172280367617907 -0.0024462029515483923; -0.005450980380693855 0.001629560979083223 -0.002750830156363578; 0.004393210848806281 0.006203472982122128 0.004332757285659413; -0.0003558653250903302 -0.00068832249435882 0.004762514361135203; -0.010066115020798603 -0.002908567141682422 -0.005770254035132986; 0.005396362553576503 0.005720336724160917 0.0028306941041910303; -0.0002798684996730952 0.0017994502228707815 0.0006380537234690748] %
+
+Mass Used: 104.1799080269584 kg
+Launch C3: 94.54573433554047 km²/s²
+||V∞_in||: 2.2072935708424943e-9 km/s
diff --git a/archive/ES_0.5620293180973104 b/archive/ES_0.5620293180973104
new file mode 100644
index 0000000..6c905dd
--- /dev/null
+++ b/archive/ES_0.5620293180973104
@@ -0,0 +1,22 @@
+archive/ES_0.5620293180973104---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:30:19.126
+Launch V∞: [7.835584726453181, -5.649338447452159, 0.44764336396025295] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004260056147926698, -0.0028672959079163057, -0.0001765783954600326] km/s
+ V∞_out: [0.0036724898414772994, 0.0016714272616407285, -0.0031746527490084447] km/s
+ time of flight: 1.8524610324320352e8 seconds
+ arrival date: 2030-03-24T12:45:22.126
+ thrust profile: [0.5711896291077573 0.01422547930046348 -0.12512706286694059; 0.07632656870314984 0.05180221375881592 -0.06963953780481959; 0.0679145491061339 0.07658650630222712 -0.11044363133927054; 0.028164743250159444 0.044610242785553374 -0.07217809513554264; 0.03898543783202043 0.07700493538582988 -0.12893543839191307; 0.03163640316612657 0.0721210953755338 -0.12797298644938565; 0.007079073310261218 0.020457313665965236 -0.04321951234833101; 0.012595691683375964 0.047337128208192976 -0.09828835944764124; 0.0036609945238744784 0.010929057089209101 -0.025625567156971403; 0.0008096303886401879 0.0018977762803228794 -0.008685699326444607; 7.106036881401003e-5 -0.0006671157886910261 0.0008796955671469173; 0.00252727226065768 0.002754914819238511 0.0002921184946012845; -0.001065442041705934 0.0016605144756165029 0.001417890277883476; -0.000855770921464312 0.008032848568885323 -0.001647986087575085; -0.0011320096660956906 -8.604703971759506e-5 -0.003261038655219299; -0.0006412175662652488 -0.0005832588498013159 -4.5487201666763455e-5; -0.005801492172074861 0.007628987574286507 -0.0012098952462728792; -0.0018289918980893957 -0.0009196221559475922 -0.00255194047858463; -0.001932532756007169 -0.0013086425002025955 0.005699165174731141; 0.009238622431924488 -0.005018598945102932 -0.009477547847762594] %
+
+Mass Used: 110.2153858101151 kg
+Launch C3: 93.5117974805852 km²/s²
+||V∞_in||: 0.0051381557135595736 km/s
diff --git a/archive/ES_0.5620346526946953 b/archive/ES_0.5620346526946953
new file mode 100644
index 0000000..7e44166
--- /dev/null
+++ b/archive/ES_0.5620346526946953
@@ -0,0 +1,22 @@
+archive/ES_0.5620346526946953---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:29:42.858
+Launch V∞: [6.537189733467448, -7.416928565582277, 0.0947962714316523] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009176065514613259, -0.00028498212639781835, 0.0062733372472985665] km/s
+ V∞_out: [-0.01063772658619262, 0.00011081155198904773, 0.0032326214676919847] km/s
+ time of flight: 1.874957778748755e8 seconds
+ arrival date: 2029-04-10T12:39:19.858
+ thrust profile: [0.23685941312937644 -0.06239349278951234 -0.08965781531774628; 0.058650421697844665 0.013907941617507271 -0.06734858189709338; 0.05778362547008877 0.026453172311492794 -0.11127838578551925; 0.051784457381710856 0.031520697232197345 -0.13982382704583265; 0.04166813056205217 0.030259990312269024 -0.14369649992134506; 0.026295113741863226 0.021974347187872865 -0.10960874929879673; 0.02123287049272462 0.019128979113363507 -0.10265150314562783; 0.011167175314447336 0.010652281071240948 -0.06272292638383273; 0.004380956669243601 0.0049157158444183965 -0.029124789687652634; 0.0008908609710975702 0.0017730024872171716 -0.00973377891309767; 0.0017085641502295778 -9.660996558019598e-5 -0.004968103534710415; -0.00015086557574451416 -0.00043107179787259427 -0.0045397798468996345; -0.0009414800833844172 0.0013002302664977122 -0.003641686079929086; 0.0023382386793191646 0.0006280483660266324 -0.0034052396345181928; -0.000248193518502339 -0.00021520980266061251 0.0009750882971433193; 0.00028250527002176705 0.00027051953493812536 -0.002325428873182439; 0.0004277896918021998 -0.001349537386725293 0.0005190779971031845; -0.0018883273239754497 -0.0003615880395598445 -0.00012451285723942757; 0.0028094105442301896 -0.0021144821248965844 -0.0011176624991229575; -0.004037300635830685 -0.004623118640291286 -0.00031567838423655415] %
+
+Mass Used: 85.47154727742827 kg
+Launch C3: 97.75466529137994 km²/s²
+||V∞_in||: 0.011119179527248604 km/s
diff --git a/archive/ES_0.5620349613398437 b/archive/ES_0.5620349613398437
new file mode 100644
index 0000000..9a83699
--- /dev/null
+++ b/archive/ES_0.5620349613398437
@@ -0,0 +1,22 @@
+archive/ES_0.5620349613398437---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T01:51:51.600
+Launch V∞: [8.072015316374058, -5.690390335455617, 0.14756015282887974] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002108769947681576, -0.0014536143837536816, -8.703994175367793e-5] km/s
+ V∞_out: [0.0018476444437504692, 0.0008779083345603388, -0.0015461479650610219] km/s
+ time of flight: 1.8749577787489063e8 seconds
+ arrival date: 2030-04-24T04:01:28.600
+ thrust profile: [0.2749703484373514 -0.0010654269558573878 -0.0890461006472779; 0.0608274376125435 0.03406075568184429 -0.07075639600742532; 0.027073730924838144 0.024274990312916963 -0.057849553903909987; 0.028689513788675867 0.03499588303854771 -0.09154072282131773; 0.02219535699482968 0.03288331971908342 -0.09721568464442322; 0.01590620493178561 0.0261377658644183 -0.08627213267196164; 0.014694761896281362 0.02703356126678941 -0.09472340543226951; 0.009371120786057131 0.021261037917656135 -0.07677916337787778; 0.0053191338577734575 0.012740344368377855 -0.05091907747879773; 0.0013223950060065276 0.004157997236861694 -0.014409350509638706; 0.0031763857627644942 0.007273772161718132 -0.03422235442081127; 0.0041070021166007414 0.004402297390540814 -0.01268841579806632; -0.009393268214103526 0.0042015795729387385 -0.01179515056502134; 0.0023113296324395283 0.003576934922658857 -0.004322131603815784; 0.001270333981171501 0.000513812406967214 -0.00801975425431973; 0.011969846285761816 0.006471149610166685 0.001297393294661343; -0.013146069347649558 -0.010709289778708303 0.003112992004184561; 0.020229496804877248 -0.000656804919672899 -0.02327153660038505; -0.00969905129556483 0.010374213648728155 0.006894692367234159; 0.0003652512454416796 0.00019616776792384395 0.00031628458210848035] %
+
+Mass Used: 86.60892818457705 kg
+Launch C3: 97.55974743632696 km²/s²
+||V∞_in||: 0.002562709780751819 km/s
diff --git a/archive/ES_0.5620530279762048 b/archive/ES_0.5620530279762048
new file mode 100644
index 0000000..f4e6633
--- /dev/null
+++ b/archive/ES_0.5620530279762048
@@ -0,0 +1,22 @@
+archive/ES_0.5620530279762048---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:51:17.284
+Launch V∞: [6.298750871620056, -7.480994156656534, 0.04162967784589882] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4999462694909455e-5, -4.00463877365598e-6, 7.009378471820575e-8] km/s
+ V∞_out: [4.7757331495445945e-6, -1.1063050744104162e-7, -2.4883018504247365e-5] km/s
+ time of flight: 1.8439403305671442e8 seconds
+ arrival date: 2029-03-04T00:25:10.284
+ thrust profile: [0.34658849429635696 -0.093114152360063 -0.12270421615098169; 0.13863880077480067 0.03475845396966808 -0.14793358822527297; 0.05188061783738573 0.02571052038048276 -0.09418450518463048; 0.05974450221105237 0.03984091717119091 -0.15159911338905246; 0.05187947093024112 0.042267574911727536 -0.16858660096114875; 0.02734624115205894 0.02515720104754133 -0.10927163125562345; 0.013617272647683585 0.013252178456869417 -0.06155142745732977; 0.0100131094822773 0.01123402253127408 -0.05402083395160272; 0.004437104580270183 0.0054774109621785255 -0.02735963317956878; 0.0008735017968103119 0.001407330552043624 -0.00673766860989239; 0.00044212914319373246 0.0005922606871556545 -0.0017989256385994104; -0.0010784256943171529 0.00025144428880657325 -0.001945837950814868; -0.0002957165418531324 7.570853356062712e-5 -0.0005896979277588644; -0.00021634768413778503 0.000704784638518351 -0.0013844625015605318; 0.00011053243321741766 0.0013753487214146186 0.00029147183059130164; 0.0005004306901681161 -2.3906301068757027e-5 -0.00036632227750964144; 0.0001968744494451903 0.0006741942175448328 6.970936101251789e-5; 0.00044099495254149685 -0.0034038667482831223 -0.0007405222818563943; -0.00062952139696636 -0.0011680202240019906 0.002255909239275997; -0.0010075914486373768 -0.000600368035069995 -0.0003610231707352365] %
+
+Mass Used: 97.82112929458208 kg
+Launch C3: 95.64126914474119 km²/s²
+||V∞_in||: 2.5318277585181312e-5 km/s
diff --git a/archive/ES_0.5620540582226423 b/archive/ES_0.5620540582226423
new file mode 100644
index 0000000..45bc12b
--- /dev/null
+++ b/archive/ES_0.5620540582226423
@@ -0,0 +1,22 @@
+archive/ES_0.5620540582226423---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T15:37:26.900
+Launch V∞: [7.878760758189055, -6.101740086415751, 0.04103507787613529] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.956889386124632e-5, 4.6873099486161933e-5, 0.002988287011171306] km/s
+ V∞_out: [-0.0026515341029489147, -0.0009255849374477466, 0.0010238774725582686] km/s
+ time of flight: 1.7730021766612983e8 seconds
+ arrival date: 2029-12-26T17:41:03.900
+ thrust profile: [0.14953123802657575 -0.017398145801761255 -0.06016707240605226; 0.03551266680387215 0.012291996634091201 -0.046014843264994; 0.04539835588843966 0.025661193947259048 -0.10222218324873822; 0.04237800642315842 0.029696301647766973 -0.1356329015371841; 0.03197751771957877 0.025257027991101272 -0.13124406141828587; 0.019383945980382213 0.016243452049243354 -0.09592230004589837; 0.0110038420556815 0.009390003137957646 -0.06829852103096273; 0.01253251888394907 0.012048583226354815 -0.08479823348336436; 0.019404038197227916 0.018503519384002066 -0.13310294026143515; 0.000543147380463287 0.0004107844155105037 -0.005508289904945076; 0.0005504305442025685 0.0018458495644625666 -0.001374851150210435; 6.1011029681863876e-5 0.000311844515053263 -0.011741657590723292; -0.003716962969796895 0.0009542453963176521 -0.003631097399890643; -0.0014128796846158372 -0.0008781948859910907 -0.004504776554187232; -0.0027397713858885882 -0.0005352640289913315 -0.002938403344883579; -0.0009441730649006806 -0.000894711433839644 -0.007387769426321845; -0.007626854373622752 -0.006909495460827635 -0.0012914340768445162; 0.002184109549853875 0.0020062315854361005 0.004139496798691534; 0.006480861818232924 0.010342556503512242 0.002951776009697711; -8.061554529797824e-5 -0.0010481242394111204 -0.0029117120777562974] %
+
+Mass Used: 76.43431016643035 kg
+Launch C3: 99.30778704456898 km²/s²
+||V∞_in||: 0.002989248200084167 km/s
diff --git a/archive/ES_0.5620554634307087 b/archive/ES_0.5620554634307087
new file mode 100644
index 0000000..d41b618
--- /dev/null
+++ b/archive/ES_0.5620554634307087
@@ -0,0 +1,22 @@
+archive/ES_0.5620554634307087---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:27:32.331
+Launch V∞: [6.405522037027001, -7.479659094590205, 0.0993383816402762] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0011943199637542532, 0.0014548757356473924, 0.0012981732263286914] km/s
+ V∞_out: [-0.0013472823261598016, -0.0009023507987784563, 0.0016120129043300404] km/s
+ time of flight: 1.835986858434507e8 seconds
+ arrival date: 2029-02-23T00:05:37.331
+ thrust profile: [0.28252147637329816 -0.0838059352674434 -0.10729692528855904; 0.07884309334610255 0.01686367314538423 -0.09157223264741843; 0.05235550528166558 0.021894758308646286 -0.1000136187235536; 0.054343903347615054 0.031511340299547 -0.14422813873170762; 0.042933232562842774 0.029742645059236003 -0.1471619587419763; 0.030292735314592874 0.02472249892512134 -0.12916173302481715; 0.020303621656826976 0.017933782238822308 -0.09984174211465598; 0.011960132544535323 0.012750001724809924 -0.07271286150776358; 0.003218317500235395 0.003661899082117697 -0.01896089323167884; 0.0010461542808592723 0.0007688990029536459 -0.006795385318637635; 0.0009938283443843192 0.0009388092067448508 -0.006216974326692222; 0.0005102229970378938 0.0003822386846518576 -0.0021313074072722695; 0.0007306650280601681 0.0008857497164988927 -0.00367418538554828; 0.0005257934903944586 0.00017445301380633558 -0.00183272631678203; 0.0001528518855080271 0.0001993210012078791 -0.0020625955994623274; 0.0016244609166936642 0.001109033803080884 -0.0029675618013954284; 0.000528773461240683 0.0005831091961184906 -0.0017072013305738597; -0.001032750360701488 0.00222519856600849 -0.003377148867065978; -9.010168433306554e-5 0.0006500306741490257 0.00018974141115717878; 3.641044130148213e-5 3.227844809488531e-5 0.0002972546144829778] %
+
+Mass Used: 89.98040236471024 kg
+Launch C3: 96.98588085219141 km²/s²
+||V∞_in||: 0.0022865514005930734 km/s
diff --git a/archive/ES_0.5620560375635767 b/archive/ES_0.5620560375635767
new file mode 100644
index 0000000..d6b667b
--- /dev/null
+++ b/archive/ES_0.5620560375635767
@@ -0,0 +1,22 @@
+archive/ES_0.5620560375635767---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T03:06:14.123
+Launch V∞: [6.552350517441419, -7.342764889407874, 0.1278769405985237] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012075554148409618, 0.0013482286844576532, 0.0012722967452006538] km/s
+ V∞_out: [-0.001501494039509899, -0.0007179711673785564, 0.0014573328505338397] km/s
+ time of flight: 1.8749577787484363e8 seconds
+ arrival date: 2029-04-09T05:15:51.123
+ thrust profile: [0.306950894651387 -0.07751052048227142 -0.10741066092642836; 0.05120203352093739 0.013422567802835034 -0.06020321313512919; 0.06099115813818892 0.034099766794887916 -0.1157510950740904; 0.05948128946868124 0.04452897626848287 -0.15462212553958082; 0.0408996893018197 0.03777763100505229 -0.14011585536129276; 0.017384326882897483 0.01683096478997405 -0.07348745332006083; 0.0145486347063741 0.018347639817224995 -0.07189682191336497; 0.009425999093122701 0.014832900683206696 -0.07140173099467145; 0.004285742654639625 0.008377097787655748 -0.046546500838821774; 0.000973753352839206 0.0013272106776724174 -0.0074007835389158245; 0.007865456365708883 0.010227905647864247 -0.05102574059425286; 0.00020210269091751811 0.00015838768443187713 -0.0003308958187379174; -0.0001463716734765241 -0.00035514097782538353 0.0004236721795453578; -0.00013941983504819232 -0.0004381196166157236 -0.00044947017892731794; 0.0001314461572711062 -1.2576322004015318e-5 -9.359784392820391e-5; 0.000388880247459164 0.00045979918411447236 0.000342924315992206; -0.0012601613024172814 -0.00033875656579866905 0.0006471705446065963; -0.00030283812794432786 -0.0003093782874136761 0.0006642695993402927; 0.00029008549437520325 0.0017625089647130097 0.0024537312799345675; -0.0004233074986218161 0.0003986963380735587 -0.00019138925992543158] %
+
+Mass Used: 90.68127527808201 kg
+Launch C3: 96.8658460364727 km²/s²
+||V∞_in||: 0.0022123855164401882 km/s
diff --git a/archive/ES_0.5620581921623204 b/archive/ES_0.5620581921623204
new file mode 100644
index 0000000..7f048c9
--- /dev/null
+++ b/archive/ES_0.5620581921623204
@@ -0,0 +1,22 @@
+archive/ES_0.5620581921623204---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T16:38:41.026
+Launch V∞: [6.507327452727676, -7.545410159718774, -0.026539867540167315] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.021092176600525092, 0.0003309263826353399, -0.014503814272756934] km/s
+ V∞_out: [0.025027095162591318, -0.00019375222980416818, -0.005420158499354076] km/s
+ time of flight: 1.8462196519745997e8 seconds
+ arrival date: 2029-03-08T12:31:26.026
+ thrust profile: [0.13531575979777388 -0.03978378143601414 -0.053809069281326914; 0.019717807575779126 0.004114763943898108 -0.023679775868422945; 0.04606687944422512 0.01905585066143683 -0.09312204657947937; 0.07681658432996466 0.041275108263855824 -0.2072982802535922; 0.04509741583973588 0.028971115329438753 -0.15754091157145078; 0.025426558022798074 0.018676552674966145 -0.10998835104654904; 0.020204972442235788 0.01622691512147501 -0.1022411457535313; 0.00621220839878387 0.0029954883202033666 -0.02226344556309703; 0.004057667397539163 0.0038639830598512738 -0.027960041033875095; 0.011428329824955133 0.013002901521608282 -0.0771747467977389; 0.0004612599475560513 0.000434949590057632 -0.003517869898726825; 0.0003548867329161957 0.00037858391688690694 -0.0027041831738425517; 4.7300916709056224e-5 -0.0001594493053257318 -0.0009743310772399355; 0.00028482809543587225 0.0006376561260108535 -0.0004952796415752253; -0.00023103112599635048 -0.00012111185677513741 -0.0006585573127121386; 8.707857599973688e-5 -0.0002115485033661903 0.00021559622715700618; 0.0004687275141502795 0.0009235925816804589 -0.0009367045829676624; -5.24808725749933e-5 0.00048750831460508606 -0.0002910779562344379; -0.00010760363045960329 6.945412032239933e-5 -0.0001019291245991723; -8.54605055125623e-5 -6.637900569581934e-5 0.0009239119715098134] %
+
+Mass Used: 76.60571923949283 kg
+Launch C3: 99.2792294199796 km²/s²
+||V∞_in||: 0.025599805750768697 km/s
diff --git a/archive/ES_0.562062805097907 b/archive/ES_0.562062805097907
new file mode 100644
index 0000000..3e92208
--- /dev/null
+++ b/archive/ES_0.562062805097907
@@ -0,0 +1,22 @@
+archive/ES_0.562062805097907---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T19:29:28.583
+Launch V∞: [6.571860186499457, -7.385283769323822, 0.09113870304602599] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01454657682660547, -0.0004252539366265439, 0.01014954751367986] km/s
+ V∞_out: [-0.016953001774283494, 0.00018131480227493414, 0.005225040139339591] km/s
+ time of flight: 1.8749577787492782e8 seconds
+ arrival date: 2029-04-09T21:39:05.583
+ thrust profile: [0.24257825695309165 -0.06000418398116018 -0.08555311226932519; 0.049012731203643856 0.01355799689274533 -0.05539213557326661; 0.059913526655213045 0.0317003809458745 -0.11200488010331319; 0.03902255232893531 0.02805743199459988 -0.10420829535330141; 0.02712545981407529 0.023282614967091875 -0.0926904517523646; 0.03779321330825294 0.037647047817166775 -0.15288356957400312; 0.015844440965373047 0.017074964646294738 -0.07736462563272736; 0.015619664687073063 0.01947171094323121 -0.0900100760035489; 0.016076658789915967 0.01998931037113448 -0.0967570002623149; 0.001535757197578224 0.0013437621515913997 -0.008512936122610375; 0.0004996882532190151 0.000814149099070483 -0.004011179163021807; 0.0007047554582539493 0.00013284148455213336 -0.0003748277358769355; 0.00023900072863508473 0.0001968350226601135 -0.0009290216380650723; -0.00019518028276103554 -7.144558409423452e-5 0.00014594998428113645; -3.574166838401249e-5 0.0002314546734349755 0.0006026477998868178; -0.0002695123735870724 0.000117191556349915 0.0009241225895989845; -0.0008111683464782163 -0.00019897056909559625 -0.001151051988405935; -0.000636679658759647 -0.0018884540732635364 0.0014334112888551864; -0.001994465014127847 5.8639596999971084e-5 -0.0008103144262407299; 0.00022570700880192676 0.00012152739923438553 0.0032578142888437167] %
+
+Mass Used: 85.58953720364798 kg
+Launch C3: 97.74006892752746 km²/s²
+||V∞_in||: 0.017742521044524555 km/s
diff --git a/archive/ES_0.562063454034127 b/archive/ES_0.562063454034127
new file mode 100644
index 0000000..a3c3ef1
--- /dev/null
+++ b/archive/ES_0.562063454034127
@@ -0,0 +1,22 @@
+archive/ES_0.562063454034127---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T07:56:52.383
+Launch V∞: [6.536984956594512, -7.439083018432889, 0.15994775619226187] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6323976981019844e-5, -2.6341695579644585e-6, 4.605341103188585e-8] km/s
+ V∞_out: [3.266072119661892e-6, -7.139011033762913e-8, -1.6209446005515875e-5] km/s
+ time of flight: 1.8498709411496896e8 seconds
+ arrival date: 2029-03-11T09:15:06.383
+ thrust profile: [0.2099203328853024 -0.05989838690346534 -0.07833658145552104; 0.04061673225084332 0.00867214754438745 -0.046974339616349926; 0.05919987704713394 0.02629746520894278 -0.11387801902023675; 0.05869430450526434 0.03487609255498369 -0.15579797969581752; 0.05274265539042918 0.03730671663950438 -0.17754391194553484; 0.035075160927030176 0.028180402794919488 -0.14478312431355073; 0.015131540603760442 0.013129543842953763 -0.07434963453200062; 0.00997264477375981 0.009232402013260293 -0.05528948473300501; 0.004014030745140038 0.003948179872532936 -0.024874868000129436; 0.0007949000542556951 -0.0012917204688432386 -0.003566726378136555; -0.002115672923590649 0.0006339158037883845 -0.00375095884053158; 0.001581381710697412 0.0014854458165996678 -0.0033432466502700165; -2.8137506065808635e-5 0.0037493888348785684 -0.003123587914811451; -2.097890332445582e-5 0.0007963045134811229 -0.0010864490125654372; -0.003291747036338858 0.0007456923205378494 -0.0025693239129762307; 0.0015152083524693563 -0.002422974607247442 -0.0009173663210669677; 0.0007627531825835849 -0.0004151274279873262 -0.004821862744593951; -0.0006111203862494323 0.0005916000228786619 -0.0015073746640380603; -0.0005323718035109307 -0.0005085779970588375 0.0026680295848174043; 0.0017609022938908417 -0.0019598456634525607 -0.0010224751495027905] %
+
+Mass Used: 83.5040444247038 kg
+Launch C3: 98.09771176259048 km²/s²
+||V∞_in||: 1.653521075322719e-5 km/s
diff --git a/archive/ES_0.5620640757646154 b/archive/ES_0.5620640757646154
new file mode 100644
index 0000000..214e963
--- /dev/null
+++ b/archive/ES_0.5620640757646154
@@ -0,0 +1,22 @@
+archive/ES_0.5620640757646154---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T20:32:14.699
+Launch V∞: [6.60178643176302, -7.450550474623167, -0.08632328734018363] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.6040050122017596e-9, -2.3525394300483028e-9, 3.783480224328888e-9] km/s
+ V∞_out: [1.6148394579515266e-9, -3.648074932774775e-9, -5.113129946919905e-9] km/s
+ time of flight: 1.8749577787493932e8 seconds
+ arrival date: 2029-04-10T22:41:51.699
+ thrust profile: [0.12259645330985822 -0.03181768590835724 -0.048823731276403055; 0.069576311825936 0.017466389237971516 -0.08235522173518627; 0.0582278473315952 0.028777298700020548 -0.11677606407913634; 0.04620034642492261 0.029631486620772692 -0.12961723565039088; 0.03624063035750422 0.02818151168937514 -0.13072882717081916; 0.02734055514262258 0.02213203446360716 -0.12090651150692583; 0.02325237353993591 0.02014983943492991 -0.11527419913603819; 0.007841662213068798 0.00855515275854536 -0.04987010315715925; 0.006293485963680623 0.007107133936296039 -0.043574090677326205; 0.0017767131980280417 0.001940847724107927 -0.013185215318463867; 0.00030286004169794453 0.00036207947776306757 -0.0021255858291551826; 0.0003773661783983804 0.00012259086785201053 -0.0026765230306944965; 0.0013622028718078749 0.0007449115839456707 -0.009691511899795455; 0.0012486344286370074 -0.0008435311503536796 0.0008282400131379784; 0.0012066872871220667 -0.0011295900251155483 0.00028275650082518926; 0.0003616092143384666 0.00018841875630580784 -0.0007514342563321325; -0.00013005941835619728 -0.0005059838662910761 0.0011603788061821515; 0.0004864242900772666 0.0007151119463934636 -0.002332177924566581; 0.0007539033133652077 -0.0010481265489199133 -0.0019130183226684354; -0.002305870273933199 0.0002445720890398381 -0.0012738337230873142] %
+
+Mass Used: 77.64794903523034 kg
+Launch C3: 99.10173817545501 km²/s²
+||V∞_in||: 6.406717297508818e-9 km/s
diff --git a/archive/ES_0.5620665448408368 b/archive/ES_0.5620665448408368
new file mode 100644
index 0000000..39eda59
--- /dev/null
+++ b/archive/ES_0.5620665448408368
@@ -0,0 +1,22 @@
+archive/ES_0.5620665448408368---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T08:46:57.716
+Launch V∞: [7.657827003625986, -5.7958421327249, -0.01992512017678546] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8815938988236393e-6, -2.5157445865459463e-6, 1.8477435995067357e-6] km/s
+ V∞_out: [-5.428471045619947e-7, -4.211306517908492e-6, 1.947628934727811e-7] km/s
+ time of flight: 1.8749577787407675e8 seconds
+ arrival date: 2030-04-21T10:56:34.716
+ thrust profile: [0.5540496610821024 0.028352523759201463 -0.13376667502126838; 0.16792997160476367 0.11920922089018518 -0.14458429016395202; 0.09669772286235205 0.11484840949055561 -0.16021598271704038; 0.050412690535165054 0.07861595640873517 -0.12388610852345498; 0.014076528691356786 0.030410648533284915 -0.052884162635281305; 0.018650336175778506 0.053466802340692274 -0.0973087476772725; 0.0034899151230710543 0.012114453572004854 -0.023530699983889406; 0.007175709016917528 0.03216372023339792 -0.06446766898546573; 0.0030530574620726584 0.016719855743046113 -0.03434003254321276; -0.0043566703048480235 0.002575301212288155 -0.004831989102058489; -0.0030841570632206723 0.0005482103129713443 -0.0005157488658433145; 0.0010804102102300107 -0.0012646326789097192 -0.004743208059391516; 0.004423367605642368 -0.0015973802561316964 0.0021928542694859606; -0.0009068272008317953 -0.0009980231034077856 0.002354246268071518; -0.003388313952149826 -0.008924495722499471 -0.004389033237842348; -0.000976331025016882 0.0014955651947412608 0.0015467749721323934; -0.0009585998977470454 -0.0018642123232234654 -0.004494807866277269; 0.008797573603556378 0.0014443741286650998 -0.00978390961810103; -0.0003904764078278554 -0.0013702132883050638 0.003182975178682913; 0.004479767045535718 -0.00424637836554167 0.00703494279685227] %
+
+Mass Used: 117.70973382478815 kg
+Launch C3: 92.23449745534653 km²/s²
+||V∞_in||: 4.248142021165366e-6 km/s
diff --git a/archive/ES_0.5620669227062465 b/archive/ES_0.5620669227062465
new file mode 100644
index 0000000..6ab5c68
--- /dev/null
+++ b/archive/ES_0.5620669227062465
@@ -0,0 +1,22 @@
+archive/ES_0.5620669227062465---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T03:35:40.028
+Launch V∞: [6.465198021046407, -7.308333583298537, 0.18198403907248947] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.320115744560355e-6, 2.126623753595831e-6, 2.4841264496568535e-6] km/s
+ V∞_out: [3.4183486292278214e-6, 2.095670331905407e-6, 6.804839771093963e-8] km/s
+ time of flight: 1.8749577787482357e8 seconds
+ arrival date: 2029-04-08T05:45:17.028
+ thrust profile: [0.4238626470255917 -0.09244845100303384 -0.12460558695983656; 0.06312014443538412 0.01985506174626777 -0.06871670800161087; 0.08500983465331023 0.04975064922559484 -0.14589583916482826; 0.049900452059204556 0.0400140911393706 -0.12510286570210738; 0.03549622449243466 0.034671864730782716 -0.11597603660115474; 0.028132240380805727 0.03181879534845826 -0.11235144898903192; 0.020513351766928145 0.0266487372187919 -0.10083784945096105; 0.008051066787755322 0.010363930375284824 -0.04728841631038219; 0.004008657275581791 0.006286568581619013 -0.026691705915524406; 0.0029175026756100937 0.005534005505328717 -0.024449595380964376; 0.0013663990866507427 0.0022460333397857782 -0.010864705944498992; -0.00018870205230640778 -0.00020664946226474611 0.0003126251879313946; -0.0001411252160343357 0.000630618683577215 -0.0011253874889081022; 0.00019664882255270892 0.0015522568805650483 0.00037992979542619116; 0.0007976181062216482 -0.00012015318213614071 0.0005905832896609213; -0.0017861220842574786 0.000401485278358752 -0.0004271779227025325; -0.0004543545443155065 0.00036748140134872277 0.0008632452311757953; 0.0004676345945443677 -0.0002567897482643024 -0.0007204465224570151; -0.0014366622444928034 0.002298563844410277 -0.0013295954184016586; 0.0005524606684905585 -0.00036121978815555343 -0.0011165324927039158] %
+
+Mass Used: 100.15682328551975 kg
+Launch C3: 95.24364340658876 km²/s²
+||V∞_in||: 4.00953237615057e-6 km/s
diff --git a/archive/ES_0.5620710845048066 b/archive/ES_0.5620710845048066
new file mode 100644
index 0000000..0163d4e
--- /dev/null
+++ b/archive/ES_0.5620710845048066
@@ -0,0 +1,22 @@
+archive/ES_0.5620710845048066---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T08:20:23.039
+Launch V∞: [7.6529303064447465, -5.878100677220699, 0.20217354603583448] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2460642670203062e-9, 1.7268160225810536e-9, 4.70234997896784e-10] km/s
+ V∞_out: [2.352605485488729e-9, -1.9117604528918132e-9, -1.4458098581894412e-9] km/s
+ time of flight: 1.769987129870158e8 seconds
+ arrival date: 2029-12-17T22:38:55.039
+ thrust profile: [0.5764164795042326 -0.034189650850764225 -0.1681542143941951; 0.12112812826998666 0.06285187567107811 -0.12458603342542611; 0.09717395591687938 0.08400310849070955 -0.17373017285924253; 0.04178206716353326 0.04838826446153466 -0.1162260764339981; 0.03833992036945765 0.053923642935371045 -0.1379283586879572; 0.018997015501753648 0.031179823514758613 -0.08942922433801934; 0.01015164307514306 0.019444208616310795 -0.06017100211519364; 0.004994713714595325 0.010558676297456363 -0.03535603515584507; 0.0014939832981381309 0.0038802818566565232 -0.012021468489963185; 0.006235082605901722 0.012858683694836545 -0.05363999095272931; 0.0014129802879759915 -0.0008485508257368424 -0.0032790727431143488; -0.00033854566563026493 -0.0013424323755435795 0.0011142814387935856; -3.6530499219005386e-5 -0.0003244050596254767 -1.0864135012868259e-5; -0.0011841265642669302 0.0005554985345575009 0.0013002627065674338; 0.00022018953154252183 0.0009453877992733652 0.003864702804779206; 0.0010357313027459431 -0.0028505652928153546 -0.0004545410367587108; -0.005181993283887218 0.0026969781306248903 0.0033629215071039444; -0.005107778134072531 0.000732007391452268 0.0021743155866360132; -0.004017223997691305 0.0021946324250999103 4.453609323249775e-5; 0.0005518184804457573 -0.002825373852268571 0.007474229628166733] %
+
+Mass Used: 112.3146086498432 kg
+Launch C3: 93.16028398955963 km²/s²
+||V∞_in||: 2.8719016732254437e-9 km/s
diff --git a/archive/ES_0.5620737200515076 b/archive/ES_0.5620737200515076
new file mode 100644
index 0000000..56b4396
--- /dev/null
+++ b/archive/ES_0.5620737200515076
@@ -0,0 +1,22 @@
+archive/ES_0.5620737200515076---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T02:26:05.416
+Launch V∞: [8.049082137642431, -5.745993328963462, 0.16079460521594063] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.725966195071455e-9, 7.40232360819992e-10, -7.667115266798789e-9] km/s
+ V∞_out: [-2.3205976885815266e-9, 8.259516023670602e-9, -1.2516203036070379e-9] km/s
+ time of flight: 1.8749577787358767e8 seconds
+ arrival date: 2030-04-25T04:35:42.416
+ thrust profile: [0.2928984791570478 -0.005488974357161348 -0.10049180368686243; 0.024518066523088317 0.012590832440382583 -0.031050586956401154; 0.022832976256900013 0.01985969101635355 -0.05497899264815855; 0.02507937130488905 0.02750345740252152 -0.08523508851955844; 0.03867699775416095 0.048862158990309934 -0.15532944669381243; 0.014083766045516687 0.018848167538904243 -0.07110853295984083; 0.011410857201706611 0.017939227414684296 -0.07654053346368125; 0.005049017452862844 0.015866083692203138 -0.06467560520923854; 0.0015487068002126036 0.0063595877647254825 -0.021619416052167138; 0.00034659299317503934 0.007883253178834374 -0.02582599192352553; 0.0069047644281443835 0.011816365071204413 -0.06327711190603406; 0.003489714728859088 0.005616249888466358 -0.03204452314447936; -0.00042615115132512555 0.001928729872612773 -0.006194661107438985; 0.013987314658390643 0.0064385479856009405 0.0012152737536179938; -0.000674930734251773 0.0003957553971144093 -0.0056895601626761536; -0.009985139030688444 -0.004389232861012724 -0.019676626796438716; 0.019832308192207625 -0.002229445038663612 0.0008730409034939902; -0.0063952356939172604 0.0007375709237258916 -0.004554460494560459; -0.009342947904761237 -0.0032855435662215156 -0.015462565642879093; -0.00023952548300467964 3.157549699837805e-5 -0.0005545067295463879] %
+
+Mass Used: 85.07757130966274 kg
+Launch C3: 97.83001750007361 km²/s²
+||V∞_in||: 7.893767146864268e-9 km/s
diff --git a/archive/ES_0.5620756453866624 b/archive/ES_0.5620756453866624
new file mode 100644
index 0000000..42cba15
--- /dev/null
+++ b/archive/ES_0.5620756453866624
@@ -0,0 +1,22 @@
+archive/ES_0.5620756453866624---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:10:39.517
+Launch V∞: [6.5799606603926515, -7.421078531088303, 0.22564695773650267] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001674542370350281, 0.010610145950832582, -0.013988162708040468] km/s
+ V∞_out: [0.012355588840760214, 0.010025367198748877, 0.0076400168911772755] km/s
+ time of flight: 1.8749577780699664e8 seconds
+ arrival date: 2029-04-10T12:20:16.517
+ thrust profile: [0.1899215614547062 -0.04944473189433927 -0.06765196908912034; 0.04942712996710993 0.012660298150109548 -0.05803198296188463; 0.05742680375698223 0.028390409088736232 -0.11054973413273939; 0.04565408240948613 0.030156841093235066 -0.12257098172883564; 0.05593793892319999 0.043402666646074534 -0.18020420805880696; 0.013370058627436074 0.012124669123376251 -0.05844237440187795; 0.01810900598609237 0.017836345608751487 -0.08986909770116627; 0.0055867688194125905 0.007744722119821344 -0.0377151157419529; 0.0066555818717603295 0.009139311390230762 -0.04899020740261094; 0.010901526505949449 0.013641226603233343 -0.07753615769606026; 0.0022917377975394298 0.0027167310456121508 -0.01799853981511744; 0.0006395874427379111 0.0006051932861050079 -0.0037166995736677743; -0.00012127763422268866 -0.00010750001984483583 -0.0004509364039269491; 0.00043049975779655737 0.00010697221880185969 -0.0002349513113723733; 0.0010262500822395717 -0.0002385530428974215 -0.0008096089683288811; 0.00046256642436633583 -0.00024107677070692526 -0.0013503415345243333; 0.0006979879979167464 -9.332324714323375e-5 -0.0006245046668742228; 0.00010123034669002831 -5.082700793495302e-5 0.001835864198639149; -3.282794401965696e-5 -3.925530387238212e-5 0.0001291361090472045; 3.826770466482016e-5 -0.0009325110644687149 -0.0003804153140940583] %
+
+Mass Used: 81.64288808026231 kg
+Launch C3: 98.41920540643036 km²/s²
+||V∞_in||: 0.017636552531452437 km/s
diff --git a/archive/ES_0.5620846505181541 b/archive/ES_0.5620846505181541
new file mode 100644
index 0000000..496c7bf
--- /dev/null
+++ b/archive/ES_0.5620846505181541
@@ -0,0 +1,22 @@
+archive/ES_0.5620846505181541---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T10:54:40.669
+Launch V∞: [6.489611563879101, -7.366805608311307, 0.08590465966237121] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.911182938247447e-9, -2.5060693439092272e-9, 6.075227796755347e-9] km/s
+ V∞_out: [2.80081024773891e-9, -6.413591340039246e-9, -8.109058305919325e-9] km/s
+ time of flight: 1.8582735702767152e8 seconds
+ arrival date: 2029-03-21T05:37:17.669
+ thrust profile: [0.3789129329246113 -0.11483491648878233 -0.14459017580890696; 0.04094200718913383 0.007886951215349313 -0.05324493198616526; 0.037209417027927745 0.014879786264339506 -0.08117221612831992; 0.03650149106006645 0.020652757643381658 -0.11323834800063114; 0.04434571145029988 0.02855624942303135 -0.1757588531156406; 0.02288478593739617 0.017107911821784096 -0.11359375872930365; 0.021995961052182017 0.01701484002064906 -0.11468087928199194; 0.011117948058677999 0.009162130641755778 -0.0700535984099657; 0.004064909975762652 0.0019925936592133644 -0.025197131220278217; 0.0009909697735223774 0.0007936575900939062 -0.0056699240904876085; 0.004243448969314804 0.003783730287088903 -0.029122636998837142; 0.00035428827991395456 0.00011823055227594856 -0.0011100563517913154; 0.0005068244377696418 -0.00033746942155529655 0.0007399869778774411; -0.00025553459573454055 5.524684069488261e-5 -0.000741260530293135; -7.816148403283772e-5 0.00016210689836876878 0.0004561725656499685; 0.0006573650193422673 0.00019280351380942092 0.0016016707299274884; -0.00010974000932123996 -0.0015141127441723828 -0.0009015187605197828; 0.0014156391524136973 -0.0006207889059769873 0.0005255811995430685; -0.0010831320530513878 -0.0005908132359077365 0.0016393525392625217; -0.00016707447894795694 0.00015312720362957596 0.0010156187890923085] %
+
+Mass Used: 93.4772263389932 kg
+Launch C3: 96.392262731232 km²/s²
+||V∞_in||: 9.536940072416995e-9 km/s
diff --git a/archive/ES_0.5620857273546801 b/archive/ES_0.5620857273546801
new file mode 100644
index 0000000..c4163b5
--- /dev/null
+++ b/archive/ES_0.5620857273546801
@@ -0,0 +1,22 @@
+archive/ES_0.5620857273546801---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T16:34:49.611
+Launch V∞: [6.517187690178141, -7.319256927198007, 0.15972608423553827] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.339608184422902e-7, -5.0887814026721175e-8, 6.534257786148251e-8] km/s
+ V∞_out: [-2.4331711384272356e-7, 2.2098018469200004e-8, -2.8857817235078285e-8] km/s
+ time of flight: 1.8749577787463188e8 seconds
+ arrival date: 2029-04-08T18:44:26.611
+ thrust profile: [0.3561387294479565 -0.08976475945128223 -0.12209623038333879; 0.06549044824125735 0.01781670579226613 -0.06995940903796716; 0.0695876971757901 0.036601789633961226 -0.12483326695366931; 0.06425074237120143 0.04543675614355748 -0.16154251424659957; 0.04094807836710691 0.034943841330556266 -0.13305969828523698; 0.017950113817435883 0.0176079023300562 -0.07158609116878484; 0.01984996747805052 0.02174950105506464 -0.09318043179081276; 0.013945289192982694 0.016760478928806687 -0.07549170179372611; 0.004758600385122149 0.006139319033104037 -0.028661361799604962; 0.0007794759753085106 0.0011886035255831739 -0.005889117373364142; 0.002108234142055033 -0.0003824376414879875 -0.004414597795956853; -0.0010807194100691643 0.0007325939410028042 -0.0053615659846123435; 0.000836807315726861 -0.000771934599589896 -0.00296607270615728; 0.00031916257048236784 0.0020613652054341184 -0.002547580613655289; 0.0006204122176617333 0.0005337938261980613 -0.001468179058358271; 0.0008460492997930002 -0.0005746437539645949 -3.57355806384998e-5; -8.639793093674582e-5 -0.0012298145700493797 -0.001480125206206293; 0.002793471196654793 0.002788036074167867 -0.002926090297637572; -0.0002828864354991055 0.0012061187067638163 -0.0008084884566901187; -0.00210188170259608 0.0013824388299513782 0.005530712248682324] %
+
+Mass Used: 95.35385821269756 kg
+Launch C3: 96.07076977733072 km²/s²
+||V∞_in||: 2.481872008468373e-7 km/s
diff --git a/archive/ES_0.5620881344984455 b/archive/ES_0.5620881344984455
new file mode 100644
index 0000000..02b8a32
--- /dev/null
+++ b/archive/ES_0.5620881344984455
@@ -0,0 +1,22 @@
+archive/ES_0.5620881344984455---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T20:28:22.130
+Launch V∞: [7.693365793951944, -6.230973590665954, -0.1362553430120321] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.590310045455812e-7, 3.2815777561542263e-6, 8.838705060080532e-6] km/s
+ V∞_out: [8.471830150063424e-6, 9.833871321873723e-7, -4.130965553339335e-6] km/s
+ time of flight: 1.6846194070226964e8 seconds
+ arrival date: 2029-09-11T15:27:22.130
+ thrust profile: [0.19628547636093874 -0.03262356351739039 -0.07791564756296875; 0.0970011626433917 0.03149092069214907 -0.11714231598850076; 0.05290373224443991 0.029251846211501 -0.10924045152632195; 0.047871726861143826 0.03391908779926557 -0.14062167626122224; 0.039485947229794205 0.032669255444055356 -0.1493590073081495; 0.03005438158087813 0.027526398840002957 -0.13767449943464985; 0.022396740740537924 0.02203949538773102 -0.11994714212746359; 0.014363276405657847 0.01461177041197677 -0.0856885737996976; 0.005045473361069696 0.005366822373469352 -0.03338376406382521; 0.0034790682082245688 0.003479562024227785 -0.024896349976995507; 0.000235391963001827 0.0008044999211876899 -0.005295057237085285; 0.0006418117285801666 0.0003483823052632392 -0.006090812118879288; 0.0004314169806482079 0.00043220676095453926 -0.003721332970774579; 0.0003611811929307453 0.00039245970089541176 -0.004336048313949774; -0.0012772847887319227 0.001059894723120449 -0.0008725129927795039; -0.001141853025517314 0.00029484005666414114 -0.0027567799880585087; 0.001247759835607259 0.00246536398996592 -0.00026448200730092714; -9.181297553512158e-5 -0.0004955320782213061 0.00041137945195017576; -0.000905114774415459 0.003046090742334021 -0.000871732634106719; 0.00029669371981495265 -0.00028687153633737833 9.854013221941406e-5] %
+
+Mass Used: 83.91922148203639 kg
+Launch C3: 98.03147464562572 km²/s²
+||V∞_in||: 9.476877132075687e-6 km/s
diff --git a/archive/ES_0.5620928083271174 b/archive/ES_0.5620928083271174
new file mode 100644
index 0000000..a4b10d7
--- /dev/null
+++ b/archive/ES_0.5620928083271174
@@ -0,0 +1,22 @@
+archive/ES_0.5620928083271174---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T22:58:21.250
+Launch V∞: [6.597789080102858, -7.462426882536764, 0.06541374848256197] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.017761594689570583, 0.00027098310368324594, -0.012071058084675993] km/s
+ V∞_out: [0.020817611260073945, -0.00019280250672640452, -0.005270062857502978] km/s
+ time of flight: 1.853849295905234e8 seconds
+ arrival date: 2029-03-16T14:47:10.250
+ thrust profile: [0.09595442126313755 -0.028331932440134606 -0.03893295589463383; 0.09766657961070062 0.022004504338407713 -0.1150683205292975; 0.05718394803535586 0.023070925835328767 -0.11604062326700988; 0.0345511349081452 0.018835654935220984 -0.0978476072124563; 0.03572146246612801 0.023068189571993452 -0.13039116234541023; 0.04707611254179433 0.031265852199525504 -0.18834956394558788; 0.013130196681747442 0.010647302082182031 -0.06849886252798584; 0.011096007060988256 0.009618903735920196 -0.06590732175352759; 0.0052423627975575465 0.004818297772691824 -0.03532806906266297; 0.0015955361240217797 0.0017228499358176892 -0.013623731287821749; 0.0012436290315168046 0.0008788794835211461 -0.007377240677408499; 0.00043512505131859387 -0.0010131008437416814 -0.00047649193540249635; 0.0008959591116606271 0.00159395823847054 -0.0010850406460804515; 0.0001146172150161026 0.00035873039128286606 -0.0015772272869871184; -0.0004952431180985388 -0.00023774576416135576 -0.0012802587133094708; -0.0006990052366237825 2.6564885712905605e-5 -0.00047035560754511295; -0.002555277216746128 -0.000428007766962783 -0.0021425630819163185; -0.0018884429121005786 -0.00020642870639625338 -0.002398080410054999; -0.0011590741398168948 -0.00013556646992962418 -0.00137371422659703; -7.830935866931705e-6 -0.0006452107471819224 0.0011565839436068477] %
+
+Mass Used: 76.97460740783936 kg
+Launch C3: 99.22291468122245 km²/s²
+||V∞_in||: 0.021476920660157158 km/s
diff --git a/archive/ES_0.5620945428132005 b/archive/ES_0.5620945428132005
new file mode 100644
index 0000000..b543aca
--- /dev/null
+++ b/archive/ES_0.5620945428132005
@@ -0,0 +1,22 @@
+archive/ES_0.5620945428132005---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T07:41:27.622
+Launch V∞: [7.684688407203061, -5.771022660041082, -0.040790003465206275] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0022078457412454e-7, -8.561674355983345e-7, 1.549557498968123e-7] km/s
+ V∞_out: [-7.197671179805267e-8, 2.8479617601917445e-7, 4.0827844199442437e-7] km/s
+ time of flight: 1.843058005017814e8 seconds
+ arrival date: 2030-03-13T11:44:47.622
+ thrust profile: [0.5128848345258262 0.004944011432226858 -0.13396848925047947; 0.21533972093630557 0.13748552409982812 -0.1890807306397808; 0.09232666070959471 0.09856640957620573 -0.15139730228896894; 0.07779380428844572 0.11435914826489779 -0.19133174666178956; 0.03602484042753125 0.06753899971810184 -0.1265631945513568; 0.009776771523000454 0.022500442958592326 -0.046746748775185636; 0.0022422529511527123 0.006512338874299772 -0.015599107238814474; 0.0021387602181980178 0.0070247849501658575 -0.01739297521561243; 0.0012844099428961596 0.00197727259702668 -0.006680228825091519; 0.00012340435594322316 0.0032271417382800536 -0.006962099215912906; 0.0005022223971280018 0.0011427052776643825 -0.002472409240593272; 0.0011084158191115821 -0.0017497245156128448 -0.001278893896515416; 0.0003631214291824963 0.000541070472385918 -0.00025198723631681915; -0.0032393563833583577 0.00411930233594295 -0.0022340359917289083; -0.0015828249609621784 0.0005498055671087842 -0.0013668794977612147; 0.0006932594034732956 -0.004588801911584532 0.0024650684131565072; -0.0049611504672848455 0.005408009089370357 -0.004292957703666984; 0.0021668556290802116 -0.007270440655178519 0.0024886334932094785; -0.00022022560412794198 -0.004608851150125233 0.008342657603663215; 0.004335590019501151 -0.010046417330547203 -0.0006941705191013049] %
+
+Mass Used: 117.00561996520037 kg
+Launch C3: 92.36080228289146 km²/s²
+||V∞_in||: 8.758299879918275e-7 km/s
diff --git a/archive/ES_0.5620998631018252 b/archive/ES_0.5620998631018252
new file mode 100644
index 0000000..13515e0
--- /dev/null
+++ b/archive/ES_0.5620998631018252
@@ -0,0 +1,22 @@
+archive/ES_0.5620998631018252---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:34:37.599
+Launch V∞: [6.323310552377897, -7.372690949881791, 0.16494198750832734] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.94946674241653e-5, -3.0176571529925828e-6, 5.155979525771417e-8] km/s
+ V∞_out: [3.492374557872595e-6, -7.794060673809948e-8, -1.941555103802608e-5] km/s
+ time of flight: 1.8749577787499148e8 seconds
+ arrival date: 2029-04-09T06:44:14.599
+ thrust profile: [0.4589760301589563 -0.12702103202419576 -0.13720103930948507; 0.08638271512691602 0.021946760756513563 -0.09283218196644959; 0.14620788358296757 0.07319639360290618 -0.2513989306841612; 0.03259180434451052 0.02182922955750266 -0.08369736110457655; 0.028054001653138514 0.022661851959776238 -0.09259870668335536; 0.01829047609459748 0.016754977925509573 -0.07215831685405824; 0.020205774551171007 0.020977876743152837 -0.09570112287224054; 0.007817002076636237 0.009630731369420395 -0.046843349030114674; 0.004238970476030076 0.005291175907401598 -0.027116879737826914; 0.0010024102703235227 0.00045640747999173476 -0.007545529542723695; 3.9855030048556624e-5 0.0007995227332172039 -0.003954636413364061; 0.0016970180811302876 0.002971954037546482 -0.013826546873714804; 0.0003274238571485966 -0.00017499868262313434 -0.0011631576230941424; 9.134989669177715e-5 8.108349138060805e-5 -0.0016297931971230922; -0.00011801734842026843 0.0010256256574877893 -0.0014663927787053263; -0.0012626354639462345 0.0019095336838778633 0.0006888266701948468; 0.000506366887767172 -6.86036986859422e-6 -0.001854900056152947; 0.00120444481570619 0.0005953157867771616 -0.00042720635881374766; 0.001691350329667772 -0.0017543284113587143 -0.003978498650800453; 0.0007265376614215617 -3.9234112239510625e-5 -0.0002605501372518529] %
+
+Mass Used: 105.30297503156271 kg
+Launch C3: 94.36803404352574 km²/s²
+||V∞_in||: 1.9726909820960454e-5 km/s
diff --git a/archive/ES_0.562106214929131 b/archive/ES_0.562106214929131
new file mode 100644
index 0000000..af1a7c5
--- /dev/null
+++ b/archive/ES_0.562106214929131
@@ -0,0 +1,22 @@
+archive/ES_0.562106214929131---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T16:26:36.808
+Launch V∞: [7.837901922659051, -5.657644045014069, 0.2618203946158095] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5276537235071914e-5, 0.0003553527896800061, 7.025927577410832e-6] km/s
+ V∞_out: [0.0003425481628130043, -5.2118991700540885e-5, 7.589155698015211e-5] km/s
+ time of flight: 1.8508287242203695e8 seconds
+ arrival date: 2030-03-22T20:21:08.808
+ thrust profile: [0.5048433274216526 0.0046608284110314264 -0.12896692730431597; 0.15544048538628777 0.09438978514240025 -0.1406084550246904; 0.08100514538976072 0.08454535925085803 -0.13609097987058313; 0.04295445007357785 0.05689106504818175 -0.10391293354759952; 0.028772805985786555 0.04112389479762535 -0.0924880483183513; 0.023938332458344924 0.04397387272846789 -0.09352001327787485; 0.010433498722757695 0.026086173446640274 -0.057967461668502786; 0.0017658206569934713 0.004123646701362588 -0.012412022166873702; 0.004903898988605664 0.0178321158563565 -0.04180130647706223; 0.00210954899349318 0.00509002290404366 -0.01928834105218076; 0.0016561138424323468 0.008973804587128402 -0.02957296697360361; 0.00019348772745326223 -1.757167994787586e-6 0.0002860379288665447; -0.0011209765313217744 0.004004874317884874 -0.0015454173246818859; -3.432558206042108e-5 0.0014892083763263465 -0.0032954695093524084; -0.000777422517587115 0.006070282443533836 0.0077661946308073704; 0.002039392118725897 5.307735309841312e-5 0.0037682156085117715; -0.004409912298077166 -0.003838066162880183 0.0017404208149740356; -0.001144136920782247 0.0011971172950693513 -0.0021612747909499296; -0.0071266684080649595 0.004929856076300219 -0.011337950174834029; 0.008932754087639883 -0.00016130876145305055 0.0013856310425151477] %
+
+Mass Used: 110.31446053532227 kg
+Launch C3: 93.5101926083424 km²/s²
+||V∞_in||: 0.00035575039196265157 km/s
diff --git a/archive/ES_0.5621098749877337 b/archive/ES_0.5621098749877337
new file mode 100644
index 0000000..4f2219a
--- /dev/null
+++ b/archive/ES_0.5621098749877337
@@ -0,0 +1,22 @@
+archive/ES_0.5621098749877337---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T01:06:23.764
+Launch V∞: [6.381635347452401, -7.444944426021042, -0.004476879552062274] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2219339918082711e-7, 8.777374646727799e-7, -5.274704896551122e-8] km/s
+ V∞_out: [3.254706822612775e-7, -7.227368217804727e-7, 4.0173590417569593e-7] km/s
+ time of flight: 1.855602878759462e8 seconds
+ arrival date: 2029-03-17T17:37:50.764
+ thrust profile: [0.3604619056281136 -0.0867059084320145 -0.11798411383892844; 0.06343712666575373 0.018603216569949493 -0.06652408356757401; 0.04077928808681895 0.022928723334069142 -0.07204964271436166; 0.04238317434962015 0.032320966184682935 -0.10319799114498453; 0.028720868033011843 0.02666875963551881 -0.09097587298297805; 0.03488656224538579 0.03777358072366661 -0.13233433167084255; 0.048811211419923554 0.06010562133546991 -0.21133516539496086; 0.012186603610590792 0.01636902010598553 -0.06529566383026424; 0.004891067763498888 0.007149318809465662 -0.03075866644174581; 0.0026979237771312596 0.004235825871931736 -0.018124742286154946; 0.0007044377205634983 0.00125649501549003 -0.005910018096020417; -0.00018187719570915935 0.0003053031301214882 -0.0006249025371460365; -4.316544985443578e-6 0.0001312195002656923 -0.0002570518309419397; -0.0006518034375856941 -0.00043595561151077807 -0.0010537961988344548; 0.00010286129449818997 -0.0008043140782106469 -0.00011496725139519839; -0.00013842751356449025 -2.1205583956059883e-5 -0.0009067234763023069; -0.0002531657674847987 0.0005552579781833026 0.00012174960570448309; -0.00033070360666655093 -0.0003814860186446398 0.0002960877643483137; -0.00015678124206557222 0.0005620707633677256 0.00037143771233272304; -0.0005420465958931614 0.0018114884619364873 -0.0011603587719304705] %
+
+Mass Used: 94.90534515408626 kg
+Launch C3: 96.15248725684624 km²/s²
+||V∞_in||: 8.877705417888873e-7 km/s
diff --git a/archive/ES_0.5621215380236475 b/archive/ES_0.5621215380236475
new file mode 100644
index 0000000..c994048
--- /dev/null
+++ b/archive/ES_0.5621215380236475
@@ -0,0 +1,22 @@
+archive/ES_0.5621215380236475---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T18:38:51.947
+Launch V∞: [7.536369482542845, -5.936690320885104, 0.08873343819284668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.010907161077447e-10, 8.360230193145042e-10, -1.7737268034290283e-9] km/s
+ V∞_out: [9.334456934153536e-10, 1.7867837436523139e-9, 4.760805543525777e-11] km/s
+ time of flight: 1.7743508224072585e8 seconds
+ arrival date: 2029-12-23T10:10:13.947
+ thrust profile: [0.6739114456595021 -0.030262089833422913 -0.16246117279652889; 0.12103010704246935 0.06964211027860683 -0.1176352008442407; 0.07608301285912676 0.07350615146661765 -0.13442625048507084; 0.026805703042349256 0.03089525043165044 -0.06412549633323579; 0.0244076223546878 0.03946779737147002 -0.0913727005590474; 0.024506687612714524 0.04002901069725797 -0.10046412528719763; 0.020513273881107942 0.04207373130153615 -0.09881792814509771; 0.007782831534745437 0.02027498684211579 -0.05968919168274316; 0.005477815166890314 0.016246431151688986 -0.04824560082303678; 0.002830777756604259 0.00952616740442239 -0.029279192525105316; 0.0009337291299570182 0.02032513243742231 -0.051608784719423234; 0.001044168491026904 0.004218612032273373 -0.0023010912239790626; 0.0010252015018521578 0.001732716107865231 -0.0040799324013164225; -0.00029571889561408424 -0.00221959592810303 -0.002650796354804666; 0.0010400984361745005 0.000158720370137355 -0.003839942536414121; 0.0012163181346021548 0.0003165360315372204 -0.002616495811091505; -0.0009832268773570325 0.0019376190124150863 -0.004122842452393803; 0.0002863220800452945 0.0010969144101725021 -0.003164917630078467; 0.0007923020799460941 -0.0019964200178009144 -0.003877471126311597; -0.0018678537269943062 -0.001246465666960315 -0.0012373288172717772] %
+
+Mass Used: 118.85578272272824 kg
+Launch C3: 92.04903056654753 km²/s²
+||V∞_in||: 2.118203861166417e-9 km/s
diff --git a/archive/ES_0.5621254915677929 b/archive/ES_0.5621254915677929
new file mode 100644
index 0000000..8bfc46d
--- /dev/null
+++ b/archive/ES_0.5621254915677929
@@ -0,0 +1,22 @@
+archive/ES_0.5621254915677929---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T20:09:56.301
+Launch V∞: [7.912568514010468, -5.873491504044481, -0.22934450791848782] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.662883876367447e-6, 9.883466805070294e-5, 1.9443519065542562e-6] km/s
+ V∞_out: [2.45079433258247e-5, 9.544080655524842e-5, 5.3829714451683e-6] km/s
+ time of flight: 1.847117754059503e8 seconds
+ arrival date: 2030-03-23T16:59:31.301
+ thrust profile: [0.311140673896069 -0.019826086393290324 -0.1060108837600962; 0.10238674330589205 0.03406284369308491 -0.12601862306847408; 0.023135179707345972 0.014934980901662547 -0.05932084365058218; 0.03692638695947292 0.034570814865279804 -0.12845967793344337; 0.01584747431178661 0.015662410343425505 -0.07085055814838578; 0.009041677705741954 0.01195278714957564 -0.05133222767181435; 0.011725865298065536 0.013216597561981689 -0.0699416822430711; 0.025896314686744675 0.03083114649929631 -0.16642067857746237; 0.004626744430260817 0.005956739759557538 -0.04576204857264255; 0.0014755636390932356 0.0009611478638453541 -0.017020864056016122; 2.5588541810539298e-5 -0.0001905327953482871 0.001230610447127222; 0.005497010951311652 0.004102032731167434 -0.004946745793402804; 0.004898191772774339 -0.0008325544188567625 -0.005693746706675705; 0.003853380603586435 -0.008936914979809796 -0.0016774444880016323; -0.007353825551124465 0.011854563048543884 0.00011501059593092399; 0.0017429976996709419 -0.0005060104661699814 0.0005369316967956915; -0.000488824879089148 0.00471067999768553 0.0038010339243422227; -0.0009881593760169146 9.823538602217778e-5 0.0006099875684326906; 0.0070002647551412975 -0.020266495365891604 0.00576510864937526; 0.000627344348384611 0.00021630784429241203 -0.005015633635886056] %
+
+Mass Used: 89.05082942731315 kg
+Launch C3: 97.1592418403049 km²/s²
+||V∞_in||: 9.896370344259379e-5 km/s
diff --git a/archive/ES_0.5621286397563757 b/archive/ES_0.5621286397563757
new file mode 100644
index 0000000..7a2cc1e
--- /dev/null
+++ b/archive/ES_0.5621286397563757
@@ -0,0 +1,22 @@
+archive/ES_0.5621286397563757---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T07:04:23.608
+Launch V∞: [7.968578445830458, -5.960669267968358, 0.8047883039950808] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1420855484327564e-9, -3.243123326598524e-10, -1.6452918858033918e-9] km/s
+ V∞_out: [4.748694019650393e-10, 1.0053149322255025e-9, 2.4636105753637124e-11] km/s
+ time of flight: 1.824442914053039e8 seconds
+ arrival date: 2030-02-25T22:02:34.608
+ thrust profile: [0.17669695105022745 -0.01866160728560164 -0.06640451136172384; 0.03697197738581524 0.012453791481701152 -0.047682983020009076; 0.04189049072151084 0.02096882863131101 -0.09337828576047232; 0.04428400852820306 0.025803234640496327 -0.13864759910528288; 0.03196582737577009 0.02028366509396404 -0.12688931644925674; 0.029889928070820224 0.019425762856701254 -0.14058214478856396; 0.01762799865662875 0.011702094282918222 -0.09543629401066028; 0.008539063905643213 0.005714177013584387 -0.05209535980225471; 0.0021814821248624734 0.001261426207621375 -0.014885683293231993; 0.0035087366121320366 0.002294434676450036 -0.023125117396643514; 0.0016337731867853845 0.0012769679706175073 -0.010741436045226057; 0.0009264646759724999 0.00101067876081731 -0.006607818774779652; 0.0004925308965674092 -9.475368452419085e-5 -0.0035613783332743443; 0.0003359838861691273 0.004511234120704658 0.0007787869899612884; 0.0016801345749467764 -0.000815832044498923 -0.0014610322393015809; 0.002497542222853041 0.0010175522345523902 0.0015865678006617753; 0.0007546041569397976 -0.0011702545242091244 -0.0032477159601950276; 0.0004289806985069249 -0.0001801945658434692 -0.0031573518325351477; -2.6438745829403005e-5 0.005001598504437729 0.0003363379124340822; 0.002331188785964717 -0.00013233221827901734 -0.009931571375631134] %
+
+Mass Used: 74.37630181083478 kg
+Launch C3: 99.67550478370347 km²/s²
+||V∞_in||: 2.028921703404226e-9 km/s
diff --git a/archive/ES_0.5621316634745377 b/archive/ES_0.5621316634745377
new file mode 100644
index 0000000..919a133
--- /dev/null
+++ b/archive/ES_0.5621316634745377
@@ -0,0 +1,22 @@
+archive/ES_0.5621316634745377---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T10:38:43.815
+Launch V∞: [6.486639388789216, -7.441650983659834, -0.07478206974399479] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.810127368156563e-8, 2.2820403144454552e-8, 1.501009748007353e-8] km/s
+ V∞_out: [-1.8860587886074495e-9, 4.06788033163614e-9, -6.058120631122385e-9] km/s
+ time of flight: 1.8749577787199324e8 seconds
+ arrival date: 2029-04-09T12:48:20.815
+ thrust profile: [0.21306246142998522 -0.04591836356429065 -0.0707369229022575; 0.06500693594023295 0.021934778923527333 -0.06678003613359063; 0.09086979420809906 0.05709055918744041 -0.14823110166196915; 0.04917361762588283 0.04196263243609846 -0.11625143825140587; 0.0361462602911308 0.03674748630001297 -0.11274329123411775; 0.064813277091695 0.08140372177970821 -0.2409775384624282; 0.014968616023696181 0.0222168572143613 -0.07183161144438466; 0.002331993527530171 0.0036820420287588997 -0.014172524798303514; 0.003416398390778289 0.004981824267884414 -0.019260025120762067; 0.0008108085975152383 0.0012432000656452146 -0.005362171965051295; 0.0006519591304746252 0.0007784813013230185 -0.003888332722877143; -0.0001181689944443283 0.0006569815015107714 -0.0010149460138557365; -0.0016637117994446904 -0.0014401592795373684 0.0004143984757054751; 0.0007243273984487863 0.00019950001239341835 -0.001961592419479136; 7.916363984138857e-5 7.928754635769414e-5 -0.0005381176326299604; 4.6811317923484315e-5 -0.0002537049999946269 0.0017672225943527829; -0.0008776455088966268 0.0009314365776547948 0.0013613151279410008; 0.0005301920675223616 -0.00037750956268984344 0.002954026085724058; 0.0013704579522657505 0.0013260814085137881 0.0038437449589297295; -0.0015225934189858062 0.003223080595711761 -0.0008061689067645718] %
+
+Mass Used: 87.30213574923891 kg
+Launch C3: 97.4602522807523 km²/s²
+||V∞_in||: 3.2767818586712195e-8 km/s
diff --git a/archive/ES_0.5621483363367723 b/archive/ES_0.5621483363367723
new file mode 100644
index 0000000..c634991
--- /dev/null
+++ b/archive/ES_0.5621483363367723
@@ -0,0 +1,22 @@
+archive/ES_0.5621483363367723---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T13:07:52.620
+Launch V∞: [6.601894523500622, -7.411996286491034, 0.148547817630531] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7457916307132955e-9, -1.6566616872775224e-9, 2.156070005181777e-9] km/s
+ V∞_out: [1.0461631685331607e-9, -2.3458224629697602e-9, -3.2098373063365883e-9] km/s
+ time of flight: 1.8749577787477186e8 seconds
+ arrival date: 2029-04-10T15:17:29.620
+ thrust profile: [0.1911097043004399 -0.05156320301876721 -0.07245771627140987; 0.023607024088898542 0.005376698507215547 -0.028687694038046434; 0.06265863686247401 0.028495012922300125 -0.12278259543035874; 0.05621985396421505 0.0338711952905045 -0.15328828674211742; 0.0567798695814569 0.04046352543159595 -0.19600363479295152; 0.0240121315334158 0.019480514243184942 -0.10378079820220784; 0.009486838146042703 0.008304987475029562 -0.04922176307500323; 0.005746934665349271 0.00533548295339321 -0.034572776530579725; 0.003318441570039487 0.0032386941162740033 -0.022088340745553485; 0.007884061773431403 0.008097985625181712 -0.05722450225622754; 0.0023655704446136103 0.0021001135912965575 -0.017392945883050435; 0.0006038793137952837 0.000745847104203025 -0.00615614886118898; -0.0011257555333167254 7.780641256678462e-5 -0.00044429485661585943; -0.0006109077111251687 0.0011289392105110494 0.0004109527420172321; 0.0016684643487286774 0.0008460029980966347 -0.0034879086862081303; -0.0014701470450477223 -0.0007166676400660232 -0.002738376456068928; 0.00044988646789563357 -0.0008494779672562316 -0.0006565993997649647; -0.0002763280036407345 -0.0006289367473361865 -0.0011490945462599527; 0.00289662128323254 -0.0019307114499004245 0.0018216126618497252; -0.0009886960192915985 -8.031022315374031e-5 -0.0054058931408481024] %
+
+Mass Used: 80.99525328327582 kg
+Launch C3: 98.54476670450718 km²/s²
+||V∞_in||: 3.864264159271845e-9 km/s
diff --git a/archive/ES_0.5621542647078327 b/archive/ES_0.5621542647078327
new file mode 100644
index 0000000..70728f2
--- /dev/null
+++ b/archive/ES_0.5621542647078327
@@ -0,0 +1,22 @@
+archive/ES_0.5621542647078327---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T03:44:40.262
+Launch V∞: [7.638865567277496, -5.982309957172997, 0.31759158213403327] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2625762596963554e-9, 1.457100294290663e-9, -1.0540614693139216e-8] km/s
+ V∞_out: [-3.022444921938836e-9, 1.0692994175350021e-8, -1.5310130413015103e-9] km/s
+ time of flight: 1.7822195631386846e8 seconds
+ arrival date: 2030-01-02T21:50:36.262
+ thrust profile: [0.433704639795631 -0.028055643893356227 -0.1206006592870624; 0.16108487618964074 0.08225382135358414 -0.16089287207296474; 0.09508182243227091 0.07901823435457268 -0.16957657164176437; 0.048263294416099556 0.05405887629798821 -0.13088486023693197; 0.03376521905491196 0.04616180319605939 -0.12306536086798361; 0.02214284828851781 0.03556575174567319 -0.10372119549882929; 0.010484960724469397 0.01900257110579814 -0.06057323316745155; 0.0020384783296751277 0.0077012585713518485 -0.023403224773569115; 0.003595876194318601 0.00558398892806693 -0.024093290032694725; -0.0028968630813697447 0.002983605902756517 -0.012366918487398; -0.0015728370321698784 0.0014303560233256323 -0.004632825353709494; 0.0009014319648245673 0.0023734308529368316 -0.0013344433927155806; -0.006676503454312321 0.004951925043566327 0.003908505487678995; -0.002110450064793 0.003605417396899636 -0.0057913231514176; 0.004541500134010707 -0.003999988970644243 0.004657313509177614; -0.001642475010364095 -0.0035162696353751963 0.010806792577572662; 0.00016125750644702702 -0.0006350243629666265 -0.00043523802583701656; 0.0006076167922517855 -0.001296285018826379 0.009642494103318217; 0.00964094724795422 -0.000872405618571488 -0.0005768944654541249; 0.002873197699476359 -4.6449079407554454e-5 0.0031642588687837195] %
+
+Mass Used: 106.10651887438871 kg
+Launch C3: 94.24116399167133 km²/s²
+||V∞_in||: 1.0878738470419529e-8 km/s
diff --git a/archive/ES_0.5621602968054525 b/archive/ES_0.5621602968054525
new file mode 100644
index 0000000..e102a34
--- /dev/null
+++ b/archive/ES_0.5621602968054525
@@ -0,0 +1,22 @@
+archive/ES_0.5621602968054525---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T20:31:51.310
+Launch V∞: [6.6280127459349165, -7.383413153556964, 0.169386720259056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5027158302241248e-5, -2.3177430119616163e-6, 4.053715061825648e-8] km/s
+ V∞_out: [2.874418034251667e-6, -6.713599164173743e-8, -1.4931359504314549e-5] km/s
+ time of flight: 1.8749577787485296e8 seconds
+ arrival date: 2029-04-09T22:41:28.310
+ thrust profile: [0.17165839758391815 -0.04422932885542605 -0.0639233141178581; 0.05598623532252942 0.01367860039482825 -0.06333449905369934; 0.06326517781806319 0.031236972903910063 -0.12064759290590298; 0.056177387407396494 0.037086399527842824 -0.1492556356453054; 0.045884274103146196 0.03621719444757434 -0.15590769919059969; 0.03281653405669396 0.029223342499158027 -0.1359173900560018; 0.010690798152419226 0.009830930774128468 -0.05279979647416062; 0.007403764935902124 0.0075806541742707454 -0.04353370927134804; 0.0037366254302416482 0.004434767353244415 -0.026036645761490704; 0.002399372665928253 0.0027662096273043434 -0.017815547620593643; 0.0036622840441793304 0.004171571142117961 -0.027534989516696556; 0.0007850073779724527 -2.6514481003567757e-5 -0.001877336894546507; 2.3294804761511538e-5 0.0006040420244426976 -0.0016039531792640099; -0.00019754228291401555 0.00170108455516704 -0.002674402403683075; 0.00044787292305905084 -0.00017429258453013148 -0.0013686630908751266; 0.0009262890323889184 0.002003806708793155 -0.005445082267835653; 0.0014194449331209583 0.0024223603230135314 -0.0020851551749747053; 0.0011899942906017308 0.0036111969324898576 -0.004355445304108827; -0.0018096381255336348 0.004030752348717772 -0.0012137865422728867; 0.0020447284790555847 -0.0021607040208146714 0.0005997831352774702] %
+
+Mass Used: 81.42181100489734 kg
+Launch C3: 98.47403461739383 km²/s²
+||V∞_in||: 1.520490258340037e-5 km/s
diff --git a/archive/ES_0.5621789012480074 b/archive/ES_0.5621789012480074
new file mode 100644
index 0000000..e999fb7
--- /dev/null
+++ b/archive/ES_0.5621789012480074
@@ -0,0 +1,22 @@
+archive/ES_0.5621789012480074---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:45:07.644
+Launch V∞: [6.67033801200765, -7.352581747435072, 0.14133805789919912] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.4002572816722315e-6, 5.167912839708006e-6, 6.869997546591406e-6] km/s
+ V∞_out: [9.372050752345163e-6, 5.196311403713066e-6, 1.403554554889537e-7] km/s
+ time of flight: 1.874957778749373e8 seconds
+ arrival date: 2029-04-09T13:54:44.644
+ thrust profile: [0.17641949018431505 -0.04396002268136869 -0.06543262457344405; 0.05118324352632382 0.016031835758605444 -0.06220067756511986; 0.05085139880838797 0.026031601905529504 -0.09973299322562805; 0.051814538773856104 0.0370134064319888 -0.1393154510572641; 0.03935690014699966 0.032739743580768414 -0.13447880611247645; 0.024418958189322007 0.023390034767082447 -0.1033109591862942; 0.01439194809305464 0.014262365297371054 -0.07133926684240995; 0.01831250560417183 0.022121500747823285 -0.10651437154241146; 0.0033788755650108037 0.0051334742024598395 -0.027599953064060816; 0.0027780940194771387 0.005458744872791966 -0.026375105957041112; 0.0019997828926276496 0.0037457768648499223 -0.017307915282331218; 0.002500758729369517 0.0024533087013141053 -0.013469087920914549; -0.0006510513037932984 -0.0010823801325863932 -0.0022175178980292885; 0.0010426155080166324 0.0006772561392835941 -0.0006583731985272592; -2.078358195406547e-5 0.001050774574848724 -0.001491160937091191; 0.0003223002001181797 -1.4412105978169054e-5 -0.0014767952195210293; 0.0008031145535536406 -0.00164365359746038 -0.00027280689704618907; -0.00011693453047254216 0.0005707138902722285 -0.0006841143282331853; -9.883468085847286e-5 0.0013785260733389791 -0.002966305270370828; 0.0013577819044982157 0.0014064258995521329 -0.0008090557741694454] %
+
+Mass Used: 80.86129482574052 kg
+Launch C3: 98.57384399376025 km²/s²
+||V∞_in||: 1.0717624861908035e-5 km/s
diff --git a/archive/ES_0.5621836274396784 b/archive/ES_0.5621836274396784
new file mode 100644
index 0000000..bfe9927
--- /dev/null
+++ b/archive/ES_0.5621836274396784
@@ -0,0 +1,22 @@
+archive/ES_0.5621836274396784---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T20:11:58.102
+Launch V∞: [7.642371409275381, -5.653123963780846, 0.15215768593223092] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.009217091227285e-7, -2.067303438956088e-6, -5.901433320523065e-6] km/s
+ V∞_out: [-5.722483726424796e-6, -6.50723172047758e-7, 2.502592957136469e-6] km/s
+ time of flight: 1.8436873442089102e8 seconds
+ arrival date: 2030-03-14T17:44:12.102
+ thrust profile: [0.8480646199259583 -0.017935637722188143 -0.23626946255462963; 0.10633801827021777 0.05932174316596332 -0.11310041487542194; 0.03411548370662655 0.030922987047521985 -0.06628653966049532; 0.06404210478632918 0.07865084185231479 -0.18275664689351465; 0.01590771607070606 0.023397843008961267 -0.0621432382554176; 0.016536352405999787 0.029030097165657798 -0.0827887720711965; 0.011273420221337158 0.022824940316356745 -0.07012212463794529; 0.006212289846665258 0.01381913606741642 -0.0455291092801924; 0.002014764651713386 0.003911038352748912 -0.0144529179635735; 0.0011507398546519677 0.0034756871684449367 -0.011894463315052744; 0.0009302210379270994 0.00254419612130933 -0.010816468574757392; 0.0021897973194792003 0.004770695693893536 -0.019180200725088834; 0.006818412995796506 0.006062347757566434 0.0012512649428418135; 0.0026422012449780216 0.0016408605271209511 -0.004758747553012392; -0.0005174621409571296 0.0019471310799403891 -0.0038631151332670665; -0.0020500988239339837 -0.003784267493761465 -0.005117353803863583; 0.0025108702627513347 -0.00018369896580403174 -0.000497906959102525; 0.006771787864182035 0.0035143121205819658 -0.0007807029775677284; 0.0026285240781055846 -0.0016372213861732383 -0.01408978229655067; 0.01361449039015043 0.01621617986003561 -0.015532239612630862] %
+
+Mass Used: 128.62454627962552 kg
+Launch C3: 90.3868032685713 km²/s²
+||V∞_in||: 6.28186004665772e-6 km/s
diff --git a/archive/ES_0.5621876642154491 b/archive/ES_0.5621876642154491
new file mode 100644
index 0000000..5f4ebad
--- /dev/null
+++ b/archive/ES_0.5621876642154491
@@ -0,0 +1,22 @@
+archive/ES_0.5621876642154491---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T15:15:04.150
+Launch V∞: [6.505919341293855, -7.413879388140834, -0.15420571078115836] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0031877867779412893, 0.004748933560923485, 0.0038235970675428825] km/s
+ V∞_out: [-0.004443243968636316, -0.002223348750278229, 0.004756260115425317] km/s
+ time of flight: 1.8749577787605017e8 seconds
+ arrival date: 2029-04-09T17:24:41.150
+ thrust profile: [0.20084412502607094 -0.051125991240113904 -0.07274292386599059; 0.15987778353307194 0.0434814102261427 -0.16974203196827695; 0.03978577392519458 0.02121680115113816 -0.07523746143963189; 0.06934587713424824 0.04919177825957796 -0.17769019687053283; 0.044629463226115614 0.03825751158351167 -0.14913816024367482; 0.01920811433621197 0.01895759674421901 -0.0810222513015444; 0.011825590167718577 0.01266099185793607 -0.058894453161194314; 0.009098046563847403 0.011266877194157157 -0.0531249074051566; 0.0029207066990144296 0.003722040520918679 -0.01922763236963956; 0.0032976640326651263 0.004770700827808163 -0.02615557159051184; 0.0007730077115007138 0.002068097168129935 -0.011348010361410856; 0.0014488226002711713 0.0014417414789232317 -0.002824298240056257; 0.00023819089229583802 0.00043098367097283027 -0.0028110595629513486; 0.000640048026397715 0.0004794429091609044 -0.0022301996474716835; 0.0005259911139052854 0.0014105799363695283 -0.0020464967596747485; -0.00020838334534163997 0.0005389959416603641 -0.0013850691371708138; 9.316950955097524e-5 0.0002816145033495395 -0.0010759149893496836; -0.0010520424039638767 -0.00032572176519908916 0.0005812726154186124; 0.00016214759661784635 -0.00035165748426200084 -0.003258881173505275; -0.00040879155767499357 -0.0009683092774157953 0.0006103520326391494] %
+
+Mass Used: 88.20676307643271 kg
+Launch C3: 97.31637345855849 km²/s²
+||V∞_in||: 0.006879989029250355 km/s
diff --git a/archive/ES_0.5621989816643226 b/archive/ES_0.5621989816643226
new file mode 100644
index 0000000..f21537b
--- /dev/null
+++ b/archive/ES_0.5621989816643226
@@ -0,0 +1,22 @@
+archive/ES_0.5621989816643226---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T07:17:12.747
+Launch V∞: [6.687494775745216, -7.294089074810475, 0.019126854878210073] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.6129613683961654e-8, -5.101635911421105e-8, -4.1713186329702775e-8] km/s
+ V∞_out: [7.3789354185512e-9, -4.071624193723899e-8, 5.703530748215417e-8] km/s
+ time of flight: 1.8749577783328566e8 seconds
+ arrival date: 2029-04-08T09:26:49.747
+ thrust profile: [0.22582244201248858 -0.05526615994875543 -0.07817046906932047; 0.06855006834270154 0.020656905224968356 -0.07229965361234594; 0.03887650796559524 0.02236411171722171 -0.07005331231752769; 0.03532178268794275 0.027305692690194706 -0.08882328553111377; 0.025297810985686817 0.023837843565412395 -0.08236094660281315; 0.0491735708953156 0.06716104521332827 -0.2127694819211813; 0.019664522783905226 0.024134635189577217 -0.0920867674319831; 0.010057377077448394 0.014314230619386088 -0.057617275946609176; 0.017544334473247186 0.02569042203557086 -0.1066545230742764; 0.0019539889174100215 0.0034173819208276135 -0.01500467979890083; 6.442698976082282e-5 0.00011179542492879484 -0.0005050308682284835; 0.0001101359870611409 0.00020716866701098814 -0.0008049135592140957; 1.5190792465668989e-5 4.1789892509894857e-5 -0.00017896326839158874; -2.2633819539221695e-5 1.2160126708256157e-5 -8.172668630405185e-5; 0.0001196871949354795 -4.101279973967388e-5 -0.00014970367416588634; -0.00014329852453907795 3.040353637197372e-5 3.381546591362558e-6; -4.0175384783492504e-6 -2.4096932240609694e-5 -0.00021821038097788266; 8.600001078981663e-6 -6.579421553295329e-7 -2.970739824568325e-5; -4.038543288425409e-5 4.8047708692963644e-5 -2.8835317501567332e-5; 6.541255333878296e-5 -0.0001217183565216518 2.378086678916006e-5] %
+
+Mass Used: 84.65980068815452 kg
+Launch C3: 97.92668764346661 km²/s²
+||V∞_in||: 7.51532287796004e-8 km/s
diff --git a/archive/ES_0.5621999361788751 b/archive/ES_0.5621999361788751
new file mode 100644
index 0000000..87e0dcc
--- /dev/null
+++ b/archive/ES_0.5621999361788751
@@ -0,0 +1,22 @@
+archive/ES_0.5621999361788751---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T03:00:31.466
+Launch V∞: [7.9810862643794165, -5.679198218793455, 0.015334804114998662] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7300292641695035e-5, 0.003185096791246241, 2.290535837794814e-5] km/s
+ V∞_out: [0.003072114572640157, -0.0004784280262613906, 0.0006675696849781893] km/s
+ time of flight: 1.874957778773729e8 seconds
+ arrival date: 2030-04-23T05:10:08.466
+ thrust profile: [0.35722343099609744 -5.090760576421146e-6 -0.11468589581524141; 0.10580185470677154 0.06406864010936511 -0.11856383385755555; 0.051569375182156776 0.04970216473910822 -0.10634689422896164; 0.032217766886593634 0.041358592488564626 -0.1001989027267178; 0.017485873710876038 0.027815720316831088 -0.07577781297513153; 0.013113669430241871 0.02477537270129425 -0.07349187592618388; 0.00787061476067215 0.01726723095598531 -0.055083049617793624; 0.006019620203957197 0.015181345810906965 -0.051332998582915366; 0.006287956123824226 0.018839228369065708 -0.06841837385943107; 0.004135955768545283 0.013776257195262709 -0.050363993931561546; -0.0025449076540621637 0.00032839599547616286 -0.0028290697575713746; -0.008208918505518466 0.0052086645751285715 -0.005203268646653278; 0.0003010319885305746 0.001975427569729876 -0.009384260218270145; 0.0041660312780868874 0.0015678736840768588 0.002700700289467863; 0.003197118345493679 -0.004092137408749672 -0.007497123731704707; 0.01172820152544354 -0.010167355117312149 0.003569808963094624; 0.0012203259385054862 0.0022126967775497157 -0.0006477691578248542; -0.013112828222212939 0.004720644910759103 -0.003701680290366254; 0.002581297987967765 -0.017243387015513263 0.014598561634251845; -0.0043837791787821895 -0.004402919921491979 -0.006553177726544611] %
+
+Mass Used: 96.18420998518059 kg
+Launch C3: 95.95126552402978 km²/s²
+||V∞_in||: 0.003185296144949139 km/s
diff --git a/archive/ES_0.5622013641040398 b/archive/ES_0.5622013641040398
new file mode 100644
index 0000000..2e489fe
--- /dev/null
+++ b/archive/ES_0.5622013641040398
@@ -0,0 +1,22 @@
+archive/ES_0.5622013641040398---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:14:47.389
+Launch V∞: [6.562610369418099, -7.444368368172067, 0.09398444724523916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.214404304957159e-10, -9.658418898793578e-10, -5.656803724424334e-10] km/s
+ V∞_out: [-6.55275636103909e-11, 9.674849778324651e-10, 2.1507264262562792e-10] km/s
+ time of flight: 1.8749577787478212e8 seconds
+ arrival date: 2029-04-10T12:24:24.389
+ thrust profile: [0.12377922363154864 -0.032383870931775645 -0.04790950384788915; 0.14628785056986704 0.03542495371838253 -0.16593654065189883; 0.0513809139882008 0.02479252465873853 -0.10042945310462716; 0.0440751283847656 0.028356808193934314 -0.1206466012934645; 0.041180149122868236 0.03159416274809722 -0.14443338860406474; 0.030369931399609112 0.026780444320551804 -0.13120263206213265; 0.014956470330282896 0.01463840076292781 -0.07635146854936924; 0.007054477244827423 0.007600239860137335 -0.042380335609298436; 0.0030058867712617785 0.003592235924145171 -0.020892214523183676; 0.0015844165040017684 0.0022745926847834853 -0.012160653585486321; 0.0016096800579447164 0.001863923807842448 -0.012636944207957999; -0.00025013660562925403 0.0003392445064125391 -0.0018420918954576138; -0.00019801961148978103 -0.0001281461584297564 0.00021550427214784965; -0.0014458672974007713 -0.0013749322191229218 -0.0003653555689973305; -0.00439539344934159 -0.00025957922640946227 -0.0008549698311494482; 0.0016957160105797642 -0.0004658288630300988 -0.0018139279055234166; -0.0007129493741046121 -0.0008055222471357881 0.0005319492497741595; -6.538108885069524e-6 0.00012333832816985044 -0.0006566509471394448; -0.0031134696259563117 -0.003578138527597194 0.0016340161719258575; -0.0009283735481006149 -0.0005647186479285505 0.003214291292328631] %
+
+Mass Used: 81.34562614878678 kg
+Launch C3: 98.4953083381588 km²/s²
+||V∞_in||: 1.234805637567264e-9 km/s
diff --git a/archive/ES_0.5622014702185865 b/archive/ES_0.5622014702185865
new file mode 100644
index 0000000..1c5e451
--- /dev/null
+++ b/archive/ES_0.5622014702185865
@@ -0,0 +1,22 @@
+archive/ES_0.5622014702185865---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T18:47:50.637
+Launch V∞: [7.515823245840825, -6.119750502566801, 0.05800904308380548] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.234691336289128e-6, -3.809778630945489e-6, 2.7322434439745627e-6] km/s
+ V∞_out: [-8.300602238869477e-7, -6.253963823363943e-6, 2.9501517001917366e-7] km/s
+ time of flight: 1.7521626390193713e8 seconds
+ arrival date: 2029-11-26T17:58:53.637
+ thrust profile: [0.3767000334838696 -0.006385929378993775 -0.08988361179655306; 0.17126635141100008 0.10376404552036693 -0.13442869679314454; 0.10916214921251703 0.11273352641836308 -0.15197565643358496; 0.07474567716566345 0.10570840136231797 -0.1495131867780317; 0.06849429035072638 0.12250039747994809 -0.1829547023042253; 0.014149472730453375 0.03310398908159759 -0.057649536747715474; 0.010741340827349432 0.028959135007640184 -0.054957864838903456; 0.018501956071987274 0.05777259493667105 -0.10753290686891953; 0.0009858854183594976 0.004880007342079204 -0.009983539168487965; 8.686973381506977e-5 0.0004138765860614106 -0.000910368841351285; 0.00024230701965018356 0.0011872260116001382 -0.0026244799058751213; -7.45153804962886e-5 0.00023908305832105693 -0.0001729058487540044; 8.599427175894386e-6 0.00015231133685531873 -0.00021648931445472533; -3.9140665334376956e-5 0.00020996430056692563 -0.00021485440136521412; 7.890597375530422e-5 -9.378158524284618e-6 -0.00011410298850376288; -2.1549997003330527e-5 7.039417670661239e-6 -0.00018614142802228983; 8.24979546353732e-6 7.110610369705548e-5 -0.00016828772280580266; -1.424459450014232e-5 -9.181287688921091e-5 -2.2073022960969772e-5; 3.324136944153764e-5 6.0817483165726027e-5 -0.00016559427550375861; -2.993341107973318e-6 9.600208390336796e-6 8.166645025608354e-5] %
+
+Mass Used: 107.90490502312423 kg
+Launch C3: 93.94231032546743 km²/s²
+||V∞_in||: 6.317608579802413e-6 km/s
diff --git a/archive/ES_0.5622088672056055 b/archive/ES_0.5622088672056055
new file mode 100644
index 0000000..e319eba
--- /dev/null
+++ b/archive/ES_0.5622088672056055
@@ -0,0 +1,22 @@
+archive/ES_0.5622088672056055---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T15:42:15.367
+Launch V∞: [6.343692891581164, -7.469783036421764, 0.09930398124660511] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1910887879760327e-5, -3.5220219506587533e-6, 6.435338072928257e-8] km/s
+ V∞_out: [4.1608511758618584e-6, -9.873962450942092e-8, -2.1796358850648764e-5] km/s
+ time of flight: 1.8278777651348346e8 seconds
+ arrival date: 2029-02-12T06:05:11.367
+ thrust profile: [0.32529202871496726 -0.09358205077509463 -0.10939685614580956; 0.04041329557492245 0.010105916442500005 -0.0437212642006592; 0.12029192413658828 0.06140618591282755 -0.20044906372377186; 0.10615396891348458 0.07150368536045322 -0.24252640504278106; 0.036794450248647165 0.030798821164888447 -0.1144260037338201; 0.02696828861210188 0.02609825876076939 -0.10283306682100968; 0.007779770523226929 0.00828462960426185 -0.03703111143095948; 0.007312771724141894 0.008569453803173376 -0.038665609585696585; 0.0017346158592469736 0.0021809713422045705 -0.010329629559258178; 0.0007948834613541011 0.0010594462940550994 -0.006523811661724195; 0.005773945279223557 0.005899828925845782 -0.03425890157211409; 0.0006488055845983946 0.0006449986760106442 -0.0031016562920027414; -0.0002111814314040239 -0.0005246046472037295 -0.0002671267846778095; -0.0012912988520048453 0.0009950804337152549 -0.0037311962697965492; -0.00058079541511327 0.00030424238072012907 -0.0007660956983467661; -0.0007920434207852215 0.0010037638893169532 -0.0009357426810125621; -0.0006949618430006931 0.0001463751498565432 0.0008284365166400558; -0.000138977987363754 -0.0012150581362232902 0.00166024530049575; -0.0007675861426451429 0.0016202352848632689 -0.0002241761328225045; 0.00031700340642649966 0.00023055991167846436 -0.0009722941983724999] %
+
+Mass Used: 95.61891527135458 kg
+Launch C3: 96.04995939460316 km²/s²
+||V∞_in||: 2.2192246115658534e-5 km/s
diff --git a/archive/ES_0.5622099699768393 b/archive/ES_0.5622099699768393
new file mode 100644
index 0000000..6cd9d15
--- /dev/null
+++ b/archive/ES_0.5622099699768393
@@ -0,0 +1,22 @@
+archive/ES_0.5622099699768393---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:31:32.903
+Launch V∞: [8.076553821266158, -5.587532847833045, 0.1619943767993141] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.928889676641374e-9, -5.3566236723786246e-8, 1.3117788592045129e-6] km/s
+ V∞_out: [5.666734581676793e-8, -1.3060119900155468e-6, 1.696319455494926e-8] km/s
+ time of flight: 1.8558968004826343e8 seconds
+ arrival date: 2030-03-30T04:12:52.903
+ thrust profile: [0.3440091609148836 -0.006796193688472508 -0.0948809688913159; 0.07147718481730962 0.042629530642501065 -0.08036166664632376; 0.05619373870768134 0.05494843022522893 -0.11550684673351762; 0.034113503788361046 0.044553334536510315 -0.10480453693767648; 0.020095424334504525 0.029185309710050348 -0.07678474573626486; 0.017463705327594368 0.031292314751961765 -0.08638401129837801; 0.012495959238563609 0.029140016569136302 -0.08292916315567637; 0.005702474222079066 0.015034973280950275 -0.05042648426759965; 0.0028728238790510854 0.007765701611195288 -0.02670082251184217; 0.004426982643330273 0.009560372498558978 -0.03369166296472168; 0.0017653322552027857 0.0052750901080693725 -0.0084152121697525; 0.0033460284765003973 0.01797605376670172 -0.06496720957968355; 0.006713676738722447 0.00438454263314478 -0.0071185159505414795; 0.0004600696300740533 -0.00045773005869745374 0.00017263177234797976; 0.0007597610149214036 -0.005949416195479339 -0.006990287719782948; -0.001915816388760666 -0.00015579120248365968 0.009472668846231314; 0.001664797738606308 0.004871395522743633 -0.004303731888758601; -0.004092470557760738 0.009482214204185182 0.0007479966600298016; -0.002698671688325923 0.00878060685857834 -0.009027903047280681; -0.003992811464384002 0.005336287605226895 -0.00462984854274332] %
+
+Mass Used: 93.1262900390143 kg
+Launch C3: 96.47748713153683 km²/s²
+||V∞_in||: 1.3129024496296363e-6 km/s
diff --git a/archive/ES_0.562213320034954 b/archive/ES_0.562213320034954
new file mode 100644
index 0000000..dff0da7
--- /dev/null
+++ b/archive/ES_0.562213320034954
@@ -0,0 +1,22 @@
+archive/ES_0.562213320034954---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T07:47:21.915
+Launch V∞: [6.643676600452952, -7.45704474939463, 0.07175917488542985] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.148544692455484e-8, 7.9548097110352e-8, 4.521263847149818e-8] km/s
+ V∞_out: [-2.8440931898729493e-8, 5.3987917663610004e-8, -8.000036059129506e-8] km/s
+ time of flight: 1.8749577787493798e8 seconds
+ arrival date: 2029-04-11T09:56:58.915
+ thrust profile: [0.09690198715556751 -0.02677510227905619 -0.03930045348364149; 0.045119026248167354 0.009399752284342752 -0.055657243263405404; 0.04813627471517229 0.020168180277873444 -0.09928514750328497; 0.04478589722810978 0.024890991622567724 -0.12878834770886424; 0.03946576253711902 0.025785511507557448 -0.14430126346797223; 0.0269875648167983 0.019648052804191567 -0.11967930230645607; 0.022072422165637196 0.017468136210316548 -0.11425440184220732; 0.014332103100273446 0.012020843282821735 -0.08502735162985653; 0.005776559421698036 0.005169177807335604 -0.04034112869922414; -0.00027700815456282817 0.000786572518042783 -0.00405303426807914; 0.0017390239718144455 0.0017918733896451293 -0.014314890492371004; 0.0008064385858354629 0.00026663868118260314 -0.0010144397535417008; 0.0010109928777209233 0.00025605732352863614 -0.0012454348895992048; 4.985218002159862e-5 -0.0001167347139728425 0.0008649226174466682; -0.0011341636337767976 0.00028768158323780844 0.0009845442324340464; 0.0010696252003387597 -0.0003835904584437223 0.0005703204936121976; -0.0033896126386594424 -0.00023152816631347595 -0.0022019993535902314; -0.00012189078044082759 0.0010974446842501855 -0.0014483287565695358; -0.00036535435895757213 -0.001986644848269911 -0.0024195582148905334; -0.0017185589551667777 -0.004048458134395428 -0.0008187656014241437] %
+
+Mass Used: 74.03409686126088 kg
+Launch C3: 99.75110454506036 km²/s²
+||V∞_in||: 1.0046454468100895e-7 km/s
diff --git a/archive/ES_0.5622166122795875 b/archive/ES_0.5622166122795875
new file mode 100644
index 0000000..550cb8c
--- /dev/null
+++ b/archive/ES_0.5622166122795875
@@ -0,0 +1,22 @@
+archive/ES_0.5622166122795875---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T13:23:59.294
+Launch V∞: [6.549249787297278, -7.485120909516327, 0.1305921382081413] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.505908311133402e-7, -5.271405459444064e-7, -5.54521994998837e-7] km/s
+ V∞_out: [-7.941354633276012e-7, -5.325460250853723e-7, -1.5504326770792457e-8] km/s
+ time of flight: 1.87495777874478e8 seconds
+ arrival date: 2029-04-11T15:33:36.294
+ thrust profile: [0.15443298720804097 -0.04229136438493074 -0.06143220086786002; 0.07113155274868072 0.014964884379603898 -0.08651400257318327; 0.0401490860214968 0.01678296453833175 -0.0830719886337348; 0.051229381856096795 0.02852934056808391 -0.1464764310468734; 0.03907957179591467 0.02555954475609404 -0.1428361190333349; 0.03297054364479861 0.02407992434775969 -0.1452783394376255; 0.0121018577926497 0.009405930512760131 -0.06324311548798651; 0.004357579936016821 0.0035513519888588007 -0.02591730599302248; 0.004555357392386507 0.0042267838534970695 -0.03218578236779119; 0.009377267017193892 0.007865612852793675 -0.06373975859389763; 0.0014853154577412842 0.0012793789959968749 -0.012811474154479256; 0.0004666635614262986 0.00019836082846959687 -0.004568575014300312; 0.0001683537835331593 0.00016295134752598053 -0.001432466879592793; 0.00014336589221285162 0.00029125617505060936 -0.0016423457195695475; -0.0007048585694104007 -0.00021648816957637592 -0.002955551414918734; -0.00020755971183897823 0.0009942520546137139 -0.0008950794976906029; -0.0007517681933162169 -0.001629571524932889 -0.000731804289985981; -2.9031257025675754e-5 -0.00020688543945444416 -0.00024983469750164; -0.0012338893376509484 -0.0003654622715993839 -0.00015515034785445027; -4.393241312827291e-5 -9.425479953353443e-5 0.00011061606374687498] %
+
+Mass Used: 78.78826866670533 kg
+Launch C3: 98.93676211305375 km²/s²
+||V∞_in||: 9.426144818652722e-7 km/s
diff --git a/archive/ES_0.5622192272754252 b/archive/ES_0.5622192272754252
new file mode 100644
index 0000000..df2d835
--- /dev/null
+++ b/archive/ES_0.5622192272754252
@@ -0,0 +1,22 @@
+archive/ES_0.5622192272754252---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:09:27.195
+Launch V∞: [7.764685789899159, -5.6354669145662655, 0.07211906361451344] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.432469362049022e-6, -2.4922130328339873e-5, -6.831763191247199e-5] km/s
+ V∞_out: [-6.576902318851559e-5, -7.784282534429136e-6, 3.091013383403984e-5] km/s
+ time of flight: 1.8485055975837886e8 seconds
+ arrival date: 2030-03-18T06:32:06.195
+ thrust profile: [0.5751002356646254 0.009357435129600647 -0.13615895052863294; 0.22796021243432105 0.15112403060702598 -0.18835233531003823; 0.09524537116027891 0.10674282650633667 -0.15012271296407018; 0.041080825268733516 0.06450381941782538 -0.10280790135885125; 0.031115751418923858 0.06378241089197621 -0.10959736933130437; 0.01736213723635764 0.0447772543115858 -0.08336307218775865; 0.0048904082054373335 0.01599317391127446 -0.03265242307015328; 0.0053825083789375465 0.021384370286956857 -0.04537721745790806; 0.00059257652424473 0.002523556231905572 -0.005468326754721298; 0.0010087025333605907 0.006839455729132452 -0.01635182539353984; 0.0005346364029642314 0.0037056062890499005 -0.00958153090882838; -0.00019138722325382212 0.0006806414412337285 -0.0006157668540661394; 1.8523915294290384e-5 -0.00016921143285751915 -3.711297616210813e-5; 0.00036320732926425724 -5.1852548358910516e-5 -0.00023556510672177573; -9.871715267955065e-5 0.0012137924539163372 -0.00041586665936855735; -0.0004957375495996657 -0.0003476299389426926 -0.0010163713966959524; 0.0012395180143245652 -0.001036558741466229 -0.0013058570978254067; -6.710230076547337e-5 -0.00035378379859315947 -0.0014139700953092913; 0.00040790092776218814 -0.0005885446239212782 -0.00010661400908804258; 0.0007370396687020988 -0.00025661475132035565 -0.0005751988370728627] %
+
+Mass Used: 118.94056728584019 kg
+Launch C3: 92.05403392036958 km²/s²
+||V∞_in||: 7.310029419262665e-5 km/s
diff --git a/archive/ES_0.5622200841033569 b/archive/ES_0.5622200841033569
new file mode 100644
index 0000000..ae734c3
--- /dev/null
+++ b/archive/ES_0.5622200841033569
@@ -0,0 +1,22 @@
+archive/ES_0.5622200841033569---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T05:46:41.605
+Launch V∞: [6.611431715867652, -7.400491219640692, 0.061429011042091246] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.2485050988682736e-8, -5.573980846881966e-8, -3.1756227833310265e-8] km/s
+ V∞_out: [2.002195847106908e-8, -4.126849759852372e-8, 6.244255595899809e-8] km/s
+ time of flight: 1.874957778728606e8 seconds
+ arrival date: 2029-04-10T07:56:18.605
+ thrust profile: [0.15750668147938088 -0.04316529072292357 -0.059596126463882994; 0.10683411052827774 0.026724967991195697 -0.12184100330658033; 0.04475091214714592 0.020568027374296815 -0.0889982620415618; 0.035168548193674105 0.02151423334820037 -0.09757979583776802; 0.03795498981991643 0.026846098838507335 -0.13576952899122818; 0.029508422461564758 0.02452522040601386 -0.1282271105562053; 0.01882054005003157 0.01634468121142072 -0.0972215894954363; 0.014709652141519565 0.014208326027451187 -0.08328511836724228; 0.007905295637579593 0.008210929172985507 -0.050763405236315236; 0.0011738657102275366 0.0015197245243501053 -0.008183533567069285; 0.00038014072550110744 -0.0002473851553826959 -0.0008894222908882644; 0.0007336150073081531 -0.0002761384794568057 -0.0030634782472365174; 8.627248624733827e-5 -2.8285341036213447e-5 -0.00037579935543627786; 0.00021050668207135123 -0.0010679131900952685 2.4777854452251273e-5; -0.0002854848574763433 -0.0008693807115906082 -0.001591681156992071; 0.0006543458407903233 -0.0003347832134743593 0.003600937778805033; 5.854772560340933e-5 0.00012049434352917772 0.0015167370205703059; 0.0005825461176490263 -0.00017278558361782345 0.0019325364154206687; 0.00011304903365038847 2.8289784642697847e-5 -0.0021405172103992403; -0.00016927938740393618 -0.001957110414061861 -0.003942828535572883] %
+
+Mass Used: 81.44467141833229 kg
+Launch C3: 98.48207314895727 km²/s²
+||V∞_in||: 8.288585423114391e-8 km/s
diff --git a/archive/ES_0.5622270647395825 b/archive/ES_0.5622270647395825
new file mode 100644
index 0000000..028f6f9
--- /dev/null
+++ b/archive/ES_0.5622270647395825
@@ -0,0 +1,22 @@
+archive/ES_0.5622270647395825---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:58:09.214
+Launch V∞: [6.546024690369152, -7.406444049414389, 0.12008035789280203] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.1977862917119936e-9, -2.0115000698114984e-9, 2.696796362253231e-9] km/s
+ V∞_out: [1.2765598532943853e-9, -2.9031322485036315e-9, -4.021699251211476e-9] km/s
+ time of flight: 1.8749577787455752e8 seconds
+ arrival date: 2029-04-09T07:07:46.214
+ thrust profile: [0.2081703219567575 -0.047138008047299035 -0.06804142875864867; 0.044549731846839635 0.01394869152034797 -0.04467861587723846; 0.039471226095908 0.023310034787472643 -0.06573924822553866; 0.1098478893980093 0.08856219939281447 -0.2412693635916923; 0.06150053701493627 0.05997959087504731 -0.1797635630084871; 0.04713260416803531 0.05193719901295959 -0.16670326800707505; 0.005470676755285334 0.007399275609261983 -0.02632730039155516; 0.001864958466851823 0.0035421843225095957 -0.01412315702851427; 0.0027972050211642297 0.004526099109664055 -0.021780832226524202; 0.0008638417358871791 0.0013640140944517257 -0.010636211342241911; 0.0013108293358787921 0.002064766100841612 -0.007855922223179063; -8.932541865832113e-5 -0.0010692881178022613 -0.0014815272565704206; 0.0038082485280275117 0.0017470190709779954 -0.002338783242423142; 0.0042346642938791545 0.0002706436737085527 -0.0004383676049772835; 0.0004118123481103421 0.0020812354447710337 -0.0006546470454004065; -0.007055376404566896 0.0017096997122143774 -0.00857681160442875; 0.00042558036810009983 0.0006977658657052045 0.0007427623869421046; -0.0009504058004275238 -0.0001256825682497647 -0.0004518272474456947; 0.0014134741971979755 0.0007763499619919602 -0.0006752975264294634; 0.0009895822108414692 -0.007687569235852137 0.0061634987380402] %
+
+Mass Used: 85.89665555062948 kg
+Launch C3: 97.72027199638002 km²/s²
+||V∞_in||: 4.641624749780519e-9 km/s
diff --git a/archive/ES_0.5622283337812997 b/archive/ES_0.5622283337812997
new file mode 100644
index 0000000..dcc42d5
--- /dev/null
+++ b/archive/ES_0.5622283337812997
@@ -0,0 +1,22 @@
+archive/ES_0.5622283337812997---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T15:11:40.231
+Launch V∞: [7.626145049744823, -5.487431905943606, 0.29633480052454003] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.030753370061080934, -0.1532991185853625, -0.2245906998783007] km/s
+ V∞_out: [0.11224398627450695, -0.09450042256464507, 0.23146256470756693] km/s
+ time of flight: 1.8749577787217095e8 seconds
+ arrival date: 2030-04-17T17:21:17.231
+ thrust profile: [0.9868237299679943 0.02564246376214863 -0.20060992947027345; 0.16977519730043206 0.11838801172275157 -0.14876818414830512; 0.06890288233644312 0.0779967895335365 -0.11818884986799749; 0.040205212685804174 0.06459365848553078 -0.10811524885392648; 0.015603799100922962 0.03299641657070882 -0.06294923816917876; 0.01024942719752341 0.026206950309778102 -0.05347189541162603; 0.008288219114474428 0.026518909576664144 -0.05834001948323404; 0.008149035872659926 0.03475870366103559 -0.07669831601024761; 0.0013486140798851052 0.006721194359577342 -0.016364906971122112; 0.001011541272750351 0.005830229521772395 -0.015248217673943703; 0.00013921276662042832 0.001825285764795926 -0.004403307250120021; 7.550432613899103e-5 0.0007119668475347823 -0.0019938544783791217; 0.0004760447911281255 0.00045024145734300135 -0.0007972719241801129; -0.00023305091502451346 -9.439761310402444e-5 -0.0009655089926304493; 0.00016909414017682176 0.0004613033645461382 -0.0007288004046158416; -0.0005697903860490273 9.280677989680739e-5 -0.00014857366320355798; 4.687596188405244e-5 -0.00013027441959875873 0.0005580448965202033; -0.0002103525871742506 -0.0007244197105605124 -0.0003283896764891421; -0.0007072478024596338 -0.0006219953714769459 0.0006578293412651541; -4.789202808145911e-5 0.0006934532563447025 6.237122507209906e-5] %
+
+Mass Used: 140.51248866749893 kg
+Launch C3: 88.35781155611727 km²/s²
+||V∞_in||: 0.27365557184349043 km/s
diff --git a/archive/ES_0.5622347196530639 b/archive/ES_0.5622347196530639
new file mode 100644
index 0000000..675737d
--- /dev/null
+++ b/archive/ES_0.5622347196530639
@@ -0,0 +1,22 @@
+archive/ES_0.5622347196530639---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T03:53:15.828
+Launch V∞: [6.548612898901235, -7.475809243737139, -0.02690019259661844] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.013901312023843121, -0.0003738350668884477, 0.008298851969325857] km/s
+ V∞_out: [-0.014955593491185953, 0.0001655571847733391, 0.00620776518246155] km/s
+ time of flight: 1.874957778749397e8 seconds
+ arrival date: 2029-04-11T06:02:52.828
+ thrust profile: [0.14918099889588013 -0.038645997097558636 -0.06100117743806049; 0.08034748288124449 0.019331193296860432 -0.09722970461209475; 0.05842602669840537 0.027909610184613444 -0.12121597297409194; 0.04238955845425342 0.027047250879007313 -0.12359283240689582; 0.030482321897780246 0.021962788163435613 -0.10998020030185235; 0.02890583433064245 0.024828853887177284 -0.1289359809067686; 0.019317982896751473 0.018011523018950638 -0.1019469860780609; 0.013607304146509036 0.013432363084613356 -0.08125666517757917; 0.005288478356340468 0.0053250840859029955 -0.034584809181236624; 0.0005893342203303363 0.000522767513612877 -0.0037496053676087594; 0.000495433254950115 0.0003309710058689334 -0.004917058867658062; 0.0005420316234146644 4.5384570953082276e-5 -0.0019731071899701763; 0.00021210819636801326 -5.4555093820621054e-5 -0.0011244127156053226; 0.0009274840734920346 -0.00016703860619666643 -0.0010343205148789546; -0.0010729132292823127 -0.0008353407888809878 -0.0012310086807365143; -0.0012529044901309016 0.001378893784379562 0.000371710737172628; 0.00269891350672824 0.0016867786927268224 -0.0009310569979676636; -0.00017784858085030403 -0.0016132122002877934 -0.0014590273552496538; -0.0006653909722709509 -0.00029560184681650683 0.002436891804949353; 0.002145235431049126 0.002963209951542488 0.0020690098618699926] %
+
+Mass Used: 79.76596577745704 kg
+Launch C3: 98.77277836876301 km²/s²
+||V∞_in||: 0.016194356197461648 km/s
diff --git a/archive/ES_0.5622489776556764 b/archive/ES_0.5622489776556764
new file mode 100644
index 0000000..b6356ca
--- /dev/null
+++ b/archive/ES_0.5622489776556764
@@ -0,0 +1,22 @@
+archive/ES_0.5622489776556764---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T10:39:47.971
+Launch V∞: [7.847978755124142, -5.548431004180986, 0.08603213912273734] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2034942897567093e-5, -1.0105284657898351e-5, 7.72463270738545e-6] km/s
+ V∞_out: [-2.636831294514807e-6, -1.7287929163818185e-5, 8.626973251110622e-7] km/s
+ time of flight: 1.858523813037744e8 seconds
+ arrival date: 2030-03-30T12:19:28.971
+ thrust profile: [0.6133845339158507 0.00435163411858807 -0.1604257195222518; 0.1593368405888385 0.10094770571886877 -0.14973074103081335; 0.0786612793338949 0.08316241037190843 -0.1371088817182133; 0.06118208297745812 0.08857459947507783 -0.16127918732135202; 0.0304494194418572 0.05594958308095271 -0.11334518104514399; 0.017705658529555225 0.03999057650818682 -0.08796521397871473; 0.0025532338804265336 0.00712746537773392 -0.017625233487752547; 0.004758130383076823 0.015583856079502781 -0.03924197345968588; 0.00020457398019365318 0.001046656916678735 -0.0031670402204454348; -0.0021687394611965474 0.0004982290484592429 -0.0012507678062789187; -0.0004669333667042378 0.0021742545140891185 -4.3805601041790724e-5; -0.0006862811518506986 -0.0018856926900934889 -0.00023358248050402982; -0.0006601495258505283 -0.0014387194657215635 0.0010696934690190756; -0.000620825027553253 -0.0001977174857478633 0.00013643519596058702; -0.0001205521584169895 -0.0001098838315993977 -0.00013104772938324311; -0.0020134359806874254 -0.00021936382300029165 0.0005054194842247462; 0.005470784224343949 0.004980118131086762 0.0027051726472482255; 0.0037897057786545427 -0.004523669839925273 -0.001274647329094122; -0.00341409659675445 -0.004122735533781539 -0.006120330875184049; 0.006604938105869023 -0.001095256104031282 0.0030523842463678623] %
+
+Mass Used: 117.05479830996319 kg
+Launch C3: 92.38325867799874 km²/s²
+||V∞_in||: 1.75107560952937e-5 km/s
diff --git a/archive/ES_0.5622489999192305 b/archive/ES_0.5622489999192305
new file mode 100644
index 0000000..4658a78
--- /dev/null
+++ b/archive/ES_0.5622489999192305
@@ -0,0 +1,22 @@
+archive/ES_0.5622489999192305---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T22:28:52.190
+Launch V∞: [6.540300018038174, -7.407364155430874, 0.2080007591174217] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.790955926770734e-8, -1.0360406039663212e-7, -7.639392605058666e-8] km/s
+ V∞_out: [3.4931246071512526e-8, -7.439055710603501e-8, 1.151233984827213e-7] km/s
+ time of flight: 1.8749577787483445e8 seconds
+ arrival date: 2029-04-10T00:38:29.190
+ thrust profile: [0.23195625915726922 -0.054465437800656 -0.0828461151926307; 0.08045163474389222 0.02244976504488768 -0.09031830118082852; 0.04186888211100282 0.022199121407291085 -0.07891227312140724; 0.06078147260235293 0.0459986685876063 -0.16577677425102355; 0.029542586853374925 0.025852262455452805 -0.10247763247374171; 0.016666497386816085 0.01607948558334665 -0.06936043871248812; 0.02429011622871034 0.02814491216524972 -0.12285190653817794; 0.02068397527270235 0.024225068392470524 -0.1069484626856088; 0.005664405523215997 0.0071745040274879286 -0.036981804142040754; 0.0016189468079146295 0.0020365651370427332 -0.011457838208402892; 0.00228317440324054 0.0021181485230655 -0.003263901531952644; 0.0003468357995238217 0.00145746518895001 -0.007139596127061095; 0.00018860437617724418 0.00014357570480797962 -0.001712794151323022; 0.0012796380233201675 -0.0014804207955089951 -0.000587778591027118; 0.0004430800512351199 9.994327930574695e-5 0.00028966413235648625; -0.002107611485816389 0.003217061465442831 -0.00043861539660691566; 0.0021753235074737547 -0.0007441606547571162 -0.0017357599591038765; 0.0010644147931341856 0.00019620081059421588 -0.001549198694175633; -0.001367005807186311 0.00046959799165257547 -0.003426564111344525; 0.0018956582602041227 0.0005612956728067078 0.0014931870095999111] %
+
+Mass Used: 86.1114777304856 kg
+Launch C3: 97.6878323729057 km²/s²
+||V∞_in||: 1.4553879726047539e-7 km/s
diff --git a/archive/ES_0.5622546082295525 b/archive/ES_0.5622546082295525
new file mode 100644
index 0000000..0427240
--- /dev/null
+++ b/archive/ES_0.5622546082295525
@@ -0,0 +1,22 @@
+archive/ES_0.5622546082295525---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T00:34:19.236
+Launch V∞: [6.389115351476858, -7.46250477487278, 0.10527699656386107] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2942378557728335e-8, 2.1719426510959322e-8, 1.365329005485993e-8] km/s
+ V∞_out: [-8.586750392866994e-9, 2.1372311943362955e-8, -2.9024899672803823e-8] km/s
+ time of flight: 1.85815004252721e8 seconds
+ arrival date: 2029-03-21T15:51:03.236
+ thrust profile: [0.34273955782376103 -0.09386346677732724 -0.12430830694479701; 0.05297839883110502 0.012334712286109169 -0.062097092650411106; 0.05598647210614365 0.026098712270563523 -0.10812379203969667; 0.050704253316241364 0.03131204234268242 -0.13588422778561948; 0.04457082343134212 0.03340383413918048 -0.15259612723829344; 0.02828257120270015 0.024032640268208595 -0.11884199455879126; 0.012975497799411883 0.01186642760351387 -0.06525605080533968; 0.013109399688872496 0.013009628111680365 -0.07485662110132496; 0.004512046696634973 0.004734704094569054 -0.029092002213623853; 0.005092620683499088 0.00540381604256485 -0.03751156093000895; 0.0003832912759179872 0.0005194861934041807 -0.004705931831576985; 0.0003055121202181581 0.0009042511827334469 -0.0071585820691463485; -0.0001172833524518079 0.001328907588099088 0.00023503911203931753; 0.0015702167282367146 7.205964216208522e-5 0.0003836071282098208; 0.0001952933619126212 0.0005261669637348567 -0.0004009933152355338; 0.0005191004320487893 -0.0005812855536811517 0.0005377249662640714; -0.00031126110156949404 -0.0008023309948517122 -0.00034139514625356593; 0.0019937544728981143 0.0027555718103527064 0.00012229844542832472; 0.0017361408676964348 0.00030651075667462575 -0.0018958059380480392; 0.0003197313328545336 0.0005349518258343085 -0.0005084488839765636] %
+
+Mass Used: 92.92538447750076 kg
+Launch C3: 96.5208557354818 km²/s²
+||V∞_in||: 2.8734143105696504e-8 km/s
diff --git a/archive/ES_0.5622614263793988 b/archive/ES_0.5622614263793988
new file mode 100644
index 0000000..da0a52e
--- /dev/null
+++ b/archive/ES_0.5622614263793988
@@ -0,0 +1,22 @@
+archive/ES_0.5622614263793988---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:30:57.204
+Launch V∞: [6.444128302876954, -7.3600883915110815, 0.1307379550974187] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.018730145517641808, -0.008839452233519503, 0.0222227627161653] km/s
+ V∞_out: [-0.019408528834239176, -0.008350287951172637, -0.02182795164365419] km/s
+ time of flight: 1.8749577787475932e8 seconds
+ arrival date: 2029-04-09T13:40:34.204
+ thrust profile: [0.37465983134478753 -0.09918202625352252 -0.13808811538127688; 0.11154452716527846 0.02926366235939016 -0.12978979565879573; 0.04617843001867602 0.02152498202049195 -0.09140361421520632; 0.05854581257505777 0.03899433718032522 -0.16867025740789252; 0.044163712217052314 0.03429662873667663 -0.16169372910871052; 0.019314659868577548 0.01667235218009046 -0.08547663662925291; 0.010028953331269129 0.009551417860161854 -0.05304853825210166; 0.007214520079904602 0.007547444296284147 -0.044478380813141115; 0.002267338813962904 0.0022316660335397094 -0.015492735336855665; 0.001258126877951697 0.0012594620759813387 -0.008585064159035063; 0.003076249471996449 0.003687666423672229 -0.02566540761999945; 0.0008946548267130244 -0.0003026338795072596 -0.001154327861057917; 0.0008405676197728434 0.00235653133568761 -0.0016456390938711014; 0.00019013433542250358 -0.0030648551619407187 -0.0008562805544541325; -0.00010685995249799384 0.0003306017090965456 -0.0010483238895703413; -0.0031416738665265087 0.0008360610191362022 0.0005609195087243604; -0.0013531046931225064 -0.0013936732303023837 0.0014271104160929837; -0.0005959476947694445 0.0008308777715873336 0.0003669745804996817; -0.00039072603384032815 0.005041201260846629 -0.0018984332354599106; -0.0004010328061079615 -0.0013330023709763683 0.002461832851129023] %
+
+Mass Used: 97.6354291977209 kg
+Launch C3: 95.71478312769904 km²/s²
+||V∞_in||: 0.03037771304163131 km/s
diff --git a/archive/ES_0.5622648818554118 b/archive/ES_0.5622648818554118
new file mode 100644
index 0000000..495c9f8
--- /dev/null
+++ b/archive/ES_0.5622648818554118
@@ -0,0 +1,22 @@
+archive/ES_0.5622648818554118---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T12:49:37.255
+Launch V∞: [7.807735167666705, -5.947777036036812, -0.5219263278051456] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.266647286982746e-7, 1.3617904985048584e-6, 1.3370874648702237e-7] km/s
+ V∞_out: [-1.0700322170069465e-7, 5.385312340690557e-7, 1.5552444268090388e-6] km/s
+ time of flight: 1.8547114217331976e8 seconds
+ arrival date: 2030-04-01T04:35:19.255
+ thrust profile: [0.3151671258362242 0.0008679277398339673 -0.10817558066751597; 0.11026943214717747 0.06397549440075556 -0.12835937350751656; 0.06745879726766321 0.063812029285653 -0.14335099851437316; 0.04104147266718949 0.05155420183922348 -0.13233843838676887; 0.019800534483261356 0.030807281934328596 -0.08986281631174592; 0.012671114828512953 0.023596885108097473 -0.07515085162237983; 0.010433814348704799 0.0229712438362449 -0.07802979284012354; 0.00380785445519639 0.009582347667268336 -0.03535293824066734; 0.003433938797629914 0.00980752977507018 -0.038567805733606686; 0.0016319755743057604 0.0050169513553274215 -0.02192481555263233; 0.0010105212933372257 0.00027585265493865457 -0.00797484099951902; -0.0030271226582442735 -0.0007474542676869675 0.0007727853380492121; -0.0041005849152528 0.0009184926887749606 0.0012480954721671563; -0.0006377618991217157 -0.0009195856492940605 0.003441431895062688; 0.00043831385983426224 -0.002296887228011133 0.0058011609860206485; -0.002666357877915712 0.0038837376897523936 0.004548159696955694; 0.0035754788956606307 -0.0040337937688517365 0.00365966498236342; 0.0004890704445622235 -0.009316776634282983 -0.00039316777308998096; -0.000249778075553875 0.0001747849056709981 -0.0006121193220427006; 0.00018520626495954144 0.005905038350907406 -0.010363925152417224] %
+
+Mass Used: 92.42210343683291 kg
+Launch C3: 96.60918721048243 km²/s²
+||V∞_in||: 1.652591573898006e-6 km/s
diff --git a/archive/ES_0.5622673539985757 b/archive/ES_0.5622673539985757
new file mode 100644
index 0000000..1eb4961
--- /dev/null
+++ b/archive/ES_0.5622673539985757
@@ -0,0 +1,22 @@
+archive/ES_0.5622673539985757---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T10:06:40.377
+Launch V∞: [6.394134394501144, -7.4476975918775, 0.09428602022483273] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3831790983843572e-6, -1.807998887974924e-7, 3.943990588426774e-9] km/s
+ V∞_out: [2.5562107789762617e-7, -5.877366757196842e-9, -1.3685860949769844e-6] km/s
+ time of flight: 1.840790283620224e8 seconds
+ arrival date: 2029-02-27T23:10:28.377
+ thrust profile: [0.327082305301812 -0.0874797828523056 -0.11420284954458254; 0.07466033891953508 0.019123338132491764 -0.07993532423447806; 0.055429409209347295 0.028219183385495405 -0.09927360075795955; 0.04619935252609643 0.0318674979711287 -0.11552196529086982; 0.062062975362696476 0.05241898041130478 -0.19498596693757228; 0.02016644135450875 0.01950253744681581 -0.07962450563617253; 0.022421095248965704 0.024201221667217603 -0.1032687789010464; 0.018858124657028574 0.022173295445311818 -0.0987501424393513; 0.002205031521019446 0.0025893361140107043 -0.01224587974127256; 0.0018869094321531167 0.00272730118380443 -0.013068333295490921; 0.0013961225984769525 0.002529261375386157 -0.010509930444408438; 0.0003288798796914417 0.00015965633256101333 -0.002462510891920836; 0.0002577386553103226 0.0001317895244966655 -0.004403429546085841; 0.0004546662493695717 0.0006974763205557477 -0.003585971108773409; 0.0004184363563099606 0.00013876753282797644 -0.001663365623486882; 0.0006417610159079163 0.0003070577846806769 -0.0023398167505958227; -0.00022860454596421674 0.0011348727710295075 -0.003175018444233622; -0.001929695602411267 -0.0004294193540447086 -0.001017857497393232; -0.0001415837242405302 -3.7032380631072336e-5 -0.00023695696081228604; 1.2480370838297567e-5 -0.0009772106212917906 0.0016598198464913305] %
+
+Mass Used: 93.86665674811184 kg
+Launch C3: 96.36204392861026 km²/s²
+||V∞_in||: 1.394951100597548e-6 km/s
diff --git a/archive/ES_0.5622680192719244 b/archive/ES_0.5622680192719244
new file mode 100644
index 0000000..7ce0086
--- /dev/null
+++ b/archive/ES_0.5622680192719244
@@ -0,0 +1,22 @@
+archive/ES_0.5622680192719244---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T07:17:53.871
+Launch V∞: [8.09963515747349, -5.687299354705682, -0.0039934281304859235] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9587725638945074e-9, 1.3305094009653446e-9, -3.8773633993101813e-10] km/s
+ V∞_out: [2.9074320499351763e-9, -2.8505578565364303e-9, 1.0374426929493417e-9] km/s
+ time of flight: 1.8695602883879486e8 seconds
+ arrival date: 2030-04-18T03:31:41.871
+ thrust profile: [0.22198368216835 -0.012250069100957352 -0.08108763492402636; 0.074135023558355 0.03346278939560146 -0.0940145153471655; 0.07635615977282159 0.050728119805801275 -0.1684206801888125; 0.024292671390822685 0.02158727818662326 -0.079308956804983; 0.022998085036383613 0.023316059970940693 -0.09881939488019428; 0.020409585914458368 0.022766686184747687 -0.10847791018101134; 0.0073848035342013426 0.009301167283652201 -0.046150653186254394; 0.008987525561663639 0.0120654482959463 -0.06640077337837348; 0.0023894900719170914 0.0005282962811793024 -0.004118670532189733; 0.0004680686633963938 0.0001311105571620856 -0.00368814840564629; 0.0013461198086415372 0.0026061763511113136 -0.018489106199625096; 2.9595352462921144e-5 -0.0025296483409443377 -0.013941978952243686; -0.0007472886996338808 0.0015534405966538597 -0.010089108348707822; 0.006630127464916271 0.004802402759820076 -0.0063774598250840525; -0.004576541883477224 0.002733750497012421 -0.0059869399245356765; 0.003625028867824371 0.004781571059602332 -0.004021511465273603; 0.0005346705499243588 0.008537484029930197 -0.0002460067874861631; 0.01052931400416625 -0.018359578890429388 -0.013503043782138187; 0.009258008001137274 -0.013396405175238584 -0.01827408169067376; -0.018789048832377718 0.005072124508317773 -0.023034777086109355] %
+
+Mass Used: 84.60739159075229 kg
+Launch C3: 97.94947958168449 km²/s²
+||V∞_in||: 2.399455082393943e-9 km/s
diff --git a/archive/ES_0.562270572632635 b/archive/ES_0.562270572632635
new file mode 100644
index 0000000..9c5dbab
--- /dev/null
+++ b/archive/ES_0.562270572632635
@@ -0,0 +1,22 @@
+archive/ES_0.562270572632635---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:26:35.754
+Launch V∞: [6.646173610948886, -7.313773895417789, 0.18909041422395753] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.017357982175743955, -0.007277971771624313, 0.017602578268243844] km/s
+ V∞_out: [-0.017147592643447937, -0.0064693886386645695, -0.018115441266262265] km/s
+ time of flight: 1.8749577787468052e8 seconds
+ arrival date: 2029-04-08T21:36:12.754
+ thrust profile: [0.25150400330839795 -0.06403920035464924 -0.09027087552716258; 0.03011864472613215 0.008386376084574688 -0.033300132510374385; 0.03905807154415958 0.021100569782435873 -0.07291559338064385; 0.10989965800030027 0.0779730488170774 -0.26361968218340687; 0.02492003120122827 0.021425600869332203 -0.08404365491732817; 0.017073911683889192 0.017149322921347993 -0.07013312838698052; 0.009919128345320152 0.010466016586090098 -0.047738908394414165; 0.017294443477466507 0.023613556684107067 -0.10681707105159824; 0.01363337879288473 0.018482275575205348 -0.08812133498291273; 0.0010000052067033398 0.0014156653745113009 -0.007393651053284935; -0.0004913910764195902 0.0003137390506436778 -0.0023944947810925427; 0.0009736698477189529 -0.0002406348145768528 -0.0022754745682996955; 0.0005870168396829526 0.000580787942005432 -0.002222746886437432; 0.0014531304643678167 0.001514257573651817 -0.0012343239804361952; -0.00019244420581504204 0.0001671127061414124 -0.0006914289283447227; 0.004614360482252338 0.0017244552260759923 -0.0026614507673345445; 0.0005188685552967062 0.0003608687250409931 -0.0025843412921572; -0.0010711898627103122 0.0031975193430625144 -0.004120877733496985; 0.000937110069624261 -0.0012218105156616794 0.0005828624127811859; -0.00028123043907478607 -0.0011321222841865093 -0.0010380928255453031] %
+
+Mass Used: 86.07344130937736 kg
+Launch C3: 97.69866744491945 km²/s²
+||V∞_in||: 0.025770509890408758 km/s
diff --git a/archive/ES_0.5622709949399418 b/archive/ES_0.5622709949399418
new file mode 100644
index 0000000..76aec66
--- /dev/null
+++ b/archive/ES_0.5622709949399418
@@ -0,0 +1,22 @@
+archive/ES_0.5622709949399418---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T13:18:47.296
+Launch V∞: [7.675416717625713, -6.229517024011618, -0.05372419841976761] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.624023345228927e-6, 6.833892390814008e-6, 6.196819174666876e-7] km/s
+ V∞_out: [-4.6547585027280394e-7, 1.390602730639201e-6, 8.145530346185177e-6] km/s
+ time of flight: 1.698499859968724e8 seconds
+ arrival date: 2029-09-28T09:51:52.296
+ thrust profile: [0.24183488170887485 -0.03509795812079399 -0.09310287912137351; 0.08668157147664257 0.030841320732164185 -0.10698042430004018; 0.039134373264203666 0.02196126419615153 -0.08305964427566155; 0.0409193418131539 0.03133721557677611 -0.12368505719011089; 0.029595565447106696 0.026761793204382815 -0.12064688918908054; 0.032772971612448215 0.03406041181662091 -0.1559683692028668; 0.015607519570508129 0.01804851322829513 -0.09120602427187383; 0.010300333751292039 0.012489589717069774 -0.06473974877081701; 0.0091563078802953 0.010402976112918549 -0.06815333545574821; 0.012658277070840378 0.010882990260809647 -0.0727929583131429; 0.0026833470772427118 0.0033265151004536852 -0.02289717348546767; 0.0011782514943901408 0.001097394575380017 -0.011618952562474801; 0.0006329510103612294 -8.908431541570117e-5 -0.0007347263721114083; -0.0013215212510655694 0.00026531431845455705 -0.0010336631059063935; -0.0007263338955651515 0.000344566275431454 -0.0010519065189275294; 0.0002469840453915483 0.0003314287685432177 -8.52234033155029e-5; 0.0008050694811734915 -0.00010969260913730737 0.0015381102815851526; -7.6332111613297e-5 -0.00019261104855040342 0.0002459218650321029; -0.000583081071690257 -0.0014059130981843365 0.001562241269055601; 7.391052815657322e-5 0.0006543327501005617 0.00022933850659880093] %
+
+Mass Used: 85.93904991486306 kg
+Launch C3: 97.72179043115469 km²/s²
+||V∞_in||: 8.274520093956078e-6 km/s
diff --git a/archive/ES_0.5622713421176451 b/archive/ES_0.5622713421176451
new file mode 100644
index 0000000..d8248be
--- /dev/null
+++ b/archive/ES_0.5622713421176451
@@ -0,0 +1,22 @@
+archive/ES_0.5622713421176451---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T20:09:49.494
+Launch V∞: [6.381661204829912, -7.51075049993692, 0.06103607441781251] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.936033544339337e-8, -2.0165306672367802e-8, 2.4609555421155267e-8] km/s
+ V∞_out: [-9.5480678575095e-8, 8.869575307401635e-9, -1.1653547581322652e-8] km/s
+ time of flight: 1.859758761557726e8 seconds
+ arrival date: 2029-03-24T08:07:45.494
+ thrust profile: [0.30609497275908826 -0.08256498650154433 -0.11725973209206536; 0.05022726491584107 0.011062096538968174 -0.06054760283385328; 0.04945981389460413 0.02204204662244788 -0.0996458323938194; 0.048874536269117586 0.029550366629649483 -0.1369637061015384; 0.03916847654016376 0.028034334408271543 -0.13954437444411072; 0.03641117287107599 0.030724616214882983 -0.16433578167994742; 0.013942762839751984 0.012003754738606532 -0.07164857677139962; 0.013521469186366776 0.012604681506578468 -0.07875916251670254; 0.002032066697059252 0.0027709420537560974 -0.01701530552244698; 0.0014272157998423869 0.0012936802262800279 -0.00836213660389509; 0.0012685711669610921 0.0007919852104000287 -0.004753822431355758; 0.0006324041360810137 -0.0007472812843006914 -0.004715184291694766; 0.00021186747013838978 0.00012726321840469525 -4.187590260701845e-5; 0.0018827640034082735 -0.0001676802609575917 -0.0015206237092947666; 0.0005389487036115576 -0.0017962298680046554 -0.0017482858628699268; -0.00025730112031272293 0.0005981088878056989 -0.0005453541457697158; 0.000491965988777078 0.002245477307160608 -0.004520848614230201; 0.0006310598663743748 2.937078009150173e-5 -0.00269215382855769; -0.0013914086618610618 0.0020487458742145604 -0.00030516931471572884; -0.0001289636630923742 0.0007854934335287274 -0.0009540022420839415] %
+
+Mass Used: 89.32915959108641 kg
+Launch C3: 97.14069820791421 km²/s²
+||V∞_in||: 9.485536021634908e-8 km/s
diff --git a/archive/ES_0.5622844455973258 b/archive/ES_0.5622844455973258
new file mode 100644
index 0000000..f9a4b7c
--- /dev/null
+++ b/archive/ES_0.5622844455973258
@@ -0,0 +1,22 @@
+archive/ES_0.5622844455973258---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T10:58:58.485
+Launch V∞: [8.001606827717625, -5.75150588793868, 0.021534989524396093] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.783002693897614e-7, -3.952951281717331e-6, 7.39915067828012e-7] km/s
+ V∞_out: [-6.080794003172568e-7, 2.2710600318829964e-6, 3.29854443271521e-6] km/s
+ time of flight: 1.850148627360028e8 seconds
+ arrival date: 2030-03-25T20:00:00.485
+ thrust profile: [0.32241454978120926 -0.008259787724855782 -0.11103750520394486; 0.04199756638055562 0.021859107290254344 -0.05376440561802379; 0.037217544845994245 0.03108301409781006 -0.084684079373345; 0.029559363274181773 0.03191075841244633 -0.09843527521260868; 0.03660262550062571 0.0478492153510246 -0.15540461886868492; 0.013311946043648168 0.019861520918296096 -0.07599025951539838; 0.008925959729792515 0.014980329908719675 -0.06242465098451909; 0.006547217756621 0.011664644451337516 -0.050513160844001544; 0.005541607546362175 0.01170660359640011 -0.05450568891144968; 0.0036785461457114667 0.007907860612783885 -0.0394466019994199; 0.0019621596350390355 0.007200597683644699 -0.034950918609164355; 0.001623138849620927 0.00410534812994538 -0.021784329634904495; 0.002547837735812024 -0.006472408550934072 -0.0036583369521707505; -0.0025835393390436175 0.0013381193834736665 0.0029406471861115717; -0.0044726936243581535 0.0035871984107102026 0.006223353539732583; -0.005214829836835213 -0.006933827783218758 0.0026251132262839465; -0.005116031034853858 -0.0004407735295880845 0.006830546623886267; -0.012496118726486618 -0.009226736134777895 -0.005269893520249597; -0.0016517773781065644 -0.0014076477190069147 0.005924741003556921; 0.008765785117082647 -0.008986867606779537 -0.0142342228279893] %
+
+Mass Used: 89.54687909603763 kg
+Launch C3: 97.10599556014444 km²/s²
+||V∞_in||: 4.049946825691411e-6 km/s
diff --git a/archive/ES_0.5622845926880451 b/archive/ES_0.5622845926880451
new file mode 100644
index 0000000..e4940b1
--- /dev/null
+++ b/archive/ES_0.5622845926880451
@@ -0,0 +1,22 @@
+archive/ES_0.5622845926880451---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T13:01:57.344
+Launch V∞: [7.782700854045567, -6.000509829739126, -0.01487147809427686] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00024264051084491544, 5.613341127217471e-5, 0.0016171314905614497] km/s
+ V∞_out: [0.0014960106764454284, 0.00020446413095634688, -0.0006284536885606281] km/s
+ time of flight: 1.757683352602246e8 seconds
+ arrival date: 2029-12-04T21:34:12.344
+ thrust profile: [0.2719152984462074 -0.01701615750153406 -0.08452680037428331; 0.10116332756777877 0.050961297462696474 -0.1013852734967581; 0.06373850445389766 0.0535451600444115 -0.11298089101978115; 0.03229000355234444 0.03582457504562686 -0.08439754301967296; 0.08888630058279001 0.12425322315974131 -0.2917469527813961; 0.014601599005378196 0.023162647138034932 -0.06517496198578449; 0.012887236426535945 0.024312517044254748 -0.07222076350994215; 0.0023080576453026226 0.005164033139683229 -0.01836411665844559; 0.005310431984357308 0.013293155333907802 -0.04302286102179153; 0.004169823771072757 0.011161325666321135 -0.03390830791551188; 0.0012994507984203465 -0.0003839743598933322 -0.0058110514849208095; -0.0076739660841461995 0.0018379681696869543 -0.0067771411753644595; -0.0010739643058136563 0.0003199679592099545 -0.011647781005710562; 0.004455995840249944 0.007503351597760644 -0.0014030086615891158; 0.0019443964173515846 -0.0008992112250976157 -0.00014690406892393362; -0.0011642717706074723 -0.0012898781384282282 0.0036551652482627903; -0.006971722549656011 0.0015501647540791803 -0.0015925745236545059; 0.0022090167434403074 -0.0004685662300292477 0.004999932046127939; -0.0006929606943410812 -0.010493822769852315 0.0031369124664900406; 0.002232290833260777 -0.0003806395751980629 0.003349009641335138] %
+
+Mass Used: 92.63418836227993 kg
+Launch C3: 96.57677196121817 km²/s²
+||V∞_in||: 0.0016361966981783176 km/s
diff --git a/archive/ES_0.5622907841777605 b/archive/ES_0.5622907841777605
new file mode 100644
index 0000000..d4b7db7
--- /dev/null
+++ b/archive/ES_0.5622907841777605
@@ -0,0 +1,22 @@
+archive/ES_0.5622907841777605---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T10:49:43.126
+Launch V∞: [7.523805486338294, -6.213057068403148, 0.04272637038986324] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.1014012813582366e-5, 3.580794443145809e-6, 3.314609869334153e-7] km/s
+ V∞_out: [-2.2760991349641494e-6, 7.045509815990104e-6, 4.0518516301634774e-5] km/s
+ time of flight: 1.697100264076296e8 seconds
+ arrival date: 2029-09-24T16:30:09.126
+ thrust profile: [0.3625007847914839 -0.03731649831174637 -0.11362722839136892; 0.14066880775977808 0.06399260611529647 -0.14232425840911178; 0.10951439533317793 0.085726253612066 -0.186444118770037; 0.05450499147768726 0.05619096543774165 -0.14018980844025267; 0.03121734620330075 0.03865830353044805 -0.10771460656908644; 0.024671568023845212 0.03554359487819213 -0.1077048635346016; 0.024791830151261796 0.042007833103831264 -0.12858914476031513; 0.006604269385745031 0.010859180227594313 -0.035733128886679524; 0.004091379651364106 0.007303587236781769 -0.027552502743609826; 0.004186909913999214 0.008082497608670719 -0.03433638885951933; 4.3658727587056055e-5 0.00018558000033085716 -0.0040008458471455614; -0.0002487086703303759 0.0005668215870820511 -0.0043751713672651365; -0.0005085887854624706 0.00019924037629058598 -0.0023962532785409794; 0.0007193085320828742 -6.210106629679228e-5 0.0006234853012227833; -0.0017347766167928316 0.0021509176307975292 -0.0007061295242851802; 0.0003296550170164273 0.005525207003229569 -6.657178794658463e-5; 0.0006450715683387764 0.002431398956217975 -0.00010684865661691556; 0.0007185234940813918 0.0013680500717699465 0.0005321769358708698; -0.0016676646480395713 0.00034114802524232184 -0.001800566399194055; 0.00032696556547632855 -0.0007756038957908483 -0.0022981934856698485] %
+
+Mass Used: 100.6051909411317 kg
+Launch C3: 95.21155267421523 km²/s²
+||V∞_in||: 4.1171363862551616e-5 km/s
diff --git a/archive/ES_0.5622910032001429 b/archive/ES_0.5622910032001429
new file mode 100644
index 0000000..c6619e8
--- /dev/null
+++ b/archive/ES_0.5622910032001429
@@ -0,0 +1,22 @@
+archive/ES_0.5622910032001429---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:44:33.882
+Launch V∞: [6.530926332371922, -7.403840046263399, 0.12972473333615112] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5054469590460887e-5, -2.3918602640363362e-6, 4.170298876835652e-8] km/s
+ V∞_out: [2.847994628895499e-6, -6.673946680819942e-8, -1.4975255778858244e-5] km/s
+ time of flight: 1.8749577787493056e8 seconds
+ arrival date: 2029-04-09T16:54:10.882
+ thrust profile: [0.22310703096204879 -0.05479399075804615 -0.07946147403072007; 0.060786245534323775 0.0165621139405922 -0.0658018361867865; 0.09622343009059792 0.05209048770613994 -0.17349785722591615; 0.07904728558434199 0.05777811177778147 -0.20048100269768246; 0.031063378697881196 0.02668155008177279 -0.10262984891373242; 0.02167250735800841 0.02151510933444666 -0.08823595503264292; 0.013504052368681857 0.015079558783793095 -0.06567136472216743; 0.011321670383143058 0.013680101053762779 -0.062404743167038326; 0.0029422442672410003 0.003853634112516042 -0.019071108783132992; 0.0006127142798215749 0.0017192505514819754 -0.006234293173249507; -0.00011434105284522766 0.0007755307523845184 -0.004778577238468073; 0.0024772579695314352 0.0017893301607622575 -0.004979937089366458; -0.002217108388548207 -0.00022612392007522277 -0.0028311315525945484; 0.0036441671146916097 -0.0012130454433828411 -0.005008014869162973; -0.0011859853504452228 0.0002805277062969636 -0.0011618035309589087; 0.003121521429080014 -0.0002973928517914789 -0.0028476457735244656; 0.002274345188309964 6.386160113414638e-5 0.004564982499617997; -0.0010050044662751048 -0.00044852693162373024 0.0008024580264259654; 0.0007074553131415066 0.0030080137085690397 -0.007698469968015879; 6.578295252604623e-5 -0.0005796510994344739 0.0023534812681641694] %
+
+Mass Used: 87.33390134039018 kg
+Launch C3: 97.48667469596171 km²/s²
+||V∞_in||: 1.5243352299020705e-5 km/s
diff --git a/archive/ES_0.5622999224215026 b/archive/ES_0.5622999224215026
new file mode 100644
index 0000000..b3af933
--- /dev/null
+++ b/archive/ES_0.5622999224215026
@@ -0,0 +1,22 @@
+archive/ES_0.5622999224215026---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T16:35:11.820
+Launch V∞: [6.587363031977515, -7.397133815824215, 0.24815357263974763] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.7462335295902565e-9, -1.8626743558227455e-9, 2.0182264632019387e-9] km/s
+ V∞_out: [1.2968660733861622e-9, -2.9754914474473286e-9, -4.2214771146995265e-9] km/s
+ time of flight: 1.8597266703145796e8 seconds
+ arrival date: 2029-03-22T03:39:38.820
+ thrust profile: [0.1839916816779471 -0.046037891296405446 -0.06761651443342126; 0.0455367799892066 0.012798496876226011 -0.04957454153781407; 0.07617657879197441 0.04207820591728281 -0.1363165186841871; 0.07337282783038825 0.054121783365272146 -0.17809627879302745; 0.05121458700351663 0.046046603548731614 -0.1596358242096606; 0.02878346751942238 0.030102754962465263 -0.1137603266408207; 0.011371215168342951 0.012789992117445935 -0.053934951027757506; 0.004952063059680425 0.008172687388752582 -0.03571088315226631; 0.003947378118576772 0.007873013069323623 -0.029984836668253384; 0.006034090258675578 0.008180265317556145 -0.04373592838946777; 0.0013745459122884343 0.000763143480352758 -0.011754578159027486; -0.0006642295657949283 -0.0011573852810572772 -0.0002551590485411129; 0.0012427386902790867 0.001812899253190581 0.00072094488878205; 0.00020590622428621214 0.00021096341264284382 -0.0006298012920827311; 0.0005776813738399534 -0.0007991872828884346 0.004377854239951413; 0.00048556724744850603 0.00018444634156142 -0.0031887688821599755; -0.0011787866733406374 -0.0008078858247819519 -0.0007762233887047554; -0.0007895993649158031 -0.00010162722515564561 0.0005066812869781172; 0.0012383321279077761 -0.0007333953975917577 0.00104328184942797; 0.0002947229025208538 0.00013686131263842356 -0.0007111026712804907] %
+
+Mass Used: 83.34353932574004 kg
+Launch C3: 98.17252059988796 km²/s²
+||V∞_in||: 4.645111351822963e-9 km/s
diff --git a/archive/ES_0.5623119713100515 b/archive/ES_0.5623119713100515
new file mode 100644
index 0000000..6996c55
--- /dev/null
+++ b/archive/ES_0.5623119713100515
@@ -0,0 +1,22 @@
+archive/ES_0.5623119713100515---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:52:25.645
+Launch V∞: [6.60727249976253, -7.451066904727743, 0.21669436613283005] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.013897557644906246, 0.006871924728584985, -0.01693709797156993] km/s
+ V∞_out: [0.014749243769224974, 0.0060280440941416725, 0.016674392875787182] km/s
+ time of flight: 1.8541314948625e8 seconds
+ arrival date: 2029-03-17T11:31:34.645
+ thrust profile: [0.12232442614702443 -0.0417029330738932 -0.05135547458190251; 0.0815333146661766 0.009953858181835707 -0.10619257441177649; 0.05650469017511018 0.01556452655413225 -0.121152576658595; 0.041819154079937824 0.01399551596931038 -0.12554617014358724; 0.036581265868845775 0.013871368873330564 -0.14181826703552627; 0.032458022989478565 0.014080166539283831 -0.14964122980282982; 0.015477453780031231 0.007119522756201414 -0.07668324142257422; 0.00849719165523322 0.003956575002365122 -0.04995766894991827; 0.005698156424238648 0.0026242600834983504 -0.03812503908093935; 0.0007288588429250764 0.0010205060911279097 -0.011361741748328226; 0.0009764761661937211 0.001959376671727484 -0.01002777828330231; 0.00028616545809384737 -7.937422674999075e-5 -0.0005511173995410763; -0.00012070912823530211 -0.0008557857003157628 -0.0020976126622343537; 0.0003950536871050349 0.0006959027159792722 -0.002928465963678621; 0.00040832446655667725 0.00034716513184115076 -0.00016203254638133872; -0.00028828839489996444 0.0006064476140339964 -0.00034956087363836365; -0.00033567500963297206 0.0010325988444353112 0.0006141600065946965; 0.0003386858331363274 -0.0017408675827111754 -0.0006939938943668682; 0.00025452073826811027 -0.0004987053762703787 0.0026225468549574828; -0.0007633124885292294 0.0003394739299244931 0.0012815193183101756] %
+
+Mass Used: 77.23910780162123 kg
+Launch C3: 99.22140435316096 km²/s²
+||V∞_in||: 0.02296150573606592 km/s
diff --git a/archive/ES_0.5623143787815081 b/archive/ES_0.5623143787815081
new file mode 100644
index 0000000..9cfa418
--- /dev/null
+++ b/archive/ES_0.5623143787815081
@@ -0,0 +1,22 @@
+archive/ES_0.5623143787815081---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T03:05:11.587
+Launch V∞: [6.535403426881107, -7.3307599665602465, 0.17778784751182164] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.014703945522581415, -0.0068915637411784275, 0.01591218086223538] km/s
+ V∞_out: [-0.014966014564261764, -0.0060331614678046765, -0.01601032250524851] km/s
+ time of flight: 1.8749577787799075e8 seconds
+ arrival date: 2029-04-09T05:14:48.587
+ thrust profile: [0.3444282002221376 -0.08803626945290337 -0.11223731751003914; 0.06629804141798779 0.01845297610688061 -0.07439199312161568; 0.049447449114352525 0.025989834369535558 -0.09276625982723165; 0.04024027464290298 0.028537320822213694 -0.10639219458165933; 0.03466913936217597 0.029741579336070367 -0.11697690823594555; 0.014997259263104643 0.014708987749035974 -0.06274419030589283; 0.021320391138862364 0.0236649267292785 -0.10199790660068184; 0.016729936591604423 0.020187314022278333 -0.09123220328421586; 0.007386806886474876 0.010064933606583934 -0.04846934562639279; 0.008516991973992045 0.012308425766655456 -0.0620688025601595; 0.004277719712208342 0.006803098208160097 -0.03446046879858004; 0.000594017064077432 0.0005990816895829089 -0.004479828702778641; 7.12480945497616e-5 7.331695850551259e-5 -0.0002156131175653368; -1.352575927015567e-5 -1.248460814726349e-6 -0.00015896553722869928; 6.911671115193907e-5 -8.61256877168682e-5 -0.00014178265107374753; 4.3282905107164514e-5 -7.809470912620008e-6 -0.00011725349383766555; 0.000169980589569006 -0.00014897787641727104 4.7544955400113546e-5; -5.1849786073165596e-5 5.2383528666258926e-5 -4.905002167280571e-6; 0.00013412576721516926 0.00013498401015232497 0.00012223950052224746; -5.6877578110243085e-5 -0.000148523025162798 0.00017892303203045082] %
+
+Mass Used: 93.21507765597426 kg
+Launch C3: 96.4831481581346 km²/s²
+||V∞_in||: 0.02273537253977284 km/s
diff --git a/archive/ES_0.5623179876227756 b/archive/ES_0.5623179876227756
new file mode 100644
index 0000000..0f88a07
--- /dev/null
+++ b/archive/ES_0.5623179876227756
@@ -0,0 +1,22 @@
+archive/ES_0.5623179876227756---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T23:27:58.344
+Launch V∞: [6.586404520322205, -7.464162818663673, 0.11216851271447843] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.1790183108309534e-7, -0.00013874649261885988, 9.52666696739251e-5] km/s
+ V∞_out: [8.895411315389754e-5, 0.00014235096284937143, -2.9596387363127423e-5] km/s
+ time of flight: 1.8749577787467685e8 seconds
+ arrival date: 2029-04-11T01:37:35.344
+ thrust profile: [0.1301942132512815 -0.03402561468798908 -0.04996229098827938; 0.03945114084472744 0.009543835015329318 -0.04767765966112494; 0.09263203942222205 0.043986747567748265 -0.1721549074493195; 0.040426159243515385 0.02629122564952892 -0.1112235264388788; 0.02900219247198204 0.02223647333578963 -0.1059192351598933; 0.025082263443758947 0.022821410090640003 -0.11054622950235501; 0.021741425611673623 0.02026941660313727 -0.1064822789985721; 0.009031338913878731 0.009632437737349784 -0.054515370513504274; 0.00895122653452353 0.009697955600477294 -0.05733569434004555; 0.001674627513211447 0.0016316003432930327 -0.010763510039221885; 0.0031363553189498565 0.0035388368202244605 -0.022943128594747328; 0.0009482327575414541 0.0009014622097366145 -0.007272064394393442; 0.0005974572933699345 0.0006577740564851994 -0.0016773032252850378; 0.001010714683363426 0.0005000693784183237 -0.0036959505963130974; -0.0001505427637852818 0.00025819835408783453 -0.0014973340485382259; -0.0013346280588653562 0.002668957317238526 -0.002955102395635796; 0.0006547017819262897 0.0003164054356242585 -0.00030799148547214087; -0.0009349011861733633 -0.0012460911748533674 -0.003968905992262588; 0.0011457947116760043 0.0016375896154772899 -0.00039229515108091527; 0.0005334991956937022 0.000294801857096026 -0.0021720458272130724] %
+
+Mass Used: 77.9132938527332 kg
+Launch C3: 99.10703286408658 km²/s²
+||V∞_in||: 0.00016830478961317924 km/s
diff --git a/archive/ES_0.5623230628156944 b/archive/ES_0.5623230628156944
new file mode 100644
index 0000000..3965c0b
--- /dev/null
+++ b/archive/ES_0.5623230628156944
@@ -0,0 +1,22 @@
+archive/ES_0.5623230628156944---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T09:30:15.206
+Launch V∞: [6.633601947457675, -7.4144634814334, 0.11154728764171581] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0505142785513003e-6, 0.000379270488355926, -0.00024173489393395712] km/s
+ V∞_out: [-0.00022728224089496815, -0.0003649275412318323, 7.644972922569881e-5] km/s
+ time of flight: 1.8749577787499386e8 seconds
+ arrival date: 2029-04-10T11:39:52.206
+ thrust profile: [0.14599210440054608 -0.03566384048023662 -0.05249837713568982; 0.05340627676993788 0.013441973212361449 -0.061678632067522034; 0.05755056357985669 0.029040324080411302 -0.11135712092101448; 0.03721753782918359 0.024990499970916312 -0.09889834914318076; 0.026839348854275344 0.02166880301197257 -0.09386591997895069; 0.023690832014158503 0.022641334400046256 -0.10514718064062027; 0.021778933956960306 0.02276997014046975 -0.11054330791589619; 0.015111972304852861 0.018809354151341804 -0.09335505756885452; 0.011438112298238908 0.012474715361015545 -0.07025178805964039; 0.005119134888861519 0.007462583937005554 -0.04077841113901417; 0.003286473120015499 0.005111770288844865 -0.02676162804177329; -0.00013117546650607493 0.00042027770672456785 -0.0013427076745943336; 0.0001610838297265956 4.5902321592015234e-5 -0.002200065271567745; 0.00011828999964011514 -0.00013874679941473913 -0.0007279883912486998; -0.0003780843676830301 -0.0005479703666426785 -0.000511321999812059; -0.000441898611994006 9.71591433956816e-5 -0.0006582514289801335; 0.0007573302176889843 -0.00023536378411190555 2.8307724565778943e-5; -0.0011283197078383322 0.0007923898741124223 -0.00013787281044988465; 0.0004661121334579064 0.00024378998486667582 0.0012624853937933565; -0.0004448786713794411 6.982798446377e-5 -0.0009301304206398394] %
+
+Mass Used: 78.59381979712043 kg
+Launch C3: 98.99138631220397 km²/s²
+||V∞_in||: 0.00044975878631023266 km/s
diff --git a/archive/ES_0.5623232543199805 b/archive/ES_0.5623232543199805
new file mode 100644
index 0000000..15daaca
--- /dev/null
+++ b/archive/ES_0.5623232543199805
@@ -0,0 +1,22 @@
+archive/ES_0.5623232543199805---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T14:20:51.357
+Launch V∞: [7.853273746532514, -5.703089865935649, 0.16050834951331167] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4691696498075067e-8, -1.0263508750341568e-8, 9.369816975184062e-8] km/s
+ V∞_out: [1.8822429807193417e-8, -6.093158691834232e-8, 9.585686046989918e-9] km/s
+ time of flight: 1.820406141171674e8 seconds
+ arrival date: 2030-02-15T13:11:05.357
+ thrust profile: [0.5121916271909394 -0.013513296351558082 -0.14451008865016401; 0.10960949717811483 0.062042440659370535 -0.11044370609034507; 0.05447997603760148 0.05082228723274954 -0.10117342325160684; 0.033294805622552257 0.041532677167999986 -0.09334540197277695; 0.021689001620700202 0.03348799493388651 -0.08229398378399358; 0.018502966615738085 0.03437410949750537 -0.091155119870526; 0.011231229019297845 0.022918547244112422 -0.06566089952029071; 0.007441142326460351 0.0184329931292896 -0.05585488876601028; 0.014142717481381566 0.03620091432638105 -0.1130382598673494; 0.0027242088892135354 0.005645509910206082 -0.020076089218095953; -0.0006043262131860217 0.0030063898498550604 -0.010134367462845094; 0.0019668070884746253 0.00386888421898137 -0.00792486366337388; 0.002482406051455728 -8.15085110896052e-5 0.004388382845916657; 0.0006098213297408518 0.00472487770527544 -0.0012595933580314416; 0.004803357330943265 0.003068558652610254 -0.002407661922585281; 0.006967476645706392 -0.000357209547642086 -0.0050006459140373265; -0.007642154686448936 -0.0057989155134061075 0.001850117515907327; 0.00794994845051854 0.009984727670727906 -0.00918255925849513; -0.00033003960670810624 -0.0008908124342207496 0.00038022384659918557; -0.0007357407024333965 0.0010167591066452435 -0.002786873753138315] %
+
+Mass Used: 106.39851469810446 kg
+Launch C3: 94.2249054871782 km²/s²
+||V∞_in||: 9.539671154030746e-8 km/s
diff --git a/archive/ES_0.5623324224639641 b/archive/ES_0.5623324224639641
new file mode 100644
index 0000000..e890ab8
--- /dev/null
+++ b/archive/ES_0.5623324224639641
@@ -0,0 +1,22 @@
+archive/ES_0.5623324224639641---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:07:42.914
+Launch V∞: [8.040198551692379, -5.631207380819259, -0.32385413955653264] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.682597726978887e-9, 8.788985331129131e-9, -4.7897270266200276e-8] km/s
+ V∞_out: [-1.3240299746354162e-8, 4.4789953866607416e-8, -6.819635207842813e-9] km/s
+ time of flight: 1.8749577787713698e8 seconds
+ arrival date: 2030-04-22T21:17:19.914
+ thrust profile: [0.35794594283399467 0.00587058221049158 -0.11628586617819507; 0.05901347897750972 0.0362509971956655 -0.06887447419546153; 0.032281001820991 0.032747326800670114 -0.06978844262267289; 0.03433288035558622 0.04645666040700519 -0.1097218277308477; 0.024353582262865357 0.04115191173826507 -0.10730219921461613; 0.017762672051592196 0.03632210233733669 -0.10286179157326925; 0.01811778101096364 0.04407322861139733 -0.1315584565707561; 0.006687990349500796 0.018825381279088223 -0.06097678835404893; 0.004025792047939618 0.01332645475950167 -0.04543366668329733; 1.021244498296774e-5 0.0006206750048722036 -0.002483445411850617; 0.0006003897995557468 -7.732041622436278e-6 -0.004792233996894235; 0.0003771684549331956 -0.0026285536726955144 -0.0008074502637672488; 0.00044065652774100974 -0.00016650932561693794 0.004964714300495408; 0.0014394300444992283 -0.0007844215934334543 0.003989764286311285; -0.0026678209952457487 -0.0051048440163831196 0.005807289453598844; -0.015248301002149696 -0.005804210146913711 -0.010102677415495712; -0.0007104238507754386 0.006542443261863208 0.004059255090842929; -0.0022810013910880087 -0.006405546616431367 0.0050999552727524055; -0.005200299512990761 0.004698616989285794 -0.003304397840757419; 0.002878274259040462 -0.006444941473308424 -0.017147219159764433] %
+
+Mass Used: 93.37016309048977 kg
+Launch C3: 96.46017082013742 km²/s²
+||V∞_in||: 4.915335059265909e-8 km/s
diff --git a/archive/ES_0.5623329864999371 b/archive/ES_0.5623329864999371
new file mode 100644
index 0000000..bd77e6d
--- /dev/null
+++ b/archive/ES_0.5623329864999371
@@ -0,0 +1,22 @@
+archive/ES_0.5623329864999371---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T08:37:35.282
+Launch V∞: [7.557652373694285, -6.38553646915778, 0.0029961918897368194] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.108628334250959e-7, -7.512185723096987e-6, 1.3389152003226587e-6] km/s
+ V∞_out: [-1.1769296813193398e-6, 4.596876412615167e-6, 6.030663851609596e-6] km/s
+ time of flight: 1.680772051205549e8 seconds
+ arrival date: 2029-09-08T16:44:20.282
+ thrust profile: [0.23185277370535912 -0.04127415515249246 -0.09384616133623082; 0.07001184870198653 0.019984432245392356 -0.08672538500881365; 0.06873589807651233 0.03394757364206988 -0.1461550043501711; 0.06361855022573644 0.03964091160163945 -0.19021845861778672; 0.05044847562599591 0.03584167402206181 -0.192579729558252; 0.03275227714826581 0.025149374528321815 -0.15070693562978218; 0.01606206507676623 0.012874784045272026 -0.08510915604121286; 0.007495042685194555 0.006431197644046476 -0.04616191018414817; 0.0012468360497419817 0.0007957908523816231 -0.006672551166380777; 0.00023819129032531333 0.0005337369466638234 -0.005399120138647005; 0.0005263270305342835 0.0008988937142015915 -0.00397117117796924; 0.0002265740022239665 0.0006528730255259699 -0.0005684470257663193; -0.0017673405904071893 0.0004174455934786933 -0.0035505458930076166; 3.1683647154776885e-5 0.0001740007881253145 -0.002607389427001685; -0.0009647015401359053 -1.786757129172104e-5 -0.0013181930997518182; -0.0013748830575242305 -0.0011534962891044133 -0.0020653148987066416; 0.0009319126541108128 0.00041754726559563185 -0.0017719163315707794; -0.0009260854268258616 0.00021302624923360224 0.0005690480803312652; 0.002406468838171731 -0.0022187036337569374 0.003585851305892715; -0.0024311702173788873 0.003692651098478669 -0.0001339276663489097] %
+
+Mass Used: 85.01151704657923 kg
+Launch C3: 97.89319437771671 km²/s²
+||V∞_in||: 7.673534178368364e-6 km/s
diff --git a/archive/ES_0.5623343987519294 b/archive/ES_0.5623343987519294
new file mode 100644
index 0000000..dd64217
--- /dev/null
+++ b/archive/ES_0.5623343987519294
@@ -0,0 +1,22 @@
+archive/ES_0.5623343987519294---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:23:55.631
+Launch V∞: [6.575082158600776, -7.441373166601024, 0.13170793533044872] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.4320474078144336e-6, -4.606850354676026e-6, -5.50326576107122e-6] km/s
+ V∞_out: [-7.715819319061386e-6, -4.62036566077096e-6, -1.502882447215361e-7] km/s
+ time of flight: 1.874957778711174e8 seconds
+ arrival date: 2029-04-10T13:33:32.631
+ thrust profile: [0.12107505761404985 -0.03397597855299791 -0.045114721576389454; 0.11760376478201594 0.02764614662643727 -0.12024476342920817; 0.05616158834621218 0.023466376195372986 -0.10928994840133305; 0.08950388738224556 0.05598411118630426 -0.20434345942433071; 0.013775734754826496 0.009825399151979067 -0.050956242484493694; 0.02347370855767211 0.018251308564190643 -0.10127108057922417; 0.015135548046822938 0.012702260231685084 -0.07240238871192707; 0.014329888571580842 0.012705016733453539 -0.08606811149440115; 0.003952543628849183 0.00397068097055912 -0.02576371720234214; 0.004782985855860263 0.0068313309802375925 -0.03730284292657064; 0.0013267247416013494 0.0015953814331027578 -0.010453871525319482; 0.0015307067926673141 0.001299481520446112 -0.013964856821485573; -0.0006358802552809963 8.563320999533476e-5 0.00032850081113332177; 0.00025031615464571224 -0.00031388879614948793 8.750023986165627e-5; 2.8801319768905485e-5 0.0001815199432816167 0.00017247868893229077; 0.0010656716790245165 -0.0006122596940306847 0.0004350599497944315; -0.00042032321644297987 -0.0009766379600610444 0.0012959053811098075; 0.0005707827368364646 -0.0004706591039776186 0.0006110199039546402; 0.0007312384655965634 -0.0006697515414178358 0.0009051607661186825; -0.002825241402811987 -0.0006450013193147825 -0.0027899949752091856] %
+
+Mass Used: 80.7554578436484 kg
+Launch C3: 98.623086977189 km²/s²
+||V∞_in||: 9.000896803546907e-6 km/s
diff --git a/archive/ES_0.5623426778190077 b/archive/ES_0.5623426778190077
new file mode 100644
index 0000000..14bd07b
--- /dev/null
+++ b/archive/ES_0.5623426778190077
@@ -0,0 +1,22 @@
+archive/ES_0.5623426778190077---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T03:16:12.743
+Launch V∞: [7.749541523925124, -6.226664684494551, -0.1480890032939253] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008135883576003202, -0.004804156269068321, -0.00034924488987558285] km/s
+ V∞_out: [0.006986540480629642, 0.003902710458075862, -0.005033489022923156] km/s
+ time of flight: 1.797384114893903e8 seconds
+ arrival date: 2030-01-25T10:36:23.743
+ thrust profile: [0.18970814352785015 -0.010389176960397957 -0.06757831277305885; 0.053917313306347296 0.02601823315361839 -0.06626493709763952; 0.060990392421536435 0.04748523939165874 -0.12449225280924879; 0.03982057224758934 0.04070319141730922 -0.12162542476068919; 0.020053925769255056 0.025372557217515714 -0.08279876149590269; 0.020745279868916985 0.02827213943820272 -0.10253173717477185; 0.009275433606319296 0.015356084818279497 -0.06216388104453188; 0.014386571430048817 0.024934121560865958 -0.10412696926500004; 0.010974035005580269 0.019409679130927414 -0.08633651764866028; 0.0038189698701322746 0.009329441233570036 -0.04661951324460329; -0.0010561144548661464 0.0004361542111549338 -0.0013395612671703147; -0.00032964497071293 0.0008248537308416722 -0.005207896121352927; 0.0002059289049129516 -0.0011775124001473102 0.001419046059294386; 0.0006486109748762412 0.00013075480254468337 0.0010704684405062404; 0.0005629976237179498 0.0011086204508266033 0.004603072865471153; 0.0037306571300456566 -0.002710913488539586 -0.0010822290443850407; 0.00037802148149902834 0.0005737083746143974 0.0007206964680071706; 0.0009072536724344266 -0.002618610472175779 0.000682661753861406; -0.00031950326506802006 -0.00038796762358988667 0.0013450482308730376; -0.003475920289376331 -0.0039181496622160425 0.003846670766983287] %
+
+Mass Used: 79.44917333927924 kg
+Launch C3: 98.84867727706796 km²/s²
+||V∞_in||: 0.009454865996565542 km/s
diff --git a/archive/ES_0.5623511152725681 b/archive/ES_0.5623511152725681
new file mode 100644
index 0000000..7bfd542
--- /dev/null
+++ b/archive/ES_0.5623511152725681
@@ -0,0 +1,22 @@
+archive/ES_0.5623511152725681---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:23:19.251
+Launch V∞: [7.9530618861158136, -5.775565433834952, 0.13737589113024284] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0383937592122927e-9, 1.2088259528505328e-9, 2.341474573452045e-10] km/s
+ V∞_out: [2.113708763902905e-9, -1.598734612965869e-9, -1.2078366057471057e-9] km/s
+ time of flight: 1.8193086661195377e8 seconds
+ arrival date: 2030-02-16T07:44:25.251
+ thrust profile: [0.337843183043183 -0.014743224878621538 -0.11094079665688375; 0.0536063646117815 0.027697456607263495 -0.06033560844103351; 0.05391730293653215 0.045333293628474436 -0.10760341010074626; 0.031679950126210187 0.03482095924716401 -0.0937957354126621; 0.023590812947972845 0.03144715284583247 -0.09322270288711923; 0.0238794091458317 0.03632743035290436 -0.11580260912733571; 0.013986380637028444 0.023586862326957857 -0.08227651526529887; 0.008299541215861397 0.01561636585188118 -0.05794435742163488; 0.00780879533048007 0.01655192892093112 -0.06324668653607594; 0.006012644833143379 0.008789829629204644 -0.03538624593280559; 0.0048218269875260995 0.0047303827265072285 -0.019764962350158656; 0.007423178947557286 -0.001668894625324504 -0.023191290811452596; 0.010252363704531161 0.0036493033261663643 -0.005972920122978477; -0.001088731273878257 0.0010406464231848217 0.001525958968423556; -0.0006899993981618771 -0.0012264837757800758 -0.0016095731714122806; 0.006785706580530647 -0.014419695168681726 -0.002261395765045397; 0.011175057023309239 0.005865982921024198 -0.01919034348989445; 7.857330079201984e-5 -0.004233859913835078 0.0063901715389376255; -0.0019502724156544974 -0.006771151232784608 0.011849890460508779; -1.4101708024472906e-5 -0.0020741399607716897 0.00277026594492313] %
+
+Mass Used: 92.41750859922377 kg
+Launch C3: 96.62722158036097 km²/s²
+||V∞_in||: 2.381414355726833e-9 km/s
diff --git a/archive/ES_0.5623589420431025 b/archive/ES_0.5623589420431025
new file mode 100644
index 0000000..e8f87a9
--- /dev/null
+++ b/archive/ES_0.5623589420431025
@@ -0,0 +1,22 @@
+archive/ES_0.5623589420431025---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:21:45.209
+Launch V∞: [6.501850389339603, -7.402221801510227, 0.10605982510278528] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6721099267308236e-7, 6.792176013167432e-8, -8.877566526739936e-8] km/s
+ V∞_out: [2.771235384222885e-7, -7.221853573697528e-8, 3.356151613914486e-8] km/s
+ time of flight: 1.8749577787492514e8 seconds
+ arrival date: 2029-04-09T16:31:22.209
+ thrust profile: [0.28210577341219795 -0.06904893253981371 -0.08618405600415913; 0.042320457793321456 0.012572191243047742 -0.045174508901047704; 0.07172465864953957 0.0416336667724849 -0.12584214741400782; 0.05067246469508313 0.04134741777456084 -0.1335242816760878; 0.03672359452572603 0.035722547956541006 -0.12078034528986521; 0.03888364644847952 0.0436746910832128 -0.15188441073057937; 0.01770050975679044 0.02143896896878345 -0.08320879415230494; 0.010206607321350288 0.012625202390262035 -0.053500521911748915; 0.004557914235761233 0.006269196540389798 -0.028270574272254517; 0.004864515021010763 0.008103210135768164 -0.03290680359510342; 0.0009600922706630777 0.0009975000163168055 -0.005255178138509351; -0.0009833064509836872 0.0003750544104474128 -0.003562423180908477; 0.0010262280703393254 0.0014669339728307067 -0.0033066890916921016; 0.0010320382467470818 0.0007001754604863642 -0.0020159242617376043; -0.0006871183901718961 -0.0008604363922615326 -0.00032603955797006054; -0.0016165485680385764 -0.0006558827487905847 0.0007785249694927614; 0.0034340253001281743 0.001918164240568763 -0.0010802213799492723; 0.0005159879105051514 -0.0029788055000639175 -0.0054223401192217136; 9.33500514155906e-5 -0.0010529793308753314 -0.0014307417341500109; -0.003680852095612357 0.0021207270873775897 -0.0037910499292438692] %
+
+Mass Used: 89.79596288839639 kg
+Launch C3: 97.0781947706097 km²/s²
+||V∞_in||: 2.8964840556852395e-7 km/s
diff --git a/archive/ES_0.5623605517309087 b/archive/ES_0.5623605517309087
new file mode 100644
index 0000000..8b782a0
--- /dev/null
+++ b/archive/ES_0.5623605517309087
@@ -0,0 +1,22 @@
+archive/ES_0.5623605517309087---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T23:22:29.666
+Launch V∞: [6.607668306586232, -7.46199341499201, 0.09769598601499958] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005433173412940174, -1.7254036141146158e-5, 0.00038707476872167323] km/s
+ V∞_out: [-0.0003615424809531639, 3.6924983921911096e-6, 0.00011028468146976344] km/s
+ time of flight: 1.8749577787457043e8 seconds
+ arrival date: 2029-04-11T01:32:06.666
+ thrust profile: [0.10510006048032117 -0.02676394220813936 -0.04092194435003136; 0.07078001217151855 0.017390007933887373 -0.08207362256943877; 0.04833999972335145 0.023052990063268847 -0.09504233608799961; 0.052030162983125496 0.03332904350253948 -0.14245502698950588; 0.028860355313166913 0.021933077421731628 -0.1025480835140045; 0.027189552099185464 0.023244270885356286 -0.11575235594092281; 0.02881749891186007 0.027382090359973302 -0.14398741999270195; 0.011305309504759734 0.011499148625098642 -0.06374240732240112; 0.006302587150128568 0.007151428253212575 -0.040512255602179026; 0.0013605679616380197 0.0016229351203891711 -0.011001137558356435; 0.001269164116003429 0.0015032396977686655 -0.005653252321794588; 0.0012009159910966727 0.001211238061222427 -0.0030898440897837607; 0.0011387614092136207 0.0006423135780348162 -0.005099796316730863; 0.00031440864442173187 0.00016371319697844967 -0.0028201662922641858; -0.00011380598591824402 0.0006072272824024547 -0.0017137935107586666; 0.00045022671505049193 0.0006419453824076942 -0.003423063779808109; -0.0016488083179213768 0.00031749769678819217 -1.8746563476899404e-5; 0.0003592391203278723 -0.0001781804955389417 -0.0018893571799419137; 0.005038282898802274 -0.001892707590913931 0.001967720150472745; 0.0036477063851042177 -0.00021709506989171247 -0.003238919310602329] %
+
+Mass Used: 76.53298138062519 kg
+Launch C3: 99.35217068093172 km²/s²
+||V∞_in||: 0.0006673217452585347 km/s
diff --git a/archive/ES_0.5623680168691505 b/archive/ES_0.5623680168691505
new file mode 100644
index 0000000..fef19cc
--- /dev/null
+++ b/archive/ES_0.5623680168691505
@@ -0,0 +1,22 @@
+archive/ES_0.5623680168691505---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T09:48:15.490
+Launch V∞: [7.629643733872236, -5.73022845651924, -0.00012706629910156871] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.729758654857395e-7, -5.769158638406017e-6, 1.0202994895411816e-6] km/s
+ V∞_out: [-8.634616226540532e-7, 3.383552304478333e-6, 4.752580564611038e-6] km/s
+ time of flight: 1.8749577787489757e8 seconds
+ arrival date: 2030-04-20T11:57:52.490
+ thrust profile: [0.6913110224113275 0.04003429403219605 -0.1377492512252091; 0.13047030980037772 0.09530173697111219 -0.11620163363449108; 0.07767841572167677 0.0951772825718807 -0.12911850609433467; 0.05254558766701747 0.09126943137144503 -0.13727155959212847; 0.03566654489028204 0.07980375159770628 -0.13115812398012217; 0.013400598691142402 0.03741657823624208 -0.06890554931308764; 0.007490521139664999 0.026810078073321256 -0.052851155703317935; 0.0019224913413763054 0.008613365758120684 -0.01721020974673902; 0.0020247972517261517 0.010660602770509299 -0.02377195790655479; -0.0039405153821381895 0.0025740356171513354 -0.006253060612022689; -0.0024177592440052732 0.004231086301019329 -0.011964957350301576; 0.0022204166150933437 -0.0017656227515046273 -0.004617782666790021; -0.005937175798786107 -0.0004144151499923506 -0.007859423048054169; 0.002786932812457454 6.352392986662587e-5 0.003878520941215487; 0.00016784315219583565 -0.0033490790761073154 -3.933858442656886e-5; -0.0025060647258908168 -0.00369913071195699 0.00013596336038827934; -9.624429349031093e-5 -0.0028932513826996718 0.006916191644951073; -0.002179128245668155 -0.0027611426460567353 -0.001380714143747676; -0.002390693266989468 -0.0017136648450937753 0.010471173679850782; 0.0003365423843268668 -0.00459504638994748 -0.0008400689422403285] %
+
+Mass Used: 124.9886265131322 kg
+Launch C3: 91.0469816858646 km²/s²
+||V∞_in||: 5.897211117043296e-6 km/s
diff --git a/archive/ES_0.5623728522101891 b/archive/ES_0.5623728522101891
new file mode 100644
index 0000000..770149e
--- /dev/null
+++ b/archive/ES_0.5623728522101891
@@ -0,0 +1,22 @@
+archive/ES_0.5623728522101891---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:07:32.619
+Launch V∞: [6.510886339860942, -7.359429331068919, 0.12197102462142953] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.565404111211632e-9, -2.767019794274579e-10, -4.7544659625223295e-9] km/s
+ V∞_out: [-1.8047879582861169e-9, 3.9496944358316245e-9, 5.495595744216346e-9] km/s
+ time of flight: 1.8749577787050948e8 seconds
+ arrival date: 2029-04-08T21:17:09.619
+ thrust profile: [0.2829445262578122 -0.06941315176570785 -0.09232267936239706; 0.08098174828720642 0.023056380135066737 -0.08190182101876103; 0.10586824705762121 0.058112055406620525 -0.17463703912316622; 0.04828268651853028 0.03551057271174368 -0.11498411460204416; 0.05458790486027134 0.04890252666913847 -0.1645751802913047; 0.02213986944635059 0.022968627324023622 -0.08530251892249356; 0.010389883710042404 0.012456883596910275 -0.04959957900537971; 0.010519078213417112 0.011810342196566556 -0.055308067244603396; 0.0040308688258040935 0.00495613097315178 -0.01831542790226743; 0.005834003553881729 0.009415476617359421 -0.04224401597719038; 0.0018167388318414924 0.0009092197875453329 -0.010576800503825692; 0.001569740482994333 0.0009954021468159913 -0.006068321324107235; 0.0004436629299593654 0.0012475592374297092 -0.0017110551131416512; 0.0001644877762349596 -0.0009251641972524022 0.0001093524773256244; -0.0007078349267650513 -0.00013291212270967738 0.0007497440875786016; -0.0009698645292750159 -0.0013442737883673163 0.0008070991942932858; -0.0010312556161742564 -0.0005193665759756841 0.0026804549251629624; -0.0016789836904247445 0.00040820609941788987 0.00021623690407071051; -0.002643859000380827 9.19064141389537e-6 0.0007313231908045276; -0.0007018551981635264 0.003156956995027353 0.00038967146142965324] %
+
+Mass Used: 92.78997292603071 kg
+Launch C3: 96.56771794043254 km²/s²
+||V∞_in||: 7.32497327608052e-9 km/s
diff --git a/archive/ES_0.5623814812023203 b/archive/ES_0.5623814812023203
new file mode 100644
index 0000000..0a117cc
--- /dev/null
+++ b/archive/ES_0.5623814812023203
@@ -0,0 +1,22 @@
+archive/ES_0.5623814812023203---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:29:22.961
+Launch V∞: [6.485415672939127, -7.401286246389414, 0.10118971560522322] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6466548805401034e-7, 4.169750967526558e-8, -5.33624672156194e-8] km/s
+ V∞_out: [1.7102390553396315e-7, -4.584038309008118e-8, 2.1344353277898754e-8] km/s
+ time of flight: 1.8749577787493187e8 seconds
+ arrival date: 2029-04-10T20:38:59.961
+ thrust profile: [0.3427572546242974 -0.10357466261549995 -0.13445067375226122; 0.015960338351291528 0.0030282119428264634 -0.02077277947012274; 0.05839205099347911 0.022769033425191695 -0.12425223415760211; 0.07697223219459955 0.04002726890316361 -0.2329738653461281; 0.03283499767100848 0.018980124963593588 -0.12197581308753414; 0.021968793939524858 0.013844738498177548 -0.09657253754291371; 0.012498511251197516 0.008511217773762307 -0.06526885434252279; 0.008483279493518816 0.0062903472257943875 -0.05133769737984437; 0.004224331720792611 0.0032943828235193918 -0.02928076413360189; 0.0007777449247369638 0.0009781333152105022 -0.009443090132044302; 0.0011819817845100486 0.0010922734890957356 -0.006307936085258685; 0.0008854010346548479 -0.000684575022807902 -0.0016862033762117953; -0.00038960971584587256 -0.00048028578175512244 -0.0035185094195765293; 0.0005647171241190586 0.0005654801084237028 -0.004592557008489634; -0.0008816410868592859 -0.001655448843942294 -0.0003042672171243774; -0.003371571185280761 0.001371307519187944 0.0025791647696326355; -0.0011481110330164592 0.002373017806096775 0.003006723787739707; -0.000540154682435384 -0.002607791302269829 0.0028148459722645183; 0.002680867099735043 -0.0010858079101303854 -0.0026162603235110075; 0.0020256864868102393 1.8607030082445724e-5 -0.0021848468864500816] %
+
+Mass Used: 91.15401359237967 kg
+Launch C3: 96.84989391034183 km²/s²
+||V∞_in||: 1.7804762895507018e-7 km/s
diff --git a/archive/ES_0.5623835890035086 b/archive/ES_0.5623835890035086
new file mode 100644
index 0000000..e1a6e35
--- /dev/null
+++ b/archive/ES_0.5623835890035086
@@ -0,0 +1,22 @@
+archive/ES_0.5623835890035086---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T09:35:54.108
+Launch V∞: [6.4354245323275086, -7.384076353364498, 0.2906212045120477] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3387492899508132e-6, -2.0736474811050686e-6, -2.4051609536001275e-6] km/s
+ V∞_out: [-3.339478836010592e-6, -2.136304536290664e-6, -6.763288102180066e-8] km/s
+ time of flight: 1.8749577787487403e8 seconds
+ arrival date: 2029-04-08T11:45:31.108
+ thrust profile: [0.318198692598574 -0.06745125775167128 -0.09522766290296321; 0.09752936665451335 0.03574341084648275 -0.09423566863698217; 0.0867333430104219 0.05749258200846554 -0.13946059157827348; 0.05724764726828311 0.050352250687854254 -0.12437313372122619; 0.05175639942098089 0.05909627468463996 -0.15072708433876073; 0.01819647562775769 0.02323526628648427 -0.06683074832087935; 0.013092142263340982 0.0220795455567489 -0.062336075068356187; 0.011000120121187769 0.017139849905625518 -0.056391590962634804; 0.00866000358486382 0.017887796517142146 -0.05191855886605357; 0.0056271366104572226 0.011205367333058274 -0.0449993332636703; -2.1161482874730336e-5 -0.000630627151379289 -0.001335199199901187; 0.00041997900417584837 0.0013320441357879487 -0.004669118939546666; -0.0002989347007771853 -0.0007435608452957504 -0.0003145033981168776; 2.994854347885764e-5 -9.746698703031748e-5 0.00025140727203370897; 0.0003773814127505877 0.0008395574640850899 -0.0007510092823874016; 0.00029956492764534096 -0.00021728074187807306 0.00013073866932730585; -8.482595716668324e-5 -0.0003932397291499657 0.0008404801341806067; 0.0007514241705716936 0.0012429714203823663 -0.0007252244993596591; -0.0009756602220138018 0.000445206478885067 -9.497238214349938e-5; -0.0010141692942410346 -0.00023900914919745207 0.00021933171003558894] %
+
+Mass Used: 95.97574357344274 kg
+Launch C3: 96.02373318811152 km²/s²
+||V∞_in||: 3.943927145607726e-6 km/s
diff --git a/archive/ES_0.5623901152367882 b/archive/ES_0.5623901152367882
new file mode 100644
index 0000000..92f5fea
--- /dev/null
+++ b/archive/ES_0.5623901152367882
@@ -0,0 +1,22 @@
+archive/ES_0.5623901152367882---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T09:39:14.806
+Launch V∞: [6.329003028339492, -7.397617727942817, 0.14423451218644542] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.947487418475093e-7, 0.0002113927226540332, -0.00014010352094560188] km/s
+ V∞_out: [-0.00012807685698547664, -0.0002142102039271571, 4.475057500454035e-5] km/s
+ time of flight: 1.8749577787496182e8 seconds
+ arrival date: 2029-04-08T11:48:51.806
+ thrust profile: [0.4144213745048421 -0.08102842562577636 -0.11225628987362121; 0.0820375819311321 0.02804820588442612 -0.07575844661852414; 0.10172700820036046 0.06815715717969067 -0.14708151441359804; 0.06906553128358375 0.05902988793570194 -0.14854981383377178; 0.03598776171185312 0.03989286933364517 -0.10197255021079284; 0.034895950046913315 0.04089372036241859 -0.11057436644571983; 0.013752891569329479 0.01884116212260843 -0.05697245102451549; 0.007923832273735193 0.013607125452852795 -0.04241990807180692; 0.008664369631303598 0.01423366859795179 -0.05101704499750254; 0.0062965827140621594 0.010989816469281837 -0.03764294221829758; 0.0025504200949055507 0.00485119749812786 -0.01989852678448461; 1.2989382668328239e-5 9.681322105175669e-5 -0.0001674431398736763; -0.00021766507498304017 -0.00010739888709358857 -0.0008851971654125462; 0.00016079195088456065 -0.00017629447877917585 -0.00033709965275404753; -0.0002547072937789358 -0.000283011476502501 -0.00040585009902954647; 0.00017408505031600948 0.00013869385693611984 0.00016378272356397394; -0.00013132284819707173 0.00017948945895027559 0.00010547055069032578; 0.0009800326779366383 -0.0001886487996328301 0.00019047002446191024; 0.0001255648251015036 -0.0002173648443549598 -0.00014756477291466268; 0.00043656233871160335 -0.0003283118479496399 -8.22662303364465e-5] %
+
+Mass Used: 103.11112041619481 kg
+Launch C3: 94.80183097600995 km²/s²
+||V∞_in||: 0.0002536064539764429 km/s
diff --git a/archive/ES_0.5624094229945071 b/archive/ES_0.5624094229945071
new file mode 100644
index 0000000..874cd33
--- /dev/null
+++ b/archive/ES_0.5624094229945071
@@ -0,0 +1,22 @@
+archive/ES_0.5624094229945071---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T07:46:39.008
+Launch V∞: [6.607801932204872, -7.444767110723294, 0.19781323600649378] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.8295363707020416e-8, -7.261995818721477e-8, -5.1566527438357106e-8] km/s
+ V∞_out: [2.2541900939532018e-8, -5.0739531047589695e-8, 7.943848179411884e-8] km/s
+ time of flight: 1.8749577787456635e8 seconds
+ arrival date: 2029-04-11T09:56:16.008
+ thrust profile: [0.16405215253301342 -0.045589085917794994 -0.06574024900064879; 0.039308767038259404 0.008614682853546699 -0.04949397464939665; 0.039586043628175596 0.016646312151460747 -0.08352050043526775; 0.03582103366244943 0.019378818660896857 -0.10530455996668868; 0.037259892427525636 0.023647195698013698 -0.13663593934877333; 0.029329784471634503 0.020516005933133442 -0.12840422368818677; 0.018848247559404122 0.014655478178800651 -0.09983617692504357; 0.014157666209115842 0.011045991966577889 -0.08571522761140914; 0.005204531517932853 0.004306723739063294 -0.03454174957087538; 0.0065100581358877715 0.0061906229985744165 -0.05009863425881037; 0.0031191553513005934 0.002759995069933629 -0.02395811733599404; 0.00019661350287640127 6.307430193986925e-6 -0.0012117877166980301; 0.0002177704260875531 0.00014504982309730528 -0.0015618592534670467; 0.0016368218339111588 0.0006443054750643814 -0.0016522102039917166; -4.746152101245991e-6 0.00021022853003533249 -0.0006172391718942511; 7.417841884453724e-5 0.0001666987377140401 0.0008728656471582706; 0.00032611396153510127 -0.0004704332529351832 -0.0003703931089082998; -0.0022858785378190327 0.00040669329073832395 0.0009461004777768089; -0.00044487814494350257 0.0007865740136048699 -0.00019649217996567066; -0.0009513376420050088 -0.00039868607132219336 -0.0016468856111350539] %
+
+Mass Used: 77.90504641735879 kg
+Launch C3: 99.12673378449706 km²/s²
+||V∞_in||: 1.0131735900010937e-7 km/s
diff --git a/archive/ES_0.5624148539713744 b/archive/ES_0.5624148539713744
new file mode 100644
index 0000000..b85c208
--- /dev/null
+++ b/archive/ES_0.5624148539713744
@@ -0,0 +1,22 @@
+archive/ES_0.5624148539713744---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:01:59.978
+Launch V∞: [7.846568220018104, -5.4493476726190675, 0.43620536126999665] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.243991619379272e-7, -2.524402484618211e-6, -7.451198335615548e-6] km/s
+ V∞_out: [-7.161423820919739e-6, -8.144791255559506e-7, 3.248470532285109e-6] km/s
+ time of flight: 1.8749577787474334e8 seconds
+ arrival date: 2030-04-17T21:11:36.978
+ thrust profile: [0.7857580721379014 0.018200815700614128 -0.1515402176115129; 0.09654979264769296 0.06948876375398047 -0.0809313402205505; 0.05428649400016094 0.06634409754847008 -0.08620307611115605; 0.033004198681461774 0.0567406787310816 -0.08360406686554198; 0.031195806335007036 0.06837271668750279 -0.10811638092887291; 0.018478320880068656 0.054385249468055376 -0.09210096895291858; 0.01576940788482804 0.05481215963715036 -0.0965284557109233; 0.007207773029504825 0.03393726306469162 -0.0656909679326989; 0.0015709019188778182 0.008483646958690486 -0.017517869197613483; 0.0010265690507728512 0.006880007052856354 -0.015333357577589551; 6.182202372399155e-5 0.0005809883332762252 -0.0009336183424658438; 7.685646082189614e-5 0.00032401639264206025 -0.0007934147355630281; -3.584775805721041e-5 0.0004444719909680926 -0.0006514425783565665; 0.000561910751462423 0.0008725457431615352 -0.00047057823919089976; 8.510203851959647e-6 0.0002706358010855106 -0.00016135217865525804; -0.0001320810364548117 0.000433057849598849 -0.00015444948626134496; -0.00042569817779409386 0.0008218845975027779 5.8536709536220166e-5; -0.0002453928316535652 -0.0006921886666064342 0.001052518982388862; 6.811043055964254e-5 0.00011734784733903256 7.4630024198987874e-6; -0.00033170128152689294 0.0007564025333459323 2.6720401295527883e-5] %
+
+Mass Used: 122.66725793348405 kg
+Launch C3: 91.4542980056776 km²/s²
+||V∞_in||: 7.910284351351122e-6 km/s
diff --git a/archive/ES_0.5624271409078471 b/archive/ES_0.5624271409078471
new file mode 100644
index 0000000..c45334e
--- /dev/null
+++ b/archive/ES_0.5624271409078471
@@ -0,0 +1,22 @@
+archive/ES_0.5624271409078471---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T07:38:47.693
+Launch V∞: [6.35806280499022, -7.393699027732768, 0.1077221041866571] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4909247831287916e-8, 1.4038723325806545e-9, -1.280012081308483e-8] km/s
+ V∞_out: [-5.186750947401088e-9, 1.1290032137009995e-8, 1.593087079649861e-8] km/s
+ time of flight: 1.8749577787353182e8 seconds
+ arrival date: 2029-04-08T09:48:24.693
+ thrust profile: [0.36168879081281147 -0.07815953661799376 -0.10371515822148929; 0.15730581399273236 0.056231235648370965 -0.14002189959418562; 0.06782618548961829 0.0448222953137612 -0.10710703651987216; 0.040728375015249715 0.03654226506817235 -0.09263275530636479; 0.04138669640579472 0.04613136339904447 -0.11972220258055466; 0.032711196436651886 0.043066135644531184 -0.11800610247080323; 0.024176223498120545 0.03632511088729051 -0.10441953432114705; 0.013324695646195735 0.02224214371971189 -0.06852269159920477; 0.004891131541426154 0.008694334797943246 -0.028855942468144755; 0.0013720998437220116 0.002782428959622526 -0.009483942541811273; 0.0017498257999931455 0.0035113507599903882 -0.012184069974611657; 8.33292859546183e-6 0.000708781215215324 -0.0029515246880814318; -1.5505691501185273e-5 3.6235427245098154e-5 0.00042397896895483974; -0.00022204107305363375 -0.0006789019547230131 -0.00021274554025970733; 0.0007618907554837375 -0.00019539965089989325 -0.00018766039284053249; 6.293749283066918e-5 -0.00011914777808325012 -0.0003349311885939677; -0.00020044036567512752 -6.159194610194776e-5 0.0004096178652759564; 0.00026910657584398526 0.0013450976790253559 0.00013593522344835737; -0.0005140984261228431 0.00012353189662594707 -0.0008451670969334144; 0.00014332503296743697 -0.0008306030847064217 0.000868112442913626] %
+
+Mass Used: 101.39544441216412 kg
+Launch C3: 95.10335199662698 km²/s²
+||V∞_in||: 1.9700244192662087e-8 km/s
diff --git a/archive/ES_0.5624335745693289 b/archive/ES_0.5624335745693289
new file mode 100644
index 0000000..163b3be
--- /dev/null
+++ b/archive/ES_0.5624335745693289
@@ -0,0 +1,22 @@
+archive/ES_0.5624335745693289---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T18:21:23.057
+Launch V∞: [6.5009064662717355, -7.430695471307858, -0.23329174110111167] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.578668592943406e-9, -2.2865889628930774e-9, 3.7181258149894484e-9] km/s
+ V∞_out: [1.5638049763703976e-9, -3.574928850871229e-9, -5.077655496210555e-9] km/s
+ time of flight: 1.8749577787493923e8 seconds
+ arrival date: 2029-04-09T20:31:00.057
+ thrust profile: [0.2271012975869099 -0.05034670447990862 -0.08118346927837729; 0.08437049321989736 0.02682919090954252 -0.09003618746004947; 0.06370211651036116 0.0381203699434826 -0.11431930175868106; 0.04964035632302043 0.041296284931877356 -0.12984397703655928; 0.03201343418339252 0.031691448392556776 -0.10634964478852714; 0.018066482616521135 0.020280310803219 -0.07341012768316046; 0.018989838906316718 0.027895913190913408 -0.1016241266896726; 0.024802932675219578 0.03738727998938245 -0.13390947975960435; 0.0061087050049346515 0.008907595246980924 -0.039119932010734215; 0.0021234829149019206 0.004152263437348956 -0.01644398174951944; 0.0004821054993997104 0.0009391099933515975 -0.004087527646113285; 6.423665513717007e-5 0.00027107670998150347 -0.0012727454773349906; -0.00014587793663507856 -0.00036213508025415583 -0.0006623103050119369; 0.00035313074242798454 0.00038437373889585994 -0.000787143095980707; -2.573481955519535e-5 0.0005198153620157907 -0.0010249188290633545; 0.0005520125579533809 0.00024434952470782 -0.0001956763208420132; 0.00018636330952407493 -0.0009116710568144201 -0.001799031202231864; 0.0005622952432993661 -0.00011600339679043693 -0.0015324941444388202; -0.001070891424734209 2.2305695295498637e-5 -7.049152920395269e-5; -0.0008936574426329528 0.000279519354664409 -0.000404576560772126] %
+
+Mass Used: 87.23907387341433 kg
+Launch C3: 97.53144510699475 km²/s²
+||V∞_in||: 6.325911376657259e-9 km/s
diff --git a/archive/ES_0.5624450755760138 b/archive/ES_0.5624450755760138
new file mode 100644
index 0000000..26e4c74
--- /dev/null
+++ b/archive/ES_0.5624450755760138
@@ -0,0 +1,22 @@
+archive/ES_0.5624450755760138---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T04:58:27.841
+Launch V∞: [7.556442393578043, -5.556436488896454, 0.42860424290408583] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.459240895426147e-6, 9.635725008808251e-5, 2.009165639571236e-6] km/s
+ V∞_out: [9.29382501186356e-5, -1.6824499587062058e-5, 1.9821647143283475e-5] km/s
+ time of flight: 1.8555402101298147e8 seconds
+ arrival date: 2030-03-25T19:45:28.841
+ thrust profile: [0.9689225780525136 -0.003945288415358737 -0.22261205843420828; 0.20082372637784277 0.12626917305949967 -0.1761323956146839; 0.10387701598177503 0.10976812093452584 -0.16966281150581572; 0.05484128443768183 0.0794211940503968 -0.1384329397183942; 0.015755893476863958 0.02832411346895327 -0.05588578480672235; 0.007319321167306224 0.01627815696018028 -0.03425919507604468; 0.008343195701724758 0.02199990729135084 -0.04953221854721525; 0.0037050222927306397 0.0108233268605722 -0.026494042285687837; 0.00043496955260568203 0.002027744702140009 -0.005438573080293483; 0.000699719983481668 0.004914681816478906 -0.011424121415970096; -0.00012916350946970054 0.0017576407380242524 -0.005044285905749231; -0.00035337325119864785 0.0012187589673621126 -0.002707596426396417; -0.0018473031907892646 -0.0008701789671909425 -0.0022332112273183054; 0.00020932962193048486 0.0003406916713803653 -0.0006376028259448604; 0.00023451379246253504 0.0033576598015525165 -0.0023869296779393083; -0.0001726755818997258 0.00041044603422083127 -0.00018750288634638602; 3.152869814842568e-5 0.00027489701305678153 -0.0023573178465888882; 0.0005621029995671199 -1.719470421013687e-5 -0.0033126678495348583; 0.0008780188905891696 -0.0003323542314541501 -0.001727190493164668; 0.004443231667264915 -0.003611408919483622 -0.0006023506127200829] %
+
+Mass Used: 141.93378159078975 kg
+Launch C3: 88.1575096996388 km²/s²
+||V∞_in||: 9.659440037626227e-5 km/s
diff --git a/archive/ES_0.5624610035492756 b/archive/ES_0.5624610035492756
new file mode 100644
index 0000000..d032702
--- /dev/null
+++ b/archive/ES_0.5624610035492756
@@ -0,0 +1,22 @@
+archive/ES_0.5624610035492756---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T16:01:45.587
+Launch V∞: [7.69986397079527, -6.164610369393484, -0.01451197117133633] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.817888712759477e-6, -8.913466775565668e-6, -8.390111242032433e-7] km/s
+ V∞_out: [5.788255422068775e-7, -1.7112348418470138e-6, -1.1114125246880259e-5] km/s
+ time of flight: 1.748531963566791e8 seconds
+ arrival date: 2029-11-26T10:21:41.587
+ thrust profile: [0.248225601127563 -0.021240759075026507 -0.08812432878407396; 0.08413858082437378 0.037925227211746335 -0.09821567254110042; 0.06053104428009197 0.044312692965884005 -0.12135928102195694; 0.05373828062274237 0.052148499816631104 -0.1563375260843679; 0.02805354796854685 0.03371540728726618 -0.11082984532368091; 0.02487205821832796 0.03113829429032249 -0.1162106173991622; 0.012685283011186342 0.019864825498921726 -0.07756923264220701; 0.01634429970516649 0.02622152876659411 -0.10775070456046802; 0.00045782371835875724 0.004410015363757178 -0.012715968724484054; 0.00435928683265048 0.0046687069391959275 -0.03152740141628384; 0.0024757590996758007 -0.0007347536938122627 -0.0022471454828098605; 0.00033224608496489766 -0.0022170951351880345 -0.007973512266952702; -0.004151459327786438 0.008867777796344338 -0.0076919587336518516; 0.0010349944258564404 0.00383020491085181 0.0026361194163503033; -0.0017671201725871278 1.8972092832690015e-5 -0.006053755525053401; 0.004313332368219425 0.0036088340115871557 -0.0034882105006202764; -0.003799976097574642 0.0005537240030927611 -0.0066544391742942525; 0.0028340914955721514 0.0007251214919199844 0.0009968701841372714; 0.019276690417478686 -0.004660268265815887 0.009013560183932222; -0.0023244247746853296 0.0023255697615092615 -0.0005199697366407457] %
+
+Mass Used: 88.67637296795147 kg
+Launch C3: 97.29053677249203 km²/s²
+||V∞_in||: 1.1253330001613874e-5 km/s
diff --git a/archive/ES_0.5624665479624193 b/archive/ES_0.5624665479624193
new file mode 100644
index 0000000..f4b2c1d
--- /dev/null
+++ b/archive/ES_0.5624665479624193
@@ -0,0 +1,22 @@
+archive/ES_0.5624665479624193---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T04:10:53.187
+Launch V∞: [6.615342335614794, -7.268544843088928, 0.23628942563972924] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.285480373565859e-7, 3.782784579491801e-6, -2.2300183224206193e-7] km/s
+ V∞_out: [1.4152580650916575e-6, -3.0923111261399234e-6, 1.7504105201317744e-6] km/s
+ time of flight: 1.874957778748364e8 seconds
+ arrival date: 2029-04-07T06:20:30.187
+ thrust profile: [0.26353279341905167 -0.06130452640431156 -0.08442109756602142; 0.15629662607967815 0.049846971428119426 -0.14910226265596366; 0.05427418484924947 0.03271469265742192 -0.09146536096628746; 0.052588170823757226 0.04222253519501332 -0.1257540755244219; 0.049450892310829234 0.0492058764051679 -0.15011587748155059; 0.03309799433411858 0.04079678026980659 -0.12066842995178044; 0.014979835773977929 0.019568529899261347 -0.06725842281254939; 0.004237298208993997 0.006011682237733687 -0.022352790296653047; 0.008377893756611144 0.014560601273578947 -0.052904395351081414; 0.001624711499591387 0.0034623676296817716 -0.013268307631838996; 0.0010088490276314976 0.0020885948572696373 -0.009640395368826687; 0.0005230920337488438 0.0009874501713863617 -0.004346964478054158; 8.801854001831728e-5 -1.2012660244262101e-5 -0.00038138072112959057; -0.0003774498022127937 0.00011793230291262713 0.00018803989278758193; -4.81629239172043e-5 0.00013242681270814817 -0.00022140404841358474; 6.968372004420617e-5 2.4037061240023822e-5 6.537699485533225e-6; -0.00013808149231337452 -8.722506824146867e-5 -0.00024113899763419054; -6.673525744848587e-5 0.00011359622121398652 -0.00035185097592862986; -4.4801366410486804e-5 0.0006034841818329308 -0.00045175502605505224; 4.8830627704974755e-5 0.00014068163004901142 -4.546589904552443e-5] %
+
+Mass Used: 92.41737485424892 kg
+Launch C3: 96.6503310460412 km²/s²
+||V∞_in||: 3.8260360714214094e-6 km/s
diff --git a/archive/ES_0.5624689895455334 b/archive/ES_0.5624689895455334
new file mode 100644
index 0000000..146c4bc
--- /dev/null
+++ b/archive/ES_0.5624689895455334
@@ -0,0 +1,22 @@
+archive/ES_0.5624689895455334---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T01:29:20.019
+Launch V∞: [6.477991645017836, -7.366749580719851, 0.2054129994403212] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.2680316126121104e-6, 4.343810738768605e-6, 4.809957397853759e-6] km/s
+ V∞_out: [6.707613061870957e-6, 3.89917508189403e-6, 1.2546757403825792e-7] km/s
+ time of flight: 1.8749577787515467e8 seconds
+ arrival date: 2029-04-09T03:38:57.019
+ thrust profile: [0.3164119001883421 -0.0765574973557712 -0.10907227973583301; 0.09147432155469241 0.026065506977634358 -0.09799538242770044; 0.08339870579030442 0.04565567995884219 -0.14992885059916897; 0.053889081905709256 0.0394663165015497 -0.13672153035663256; 0.04920481504306529 0.0435399219438994 -0.1593415351352295; 0.025446323746826028 0.025830217239090285 -0.10258198755612509; 0.008385609295723472 0.010327923007865268 -0.04117006393272408; 0.005289318152821861 0.007844057883061166 -0.03179162143340798; 0.003484218735659084 0.006221789670240308 -0.026722421596938415; 0.0023349287996553276 0.004752922547627231 -0.0228379780803348; 0.0009331072170089469 0.0015364038964665074 -0.0067124627439980105; 0.001919850788532564 -0.0006570376245578278 -0.008626125044649503; -0.0003456311507007301 0.0006020448816854858 -0.0007335607633324154; -0.0006354998098596315 -0.0007988428429898096 0.0024513159369058384; 0.0006655852937207263 0.0008426450233024159 -0.007278189291499492; 0.002354523846818113 0.0016442158494707954 -0.008783204162655326; 0.0029105275029437903 -0.001526632969674046 -0.008417686874248391; -0.0006304595401858846 -7.861498754367299e-8 0.0014539338323125064; 0.00019203289903912404 -1.319495243751141e-5 0.0006829166920320638; -0.0006261111688555151 0.0003988049550400699 -0.0012869528366878428] %
+
+Mass Used: 94.6063315797287 kg
+Launch C3: 96.27556963829605 km²/s²
+||V∞_in||: 7.760185290936415e-6 km/s
diff --git a/archive/ES_0.5624741766215922 b/archive/ES_0.5624741766215922
new file mode 100644
index 0000000..6f91f34
--- /dev/null
+++ b/archive/ES_0.5624741766215922
@@ -0,0 +1,22 @@
+archive/ES_0.5624741766215922---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T09:55:31.653
+Launch V∞: [7.824396486542014, -5.736754702628618, 0.11872022319027403] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.5172201478112122e-6, -3.1787864588611214e-6, 2.26428611049874e-6] km/s
+ V∞_out: [-1.00796508630612e-6, -5.136617498275638e-6, 4.025031411818177e-7] km/s
+ time of flight: 1.8265571803253767e8 seconds
+ arrival date: 2030-02-23T11:37:29.653
+ thrust profile: [0.5123335997863377 -0.014420293660071765 -0.14868766851376955; 0.09728358154677805 0.053222608052251055 -0.1006110033363314; 0.03956712579460577 0.0349496053796428 -0.07492825706511268; 0.07071605939139859 0.08711335502199827 -0.19455574649629714; 0.0155664440693303 0.022655602589528662 -0.059617962977538574; 0.015050913864287252 0.025332690501516753 -0.07234042191366419; 0.01926147601932269 0.038725083251867326 -0.11518305040110942; 0.01061462321934871 0.02333031390150025 -0.07422714203698484; 0.002524886094916057 0.00261881666298384 -0.00730811121743565; 0.0011780464315616435 0.0027488594020584887 -0.006281408311329452; 0.0016686640309868735 -0.001732638484281998 -0.006740826540210222; 0.00951860034282593 0.008210394182126693 -0.008597167227333825; 6.920362466282819e-5 -0.0009440335663850254 0.0014365795290687336; -0.0021242875741941626 -0.0029892957031948933 -0.0044478790765586675; 0.0010412577895708693 0.0017446544686771305 0.0011187597610815506; -0.018650894359861652 0.005884871821356209 -0.0067355971623003965; -0.0014877828120615309 -0.0015277061719283565 0.000654439586202646; 0.012485353182402632 0.0006046174254514558 -0.042084828436100105; 0.00035361913323909673 -8.119585029271704e-5 -0.002922575176767697; -0.008262979463692626 -0.0005329394940909276 0.004897554042943194] %
+
+Mass Used: 107.03703462772546 kg
+Launch C3: 94.14562938813692 km²/s²
+||V∞_in||: 5.253809333179637e-6 km/s
diff --git a/archive/ES_0.5624742880470226 b/archive/ES_0.5624742880470226
new file mode 100644
index 0000000..19042dc
--- /dev/null
+++ b/archive/ES_0.5624742880470226
@@ -0,0 +1,22 @@
+archive/ES_0.5624742880470226---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T16:36:11.184
+Launch V∞: [7.6545339868106215, -6.213605009404769, -0.12390743567654716] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.016678558788284715, 0.10005785107426136, 0.11752507204437833] km/s
+ V∞_out: [-0.05967111088989711, 0.05059031383784263, -0.13407076099662613] km/s
+ time of flight: 1.6932170790746853e8 seconds
+ arrival date: 2029-09-21T10:24:38.184
+ thrust profile: [0.19691657559151476 -0.03643997555920107 -0.07118236606956288; 0.1629206400871216 0.04036098762802553 -0.1664486175291201; 0.09960207338674633 0.049607548145491794 -0.1830657121179268; 0.061087215578355364 0.04101191602215431 -0.16677101193995106; 0.03913121311053931 0.031090616740599177 -0.1415386028274726; 0.01832230009536771 0.01690052074236914 -0.08934989794210813; 0.016502473031431722 0.013151895769750377 -0.07624824416746004; 0.01156080512564125 0.010894827459828019 -0.0632187694460815; 0.0033388591027952866 0.004463795519172259 -0.030536944593192072; 0.0004342583937945565 0.0007677606057621296 -0.005022820062191551; 0.0014895257334003166 0.001985301322690922 -0.015439654001258737; -0.0006399021471740094 0.0017543340114457543 -0.00731083942582819; 0.0008346052847901476 0.00040075701851746313 -0.0012150836037963168; 5.56766679525424e-5 0.0006697503282727577 -0.0011632253346404759; -0.00308040342666459 -2.5477626576296002e-5 -0.0007398329104895214; 0.0002771818854365282 0.0031125196044457883 0.003931410576383814; 0.00018958122299419746 0.004181288480711 -0.0003891416346901858; -0.00017119895412217234 -0.0010679332242324773 -0.00019114572506310394; -0.0004340972091016876 -0.004780573354527016 -0.00641040433310412; -0.0002193014020523491 -0.0034396467776542814 0.004434202358053486] %
+
+Mass Used: 89.1259062671229 kg
+Launch C3: 97.21613082075488 km²/s²
+||V∞_in||: 0.1552478355529946 km/s
diff --git a/archive/ES_0.562474993128272 b/archive/ES_0.562474993128272
new file mode 100644
index 0000000..d18eddd
--- /dev/null
+++ b/archive/ES_0.562474993128272
@@ -0,0 +1,22 @@
+archive/ES_0.562474993128272---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T11:54:23.949
+Launch V∞: [6.47502669307198, -7.247748387945566, 0.19097403016063483] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.546877020763718e-7, -4.806251051031503e-8, 6.066737509177547e-8] km/s
+ V∞_out: [-3.5914830572844625e-7, 3.2483828857808794e-8, -4.280850964367328e-8] km/s
+ time of flight: 1.8749577787402982e8 seconds
+ arrival date: 2029-04-07T14:04:00.949
+ thrust profile: [0.48635407047409085 -0.11772519143797916 -0.15762390645123256; 0.09303059048661974 0.02816562925631432 -0.09761574763961246; 0.042531557089322776 0.024280598483340694 -0.07759444824452058; 0.0769599327373024 0.06049152714967825 -0.18888724819963884; 0.03057511422878193 0.02926594963076632 -0.10107349729861594; 0.021165840234082026 0.02330221098733568 -0.0863165386365188; 0.015003162286321611 0.018139657088056666 -0.07300516795292587; 0.008963191270424095 0.011360428418142443 -0.049412011642336905; 0.008245656284095558 0.012327497402919368 -0.053544736785387875; 0.00243220699906058 0.0037770408535337387 -0.01798933672211468; 0.000938668920640557 0.003228855685969207 -0.013098100356620897; 0.0011307123034823127 0.003844970927854385 -0.01691613404377452; 0.00044434512424736014 0.00036115314254395506 0.00045064567469393994; 0.00019331322534596836 -0.00020344310137539412 -1.3225110148498025e-5; 0.0004036479765410811 -0.0006538980146586281 -0.0003462432589161361; 0.00011698776708071691 -0.0001346894955858546 0.00014947119609159737; -3.5051673866665424e-5 2.7114661271083604e-5 -0.00030992117836254994; 0.0005105515573996006 -3.299477492578137e-5 3.26293135501978e-5; -0.000723730749408216 0.0009746934513747293 0.0006108567605821424; -0.0002290739368681437 -3.69204180341308e-5 0.0007437489715865404] %
+
+Mass Used: 105.01575101789558 kg
+Launch C3: 94.492298451158 km²/s²
+||V∞_in||: 3.630342977203358e-7 km/s
diff --git a/archive/ES_0.5624770444150198 b/archive/ES_0.5624770444150198
new file mode 100644
index 0000000..3af81dc
--- /dev/null
+++ b/archive/ES_0.5624770444150198
@@ -0,0 +1,22 @@
+archive/ES_0.5624770444150198---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:14:17.974
+Launch V∞: [6.505377313828419, -7.375778090388343, 0.18620660897509694] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9239329840975577e-5, -2.8305316002230192e-6, 4.9630728465172736e-8] km/s
+ V∞_out: [3.7247482984060673e-6, -8.40649408503162e-8, -1.9085245778104873e-5] km/s
+ time of flight: 1.8749577787490153e8 seconds
+ arrival date: 2029-04-09T06:23:54.974
+ thrust profile: [0.25385666204160545 -0.06269763985892908 -0.08608780638886614; 0.1405791353108641 0.0367793351859259 -0.14352550880055048; 0.07335820893864742 0.03770829797376431 -0.12964949277167173; 0.047907188619815834 0.032783450508983354 -0.12021266827381259; 0.03850131395372804 0.032866496453332825 -0.1246727029903094; 0.026663534486245356 0.024789301870509706 -0.10334457869774519; 0.015261862116982309 0.016849723284038203 -0.07436841141549545; 0.008086008749655081 0.00926670749852496 -0.045184302860820494; 0.0013666594009747392 0.0016037495072631443 -0.009024825064512434; 0.006980729285886089 0.0093417698309214 -0.04781654103164112; 0.0007980980117649344 0.0006548152729008653 -0.0038218510047591694; -3.2367920274919905e-5 0.0006132412276146858 -0.004000606336212768; 0.00019988485577649535 0.0004948524803658288 -0.004060082744678712; -0.0005841186213519629 0.0026318373892078965 -0.0016664566965577023; -0.0021330272404725937 0.0031566832855406636 -0.0030747463355029325; 0.0015625570758160648 -0.0015411195322179965 -0.004304432862540517; 0.0023749853897160576 0.0009970544444068109 -0.0015083135350562062; 0.0006993221491002269 -0.0020076497997356803 -0.0015099364399851994; 0.00037773052674642377 -0.0003104405094289829 -0.0006543421520914491; -0.00013878434670003753 0.001131571272966187 0.004254974715275768] %
+
+Mass Used: 91.8090806958021 kg
+Launch C3: 96.75670933515218 km²/s²
+||V∞_in||: 1.944649544465332e-5 km/s
diff --git a/archive/ES_0.562479126397135 b/archive/ES_0.562479126397135
new file mode 100644
index 0000000..7772a87
--- /dev/null
+++ b/archive/ES_0.562479126397135
@@ -0,0 +1,22 @@
+archive/ES_0.562479126397135---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T08:28:07.993
+Launch V∞: [7.764085139695784, -5.97859959894564, 0.07866096695182498] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.191474300543822e-10, -8.16726780701857e-10, -1.0500437615660537e-9] km/s
+ V∞_out: [-1.8643871304880268e-10, 1.6995755093789224e-10, -6.081296314115122e-11] km/s
+ time of flight: 1.8161935035869303e8 seconds
+ arrival date: 2030-02-14T10:17:17.993
+ thrust profile: [0.38095057901431933 -0.022562273265493985 -0.12347506056958787; 0.07915515990975959 0.03775604748005744 -0.092707404852606; 0.04626985652291045 0.03501061728039756 -0.0916147583643218; 0.036056866873460734 0.03543895506226574 -0.10616540224205306; 0.03502943608647326 0.04127005640708275 -0.1388206585662737; 0.02619128258789202 0.034814429066505365 -0.12740969417276815; 0.013265603810359015 0.01986777084658274 -0.07820851760365913; 0.009939825140753384 0.017139992528562364 -0.07495915402160594; 0.0016680344749501882 0.0025829157577400693 -0.010129287105515014; 0.008573585355391473 -0.000617147535182056 -0.008889621782507986; -0.0008220019558695061 0.003307540246723863 -0.00880306915314656; -0.0016546097601303003 0.002519722738095669 -0.004137194248860113; 0.003710012519816253 -0.0039199977469294225 -0.004907539632069891; 0.0008270984783504032 0.0009697027160980085 -0.005537966300255611; 0.009123158143954922 -0.0070430734684154145 -0.004117946605101126; -0.0028728530194373587 0.00013768126295739377 -0.0013568576781048556; -0.009190486894080016 0.01875108254104167 0.001526706818286084; -0.019331869291698008 0.0021972437657099254 0.002999795860791809; 0.007512535875717367 0.0037992890828162304 -0.0022748538784879728; 0.0018287543558354968 0.014957649874443563 0.0012643689425296] %
+
+Mass Used: 96.04563797935953 kg
+Launch C3: 96.03085876867966 km²/s²
+||V∞_in||: 1.4673029938163257e-9 km/s
diff --git a/archive/ES_0.5624840592485221 b/archive/ES_0.5624840592485221
new file mode 100644
index 0000000..c2a98a5
--- /dev/null
+++ b/archive/ES_0.5624840592485221
@@ -0,0 +1,22 @@
+archive/ES_0.5624840592485221---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:15:55.298
+Launch V∞: [6.417233278252971, -7.421313186148262, 0.24638263511075312] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.0088509441125115e-5, -6.222985159190491e-6, 1.0628052471563625e-7] km/s
+ V∞_out: [1.720291057781452e-5, -3.884579330081208e-7, -3.673333912473193e-5] km/s
+ time of flight: 1.8749577787526786e8 seconds
+ arrival date: 2029-04-08T21:25:32.298
+ thrust profile: [0.226386875280917 -0.05111704474789963 -0.07220238964922482; 0.23028507753299832 0.0733213687124709 -0.20646814849824172; 0.057300796724559344 0.03551350280964213 -0.09808819543039911; 0.04854149921440361 0.04020815320062011 -0.11481015033574629; 0.03918928774358266 0.040923762261498624 -0.12299248308923966; 0.03205517963870322 0.03886111504457008 -0.12277882562913786; 0.014745801629969071 0.019414477393655497 -0.06374908838902354; 0.007873947195862098 0.013928034848389687 -0.050390884868499096; 0.006630003814476035 0.009436862686909705 -0.035791275696156116; 0.0008577992581337947 0.001301099388439206 -0.005332335695591099; 9.835979496551227e-6 0.00031527507943058484 -0.0013294810007155266; 1.9614341269017215e-6 0.0008033012845586767 -0.003877303894977166; -0.0019439067519396863 0.0015955904565846672 -0.0008568937519783555; 0.00039359273839980317 -7.003370352591434e-5 0.0017175529568249281; -0.001399363559439086 9.58787691450315e-5 -0.0011620461347778088; -0.0002780666465501542 -0.0006233831505438939 0.0013903647181256456; 0.00023826538747852679 0.0002624773375366503 -0.000422579532351151; -0.0014948720909783273 0.0006434984802858234 -0.0007955846910933143; -0.0010090654077127073 0.0005632907571214771 -0.000198365691736189; 0.001862881797251292 -0.0034273198599577793 0.001453131188161987] %
+
+Mass Used: 94.37945470569503 kg
+Launch C3: 96.31747675729954 km²/s²
+||V∞_in||: 4.056877406395979e-5 km/s
diff --git a/archive/ES_0.5624989423538167 b/archive/ES_0.5624989423538167
new file mode 100644
index 0000000..59469cb
--- /dev/null
+++ b/archive/ES_0.5624989423538167
@@ -0,0 +1,22 @@
+archive/ES_0.5624989423538167---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T21:12:32.324
+Launch V∞: [6.513114762320057, -7.463953934913978, 0.1859439381831087] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.316204368127439e-6, 4.1735553538676255e-6, 4.844313279529403e-6] km/s
+ V∞_out: [6.43257282693189e-6, 4.256614393877074e-6, 1.5086104159405055e-7] km/s
+ time of flight: 1.8353695539817083e8 seconds
+ arrival date: 2029-02-22T03:41:47.324
+ thrust profile: [0.21317491471510075 -0.06229395613773833 -0.07940076174166129; 0.021291590834692595 0.004490438208634555 -0.025108403921017895; 0.06788369572747571 0.030191089739782455 -0.1276974257438681; 0.05601098014271953 0.033482657689394894 -0.146453644931716; 0.047309378460901864 0.0338630308302544 -0.15731089089216455; 0.037390980042361154 0.030372343987206007 -0.15072536637745163; 0.01540558281930896 0.013693073048598275 -0.07431284895797785; 0.008682421137620203 0.008228903260804875 -0.04812275982346394; 0.004568843898098114 0.00456618001922739 -0.028738532475996784; 0.007338506692526304 0.007793613390244167 -0.04932287207318788; 0.002022230952246362 0.0021816571610006174 -0.013845957991670236; 0.00020696707412351653 1.979823262693377e-5 -0.0016328705339009259; 0.0012514057141636557 -0.00014126208962748297 -0.0028725515708376854; 0.0002563547853994605 6.153281503670625e-5 -0.0011532669118436522; -0.00090198382072105 0.0023459618187470473 -0.0011877352270692127; 5.0448616446754566e-5 -0.00011701969707143844 -0.001886971819526469; 0.00013869821520981257 -0.0010620438849940953 -0.0006948379717578684; -0.0009297167730377544 -0.0016126871557369847 -0.0006580701035986466; 0.0007445880288685402 0.0004467911073203005 -0.004544137968190991; -0.0006641235483207195 -0.000810086354436365 0.0013223781671552995] %
+
+Mass Used: 83.6146562588574 kg
+Launch C3: 98.16584739781635 km²/s²
+||V∞_in||: 7.714632563477306e-6 km/s
diff --git a/archive/ES_0.5625155224971317 b/archive/ES_0.5625155224971317
new file mode 100644
index 0000000..2da82d5
--- /dev/null
+++ b/archive/ES_0.5625155224971317
@@ -0,0 +1,22 @@
+archive/ES_0.5625155224971317---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T23:48:40.753
+Launch V∞: [6.554685652830953, -7.469547435983097, 0.06424346021519765] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0026682189534927786, -0.017311645385599067, 0.02208719935541121] km/s
+ V∞_out: [-0.01895057926055391, -0.015790089693678417, -0.011788026329954394] km/s
+ time of flight: 1.8749577787574357e8 seconds
+ arrival date: 2029-04-11T01:58:17.753
+ thrust profile: [0.1631914021214648 -0.040775014505725106 -0.05979704662905804; 0.06268223728035491 0.015156517184521292 -0.06677992756345859; 0.04171537454331339 0.022525906953437255 -0.08065556744470476; 0.047802973479428586 0.032758380775045046 -0.12577617639006217; 0.023909702455197992 0.020505943459432508 -0.08484171056947379; 0.023077004154945624 0.0179068762004913 -0.09825348388749744; 0.029030505041949213 0.030475380229601296 -0.13651043640741756; 0.013190404312347595 0.013455122095807215 -0.0640911363842322; 0.017086508547807022 0.021314083126837406 -0.10748065351723704; 0.0029457611164076846 0.004127500683055917 -0.021381013771454266; 0.0036493554599159794 0.0053836004340372685 -0.02402915226835358; 0.0006803125333743616 0.0005073993193997059 -0.003859109325374627; 0.00014653335444277392 9.580030334373365e-5 -0.0005535374861641047; -0.0005614224017531852 -0.00018629735842620685 0.0006031629033328632; -0.0003368254399734657 -0.0006034864591082933 8.212178351064503e-5; 0.0002481010723311225 8.326251082592989e-5 0.0009039590424418992; -0.0004363796350811221 -0.0003646869189532025 0.00025043347025375775; 0.0002432716605917738 -0.0002273399976123525 0.000972794326154958; 8.381247792134925e-5 8.206979011644725e-5 -4.451435257588425e-5; 0.0005693764843239954 7.238888565680634e-5 0.0008302550805978233] %
+
+Mass Used: 80.15545049992852 kg
+Launch C3: 98.76217012801001 km²/s²
+||V∞_in||: 0.02818965827579662 km/s
diff --git a/archive/ES_0.5625171412182381 b/archive/ES_0.5625171412182381
new file mode 100644
index 0000000..74269f9
--- /dev/null
+++ b/archive/ES_0.5625171412182381
@@ -0,0 +1,22 @@
+archive/ES_0.5625171412182381---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T22:31:37.720
+Launch V∞: [6.35484937022314, -7.567090349025424, 0.21725481725034315] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.980038395939623e-9, 7.640725610683358e-9, 4.169134637411801e-9] km/s
+ V∞_out: [-3.040492851951531e-9, 5.862192942527976e-9, -9.18625438770528e-9] km/s
+ time of flight: 1.8423345298937756e8 seconds
+ arrival date: 2029-03-04T06:29:09.720
+ thrust profile: [0.28473280530988987 -0.08570457490322443 -0.11280729225097554; 0.02472663537868366 0.0042474481281961785 -0.030994298640286345; 0.0436589381681385 0.016278020839658514 -0.08979421526722862; 0.055148821141146984 0.027383253681920076 -0.1550780161387622; 0.04743606870014418 0.027720540837525218 -0.1688799409611087; 0.035175147460362884 0.022908868636938026 -0.15157384426705495; 0.023943254512457757 0.016704627363319676 -0.12082293472838851; 0.004072021393333478 0.0029488043309198277 -0.024394575810619407; 0.003857750248198482 0.002918718187991666 -0.025601408192629856; 0.004049573019395152 0.0032692562275945564 -0.029684409517436224; 0.0010574850098359332 0.0008848568875722695 -0.004528653316358638; -0.00012021727777657381 -0.00021851701283080006 -0.0012183193664178796; -0.0002665457218355952 -0.00024973105796316486 0.0021006355547283674; 7.67507630460544e-5 0.0002273314114321363 0.0002358365318149584; -0.0002299121663674563 0.00022152062802694445 0.0006989418751448572; 0.00019135740208464983 0.00044084247549741287 0.00035880587950497755; -0.00022062361440275082 -2.934358751061574e-5 -5.389761594863196e-8; 3.2018358601994877e-6 -0.00012361157627883905 3.640796771461286e-5; -0.00012970260457025224 0.00022387422473806688 1.2016869202077177e-5; -0.0008962003112473521 4.7896586285286504e-5 -0.0006695406953142211] %
+
+Mass Used: 86.39902669702496 kg
+Launch C3: 97.69216652415764 km²/s²
+||V∞_in||: 9.570949645451754e-9 km/s
diff --git a/archive/ES_0.5625204760586587 b/archive/ES_0.5625204760586587
new file mode 100644
index 0000000..5e66b4e
--- /dev/null
+++ b/archive/ES_0.5625204760586587
@@ -0,0 +1,22 @@
+archive/ES_0.5625204760586587---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T06:54:54.399
+Launch V∞: [6.4365985709422295, -7.276828958833714, 0.18562255342553458] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.016947611449583372, -0.007869645407861139, 0.018530241656066898] km/s
+ V∞_out: [-0.01696733331685169, -0.006961520131736909, -0.018871554122677946] km/s
+ time of flight: 1.8582048878582463e8 seconds
+ arrival date: 2029-03-18T23:43:02.399
+ thrust profile: [0.5005836604975353 -0.13677436428694678 -0.17142219465103795; 0.06682118843809433 0.017197493012490097 -0.0721470060228193; 0.07656438506011366 0.038959018886124464 -0.13873684558766167; 0.049599103321829055 0.03402669110207752 -0.12663553007012646; 0.03797706589129864 0.031581176847060285 -0.1247420370194791; 0.03355929760715747 0.03211718080013489 -0.1344493808232169; 0.013879136750289726 0.015012315016201098 -0.06688062925136803; 0.00794910199827897 0.009668719298698971 -0.044451100006264045; 0.0037211294204173634 0.005286259329530579 -0.02457796396664019; 0.0014750695134810978 0.002299537538818497 -0.011853380535807985; 0.004137973913918188 0.005429089399611735 -0.029563205687233376; 0.00020832493945479883 -3.293994192722719e-5 -0.001861944051021873; 0.000723018021380433 -0.0015370176890273912 -0.0022052902545520356; -8.181797161349916e-5 0.0003158574034830708 -0.001428931415734694; 7.464820871236485e-5 0.000121464196763734 0.00010225871342369722; 0.00015590267465564057 0.00014673585832320125 -0.001126023962522177; 0.00017949023098401407 0.00033735524560409035 -0.00139851204962196; -0.0027709107437511697 -0.0011212679942628838 -0.0013233210236246358; 0.0015372618369416747 0.00020226098783817213 -0.0008238925308304955; -0.0015615167259400806 0.0004942580708711523 -0.0009518343196864051] %
+
+Mass Used: 105.51099194892095 kg
+Launch C3: 94.41649659191673 km²/s²
+||V∞_in||: 0.02631582619876785 km/s
diff --git a/archive/ES_0.5625231428769984 b/archive/ES_0.5625231428769984
new file mode 100644
index 0000000..90e9114
--- /dev/null
+++ b/archive/ES_0.5625231428769984
@@ -0,0 +1,22 @@
+archive/ES_0.5625231428769984---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T21:33:09.871
+Launch V∞: [6.603777385914259, -7.310235043739302, 0.16055099144389504] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.020734315489317513, -0.007604164590646158, 0.018760824959449838] km/s
+ V∞_out: [-0.018984003984887702, -0.007658881645868126, -0.020509711717861943] km/s
+ time of flight: 1.8749577787493852e8 seconds
+ arrival date: 2029-04-08T23:42:46.871
+ thrust profile: [0.30708915124922964 -0.07796718009055707 -0.10793241884015166; 0.038837776853699664 0.010753502397250488 -0.04493487461818058; 0.039580407122698204 0.02093155852124455 -0.07657519530154985; 0.06632375614843093 0.04791255251767187 -0.17136354720752928; 0.04357974673438553 0.03835744453704729 -0.14701212200429342; 0.022656788019282274 0.022322974085887876 -0.09615451040544627; 0.017097765108860307 0.018980228510629218 -0.08576645113215453; 0.012918756217061848 0.01550904807911245 -0.0745513680674558; 0.0055450241666790984 0.007405345478171315 -0.036211585304441185; 0.0017978465144952772 0.003026540534147932 -0.015469945145255277; 0.004496523637541865 0.005526369274950899 -0.031340032058310874; -1.2857464195269153e-5 -0.00027497700671576204 -0.0013635061475210611; 0.00022632226294858784 0.0005503929496370934 -0.0018069038710284465; -0.00010150504464836702 -0.0016862874754251253 0.0014379760326249233; -9.258529549046814e-5 0.0007782715346243868 0.0014086806723323066; 0.0006616566750789659 -0.0001475737625301965 -0.0007243250809431641; 0.001956641025097891 -0.00341289419153628 0.0021963991519230053; 0.00033087684252064366 -0.0009855303408849458 0.002970003132698371; -0.0007267523026960585 0.00041697219452618134 -0.0005368501018982822; -0.002606480110707309 -2.1860283999677722e-5 -0.002584721450796171] %
+
+Mass Used: 90.00506548319618 kg
+Launch C3: 97.07518877828035 km²/s²
+||V∞_in||: 0.028977641572276117 km/s
diff --git a/archive/ES_0.5625388735637512 b/archive/ES_0.5625388735637512
new file mode 100644
index 0000000..5fe9d71
--- /dev/null
+++ b/archive/ES_0.5625388735637512
@@ -0,0 +1,22 @@
+archive/ES_0.5625388735637512---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T11:01:17.778
+Launch V∞: [7.891747630086179, -5.8593826269598885, 0.28905160168076227] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.361022166643113e-8, 4.3429052195469585e-7, -9.751252400419689e-6] km/s
+ V∞_out: [-4.3016171025285537e-7, 9.745735304539037e-6, -1.5441000503710304e-7] km/s
+ time of flight: 1.8749577787421045e8 seconds
+ arrival date: 2030-04-25T13:10:54.778
+ thrust profile: [0.35718832214644053 -0.006038855657089107 -0.1127081959635747; 0.060584849641675334 0.031186151693250504 -0.06939818499366028; 0.05113144734673074 0.041045338594818646 -0.10576172077769183; 0.03175976712162205 0.03241708088251211 -0.09540290295059946; 0.03054411987168462 0.03747154422409211 -0.12130935424375536; 0.02655150526186698 0.03783980819478657 -0.13498836524833088; 0.009947425885258878 0.014807512162447817 -0.05976995070458979; 0.005945246944019008 0.010847843904844516 -0.046326985038285425; -0.00033215267830932435 0.007610377478384213 -0.011337581982426336; 0.003388805165261554 0.0003361920925017769 -0.022627820641741944; 0.002505010266986771 0.003169360615495394 -0.01624981502623041; 0.0011828876670420764 0.0006672524042511742 -0.005208084535834873; -0.0018117740249531107 0.010244098040681953 -0.0005919581662603871; 8.090334427294978e-5 4.4615207741818125e-5 -0.00015796788514587593; -0.0013877766913269962 -0.0005153797359032149 0.0006709729613509018; -0.006790800809837702 0.0012430745739155865 0.0010712089136502919; -0.0007969124820845139 0.0017773171290727783 -0.0045812217544738175; -0.003114601450401076 0.005005410661131795 0.004072592636279599; 0.010215589164139723 0.01862439504994759 0.00930877052190923; 0.01643968200985535 -0.02465287318679734 0.02164885844392598] %
+
+Mass Used: 92.23770767298402 kg
+Launch C3: 96.6955962545244 km²/s²
+||V∞_in||: 9.761125851788352e-6 km/s
diff --git a/archive/ES_0.5625420168253095 b/archive/ES_0.5625420168253095
new file mode 100644
index 0000000..c7f6d72
--- /dev/null
+++ b/archive/ES_0.5625420168253095
@@ -0,0 +1,22 @@
+archive/ES_0.5625420168253095---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T19:46:19.774
+Launch V∞: [6.647852300183904, -7.431802246901744, 0.012604394576746517] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01260509784128854, -0.00034835175788381766, 0.008384320079346511] km/s
+ V∞_out: [-0.014497410497736252, 0.00014689464085062876, 0.00436970859420937] km/s
+ time of flight: 1.8749577787493953e8 seconds
+ arrival date: 2029-04-10T21:55:56.774
+ thrust profile: [0.11523709406125515 -0.03097067860127594 -0.04716674040424291; 0.04658707954750199 0.010955452763120745 -0.06026175304302694; 0.05121920665058666 0.024009994729225458 -0.10698568821549001; 0.04786182214452747 0.029922549052594845 -0.1380686040481141; 0.0408275395466004 0.030648716821679536 -0.15035280989034727; 0.022576767924948775 0.019989694482260605 -0.10613167182483951; 0.01769132787887328 0.015530233770797127 -0.08782646188310604; 0.0085760012337997 0.009326284252555996 -0.056944731579471546; 0.006619347842050665 0.006889880142762974 -0.04562771976588038; 0.003769455554889456 0.004396170061521418 -0.030293691456195013; 0.0016757301645911964 0.0006169069456166893 -0.007040205381135622; 0.00022159489287047187 0.002738117741933923 -0.017877566688584832; 0.002205232785644427 0.0015793890045801553 -0.0015970729204363091; 0.002507469674508368 -6.156747767817295e-5 -0.00549250662663923; 0.0005114466034614088 0.001567982745587477 -0.00245368182128227; -0.0010030710805153291 -0.0009736357756625269 -0.000295765258599577; -0.0009847301511999016 -0.0007387339938285155 -0.0022680413186748688; 1.9389373778041477e-5 0.0009189553034825669 -0.00013298533526010718; 0.0006079912695258261 0.000395912673991343 -0.0028694754955645653; -0.0026708811159900907 -0.0018661130319799454 -0.004442157473395403] %
+
+Mass Used: 76.31528130441257 kg
+Launch C3: 99.42578371287688 km²/s²
+||V∞_in||: 0.015142875015287249 km/s
diff --git a/archive/ES_0.5625427973691797 b/archive/ES_0.5625427973691797
new file mode 100644
index 0000000..0134111
--- /dev/null
+++ b/archive/ES_0.5625427973691797
@@ -0,0 +1,22 @@
+archive/ES_0.5625427973691797---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:44:01.713
+Launch V∞: [6.684671218632711, -7.338655296183937, 0.16797875602360418] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.176449417747467e-7, 0.00029582124085957896, -0.00018760820041496652] km/s
+ V∞_out: [-0.00017253442296262766, -0.00029785651676800853, 6.482893033253052e-5] km/s
+ time of flight: 1.8749577787490368e8 seconds
+ arrival date: 2029-04-09T06:53:38.713
+ thrust profile: [0.1527179734961824 -0.038539721791702834 -0.05562892588182978; 0.10124510948686885 0.02686136655806482 -0.11313250678574856; 0.043342935322881956 0.022479843455947526 -0.08314507939058323; 0.04723958480371111 0.032821018438694456 -0.12413174148590064; 0.03410802246555877 0.028541387642009076 -0.11609400157426343; 0.019118149476968938 0.018308631370021783 -0.0811962010547189; 0.019837962550251338 0.02123547871904843 -0.09953774668985876; 0.018145477398337242 0.02072952830923932 -0.1003858300433609; 0.005599657124559718 0.007041731026525666 -0.0372049855997856; 0.00528270023973078 0.006569694131957652 -0.03661781763299287; 0.003497846169062332 0.005042313710931727 -0.024863794844001495; 4.8414503615853977e-5 0.0007785871152381517 -0.0028457065526761678; 0.0001963037968571025 -0.0001506110563378802 -0.0014599311519122309; 0.0004680521535994122 0.00031626044975160343 -0.0013680054789231113; 6.338727273990688e-5 0.0005881853513526163 -0.0010703186032310831; 2.370296439970865e-5 -0.00017834404334501658 0.001231809721140475; 0.00018129583097403187 -0.001902660061905003 -0.0010734089969159312; -0.0015293935782169149 6.349547072761845e-5 0.0006287069511543968; 0.0019492278220881946 0.000357132049647514 0.0003776328307884068; -0.00011660740970396142 -0.000932659112938147 -0.001134206639606466] %
+
+Mass Used: 81.31463523129105 kg
+Launch C3: 98.56890771990032 km²/s²
+||V∞_in||: 0.0003502966056785222 km/s
diff --git a/archive/ES_0.5625432579358421 b/archive/ES_0.5625432579358421
new file mode 100644
index 0000000..6d9a528
--- /dev/null
+++ b/archive/ES_0.5625432579358421
@@ -0,0 +1,22 @@
+archive/ES_0.5625432579358421---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T20:34:02.482
+Launch V∞: [6.529758138860604, -7.470035648322979, 0.0923251343244855] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010602495466146838, -0.00031689246404703326, 0.007181067728431393] km/s
+ V∞_out: [-0.01230499626477287, 0.00012174193320246898, 0.003553579682653246] km/s
+ time of flight: 1.8558575305506644e8 seconds
+ arrival date: 2029-03-18T20:09:55.482
+ thrust profile: [0.18349409537354733 -0.04660132317060512 -0.06937190807387766; 0.05597379608446008 0.014924964428276732 -0.06436388308024131; 0.05485487830349511 0.028201948202873615 -0.10440874095773675; 0.03536938904773916 0.02442567346107579 -0.09461340734777936; 0.03061756160329426 0.026190819876215576 -0.10467449376495001; 0.0289440220689395 0.027637127689944946 -0.1197345875554408; 0.012070156950865897 0.012272014326629051 -0.05837075234480191; 0.031517713072339304 0.039835653304632686 -0.17707333478500173; 0.004417156783336599 0.005430294687640206 -0.02802149901702616; 0.009452261861677755 0.012404333055633621 -0.06383735858946375; 0.0011213444929764776 0.001425277882831407 -0.008529548216180802; 0.0002883061691565401 0.0004266631447931493 -0.002613603296018429; -0.0004023550664072228 0.00016717269475592482 -0.0007873376532618431; -0.0001564978124965515 0.0002651262896581913 -0.0003825218757592607; 0.0001941661827679644 -0.0006004342673008097 -0.0007446304691636348; -0.0007384214762207996 0.0008802913826488676 -0.0009580430607426351; -0.0001973957620014263 -0.0007605410171996494 -0.0008924854730075554; 4.4185101657975086e-5 0.0001313749133011957 -0.0004576090800271287; 0.00033396934789516487 0.0001306059793065947 -0.0008128358078763161; -7.928924459571382e-5 -4.675893298005746e-5 -0.0006372024999133207] %
+
+Mass Used: 82.02223001879656 kg
+Launch C3: 98.44769786966044 km²/s²
+||V∞_in||: 0.012809413127218314 km/s
diff --git a/archive/ES_0.5625432757957365 b/archive/ES_0.5625432757957365
new file mode 100644
index 0000000..71c3128
--- /dev/null
+++ b/archive/ES_0.5625432757957365
@@ -0,0 +1,22 @@
+archive/ES_0.5625432757957365---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T19:37:35.203
+Launch V∞: [6.478191390081077, -7.330393674726949, 0.1303699161787537] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.4316322651076903e-7, 3.277611264893133e-6, -1.915752218154396e-7] km/s
+ V∞_out: [1.1053007037027323e-6, -2.5402299029272505e-6, 1.4508571462903118e-6] km/s
+ time of flight: 1.8749577787523532e8 seconds
+ arrival date: 2029-04-07T21:47:12.203
+ thrust profile: [0.32468466820925534 -0.07402678439997783 -0.10102634413818223; 0.1360814394565276 0.043634680214177976 -0.12713064572464364; 0.07778905177710001 0.04733909433519661 -0.12268924016253796; 0.047337430207139326 0.03853283730428371 -0.10568456171050505; 0.054194649841711975 0.05436415043250698 -0.15561556019447442; 0.02496189956704708 0.029699041969141138 -0.09022217679444071; 0.028782691923728707 0.038121291922496116 -0.11994919488799535; 0.00335439876588024 0.005428293930442621 -0.01818493728600578; 0.002714652025098333 0.004864687814195997 -0.017792576955020102; 0.0033424452473583112 0.0059664861359131505 -0.02143718132945961; 0.0013418425074687562 0.002725138255725686 -0.01016712310852959; 0.0004961928598207047 0.001781161940505886 -0.007627026049970399; 0.00031202766290355636 0.0009725028508593637 -0.003591393340765628; 0.0004273387494405892 0.0014454164505048352 -0.002036692966155853; 0.00019318102982950817 0.000501492946463383 -0.0026944390145970725; -0.0002669793025976124 -0.0007482039436862015 -0.002286371628714706; -0.0015890730570389093 0.000577648175466048 -0.0003087179950782741; -0.00015742129276863316 -0.0013745441148357714 -0.0002616246792681028; 0.0005637792890000341 -0.00028415719507949926 0.0008502502372288048; -0.0003993234886557507 -0.0013182211561401996 -0.001976083245669306] %
+
+Mass Used: 97.94180509811486 kg
+Launch C3: 95.7186314280419 km²/s²
+||V∞_in||: 3.3129790694629256e-6 km/s
diff --git a/archive/ES_0.5625438422152435 b/archive/ES_0.5625438422152435
new file mode 100644
index 0000000..0cbf9fc
--- /dev/null
+++ b/archive/ES_0.5625438422152435
@@ -0,0 +1,22 @@
+archive/ES_0.5625438422152435---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T23:38:15.377
+Launch V∞: [7.6304575795162055, -5.777947601169678, 0.05158917265878432] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0265708962549971e-7, -8.673372231755301e-7, 1.615324620401491e-7] km/s
+ V∞_out: [-1.3369105324352574e-7, 5.079388523212147e-7, 7.183278844609876e-7] km/s
+ time of flight: 1.8535666907877272e8 seconds
+ arrival date: 2030-03-25T07:36:04.377
+ thrust profile: [0.5725143111049943 0.0242086694942478 -0.12341196439140524; 0.17688144033066752 0.12496866353547814 -0.1438483771047898; 0.13613337200916256 0.16449455958518014 -0.19907000282557893; 0.05683548728321601 0.09484589506056153 -0.13436398219062792; 0.024743356429258217 0.05384993810173719 -0.08600659695957538; 0.01572674057738976 0.04327458319488011 -0.07447899033812934; 0.00857825293795928 0.029739392213757498 -0.05505062336213323; 0.003691113897859593 0.015409650439809356 -0.03084118161578731; 0.0006415676373364974 0.00340813044950911 -0.007419661267692535; 0.00016580941843122082 0.000370476873669393 -0.001637732695790361; -0.0004561096011286866 0.0005812164488663185 -0.0031747329406220937; -0.0006635439058987652 -0.0003461484584113228 0.002096573279491934; -0.0013177020123644203 0.0008290575483218301 -0.00044905842606140806; -0.003263855339335869 0.005447074124802446 0.0004755598435742959; 0.0013738632212329997 -0.004286681645155685 -0.000872713296307821; 0.0005140127759068963 -0.0015619831954573468 0.0011990047092676594; -0.0024895212704662433 0.0012442478170128523 -0.0014322387894986945; 6.373559805321582e-5 -0.0003565429509506433 -0.0055200285669503475; -0.0033949031909283147 0.00469648966091054 0.005434484733623414; -0.0014246442474289873 0.001795197059265181 -0.002118753145175481] %
+
+Mass Used: 121.90234959965028 kg
+Launch C3: 91.61122279739436 km²/s²
+||V∞_in||: 8.882032836287925e-7 km/s
diff --git a/archive/ES_0.5625470715930391 b/archive/ES_0.5625470715930391
new file mode 100644
index 0000000..dd7ba34
--- /dev/null
+++ b/archive/ES_0.5625470715930391
@@ -0,0 +1,22 @@
+archive/ES_0.5625470715930391---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:23:45.576
+Launch V∞: [7.746513653398897, -5.717622801503839, -0.05807472889523581] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.338490791529402e-6, -1.8447173425866422e-6, -1.4824334174636728e-6] km/s
+ V∞_out: [-1.5398739788794522e-7, 1.5412193278006177e-6, -2.923497657172108e-6] km/s
+ time of flight: 1.855527864809276e8 seconds
+ arrival date: 2030-03-29T14:50:11.576
+ thrust profile: [0.5960636331170056 0.007861824908555859 -0.16400582398842325; 0.14189591650333416 0.08933463576475366 -0.1426862779620167; 0.053181201149677636 0.055215318636437145 -0.10207845764116254; 0.03537674878833204 0.04989451401966046 -0.10296330142557998; 0.019581308118802765 0.03373286871730955 -0.07750008462777215; 0.010694536346742427 0.021873974951858006 -0.054761222698900165; 0.012547037205902221 0.03140731570917864 -0.08200681787975736; 0.007878063768641443 0.022748628830477537 -0.06427080065426345; 0.0023738753102188043 0.008820011934428603 -0.025066288502043867; 0.0035924425447766365 0.013309439548292671 -0.04123677460563262; 0.00011428492029497554 0.0010719586723651725 -0.002157667374952849; 0.007590370952883394 0.00043320974923441723 -0.0043170097089277075; 0.0005927172855457476 0.0005333966313964507 0.0013143848418180756; -0.006791866249535147 0.00789791812442757 -0.006802984340963767; 0.00923745384498616 0.00044265065488621703 -0.00798752246287662; 0.0005756869825548532 0.013232240939110428 -0.02215113744723335; 0.008006422715237282 -0.005957692505273639 -0.012106553423245937; 0.003932064621683409 0.0007071780155179447 -0.007596171810664476; 0.003568195632672002 0.0025197026408423813 -0.008044672436910458; 0.0018635052173990203 -0.004609943407743897 -0.005070984799652984] %
+
+Mass Used: 115.53708461107999 kg
+Launch C3: 92.70305695670838 km²/s²
+||V∞_in||: 3.3270302212815494e-6 km/s
diff --git a/archive/ES_0.5625498356888813 b/archive/ES_0.5625498356888813
new file mode 100644
index 0000000..11f2180
--- /dev/null
+++ b/archive/ES_0.5625498356888813
@@ -0,0 +1,22 @@
+archive/ES_0.5625498356888813---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T19:55:59.622
+Launch V∞: [7.801077762288141, -6.153400836605112, -0.31762273187366047] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.0007475801507978e-5, 2.9137478605179487e-5, 2.099650943737695e-5] km/s
+ V∞_out: [4.113385599281764e-6, -2.9204628295452303e-5, 3.651440171646849e-5] km/s
+ time of flight: 1.874957778313899e8 seconds
+ arrival date: 2030-04-27T22:05:36.622
+ thrust profile: [0.2533597325033326 0.012475416036809945 -0.07900651524626362; 0.04324306645775977 0.02741337812260633 -0.05286664002660125; 0.028631974731151186 0.028701145485769877 -0.06249438059576354; 0.0655264431624069 0.09127457898582476 -0.18321847653851553; 0.014584557144452432 0.025507142006201158 -0.06659855071489892; 0.016758561744216215 0.03829338259798863 -0.10246141207229806; 0.007201999524238985 0.024224884803058542 -0.06966986965064094; 0.007821832026117895 0.02211385208923937 -0.06514675880350171; 0.004329868634525173 0.010348559723026358 -0.03543097821922412; 0.0027084235517701597 0.010596224940452167 -0.03796544675788154; 0.0007892721389273036 0.004001394178614117 -0.01610958174904483; 0.00017647886592420678 0.0005249735313282535 -0.0019863733804974244; -0.000279740421907565 0.00038248584378722055 -0.0013088627930848; 0.0005279821143063276 -0.00024140597854259752 -0.0020115222912324357; 5.630321706022486e-5 -0.0005561655369376562 -1.347887256716515e-6; 0.002368443773275807 -0.0011550910758111018 -0.003787119346367186; -0.0006777292590012334 0.0022461546946072482 -0.004441984537156934; -0.000162040505824636 -0.0010993938619711118 -0.0015906663915357263; -0.00020807493279407797 0.0008440343898087852 -0.0022317720635644384; 1.2206202129105836e-5 0.0005840072007294371 -0.00014276207413002585] %
+
+Mass Used: 79.84623983451684 kg
+Launch C3: 98.82204030900193 km²/s²
+||V∞_in||: 4.6800584098910975e-5 km/s
diff --git a/archive/ES_0.5625507331181807 b/archive/ES_0.5625507331181807
new file mode 100644
index 0000000..19aaa08
--- /dev/null
+++ b/archive/ES_0.5625507331181807
@@ -0,0 +1,22 @@
+archive/ES_0.5625507331181807---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T14:43:25.841
+Launch V∞: [6.23473407920208, -7.449180776950977, 0.2937116331078977] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.028527391608032e-7, -4.399129313513715e-8, 5.6411163072349654e-8] km/s
+ V∞_out: [-2.130204845242595e-7, 1.958766322669163e-8, -2.4689912105617564e-8] km/s
+ time of flight: 1.810646596554125e8 seconds
+ arrival date: 2029-01-22T06:27:44.841
+ thrust profile: [0.462385491515469 -0.1374133773168974 -0.15171609988183318; 0.08356616054186518 0.0196015775311563 -0.0867108653720649; 0.10096284469654884 0.049173640016279135 -0.17071745748463524; 0.06268183935148249 0.04146876266069766 -0.14893107774247694; 0.04327249381752693 0.034689797782849814 -0.13190491875111102; 0.03393697109048928 0.03151250397115519 -0.12500501091986074; 0.021355724349534793 0.02207445128047071 -0.09242843283541281; 0.007174556154178928 0.007991535265732128 -0.03700210099148604; 0.001820803185972608 0.002335194978731134 -0.01055056954949292; 0.0035716309637613187 0.0044660642202437005 -0.022701047947896638; 0.0005345615723178779 0.0007319061399653269 -0.003643615330050235; 0.0001862814851685258 0.00020655310378207576 -0.0011890226535203306; 0.0011095785067608884 0.0003000670284708198 -0.0007871701093972513; 0.0003630946445885592 -8.972819107319467e-5 -0.0013481207686319428; 0.00017658227339953283 8.298738085141868e-5 -0.000738092807357031; 0.00021186469868310408 -0.00037782444459876895 -0.0006932069734861746; 0.0001163378726010428 0.00016165638924763677 -0.0010736266313899857; -0.0006832480719937018 0.0011307376114632504 -0.0009422105926249272; 0.0009679225311479802 0.0009832602435635395 -0.002041511219380804; -0.0009056415424911463 -0.00037368504296921576 -0.0008138355122274753] %
+
+Mass Used: 105.35978141589521 kg
+Launch C3: 94.44846980948267 km²/s²
+||V∞_in||: 2.1509692460822784e-7 km/s
diff --git a/archive/ES_0.562552435892545 b/archive/ES_0.562552435892545
new file mode 100644
index 0000000..c92f0c8
--- /dev/null
+++ b/archive/ES_0.562552435892545
@@ -0,0 +1,22 @@
+archive/ES_0.562552435892545---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T05:22:53.561
+Launch V∞: [8.022248050980414, -5.59737704654988, -0.15426666379890694] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.09429943211107e-9, 4.6188277576700314e-10, -2.0729331475116724e-9] km/s
+ V∞_out: [7.834299830016219e-10, 1.6133115969390082e-9, 4.1478114372948854e-11] km/s
+ time of flight: 1.874957778750729e8 seconds
+ arrival date: 2030-04-22T07:32:30.561
+ thrust profile: [0.3966803733933365 0.00016704544599506894 -0.12651370378783616; 0.08062900387442656 0.04896722449025851 -0.0936505881884324; 0.046188364017324256 0.045915831341029056 -0.09923287098308554; 0.03875103447793798 0.05169926075979828 -0.12429914635398323; 0.030615604723562156 0.05089233667194988 -0.13450277362024757; 0.010488342557266063 0.020240088725066368 -0.06092434852324225; 0.004814669197285984 0.010700826702134061 -0.03524588443664396; 0.005543767399253688 0.01372839603099933 -0.04757155317018817; 0.005819533212285135 0.018830369166705628 -0.0672049142629029; 0.0007644109279289369 0.004971046200408831 -0.020836443712284988; -0.0005052091733113695 0.0012904004070308655 -0.00680698257984925; 0.00040329623295787725 0.001173772595383614 -0.004323235526782165; -0.003900695295770949 0.00021737126714829568 0.00043489082366005016; 0.00464792875467044 0.0023749819941868626 -0.017018699960558447; 0.0028380555705760997 -0.004140571229331326 0.0028223079546764356; 0.0005845512677695011 -0.007535272237804677 0.004561634677484769; -0.007326574714802246 0.016070399454728365 -0.003423758706843387; 0.0038356551044074626 0.004858505216361487 -0.007814579625447012; -0.004730794764774221 0.007781782065589171 -0.012927461012793105; -0.020766268362298723 -0.003354643430224666 -0.007893504127862432] %
+
+Mass Used: 97.99763972977325 kg
+Launch C3: 95.71089179626216 km²/s²
+||V∞_in||: 2.389116736311035e-9 km/s
diff --git a/archive/ES_0.5625589616491999 b/archive/ES_0.5625589616491999
new file mode 100644
index 0000000..2a58503
--- /dev/null
+++ b/archive/ES_0.5625589616491999
@@ -0,0 +1,22 @@
+archive/ES_0.5625589616491999---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T18:50:09.468
+Launch V∞: [6.21819311372079, -7.463771486758071, 0.1790978048744867] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2531398344236297e-5, -1.9616671229514414e-6, 3.210902164614843e-8] km/s
+ V∞_out: [2.5686416979582545e-6, -5.9061879740911016e-8, -1.2414026257158989e-5] km/s
+ time of flight: 1.8471847843497428e8 seconds
+ arrival date: 2029-03-07T17:31:27.468
+ thrust profile: [0.48470505998571306 -0.12186040020543598 -0.1558152271281727; 0.10592603357564698 0.030629558331429628 -0.11413688797378083; 0.05600430710662427 0.030239566979173262 -0.09897618010169836; 0.027368741233918113 0.01992601634297471 -0.0705830099735385; 0.02989285977366964 0.02669194135773242 -0.09627821462836726; 0.04311668585709772 0.0453899079963278 -0.1669698694183403; 0.03219998317763351 0.03584848386706799 -0.1401310091821898; 0.00845977680491903 0.011419986234676596 -0.04854027535173987; 0.005675747964502079 0.008317951633681693 -0.03744976765375747; 0.002758105038984865 0.004040107477826751 -0.019602064729104543; 8.701231552665106e-5 0.0006489998702455182 -0.0054611595181200115; 0.0004316162564283044 0.0003674040900238728 -0.0022366738753222815; 0.00026114763691988303 0.00043679358705641335 0.0005864254665081208; -0.0006397737314338456 -0.0009726376474522326 -0.0011875570871898034; 0.00013983569132922026 0.0003641898047657362 -0.0006777587442647699; 0.00013959622516833588 0.00025973807634244644 -0.00039417303142047294; 0.001721660601919043 0.00036369326517931167 4.368349054260142e-6; -0.001546008200259988 -0.0007993850343488201 0.0005312772192982897; 0.00034435009136629864 0.00020790670370876509 -0.00011455941035025125; 0.0008909990062487348 0.000551434120811653 0.0015803477379622136] %
+
+Mass Used: 105.61778441702654 kg
+Launch C3: 94.40588642977829 km²/s²
+||V∞_in||: 1.26840495644123e-5 km/s
diff --git a/archive/ES_0.5625627339871716 b/archive/ES_0.5625627339871716
new file mode 100644
index 0000000..8d8576c
--- /dev/null
+++ b/archive/ES_0.5625627339871716
@@ -0,0 +1,22 @@
+archive/ES_0.5625627339871716---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T19:44:40.703
+Launch V∞: [6.465687763176433, -7.576003836750156, 0.0606652644520912] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.226177339341007e-9, -2.3807637750779902e-9, 4.147852159352192e-9] km/s
+ V∞_out: [1.4241268383175582e-9, -3.4295789680876968e-9, -4.600610281270962e-9] km/s
+ time of flight: 1.8265457875363907e8 seconds
+ arrival date: 2029-02-12T21:07:38.703
+ thrust profile: [0.10160396054465566 -0.03051939752333709 -0.04180461615353497; 0.08947741454700742 0.018100971748724024 -0.10631520447385304; 0.04905061971989924 0.020278477928192606 -0.09745637228081047; 0.04834639005005679 0.02718763006654582 -0.13383073189070085; 0.038613300681383134 0.026130118857900612 -0.13514644990636926; 0.024286863392917045 0.01798313034774826 -0.1019487581169117; 0.02032773956642315 0.01693517901593075 -0.10510540260629529; 0.013615900955241667 0.012164701103716334 -0.07997114368086972; 0.012576120337447956 0.010514543576250177 -0.07585260906567962; 0.004710900577566661 0.004486133584557477 -0.03331769207032486; 0.0001287228378753311 0.0001292598678407579 -0.000935964063813014; -7.969969084122493e-6 5.639695640355051e-5 -2.236929641060979e-5; 0.0007890388937885295 0.0009740716796417636 -0.004154697102037221; 6.3081876489490836e-6 -7.9844345612851e-6 -6.284867391060387e-5; -6.872355587015549e-5 -1.2538220751150331e-5 -0.00010476406569835572; 2.746453167063881e-5 2.9971856925420534e-5 -7.708259356339407e-5; -0.00011689993792042162 6.199350625700905e-5 -0.00021558095741232267; 6.847394106032596e-6 8.090497682253562e-6 -6.95503529283732e-5; -6.62952877318433e-6 1.587327969037236e-5 6.050624841394903e-5; 1.6610312428529203e-5 -4.9875956002937816e-5 4.133942623414262e-5] %
+
+Mass Used: 77.62949913705415 kg
+Launch C3: 99.2046326596536 km²/s²
+||V∞_in||: 6.382263594691595e-9 km/s
diff --git a/archive/ES_0.5625653295953555 b/archive/ES_0.5625653295953555
new file mode 100644
index 0000000..78f2075
--- /dev/null
+++ b/archive/ES_0.5625653295953555
@@ -0,0 +1,22 @@
+archive/ES_0.5625653295953555---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T12:05:40.051
+Launch V∞: [6.675010073636029, -7.397818548894842, 0.05293669529396286] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.991527035151663e-7, -0.00018039547789558882, 0.0001340367317563617] km/s
+ V∞_out: [5.385058018328623e-5, 0.00021202993057443364, -4.6361567655480556e-5] km/s
+ time of flight: 1.8749577787456033e8 seconds
+ arrival date: 2029-04-10T14:15:17.051
+ thrust profile: [0.1249280613459605 -0.0338458552316452 -0.049483538794939635; 0.053027703573189075 0.012079721878260664 -0.06486117579645276; 0.04894048873766931 0.02197067118814504 -0.10048668616710468; 0.04749229299771017 0.02829067098720405 -0.13485476280694425; 0.036479168444244585 0.025781670867091638 -0.13290136789069165; 0.025511287423737174 0.020387052367635224 -0.11377788655106799; 0.013864347822674978 0.012063664943492387 -0.07355566955053805; 0.010219981709780097 0.008810341170469901 -0.0585575317721547; 0.008637122188917759 0.006944838672479751 -0.051467689443699144; 0.009465591322410878 0.007459660180687708 -0.0597205254283356; 0.003916252689216783 0.0030752438483841946 -0.02633046117539122; 7.58982089270352e-5 9.862557954425712e-5 -0.000710297481764913; 0.0011278380665760129 -0.00038533363544690193 -0.0003791150807243479; 0.00038906767346972546 0.0003177766757014565 -0.0009379836286616062; 0.000295005867692913 -7.016829464727382e-5 0.0008383991829797647; 0.0013526301442172907 0.001223337819632996 0.0006403829833831606; 0.002165349055742548 -0.0011045191687632213 0.0012888922690355836; 0.0009741074336407499 0.00024087387640223964 -0.0019465399044979587; 0.00018118485441371218 -8.957958580503114e-5 -0.00034158012090404824; -0.003043086842673642 0.0031024981869064404 0.0012544093395127607] %
+
+Mass Used: 77.15624501577668 kg
+Launch C3: 99.28628105922368 km²/s²
+||V∞_in||: 0.0002247414801256476 km/s
diff --git a/archive/ES_0.5625690140581341 b/archive/ES_0.5625690140581341
new file mode 100644
index 0000000..b27bb88
--- /dev/null
+++ b/archive/ES_0.5625690140581341
@@ -0,0 +1,22 @@
+archive/ES_0.5625690140581341---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T05:56:21.983
+Launch V∞: [7.855544560532541, -5.71300784136092, 0.07385434056678351] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.337034345446958e-5, -2.569216492654994e-5, -2.198972728300355e-5] km/s
+ V∞_out: [-4.179275239545147e-6, 3.0273214148791032e-5, -3.634365161599976e-5] km/s
+ time of flight: 1.8549029978598747e8 seconds
+ arrival date: 2030-03-28T03:01:20.983
+ thrust profile: [0.4077249235220596 0.006681766198488071 -0.10108243176412714; 0.1565916374124992 0.10210439648304646 -0.1378994234626441; 0.055268291117998566 0.06390331264299709 -0.09182271671850632; 0.06931363334664795 0.10497967155746168 -0.16824243161648464; 0.03172636001750451 0.06010072184596202 -0.11158010498596128; 0.015157346407436937 0.03762810251591306 -0.08015024002207684; 0.00445316313233704 0.015908806918640005 -0.03560307043047502; 0.004527769941231443 0.023831413448779426 -0.04443982457937043; 0.003562034479618303 0.005170238434673717 -0.014943907125492742; 0.008310693431836439 0.010700701534445621 -0.027395503557042525; -0.0028783540799751425 0.003587662331030991 -0.004924984855889851; 0.0014131654035723748 -0.0029560361823924098 -0.0020258259039598434; -0.0030088652436624994 -1.8738541664724273e-5 -0.005875433940806265; 0.0007026673697701802 0.0028945415862807254 -0.01146011932933404; -0.003801265384530227 0.007726376617782271 -0.0010450886821717752; -0.0012710313776967122 0.0038305694021876736 0.004826830341060302; 0.008570660598225515 -0.0026462824304117898 -0.012232869740943087; 0.0001062808973048186 0.0009538770914480311 -0.0053147785713103125; -0.009533458094074368 0.01398622512515 -0.007308405095731107; 0.0067784452911954455 0.0007735955058679384 0.0006556549733322597] %
+
+Mass Used: 105.93513822524801 kg
+Launch C3: 94.3534934015843 km²/s²
+||V∞_in||: 4.7510159617319475e-5 km/s
diff --git a/archive/ES_0.5625723112425767 b/archive/ES_0.5625723112425767
new file mode 100644
index 0000000..697025b
--- /dev/null
+++ b/archive/ES_0.5625723112425767
@@ -0,0 +1,22 @@
+archive/ES_0.5625723112425767---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T17:31:26.319
+Launch V∞: [6.5558163804877685, -7.404037198708423, 0.17294249106962994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.409818689859969e-6, 4.1730253126394896e-6, 4.843634027100942e-6] km/s
+ V∞_out: [6.578476371185273e-6, 4.126830666618282e-6, 1.313835483436263e-7] km/s
+ time of flight: 1.850979530587506e8 seconds
+ arrival date: 2029-03-12T01:37:19.319
+ thrust profile: [0.20025357175797381 -0.05661691849808141 -0.0727982431932646; 0.10039891243296291 0.023919288144157676 -0.11115026546515841; 0.06857052189354869 0.03186970773513539 -0.1274480415813266; 0.04573522885707997 0.02798676240044531 -0.11954707624723859; 0.02779556520068247 0.02074429457115397 -0.09574504838135649; 0.027629668314881384 0.02321507480665551 -0.11408863053609715; 0.022873013512949895 0.020988752204705464 -0.10734357635974345; 0.008196760648136764 0.00799347738128064 -0.04541113528845111; 0.009400053332168102 0.009818713322185911 -0.05589201653202013; 0.004390508299644943 0.00464010697297792 -0.029373489616042064; 0.004019240344149031 0.005276483124767807 -0.03027684275037244; 0.0006916342885732389 0.000980598961486043 -0.006964097589835168; -0.00015921035270493366 -0.00014990009371704168 0.0013285828843275732; 0.00024253886057924194 -4.4416004344044834e-5 0.0003628118282459578; -0.0002135290386721968 8.312649064952474e-5 -0.000560408221553075; 0.0006221744995684055 0.0002685437248577996 -0.0001932921905511909; 0.0003681919540496566 -0.00042760732422993466 0.0005435813931036716; 0.00025665226874763 -0.0003247180902605073 0.0006201895123900574; 1.2275842610447941e-5 -3.080368361777359e-5 0.0004399423493927897; -3.8950120742727135e-5 -5.689444623627327e-5 0.00018096427628688075] %
+
+Mass Used: 85.66867101781418 kg
+Launch C3: 97.82840435974718 km²/s²
+||V∞_in||: 7.766687307073608e-6 km/s
diff --git a/archive/ES_0.5626182201950515 b/archive/ES_0.5626182201950515
new file mode 100644
index 0000000..5fc5597
--- /dev/null
+++ b/archive/ES_0.5626182201950515
@@ -0,0 +1,22 @@
+archive/ES_0.5626182201950515---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T02:39:46.375
+Launch V∞: [7.714503915368581, -5.820967064764192, 0.10247080770907231] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.024365956278261e-7, -1.7965407428076913e-6, -1.1216602376765745e-7] km/s
+ V∞_out: [1.4078061499460768e-7, -6.967221272284801e-7, -1.8378033934345098e-6] km/s
+ time of flight: 1.8224892082846826e8 seconds
+ arrival date: 2030-02-17T11:21:46.375
+ thrust profile: [0.4947613681539433 0.004915146442306184 -0.11792802465059665; 0.12158156195767675 0.07963675960884536 -0.10451168281831494; 0.09591933838068381 0.1064139126940645 -0.14579167850405622; 0.05491815572744143 0.08256529208829957 -0.12988337792349955; 0.04343990228926178 0.08172656304472307 -0.1377003440644529; 0.017866028379100236 0.042391800951887645 -0.08280956918389948; 0.00576318298284918 0.020679234793798455 -0.04519286911891052; 0.007977087457541865 0.023928517003712773 -0.04981070117991902; 0.0026458416990415836 0.007564411934804273 -0.022330960541806465; 0.0022468650069983978 0.008275964744463031 -0.023342166985564076; -0.003125305108269203 0.0024063126080711116 -0.0047507700771095744; 0.003543011716251375 0.005908771701350785 -0.0032221623386475273; -0.00010138214109389369 0.006131368419303943 -0.004758608853109129; -0.0023803918584190406 0.0030456282638218002 0.00043907048594806364; -0.0021234593987400872 -0.0038616772585833995 -0.005789174332305431; 0.0003915392205787766 0.002752096061137005 -0.0010162706319983578; -0.0031317522323146023 -0.0011608261922415413 0.006244868911166794; 0.004061678027923258 -0.009408100969797953 -0.008931371497442556; 0.0003154457495030022 0.0024994257609666764 -0.003547963636580829; -0.002691351959160369 -0.0009298674765732418 -0.004485933117640867] %
+
+Mass Used: 111.50950733574837 kg
+Launch C3: 93.40772849573915 km²/s²
+||V∞_in||: 1.9707978961473022e-6 km/s
diff --git a/archive/ES_0.5626203665490834 b/archive/ES_0.5626203665490834
new file mode 100644
index 0000000..3bd3573
--- /dev/null
+++ b/archive/ES_0.5626203665490834
@@ -0,0 +1,22 @@
+archive/ES_0.5626203665490834---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T14:02:16.581
+Launch V∞: [6.518285402558134, -7.468437865166029, 0.21483899290890865] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.333386417601406e-7, 2.782246127687642e-8, -3.651255561451146e-8] km/s
+ V∞_out: [1.3668339294832382e-7, -1.2150177677571214e-8, 1.5197322594952988e-8] km/s
+ time of flight: 1.8749577787459654e8 seconds
+ arrival date: 2029-04-11T16:11:53.581
+ thrust profile: [0.2289784163496211 -0.06604333557758446 -0.08943828273449851; 0.03548326064997442 0.006849877933187687 -0.04360441463864825; 0.049276436632701474 0.019082444215360716 -0.10036084677207666; 0.04995824278822692 0.025289618434414893 -0.1413219475923497; 0.03987777614573987 0.0235709223260026 -0.14378414129269057; 0.029545924163524893 0.019397329722341667 -0.12868504804254932; 0.019747075454654737 0.013751602637173097 -0.09990651330224017; 0.006499863141319352 0.004878865399491721 -0.03867439849959532; 0.005286964328575342 0.004298891223674635 -0.03569500292889392; 0.005431001656546649 0.004417073212720544 -0.03899374269507099; 0.0006479752564478666 0.0006637941419239294 -0.005204623415805687; 0.0006131963716660512 0.0009081460187182475 -0.005704448887433593; 0.00028830321897494685 -0.0008739226315343266 -0.00010431113515843875; -0.0007559267600485371 -0.000322205480679853 -0.0003035073130997953; -0.0005256673541875674 -0.001354810425821575 -0.001329589366870909; -3.560698995899421e-5 -0.002371033553981212 -0.0015911788364808871; 4.723788149289417e-5 0.0011692762896472397 -0.0004719388676383909; -0.0009988882092528124 -0.0023764819820216413 -0.005475019765309862; 0.0008936025508032744 -0.0013179050621022373 -0.0047786360303448145; -5.724545523033417e-5 -0.00018790428046067765 0.0009962449946624439] %
+
+Mass Used: 82.90513456105055 kg
+Launch C3: 98.31176452792229 km²/s²
+||V∞_in||: 1.4101932298605462e-7 km/s
diff --git a/archive/ES_0.5626231908825374 b/archive/ES_0.5626231908825374
new file mode 100644
index 0000000..fb3c901
--- /dev/null
+++ b/archive/ES_0.5626231908825374
@@ -0,0 +1,22 @@
+archive/ES_0.5626231908825374---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T09:50:45.443
+Launch V∞: [6.447636365914447, -7.392232449464915, 0.18532833359906017] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006359001261919778, 0.0007844091319291228, 0.0006786002046583209] km/s
+ V∞_out: [-0.0009866438182833835, -0.0003015422661532273, 0.0006441561977104906] km/s
+ time of flight: 1.8376412640056524e8 seconds
+ arrival date: 2029-02-23T07:26:11.443
+ thrust profile: [0.3103001782112933 -0.07617787250152544 -0.11103833621197068; 0.12037010563678328 0.027456574074561486 -0.13111150637643693; 0.08022831127748528 0.038846653669128706 -0.14220770103781288; 0.04275409819104012 0.028261848900449037 -0.10997374335878872; 0.0558175942839929 0.04532955538469418 -0.1886150842584728; 0.018242951932269984 0.01722176056246311 -0.07631753219753358; 0.02048848903632786 0.021020092961271816 -0.09651434517462365; 0.01062830769917538 0.010091160536559325 -0.05210192349692155; 0.002922273581719044 0.0038355304182554626 -0.017706269793712603; 0.0019546114577220722 0.002257738830460505 -0.01325617370762031; 0.0005487246872002459 0.0006525724134828216 -0.003601554362429; -1.6396164926209906e-5 2.4894410535435422e-5 -0.0011051017506763477; 0.0006344634988755748 6.738620168760017e-5 -0.0010957024717690705; 0.00015177199802056098 -0.0008308883723759226 0.0007519379426881069; -0.0006269429394603042 -0.0013717919777522431 0.00014095587623178852; -0.003289012676799603 -0.0011705929999427716 -0.00021824972002816714; 0.0019221503106617273 0.0030096770407001647 -0.0007710760860630012; -6.4056113196041e-5 -8.549484861654188e-5 -0.0002979264424367292; 1.8569675591872205e-5 0.00023007792730315047 -0.00037745001689942596; -0.0035306310664175913 -0.001208606787565153 0.0014697340167334253] %
+
+Mass Used: 94.92686169918215 kg
+Launch C3: 96.25146188521911 km²/s²
+||V∞_in||: 0.0012166202753970067 km/s
diff --git a/archive/ES_0.5626338323093956 b/archive/ES_0.5626338323093956
new file mode 100644
index 0000000..b85691b
--- /dev/null
+++ b/archive/ES_0.5626338323093956
@@ -0,0 +1,22 @@
+archive/ES_0.5626338323093956---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T07:59:56.609
+Launch V∞: [6.299621869764778, -7.37050046802426, 0.20156702310746386] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004800413475527342, -0.0005659326242701836, -0.0005214572713050389] km/s
+ V∞_out: [0.000596780062457723, 0.00029117226676527846, -0.0006096405357153643] km/s
+ time of flight: 1.8749577787472397e8 seconds
+ arrival date: 2029-04-10T10:09:33.609
+ thrust profile: [0.5863610418410914 -0.17773785935336636 -0.21491479646242745; 0.024186932038074063 0.005230624730631896 -0.029555144765685704; 0.04195088239046787 0.018329566388884735 -0.08736876939425778; 0.04597093396199646 0.02750305505611232 -0.13507983518907601; 0.03243609832715324 0.02242464145206324 -0.12148392822543443; 0.023325992767940448 0.018475654907432977 -0.10599329771104568; 0.01073318085801086 0.008799832797556842 -0.055921448562248996; 0.012479519222709998 0.01073333113616662 -0.07102233940615929; 0.0167870490530384 0.015877103705264958 -0.10407965891636482; 0.0011416669090436255 0.0009416029409743574 -0.008574293557058908; 0.0008348283957286168 0.0008523764632567249 -0.007024771227087474; 0.000512126162667479 0.00039316689425388743 -0.003772120232751735; 0.0005559218301534472 0.0009073472126632299 -0.00472984059955905; 0.0006254698512697268 0.00032474048943745835 -0.0014353046614932422; -0.00025889226701830025 -0.0008691954566909695 -0.000478254732778781; -0.0006524921321845829 2.501745675592269e-5 -0.00261916865961102; -0.0004597376425488611 -0.0006366423161298898 0.0014906425014609816; 0.0009328371037372269 0.0019548833168365077 -0.0003242933609750849; -0.0011021116088699762 0.00033369881677943115 -0.0003652341907399773; -5.380289409436488e-5 -0.00013313254985417738 -0.0019646803258973507] %
+
+Mass Used: 107.78030868447604 kg
+Launch C3: 94.05014211596892 km²/s²
+||V∞_in||: 0.0009069934489126582 km/s
diff --git a/archive/ES_0.5626532784742264 b/archive/ES_0.5626532784742264
new file mode 100644
index 0000000..42c37b3
--- /dev/null
+++ b/archive/ES_0.5626532784742264
@@ -0,0 +1,22 @@
+archive/ES_0.5626532784742264---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T22:02:23.902
+Launch V∞: [6.5604904689398085, -7.394225786910709, 0.21461920450213676] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.493556361783979e-6, 4.3522641517377326e-6, 4.924927036732037e-6] km/s
+ V∞_out: [6.721204141898175e-6, 4.2661529818991275e-6, 1.322084973764258e-7] km/s
+ time of flight: 1.859648160708547e8 seconds
+ arrival date: 2029-03-22T06:55:59.902
+ thrust profile: [0.2106752391837042 -0.05636896405878917 -0.07767475205816024; 0.07023879115695394 0.017467988802157584 -0.07710730465049265; 0.07941317990795897 0.03932135214565672 -0.14623907023844343; 0.05736104765933204 0.037873722316207 -0.14760671085691907; 0.046105677999606125 0.03657042233585017 -0.15186158371985078; 0.02887104760776049 0.02602545051359301 -0.11568358782179869; 0.012545303303527764 0.012589718998668066 -0.058623696250444675; 0.013553090898886525 0.014534577088319914 -0.07412280033374635; 0.002659963718333716 0.0034915113071241222 -0.014290727610096443; -2.7063364753625438e-5 -1.6792937178119463e-5 -0.005440542745830901; 0.000558237899382186 0.0012007291116479658 -0.005808232744491851; 0.0010464125542523786 0.0013564015699359011 -0.0024709911712617527; 0.001408031515151361 -0.00038978093787759026 -0.0069531813456172285; -0.0008663359826899105 0.0009742563304225241 -0.004673711414177205; 0.0015483948342467602 -0.0026467415720712144 -0.0026934458343604627; -0.0004902045573463801 0.00015183669237542395 -0.0010318954643919686; -0.004972079127184799 0.0011902126278865064 -0.003978498995559552; 0.00461422530422157 0.0013748051707556312 -0.0002061169005919939; 0.0003731627263763209 0.001214245374876841 -0.006237559416257779; 0.0005160963884471019 -0.00015925879195255953 -0.00530397262864151] %
+
+Mass Used: 86.15824064772642 kg
+Launch C3: 97.76067158380648 km²/s²
+||V∞_in||: 7.96173086333398e-6 km/s
diff --git a/archive/ES_0.5626560576778113 b/archive/ES_0.5626560576778113
new file mode 100644
index 0000000..6f1b8f2
--- /dev/null
+++ b/archive/ES_0.5626560576778113
@@ -0,0 +1,22 @@
+archive/ES_0.5626560576778113---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T22:25:57.548
+Launch V∞: [6.6392940180445255, -7.4336066927813755, 0.15131663110538465] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.926375324517289e-9, 2.903497616458727e-11, -6.173123534967993e-9] km/s
+ V∞_out: [-1.200115687375496e-9, 2.7380139612585106e-9, 3.776732630574377e-9] km/s
+ time of flight: 1.8749577787632945e8 seconds
+ arrival date: 2029-04-11T00:35:34.548
+ thrust profile: [0.12802829181050804 -0.03535081032791001 -0.050703853257350315; 0.025416080932114515 0.005307047485366725 -0.03104084836718282; 0.05289107345656701 0.022532997141618463 -0.10706734850864347; 0.06457406695792603 0.03633264082742714 -0.1813160837776292; 0.05181740778162195 0.03428113375186385 -0.18584968081986608; 0.0294045697328853 0.021810802549482446 -0.12816896278149048; 0.0107172433301899 0.008705781315811073 -0.055644348784018555; 0.006414855417040489 0.0055635638488775495 -0.039120407226479484; 0.002237322969782033 0.0018762101865078048 -0.01432943276797619; 0.006125172710997903 0.005780829861801209 -0.04377268151110591; 0.00016533087911279245 0.0005009826720990796 -0.001170021186406647; -0.000588141022479699 -0.0008194489140892607 0.00017006147011984127; 0.00044520207184952233 0.000832296819465383 -0.004519583201498114; 0.0026303408755134123 0.00139426522646362 -0.002909816917854026; -0.0007681452836112162 0.0008064910165345616 0.001995118277259978; 0.001418485295588372 -0.003585012588716453 -0.008229667474971822; -0.0024353594774779363 0.006761334056062865 -0.0017099573109144815; -0.0025845181084983558 0.004972830239045448 -0.0038063117442029984; -0.00031282572643321325 0.001612251859040511 0.005426539311682457; -0.0002429038858743873 -0.0007862459024128938 0.00014740619478963287] %
+
+Mass Used: 76.82255753495929 kg
+Launch C3: 99.36163024385496 km²/s²
+||V∞_in||: 9.27809098596789e-9 km/s
diff --git a/archive/ES_0.5626579997417762 b/archive/ES_0.5626579997417762
new file mode 100644
index 0000000..c864ee8
--- /dev/null
+++ b/archive/ES_0.5626579997417762
@@ -0,0 +1,22 @@
+archive/ES_0.5626579997417762---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T14:31:15.969
+Launch V∞: [6.5572613842818805, -7.422569058981841, 0.09230806884593316] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9071901250702928e-7, 5.02153139448389e-8, -6.188719454475429e-8] km/s
+ V∞_out: [1.949903700825737e-7, -5.063155124906662e-8, 2.430831280440128e-8] km/s
+ time of flight: 1.8749577787460968e8 seconds
+ arrival date: 2029-04-10T16:40:52.969
+ thrust profile: [0.21854003923421036 -0.06209042095170705 -0.07195205835474779; 0.04346638785321885 0.010204763771725056 -0.050446228924002676; 0.045401881708003404 0.020570900299696562 -0.0871768819990499; 0.07569334955944625 0.04212916855437949 -0.20085239629209242; 0.033641014062393323 0.024482866801594512 -0.11537962328063212; 0.021126448924648204 0.017005959487896728 -0.08858678817145335; 0.017597709197034173 0.015300003801653472 -0.08548656587926266; 0.012947483180146616 0.013015338039325504 -0.07534474779542889; 0.009182600677955585 0.010369953541959239 -0.06311244194400494; 0.0024223105274907286 0.002711035583771311 -0.018804673957516466; 0.0009930403461597436 0.0007164084079591653 -0.006752307318989281; 0.00039167644601790076 0.0008919871079216292 -0.0017594894000209985; -2.2251261819595126e-5 0.0005077332378288926 0.0005080424674732101; 0.0007564175015963533 0.0011794424096377223 -0.0037849450627222827; 0.00022384252364408266 0.001987274268790197 -0.0018332458177977525; 0.0008747246496750274 -0.0006034363373641085 -0.0029009542736778363; -0.00030724035669932293 0.005362007513312696 0.0010566547179439783; -0.0005238154605290752 0.0004195300000878405 0.0009701922944411177; 0.00030981787818097905 -0.00017124632308934115 0.004640093677528536; 0.0028270032621983293 0.005141310399903624 0.0032951800685182926] %
+
+Mass Used: 84.1800800845217 kg
+Launch C3: 98.10072907672296 km²/s²
+||V∞_in||: 2.067010990170478e-7 km/s
diff --git a/archive/ES_0.5626611829537707 b/archive/ES_0.5626611829537707
new file mode 100644
index 0000000..fed6403
--- /dev/null
+++ b/archive/ES_0.5626611829537707
@@ -0,0 +1,22 @@
+archive/ES_0.5626611829537707---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:16:16.321
+Launch V∞: [6.61010204734902, -7.353062640991926, 0.12757807448177302] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3512987484300638e-7, 2.772452706928126e-7, 1.1922539432489334e-7] km/s
+ V∞_out: [-1.0557144028498186e-7, 1.6833228792804748e-7, -2.6440014593720274e-7] km/s
+ time of flight: 1.874957778748669e8 seconds
+ arrival date: 2029-04-08T17:25:53.321
+ thrust profile: [0.2011273886416025 -0.04316625878409013 -0.06800085300786023; 0.09700210526054336 0.032664250641491616 -0.09839532517554263; 0.05625849711557318 0.03465062510420289 -0.09707590765203061; 0.04289747378304719 0.03525505052548158 -0.1033825554481174; 0.030512060658363784 0.031047178956746906 -0.09618881203172885; 0.027597289034406777 0.03313917640081035 -0.10659980304923701; 0.0333083730509816 0.045913491906352355 -0.15084003916626407; 0.014801810576837056 0.022276979727180353 -0.07987763958401782; 0.005555990407504918 0.008752406616083662 -0.03360913585982565; 0.001266285284826662 0.0022265076456739505 -0.009094564617640468; 0.004307518457510322 0.0072644375047992175 -0.02951373851207821; -0.0006714341536070937 0.000871353088715409 -0.0020605829181023195; 0.0002851984714189696 0.0011482885953333947 -0.002523663109842016; -0.0004418209858164664 0.00019769735285525856 -0.00102011059679999; 0.0003890466036600968 0.0007476613361002482 -0.002873004332385759; 7.577622048950084e-5 0.0001815311241431302 -0.0016542906288674682; 0.00046614014714761726 -0.001112843037103212 -5.6928261775913156e-5; -0.001009818535402359 0.0015851345727763593 0.0004520958876798359; 0.0002647305410503853 -0.000221101654227831 0.0008826118345807747; 0.002832169642227312 -0.00027491050505325254 0.0013645487320459102] %
+
+Mass Used: 86.07072335718976 kg
+Launch C3: 97.77725544380732 km²/s²
+||V∞_in||: 3.3066556798152393e-7 km/s
diff --git a/archive/ES_0.5626612283332997 b/archive/ES_0.5626612283332997
new file mode 100644
index 0000000..49a438f
--- /dev/null
+++ b/archive/ES_0.5626612283332997
@@ -0,0 +1,22 @@
+archive/ES_0.5626612283332997---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T00:10:08.769
+Launch V∞: [6.438308082513904, -7.307204291526087, 0.14279432385900406] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.3243174204664513e-7, 1.0751831246331196e-7, -1.4353060307603156e-7] km/s
+ V∞_out: [4.479122259094348e-7, -1.1974754332886195e-7, 5.516373541038714e-8] km/s
+ time of flight: 1.8749577787499806e8 seconds
+ arrival date: 2029-04-08T02:19:45.769
+ thrust profile: [0.4692615636411774 -0.10202371293200087 -0.13571336610864634; 0.061613445928819725 0.02035128368603841 -0.06130544131842576; 0.04989626252704361 0.03114856423803041 -0.08351663517144385; 0.0393002044994997 0.03307563067877258 -0.09216670705323783; 0.027659377365957305 0.02844469095507671 -0.08361810772889647; 0.03191325246826712 0.03927438580457556 -0.11875801763828892; 0.03149246070086594 0.04434197067561881 -0.13558634679627993; 0.019123081680169293 0.029645858589854735 -0.09809009597848993; 0.015315709174136638 0.025990400897740226 -0.08921184938741844; 0.0007194366389719721 0.0011399626376343997 -0.004001664841425629; 0.00045664906952179614 0.001470180992958881 -0.004650679100949902; -0.00026163676005811246 5.549517430364943e-6 0.00028178956922530964; 0.00020939229528332555 0.0002912796563834065 -0.0006283844497242909; -0.0005493206567835431 1.628042554073771e-5 -7.860581574380566e-5; -0.00020525429967332975 4.192808065027817e-5 -0.0007933858153499991; 0.0004125509921725101 2.779567004861848e-5 -0.0010620344615497686; -0.000881747232915878 -0.00014491799959557108 -0.0002155243476784131; -0.0002228562624161736 0.0002328742214133356 0.0021272399122819773; -0.0005001533680841644 0.0014820998307135535 0.0015123673955411486; 3.865727667988684e-5 6.709968942257436e-7 -9.13388379116288e-5] %
+
+Mass Used: 103.0447245582559 kg
+Launch C3: 94.86743574238749 km²/s²
+||V∞_in||: 4.681436030363161e-7 km/s
diff --git a/archive/ES_0.5626615182605049 b/archive/ES_0.5626615182605049
new file mode 100644
index 0000000..947c10e
--- /dev/null
+++ b/archive/ES_0.5626615182605049
@@ -0,0 +1,22 @@
+archive/ES_0.5626615182605049---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T03:28:49.930
+Launch V∞: [6.408130416840496, -7.41344159716131, 0.3154658896745449] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.508466706518613e-5, -1.919098716552173e-6, 3.113540058661156e-8] km/s
+ V∞_out: [2.795566660701971e-6, -6.277747175246767e-8, -1.4939163680910826e-5] km/s
+ time of flight: 1.8616475988426253e8 seconds
+ arrival date: 2029-03-24T19:54:48.930
+ thrust profile: [0.3585138091539157 -0.09117420195643697 -0.12213171672144033; 0.062107709445071824 0.0171591236524783 -0.06925239239171736; 0.06991339682714624 0.03716964579291891 -0.12530580292897772; 0.057767649819260275 0.04118190774029459 -0.14369360097369663; 0.038628629367927464 0.03313822637056099 -0.12571966783707283; 0.02912796995499796 0.02908081387688799 -0.11650187381519304; 0.014794017998981836 0.017139501979136895 -0.0734638028198092; 0.0073985570936901226 0.009241385067108528 -0.04296988193509193; 0.009537095277642021 0.011335851672823572 -0.05573247784312442; 0.0033910502367298654 0.005009533012242856 -0.026061299529712548; 0.0010993819230145365 -3.523137700114745e-5 5.8226667177364334e-5; 0.002168336450376245 0.00265260925478237 -0.01542852220302597; 0.001138131192977235 -0.0003393233590696766 -0.00048440602994883394; -0.0004154430120408178 0.00019585998753626484 0.00028714606598989763; -0.0012539016181448096 0.001278662459098403 -0.00014613797560659417; 0.0013454335956653526 -0.0008003341564903042 0.00039089735798556596; 0.0008091458396722576 0.0026130896495941314 0.0028177625855698735; -0.0001426498080048171 0.000926504011294615 0.0010240532122556324; -0.00014744575931388343 -0.002532962767159703 0.0002109338715180066; 0.0023043814991587095 0.0003321658933437053 0.0027427591081877886] %
+
+Mass Used: 95.72227682963648 kg
+Launch C3: 96.12277048130615 km²/s²
+||V∞_in||: 1.5206284548322547e-5 km/s
diff --git a/archive/ES_0.5626615680368956 b/archive/ES_0.5626615680368956
new file mode 100644
index 0000000..650e403
--- /dev/null
+++ b/archive/ES_0.5626615680368956
@@ -0,0 +1,22 @@
+archive/ES_0.5626615680368956---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T20:04:37.087
+Launch V∞: [6.264704728445887, -7.690392440708955, 0.08339509357895741] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7949914132005743e-9, 1.821816865375854e-9, 1.210126696499389e-8] km/s
+ V∞_out: [-5.770992221498057e-9, -8.359089279516772e-9, -4.1717514814437e-9] km/s
+ time of flight: 1.7787509117376494e8 seconds
+ arrival date: 2028-12-18T13:49:28.087
+ thrust profile: [0.17323729152385656 -0.06091841997350759 -0.06995296033539933; 0.02952966328315164 0.004384963438528074 -0.03676453456269555; 0.09675245778267544 0.03245864010010735 -0.18452487427780212; 0.06105798340822715 0.027877874090281154 -0.16297716875013307; 0.07352561482066959 0.0402508655698363 -0.24421006068988926; 0.03150903919303074 0.019193401247566407 -0.12790404584074572; 0.008820233232943826 0.006258259061268468 -0.04386831532799161; 0.008253397498908644 0.005537034587859645 -0.043690683496757046; 0.004691641641154584 0.004130011663040014 -0.038128543709443644; 0.0009640092852232242 0.0007438514080794986 -0.006287008810797684; 0.0002671315319866708 0.0002816069172158185 -0.0024820933972690023; 0.00017812886251247006 -0.00013551903073390635 -0.0004650447995173573; -6.188075139043902e-7 -0.00040789295642203475 -0.0004577914458810435; 6.192516384206662e-5 -0.00018329059494841404 0.0003867683762391055; -1.93134671199833e-5 0.00014091565669554704 3.985689888430863e-5; -0.00014883208395382035 0.00018001607575341926 -9.559617252389869e-5; 0.00025373028522527745 -0.0005984166094365646 -0.00010220578880418691; -0.00021639824231453147 -4.6801022620071467e-7 -0.0003088236130430261; -0.0001403034549699291 -0.00014228574358669452 0.0009225062952532404; -0.00010174488257985174 -0.0003654128357739182 -0.00031953095494385197] %
+
+Mass Used: 82.46406956095234 kg
+Launch C3: 98.39561596835873 km²/s²
+||V∞_in||: 1.2368576030509095e-8 km/s
diff --git a/archive/ES_0.5626773811836866 b/archive/ES_0.5626773811836866
new file mode 100644
index 0000000..cf54b19
--- /dev/null
+++ b/archive/ES_0.5626773811836866
@@ -0,0 +1,22 @@
+archive/ES_0.5626773811836866---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T12:40:47.403
+Launch V∞: [6.184488707646537, -7.457972011878177, 0.15476890628483186] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009100837483532875, 0.0009833128534383424, 0.0009186951630124568] km/s
+ V∞_out: [-0.0010774075680861888, -0.0004911190385480093, 0.0011118399354123657] km/s
+ time of flight: 1.8098013419966063e8 seconds
+ arrival date: 2029-01-21T04:56:21.403
+ thrust profile: [0.498856472839279 -0.14593272711745717 -0.16146827900272645; 0.10910766299547653 0.026571245451095887 -0.10846971658182251; 0.048332194244849684 0.02400701650044796 -0.08052147094326687; 0.07501402278094786 0.0515560287138575 -0.17137659084992518; 0.0741113599630127 0.062360280909159814 -0.21586752934362088; 0.028235983724011208 0.02700794567336253 -0.10147483587514607; 0.016976394057500333 0.018351547039636297 -0.07195751134367823; 0.008099853206011047 0.010055369574650133 -0.04280611760185827; 0.0018828391403447142 0.0023865336465867305 -0.00996084317750041; 0.0011906621010790283 0.0017596707439575235 -0.008413027158055494; 0.0033000730193684462 0.0038117919418750985 -0.018735374969545037; 0.0005354962352944886 0.0006621985179361804 -0.0013810826171153387; -0.00017048075679732477 0.000364325614511105 -0.0018170675820864918; 0.0005280082934702265 -0.000264671393609123 -0.00010303225354226712; 6.53174582533314e-5 7.131208338121103e-5 -0.00013089767359648864; -0.0017139613751818755 -0.0005858218454409777 7.074080805949618e-5; -7.332088455602693e-5 3.943785469600643e-5 -0.0004933768667466983; 0.0007065556976583343 0.0004027156113900136 -0.0028061883442282356; 0.0011991537753720835 0.0010372699319435357 -0.00028310533011290914; 0.0009928819727157761 4.065986499466682e-5 0.0015333931786588272] %
+
+Mass Used: 108.74660835161058 kg
+Launch C3: 93.89320051931837 km²/s²
+||V∞_in||: 0.0016245483677922025 km/s
diff --git a/archive/ES_0.5626813123325238 b/archive/ES_0.5626813123325238
new file mode 100644
index 0000000..f1eaa58
--- /dev/null
+++ b/archive/ES_0.5626813123325238
@@ -0,0 +1,22 @@
+archive/ES_0.5626813123325238---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T03:16:08.265
+Launch V∞: [6.3271247975132106, -7.468659316009123, 0.41336050342380326] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.360403288975106e-7, 4.2662592185469345e-6, -2.4590599128515965e-7] km/s
+ V∞_out: [1.599751767860669e-6, -3.411373240742108e-6, 2.113074537870776e-6] km/s
+ time of flight: 1.850205424548676e8 seconds
+ arrival date: 2029-03-10T13:51:50.265
+ thrust profile: [0.3032898355721107 -0.0726531771235921 -0.09177297578933327; 0.14192051992581176 0.04720437032207917 -0.12979182892320087; 0.07251898550028915 0.04470070021630023 -0.112974337231762; 0.04659333237825757 0.038826775098982406 -0.10370817457483077; 0.05015575338063473 0.05398685765670767 -0.14488815267850472; 0.033358979446545554 0.04094370981224435 -0.1156214816691149; 0.02237508718234525 0.030276643495286675 -0.09390540504857288; 0.007435135807603185 0.01087250356258123 -0.03625518449424433; 0.0064326997821456035 0.010233298432495387 -0.03517171705003873; 0.005011686231448125 0.008507203632980045 -0.030268839382310734; 0.0027949654990473095 0.005118639897758507 -0.01961583637867704; 0.0003207697940741815 5.987623767740149e-5 -0.0006866782907309901; 0.0004999162388933602 0.00042532537086004417 -0.0007508615375450415; 0.0004473655216632938 0.0001983729006522621 -0.00018318552161912267; 0.00019901141070623388 0.00016807548752275465 -0.001111705447719095; 1.2815995223443917e-5 0.00015118320163977356 -0.00036141786527349635; 4.072496188029545e-5 0.0006723748278249844 -0.0008632065796771113; 0.00015409906890966946 0.000317090653852813 -0.0008909284906709091; 0.00014619011038554005 0.0004900834170237388 -0.0001719089611510689; -0.0003736467789961698 0.00029844945178610907 -0.00012748625627689565] %
+
+Mass Used: 96.55342304298574 kg
+Launch C3: 95.98424708770722 km²/s²
+||V∞_in||: 4.320414884750155e-6 km/s
diff --git a/archive/ES_0.5626855665436002 b/archive/ES_0.5626855665436002
new file mode 100644
index 0000000..fdbc55a
--- /dev/null
+++ b/archive/ES_0.5626855665436002
@@ -0,0 +1,22 @@
+archive/ES_0.5626855665436002---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T22:00:35.232
+Launch V∞: [6.595260832089645, -7.478144281538191, 0.11387966773623517] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.033075076392612e-6, 4.248941993843497e-6, 5.29685779064891e-6] km/s
+ V∞_out: [7.208081084037613e-6, 4.41198611697101e-6, 1.4487573305778908e-7] km/s
+ time of flight: 1.8504038301477548e8 seconds
+ arrival date: 2029-03-12T14:06:58.232
+ thrust profile: [0.09858251890689053 -0.02824528228557246 -0.03699003853594597; 0.05574625292735707 0.011871773535915372 -0.06164768140234049; 0.04603429992691862 0.019893150290233898 -0.08570543050751782; 0.05505457261113319 0.031830551798120346 -0.144016944233185; 0.04273121906518609 0.02936838952742391 -0.14237887352264172; 0.03374803071771966 0.026186160836236577 -0.13580180459959648; 0.03247013738318715 0.027729000047814183 -0.15267065663751497; 0.01543420880472911 0.014107817857304366 -0.08163887854272311; -0.0010561278756580999 0.0016055945129701027 -0.003580064019380544; -0.001675176405696497 -9.497692923217155e-5 -0.002241540187639693; 0.001272158122074757 0.001678781314885199 -0.00937108077469211; -0.0005992911663093028 -0.00035947776835222145 -0.004912118584599364; 0.0011454668486313604 -0.00018284424550270555 -0.0032436325487205284; -0.0001853482496746123 -0.0011489189325318274 0.00011023580492155387; -0.001699052707981041 -0.001939361729106397 -0.0027735916105727787; 0.0014254241120117603 -0.002546490603289528 -0.004104633076568805; -2.4877354903299212e-5 0.0013486454101062195 -0.0010358550137831175; -0.00015962255728776595 0.0006347850729073538 -0.001589372837226469; -0.0022223919849814772 -0.004499115304916755 0.0009983219076463007; 0.0045462169098430755 -0.0002465717120774775 0.006138509521038463] %
+
+Mass Used: 76.44021811532275 kg
+Launch C3: 99.43307591752186 km²/s²
+||V∞_in||: 8.452340223039374e-6 km/s
diff --git a/archive/ES_0.5626862626612322 b/archive/ES_0.5626862626612322
new file mode 100644
index 0000000..7499412
--- /dev/null
+++ b/archive/ES_0.5626862626612322
@@ -0,0 +1,22 @@
+archive/ES_0.5626862626612322---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T18:10:02.632
+Launch V∞: [8.048980624656899, -5.3912073133142915, 0.5243538635778328] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0577315972240589e-5, -9.065050421506992e-6, 6.636457490471292e-6] km/s
+ V∞_out: [-1.8092407194726319e-6, -1.5248243360524582e-5, 6.250856803195016e-7] km/s
+ time of flight: 1.8749577787384242e8 seconds
+ arrival date: 2030-04-17T20:19:39.632
+ thrust profile: [0.5774531688794032 0.011313052847873071 -0.11082750279955486; 0.09894610521895215 0.07035158094327675 -0.08631151212753269; 0.04548218698671421 0.05358431453669156 -0.07276818096831861; 0.07390532386916608 0.12970713919821114 -0.1820362451583632; 0.021844104381096775 0.04460591210286353 -0.0784444860476867; 0.017248886038913065 0.04642353991118764 -0.08733817348417673; 0.0082260615760006 0.029652309062551976 -0.061428637129128084; 0.005391199605263433 0.027522052268809834 -0.05928021904554911; 0.0010225459027207319 0.0052813747977767805 -0.012069147598322616; 0.000799757915479011 0.007163526531152366 -0.01643884881543783; -3.114825740218344e-5 0.0001638668381839683 -0.0004408528131885214; 7.301000430694187e-5 0.0003636341813169024 -0.0010981745411843798; 6.542468107013211e-5 0.0003185412457760641 -0.000818901933880996; -0.0002595695338405646 0.0004352130693346869 -0.00019783865172270405; 2.5653155855445195e-5 0.00023347641391372083 -0.00017892262623654822; 8.618255042728491e-5 -0.0005539255369608404 -0.0002546264426181421; -0.00022442954574251178 0.00048467404228024434 -0.0008968309335754044; 1.2162139123876722e-5 -2.7996074589953755e-5 0.00010979872685689491; 0.00014140179489623335 -0.00020113512405680917 0.00039710763393885373; -4.691632303450489e-5 -0.00016590171298896982 -0.0005473876374180481] %
+
+Mass Used: 107.39808430611038 kg
+Launch C3: 94.12615236548466 km²/s²
+||V∞_in||: 1.5430402468630315e-5 km/s
diff --git a/archive/ES_0.5626885828880006 b/archive/ES_0.5626885828880006
new file mode 100644
index 0000000..7aa151d
--- /dev/null
+++ b/archive/ES_0.5626885828880006
@@ -0,0 +1,22 @@
+archive/ES_0.5626885828880006---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:48:47.362
+Launch V∞: [6.578286677288327, -7.428225469099222, 0.08789394197401422] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3433498402186928e-9, -2.527972012235456e-10, 5.544058557540606e-9] km/s
+ V∞_out: [-9.404559336577544e-10, 2.154229139508857e-9, 2.988293583493382e-9] km/s
+ time of flight: 1.874957778744414e8 seconds
+ arrival date: 2029-04-10T20:58:24.362
+ thrust profile: [0.19087812033288282 -0.051274268314865847 -0.07439458016983722; 0.05200725770368752 0.011887451675131179 -0.06344669893749036; 0.051354056041595875 0.023080623319738036 -0.10463795979233187; 0.05145976499039695 0.03079572421138714 -0.14552564989325503; 0.04675688586884377 0.0332487783963554 -0.16850350699592348; 0.020606723552495203 0.016440256083553626 -0.09230267853389425; 0.013197180569930432 0.01134420422742778 -0.06983710843879155; 0.010632725498596047 0.00979669973633893 -0.06420101735924781; 0.006499916665214373 0.00675625199612968 -0.04762379608405519; 0.0018185160621109666 0.001091530295265652 -0.011503245378027965; 0.0042217890694666044 0.004230757701879753 -0.030228307417786947; 0.00029533760457097304 0.001240773713608102 -0.007508855674116313; 0.0014597083431440142 -0.0021145642663299427 -0.0006597988434185503; -0.00027071882768356045 -0.00033091152584336346 6.514674524533363e-5; 0.00030551050137569925 0.0006880254431251894 0.0009105415379046459; 0.0006145111791109417 -7.30789339819266e-5 0.0018385602350685214; -0.00032305777483547765 -0.0020954241138625603 0.002100097546888631; 0.0024930307326671963 0.00020537038353843546 0.006731674614516139; 0.00043987612508814434 -0.0006396652600486325 -0.000931312059599365; -0.0004385849918649682 0.0013641402496890214 -0.0007071168997197363] %
+
+Mass Used: 82.11934502450549 kg
+Launch C3: 98.46011457339918 km²/s²
+||V∞_in||: 6.024265945991981e-9 km/s
diff --git a/archive/ES_0.5626935094653962 b/archive/ES_0.5626935094653962
new file mode 100644
index 0000000..9ae61bc
--- /dev/null
+++ b/archive/ES_0.5626935094653962
@@ -0,0 +1,22 @@
+archive/ES_0.5626935094653962---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T08:38:42.096
+Launch V∞: [6.5168259408163065, -7.413162033664004, -0.03725943609582283] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.394960726777937e-9, -1.8993209919165205e-9, 1.9982588795973186e-9] km/s
+ V∞_out: [1.0764409556555833e-9, -2.3761597193790014e-9, -3.3961223743502566e-9] km/s
+ time of flight: 1.8749577787479448e8 seconds
+ arrival date: 2029-04-09T10:48:19.096
+ thrust profile: [0.21957454724237924 -0.05240343568514346 -0.06898129565986337; 0.06977270873070841 0.021921444506674707 -0.07280664642061419; 0.07298332753329924 0.04341727786628029 -0.12631304987685768; 0.0763705266292596 0.06250972904913196 -0.1876737993370964; 0.051767668427463776 0.053535923467550116 -0.16695529327673853; 0.022320339002820246 0.02596511106279539 -0.08977987788632233; 0.015561706900885104 0.017293726659934554 -0.06759707498302507; 0.006510354716440667 0.009184968495219926 -0.036788727227570046; 0.006008750964038946 0.00920865060712521 -0.03766686636829867; 0.0002733808011428653 0.0019924276114963654 -0.008916017888470552; 0.00040529252540852194 0.0010652949055541662 -0.004185380886666711; 0.0021376310019373037 -5.179164309049864e-5 -0.007036356752905673; -0.0019100130963395742 -3.680722667667507e-6 -0.0017015813423902379; 0.000447162808954478 0.0002459239049414383 0.0007828531951171807; -0.002726283315187274 -0.001205638595365852 0.0011363680507233236; 0.0013648183033755528 0.0054748115574465685 8.829264116673625e-5; 0.0015963120670631956 2.2904866325136868e-5 -0.004236006168436154; 0.0003004048240158101 -0.003056099685757127 0.004917996438626348; -0.002497067616340759 0.0008014234740138912 0.0031562786453431108; 0.0013916266522762469 0.0006660866157466049 0.0006490765720620739] %
+
+Mass Used: 88.16104469227594 kg
+Launch C3: 97.42537994583195 km²/s²
+||V∞_in||: 3.6518893278730382e-9 km/s
diff --git a/archive/ES_0.5627038435425895 b/archive/ES_0.5627038435425895
new file mode 100644
index 0000000..cedcee4
--- /dev/null
+++ b/archive/ES_0.5627038435425895
@@ -0,0 +1,22 @@
+archive/ES_0.5627038435425895---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T16:55:59.427
+Launch V∞: [6.368745239634983, -7.292677231640499, 0.09978677385492865] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.676405756726173e-6, 1.140103219534165e-6, 6.655334808072213e-9] km/s
+ V∞_out: [-1.6153523062310933e-6, 3.6271007588978225e-8, 8.600063838998684e-6] km/s
+ time of flight: 1.8749577787461087e8 seconds
+ arrival date: 2029-04-07T19:05:36.427
+ thrust profile: [0.524960951034745 -0.12120202135244017 -0.16317607181446697; 0.08396057792453633 0.026202229547562537 -0.0866641977436068; 0.07640869541304748 0.046097251933224385 -0.13169320035500082; 0.08588695886464284 0.0697071700218291 -0.2032425885295645; 0.025437936295088046 0.02476355433518508 -0.0815557717084757; 0.012718620691440176 0.014262675746063077 -0.05060295822825132; 0.021588608516482314 0.027214786731095054 -0.09997273327862818; 0.007868942697356478 0.011147400631447714 -0.04326731439346547; 0.006807028086185714 0.009621946125394397 -0.03867844916769552; 0.003404200275655711 0.006199349542539893 -0.025132386138333695; 0.0016663794238191332 0.0027678933713831937 -0.012337081097610138; -0.000805267044430743 0.0015744679026600652 -0.0009647660907770267; 0.00017457303177471472 0.00023459627705768452 -0.0013905306749639182; -0.0008487041366367806 0.0008857129588793279 0.00035640394544607097; 0.0006201949747244493 0.0002837305699471478 -0.0014122917633831039; -0.0009963904305953925 0.0008367666853155652 -0.0005176139552618313; -0.00041255975482770393 0.0001091961372134602 -0.00043544358458219817; 0.0030219925637760547 -0.00015573799968331289 0.0014012329311506634; -2.020209500544349e-5 0.00021251806766412167 -0.00045740806709802253; -0.004119783113225445 -0.0027776256323488054 0.0018600699699387823] %
+
+Mass Used: 109.58939936011984 kg
+Launch C3: 93.75401453249737 km²/s²
+||V∞_in||: 8.75099402925317e-6 km/s
diff --git a/archive/ES_0.562716378949776 b/archive/ES_0.562716378949776
new file mode 100644
index 0000000..60f1afe
--- /dev/null
+++ b/archive/ES_0.562716378949776
@@ -0,0 +1,22 @@
+archive/ES_0.562716378949776---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T22:43:20.638
+Launch V∞: [7.45961209647339, -6.313401250370333, -0.45540005818254137] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.247421872732936e-5, 3.1324261652969426e-5, 2.8119507400926616e-6] km/s
+ V∞_out: [-2.0982169313997193e-6, 6.376473095739519e-6, 3.805022357241657e-5] km/s
+ time of flight: 1.6773675382734132e8 seconds
+ arrival date: 2029-09-03T08:15:53.638
+ thrust profile: [0.4101136161886014 -0.06762449576080028 -0.15648100350051367; 0.11666013582649407 0.040205628116361906 -0.1428123277429246; 0.06118265953027122 0.03663127856831379 -0.13100440675432942; 0.053374299379787944 0.04130528583730796 -0.1638364989679565; 0.026350548158162443 0.023788316144419848 -0.10482524544434696; 0.026349592824253403 0.026683546476125173 -0.12705670508191896; 0.013895896529414373 0.015441483015042771 -0.07845362972679835; 0.014994774845989479 0.018042005634587164 -0.09784150607869517; 0.00453799541237133 0.005694472460975027 -0.03273480794874844; 0.003973082859340933 0.005194578402962216 -0.03141819960162633; 0.0011736936118179014 0.001012209057205937 -0.0035862024847028023; -0.0003693095825470332 -0.0007778482253625103 -0.0011161195132207945; 0.0007141991461806095 -0.0003947171453747532 -0.0029494665865095644; 0.00016004351670691305 9.931384926658519e-5 -0.0017601161244727818; -0.0007171811100412949 0.00038001281705825975 0.0006695500770205235; -0.00048719038200197625 0.0006334443324637084 -0.0007840151441500978; 0.0001719031155424874 6.690260219655323e-5 -0.002468261225349178; 0.001037931856837026 0.0013379910345817255 -0.00038658820960981246; -0.0003234386952271058 -0.00010829252270416962 0.002301479238605477; -0.00046298634769267053 -0.0010669374086329049 0.0006845877140057962] %
+
+Mass Used: 98.18105849377434 kg
+Launch C3: 95.71223719102247 km²/s²
+||V∞_in||: 3.8654973062624684e-5 km/s
diff --git a/archive/ES_0.5627173459204741 b/archive/ES_0.5627173459204741
new file mode 100644
index 0000000..3db621b
--- /dev/null
+++ b/archive/ES_0.5627173459204741
@@ -0,0 +1,22 @@
+archive/ES_0.5627173459204741---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T09:51:13.276
+Launch V∞: [6.500944902553005, -7.4252316046059885, 0.16897411797648126] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.760225244203671e-9, 4.741279020834579e-9, 2.1852701400528995e-9] km/s
+ V∞_out: [-1.9823880776969637e-9, 3.811621085720277e-9, -6.195223149705042e-9] km/s
+ time of flight: 1.874957779420617e8 seconds
+ arrival date: 2029-04-09T12:00:50.276
+ thrust profile: [0.1997905387809184 -0.0453262745305734 -0.06517097453407321; 0.08433401073594717 0.026625759128739775 -0.08519136081463603; 0.1445371752274051 0.07489541762018383 -0.21803010894197905; 0.030203376360174127 0.024049544242197466 -0.0747085023976453; 0.025315691424745986 0.02450280065828401 -0.08028791049748038; 0.026860884454049775 0.030120251581770504 -0.10279561248854581; 0.03342923805377894 0.04436230133859041 -0.15125749860452517; 0.007970636941565497 0.011676339625525584 -0.044204365919707826; 0.0023358538617405536 0.003545920239463486 -0.014747782915794115; 0.00565395562685547 0.008853058998670211 -0.03688497844294591; 0.0007779399518340787 0.0006508334088438496 -0.003902412278826509; 0.0005623401437220272 -9.834878184089037e-5 0.0003259115369396038; -1.6708173929569738e-5 -8.318571662746922e-5 0.00045348887105237383; -0.0005123389981995334 -0.0005839142418299818 -0.00021504146883227705; 0.0006843448381891792 0.0014205939473800984 -0.0033412548523591877; -0.0034729121357587856 -0.0033003365835076377 -0.002628363599421745; -0.0014354520187991342 0.002658348330297135 -0.00020217527221167168; -9.12594454743738e-6 -0.0004887384824327475 0.003199735918481939; 0.00016423250761787904 -0.001045883851179504 -0.00030430554544364895; 0.00022261897406058856 -0.0010904058343994174 0.005333627278417769] %
+
+Mass Used: 88.1916462202962 kg
+Launch C3: 97.42490126061547 km²/s²
+||V∞_in||: 5.90541918386427e-9 km/s
diff --git a/archive/ES_0.5627187632699325 b/archive/ES_0.5627187632699325
new file mode 100644
index 0000000..d0bade5
--- /dev/null
+++ b/archive/ES_0.5627187632699325
@@ -0,0 +1,22 @@
+archive/ES_0.5627187632699325---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T09:35:11.251
+Launch V∞: [6.277192030205552, -7.48180758058015, 0.0979963166133478] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.839314825057355e-9, 4.704917460847284e-10, -4.340179185257579e-9] km/s
+ V∞_out: [-2.2089090727829972e-9, 4.837920744060183e-9, 6.970591471822038e-9] km/s
+ time of flight: 1.846336178016674e8 seconds
+ arrival date: 2029-03-06T08:42:08.251
+ thrust profile: [0.38056145056902335 -0.09664814459181409 -0.10469947159801869; 0.08957046684502125 0.02892541581714261 -0.08825779285639697; 0.0663973113566322 0.04039643900884982 -0.1054064144108716; 0.054595327111693744 0.044456492074991034 -0.12179517457584672; 0.03574728626370883 0.035394962502328556 -0.105851593633433; 0.03779921828063325 0.044576249439766416 -0.13509714512414836; 0.028820079571770883 0.043648354226975966 -0.13331469646888378; 0.0100284740128196 0.014586728620460343 -0.05126708373210211; 0.009145244170948372 0.014689874384327364 -0.050948629061214; 0.002103600255600335 0.00408000832111027 -0.016780445406357133; 0.0004874126245470576 0.0013928462256002903 -0.005546606742460178; 0.0004928324704173586 5.430058778235613e-5 -0.0012919901444958062; 0.0007961853529503648 0.0011663810679854235 -0.0012382085520251437; 0.0005533741515439939 -3.280771783590594e-5 -0.0020941355061353715; -0.00032217864091726523 0.0008830628573113025 -0.0006431387405947724; -0.0008686097075802351 0.0010113529976491344 0.0006418421970554478; -9.625389302282352e-5 0.0007335439421000444 -0.001599400067652115; -0.00021869969248401822 -0.0001554429898827559 -0.002725742389205226; -0.0003098380270759774 -0.0005236008663615822 0.0002516271359493447; 0.0015362095795578572 0.00027425366604391513 -0.0012669878725181487] %
+
+Mass Used: 100.06246202758166 kg
+Launch C3: 95.3901877349725 km²/s²
+||V∞_in||: 6.51747541762122e-9 km/s
diff --git a/archive/ES_0.5627259166882693 b/archive/ES_0.5627259166882693
new file mode 100644
index 0000000..b5a1543
--- /dev/null
+++ b/archive/ES_0.5627259166882693
@@ -0,0 +1,22 @@
+archive/ES_0.5627259166882693---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T09:07:23.196
+Launch V∞: [6.5540361466079995, -7.426001250544117, 0.14991356538757872] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.449893333115285e-9, -8.28222566046145e-12, -5.805657816342807e-9] km/s
+ V∞_out: [-2.3280708305769783e-9, 3.978120165423665e-9, 7.340746285200155e-9] km/s
+ time of flight: 1.8575715818262187e8 seconds
+ arrival date: 2029-03-20T08:20:01.196
+ thrust profile: [0.18875154004647354 -0.05139811758831257 -0.06811313124810305; 0.08030507254058399 0.019570821384442112 -0.08999175064352535; 0.05794275929112292 0.028412049762831577 -0.11034926385862949; 0.037113423536407994 0.024985269553781213 -0.10144704199418131; 0.04494847733607042 0.033823727058194 -0.1468317840696763; 0.042187684324259456 0.03180508840065437 -0.1511408153670405; 0.01585418222041821 0.01582450883496569 -0.07747754758597544; 0.0066665428094015095 0.007192433016095798 -0.03822341846305997; 0.0063308322794505935 0.007484985300583358 -0.04472235993648209; 0.008589644112318167 0.00847990345421305 -0.047719182413622975; 0.00039940718712652863 0.0012781928013177338 -0.003514789612624431; 0.001429807087643898 0.0017057075595605165 -0.012020168227645425; -0.002284857341343631 0.00011279475702394163 0.001442246770782195; -0.0005867012706252386 0.0006289377026310264 -0.0033221236289716054; -0.0010973407628595512 0.0032844963942565294 -0.0018132430210341904; -0.0005585813597354487 -0.000508085533783125 -0.0015314656715233975; -0.000225165230720041 -0.00031386857517205123 -0.0019045774402190589; -3.5745329340950566e-5 0.00017579194725747614 -0.000982837639079768; 0.000871171692602463 -2.180125552559983e-5 -0.0003783354705243253; 0.003082720735590096 -0.0006428478790425707 0.004172751973511376] %
+
+Mass Used: 84.12731177923115 kg
+Launch C3: 98.12335846121424 km²/s²
+||V∞_in||: 8.677952251786663e-9 km/s
diff --git a/archive/ES_0.5627280250016633 b/archive/ES_0.5627280250016633
new file mode 100644
index 0000000..a1d815e
--- /dev/null
+++ b/archive/ES_0.5627280250016633
@@ -0,0 +1,22 @@
+archive/ES_0.5627280250016633---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T07:43:37.459
+Launch V∞: [6.375824807848056, -7.342536790196925, 0.06325529633420743] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1763925411846936e-5, 1.5366515022646352e-6, -3.2643191537090305e-8] km/s
+ V∞_out: [-2.2926597119883233e-6, 5.249697875676675e-8, 1.1638721034104606e-5] km/s
+ time of flight: 1.874957778750514e8 seconds
+ arrival date: 2029-04-07T09:53:14.459
+ thrust profile: [0.39432594092791495 -0.07735239886341229 -0.11453618319979827; 0.1683014999668032 0.06438671064447887 -0.1540308505075896; 0.09298831297011617 0.06750194425481763 -0.14873927554845776; 0.037635711573166974 0.03572334246156351 -0.08639812249357338; 0.03540579898570081 0.04205340393120068 -0.10602809208445285; 0.021980287454700643 0.03138756468758215 -0.0869875631960744; 0.023448216496487973 0.04383357193608814 -0.11543865320678419; 0.013695963516784588 0.02117430584479244 -0.06307160317478787; 0.004072196482905346 0.008444765341001017 -0.02640597165567753; 0.0005380442086528856 0.0012839334915132495 -0.004356371687124506; 0.001779637607948029 0.004417313508336477 -0.017689519892169447; 8.610750139515153e-5 4.869177097914476e-5 -8.253670346739601e-5; 2.7370600051500073e-5 8.578330516399908e-5 -0.00027454262283109477; 1.2804980448886055e-5 2.7363130722441364e-5 -0.00010545377078272701; -2.7575525793696034e-5 -0.00016659349161551103 -0.0001925482466388747; -1.4278512877641474e-5 7.598051159206609e-5 -0.00015189796164150952; -0.00010176706334491531 0.0001998883583341073 -0.00021545512053335866; 0.00016960766728823438 0.0002223443392688959 -0.00034028496395594577; -0.0001419844935122011 0.00011899346623932082 -0.00010595050662395064; 2.5806389745332108e-5 -1.4587397664998222e-5 6.575912540373783e-5] %
+
+Mass Used: 104.869422420305 kg
+Launch C3: 94.56798972828038 km²/s²
+||V∞_in||: 1.1863907640944613e-5 km/s
diff --git a/archive/ES_0.5627292841526533 b/archive/ES_0.5627292841526533
new file mode 100644
index 0000000..1a53fa4
--- /dev/null
+++ b/archive/ES_0.5627292841526533
@@ -0,0 +1,22 @@
+archive/ES_0.5627292841526533---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T07:44:38.347
+Launch V∞: [6.627003467355458, -7.46209122908553, 0.12665091668066916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.766146778073685e-7, -0.00010367742838795581, 7.122595230111395e-5] km/s
+ V∞_out: [6.53153356281739e-5, 0.00010647215943637195, -2.114361427308062e-5] km/s
+ time of flight: 1.8749577787458923e8 seconds
+ arrival date: 2029-04-11T09:54:15.347
+ thrust profile: [0.10637500327336162 -0.029144907822321087 -0.04202807312894041; 0.04376767683896558 0.009363777529634664 -0.05258246015555343; 0.05211376549503461 0.02228876439768786 -0.1044969290361076; 0.0480684118971726 0.02686472412086689 -0.13423983270723117; 0.03835739323987912 0.02529521283948855 -0.1366115616552529; 0.028122442556726888 0.02065221943775368 -0.12062282320169809; 0.023380164570537057 0.018718397639303722 -0.11750164487048291; 0.006642330459269189 0.0058020354210551245 -0.03942688969366818; 0.010647641880713304 0.009691531152327773 -0.06854171260931557; 0.0020949526270702557 0.0035068973372669033 -0.006596170589159767; 6.014921269667647e-5 -0.0001590624098533654 -0.007847153523421883; -0.0022506424163917685 -0.000994769300872359 -0.006755192048187961; 0.0004600685866338445 0.0008988271066365482 -0.009472871645113071; 0.0010916058300042184 -0.0032510609233971596 -0.005092198946969278; -0.0018762601877958971 0.00339667744096065 -0.003837219134871032; 0.0003786318069585047 0.0007847612232566028 -0.0006467368907969789; -0.0009882090013408867 0.0018886135122448992 -0.001795298742400762; 0.00047297466262831303 -0.0020419112176406472 9.329501920534561e-5; 9.648995548026712e-5 -0.00021287295697170437 -0.00034581121454911037; 0.004314133096858496 -0.004895575255669259 -0.0036653423205486773] %
+
+Mass Used: 75.42404279840594 kg
+Launch C3: 99.61602092223251 km²/s²
+||V∞_in||: 0.00012578667368587105 km/s
diff --git a/archive/ES_0.5627304029086351 b/archive/ES_0.5627304029086351
new file mode 100644
index 0000000..e7b2db6
--- /dev/null
+++ b/archive/ES_0.5627304029086351
@@ -0,0 +1,22 @@
+archive/ES_0.5627304029086351---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:07:28.346
+Launch V∞: [6.679987908270418, -7.305773944169552, 0.20590291191058224] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.643933193657651e-5, -4.4838373205921896e-6, 7.147001937252978e-8] km/s
+ V∞_out: [5.7924468182983775e-6, -1.3001266740780488e-7, -2.6182245959315646e-5] km/s
+ time of flight: 1.8749577787505382e8 seconds
+ arrival date: 2029-04-08T17:17:05.346
+ thrust profile: [0.2355142231535343 -0.054719536273983904 -0.079092906215378; 0.04739356230977748 0.015258033329120487 -0.05232083267064786; 0.025047437240531815 0.014255199991483643 -0.04638236589943847; 0.05306187377049844 0.040358522534891195 -0.1311938833259611; 0.03070215998374108 0.029712918397313708 -0.10031758306497451; 0.02038505541410652 0.023575148293323536 -0.08370830092992042; 0.033209329971740094 0.04314992751074302 -0.1464009894076945; 0.018332031119464902 0.02479838849736709 -0.09812515374280471; 0.00629103232909602 0.00931636928450611 -0.04110872658376143; 0.008590461289467239 0.014133869091739281 -0.0605537466237289; 0.004573952003735542 0.00749361915152067 -0.0342426297141518; 0.0004033029388858092 0.0006577581946724558 -0.0030615429620930905; -1.0015856049901201e-5 -8.872409540946775e-6 -0.00018344905539937107; -4.955823134219348e-5 -1.6896036364598665e-5 -0.0002659082726608816; 0.00013104263839398562 8.478027485849771e-5 4.3634221312310786e-6; -0.0004247562229757163 0.0001093641175786663 -0.0007067710660010028; 0.00010400357402816487 0.0002453505219447308 0.00035552250579404677; -0.0008003878677823142 -0.00015136756353632938 9.181748702182744e-5; -0.00014777695170652494 0.00031878520005862074 -0.00020549920936540464; -0.00023511320861386925 0.00035665904421039153 0.0005163563313111488] %
+
+Mass Used: 84.62482696878033 kg
+Launch C3: 98.03896738707897 km²/s²
+||V∞_in||: 2.6816938272921447e-5 km/s
diff --git a/archive/ES_0.5627307070157943 b/archive/ES_0.5627307070157943
new file mode 100644
index 0000000..6ef25fd
--- /dev/null
+++ b/archive/ES_0.5627307070157943
@@ -0,0 +1,22 @@
+archive/ES_0.5627307070157943---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T05:03:51.501
+Launch V∞: [7.4720888261079965, -6.329468175291842, -0.2820238369534829] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.551414322251315e-5, -5.625002690983722e-5, -4.83343215679139e-6] km/s
+ V∞_out: [3.5656111366625402e-6, -1.7832797696688263e-5, -6.387096862513867e-5] km/s
+ time of flight: 1.6684702095020598e8 seconds
+ arrival date: 2029-08-23T07:27:31.501
+ thrust profile: [0.33933702341113 -0.052699302953313425 -0.11821029192964819; 0.13545546305219125 0.04890228859310777 -0.14414755180168398; 0.07116153027852501 0.04475770515263447 -0.13195195699811477; 0.06353528648789558 0.05233589332333107 -0.16626826387778146; 0.05704678017066249 0.056025458936927286 -0.1931781180118532; 0.02157394719575262 0.024078134346755015 -0.09295046714503892; 0.008200394509427705 0.01059662234538811 -0.04612458393087528; 0.0035388984375797545 0.0047573515922057705 -0.023436259744821043; 0.010504890880648215 0.014373985897584802 -0.0950080341740411; 0.0019298410085178642 0.0029959324792441303 -0.016130700438548935; 0.004372223103141533 0.009249645251141782 -0.04188038317294347; 0.00026630926894292094 0.0006944013401786271 -0.0018492757185022122; -0.0002211577232566201 -4.1668589803275414e-5 -0.0016433881368133748; 4.399138544515361e-5 0.0004378250397725832 -0.0012457952051463115; 0.000287765607016942 0.0006441829075222105 -0.0011460494216969418; 0.00016072063403239922 0.0006985283363085723 -0.0008673367914248339; 5.4169572060704216e-5 0.00020434857693001594 -0.0010193690815710693; 7.380744056444748e-5 -2.711797382355408e-5 -0.00047553601180540467; -0.00014397467870877674 -7.907185787948533e-7 -0.0004122076784343979; -0.00012847550168536726 0.00033410629953373666 0.0006927947744510885] %
+
+Mass Used: 96.67189671573396 kg
+Launch C3: 95.97381625189018 km²/s²
+||V∞_in||: 6.669844048102544e-5 km/s
diff --git a/archive/ES_0.5627346395676246 b/archive/ES_0.5627346395676246
new file mode 100644
index 0000000..d40ed9d
--- /dev/null
+++ b/archive/ES_0.5627346395676246
@@ -0,0 +1,22 @@
+archive/ES_0.5627346395676246---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T04:11:40.284
+Launch V∞: [6.5858282616417005, -7.396659182024872, 0.10754437228624349] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4318269928607324e-7, 3.5727587691311854e-8, -4.4689700620226385e-8] km/s
+ V∞_out: [1.48175956569849e-7, -3.965294958011397e-8, 1.8484371071284686e-8] km/s
+ time of flight: 1.874957778749329e8 seconds
+ arrival date: 2029-04-10T06:21:17.284
+ thrust profile: [0.18429067525196222 -0.05005872789391952 -0.07001599549066878; 0.12062171274927495 0.028306669365648695 -0.1411705162824713; 0.042365116103685485 0.0189628115468731 -0.0846925223463851; 0.04535255492475915 0.02751978971014456 -0.12713275068689064; 0.026753850714202408 0.01901667750512564 -0.09636639605777994; 0.02491343853600884 0.019993141504164237 -0.10837282865282914; 0.014168922764227312 0.01355601832489548 -0.07507718490381109; 0.010844227573525708 0.010920829268790377 -0.06571439861218357; 0.013978399433346108 0.013966646920266508 -0.09111190009884099; 0.0033243548052633186 0.003432712663860179 -0.02429106974236972; -0.0003385778808299713 -0.00020261776342701446 -0.002655068072744846; -0.0019032725007890176 0.0005683449484441693 -0.002323673858219695; 0.0006375628910221555 -0.00012602783671452082 -0.001140713691182264; -0.0014608597952887495 0.0008228967814717243 -0.00116973639703528; 0.0002714056728624403 -0.0007688523252794067 -0.0013130201588677365; 0.0005514378589691289 0.00010377843574801027 0.0023784161827414127; 0.0029587478970505717 0.0008979824349133679 -0.002047712683964382; -4.0270406452822156e-5 -0.00022446037491357903 -0.0008074350471583942; -0.005454158280490458 0.001930394517390849 -0.002375452290510123; 0.0017411990305649916 0.0005853756448013347 4.681866640247629e-5] %
+
+Mass Used: 84.30135685208461 kg
+Launch C3: 98.09526673888185 km²/s²
+||V∞_in||: 1.5419116459321502e-7 km/s
diff --git a/archive/ES_0.5627369666565475 b/archive/ES_0.5627369666565475
new file mode 100644
index 0000000..f61117e
--- /dev/null
+++ b/archive/ES_0.5627369666565475
@@ -0,0 +1,22 @@
+archive/ES_0.5627369666565475---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T07:41:54.083
+Launch V∞: [6.434357241691751, -7.467600728071105, 0.1421438808209085] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010443828507238119, 0.0011321171194194212, 0.0010710979382515548] km/s
+ V∞_out: [-0.001264002087430115, -0.0005673188389942027, 0.0012647083669638977] km/s
+ time of flight: 1.8438334498061812e8 seconds
+ arrival date: 2029-03-03T09:17:38.083
+ thrust profile: [0.20434156980629478 -0.0523997891950304 -0.07078401030439825; 0.15070350808751148 0.04299458588383303 -0.15337109094461923; 0.04153625976028631 0.022158527956200113 -0.07284701229068992; 0.07514651411797325 0.054970824122311114 -0.17621630944576977; 0.0420702589758459 0.037090549081135564 -0.12968808061217602; 0.031979865395619485 0.032382505201351365 -0.119476901004006; 0.02330026267775636 0.02663889272976419 -0.10327671675563858; 0.008985783083309933 0.011053221494524954 -0.046458427677233; 0.003436645643957235 0.0044925434237214545 -0.021218014953355322; 0.0023972929700528116 0.0022778798608513945 -0.006547074676007377; 0.0008942739100747677 0.002020153009726622 -0.013935824138506428; -0.00041152748468687675 0.0009341339091193156 -0.0038611103535417727; -0.00028598527460075814 0.0002810550056444259 -0.0006214908165172138; -0.00031933638382969777 0.000297897923204671 -0.002196255244571674; 0.0021888851650924772 -0.00038435381782225483 0.0007171472209140588; -0.0022088497615056425 0.0007471476974728749 0.0005120055891823284; -0.001964976674807538 -0.00015922548543077086 0.0028108282035517232; 0.000799694438224317 0.00011402013042156894 0.0006158274532157204; 0.0013444278670774856 -0.001696924988703163 0.0021424890818124757; 0.0006199153070126786 0.0008002390627503943 0.0029729735531558305] %
+
+Mass Used: 89.6068524216571 kg
+Launch C3: 97.18621863045401 km²/s²
+||V∞_in||: 0.0018760798235403673 km/s
diff --git a/archive/ES_0.5627369875250436 b/archive/ES_0.5627369875250436
new file mode 100644
index 0000000..daa6b2b
--- /dev/null
+++ b/archive/ES_0.5627369875250436
@@ -0,0 +1,22 @@
+archive/ES_0.5627369875250436---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T21:44:41.954
+Launch V∞: [7.856548034382041, -6.048466800288793, -0.002134381432106768] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.7969366110986997e-8, -2.926131328827907e-7, 5.001052214941209e-8] km/s
+ V∞_out: [-4.349466264569281e-8, 1.7010103567304988e-7, 2.428400781526645e-7] km/s
+ time of flight: 1.7921529256581196e8 seconds
+ arrival date: 2030-01-18T03:46:13.954
+ thrust profile: [0.22364533387110752 -0.024528118822463404 -0.08887212380730417; 0.05351944886947384 0.019362470225772588 -0.07169900636673093; 0.04839384959589225 0.028220739985999454 -0.11300789920486091; 0.041955004570295704 0.030568492712165145 -0.1398894520624518; 0.03299665121034505 0.027305791531317066 -0.14230611430916945; 0.02329781401787659 0.02074244135281719 -0.12268348806858628; 0.014641915283499677 0.013513401949998878 -0.09068425104415427; 0.007527097907591561 0.007194271018991754 -0.05330925757745547; 0.0029171592619979233 0.004018974614026914 -0.026891094116601136; 0.003421502099629386 0.004473857012474079 -0.020038624238946066; 0.0008879604980794616 1.3644753355729951e-6 -0.011069679972075815; -0.006645032241331872 0.002566672620807787 -0.0023841911590017223; 6.193135036694036e-5 -0.002143025561648591 0.004938913339314385; -0.0011867771972474965 -0.0014067178715460483 -0.0018152038259658034; -0.001179162841388989 -0.008571852783202532 -0.0011055910523456672; 0.0014185945651710948 -0.009255592821273044 0.004939169443340801; -0.001784490365672563 0.00574635261046055 0.007336858497744264; -0.002238978655527868 0.005779284825520583 -0.001308295155148944; -0.0065164211522034925 -0.0004570912307999673 -0.0023173820873387684; -0.015545193679939635 0.00018328057950227404 0.003355071845819688] %
+
+Mass Used: 83.05555590894664 kg
+Launch C3: 98.30930220633218 km²/s²
+||V∞_in||: 2.9927440689776456e-7 km/s
diff --git a/archive/ES_0.562743467320991 b/archive/ES_0.562743467320991
new file mode 100644
index 0000000..8c6df6b
--- /dev/null
+++ b/archive/ES_0.562743467320991
@@ -0,0 +1,22 @@
+archive/ES_0.562743467320991---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T22:42:40.350
+Launch V∞: [7.8017571834962105, -5.7844265023797234, 0.1061102366094553] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3387920633969054e-8, -1.230900334706599e-7, 4.3270114007906165e-8] km/s
+ V∞_out: [-1.9563146798423392e-8, 7.115704967127471e-8, 1.0930258860152588e-7] km/s
+ time of flight: 1.800406653298426e8 seconds
+ arrival date: 2030-01-22T18:00:25.350
+ thrust profile: [0.46812763122750256 -0.020710275199640284 -0.13239851001364913; 0.1285019931459912 0.07137472224532661 -0.12547969016912908; 0.08172665637500148 0.07593631908456085 -0.14337241415708218; 0.03573699930076184 0.044850014498279155 -0.09770491043194492; 0.02430220925257088 0.037703929743606764 -0.09016054839222612; 0.019003941975590088 0.03558734787397902 -0.09093169461572584; 0.014457220930138258 0.0347074864638359 -0.09171105833605775; 0.005309640405414962 0.012778245662144812 -0.03766836187996379; 0.0044707611595437265 0.012478879754306973 -0.03403421730630955; 0.0025115496051166548 0.0072036192773922755 -0.025971899266919847; 0.004745847792640315 0.014217240544917653 -0.046800993706750144; -2.7139250101147283e-6 0.0013154243313428754 -0.00037513927545513226; 0.0026728983817142396 0.002367650167681553 -0.002757797936545543; -0.0002656477168429133 0.004222340499145584 -0.001601484694435173; 0.0005285365718017348 0.001860360869037955 -0.0018583341153598598; -0.009847344083004746 0.005035383080357916 -0.007211668403531235; -0.004767462677718889 0.002339558226859375 0.004943661071853778; -0.0015526551426388816 0.002415037959580687 -0.0018675054904554289; 0.0007185240226237801 0.004658329605986939 0.003707224488902; -0.0001846813853654297 0.005946864459427583 -0.009801796532229031] %
+
+Mass Used: 106.22750232626731 kg
+Launch C3: 94.33826449398094 km²/s²
+||V∞_in||: 1.311590466760369e-7 km/s
diff --git a/archive/ES_0.5627478947251071 b/archive/ES_0.5627478947251071
new file mode 100644
index 0000000..5063576
--- /dev/null
+++ b/archive/ES_0.5627478947251071
@@ -0,0 +1,22 @@
+archive/ES_0.5627478947251071---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T06:08:11.016
+Launch V∞: [6.588332259199405, -7.487452474343356, 0.077550972496214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.536008829971837e-8, -3.787544232308049e-8, -2.4197270735985146e-8] km/s
+ V∞_out: [1.0612005008251035e-8, -2.3914819966455462e-8, 3.506895152177392e-8] km/s
+ time of flight: 1.846458765440666e8 seconds
+ arrival date: 2029-03-08T08:39:27.016
+ thrust profile: [0.10711524435387143 -0.03355297764741457 -0.044838481570653475; 0.05417504512219692 0.009365871097923048 -0.07073568205952563; 0.055518477615181576 0.019624857890534662 -0.11721580918593938; 0.049672109698456146 0.0232396888838415 -0.1460356287194249; 0.03958532781368836 0.021628043049262392 -0.14796799153330797; 0.02473921820890365 0.014886474247552161 -0.11316589679306611; 0.01830122391935323 0.012273499777612865 -0.09716172420709947; 0.0115321400277633 0.007749707194746648 -0.06923272172258628; 0.00457472877526852 0.0030374069796105466 -0.030508875653675892; 0.004576516084175795 0.0031435132531387037 -0.03394483166400282; 0.0014317713720778508 0.001059588126102558 -0.011064406679000865; 0.0011757857268630443 0.0003651257862383353 -0.0015103609289325232; 0.0007264063985047285 0.001798938453431183 -0.000997367069090086; 0.0007277379064543964 -0.0005174549872034508 -0.0009228301431938163; 0.0012471243110666055 0.0010564842106900257 -0.001891860942370674; -0.002927130318501675 -0.0003439978220647421 -0.001173062370335211; -2.058021694706152e-5 0.00026095148580235965 -0.0007235547510916571; -0.0013098679838795984 0.0002624654944596398 0.0007816836273624173; -0.0011933634900800532 0.0009035361664708685 -0.0016996242235405093; -0.0016206228341037914 0.002406139742159542 -0.004989806459883659] %
+
+Mass Used: 76.27373995808193 kg
+Launch C3: 99.47408066649308 km²/s²
+||V∞_in||: 5.160611514936067e-8 km/s
diff --git a/archive/ES_0.5627518345751642 b/archive/ES_0.5627518345751642
new file mode 100644
index 0000000..0a7d9ca
--- /dev/null
+++ b/archive/ES_0.5627518345751642
@@ -0,0 +1,22 @@
+archive/ES_0.5627518345751642---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T19:16:26.594
+Launch V∞: [7.950173162274063, -5.883664007913288, 0.02005757616051744] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.8486132478258e-5, -6.533721288721761e-5, -5.402415020314006e-5] km/s
+ V∞_out: [-1.0542818727452928e-5, 7.37180157283885e-5, -8.826133344734673e-5] km/s
+ time of flight: 1.852965664837569e8 seconds
+ arrival date: 2030-03-30T10:32:32.594
+ thrust profile: [0.2144977297311318 -0.007180188505592752 -0.07908237805466913; 0.12118455008281927 0.06003497099527979 -0.14797085715046887; 0.03657529468880478 0.028775000447568158 -0.08429245313850965; 0.03910618663192445 0.04031079940719279 -0.13014029132475385; 0.023514578802202233 0.028247276003965056 -0.105679108263672; 0.014355448681286645 0.019134921265637123 -0.08002369752920234; 0.010237870909275438 0.015491759073698694 -0.06965769524764087; 0.012255340677661396 0.01880290815023613 -0.08949148174997347; 0.002413564436896328 0.004765661939059218 -0.025068721425255534; -9.542964304126592e-6 0.00011526111005750225 -0.00210943511956819; 0.001097778270770999 0.0019811953512704284 -0.013087726684425415; 0.0010145729277080922 0.00065576500879101 0.002119965223212096; 0.0006833801480672416 8.3267967341288e-5 -0.0014923000679698743; 0.00226434929620031 -0.005567911795798633 -0.0033827634646611086; -0.0010344096820571363 -0.002498971689287547 0.0045410078938684754; 0.00037250624380413545 -0.00015384518965522187 -0.0013268965367570316; 0.0053857702430026985 0.006918461144577252 0.007723639809810067; 0.0011449443490284474 -0.009211195182890819 0.00010003485395712597; 0.0002572728460819866 0.02270568375537423 0.009269718188829568; 0.018575250505146253 0.018208789298860807 -0.02060868525374937] %
+
+Mass Used: 85.90871998633384 kg
+Launch C3: 97.82315777451846 km²/s²
+||V∞_in||: 0.00011553195741627377 km/s
diff --git a/archive/ES_0.5627521337908287 b/archive/ES_0.5627521337908287
new file mode 100644
index 0000000..5b3139b
--- /dev/null
+++ b/archive/ES_0.5627521337908287
@@ -0,0 +1,22 @@
+archive/ES_0.5627521337908287---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T18:37:54.194
+Launch V∞: [7.7535213171554105, -5.810879221798674, 0.022119137365150653] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.157793008494802e-5, -1.5129430466608904e-5, -0.0009934570603525312] km/s
+ V∞_out: [0.0009282184604543203, 0.00030016780935313107, -0.00015859233039365543] km/s
+ time of flight: 1.8530135099532005e8 seconds
+ arrival date: 2030-03-27T11:13:44.194
+ thrust profile: [0.4666714817040469 0.008267615324082822 -0.12949097524526504; 0.14476180198108857 0.09251567968447359 -0.14634523707114136; 0.08205881581881001 0.08681380051917265 -0.15364330397732395; 0.03334029733191658 0.04633912472517847 -0.09551455535227171; 0.029586312777202476 0.05232732210388198 -0.1161455475030084; 0.012221586250973073 0.02574432054587918 -0.06432130485812554; 0.007060126862041252 0.017210035821970098 -0.046216448742666554; 0.008022108565453517 0.023808927343200663 -0.06629890415520677; 0.0010348369900206465 0.006286687204021532 -0.01995882309805672; -0.0010379888344537402 -0.002569531462712828 -0.012502910031788503; 0.004942334959437646 0.007899580045844064 -0.004799973882780043; -0.00021429646469857725 0.0010999877802647623 -0.005260486548113642; 0.001369430786928129 0.000572985147649354 0.001459341956486887; -0.002027992247737102 -0.007702972583930658 -3.750401800117482e-5; 0.0007293126388755138 0.0006339526833138416 -0.0030364429123448996; 0.0014517955435120406 0.0025745247509864466 -0.0004624808601787888; -0.016226345729703696 -0.002686747582362939 -0.005506771796140635; -0.012513575267414461 0.016373810521194826 0.006802911990443609; 0.0015319474903502579 0.0053861199373069785 -0.01409963704242946; -0.006767269638516525 -0.015443682935665217 0.005958066104514315] %
+
+Mass Used: 108.88807624340916 kg
+Launch C3: 93.88389940215272 km²/s²
+||V∞_in||: 0.0009938065392707414 km/s
diff --git a/archive/ES_0.5627545153438122 b/archive/ES_0.5627545153438122
new file mode 100644
index 0000000..db4d151
--- /dev/null
+++ b/archive/ES_0.5627545153438122
@@ -0,0 +1,22 @@
+archive/ES_0.5627545153438122---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T08:52:02.982
+Launch V∞: [6.52553314673395, -7.358183088057568, 0.15742067387236353] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.2428349156973596e-9, 3.3612990180033606e-11, -6.104847425445475e-9] km/s
+ V∞_out: [-2.304893131732801e-9, 5.36651845647366e-9, 7.459800008534406e-9] km/s
+ time of flight: 1.8749577787494013e8 seconds
+ arrival date: 2029-04-09T11:01:39.982
+ thrust profile: [0.31610054479435534 -0.07894716102575972 -0.11084047403793075; 0.0612551170908591 0.017484070253542646 -0.07021638343573516; 0.04733762730610832 0.025944052150535506 -0.09191353686959552; 0.06454369761340613 0.04671518102248233 -0.1709545334177791; 0.03027541097932705 0.028171117307277706 -0.10867655443943336; 0.026698564872737276 0.026828738881116792 -0.114913976598672; 0.019232371936861125 0.022115490963021688 -0.0969004122373056; 0.013924764745287836 0.016253684431884085 -0.07749472021144366; 0.002663079791993134 0.0033616207590021303 -0.017798730012138053; 0.0027306732815399193 0.0039264743126174355 -0.021170108173832698; 0.0014445543320861375 0.0022847666999706038 -0.01325613911116083; -0.0005564156133205096 0.00037597070479149155 0.00017872187270631668; -0.0019534972970880814 -1.0210596062862126e-5 9.334280848268461e-5; 0.0007661487949511589 -0.002716500515354448 0.002234277201821396; 0.00013661793778307343 0.0005103112654867783 -0.0030460637878588393; -0.001183058330775749 -0.0011135591106181688 -0.0005791049003639444; -0.0020492554425093424 -6.876849044664886e-5 0.003933723451920811; -0.0040634675393136956 -0.00022782897305243877 0.0010843873435697176; 0.00444774069067714 0.001504334638853627 0.0011881472276620017; -0.0009115324033379368 -0.0010057567260374069 -0.003118341998249572] %
+
+Mass Used: 92.17063679658395 kg
+Launch C3: 96.75022247506232 km²/s²
+||V∞_in||: 9.472536594657308e-9 km/s
diff --git a/archive/ES_0.5627575712474722 b/archive/ES_0.5627575712474722
new file mode 100644
index 0000000..7796e76
--- /dev/null
+++ b/archive/ES_0.5627575712474722
@@ -0,0 +1,22 @@
+archive/ES_0.5627575712474722---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:15:28.654
+Launch V∞: [6.492163992163593, -7.441427770106685, 0.08564000964938974] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6683219127641417e-7, -3.6103772805125744e-8, 4.5435178186867664e-8] km/s
+ V∞_out: [-1.7505356588602983e-7, 1.5977142267395454e-8, -2.271360447736543e-8] km/s
+ time of flight: 1.8484356677393162e8 seconds
+ arrival date: 2029-03-09T11:41:34.654
+ thrust profile: [0.2638222684219522 -0.06976937150418668 -0.08775020001538998; 0.04035581805970454 0.01003849321712909 -0.04432132343821869; 0.05549668176943989 0.02843836734888081 -0.10529219105197937; 0.03988146615399876 0.03171575773488213 -0.10902904218596492; 0.029490774488592993 0.024499523575764823 -0.10692140211203652; 0.025856195357900454 0.022712216745167435 -0.09728802104268001; 0.0178264511455486 0.016310127151831586 -0.08149306066254663; 0.03980182577988357 0.045398840945445426 -0.19128621647589003; 0.005996326790335671 0.006999050438268357 -0.036040434186436564; 0.0031401286281076196 0.004264920567147925 -0.02244605840094812; 0.003565535467317762 0.004687322364205727 -0.024877616643883386; 0.000434569977224652 -0.00022615185339896278 -0.00019434968730958025; 0.0010346036189105286 -5.570096726417544e-5 -0.0022874546709562215; 0.000107127311420571 -0.00043585517282329286 -6.73426662147011e-5; 7.948074960851788e-5 -0.00025802635748752007 -0.002003144619873626; 0.00013606522907974708 0.0011482864025600431 0.00019605924666857213; 4.848456475847578e-7 5.5766549234884306e-5 -0.0006356186379134939; 0.0002702724101943796 0.000367164624218318 0.00013493888602420054; 0.00018736697168702328 0.0010397331876681 -0.0021838826435722; 0.0006720505933891284 0.00044137497013394997 0.001733693688342931] %
+
+Mass Used: 87.62331362972373 kg
+Launch C3: 97.53037477011323 km²/s²
+||V∞_in||: 1.766375324604785e-7 km/s
diff --git a/archive/ES_0.5627578457766789 b/archive/ES_0.5627578457766789
new file mode 100644
index 0000000..57e4742
--- /dev/null
+++ b/archive/ES_0.5627578457766789
@@ -0,0 +1,22 @@
+archive/ES_0.5627578457766789---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T18:56:36.427
+Launch V∞: [6.606198180342671, -7.393533470928419, 0.10685957060502407] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.3091830891605156e-8, 2.603942421780119e-8, 4.950110627950862e-8] km/s
+ V∞_out: [-1.8915626316581746e-8, 4.1048826089659705e-8, -5.4403210610457884e-8] km/s
+ time of flight: 1.8749577787493864e8 seconds
+ arrival date: 2029-04-09T21:06:13.427
+ thrust profile: [0.1551917697287775 -0.03960392679707073 -0.05781740537536582; 0.11349655293543487 0.030397337746159214 -0.12823520753771903; 0.06921912276829771 0.03563644244611294 -0.13219742693490044; 0.03906256726995343 0.02761114535799668 -0.10838105443380039; 0.022620542932744687 0.018709085161687507 -0.07965223116749492; 0.018127818772782224 0.01761045815718169 -0.08070272484351178; 0.014659504364658448 0.015416771181452736 -0.07548988354356796; 0.020767464947498662 0.02588404991788391 -0.11421658350166135; 0.010786170428573275 0.013330892539880857 -0.06738377104177391; 0.0038206293436622678 0.0069934194268030285 -0.03651634547363243; 0.00031153183732888845 0.0006005012934167347 -0.0040540642948680115; 9.145639867480339e-5 -0.0009091470229140738 -0.0010231873112317475; -0.00015354548318585954 0.00022740063204747057 -0.0016475522701778866; 0.0007358611237352564 -0.0007057798249090216 -9.824539235889738e-6; 0.0007857601320361134 3.972831443378722e-5 -0.0014857970915586685; 0.001307755293657938 0.0006644313028728432 0.0020155063931559056; -0.0023218695447751983 -0.0020099896174471093 0.0006301232582476791; -0.0005448953904822024 0.0005720962195911469 -0.0003061180493294747; 0.001617171609152157 0.0010152361873125364 -0.0036630257236264663; -0.0013106804285530499 8.639519112764763e-5 0.0013094966251837778] %
+
+Mass Used: 83.03142518885807 kg
+Launch C3: 98.31761055153153 km²/s²
+||V∞_in||: 7.060677747978953e-8 km/s
diff --git a/archive/ES_0.562762923782554 b/archive/ES_0.562762923782554
new file mode 100644
index 0000000..72b3d6e
--- /dev/null
+++ b/archive/ES_0.562762923782554
@@ -0,0 +1,22 @@
+archive/ES_0.562762923782554---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T06:42:02.619
+Launch V∞: [6.5276410610224795, -7.442101972556684, 0.183841343795956] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2065896028107728e-9, -1.622213429005528e-9, 2.0240188443857513e-9] km/s
+ V∞_out: [9.173789658104903e-10, -2.063316311482681e-9, -2.7018442480566305e-9] km/s
+ time of flight: 1.8749577787463197e8 seconds
+ arrival date: 2029-04-11T08:51:39.619
+ thrust profile: [0.23986318740418747 -0.07128473390968905 -0.09639490899558019; 0.04540199611511123 0.007901201012371122 -0.05661238191584195; 0.049879454003946805 0.018176533126832657 -0.10475123146178492; 0.057219794832211665 0.027308932202507012 -0.16719344320570917; 0.042218362969601415 0.02337132422794198 -0.15705554799389712; 0.031768261371843694 0.01935257500910644 -0.14244469209510935; 0.015582253717953009 0.010017326867562376 -0.08170672143079301; 0.006265760145683163 0.003805799794672329 -0.037213740376617885; 0.002193486139148122 0.0003297876336002697 -0.013904106117270946; 0.0009631055623378982 0.0013213343218964186 -0.003061961034488562; -0.00016309131703443985 -0.0014669593173972288 -0.003431011731230143; -0.0011149573393650384 -0.0004977198947884558 -0.0003436180961493944; 0.0005815437318473851 0.00015921930232145253 0.0010608221938952236; 0.002451195634367141 0.000428729910505925 -0.007524999600112537; 0.001021139289834135 0.0028845084549661165 -0.001244856635302043; -0.002475978309580859 0.002462981515295012 -0.0016995901152361962; 0.001399543797673158 0.0010998971900415544 -0.010644356251478134; -0.0037301827818024286 0.00037957825329604244 -0.0052170469785736235; 0.0021763565908981637 -2.3625995504804044e-5 -0.00133971165051989; 0.0019461791156250709 -0.0020440368573704376 -0.004712513087859539] %
+
+Mass Used: 84.7222105645028 kg
+Launch C3: 98.02877723116747 km²/s²
+||V∞_in||: 3.4054759383832253e-9 km/s
diff --git a/archive/ES_0.5627638749857773 b/archive/ES_0.5627638749857773
new file mode 100644
index 0000000..fdc7bc5
--- /dev/null
+++ b/archive/ES_0.5627638749857773
@@ -0,0 +1,22 @@
+archive/ES_0.5627638749857773---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T17:36:50.192
+Launch V∞: [7.567262318806996, -6.3232717011969894, -0.08669258565972077] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009752439593499618, 0.0008020441651768877, -0.0006114897124908876] km/s
+ V∞_out: [0.0001760333931204086, 0.0013905467913231868, -6.172247975778327e-5] km/s
+ time of flight: 1.6630343398279056e8 seconds
+ arrival date: 2029-08-17T13:00:43.192
+ thrust profile: [0.28836285365157643 -0.05029485604753917 -0.11040142757801588; 0.06435794523428673 0.019792176669709154 -0.07801449049163259; 0.06782086773996383 0.03609371831525963 -0.13555741958409037; 0.05245668213452627 0.0373116595895244 -0.15311554150626513; 0.039065769489860055 0.03166205085325677 -0.1456453180063326; 0.02885044310485999 0.026578411884475465 -0.1334087428872082; 0.01923638933814066 0.019213523333072583 -0.10235409335663846; 0.009354515044285732 0.00987935570222284 -0.0595003742447185; 0.01371275031403105 0.01787847442802338 -0.09518666632799963; 0.004775597234782967 0.0053192862744128565 -0.03526547383435086; 0.00044310960284414647 0.0005544981921018311 -0.003670783535203374; 0.0007431337294520026 0.0009620103123696304 -0.0049721175936492225; 0.00036791355320568605 -6.315007928364426e-5 -0.0008765869878917267; 0.0005061386500825457 0.0003032880436039458 -0.0009135718057484241; 6.936757851340777e-5 0.00018697854502479412 -0.0010123424113075666; 0.00021157044672512554 -0.0002823111418381128 -0.00043451991502080394; -0.00012250854937972315 -0.0006334805520606438 -3.720886624007896e-5; 0.00014220633769177477 -0.0008494765490832297 -0.0005811524616514718; 0.0013283634991130334 0.00035967923317147357 -0.00037731639510934324; 4.282528798260372e-5 0.00020055366355414112 -0.00023257121088486078] %
+
+Mass Used: 89.23853973972109 kg
+Launch C3: 97.25473961320327 km²/s²
+||V∞_in||: 0.0014029594761164946 km/s
diff --git a/archive/ES_0.5627693150336442 b/archive/ES_0.5627693150336442
new file mode 100644
index 0000000..f3b4ed1
--- /dev/null
+++ b/archive/ES_0.5627693150336442
@@ -0,0 +1,22 @@
+archive/ES_0.5627693150336442---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:43:20.147
+Launch V∞: [7.488712719650007, -6.103273596928697, 0.1122476596068265] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00017992566563987915, -0.0001174534279919255, -0.007598090080734925] km/s
+ V∞_out: [0.007079262195335519, 0.002533845638429409, -0.0011880288817578354] km/s
+ time of flight: 1.7739174603328162e8 seconds
+ arrival date: 2029-12-23T07:12:26.147
+ thrust profile: [0.42476942765827985 -0.006074169724481333 -0.10385408624044552; 0.2019530357502391 0.12136050628964598 -0.16211099823008718; 0.11082666300208477 0.11178016423075474 -0.16185879758563726; 0.06882462703596536 0.10028199667168324 -0.15716114302456968; 0.03401156708827074 0.061717266508157766 -0.1106685116594159; 0.013561810061616447 0.030640322538905616 -0.059797777967090175; 0.010736256269457083 0.028729280327360794 -0.059386000286590974; 0.008861007740171267 0.025822069777519188 -0.05632454114410094; 0.004752692517882941 0.016385125401414246 -0.039552980925996954; 0.0007494344433955169 0.0032202405825486075 -0.008647529998660116; 0.0014882271106182415 0.009764410813256571 -0.024356628183124115; 0.0008102365382981244 -0.001208209130055621 0.0012646880235311232; -0.001012953451608708 0.00016876235667677918 -0.001362234952455194; -4.736001482632244e-6 -0.0005722799510117538 0.0014443651457780125; 0.0032008375473719704 -0.0014697274424409232 0.002361136198166152; -0.0007528025807774508 -0.0012736832796874137 0.0034065109101559074; -0.00038311243096618756 -0.000855468252609978 0.00015604520890788324; 7.854959760626882e-5 0.0029702815108539056 0.0019424317566028465; 0.004669912449731402 0.004258826673519079 0.0034692536602804382; -0.0058164747308217316 8.277253996382933e-5 -0.0014636274780542092] %
+
+Mass Used: 112.06123059382344 kg
+Launch C3: 93.34336633350198 km²/s²
+||V∞_in||: 0.007601127641861138 km/s
diff --git a/archive/ES_0.5627702101062592 b/archive/ES_0.5627702101062592
new file mode 100644
index 0000000..660b26e
--- /dev/null
+++ b/archive/ES_0.5627702101062592
@@ -0,0 +1,22 @@
+archive/ES_0.5627702101062592---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:28:43.699
+Launch V∞: [6.502502999671004, -7.462834525011796, -0.3299053772780357] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.0424536196728205e-9, -1.463400478782038e-11, -3.950388554085201e-9] km/s
+ V∞_out: [-1.4244521234408578e-9, 2.931220241074077e-9, 3.9536103630551675e-9] km/s
+ time of flight: 1.8749577788084355e8 seconds
+ arrival date: 2029-04-10T13:38:20.699
+ thrust profile: [0.20510069392095032 -0.04969975403518591 -0.07598744516117374; 0.031920082721069824 0.009001281429885726 -0.03612333853441942; 0.08377263916118655 0.04536879960993438 -0.152860826206249; 0.06795356006502103 0.048464158963100225 -0.17089405442977104; 0.04929724196098824 0.04241493746347276 -0.16035478577490686; 0.022845178046219 0.02639940359496779 -0.1004160095694994; 0.013048630889034778 0.014713452142207243 -0.06402188668453616; 0.009987582618318927 0.012790717393565012 -0.05867430897722975; 0.0016729962362552113 0.0023521034228634378 -0.012346615877790203; 0.0061969180071090625 0.007850674309595452 -0.040786549671088496; 0.0004944778673782081 0.0007711073427599347 -0.0036980897720898165; 0.00010133381883683297 0.0004777033305809899 -0.003625878825236398; 0.00039275638688744116 -0.0003318942449539481 -0.0004833468029352525; 7.689953995284957e-5 -0.0004229089599302708 0.00047820229305566963; -0.00033703713095597685 0.0004205238941442864 0.00012491109125024468; -0.0005680339176461708 0.0013227703999044499 0.0012949117751136169; -0.002743547630885194 -0.0023155530920906373 0.0004417624417757801; -0.0005245828884378592 -0.004125494877376844 0.0027979593814416457; 0.0012735599054890905 7.2885979867506e-6 0.0017959065690811345; 0.0002903052724798205 -0.001121461333725308 -0.0025785027095803926] %
+
+Mass Used: 84.40110031999575 kg
+Launch C3: 98.08528196639541 km²/s²
+||V∞_in||: 5.65218675819805e-9 km/s
diff --git a/archive/ES_0.5627747004939948 b/archive/ES_0.5627747004939948
new file mode 100644
index 0000000..39a7f0b
--- /dev/null
+++ b/archive/ES_0.5627747004939948
@@ -0,0 +1,22 @@
+archive/ES_0.5627747004939948---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T04:56:22.720
+Launch V∞: [6.579325912884272, -7.288940540746787, 0.28280262627313846] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.118001444243e-6, 9.308577244921591e-7, -1.661805192812781e-8] km/s
+ V∞_out: [-1.2434730156452512e-6, 2.7864044008551626e-8, 6.212032552710396e-6] km/s
+ time of flight: 1.8749577787130356e8 seconds
+ arrival date: 2029-04-08T07:05:59.720
+ thrust profile: [0.317700282390669 -0.08051401225095578 -0.10817683737931691; 0.08881720847703693 0.025205643469142863 -0.09316766163890901; 0.05935144462627597 0.03177075696068279 -0.10670930761205055; 0.06268260799871117 0.04482224295452064 -0.1535606423018505; 0.04003834058279472 0.03537080067168356 -0.1309124409083164; 0.024499295812000825 0.02469224094073081 -0.09748794145639787; 0.019198386358351353 0.021699714292578904 -0.08991524831408064; 0.010240598564249321 0.012796340393261321 -0.05814683872399065; 0.006250835428364749 0.00813732660559109 -0.03687364446260108; 0.0010995083061135372 0.002129155361930943 -0.008618438295654831; 0.0005703140296025144 0.00035754067960573643 -0.0034087866389794054; 0.00039948271648964533 0.0010341638119442935 -0.001462574416352999; -0.0016825898942412153 0.0018275713016292594 -0.0020273510973845663; 0.000744340780750371 0.0010675954897012333 -0.003199299716420403; 0.0005878275719582412 -0.0004108080645600057 0.0012473857539004754; 0.0007043144649086446 -0.0017156010825228381 -0.0023859292576268237; -0.0005082207408235702 -0.0024652273597895345 0.0012013324845937395; -0.0017621954934845347 0.0012865496209941258 0.0007472378334709708; -0.0009290050960633219 -0.003871137423827317 0.0033514521719544086; 0.0014224063796630748 -0.0011795068379470627 0.006447928794414927] %
+
+Mass Used: 93.67621141013024 kg
+Launch C3: 96.4961609999195 km²/s²
+||V∞_in||: 6.188433883839759e-6 km/s
diff --git a/archive/ES_0.562785204931695 b/archive/ES_0.562785204931695
new file mode 100644
index 0000000..be70ffc
--- /dev/null
+++ b/archive/ES_0.562785204931695
@@ -0,0 +1,22 @@
+archive/ES_0.562785204931695---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T13:11:29.973
+Launch V∞: [7.700257130845432, -5.765466517402971, 0.24515005887731398] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.3506441323852954e-6, 5.28622813315513e-5, -0.0010468244016528898] km/s
+ V∞_out: [-4.258437991624517e-5, 0.0010519608454584292, -1.1063114021196065e-5] km/s
+ time of flight: 1.8085731622307774e8 seconds
+ arrival date: 2030-01-31T19:20:05.973
+ thrust profile: [0.5985945614110588 -0.0219916651527684 -0.15768216964728418; 0.15567094186084499 0.08826788384028857 -0.14153211922128126; 0.09096203806165545 0.08651568637179288 -0.14984793991734283; 0.03881931963047066 0.04980778104247145 -0.09806733112898315; 0.02235367413573818 0.035442140485358 -0.07718108643831141; 0.009656928027171996 0.01771749171896824 -0.04456076342827341; 0.02231228903458449 0.04772308562216408 -0.11479779226644277; 0.005390385003128406 0.01616109549530917 -0.042919038097869566; 0.006406372520851885 0.018356831765550728 -0.05134209670476985; 0.0010489584911895122 0.005674143652910116 -0.013558882611637204; 0.0015420524663505254 0.007005512086917069 -0.022603562824885896; -0.0025519435832355433 0.0027714225840514595 -0.002513233836849313; 0.0007035815349638254 -0.002261469394440163 -0.008307912500607648; -0.0012165441955869002 0.0008075341729703974 -0.0016461771420360777; -0.003965775313202741 0.005233983190281812 -0.0005401880127780933; 3.2952676404473386e-5 0.0015251196050623207 -0.0017726121081498274; -0.008036815927106243 -0.0014312059625763327 -0.00206355803688457; 0.002109237249759842 -0.005084199385815685 0.005089999473340146; -0.007489900493288555 0.010443699079013578 0.0012258982724130943; -0.0004283103829288497 0.0007603470760106927 0.0013253425290674983] %
+
+Mass Used: 116.44720727815456 kg
+Launch C3: 92.59466259579823 km²/s²
+||V∞_in||: 0.001048171922003322 km/s
diff --git a/archive/ES_0.5627855638840675 b/archive/ES_0.5627855638840675
new file mode 100644
index 0000000..b21a8f6
--- /dev/null
+++ b/archive/ES_0.5627855638840675
@@ -0,0 +1,22 @@
+archive/ES_0.5627855638840675---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T10:31:29.593
+Launch V∞: [7.432991904620454, -5.967834624648714, -0.3968870326749141] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009647595675662221, 0.002615745047780851, 0.0064856265601308544] km/s
+ V∞_out: [0.006404527981791798, 0.0008176138686036172, -0.002860341343941618] km/s
+ time of flight: 1.7943680441027987e8 seconds
+ arrival date: 2030-01-16T06:04:53.593
+ thrust profile: [0.682477804216561 -0.02514259309384213 -0.18689015840957246; 0.24535583763941796 0.14019616122273126 -0.22708372842627045; 0.03924381493981594 0.03963204930969242 -0.0750467683825446; 0.039840514384338575 0.053338839496318395 -0.10777513541841104; 0.036868075127535545 0.06264735366989434 -0.13552276558422405; 0.013232361891896409 0.028730452082972147 -0.06932414490146117; 0.010608099601928045 0.027952952060652896 -0.07455561452349252; 0.003829811435171639 0.011027114820907654 -0.028816132609547095; 0.0018230749207362304 0.010593788830255696 -0.028074241654297494; 0.005918809333771532 0.015297232719973998 -0.04615190712786552; -0.0006881117987563099 0.0017598476262833554 -0.004657532200649813; -0.00017832121809153924 0.003338208389532185 -0.010927342841182006; -0.000733291880706797 0.0002251462916513507 -0.00017192603215281837; -0.0008480036339523794 -0.0018440883958888107 0.00042717362658321835; 0.00018551328626121427 -0.00018573249661748312 -0.004380466776748726; -0.000950197819359632 0.00022776051909195044 -0.0009787526976950873; -0.005988332771229156 -0.003280927781187215 -0.0046914211482639735; -0.0001050169418464772 -0.00033421072322370763 0.0002735971958564539; -0.003641552522993501 0.007055299984576872 0.002509628713518115; -0.0021134379878571894 0.0022366845836228957 0.0037301081885102176] %
+
+Mass Used: 125.62185240965937 kg
+Launch C3: 91.02193807801476 km²/s²
+||V∞_in||: 0.0070594783841070995 km/s
diff --git a/archive/ES_0.5627887344097992 b/archive/ES_0.5627887344097992
new file mode 100644
index 0000000..20ab418
--- /dev/null
+++ b/archive/ES_0.5627887344097992
@@ -0,0 +1,22 @@
+archive/ES_0.5627887344097992---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T03:51:51.958
+Launch V∞: [6.637211583632461, -7.450474699853282, -0.1038425488381805] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3172623327504985e-9, -1.7397408868032948e-9, 9.674926998951823e-10] km/s
+ V∞_out: [8.897822813962512e-10, -2.030725928226414e-9, -2.897731623986195e-9] km/s
+ time of flight: 1.8749577787479493e8 seconds
+ arrival date: 2029-04-11T06:01:28.958
+ thrust profile: [0.12218449449185799 -0.03221739004242287 -0.048758180701071185; 0.029850565820051647 0.0072689858022853705 -0.03694123742637232; 0.03336370606456407 0.01559948371727533 -0.06835325408588654; 0.04895321106630232 0.030011586108699848 -0.13708678716197875; 0.03638191045500705 0.02649470537668246 -0.13054847220210894; 0.029317756924571517 0.023997412165726158 -0.1276684950925273; 0.02390718754015377 0.021081899609646043 -0.12213267470648573; 0.013790927238057677 0.013585335112376858 -0.0810153407535919; 0.008129869592163146 0.0088874173009808 -0.05565999297621715; 0.0054569445926873645 0.006178045884633824 -0.04119083894075797; 0.0008426652704705872 8.46737168791505e-5 -0.003969815411640692; 0.0031807702753222054 0.0009798147321804541 -2.1025969905371332e-5; 0.00010464862326296269 -3.2124808757400405e-5 0.0012304764609479613; -0.0008863987887498101 0.0011520902647649733 0.0004674038906861272; -5.5276838717691046e-5 0.0004261053511190278 -0.000575293063589012; 0.0008180082906299795 -0.0005916798244168712 0.002049952025316561; 0.000733586417491306 0.0013443146390838697 -0.0017120106460202138; 0.0019076227774866565 -0.0013430083540720624 0.0018093342662124162; 0.0004796201139540834 -0.0015894090060544796 -0.0011752857970201785; 0.0032348484116410405 0.0003874250389306187 -0.0032613487814325912] %
+
+Mass Used: 75.74474102971908 kg
+Launch C3: 99.57293413400798 km²/s²
+||V∞_in||: 2.3870317406454545e-9 km/s
diff --git a/archive/ES_0.562788762880786 b/archive/ES_0.562788762880786
new file mode 100644
index 0000000..14a091e
--- /dev/null
+++ b/archive/ES_0.562788762880786
@@ -0,0 +1,22 @@
+archive/ES_0.562788762880786---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T23:54:02.390
+Launch V∞: [6.571512106920172, -7.3542520901986235, 0.16012329210719514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012570181046008479, 0.001405977466814706, 0.0011454180866811092] km/s
+ V∞_out: [-0.0014897918462397216, -0.0007102445967869923, 0.0014643380564689685] km/s
+ time of flight: 1.8749577787487665e8 seconds
+ arrival date: 2029-04-09T02:03:39.390
+ thrust profile: [0.258091326305198 -0.05944716475027714 -0.09608609628050165; 0.06230967022856088 0.019867496766861267 -0.07036362732614196; 0.06459750291414747 0.04083337863103845 -0.12930156182950728; 0.055823625080034245 0.04525092510019279 -0.15447147986610762; 0.03879128566155045 0.0327502882092532 -0.12367098620312594; 0.03484389499510035 0.03748499881691339 -0.13191433576366257; 0.01567202023270364 0.01758298107113955 -0.07532603390821846; 0.014143025312392246 0.018095420727963125 -0.07464782407499423; 0.0031480103823024468 0.004408577732846136 -0.019903920124454823; 0.001174121832689711 0.0005682644924551662 -0.002441273137971143; -0.0010197874777116258 0.00010852593437634902 -0.0021602561700128633; 0.0013934027766803851 0.001243621095594616 0.00028070076383701734; -0.002183861739679473 0.0010193578267684 -0.002975799078674123; 0.0020054992159174393 -0.0012258039068649708 -0.0008650309463334731; 0.0009485165716772066 -8.981639094948277e-5 0.0008563863828144579; -0.001719073214845745 0.0007096996895102924 -0.003746953724322155; -0.0024096392709151396 0.004297569690222004 0.001981330849913509; -0.00038326041994303495 -0.0011093683130252946 -0.00039822240896935507; -0.0010812360967460714 -0.004285983510020233 0.006389113290993514; -0.001572329488051278 -0.0030601501912162904 0.007359804545719753] %
+
+Mass Used: 89.03018792437433 kg
+Launch C3: 97.29543464626447 km²/s²
+||V∞_in||: 0.002206547018710732 km/s
diff --git a/archive/ES_0.5627903742154157 b/archive/ES_0.5627903742154157
new file mode 100644
index 0000000..c849d43
--- /dev/null
+++ b/archive/ES_0.5627903742154157
@@ -0,0 +1,22 @@
+archive/ES_0.5627903742154157---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T18:43:52.651
+Launch V∞: [7.6920345043107465, -6.083461438466874, 0.19966929679968282] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.054369966751638e-8, -3.3004822630086075e-7, 6.466217686717664e-8] km/s
+ V∞_out: [-5.144748406930409e-8, 1.9079828512411223e-7, 2.6960377872430674e-7] km/s
+ time of flight: 1.7492054359775984e8 seconds
+ arrival date: 2029-11-26T07:46:15.651
+ thrust profile: [0.3315836959607369 -0.03626757107814669 -0.1079995203972283; 0.09417471604052077 0.038676451189051546 -0.10103546939253927; 0.06738917889452328 0.04651243938407052 -0.12630477400597143; 0.06264396461301591 0.05813355888793751 -0.17403870060757687; 0.030404112509949698 0.03331340654980326 -0.11768073962812858; 0.014646547320175288 0.01786341069471157 -0.06950667763127119; 0.02705227597853192 0.03827172136377061 -0.14677985010396233; 0.002904786386719714 0.005343112557468725 -0.021464067663856775; 0.0029852045857663477 0.005147436930259342 -0.027607392388322737; 0.0023623563093964203 0.0045229968765188614 -0.02069480969814393; 0.0018120967572684977 0.0024932384247600223 -0.018441928788684097; -0.0003863455448474412 0.0019792037139382485 -0.0068494212715169735; 0.000579071843360225 0.003133075672126785 -0.007778660896464607; -0.003927205397034535 0.0017623432499881755 -0.004104019517303315; 0.0006450773810053249 0.004823887590368015 -0.0024889323931398867; 0.0009851630867950757 0.0001236248000955718 -0.0018337744972239363; 0.015537151613799052 -0.005839535275098647 -0.01020375029476948; -0.010931264046160892 -0.002068739702119609 -0.00022067468366455262; 0.006548274532138629 0.0062175654326094626 -0.006700457431168476; -7.905550681044918e-5 -0.002136717605714493 0.015246800508036389] %
+
+Mass Used: 95.33013656937237 kg
+Launch C3: 96.215765716905 km²/s²
+||V∞_in||: 3.387577606259021e-7 km/s
diff --git a/archive/ES_0.5627938446411662 b/archive/ES_0.5627938446411662
new file mode 100644
index 0000000..1331663
--- /dev/null
+++ b/archive/ES_0.5627938446411662
@@ -0,0 +1,22 @@
+archive/ES_0.5627938446411662---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T13:13:56.073
+Launch V∞: [6.614677741421812, -7.264180165260562, 0.22291601118788262] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.924142974101028e-7, 3.7551224591642906e-6, -2.080413167619172e-7] km/s
+ V∞_out: [1.361176100911847e-6, -3.0650125288721072e-6, 1.7692335660788955e-6] km/s
+ time of flight: 1.8749577787483278e8 seconds
+ arrival date: 2029-04-07T15:23:33.073
+ thrust profile: [0.30060968587988407 -0.07220271006852065 -0.10259261164952514; 0.08349735181245407 0.02484515515757224 -0.08772631209933018; 0.09606457577055956 0.05561423115839907 -0.17172278100798852; 0.06178937978476299 0.04782605520039311 -0.15331501360511998; 0.039000015405890646 0.03645920951947065 -0.12422598908948192; 0.019143799139921272 0.020106113294523716 -0.07479439177826852; 0.014830941829184919 0.01800763908222033 -0.06941410570953913; 0.01146941737955087 0.015454002600880527 -0.06293769126083368; 0.00526981888183439 0.007485255362660944 -0.032506194413620196; 0.0012512852706758775 0.0015085154734220422 -0.007162889632954001; 0.000577004103181999 0.0005377382606413002 -0.0027993566715789776; 0.0008005139771389519 0.0007100501220023266 -0.0021333186953669623; 0.0017144770058355999 -0.000804338259319129 -7.749302665901287e-5; 0.0008712823265179825 -0.0003833015848041894 0.0014326172182327868; 0.0006186582110379232 0.0020625587853473942 -0.0032376482017224028; 9.223232386276565e-5 0.0016361987896841047 -0.002187568136843486; -1.7495115415774588e-5 0.001204214096248517 0.0012750104288334696; -0.0005197395935930612 0.0018927308971925885 -0.004702846893301037; -0.0005867746650717698 -0.0018395922113123623 -0.0018322885942823556; -0.00030496843124357093 8.09817673417413e-5 -0.0028792174662690966] %
+
+Mass Used: 93.25634665645202 kg
+Launch C3: 96.57196664427005 km²/s²
+||V∞_in||: 3.7929800570387906e-6 km/s
diff --git a/archive/ES_0.5628007891454023 b/archive/ES_0.5628007891454023
new file mode 100644
index 0000000..bbe4d85
--- /dev/null
+++ b/archive/ES_0.5628007891454023
@@ -0,0 +1,22 @@
+archive/ES_0.5628007891454023---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:10:57.207
+Launch V∞: [7.743243644444229, -5.499121042273045, 0.2660228882308396] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.172310953688274e-10, 1.290799913999047e-9, -1.6505528357832106e-9] km/s
+ V∞_out: [1.0766881685484106e-9, 2.2047623546135412e-9, 6.106459081457821e-11] km/s
+ time of flight: 1.874957778739499e8 seconds
+ arrival date: 2030-04-19T05:20:34.207
+ thrust profile: [0.8802032022121634 0.012150433524692137 -0.21092082212892932; 0.07851977572683698 0.0526854334365846 -0.07651349417195745; 0.0573082782745446 0.0640644871442533 -0.10216824988815407; 0.03254259955454274 0.05053320326763583 -0.09017519807706074; 0.026907234798051956 0.053538694456761265 -0.10372662741071963; 0.013112200370473625 0.03282324054196896 -0.06977061413074348; 0.005279185708603677 0.016433523425526765 -0.03828221743078651; 0.0023793893020969304 0.009694731257163382 -0.024265643936249876; 0.00567417585194894 0.025459216399734908 -0.062060552638963415; 0.0037105390516871746 0.020384359925530733 -0.05275035247936931; 0.0017817937676117101 0.011997946287791272 -0.032814202600484496; -0.000185135160681886 0.0023126105486683634 -0.00997638248595946; 0.00077018363323418 0.00031228586719202753 -0.0017150030499542258; 0.0013935488631194439 0.003889582342527941 -0.002510444500646106; -0.0012525212679856154 -0.001177384036980212 0.001137699884457924; 0.0029609110686602902 -0.0031545561382118103 0.0015738395841814131; -0.002133871719025196 0.004678869060451533 0.0064795675795594745; 0.0006616331649346011 -0.001659917105631735 0.006910926589669516; 0.0005720425802284861 -0.001704887805054019 0.006111962265635977; -0.0003772824766783353 0.0017881474659341612 0.0014147404674358498] %
+
+Mass Used: 130.03220578379296 kg
+Launch C3: 90.26892255185881 km²/s²
+||V∞_in||: 2.249078865875912e-9 km/s
diff --git a/archive/ES_0.5628008163183899 b/archive/ES_0.5628008163183899
new file mode 100644
index 0000000..9a1399b
--- /dev/null
+++ b/archive/ES_0.5628008163183899
@@ -0,0 +1,22 @@
+archive/ES_0.5628008163183899---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T07:33:07.047
+Launch V∞: [6.692003528103475, -7.3877721411397825, 0.3139434552331897] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.217983949334189e-6, 4.4257326387775944e-7, -1.0750176725136664e-8] km/s
+ V∞_out: [-4.887980121186915e-7, 1.4287359926196959e-8, 3.2099915675962627e-6] km/s
+ time of flight: 1.8749577787489623e8 seconds
+ arrival date: 2029-04-10T09:42:44.047
+ thrust profile: [0.1018360901932922 -0.02914957656991673 -0.0400226738106886; 0.06558590904804797 0.01382070443443242 -0.07737292208323344; 0.05176258037574136 0.021618611464254374 -0.10268169601272034; 0.053809341535738034 0.02974082482234779 -0.1484064381643266; 0.045499762841835954 0.02957828185535934 -0.15970697655028013; 0.032221225961136975 0.023273171225153474 -0.13646543154811294; 0.01909822129407767 0.014784626268684301 -0.09470429744768871; 0.008034682486635055 0.007018126406480804 -0.04706016410072662; 0.0018134800127140545 0.0012994347404337492 -0.012068391850988172; 0.001611261877877289 0.0014888452450202878 -0.012281479774013082; 0.0004653621859617318 0.0006875018462627904 -0.004937440472388956; -0.0014847721382939207 0.000567454649460048 -0.004503564543607877; -0.0004885223867350134 0.00210955385332891 -0.002122153044405295; 0.0030842386099771413 -0.003445928882188394 -0.0001014263253805883; 0.0013193080549752853 0.0036047372296827314 -0.003729762083374751; -0.0008828328759367102 0.001127527259146885 -0.00017648857529501696; 0.0018982876764556229 -0.003128769810525998 0.0017072186570256396; 0.0009549210444466066 0.0006151901958776737 0.0011647419573086572; -0.003969971845585765 0.00406422008777137 -0.009459158737782143; 0.0044722536090112865 -0.001030922618395969 -0.006274655506219293] %
+
+Mass Used: 76.41383365608863 kg
+Launch C3: 99.4606489226342 km²/s²
+||V∞_in||: 3.248292991460515e-6 km/s
diff --git a/archive/ES_0.5628177193323948 b/archive/ES_0.5628177193323948
new file mode 100644
index 0000000..2df9e9a
--- /dev/null
+++ b/archive/ES_0.5628177193323948
@@ -0,0 +1,22 @@
+archive/ES_0.5628177193323948---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T00:58:57.827
+Launch V∞: [6.595168406706716, -7.379273240777178, 0.13628473997016735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009880201272881878, -0.006243138576674505, 0.006146779313226493] km/s
+ V∞_out: [-0.006075308180441379, -0.00523589640312671, -0.003661987054509423] km/s
+ time of flight: 1.8749577787493482e8 seconds
+ arrival date: 2029-04-10T03:08:34.827
+ thrust profile: [0.23318749833328672 -0.06192092926928255 -0.08595145467461779; 0.03529552625558941 0.008173050933138916 -0.04143573639097233; 0.058958980004904155 0.028958194880609914 -0.1133213049653871; 0.05669192395251301 0.03562393200573571 -0.15311215204866535; 0.03506099283721963 0.026195639188074066 -0.12350349705941169; 0.03307701247860923 0.028688498562112565 -0.13258489062703915; 0.007061559741870036 0.006688505691984239 -0.03616914066357553; 0.011534601658362387 0.015001552178552405 -0.08475261582158505; 0.001899768455484425 0.0019895767399182858 -0.011538925345398774; 0.01379476667920398 0.010739992031101734 -0.07951522395267267; 0.002317877230163524 0.0033086146114476747 -0.019302185069359178; 0.00010011731805905424 0.001010019295855839 -0.001509366412233885; -0.0009558910471270974 -0.0017050667681650592 -0.0017085792810151014; 0.0014730684167406371 0.0007320434869351865 -0.0013748458967095237; 4.008770224735778e-5 0.00017413186186435124 -0.00013751122544422936; -0.0003863622452888072 9.623738333844461e-5 0.0018601314553690841; 0.0028792778134522105 0.0010819542974233312 0.005020987268122659; -0.0017185508762641254 -0.0023927008847497936 0.0004896541480389873; -0.004164047242541433 0.00040782161218877656 0.0034808142846694326; -0.00010012836706076134 9.171885247354761e-6 -0.00010642537481751497] %
+
+Mass Used: 85.13779435733659 kg
+Launch C3: 97.96849340522125 km²/s²
+||V∞_in||: 0.008816794144415366 km/s
diff --git a/archive/ES_0.5628270603919783 b/archive/ES_0.5628270603919783
new file mode 100644
index 0000000..4d7818b
--- /dev/null
+++ b/archive/ES_0.5628270603919783
@@ -0,0 +1,22 @@
+archive/ES_0.5628270603919783---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T22:04:45.530
+Launch V∞: [6.341230629094208, -7.570660574945295, 0.06733165070556912] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5142335626548446e-7, -3.286297730693907e-8, 4.2656042201274816e-8] km/s
+ V∞_out: [-1.597235325732744e-7, 1.4684781158156308e-8, -1.8328049052178635e-8] km/s
+ time of flight: 1.8154580720201203e8 seconds
+ arrival date: 2029-01-30T03:28:12.530
+ thrust profile: [0.24758059080980677 -0.07238467228045635 -0.09172510244249103; 0.04902066637872397 0.010670642211216642 -0.0551784383546797; 0.0516414380055391 0.0235440826472672 -0.09562476798630572; 0.06353499862263917 0.03952254947658419 -0.16037608166532855; 0.04894639670331701 0.036674791296692336 -0.15762170655249705; 0.028604843351493138 0.024400104748208917 -0.11327065572427081; 0.02792773330893934 0.026274885124931525 -0.12838775348511777; 0.01204620844783518 0.010568662207482165 -0.06065511467936114; 0.004159122356712862 0.004294652647452458 -0.025802652909598194; 0.003553271467348944 0.0047962357660759495 -0.029034625795544482; 0.0015957284956038878 0.00200166287375377 -0.01288997808841354; 0.0008666268796970651 0.0017756156294818821 -0.008251373784437029; 8.207583387683073e-5 0.0008328501212267876 -0.0033122837383633033; -1.3436429543339182e-5 0.00021966157481705616 -0.0014809214362260083; 0.0004346680340004816 0.0013224262297629181 0.0008226603134284449; -0.00022166112106256064 -0.0003300366466166644 -0.0012762016177115894; 0.00027635416718181476 -0.00021445938546610659 0.0001894750151317075; -0.000753206675265413 -0.0001519800655639447 -0.0018838033076815199; 4.3102214253538686e-5 0.0005574183015415464 0.00012099076740784188; 0.0014109119237598598 -0.0025525272631536557 -0.00017321113938562136] %
+
+Mass Used: 87.70283138642299 kg
+Launch C3: 97.5306409835803 km²/s²
+||V∞_in||: 1.6071261940637135e-7 km/s
diff --git a/archive/ES_0.5628319273715768 b/archive/ES_0.5628319273715768
new file mode 100644
index 0000000..4dcddeb
--- /dev/null
+++ b/archive/ES_0.5628319273715768
@@ -0,0 +1,22 @@
+archive/ES_0.5628319273715768---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T17:54:27.350
+Launch V∞: [6.634541919352205, -7.427066094572144, 0.24303727556416319] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004103006721938529, -0.00047896853717202824, -0.0004126895102829831] km/s
+ V∞_out: [0.0004919812671617813, 0.00023536962371687668, -0.0005183490094622997] km/s
+ time of flight: 1.8749577787468797e8 seconds
+ arrival date: 2029-04-10T20:04:04.350
+ thrust profile: [0.14339707798039744 -0.038358628985278066 -0.052964980464538035; 0.015245152134568033 0.003679492433149123 -0.01893139259412252; 0.0514088991766393 0.023801378684507168 -0.09844044408446158; 0.06730730782501387 0.03964811902725909 -0.1751300734316027; 0.05021507213940969 0.035216956623146 -0.16727801425756858; 0.02853195888676427 0.02335309998078826 -0.11763318346560983; 0.00879852304443285 0.008953467429736085 -0.04617088687362398; 0.009466239141725548 0.005948582247902678 -0.040715022847076884; 0.006880268486390117 0.008086239180807012 -0.04618992802511236; 0.0020760751749392056 0.0029565434513265784 -0.019755552116586413; 0.008213460945888743 0.010068052943728499 -0.06307034735675003; 0.0008014525142237823 0.0005011246362642782 -0.006735065391553851; 0.0005548682652947813 -0.0002812258275293428 -0.0014056983962987429; -0.001603081305690431 0.0005041743745897464 -0.002268225390373608; 0.0009709967064650286 -0.0011702415273906665 -0.001865271269776896; -0.0013686012238725298 0.00040826972464001114 0.0022926254953390176; 0.0009981116406566968 0.0032691665038371985 -0.002407687816469741; -0.0037423518597992245 -0.00028346897877438624 -0.0019011542243274318; 0.0011180272550774164 0.0023000768078151623 0.002665855244877057; 0.002053497140546259 -0.0005960022867582978 -0.0002919227026034008] %
+
+Mass Used: 77.75168977459907 kg
+Launch C3: 99.23752437009838 km²/s²
+||V∞_in||: 0.0007537042743019629 km/s
diff --git a/archive/ES_0.5628334584347118 b/archive/ES_0.5628334584347118
new file mode 100644
index 0000000..58cde4f
--- /dev/null
+++ b/archive/ES_0.5628334584347118
@@ -0,0 +1,22 @@
+archive/ES_0.5628334584347118---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T08:10:46.116
+Launch V∞: [6.39910811135543, -7.5104898538286715, 0.07760850293658843] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.458105495808217e-8, 5.300074586148709e-8, 3.7176476613523355e-8] km/s
+ V∞_out: [-1.8808772564304116e-8, 4.235655597484565e-8, -6.436006576975574e-8] km/s
+ time of flight: 1.8421538780188403e8 seconds
+ arrival date: 2029-03-02T11:07:13.116
+ thrust profile: [0.2204173441351974 -0.059729232112586586 -0.07958760297726672; 0.1369238795624199 0.0340843234131508 -0.14524714454759616; 0.04850153293182486 0.023656315798985084 -0.09018479746813408; 0.03560065670857361 0.023564454776850607 -0.09320698317688941; 0.04275991782779628 0.03309495515494315 -0.14187248678258904; 0.01809944956173005 0.01651442070775664 -0.07493536108139898; 0.018550343513600357 0.01845115022900538 -0.08875599569935648; 0.025139377599020647 0.0333740632871675 -0.15106706124771713; 0.007990538272009441 0.009190199529049963 -0.046590389170258956; 0.000536591950997902 0.00024007931928798828 -0.002402160550748179; 0.0017310149713240194 0.002254992101007211 -0.01177094726251253; 5.998257845758915e-5 -0.000526134736495274 -0.0006396956707140065; 0.00030590607978938863 -0.00042575994537574107 -0.0005357009116389508; 0.0014117621893745412 3.227141341932002e-5 -0.0007636987728839742; 0.00030628871026619616 -0.00040396055428148364 -0.0005856756262605109; 0.0003723586007433633 -0.0005989405182668993 -0.0010435035752731606; -0.0010233496765515103 6.308357781785624e-5 -0.002339830484688015; 0.001378283630396104 -0.002505410352758753 -0.0007719559130216756; -0.0005650392988792226 -0.0007091399085059681 -0.0027076234325819656; -0.0008470166220479232 0.0001301068709116951 0.0003220510056074215] %
+
+Mass Used: 88.6936524946268 kg
+Launch C3: 97.36206554500633 km²/s²
+||V∞_in||: 7.339631351289852e-8 km/s
diff --git a/archive/ES_0.5628335231675016 b/archive/ES_0.5628335231675016
new file mode 100644
index 0000000..167d013
--- /dev/null
+++ b/archive/ES_0.5628335231675016
@@ -0,0 +1,22 @@
+archive/ES_0.5628335231675016---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:33:45.675
+Launch V∞: [6.361300560704977, -7.557697655739578, -0.011524894758853573] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4043620384612585e-7, 2.0854954062650485e-7, 1.2128252519052115e-7] km/s
+ V∞_out: [-8.799289210790145e-8, 1.366781296650065e-7, -2.2736561102437003e-7] km/s
+ time of flight: 1.823398788748175e8 seconds
+ arrival date: 2029-02-08T05:31:43.675
+ thrust profile: [0.19410995037625306 -0.05595292950623706 -0.07470956220859079; 0.1040730726254978 0.02492773535459552 -0.1173870614266676; 0.08294940091031779 0.04116786759840902 -0.15836608389895906; 0.05233325561281282 0.03379232545727203 -0.1367206569114849; 0.05008924692468771 0.038931115921277834 -0.16127403610911165; 0.023316247767573527 0.020270757104822998 -0.09391007680199308; 0.027999246049346005 0.027910471522260973 -0.13373874414799553; 0.006066304271971342 0.005430981225717572 -0.0321359527858705; 0.001621237255867719 0.0014466875675565986 -0.009245238839686337; 0.0005686799249787111 0.0016523669843269665 -0.0040053329233713285; 0.0011505123494910255 -0.00019329169016882807 -0.004945454848133965; 0.0010039624598532026 0.0010294501776562971 -0.006442807948889599; 0.0007188043341368012 0.000897108180721044 -0.006029527044573866; -0.0013035088489002824 0.00016680455132738083 -0.0014660414742915246; -0.00041168003338331325 0.0011075015190057458 -0.0028615106672957875; -0.0006581359841045422 0.0009207690350207818 -0.000760116712889405; 0.0004515395561295452 -0.0005500661931316321 -0.0002273885574424772; 0.00017789467667357758 0.0004316306348443879 0.004901430306325873; 0.0007415921116137207 0.0013403170087917908 0.0008819536116469349; 0.0036818508805163573 -0.0032535302378074856 0.002237408498318684] %
+
+Mass Used: 87.39285993144085 kg
+Launch C3: 97.58507150239618 km²/s²
+||V∞_in||: 2.7914994028805775e-7 km/s
diff --git a/archive/ES_0.5628402590793374 b/archive/ES_0.5628402590793374
new file mode 100644
index 0000000..e7b7c77
--- /dev/null
+++ b/archive/ES_0.5628402590793374
@@ -0,0 +1,22 @@
+archive/ES_0.5628402590793374---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T15:43:44.956
+Launch V∞: [6.509332143717427, -7.410713157951848, 0.14460362569554855] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007114705384958235, 1.60613740262605e-5, -0.00047679775365558547] km/s
+ V∞_out: [0.0008338876168969619, -5.033568875908347e-6, -0.00013974012256441428] km/s
+ time of flight: 1.8749577787491593e8 seconds
+ arrival date: 2029-04-10T17:53:21.956
+ thrust profile: [0.2914111613857974 -0.07740407655716014 -0.10978631962852939; 0.060851521842519615 0.014534893754664506 -0.072632124620567; 0.04669401353602803 0.019200931235054015 -0.09773086917205973; 0.04006596830850362 0.022055071979074626 -0.11886458894810292; 0.034637780243308054 0.021920600209036478 -0.12812217136588663; 0.025302320341013634 0.01808374755622299 -0.11383785075775932; 0.014727958168325355 0.011514814304257215 -0.07530013248195411; 0.018232566566369367 0.021091080064681755 -0.11386585974418036; 0.005915151612689023 0.00499203856826818 -0.04052763155174503; 0.00128426304441694 0.0010011653554923014 -0.010291456305130935; 0.0012084084746516312 0.0013796242551586384 -0.007946176281001287; 0.0005708093421810677 0.0011642101583967726 -0.008271257586130213; 0.0005723451299240071 -0.0015938719387831382 -0.0011088910882226391; -0.0009281174479337936 -0.0006916412388500829 0.0027665079935493588; 0.00015450638030850065 0.0022787957660002412 0.0016293640440167337; 0.00393536987721774 0.0012267268956053456 -0.00024187348975266462; 0.0020088830190296003 -0.0014906039674391493 -0.0010943785622621284; 0.0012350542095851049 0.0015086261803967703 -0.001464423973613665; 0.0019609593379234617 0.0009670587460224576 0.0029133591280025694; -0.0003424587638894231 0.0004319058144564667 0.001558926438424291] %
+
+Mass Used: 88.99955832033947 kg
+Launch C3: 97.31098467523786 km²/s²
+||V∞_in||: 0.0008566121600667135 km/s
diff --git a/archive/ES_0.5628467398137333 b/archive/ES_0.5628467398137333
new file mode 100644
index 0000000..ae5c6dc
--- /dev/null
+++ b/archive/ES_0.5628467398137333
@@ -0,0 +1,22 @@
+archive/ES_0.5628467398137333---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T07:25:03.170
+Launch V∞: [7.915034179464507, -5.649957815315947, 0.02037083405768369] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.051963466308409e-7, -1.361035193017257e-6, -1.2863598042183103e-7] km/s
+ V∞_out: [1.1359722513043041e-7, -5.562971524322513e-7, -1.5587149369899564e-6] km/s
+ time of flight: 1.8491725512146366e8 seconds
+ arrival date: 2030-03-21T13:19:18.170
+ thrust profile: [0.4483258685933702 -0.006399550204052683 -0.13597789529783552; 0.14445203538238316 0.09270554242410722 -0.13786646860182167; 0.04798911714745375 0.04946461124163864 -0.09008604881780936; 0.023443077778217716 0.03200799377232367 -0.06766194888007565; 0.01542817144950656 0.02635755879444022 -0.06208497913115802; 0.017138478856016333 0.03650151868813493 -0.08825321444693478; 0.021748133727129443 0.056915887600380674 -0.13307562611969914; 0.00919796655572927 0.021417141583664003 -0.06510093540928918; 0.0028724683408854427 0.013583869912204937 -0.041126454270449385; 0.00235937109813509 0.012737902762806955 -0.02748729510135337; -8.56013402233955e-5 0.005313874874869262 -0.009794322765755821; 0.0031364173371497637 0.0028337254406124905 -0.0031754197233172616; 0.0005922853076535632 0.001734345236859924 -0.0054002472649823715; 0.00021894342570157486 -0.003475602775009042 -0.0007665107435470353; 0.002126638000354679 0.0021431877424156953 -0.0022526600755748178; 0.003356872980756328 0.002251648376511442 0.008691604152253155; -0.006859557216464857 0.013148796404710426 -0.004456155842212782; 0.00652580912660989 -0.008140970784867663 -0.017203479161649; -0.000713298692406068 0.0030197380937933343 -0.0071187793862822635; -0.00198107926232157 0.007141944178170788 -0.0006386065027932852] %
+
+Mass Used: 104.99500442039789 kg
+Launch C3: 94.57020434782132 km²/s²
+||V∞_in||: 1.63961716203644e-6 km/s
diff --git a/archive/ES_0.5628488941147338 b/archive/ES_0.5628488941147338
new file mode 100644
index 0000000..0a6a6cd
--- /dev/null
+++ b/archive/ES_0.5628488941147338
@@ -0,0 +1,22 @@
+archive/ES_0.5628488941147338---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T02:22:25.281
+Launch V∞: [6.499425419015937, -7.571743131719401, -0.13793990337791134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.015496878795146728, -0.00021123444038396598, 0.01069593437314738] km/s
+ V∞_out: [-0.01805190564720283, 0.00016761055860239712, 0.005389505944261829] km/s
+ time of flight: 1.8599546592348725e8 seconds
+ arrival date: 2029-03-25T19:46:50.281
+ thrust profile: [0.140541598637974 -0.041276394045096525 -0.06029793541575775; 0.023574606744063656 0.003959055381272015 -0.03040711236820235; 0.04232475211500324 0.015584162841703771 -0.09152523792538621; 0.0554601665458098 0.027262328881337117 -0.16557478115122162; 0.03556560097106086 0.020190089143525942 -0.13573450461845535; 0.026453270627275736 0.016630051496909697 -0.1218056969466265; 0.023472655687039472 0.015953158555693875 -0.12613827377756603; 0.012682016809456497 0.009107460037942668 -0.0789100879472657; 0.004079777210903518 0.0029175861131135066 -0.02893645970783367; 0.0019747473419388373 0.0014015942252916028 -0.014988015857535845; 0.0007639062014347105 0.0007455976437384058 -0.007221780865937953; 0.00037780616417300587 0.0004767190035398143 -0.005827921952666199; 0.0003146173155017376 -0.0005881391872509976 -0.0010791438859073894; -0.00015297647441810412 0.0005354281233474396 -0.00061958475085072; -0.0002526157124511916 0.0006230489573376049 -0.0003129991783769742; -0.0006563188536291602 0.0009884941262130497 0.00027593226313812707; 0.00047595828088922796 -0.00012468579097200884 -0.0014915876473464208; 0.0016298572044952356 -0.000638725039508493 0.0012801014061100846; 0.001964550602553408 -0.001752270406131927 0.0008218568337237576; 0.0002559792013332303 -0.00020435303977357267 0.0006686892968169815] %
+
+Mass Used: 75.6987383594892 kg
+Launch C3: 99.59285224703433 km²/s²
+||V∞_in||: 0.018830849277049304 km/s
diff --git a/archive/ES_0.5628491171948213 b/archive/ES_0.5628491171948213
new file mode 100644
index 0000000..2020691
--- /dev/null
+++ b/archive/ES_0.5628491171948213
@@ -0,0 +1,22 @@
+archive/ES_0.5628491171948213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T03:38:36.640
+Launch V∞: [7.817402303531949, -5.836529702156377, 0.14504614645260028] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2955055929704954e-9, -2.083699076870205e-9, -1.8264848000988507e-9] km/s
+ V∞_out: [-5.52232941966513e-10, 5.19066763861734e-10, -1.9911277724833117e-10] km/s
+ time of flight: 1.7849346611387116e8 seconds
+ arrival date: 2030-01-04T01:09:42.640
+ thrust profile: [0.3878448989973736 -0.008678020876246292 -0.1029926772932243; 0.10246305982305014 0.06041725728657923 -0.09584602977259768; 0.0812647057306246 0.08081148411254435 -0.13462176838139897; 0.06505268329207432 0.09008806133086697 -0.1601142716669194; 0.040740824521358195 0.0736135409418903 -0.14288854878093593; 0.027432970544504578 0.054212128000287865 -0.12225977486641858; 0.011722529966219319 0.029558441130016627 -0.0685467166890532; 0.0033802373487069187 0.01006846735746187 -0.02563475069478701; 0.0006785223556394555 0.0049066179878929994 -0.01199722938360675; 0.002918094614560055 0.010628005135472266 -0.025579250392178246; -0.0011050345274463869 0.0017950663625301074 -0.002545736609660785; 0.0008057699891004179 0.0017138241638701814 -0.006847214082518936; -0.00023526057210838095 -0.0003181394371875373 0.001166846768289133; 0.005512695801537243 0.0008089753236721737 -0.0014318286547209368; 0.0034078644775127186 -0.0005258400930468582 -0.0051162109015761; 0.0001832182724312539 -0.003830732558002039 0.0048262092722705825; 0.001468576584848984 0.0014922002080703489 0.0007740112166929347; -0.00894727246982353 -0.006225963847923924 0.0029812969969502503; 0.0015594134983389454 0.006286701778101992 -0.004846776247004229; 0.001329475954015626 -0.0013156072038949843 0.0009667959805321783] %
+
+Mass Used: 101.33624267050254 kg
+Launch C3: 95.19789612402097 km²/s²
+||V∞_in||: 3.5982210181283624e-9 km/s
diff --git a/archive/ES_0.5628517193423782 b/archive/ES_0.5628517193423782
new file mode 100644
index 0000000..c601514
--- /dev/null
+++ b/archive/ES_0.5628517193423782
@@ -0,0 +1,22 @@
+archive/ES_0.5628517193423782---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T18:12:33.849
+Launch V∞: [7.6099263629201985, -6.290168864581452, -0.11230312636717026] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006972378123023489, 0.00044657717481875255, -0.0002124655561841578] km/s
+ V∞_out: [-0.0003193446247281596, -0.0005837787566031396, 0.0003809966610680223] km/s
+ time of flight: 1.6741509156171966e8 seconds
+ arrival date: 2029-08-30T10:24:04.849
+ thrust profile: [0.26473977383349384 -0.03855701226735257 -0.09801358859146726; 0.06811583956973812 0.024371654735362534 -0.08150759895665416; 0.05327695855860973 0.03128097624570755 -0.10690730332321803; 0.047891663899633626 0.03895087208012104 -0.1381904001237812; 0.0398428050797626 0.03677954281476738 -0.147561184814306; 0.016407075790450438 0.017292455940410192 -0.07371057707343062; 0.01732728941622518 0.02150774102634438 -0.09305735749360032; 0.03786244581387243 0.04630111527804241 -0.23126942136203274; 0.003419303482527858 0.006179434175182051 -0.031020189920034125; 0.004432115096918797 0.005952674367640273 -0.0348171533118242; 2.6298694728817224e-5 6.318729517955542e-6 0.0001245386838051413; -0.00022376811350885344 -0.00031211140136864183 -4.4821693333969674e-5; -0.00010852718474085255 0.0002813819609210741 0.00027634309993125107; 0.00017794449230324694 0.000352895315136916 -0.0013601202721570352; -0.0007982935321492954 0.00012303733247026518 0.0012493654421653424; 0.0003312740213906304 0.0011198084589092053 0.0016326175818889206; 0.0008780358216871334 0.00024875356131640904 -0.002405443176724518; 0.0006918847916338297 -0.002329052586911088 0.0003501470514802184; 0.00024257526806300167 -0.00011929970648022644 -9.53666528372698e-5; 0.0013137453781473028 0.00028729250728569313 -0.0010358456731877097] %
+
+Mass Used: 87.96974831321859 kg
+Launch C3: 97.4898155862096 km²/s²
+||V∞_in||: 0.0008548177305940185 km/s
diff --git a/archive/ES_0.562853987993083 b/archive/ES_0.562853987993083
new file mode 100644
index 0000000..b0656d5
--- /dev/null
+++ b/archive/ES_0.562853987993083
@@ -0,0 +1,22 @@
+archive/ES_0.562853987993083---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:47:14.127
+Launch V∞: [6.600993749251053, -7.333844352370327, 0.26384110042433395] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.794554874609765e-8, 4.954313169614499e-7, -2.8521365326777765e-8] km/s
+ V∞_out: [2.1150932749711195e-7, -4.4409669979568465e-7, 2.9022044089663458e-8] km/s
+ time of flight: 1.874957778760391e8 seconds
+ arrival date: 2029-04-09T04:56:51.127
+ thrust profile: [0.2622740317683954 -0.0655910442497773 -0.09309701625189541; 0.05505233288258174 0.014809818301551439 -0.06393270389392805; 0.061008410674483815 0.03156871330154464 -0.11595311614230534; 0.06309662815497186 0.045268344089168015 -0.16518025535038455; 0.034203740998729304 0.028835170440369557 -0.11873421598987444; 0.023263076858623683 0.02262192950882942 -0.09890666927141531; 0.02359912266381161 0.0254543982373867 -0.11692691244124809; 0.006791913325104324 0.008136046965182893 -0.038818025457535515; 0.007460779015662323 0.009503389154211015 -0.05018893681828061; 0.002843030945626072 0.0035956346316774576 -0.016283211143729288; 0.00047292276024291546 0.00018417317607970094 -0.002835031987610849; 0.0005543151624054718 -0.0009443383437733617 0.0008115586851817885; -0.0009039519517741901 -0.0011318370628331802 0.0011006800162716838; -0.0002467374250143385 -0.00021794153730218455 0.002147872295988837; 0.0006728613586769349 0.0009236808029209947 -0.0018163829005712175; 0.0022797144673944213 -0.002119522697288122 0.0010283554948810744; 0.003137893212038024 0.0010801053620507828 0.0005926006542818483; 0.0030879774390304548 -0.0016501499200968733 0.003008253608686885; -0.0007474267312778924 0.002608460906222909 0.0010170870212831986; -6.46347628984092e-5 0.007934033858528203 -0.0009873434370205499] %
+
+Mass Used: 88.33296505773751 kg
+Launch C3: 97.42800358871874 km²/s²
+||V∞_in||: 5.00881478695977e-7 km/s
diff --git a/archive/ES_0.5628559995596367 b/archive/ES_0.5628559995596367
new file mode 100644
index 0000000..596c2ce
--- /dev/null
+++ b/archive/ES_0.5628559995596367
@@ -0,0 +1,22 @@
+archive/ES_0.5628559995596367---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:03:00.045
+Launch V∞: [6.459774372749673, -7.375714366566673, 0.011904333918488233] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4114543121456023e-7, -6.624595862734421e-8, 7.65455506662136e-8] km/s
+ V∞_out: [-2.460401877373688e-7, 6.458633430381358e-8, -2.93686003830654e-8] km/s
+ time of flight: 1.8600345396396342e8 seconds
+ arrival date: 2029-03-22T19:40:33.045
+ thrust profile: [0.3583528151730406 -0.09874419434852089 -0.13321516384555668; 0.0822205800087926 0.01945875375307835 -0.0951679801370989; 0.05163088493330707 0.02442440992526033 -0.1019015440046043; 0.04659016112218277 0.02959654137680646 -0.1278464769861089; 0.04190539385408142 0.03202347032986302 -0.1469272257530047; 0.021509745087444597 0.018605696255458135 -0.09258089877677071; 0.011435679333485228 0.011186669980114073 -0.058038820270841965; 0.008556664930763274 0.008892417863867658 -0.05059685730076599; 0.005042710469599654 0.0049136301411883 -0.04009988247237647; 0.012231809299063813 0.014641521880397343 -0.08802947874554186; 0.0007934987914917551 0.001542585586668741 -0.006636616741596884; 0.0007302850268101519 0.0005565201748142507 -0.0011547728717714242; -0.00014507325887259522 -0.00036737175786763585 -7.982703749677932e-5; -0.000837238614243464 0.0001584554270667834 -0.00013399822254985645; -0.000423446507273776 0.0016407885979692405 0.0006298829748472382; -0.00046870441906031246 -0.0001954808984520667 -0.00023306612389447723; -0.0027894552920873696 0.0004974849947605095 0.001267358821864135; -0.00032133611638307096 0.000492446598764205 -5.202695235123991e-5; -0.00011900845048041986 -0.0013119609187850123 0.0023415408959731273; -0.00046910833629171207 -6.898001479518754e-5 0.002292362065498293] %
+
+Mass Used: 95.90706320270738 kg
+Launch C3: 96.1299890771775 km²/s²
+||V∞_in||: 2.615317712189207e-7 km/s
diff --git a/archive/ES_0.562857133371359 b/archive/ES_0.562857133371359
new file mode 100644
index 0000000..3e589fd
--- /dev/null
+++ b/archive/ES_0.562857133371359
@@ -0,0 +1,22 @@
+archive/ES_0.562857133371359---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:26:32.212
+Launch V∞: [7.7660351952921545, -5.972059053985529, 0.10887282945552067] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.335211618614604e-5, -7.752089657234937e-5, 5.662802824532393e-5] km/s
+ V∞_out: [-2.0558801185838276e-5, -0.0001321563141058545, 6.388616184530887e-6] km/s
+ time of flight: 1.77162710315458e8 seconds
+ arrival date: 2029-12-22T12:18:22.212
+ thrust profile: [0.37876274138854454 -0.025055897229588547 -0.12317836018417472; 0.07993141796738007 0.03631424592762977 -0.08507778556771878; 0.061702970658201274 0.04518058767300189 -0.11543473995800636; 0.027612919970865204 0.02767296065390563 -0.07661750948393505; 0.027988064824207928 0.01915329683415597 -0.10269266582444996; 0.018866810256854945 0.021565611433875587 -0.11129832853879658; 0.023865173916965465 0.026152796680418998 -0.09648764777346765; 0.017189472946508435 0.0269118416756897 -0.09832886684963509; 0.004718815038199356 0.01007543314699286 -0.04224042894387738; 0.007924801848677528 0.009422890554973602 -0.046610236501335583; 0.0019005911063632646 0.0030311041940424967 -0.01255158563425247; 0.000663790109981973 0.0039610471502801396 -0.010851299143112659; 0.003222592160481911 -0.0023950699757573886 -0.0102137471802645; -0.0013138180577177536 0.004580219423392634 -0.0038547771816813082; 0.00017443844638306925 0.005217083579395981 -0.006811456062815255; -0.008462694581315076 -0.008601411152586183 -0.0032806596139419238; 0.0015067015615531179 0.005319075722401959 -0.0021832505886688596; -0.00019656506182087578 -0.002363400978149191 0.004212816340002346; -0.010634243429926605 0.015361296351970127 -0.009830362510406209; 0.001207555992086999 0.003042849037510193 -0.009011795605426195] %
+
+Mass Used: 96.73289139774852 kg
+Launch C3: 95.98864529180064 km²/s²
+||V∞_in||: 0.00013390608867697466 km/s
diff --git a/archive/ES_0.5628638412246844 b/archive/ES_0.5628638412246844
new file mode 100644
index 0000000..f0eb119
--- /dev/null
+++ b/archive/ES_0.5628638412246844
@@ -0,0 +1,22 @@
+archive/ES_0.5628638412246844---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T15:35:50.105
+Launch V∞: [7.785641132810141, -6.228674951184134, 0.30207709359851687] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005183153737126536, 0.00035157662716322455, 0.021026133108969388] km/s
+ V∞_out: [-0.02086325719367983, -0.008008195671602986, 0.003843867115053713] km/s
+ time of flight: 1.8101275223279926e8 seconds
+ arrival date: 2030-02-10T16:55:02.105
+ thrust profile: [0.20801666086453974 -0.01710378593832526 -0.08159512162787436; 0.038756939964924166 0.014192011950159388 -0.05099694464861339; 0.038775023658888755 0.022012623143196203 -0.08846756727029481; 0.03625629576086073 0.02520772240611171 -0.1168240143207366; 0.046609229766051634 0.037273033810324686 -0.19014686476459666; 0.01955430837617813 0.01604203161526284 -0.09783163808522702; 0.02278592113523142 0.019903406682468008 -0.13108858767117407; 0.005698851165383619 0.004918394929219674 -0.03766792123048106; 0.0020041195319301028 0.0017440763732383326 -0.015221488850516942; 0.00187442871214539 0.001824470856826191 -0.01568177574723599; 0.0002793685473509752 0.00033446808646598914 -0.002363237787458287; 0.0010157437151511876 0.0009549791257385006 -0.008639603562553897; -0.0019689454653871057 0.0006951254578045097 -0.0050491413753807005; -0.002429648965636335 -0.0006564268295147133 -0.005060168441702891; -0.0003231199456028535 -0.0007817129030956399 -0.0011673481663116152; -0.000474522635490114 0.002664064271039101 -0.0031643430825868506; 0.0020154143791758818 0.0004428426522173127 -0.001936443060477179; -0.0005062313104291785 0.00023337123822531113 -0.0017286947370805381; 0.0016771412335267247 0.0013473489154871609 -0.0030007426856110244; 0.0016503359350318707 0.0009731905625972612 -0.0025206273346441792] %
+
+Mass Used: 76.23535603860228 kg
+Launch C3: 99.50385006689076 km²/s²
+||V∞_in||: 0.021035458884167302 km/s
diff --git a/archive/ES_0.5628652185946205 b/archive/ES_0.5628652185946205
new file mode 100644
index 0000000..4f27ffe
--- /dev/null
+++ b/archive/ES_0.5628652185946205
@@ -0,0 +1,22 @@
+archive/ES_0.5628652185946205---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T15:50:06.823
+Launch V∞: [6.304474058988152, -7.2540664449837555, 0.17594204023622625] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.324146425501685e-7, -1.456889549259234e-7, 1.8482199529511975e-7] km/s
+ V∞_out: [-6.638487799939784e-7, 6.028596941368763e-8, -7.860869106694315e-8] km/s
+ time of flight: 1.874957778749271e8 seconds
+ arrival date: 2029-04-06T17:59:43.823
+ thrust profile: [0.6327366348724277 -0.1380973799794996 -0.17428751701004702; 0.08442797868228911 0.02900851298759688 -0.08196395920014427; 0.08177879803367148 0.0532350309284852 -0.13105278884677649; 0.06952823234287625 0.06191038067944651 -0.15855175530031204; 0.05531050980207123 0.060408054943838316 -0.16082258919506157; 0.022305613662611436 0.028131744201641024 -0.08334933571461309; 0.0170421588396079 0.02460168958539817 -0.07645109554182031; 0.0051730654887367005 0.008146932178773995 -0.027594268293191938; 0.0039429545709038965 0.006745379680514422 -0.023681295882819395; 0.0003445279511680883 -0.00013042918191102687 -0.000659744671540766; 0.0012947022796868945 0.0025189483312758856 -0.009730501094179403; 0.0002586585127935916 0.00039791760621145535 -0.0016042327407196884; -0.0007508646191462589 -0.0002870041873301412 -0.0015612385244574644; 0.0009315001442350457 -0.00014291555367313942 0.0003784705357494642; 0.00021756865648658814 -0.00047765423239708713 -0.0020757035794945; -0.0018095940268599 0.0007732820537499921 0.00012918947885438964; 0.0012466874748330256 0.002514022032555252 0.0009557861188502981; 3.752112600259063e-5 0.0001991655961755499 -0.0009453896196889627; -0.00016759406778527609 0.0020612939765557933 -0.0044285584768419956; -0.00019096152932883756 0.00016419699528249823 0.0013602415151113072] %
+
+Mass Used: 117.6829206507955 kg
+Launch C3: 92.3988287502163 km²/s²
+||V∞_in||: 6.747834627820501e-7 km/s
diff --git a/archive/ES_0.5628673833105922 b/archive/ES_0.5628673833105922
new file mode 100644
index 0000000..af4798c
--- /dev/null
+++ b/archive/ES_0.5628673833105922
@@ -0,0 +1,22 @@
+archive/ES_0.5628673833105922---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T18:47:52.237
+Launch V∞: [6.158861987310452, -7.4137085635418405, 0.08433680359210048] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.7669596581373445e-9, 4.3038162163442136e-10, -6.242142991278078e-9] km/s
+ V∞_out: [-2.2914154026710846e-9, 5.3353249115773345e-9, 8.596671969837152e-9] km/s
+ time of flight: 1.874957778749573e8 seconds
+ arrival date: 2029-04-07T20:57:29.237
+ thrust profile: [0.548566203068457 -0.09895849939823459 -0.14081729794224024; 0.10611279598765969 0.04135810257543252 -0.09041561687649159; 0.09329288409253021 0.06738630488302441 -0.13160988297106263; 0.06602908775838368 0.06515703461787963 -0.13196514777911597; 0.04209691830455508 0.05111687129838032 -0.11055736885499318; 0.040431957152786926 0.05959063415746523 -0.1319011487925528; 0.019753077964235324 0.032418746570938156 -0.07831471165914887; 0.00747646194086364 0.013723342781073915 -0.035998469305431526; 0.011266072479243883 0.02410479498319664 -0.06120389599080711; 0.0007588937748911407 0.0016027600927961403 -0.005085027324868566; 6.701881740940727e-5 -7.080051959496323e-6 -0.00013929839429576322; -5.171711524293323e-6 7.436359572954701e-5 -0.00028145727437455746; -2.7046368139403156e-5 0.00011284490658130649 -0.0004122465735656157; 6.044633300347471e-5 0.00017752353516346686 -0.00024298867625063725; -8.38019510176957e-5 9.698569405949796e-5 -8.519106719902929e-5; 8.362313399104871e-5 -2.8158584206978445e-5 -0.00027157689314572853; -7.826294775190752e-5 0.00011814423483602022 0.0001381782189812087; -0.00013423307735291028 0.0002041877120390571 -0.00019143753908777543; 0.00039317789294425416 0.00022261834481145074 3.2720514782516987e-5; 0.0002544301433676361 0.0002794736233331655 0.00010962275591334535] %
+
+Mass Used: 114.75163187720773 kg
+Launch C3: 92.90176834031139 km²/s²
+||V∞_in||: 9.216361564015432e-9 km/s
diff --git a/archive/ES_0.5628691150507658 b/archive/ES_0.5628691150507658
new file mode 100644
index 0000000..09689bf
--- /dev/null
+++ b/archive/ES_0.5628691150507658
@@ -0,0 +1,22 @@
+archive/ES_0.5628691150507658---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T03:15:14.787
+Launch V∞: [7.703589747976635, -6.211850169696722, -0.0924716527681368] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006468181645442435, 0.0004322729468982248, -0.00026950656916856084] km/s
+ V∞_out: [-0.0003543917915573563, -0.0006090307763685359, 0.00042577895375054157] km/s
+ time of flight: 1.7017844266181627e8 seconds
+ arrival date: 2029-10-01T19:02:36.787
+ thrust profile: [0.18572781871512076 -0.025360060517731316 -0.0702891723552638; 0.09138997361020969 0.03425255294241374 -0.10686852501732161; 0.0702538816502784 0.04481560778181779 -0.14156881411346572; 0.052143893716193206 0.04300710762334568 -0.14988864582008848; 0.0421096157810119 0.04097712042847211 -0.15754386980853105; 0.024939913747511526 0.02719430446686366 -0.11664011100271482; 0.009731362557325696 0.011728335730391982 -0.05425058899385777; 0.014340710811258714 0.01928192096877674 -0.08869742489985552; 0.013651034611960891 0.0193943702236139 -0.09520810735330143; 0.00042877271614857036 0.0012376562532596005 -0.0037247016138513564; 0.0007516674980766005 0.0021315253204121074 -0.008602798755808043; 0.0002143707759904786 -0.00029679786799138624 -5.051881886390685e-5; 0.0021339840181077326 -0.0002799042888515337 -0.0017052117822820316; -0.0003972022094972621 0.0005274029907452996 -0.0030740224555123653; -0.00022142911790649794 -0.0014178997502566266 0.006808997851922223; -0.000331078599533065 -0.001430354240117575 0.004159420672944848; 0.0014153524659083947 -0.002648392318034691 8.52122373939748e-5; -0.00015953644161923196 -0.0005668663666590255 0.0026468734473091143; -0.000298588238084794 -0.00633368824058338 0.0038078479513294194; 0.00011802296498588923 -0.0009517197852706775 0.0055215023940623316] %
+
+Mass Used: 85.35855106155759 kg
+Launch C3: 97.94092854245757 km²/s²
+||V∞_in||: 0.0008233270488872985 km/s
diff --git a/archive/ES_0.5628749310565506 b/archive/ES_0.5628749310565506
new file mode 100644
index 0000000..8d3311f
--- /dev/null
+++ b/archive/ES_0.5628749310565506
@@ -0,0 +1,22 @@
+archive/ES_0.5628749310565506---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T20:04:27.263
+Launch V∞: [7.929713952420536, -5.392021827225333, 0.27081694034909054] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.04866708893783537, -0.29195497633973616, -0.41874205213572707] km/s
+ V∞_out: [0.2366801136760674, -0.202426164675982, 0.40714559782133164] km/s
+ time of flight: 1.8749577787485555e8 seconds
+ arrival date: 2030-04-18T22:14:04.263
+ thrust profile: [0.7654026747191672 0.0032643564041139952 -0.20282587270135546; 0.08095357339391927 0.04949633570647204 -0.08300515011922657; 0.04221834513548214 0.04210404692481354 -0.07909105908673825; 0.04309586782552104 0.05857701979506017 -0.12237517905816857; 0.0277977383500496 0.04725726572676549 -0.10870901668244767; 0.018261835493861248 0.03749690931169947 -0.09267968316716971; 0.009275653687025457 0.022752636066147015 -0.058784899926974395; 0.004655966166379055 0.016026685420737694 -0.0450459387869468; 0.0016909705366173987 0.008277248919214495 -0.022153422940603226; 0.0016138646869062298 0.00478182193167824 -0.018107521749120517; -0.004186760540562728 0.00084782198427308 -0.0036017097325201906; -0.002763943678455427 0.0018589269241759622 -0.009765883582299668; 0.0014084706112929995 0.0008371215919131254 -0.004936345292328558; -0.002346303454799028 -0.00018774463312436532 -0.0013211806210660605; 0.006362313589158659 -0.0037918380877979916 -0.0021844098381570733; 0.007975624416790016 -0.0008300559866103005 -0.0008965167268747101; 0.00016870237312146858 -0.00037758097831599004 0.0013188708355843953; -0.002988972453872383 -0.0008073901922496854 0.008669249039456808; 0.00294047389178571 0.0035546110265055973 -0.012869910901048096; 0.0006238822599947528 0.0011965763802302414 -0.004431582016885725] %
+
+Mass Used: 119.85972625458271 kg
+Launch C3: 92.02760456766738 km²/s²
+||V∞_in||: 0.5127875778351685 km/s
diff --git a/archive/ES_0.5628760267122366 b/archive/ES_0.5628760267122366
new file mode 100644
index 0000000..8c80cb6
--- /dev/null
+++ b/archive/ES_0.5628760267122366
@@ -0,0 +1,22 @@
+archive/ES_0.5628760267122366---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T22:07:47.279
+Launch V∞: [7.588818373956609, -6.427168429089219, 0.05231353498580904] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0001379669068000712, -9.248810628615174e-5, -0.005858273426031967] km/s
+ V∞_out: [0.005527934776531756, 0.0017760055227202154, -0.0008460470266644788] km/s
+ time of flight: 1.7524391777686703e8 seconds
+ arrival date: 2029-12-04T04:59:44.279
+ thrust profile: [0.1923254394668969 -0.020266636752091238 -0.07498400558493325; 0.07631397184307903 0.028271735950899005 -0.09605161776092612; 0.04804874133698969 0.02829206388692809 -0.1063417952236573; 0.09504833503922601 0.07314114161344015 -0.27236948063429006; 0.025632994159690854 0.023719742387374863 -0.10241531961860413; 0.02395825227891188 0.023413957514931184 -0.11522649770314035; 0.011844795822169617 0.012516496424054484 -0.06971372887612338; 0.0034446285232588767 0.003626755476473181 -0.023869517593560156; 0.001566080791227958 0.00159140117441663 -0.011607637578552113; 0.0022747130106179356 0.0029267105981627636 -0.02192583753269097; 0.002293036257804785 0.0026496259498239344 -0.020719525004772987; 0.0008341586203523668 0.0009139232926558302 -0.0061473119268184336; -0.0001778882417546568 0.000908696010634403 -0.00047802405123412834; 0.0002606872149321061 0.0004357622163410997 -0.001009887195443031; 0.0007184956074679874 -3.5067199682645224e-5 -0.0006494808180861225; 2.7726987586315215e-5 -0.00044688942235027613 0.00015860430086482395; -1.2914640212247723e-5 1.4859896002068995e-5 0.0002424336912407928; -0.0001250289791962945 -0.00023965608822742882 0.0002687442286663567; 0.0006620404640967003 -0.001057455308839586 -0.001227511000293524; -8.785356843752244e-5 -0.00020203546392817906 0.00026147492878815493] %
+
+Mass Used: 79.76389346171163 kg
+Launch C3: 98.90139503472531 km²/s²
+||V∞_in||: 0.005860627649947461 km/s
diff --git a/archive/ES_0.5628780437545017 b/archive/ES_0.5628780437545017
new file mode 100644
index 0000000..7e00cf3
--- /dev/null
+++ b/archive/ES_0.5628780437545017
@@ -0,0 +1,22 @@
+archive/ES_0.5628780437545017---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T12:33:35.586
+Launch V∞: [7.663015273764813, -6.039657606564458, -0.013262422806747717] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.39032073153133e-5, -1.1196869052882814e-5, -9.608694345273618e-6] km/s
+ V∞_out: [-1.693332733269456e-7, 1.2242932510532236e-5, -1.602346804863461e-5] km/s
+ time of flight: 1.774374886597686e8 seconds
+ arrival date: 2029-12-25T04:45:03.586
+ thrust profile: [0.31825781028413835 -0.02164124679504356 -0.10086546812862875; 0.2240613719342388 0.10700859221311564 -0.22042936347319267; 0.055669486471243014 0.048797902180715017 -0.11034198769502758; 0.04318967279834469 0.05202167931764981 -0.12805392708945187; 0.029550334321160943 0.04163605407342789 -0.10920026882014484; 0.020111509123135595 0.032722176951643867 -0.09149450280707828; 0.019268598570281487 0.032327809762571255 -0.09424182108840184; 0.005938820472406433 0.01382916465105802 -0.04726837262076434; 0.003847391743216047 0.00655819468085667 -0.012057595096628924; 0.0016957542930556243 0.00400549222257341 -0.016304024484734347; 0.001406384740108925 0.0008289136654336579 -0.0025972047637605475; -0.00012814107116658209 -0.0023135704797309408 -0.0011921977714513662; 0.004144721281202115 -0.001016592445444807 1.3565239181981617e-5; 0.0008650976438559986 0.00033388134523137806 -0.00796215635824578; 0.004485765946399085 0.0019990261105344072 -0.0065669044635166905; 0.00027751718061606173 -0.008381865364463776 0.0014128957657050193; 0.0022014599534721053 0.005502744971598448 -0.0030048283172292977; 0.0035666701760089575 -0.0006905107766067526 -0.008362318383097651; 0.010943656533582776 0.010140628068869565 0.006773912918168236; -0.018240213808042513 -0.0010532318866909702 -0.011408783834618234] %
+
+Mass Used: 101.36096698324855 kg
+Launch C3: 95.19944298234344 km²/s²
+||V∞_in||: 2.0273037691990795e-5 km/s
diff --git a/archive/ES_0.5628905455096935 b/archive/ES_0.5628905455096935
new file mode 100644
index 0000000..020fe72
--- /dev/null
+++ b/archive/ES_0.5628905455096935
@@ -0,0 +1,22 @@
+archive/ES_0.5628905455096935---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T23:10:22.007
+Launch V∞: [7.6694671604307425, -6.088276635017272, -0.0458759154177466] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4532097352338231e-5, -1.005786460810563e-5, -0.0007123841368645852] km/s
+ V∞_out: [0.000649816134165634, 0.00018183856388720307, -0.0002298554270570713] km/s
+ time of flight: 1.7181439612379953e8 seconds
+ arrival date: 2029-10-19T13:23:38.007
+ thrust profile: [0.33977749711092947 -0.041588287446124195 -0.11891053398595461; 0.13542600816421316 0.0562287920174146 -0.14814386448441524; 0.04946273956782386 0.03480849844816541 -0.094403396561731; 0.06882976108220967 0.06358624830592942 -0.1881859955831849; 0.03454702324196558 0.0383145262174961 -0.12426223660175303; 0.023016013427980816 0.029679191484842753 -0.10277160949111269; 0.021932482723906816 0.03114258955143651 -0.11692556922131743; 0.0064807234846575145 0.013042139776017796 -0.04809305659160665; 0.003434598133938754 0.009798881470546113 -0.03842622450008858; 0.0009189015006915976 0.0011636055559209554 -0.006566843762712658; 0.0004003272962098258 0.0005558339725788299 -0.004000367046364228; 0.00042471036415082675 0.0008135784554762686 -0.0054339042747812375; 0.003985527001923932 0.0024227056597442872 -0.005141727078265004; -0.0002611646524764527 -0.00023070190610843702 0.0015136169379004467; 0.0003807430502427607 0.0005786225403539632 -0.007101127315861172; -0.0016721384129967838 -0.004003767577786342 0.0026664222911085326; 0.0011640540662897158 0.0005883081543840736 -0.003803823946051248; -0.010942844937130589 0.0028848066585305913 -0.006992350572133474; -0.001839900324140277 0.0004996442142344393 -0.0011556395990211087; -0.015096877114713346 0.002549534549553891 -0.0051925668842930425] %
+
+Mass Used: 97.34763262525257 kg
+Launch C3: 95.88994350903826 km²/s²
+||V∞_in||: 0.000712603326507976 km/s
diff --git a/archive/ES_0.5628941996683593 b/archive/ES_0.5628941996683593
new file mode 100644
index 0000000..3106134
--- /dev/null
+++ b/archive/ES_0.5628941996683593
@@ -0,0 +1,22 @@
+archive/ES_0.5628941996683593---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T23:18:39.180
+Launch V∞: [7.497425718029243, -6.005861373700312, 0.0466828020025509] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9492433512034184e-9, 2.3255165088796397e-9, 9.009704241835945e-10] km/s
+ V∞_out: [2.0801767805931194e-9, -1.8525065122513571e-9, -1.522267554026196e-9] km/s
+ time of flight: 1.751168598564027e8 seconds
+ arrival date: 2029-11-26T18:52:58.180
+ thrust profile: [0.6262735525025883 -0.07038093563512124 -0.16843679934793357; 0.17871744065357603 0.07866252771195531 -0.1830799749268711; 0.04948944089725006 0.039593850837907 -0.0984989227177465; 0.05266754369209984 0.05605955186244207 -0.14280837278017106; 0.03882453764551674 0.04865454323049892 -0.14239048386744485; 0.029031351884012666 0.041992471364989646 -0.12833742166183243; 0.009463661454034064 0.013220943764518215 -0.04798862148936899; 0.004154239717279804 0.007164448113774639 -0.028530536778362075; 0.0028516902054197013 0.006832167163680364 -0.025767390028964932; -0.0003348164541599236 -6.385625184980159e-5 -0.009138784655868116; 0.0011260727552746296 0.0017638043650450694 -0.011034997174241687; 0.00150871820698379 -0.0011803168184492392 -0.004879143672491163; 0.0034760023530948443 0.0029197550183634067 -0.0004555598130194013; -0.002731647890062527 0.00323695047130288 -0.00025577620944190966; 0.001690652353019288 0.0008799800182161738 -0.0037212884066122488; 0.001210312083916593 0.005169703079628414 -0.00145883404326417; 0.0016071433645250671 -0.00033360865822522627 -0.004013824077443798; 0.00018796355128873358 -0.0005123802346246329 -0.01543401731519328; -0.005148337312832637 0.012997284203035144 -0.019446232404703827; 0.001660331939290703 0.007392563446666769 0.0063833523909506635] %
+
+Mass Used: 118.38690157115116 kg
+Launch C3: 92.28394252147451 km²/s²
+||V∞_in||: 3.165331638317863e-9 km/s
diff --git a/archive/ES_0.5628948593052597 b/archive/ES_0.5628948593052597
new file mode 100644
index 0000000..34b0cdf
--- /dev/null
+++ b/archive/ES_0.5628948593052597
@@ -0,0 +1,22 @@
+archive/ES_0.5628948593052597---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T08:51:39.219
+Launch V∞: [6.497707763434663, -7.549381713918112, 0.12428844148120335] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001087384908435919, -0.006880582637999635, 0.009513816047794298] km/s
+ V∞_out: [-0.008188188141925417, -0.006582539214350279, -0.005351938478854004] km/s
+ time of flight: 1.8203694700053963e8 seconds
+ arrival date: 2029-02-05T06:40:46.219
+ thrust profile: [0.12560243328937626 -0.040363169259940324 -0.04977154862267195; 0.019185890660857758 0.0030874025951363637 -0.02320449139296813; 0.05849336067987823 0.0216775847343811 -0.11405245054310915; 0.0721255480920504 0.035820672192586424 -0.19468817885779618; 0.05877799832969284 0.03453326852940422 -0.20122843439382854; 0.036429900089269183 0.02400668473280759 -0.1503100223529574; 0.017277216660277147 0.012386330500835133 -0.08332365474706659; 0.006857066291469453 0.005259654023769028 -0.0379371071636918; 0.001888940395179606 0.0011525908411049955 -0.009724487531336442; 0.002844972751181921 0.002435624526635939 -0.020261041248470116; -1.4229386985928263e-5 0.001930759692765443 -0.012024959632612246; -0.0007390310754892669 0.0008266238926625008 -0.0016013023586518265; 0.0025725691347240334 -0.0006069339235387542 -0.0022507839948719332; 0.0007943197653503912 -0.000696674008468325 0.002703888289234573; 8.980808876965759e-6 -0.0007935151191867181 -0.0005280314337182345; -0.0026434359305272824 0.00342751106586476 -4.009988295545445e-5; -0.00023603100604869176 -0.0003477024439926561 0.00012066194433247007; -0.008258607000435464 -0.0033406423074021077 0.0031202868312570093; 0.00015588743176246845 -0.00029682233635302483 -0.0008915330227955605; -0.0008936646977161131 0.00026594328922852995 0.0009675280018218951] %
+
+Mass Used: 77.8758971837342 kg
+Launch C3: 99.22881805812608 km²/s²
+||V∞_in||: 0.011791417182370596 km/s
diff --git a/archive/ES_0.5628952748338936 b/archive/ES_0.5628952748338936
new file mode 100644
index 0000000..69b65b1
--- /dev/null
+++ b/archive/ES_0.5628952748338936
@@ -0,0 +1,22 @@
+archive/ES_0.5628952748338936---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T17:21:53.053
+Launch V∞: [7.8444655222369075, -6.192590854892286, -0.14007321193149996] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.0831962523178454e-7, -3.917396748643578e-6, 6.994555666867883e-7] km/s
+ V∞_out: [-6.123945154914923e-7, 2.4120167618846303e-6, 3.131812086308483e-6] km/s
+ time of flight: 1.8317950305656353e8 seconds
+ arrival date: 2030-03-08T20:33:36.053
+ thrust profile: [0.19648505392943352 -0.01625109591218308 -0.08237454674755755; 0.04257932996853145 0.01524116921468226 -0.05938666349259774; 0.041669423409096726 0.022680000399719846 -0.10182892704331538; 0.03548780372344519 0.022997426179532626 -0.12305054129803962; 0.02730038483955454 0.01938253162444102 -0.12118389162847952; 0.018489422862502776 0.013785423824600511 -0.09903395020030455; 0.011305543612433138 0.008656701365888367 -0.07023547174082191; 0.006079369407862238 0.004778069729989926 -0.04280590962214061; 0.01150269177040017 0.009107367669303151 -0.08873093059827457; 0.002935804955576841 0.00240631867088394 -0.02489809166136337; 0.0004020152864661113 0.00043480181799219027 -0.0042412140022452536; 0.00040258934174938846 -5.387365370110417e-5 -0.0019287843896018252; 5.629387338078047e-5 -0.0003994814327171344 -0.004323548831706155; -0.00010622159320766472 0.00019633335345158162 -0.0016966818912199256; 0.0007570861682571848 -2.587588709092835e-6 -0.0013629269004913724; 0.0002298927759143589 5.879002969641462e-5 -0.002018597003344556; -0.0013978026458585286 -0.0006482593270997383 -0.0033377599289690606; 0.0010370599611539406 0.0008854437668976546 0.0006197850417935797; -0.000307993620754487 -0.0006194658603603713 0.000508894246253062; 0.0003061347418325547 0.002334244851470675 -0.00234703115658653] %
+
+Mass Used: 73.94107954577612 kg
+Launch C3: 99.90344133035994 km²/s²
+||V∞_in||: 4.000245029045326e-6 km/s
diff --git a/archive/ES_0.5629014463512015 b/archive/ES_0.5629014463512015
new file mode 100644
index 0000000..171fae2
--- /dev/null
+++ b/archive/ES_0.5629014463512015
@@ -0,0 +1,22 @@
+archive/ES_0.5629014463512015---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T07:57:20.228
+Launch V∞: [7.817314521515055, -6.235852766131479, -0.10852681762659025] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004014674456515848, 0.001034587475922613, 0.0023640188251303628] km/s
+ V∞_out: [0.0023999689985043852, 0.00028580060595660267, -0.0009890650810161152] km/s
+ time of flight: 1.754381730744422e8 seconds
+ arrival date: 2029-12-05T20:46:53.228
+ thrust profile: [0.11628717799968841 -0.017022609870760135 -0.05040217373505398; 0.03853069227496792 0.01094493231161924 -0.05209062942272689; 0.03487391763888576 0.015844699286960348 -0.08415535485970388; 0.03657808370888588 0.02078872561327614 -0.12376431392786007; 0.03628177050734153 0.023323177361453253 -0.15938521643840858; 0.03138362375073863 0.02120213668148198 -0.1667077087032913; 0.015738632452047555 0.009782107757389559 -0.08867971059258442; 0.013534364813752225 0.010143911067435177 -0.09382105951234855; 0.0030765789667014914 0.002441044055494346 -0.02147737643203558; 0.003722120898672205 0.003879030260212737 -0.030894609677413094; 0.0003314743452191195 0.0011680616271147878 -0.0039324372705010656; 0.0008634756206832436 0.0006500209715967116 -0.006692574647712951; 0.001383932225810693 -0.0013549400431750612 -0.003258332079845906; 0.006378656698834178 -6.732052171861598e-5 -0.0028998205074432246; -0.00035421569775183993 0.0014020038074479449 -0.0044004048311911854; 0.004128502961094533 -0.007197440334624121 -0.00277227653477345; 0.0008011408058150745 3.1669309014272976e-5 -5.4438682693870154e-5; 0.0030287046776178777 0.000948427655567966 0.001233887890876366; -0.0018740854948295763 0.011860950835381441 0.0047373894465323856; -0.0021348523955184735 0.004716707212719124 -0.002293010735036104] %
+
+Mass Used: 73.3380967137955 kg
+Launch C3: 100.00804411930393 km²/s²
+||V∞_in||: 0.0026115383131067927 km/s
diff --git a/archive/ES_0.5629041018271757 b/archive/ES_0.5629041018271757
new file mode 100644
index 0000000..96b56c0
--- /dev/null
+++ b/archive/ES_0.5629041018271757
@@ -0,0 +1,22 @@
+archive/ES_0.5629041018271757---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T23:09:00.349
+Launch V∞: [7.576231439320425, -5.938163863088335, 0.5239187574040877] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012468295883809846, 0.07526220051318322, 0.07824790931829007] km/s
+ V∞_out: [-0.01871183624115505, 0.017274133375528234, -0.10620621210436844] km/s
+ time of flight: 1.858087362163186e8 seconds
+ arrival date: 2030-03-31T12:41:16.349
+ thrust profile: [0.35013545769326093 0.023847250426134326 -0.08026185248529229; 0.31080109967844805 0.227494183789978 -0.18913981496552315; 0.10577922943295708 0.13299894411976698 -0.1423614902090787; 0.059942851499885624 0.10427160760355114 -0.1240810255215283; 0.03703014196759901 0.08415577761766965 -0.10991897260581214; 0.021961379249055037 0.0633382851952605 -0.08965056264509991; 0.009334232034154392 0.033924796712294474 -0.05268672315671152; 0.0014604034173633185 0.006725174208621068 -0.012232462445937214; -0.00021311385996125392 0.0031099625809975677 -0.0046767936330522125; -0.0004432673766163164 0.001740279586933888 -0.0017039811666666727; -0.002108904938752817 0.0011880642705852683 -0.0013593194712826849; -0.0011628747699261343 0.0002242042941390356 0.0002094359369528532; 6.391088613178481e-5 -0.001928352951266865 0.001759353822253831; -0.00016918579498518416 -0.0007993942360191697 0.0010384658548199086; 0.00024064311285023276 -0.0008651755675049004 -0.00037677960443267204; 0.0012983466505396206 0.002284538099299424 0.001011485039730979; -3.536369334031437e-5 -0.0006739963151776435 -0.0006966552499458733; -0.0008024727812458594 -0.001678475328761751 -0.001074347666825862; 0.001740196282786401 -0.004558134090272005 -0.0028399271934523122; -0.0020400713914165407 0.00292134416177178 0.001996198148151642] %
+
+Mass Used: 114.59733024856587 kg
+Launch C3: 92.93556375139528 km²/s²
+||V∞_in||: 0.10928216936452247 km/s
diff --git a/archive/ES_0.5629088266608935 b/archive/ES_0.5629088266608935
new file mode 100644
index 0000000..963083c
--- /dev/null
+++ b/archive/ES_0.5629088266608935
@@ -0,0 +1,22 @@
+archive/ES_0.5629088266608935---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T12:53:31.474
+Launch V∞: [6.512357656582506, -7.478525479715535, 0.07714945812013496] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.663438758967266e-7, -0.00018937636729819031, 0.00012183524741872001] km/s
+ V∞_out: [0.00010845028726276, 0.00018932626560663336, -5.575050581927132e-5] km/s
+ time of flight: 1.874957778951711e8 seconds
+ arrival date: 2029-04-10T15:03:08.474
+ thrust profile: [0.16598766622300784 -0.03801824628423614 -0.05810149182367575; 0.07262055379439192 0.021784833036433443 -0.07611344919662381; 0.07568629340996325 0.04234041222766147 -0.13262796606611615; 0.031409600724278536 0.023467959803073462 -0.0763717805198689; 0.03712330860702164 0.032965391293145574 -0.1207918255133594; 0.03753946204046274 0.03822524263658676 -0.13973937255329452; 0.02558783041551436 0.030056115773394478 -0.11578213220623203; 0.008698677553832624 0.009955352557046673 -0.043319836109222416; 0.011183819611362054 0.01750668173839072 -0.07229876650472601; 0.0017559422746911601 0.004192627216524947 -0.013940368442471577; 0.00144395222952678 0.003408368974807852 -0.010036260343461133; 0.0002267726601832469 0.0003770589521983379 -0.0015602147282669958; 0.004091880917023657 0.0006019725973041635 -0.007659912627028702; -0.0008300976494049334 -0.0005405399054444146 -0.001236832652583631; 0.0008716899788402856 0.0012890078825930679 -0.0021790071663649415; -0.0005630224988090807 0.001775285561950418 -0.0010858205656464556; -0.002093855641640472 -0.0026636951195451444 -0.0025141750771452073; -0.0014990432402803735 0.001439856381777154 -0.0007500961147819629; -0.0009823257876109082 -0.0016249591190192676 0.0019961331738426085; 0.0016542100164147605 0.0023331724532021634 0.005610377464144499] %
+
+Mass Used: 83.04722822250869 kg
+Launch C3: 98.3450976368915 km²/s²
+||V∞_in||: 0.00022518338471127388 km/s
diff --git a/archive/ES_0.5629112945339337 b/archive/ES_0.5629112945339337
new file mode 100644
index 0000000..78de322
--- /dev/null
+++ b/archive/ES_0.5629112945339337
@@ -0,0 +1,22 @@
+archive/ES_0.5629112945339337---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T00:35:08.458
+Launch V∞: [6.431530182827828, -7.4616330333789325, 0.04878723470939129] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.051238058700398e-7, -1.9365473849683374e-7, 2.531935772173751e-7] km/s
+ V∞_out: [-8.2212254463483e-7, 2.037113556019284e-7, -1.1272004744988389e-7] km/s
+ time of flight: 1.8570346576480913e8 seconds
+ arrival date: 2029-03-20T08:52:53.458
+ thrust profile: [0.2939525903729688 -0.08414979514333074 -0.10861016111091953; 0.08321746504113639 0.018861870386374477 -0.09592233868663279; 0.04920594844885958 0.02281821655052391 -0.09648590594558679; 0.029336179079830743 0.01823096963808859 -0.08187893188548188; 0.03478874143516563 0.02601877968264138 -0.12216273158387918; 0.016795269498487583 0.014366673756747963 -0.0738991871700041; 0.013691551276423434 0.01313076638020968 -0.07106089871012478; 0.024633426058892034 0.03256555391849125 -0.1688104100175049; 0.008187089575900823 0.00987942535403306 -0.05945023030377001; 0.003062395502686093 0.003479990304846389 -0.023055081733492473; 0.0017825777819691073 0.0021657321191550223 -0.014448413242448319; 0.0013927952135703975 0.0018300594014374351 -0.011498874182790593; 7.998972319111781e-5 0.00013816324288351534 -0.0005008451776149392; -0.0009272098231971077 0.0005942525706318467 0.000410939246627217; 0.00022684154791825288 0.00021963160133320168 -0.0007378486436663571; 0.0004589167560427645 0.0006400299866663485 -0.0007844125622657403; 0.00041952339360033314 5.558232099912662e-5 -0.0002237864044684761; -0.00028062813223152385 0.0009156620832874786 -0.0021740787349359505; 0.0005472062189667669 -4.372479549030864e-5 -0.0010757252822286034; -0.0009492483930257727 0.000142991241971759 -8.945169702451686e-5] %
+
+Mass Used: 90.64609572129484 kg
+Launch C3: 97.04292821170763 km²/s²
+||V∞_in||: 8.659292627374741e-7 km/s
diff --git a/archive/ES_0.562914934120654 b/archive/ES_0.562914934120654
new file mode 100644
index 0000000..334fce7
--- /dev/null
+++ b/archive/ES_0.562914934120654
@@ -0,0 +1,22 @@
+archive/ES_0.562914934120654---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T15:20:55.266
+Launch V∞: [6.395371902093704, -7.336942211236694, 0.12018964350694215] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4861761056614147e-6, 0.0004467864830286202, -0.0003306737226702085] km/s
+ V∞_out: [-0.00025723508360151745, -0.00048252766503052236, 9.974834928832065e-5] km/s
+ time of flight: 1.8527420221155044e8 seconds
+ arrival date: 2029-03-13T00:24:17.266
+ thrust profile: [0.4818497575188454 -0.1272626560887123 -0.1464066931591793; 0.06275107345694962 0.017877625879592112 -0.06498295972370931; 0.042717193118634034 0.023564086015776094 -0.07381222199730575; 0.05066446525919345 0.03777084177698513 -0.12197382058059034; 0.03487119275496944 0.03178660688893362 -0.10975039056739072; 0.024396842025690084 0.02603305646596129 -0.09597954981765228; 0.024190095577826535 0.027957091559915537 -0.10416488430722283; 0.014095965062411422 0.017549831074420156 -0.07048394434314019; 0.018831988530418665 0.024812100732267226 -0.10642642132508574; 0.004051553040798481 0.006089761889545607 -0.027130508480896685; 0.00030005332371603043 0.004652586504096823 -0.020533025021284977; 0.00025043431415162833 0.0003919247044218517 -0.0010315294352387634; 0.0005039892414669603 0.00016868124415533165 -0.0017856148558149086; 2.325484073769453e-5 2.8110438151799266e-5 -0.00046755484325664503; -0.0003920875117863823 -9.911148762767449e-5 3.146067036749239e-5; -0.00017187665982134145 -0.00021410610173363133 -0.00038856203518960135; -0.0006350927046028415 0.00010316772412901368 0.0005752367799947757; 0.00025282576885187353 -0.00013325461866840489 -2.482919033384729e-5; 0.00046585707124849655 0.0007857370921550674 -4.610627072314836e-5; 1.6311256743662246e-5 -8.43958392435651e-5 0.00014052237714454917] %
+
+Mass Used: 104.04939123021359 kg
+Launch C3: 94.74594832752275 km²/s²
+||V∞_in||: 0.0005558466344245277 km/s
diff --git a/archive/ES_0.5629240269831859 b/archive/ES_0.5629240269831859
new file mode 100644
index 0000000..9c7f69d
--- /dev/null
+++ b/archive/ES_0.5629240269831859
@@ -0,0 +1,22 @@
+archive/ES_0.5629240269831859---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T19:01:10.170
+Launch V∞: [7.967714623752139, -5.775095048426693, 0.11145395229214636] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5189134581891968e-9, -1.082114378568756e-8, -6.221041628375305e-9] km/s
+ V∞_out: [-8.014743955217896e-9, 8.358672947934531e-9, 4.894452029558122e-9] km/s
+ time of flight: 1.82765431804457e8 seconds
+ arrival date: 2030-02-26T03:11:41.170
+ thrust profile: [0.2807752728978226 -0.011810316493673343 -0.09008602552247758; 0.09205916621495577 0.047147948652603945 -0.10169731733379675; 0.058921688422150724 0.049138734176474366 -0.11723147234494834; 0.05190562028346884 0.05640776349093341 -0.1493273019041275; 0.03387812863984324 0.044454498361367924 -0.13215937016900456; 0.01081974164758109 0.017744714994014633 -0.05729779703951214; 0.005345230761723602 0.01181332410677982 -0.03532638365951171; 0.004312185829077655 0.010574302896153577 -0.03688899623668083; 0.0077100131336798414 0.017240251019581616 -0.06655811336031142; 0.001110819784006613 0.002541536770439637 -0.011864431027056538; 0.003220815088516831 0.008771013022081818 -0.03498839402081898; -0.002048633422518359 -0.00015073290671761407 -0.010765409969803751; -0.005649507759317904 -0.005518409315719841 -0.00323144917309196; -0.0038935341173415754 0.0010884576457928087 -0.01711982629306653; -0.00023129171265938415 -0.012584983362985547 0.0007472667113059984; -0.0009460272121864129 0.0019030173041766948 -0.007752022456260167; -0.0007943197495988029 -0.003486235064539491 0.00884329816101631; -0.00011851123488674131 -0.0007151494323230803 0.004751077428735704; 0.011301550186170727 0.015301252914090763 -0.015082504249054406; -5.608060634916607e-5 0.0013982667756638006 -0.018537354577264624] %
+
+Mass Used: 91.79440823723007 kg
+Launch C3: 96.84862112739773 km²/s²
+||V∞_in||: 1.2574005323124816e-8 km/s
diff --git a/archive/ES_0.5629336953223094 b/archive/ES_0.5629336953223094
new file mode 100644
index 0000000..6da210f
--- /dev/null
+++ b/archive/ES_0.5629336953223094
@@ -0,0 +1,22 @@
+archive/ES_0.5629336953223094---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T12:12:55.756
+Launch V∞: [6.389769196278984, -7.5400742825024745, -0.014818274904491434] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.113380534708226e-9, -1.9530076271738233e-9, 1.7223448882808653e-9] km/s
+ V∞_out: [1.0069290269692853e-9, -2.2847491594897954e-9, -3.1629092761356544e-9] km/s
+ time of flight: 1.85265000579738e8 seconds
+ arrival date: 2029-03-15T18:42:55.756
+ thrust profile: [0.19398053661840708 -0.055676880327108005 -0.07622305278698714; 0.14976018487477555 0.031005422770909896 -0.1718623092789702; 0.041691648838329716 0.0194784425050867 -0.08422774839352855; 0.06120600861119164 0.036245084494396965 -0.17051258503242037; 0.036291401406211114 0.024270260448947756 -0.1251466625479225; 0.01927373864284516 0.013974110189937465 -0.08283952844848376; 0.02007568830271998 0.017265793209413096 -0.10004630526518417; 0.01243755527994393 0.00988958670333352 -0.06013423746398805; 0.005894765547432699 0.00557236261288544 -0.03734553563189261; 0.0006357386740539109 -0.00017423839111825503 -0.002477250931035661; -4.560255689434645e-5 0.00012004347734033587 -0.0012862347158338885; -0.0017559438031159993 0.0006357252514716978 -0.004373417491838989; 0.0012572179669211893 -0.0017111783840010985 -0.0014808609326743603; -0.00016391348513214866 1.2187221277666516e-5 -0.00018674324070546311; 0.0033470346218499357 0.0011370398389005962 -4.382070376881099e-5; 0.0009844166503467306 -0.0021973463939162128 -0.002762716482138299; 0.0013309288790147897 -0.0013638159919595843 0.0011489761163087846; 0.0011525859395451715 0.0011942405914167828 -0.0013502609461354602; 0.001148382118052367 0.00042552926624279236 -0.0033655142681172957; 0.0008331483981483404 -0.0008272108894657 -0.002555005170897736] %
+
+Mass Used: 86.9437853422819 kg
+Launch C3: 97.68209014864213 km²/s²
+||V∞_in||: 3.3536678414043905e-9 km/s
diff --git a/archive/ES_0.5629344721049263 b/archive/ES_0.5629344721049263
new file mode 100644
index 0000000..9c10007
--- /dev/null
+++ b/archive/ES_0.5629344721049263
@@ -0,0 +1,22 @@
+archive/ES_0.5629344721049263---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T19:51:57.552
+Launch V∞: [7.666755995541986, -5.767523065871479, 0.1661829192984832] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.7680776665785057e-7, 3.0217588992140568e-6, -5.9996804008380977e-5] km/s
+ V∞_out: [-2.253956939562095e-6, 5.9976311358883435e-5, -6.476233805858469e-7] km/s
+ time of flight: 1.8749577787343755e8 seconds
+ arrival date: 2030-04-20T22:01:34.552
+ thrust profile: [0.5669192123410858 0.014221538476147672 -0.11400980346283197; 0.19576058362380436 0.1389833311374319 -0.1547604181414724; 0.041365561830812046 0.049152548553704004 -0.06337289614642655; 0.04356558553420651 0.07230690873885899 -0.10104099962458311; 0.03215181274177996 0.06921379546026903 -0.10502186131964054; 0.03525204665491476 0.10007461121858756 -0.1554528344569777; 0.009124592822308231 0.03068712577712531 -0.05377920566425296; 0.0024717347153220192 0.010388663551111982 -0.018952648579697272; 0.002376333152548203 0.013274540083410028 -0.025150968151475137; -0.004167631857192261 0.0014675991178899348 -0.006126770482301458; 0.00038621309902557967 0.0032941155685731424 -0.0062392927173002865; -0.008676944740691526 0.0032838755831971498 -0.002607942082416769; 0.002070054019785556 -0.0012526338920695315 -0.004056817163279847; 0.0035632447104048904 -0.007435051403447482 -0.013487341783266302; -0.002092738330158206 0.0015504544729017617 0.0007096239196897215; 0.00019636686495691806 0.0010576837855179007 -0.002537669643206248; 0.0030912554555195954 0.00013040656823108893 0.0025456114894194266; -0.0004477173671612602 -0.0033405542023319506 0.004237585462096821; -0.000554694286793633 -0.005358656193129873 0.012646384122470808; 0.0012867776795067649 -0.009033895742210408 0.008760934361095986] %
+
+Mass Used: 119.6755457787176 kg
+Launch C3: 92.07108657320511 km²/s²
+||V∞_in||: 6.007403350997894e-5 km/s
diff --git a/archive/ES_0.5629425151586425 b/archive/ES_0.5629425151586425
new file mode 100644
index 0000000..4739684
--- /dev/null
+++ b/archive/ES_0.5629425151586425
@@ -0,0 +1,22 @@
+archive/ES_0.5629425151586425---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:09:23.109
+Launch V∞: [6.2025360119691735, -7.655346644933916, 0.18316982248883804] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.634986532713661e-7, 1.220813443548804e-7, -1.398042585610333e-7] km/s
+ V∞_out: [4.7657298199553413e-7, -1.2573784302444698e-7, 5.973230935383873e-8] km/s
+ time of flight: 1.805291891830332e8 seconds
+ arrival date: 2029-01-18T15:09:12.109
+ thrust profile: [0.25210492795952616 -0.07349556887473752 -0.09322935125627835; 0.09041462768747835 0.01877331303047129 -0.0974252740130962; 0.0719181211146749 0.03141551470330789 -0.12830977034650534; 0.07179355670696509 0.04217321702904401 -0.17141364168713574; 0.031645346261725646 0.02309450411291648 -0.10328267030902251; 0.053002256685653455 0.04358785991571243 -0.19624711566078754; 0.01779466313082464 0.016778584403679988 -0.0778561727409362; 0.007826677549684639 0.007012468889171236 -0.041095578285677566; 0.0042716191299929825 0.004041511382759774 -0.02517886300476295; 0.0025128571673268237 0.0027393329070552817 -0.017243986460536924; 0.0008009916595051008 0.00083919296586018 -0.005313059788503157; 0.000173050652027424 0.00039735849773763675 -0.001507079831571795; 0.0006782215466894625 -0.0009732558916717874 -0.0016067958940477912; 0.00045441764839309457 -0.00026316098605500183 0.0001885472946762509; 0.0003503827542436968 -0.0004967195327760163 -0.0011262070775967163; -0.0008372644260832515 -0.0003171836256346919 1.3382795233945143e-5; 0.0008892252890629084 0.0010402898195895213 -0.0004681851632950656; -0.00027355882101424956 0.00030312576837203907 -0.0005697881081499002; 0.0009437713267009496 0.00019058946476551174 0.0005647524463568246; 8.20556457191557e-5 -0.0012341167011855527 0.0005501526062225422] %
+
+Mass Used: 90.29513858156452 kg
+Launch C3: 97.10933641774601 km²/s²
+||V∞_in||: 4.992795679132736e-7 km/s
diff --git a/archive/ES_0.5629512323581518 b/archive/ES_0.5629512323581518
new file mode 100644
index 0000000..070237c
--- /dev/null
+++ b/archive/ES_0.5629512323581518
@@ -0,0 +1,22 @@
+archive/ES_0.5629512323581518---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T04:15:04.339
+Launch V∞: [6.591779631308047, -7.5132781623831955, 0.0836989177620478] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.8363375073343116e-7, -7.605613470120398e-8, 9.149230564085776e-8] km/s
+ V∞_out: [-3.863438232507162e-7, 9.873292755741724e-8, -4.8068657410725666e-8] km/s
+ time of flight: 1.8749577783681145e8 seconds
+ arrival date: 2029-04-12T06:24:41.339
+ thrust profile: [0.09086584866118837 -0.02660491794926544 -0.038084300107123055; 0.04389978538100278 0.007982238893439351 -0.05660751294765649; 0.05439430921119514 0.01937541590590304 -0.11657142412829423; 0.061493374757444506 0.028724385728459544 -0.18157991851926203; 0.03635755449278362 0.019284049905404024 -0.1373305586198861; 0.027898583661120403 0.016252369832954316 -0.12767272633955656; 0.018282243582569503 0.011438350731183228 -0.0976519454608688; 0.010882367685072468 0.007141631785440254 -0.0640671903365745; 0.0024197104968484763 0.0019081187983414631 -0.016395569316845153; 0.0005921719989569322 0.000342280532099847 -0.003884558477094388; 0.0005377269661648718 0.00029894677015915614 -0.004113776354936628; 0.0011772627857556625 -0.00037158680171586137 -0.001358865363674329; 0.0012139818928389818 0.0006298997240451785 -0.0010551038087068774; 0.000618393520358878 -0.001093623420156228 0.0019604132267300707; -0.0007911966595091901 -0.0008977137949651635 0.0035202816549667103; -0.0005346882176674163 0.0017592027090404991 -0.0019707566791207576; 0.0006887855371854015 -0.002823857598345977 -0.0032422251218477078; -0.0014146823641001706 -0.003932904222217889 0.005908479737107432; -0.000802970062052712 0.0015176844818301305 0.0024634623378927845; 0.00045757439891219774 0.00027547876315482526 -0.00047423107113199166] %
+
+Mass Used: 73.98027880672316 kg
+Launch C3: 99.90791296190639 km²/s²
+||V∞_in||: 4.016593486014837e-7 km/s
diff --git a/archive/ES_0.5629552350542787 b/archive/ES_0.5629552350542787
new file mode 100644
index 0000000..c2582a3
--- /dev/null
+++ b/archive/ES_0.5629552350542787
@@ -0,0 +1,22 @@
+archive/ES_0.5629552350542787---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T07:37:14.202
+Launch V∞: [6.608495631145146, -7.277928064147864, 0.20012975027333563] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.36322686496415e-7, 0.0002679670071332751, -0.00017658968058228148] km/s
+ V∞_out: [-0.00016618922958522268, -0.000268551470016271, 5.625407815093571e-5] km/s
+ time of flight: 1.87495777874837e8 seconds
+ arrival date: 2029-04-07T09:46:51.202
+ thrust profile: [0.2918821391221113 -0.06518916101451747 -0.09219736074177895; 0.07270218623515146 0.024466155826542237 -0.07204854886447064; 0.08589692938044756 0.05430954718969044 -0.14000042867021043; 0.06715431581415054 0.05690634540157544 -0.15175198210060478; 0.04380413929537253 0.04650891602472333 -0.13248247218417075; 0.024165634851707855 0.029866663202009872 -0.0919254261910592; 0.013678079154231084 0.018479496779867658 -0.06141622224938129; 0.016126369267890506 0.02809804626267217 -0.09467292815168825; 0.005740627003092273 0.00995142659229449 -0.03556449805398749; 0.0012584414480437361 0.0021051537647312837 -0.008195457139350966; 0.00015570421190443947 0.00021718725156226254 -0.0006681236730713847; 8.423544514372098e-5 6.226591075304171e-7 -0.0015636038303694336; 0.0006227524113418405 0.0009259276030915593 -0.0011731959307979105; 0.002169955445730856 0.0009756063764987345 -0.0021661620888147612; -0.00031016657345484596 0.00015033778635203628 0.002422245512767323; -0.0002842510976329616 -0.0005701198970705951 0.002897200999123372; 0.0029191423616524133 0.0002259518678206364 0.0012401286288742047; -0.0001800871368922965 0.0012458591542139378 -0.0007279676580651208; 0.00035512428383136586 -0.00010951875830152711 0.00017295027345851045; -0.000546532323952755 -7.141170573395908e-6 -0.0003420881850545658] %
+
+Mass Used: 92.81150480079168 kg
+Launch C3: 96.68050333072003 km²/s²
+||V∞_in||: 0.00032092200241764797 km/s
diff --git a/archive/ES_0.5629610730739878 b/archive/ES_0.5629610730739878
new file mode 100644
index 0000000..7ef3ce7
--- /dev/null
+++ b/archive/ES_0.5629610730739878
@@ -0,0 +1,22 @@
+archive/ES_0.5629610730739878---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T12:08:52.560
+Launch V∞: [6.630219444136853, -7.44819177427371, 0.07362389590751606] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.593132937894924e-9, 1.284218553911384e-9, -8.100198032005982e-9] km/s
+ V∞_out: [-2.42389629951714e-9, 5.847391718586059e-9, 7.67811313095963e-9] km/s
+ time of flight: 1.8483562343631986e8 seconds
+ arrival date: 2029-03-09T19:22:35.560
+ thrust profile: [0.10158463087380963 -0.029226124006595373 -0.04090862886084626; 0.055868345610171934 0.01194859772944431 -0.06610492904303993; 0.05266533190419289 0.023261772122636897 -0.10505299135677588; 0.04830336240053231 0.02897881098014383 -0.13520542414765627; 0.03789736142760491 0.026970340647575607 -0.13509034626389135; 0.029001639265465184 0.023301000412863947 -0.12468732936675965; 0.020785090588919294 0.01814234011095135 -0.1044559591412511; 0.013102449515007681 0.012159354084538209 -0.07473147497332976; 0.006065574140398273 0.005917988495518088 -0.03854611536598946; 0.006187763273089658 0.006210319809882766 -0.04224388281605275; 0.0011053887265297707 0.0007779811017218166 -0.005670330682746201; -0.0010573065378240054 -0.0006488702137266054 -0.0037184735229537666; 0.00037193954229597836 0.0007746261854869144 -0.004497054702859641; -0.0005717026044162849 -0.0009509058469093458 -0.0013630625082060518; 0.00010744298718005224 0.00040053145718631266 -0.0018951661851685426; -0.000324601140486917 -0.00019776783970611406 0.00021936429501736568; 0.0007165883075502036 -0.0006404146621402471 0.001290912262265808; 0.0009764658613735705 -0.0002663103479513025 -0.0036484971100872766; -0.004640856762621945 0.0013884840487108996 -0.0020794952630571626; -0.0022819240558983912 0.004187845300186918 -0.0032175833397077897] %
+
+Mass Used: 76.71663739238329 kg
+Launch C3: 99.44079106181756 km²/s²
+||V∞_in||: 9.927011711128829e-9 km/s
diff --git a/archive/ES_0.562961082456004 b/archive/ES_0.562961082456004
new file mode 100644
index 0000000..fa7a85e
--- /dev/null
+++ b/archive/ES_0.562961082456004
@@ -0,0 +1,22 @@
+archive/ES_0.562961082456004---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T18:07:19.023
+Launch V∞: [6.166380893544428, -7.525943529823456, 0.0616778519949566] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006837352254674809, 0.0008281989602324132, 0.0007200560521923254] km/s
+ V∞_out: [-0.0008266017712326921, -0.00045563829842690083, 0.0008833552287034104] km/s
+ time of flight: 1.789279162425152e8 seconds
+ arrival date: 2028-12-28T16:19:15.023
+ thrust profile: [0.45773765778956893 -0.1482952350066864 -0.15997429458661103; 0.041480463802682346 0.008650011541432471 -0.04383697137948553; 0.10975852312355698 0.048118025213215225 -0.18480076114718982; 0.06827321162562154 0.04098692695541981 -0.1597454663684932; 0.05065677656125025 0.037076388677775136 -0.1519320248731343; 0.021183833258506368 0.018025538202439607 -0.07803616638386977; 0.023329809009817997 0.021930707835689418 -0.09973932204248274; 0.014290420615758649 0.014634571426026253 -0.07020478603618707; 0.00408080993010916 0.004646221475446296 -0.022966843181788963; 0.006873308362741061 0.008037842053486488 -0.036684116095080495; 0.0002405767005243243 0.0006096895692477906 -0.001866831114681114; 0.0011603436051654467 0.0009701458729233945 -0.007009113888403007; 2.602941443149214e-6 2.0077158756476136e-5 -0.00017799153065351861; -0.0001883243667625403 0.000258528822986154 0.0003673609757612105; 2.5375360144534753e-5 0.00010156840546905334 0.0003109795979146316; -0.00010543354380254379 9.116044709108131e-5 0.00029441689526239854; -0.0002998863786339745 -1.7108650428886477e-5 0.00033676062453472257; -0.0004022084535815121 0.00032040576407436363 0.0003207686615978561; 0.0006946783748860322 0.0005774727711012204 -0.0008838551095800999; -0.0007460870803028905 -3.7384076591340644e-5 0.0005030585227207863] %
+
+Mass Used: 104.55860913990773 kg
+Launch C3: 94.66788349578803 km²/s²
+||V∞_in||: 0.0012930151176896248 km/s
diff --git a/archive/ES_0.5629660880627777 b/archive/ES_0.5629660880627777
new file mode 100644
index 0000000..c955304
--- /dev/null
+++ b/archive/ES_0.5629660880627777
@@ -0,0 +1,22 @@
+archive/ES_0.5629660880627777---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T22:38:15.928
+Launch V∞: [6.506268356737844, -7.565059091807201, -0.031182876024331094] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012773277769634123, -0.00035591092256944166, 0.00897581924612454] km/s
+ V∞_out: [-0.015041803124011335, 0.0001432758290515128, 0.004188692357808605] km/s
+ time of flight: 1.8568220545820457e8 seconds
+ arrival date: 2029-03-21T01:01:40.928
+ thrust profile: [0.10051407537799785 -0.024035715269606572 -0.03824783703779798; 0.04282066778172882 0.011700353156600854 -0.04720948130625767; 0.052059921645881434 0.028658196587636707 -0.09566548188098743; 0.03204429160436005 0.023602022266838454 -0.08466980781819125; 0.03757217281569341 0.03268304453900067 -0.12347794981861256; 0.02720274812185457 0.026796236480690332 -0.10125342735315859; 0.0331477775167375 0.03467486561588758 -0.14156598900963235; 0.024650211740205655 0.02993123585262709 -0.1268035895077981; 0.00896159685921584 0.012407119714873542 -0.05710291428466869; 0.0021087286229188023 0.003179451144124972 -0.01557353461406365; 0.00037779571742631334 0.0007039635789010311 -0.003370905602933389; 0.00498312512336695 0.00805709753933532 -0.04231088015518839; 0.00015824408476105165 3.22480316526213e-6 -0.00013229761143941044; 8.839271642280017e-5 0.00010985196237532974 -0.00021301764682538923; 0.00015947364304880513 -0.00012768185858099768 1.6683334577841563e-5; -7.902130022515856e-5 0.00012427528996659463 -2.3489847683083685e-5; -9.104980763844755e-5 -0.00012641955620704574 -3.2962467467237446e-5; 3.194617468948428e-5 -0.0001530113342663748 -3.508299645934135e-5; -2.6759314288825927e-5 1.3748404294586298e-5 -2.8141040274752663e-5; 7.838395215076861e-5 7.509963975638275e-5 0.000286464616625001] %
+
+Mass Used: 76.01182311552338 kg
+Launch C3: 99.56261936418011 km²/s²
+||V∞_in||: 0.015615653323000394 km/s
diff --git a/archive/ES_0.5629699336834778 b/archive/ES_0.5629699336834778
new file mode 100644
index 0000000..3375b3c
--- /dev/null
+++ b/archive/ES_0.5629699336834778
@@ -0,0 +1,22 @@
+archive/ES_0.5629699336834778---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T10:37:58.398
+Launch V∞: [7.833128630205404, -5.600021355530694, 0.2031285298439677] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8307997364367636e-6, 1.5690475512335009e-6, -1.1847526628509775e-6] km/s
+ V∞_out: [3.517368169202993e-7, 2.6594329358408217e-6, -1.2399142701866943e-7] km/s
+ time of flight: 1.8530596213016438e8 seconds
+ arrival date: 2030-03-25T04:30:40.398
+ thrust profile: [0.635361525631605 -0.002564355735813012 -0.1458217881543325; 0.09578219584304053 0.05934007382724478 -0.09278148231218128; 0.0566855915490099 0.060054600312552296 -0.10115058035164187; 0.03582243894499629 0.04783674717137098 -0.0915440938012398; 0.03973963190624443 0.0689988956356222 -0.14133014322294254; 0.016747659169285587 0.03793164585454499 -0.08207335076350389; 0.01593316068184302 0.04044844332416133 -0.09680645405669133; 0.0018486709313224412 0.010909178792295528 -0.03253059209578526; 0.002979898214250699 0.010954337033318126 -0.027140524263287967; 0.0005343465890430433 0.007312786752396053 -0.0074898579874240765; 0.0015625465251456081 0.0035868171988226176 -0.007624933151657527; 0.003634125429762141 -0.0010809904461431012 -0.003506730364856681; 0.0035390516400073437 0.005592712963662539 -0.005565616822858944; 0.0019121354791894337 -0.0021569463940358663 -0.0051272112080029296; -0.0033800097653181108 0.0037914565401947816 -0.010012885930369822; -0.015251911695284379 0.0043300423942942215 -0.0023078577450335383; -0.006138365206466568 0.004286409693784101 -0.0011536384241145779; -0.0016564321245489877 0.0009484603805619109 -0.0015193170289273406; -0.0016691385347483425 -0.007153883871977056 -0.0010694018082219202; 0.002933890733142097 0.022066184997148828 -0.004914144709856002] %
+
+Mass Used: 115.70172960100763 kg
+Launch C3: 92.75940451937997 km²/s²
+||V∞_in||: 2.6865175906926892e-6 km/s
diff --git a/archive/ES_0.5629924629565605 b/archive/ES_0.5629924629565605
new file mode 100644
index 0000000..78c796a
--- /dev/null
+++ b/archive/ES_0.5629924629565605
@@ -0,0 +1,22 @@
+archive/ES_0.5629924629565605---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T22:59:26.474
+Launch V∞: [6.399267405494815, -7.333065226516113, 0.1150548476961402] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01687473103757501, 0.0004959600458222379, -0.012119431545551425] km/s
+ V∞_out: [0.01996445000067212, -0.0002060099967662224, -0.00532569522258306] km/s
+ time of flight: 1.8749577795682466e8 seconds
+ arrival date: 2029-04-08T01:09:03.474
+ thrust profile: [0.4025183731294069 -0.09283321062353093 -0.12885374269517388; 0.12029581599901837 0.037024268719660004 -0.11866926269100792; 0.12234505590781794 0.07252791934023405 -0.20076141935354772; 0.04270499055309215 0.033643405700788324 -0.10121992503551082; 0.02798288196909353 0.02698951920480405 -0.0853095140632673; 0.0403097344726417 0.045377706605137264 -0.1502107052869363; 0.016014361411459357 0.020063388419958344 -0.07145359922696902; 0.005860285185698854 0.008334447378655845 -0.029771551164420495; 0.002022115359569571 0.0008815396655069364 -0.008816529895018268; 0.00307368503307874 0.0031713503850007273 -0.0064782821877686384; 0.0006266374998882997 0.003049739942837036 -0.007403018193980539; 0.0009383642764361037 0.0008155206661172741 -0.0026643753668323293; 0.0027503947344701815 0.001928442226263868 -0.00727230173731991; 0.0023286788750737984 -0.0006384500813681917 -0.0017410725363359025; 0.0006707924787050007 0.0018515086808949524 -0.0026094828247708304; 0.0022963446179322415 0.004054144887231821 -0.004052232846339372; 0.0007977408121037912 -0.0006210809167150914 -0.0005085037671180397; -0.0017993288592039343 -0.00023736082930092637 -0.004229641353920231; 0.000904821406389234 -0.003218021411790381 -0.006733507924187114; 0.0030396384894455708 0.002478752580957646 0.0013458855817750977] %
+
+Mass Used: 104.1879185081325 kg
+Launch C3: 94.73770656134653 km²/s²
+||V∞_in||: 0.020781798404971026 km/s
diff --git a/archive/ES_0.5629977755859416 b/archive/ES_0.5629977755859416
new file mode 100644
index 0000000..6b4406d
--- /dev/null
+++ b/archive/ES_0.5629977755859416
@@ -0,0 +1,22 @@
+archive/ES_0.5629977755859416---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T01:37:38.578
+Launch V∞: [7.8335872642087585, -5.6051593288283685, 0.2982466584135096] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.873497296532172e-8, 7.428322476891996e-7, -1.432666802037673e-5] km/s
+ V∞_out: [-6.900242338018537e-7, 1.432262264158787e-5, -1.5779501917439964e-7] km/s
+ time of flight: 1.8749577785211337e8 seconds
+ arrival date: 2030-04-19T03:47:15.578
+ thrust profile: [0.5196843355701092 0.02683341087936555 -0.11043960452175546; 0.21551581343385393 0.15629107914064158 -0.171435165231942; 0.059025489373409595 0.06970040375069189 -0.10094165089369146; 0.031835202649340665 0.05714290091036871 -0.07490374740372266; 0.026990889206113526 0.07161723431610355 -0.10857905368413918; 0.013534909416927511 0.05361052085297381 -0.08461948731555098; 0.013330028836058163 0.05104868397387476 -0.09154717730085485; 0.003226021740879367 0.0164387318387558 -0.03372587515836847; 0.0005947370775786884 0.005124893442926227 -0.01182527534689727; 0.0005823921302120134 0.004068821373445073 -0.01006826409499207; 0.0004154454841019111 0.004671705098070997 -0.010918852903886535; -0.0025616921891765754 -0.00195579285201263 0.0006833162932443231; -0.00025026720285112433 0.0016362138836823724 -0.0023133213034683704; -0.003140649652428941 0.002408612326755202 0.00022668371011216404; -0.0010372589336057041 -0.0018751645807531462 0.0025842044316597324; -0.0015091723802981602 -0.00036754875576348466 -0.002719165026148868; 0.00013004403367579035 0.0007564737853351443 -0.005063144004535063; -0.0026831514750046926 0.0015459293471301008 -0.008019238502728893; 0.0021123830542400146 0.004449654426536678 0.006232928107323931; -0.005158622073818061 -0.0023971990245016278 -0.002026094715605262] %
+
+Mass Used: 115.07827053571418 kg
+Launch C3: 92.87185159678017 km²/s²
+||V∞_in||: 1.43461289381582e-5 km/s
diff --git a/archive/ES_0.5630015779388317 b/archive/ES_0.5630015779388317
new file mode 100644
index 0000000..8093a31
--- /dev/null
+++ b/archive/ES_0.5630015779388317
@@ -0,0 +1,22 @@
+archive/ES_0.5630015779388317---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T03:13:14.950
+Launch V∞: [7.656002270286995, -5.698021576003701, 0.47798775157399476] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.602382760273638e-7, -2.099215343625588e-6, -6.040852698432591e-6] km/s
+ V∞_out: [-5.858807437906627e-6, -6.566823427041859e-7, 2.547261968332326e-6] km/s
+ time of flight: 1.84037941966225e8 seconds
+ arrival date: 2030-03-08T04:52:15.950
+ thrust profile: [0.5919623084155815 0.004429971568297969 -0.11809292783634341; 0.3123184664460003 0.20498018738359383 -0.21520704270713892; 0.06757944422267684 0.07711639712526813 -0.09860266304997072; 0.05731996803428009 0.09059172128193607 -0.1267138710760927; 0.04415421124026229 0.09097844062017325 -0.1359454831644557; 0.011611464969049428 0.030546693967768337 -0.05156338959171289; 0.005725260124292214 0.018332091209801393 -0.033552409950986455; 0.002314773061528126 0.008999869570366347 -0.017723953642186496; 0.004334708247758155 0.02063858902085853 -0.04020666318212626; 0.0007384485852529589 0.003504782078872773 -0.00761523931293315; 0.0003927809773925565 0.003003140882816121 -0.006697528976840447; 4.9124077317369805e-5 2.786244420111114e-6 -0.00013829808445317088; -1.167395688072e-5 4.238864955946099e-5 -0.00010645602021047744; -2.370284906339581e-5 0.00010909200216345169 -0.00015848334617547924; -2.928943943089785e-5 2.6867201527567067e-5 -0.00016108406157872593; -5.765733817916304e-5 -0.00016042094140092747 -3.1036231549279065e-5; 5.567601196958537e-5 8.689093987029776e-5 -1.612296611986898e-5; -0.00016615042097876034 -0.00015479007471122402 3.2940245252236034e-5; 4.292935907012431e-6 -6.088681994569122e-5 0.0001253288070524198; 3.7165635631059195e-5 -9.790237608518663e-5 -3.469999036492959e-5] %
+
+Mass Used: 124.19179881423133 kg
+Launch C3: 91.3102929338981 km²/s²
+||V∞_in||: 6.429192870353556e-6 km/s
diff --git a/archive/ES_0.5630068124978782 b/archive/ES_0.5630068124978782
new file mode 100644
index 0000000..6815d95
--- /dev/null
+++ b/archive/ES_0.5630068124978782
@@ -0,0 +1,22 @@
+archive/ES_0.5630068124978782---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T19:14:41.824
+Launch V∞: [6.557623878061614, -7.444627330388102, 0.043970915418476975] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0920695419615887e-9, -1.7690529469107783e-9, 1.8020077506968328e-9] km/s
+ V∞_out: [1.4039428788074018e-9, -2.193454542082814e-9, -3.040066720018235e-9] km/s
+ time of flight: 1.874957778748862e8 seconds
+ arrival date: 2029-04-10T21:24:18.824
+ thrust profile: [0.18160765542800245 -0.04751288588198327 -0.06960694207694143; 0.08187357288256124 0.019934453290239414 -0.09613992045557129; 0.03802571393869049 0.018152040333877257 -0.07724765227311925; 0.042604958116851145 0.02699071565850012 -0.11990276582433443; 0.0487798773891207 0.0374018533506587 -0.16946651110713737; 0.01915184341236328 0.016214487218515337 -0.08434793152740212; 0.013705819830061304 0.01254981955254417 -0.07199260017213396; 0.012964141585304984 0.013438720293731752 -0.07888022751400758; 0.004252697061627942 0.0044787801314192435 -0.029951747169612807; 0.0054736529880907905 0.005858778079196264 -0.04001868557752426; 0.00039013108961824733 0.0009699378946960927 -0.005676823456654193; 0.0043316794425376694 0.0048381387335741065 -0.03119138561070828; -0.0006944989413828849 0.00265879664901811 -0.017048118773054767; -0.0006029292576585734 0.0004042880795391921 0.0018596673507037234; 0.0002694770070563026 -0.0016343945119479289 0.0011111443379096977; -0.0012258562030179293 0.0025804577941204747 -0.000988868260338303; 0.00015041255170033586 0.0004897166104723042 -0.001986640766270544; -0.00023402339480327745 0.0007344559533871839 -0.001024526583544674; -0.0004081818570616162 0.0007404577762399251 0.00023950779811990949; -0.0001390493899975718 9.21500833774511e-5 1.7624834502720377e-5] %
+
+Mass Used: 82.68471192151083 kg
+Launch C3: 98.42684045588807 km²/s²
+||V∞_in||: 3.2792583355003523e-9 km/s
diff --git a/archive/ES_0.5630156359548188 b/archive/ES_0.5630156359548188
new file mode 100644
index 0000000..142637f
--- /dev/null
+++ b/archive/ES_0.5630156359548188
@@ -0,0 +1,22 @@
+archive/ES_0.5630156359548188---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T09:26:41.791
+Launch V∞: [7.557476940986646, -5.630370090423215, 0.09118895022703455] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.795587296624201e-7, -6.375133442696278e-6, 0.00011257945135694567] km/s
+ V∞_out: [4.248983695549448e-6, -0.00011266079484604866, 1.2426660153162686e-6] km/s
+ time of flight: 1.8749577787366056e8 seconds
+ arrival date: 2030-04-19T11:36:18.791
+ thrust profile: [0.8589877052298521 0.01745805619701747 -0.2070945522079643; 0.23136417285166472 0.15274742324479823 -0.20681940169923088; 0.06465521112025281 0.0701301761350444 -0.11242744916825557; 0.036166207482135254 0.05347528825322561 -0.09689286424499291; 0.026183986515989303 0.05000723626099551 -0.09859716663958085; 0.008539568228160611 0.01932689972471216 -0.04152127745444737; 0.0038380550129401042 0.00957743465825409 -0.023589914635574912; 0.0049135317534556 0.01679553954113177 -0.0426479702061347; 0.00433940006121766 0.01639878209247046 -0.04319226019991761; 0.0002745336433850154 0.0016589281021560302 0.0008861591655339859; -0.00029005820072027216 0.004730746968631943 -0.010947650780529363; -0.006360950600578636 0.003574934266316245 -0.007550351381929526; -0.004333203018044284 -0.0023074529887569632 -0.006422855306834814; 0.0034670759938870855 0.001197164900266148 -0.0025155092569559756; 0.003570720446111274 0.006613655504004811 -0.009344229907260389; -0.0011115755346983273 -0.006971603704932173 -0.0056941158186406; -0.0023174384744677114 0.002198281972976371 0.0001719759501457108; 0.0006510390290088265 0.006022096405880244 -0.002262913327481299; -0.00045063626182231136 -0.001277769585449189 -0.004090877151364668; -0.007071311157278484 -0.007941748379950677 0.009097755207471567] %
+
+Mass Used: 138.70667240291777 kg
+Launch C3: 88.8248404933207 km²/s²
+||V∞_in||: 0.00011276250665028724 km/s
diff --git a/archive/ES_0.5630162196275494 b/archive/ES_0.5630162196275494
new file mode 100644
index 0000000..7d605af
--- /dev/null
+++ b/archive/ES_0.5630162196275494
@@ -0,0 +1,22 @@
+archive/ES_0.5630162196275494---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T13:19:09.898
+Launch V∞: [6.226101590196942, -7.275610023407713, 0.3237762916695758] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.302633894381066e-5, -2.252123431762445e-6, 4.002129812089853e-8] km/s
+ V∞_out: [2.4615522972785188e-6, -5.4805400765225084e-8, -1.2988094213343373e-5] km/s
+ time of flight: 1.8461640468338692e8 seconds
+ arrival date: 2029-03-03T07:39:13.898
+ thrust profile: [0.6684700520518386 -0.17236848316048922 -0.1996788850960936; 0.11287684192518219 0.03232337091444769 -0.10643826553316413; 0.10135523464653501 0.05725051845167967 -0.1595081470638902; 0.0775790179322803 0.0597191469828939 -0.17131624909923934; 0.03924801976643635 0.03685694975582188 -0.11275899201679526; 0.02763766933717032 0.03019711719306721 -0.09751715693169255; 0.02243954414689769 0.027755967477769067 -0.09372279524794722; 0.0012335814660716419 0.0017847317115368883 -0.005857497712362421; 0.0018193354065559214 0.003439442380389867 -0.012504681448911356; 0.0004968118464808397 0.0007372760931813101 -0.002840392559919936; 0.0004522683386291612 0.001026399194396915 -0.0037927523847598637; 0.0013633111044900107 0.0028174760328913253 -0.011246771686726704; 0.0001327488661935939 0.0013090759591107748 -0.0005848173876222564; 0.00029320471792051246 0.0006517639255314155 -0.0006419320864389006; -5.7598935039056626e-5 -0.0004904498479082114 0.00010615911665892572; -0.0007708910690642146 -0.00139965461636643 -0.0003081965154135168; -0.0009949811148558996 -0.0005127218470729197 -0.002023591058537497; -0.00014831841247043762 -0.0001741673648901856 -0.0002267890989819223; -8.013356970892554e-5 0.0008523849289916853 -0.00033545523982402166; -0.0013298077260341567 0.0005469416218746739 0.0005619458476755087] %
+
+Mass Used: 121.3308285834105 kg
+Launch C3: 91.80367331121096 km²/s²
+||V∞_in||: 1.3219650825011791e-5 km/s
diff --git a/archive/ES_0.5630230865478905 b/archive/ES_0.5630230865478905
new file mode 100644
index 0000000..de6b8c4
--- /dev/null
+++ b/archive/ES_0.5630230865478905
@@ -0,0 +1,22 @@
+archive/ES_0.5630230865478905---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T04:37:35.365
+Launch V∞: [6.439097929193311, -7.501814047602061, 0.13825833044252728] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.02047141050412828, -0.009224859965420374, 0.03099978875218604] km/s
+ V∞_out: [-0.02377545851077089, -0.010194466128193582, -0.028211417034373056] km/s
+ time of flight: 1.83365601549131e8 seconds
+ arrival date: 2029-02-19T11:30:56.365
+ thrust profile: [0.1928481970838944 -0.04786165233670605 -0.06461021939333443; 0.08377720958545837 0.02583114450666227 -0.08723557201433112; 0.06435701682322896 0.03874374915681546 -0.11146907335130073; 0.051051871865362655 0.04204701666475233 -0.12168252160236533; 0.039166705930769576 0.03916904586509723 -0.11979892403518551; 0.037325600404318635 0.04249795560813455 -0.13865664730960311; 0.018908837524100015 0.023600368068855425 -0.08307445279683333; 0.014611511562861702 0.020483671245907192 -0.07457580202512845; 0.016758640473347783 0.02583923719173993 -0.09558805071404788; 0.0024605103739529103 0.005154300620641182 -0.020773794113111248; -1.1882926261476325e-5 4.042001232200051e-5 -0.00012814308198064888; -2.458454946508386e-5 -6.069276348468226e-5 6.591719651907572e-5; 0.00033093931443044206 0.0007462950231383572 -3.6576037186687076e-5; 1.749400716838297e-5 -0.0010573478507180352 0.001358791011313676; 7.910382437675001e-5 8.896142251063241e-5 -0.00014412421470305658; -0.0019031547376720216 -0.0005678081074935635 0.0022854553862133283; -0.000613458395255929 0.00021500016762223892 0.0009205139111118058; 4.704188794633789e-5 -0.0004027149791486081 0.0008113102162114686; -0.0003285761222252916 0.00012136838234079898 0.000203221639932239; 0.00014463830444038219 -0.0002648981753737589 -0.0013099561081643457] %
+
+Mass Used: 86.60345048308409 kg
+Launch C3: 97.75831151247797 km²/s²
+||V∞_in||: 0.038277455402499126 km/s
diff --git a/archive/ES_0.5630249867655879 b/archive/ES_0.5630249867655879
new file mode 100644
index 0000000..9f9e695
--- /dev/null
+++ b/archive/ES_0.5630249867655879
@@ -0,0 +1,22 @@
+archive/ES_0.5630249867655879---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:35:24.970
+Launch V∞: [6.565237259043569, -7.408964310695651, 0.08350767343788693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0357012208639798e-9, 2.459233425521363e-9, 1.538290733411224e-8] km/s
+ V∞_out: [-7.976709504565365e-9, -1.1563530659635682e-8, -5.947070411169235e-9] km/s
+ time of flight: 1.851378411800159e8 seconds
+ arrival date: 2029-03-12T21:46:05.970
+ thrust profile: [0.21452591208226432 -0.060495266844422975 -0.0834862190605835; 0.06660826575467607 0.014472275754464057 -0.07905488116070933; 0.04202478018838593 0.01845138542782467 -0.0840761893568389; 0.060777528419962715 0.03664296319123209 -0.16771309379566243; 0.041931634534851284 0.030056678079204886 -0.14903915521254638; 0.02715582203099804 0.02176997721599654 -0.11711124356062429; 0.011272229049083031 0.009728828187040996 -0.057902345619024166; 0.016395671564173073 0.0154939237195241 -0.09445666509866815; 0.0062140267418438885 0.0061459673804061705 -0.041036511052638766; 0.0009925354417274308 0.0005832340046623668 -0.00625734176901959; 0.00216658155909007 0.002339114747660149 -0.017111238435923784; 0.0007822077824256633 0.000998552054049126 -0.007188001894156731; -0.0003378007788289153 -0.001206964629897156 -0.0011455086710832878; -0.0010490160100855733 -0.0002225986027008081 -0.001810027254882717; -1.146218540257767e-5 3.952297829857109e-5 -0.0017420908310821846; -0.002866597884975896 0.0023445160279562016 0.001971629871142305; -0.004577117502319421 0.0015195478131398302 0.0011198464637543295; -0.00020995632702101077 -0.00045370364811260126 0.0002731675716018078; -0.0004662846959856369 -0.0009340721932089789 0.004458174014057566; 0.004851113607745145 -0.0005740941953941354 -0.002640951158674807] %
+
+Mass Used: 85.18376648190952 kg
+Launch C3: 98.0020659562188 km²/s²
+||V∞_in||: 1.571068892670569e-8 km/s
diff --git a/archive/ES_0.5630307139585418 b/archive/ES_0.5630307139585418
new file mode 100644
index 0000000..db44c35
--- /dev/null
+++ b/archive/ES_0.5630307139585418
@@ -0,0 +1,22 @@
+archive/ES_0.5630307139585418---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T05:18:53.911
+Launch V∞: [6.577206511371051, -7.395410929886302, 0.15728495560052747] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.347049508002485e-9, 5.083832564308327e-12, -5.8926643329992e-9] km/s
+ V∞_out: [-2.145443215008457e-9, 4.60805572503537e-9, 7.000770366037043e-9] km/s
+ time of flight: 1.858214205202385e8 seconds
+ arrival date: 2029-03-20T22:22:33.911
+ thrust profile: [0.24189275807776375 -0.05951727501762905 -0.08735531106667413; 0.040992553690177944 0.010417699588766864 -0.04386516968835289; 0.029701133969143437 0.014143153855219146 -0.05688559013012349; 0.04335727120284386 0.02786740477069721 -0.11457182808170469; 0.017618453350312677 0.014720823477522803 -0.05725843139221958; 0.05015948901734493 0.042927637589110154 -0.17489064494530848; 0.01973572306220452 0.02067239213958381 -0.10692461768244108; 0.025198269313473756 0.025548918226637955 -0.11965561253519263; 0.020283126949672752 0.02340329283189124 -0.10870038955940237; 0.002116689876637074 0.0025045116061011476 -0.015175892478286003; 0.0009902109604802488 0.0005616966555571331 -0.005602445471019851; 0.0003292195400399374 0.0006331714203406046 -0.004185558783160679; 0.0006890076081818299 -0.00016508490409714022 -0.0005933909629435544; 0.0012091753679289463 0.0008321278612523463 0.00039484055312699324; 0.0001732963050765684 -0.00022552877524981393 0.0018362284581027425; -0.00012642369267642573 0.000411436450651308 0.001216762395584772; -0.00023115135283376505 -0.0003631055946785161 0.0029207886367570114; 0.0005546099119472371 -2.08123621595018e-5 -0.0006921561947585407; -0.0008660448147140625 0.0001173802401759031 0.001097868211318414; 0.0021789332435877677 0.00020727197964938793 -0.002759886079921365] %
+
+Mass Used: 85.33965952952167 kg
+Launch C3: 97.97648687236179 km²/s²
+||V∞_in||: 8.660748018721537e-9 km/s
diff --git a/archive/ES_0.563031888927629 b/archive/ES_0.563031888927629
new file mode 100644
index 0000000..14a9cf7
--- /dev/null
+++ b/archive/ES_0.563031888927629
@@ -0,0 +1,22 @@
+archive/ES_0.563031888927629---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T00:28:25.586
+Launch V∞: [6.497912590901998, -7.329051925083856, 0.04854899262551557] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.662217327594438e-8, 6.988248098249554e-7, -4.224331168360467e-8] km/s
+ V∞_out: [1.7984745337057436e-7, -4.791808073665118e-7, 2.5755503974603564e-7] km/s
+ time of flight: 1.8749577787532344e8 seconds
+ arrival date: 2029-04-08T02:38:02.586
+ thrust profile: [0.3482932141379723 -0.0789774385261974 -0.10513947331460663; 0.08200819077932915 0.02803846210066566 -0.07842811128651585; 0.06644563297560147 0.04239243901235557 -0.10606614869207398; 0.05060872637330987 0.04381549572343662 -0.11391158039354651; 0.028090276260319805 0.03008123946803681 -0.08318803797334623; 0.03341201040278472 0.04122593201796522 -0.11935615147345344; 0.027141410966833365 0.038095619221408646 -0.11387526432570033; 0.018733806030530636 0.030601149878887336 -0.09551554071529948; 0.00845678547980097 0.014664496231887996 -0.04954857477995305; 0.0014377904232982922 0.0025948635725212233 -0.009924673345132192; 0.0024607194700514926 0.0046399575531435025 -0.016516654904357466; 0.0004562067794391668 0.0011193821172469835 -0.006929336746275986; 0.00015183883398299145 -1.6398532669601286e-6 0.0003694259349142819; -0.0015294548091214747 -0.0009789502108428403 -0.0018793862889910874; 0.0009201835450300301 -0.0013089591878024645 -0.000968019922947699; -0.0007183523501389602 0.0009013098470475846 -0.0014365452621428448; 0.0010316131859395923 0.00021453063634826347 -0.0003044382422703238; 0.0009799328154178606 0.0023849225079606907 -0.0008929287698898809; 0.00044232211544326295 0.00035837361828279307 -0.00023179602874229136; -0.00044545328269653253 -0.0018287616171848967 -0.00030601484502672303] %
+
+Mass Used: 97.21921195736604 kg
+Launch C3: 95.94022716426305 km²/s²
+||V∞_in||: 7.067364831232713e-7 km/s
diff --git a/archive/ES_0.563032528879805 b/archive/ES_0.563032528879805
new file mode 100644
index 0000000..319feaa
--- /dev/null
+++ b/archive/ES_0.563032528879805
@@ -0,0 +1,22 @@
+archive/ES_0.563032528879805---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T10:17:41.099
+Launch V∞: [7.795249204210905, -6.289131136016516, -0.11514521126037802] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.649092014363753e-11, -3.146339177438607e-9, 8.632894503005513e-9] km/s
+ V∞_out: [2.2244100525975475e-9, -7.339199626399386e-9, 1.1367941262357347e-9] km/s
+ time of flight: 1.7292213055083957e8 seconds
+ arrival date: 2029-11-05T20:13:11.099
+ thrust profile: [0.08733341865014078 -0.012104090521769664 -0.0375109409880457; 0.022670191111712732 0.007408514833399055 -0.030798007949005238; 0.032267302719535894 0.01764720936427089 -0.07458344049976508; 0.03599502109643919 0.025008018231701627 -0.11612360059246937; 0.02420675435686065 0.018943890680235387 -0.10056335102576362; 0.017961438334008067 0.015300490133187353 -0.09061605812509153; 0.012366874981160196 0.010504591667722349 -0.07254195524402589; 0.014993681238183015 0.016410554766304136 -0.10515244352111842; 0.04296349123437669 0.040463255545103785 -0.24969195830661725; 0.0017622514672954138 0.0018467089373664497 -0.011191014318857955; 0.0042155586623984585 0.0041039638485856605 -0.043259223820446925; 7.382344971541919e-5 4.663699469667222e-5 -0.0004745596999185955; -3.345108153762267e-5 5.5178317457946126e-5 -0.00025062468339944903; 0.00033469282868428193 -8.880752175455871e-5 -0.0003673680727835512; 9.811956292545842e-5 -0.0003018456453336893 0.00027744136803851635; 6.956020700315868e-5 -5.125921581326841e-5 -0.00021266112935206758; -0.0010798896253462443 0.00014022928503962034 0.00022159643524912004; -3.898166756440646e-5 0.0003921186672365207 0.0001014065527721262; -6.31426970271321e-5 3.4629727939244415e-5 0.0005743541490598077; -0.00032573124966483937 -1.2250046232153488e-5 0.0014515937711795934] %
+
+Mass Used: 71.599306068043 kg
+Launch C3: 100.33233902143934 km²/s²
+||V∞_in||: 9.188451953771145e-9 km/s
diff --git a/archive/ES_0.5630344922364472 b/archive/ES_0.5630344922364472
new file mode 100644
index 0000000..7ba9414
--- /dev/null
+++ b/archive/ES_0.5630344922364472
@@ -0,0 +1,22 @@
+archive/ES_0.5630344922364472---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T04:54:43.444
+Launch V∞: [6.542500673254356, -7.375135688435655, 0.11097360010191284] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.219384081000686e-6, 1.0725723927791248e-6, -2.153903611652116e-8] km/s
+ V∞_out: [-1.4204317242572465e-6, 3.008823997189252e-8, 7.1593610072405964e-6] km/s
+ time of flight: 1.846182869636346e8 seconds
+ arrival date: 2029-03-05T23:46:09.444
+ thrust profile: [0.28743855712735367 -0.08157129577562225 -0.10407883219533842; 0.035539880671876384 0.008375955942077958 -0.04110926947053927; 0.05887768179446508 0.028053416578287263 -0.11119071562938006; 0.06720982882608516 0.04305711505828454 -0.17379097015165607; 0.044125069736447274 0.034057547205811584 -0.1476633846109435; 0.02369700858679123 0.020923292769599224 -0.0984582939383155; 0.015574656641342511 0.015276375217991885 -0.07655927499447328; 0.006264641840198678 0.006605113526702042 -0.035502874322729965; 0.004550643866587046 0.005162179514440258 -0.029299076876925435; 0.015128294410176362 0.018246199944017955 -0.10228935572155486; -0.00020113832476557157 -0.00029553900574096797 -0.0001596985843451027; -0.00077151302694723 0.00023091393497799435 -0.0003214563003548878; 0.0007943742114027781 -0.0005714860836585126 0.00014697222976686698; 0.0005726883999519353 0.0006667044264016184 -0.0022212397471806393; 0.00010304988559006272 -0.0008316679988758856 0.0003939291770772037; -0.000363150881369265 0.00014237696682330565 0.0006133953988392949; 0.0009512340965894309 0.0033277264840213617 0.0014613161783278586; -0.0017973985298889552 0.0004555292620725616 -0.00020239703412383304; -7.832722560107749e-5 -5.076224904506792e-7 -0.0011057649605035126; 0.004154020474405757 0.0001006657663348045 -0.0021212936356612274] %
+
+Mass Used: 89.8195773124935 kg
+Launch C3: 97.20925662229054 km²/s²
+||V∞_in||: 7.298656176093986e-6 km/s
diff --git a/archive/ES_0.5630386954889394 b/archive/ES_0.5630386954889394
new file mode 100644
index 0000000..6aea404
--- /dev/null
+++ b/archive/ES_0.5630386954889394
@@ -0,0 +1,22 @@
+archive/ES_0.5630386954889394---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:11:28.809
+Launch V∞: [6.500232724700241, -7.395313395981474, 0.199511313804635] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0399039392290008e-5, 1.6334187095274346e-6, 1.2370817483022961e-9] km/s
+ V∞_out: [-2.094010755377158e-6, 5.0216477557380635e-8, 1.0303797688055901e-5] km/s
+ time of flight: 1.8749577787473392e8 seconds
+ arrival date: 2029-04-10T12:21:05.809
+ thrust profile: [0.3165083211353569 -0.08845642569223303 -0.11903030328939805; 0.04976186255982653 0.010571442781769363 -0.05710818242402541; 0.043706057372160434 0.018549833031963194 -0.08458727685060038; 0.05222900262034041 0.02927225006833746 -0.1413311419013506; 0.04138108314983397 0.02735330058961902 -0.1429067910099878; 0.04005865275307787 0.02979621448570292 -0.1676318525354996; 0.017839834246242765 0.014429778369485786 -0.08713455700713976; 0.007315052794216699 0.006504494492471358 -0.04156852281235469; 0.0010160630854502452 -3.389886011779717e-5 -0.01709328300629686; 0.0011183482461770487 0.0020618366189701196 -0.012121363731939321; 0.0005709947033412154 0.0005233558475938567 -0.005451831903991694; 5.16476149830656e-5 0.0012719897498518575 -0.007460969438317179; -0.0004979337214442254 -0.002860532754933367 -0.0023096062782640603; -0.00041205909544455373 -0.00014164521636606084 -0.0011855897832203886; 0.00040565424624179917 0.0003359662354269989 -0.003030220997604806; 0.0022689211745583965 -0.0006184100069430968 0.00037188204204757617; 0.0008305039012278777 -3.642569241943752e-5 -0.005001493630325806; 0.00446272115012729 0.005064494973942322 7.832300940402242e-5; 0.004016392307752461 -0.0014976336478987478 -0.0026313664341255883; 0.006725632761672101 0.01349389663770502 -0.003382787742193063] %
+
+Mass Used: 91.14145036152831 kg
+Launch C3: 96.98349046438301 km²/s²
+||V∞_in||: 1.0526541620751084e-5 km/s
diff --git a/archive/ES_0.5630456060704545 b/archive/ES_0.5630456060704545
new file mode 100644
index 0000000..0539ffb
--- /dev/null
+++ b/archive/ES_0.5630456060704545
@@ -0,0 +1,22 @@
+archive/ES_0.5630456060704545---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T08:01:40.871
+Launch V∞: [6.5192269958354, -7.473720500095534, -0.059103340980841856] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.427910422309547e-7, -5.166184006582324e-6, 3.3016702752383753e-7] km/s
+ V∞_out: [-1.848367808155891e-6, 4.261493401197852e-6, -2.33828743035997e-6] km/s
+ time of flight: 1.874957778536817e8 seconds
+ arrival date: 2029-04-11T10:11:17.871
+ thrust profile: [0.21673808315660617 -0.05555259532064532 -0.08574818259317367; 0.04639290743706914 0.010996191266062258 -0.057659862876335934; 0.03307406203176063 0.01515428060824418 -0.06894445399721179; 0.05216600944426941 0.0339769514087647 -0.15095232804886535; 0.04301951094672876 0.03358601343671933 -0.15947920367031454; 0.01678713156882857 0.01360911948662602 -0.07589084239750145; 0.015390636244907956 0.014051459384677946 -0.0823022062001622; 0.01074600823464541 0.01061351706491741 -0.06533930833266716; 0.004642067288650248 0.004761707087194594 -0.03423167725321234; 0.010266171130950243 0.011857636076248073 -0.08115965422257487; 0.0018156111928093687 0.0019250106421703154 -0.014501230652323506; 0.0009489299539076647 0.0006402861841778092 -0.004436231421142011; 0.0004610518862540853 -0.00020337249434684634 -0.0006272160060243362; -0.0002385174838712833 0.0007175073656149265 -0.001975113678152399; 0.0038103413798012387 0.0019096113201176944 -0.004215871593756483; 0.003577899400845965 0.0024641308170598652 -0.004197534024640071; -0.00023550075745181246 -0.00014971894780147318 -0.0002948827992266946; 0.00026429624249942686 -0.000151006770935419 -0.0006363807921112618; 0.0010336097354092 0.0012218145869822292 -0.0029715164624233023; -0.0017178655846596662 0.0006631949208298472 0.0004814403488624165] %
+
+Mass Used: 83.11805408899136 kg
+Launch C3: 98.36031194169239 km²/s²
+||V∞_in||: 5.2297424399629346e-6 km/s
diff --git a/archive/ES_0.5630540916408143 b/archive/ES_0.5630540916408143
new file mode 100644
index 0000000..2d28989
--- /dev/null
+++ b/archive/ES_0.5630540916408143
@@ -0,0 +1,22 @@
+archive/ES_0.5630540916408143---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T21:06:13.673
+Launch V∞: [6.399575781809198, -7.4716516811947375, -0.10670106149083883] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.4950200434098695e-6, 3.348750458196076e-6, 3.6676636898138038e-6] km/s
+ V∞_out: [5.184735708825385e-6, 3.156466559793654e-6, 1.0202223949419701e-7] km/s
+ time of flight: 1.8749577801334444e8 seconds
+ arrival date: 2029-04-09T23:15:51.673
+ thrust profile: [0.26601888720659955 -0.05835289055118082 -0.08994605248605478; 0.06816066280712726 0.02219927154916227 -0.06972048007454879; 0.10395701886448257 0.06361702271161215 -0.16925100459064443; 0.06731049956155519 0.055734729154084915 -0.15843380635093743; 0.03940479708978955 0.04060683869362181 -0.12462443902072959; 0.02282095549742888 0.027091470421246527 -0.08988966409961816; 0.01402071294146213 0.01869930891200599 -0.06498190182097198; 0.007101488911261168 0.010537239743957441 -0.0384337075011749; 0.008011186208575582 0.013049745514141457 -0.049319361779798794; 0.0028764718093320166 0.005192511128285805 -0.020285561890765524; 0.0014845206350319556 0.002983742653136265 -0.011424729392456857; 0.001758499716562772 0.0006646227273311985 -0.0007759099095394303; 0.0018681618318879053 -0.0008587798941606005 -0.006276311872773636; -0.001369698933200339 -0.001115610975471304 -0.0009649831658024304; 0.00022347532474208684 0.0007241047226913743 -0.0028830689037712695; 0.0019711121166496055 -0.001312139639557966 -0.002582155178610143; -0.0007919091076455823 0.00031660339420152455 -0.0035715903801781333; -0.0008761453734982736 -0.00034708994502212183 0.00029627661897643743; -0.0008308506373580797 0.0011332212140573398 0.0022384188212672927; -0.003432031825392287 0.006225120585920275 0.0025526150110809043] %
+
+Mass Used: 92.27915771328708 kg
+Launch C3: 96.79153414874223 km²/s²
+||V∞_in||: 6.072977167475912e-6 km/s
diff --git a/archive/ES_0.563056944904476 b/archive/ES_0.563056944904476
new file mode 100644
index 0000000..fea24b0
--- /dev/null
+++ b/archive/ES_0.563056944904476
@@ -0,0 +1,22 @@
+archive/ES_0.563056944904476---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T12:41:16.343
+Launch V∞: [6.619336119277472, -7.307190332408997, 0.15799901361143276] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009218886544487348, 0.000981024628642757, 0.0009120775870333059] km/s
+ V∞_out: [-0.0008657884476385598, -0.0010591015307593438, 0.0008791949926460609] km/s
+ time of flight: 1.8749577787493268e8 seconds
+ arrival date: 2029-04-08T14:50:53.343
+ thrust profile: [0.26123230745080595 -0.06468719894401694 -0.08925029193581871; 0.07623625045114929 0.021523003139708306 -0.08333421924837936; 0.06163511396624147 0.03349422216299966 -0.11347005908502421; 0.05644085873352604 0.041452958802457474 -0.14550661308281337; 0.03885831977528654 0.03452114101886288 -0.12979293014014345; 0.0295331256182478 0.030256704283943624 -0.12109241993591152; 0.02276117787234489 0.026018451292066796 -0.10996809557290957; 0.00881372182007024 0.010715766240687588 -0.04889081584860885; 0.0035432718040033667 0.004510845230103186 -0.021784181262473033; 0.0007739313524302045 0.0018224972764178387 -0.009129397626704389; 0.0004911051088300426 0.0005033211852195711 -0.0020958004861215632; 0.00015441373431689006 0.0005092859789612271 -0.001946365152221026; 0.00028001601746225285 -0.0005355018359429674 0.00032413282496832085; -0.001693058970137652 -0.0011125581504107904 0.0012897348878355354; 0.0034804577922102073 -1.616820997309273e-6 0.0003390359835460247; -0.00015998469396585977 0.0003722444165027898 -0.001575855224857356; 0.0020304785072060303 0.00014593148276453486 -0.0023063270161849912; 8.870616215400595e-5 -0.0002434117748906772 -0.009151758793699597; 0.0001153239457566881 0.001657848299255335 -0.006060275006331793; 0.003090419072605233 -0.008694454625876124 -0.005923364380706498] %
+
+Mass Used: 89.69207379165937 kg
+Launch C3: 97.23560490232502 km²/s²
+||V∞_in||: 0.0016260914912677748 km/s
diff --git a/archive/ES_0.563057966222209 b/archive/ES_0.563057966222209
new file mode 100644
index 0000000..a261f46
--- /dev/null
+++ b/archive/ES_0.563057966222209
@@ -0,0 +1,22 @@
+archive/ES_0.563057966222209---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T12:21:11.372
+Launch V∞: [6.566988579417365, -7.36153159999505, 0.12002672247795326] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.717567710835324e-8, 1.7879101740552487e-7, 7.519566748135134e-8] km/s
+ V∞_out: [-6.728258865760983e-8, 1.0727529211634675e-7, -1.7174687677077537e-7] km/s
+ time of flight: 1.8749577787490672e8 seconds
+ arrival date: 2029-04-10T14:30:48.372
+ thrust profile: [0.27414617433326105 -0.09107469845898258 -0.095341120166128; 0.10968897338444422 0.01653064381937942 -0.13704117084090803; 0.026843533571711806 0.00927268788730798 -0.06061993523862893; 0.038350999566223155 0.015449838764360487 -0.11789934567870891; 0.0276576185564308 0.01314300361208635 -0.11035872982969329; 0.019785624024743056 0.010506058402530306 -0.09542989316845354; 0.015901121724215376 0.008699920160805775 -0.0877518933992151; 0.013977621781198974 0.00831026178265025 -0.08848548540723296; 0.007581748156636158 0.005148103652951849 -0.05447432747800614; 0.0025200260561192506 0.0016585988621267863 -0.019569929055214322; 0.003468229795067097 0.0022896326399952103 -0.027641725321184283; 0.0010051719935956183 -7.749641019039015e-5 -0.004061991106533309; 0.0003575045586568386 0.0002689836888282133 -0.0031635349400845046; 0.0022434022608512683 -9.870798491340969e-5 -0.004438101159440995; -0.0006446877717908276 0.0007611353146297554 -0.00041153515570640413; -0.00022075140609948796 -6.9589173125535e-5 -0.00027571146901332264; 0.00017592565611817374 0.00031107581677171066 -0.002218745102422909; -0.0009780560135782578 0.00218012235571432 -0.0022476967875120117; -0.0015122314389637384 0.000825517746695003 -0.001962149563911406; 0.004057492534665915 -0.0001774923869997737 0.001698075815274696] %
+
+Mass Used: 89.13158526072039 kg
+Launch C3: 97.3318929140326 km²/s²
+||V∞_in||: 2.1265045260278315e-7 km/s
diff --git a/archive/ES_0.5630610001722021 b/archive/ES_0.5630610001722021
new file mode 100644
index 0000000..42b772b
--- /dev/null
+++ b/archive/ES_0.5630610001722021
@@ -0,0 +1,22 @@
+archive/ES_0.5630610001722021---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T16:12:23.616
+Launch V∞: [7.965982408826417, -5.906868093055274, 0.017012445701581412] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0013174575169611887, 0.0009221245487874309, 0.05607409111082413] km/s
+ V∞_out: [-0.05234181245441945, -0.018317398022126268, 0.008443608182858721] km/s
+ time of flight: 1.8049969873255453e8 seconds
+ arrival date: 2030-01-31T19:00:41.616
+ thrust profile: [0.1855967951691016 -0.015997218053969472 -0.06514273149759547; 0.04767011655761449 0.020389994224326975 -0.05172342601682749; 0.050377058802383023 0.03435658099639018 -0.10112536284774644; 0.04854596045692629 0.041640020947420045 -0.14169741817962928; 0.052477429814103686 0.051729369093922735 -0.2023597389143394; 0.019590720983998906 0.019904779965548545 -0.08402569133341901; 0.01059738095151011 0.010810502761391675 -0.05418219157343517; 0.008574869596102798 0.00732134745550244 -0.04583193303843276; 0.011557592082354361 0.015041896745757602 -0.023446787868137225; 0.003268516350066376 0.016539062206529495 -0.02083353312302055; -0.003554864152737959 -0.006422313374153701 -0.021604656829729015; -0.002768577183003478 -0.0033451768297322253 -0.02797912217691101; -0.0015128601739167018 0.003588570939569485 -0.002649713856908169; -0.0007262932810511583 0.006163060343244851 0.009345936077315336; -0.0007220903233025008 0.009431129075136725 -0.005902566451302714; -0.0026120909847054145 0.001520734098107959 -0.0066947364613182386; 0.005742146290212633 -0.006215571175964463 -0.017299672399053338; -0.0002585826831740923 -0.00340301926289191 0.00017003191846779895; 0.003372873342324915 0.006690978491145336 -0.03913459168406766; -0.00046172530774810355 0.0009427565270433633 -0.0004757400850579768] %
+
+Mass Used: 83.20634119376427 kg
+Launch C3: 98.34825582979511 km²/s²
+||V∞_in||: 0.05609714522056786 km/s
diff --git a/archive/ES_0.5630610919211645 b/archive/ES_0.5630610919211645
new file mode 100644
index 0000000..719f9f7
--- /dev/null
+++ b/archive/ES_0.5630610919211645
@@ -0,0 +1,22 @@
+archive/ES_0.5630610919211645---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T07:07:48.790
+Launch V∞: [6.375242623406973, -7.288690976264575, 0.28343331795720217] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.8625402571734365e-6, 8.322123944759966e-7, -1.862879026762861e-8] km/s
+ V∞_out: [-1.3042060207159378e-6, 2.8508763935880335e-8, 6.78607807403097e-6] km/s
+ time of flight: 1.8503743994740665e8 seconds
+ arrival date: 2029-03-08T22:25:07.790
+ thrust profile: [0.5359127065593253 -0.13399692401114566 -0.16174803370246874; 0.0767718260773417 0.024590815029853014 -0.07812666472859982; 0.08592682935212392 0.05155860427995662 -0.141006152176309; 0.05251466471398463 0.04257951992392281 -0.12274781702476213; 0.04279967581946559 0.042642664691732224 -0.12864044488667278; 0.02676288254759433 0.030989514299537373 -0.10093204685300444; 0.011168485581519913 0.014074910646609543 -0.050852901748447685; 0.014837095076690184 0.020655823165038206 -0.07812565299798237; 0.00828636706157551 0.01274358358831501 -0.04915611690541393; 0.0035828637717597624 0.005680505624388589 -0.02328612455440861; 0.002368672136737596 0.0039838869858850375 -0.017598300408903287; 0.00015491187499795477 1.2182683314004344e-5 6.142957199023447e-5; 0.00016440122301307822 -0.00011261191756007581 0.00012976153918517713; -0.00022472017111325727 -0.00027000141033310893 0.0005123784950123558; 0.0005190318215615927 -0.00020010910798722885 0.00039463014585756147; 0.00024239255839891605 0.00020947046737917062 -0.0001467459893626751; -0.00011242099903666467 0.00047774987269064004 -0.00013710189339857025; 0.00029298027926748157 -9.553191221397401e-5 -0.0002564553824000124; -0.00011925684744250964 -0.00013198915807820536 -0.0003375702406516737; 7.418754107943112e-6 -0.00011178748228930686 -7.371708696139793e-5] %
+
+Mass Used: 109.45170415502753 kg
+Launch C3: 93.8490691005139 km²/s²
+||V∞_in||: 6.912841910724732e-6 km/s
diff --git a/archive/ES_0.5630614950061803 b/archive/ES_0.5630614950061803
new file mode 100644
index 0000000..ab24752
--- /dev/null
+++ b/archive/ES_0.5630614950061803
@@ -0,0 +1,22 @@
+archive/ES_0.5630614950061803---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T05:51:41.849
+Launch V∞: [6.528450473394872, -7.445062041246388, 0.1644576641799662] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.21629450482611e-8, 2.048753990483142e-5, -1.4528509032621178e-5] km/s
+ V∞_out: [-1.2713121583785595e-5, -2.1130124973706106e-5, 4.424499927829325e-6] km/s
+ time of flight: 1.874957778747596e8 seconds
+ arrival date: 2029-04-10T08:01:18.849
+ thrust profile: [0.19635691402658315 -0.046208607525336426 -0.06656183735562266; 0.08106771642981066 0.024541957870750617 -0.08657263056849271; 0.04911028397027421 0.028551237196733782 -0.09085636722567271; 0.042067436684386124 0.032373749300857534 -0.10765509366808662; 0.030413818613176602 0.028724981863313 -0.1016132475776169; 0.033340057274970226 0.034978306086867784 -0.1318749766105658; 0.01816028176192977 0.020996857713794077 -0.08508652158256504; 0.01599712269657795 0.022264150516721478 -0.08932081609816894; 0.008663077697891996 0.011129593628434483 -0.04934446385504232; 0.008566466227661773 0.01174432642668974 -0.055103920382904445; -3.751462343095453e-5 0.0011011668760422637 -0.0010879051672792368; 0.0016618640851559562 0.0019166345581436576 -0.007136341732735134; -0.0016825187516665968 -0.0006464826280399411 -0.0019227558780287963; -4.918850235329777e-5 0.0006235216160184582 -0.0016058858326717818; -0.001760120833417054 0.00016613507319308124 0.00026783893863918033; -0.00020649917462660502 0.000589540195356908 -0.0017719341229551011; -0.001447331375049668 0.0006601454122468452 -0.005652505879000855; 0.0011189451951899155 -0.0013237971776789586 0.00022782508879774874; 0.002207584646272803 -0.00041464501918702117 -0.00048784129860887535; -0.0021448457604284843 0.0041765301105776064 0.004268395710858152] %
+
+Mass Used: 84.79122339538071 kg
+Launch C3: 98.07666070488509 km²/s²
+||V∞_in||: 2.5116144813540792e-5 km/s
diff --git a/archive/ES_0.5630631648261913 b/archive/ES_0.5630631648261913
new file mode 100644
index 0000000..df459ba
--- /dev/null
+++ b/archive/ES_0.5630631648261913
@@ -0,0 +1,22 @@
+archive/ES_0.5630631648261913---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T01:07:35.531
+Launch V∞: [6.473853066214604, -7.400813387927307, 0.23963749238474422] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.735958240492556e-9, -1.9667746935844906e-9, 2.2240772839401556e-9] km/s
+ V∞_out: [1.154847191472112e-9, -2.5983876882726016e-9, -3.6819817926519858e-9] km/s
+ time of flight: 1.8314440099299255e8 seconds
+ arrival date: 2029-02-15T18:34:15.531
+ thrust profile: [0.28071074920635064 -0.07484755036983709 -0.09592365726491085; 0.09404541411916874 0.0246164552910271 -0.0987469544860376; 0.07354345189873944 0.038529718194958165 -0.12957530051944569; 0.06526551318777771 0.04633548771353377 -0.15733537160734423; 0.03761099471503422 0.03167041211148011 -0.11845090488234719; 0.03629240637719523 0.03546379762271363 -0.13710599141609814; 0.018532187781973714 0.020289561282564837 -0.08504687122771182; 0.010087964995721843 0.01187416455536031 -0.05313416768672633; 0.004237476881405259 0.005264193443994852 -0.02518856640015477; 0.003735780964925187 0.0049650269798863075 -0.024530990479675108; 0.0005197347059156114 0.0005396521972644817 -0.003577020751109039; -1.9719668063105045e-5 -0.00015291634379638113 -0.0006527150737134777; 0.0003045517804660296 -0.002153171104129723 -0.0018630002504553649; -0.0001495769668096399 0.0017664866532470505 -0.0024323712289031456; -0.000650426480707065 0.002265119336136655 -0.001566345223902477; -0.0010620618236613238 0.0010554498544321242 0.0007860439064891231; 0.0005351598542063939 0.0038271807204712715 0.0002212142424178041; 0.0016822025024848444 -0.0006855344180547085 -0.0009415252720606372; 0.0004107557927216973 -0.002118180134767202 -0.001640093217267277; 0.00031688916877870097 0.0005032185407223627 -0.000484189182457439] %
+
+Mass Used: 92.58896798445903 kg
+Launch C3: 96.74023845361673 km²/s²
+||V∞_in||: 4.037349372296397e-9 km/s
diff --git a/archive/ES_0.5630644416336017 b/archive/ES_0.5630644416336017
new file mode 100644
index 0000000..b89bf79
--- /dev/null
+++ b/archive/ES_0.5630644416336017
@@ -0,0 +1,22 @@
+archive/ES_0.5630644416336017---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T09:05:57.554
+Launch V∞: [7.747213674526815, -5.831083136140255, 0.03675690038623053] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1462004932512067e-5, -0.0008423628599510633, -1.4903911171984022e-5] km/s
+ V∞_out: [-0.0008128450449742322, 0.00011254386003849625, -0.00019296510728543972] km/s
+ time of flight: 1.833258866557749e8 seconds
+ arrival date: 2030-03-02T04:57:23.554
+ thrust profile: [0.42139671464726886 0.01156330361525872 -0.08566898322098421; 0.14028167415705592 0.09566554050538892 -0.10988523014519148; 0.062217241242387575 0.07619666872298289 -0.09723359439568197; 0.05840072266920992 0.0938603488171605 -0.13006028722731394; 0.03208047513169724 0.07049418441841411 -0.10715457981287703; 0.027863184485293305 0.07182296292635654 -0.10723481462448589; 0.019854145074249516 0.05612184485391087 -0.0922041397785666; 0.008571227288691299 0.030975661257239 -0.05738807105297656; 0.005154267274328449 0.019573561903082057 -0.036250516697835904; 0.0007692224183772108 0.010379497925241317 -0.01855022439192402; -0.0011709198653183698 4.5769946903070956e-5 0.0004966603939016133; 0.0004983715078418079 0.0005444587597705666 -0.0013979522537343456; 0.004437517995523833 0.0036635175132018125 0.0012600244120287906; -0.0013537764963099247 -0.0019513828268609978 0.0011094861243626402; 0.005468706644226573 0.0011919294790406498 0.0027646938084062516; -0.0005422617096670547 0.0018071087586926998 -0.0048788601192756185; 0.007415250358456776 -0.00436270183627535 -0.0006306071277655163; 1.7565764771781045e-5 -9.843387453953149e-5 0.00029338394619473815; 0.003284134307740137 0.0028258068699710667 0.0019798913416675928; 0.0038909927451147228 0.0005502382481263626 0.003162192505158341] %
+
+Mass Used: 108.44567415289885 kg
+Launch C3: 94.02220132908054 km²/s²
+||V∞_in||: 0.00084257266271238 km/s
diff --git a/archive/ES_0.5630782169424235 b/archive/ES_0.5630782169424235
new file mode 100644
index 0000000..966d44e
--- /dev/null
+++ b/archive/ES_0.5630782169424235
@@ -0,0 +1,22 @@
+archive/ES_0.5630782169424235---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:10:58.710
+Launch V∞: [6.285544316833942, -7.604705623118572, 0.016602712779221585] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.637179433035772e-9, 1.7137665621119397e-9, -9.38766735849544e-9] km/s
+ V∞_out: [-2.235785904703983e-9, 5.123656885670365e-9, 6.829085778828986e-9] km/s
+ time of flight: 1.816183282749162e8 seconds
+ arrival date: 2029-01-31T12:43:06.710
+ thrust profile: [0.23432859199402326 -0.07345043359559986 -0.09242602257836872; 0.10564519264122789 0.01921036405919468 -0.1228868037141056; 0.053027620486586304 0.020766669624442402 -0.10476970554165613; 0.08121052293125608 0.043951503500515354 -0.21729745909017673; 0.03469436641635425 0.021929359686384434 -0.12121049349303918; 0.032493392201602425 0.023257153566243787 -0.13633091180226362; 0.016478605031862683 0.012682352994423154 -0.08221961245758748; 0.005933336443296233 0.004948894455572725 -0.03506093485514486; 0.0036599117216542403 0.0032237575622901197 -0.02453424891259018; 0.001984900513947623 0.0019485141470449558 -0.01337094734953639; 0.0006572076549190126 0.0004475333836288167 -0.00493474543846318; -0.0001831997638512218 0.0007035722937974523 -0.0005975620158521688; -0.00015878122863600443 0.0003657209518631789 -0.0011694695980798715; -0.00014188481804929838 0.0007265643765344709 0.0007130013226891845; -0.00010183667940930015 -2.212500862097661e-5 0.0016991569249073621; -0.002560084524265027 -0.0013335987939414604 0.0017673925418938558; -0.0005217982802024268 -0.0005501703328333721 0.0038349408435389212; -0.0003310800749180019 0.0006720129910060549 -0.000797643551965904; 0.003271649813046895 -0.0004933624611626758 0.0006463265054535229; 4.9788909355826525e-6 7.535247228252298e-5 0.00013110214550626515] %
+
+Mass Used: 89.10855779722397 kg
+Launch C3: 97.33989062324632 km²/s²
+||V∞_in||: 1.1624002971846092e-8 km/s
diff --git a/archive/ES_0.5630897035580257 b/archive/ES_0.5630897035580257
new file mode 100644
index 0000000..3da6e94
--- /dev/null
+++ b/archive/ES_0.5630897035580257
@@ -0,0 +1,22 @@
+archive/ES_0.5630897035580257---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T11:45:44.133
+Launch V∞: [6.417743277296719, -7.382772812191689, 0.08634775411367693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4273484750986522e-7, -2.1769936618427623e-7, -1.50483062268725e-7] km/s
+ V∞_out: [7.178183338113062e-8, -1.5798618364778102e-7, 2.3549472302118954e-7] km/s
+ time of flight: 1.8420221202794325e8 seconds
+ arrival date: 2029-02-28T11:02:36.133
+ thrust profile: [0.3693441292531285 -0.10441814243710162 -0.11271945309920699; 0.08536898285480457 0.022770993519906583 -0.08816147544045437; 0.08237079111446591 0.04376839231265931 -0.14101163534551645; 0.03816424420270251 0.02705971747143009 -0.09203281797070917; 0.034453993002131644 0.030053602887145016 -0.10703970315888725; 0.03296235687810551 0.03325156597682484 -0.12481865024761424; 0.026523217168408535 0.029680416164290027 -0.11872559841527146; 0.006368076089141407 0.008523252167782732 -0.03641992732644095; 0.003033702684226064 0.004887699568362132 -0.02040801118938096; 0.015797021826860644 0.022136157907827813 -0.09830062355558683; 0.0005095102115120653 0.0007306730239352839 -0.002888230774848328; 0.00024965636416069586 0.00047725447226259576 -0.0020452695853902026; 0.001062827012014313 -0.0003653784362656684 -0.0005273096344588433; -0.0004109285868584046 -1.8560826969209486e-5 6.418369870562731e-5; 0.0005332879545302977 0.0003756854256187932 -0.0006702535729819399; 0.0006267543726683454 -0.0008112221804262913 0.00017560658654162825; 0.0006166126672467735 0.0009821667976998903 0.0011815709575803306; -2.550880590745328e-5 -0.0002289273605961923 0.0005946367690163532; 0.00026157866346491077 -4.36536926491548e-5 -0.00024841544593757423; 0.00039152489190664807 0.0006973237645554392 0.00016559957287762132] %
+
+Mass Used: 98.68670937557044 kg
+Launch C3: 95.70021910436448 km²/s²
+||V∞_in||: 3.0068488947812635e-7 km/s
diff --git a/archive/ES_0.563095550796608 b/archive/ES_0.563095550796608
new file mode 100644
index 0000000..8880542
--- /dev/null
+++ b/archive/ES_0.563095550796608
@@ -0,0 +1,22 @@
+archive/ES_0.563095550796608---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T11:46:51.040
+Launch V∞: [8.111408133520898, -5.819385650599274, 0.17548945157488924] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007251449000908488, -0.04294403065861279, -0.04154071037012927] km/s
+ V∞_out: [0.010267509531406557, -0.009228270986974296, 0.059121646631136456] km/s
+ time of flight: 1.874957778298609e8 seconds
+ arrival date: 2030-04-26T13:56:28.040
+ thrust profile: [0.13568666912041036 -0.004310451353310866 -0.05015062331850225; 0.07392670752620956 0.03464728031750686 -0.09304955960932783; 0.01819869226984408 0.013432445882753035 -0.04578010908041305; 0.02930196793141829 0.025920474725593712 -0.09818965623440154; 0.018635428022932783 0.01912275985993125 -0.08381002973780387; 0.008517824169765079 0.010375691085007766 -0.051215720269657365; 0.010185149780006576 0.013633062052700127 -0.0725354419797495; 0.004172303839012745 0.00306265350780998 -0.036134858798270886; 0.009189683793284789 0.013249481238583518 -0.08081418775632286; 0.013588368956608646 0.017218620801089365 -0.1483480692791357; 0.001616080959388165 0.004912029779609741 -0.015107320852610682; 0.002029408126559992 -0.0008992133552590499 -0.005242442206177521; 0.00042293489802799645 0.0025382520948412407 -0.009479403830971206; 0.001960553578198367 -0.0010153396018150586 -0.0007524001616402327; 0.0028867710205633954 0.0007138634725232614 -0.009382721866057361; -0.0002373008592967088 0.0004081048597687766 0.0042548010781834275; -0.0026123458289776646 -0.003253730318705391 0.007174848779976705; 0.0041084603218924315 -0.0020115133747863733 0.004355503514438846; -0.006629700861064352 -0.004976658503484789 -0.023315480424078827; 0.007010092657685898 0.0056055147535848775 0.009756726137553677] %
+
+Mass Used: 75.41404705775403 kg
+Launch C3: 99.69098780656377 km²/s²
+||V∞_in||: 0.06018640959448916 km/s
diff --git a/archive/ES_0.563107955833649 b/archive/ES_0.563107955833649
new file mode 100644
index 0000000..259ec76
--- /dev/null
+++ b/archive/ES_0.563107955833649
@@ -0,0 +1,22 @@
+archive/ES_0.563107955833649---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:57:58.602
+Launch V∞: [6.6354174687603615, -7.334704009239489, 0.17125589865232935] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6640229721180406e-7, 4.605196800286606e-8, -5.346645845969386e-8] km/s
+ V∞_out: [1.737051135406509e-7, -4.596669294717496e-8, 2.1389386920079518e-8] km/s
+ time of flight: 1.8749577787423053e8 seconds
+ arrival date: 2029-04-09T05:07:35.602
+ thrust profile: [0.23494203246053671 -0.0576118138109325 -0.08537418702118607; 0.04333131406538113 0.012179834717702193 -0.05094548801691711; 0.0663788073987215 0.03656310054657551 -0.1288477096442508; 0.0424501962460032 0.032315998687959493 -0.11570231705717281; 0.0353711936600965 0.03352909131237025 -0.12476344824697057; 0.03787798284581238 0.03463190942218699 -0.14615293132088406; 0.018500121032966346 0.024189419918980076 -0.10481112704615499; 0.006199738163914175 0.008088854214729928 -0.03801068555496648; 0.003917109646275173 0.006088778435752157 -0.03169565600697801; 0.004746948962529215 0.00686425683858823 -0.03559139859945137; 0.0018283259422232395 0.0019190126108007874 -0.012158774397065444; 0.00034124595760357386 0.0015213094905975478 -0.005094372638259922; -0.0015546717354071628 -0.0007294925663728863 -0.00030337839662245535; -0.0025586881972441576 -0.0010308958898664101 0.0015312456588009319; -0.0007112114518486353 0.0009521077119037882 -0.0027962516568494486; 0.001777305750516312 -0.0032982078948854947 0.0027944811912060056; 0.0011506008014437064 -0.0018477503811564454 0.005057785097095542; -0.0004018423886559103 -0.00039337518295152183 0.002846365021441713; 0.00025791707004959983 0.002890777248546722 -0.001042409435242355; 0.002205121577594662 0.00278044743932145 -0.0018298871507569277] %
+
+Mass Used: 86.13275239346513 kg
+Launch C3: 97.8559764707072 km²/s²
+||V∞_in||: 1.8074614921077778e-7 km/s
diff --git a/archive/ES_0.5631092366569079 b/archive/ES_0.5631092366569079
new file mode 100644
index 0000000..c08e2d7
--- /dev/null
+++ b/archive/ES_0.5631092366569079
@@ -0,0 +1,22 @@
+archive/ES_0.5631092366569079---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T06:48:32.627
+Launch V∞: [7.954370499765636, -5.737257259409638, 0.16314075059588448] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.630812317859176e-5, 5.2987754472081116e-5, 0.005596476007608518] km/s
+ V∞_out: [-0.005047103760364032, -0.001522848656204155, 0.0018793070687851267] km/s
+ time of flight: 1.874957778748043e8 seconds
+ arrival date: 2030-04-22T08:58:09.627
+ thrust profile: [0.26950089907697194 0.01840136585458244 -0.07426300339880204; 0.11964755225900363 0.08330903790494094 -0.11192835622263034; 0.07468673692361737 0.08968148760842896 -0.13401380200044016; 0.040148158566620774 0.06462581597754515 -0.10956836118191493; 0.022514681872733477 0.04495693039963764 -0.08679381166258233; 0.02170084572413456 0.053277158630392174 -0.10723564822574419; 0.015370902584310005 0.04233003452264459 -0.09356372363510063; 0.002729646143507843 0.008274764801399626 -0.019512766986448892; 0.002588372616036434 0.009609714991223477 -0.02362844285596108; 0.0014181802785476088 0.006979099672176885 -0.012699736551357563; 0.0011753155494058736 0.00570417928386646 -0.01490544290146291; 0.0009812100114409547 0.0012773749711905563 -0.005968504286209996; 0.002083119490454746 0.00016623338512299036 0.004693956488057914; 0.0016857973555680166 0.005313950591103119 -0.0019400049920403999; 0.011327500037177425 -0.001069863087273002 0.0016363239402433435; 0.0021659131270732766 -0.0017411814551004864 0.0046193283587648674; 0.005067865906065203 0.0056166885013660675 -0.014556572287871886; -0.0024420044310123163 -0.009212443152404062 0.012409678845934753; -0.011213372086566363 0.015429468850879837 0.00252400361595256; -0.016939517626650042 -0.005638511308130174 -0.0027983216854794053] %
+
+Mass Used: 95.70809219233615 kg
+Launch C3: 96.21474581269538 km²/s²
+||V∞_in||: 0.005597247031847425 km/s
diff --git a/archive/ES_0.563109492606354 b/archive/ES_0.563109492606354
new file mode 100644
index 0000000..49a9ca6
--- /dev/null
+++ b/archive/ES_0.563109492606354
@@ -0,0 +1,22 @@
+archive/ES_0.563109492606354---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T00:54:15.495
+Launch V∞: [7.442640119693165, -6.257610166483353, 0.003460722598698644] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.09516760813286e-5, 0.00011228908887145404, 9.894089492076453e-6] km/s
+ V∞_out: [-7.112951017886378e-6, 3.549091308007638e-5, 0.0001279723446696959] km/s
+ time of flight: 1.7001733097284484e8 seconds
+ arrival date: 2029-09-28T19:56:25.495
+ thrust profile: [0.42015510672343015 -0.04043348681000135 -0.13068065448603314; 0.17063987571703781 0.07838526966864073 -0.1691241099821062; 0.0649813417548707 0.052173075484578856 -0.12166268172734777; 0.06455003998576996 0.0648983439448906 -0.16274125066024928; 0.04415653179803518 0.05317166175363764 -0.1470248904499054; 0.020824611173736022 0.033828820092698005 -0.10066004905087664; 0.011464450236673902 0.017385212650176108 -0.0586691428413349; 0.006634774753908822 0.012488676153008272 -0.04180666027768794; 0.0046507648151978935 0.01826271526463208 -0.06452058175841663; 0.0021412597938148857 0.010359006137631547 -0.03634283505411816; 0.000360723763320938 0.0020427737675520283 -0.006635340470169326; 0.004024631892108152 0.0012042984390774668 -0.00360636359886756; -0.00012633193202217258 -0.0009383886659760769 -0.0006456511138063026; 0.0018779924176847908 0.001470935731130807 -0.004562069803317623; 9.141474249064932e-5 -1.1957277101734998e-5 0.003189851369758201; 0.004982841721337744 7.697646084931818e-5 0.0008964111034970622; -0.0008881423915490709 0.0002673321658771869 -0.00012923771867040957; 0.0021817703519591176 0.0038062155377844064 0.0015815119218784463; 0.0023809253377639404 0.0035603413138238986 -0.005464521319319835; 0.0012832502617197955 0.0041008739147045765 -0.005070160177354919] %
+
+Mass Used: 105.41597265341215 kg
+Launch C3: 94.550588923543 km²/s²
+||V∞_in||: 0.00013319486786362414 km/s
diff --git a/archive/ES_0.5631101783293997 b/archive/ES_0.5631101783293997
new file mode 100644
index 0000000..c385033
--- /dev/null
+++ b/archive/ES_0.5631101783293997
@@ -0,0 +1,22 @@
+archive/ES_0.5631101783293997---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T21:24:05.942
+Launch V∞: [7.863038739005571, -5.398308793663112, 0.47857775524047125] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.735646355814285e-5, 4.103395125034856e-5, 0.002802340825276783] km/s
+ V∞_out: [-0.0025347114209508625, -0.0008865007516467649, 0.0007968125036277949] km/s
+ time of flight: 1.8749577787479022e8 seconds
+ arrival date: 2030-04-18T23:33:42.942
+ thrust profile: [0.8698803857634921 0.0001453721812599678 -0.215360938989103; 0.042476967977825186 0.024383759091554637 -0.045137700388377576; 0.05207211687147601 0.05088919330430357 -0.09800507185584027; 0.03334658420467018 0.04248984067879233 -0.09057137420774676; 0.03459844999532969 0.05635782133349369 -0.13258932673886786; 0.019898833240051407 0.03775549474733698 -0.09991051223388947; 0.010216873219112419 0.024581762589314465 -0.06629996247299816; 0.0020547298257234128 0.010791604338415993 -0.023968368341834575; 0.0005598836492955515 0.0014448576070309727 -0.00938029731060443; -0.0039142428494585565 0.0074948053559919636 -0.011126796753017497; -0.004115167139460131 0.007431642148699831 -0.008619986555925408; 0.00525363697379709 0.013612608170548043 -0.02621668505297346; -0.00038879541261972847 0.0013451693120041517 -0.002952872096076894; 0.0006368881569353243 -0.00011128390420986865 -0.003844062417254117; -0.0007963188375036036 1.8906715021760074e-5 0.002592208173738261; 0.00361883160147814 -0.003073299938846954 -0.00348551355961844; 0.00024160988268355716 0.0026091598182180612 -0.013967497173686099; -0.0009744737937264518 0.005564519404215915 -0.005211348492689595; -0.009035316849398761 0.005007857187519827 -0.003192093610002501; -0.013005276408940385 -0.005656176573492936 -0.004672334511131112] %
+
+Mass Used: 124.97265057215236 kg
+Launch C3: 91.19815271065382 km²/s²
+||V∞_in||: 0.0028032280767144283 km/s
diff --git a/archive/ES_0.5631176730090063 b/archive/ES_0.5631176730090063
new file mode 100644
index 0000000..835e544
--- /dev/null
+++ b/archive/ES_0.5631176730090063
@@ -0,0 +1,22 @@
+archive/ES_0.5631176730090063---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T17:33:38.703
+Launch V∞: [7.659705168235969, -5.901389858070916, 0.09119891841171406] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.653289372829137e-9, -2.069156532124348e-9, -1.4976063156711042e-9] km/s
+ V∞_out: [-2.1489084005744146e-9, 1.930397121770681e-9, -7.228442810435489e-10] km/s
+ time of flight: 1.8327387342065415e8 seconds
+ arrival date: 2030-03-04T22:58:11.703
+ thrust profile: [0.5983944597618145 -0.016152540793372156 -0.1734655146739211; 0.08115023049341888 0.04286331010560792 -0.08980807089783141; 0.03848729491473261 0.03202637373910121 -0.07602976676502089; 0.036528584931165856 0.040514894233579415 -0.10673872824613478; 0.028680385446669374 0.038431520801058355 -0.1124277925109423; 0.015462750181262417 0.022995881836535795 -0.07465292903653793; 0.017675171303289047 0.033166376714595464 -0.10791547342642091; 0.010427235307045542 0.019189218731716622 -0.06937934974298852; 0.004703701221012675 0.00877422310851297 -0.034438973875726024; 0.004813214652438747 0.0005360430241460479 -0.009024794808260376; 0.0013912621280739814 0.003749237378313926 -0.0003426456817876202; -0.011760775318462592 0.00505947562678802 -0.010567325545316655; 0.0006676080310223527 0.0013125130052236414 -0.007358344381700129; -0.0009805163547364493 0.0015198375382844999 -0.00031705842873600183; 0.00028249552601147636 0.0005287869935795637 -0.008126973919011491; 0.011451602369895585 0.010921988977345204 -0.027153566023744018; -0.0038748870702831153 -0.0014768524251051207 0.0020358724052314337; -0.001006918448862677 0.0013340829215739347 -0.001653397192810717; 0.00593030055514027 0.004468250913629422 -0.01516006237856362; -0.02392163065091815 0.011058931819171789 -0.02631475784974542] %
+
+Mass Used: 111.5201023873924 kg
+Launch C3: 93.50580276396255 km²/s²
+||V∞_in||: 3.6829577688508555e-9 km/s
diff --git a/archive/ES_0.5631183794210296 b/archive/ES_0.5631183794210296
new file mode 100644
index 0000000..f2b8b7a
--- /dev/null
+++ b/archive/ES_0.5631183794210296
@@ -0,0 +1,22 @@
+archive/ES_0.5631183794210296---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:21:25.077
+Launch V∞: [7.762742584117571, -6.270644062322349, -0.1720054169236871] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6219478610788513e-9, 2.836102384869447e-9, 1.081480600707054e-9] km/s
+ V∞_out: [1.6823305072723346e-9, -1.214623650050936e-9, -8.268861146294274e-10] km/s
+ time of flight: 1.7140503291074222e8 seconds
+ arrival date: 2029-10-18T03:51:57.077
+ thrust profile: [0.08998149496903086 -0.01568212538259162 -0.038176642879246325; 0.06496958819191516 0.01821760159865946 -0.08601820295387899; 0.06533771623414923 0.030542119423437732 -0.14880330906607403; 0.0446927159915581 0.025596536284607976 -0.14390189074302487; 0.045372098819297706 0.029007951329994182 -0.18539325130778583; 0.034084885883322154 0.023272695612509584 -0.16775132771758178; 0.010007857725586296 0.006947255231729517 -0.05759915110670385; 0.00846525503379887 0.006243261423789003 -0.05387234554437086; 0.004332915555636589 0.003226877650191222 -0.030308359941904554; 0.0007527145494049848 -8.795696227688245e-5 -0.0045814974426399676; 0.0006141484407501029 0.00036619018732101034 -0.007997893210553353; 0.0012961289866453675 0.0005807759498796338 -0.006599396540539052; 0.0007438884841233902 0.0005595823817047215 -0.0073933685271058355; -9.439617680260322e-6 0.0006500765518288889 0.0007365756856674063; 0.001327692634611567 -0.0012147421572087664 0.0023926516939091645; -0.0028865624592760287 0.003757413492167346 -0.001915055430760381; 0.002389707428833471 0.003051330465826084 -0.003137884522704973; -0.0007918376312973901 -0.0052075387119788295 -0.0044099373216000765; -0.0057248871535949845 0.004413739226958325 -0.007869908045582298; 0.006891836840456908 -0.008057431998296491 -0.013030660344833878] %
+
+Mass Used: 75.90882038333984 kg
+Launch C3: 99.61073524706195 km²/s²
+||V∞_in||: 3.441481060710071e-9 km/s
diff --git a/archive/ES_0.5631209497353563 b/archive/ES_0.5631209497353563
new file mode 100644
index 0000000..b241124
--- /dev/null
+++ b/archive/ES_0.5631209497353563
@@ -0,0 +1,22 @@
+archive/ES_0.5631209497353563---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T09:29:11.144
+Launch V∞: [7.724220452961072, -5.521868388200509, 0.1058716498718392] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.2667494719200027e-6, -7.821249130541392e-6, -2.5928525805212267e-5] km/s
+ V∞_out: [-2.499174739196877e-5, -2.933022653124726e-6, 1.0663425127564282e-5] km/s
+ time of flight: 1.852816571769985e8 seconds
+ arrival date: 2030-03-22T20:36:48.144
+ thrust profile: [0.8487009374217002 0.003367749948192594 -0.19651551832625566; 0.15028667260000522 0.09758170586964172 -0.1381464313396034; 0.06727315742450539 0.07345313239257313 -0.11673034772685174; 0.04689406826397853 0.0711769606938645 -0.1253845167542008; 0.02297656363141313 0.044964215448832154 -0.08828764579941803; 0.012214863560886633 0.029940929289567795 -0.06422519719630836; 0.007440541950495455 0.022337890030304973 -0.05129814663929089; 0.007236862835502022 0.02717185494805264 -0.0647013150724622; 0.0023816546580041047 0.010688219352795942 -0.0272199275635925; 0.0005587440305608903 0.004657060891559659 -0.012356683508982244; 7.455914174391747e-6 0.0028079578914756084 -0.007623355099516417; -0.0007971808981983877 0.0005519129760458333 0.0011900698411813097; 0.001167827529963314 0.003151739451358938 -0.011547377680738014; -0.0008294098708273328 -0.00019213329963708314 1.7275694992876454e-5; -0.00012790063151286348 -0.0007733499861770618 0.0009251845222334935; -0.000346727661073271 0.00034624553058746244 -0.00020831002666185704; 0.0003227320234634865 -0.00044243617577540946 -0.0005568504827640909; 0.00011568667414745611 -0.00021264842582549177 0.00022598147354946038; 0.0012810857476854508 -0.0006532789717253473 -0.0009304506829674776; 0.001605204413419385 0.001294701416631402 0.0021176334691609825] %
+
+Mass Used: 131.0071527232676 kg
+Launch C3: 90.16582090879682 km²/s²
+||V∞_in||: 2.7278783706496934e-5 km/s
diff --git a/archive/ES_0.5631241361991076 b/archive/ES_0.5631241361991076
new file mode 100644
index 0000000..feb9ea2
--- /dev/null
+++ b/archive/ES_0.5631241361991076
@@ -0,0 +1,22 @@
+archive/ES_0.5631241361991076---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T07:11:34.156
+Launch V∞: [6.394575080133692, -7.372895402259862, 0.14792027075599518] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.644787362438369e-7, 6.696009411823092e-8, -8.372979445047101e-8] km/s
+ V∞_out: [2.9030830205984515e-7, -7.914409285137919e-8, 3.5714568496842297e-8] km/s
+ time of flight: 1.8535706376454315e8 seconds
+ arrival date: 2029-03-13T15:15:57.156
+ thrust profile: [0.33896310494942916 -0.08358090160384343 -0.1110578101610448; 0.18829884724861826 0.05684414364185377 -0.18237524002041605; 0.07343696416461443 0.04219396185309609 -0.12304176529416798; 0.05322749238119914 0.04122855356415896 -0.1253913462749331; 0.03310236024829079 0.03145597354331202 -0.1019609427440402; 0.023582294578762913 0.026080338191178828 -0.08942124472988681; 0.0140250150741424 0.017696820103169607 -0.0639635671628434; 0.008979049768558553 0.012644173325022037 -0.04798984418771916; 0.013098112918417741 0.02051055656265641 -0.07677622598744141; 0.002966904893915201 0.004812267848332272 -0.020442058696982505; 0.0009898882906270502 0.0007599042777604286 -0.005405961553141016; -0.0004027811452983447 -0.00014355839915358335 -0.0010473895036126227; -0.0002548607912739955 8.869115369865922e-5 0.0010940274529601844; 0.0002590476993939874 -0.001081823825344249 -0.00015975596389914532; -0.000146037152103901 3.439407019953074e-5 -0.0014006048393828364; 0.0008253835904855372 0.0011021114181915949 0.0005784236099843136; 0.00023361264939724622 -0.0006642661200486536 -0.0003148649784542874; -0.0007994993494864313 -0.0008726040796046749 -1.0116086118057573e-5; -0.0003878475536647779 0.0004187314685236267 0.0014314394464349613; 0.0007212635049082673 -9.511776937986044e-5 -0.0018993876035740198] %
+
+Mass Used: 101.22449029693917 kg
+Launch C3: 95.27205747463195 km²/s²
+||V∞_in||: 2.853827861104757e-7 km/s
diff --git a/archive/ES_0.563125586872211 b/archive/ES_0.563125586872211
new file mode 100644
index 0000000..692e721
--- /dev/null
+++ b/archive/ES_0.563125586872211
@@ -0,0 +1,22 @@
+archive/ES_0.563125586872211---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:18:00.465
+Launch V∞: [6.501510692573276, -7.323418510065168, 0.17038485128940586] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003675794816877364, 0.0034124574046625364, 0.0037324949343304744] km/s
+ V∞_out: [-0.004446345387428382, -0.0022537254436750228, 0.0037641845644624705] km/s
+ time of flight: 1.8749577791572145e8 seconds
+ arrival date: 2029-04-09T02:27:37.465
+ thrust profile: [0.3914221427357156 -0.10235344944304908 -0.13678080261450057; 0.03464810470682969 0.008807038030520086 -0.03771818045974762; 0.05757459995266626 0.02827102794678755 -0.10262415687868101; 0.06006623948021612 0.03956444276175746 -0.1501837830923028; 0.05429067001040388 0.04298590519067791 -0.17422532056889156; 0.02972916163419364 0.026762828199763975 -0.11628270960950092; 0.021688898539321225 0.02179681168737079 -0.10013225462459648; 0.002945193397375998 0.0033475591179129966 -0.017317351219602647; 0.0037289840924175036 0.0051665437409903125 -0.024999297701007332; 0.003201728827805571 0.00465261260269102 -0.025011367976770255; 0.000831313844408825 0.0005911326776758061 -0.0058705019100764215; 0.00033999352617421674 0.003459107486397388 -0.005263784658653128; -0.0037087518568501157 -7.284074988783744e-5 0.0007256025901172492; 0.0005017200055414204 0.001993918385557144 -0.0006668780780023543; -0.0021290021360163194 -0.00088514526745371 -0.0008275517954407026; 0.004619065187815387 -0.004438090358741813 -0.005060602253913897; 0.0008922595744057973 0.0030093326503025557 -0.00042850496744677993; 0.0021741624007848384 -0.00595815720579123 0.001525177310172997; 0.004359950246192846 0.004644919741206805 0.0007363764990573922; -0.0048981128275261375 0.006714472445184012 0.0003272543569637741] %
+
+Mass Used: 97.38158743648728 kg
+Launch C3: 95.93113095675868 km²/s²
+||V∞_in||: 0.006252027791782544 km/s
diff --git a/archive/ES_0.5631255890916799 b/archive/ES_0.5631255890916799
new file mode 100644
index 0000000..62a3f9d
--- /dev/null
+++ b/archive/ES_0.5631255890916799
@@ -0,0 +1,22 @@
+archive/ES_0.5631255890916799---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T22:36:33.280
+Launch V∞: [6.349643617411004, -7.51021376667677, -0.03534922839337669] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1346479905299045e-8, -2.706517648015292e-9, 9.722787024281808e-9] km/s
+ V∞_out: [2.532367741655969e-9, -5.7148089174079255e-9, -7.933216976958482e-9] km/s
+ time of flight: 1.874957778448987e8 seconds
+ arrival date: 2029-04-12T00:46:10.280
+ thrust profile: [0.3748170980966018 -0.10491183760351737 -0.13614694128694876; 0.03729376684881694 0.00786316664705454 -0.0462671872318549; 0.03326771506563252 0.014514660987532332 -0.06987548128818817; 0.05411932132963384 0.02994254374284204 -0.15419906011141732; 0.022565961341881866 0.014675744014687605 -0.08593754089492109; 0.040958575710493286 0.029623373050630317 -0.17914454548225597; 0.015114998238352356 0.011636411262077965 -0.07966975801120411; 0.00593532300911566 0.004905958219568575 -0.03615723343484435; 0.008563822127618846 0.008191080499908812 -0.056630123817936716; 0.006196887662920593 0.006812898962689557 -0.0462928009877487; 0.0014753787150836564 0.0014686840572594477 -0.011085550232814283; 0.00042398211624300285 7.597171244398031e-6 -0.0024163973158061384; 0.00014077056686605797 0.0006776966907535817 -0.0009995921257062944; -0.0006015006772787763 0.0005371213195967058 -0.0014358080454776982; -0.0006631633368234477 -0.0004897527591069479 -0.0018665368500443299; -0.00031444501835127384 -0.0005846696202730902 -0.0014301797663828076; -0.00021120571697992281 0.0004663269692267314 -0.000876575723273641; -0.00024128673289914063 -0.0014661663230974172 -0.0010157076566023975; 0.00019584013549351687 -0.00013758748331802806 0.0009560328189735824; 0.00021722644133543136 2.3125647760946586e-5 0.0011694030354462378] %
+
+Mass Used: 92.76506960629058 kg
+Launch C3: 96.72253445725758 km²/s²
+||V∞_in||: 1.5185533627104314e-8 km/s
diff --git a/archive/ES_0.5631259321905832 b/archive/ES_0.5631259321905832
new file mode 100644
index 0000000..76d8461
--- /dev/null
+++ b/archive/ES_0.5631259321905832
@@ -0,0 +1,22 @@
+archive/ES_0.5631259321905832---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T07:17:58.364
+Launch V∞: [6.3748434354299315, -7.62916353601247, 0.06859238760208321] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.21732656106025e-10, -2.806879651650131e-9, -8.706335384660744e-9] km/s
+ V∞_out: [1.865425212136861e-9, 2.8574467014081833e-9, -3.989792124652236e-9] km/s
+ time of flight: 1.8430181334200266e8 seconds
+ arrival date: 2029-03-05T10:14:51.364
+ thrust profile: [0.17317462043038473 -0.0488913485089153 -0.06422822670117541; 0.04484703075790358 0.010082610088148194 -0.053339591480594514; 0.043796106458726336 0.019402879177177947 -0.08698831690952624; 0.06310848900107638 0.0393007036247157 -0.16467527876649288; 0.02695200054577258 0.019496559396543257 -0.09612543549710773; 0.03663700863737932 0.03138498325124765 -0.1597167945154318; 0.01822562044794621 0.015006407495436394 -0.08698112663415951; 0.015109304756328287 0.015283987099456851 -0.08677522383530445; 0.008128224859527373 0.008317399846032199 -0.05179467745716751; 0.0033943678908724523 0.0035969466447624138 -0.02375818962985008; 0.0022207365804265762 0.0030263664283304782 -0.018147417677425386; 0.00041694577422347873 0.0004896809241914444 -0.0033087578936019557; 2.7259696412964776e-5 -1.149150699096481e-5 -0.0003887069558060611; 3.349387497315784e-5 0.0003661883755488178 -0.0015256509015295528; -2.465742523586451e-6 0.0002554505785177844 -0.000730534980493984; 0.0004044012777254405 0.0005542569337624178 -0.000575583162270035; -0.00011198997643901049 5.641217888129773e-5 -0.0004875355529166453; -0.00011923448545216118 1.789937412410701e-5 -0.0010408157493975085; 0.0006044788779122866 -0.00010111122044258441 -0.0006469156309471694; 6.959146534875555e-6 -0.00013041548384153155 0.0002433740722449407] %
+
+Mass Used: 80.37001254924417 kg
+Launch C3: 98.84747000110335 km²/s²
+||V∞_in||: 9.16871859665853e-9 km/s
diff --git a/archive/ES_0.5631260269807713 b/archive/ES_0.5631260269807713
new file mode 100644
index 0000000..0c9e846
--- /dev/null
+++ b/archive/ES_0.5631260269807713
@@ -0,0 +1,22 @@
+archive/ES_0.5631260269807713---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T02:35:23.001
+Launch V∞: [6.675046645263064, -7.372120964255549, 0.22958244264198108] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.936586438608253e-9, 5.1880399632071974e-11, -6.2780449407778364e-9] km/s
+ V∞_out: [-1.3145201911665244e-9, 2.8719869846950403e-9, 3.970350512864408e-9] km/s
+ time of flight: 1.8749577780715004e8 seconds
+ arrival date: 2029-04-10T04:45:00.001
+ thrust profile: [0.15367172466785076 -0.04281375178488372 -0.05603388380468919; 0.04300228429005144 0.009807169089622482 -0.05006689390232389; 0.05380762252455155 0.023599333801719257 -0.10258633140408589; 0.053067899253110125 0.030785640198564133 -0.1395130331380325; 0.04268594639798124 0.02937913262044913 -0.14357440003990854; 0.028254810741058543 0.021940462972231015 -0.11631236445450846; 0.014245577014034344 0.012439703830310874 -0.07013843815215534; 0.0038417805440723704 0.0038262038674225203 -0.022929239755339857; 0.007868106354971921 0.0093036363513755 -0.05476251168444793; 0.011868910850867064 0.011587589926154525 -0.08771738169148126; 0.0013096014473143224 0.0008008446635802005 -0.006563814174172699; 0.00211042624358409 0.000345678982239223 -0.004473382404797343; 0.0006706458412931033 0.0017059176531657567 -0.0076078731963766955; 0.0009789420065048065 0.0007753056271703293 0.00019883647197565298; 0.0014042836211932649 0.001782480018257434 -0.0017435082587533295; 0.0010190638083041727 -0.000789412532743096 -0.0022169545876195166; 0.002457934996795888 -0.0032145575044375883 -0.0007920980802587083; 0.00022460425661763306 -0.00045522645653546957 -0.0045166790052330215; -0.0006593415498254334 0.003677536857803379 -0.002495177312745207; -0.002935134815881115 0.0017975278268714157 -0.0051721775168046095] %
+
+Mass Used: 79.73047874243048 kg
+Launch C3: 98.95712332602332 km²/s²
+||V∞_in||: 9.355895001258624e-9 km/s
diff --git a/archive/ES_0.5631272064640581 b/archive/ES_0.5631272064640581
new file mode 100644
index 0000000..8419661
--- /dev/null
+++ b/archive/ES_0.5631272064640581
@@ -0,0 +1,22 @@
+archive/ES_0.5631272064640581---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T09:53:56.377
+Launch V∞: [7.821402686337868, -6.114551247460339, 0.17579988256736834] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009532212080233354, -0.0006844297185663464, -0.03965169828499193] km/s
+ V∞_out: [0.03640579673978709, 0.014442064960875224, -0.006835620723818804] km/s
+ time of flight: 1.8749577781101742e8 seconds
+ arrival date: 2030-04-28T12:03:33.377
+ thrust profile: [0.26983181409471335 -0.007444875281272192 -0.10033360810211749; 0.0917836088000568 0.04138507004941799 -0.11544069725002194; 0.05117545405219221 0.03488587754812479 -0.11464966928125035; 0.0390260646024091 0.03259126253445731 -0.12604950740517218; 0.028898922544986234 0.027305269097481814 -0.12160902949980472; 0.019343845510978817 0.01971752609265717 -0.09973857550335558; 0.010937810244922451 0.011574717782997172 -0.06619069239417559; 0.0036734726395768968 0.0036646659314252352 -0.02452405263968195; 0.0016210102194786627 0.000981536396229811 -0.007386270203545958; 0.0006923682425122543 0.0015545837499580095 -0.004568653883350566; 0.0015155479729946257 0.002562901096516292 -0.0027639526763908436; 0.0015695763644617343 0.001983083863966382 -0.011615248868347217; 0.0025762075040444525 -0.001073866027737153 -0.0034322109240645586; 0.00010810881540716539 -0.00023474955198381832 -0.00045275232085016843; 0.0007059760003285836 0.0003370543383778992 0.0002446637245644952; 0.005404723927593167 0.005314981229449839 -0.01144767327700014; 0.0032187804176610543 0.0001705003356553152 -0.0008292172333083317; 0.00042683877298086564 0.0006099464421577578 -0.003309638424144276; 0.0014160368048132528 0.0031169640546662514 -0.0009609947850457632; 0.0006237682420841848 -5.8305460608825636e-6 -0.006178186191747771] %
+
+Mass Used: 81.85600940083532 kg
+Launch C3: 98.59298253838271 km²/s²
+||V∞_in||: 0.039669059121626694 km/s
diff --git a/archive/ES_0.5631307715394686 b/archive/ES_0.5631307715394686
new file mode 100644
index 0000000..bb28720
--- /dev/null
+++ b/archive/ES_0.5631307715394686
@@ -0,0 +1,22 @@
+archive/ES_0.5631307715394686---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T11:07:18.323
+Launch V∞: [6.557143169616849, -7.354367867812205, 0.10542111366833992] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005563585477661404, -0.0035875812496256793, 0.0050682666848637144] km/s
+ V∞_out: [-0.004345872234195327, -0.0033700890429713875, -0.0026623785533602994] km/s
+ time of flight: 1.8749577787504765e8 seconds
+ arrival date: 2029-04-08T13:16:55.323
+ thrust profile: [0.2205900075591794 -0.051093597578176574 -0.07257099536144586; 0.13165042045502284 0.04095036593153822 -0.12816404018377284; 0.0751217056556292 0.04400707667510081 -0.12450980817188409; 0.05587372194491444 0.044231087397493554 -0.13071770442668226; 0.037660477953556266 0.03635920191596844 -0.11504751093893452; 0.022565172079590304 0.02466777033292644 -0.08485021447850843; 0.018331559210325265 0.022540222560408534 -0.08181660301672118; 0.012522316329328013 0.017132886886730682 -0.0678808247059965; 0.005367205468760105 0.009461510745108911 -0.031199778792044233; 0.002197319639930971 0.003449839507681004 -0.014575841493839147; 0.0026793272272000205 0.0065314360415946555 -0.029472481913019967; 0.0021349495615814807 0.004056723261955454 -0.016218079218086764; 0.0005727976766788062 0.0002702873352729543 -0.0009100098120564236; -0.00018951531333639358 8.462901672718379e-5 0.0009678053637633176; -0.0009568524669531003 -0.0008409176461969723 -0.0003138714726482648; -0.0017430626393532358 0.0018519767424252096 -4.951648571186373e-5; -0.00034102820663015076 0.0016217727027047846 0.001680390593833812; 0.0008627899331875465 -0.00023407320233373286 -0.00019401398631564725; -0.0015654338971001214 -0.002069316310499582 0.00015165161517515413; 8.00025046984761e-5 0.0010450224900271964 0.0039037366675530585] %
+
+Mass Used: 90.60442658589636 kg
+Launch C3: 97.09396689316863 km²/s²
+||V∞_in||: 0.006234388602360108 km/s
diff --git a/archive/ES_0.5631317492764402 b/archive/ES_0.5631317492764402
new file mode 100644
index 0000000..773b7f1
--- /dev/null
+++ b/archive/ES_0.5631317492764402
@@ -0,0 +1,22 @@
+archive/ES_0.5631317492764402---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T09:01:34.457
+Launch V∞: [7.563400714758352, -6.085782133035659, 0.16806655676859514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.272117626039702e-6, 4.713376575674882e-5, -0.0008901308144612039] km/s
+ V∞_out: [-4.035455003207063e-5, 0.0008899880783940695, -1.1985300380886512e-5] km/s
+ time of flight: 1.7307892943731803e8 seconds
+ arrival date: 2029-11-02T14:30:23.457
+ thrust profile: [0.43918563765536256 -0.033353850662341415 -0.12404759701504431; 0.1640421395462435 0.08210150150539505 -0.1559413578731501; 0.06701677459187522 0.05566429355208943 -0.11257637888167565; 0.06392916123950984 0.06370621568896498 -0.14513918050780739; 0.04215909734736957 0.05631671368353784 -0.1285723941418666; 0.02563717962990285 0.04124232205764911 -0.10240324534244648; 0.01137197670435355 0.021445141139416035 -0.056837832595390804; 0.008810259425966267 0.02306906161565482 -0.06578090907866496; 0.006353344610210954 0.014836599208193073 -0.045428435545532254; 0.005287442451431477 0.013938610817303368 -0.04336111695516146; -0.0018590514002318175 0.002009464383136363 -0.003505228439887137; 0.00018974351092099846 0.0014637777939081852 -4.460519570401774e-5; 0.0018391357546652001 0.0018483178654620477 -0.003369385557176115; 0.0001337939693589508 0.00011558935116366025 -0.007551488495073173; -0.0007687912131121826 0.0036791085353000343 -0.005844236316629337; -0.0010370329376586554 0.0008840927208476283 0.0008360117294940925; 0.005468548998339206 -0.0005533667176032352 -0.01080034446397109; 0.0016748661463598042 -0.0029302399372449738 -0.0047719406655940795; -0.007509051563621296 0.002097419039304066 0.0062016128824493675; -0.0005521706367398779 -0.0008941600844652962 0.0015273218916352447] %
+
+Mass Used: 107.07858551250456 kg
+Launch C3: 94.27002091028724 km²/s²
+||V∞_in||: 0.000891399909236754 km/s
diff --git a/archive/ES_0.5631373829775117 b/archive/ES_0.5631373829775117
new file mode 100644
index 0000000..9b6d3e5
--- /dev/null
+++ b/archive/ES_0.5631373829775117
@@ -0,0 +1,22 @@
+archive/ES_0.5631373829775117---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T07:15:41.730
+Launch V∞: [7.745108310807945, -5.7044414978709925, 0.3376178083557261] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.212421485936389e-9, -2.434042813430446e-9, -1.5576179899451285e-9] km/s
+ V∞_out: [-2.6830399100776095e-9, 2.6641697601983377e-9, -9.442286585521622e-10] km/s
+ time of flight: 1.8367542909864882e8 seconds
+ arrival date: 2030-03-05T04:12:50.730
+ thrust profile: [0.5139395100356668 0.005014667925149693 -0.1201903552388667; 0.2782650835302048 0.18024396217476166 -0.22315342844656402; 0.060347808067759426 0.06550215779105921 -0.09807118773289797; 0.03474532368011236 0.051820580128696656 -0.0873065279544971; 0.02551701109414031 0.04903610349877046 -0.08906256543564761; 0.01590040661111791 0.03798583050342892 -0.07511706246954486; 0.010242781131159104 0.02959360636621911 -0.06274922086144123; 0.007047271967744909 0.0238105566074489 -0.052445870046358666; 0.0019905729488044438 0.009262078947006556 -0.021048765396380283; 0.0017584554269783506 0.007389734400918915 -0.018167396404509383; 0.002002208460313938 0.008344565954088464 -0.020990855549160258; -0.0024431030154077925 0.000703248028613731 -0.003144947602918655; -0.0038527327774091503 -2.8839360743215152e-5 -0.0015266130428407234; -0.0017943881127535834 0.0001778661954012215 -0.001997969463694316; -0.001599263098740522 0.0026206287265755 -0.002985475929575968; 0.0011596050679269713 0.0008887365941959756 -0.0028094840939327324; 0.0004978329682543666 -0.0006186460260233569 -5.450756002578147e-5; -9.248968550671253e-5 0.012291094725500232 -0.0015889603877137113; -0.0016458247279370719 -0.0026526973386693346 -0.001843804585430473; 0.0004884861504569798 -0.005437063685149834 0.005223111115852445] %
+
+Mass Used: 116.58578902952604 kg
+Launch C3: 92.64134133329787 km²/s²
+||V∞_in||: 4.320924672280097e-9 km/s
diff --git a/archive/ES_0.5631385347638227 b/archive/ES_0.5631385347638227
new file mode 100644
index 0000000..2873ce9
--- /dev/null
+++ b/archive/ES_0.5631385347638227
@@ -0,0 +1,22 @@
+archive/ES_0.5631385347638227---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T04:00:17.003
+Launch V∞: [6.018013745570062, -7.441962824920683, -0.028508982700458048] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.65949717103172e-9, 5.639370122855033e-9, 3.8284018801565926e-9] km/s
+ V∞_out: [-2.3961028459222574e-9, 5.4985506044111085e-9, -8.137543017017272e-9] km/s
+ time of flight: 1.8555904937173668e8 seconds
+ arrival date: 2029-03-16T20:11:06.003
+ thrust profile: [0.6351557884326726 -0.15917826167880403 -0.18862726099897262; 0.20625832245821982 0.061754980438145646 -0.1989678735212001; 0.06368405781738876 0.03773423453567815 -0.11033207638815483; 0.06727958999345864 0.054055463974631034 -0.16032720694277816; 0.03197976064065933 0.03165788980294202 -0.10216202534413066; 0.016507045845823822 0.01910908268831246 -0.06651242258569663; 0.010025559390981532 0.013206513861745211 -0.048695236363809784; 0.005372475607246087 0.007660998714260214 -0.02986053487136801; 0.006940520382456588 0.010338567162719841 -0.04652124218644896; 0.006080587384945944 0.010321803529316708 -0.043471037848912056; 0.0010723114743800667 0.0018422017186122237 -0.008312876707177074; 2.4288549600028433e-5 0.00013419012098323075 -0.0004269540628531149; 7.489015617615229e-6 7.120478106900532e-6 -8.422088077594434e-5; 2.83426658168513e-5 5.718572749572356e-5 -0.0003699913526802127; -0.00011843776685695453 0.00022288031124201565 -0.0003570207309973436; 1.5769803749870022e-6 -9.937041204911189e-5 -0.0002491244248688067; 4.5325208403649675e-6 0.00032199572373707455 0.0002892864297814556; 0.00041847579333255207 -0.00014011023614095362 -3.762299173925058e-5; 0.00019480730383130047 -0.00035077743835943093 -0.00011131415740128477; 0.00019109792004651826 -2.2963011230553614e-5 0.0002485478829796483] %
+
+Mass Used: 122.66096535757333 kg
+Launch C3: 91.60011289146625 km²/s²
+||V∞_in||: 7.736347709567203e-9 km/s
diff --git a/archive/ES_0.5631387800645726 b/archive/ES_0.5631387800645726
new file mode 100644
index 0000000..d528568
--- /dev/null
+++ b/archive/ES_0.5631387800645726
@@ -0,0 +1,22 @@
+archive/ES_0.5631387800645726---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:43:56.840
+Launch V∞: [6.5306238608384195, -7.339212027913128, 0.10470169018689765] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009455158866542761, -0.006309196662554632, 0.007889602951280607] km/s
+ V∞_out: [-0.0068522920317344435, -0.006368699112150813, -0.003923297036720079] km/s
+ time of flight: 1.874957778764526e8 seconds
+ arrival date: 2029-04-09T13:53:33.840
+ thrust profile: [0.36028276707923346 -0.09025651916084002 -0.12475709225331312; 0.04140038580046882 0.011283740973375072 -0.048465727832799205; 0.04521017455288981 0.023449325474893888 -0.08981000873603129; 0.039621392973134356 0.027575001325613198 -0.11005334240326768; 0.03779004803076468 0.03189543648224868 -0.13387645509237123; 0.02472679344118752 0.023753628324768496 -0.10777961026709763; 0.013765391470457225 0.013986103130528468 -0.07158040324940912; 0.012563973903126536 0.014430272805048504 -0.07519628170408753; 0.01584711483633977 0.01990615464569171 -0.10353141328687784; 0.003427531130368912 0.004539318846383426 -0.02639606738093806; 0.0006406396714334523 0.0009652877028459209 -0.006504400736877218; 0.0006060150018746325 -0.0022704560849378798 -0.0019954265683105425; 0.0006395398482014144 -0.0007757739091863495 -0.004016190028451423; -0.001221593741264679 0.00021085687718897406 -0.00026442060784496123; -0.0009462973275929885 -0.0010068858262723451 -0.0013423314372314286; 0.003624723141331373 -0.0025372018921429582 -0.0006754188739975372; 0.0005837131960304275 0.0014607233380703006 -0.0021166418907257404; -0.00037567881675878534 -0.0011370678993615603 0.0038023569191625237; -0.002866938577299704 -0.0001040415005190435 0.0010305452299896908; 0.0018127160545956603 0.0011391544016025458 0.005444292170886402] %
+
+Mass Used: 93.9383221383232 kg
+Launch C3: 96.52404364634482 km²/s²
+||V∞_in||: 0.010146220850521725 km/s
diff --git a/archive/ES_0.5631403985984627 b/archive/ES_0.5631403985984627
new file mode 100644
index 0000000..0a045c4
--- /dev/null
+++ b/archive/ES_0.5631403985984627
@@ -0,0 +1,22 @@
+archive/ES_0.5631403985984627---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T13:38:21.158
+Launch V∞: [6.4226731963173425, -7.678284206159425, -0.05474095354976099] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011859103011865026, -0.0003662021147496042, 0.008856882889335477] km/s
+ V∞_out: [-0.01419833870586378, 0.00013883325423149503, 0.004193473263725734] km/s
+ time of flight: 1.809203485145635e8 seconds
+ arrival date: 2029-01-24T13:17:29.158
+ thrust profile: [0.061570234559453804 -0.020356331311062296 -0.027394317265341514; 0.03965466085304665 0.005812214432066018 -0.05144151863742983; 0.0386770221972752 0.013090259959421048 -0.08303240082487709; 0.06000265925098331 0.027649546987385695 -0.17240475863759366; 0.049581968832447115 0.026913520318714967 -0.18023638091250732; 0.026731575520830633 0.01589831944706889 -0.11981872497684545; 0.024261410038258217 0.015856202168346132 -0.1260274737926133; 0.008656559691985276 0.006258112777299956 -0.0533058948820863; 0.00948055720103211 0.006678075567504091 -0.06259990121771841; 0.0012808956290852164 0.0010409196089788775 -0.010106175027331486; 0.0020527026045108216 0.00102108482092573 -0.018323217493909787; 3.1601663024984766e-5 3.502272103345761e-5 -0.00030105264201264027; 6.4073760135454e-5 0.0001255819530441597 -0.00044537352025355475; -3.0444290775113482e-5 4.321157134829488e-5 -0.0003326486899640284; 2.169741404204757e-5 0.00010098533616124868 -0.0002695816578859818; 0.00019437090721700911 8.289205636891062e-7 -0.0001255168192746938; 0.0003767522729381086 0.0004133121665881494 6.455905014356037e-6; 0.00011542348054990978 -0.00016189227960509322 -0.00012841141688303004; -0.0003350414220344559 0.0001664469573420226 0.00013545112257822337; -6.721839988223824e-5 0.00042710027347691123 0.0011730215298246353] %
+
+Mass Used: 72.44010556093781 kg
+Launch C3: 100.20977590924605 km²/s²
+||V∞_in||: 0.014805971861052442 km/s
diff --git a/archive/ES_0.5631405587952194 b/archive/ES_0.5631405587952194
new file mode 100644
index 0000000..4176105
--- /dev/null
+++ b/archive/ES_0.5631405587952194
@@ -0,0 +1,22 @@
+archive/ES_0.5631405587952194---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T21:26:40.787
+Launch V∞: [6.6310937647573835, -7.455627721417201, 0.06879906718630574] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.538278062952037e-9, -1.2999578140784139e-8, -6.895233540578338e-8] km/s
+ V∞_out: [4.844091917809001e-8, 4.5406690124123544e-8, 2.2118401380231487e-8] km/s
+ time of flight: 1.874957778742449e8 seconds
+ arrival date: 2029-04-10T23:36:17.787
+ thrust profile: [0.09696139183771493 -0.02434277206849596 -0.038182979628527465; 0.05577254945358399 0.01421607283077919 -0.06554217195743257; 0.046988171489498014 0.023529954826436654 -0.09222133226841196; 0.0382717968588635 0.025016075938364673 -0.104690078752393; 0.03731964448072597 0.029204694819375026 -0.1287837654186437; 0.028628914722370703 0.02575481445476479 -0.12156256518736572; 0.03669912570097276 0.03937448894823461 -0.18400811399049385; 0.011105860364686283 0.012330024499909425 -0.066420179359868; 0.004889778095893908 0.005769972015693283 -0.03409819778173859; 0.0008856383596838259 0.0010604741706513971 -0.006504849311587181; 0.000699887744291498 0.0007426236136424398 -0.0053167898187596995; -2.0027731355129767e-5 0.0004899987884251918 -0.0034913703757238823; 0.0012164628135305504 0.00039084518440426076 0.00042356040813611314; 0.004002229133448739 0.0015793545534951306 0.0028741436297189376; -0.00029326108831570225 0.0009428317879205247 0.002695798244052193; -0.004240045722101361 -0.0002058410507371113 0.0021169730646280597; 0.005759773560869947 -0.0033047877364730228 0.0009877085808616807; -0.004192789314789347 -0.004739630266133289 -0.0009447506496724014; -0.0007631617227470307 -0.00026920435697714716 -0.000666704217212458; 4.9993341030818826e-5 0.0017249438819798 0.0018039851413547284] %
+
+Mass Used: 76.2159370585041 kg
+Launch C3: 99.5625225490146 km²/s²
+||V∞_in||: 7.068462196284485e-8 km/s
diff --git a/archive/ES_0.5631541337471648 b/archive/ES_0.5631541337471648
new file mode 100644
index 0000000..cf3b109
--- /dev/null
+++ b/archive/ES_0.5631541337471648
@@ -0,0 +1,22 @@
+archive/ES_0.5631541337471648---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T10:15:36.186
+Launch V∞: [8.057456182719951, -5.814300090507125, -0.9839778099364864] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.730828734812961e-8, -1.6323990009686132e-7, -1.4617612377906156e-8] km/s
+ V∞_out: [1.2702858683507388e-8, -8.987924555199743e-8, -1.694216902560873e-7] km/s
+ time of flight: 1.874957778746406e8 seconds
+ arrival date: 2030-04-26T12:25:13.186
+ thrust profile: [0.22059453526628856 -0.011692280533738875 -0.09028772319673939; 0.02288446861038553 0.011033300009340004 -0.032652585624917824; 0.03009134822428732 0.02259941890387342 -0.0793025436217723; 0.029635139739842636 0.02859235929764178 -0.11481593413618293; 0.0194050920581156 0.02133059154285051 -0.10120437568823154; 0.013132885114972466 0.016763118726146515 -0.08605520929070115; 0.00964326642633863 0.013397114324515586 -0.07839958590260701; 0.0058440664910317614 0.00835092640054498 -0.05134429539716217; 0.002735395032713971 0.004507171713597547 -0.02853786724786394; 0.007224989508246133 0.013893333213976813 -0.09154285751438873; 0.003810649885601209 0.004833648278898446 -0.03484493259417903; 0.0008037146940381853 0.0014806092497784322 -0.011707821031091; -0.0016891488465155613 0.0011186576446593935 -0.0017984273750997182; 0.0013246290148885265 0.0002756741983067084 -0.001683530965331389; 3.681163503947966e-5 -0.0003507470360662899 -0.001331535876575103; -0.0006272211711308993 -0.0015676373622859358 -0.0011457351276334678; -0.0024698561813457755 0.0018967861720669684 -0.00019098008779109025; -0.004204885068747053 -0.0013886784891763673 -0.003511188208338398; -0.0005921504320059915 0.00034806820896609626 0.005138552260669954; -0.0016885747312671774 -0.002552963878092977 0.0004810672501678059] %
+
+Mass Used: 75.44791765036416 kg
+Launch C3: 99.69689800937054 km²/s²
+||V∞_in||: 1.9060388863265655e-7 km/s
diff --git a/archive/ES_0.563159955773041 b/archive/ES_0.563159955773041
new file mode 100644
index 0000000..6b8ea5e
--- /dev/null
+++ b/archive/ES_0.563159955773041
@@ -0,0 +1,22 @@
+archive/ES_0.563159955773041---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:46:15.238
+Launch V∞: [7.604654889588338, -6.15616652446283, -0.02856248727040441] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.730070504992133e-6, 2.1685928739027514e-5, 6.230041478496162e-5] km/s
+ V∞_out: [6.488484313611591e-5, 8.42203964518479e-6, -1.1731520953235242e-5] km/s
+ time of flight: 1.688762463863114e8 seconds
+ arrival date: 2029-09-14T09:50:21.238
+ thrust profile: [0.407828178668456 -0.04633285625597172 -0.12887350706656356; 0.06372690463291612 0.029031032098792386 -0.06369918809836812; 0.0495987625174646 0.0393277843756534 -0.08512069797530251; 0.03361014689699962 0.034518306127855204 -0.0831136089013573; 0.02184273087893954 0.027889877879134828 -0.07162733300906063; 0.06659822385035012 0.09276626350674973 -0.22828911670080257; 0.03209467709499493 0.061604633486439214 -0.1627745432224924; 0.014416008455267042 0.029529865382285036 -0.08373423826352897; 0.015569094537812779 0.031278359279401695 -0.09492330667329066; 0.0011908989803054817 0.0029801261905659506 -0.009651396874565083; 0.000776299056316261 0.0019724425063837076 -0.007263949720467544; 0.0009585276203331177 0.004407998198872717 -0.013854695610659875; 1.5195518079622623e-5 4.1297639009047385e-5 -0.0004092029122109047; -4.01539203662765e-5 -0.0002442116660720318 -0.0006742194878246971; -0.00013032503520264376 0.0004947625731406901 -0.0006952565197683493; 0.00019264921036088627 0.00041417824587050025 5.1591265537303925e-5; -0.0002442026155408226 3.6542980545303593e-7 3.239720884248698e-5; 3.0366376125269128e-5 7.933195289199376e-5 -4.616386470036082e-5; 0.00011680268676918 -0.00017443069078498116 0.00025705335236930185; -5.071286000997949e-6 -0.00025473701481238883 -0.00044165848610841366] %
+
+Mass Used: 98.59507625492324 kg
+Launch C3: 95.72997808233565 km²/s²
+||V∞_in||: 6.654198162569685e-5 km/s
diff --git a/archive/ES_0.5631620704129955 b/archive/ES_0.5631620704129955
new file mode 100644
index 0000000..5b0b932
--- /dev/null
+++ b/archive/ES_0.5631620704129955
@@ -0,0 +1,22 @@
+archive/ES_0.5631620704129955---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T12:46:00.438
+Launch V∞: [6.627087505348449, -7.485852547697737, -0.03379489482806883] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.831566610435265e-9, -1.7871925404723802e-9, 3.86936765578676e-9] km/s
+ V∞_out: [1.3821281814848198e-9, -2.573837627547209e-9, -3.76890650538997e-9] km/s
+ time of flight: 1.857307049772251e8 seconds
+ arrival date: 2029-03-21T04:37:44.438
+ thrust profile: [0.09339732419799804 -0.025165412331659847 -0.03601845676995913; 0.009983058778325279 0.0022224792724867813 -0.012355518398029995; 0.03409103842098043 0.016287717766769346 -0.06629758725728477; 0.04539694868066186 0.027912712154397303 -0.11917061192302038; 0.03553493169399356 0.026017085735203133 -0.1190931352553749; 0.05213120154620085 0.044792074506572646 -0.20903582433417855; 0.028200154067404722 0.025660230346777897 -0.13271056711115706; 0.0033658486855484278 0.0031644022341561365 -0.019392170871917396; 0.0012044622769157983 0.0019486916881249745 -0.010164380358484229; 0.010836313241179969 0.015244041084205132 -0.09022192289866253; 0.008418160023128769 0.009340958009756992 -0.050266244630466125; 0.00012558611951037145 -5.6262075126508e-5 0.00028972091026551903; -0.00013798100506919254 -0.00019325735808769752 0.0006186625849547065; 9.894426058584975e-5 -0.0005043203705570607 0.00010813443185504843; 0.0006066906178926811 0.0007915907435109189 0.00032510158678100936; 0.00040009661960563835 -0.0007976746040913485 0.0020228534007063924; 0.00015499626978503407 -0.0008398693488706037 3.753178579915062e-5; -0.001345528786121868 0.0006657972060341273 -0.0027162322640379697; -0.0018003662569086832 -0.0019183452819695166 0.0011557507077579823; -0.00029973478570495256 -0.00020047200641915269 -0.0026044370485844084] %
+
+Mass Used: 73.93746977320916 kg
+Launch C3: 99.95741926433467 km²/s²
+||V∞_in||: 6.442833161229752e-9 km/s
diff --git a/archive/ES_0.5631683845503281 b/archive/ES_0.5631683845503281
new file mode 100644
index 0000000..a81ce20
--- /dev/null
+++ b/archive/ES_0.5631683845503281
@@ -0,0 +1,22 @@
+archive/ES_0.5631683845503281---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:52:32.938
+Launch V∞: [6.590032004226071, -7.335153235727501, 0.12472666188473963] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.208308090374383e-6, 1.1328011816885617e-6, -2.5100858041923795e-8] km/s
+ V∞_out: [-1.5535934971923521e-6, 3.5764293563765574e-8, 8.139066755021042e-6] km/s
+ time of flight: 1.8749577787490317e8 seconds
+ arrival date: 2029-04-09T03:02:09.938
+ thrust profile: [0.271756587090507 -0.0678270636691626 -0.09458632461437222; 0.06345096998637866 0.017513940107550533 -0.06873177804673757; 0.04429175901232273 0.023508168582608843 -0.08129041828627553; 0.05106231352009632 0.0363365966504865 -0.12924378052388547; 0.05104526897080985 0.043870392542110205 -0.16455744368091169; 0.0348882353131838 0.03449176169712434 -0.13819277112204686; 0.020861630540687872 0.023021750782057916 -0.0987786404612022; 0.005025249436310376 0.005795998402508726 -0.02657773751364216; 0.002649053043041942 0.004219910328774574 -0.01990243256660008; 0.006259055236265653 0.008954928244339305 -0.04493624020235442; 0.0025377828254099025 0.0019766026187236488 -0.008085208258695395; 5.550809498361105e-5 0.0007076367994674508 -0.0037867098984655165; -0.0018369611831539382 -0.0019475695738977944 -0.00384625928525077; 0.0012627334214204676 -0.00012011277062342902 0.002951608278569828; 0.0024433382993677283 0.002762103225986908 -0.0041453572051050195; 0.0007176975684173399 -0.002041163438039808 -0.0027655979750495704; 0.0010537269723603013 -0.003789149317379013 0.0019518003016363147; 0.0005425217559371279 0.0001776814790578172 -0.00046038084345223626; -0.0033261268119070646 -0.001755642546633156 0.0021608859282521513; 0.0019516117783576934 0.005362525489784542 -0.009115946094655169] %
+
+Mass Used: 89.74656460906044 kg
+Launch C3: 97.24855154851241 km²/s²
+||V∞_in||: 8.286144475980069e-6 km/s
diff --git a/archive/ES_0.5631684681684299 b/archive/ES_0.5631684681684299
new file mode 100644
index 0000000..320a985
--- /dev/null
+++ b/archive/ES_0.5631684681684299
@@ -0,0 +1,22 @@
+archive/ES_0.5631684681684299---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:44:32.280
+Launch V∞: [6.54136062583993, -7.507570410839597, 0.08745699705452055] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2140279871796328e-7, -8.951478343198728e-7, 5.265478605765991e-8] km/s
+ V∞_out: [-3.6311961775497537e-7, 7.533504144278775e-7, 8.385947679538363e-8] km/s
+ time of flight: 1.8534801174318132e8 seconds
+ arrival date: 2029-03-16T17:18:03.280
+ thrust profile: [0.12191597891433945 -0.034027806568330723 -0.04849149285351178; 0.07035856042985945 0.014604972694922823 -0.0813291847130154; 0.04541288299186191 0.020684349478521154 -0.0900350236782605; 0.0412431003585591 0.024688759935514316 -0.11461403376744976; 0.03217522411610387 0.02300068983976198 -0.11684380116339016; 0.04918048294570242 0.03478106825449322 -0.1940038851995836; 0.015375397094890735 0.01212931231935848 -0.07039619299390036; 0.013691651562617268 0.012819578724888104 -0.07822435303618527; 0.011680326594734211 0.010807185553875968 -0.07060819182306745; 0.0008716009411095732 0.0015045329277874825 -0.009491905893680333; 0.00024492530962952753 0.00034600544527746207 -0.0065222863080634476; 0.001328960588718153 0.00019999838787925178 -0.003200366514788064; 0.0008047929490677056 0.0011133271947106967 0.00033396341212960524; 2.8366443059498424e-5 -0.0006315876987399377 0.0007935002157606794; 0.0012072923929871936 -0.00017260734351780025 0.002343954394820157; -0.000182088868795479 8.867292626368845e-5 -0.0007340484204919303; -0.0032441388547165004 0.0006651626581790307 0.0027459067022193788; -0.0034370011105794083 -0.0018613938029810766 0.0013915961424169417; 0.004423759336467452 -0.0016428409629927216 0.0036028669761971393; 0.00026935121467162133 0.00031115839219383293 0.0012588908623922639] %
+
+Mass Used: 78.59269014536903 kg
+Launch C3: 99.16066103733701 km²/s²
+||V∞_in||: 9.048761303730421e-7 km/s
diff --git a/archive/ES_0.5631691791746974 b/archive/ES_0.5631691791746974
new file mode 100644
index 0000000..536987f
--- /dev/null
+++ b/archive/ES_0.5631691791746974
@@ -0,0 +1,22 @@
+archive/ES_0.5631691791746974---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T09:21:45.083
+Launch V∞: [7.581662881160417, -6.356410347123624, -0.13368285133000513] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005721990173241095, 0.00045009934543142394, -0.00034429899160374046] km/s
+ V∞_out: [0.00013849023067314076, 0.0007925280458677537, -3.5233938312438415e-5] km/s
+ time of flight: 1.669887562294303e8 seconds
+ arrival date: 2029-08-26T03:07:41.083
+ thrust profile: [0.22389308193226465 -0.038332208765689206 -0.08835554344633745; 0.06768618473689957 0.02176241331339233 -0.08509616501720252; 0.05749214942652103 0.03221900888051219 -0.12315134050037431; 0.07808613863145196 0.05548832495040816 -0.227167473896806; 0.03861963769553482 0.03200046853133272 -0.14896849513616106; 0.02967487018131129 0.02758551432216473 -0.1394976580643196; 0.011362633570404476 0.011200559618392752 -0.06525741389479388; 0.010108134947882113 0.010626416990301875 -0.06543266871564066; 0.003245574165990593 0.00341826372703292 -0.022473820951367247; 0.008059776613078025 0.00980059469778583 -0.06587050342754872; 0.0004135597694353161 0.0005461078701933205 -0.001606145340730105; 6.195296261722221e-5 -0.0004034712724574895 0.0011218121316940856; 0.001147462762431178 0.0003054301265196535 0.0001726765094716752; -0.0016682898238202617 0.0006454340195400017 -0.0007029978453541785; 0.0027035494472337647 0.0005297294932802359 0.001010302719249418; 0.00024051403720247346 -0.0002270281498125352 -0.003030213450612263; 9.704368370235656e-5 0.00018912267169546768 0.0019077952075495794; -0.0007288848673578556 0.001777879502353157 0.0022176217410055116; -0.0011689827984765642 0.004737265631793743 0.0011642101021314818; -8.264442501660443e-6 -0.0014196365417741765 -0.002404993892148477] %
+
+Mass Used: 85.92733441608061 kg
+Launch C3: 97.90343564932567 km²/s²
+||V∞_in||: 0.0008053216325194707 km/s
diff --git a/archive/ES_0.5631717370673834 b/archive/ES_0.5631717370673834
new file mode 100644
index 0000000..0295d5f
--- /dev/null
+++ b/archive/ES_0.5631717370673834
@@ -0,0 +1,22 @@
+archive/ES_0.5631717370673834---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:00:14.604
+Launch V∞: [6.63608498968559, -7.3773098824445, 0.19724012595319512] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009554472567638549, -0.00022148480493405166, 0.0050553075340329275] km/s
+ V∞_out: [-0.01038126923267872, 0.0001011509823767678, 0.0030124586221626512] km/s
+ time of flight: 1.8749577787179473e8 seconds
+ arrival date: 2029-04-09T08:09:51.604
+ thrust profile: [0.16374593791905098 -0.03662932527888424 -0.05667453061259569; 0.059931324366184986 0.019413607687620595 -0.06462602768420035; 0.05300952720985926 0.03112882122768177 -0.09455417878560998; 0.040412674564895314 0.031844501988647834 -0.09923808303454906; 0.06329565399833327 0.05974603368053414 -0.1891885013619695; 0.021505105630123797 0.024198423202837924 -0.08551316548909454; 0.03226710765414521 0.04034710196777568 -0.14879455450752102; 0.00895298145616628 0.012256504145248065 -0.04977036383549332; 0.005366421351334816 0.0078057598299107345 -0.033273597664847165; 0.0027601924846982996 0.005094278553943565 -0.021852362507566614; 0.0003216879508842885 0.0002736545451716846 -0.0040891073410365165; -0.00035148173462568435 -0.0006213809980483748 -0.0046286574616072156; 0.0001242031496007428 5.7845807073120194e-5 -0.0005885398439326615; -0.0013484252823038865 0.001530093526285181 -0.0004977187133194355; -0.0025513283061184876 0.0028435133779649026 -0.003090507202663161; -0.0011420248642999885 0.0009117107995952722 -0.0002859185389744439; -0.0007957915535173842 -0.001686376117527916 0.0010031591907805146; 0.0006678184376227815 -0.00034033401650799145 -0.0015880942625144043; 0.006990280892015251 0.001866278319633314 -0.010169087918147796; -0.010531724733221523 -0.00263853409417995 0.004242165570564805] %
+
+Mass Used: 82.44319214977395 kg
+Launch C3: 98.50122875922972 km²/s²
+||V∞_in||: 0.010811712899824168 km/s
diff --git a/archive/ES_0.5631762693257443 b/archive/ES_0.5631762693257443
new file mode 100644
index 0000000..e635190
--- /dev/null
+++ b/archive/ES_0.5631762693257443
@@ -0,0 +1,22 @@
+archive/ES_0.5631762693257443---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T00:11:24.140
+Launch V∞: [6.654535081449743, -7.476195411393045, 0.10182438635768579] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.4794950534937e-10, 5.197163372336975e-10, 4.1702711642406826e-9] km/s
+ V∞_out: [-1.5138105997257912e-9, -1.4710060256562696e-9, -7.16747744498388e-10] km/s
+ time of flight: 1.8585437657614055e8 seconds
+ arrival date: 2029-03-23T02:24:20.140
+ thrust profile: [0.07164440567993972 -0.02226868262519648 -0.030633606031891587; 0.030869883511769246 0.005170446188712489 -0.041044992283875696; 0.047108964725087146 0.015501096276613991 -0.10153080352607341; 0.04976639809510113 0.0208738265725608 -0.14596497988525098; 0.043914726213616785 0.021076130130952803 -0.1622300809896319; 0.0297012015198798 0.01569516852389515 -0.13331973437813444; 0.02298293445539959 0.013025167251212173 -0.12037516459494564; 0.00932970633558027 0.006448971372051322 -0.05888566494402348; 0.001995727496473356 0.001172148274359967 -0.013286820273830121; 0.004439947571045837 0.0023044264635066996 -0.031073065923594344; 0.0005980023640962116 0.000442524927347779 -0.005292142979743022; 0.001201166559505769 0.0028112602835699135 -0.0028922511384899493; 0.00021091679098341842 0.00014712628737982423 -0.0033045137480163483; -0.0023517078993021347 0.0023573115535544566 -0.009130503138164131; 0.00016040567447537482 -3.2172479757040155e-5 -0.0015778071156466967; -0.00035133130042566793 -0.003643492170518861 0.004788886603281122; 0.0003737344797113994 9.076418056735676e-5 -0.0008241352250770327; 0.00028235876807621203 -0.00041454100156782707 -0.0004143780854697234; -0.0006519626951040276 -6.64309809606278e-5 0.001022377244431087; 0.0013797575648492925 0.011807992256418818 0.0011564705183883125] %
+
+Mass Used: 72.6165456328199 kg
+Launch C3: 100.18670318523687 km²/s²
+||V∞_in||: 4.26857061755306e-9 km/s
diff --git a/archive/ES_0.5631885467145188 b/archive/ES_0.5631885467145188
new file mode 100644
index 0000000..e7a3c54
--- /dev/null
+++ b/archive/ES_0.5631885467145188
@@ -0,0 +1,22 @@
+archive/ES_0.5631885467145188---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T21:07:41.078
+Launch V∞: [6.349851203579913, -7.695571727527363, -0.009439582039652854] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.951484429893551e-8, 7.210688759399152e-7, -4.095190247002262e-8] km/s
+ V∞_out: [2.6283268294878995e-7, -5.985129053220882e-7, 3.2684339230442677e-7] km/s
+ time of flight: 1.818347264807694e8 seconds
+ arrival date: 2029-02-04T10:46:27.078
+ thrust profile: [0.08197407806811528 -0.026019403577427217 -0.03431493603730875; 0.08928919134813008 0.01430147242510331 -0.10536371455590512; 0.04132893855186884 0.015072537554735397 -0.08411044854997941; 0.06916730194082363 0.034492111961321494 -0.1871127790876355; 0.06359156326574368 0.0356507233532432 -0.21957493502530748; 0.022918613543723876 0.014932086327024658 -0.09771660270257432; 0.014896485674165124 0.010431002339795938 -0.07511580407885546; 0.008227705678620398 0.006005820841024647 -0.04777723204203196; 0.007545409428384086 0.005868387528663581 -0.04811672617542692; 0.0007534498583028426 0.0007893750024556547 -0.005693019923021068; 0.00010528733158820322 0.00016542287961106845 -0.0007281733004560807; 0.0003350223168702508 8.26355289503303e-5 -0.0020356984396091124; -0.0006306968732497259 0.0003189494058693951 -0.0003092256061956538; -9.890794170257465e-5 -0.00016724215125346717 -0.00045731582208612034; -9.800665795805091e-5 -0.0016775493995367537 -0.0008719617968013947; 0.001470419722126943 -0.001004565708651265 0.0010570458707304972; -0.0017605045024639394 -0.0007805929648108289 0.00021507081857655857; -0.0004876505109557319 1.614269289574811e-5 -0.0005348019131464199; 0.0008607234327363893 0.0006923043079423686 -0.0001458042229449685; 0.00035630139010285866 0.0001036408865991436 0.0004132856402330922] %
+
+Mass Used: 76.38858334374709 kg
+Launch C3: 99.54252362683283 km²/s²
+||V∞_in||: 7.290545839654316e-7 km/s
diff --git a/archive/ES_0.5632059488747134 b/archive/ES_0.5632059488747134
new file mode 100644
index 0000000..a34213d
--- /dev/null
+++ b/archive/ES_0.5632059488747134
@@ -0,0 +1,22 @@
+archive/ES_0.5632059488747134---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T05:16:45.187
+Launch V∞: [8.093650411325152, -5.361249343199949, 0.26145978268792236] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0018045495322919277, -0.0009939335968760683, -7.219500711037565e-5] km/s
+ V∞_out: [0.001424150793069293, 0.0008954922029882007, -0.0011929427843803515] km/s
+ time of flight: 1.874957778741413e8 seconds
+ arrival date: 2030-04-18T07:26:22.187
+ thrust profile: [0.5398357849174693 0.006910646741517628 -0.1429164604040862; 0.1451815689971349 0.09666887879839994 -0.1428094058421563; 0.05694285153262537 0.06289976394412948 -0.10779129035130924; 0.032649435310912196 0.04905341400213402 -0.09509931608220515; 0.024438758897384137 0.04705098507048967 -0.0995362555252273; 0.010285898906221386 0.023990169438563212 -0.0560425806332443; 0.008615234275133285 0.024302035572642704 -0.06192234191170866; 0.00792391059516295 0.027706120701031078 -0.07177557116793766; 0.0030200552007363444 0.014966196648744167 -0.041144854130330366; 0.0005475826843738421 0.003068023584399395 -0.009161839304317002; 0.00017749278194789545 0.000694669278398923 -0.00111362660857567; -0.0007654236168167179 0.0020975887561238142 -0.004166442021286558; 0.0008041840511218831 0.0013499365386923311 0.00019925903020037933; 0.0004263638503491671 -0.0004931160236271478 -0.0009432953460347376; 0.0003258042228350772 -0.0005253230225787711 0.002035839260173775; -0.0001943807159224465 -5.655911211515578e-5 0.0033861575119249593; 0.0011321676140984794 -0.001607693319400457 -0.000912036642055741; -0.0014468945792160894 -0.004058048425168648 -0.0009452911555603235; -0.0001441059609940585 -0.0009818676292299795 -0.00028814688087243747; 0.0017209033792394165 -0.0027068666372608184 0.002633651333915376] %
+
+Mass Used: 106.88216616159707 kg
+Launch C3: 94.3185327186689 km²/s²
+||V∞_in||: 0.0020614352108532736 km/s
diff --git a/archive/ES_0.5632064816077689 b/archive/ES_0.5632064816077689
new file mode 100644
index 0000000..7db1494
--- /dev/null
+++ b/archive/ES_0.5632064816077689
@@ -0,0 +1,22 @@
+archive/ES_0.5632064816077689---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T07:40:19.494
+Launch V∞: [6.5836896033927665, -7.4336531656392655, -0.14244938249009437] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.590353577817574e-9, -1.8006579013208238e-10, -6.409406432292372e-9] km/s
+ V∞_out: [-1.144027943247962e-9, 2.538482073548494e-9, 3.865322436706133e-9] km/s
+ time of flight: 1.8461147474278122e8 seconds
+ arrival date: 2029-03-06T00:38:13.494
+ thrust profile: [0.13206042322993417 -0.034593863689057834 -0.047003615460028; 0.0570440948168637 0.015119868342545643 -0.061872683368347926; 0.07026545554194602 0.03625890655018008 -0.12285884008214602; 0.07118561964387853 0.049879516931987486 -0.17017809957538235; 0.0599559368900653 0.051523810356970616 -0.18328724430475615; 0.040759367134489195 0.041425316102795644 -0.14897637231467695; 0.012876710729672662 0.014764940220490078 -0.06079310032126097; 0.005176284742985457 0.006345691509829238 -0.028295305067372448; 0.004211296699226325 0.004890681409036533 -0.029220959857674908; 0.0012748861651580966 0.0031683700592288486 -0.012922542335425564; 0.0017044180699399719 0.002780515107016904 -0.014118843157553827; -0.0016241293318635802 0.00035321947392515064 -0.004681660096316494; 0.0019632161812807385 0.0008132012722453624 -0.000746533382025518; 0.00376159914951089 0.0010350228867981176 -0.005792282872324496; 0.0028169410959996612 4.941203849162263e-5 -0.0026969263671982177; 0.00015157907811850992 -0.00010215093073899636 0.002041328354926892; -0.003553125984836423 -0.0017861697351650892 0.0018504157659181581; 0.0005070155951975489 -0.000288128761437159 0.0005068055514630618; -0.005100951848916927 0.0014467244214078608 -0.006022604310328913; 4.930717142564707e-5 0.0012374984648269491 8.661094462505091e-5] %
+
+Mass Used: 81.76487849915748 kg
+Launch C3: 98.62446000741248 km²/s²
+||V∞_in||: 9.194872200511523e-9 km/s
diff --git a/archive/ES_0.5632079571756331 b/archive/ES_0.5632079571756331
new file mode 100644
index 0000000..dc07ece
--- /dev/null
+++ b/archive/ES_0.5632079571756331
@@ -0,0 +1,22 @@
+archive/ES_0.5632079571756331---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T05:42:14.646
+Launch V∞: [7.826038627694727, -5.938093379109502, 0.15306708513116973] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002268273784565539, -0.00046555357573279017, -0.02565735377410132] km/s
+ V∞_out: [0.022956395070096412, 0.010367316148625206, -0.005364910950017337] km/s
+ time of flight: 1.7831229521400425e8 seconds
+ arrival date: 2030-01-05T00:53:49.646
+ thrust profile: [0.3547085223175926 -0.0228169190987891 -0.11224861299468195; 0.05206092290396762 0.025783316805240257 -0.060442448379300344; 0.03005990668455531 0.02422589214754813 -0.06224484475892359; 0.04179879761806115 0.04567071415791219 -0.12579328371526355; 0.017929875470878872 0.022600052904775406 -0.07070780350586868; 0.035056219425109184 0.05296242220449775 -0.16463071112232908; 0.014611974600227336 0.02489560188037162 -0.08697810113969383; 0.010361681919794894 0.018956836691069325 -0.0734287725459715; 0.009025060474849076 0.01816362129872439 -0.07192105751544818; 0.00525944169827975 0.010904874683109786 -0.045342335377255946; 0.003668344425133015 0.00775643656188526 -0.034948622785036625; -0.0007221333114597094 -0.000683543854319638 -0.002425640412144024; -0.0004152095325902442 0.004311035040298183 -0.0013301401150473886; -0.0012226246471492479 0.00029359169943732983 0.000827347097432235; -0.0005369412667542756 -2.6140690109712232e-5 0.0034478133436436145; -0.0010884306616099958 0.0008901431914936858 -0.0006400101751793969; -0.0027850264382699857 -0.0036949720325292687 -0.0029906154209459273; 0.0022227199244263178 -0.006206218199189763 -0.0028576628311034074; 0.002965973402759761 0.006967091153917564 0.01753942711860539; 0.006072358677208723 0.023058205764701495 0.017208162235702887] %
+
+Mass Used: 93.97691520806165 kg
+Launch C3: 96.53126311374461 km²/s²
+||V∞_in||: 0.0257616305536551 km/s
diff --git a/archive/ES_0.5632153195201067 b/archive/ES_0.5632153195201067
new file mode 100644
index 0000000..3203802
--- /dev/null
+++ b/archive/ES_0.5632153195201067
@@ -0,0 +1,22 @@
+archive/ES_0.5632153195201067---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T12:16:22.944
+Launch V∞: [6.476450260680268, -7.404085578579114, 0.08484792741443282] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012639343043457872, -0.006867918533672989, 0.017126780488895543] km/s
+ V∞_out: [-0.014324723191014107, -0.006130725950698167, -0.016045534467236455] km/s
+ time of flight: 1.8749577787476388e8 seconds
+ arrival date: 2029-04-09T14:25:59.944
+ thrust profile: [0.24347465061087678 -0.06022815872990352 -0.08670952556700642; 0.14202074640341558 0.038932991864560486 -0.1508499983626363; 0.10179777321662796 0.053685930096216 -0.18463763701283747; 0.04225633306492262 0.02965523066018847 -0.11170510331604627; 0.024194610049149502 0.020596327226186463 -0.08328335452878437; 0.0186909226702122 0.01847911885553049 -0.07962190368604757; 0.019558127485017302 0.02110716255466874 -0.09846692987810406; 0.007032888433944956 0.007746240155328768 -0.03949254011721602; 0.0062802251113083804 0.008110223767571301 -0.04170763650185781; 0.0017900526972474081 0.002598352363593772 -0.014728570566581042; 3.742815827189553e-5 0.002440359860713531 -0.004324279155096365; 0.0027079540336517284 0.0020647284670787043 -0.00764994875403217; -0.0008675681821630143 0.0009091304628340004 -0.0024972807863611352; 0.0016205394348438686 -0.002889770287820101 -0.006357976788262948; -0.00027883540764907233 -0.0007598651718866358 -0.0005517948324946648; 0.0021005053491491635 -0.0039113040182565265 -0.003263650613038844; -0.0005740256398901507 0.0001437221045167323 0.0005327248539537871; -0.0027634991734568873 0.006355224709329442 -0.00026134442757166037; -0.0014375381242706362 -0.00040708133092743357 -0.0020809278654318874; 0.001998569244112714 -0.0038196315012768546 0.007560779207475504] %
+
+Mass Used: 92.5806787456022 kg
+Launch C3: 96.77209040477524 km²/s²
+||V∞_in||: 0.02236622246760031 km/s
diff --git a/archive/ES_0.5632166600066009 b/archive/ES_0.5632166600066009
new file mode 100644
index 0000000..8e030c3
--- /dev/null
+++ b/archive/ES_0.5632166600066009
@@ -0,0 +1,22 @@
+archive/ES_0.5632166600066009---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T00:38:23.655
+Launch V∞: [7.886808400772277, -5.835513385622918, 0.12414801704058981] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.101436037214009e-6, 0.00011960440059116529, 2.159719770100945e-6] km/s
+ V∞_out: [0.00011583927716108285, -1.748833414932342e-5, 2.4075767066390223e-5] km/s
+ time of flight: 1.7632702464786416e8 seconds
+ arrival date: 2029-12-09T20:22:07.655
+ thrust profile: [0.3422021135091869 -0.021558773488609715 -0.09399813467622022; 0.10012702278094629 0.0537174631006758 -0.09933406998687778; 0.06597989938949345 0.057021350608751846 -0.11551436206624674; 0.03728445551460797 0.04305538676324643 -0.09686158386574564; 0.03347454667531287 0.04650856229465625 -0.11197255835824736; 0.02598743062263788 0.04363751076153138 -0.11032335444580063; 0.02633761908248732 0.0460272570714319 -0.12203765566026321; 0.013347938697395747 0.029755678469383463 -0.0881807478030895; 0.0041483805433258514 0.009735022745690337 -0.031519964996095516; 0.004713610563577546 0.012427455391306366 -0.03914872652180248; 0.00017930987550168254 0.00026995255850239446 -0.006458677433180845; -0.0005048750524193767 0.001893601006627031 -0.00248443079848951; 0.0007349984042814397 0.0021545628049857404 -0.0055733857900517395; -0.0019059466437534934 0.0013641208145558866 0.0022056397419453187; -0.003657833694052886 5.995334154244283e-5 -0.003594798216295672; -0.0011806488153488337 0.0012882431839120057 -0.010992276770963094; -0.0005098955290313983 -0.0028356380613908587 0.0006636469578032572; -0.0007779138790188717 -0.0022490675702657773 0.0021584045081723007; 0.0011885623248141727 0.0022597106769988327 -0.00012126716896218928; 0.001505249721724743 0.00016233491897240559 0.0036779435535656824] %
+
+Mass Used: 95.50891027363377 kg
+Launch C3: 96.27037595441153 km²/s²
+||V∞_in||: 0.00011973262579555787 km/s
diff --git a/archive/ES_0.5632225216242194 b/archive/ES_0.5632225216242194
new file mode 100644
index 0000000..c7eeba5
--- /dev/null
+++ b/archive/ES_0.5632225216242194
@@ -0,0 +1,22 @@
+archive/ES_0.5632225216242194---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T23:55:23.394
+Launch V∞: [6.105067282789713, -7.594996475895405, 0.1342876250539707] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.898706683666214e-7, -2.2653589114267853e-7, 2.964879140545136e-7] km/s
+ V∞_out: [-8.286724323421346e-7, 2.1090139827314727e-7, 4.27222340700214e-7] km/s
+ time of flight: 1.855517070472798e8 seconds
+ arrival date: 2029-03-18T14:03:50.394
+ thrust profile: [0.4266372497212314 -0.08916067645660763 -0.12852740420528397; 0.09111933991137172 0.029564967330773784 -0.08753053237270998; 0.07143348806452875 0.04335669467093039 -0.11362214676717008; 0.06310620160860532 0.053254657170512414 -0.1414538294139545; 0.05383533635906032 0.055606363552739735 -0.15401179623398453; 0.03647040788285928 0.04430616098618881 -0.12714735835000254; 0.017385125609271714 0.023349203114559732 -0.07556217641710854; 0.011687118069162157 0.017313848593892314 -0.05884713235742516; 0.0018475133416284717 0.0028569854642211743 -0.010759796356913395; 0.0036802150884410402 0.006345741572364066 -0.023789498836465063; 0.0015738571230519433 0.0008598231002259985 -0.0009784427979447014; 5.330454046013669e-5 0.0003591064622844192 -0.0010484364922741572; 0.0004975716920907268 0.00025643365383752576 -0.0011046738105854213; 0.0003521420157559356 0.0002392748817144927 -0.00082395361721724; 0.00011015274600700533 0.0005918812594560522 -0.0011591860216217291; 0.00033603260361265877 0.0004851232586332779 -0.00018930568267393644; -1.3854051312562048e-5 0.00020767660565723374 -0.0012728635878778917; -7.736480604994723e-5 -0.00016693979308602218 0.0015151890410880476; -0.0009580257678192658 -0.001701063205821965 -0.0005346648093872933; 0.0019469828933343014 -0.0015952049391673494 0.0005329129480252835] %
+
+Mass Used: 103.07881011369818 kg
+Launch C3: 94.97385116249562 km²/s²
+||V∞_in||: 9.649318108423318e-7 km/s
diff --git a/archive/ES_0.5632283514374797 b/archive/ES_0.5632283514374797
new file mode 100644
index 0000000..b1fa9e5
--- /dev/null
+++ b/archive/ES_0.5632283514374797
@@ -0,0 +1,22 @@
+archive/ES_0.5632283514374797---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T23:55:52.405
+Launch V∞: [7.992144971836176, -5.518744168953493, 0.33073614939278767] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3317513044522168e-7, 1.5169122865765429e-7, -6.622513813701018e-8] km/s
+ V∞_out: [3.727367953063186e-8, 2.8214307024211794e-7, -1.2611192823877265e-8] km/s
+ time of flight: 1.8749577787403297e8 seconds
+ arrival date: 2030-04-21T02:05:29.405
+ thrust profile: [0.5366913496841028 0.002014600151962039 -0.1532190633232118; 0.05622040990469372 0.034703542166877925 -0.0613032064227422; 0.054337571452609604 0.054633637976365494 -0.10569023812688372; 0.03590363766458118 0.04836357222017913 -0.10574202182013638; 0.029785827928057253 0.050146442689670306 -0.11965122982870591; 0.01025547210674731 0.02130165946508235 -0.056054996091793687; 0.006004927890036538 0.014839370953271987 -0.04185628918569953; 0.011259841518542328 0.031225143560092695 -0.09210468234471478; 0.0036639061365749963 0.011202739031169836 -0.03486082646504425; 0.0017363779022441736 0.007533645380788737 -0.023484168018581553; 0.00044094452417152056 0.0017253166309626857 -0.008479706263264464; 0.001019797013255545 0.003825128880906405 -0.015516526353157685; -0.007912693710962055 -0.0036383621238631537 0.0006439513014137863; -0.0029548480611552314 -0.0013800956696022552 0.005277101234785975; 0.0024900021967445007 -0.00011971354361102457 -0.015063105259516246; 0.004552757915142251 0.015571832567971861 0.003796129428118; -0.001331160669647033 -0.003485353684284556 0.0054341747378815605; -0.0017865068096347859 -0.0009503119771422729 -0.00040770897061642833; -0.00699298959087584 0.011820130428122166 -0.015269731131362409; 0.0005413796333512746 0.0017576998556398512 -0.02268283467231532] %
+
+Mass Used: 106.19796503036196 kg
+Launch C3: 94.44030485371961 km²/s²
+||V∞_in||: 2.8594866537733827e-7 km/s
diff --git a/archive/ES_0.5632301295585227 b/archive/ES_0.5632301295585227
new file mode 100644
index 0000000..59338cc
--- /dev/null
+++ b/archive/ES_0.5632301295585227
@@ -0,0 +1,22 @@
+archive/ES_0.5632301295585227---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T05:58:19.623
+Launch V∞: [6.5282520994543285, -7.440507880603516, -0.03433312369807969] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7365151389330433e-9, -1.414224022691199e-9, 1.2690710879885655e-9] km/s
+ V∞_out: [5.997884302701301e-10, -1.2964260696604125e-9, -1.763910068210946e-9] km/s
+ time of flight: 1.859640190902769e8 seconds
+ arrival date: 2029-03-22T14:38:38.623
+ thrust profile: [0.15559289088679232 -0.0414304083975633 -0.05798927956238714; 0.11600299455541274 0.029493749407532147 -0.12593484439207875; 0.0993701808263286 0.04980246888910408 -0.18079367248910366; 0.03604224086323409 0.024539734256637594 -0.09397620266863498; 0.04598264850227986 0.03760843874318961 -0.1528302526073257; 0.023096736953045767 0.021340053006549415 -0.09361377321816033; 0.016003162197734865 0.016872827164188205 -0.07969780267578241; 0.007549405559454404 0.008429100931831945 -0.04233323454724538; 0.0037540061037244256 0.0045380452022086475 -0.023333826220947658; 0.0024098437325427396 0.0031030033278686467 -0.018595207135129604; 0.001868054821560581 0.003833433134363613 -0.019345832990529565; 8.180219554929915e-5 0.0014850843428873728 -0.004646246870129883; 0.0013204025413036528 0.001233775722005085 -0.007262646277675536; 0.0002773994154287244 0.0005640094414467078 -0.0031757522742793727; -0.0016488585986367838 0.00027501021537978043 -0.004269851733070802; -0.0012009972028579298 0.00029722988901496536 -0.0013685116425097097; 0.0027416417166604024 0.002045090583803158 0.0015052703515834754; 0.005288050914262347 -0.0007097935925708234 -0.002392349067356964; -0.0008337282526899971 0.0014535541921809223 -0.0030810006922377987; 0.006152575561531818 -0.002218580300275314 -0.0025797647432310544] %
+
+Mass Used: 85.54941589231794 kg
+Launch C3: 97.98041175873574 km²/s²
+||V∞_in||: 2.5741126316595016e-9 km/s
diff --git a/archive/ES_0.5632371881297397 b/archive/ES_0.5632371881297397
new file mode 100644
index 0000000..870e1f2
--- /dev/null
+++ b/archive/ES_0.5632371881297397
@@ -0,0 +1,22 @@
+archive/ES_0.5632371881297397---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T13:09:58.632
+Launch V∞: [6.364123081276241, -7.294096812156179, 0.06867647383220103] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006371502255231897, 0.005151194590137343, -0.010265193774927597] km/s
+ V∞_out: [0.008704191085954952, 0.003015594221351461, 0.009375129932069013] km/s
+ time of flight: 1.85793047719289e8 seconds
+ arrival date: 2029-03-17T22:20:45.632
+ thrust profile: [0.5093326319396507 -0.1286787958247523 -0.16034465019165323; 0.11122158446098593 0.033638513576890634 -0.10897750462610221; 0.08369122961295149 0.04901324061494188 -0.1375956264908724; 0.05940046032825253 0.04740152272045504 -0.13774637920358132; 0.05355554915973635 0.05229661972570325 -0.15980027493598797; 0.022168630112701534 0.025814103702014046 -0.08269438525502412; 0.011043022221985903 0.014914897607839395 -0.05023634620051184; 0.011842158845911065 0.017574692541068828 -0.06105341098294569; 0.005509547564321326 0.009447386893372071 -0.033014389475784174; 0.0021478397657903837 0.0035271149301901537 -0.014407401648877738; 0.0010238155164904522 0.001601008272996704 -0.007586021014951815; -9.83670104225074e-5 0.0013361357010071965 -0.004233406957111446; -0.000193868671793423 0.0005032815230769886 1.573673028654036e-5; 5.7872560971483625e-5 0.00011525165120668181 0.0005101387567717057; 0.002706348070160806 0.0004061714459951751 0.0004362418147190303; -3.057497897836273e-5 0.000215406213701262 -0.00037613395289040825; 0.0003155473485196689 0.003248564344895117 0.00021773631856804548; 0.00011142410740381338 0.00048801488505413517 -0.0009898270933950642; 0.00035688661865613316 -0.002100439536382257 0.0010926729625418017; -0.00024235961396417105 -0.001716229863942409 0.0004149149276372918] %
+
+Mass Used: 110.46472657004142 kg
+Launch C3: 93.71062735679797 km²/s²
+||V∞_in||: 0.013134117782732787 km/s
diff --git a/archive/ES_0.5632405899155901 b/archive/ES_0.5632405899155901
new file mode 100644
index 0000000..39c2f76
--- /dev/null
+++ b/archive/ES_0.5632405899155901
@@ -0,0 +1,22 @@
+archive/ES_0.5632405899155901---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T07:54:20.055
+Launch V∞: [6.418597897956327, -7.38967209978644, -0.08121854639614018] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.460524411996983e-6, 6.149077586399373e-6, 9.850119697640497e-6] km/s
+ V∞_out: [1.1759090725463184e-5, 7.2213895536094e-6, 2.4965534550011946e-7] km/s
+ time of flight: 1.874957778745152e8 seconds
+ arrival date: 2029-04-09T10:03:57.055
+ thrust profile: [0.3830285851718139 -0.09022347985829768 -0.12411940503611363; 0.04978114602992378 0.015556162535172587 -0.05286767222607166; 0.08351315721441147 0.049521853305677314 -0.1432650506744009; 0.040174253317195034 0.03215099472296646 -0.10018815159892992; 0.029499296472036106 0.028696526898487354 -0.09534198490807431; 0.024669257057467007 0.02771855331650991 -0.09729446213939699; 0.023225743248100627 0.02889402866660696 -0.10618151519634157; 0.01545997174273234 0.021803636330953523 -0.08422405961494563; 0.003191595416736233 0.004845619408258161 -0.020501518924152598; 0.010785954051134842 0.017921702836006345 -0.07319912751999515; 0.000436548111360969 0.0005696810735903448 -0.0005668787895312928; 0.0005389905456632364 0.00019677410514883475 -0.004424358426313952; 0.0019802288811262073 0.00442823476258314 -0.017618597009471212; -0.0006588949351153148 -0.0006247038579753386 -0.001478253810577665; 0.0016299628326781359 8.216478227528483e-5 -0.0002430997916732739; -0.0008381948880030148 0.0010795941164086146 0.000573768497477958; -0.0013403907647870845 0.0010761495462722212 0.0013504662967302704; -5.0065828732142145e-5 -0.00031148690384300037 -0.0003196638747060094; 5.932043540454038e-5 -0.0006698220233679809 -0.0018288590756742969; 0.00010175097690873024 -0.0012871034510466655 -0.0032670847398204284] %
+
+Mass Used: 98.2092347414955 kg
+Launch C3: 95.81224917029022 km²/s²
+||V∞_in||: 1.3802008467009699e-5 km/s
diff --git a/archive/ES_0.5632444216163424 b/archive/ES_0.5632444216163424
new file mode 100644
index 0000000..0ec09b8
--- /dev/null
+++ b/archive/ES_0.5632444216163424
@@ -0,0 +1,22 @@
+archive/ES_0.5632444216163424---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T12:23:30.818
+Launch V∞: [6.521840002385613, -7.432769152768736, 0.1499306625464355] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008442732329394351, 0.0009966401063753352, 0.000862525190784922] km/s
+ V∞_out: [-0.0010481822902399733, -0.000516010195804919, 0.001041689640499188] km/s
+ time of flight: 1.8348092901277635e8 seconds
+ arrival date: 2029-02-21T03:18:59.818
+ thrust profile: [0.2277837338237068 -0.07098122308401082 -0.08646038150679085; 0.05416853778506383 0.010787011607738891 -0.062254846408235996; 0.05986078402079314 0.02425043906296266 -0.11454832400446878; 0.06008082434722884 0.03234377184299089 -0.15981778274720643; 0.044696275393668376 0.02870775736242622 -0.1515745483529147; 0.03219953899538642 0.02350545591006379 -0.13216486504280403; 0.02157808661837175 0.017637601800216948 -0.10404674431709673; 0.006078069062259835 0.00711663030217128 -0.03828213584923889; 0.004850482543631694 0.004032622255229289 -0.025711282751802605; 0.0008348603838101619 0.0021423559348866493 -0.016138553177352376; 0.0013586860713038426 0.002073824117404746 -0.011276522872800543; 0.0009763378190507108 -0.0006696261238181523 -0.004840949199539826; -0.000921557921440129 0.00021710452739612338 -0.004164306021220547; -0.0006936708478582783 0.0026898151509220786 -0.0014904934331670793; -0.0004264820358181585 0.002133687532900074 -0.010172916440830909; 0.0028820872416775397 0.000638363966323726 0.003769121336056253; 0.0004800201922493235 0.0007015937827892726 -0.005772247988971184; 0.0005890025691490743 -0.0003721223590115975 -0.0027653073152527283; -0.002130775868987275 0.0008126567000516499 0.0009667713966637413; -0.0005726248529389273 0.00015416321961399726 -0.0041617339140464634] %
+
+Mass Used: 86.60137981033722 kg
+Launch C3: 97.80293349863925 km²/s²
+||V∞_in||: 0.0015652598820107833 km/s
diff --git a/archive/ES_0.5632477520836766 b/archive/ES_0.5632477520836766
new file mode 100644
index 0000000..872e026
--- /dev/null
+++ b/archive/ES_0.5632477520836766
@@ -0,0 +1,22 @@
+archive/ES_0.5632477520836766---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T20:07:19.919
+Launch V∞: [6.440003606029692, -7.492867670049405, 0.12820291484572896] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.227898049588678e-9, 2.456522255154649e-10, -3.79609139080429e-9] km/s
+ V∞_out: [-1.9948020213607155e-9, 4.3734058548192585e-9, 6.14224084005122e-9] km/s
+ time of flight: 1.829810212745818e8 seconds
+ arrival date: 2029-02-15T16:11:00.919
+ thrust profile: [0.24068370658090069 -0.06958022822671511 -0.08695467444678452; 0.06654813353434151 0.014717725825200081 -0.07547319950460368; 0.04991643514612409 0.022744774639584277 -0.0947190556889779; 0.047744674650516024 0.029680918868513022 -0.12681358614256344; 0.03554986493397618 0.02653979722360873 -0.12110831064693464; 0.031224277073167793 0.026938597429658262 -0.12455812613919164; 0.0191288523161345 0.018140137692797816 -0.09379486671285486; 0.015052607475976545 0.015940409274600414 -0.08524527101291428; 0.010730280616736207 0.01151910123917377 -0.06589239812487149; 0.006891145829485397 0.008468191701348736 -0.05335887568129395; 0.0001790243809035934 0.00010490548983236713 -0.0012024801611487852; -0.00012795594558091285 0.0002636348596738578 -0.001962214234123048; -0.00180505854898507 0.00045719733393457016 -0.0004298871889353965; -0.00035330319731436717 -0.00030062402402912574 0.0011817020898999729; 0.00028239039530780416 -0.0001275637147469157 -0.0012980648057905862; -0.00014634755536543762 -0.0005937267100180276 -0.0005605733551775987; -0.0013075075151734613 0.000293550901256992 -0.0008292283485232418; 0.0012932785239796883 0.0008651492660280006 -0.0011124601837975273; 0.0001689212221553246 3.8929462971963656e-5 -0.0019482200743519207; 0.0050362813569527895 -0.0010516764157429504 0.0013531892975515724] %
+
+Mass Used: 87.59567869974444 kg
+Launch C3: 97.63314835392198 km²/s²
+||V∞_in||: 5.687334769551982e-9 km/s
diff --git a/archive/ES_0.5632486275563462 b/archive/ES_0.5632486275563462
new file mode 100644
index 0000000..101431f
--- /dev/null
+++ b/archive/ES_0.5632486275563462
@@ -0,0 +1,22 @@
+archive/ES_0.5632486275563462---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T10:06:00.004
+Launch V∞: [6.637026871149896, -7.336410419902028, 0.15182356411601866] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.021007160924056415, -0.010321180861431058, 0.02565924340890056] km/s
+ V∞_out: [-0.022474681976040654, -0.009450433283644125, -0.024732661713084237] km/s
+ time of flight: 1.8749577787485722e8 seconds
+ arrival date: 2029-04-09T12:15:37.004
+ thrust profile: [0.22933624099424169 -0.05717478028165813 -0.08053693427560724; 0.08559003201294191 0.023730248741975362 -0.09483958262818741; 0.03762451129522155 0.015778048001189184 -0.07254573289446015; 0.028141580658425824 0.019197543883376172 -0.07624339928026386; 0.025107167907246965 0.021183807748798095 -0.08862749070146797; 0.01684708856614016 0.01485514402550866 -0.07326146156063743; 0.02000583971200638 0.019210116299761056 -0.09844802615600456; 0.038332103314964526 0.034544194698652074 -0.160854799313989; 0.011229544698710034 0.013884843475148 -0.072790025419609; 0.0034390970272178954 0.004242211056468722 -0.026154454308947646; 0.006211862244369314 0.007924461335601507 -0.04201369612912437; 0.001349852920224689 0.0017272858378185668 -0.008381432584066107; 0.0001567093108171467 8.813316303798958e-5 -0.0008136548763392523; -0.0007018351764819863 0.0005311145945009919 -0.0004943926144865651; 0.00035501259241894743 0.00018725800213835635 0.0006498043536731578; -0.00037464125616646385 6.939905337022384e-5 -0.0010237821724966177; -8.855153254737111e-5 1.909163207239453e-5 0.0009538176915090607; -0.0005572849050487324 -0.0005570053884086317 -0.001824489474953919; 0.000488871089359043 0.0015114748105767367 -0.0019465207340737998; -0.00019080698302801063 0.0010184585878532295 0.0008226189799258605] %
+
+Mass Used: 86.0628508777072 kg
+Launch C3: 97.89609393223373 km²/s²
+||V∞_in||: 0.034730740803800605 km/s
diff --git a/archive/ES_0.5632552112732241 b/archive/ES_0.5632552112732241
new file mode 100644
index 0000000..eff3d85
--- /dev/null
+++ b/archive/ES_0.5632552112732241
@@ -0,0 +1,22 @@
+archive/ES_0.5632552112732241---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:31:29.069
+Launch V∞: [6.50703280746676, -7.51137419935908, 0.11229696374445684] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0011365613909668922, -0.007487993052884237, 0.009491069687951059] km/s
+ V∞_out: [-0.007902813436893946, -0.007781959235422298, -0.004941179799598917] km/s
+ time of flight: 1.8371620066444838e8 seconds
+ arrival date: 2029-02-24T14:48:09.069
+ thrust profile: [0.11675206096611784 -0.03366038186974915 -0.04483232291793368; 0.09667381350150567 0.02064483303594668 -0.10706192854039122; 0.04170460678935016 0.018397989641418446 -0.07970535395356355; 0.09086612841493091 0.056012766250379716 -0.22416707795224103; 0.03209243743755263 0.02296844938465375 -0.10903437798766778; 0.023818462869422113 0.019129182052844182 -0.09676404872575925; 0.018022550666851843 0.017141923539908444 -0.09082813815100492; 0.01579832176777799 0.014810202919998414 -0.08534912496514736; 0.00330002513155739 0.00306133490877835 -0.01995850988522866; 0.002421825715543973 0.002290791485342415 -0.01592726411097044; 0.0029405439611584674 0.0022250728624727857 -0.010499773293388403; 0.0006176871903275598 0.000997502127334346 -0.004190032841383484; -0.001150496875580409 0.003258990847451975 -0.004661300718811498; 0.0015182768922658355 0.0005457103079854976 -0.005155543565058925; -0.0036658356899356426 -0.0007096073726893089 -0.002686619809802961; 0.00017810308693728215 -0.00017505554132085177 -0.008940195211439461; 0.0027277682360009525 -0.003738974166350104 -0.0045361504839797; 0.0010522636205003016 0.0011215506022931414 -0.0036675807419683385; -0.0006160057378728237 0.0029087996125211615 0.0008596189584537935; 0.0004137682562307267 0.0007686614291050327 0.0004670820870637816] %
+
+Mass Used: 80.94457773694012 kg
+Launch C3: 98.77482892831223 km²/s²
+||V∞_in||: 0.012142578621405858 km/s
diff --git a/archive/ES_0.5632554988449558 b/archive/ES_0.5632554988449558
new file mode 100644
index 0000000..a3f7054
--- /dev/null
+++ b/archive/ES_0.5632554988449558
@@ -0,0 +1,22 @@
+archive/ES_0.5632554988449558---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T15:26:56.124
+Launch V∞: [6.447849149802873, -7.525236473484041, 0.1073184155878377] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.240295462009703e-9, 6.210437420281911e-10, -6.021646665295876e-9] km/s
+ V∞_out: [-1.8834677945059603e-9, 4.293548247361879e-9, 5.58548716020057e-9] km/s
+ time of flight: 1.845764769233382e8 seconds
+ arrival date: 2029-03-06T22:41:32.124
+ thrust profile: [0.1568341085809774 -0.040900927510592336 -0.05842433504405921; 0.09975135492592295 0.025480048215841457 -0.1076498869448952; 0.06406332840594839 0.03297409319086005 -0.11769895057570245; 0.061779114961443594 0.04164601658302709 -0.15386957916334484; 0.034451672951382684 0.02820015678593813 -0.11344278328262375; 0.02977363595848587 0.027925522198280938 -0.11916725825474664; 0.013849729552510714 0.014578392336170722 -0.06746841724540913; 0.0157117934049353 0.016623347236968716 -0.08199140101833877; 0.007996031654079402 0.00949965802599764 -0.048873709236700584; 0.0034183650989186207 0.004270076799159407 -0.024060922541419838; 0.0011202547063637017 0.000904788511630955 -0.007473131108622657; 0.0010687735503922425 0.001017765672526167 -0.005693697799404028; -0.00011525037021160093 0.0004462594467423646 -0.0012368888925536501; 9.96923765995253e-5 5.245510904004866e-5 -0.0001240021256668463; 0.001019230774407476 0.0021847748965091243 0.0003681233866972811; 0.001351219289482393 -0.0024901749621061248 -0.0005824529346478602; -0.0005959752686994636 9.54608718811208e-5 0.0032707206018988337; 0.0025253834591759208 -0.002568256485734494 -0.0008840503968661499; 0.0014288845601443927 0.000561669814877466 -0.004749773881589158; -0.0014649662045528697 0.0020992269914596735 0.003988969929742771] %
+
+Mass Used: 84.20789933615924 kg
+Launch C3: 98.21545988279244 km²/s²
+||V∞_in||: 7.3909423956841525e-9 km/s
diff --git a/archive/ES_0.5632584186521347 b/archive/ES_0.5632584186521347
new file mode 100644
index 0000000..566ec13
--- /dev/null
+++ b/archive/ES_0.5632584186521347
@@ -0,0 +1,22 @@
+archive/ES_0.5632584186521347---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T19:38:41.978
+Launch V∞: [6.21082786101463, -7.342923011335667, 0.09932834533701812] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.758005217615639e-7, 0.00038600189969239016, -0.00025636747489398847] km/s
+ V∞_out: [-0.00022965330359713324, -0.0003938359190180087, 8.264967186257851e-5] km/s
+ time of flight: 1.8749577787495926e8 seconds
+ arrival date: 2029-04-07T21:48:18.978
+ thrust profile: [0.6254997250034235 -0.14454278480376845 -0.16254751626252512; 0.05214922545480537 0.018358148933974885 -0.04937448041256673; 0.09484177611384416 0.062056648451665 -0.14344746426404575; 0.05791840537378705 0.052719246607008316 -0.12748692513897397; 0.05781437080630266 0.06376224383658753 -0.16134416479961186; 0.024159628331341405 0.032080304837492905 -0.08679148148387615; 0.021505124432324437 0.032167085660663904 -0.09159934333958857; 0.0060600287078610435 0.010702965858787349 -0.031702948005335053; 0.006200081740067191 0.011700348022446589 -0.03692865720762035; 0.003833547903062464 0.007346510267796013 -0.026478178202671943; 0.0017410956208251036 0.0016891288260810072 -0.0020372221712247297; -0.0009935248501776728 0.0007251685540563349 -0.00348753144113899; 0.00018506589758528726 -0.0024320817324301183 -0.001252505065248555; 0.002318206832507037 0.000482351497833266 -0.0008727838290996047; 4.774461997084176e-5 -0.0010432527374816924 -0.0016534343803091631; 0.0003769667882783781 -0.0006895502525591132 0.0025098993285311215; 0.00029258699193555405 -0.0010755251213005602 0.0016469806637786511; 7.536237430764048e-5 -0.00033902814369325424 0.0002492624174626006; -0.002856357990911557 0.003278640026290447 0.0004775575480125573; -0.00029989505196379297 -0.0005324132487645098 0.0030008312251392725] %
+
+Mass Used: 117.53534648730647 kg
+Launch C3: 92.50276718974582 km²/s²
+||V∞_in||: 0.0004633814310221153 km/s
diff --git a/archive/ES_0.5632628659294385 b/archive/ES_0.5632628659294385
new file mode 100644
index 0000000..2416da0
--- /dev/null
+++ b/archive/ES_0.5632628659294385
@@ -0,0 +1,22 @@
+archive/ES_0.5632628659294385---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T22:59:06.471
+Launch V∞: [6.397515360938989, -7.293901915114199, 0.11361903198722197] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9566547428283607e-6, 2.633983118632067e-7, -5.621584015621236e-9] km/s
+ V∞_out: [-3.6708162607997965e-7, 8.619054108000941e-9, 1.9406612371476173e-6] km/s
+ time of flight: 1.874957778748262e8 seconds
+ arrival date: 2029-04-08T01:08:43.471
+ thrust profile: [0.49897260491409 -0.11973349074237756 -0.16284482722432853; 0.08343438055488109 0.02503172127768115 -0.08630853553950973; 0.0788481906612584 0.04520661979397167 -0.13620807764377743; 0.06636088640552645 0.05147575000803383 -0.16091193439263887; 0.029951346206387428 0.0283140236450709 -0.09587467895752654; 0.01600126239433453 0.017631292872937274 -0.06396261108720101; 0.022330326932214192 0.027762339035750597 -0.10379519813405771; 0.004637341949763673 0.0062456960497903865 -0.025963007030590166; 0.010975301652103876 0.016590248287113786 -0.0682330979040778; 0.002040450668730913 0.0030329798496633756 -0.01127278005394384; 0.0018204821927454112 0.0019884253480658147 -0.007687565868040961; 0.0008175223823730331 0.0016562359460086298 -0.011081853173483503; 0.0005352903761333128 0.0010429478578878107 -0.0033411261777621043; 0.00015409699985959475 -0.0009558348244640734 -0.002439182447671745; -0.000978484802370838 -6.616673127344587e-5 -0.0029006636330079502; -0.0008332716890297804 -0.0009131908922930102 0.003038980653953419; 0.0005245639541610471 -0.0008141356460018527 0.0036077710206346677; 0.0012241001277834328 -3.31456380740431e-5 -0.006907661850757118; -0.0004951517720489951 -0.00022229153942873313 -0.004126027880587836; -0.0002492222199831823 0.0004416990591011089 -0.0006914985349139993] %
+
+Mass Used: 107.97765977075642 kg
+Launch C3: 94.14211722518661 km²/s²
+||V∞_in||: 1.9743120461396043e-6 km/s
diff --git a/archive/ES_0.5632671395554337 b/archive/ES_0.5632671395554337
new file mode 100644
index 0000000..83cda8e
--- /dev/null
+++ b/archive/ES_0.5632671395554337
@@ -0,0 +1,22 @@
+archive/ES_0.5632671395554337---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T04:16:14.042
+Launch V∞: [6.685500809099342, -7.3754098606117475, 0.09233389617606777] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2089351730298556e-7, -3.353999489312853e-8, 3.695544043281264e-8] km/s
+ V∞_out: [-1.2223889745336892e-7, 3.385414969822797e-8, -1.4287973993787892e-8] km/s
+ time of flight: 1.87495777874471e8 seconds
+ arrival date: 2029-04-10T06:25:51.042
+ thrust profile: [0.12737268040202734 -0.035279169284249096 -0.050107205095515805; 0.08140351883121191 0.018685187060618197 -0.09942191698080645; 0.03758367576687126 0.016264646191919682 -0.07762851150670548; 0.05823231026199224 0.034862877985155 -0.16288350918781602; 0.025916208945086994 0.017413429541069367 -0.09570884086417583; 0.021965342652940152 0.016409039003206033 -0.09803023905244763; 0.01842029081310543 0.015063813715757554 -0.09615806874279252; 0.01088196622411414 0.00863310290954066 -0.06325808955728737; 0.0069628476789407165 0.006480105630344069 -0.045755069117129114; 0.009926722421125128 0.010379606271756246 -0.07308620548876885; -0.0005754632759756723 -0.0005301338239081801 -0.0008841365148142839; 0.001420553996110632 0.001926261153955959 -0.007181154556528669; 0.0003751797649697306 0.00034423876804299305 -0.0018891675932724353; -0.00018958328412689232 0.002066034227032048 -0.0010574743012834499; -0.00036210555895675126 -0.0004579833764638275 -0.0012505385696985807; 0.0005946529025514961 -0.0003190125666227924 -0.00034871780361521746; -0.0008504550360674372 0.002412452323872515 0.0008650755064861524; 0.0037682346951441355 -0.0026489542383552646 -0.003256864626742178; 0.005313702289909384 -0.001873605781036037 0.001485088550192755; -0.0019315409895537907 -0.0029835961500181106 0.005574146719485564] %
+
+Mass Used: 79.05514564632267 kg
+Launch C3: 99.10111722886 km²/s²
+||V∞_in||: 1.3078944284957223e-7 km/s
diff --git a/archive/ES_0.5632716229953393 b/archive/ES_0.5632716229953393
new file mode 100644
index 0000000..be757d4
--- /dev/null
+++ b/archive/ES_0.5632716229953393
@@ -0,0 +1,22 @@
+archive/ES_0.5632716229953393---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T00:24:17.394
+Launch V∞: [6.5629807850164905, -7.4628847899905955, 0.09479670582395838] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.12505841539239e-8, -1.4768908052258605e-7, -9.799308590871197e-8] km/s
+ V∞_out: [4.788278328860854e-8, -1.0547839995170222e-7, 1.544455137828215e-7] km/s
+ time of flight: 1.852732720935163e8 seconds
+ arrival date: 2029-03-15T09:12:09.394
+ thrust profile: [0.15492279847485643 -0.04453422100584645 -0.061128896246910945; 0.06890494597357166 0.01456488330664534 -0.08023310687474491; 0.043184950056251024 0.01821472653712124 -0.0876428631214015; 0.041094713537862905 0.02116242685724616 -0.11858098275862317; 0.0434120326966865 0.029193428558258017 -0.1449771785002506; 0.03207076751968271 0.02011409251735258 -0.12680070435791216; 0.023816881256600596 0.016449329161318214 -0.10848920665554185; 0.017279496595662306 0.014484744555434161 -0.09131547348041379; 0.0018210207789667006 0.0018197536006269925 -0.013512400088211083; 0.0034953020878862296 0.003140189844395783 -0.025590586940996914; 0.0003987184162779205 0.00017959440479722573 -0.007415917396871936; 0.0010852372684473372 0.0010437758798524338 -0.008760952270209545; -0.0005561316238892463 0.0005017625011608952 -0.004010107190101777; 0.0044236043524266775 0.005522028389649043 -0.005331316001364767; 0.0004058873564705557 0.0018622840136424525 -0.005816953299593412; -0.0021790584230396777 0.001113723901802029 -0.002838876158461823; -0.0014260411663363508 -0.0011703944753502556 -0.012456390442337657; 0.0013002510613873781 0.0013540752395066905 -0.003727038003934504; 0.0012359585371129716 -0.0015926428186606378 -0.00011951614461259627; -0.0005592985804342273 -0.0007429067768022213 -0.00044896431839637116] %
+
+Mass Used: 80.95483672770752 kg
+Launch C3: 98.77635258860371 km²/s²
+||V∞_in||: 1.9935239777828472e-7 km/s
diff --git a/archive/ES_0.5632727880244985 b/archive/ES_0.5632727880244985
new file mode 100644
index 0000000..efe87a4
--- /dev/null
+++ b/archive/ES_0.5632727880244985
@@ -0,0 +1,22 @@
+archive/ES_0.5632727880244985---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T11:20:22.791
+Launch V∞: [7.712132371016732, -5.585275474156829, 0.5525223320179623] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.127333730705655e-8, -5.646758270031725e-7, 8.755903199615382e-8] km/s
+ V∞_out: [-9.035942782674196e-8, 3.328034434456646e-7, 4.5933964307874263e-7] km/s
+ time of flight: 1.8190389057688454e8 seconds
+ arrival date: 2030-02-10T20:11:52.791
+ thrust profile: [0.8216254334960267 -0.023704386124783944 -0.19069622315131893; 0.1547170908137498 0.09290096537450701 -0.13086009663033063; 0.05621874243118176 0.05718638086277794 -0.08879552687369342; 0.051667273347929775 0.07132211823662118 -0.12035242920784668; 0.022878400491926878 0.040814334018067965 -0.07544809201745581; 0.021032669146140392 0.04963251467309012 -0.09570100052838339; 0.009304119202966967 0.02290536483127484 -0.05162792912171444; 0.02080006335576294 0.0441062956165016 -0.11306269856062241; 0.002310638658847091 0.006747519413495753 -0.01705797677073135; 0.0005166942488213065 0.0019879460794454827 -0.005379557758212208; 0.0002890317083926971 0.0013339395227534591 -0.0037454286249411555; 0.00010082654883026815 7.138694183243756e-5 -0.0002487743884319784; 6.15237944641916e-5 -4.063271605334498e-5 1.969333930032784e-5; 0.00012729614176061293 0.00015245842691084414 0.00010322253259098356; -0.0004482067557057351 0.00023377100170112735 -9.237804569913149e-5; 9.237819212833095e-5 1.8530058671445063e-5 -0.0003657820921299617; 7.154481263857226e-5 1.1029742690009392e-5 6.562979146139985e-5; 8.670896611481174e-5 -0.00030670643710133377 -1.3575741084665522e-5; 0.0008699062191382951 -0.0002820907164214344 0.00036127455405593267; 1.1085892335363295e-5 -3.8591794726528764e-5 -0.00015710259684542036] %
+
+Mass Used: 126.44910160877862 kg
+Launch C3: 90.97756875768052 km²/s²
+||V∞_in||: 5.746997438232982e-7 km/s
diff --git a/archive/ES_0.5632743907995601 b/archive/ES_0.5632743907995601
new file mode 100644
index 0000000..57ef246
--- /dev/null
+++ b/archive/ES_0.5632743907995601
@@ -0,0 +1,22 @@
+archive/ES_0.5632743907995601---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:57:36.638
+Launch V∞: [6.572839534537852, -7.350170564203878, -0.09180754366283957] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7364109528741364e-5, -3.297736583327458e-6, -3.900528884189032e-6] km/s
+ V∞_out: [-1.5069730815035218e-5, -9.984580107320981e-6, -3.147132710942604e-7] km/s
+ time of flight: 1.8749577784728715e8 seconds
+ arrival date: 2029-04-08T22:07:13.638
+ thrust profile: [0.25104648219967923 -0.05967480409731499 -0.08940148321859784; 0.08427456928957743 0.02779578806973918 -0.09158808899849294; 0.06118851904519958 0.03400062041022074 -0.10712362279301248; 0.050641495864001615 0.0435428150898333 -0.13496710410429297; 0.040122893905554714 0.04046734550004477 -0.13934281803963827; 0.01976283934436867 0.02262653125749138 -0.08441938157144091; 0.02013140622262394 0.027321672819789592 -0.09829766876259839; 0.010186815019913944 0.014413951701909856 -0.05843694660055993; 0.007543659374610779 0.011675443825623232 -0.05057770340340325; 0.0015849557441982311 0.0027005801288199458 -0.01219696553345825; -0.0005556543217298269 0.0002698256542746388 -0.0013230951281584023; 0.0032984482915914444 0.0066458989439905965 -0.030123111004401456; 0.0007884451881424479 0.00015986513530269643 -0.0011821610224146272; 0.0009946546257642269 -0.0003226420532269392 -0.002275320713652408; -0.0010169329354772654 0.0010594324314580233 -0.0024369311568168883; 0.00088133768487666 0.00021020876117117332 -0.0013073656312828554; 0.001290264794828712 -0.0010228629898983883 0.0004935928352456441; -0.0015392744690894352 -0.004928854727245328 0.003225695355924793; -0.0005420082086306414 0.001938912810450361 -0.0031009429224309573; -0.0004095070918761893 -0.0008336158828445732 0.0028399069218725532] %
+
+Mass Used: 89.94546554679982 kg
+Launch C3: 97.23565549474634 km²/s²
+||V∞_in||: 1.8099764967411478e-5 km/s
diff --git a/archive/ES_0.5632924724725766 b/archive/ES_0.5632924724725766
new file mode 100644
index 0000000..3a0edc2
--- /dev/null
+++ b/archive/ES_0.5632924724725766
@@ -0,0 +1,22 @@
+archive/ES_0.5632924724725766---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T18:16:58.711
+Launch V∞: [7.989738362559125, -5.893713193889766, 0.020867267096024385] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.427345033296749e-8, -3.569489341029126e-7, 5.853866869694083e-8] km/s
+ V∞_out: [-5.7036796893320146e-8, 2.114713711424689e-7, 2.9011574788615807e-7] km/s
+ time of flight: 1.8199201736375532e8 seconds
+ arrival date: 2030-02-19T03:37:15.711
+ thrust profile: [0.1910268681095348 -0.013776957005154186 -0.07032054397193149; 0.04712474244058465 0.019115649718153677 -0.06080432574918376; 0.052706953446937134 0.03214493936013512 -0.11131387962810936; 0.04180806786537722 0.03193170738556777 -0.12723520228712015; 0.029386995106262914 0.02614794844167848 -0.11935965904908064; 0.023230566902550237 0.022222835783333172 -0.11559028630323116; 0.010367890923284892 0.0112185517710169 -0.06281633884691362; 0.006311203978362441 0.007580482219486143 -0.050111610261398876; 0.004367777706530728 0.00656631160188738 -0.045581697940741024; 0.006531565284192075 0.008554169647194172 -0.05813715795094419; 0.0019478372448409674 0.002242995512819619 -0.019211762300047952; -0.0008965664328833561 0.010450968504001179 -0.0012775021228759193; -0.0024003211071949113 -0.00530488599631238 -0.0038565062326399975; -0.00467214615207885 -0.0009879086853769193 0.0027773829985342927; -0.00013409872665568216 -0.00012961744231171823 -0.0020333708169290848; -0.0015847415485975849 -0.0015256729391131985 0.0069420506995536615; -0.0007639337030767271 -0.0003590877806199952 0.002046575023638874; 0.00042854269884923116 0.017252140472675252 -0.0006944772517102301; -0.022083810892091764 -0.0007780750540864914 -0.01324558614548058; 0.0092786675913685 -0.019522836037527858 0.0026852089101102538] %
+
+Mass Used: 82.16999430324995 kg
+Launch C3: 98.57220975681534 km²/s²
+||V∞_in||: 3.633372905273309e-7 km/s
diff --git a/archive/ES_0.5632985095940968 b/archive/ES_0.5632985095940968
new file mode 100644
index 0000000..d24e35b
--- /dev/null
+++ b/archive/ES_0.5632985095940968
@@ -0,0 +1,22 @@
+archive/ES_0.5632985095940968---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T21:10:53.855
+Launch V∞: [6.598631176290975, -7.431698338778772, -0.25684152797662796] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.732931332411626e-11, -3.6116411216755616e-9, -1.3893821344442991e-8] km/s
+ V∞_out: [5.302678141998885e-9, 7.847678219305479e-9, 3.829454280851166e-9] km/s
+ time of flight: 1.796976456116073e8 seconds
+ arrival date: 2029-01-06T17:11:38.855
+ thrust profile: [0.16297676262656557 -0.06234489356261299 -0.06640876667081984; 0.023896434344970432 0.003036309180636614 -0.030909023777253977; 0.09105845476112452 0.02430830379389365 -0.18500946722057768; 0.05895348810208529 0.022017164313944914 -0.16507220772596473; 0.06688891233643442 0.028891401136224442 -0.23184880127474428; 0.031634029683138574 0.016297596422259645 -0.14138284238327764; 0.010229536667377486 0.006261762549533042 -0.05466485990182755; 0.00667409039525994 0.0043581022733401404 -0.041314472652355806; 0.0024839276301800743 0.0016570519126089104 -0.018945865796537037; 0.0005642390275531233 0.0004100124299776373 -0.004071370652730612; 0.0001698829445856682 0.00010403409375068484 -0.0010617423492258222; 0.0005714808822647126 0.0001618988235856549 -0.0035815333320175467; 5.7984489480908895e-6 -2.4513454160471397e-5 -6.212984535226658e-5; 7.066151911402455e-5 -1.3516730125535481e-5 -0.0002580715735660937; 1.8914948353785288e-5 0.0001527918440805847 -0.00015014360159414198; 9.476839166041276e-6 6.20670768567857e-5 -0.00012050815875054788; -6.600005133060777e-5 8.837470674675929e-5 9.570421512882407e-5; -0.00033728423941556705 -0.000392515031665271 -9.764473189037588e-5; -4.4419356576594216e-5 -2.9273224770554263e-5 -8.909505758929404e-5; -6.18165110909327e-5 4.86061692482304e-5 0.0002497200719176081] %
+
+Mass Used: 80.62635436916435 kg
+Launch C3: 98.83804116981975 km²/s²
+||V∞_in||: 1.4355642208099827e-8 km/s
diff --git a/archive/ES_0.5632997397696797 b/archive/ES_0.5632997397696797
new file mode 100644
index 0000000..325db0c
--- /dev/null
+++ b/archive/ES_0.5632997397696797
@@ -0,0 +1,22 @@
+archive/ES_0.5632997397696797---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T22:24:44.519
+Launch V∞: [6.202219320819751, -7.44036156003317, 0.10922195593101514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1067685335536565e-7, 1.8638013274146152e-7, 8.494113679698054e-8] km/s
+ V∞_out: [-7.285593503802875e-8, 1.198718109072981e-7, -1.8617512531781893e-7] km/s
+ time of flight: 1.8095906056086072e8 seconds
+ arrival date: 2029-01-20T08:49:04.519
+ thrust profile: [0.4571559796067316 -0.13333293534731042 -0.1503133879096471; 0.1689121907943019 0.04259180864825761 -0.16548757371285958; 0.10034088279497066 0.05189020610469701 -0.16567931180541662; 0.045151007357901514 0.032240919043786745 -0.1076101965174572; 0.05303479618105031 0.04632857396509698 -0.15913688009178012; 0.028512355929570004 0.028968720888389886 -0.10582700998135947; 0.016162344497703648 0.020156144784745464 -0.07578401411009729; 0.005864398498984231 0.007459965050094756 -0.02999295652116714; 0.005084966718614225 0.006607495218162668 -0.02889681004122618; 0.0007573541392207971 0.0010263471767252893 -0.005919586728251726; 0.002548314478318531 0.004070045905203577 -0.018647095423927118; 0.00042823239130801313 0.00045493473562436084 -0.0005508198149123877; -3.4844182394087186e-5 -5.287014950655926e-6 0.00017784659046809982; -9.065882298626068e-5 6.1820927350973e-5 0.0005146820217537796; -0.0001970841227836721 1.6865135340715735e-5 0.0005258153997583356; 0.0008116499847392316 -0.0004321052967459591 0.00035200704797754413; -1.5648725789785737e-5 -6.902545968695453e-5 0.0014344763660778352; -0.0006060374118026755 -8.255369187546238e-6 -0.00046499405426714805; 0.00034523393098518995 -0.0002455924987829219 0.000231710097225324; 0.0023545762911726534 0.0003669496641251855 0.00029539773911585595] %
+
+Mass Used: 109.79216424580545 kg
+Launch C3: 93.83843408322643 km²/s²
+||V∞_in||: 2.3281305047125962e-7 km/s
diff --git a/archive/ES_0.5633095242234587 b/archive/ES_0.5633095242234587
new file mode 100644
index 0000000..1206c80
--- /dev/null
+++ b/archive/ES_0.5633095242234587
@@ -0,0 +1,22 @@
+archive/ES_0.5633095242234587---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:06:57.196
+Launch V∞: [6.425688048448591, -7.4933304471384625, -0.04223401289804415] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.298884726644201e-7, -0.00014833988853278353, 9.506380310563971e-5] km/s
+ V∞_out: [9.620353997336157e-5, 0.00014297955445401417, -3.021234644043387e-5] km/s
+ time of flight: 1.8535881388202497e8 seconds
+ arrival date: 2029-03-16T19:40:30.196
+ thrust profile: [0.27159882904184446 -0.08355306622585389 -0.09521369014533426; 0.08647057005260385 0.02058584710116334 -0.10034599590500981; 0.027650677638253265 0.01202750360664661 -0.05777690127322551; 0.03277206487312596 0.01931709926473544 -0.0918826257150086; 0.027019874395794733 0.019037798981557445 -0.09749025028344753; 0.019986762655545613 0.0162470261305777 -0.08884494841754398; 0.033711871885489075 0.028768779992183496 -0.16898995238847858; 0.011416315229823825 0.010963676062453244 -0.07328676122994351; 0.010997326694533896 0.008830887414572719 -0.0658332970284727; 0.00744155563269119 0.007101436506876588 -0.055998460114780046; 0.003478929717979235 0.002898772966363819 -0.027572969673788972; 0.00022742555763738385 0.0002530066943396196 -8.039518397289798e-5; -0.0003395225165148198 -0.00014102026758764478 -0.0005011023506493957; 0.0004183624160817928 0.0007362021061821928 8.500640020935794e-5; -0.0008285256883741792 0.0003404821037084684 -0.0008962585276987659; 0.00027823762710462504 2.7201401194646135e-5 0.0003643775944350373; 0.0003878817709740745 0.0006091014258720843 -4.397994128531996e-5; -0.0010746213486592829 0.00019977036171386442 -0.000730983073703289; -0.0011571392118377936 -1.255618085944677e-5 0.0008398556481668341; -5.0720461375219905e-5 -0.00016874855518655632 -0.0001609696973496734] %
+
+Mass Used: 88.78714277334348 kg
+Launch C3: 97.44125179783285 km²/s²
+||V∞_in||: 0.00017618749670429343 km/s
diff --git a/archive/ES_0.5633135339934838 b/archive/ES_0.5633135339934838
new file mode 100644
index 0000000..54818af
--- /dev/null
+++ b/archive/ES_0.5633135339934838
@@ -0,0 +1,22 @@
+archive/ES_0.5633135339934838---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T23:44:34.744
+Launch V∞: [6.5831667413117225, -7.56188252807106, -0.09272776966657827] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9030381008800875e-6, -2.513064644179384e-6, 1.4881432340715056e-7] km/s
+ V∞_out: [-1.1276679797075734e-6, 2.559832110678636e-6, -1.460932627286458e-6] km/s
+ time of flight: 1.8749577782277295e8 seconds
+ arrival date: 2029-04-13T01:54:11.744
+ thrust profile: [0.07585371624041394 -0.02215882748587853 -0.03359499252025946; 0.027290765178961982 0.004461888561138972 -0.03629364150313781; 0.04619854580734241 0.016334013041753928 -0.10373842918013082; 0.045912191976347425 0.020466937975932804 -0.1428660967190459; 0.02864920459249076 0.014841761905727823 -0.11412713097424282; 0.02821407694155192 0.015776639713545173 -0.13537973568606596; 0.0179338037870649 0.010860357735580039 -0.10007676153269975; 0.012837354880290412 0.008137677883650076 -0.08148862434805425; 0.006310949863512287 0.00402358041461355 -0.04377574688748018; 0.002954072245645777 0.0018117671532352372 -0.02205284801549518; 0.001968806542388248 0.0011928606338136992 -0.015817674690618743; 0.0007489196779684822 0.0005538285322658739 -0.006862777780801464; -0.0012136614038273116 1.009779654608683e-5 -0.005208376053799692; 0.0015077830600268081 0.0008357135274579769 -0.003656815292163199; -0.00020183517672510453 -0.0005682760404568925 -0.0017213212138554737; -8.937952011265379e-7 0.001187222061681105 -0.0012702603142135949; 0.0002535927806318506 -0.000911029694967289 -0.002160050021369861; -0.0008408657524674502 -0.0005163771513488394 -0.0009098038844489106; 0.0003669973308471051 -5.8898671122106176e-5 -0.00038579811789344514; 0.00027192071086639465 -0.00025102276572515667 -0.000499624045095243] %
+
+Mass Used: 70.78141377515976 kg
+Launch C3: 100.52875015152651 km²/s²
+||V∞_in||: 3.155819009714732e-6 km/s
diff --git a/archive/ES_0.5633177094430127 b/archive/ES_0.5633177094430127
new file mode 100644
index 0000000..56814b9
--- /dev/null
+++ b/archive/ES_0.5633177094430127
@@ -0,0 +1,22 @@
+archive/ES_0.5633177094430127---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T01:37:51.216
+Launch V∞: [6.477888670650406, -7.293741857048379, 0.3845485536167123] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0565465781199118e-8, 2.2002668077934888e-8, 1.2155621617526397e-8] km/s
+ V∞_out: [-8.190442922512165e-9, 1.5861757030759808e-8, -2.3905553966499942e-8] km/s
+ time of flight: 1.87495777874956e8 seconds
+ arrival date: 2029-04-07T03:47:28.216
+ thrust profile: [0.35905311421032626 -0.07698134481306315 -0.10420116202699761; 0.15621939566984538 0.05294134664778728 -0.14053135070607847; 0.07400885203443991 0.047619097608607094 -0.11541753423018487; 0.054021787950164435 0.04790609410635757 -0.12090659502878909; 0.060227878588594054 0.06325883760486112 -0.16259866600998407; 0.024032702268212632 0.030346260571973052 -0.08704861955773835; 0.007814444300275199 0.011088079411085734 -0.03476339362719524; 0.006884590746052359 0.011242805715914428 -0.03681604664998176; 0.0040873888413963475 0.006945616733994733 -0.02384131540814862; 0.008832615873735699 0.016836830225938838 -0.057139081071694894; 0.001617509161334904 0.0034636407837777706 -0.011915301530237107; 0.0006431373563661885 0.0009912378423614508 -0.0030204324551981764; 0.00011320222936554085 -0.00028440338955280334 -0.0011946818773632705; -0.0006708295159436441 0.0006211809529699562 -0.00210592078282867; 0.00029015008162529613 0.0004331010528194528 -0.0009226423612116388; 0.0009340428192642254 0.00034105088913244635 -0.0011322440485919331; 0.0002857658042548756 0.0005149986629299733 -0.0018128138574042968; 0.0012881273451294546 -0.0009310778182649608 -0.000876340926508824; 0.0002376058176064277 -0.0015832625639504386 0.0016282094101510618; -0.00019924546819387199 -0.0016704141096422528 0.0011505226935873795] %
+
+Mass Used: 101.23138895282818 kg
+Launch C3: 95.30958949668914 km²/s²
+||V∞_in||: 2.7267299217743207e-8 km/s
diff --git a/archive/ES_0.5633229972312084 b/archive/ES_0.5633229972312084
new file mode 100644
index 0000000..d2198b5
--- /dev/null
+++ b/archive/ES_0.5633229972312084
@@ -0,0 +1,22 @@
+archive/ES_0.5633229972312084---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T20:05:30.339
+Launch V∞: [6.627574188413379, -7.389774330564545, 0.10322108711034526] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.09502782138532e-8, 8.240069947728406e-8, 4.391471501988764e-8] km/s
+ V∞_out: [-2.633417362272789e-8, 5.718962752110264e-8, -8.038992640213236e-8] km/s
+ time of flight: 1.8749577787493843e8 seconds
+ arrival date: 2029-04-09T22:15:07.339
+ thrust profile: [0.16414438967574374 -0.04170699854353287 -0.05980531228116724; 0.058671144029516384 0.01686205612843713 -0.06944828742678522; 0.06805191252046107 0.035979590570555824 -0.12903683846189054; 0.05506704763917407 0.03891177658584923 -0.14605028791190108; 0.027462667209766277 0.024138056792306472 -0.09896568533483739; 0.025603481486127788 0.025465248057603595 -0.10500405962563492; 0.01584372596891309 0.017360951589117237 -0.07650514871538427; 0.009045491007879535 0.010071888556110199 -0.05119383393138611; 0.006539768921349026 0.007949404599372628 -0.0437778124710128; 0.005205822931644415 0.006039480703881194 -0.0325898345594203; 0.005377812077778255 0.00760160237249816 -0.04256467539900316; 0.0023184242921032855 0.0036400042441567604 -0.021281999766843262; 0.00034181012332867833 1.9688126544313784e-5 -0.0017423430805903093; 0.0014716560863921539 0.0004423517988775558 -0.0022056810248025373; 0.00013938672060417835 -0.0007578739718514659 0.00045585639653301013; -9.870042597473276e-5 0.0021601810949709206 -0.004120071890353715; -0.0001401114400041734 -0.00042263778570504336 -0.0009016686666759488; -0.00017819171226535267 0.004193413170970385 0.0009405174259811038; 0.0012927898849195627 0.001631449988735404 -0.0069075496780987705; -0.00022998470866260237 0.0010330389425299551 -0.004071021489670765] %
+
+Mass Used: 82.36923668063719 kg
+Launch C3: 98.54415887241817 km²/s²
+||V∞_in||: 1.0195735753448892e-7 km/s
diff --git a/archive/ES_0.5633271353861057 b/archive/ES_0.5633271353861057
new file mode 100644
index 0000000..e873ce3
--- /dev/null
+++ b/archive/ES_0.5633271353861057
@@ -0,0 +1,22 @@
+archive/ES_0.5633271353861057---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T19:41:00.476
+Launch V∞: [7.861264471543724, -5.793374527281766, 1.3307149620532066] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.250282647833866e-5, -2.0595355480345567e-5, -0.0005758738651071361] km/s
+ V∞_out: [0.0005142491875777286, 0.00017268173440234178, -0.0001964108511641236] km/s
+ time of flight: 1.8749577786630785e8 seconds
+ arrival date: 2030-04-23T21:50:37.476
+ thrust profile: [0.3637822275279491 0.004625974285378492 -0.07696704910623316; 0.06778818364618412 0.043135230507590154 -0.06804650438931745; 0.07436255240238467 0.07606038961648662 -0.12709435167822153; 0.06347921886829284 0.08594471588257148 -0.15769267215423396; 0.01766630557384591 0.02840327511494444 -0.06759395774068484; 0.01663135219866448 0.03038762764241381 -0.07571760507353686; 0.008487099956043881 0.019093159719702095 -0.05122495911137304; 0.005429242823577737 0.013592520241619947 -0.03934378475284749; 0.004831375792120475 0.013847023316961008 -0.04103059726964871; 0.0030750547835568906 0.009149517477499276 -0.029278834489741938; -0.0003673945345998109 0.0014250843063318187 -0.004811071590860092; 0.0010123618875314188 0.0018980358044673813 -0.006125062094743106; 0.0027052395359148727 -0.0008948472089746113 -0.0004451817917205832; -0.0006339653965799772 0.003051983817794548 -0.0005588766854987665; 0.00013950416057957789 0.0032615917032198633 -0.0056088926567513415; 0.0004526603792251254 0.0008654661338261505 -0.002839281347368504; -0.0001471450486107478 7.245244025540524e-5 -0.0005904271346204159; 0.004086011614919114 0.0010048785646358065 -0.004482796863429304; 0.00025668668442848817 0.00035398178584060847 0.006148072536404093; -0.009464842505664187 -0.0025822893627058564 2.3007066805038408e-5] %
+
+Mass Used: 90.60308402877672 kg
+Launch C3: 97.13346981514512 km²/s²
+||V∞_in||: 0.0005771579601026696 km/s
diff --git a/archive/ES_0.5633301254291854 b/archive/ES_0.5633301254291854
new file mode 100644
index 0000000..40bf3a5
--- /dev/null
+++ b/archive/ES_0.5633301254291854
@@ -0,0 +1,22 @@
+archive/ES_0.5633301254291854---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T02:17:22.581
+Launch V∞: [6.381593891391033, -7.489120448469649, 0.10666415700893167] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.351302227358847e-6, 3.08610594272355e-6, 2.538368382422998e-6] km/s
+ V∞_out: [4.385461128951578e-6, 2.823930314577965e-6, 9.126375164370433e-8] km/s
+ time of flight: 1.8326815406494915e8 seconds
+ arrival date: 2029-02-18T06:06:36.581
+ thrust profile: [0.2794207220195891 -0.06969067408558476 -0.09292788945059277; 0.07102502609412444 0.019278997725702005 -0.06967962698470848; 0.060681318602667914 0.03372887996207727 -0.10391885227522908; 0.0499991838465702 0.03782790838917552 -0.11721728819539923; 0.052733955799823304 0.05022294285218747 -0.1591069846887082; 0.035862764981822344 0.03879568549434063 -0.13046844939542385; 0.027090303123938068 0.03234874619767098 -0.1165996376723433; 0.011159587049352136 0.015509291825915643 -0.05863902077327212; 0.012036675517037252 0.01705942165697659 -0.06852160532977579; 0.0007538050452726625 0.0016678246215010792 -0.0012799665013322416; 0.0005159762191383542 0.00013646893589291183 -0.0029453069157419146; -0.00016770550145726854 0.0027098455251967804 -0.000697008848270403; 0.0006716526801971367 -0.0020473699442268224 0.0010701396215819184; -0.003295892543143541 -0.0016936571465607053 -0.0021697956717049234; -6.748917076131942e-5 0.0005104975527294891 -0.0012143955432499447; 0.00033931642219015663 0.00042841703013164886 -0.00010157115058693502; -0.004173330049637587 0.0011607751879444254 -0.0018210591795514222; -0.0010677586622255138 -0.0009848721938903711 5.2690533112338114e-5; -0.001546770464194045 0.0007294711783131865 0.0010333170992908045; -0.006207912356938863 0.0018397304530983522 -0.0019279414228789682] %
+
+Mass Used: 92.41739591653959 kg
+Launch C3: 96.82304292871599 km²/s²
+||V∞_in||: 5.215226797915766e-6 km/s
diff --git a/archive/ES_0.5633301601596301 b/archive/ES_0.5633301601596301
new file mode 100644
index 0000000..e752e06
--- /dev/null
+++ b/archive/ES_0.5633301601596301
@@ -0,0 +1,22 @@
+archive/ES_0.5633301601596301---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T15:42:39.523
+Launch V∞: [6.605598770749172, -7.428470202036419, 0.19609379796920906] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9039523917036127e-6, -3.911593886664157e-7, 3.379433340393781e-8] km/s
+ V∞_out: [5.700147816110852e-7, -1.3103182526987299e-8, -2.8912910153060405e-6] km/s
+ time of flight: 1.8749577787464294e8 seconds
+ arrival date: 2029-04-10T17:52:16.523
+ thrust profile: [0.12558422707993364 -0.03485469053288181 -0.04957876065458409; 0.10798629295577918 0.02369271637152107 -0.1272678262987738; 0.06463290135839209 0.028005047658074784 -0.12801816605902064; 0.03915957922225127 0.021190751244211978 -0.11227911459097834; 0.03782593162972583 0.02440030038762997 -0.13482547080938923; 0.02333810680877159 0.020827258851257715 -0.10623475937108867; 0.009276530084873173 0.007689372232954102 -0.048515843591318185; 0.011014146745815821 0.010016059468629063 -0.07473547622317962; 0.0036179692285608737 0.0034804230384730384 -0.022192280530364015; 0.0035917531027603814 0.0019716333639337455 -0.03440133607769264; 0.003826002060182667 0.005319172027715587 -0.029827892044537587; -0.00048344723203414073 -0.0009706124442062764 -0.00538454876309017; -1.1115673077466935e-5 0.0007975118448716964 -0.0052449881871180805; -0.0030169956380122023 2.9188103917322317e-5 -0.0031483445234056088; 0.0004048100846157902 -0.0035423843431196715 -0.0018346352894079558; -0.0028731565500645304 0.0038293001671275678 0.0013199472760723266; 0.003260575933336968 0.002325701021021519 0.001921005260092445; 0.00011507121538633329 0.0018451323695077015 0.00039276795339758357; 0.0009634916303956295 0.00039407730195292897 -0.0038784925461613556; 1.2625828023271526e-5 0.0021101696653966066 -0.0016963533428194487] %
+
+Mass Used: 80.5669351180054 kg
+Launch C3: 98.85455744026795 km²/s²
+||V∞_in||: 2.9303732215527145e-6 km/s
diff --git a/archive/ES_0.5633349227007522 b/archive/ES_0.5633349227007522
new file mode 100644
index 0000000..b529f73
--- /dev/null
+++ b/archive/ES_0.5633349227007522
@@ -0,0 +1,22 @@
+archive/ES_0.5633349227007522---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T10:08:02.810
+Launch V∞: [6.599049083820333, -7.288976977938084, -0.04791701522610356] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00046303580571438176, 0.0030605169215151082, -0.004144412894675106] km/s
+ V∞_out: [0.0035964194251489226, 0.002929625685155409, 0.002295179409633156] km/s
+ time of flight: 1.8749577783577138e8 seconds
+ arrival date: 2029-04-08T12:17:39.810
+ thrust profile: [0.3185247691401971 -0.08313874164490409 -0.10945050705958007; 0.0563328869061184 0.014946297270706102 -0.059786413421969144; 0.05750039832776472 0.029939361138521466 -0.10251904398590307; 0.058861033016274995 0.04133385487212839 -0.14628923422587314; 0.05085409303030537 0.04310560838978968 -0.16277933035602002; 0.026545795816312945 0.025582468991162694 -0.10522608036153457; 0.008890798571188328 0.010762886617511309 -0.04551132669539234; 0.005631965840589545 0.0060650806492215485 -0.03037853041655827; 0.01608643732809356 0.018394757763690206 -0.09512876567566537; 0.00024757294548648874 0.0014254027414554262 -0.007904253844711578; 0.0037427815892264547 0.0052942197140940055 -0.022799140132440124; 0.0019415493714693014 0.0009113251661422412 -0.0036205372297961023; 0.0007475322291863223 0.0016751698304813146 -0.006116360145175541; -0.0005053470759135173 9.432849748859272e-5 -0.00598197881283378; 0.0003067244407963525 0.0005143454635983301 -0.004024186078994088; -0.00288525244313726 0.0002790232050282824 -0.0005351794346095395; 0.00014982646629445518 -0.0028982245015261115 -0.001036610098665709; 0.0013495772882714354 0.003560735776191152 -0.004939112817699465; 9.152362356749152e-5 0.0003058821890019195 -0.0005810738547238868; 0.00039811510633268684 0.0017254986995004 0.004066411991737556] %
+
+Mass Used: 93.26365010795507 kg
+Launch C3: 96.67893023592957 km²/s²
+||V∞_in||: 0.005172748227567544 km/s
diff --git a/archive/ES_0.5633382945542251 b/archive/ES_0.5633382945542251
new file mode 100644
index 0000000..c274888
--- /dev/null
+++ b/archive/ES_0.5633382945542251
@@ -0,0 +1,22 @@
+archive/ES_0.5633382945542251---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T20:45:45.132
+Launch V∞: [7.54309665105469, -6.415278938799421, -0.1887905573746614] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008508597071325611, 0.0007048543137215416, -0.000523438900967257] km/s
+ V∞_out: [0.00013032377547797356, 0.0012144273619804392, -5.434507139954915e-5] km/s
+ time of flight: 1.644508815439435e8 seconds
+ arrival date: 2029-07-27T05:33:46.132
+ thrust profile: [0.21912188180140588 -0.04184415416196593 -0.08610880906521069; 0.056384515813632845 0.016944175621581552 -0.06820683877029442; 0.0658966749085367 0.0350880001545748 -0.13264693037978542; 0.06417170203112993 0.04361893404341136 -0.17986402120720232; 0.04829923762202337 0.03840733120272637 -0.17370237434472086; 0.03368456327686254 0.029981300877083658 -0.14774193200286953; 0.019554080582149747 0.018672740481333657 -0.10167520301566808; 0.007432174929732052 0.007324293012135289 -0.04534069861008; 0.009834685748414005 0.010130500947517869 -0.06859886602528782; 0.006730228716031622 0.0071400818445941285 -0.048587024848920184; 0.0007376422111236891 0.0008083600502592492 -0.006083532795175268; 0.0004758709192713644 -3.236300284136095e-5 -0.0012564563493061359; -8.550099693129882e-5 7.98927876812406e-5 -0.00026270654965283684; 0.0001506235056890654 -1.5072722529209362e-5 0.0005634977122889565; 4.8750479799330114e-6 -0.00017625985257946689 -0.0002818371884413794; -0.00044873504846509833 -1.2974304610910455e-5 -0.0004207990664838143; 2.323061573117577e-5 0.0001408078758487552 -0.00038763383302783613; 9.649200309876362e-5 0.0002971274625925587 4.187499401373646e-5; 0.00022909475926933848 0.00037442589484510763 -0.0006793484631008273; -0.00019881313786229693 0.00018648789931939135 1.2893743569561216e-5] %
+
+Mass Used: 85.0377855047891 kg
+Launch C3: 98.08975282430974 km²/s²
+||V∞_in||: 0.001222607920733128 km/s
diff --git a/archive/ES_0.5633400761844036 b/archive/ES_0.5633400761844036
new file mode 100644
index 0000000..1ec5910
--- /dev/null
+++ b/archive/ES_0.5633400761844036
@@ -0,0 +1,22 @@
+archive/ES_0.5633400761844036---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T19:55:17.015
+Launch V∞: [7.892132459199824, -5.5735917577963034, 0.20299909466236882] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00021658605193979142, 0.00045044071733191184, 0.00015420827366730117] km/s
+ V∞_out: [4.82773986182251e-5, -0.00029973844733643875, 0.0004411075434799198] km/s
+ time of flight: 1.8594684159531394e8 seconds
+ arrival date: 2030-04-02T23:49:18.015
+ thrust profile: [0.6476025396944252 -0.006187513322626859 -0.18163791324741513; 0.0532034287181704 0.03234017283135626 -0.057139523436151446; 0.03498390033319014 0.03467159641112591 -0.06767417813692407; 0.020869211076958678 0.027543790408658307 -0.060164073648309314; 0.013832570387700556 0.02313657786606312 -0.05562781352292191; 0.013125093653261966 0.02586689103614435 -0.07167268142675318; 0.009974337275689664 0.025165619214256595 -0.07020253676860724; 0.01073992457550446 0.02985346973886919 -0.08679365078718115; 0.003810075921768166 0.014584058389042196 -0.047082762055435434; 0.00943694525311926 0.042805400744803906 -0.13465361159470818; 0.0014380995853521326 0.010324506369073368 -0.03436770039826258; -0.000227612407168109 0.0008337174118181587 -0.005559089518169671; -0.0013534535497429442 -0.0006199325114232251 -0.002916657466169526; -0.0008131693189870231 0.0017209852826643353 0.0013962884683167537; -0.0015636171981723214 -0.008094431526947766 -0.003290306454820039; 0.0017849783504813432 0.0024912832579251244 -0.007597821515155801; 0.0023051147409577488 0.012567153565135453 0.0014961529270645024; 0.0065247840195881025 -0.010909059907901534 0.0002741103330234397; -0.0023447613343805128 -0.0005135197172377279 0.0011425907669847554; -0.0041086558161365 -0.006344532871796187 0.01647151339183942] %
+
+Mass Used: 112.44407281518033 kg
+Launch C3: 93.39188846856409 km²/s²
+||V∞_in||: 0.0005230550156463492 km/s
diff --git a/archive/ES_0.5633465338871801 b/archive/ES_0.5633465338871801
new file mode 100644
index 0000000..f431556
--- /dev/null
+++ b/archive/ES_0.5633465338871801
@@ -0,0 +1,22 @@
+archive/ES_0.5633465338871801---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T14:22:01.994
+Launch V∞: [6.641352847017035, -7.400649996933863, -0.10479822106609216] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0393100445646903e-8, 1.1991375322839921e-8, 6.640649824894731e-8] km/s
+ V∞_out: [-4.400696341665344e-8, -4.045260991666802e-8, -2.005635416640478e-8] km/s
+ time of flight: 1.874957778502819e8 seconds
+ arrival date: 2029-04-10T16:31:38.994
+ thrust profile: [0.15370810280248443 -0.044405908418605526 -0.059803183298532916; 0.06338302708809988 0.0135975393172647 -0.07786554898841772; 0.05091524913004638 0.02189702042921598 -0.10601067281880289; 0.04200213404028309 0.023831805389410553 -0.12233401759327274; 0.03281340644291336 0.022078900805101078 -0.12115533930974756; 0.026453569690938934 0.02012381595077979 -0.12185853823820449; 0.022325112493625284 0.018767216485335615 -0.11888716793416017; 0.007381165271145735 0.007198390222030397 -0.0478351113175149; 0.00460985385153716 0.0049439666675466344 -0.03354399603857004; 0.00879545222601021 0.006839905825423085 -0.04805446254203808; 3.435734304306078e-5 -3.853319115122788e-5 -0.0020716598059765234; 0.0008748484228797205 -0.0006158002136626701 -0.0019351918405682614; 0.0008066909959053336 0.00037074417380985616 -0.001318448911210079; 0.004559181883129878 -0.000761457681602183 -0.004392337369304658; -0.002028782722063246 -0.004267003664871054 -0.007007856407174559; 0.0002355824974926467 0.0016284466108193525 -0.0010011726277713124; -0.0021090005504673676 0.0006432641731033259 -0.005137351700372336; -0.00025645744857539826 -0.005621310243155516 -0.00578837970306543; 0.0046013304334305 -0.000747198611272067 -0.0010353018070965014; -0.0013585187818691603 0.002893268330810739 0.002008376195148642] %
+
+Mass Used: 80.38996055182724 kg
+Launch C3: 98.88817068283709 km²/s²
+||V∞_in||: 6.827614977936264e-8 km/s
diff --git a/archive/ES_0.5633475864436334 b/archive/ES_0.5633475864436334
new file mode 100644
index 0000000..006afed
--- /dev/null
+++ b/archive/ES_0.5633475864436334
@@ -0,0 +1,22 @@
+archive/ES_0.5633475864436334---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T22:26:31.265
+Launch V∞: [6.394135414774907, -7.530745944926503, 0.09872749293830951] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4793896077640155e-6, -0.0004940372256778232, 0.00040964535305132026] km/s
+ V∞_out: [0.0003312692209315898, 0.0005372155555321257, -0.00011545115852971162] km/s
+ time of flight: 1.7990754453515232e8 seconds
+ arrival date: 2029-01-09T04:45:35.265
+ thrust profile: [0.2007372038128276 -0.05776487407429738 -0.06873560857259788; 0.09055195539202672 0.022223051754575385 -0.09269842615843378; 0.06235597204247379 0.030994120457343823 -0.10479179413273403; 0.054583395423320476 0.037017186799869234 -0.12612595659779208; 0.06472991307994752 0.05563540037883867 -0.19049706753866155; 0.029760582599172997 0.02939600109352371 -0.11052101042499515; 0.022499443058634896 0.024607824278601684 -0.09864467650670182; 0.012716608155422996 0.014935815354723242 -0.06378036906765754; 0.008101817565514478 0.010455866436620017 -0.046007657055033804; 0.005668994979948625 0.008245959212616324 -0.03740069286571575; 0.0029653123622235687 0.0029855993303069305 -0.01476489439105726; 0.0001008178007904884 0.0007205743478212878 -0.003908869502501286; -0.00011132914868855198 -0.000288933514508269 0.0005442564990011479; -4.005531637701109e-5 -5.970339952620774e-5 0.00036600680161823077; -0.0002104838111045026 -1.7882897978791795e-5 0.0003048693382714902; 0.00017158996526109505 2.2560608603473398e-5 0.00038339089076577386; -0.00023484266891964472 0.00021646033662765568 0.0003610883877280571; -0.00023747324724588672 -3.61014660035103e-5 0.00015090919683207873; -0.00033432638446135183 0.0004986366053005189 8.067797163333314e-5; -2.387236244196044e-5 -3.588989410684926e-5 -0.00014539649583105655] %
+
+Mass Used: 87.86556322459501 kg
+Launch C3: 97.60684930736753 km²/s²
+||V∞_in||: 0.0006417821158505375 km/s
diff --git a/archive/ES_0.563355697095525 b/archive/ES_0.563355697095525
new file mode 100644
index 0000000..1ad781c
--- /dev/null
+++ b/archive/ES_0.563355697095525
@@ -0,0 +1,22 @@
+archive/ES_0.563355697095525---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T09:43:19.560
+Launch V∞: [6.588306931352555, -7.3459738649834545, 0.19099246950106938] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7665834661036254e-5, -3.0087467991112727e-6, 5.078287748516363e-8] km/s
+ V∞_out: [3.7238310621214184e-6, -8.852194688308129e-8, -1.7528251689654723e-5] km/s
+ time of flight: 1.8749577787493724e8 seconds
+ arrival date: 2029-04-09T11:52:56.560
+ thrust profile: [0.27713185927775896 -0.07404513084199887 -0.09421830813933334; 0.044993272249769505 0.012552620738091404 -0.05336787339212564; 0.0567980500443705 0.029733427877965388 -0.11079120366259049; 0.04786167170421146 0.03525772177801228 -0.13260575508396666; 0.025674692249024172 0.022244682159400214 -0.09019001229852149; 0.025972321091851186 0.0273583662458389 -0.11132765087658585; 0.010485728369077388 0.011507114486826344 -0.055043320301676246; 0.02605286115698717 0.03027916394746943 -0.1401733359079317; 0.004993396641991119 0.006532795633852213 -0.03431570772251166; 0.004339443330091435 0.005447186118089872 -0.029932005720219423; 0.0023728535809049676 0.0032294883495756423 -0.018913068185219095; 3.215970451318751e-5 0.0044938312779280185 -0.02243165555576749; 0.0011291525999157991 -0.0001546745852117012 -0.0006270742365837544; -0.00022201052143099037 0.002905636381596451 0.002061074956618887; -0.0014836017839217621 -0.0007180370833289765 0.0009664003619698817; -0.0012614086056642372 -0.00016496248432991314 0.0013959424380123875; 0.002134927752082636 -0.0012034696387601324 -0.0004703842181888419; -0.0003661171398930157 0.00028862143327890426 -6.686706813666728e-5; -0.002106483386461232 0.00551315240311669 0.0018088495572018426; -0.0030828292742374197 0.0004078570607614427 0.0019107838043624864] %
+
+Mass Used: 89.0489894523298 kg
+Launch C3: 97.40559837013419 km²/s²
+||V∞_in||: 1.79202915844826e-5 km/s
diff --git a/archive/ES_0.563358013615457 b/archive/ES_0.563358013615457
new file mode 100644
index 0000000..6a03f82
--- /dev/null
+++ b/archive/ES_0.563358013615457
@@ -0,0 +1,22 @@
+archive/ES_0.563358013615457---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:29:36.628
+Launch V∞: [6.555793239781128, -7.448980126598163, 0.14168358752519947] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010406269343807054, 0.0011267206741356565, 0.0011067370220010744] km/s
+ V∞_out: [-0.0011908170822815675, -0.0005494321604622172, 0.0013626292659566811] km/s
+ time of flight: 1.8429513842761663e8 seconds
+ arrival date: 2029-03-02T16:35:14.628
+ thrust profile: [0.17012064700925392 -0.043483151263408834 -0.06120779887770062; 0.048606680743448386 0.012853337736421944 -0.054696140047657625; 0.058095298391813266 0.02758673800946025 -0.10737856402615303; 0.03810149786249199 0.027471391569685966 -0.09774081642104257; 0.05150195620542309 0.04417782878511091 -0.15855294001476214; 0.03620962701028212 0.03554688284608956 -0.13735675038466083; 0.02957008173961419 0.03506104513965465 -0.13495243693062275; 0.012629188742687092 0.012718599037504634 -0.06309400767340524; 0.003686145037188378 0.0036258712273072903 -0.02132353408316218; 0.004844823183274046 0.006202318534988626 -0.0325034698827412; 0.0015415171917074531 0.0013260205879666869 -0.010932612449771095; -0.0006662877581098508 0.0004916834203796579 -0.004432534580511115; -6.647438527856021e-5 0.003710081230781046 -0.0022612608776542407; -0.0011734597280936283 0.0023255489434245366 -0.005061982740660767; 0.0028171496476367395 0.0001055955108587353 -0.0032874623671048063; -0.0007196345193687256 -0.0006707917204813066 -0.005038453660178239; 0.0023190324768794365 0.0037404356285626918 0.00026886317247348595; 0.0008989999291757853 0.0007215129183703339 -0.0027159144417428023; 0.006217030687630847 0.0037887448702137597 -0.0009347141008534256; 0.0010401395854120858 0.0011401601112344946 -2.913913047520667e-5] %
+
+Mass Used: 82.75049157026797 kg
+Launch C3: 98.48580416818832 km²/s²
+||V∞_in||: 0.0018913674233080942 km/s
diff --git a/archive/ES_0.5633749491143726 b/archive/ES_0.5633749491143726
new file mode 100644
index 0000000..3017fa4
--- /dev/null
+++ b/archive/ES_0.5633749491143726
@@ -0,0 +1,22 @@
+archive/ES_0.5633749491143726---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T20:05:05.076
+Launch V∞: [6.361650615604543, -7.452302174009063, -0.21416144025244738] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.628067851762664e-6, 4.625371881232973e-6, 4.507272868210123e-6] km/s
+ V∞_out: [6.693808971435082e-6, 4.278321571843955e-6, 1.2011495792248306e-7] km/s
+ time of flight: 1.829456352577444e8 seconds
+ arrival date: 2029-02-14T06:19:00.076
+ thrust profile: [0.32584782455948585 -0.09134965523759493 -0.12188161943274287; 0.1183776518293007 0.028303128702067887 -0.13150904485115153; 0.06901409453245998 0.033384223785992914 -0.12891388447405663; 0.051149784276806526 0.03393974928426388 -0.13508526642975358; 0.03491690612301626 0.02822809692510836 -0.11839688703057501; 0.026600566612442183 0.02460969553663777 -0.11123810401429236; 0.022226747428085877 0.023853683768945876 -0.10785532433842521; 0.01214253373632781 0.013986768092528386 -0.06936954282752827; 0.006338396881292872 0.006550802329229233 -0.037422089623654634; 0.0004227235965394624 0.0008921188886666593 -0.00336396342507206; -0.00032235333881993234 0.0004113373351054409 -0.002216065940676187; 0.0003703442736365618 0.00033062479367982137 -0.002715834592177813; 0.0008029046995480445 0.00038981970001484304 -0.0010568180689004589; -0.0009696585585983856 0.0030891174602601795 -0.0011067167119362571; -0.0003836190974570232 -0.00026869975815416495 -0.0006668643789631695; 0.004031912285503687 -0.0013028443029264108 -0.00018562189118206528; -0.00014117230012503047 8.996112091539323e-6 -0.00016785276208320415; -0.0003133359362201504 -0.0008543363595588766 0.0021625804173220397; -0.0005192945584122004 -0.00010891115556204456 -0.00031387721284464496; 0.0032596868974540203 -0.002422038196453435 0.003803307819893264] %
+
+Mass Used: 96.96002430695944 kg
+Launch C3: 96.05327137025289 km²/s²
+||V∞_in||: 7.945349947530495e-6 km/s
diff --git a/archive/ES_0.5633799334953303 b/archive/ES_0.5633799334953303
new file mode 100644
index 0000000..79d06c8
--- /dev/null
+++ b/archive/ES_0.5633799334953303
@@ -0,0 +1,22 @@
+archive/ES_0.5633799334953303---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:53:11.150
+Launch V∞: [7.661412005837325, -5.796062123442398, 0.04702504505440858] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9543241748145093e-6, -1.981682437836004e-5, 0.00037143297560336555] km/s
+ V∞_out: [1.5966712139010416e-5, -0.0003714471878563814, 4.0591168000460385e-6] km/s
+ time of flight: 1.836250483447667e8 seconds
+ arrival date: 2030-03-05T18:50:39.150
+ thrust profile: [0.5821616326217978 0.006441879313587664 -0.14046731232167053; 0.1763736422322465 0.11535763859350447 -0.14751296281374612; 0.06939834528886063 0.07842994762659058 -0.1101927417051876; 0.030077776300747892 0.04791310599089385 -0.07570465129411884; 0.025125905086449463 0.05167299704362456 -0.0874581479643496; 0.008061005163210799 0.022863497420209152 -0.04229788470183502; 0.015400827880592032 0.0488195277349852 -0.09262872349454324; 0.008855366543594569 0.023861670335336673 -0.04679818230391314; 0.006028067904434414 0.026317452779711724 -0.05593042334417812; 0.0054704123838436895 0.030338854899360047 -0.06545052543942385; 0.00042360590449164984 0.0062360367293783706 -0.013619636984245757; -8.888363100462311e-5 0.0027283432559888857 -0.001076885340856789; 0.00047955381652122544 0.006708057509449434 -0.014376632384031014; -0.0013081598365631535 0.0010085090643593905 -0.0012987993510082552; 0.0027953072910606655 -0.0009249908634933926 -0.0022036846329268555; -0.006426848567014392 0.00028444023470245794 -0.004066930978147513; 0.001677383827858352 0.00221081561017502 -0.008978436270197569; 0.004821230680738267 0.004846434851968506 -0.0005945140306755812; 0.0003610711752227839 0.0017033808387276143 -0.004682657812617903; -0.0010530473515627105 -0.0057253437396101075 0.005525176921571337] %
+
+Mass Used: 118.89619747956885 kg
+Launch C3: 92.29378141685427 km²/s²
+||V∞_in||: 0.0003719663711641059 km/s
diff --git a/archive/ES_0.5633823311410312 b/archive/ES_0.5633823311410312
new file mode 100644
index 0000000..3d8a0a2
--- /dev/null
+++ b/archive/ES_0.5633823311410312
@@ -0,0 +1,22 @@
+archive/ES_0.5633823311410312---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T14:37:10.610
+Launch V∞: [6.441856515132233, -7.48181538059899, 0.02159597167117254] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012229311591476489, -0.00036924199348023544, 0.008454995602495576] km/s
+ V∞_out: [-0.01426768820338074, 0.00014417652090137153, 0.0041924012280238395] km/s
+ time of flight: 1.8523647028561804e8 seconds
+ arrival date: 2029-03-15T13:11:40.610
+ thrust profile: [0.3003665500038398 -0.094652512750505 -0.1048576916437855; 0.019185342256188818 0.003984912230915928 -0.023591009526515185; 0.046145475894340725 0.01682015011550279 -0.0951018837570868; 0.03960518489255373 0.017979597692618084 -0.11209033254690565; 0.052021743576285785 0.029188748990810604 -0.19233287889361045; 0.022439143472123835 0.014973678439038143 -0.09854542639760157; 0.02640383815780137 0.01832016837206934 -0.13886773404350444; 0.012018949765752558 0.008332609543003208 -0.06357608089214763; 0.006217279504211124 0.007752793390170229 -0.056271771012585424; 0.0013510364160638337 0.0005385466121338443 -0.002427452056829425; -0.0002830626813542256 0.0018890905671892291 -0.00402947736403547; 0.0003411073326648208 -0.0005838916312900563 -0.00614146486393145; -4.588042612560408e-5 0.0008937180207914918 -0.004981934736107009; 0.0009644405669485487 0.002379901869754532 0.0009214086238226093; 0.0006055867909441209 -0.001443627783878146 -0.00011969135971949324; -0.0005227607716290594 -0.0035708931451997926 0.0016077539123027598; -0.0010481670345991187 -0.0003840900161583417 0.0005351098618132429; -0.006810544693010198 -0.003262336720957143 4.037273191712185e-5; 0.0035093136653445286 -0.0009480818767774626 0.00016294157020466668; -0.0036290293814493038 -0.002580196373428125 -0.0013453493550817856] %
+
+Mass Used: 88.67205136588518 kg
+Launch C3: 97.47554313691164 km²/s²
+||V∞_in||: 0.014872099794225092 km/s
diff --git a/archive/ES_0.5633831303580078 b/archive/ES_0.5633831303580078
new file mode 100644
index 0000000..36aaf27
--- /dev/null
+++ b/archive/ES_0.5633831303580078
@@ -0,0 +1,22 @@
+archive/ES_0.5633831303580078---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T13:19:39.921
+Launch V∞: [6.641352317371529, -7.426733135601996, 0.07361768489539043] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.929026889726817e-9, 1.0033854683481074e-9, -7.305327984689297e-9] km/s
+ V∞_out: [-2.2534170734471745e-9, 5.223505693022778e-9, 6.808032121164169e-9] km/s
+ time of flight: 1.8660188368185934e8 seconds
+ arrival date: 2029-03-31T07:11:02.921
+ thrust profile: [0.13484049833615824 -0.038839000436049306 -0.05542595945400534; 0.04695117111411346 0.009595012107047248 -0.059604769707895626; 0.049362156856083694 0.020274657388439598 -0.10466952364654462; 0.04419293129421871 0.023878472820927917 -0.13002997877084924; 0.0370715539183414 0.02365124501982113 -0.13903548634020665; 0.024068966517222932 0.017004205358075425 -0.1087307314020944; 0.012999032108148938 0.010036798231747855 -0.06944984834149211; 0.011045929815019917 0.008838815324454637 -0.06573204060464492; 0.009929291017866293 0.008229683030593023 -0.06504157149307696; 0.005225617706900257 0.004273877554250368 -0.037073912450564885; 1.6561172049072207e-5 -0.00021671905684908684 -0.001345508943583008; 0.0018302254640021735 0.0025080578479118355 -0.020961334132314744; 0.0022474916301505393 0.0023083350623576853 -0.020957908501996293; -0.00022268725022260097 -0.0001277186315204082 -0.0035672695058747298; -0.000268742849077572 0.00037238951246008065 -0.00256589910948605; 0.0033498209589684206 -0.00044119934480426915 -0.003997933442334125; 0.0001271078185253677 0.00018560246440689937 -0.0009556272776302243; 0.00017257321871125852 0.0002235323999114877 0.000397263888420399; 0.004171352144745115 -0.00037211343370112827 -0.0053527794353156995; 0.0019502252211941085 -0.002719178523309632 0.0018468993519452689] %
+
+Mass Used: 78.2091382168096 kg
+Launch C3: 99.2693452344342 km²/s²
+||V∞_in||: 8.869605709479241e-9 km/s
diff --git a/archive/ES_0.5633954611579176 b/archive/ES_0.5633954611579176
new file mode 100644
index 0000000..a5bb4f7
--- /dev/null
+++ b/archive/ES_0.5633954611579176
@@ -0,0 +1,22 @@
+archive/ES_0.5633954611579176---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T19:46:39.001
+Launch V∞: [6.446463644515437, -7.3798987810767915, 0.21049081498619154] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.0690314902201744e-6, 6.641285705503458e-6, 7.793253670886336e-6] km/s
+ V∞_out: [1.0473346934590827e-5, 6.711015629280747e-6, 2.1106497875601628e-7] km/s
+ time of flight: 1.8401742495011395e8 seconds
+ arrival date: 2029-02-26T15:43:43.001
+ thrust profile: [0.3777754311290419 -0.10587716525926924 -0.13512056298070294; 0.04679880447585072 0.011645785991791127 -0.05366202279983209; 0.05842510651323853 0.02897235502544666 -0.10928893020938192; 0.05508063646503762 0.0366050065580478 -0.14234936482417887; 0.04638762455062328 0.03717222040493293 -0.15285569397355453; 0.03181275758667209 0.029363595727259193 -0.12867908632980343; 0.020825030039315646 0.021637381449418087 -0.10014753968579491; 0.008236611671535221 0.010361904209007579 -0.050718129572182136; 0.0042590333563529564 0.005159389721274119 -0.031036870911512124; 0.0038298188490199442 0.004772450044791847 -0.02489151293359063; 0.0005955003923677647 0.0011342401176231943 -0.004531441406733016; 6.941720690624301e-5 -0.0018575960875944495 -0.002195718060890303; -0.0010641521167909977 -0.0008791718398939484 0.0009048195530392033; -0.0012268248098696206 0.0019299474646398132 -0.0003072165001641383; 0.0005279696211695044 0.0006816490966667064 -0.004534965913845949; 0.0003943515972190253 -0.0027609555564619805 -0.0009884528043595812; -0.0004627191683531486 -0.0038545177636941643 0.006647365504634422; 0.00021507255873165704 0.0005531384243717455 -0.003447252082350528; -0.0026802905031750738 0.0015464289715562195 0.001519738708863324; 0.0032621470053430385 -0.000528297888583881 -0.001158288673070963] %
+
+Mass Used: 96.92075347145328 kg
+Launch C3: 96.06410592219153 km²/s²
+||V∞_in||: 1.2442374564793988e-5 km/s
diff --git a/archive/ES_0.563403523803117 b/archive/ES_0.563403523803117
new file mode 100644
index 0000000..c36fed5
--- /dev/null
+++ b/archive/ES_0.563403523803117
@@ -0,0 +1,22 @@
+archive/ES_0.563403523803117---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:24:38.841
+Launch V∞: [6.35770530689376, -7.469724538596185, -0.3138749895103898] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03135425632179639, -0.000506358032853029, 0.02595492168825008] km/s
+ V∞_out: [-0.03987503067271746, 0.0003058975174129201, 0.008170889449957773] km/s
+ time of flight: 1.8749577787456682e8 seconds
+ arrival date: 2029-04-10T12:34:15.841
+ thrust profile: [0.3388692471806347 -0.0754456800062265 -0.12125973892853303; 0.0941442228964058 0.02997494324468229 -0.1104075320629617; 0.06257257795535563 0.03662320684289178 -0.1236498898308651; 0.04723615775475421 0.03560733699447481 -0.12655458696967442; 0.030128332787147584 0.02794294178868886 -0.10683062195583222; 0.02405945811088027 0.025067147387103358 -0.10287985708094953; 0.017836058623519148 0.02139098332541557 -0.09279338089052949; 0.009697481777216677 0.012803782155352151 -0.05880065762518143; 0.0040775759988494285 0.0056482281739835445 -0.027340962928319973; 0.00446195071444302 0.0065691365470676565 -0.03170522200281147; 0.0022269018918879566 0.0032891128312404557 -0.017636864168497277; -0.001251731580955234 -0.00036609783796743835 -0.003283701967673309; -0.0007456204960280648 -0.00032055723130328573 -0.000938733382074893; 0.000933037813375193 0.0006757546804294424 -0.0012998871062252439; 0.0010706746256966804 0.0015142656095131254 -0.0008446752917551881; -0.0002647876645792411 0.0015048177094366356 -0.0017658283327088551; 0.0009485926049750197 -0.0022295302709508464 -0.0005821046331695623; 0.002119497289171223 0.0008154615603996864 -3.322761062865044e-5; -0.0005537756661400869 0.0007670094068433159 0.0007276290664485093; 0.0006803237560138887 0.0020502538679786123 -0.002095573008945979] %
+
+Mass Used: 95.46241716533768 kg
+Launch C3: 96.31571896085121 km²/s²
+||V∞_in||: 0.04070631090867285 km/s
diff --git a/archive/ES_0.5634070027207263 b/archive/ES_0.5634070027207263
new file mode 100644
index 0000000..68f41cd
--- /dev/null
+++ b/archive/ES_0.5634070027207263
@@ -0,0 +1,22 @@
+archive/ES_0.5634070027207263---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T01:50:48.172
+Launch V∞: [6.370032804858611, -7.435426427374005, 0.21997036641068735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7251782833286014e-8, 2.7701797133292265e-8, 1.8727358204618386e-8] km/s
+ V∞_out: [-9.603442233526822e-9, 2.0172446001937892e-8, -3.174726869582695e-8] km/s
+ time of flight: 1.8403151077044228e8 seconds
+ arrival date: 2029-02-27T01:42:38.172
+ thrust profile: [0.3716017678789225 -0.09633859183112047 -0.12618092989643753; 0.058058765637696 0.016498453463243322 -0.06032199770220936; 0.06112282926232205 0.03351786194032604 -0.10537066045846076; 0.059552702676188285 0.04409891047131167 -0.14231017251835876; 0.04112719210262032 0.037170913839122244 -0.12668210245852854; 0.023985658613501423 0.025481995449985355 -0.09081662821928295; 0.02652105900614783 0.03043711511142605 -0.1172689379474093; 0.023596724688223013 0.03035697557815402 -0.11950531382681685; 0.004568889128204435 0.006437495141723423 -0.027978136643954522; 0.0008487410324708608 0.0015777171131553993 -0.002966659121830925; 0.0011067770638780799 0.0010022678504980815 -0.005510796317605885; 8.014941169894423e-5 0.0022710712688263435 -0.0024888381848175963; 0.0005447036964950013 0.0007283854268336787 -0.005592148313370216; 0.001319432891576962 -0.0010450206921100305 -0.002219926394375048; 0.0005224739270857919 0.0012339958492807097 -0.0019253185167919858; -0.0004417174087472856 -0.0034142261354485294 -0.0003383604319506005; -0.0006297277566321617 -0.003308808684000451 0.003132503534959771; 0.0014085088562409242 -0.0017019822428872553 -0.0005307588168698121; -0.0023612505065142156 -0.006775514422243373 -0.0010547937290687744; 0.0010252400772815574 0.0028300528097433826 -0.0019480078894427084] %
+
+Mass Used: 97.82575535938213 kg
+Launch C3: 95.91127105396546 km²/s²
+||V∞_in||: 3.762615474194817e-8 km/s
diff --git a/archive/ES_0.5634107202626096 b/archive/ES_0.5634107202626096
new file mode 100644
index 0000000..68b66b7
--- /dev/null
+++ b/archive/ES_0.5634107202626096
@@ -0,0 +1,22 @@
+archive/ES_0.5634107202626096---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T00:36:21.605
+Launch V∞: [7.736667873868173, -5.779910555341807, 0.10686089862877561] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4751526436198535e-9, -2.185547556403502e-9, -1.9605809652205805e-9] km/s
+ V∞_out: [-7.052500718714226e-10, 6.179876630309506e-10, -1.7943010111841346e-10] km/s
+ time of flight: 1.803084967234031e8 seconds
+ arrival date: 2030-01-25T22:17:57.605
+ thrust profile: [0.5764260293795694 -0.015669499986623765 -0.16410555454744832; 0.10590257631367633 0.05866383975020646 -0.10718219403192535; 0.054365792243982095 0.04993502840453645 -0.09864990026276278; 0.05187783167506651 0.06417629961578838 -0.13900540878449025; 0.05280489606046715 0.08156072791939072 -0.18951906272366667; 0.020745403403766766 0.03773848882336361 -0.09666728033117834; 0.007841753094396345 0.016829497974864452 -0.04542278716281047; 0.006127065525976335 0.015148759735208744 -0.042924598589141924; 0.001050759667824713 0.004255971011051676 -0.009364300558906705; 0.004400931477199671 0.0004876982176626344 -0.005651336620368292; 0.005691346566709785 0.0004760739982045247 -0.0047784621865293924; 0.0009572410170240675 -0.002559124174582853 0.0011723187006616835; 0.006053307846118971 0.008049070082723774 0.0005479309259967752; -0.0060743410271500865 -0.006790697573061502 -0.002512780968082515; 0.001040219622330693 0.0043772019084578765 -0.004669706113694763; 0.008775184224304624 -0.00868183936608942 -0.0045325009038361674; -0.00427851703030251 -0.0006195787207599612 -0.017135339197712034; -0.004378966572812922 -0.0011651215236825451 0.004862262371858083; -0.00042065150301931096 0.0048723900011309685 -0.021796860021313872; -0.002425003444001657 0.0014992411936584223 0.001294230531888046] %
+
+Mass Used: 113.20941906499547 kg
+Launch C3: 93.27481506995127 km²/s²
+||V∞_in||: 3.840166201052362e-9 km/s
diff --git a/archive/ES_0.5634114615211568 b/archive/ES_0.5634114615211568
new file mode 100644
index 0000000..2a0aecf
--- /dev/null
+++ b/archive/ES_0.5634114615211568
@@ -0,0 +1,22 @@
+archive/ES_0.5634114615211568---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T02:35:04.660
+Launch V∞: [7.824538072550298, -6.164125033926476, -0.05819971335718422] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0001121460217175034, -9.70819455079905e-5, -7.420790748158006e-5] km/s
+ V∞_out: [-1.5077806479029623e-5, 0.00010429654251448545, -0.00012806775744707652] km/s
+ time of flight: 1.756002596641084e8 seconds
+ arrival date: 2029-12-06T12:26:03.660
+ thrust profile: [0.1383620607960002 -0.016776986142456846 -0.054276123532246555; 0.030884514070401454 0.010702949422768398 -0.0394453996429163; 0.05340051761767081 0.031152530080891788 -0.11502874508338769; 0.053902071596795914 0.03946585646052759 -0.1639864358791223; 0.04277972157562216 0.03577103814804742 -0.16743875328679278; 0.026880046567022673 0.023961070684468285 -0.12736441008873012; 0.015121687006615973 0.013858149987550365 -0.08390580602790383; 0.012068701886788996 0.010843923404278904 -0.07142073162474924; 0.005885588853168644 0.00554535943007493 -0.03840331412219853; -0.0007661366441585971 -0.0014947955643010145 0.0015667822557674403; -0.0018160053459488712 0.007264064244381614 -0.0019033238959764633; 0.0026214122726073716 0.002265710021746542 -0.02040653553733429; 0.0012145837379660552 -0.00040421902059877696 -0.009019864572420943; 0.0003913695945368309 -0.0014357349907016662 0.007603199920565173; 0.0008123567287359911 0.0012830940869997284 -0.010633930675120674; 0.003448535586299857 -0.00041099610445254476 0.001307113248359723; 6.053577289751705e-6 0.00011645564363329847 -0.001390271229874989; 0.0034457945093609916 0.0027431154479514498 -0.008077169984082658; -0.000927291481294913 0.007885376098597206 0.003083484804068599; 0.003409139194549793 0.004411360002912057 -0.02491292178391629] %
+
+Mass Used: 78.51125108708175 kg
+Launch C3: 99.22322068930306 km²/s²
+||V∞_in||: 0.00016585670882865707 km/s
diff --git a/archive/ES_0.563414645034103 b/archive/ES_0.563414645034103
new file mode 100644
index 0000000..e5af3ed
--- /dev/null
+++ b/archive/ES_0.563414645034103
@@ -0,0 +1,22 @@
+archive/ES_0.563414645034103---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:51:25.927
+Launch V∞: [7.682909250862634, -5.569200669558539, 0.5458512509663764] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.956527937871431e-7, -2.0326658549658772e-6, -5.761573436518458e-6] km/s
+ V∞_out: [-5.4734343709396415e-6, -6.40805788031278e-7, 2.683161433314908e-6] km/s
+ time of flight: 1.874957778746238e8 seconds
+ arrival date: 2030-04-17T19:01:02.927
+ thrust profile: [0.7633749329958422 0.03373308293954463 -0.1313575792091989; 0.17746693229030674 0.12286985825513241 -0.12589937139911705; 0.09731464125580519 0.11762582017074352 -0.1410375827423246; 0.05224069579225081 0.08946828605590451 -0.11555310000241949; 0.03326546506459786 0.0758629415415694 -0.10798372166671595; 0.017232822187768355 0.05649361213181348 -0.08610503272024837; 0.004963390191613054 0.020321981261533485 -0.03556937852967991; 0.0017117711706613596 0.009431189834573483 -0.01809139385554717; 0.0009915401935490357 0.0057577052754089605 -0.011740954314836613; 4.3682929474731414e-5 0.0018367155625936746 -0.0031812275502026066; 0.0001954128250884744 0.0025488546918643615 -0.006075654973676969; -0.002389653952743203 0.006096203918026168 -0.015171435930336801; -0.0007255295661433406 0.0006679852778598595 0.002001526458426667; -0.0016785022541348923 -0.0011488680132220894 -2.0392552559673734e-5; -0.0015531591294868359 -0.0006889162576700423 -0.0002900803260385554; -0.0012587470302712978 0.00017727010186233735 -0.0020191692259080387; 0.0013268302718368109 0.0004144212873604322 0.0005935428360811775; 0.0002937713210145312 0.0021588391636805536 -0.0007986713393668627; 0.00031405041863395104 -0.0008979741247506533 0.000297426183773466; -0.0006921474650609636 -0.0018846997910896778 0.000295422133842108] %
+
+Mass Used: 130.32766112238323 kg
+Launch C3: 90.34104424298347 km²/s²
+||V∞_in||: 6.138587882655562e-6 km/s
diff --git a/archive/ES_0.5634178556125704 b/archive/ES_0.5634178556125704
new file mode 100644
index 0000000..82029b5
--- /dev/null
+++ b/archive/ES_0.5634178556125704
@@ -0,0 +1,22 @@
+archive/ES_0.5634178556125704---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T19:34:19.786
+Launch V∞: [7.60991402473862, -6.318350841482311, -0.20385974930089826] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00019704883619046828, -0.00016261026934149539, 0.00011640463823286323] km/s
+ V∞_out: [-4.2706426358176995e-5, -0.00027720868514484383, 1.2240611835802532e-5] km/s
+ time of flight: 1.6969358171355668e8 seconds
+ arrival date: 2029-09-27T20:40:40.786
+ thrust profile: [0.2559324047304462 -0.04693436168244024 -0.10717717739583893; 0.07272609442005253 0.019581077511420335 -0.09449505530125156; 0.05248984563376871 0.023897882379450907 -0.11719228196600057; 0.04445801700142856 0.02506597713438689 -0.13933461787475376; 0.04421660893340273 0.027779793522518557 -0.17633534043082139; 0.025283631832219714 0.01714880103078346 -0.12335074549710899; 0.01745067069102657 0.012535207480397487 -0.0999554006678818; 0.008529181543842513 0.006427018889584565 -0.05610717899740961; 0.007139219794199015 0.005511549560635972 -0.052247498279131534; 0.0005442088269813193 0.0010257824503396148 -0.007541281923448795; 0.004115818054778902 0.003344509524654985 -0.03375088282313815; 0.00039878646401084617 0.001031183573380754 -0.0018247403500172665; -7.110192680504358e-5 -0.0009362034489935574 -0.00021504928037174983; 0.0007729780020895456 -0.000623051554705728 0.0013933653408832727; -0.0022382384553976385 -0.0002582842235110995 -0.0007306677056856401; 0.0026774951502008884 -0.004824044818135803 -0.0011238400959795564; -0.00011104713222019039 0.0002626358471038827 0.005097484763200764; -0.0063661070762081814 0.002349496736411523 0.0024047177276692168; -0.003080992564492986 0.003314038818745762 -0.0031917865797070283; -0.00042497672776704084 -0.0013400905501608764 -0.0004075371125987397] %
+
+Mass Used: 86.38970378007252 kg
+Launch C3: 97.87390761735878 km²/s²
+||V∞_in||: 0.0002807496809285016 km/s
diff --git a/archive/ES_0.563420324712669 b/archive/ES_0.563420324712669
new file mode 100644
index 0000000..a53d6ea
--- /dev/null
+++ b/archive/ES_0.563420324712669
@@ -0,0 +1,22 @@
+archive/ES_0.563420324712669---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T18:22:27.914
+Launch V∞: [7.81148846926367, -5.558335355719731, -0.20990947648168698] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.983654870365487e-8, 3.921974772353271e-7, -7.12665321708219e-6] km/s
+ V∞_out: [-1.2740496597908742e-7, 3.73563079364305e-6, -3.286876925674719e-8] km/s
+ time of flight: 1.874957778713299e8 seconds
+ arrival date: 2030-04-19T20:32:04.914
+ thrust profile: [0.637195205744195 0.008807282034527837 -0.17336066712669287; 0.18396211256204362 0.1198795561338053 -0.18184021097051448; 0.056693422216328525 0.060423626669604186 -0.10711956362973993; 0.03523810755010706 0.05221213686146597 -0.10229742961964389; 0.018779451279213214 0.0362140363004438 -0.0774870262681336; 0.02980308920051905 0.05138114523567772 -0.1248575134956279; 0.00562055550976036 0.016827954568264195 -0.042430260596498015; 0.0047557664582317735 0.015821312462522472 -0.04129760148342008; 0.001993853513274415 0.0072883587273727055 -0.02159592206599789; -0.0005536353325872544 0.0018699881693445654 -0.0022474257905426755; 0.0005126154903145851 0.0020939504983706657 -0.008015379668136232; -0.002900216753350473 -0.0005052694299270682 1.4178968460347614e-5; 0.0006018003688609863 0.0048510980155738745 -0.014513272962007308; -0.0011749455738387653 0.0026013362741518203 0.0027952979946009437; -0.00039573164479424466 0.0029461694067341787 -0.0028647055746590013; -0.0012470863880957779 -0.00527237090886206 -0.0013616478879721486; -0.0036689663087224066 -0.006422099034767978 0.003296658225898551; -0.00042644172965524774 -0.003181969306184142 0.010687044362738192; -0.00959806179097522 0.010264236503541448 0.005486224509910062; 0.00033404831642844593 -0.000400412652000168 0.0014141333147124065] %
+
+Mass Used: 120.89909371244676 kg
+Launch C3: 91.95850602040008 km²/s²
+||V∞_in||: 7.137610848125889e-6 km/s
diff --git a/archive/ES_0.5634207059300949 b/archive/ES_0.5634207059300949
new file mode 100644
index 0000000..91a3668
--- /dev/null
+++ b/archive/ES_0.5634207059300949
@@ -0,0 +1,22 @@
+archive/ES_0.5634207059300949---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T07:27:58.969
+Launch V∞: [6.186874049391928, -7.382665879809458, 0.17494607675112514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.777698825300361e-9, 5.680843603649377e-10, -8.680291319500034e-9] km/s
+ V∞_out: [-1.977962508080563e-9, 4.617138922315419e-9, 6.439180921210671e-9] km/s
+ time of flight: 1.8318918757362413e8 seconds
+ arrival date: 2029-02-15T13:21:05.969
+ thrust profile: [0.5752133589475813 -0.15152793998812006 -0.18002653497960214; 0.09556420727298684 0.026637935581747273 -0.09444663160404644; 0.11706471043684609 0.06473557005614239 -0.18823316996892692; 0.06779526546545461 0.05117885851738616 -0.15492899670489038; 0.04708163609079833 0.043585478008580425 -0.1393192623050297; 0.036205354561647356 0.039049477594260196 -0.1312875614616273; 0.010866709809908878 0.013381615276285924 -0.04855186233078925; 0.0025596588924402053 0.0033646552079759913 -0.01319462968649552; 0.0027290797715774787 0.004176276687928142 -0.016473516347997638; 0.0020785142695876535 0.003729338753273361 -0.014632863546286809; 0.00019094527318306575 0.0005225853565130207 0.00039949982237416203; 0.0012782592047809556 0.0018284775638646256 -0.0010524755698561828; 0.0005567470869667164 -0.0006500672337226559 -0.0016552541139937022; 0.000985656667903885 -0.00011681525338777277 -0.0035245213431627713; -0.001457917884884581 0.0010998941283025495 -0.000629379517484571; -0.0024604690301915704 -0.0056791905429726 -0.001433846003468045; -0.004179363652560606 -0.0031335909967666327 0.0011017015104575877; -0.0003653352657313429 0.0007350796280439821 -0.0007989120729346901; -0.003084611382449564 0.0016069221334099769 0.0014319162172111467; 0.0019208409829301167 0.0018345412928376503 -0.0014380111126861956] %
+
+Mass Used: 115.9221528517869 kg
+Launch C3: 92.81177212571265 km²/s²
+||V∞_in||: 1.308715291995012e-8 km/s
diff --git a/archive/ES_0.5634207403872425 b/archive/ES_0.5634207403872425
new file mode 100644
index 0000000..f3a6791
--- /dev/null
+++ b/archive/ES_0.5634207403872425
@@ -0,0 +1,22 @@
+archive/ES_0.5634207403872425---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T01:47:27.014
+Launch V∞: [6.325758214116424, -7.424858771499747, -0.04368426447073303] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.183890791511984e-8, -5.1220993116553984e-8, -3.531237329687045e-8] km/s
+ V∞_out: [1.56692508862e-8, -3.1937113451693114e-8, 4.928018243546913e-8] km/s
+ time of flight: 1.8749577789578754e8 seconds
+ arrival date: 2029-04-08T03:57:04.014
+ thrust profile: [0.33529363731295053 -0.0702867170610771 -0.09325147238805222; 0.12206012931091331 0.04858656915409086 -0.10611978874382952; 0.13818078561793048 0.09585139908454413 -0.18798415692880502; 0.04132685521940444 0.039299787490297014 -0.08750456514537072; 0.04187815899045552 0.05136846904738714 -0.1139370681734744; 0.02994585552200122 0.04231449946271185 -0.10385030276150482; 0.012730912101487492 0.02028149583047038 -0.05271373946416573; 0.011373119180416634 0.022998675808922574 -0.05595175439996013; 0.011189136832796284 0.01976818064383648 -0.05785720018363433; 0.006251466485489356 0.016165129555427392 -0.042827421263286806; 0.0009640311127960315 0.0024050171279455263 -0.007143258840287414; 0.0003968189827677398 4.7811979601883016e-5 -0.00034627309862124065; -0.00024368358316709265 0.0007306193289324495 -0.00111863370012566; -0.00010612223191452147 -1.3163686265878672e-6 -0.0003223408212285095; -0.000737108034053991 -0.00010528966332258084 -0.0006099625320679244; 0.00017152081941346117 -7.213456117238651e-6 -0.0004974858085680712; -2.4951024988907318e-5 0.00011083185242762086 -9.528937789733314e-6; -0.00012916428370044597 0.00016921916341997728 -0.00024301673500574993; 0.001293102626940419 0.00048245343407764333 -0.0010331660806154875; 0.0001783192153923282 -0.0004084915870648804 -0.0003469251044483047] %
+
+Mass Used: 102.30788751346336 kg
+Launch C3: 95.1456530751405 km²/s²
+||V∞_in||: 6.988755183100265e-8 km/s
diff --git a/archive/ES_0.5634246253484524 b/archive/ES_0.5634246253484524
new file mode 100644
index 0000000..d851547
--- /dev/null
+++ b/archive/ES_0.5634246253484524
@@ -0,0 +1,22 @@
+archive/ES_0.5634246253484524---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T01:03:31.676
+Launch V∞: [6.63139969290713, -7.141325070128351, 0.2874208251659788] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01528186730374287, -0.0072042665106115305, 0.017620315389132817] km/s
+ V∞_out: [-0.01575430364254825, -0.006226805799643851, -0.01757668907427802] km/s
+ time of flight: 1.8749577787363e8 seconds
+ arrival date: 2029-04-06T03:13:08.676
+ thrust profile: [0.4815286599041215 -0.1207020583848651 -0.15338949049876358; 0.07606826652718428 0.02403258553596756 -0.08032082505067871; 0.04778193255997446 0.028419395260145194 -0.08472093610191164; 0.05246570008816897 0.04344344337148813 -0.13367448213746938; 0.05282311267264545 0.0532483376208253 -0.1710703700431418; 0.022755439718756317 0.024782073763551266 -0.08849147419797679; 0.017370643634380258 0.020173674181388268 -0.07816359419227792; 0.007283059845673531 0.009636824106021413 -0.0397130116691188; 0.010283409796131269 0.01730918999203173 -0.06645689610655078; 0.0014761902361541369 0.002380112488439876 -0.009968312580421154; 0.0004382169554725782 0.0005620652374181484 -0.002520146310521656; 0.0003310623554918723 0.0005358105258373052 -0.002780754707345885; -0.00023516833512022748 0.0002952405793229808 -0.0005130624113705868; 3.7327057285451695e-5 5.5032797534902646e-5 -0.0002999770490180821; 9.276267375526672e-5 8.211518230637812e-5 -0.00025907632365653897; 6.0131293409407174e-5 0.00010829428306907804 -0.00011692269865946592; -0.00011927861635834105 0.00017332522042995825 -0.0001848646783213421; 0.00019425188562726114 -0.0001519584903376915 9.665910020293343e-5; -9.932712457329007e-5 6.589971143921757e-5 1.9424442810854915e-5; 8.888529230630847e-5 4.555757302935286e-5 -0.000310389089861222] %
+
+Mass Used: 102.83191738527694 kg
+Launch C3: 95.05659637507158 km²/s²
+||V∞_in||: 0.024411317839429215 km/s
diff --git a/archive/ES_0.5634306628168847 b/archive/ES_0.5634306628168847
new file mode 100644
index 0000000..8c8ac87
--- /dev/null
+++ b/archive/ES_0.5634306628168847
@@ -0,0 +1,22 @@
+archive/ES_0.5634306628168847---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T09:52:37.677
+Launch V∞: [6.172619218188467, -7.553732084695206, -0.14286652555361715] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012117508157168484, 0.0056143100166567905, -0.013253951724499788] km/s
+ V∞_out: [0.012448962854343375, 0.0050292289894831995, 0.013119746341920317] km/s
+ time of flight: 1.8570951509699023e8 seconds
+ arrival date: 2029-03-20T19:51:12.677
+ thrust profile: [0.4351240088778452 -0.10803841022398328 -0.14961735164115658; 0.08190109716103028 0.022477459033779956 -0.08923296978826968; 0.06351404677128392 0.03392368357600211 -0.11577275198279614; 0.056063585775830586 0.04057646413625687 -0.14245527173735217; 0.046999219543876085 0.04138678087807267 -0.15337295535062842; 0.030274415409717852 0.030754108793611356 -0.12265916689114306; 0.01208940967450837 0.013697086876810418 -0.059576228061258334; 0.009345011262557028 0.01091919389748892 -0.050156897568044825; 0.005857878763255774 0.007343333723929954 -0.03694968223966281; 0.0013963012598429815 0.001997558854518575 -0.010952623530945085; 0.0007839511186162549 0.0011227704700130549 -0.006182308184080004; 0.0019511943722609888 0.0017468357802443374 -0.0009332604784345149; -0.000117334614761396 0.0004709163038623075 -0.0004792745494161638; 3.2419368070801786e-5 0.0023811200772773326 -0.000448545382190904; -0.00022421247775015552 -0.0010771598303781268 -0.0018862633678950746; 0.0012705831572848586 0.002783699153045956 -0.004809759675885845; 0.001605362284859457 -6.825490605059687e-6 -0.0032131048748693636; 0.0016686284954691402 -0.0028614290886337353 -0.0010339846350415369; -0.0008900150111158308 -0.0017742505556891542 -0.0026415585069962315; 0.00012570717650498995 0.00031188214070165766 0.00017251714897703347] %
+
+Mass Used: 102.11614757837378 kg
+Launch C3: 95.18050726422715 km²/s²
+||V∞_in||: 0.018815464841920555 km/s
diff --git a/archive/ES_0.5634368062089622 b/archive/ES_0.5634368062089622
new file mode 100644
index 0000000..be882ae
--- /dev/null
+++ b/archive/ES_0.5634368062089622
@@ -0,0 +1,22 @@
+archive/ES_0.5634368062089622---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T22:44:06.417
+Launch V∞: [6.545089719908829, -7.351305872116502, 0.23404928579486256] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.3552760823924776e-8, 6.440340748887186e-8, 3.642214198957844e-8] km/s
+ V∞_out: [-2.1108959034147337e-8, 4.281920499268301e-8, -6.629809653626639e-8] km/s
+ time of flight: 1.8374054576673046e8 seconds
+ arrival date: 2029-02-21T13:46:31.417
+ thrust profile: [0.2412326982953031 -0.06375211063678513 -0.07609252843655871; 0.115634802474997 0.03389271077225849 -0.10868857773574347; 0.09055888886594417 0.05159677719758806 -0.141223202603371; 0.0661915613887608 0.05147608140094259 -0.14436243366049534; 0.053618938225946086 0.05136684922718026 -0.15141479332313135; 0.023002046465363288 0.026945872165895102 -0.08262410872144335; 0.027998650746002864 0.040228896196789876 -0.11298423746406931; 0.013042981113946592 0.018591738657671067 -0.06073133982791998; 0.0038480554136469426 0.0055799161048212 -0.021337333367927445; 0.0009759281561012257 0.0015655829619310377 -0.005978791944151044; 0.0007378519256066341 0.0010885190103348012 -0.004303233711397452; 0.0008803225820915446 0.0015281346830757763 -0.0061258589928002895; 0.0001594711402403574 0.0003515027815472858 -0.0002774185589655182; -4.497149854630453e-5 -0.00043269522736240823 -0.000233782448956263; -0.00032148687714441754 -0.0005843051869612778 -7.73892950048914e-5; 0.0003236672703786107 -2.266286614230326e-5 -0.0005678565641079836; -0.00035161179219133276 0.0001135438685308346 -0.00024332236133491972; -0.0003185129961154647 0.0005003478881779608 0.00031167809775100317; -0.000510626844906368 0.00019833151364560402 2.237746452890863e-5; 0.00029276103345913086 0.00012562773443870783 -0.0001308937940296318] %
+
+Mass Used: 91.89066078815313 kg
+Launch C3: 96.9346765352519 km²/s²
+||V∞_in||: 8.124136312368343e-8 km/s
diff --git a/archive/ES_0.5634393129870765 b/archive/ES_0.5634393129870765
new file mode 100644
index 0000000..a7c096a
--- /dev/null
+++ b/archive/ES_0.5634393129870765
@@ -0,0 +1,22 @@
+archive/ES_0.5634393129870765---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T13:29:39.628
+Launch V∞: [6.525784890687749, -7.426257887636204, 0.011792779345806494] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.3250594384207067e-9, -1.5357548903573557e-9, 2.7580645371942293e-9] km/s
+ V∞_out: [1.376562269171585e-9, -3.1378825072690373e-9, -3.80538383436286e-9] km/s
+ time of flight: 1.874957778749053e8 seconds
+ arrival date: 2029-04-10T15:39:16.628
+ thrust profile: [0.242828539879156 -0.06231745528633242 -0.09536679808544772; 0.07380556160335486 0.018531957915705128 -0.08690747400504258; 0.04570809065836892 0.02174964324337007 -0.09274378180354192; 0.03724630075508183 0.02380335450668399 -0.10643797473338759; 0.037688484390634644 0.029533883983376304 -0.13765055978011806; 0.02854802252523592 0.026621796736020466 -0.13646926228215472; 0.011582663950916979 0.010522007134787272 -0.060599471897946115; 0.014160908672917086 0.014514484131282465 -0.08471773984476928; 0.005043762274789127 0.0055288816762416445 -0.035007852049736846; 0.007035643828568702 0.007925942682857024 -0.051250594111576286; -0.0002547769365607421 0.00032485580151033074 -0.005847137649787168; -4.036274078079798e-5 -0.00040234034870008514 -0.0013253574915097102; 0.00032410000554102653 0.0018039025514738263 0.0009443241484153606; -0.002577264897326818 0.0008467490786540115 0.0014335816055579876; 0.00045701435874734514 -0.0007694515641107464 0.0019313413766506738; -0.002434677260748474 0.0024346379050155798 0.002618451042654871; -0.0051804710256586825 0.003700507402440243 -0.006447215993142599; 0.00018434852824056016 -4.64055385108884e-5 -0.0009885357644074289; 0.0012887518722956765 -5.754324091845789e-5 -0.006423085090118219; 0.0006220602473639083 0.0014186891292857235 -0.002178976118364908] %
+
+Mass Used: 87.22320176828498 kg
+Launch C3: 97.73531372285215 km²/s²
+||V∞_in||: 4.584919120727821e-9 km/s
diff --git a/archive/ES_0.5634469709840163 b/archive/ES_0.5634469709840163
new file mode 100644
index 0000000..52389b7
--- /dev/null
+++ b/archive/ES_0.5634469709840163
@@ -0,0 +1,22 @@
+archive/ES_0.5634469709840163---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T21:20:10.250
+Launch V∞: [7.625998759308498, -5.873661195779083, -0.09741494924237828] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.099237687911611e-6, -3.737834163092041e-6, 3.1373600800254638e-6] km/s
+ V∞_out: [-8.821292974430858e-7, -6.303116375560397e-6, 2.982129268734162e-7] km/s
+ time of flight: 1.851987262035461e8 seconds
+ arrival date: 2030-03-23T09:25:36.250
+ thrust profile: [0.36369186476249427 0.01728617064508563 -0.07950440049150394; 0.30283643025259327 0.21722102382586442 -0.2073302832768441; 0.12743999223173053 0.1563781221710679 -0.16821095936839797; 0.03214515240781869 0.0555309821484913 -0.07111725813376121; 0.05002816994552426 0.11180243381396458 -0.14520430256976638; 0.02751943439563356 0.08151077259515876 -0.11572049092642303; 0.00622395603955447 0.023267223084547147 -0.03587166006586187; 2.5154372550232522e-5 0.0028709002628692862 -0.004769373744062356; 0.0009487106071335223 0.006984551267287244 -0.011278497031597357; 0.0007668858830724844 0.006032028780115409 -0.010448577052230124; 0.00014214468514046473 -0.000592929989699746 -0.0010715822026630168; 0.00036176849838501023 -0.00017190019543127447 -0.001481774756788586; 3.939868641465141e-6 0.000528539911268633 4.788741201910583e-5; -0.000441112100353095 0.0012934556201066143 -0.0028828826485311743; 0.00033934376996124123 -0.0009062993708083967 -0.0018258196281879014; -0.001985426964961054 -0.0006980521350720068 -0.0004454585916106803; 0.001184528121680225 -0.0019191556418722477 0.001134906303259858; 1.4860890569587696e-5 9.738366580193674e-5 -0.00047080379498422005; -0.0021947555009473253 -0.0014575538629404466 0.0005759030781358089; 0.0006288839327184651 -0.00033063871348744086 0.0014526725154317978] %
+
+Mass Used: 116.80755102736794 kg
+Launch C3: 92.66524259211161 km²/s²
+||V∞_in||: 6.373239531392987e-6 km/s
diff --git a/archive/ES_0.5634511926427629 b/archive/ES_0.5634511926427629
new file mode 100644
index 0000000..9f23ad0
--- /dev/null
+++ b/archive/ES_0.5634511926427629
@@ -0,0 +1,22 @@
+archive/ES_0.5634511926427629---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T11:03:33.718
+Launch V∞: [6.2806240613271775, -7.502223066888192, -0.00430703172739723] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.839634174338166e-10, -1.936391918822614e-9, -5.52087704173233e-9] km/s
+ V∞_out: [1.5969653007286434e-9, 1.8724093114104436e-9, 9.996151741338598e-10] km/s
+ time of flight: 1.8077968289478397e8 seconds
+ arrival date: 2029-01-19T19:38:15.718
+ thrust profile: [0.3569483023156197 -0.11158931407267615 -0.13099463518454366; 0.08605806951346245 0.017873642575992554 -0.09428852157445133; 0.07911456903566633 0.0348988841541104 -0.14322025091851295; 0.07062036547204448 0.04259533381441262 -0.177802990687314; 0.0390343438050002 0.028156634265757784 -0.12673440783937961; 0.040208363114116866 0.03369604779917141 -0.15723490714144747; 0.018300057920151543 0.01703138301631119 -0.0857917478483697; 0.004865370650900397 0.006327592949079305 -0.03112655752062536; 0.0012157998929167844 0.0012572874662339574 -0.008449446135167115; 0.000918633603090615 0.0009656757314029149 -0.006612131367367964; 0.002185135502310687 0.003093970388050319 -0.017364003306899658; 0.00048407504745330153 0.0006118237162376104 -0.004215957795864328; 0.000691275973751311 0.0032605611375406103 -0.0011327659780129785; -0.00046269330109678804 3.670915295858341e-5 0.0006959430203271133; 0.0012873591371536422 9.484959034663707e-5 0.000366610782268515; 0.0012784107240170978 -0.0050213619643946295 -0.0014736380126257477; 0.000585781294308305 -0.000890483567240626 0.003667789882503814; -0.002417237330072476 -0.00041035190852037155 -0.0040829595494159265; -0.0015240944845158495 -0.000488915191393076 0.0023253459208675744; -0.0031526878201128435 0.0002838759287338664 -0.0005549944703465532] %
+
+Mass Used: 98.93701085892826 kg
+Launch C3: 95.72960809559345 km²/s²
+||V∞_in||: 5.879686237046125e-9 km/s
diff --git a/archive/ES_0.5634558495560347 b/archive/ES_0.5634558495560347
new file mode 100644
index 0000000..52874ce
--- /dev/null
+++ b/archive/ES_0.5634558495560347
@@ -0,0 +1,22 @@
+archive/ES_0.5634558495560347---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T01:46:05.374
+Launch V∞: [6.537949329927846, -7.415858177028391, 0.11196031360446669] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.263086722908291e-8, -6.044124315992695e-9, 1.875181904434901e-8] km/s
+ V∞_out: [5.820232884488108e-9, -1.309186454200684e-8, -1.780894567616227e-8] km/s
+ time of flight: 1.860842587886374e8 seconds
+ arrival date: 2029-03-23T19:50:23.374
+ thrust profile: [0.23424689463362697 -0.054777354976170124 -0.07918590132565981; 0.05160684113726102 0.01526062124760183 -0.055017062826611875; 0.04789914013502554 0.027413381202065025 -0.08410509805345796; 0.04488155835960134 0.036887946797392324 -0.11079639001145755; 0.042636568337112775 0.042348772987631345 -0.13719474121546812; 0.02686409563806282 0.028773175640022564 -0.10078264784348633; 0.019009270720087908 0.022181022626746785 -0.08619652212247397; 0.018322494197053 0.02170861376971749 -0.08923325938710591; 0.009640848169135557 0.013673677776744613 -0.05617063553608763; 0.0074249098457972226 0.011408633988669818 -0.04890968925585291; 0.006175313936728629 0.01046410769050491 -0.044892154106138955; -0.00019247874735156388 0.0003006619389588542 -0.0016088086479142348; 0.0002088529380211267 5.3837265793139715e-5 -0.0021323034657523394; 0.0015730466087762913 0.000709179641058809 -0.00027601603825743424; -0.002247064226712723 -0.001365615753840703 -0.0009099722858373878; -8.27781111024104e-6 -0.0005955372593854599 0.00035873528617422245; -5.868681933898846e-5 -0.0007520217769064106 -0.0018541900514294674; -0.003281525516525979 -0.0009876567469752212 -0.004242880167229079; 0.00025013876808349894 -0.002740505881069171 -0.0035867950527683334; -0.00014861448859564564 -0.00036958274976718283 0.0004976785564129961] %
+
+Mass Used: 87.14358833180995 kg
+Launch C3: 97.75226905432524 km²/s²
+||V∞_in||: 2.34030118398873e-8 km/s
diff --git a/archive/ES_0.5634567193688029 b/archive/ES_0.5634567193688029
new file mode 100644
index 0000000..1df4869
--- /dev/null
+++ b/archive/ES_0.5634567193688029
@@ -0,0 +1,22 @@
+archive/ES_0.5634567193688029---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:24:15.799
+Launch V∞: [6.391603332769547, -7.527991081073687, 0.09828898541560392] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.147839995591078e-7, -1.1506281132267373e-7, 1.374414038104891e-7] km/s
+ V∞_out: [-4.294372871748451e-7, 1.0497115122900978e-7, -5.325614739583983e-8] km/s
+ time of flight: 1.8514794760737482e8 seconds
+ arrival date: 2029-03-14T08:23:22.799
+ thrust profile: [0.2655923702879958 -0.07283180933845441 -0.10076637199250918; 0.03349804385417125 0.007763459301283618 -0.042268776341997306; 0.06790521799834598 0.03192443697565757 -0.13198352732891264; 0.06464255207571948 0.04158400828120283 -0.1744619125015407; 0.043287432978870936 0.033209050895208786 -0.15049855782135835; 0.019930309967857343 0.017666724704582085 -0.09102187926961695; 0.0161429869773884 0.015853565517955432 -0.08574399068835178; 0.00767902572317603 0.007698755039155964 -0.048208406178175435; 0.004124027069398173 0.004797530424557486 -0.03428849950645087; 0.003157736927856793 0.006922394944766387 -0.03492152577093881; 0.004761292388459604 0.003090513182453928 -0.02126663558466292; -0.0007682592136750172 -0.0022479239986117785 -0.0006127090345648769; 0.00021824638968268197 -0.0008608945691015306 7.69052588469243e-6; 0.0015073059694672816 0.0015589222992888688 0.003339037943926329; 0.0009524862661600855 0.0026093954663824422 0.0020119993239901953; 0.0013494732897967282 0.00020131358796717582 0.0021267053231941984; -0.0002835758235443875 0.00031482807491819905 -0.00018840132722452985; -0.0007182392501834485 -0.0005280889358331615 0.002126481967710264; -0.0011164781872255835 0.0005519948367747503 -0.00042125318484580437; 0.00046310155032873034 -0.0018516293895893144 0.005880346883483191] %
+
+Mass Used: 88.42423490197962 kg
+Launch C3: 97.53290360484979 km²/s²
+||V∞_in||: 4.5185767263721997e-7 km/s
diff --git a/archive/ES_0.563469282809802 b/archive/ES_0.563469282809802
new file mode 100644
index 0000000..966567c
--- /dev/null
+++ b/archive/ES_0.563469282809802
@@ -0,0 +1,22 @@
+archive/ES_0.563469282809802---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:00:05.020
+Launch V∞: [7.3063041154475865, -6.0982882430825525, 0.28405885541568165] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.0813864638655374e-6, 0.00016368529229872497, 2.8920585718903256e-6] km/s
+ V∞_out: [0.00015812122975955407, -2.3716715926513712e-5, 3.5205376386310376e-5] km/s
+ time of flight: 1.7490076030591255e8 seconds
+ arrival date: 2029-11-22T13:32:45.020
+ thrust profile: [0.6537701471537559 -0.030764777188033606 -0.1385744881812208; 0.27872102714485575 0.15865856611722937 -0.20797978949419965; 0.07173023164867154 0.06907222434111472 -0.10595040034873575; 0.06284589188002454 0.08260553225935681 -0.13437762599334024; 0.06282771732513229 0.10562493882787388 -0.1790994864920195; 0.015919186269110826 0.031822953244246784 -0.06264424818584147; 0.010563509995368868 0.025744202984390997 -0.054026714124120113; 0.009420309816374576 0.027793443747213334 -0.059679195690306386; 0.0021884957082204982 0.006676009352278825 -0.016476056030415197; 0.0012672067720388377 0.004962490194828045 -0.01280839209003171; 0.0009643906025902832 0.0035358456266889916 -0.010052239312671204; 0.00039266997478786247 0.0013114488600394832 -0.0002830617737461815; 2.913702298486758e-5 0.000527420119458588 -0.0014077955721255215; -0.00045569208402074604 -0.0002531525627953871 -0.00042752671687872003; 0.00027678870227887625 -0.0010165565477590565 0.0009718334468152459; -0.00016301766776573965 0.0023987975007109274 -7.72460731452468e-5; -0.0004437311113988185 -0.0007125085301926405 0.001054057766106445; -0.00023658005212415348 0.0032458772754435537 -0.004473192177717397; -2.4802094358252268e-5 0.0019764904242167898 -0.0006886423756571992; 0.0006825381159992388 -0.0035924748185797517 0.002538321730720629] %
+
+Mass Used: 128.5781455320548 kg
+Launch C3: 90.6518887564653 km²/s²
+||V∞_in||: 0.00016386392205715354 km/s
diff --git a/archive/ES_0.5634699065538465 b/archive/ES_0.5634699065538465
new file mode 100644
index 0000000..934c3cd
--- /dev/null
+++ b/archive/ES_0.5634699065538465
@@ -0,0 +1,22 @@
+archive/ES_0.5634699065538465---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T22:50:07.850
+Launch V∞: [6.268870513435043, -7.571649358641004, 0.06557942408272693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004933774649121342, 0.003395080699141875, 0.005103079303188185] km/s
+ V∞_out: [-0.005443531797962775, -0.002933679880170692, 0.004864746027902429] km/s
+ time of flight: 1.7751204772106048e8 seconds
+ arrival date: 2028-12-12T11:44:14.850
+ thrust profile: [0.3156522075560549 -0.10668798574490977 -0.1208179137155838; 0.03537677096013495 0.006274559843731925 -0.04074767791912007; 0.06317758684569323 0.025227094473043683 -0.1165101319502114; 0.08928107293357201 0.049058979390440065 -0.22491066428852; 0.06561433001940647 0.04374681045413937 -0.20990096333369979; 0.025668284337526413 0.019432117129539173 -0.10067593519700196; 0.01096016735062704 0.0092889216966676 -0.05163185829566259; 0.008399372149416036 0.007706213985857365 -0.04501704612506474; 0.0017913094140576467 0.0018232072814244366 -0.010954574864092431; 0.007059443040054067 0.007269526388497671 -0.045840526087328026; 0.004654240145780772 0.0049309355511129895 -0.03196075446404079; 0.000564667432621486 -0.00017354982252279713 -0.0009916166687352194; 0.0007870339387719297 0.0008762902683822487 -0.0020828754310802237; 0.0006442735922642754 -0.00042561283403123656 -0.000851475432877458; -1.0076453392449456e-6 -0.00010532348844511692 -0.0012479244952647156; -0.000711521209838685 -0.0006978831785033723 -0.0019179458881179211; 0.0009055007089493573 0.00026088107792056917 -0.0009768829287292308; 1.9192543381084027e-5 -6.260796388455302e-5 -0.00010206699224444269; -0.0018973978591235664 -0.0006883236553463812 -0.001373000129692532; 0.00037136024096263856 0.00016801195412029137 -0.00201179610844576] %
+
+Mass Used: 93.68956989864637 kg
+Launch C3: 96.63291218528708 km²/s²
+||V∞_in||: 0.007868298648159315 km/s
diff --git a/archive/ES_0.5634737479917851 b/archive/ES_0.5634737479917851
new file mode 100644
index 0000000..cc0e3d4
--- /dev/null
+++ b/archive/ES_0.5634737479917851
@@ -0,0 +1,22 @@
+archive/ES_0.5634737479917851---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:24:33.089
+Launch V∞: [7.516116281104868, -5.677180637424939, 0.011623335906044597] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.976040731436137e-5, -5.7101480365928066e-5, -4.6082886311387174e-5] km/s
+ V∞_out: [-9.424057654872186e-6, 6.327621239534564e-5, -7.835498184248351e-5] km/s
+ time of flight: 1.8559386178030565e8 seconds
+ arrival date: 2030-03-26T18:15:34.089
+ thrust profile: [0.7970246800619629 0.006405897370524198 -0.18290695805922427; 0.3024278931208139 0.19996384978017673 -0.2428744049844204; 0.08806715282042253 0.09963099097131305 -0.13823818431629514; 0.052728256272246934 0.08294089225950849 -0.1292096803928654; 0.020169717638571602 0.041272081533940075 -0.07230584650915169; 0.0073344543988018715 0.01844635607605562 -0.03481069574209994; 0.00971776174561734 0.03136655229312888 -0.06212249411429959; 0.0022982345291728927 0.009102723153605599 -0.018611672814698228; 0.002298692855587313 0.00967623244921392 -0.021488706887694293; 0.0001738168369804971 0.002104484364524093 -0.005224741834583149; 0.0003555691194930353 0.002416556193033709 -0.0047251982432117935; -0.00036229822403916406 0.0006255330504038887 -0.0018532250967384784; -0.001029980286646927 0.0022454988237743637 -0.0017791729645115757; 0.00625302983960176 0.003027839689260705 -0.006401012163385134; 0.0005693187452227849 -0.002165304191859626 -0.004938744960253658; 0.0005713839690488484 -0.0003487011424227898 -0.0015966659539699518; 0.0013274682603587017 0.0057121357033033514 -0.0034210442612303523; 0.0001427137644261708 -0.0010422542733604812 -0.0010130875485081805; 0.00037253917895636597 0.0008569402929175474 0.0012286008016782809; -0.0008213238866218919 -0.0005483441515920385 0.0001107714913980689] %
+
+Mass Used: 139.83801157303333 kg
+Launch C3: 88.72251904297988 km²/s²
+||V∞_in||: 0.0001012458685548912 km/s
diff --git a/archive/ES_0.563473810606198 b/archive/ES_0.563473810606198
new file mode 100644
index 0000000..53a4f96
--- /dev/null
+++ b/archive/ES_0.563473810606198
@@ -0,0 +1,22 @@
+archive/ES_0.563473810606198---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T15:37:37.429
+Launch V∞: [6.327781454662799, -7.4030935492674175, 0.1912858846794495] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00041392359781674073, 0.0005154903669026919, 0.00047567444871466486] km/s
+ V∞_out: [-0.0005081672909746393, -0.00023947940263718205, 0.0005890308737593786] km/s
+ time of flight: 1.8296756900418416e8 seconds
+ arrival date: 2029-02-13T07:57:06.429
+ thrust profile: [0.39948438480973314 -0.10945983577190369 -0.13278989865489632; 0.10581980187369776 0.02748695090923662 -0.10689477618736225; 0.12358270081082333 0.06506083895209853 -0.20544465959856065; 0.05426389006771756 0.038668344583357744 -0.12831559869965423; 0.049408824431191246 0.04280887494148785 -0.14929140546216071; 0.02833227262386491 0.028833875623774874 -0.10594866761955461; 0.010803378401958521 0.012630934518733036 -0.04926466580074074; 0.00811835165475484 0.010314233425350615 -0.042928807936418525; 0.0030695721220720435 0.0036967566750392275 -0.017450408370555764; 0.003854685928369813 0.005649728399899769 -0.025800118774725295; 0.0006563334845120056 0.0010147527467775773 -0.004111264452101736; 0.0026001610614671913 -0.0011222608204942903 -0.0021315416978730187; 0.0023931786612547564 -0.0014263811536809271 -0.00035644974254770995; 0.0012043765822107554 0.0015715819054402261 -0.0005924021489230611; -0.00037365133687800815 2.0643573024866746e-5 0.0014749313029581174; -0.00012805029500619002 0.001067807962645698 0.0037524244964845244; -0.001048245072859686 2.5776626103791268e-5 0.0024558218661012788; -0.0015704817117602502 -0.00015852636980446928 0.005166651009155343; 7.540498051080834e-5 0.00016765977323515875 -0.0006912679946929499; 4.4688731811339205e-5 -2.4661030663775e-5 -0.00025284319056694416] %
+
+Mass Used: 103.9007643005657 kg
+Launch C3: 94.8832025268569 km²/s²
+||V∞_in||: 0.000814450271262173 km/s
diff --git a/archive/ES_0.563476756703302 b/archive/ES_0.563476756703302
new file mode 100644
index 0000000..b2e636f
--- /dev/null
+++ b/archive/ES_0.563476756703302
@@ -0,0 +1,22 @@
+archive/ES_0.563476756703302---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T04:44:47.960
+Launch V∞: [6.506161784731938, -7.470712291559213, -0.49709378787016095] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.635678327375179e-9, -2.678351746451138e-9, 5.2685747126398376e-9] km/s
+ V∞_out: [1.7347749448454822e-9, -4.4106198925177305e-9, -5.1543988314261176e-9] km/s
+ time of flight: 1.8582719978220466e8 seconds
+ arrival date: 2029-03-21T23:24:46.960
+ thrust profile: [0.20096361817880615 -0.057326058731156815 -0.080275753630998; 0.04106926152591861 0.009449028953060757 -0.04854558196988789; 0.04821770033153182 0.021930968871321187 -0.09546722814077263; 0.07581043050211202 0.045971945867959524 -0.21062183824892328; 0.040816471296427376 0.029965276988300406 -0.14550861005254626; 0.044870119747226996 0.03730208730630117 -0.19502645046023087; 0.012753403434529919 0.012053231206878899 -0.06616205940598832; 0.0018640659793367556 0.0017514154768009152 -0.011297380240296516; 0.0010153515623435446 0.0009656914954036328 -0.007918324513371999; 0.0004916966969211277 0.0006439238977257822 -0.004691842807037121; 1.0005536967727007e-5 0.0013470142526822793 -0.0068571102735845565; 0.0020664150277981104 0.0028187571111608473 -0.0184831753223565; -0.0010288961360883355 0.0006057564247389173 -0.002209298743561943; 0.0021514640885429027 -0.0003347892235995071 -0.003155278951226612; -5.3432209063202527e-5 -0.0014732280401327062 0.0028396796822868432; -0.001671479048879427 0.000331683748786822 -0.0007894804139227662; 0.0011618311561519767 0.0004603224269338135 0.0008672213915977625; 0.0013861327699970136 0.00029703018992904406 -0.0032383467727438715; -0.003404983529983635 -0.0001645973823975891 0.0031224373827647635; 0.0008366857896732002 -0.0016021556230948152 -0.004258662352679898] %
+
+Mass Used: 83.45496713377315 kg
+Launch C3: 98.38878554629929 km²/s²
+||V∞_in||: 6.471340496819885e-9 km/s
diff --git a/archive/ES_0.56347820384846 b/archive/ES_0.56347820384846
new file mode 100644
index 0000000..b40f8b3
--- /dev/null
+++ b/archive/ES_0.56347820384846
@@ -0,0 +1,22 @@
+archive/ES_0.56347820384846---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T13:03:26.123
+Launch V∞: [6.534739169893552, -7.24952954283285, 0.25235053574337735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.763654534599298e-6, 4.517994795960724e-6, 5.241088470141027e-6] km/s
+ V∞_out: [7.089568804086564e-6, 4.504412709199387e-6, 1.3951414821520732e-7] km/s
+ time of flight: 1.8749577787191415e8 seconds
+ arrival date: 2029-04-07T15:13:03.123
+ thrust profile: [0.4378039908738456 -0.10426449037210019 -0.1280214041732442; 0.050324697997711144 0.015443412704849384 -0.05224478833323473; 0.076759555685154 0.04497821647695365 -0.13024236828782612; 0.053754403590319154 0.04266631708120213 -0.12769375118732093; 0.020373695074706186 0.019474254617050837 -0.06473146980156474; 0.028619927792889084 0.032238667659553306 -0.10959098998644581; 0.024012920170648232 0.030416199033745595 -0.1116104347194005; 0.019857484638984874 0.026458495088922635 -0.10170394749642413; 0.008356156480904235 0.012895563788656072 -0.05120332879629138; 0.0006990256391894851 0.001328608986249674 -0.005703546579618038; 0.0005934352256985623 0.0022305012212402013 -0.0026275074837216437; 0.0018885226615348125 0.003227925539189858 -0.01515581469572786; 1.7967206517640472e-7 3.908278592928949e-5 -0.0016272393334092216; 0.00021422115223947982 -0.0004023271103256274 -0.0008241336608793726; 0.0011585339862766062 -0.002322593540583741 0.0024787253017325914; 0.0010865123484092834 -0.0034668241803532764 -0.000870987823638102; 0.0024676246555422063 -0.0008062551760115074 -0.002204872663050079; 1.4645073245510276e-5 0.00012443863677496809 0.0014015275950715594; 0.002466090111879853 -0.0018842736947782724 0.0025515729742551507; 0.0016476153491044164 -0.0006125420557068499 0.0010030852926484672] %
+
+Mass Used: 101.3452146341524 kg
+Launch C3: 95.3221754038373 km²/s²
+||V∞_in||: 8.400814832692233e-6 km/s
diff --git a/archive/ES_0.5634859251562109 b/archive/ES_0.5634859251562109
new file mode 100644
index 0000000..fd0ce31
--- /dev/null
+++ b/archive/ES_0.5634859251562109
@@ -0,0 +1,22 @@
+archive/ES_0.5634859251562109---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:01:16.963
+Launch V∞: [6.534732676563052, -7.407195426767307, 0.1113434697738599] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.4925667152683463e-7, -0.00011576464202169034, 8.445556448052171e-5] km/s
+ V∞_out: [7.212140499445804e-5, 0.00012145405411058565, -2.5017342243075064e-5] km/s
+ time of flight: 1.8585133691628703e8 seconds
+ arrival date: 2029-03-21T07:23:32.963
+ thrust profile: [0.23233053932349257 -0.06458519208277262 -0.08491546903232203; 0.07531934883661241 0.017765736340846803 -0.08616747281466072; 0.08418406061360016 0.03887805945936585 -0.15750908975472644; 0.03465082581794016 0.023101741182964295 -0.09742697302347363; 0.032859584384095 0.024506103957171614 -0.11401065783885792; 0.027069152845470547 0.025459038041332042 -0.12144008038585122; 0.011964232295864493 0.011628359321012126 -0.06045731816242777; 0.009336570556414755 0.009491652009090887 -0.054090272814485946; 0.008061712887798311 0.00960062498408637 -0.0545085339607874; 0.00839537629498734 0.009755942327840699 -0.058183390104201586; 0.0018599912056017466 0.002106574080927787 -0.014753541354817535; 0.0018985321280823996 0.000977319304936174 -0.004991440227594355; 0.00132046698382311 -0.0013402180938339734 -0.0019856607926575847; -0.0024587847527295873 0.0010744015278247201 -0.0019456899073302062; -3.520594187532769e-5 6.443769159169774e-5 -0.0013141278636879922; 0.0011018124216452107 0.0028191920921125423 0.00035265467053325955; 0.001030367875696595 0.0022286525609947344 -0.0009307389372959114; -0.0002054097155025159 0.0010213408244049565 -0.0037250009292873034; 0.005844734249521677 -0.0009169432399435668 0.0012578332186332414; -0.0005450849092507959 0.002406949309169009 -0.005210141579161455] %
+
+Mass Used: 88.17382244135206 kg
+Launch C3: 97.58167261272467 km²/s²
+||V∞_in||: 0.0001432979996174276 km/s
diff --git a/archive/ES_0.5634866650223983 b/archive/ES_0.5634866650223983
new file mode 100644
index 0000000..cf6b8ad
--- /dev/null
+++ b/archive/ES_0.5634866650223983
@@ -0,0 +1,22 @@
+archive/ES_0.5634866650223983---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T02:01:18.077
+Launch V∞: [7.515087298333112, -5.970135400362194, 0.29262347967279645] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.452413937452306e-7, -6.244348418251155e-6, 0.0001229633534156489] km/s
+ V∞_out: [4.617649145943864e-6, -0.00012372959467524375, 1.2688528965439036e-6] km/s
+ time of flight: 1.7690651384731737e8 seconds
+ arrival date: 2029-12-15T14:43:11.077
+ thrust profile: [0.5586731516516447 -0.014746175966159772 -0.12986059872432235; 0.1280669041197276 0.07502960895045745 -0.10676210465871773; 0.20329591395593646 0.2028598435751407 -0.2778978837521193; 0.06328212972574757 0.08739370532335188 -0.14197389997606621; 0.03239743425439807 0.05512415124949761 -0.09843696866452838; 0.02769754022842771 0.05740516194468709 -0.10825569039395114; 0.006005223463139445 0.01571802988602017 -0.031984755825324646; 0.004184473313145079 0.011861179031338723 -0.025191194512314635; 0.0020390635049000465 0.007365374418341027 -0.017435327065805098; -0.0001705554977884426 -0.00011392727855335113 -0.0011990720455686775; 0.0005206766163129716 0.000880845212164325 -0.001552874349527613; -0.00014114789397863775 0.00038568905912561227 -0.001480783276905948; 0.004607581691012404 0.0020066035552496185 0.0013275497538586332; 0.0016703682179859888 0.0016170818636996715 0.00265376651203193; -0.004333099222223475 -0.002544170657352321 -0.0004106516838734394; 0.0012002966428383117 -0.003425201173684493 0.0005948286058597213; 0.0007449549688696641 -0.0008318379018363738 -0.0009944125342010097; 3.904796637215057e-5 -0.0007515122957460387 -0.0006768433312585165; -0.00022872225061350054 0.00046981541697576257 0.0007871058229395802; 0.0022385862399049556 -0.010221193258025178 -0.0016509773389793805] %
+
+Mass Used: 119.54046243649009 kg
+Launch C3: 92.20468230108136 km²/s²
+||V∞_in||: 0.0001231234929119804 km/s
diff --git a/archive/ES_0.5634868894024057 b/archive/ES_0.5634868894024057
new file mode 100644
index 0000000..a97b019
--- /dev/null
+++ b/archive/ES_0.5634868894024057
@@ -0,0 +1,22 @@
+archive/ES_0.5634868894024057---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T15:40:42.765
+Launch V∞: [6.150572816612523, -7.412290894182536, 0.12941570328641186] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.146944181155908e-5, -5.36513030861705e-6, 8.694796249156167e-8] km/s
+ V∞_out: [8.325197025050044e-6, -1.7871448063159357e-7, -3.0806342398917964e-5] km/s
+ time of flight: 1.807099647264182e8 seconds
+ arrival date: 2029-01-17T04:53:26.765
+ thrust profile: [0.5903947138118526 -0.1709137289715153 -0.1909294584992472; 0.09917661889881156 0.02493112382542933 -0.09743621976701115; 0.08184748779587687 0.042431849890901666 -0.1334038917521624; 0.07415910460618126 0.05256574325025204 -0.16730127812536671; 0.06162497053647575 0.05344207247233777 -0.17765851124739815; 0.02783661438518326 0.02822278006325233 -0.10015537681208801; 0.01140606816862672 0.012891079427192993 -0.04939287272388218; 0.006458410294978064 0.008001889815335768 -0.03196505887087814; 0.007950661175622676 0.010542873504270087 -0.0437627629622901; 0.00204480409920225 0.003232572884558521 -0.012824218097048045; 0.0009239209824198366 0.0016066300072235535 -0.007442898086558038; 0.0010055232251959133 0.0006770970461179912 -0.0027708986232318983; 0.00023999458005957833 -0.00022795038571749254 -0.002655528808377719; 0.0008894005971094342 -0.0006831534311428685 -0.00098736026581715; 0.00020577990975942536 0.00038368002343729585 -0.0023772943422883407; 0.0005922812031015283 0.0002484084501958541 -0.0020991857415507474; 0.000438758108556835 0.0007187961069925882 -0.001817165090802995; -0.0011630334369531442 -0.002251640938085217 -0.00046412654591188664; 0.001146043241356459 -0.0010184003751857725 -0.001972512302746926; 0.0003811519938007181 -0.001617608356754713 -0.0007091006608303798] %
+
+Mass Used: 116.13599190544028 kg
+Launch C3: 92.78835069669135 km²/s²
+||V∞_in||: 3.19236268476457e-5 km/s
diff --git a/archive/ES_0.5634901880544378 b/archive/ES_0.5634901880544378
new file mode 100644
index 0000000..3a38d8a
--- /dev/null
+++ b/archive/ES_0.5634901880544378
@@ -0,0 +1,22 @@
+archive/ES_0.5634901880544378---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T19:37:16.253
+Launch V∞: [6.424957653086294, -7.4334650294394224, 0.025460164427731805] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.867024081622213e-9, -4.796076110820091e-9, 1.4390459645594268e-8] km/s
+ V∞_out: [4.938168351437706e-9, -1.1051745620077047e-8, -1.50122280869674e-8] km/s
+ time of flight: 1.842811781372293e8 seconds
+ arrival date: 2029-03-01T16:50:14.253
+ thrust profile: [0.28901689274192216 -0.07147113299037786 -0.0960236327228528; 0.08866690849172318 0.024970821799299468 -0.08932336662285165; 0.0575450350304959 0.0316341719805464 -0.09669677124541952; 0.04737372586601949 0.03587495971172654 -0.11207871794167108; 0.057062959843888 0.051871424609578165 -0.16092109844859467; 0.0695166227167375 0.07429065091415384 -0.24340105508371523; 0.00740335498427527 0.009878468789432078 -0.034708284006934396; 0.0059929926991229825 0.00902752363121196 -0.027927075421253476; 0.005587737410676664 0.006512352009731085 -0.028776784279686704; 0.00036931954208948843 0.0013553600739985975 -0.008446071253295592; 0.0026077489958463615 0.005494208857515789 -0.015217232730768472; -0.001365130987083566 -0.0010080949692610878 0.00012947685643512107; 0.0004222196272288184 -0.0005807362656026657 -0.0036233300783050744; -0.00040420063737410744 -0.00045739389732145364 0.0009317533039124846; 0.003603043940995891 0.0012898030533832795 -0.009503361509540335; -9.100713351879519e-5 0.0003052948041009115 2.9058036637306245e-5; -0.0014554816903942598 -0.001529447679833617 0.0006903679874812347; -0.0005988563589300936 -0.0002875365406146504 0.0020348560327949714; -0.0004751957869909582 -0.005658436090629253 -0.00036975944416669615; -0.0019241789842896905 -0.0007045530751917846 0.008445993266499328] %
+
+Mass Used: 94.27195285120615 kg
+Launch C3: 96.53713140782367 km²/s²
+||V∞_in||: 1.809546460026846e-8 km/s
diff --git a/archive/ES_0.5634906098867827 b/archive/ES_0.5634906098867827
new file mode 100644
index 0000000..0c480fe
--- /dev/null
+++ b/archive/ES_0.5634906098867827
@@ -0,0 +1,22 @@
+archive/ES_0.5634906098867827---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T13:58:49.419
+Launch V∞: [5.959451642895708, -7.601947752945533, -0.3024313651268251] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.03384682071768639, -0.015370773511420502, 0.03738638235654148] km/s
+ V∞_out: [-0.03392879757780683, -0.013887040619290065, -0.038276214290869734] km/s
+ time of flight: 1.7854638367416054e8 seconds
+ arrival date: 2028-12-24T02:11:52.419
+ thrust profile: [0.49256523390868057 -0.13996765369697875 -0.16232242201360877; 0.1551187891643469 0.03936465617728912 -0.1512991060165385; 0.09333791694228974 0.04873375776693707 -0.1511414531142624; 0.08011325259748449 0.05801669846326704 -0.18000961696310133; 0.05190409937599746 0.045930880665383346 -0.15038463364784568; 0.03501948871001628 0.036016092322578776 -0.12406231704135444; 0.018539672602063934 0.021468778114883305 -0.07849646406686722; 0.004871257680364903 0.006267159959320301 -0.024669255742709; 0.0005310100540597067 0.000700958066860887 -0.0032238020072136576; 0.0031086305727204655 0.0045800693688046 -0.01943519193627131; 1.1591059872677974e-5 0.00033355454812102596 -0.0003914438305223531; -7.326952474474269e-5 0.00020351048098219316 -6.462432230408614e-5; 5.837580989015799e-5 7.404022684551858e-5 -0.0002334358479324618; 3.802298750073773e-5 -0.000543833325299445 -5.86331170892891e-5; 0.00042846466325593285 -0.0003376817999901415 0.00024778831256587887; -0.00015944880976790195 -4.2887994282144815e-5 0.00026909635738530465; -5.5737985976092165e-5 0.0009146375213151991 3.399639102351961e-5; 5.201214865222236e-5 -0.00019883600434782893 0.0002757036453630812; -0.00014403483791916336 0.0002465468116476726 -2.6540802884236363e-5; -0.00031123887323791387 -0.00012923804619866325 1.2190442599876092e-5] %
+
+Mass Used: 112.59490505793883 kg
+Launch C3: 93.39613825313845 km²/s²
+||V∞_in||: 0.052722002396951 km/s
diff --git a/archive/ES_0.5634923615154959 b/archive/ES_0.5634923615154959
new file mode 100644
index 0000000..6758212
--- /dev/null
+++ b/archive/ES_0.5634923615154959
@@ -0,0 +1,22 @@
+archive/ES_0.5634923615154959---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T10:51:48.600
+Launch V∞: [8.070549493929054, -5.908609468742996, 0.10168226849915815] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002577326719920211, -0.015309928448245493, -0.018862693875674418] km/s
+ V∞_out: [0.010349049958929766, -0.008765266708306567, 0.020920056948110676] km/s
+ time of flight: 1.8749577779297474e8 seconds
+ arrival date: 2030-04-27T13:01:25.600
+ thrust profile: [0.14005499122553736 -0.006913390588316709 -0.053328081195499255; 0.023474541184556368 0.010874639173912846 -0.029705435102641967; 0.03648165563299965 0.02356198650280525 -0.0826480049692921; 0.04900600672071662 0.03759968032630397 -0.16041795449056567; 0.030505375367398887 0.026260767278231532 -0.12885069093907778; 0.02048394287936049 0.019133511914801282 -0.10514803244378329; 0.008596120231143707 0.009393746875161526 -0.05235733866351075; 0.011459897496614963 0.0120547960292368 -0.07788660146391742; -0.0007059965631579115 -0.0019084489561628972 -0.013277352323865899; 0.003320860915226759 0.005064705834018933 -0.030284170095186996; -0.0010392283290530345 0.000503406057990273 -0.013901126502957531; 0.006257268841050647 0.0028236804507295495 -0.004347003720435993; -0.0012774108402162697 0.004774048292202539 -0.002467356379834338; 0.005024562855212807 -0.011169724697586824 -0.00476871336181892; -0.0009623713916311037 0.008512735007538883 -0.003111612223749745; -0.0025711260644731204 -0.0014640595415224985 0.005720559163684662; 0.0004066609630065289 -0.004657615128393448 0.001237665520507223; -0.004976528421652314 -0.015800030596428823 -0.010141287884711903; -0.0038697408682429814 -0.003443951554313455 0.01393105117030822; 0.008676285493103224 -0.007312170040683643 -0.011366248933276226] %
+
+Mass Used: 73.74907184921585 kg
+Launch C3: 100.05577427180502 km²/s²
+||V∞_in||: 0.024430262838516834 km/s
diff --git a/archive/ES_0.5634925836508224 b/archive/ES_0.5634925836508224
new file mode 100644
index 0000000..7c889ab
--- /dev/null
+++ b/archive/ES_0.5634925836508224
@@ -0,0 +1,22 @@
+archive/ES_0.5634925836508224---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T02:43:42.229
+Launch V∞: [6.380529586696, -7.347119062012265, 0.10152736040489581] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001102858719113908, 0.0012639638088036557, 0.0011623731188644478] km/s
+ V∞_out: [-0.0013488655972612345, -0.0007042851632380443, 0.001359751563685791] km/s
+ time of flight: 1.874957778747503e8 seconds
+ arrival date: 2029-04-08T04:53:19.229
+ thrust profile: [0.45469534909517556 -0.1133704387107574 -0.1278522413663465; 0.03503511788414646 0.011098157177112206 -0.03522928498555545; 0.03960447415159159 0.025158058714513917 -0.06540884972404579; 0.15213596221856032 0.12548780273328664 -0.27830917881377626; 0.016647880119748333 0.016239842098352834 -0.04519737082485081; 0.009533802949531168 0.013385071862612846 -0.04076310264486481; 0.0416146751824165 0.05214486158002816 -0.15636936034419804; 0.005638145379432002 0.009234701835692916 -0.031111769747335098; 0.015222166597990147 0.0264859159558973 -0.08598552744597437; 0.004571618313747442 0.008242914438499173 -0.026669180641614547; -0.00199596045552829 0.0006423470192912758 -0.0020624458466854726; 0.0006400877793732208 0.0022838881291703536 -0.00205599664173161; 0.0007185022738611239 0.0011437684514071084 -0.004351862807526143; 0.001968167300181603 -0.0010052473689664216 0.0012275686026899583; -5.943126620368874e-5 0.0009073150210321806 -0.0022736688479934423; 0.00028273620900030796 0.0004329327901017629 -0.00026062357776997225; 0.0025683187636491136 0.0025915708773362072 -0.0029849342804552474; -0.003545235334570092 -0.0005112890940341087 -0.0011456351223683874; -0.0033404821039094202 0.00013259707166549757 0.0038187664867785523; 0.0006312659312327315 -0.0006301601818445515 -7.761309044306735e-5] %
+
+Mass Used: 104.98187354180573 kg
+Launch C3: 94.7016241229978 km²/s²
+||V∞_in||: 0.002040836380445448 km/s
diff --git a/archive/ES_0.5634965301412038 b/archive/ES_0.5634965301412038
new file mode 100644
index 0000000..9b077a0
--- /dev/null
+++ b/archive/ES_0.5634965301412038
@@ -0,0 +1,22 @@
+archive/ES_0.5634965301412038---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T00:01:22.855
+Launch V∞: [6.543185790316541, -7.446929053461066, 0.18262235115295605] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9731709746678447e-9, -5.830216838335367e-10, -1.7932107893497448e-8] km/s
+ V∞_out: [1.3439071587127452e-8, 1.2075021610017939e-8, 7.635147825124838e-9] km/s
+ time of flight: 1.8749577787496153e8 seconds
+ arrival date: 2029-04-11T02:10:59.855
+ thrust profile: [0.19772153002310866 -0.0530155490066711 -0.07522966124233076; 0.08873660433998574 0.022548701316827027 -0.10516676625507788; 0.04432846432260493 0.017401007941614633 -0.08626515752519817; 0.02280221184147503 0.01288098724916248 -0.0640231723056244; 0.03578906154715512 0.02543326016532632 -0.13223414336260525; 0.02747401624081641 0.020680413062435263 -0.1188717046471693; 0.02581349363554881 0.023699843606084056 -0.1319892480516455; 0.01298566458711827 0.01174711912591161 -0.0756111863117242; 0.007570570579559455 0.006869755186481993 -0.049468180350013456; 0.0034653405828089165 0.002840554573257054 -0.022325254435083028; 0.001666976943450927 -0.0019304710309061767 -0.00437629394309064; 0.002099632787273901 0.0067438372100126045 -0.010196315180711108; 0.0003162966955852495 0.0006348137008230618 -0.0013500788167926342; 0.001945913853050935 -0.00278786963267043 -0.004957181999407985; -0.0007020108112672032 -0.002065159647324302 -0.0003689306334230902; -0.0017515497496808923 0.000909855850723473 -0.0016808814764936418; -0.0030946894470358036 -0.0009153735366205392 -0.00021001364587457772; 0.0003139834624353988 0.0012207302878216655 -0.005557577209512747; 2.076949420566892e-5 -7.378366924193011e-5 -0.0016521086125569754; -0.0013062690437963941 0.007392593791310766 0.00424713125411485] %
+
+Mass Used: 83.97621453210104 kg
+Launch C3: 98.30338353702345 km²/s²
+||V∞_in||: 1.8186262767057472e-8 km/s
diff --git a/archive/ES_0.5634989976329695 b/archive/ES_0.5634989976329695
new file mode 100644
index 0000000..7771ee0
--- /dev/null
+++ b/archive/ES_0.5634989976329695
@@ -0,0 +1,22 @@
+archive/ES_0.5634989976329695---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T06:58:12.629
+Launch V∞: [7.997586454359877, -5.860800660590945, 0.05466724150541501] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.617464567001399e-9, 7.350009727045483e-8, -1.3425964422234091e-8] km/s
+ V∞_out: [1.1901193870762736e-8, -3.958281740167719e-8, -5.953501949366798e-8] km/s
+ time of flight: 1.8077669808528915e8 seconds
+ arrival date: 2030-02-03T14:43:10.629
+ thrust profile: [0.187995672180423 -0.011590394628726991 -0.06580669378687848; 0.06065189570531285 0.029025289250774307 -0.071136428611364; 0.039587463506338155 0.031017276356422496 -0.08259885408671058; 0.04257683928340672 0.04228453038959434 -0.12775474073407347; 0.044522491350919256 0.052840325192665696 -0.17337800594073313; 0.027812329422690345 0.03837853113321324 -0.138356268409746; 0.005636301189078775 0.00936569766143613 -0.0338586224248551; 0.00928705992395757 0.015654507667482366 -0.0667051097663155; 9.530673154156157e-5 0.007612657069529115 -0.015010328743314847; 0.004183921246631659 0.010593416741291287 -0.050152315174580984; 0.0014642219447938529 -0.0014623002353714594 -0.0061759810579103845; -0.002423084185897688 -0.0025120532624544546 -0.004827399061826607; 0.00024095340296146457 -0.0027906305833167015 0.0030467503621071576; -0.01065190756251471 -0.0025396508760637776 -0.002899766789452985; -0.003112036055576804 -0.012943009126026837 -0.008788542985471402; 0.012799307970445291 -0.012834281873458338 -0.004915862900371116; -0.002669281738937656 0.0030781316418382458 -0.008651341561976323; -0.0028000109721958814 -0.000977272667500546 -0.0016346458252182246; -0.01733127782522552 -0.014606776333263866 -0.013192981777733592; 0.0143914707733238 -0.01766510604444753 -0.0019072535639548041] %
+
+Mass Used: 83.92088565674476 kg
+Launch C3: 98.31336198543765 km²/s²
+||V∞_in||: 7.521157833071275e-8 km/s
diff --git a/archive/ES_0.5635112551432438 b/archive/ES_0.5635112551432438
new file mode 100644
index 0000000..c35ec9c
--- /dev/null
+++ b/archive/ES_0.5635112551432438
@@ -0,0 +1,22 @@
+archive/ES_0.5635112551432438---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T08:29:56.872
+Launch V∞: [6.548864099523812, -7.246855546180514, 0.1454915887312976] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00020000149152221374, -3.2430899376802734e-5, 5.848046150939616e-7] km/s
+ V∞_out: [3.901481603335859e-5, -9.007998658767985e-7, -0.00019881808812739294] km/s
+ time of flight: 1.8749577787499207e8 seconds
+ arrival date: 2029-04-07T10:39:33.872
+ thrust profile: [0.40750430974715907 -0.09986891346023777 -0.13119056893522904; 0.06562418798242288 0.019719284413343346 -0.0679133895842874; 0.09753860443738009 0.055890329247693916 -0.1646098646018714; 0.047004154327375036 0.03626948859823466 -0.11467395597303301; 0.03490604761252898 0.03291409886451478 -0.11045359289388287; 0.023936187630944065 0.02639831469663366 -0.09356237694392652; 0.0252089327940541 0.03102102205449062 -0.11582673741142377; 0.008063532428587396 0.010940617290430893 -0.043262548639933326; 0.008812088449299142 0.013246819424289092 -0.05386985181917948; 0.000720349661365567 0.0008127936407867512 -0.005161897139016028; -0.0012043324535642367 0.00023285766711591177 -0.0021449667093105945; -0.0003031384719045745 0.0008453854262635677 -0.0033285120437979883; 1.6376317353721448e-5 0.0002538076032960893 -0.0015849632957198661; -0.0007987764027794052 -0.00038617556411719626 -0.0006710101847198927; 0.0016814062338969614 0.004613331960304545 -0.0028987565537733516; -0.00161408637114292 0.00016625156361849158 0.001722723795095321; 0.0008263795438591096 0.0010743135512058463 -0.005167228424576932; 0.0007580483459509438 0.003621100416047618 -0.0010797278727454802; 0.006242441382155038 -0.003690533989072959 0.003806784881009547; 0.0010556863944426065 0.0008451942657068655 -0.00025098985178610727] %
+
+Mass Used: 100.77985706260552 kg
+Launch C3: 95.42570410363068 km²/s²
+||V∞_in||: 0.00020261466344254623 km/s
diff --git a/archive/ES_0.5635116026686802 b/archive/ES_0.5635116026686802
new file mode 100644
index 0000000..02bd6af
--- /dev/null
+++ b/archive/ES_0.5635116026686802
@@ -0,0 +1,22 @@
+archive/ES_0.5635116026686802---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T03:38:04.368
+Launch V∞: [6.479771981704077, -7.517565929588745, 0.058378904987046946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008866835361704872, -0.006284918953157879, 0.008009599040640011] km/s
+ V∞_out: [-0.007010666347844656, -0.0057439838493328135, -0.004717592260419503] km/s
+ time of flight: 1.859687148344606e8 seconds
+ arrival date: 2029-03-24T13:36:38.368
+ thrust profile: [0.207570354334916 -0.054107625504306985 -0.08600596591763164; 0.052035001162167006 0.011090569773707329 -0.06730630845516802; 0.04072491292961981 0.018837775439574187 -0.09132821570787984; 0.037745147034532966 0.024188728851083828 -0.12054250435985965; 0.033717120977022556 0.026945791759438436 -0.14319009653421894; 0.02115901117433994 0.017791192637865733 -0.10619012411486142; 0.017912048888093425 0.014377017024848464 -0.08924966917696575; 0.013395266165193936 0.012531268287788666 -0.08207428347758929; 0.005097085507286123 0.004670742547225366 -0.034917740680141286; 0.006180440118410803 0.005917400139826939 -0.04659680471837114; 0.003684115968906232 0.004024202627311273 -0.03092932584710256; -0.0005221190542552193 0.00029582541283826194 -0.0018302931651240808; 0.0007229237364722177 -0.00037869709043898627 -0.00033036445227828946; 0.0006557978053913782 -0.0001933013491348599 -0.0026943809896926123; -0.0013030591835782213 0.00015324202069725865 -0.0012047917886337924; 0.0006259243530615456 -0.0008049848969941017 -0.000709343192875673; 0.002273514921331554 -9.474528398541505e-5 -0.0011703744426323373; -0.00140798683693472 -0.0011334065638345283 0.002005531608177979; -0.00025797061041272053 0.00010063393607597079 0.0031800959749916004; -0.0023170263047564603 -0.003466159661879544 7.148623435261927e-5] %
+
+Mass Used: 82.81974164682106 kg
+Launch C3: 98.50465053713815 km²/s²
+||V∞_in||: 0.010219593471997813 km/s
diff --git a/archive/ES_0.5635129328639994 b/archive/ES_0.5635129328639994
new file mode 100644
index 0000000..1c7af24
--- /dev/null
+++ b/archive/ES_0.5635129328639994
@@ -0,0 +1,22 @@
+archive/ES_0.5635129328639994---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T01:05:37.816
+Launch V∞: [6.450890217681036, -7.2383451293098595, 0.2573299324935087] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00030437700365518926, 0.00034688953971678365, 0.00032994747024267616] km/s
+ V∞_out: [-0.000379953552349582, -0.00018380607844844016, 0.0003807288360565202] km/s
+ time of flight: 1.874957778749441e8 seconds
+ arrival date: 2029-04-07T03:15:14.816
+ thrust profile: [0.5406176622774167 -0.1270613275353864 -0.16048143288137193; 0.055909777113937666 0.020162829237911722 -0.055353755436300354; 0.0499380408984254 0.03378477603067042 -0.0827669106849839; 0.06240522093325379 0.05202405493489971 -0.14097465637237275; 0.040191634386229455 0.04114999050771562 -0.11960251668142835; 0.011510881074566876 0.01448654773382796 -0.044518754195745726; 0.029735144350689673 0.04048235942477826 -0.12499979189335587; 0.009832539748314387 0.014586699859301595 -0.051587085501421034; 0.020186947385367117 0.03717620261625483 -0.1155908746712561; 0.0012273974379568477 0.0018862376598365014 -0.0070238353605986325; 0.0010014529918771606 0.0020518331301516333 -0.007630417289803021; 0.0015182912075605078 0.0027575420288863967 -0.011662134098154614; 0.00030634550370535956 0.0005591323151697735 0.0005142173206358108; -0.00031335163021606273 0.0007493720503838253 0.0005334513977438946; 0.000277031630499768 -0.00042240973147184306 -0.0010234817989912518; 0.0003011210644034671 -0.00043814794555754486 0.0010228932004437384; 0.00036918121216646506 -0.0008401889786304306 6.642322004183482e-5; 0.0011608339304676474 0.0001085940674714571 -0.000574064814657607; 0.0010668614404455005 0.00010057714787076524 -0.0007939176722721196; 0.00016794900051413276 -0.0021392619633841354 0.0018413225501099568] %
+
+Mass Used: 108.66766789121903 kg
+Launch C3: 94.07384350573376 km²/s²
+||V∞_in||: 0.0005673121241773128 km/s
diff --git a/archive/ES_0.5635131595818493 b/archive/ES_0.5635131595818493
new file mode 100644
index 0000000..42946a8
--- /dev/null
+++ b/archive/ES_0.5635131595818493
@@ -0,0 +1,22 @@
+archive/ES_0.5635131595818493---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:28:07.078
+Launch V∞: [6.568558956180269, -7.350349978497359, 0.1556949540736369] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.016093123056863e-9, 2.3502095042165574e-11, -5.991411063020206e-9] km/s
+ V∞_out: [-2.237720337837864e-9, 5.204754503049987e-9, 7.282546005599983e-9] km/s
+ time of flight: 1.874957778749398e8 seconds
+ arrival date: 2029-04-09T16:37:44.078
+ thrust profile: [0.30488879613158154 -0.07762924466004059 -0.11211645774590948; 0.03596219059618846 0.009322322569713307 -0.04222938064321226; 0.04008270265425038 0.02008865243628246 -0.07768160832029819; 0.05297128820615414 0.035798864907451926 -0.14144941634181318; 0.0448835843625035 0.036273302852290155 -0.1511185891366843; 0.022137720903277758 0.020500228310882777 -0.09468647575315281; 0.017971550641631626 0.01822218718420497 -0.08911209890721607; 0.014688413132176002 0.016193476278786968 -0.08337599559468471; 0.004855377913146824 0.005762720031176574 -0.03230442208762943; 0.0030917019487944064 0.0033242373048519794 -0.0215184743670202; 0.0015422567813391554 0.003285815545298052 -0.01605928479786707; 0.0002966242765206331 0.0016060271944829956 -0.017811465752846107; 0.0008668805498274785 0.0010551418064659482 -0.008320575105800171; -0.0017135213842457953 -0.00038137207012810606 -0.0016902474419725737; -0.005665776907618271 0.0007905707075676629 -0.006816570354750236; -0.0004904836167944375 0.0026445163342478416 -0.0032717565536150143; -0.0005665905626051831 0.002702488367142173 1.1451735025514408e-5; -0.004082425293366158 -0.00023308807289903067 -0.0019893337138232408; 5.520215830397894e-5 -0.002786892256933839 -0.005904728822619255; 0.008844295694610576 0.0006483836166269597 -0.00013819389982181775] %
+
+Mass Used: 90.44454667753007 kg
+Launch C3: 97.19785248593614 km²/s²
+||V∞_in||: 9.226219246579721e-9 km/s
diff --git a/archive/ES_0.56351626206407 b/archive/ES_0.56351626206407
new file mode 100644
index 0000000..c004ab1
--- /dev/null
+++ b/archive/ES_0.56351626206407
@@ -0,0 +1,22 @@
+archive/ES_0.56351626206407---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T20:52:38.074
+Launch V∞: [6.395481468234773, -7.449504774163638, 0.08927440296559064] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5379751878417807e-8, -1.024999728316277e-8, 3.377596002723144e-8] km/s
+ V∞_out: [1.1231601322309952e-8, -2.560143283680545e-8, -3.396747028332524e-8] km/s
+ time of flight: 1.8133669472211567e8 seconds
+ arrival date: 2029-01-25T16:10:52.074
+ thrust profile: [0.2888952629251545 -0.08801332889239483 -0.10187392880575445; 0.12486952017914459 0.027498699420221616 -0.1289006413342874; 0.070548022434929 0.033028245198290514 -0.1215349271496539; 0.051252712754321944 0.03115253080111663 -0.12077657510257792; 0.03869116368358231 0.028206386668443512 -0.12162440858966704; 0.039574547964831876 0.03533586896019177 -0.14885925263821995; 0.021634333036894805 0.021878309965050108 -0.09666574218061402; 0.011176931686590529 0.013350587553247672 -0.060512685289300885; 0.004361078131643489 0.0047811814930507806 -0.02440898217642625; 0.0030424877387549933 0.004816792995250115 -0.02411315338469002; 0.0025701283768373756 0.0036180353529640824 -0.019657651146427365; 0.00019109447665041008 0.00024648827872523305 -0.0002613680741753012; 0.00031360024620654303 -0.0017016356238856282 -0.00018895581842446032; -0.0002494398377326998 -6.106065270639408e-5 -0.00022220186107577145; 7.063539533637897e-5 -0.0004948324478926697 -0.00021923698046437629; -0.0015065565476589497 0.0010781201783670261 -0.0007429193687766744; -0.0003922082226779299 -0.00020329483303895994 0.0001115324662391583; -0.0009772350124097264 0.0002821852802037842 0.002190139684853625; -0.0009515493817945001 -0.0013612155632659086 -0.0009117806319219692; -0.004031592465608202 0.00010697761138869364 -0.00027391614679404336] %
+
+Mass Used: 95.07153776731275 kg
+Launch C3: 96.40527450984611 km²/s²
+||V∞_in||: 4.347424209202539e-8 km/s
diff --git a/archive/ES_0.5635190409478446 b/archive/ES_0.5635190409478446
new file mode 100644
index 0000000..6b63fcc
--- /dev/null
+++ b/archive/ES_0.5635190409478446
@@ -0,0 +1,22 @@
+archive/ES_0.5635190409478446---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T22:28:13.805
+Launch V∞: [6.600427716918006, -7.415323242794749, -0.46565062127275314] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7810344470181475e-7, -3.646704467633742e-8, 4.218000873507519e-8] km/s
+ V∞_out: [-1.788434157738641e-7, 3.186529530364806e-8, -2.048383749854308e-8] km/s
+ time of flight: 1.874957778481695e8 seconds
+ arrival date: 2029-04-11T00:37:50.805
+ thrust profile: [0.19069958446135504 -0.05639258553723319 -0.07831767953941268; 0.033931736544102475 0.006890563814884456 -0.04410193499251822; 0.045235222982908614 0.018400281838191136 -0.09863051705211093; 0.06964351733266322 0.03616783938108388 -0.2083037423157258; 0.035903052723591254 0.022603559026074114 -0.14043040575776786; 0.02301139069013759 0.016424484156419415 -0.11034331420176306; 0.01626197617265226 0.012659517966220087 -0.09162897775948595; 0.009446538206106712 0.007934829249325238 -0.06137593607435491; 0.0030583932745130355 0.002826564600948733 -0.022698211334480134; 0.00123237181388684 -0.0007863641330323858 -0.006201166136870178; 0.0013548564262883455 -7.169027549309309e-5 -0.004062685471095742; 0.003069189740639199 0.0002500799349363322 -0.0026852466129070923; -0.0024152348842506432 -0.0009605971190656004 -0.0008974643454855583; 0.0018765622189656935 -0.0011556276001887691 0.00036255827779535033; -0.0007598823041314806 0.0010008222910262183 -0.003933203864642595; 0.004007078716081373 0.001667470268225905 -0.003024150869646338; 0.0006033734133856902 0.0007265976421203885 -0.004452300964430345; 0.002930467128300751 0.000790072732801567 -0.0014076757555773218; -0.0008650962631210626 -0.00047152384293169965 -0.0015655189813672706; -0.007020665581701262 -0.0014327747155595705 -0.0004907164304197836] %
+
+Mass Used: 81.28349160800008 kg
+Launch C3: 98.76949534248317 km²/s²
+||V∞_in||: 1.8662753146031104e-7 km/s
diff --git a/archive/ES_0.5635294243718594 b/archive/ES_0.5635294243718594
new file mode 100644
index 0000000..e0b66f5
--- /dev/null
+++ b/archive/ES_0.5635294243718594
@@ -0,0 +1,22 @@
+archive/ES_0.5635294243718594---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T08:42:22.567
+Launch V∞: [6.223051585559045, -7.646044624250298, -0.16247547424066924] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.174640103432524e-6, 8.409046064696996e-6, 1.2307712313317235e-5] km/s
+ V∞_out: [1.4846806797821656e-5, 9.267336651577037e-6, 3.9554544829573464e-7] km/s
+ time of flight: 1.773444669825305e8 seconds
+ arrival date: 2028-12-10T23:03:28.567
+ thrust profile: [0.23592742525926197 -0.076178863216794 -0.08818045214161321; 0.06040444648069279 0.011872659133797075 -0.06554369402695706; 0.0854003319730193 0.03716140365666079 -0.14843730358373355; 0.08190319118241292 0.049410153950999444 -0.1961011698626105; 0.05854554573503048 0.04287222972454732 -0.17891146510597186; 0.03231100296640391 0.02702662907791723 -0.12116238548410198; 0.024024674259191303 0.022455011702527443 -0.10598640830499147; 0.004305976342757039 0.0042749482230455 -0.021836872493303492; 0.002327775246730622 0.0020640826099862495 -0.01348025363288932; 0.006512983954058137 0.007247371320903067 -0.03816105936818705; 0.001892541410101041 0.0022019861070517715 -0.012167621715974387; 2.6098024155048702e-5 0.000359222514419904 -0.0007206911451394869; 0.0003292426239544645 -0.0006649722021038801 -0.0007238899509612485; -0.00022391022847071572 -0.00025419645002830915 0.0013510786585998174; 0.0005704696558173527 -0.001700444115567276 0.0007292597417023405; -0.0009472006942137774 0.00112657144560358 -0.0014696054018316922; 0.0003050530580792102 0.0010269004046173438 0.0002963038535685296; 0.00016338241533873465 -0.001080382829107792 -0.0005938192957134589; 0.0005277220610664973 -0.0008118437918044267 0.0008921270611341463; -0.00022038226909167676 0.000332263405685823 -0.0014868135691674805] %
+
+Mass Used: 90.36485011217019 kg
+Launch C3: 97.21476771228555 km²/s²
+||V∞_in||: 1.7503309947923824e-5 km/s
diff --git a/archive/ES_0.5635314254034861 b/archive/ES_0.5635314254034861
new file mode 100644
index 0000000..2c4e3a4
--- /dev/null
+++ b/archive/ES_0.5635314254034861
@@ -0,0 +1,22 @@
+archive/ES_0.5635314254034861---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T02:32:50.396
+Launch V∞: [7.657353169406436, -6.25917273901781, 0.05095972483712799] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.3090856791187415e-6, -7.630618802352464e-6, -6.009405114712161e-7] km/s
+ V∞_out: [3.733784413397984e-7, -1.976397184022825e-6, -8.556402404622432e-6] km/s
+ time of flight: 1.685214094552259e8 seconds
+ arrival date: 2029-09-12T14:02:59.396
+ thrust profile: [0.24629733273483576 -0.03483443305042458 -0.09331081841080711; 0.048804463123829175 0.017088703003931557 -0.058467768344551176; 0.04689312482792414 0.02792974414889292 -0.09397149874192787; 0.03414047059350488 0.02621886267647399 -0.09863303768972768; 0.06363124417565388 0.06054643806057547 -0.23222530310772374; 0.03251056812060939 0.03245221279950583 -0.14505344272472864; 0.015053449335887389 0.016699376556355894 -0.08257824738509772; 0.013140182840695633 0.015257563400822615 -0.07953530199030556; 0.007304260208080912 0.008095780586508306 -0.047544295668798885; 0.008085648352667655 0.010401158791964491 -0.060368681872434646; 0.001017480161987125 -0.00010404159233270331 -0.003996380140054618; 0.007176464138481119 0.00021266009829993518 -0.006853899346657859; 0.0008701194345031606 0.0024418341868268443 -0.009895561794628015; -0.005050474017303246 0.004282546031944651 -0.005565849958965521; -0.0004813765991842538 0.006359416697359902 -0.0006385000761270597; 0.0005502255178049069 -0.0007816509165138395 0.0004594262858736236; -0.0020360984226921687 -0.0038923904406635286 -0.001478857687373257; 0.0014204685913908077 -0.0014511942258636724 -0.0009752016720563613; 0.0020178743052287045 -0.0023209513305331993 0.0005527982316089934; 0.0017327752472559342 -0.0037932872258231764 0.003508229928626402] %
+
+Mass Used: 86.86642562067891 kg
+Launch C3: 97.81489783143797 km²/s²
+||V∞_in||: 8.783831293639948e-6 km/s
diff --git a/archive/ES_0.5635360023403189 b/archive/ES_0.5635360023403189
new file mode 100644
index 0000000..644c805
--- /dev/null
+++ b/archive/ES_0.5635360023403189
@@ -0,0 +1,22 @@
+archive/ES_0.5635360023403189---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T17:20:22.243
+Launch V∞: [6.363574865590822, -7.438712458924897, 0.16316821351537025] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.5794718437429663e-6, 3.0837490594071768e-6, 3.6946096242981013e-6] km/s
+ V∞_out: [5.13842568322607e-6, 3.065206607080305e-6, 1.0285492865090904e-7] km/s
+ time of flight: 1.8491877751125428e8 seconds
+ arrival date: 2029-03-09T23:39:59.243
+ thrust profile: [0.33960003419000756 -0.09021332625574663 -0.1162453208775187; 0.13554292691265488 0.034261546834059055 -0.1412101014693525; 0.060629809092666874 0.03005269636292165 -0.11018371977696297; 0.04486679630359986 0.029980379329624517 -0.11549171035210468; 0.03489586916951537 0.0279466967599913 -0.11440651043897276; 0.018066708632768436 0.016710235470066417 -0.07418975288839458; 0.022995805875044354 0.023156262580325212 -0.10728867458496512; 0.01608927625358854 0.017275142235679147 -0.0848302269994258; 0.005092314008876359 0.005246111796568471 -0.028751008672050084; 0.004437763009838989 0.0060525488333581816 -0.0308724248299781; 0.0026216418859285624 0.00288064368159235 -0.01892484408414743; 0.00019116479318276845 0.0003294618132688704 -0.000968759668121687; -0.00022542476402133578 -0.0003494767290437165 -0.0010638222168718957; 0.00010154262761674914 0.0013865301144270494 -0.0006579950663297154; -0.0003851692694595803 0.0005615758845156818 8.130862794576872e-5; 0.0023441427429852866 -0.001720072715205348 0.00015089718594021124; -5.018338795061142e-5 0.003751143381754309 -0.007259126074343647; -0.0004095663346724203 -0.0008131962353463583 0.004696201211634921; 0.0004934004471104285 0.0008303331387465492 0.0010553863620406442; -0.004643544838396467 0.0032440943642018235 -0.0007653356791768361] %
+
+Mass Used: 98.29778283277301 kg
+Launch C3: 95.85615198244554 km²/s²
+||V∞_in||: 5.997688489534903e-6 km/s
diff --git a/archive/ES_0.5635383220075609 b/archive/ES_0.5635383220075609
new file mode 100644
index 0000000..24cd88d
--- /dev/null
+++ b/archive/ES_0.5635383220075609
@@ -0,0 +1,22 @@
+archive/ES_0.5635383220075609---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:23:33.104
+Launch V∞: [6.226322479375943, -7.518570144070238, -0.18723672494745794] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.25451045010751e-8, 8.22209938677599e-9, -3.130841877986835e-8] km/s
+ V∞_out: [-9.885506519985582e-9, 2.326974950701159e-8, 3.0457930758415664e-8] km/s
+ time of flight: 1.8314221527634975e8 seconds
+ arrival date: 2029-02-17T23:13:48.104
+ thrust profile: [0.4536610969309479 -0.12286208785941714 -0.16220065043231618; 0.049300723821010306 0.011202836817996602 -0.05799708854127971; 0.0504264929203243 0.02386463874814186 -0.09815965946398823; 0.04904310247711019 0.03118406002868251 -0.13161842947999977; 0.031811284062659706 0.024745352272692027 -0.11054508234389357; 0.02117480663806295 0.018201805020077778 -0.08801712305367802; 0.01321954791311207 0.012833549150566632 -0.0656110158119177; 0.01513215417150233 0.016452476123150706 -0.08897890261389649; 0.02424677971706774 0.028887729365438777 -0.1516609290802433; 0.00037746066723367964 0.00038000315112957285 -0.002558337026387145; 0.002480599047740238 0.002924339957515344 -0.020433567382145697; 0.0005068163933482889 0.0006761539405546636 -0.004600774674567606; 5.6171901200121874e-5 -0.00015138361084817046 -0.0004432592843323764; 4.6055155662751466e-5 -2.3476450580552477e-5 -0.00012634988504547754; 1.0829225320992835e-6 0.00015715131270486958 -0.0003798666846680528; -0.0005038028723585628 0.0001062648304838107 -0.0006373336265952483; -0.00043176958427212334 0.00020872789320188487 -0.00015189694444619307; 0.0007167695885765023 0.0005755681719693517 -0.0003162671044434181; 0.0006224299097629923 -0.00014950677720310525 -0.0008494010081079397; 7.975422336950255e-5 0.0001695595073355482 0.00035046314491580556] %
+
+Mass Used: 101.36360606083008 kg
+Launch C3: 95.3310462196556 km²/s²
+||V∞_in||: 3.9447455453882345e-8 km/s
diff --git a/archive/ES_0.5635504089930945 b/archive/ES_0.5635504089930945
new file mode 100644
index 0000000..2297c98
--- /dev/null
+++ b/archive/ES_0.5635504089930945
@@ -0,0 +1,22 @@
+archive/ES_0.5635504089930945---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T19:19:32.472
+Launch V∞: [6.625178557389008, -7.240717833313996, 0.29357059552945586] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.772940810568435e-7, -7.389187068938032e-7, -2.2816915804365875e-7] km/s
+ V∞_out: [2.750735368908719e-7, -5.513012341297586e-7, 5.989249826549929e-7] km/s
+ time of flight: 1.8749577797886306e8 seconds
+ arrival date: 2029-04-06T21:29:09.472
+ thrust profile: [0.3021911230754612 -0.06996596494412172 -0.09474083286073162; 0.11904146113984734 0.038169122640085554 -0.11427037997104175; 0.07965354033382396 0.048126995467357034 -0.12897409134429844; 0.06723633539854472 0.05510182288241247 -0.1529087547569823; 0.043961919908327075 0.04397371081881182 -0.1299185166254535; 0.01923340831647701 0.022273034107475307 -0.07074488844041772; 0.013567813001442318 0.017784468465728513 -0.0594152692114074; 0.004904865071652074 0.007137824285244056 -0.025472024044833553; 0.012830036313925241 0.020578049061397593 -0.07367308678449602; 0.0025601624353416143 0.004480077474640604 -0.01737458674083086; 0.0023293489597147614 0.005213746007578846 -0.019750310678943457; 0.00043189252530169203 0.00019363509860154332 -0.0030367890815021156; 0.00043952914211963716 0.0005638390085416346 -0.0031904360647921383; 0.00016249393323511136 0.0007371404064084471 -0.001232027928037021; -0.00012116187916525975 0.0007753590453718894 -0.002226218354273564; -0.0009244467904539651 0.0009718186441729437 -0.0023872301036561338; 0.00034460514538368794 -0.0005053147121369282 -0.00031458872565600857; 0.0003127648869843327 -5.288898022866393e-5 6.299170910644249e-5; 0.0002039697330612055 -0.00016953590174616315 -0.00044833926676425334; -0.003051340754710671 -0.0013657351825470867 -0.0008571765994773156] %
+
+Mass Used: 95.1003225964223 kg
+Launch C3: 96.40716935351794 km²/s²
+||V∞_in||: 8.604724537604271e-7 km/s
diff --git a/archive/ES_0.5635669208009307 b/archive/ES_0.5635669208009307
new file mode 100644
index 0000000..f569c06
--- /dev/null
+++ b/archive/ES_0.5635669208009307
@@ -0,0 +1,22 @@
+archive/ES_0.5635669208009307---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T16:18:48.099
+Launch V∞: [7.711298522073738, -5.444659959581249, 0.3202892859798624] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3080101626469037e-5, -4.3577052969692834e-5, -0.00012373940161691118] km/s
+ V∞_out: [-0.00011898877400313394, -1.4333603316243835e-5, 5.4839937822034075e-5] km/s
+ time of flight: 1.8749577787587565e8 seconds
+ arrival date: 2030-04-16T18:28:25.099
+ thrust profile: [0.8616512118897147 0.010919769192138783 -0.19583451945546496; 0.2607214174970928 0.1746638049722382 -0.22191799452479466; 0.08640454078646742 0.09715539669741322 -0.1420260174675184; 0.027528154578371947 0.043169042097957674 -0.07170615329270254; 0.03386189303701089 0.06780692273156468 -0.12175899545516194; 0.015607174990401512 0.03914753312497596 -0.0766373110379144; 0.002737644975270095 0.009337124441174849 -0.02046256615188799; 0.0008256545330019814 0.003293113781051849 -0.007813566202375322; 0.001026012686584845 0.005125920795575591 -0.013155275862912057; 0.0002311676025199114 0.001417330896333317 -0.003716501679908278; -0.00014083236782512655 0.0004642138786424986 -0.0017335317034893414; 0.0001438654213235826 -0.00027616687936484407 -0.00041397601869115565; 9.245426321160535e-5 7.473221323921409e-5 -0.0002045669757094723; 0.00014443853831485123 0.0005459252036794015 -0.0005346719105617632; -0.00045484657403928953 -8.616404074108852e-5 -0.00033765876572026737; 6.198145546364023e-5 -0.00036811012306022385 0.00034348718713793185; -0.00031318279777003456 -0.0003230308531687841 0.00013620577233421105; 0.0001695126804518304 0.0006488096606297965 -0.00018485141269837687; -3.539391666606772e-5 0.0002404638091893076 9.89201377868104e-5; 0.0004962190090495149 0.001030756895301436 -0.001055614802897301] %
+
+Mass Used: 137.0970531085677 kg
+Launch C3: 89.21103219871739 km²/s²
+||V∞_in||: 0.00013183887179657377 km/s
diff --git a/archive/ES_0.5635680776535611 b/archive/ES_0.5635680776535611
new file mode 100644
index 0000000..d4c2c6c
--- /dev/null
+++ b/archive/ES_0.5635680776535611
@@ -0,0 +1,22 @@
+archive/ES_0.5635680776535611---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T18:48:30.964
+Launch V∞: [7.445509482875414, -6.264145112333782, -0.10377595780322386] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.234255324033518e-5, 9.186942541072218e-5, 8.349411194020625e-6] km/s
+ V∞_out: [-5.92093992527345e-6, 3.058596039910139e-5, 0.00010688975424116246] km/s
+ time of flight: 1.6670089544819164e8 seconds
+ arrival date: 2029-08-21T04:36:45.964
+ thrust profile: [0.5233949897453383 -0.08722177412199235 -0.19183320791592057; 0.04840260132284487 0.017299983018388622 -0.05741360643121002; 0.0659468335356532 0.04078703141974214 -0.1294296775353905; 0.06282149260657795 0.05032508201118332 -0.1737888296888519; 0.03769436463268136 0.03759386624629123 -0.13470486769031773; 0.039938400019372614 0.043878285521211806 -0.1731542499597087; 0.012565525796325193 0.014848201586144619 -0.06747402921576602; 0.007580901668101755 0.009650790708328253 -0.04602460661054023; 0.014040778410435361 0.018909005359199607 -0.09402646367615917; 0.0012051643622714716 0.0014990325753526214 -0.006460829304755231; 0.0009921796921784185 0.0030303131798209595 -0.01764236803679935; 0.00017123350903479955 -0.0011701401012613542 0.0013166389033169852; 0.0010870366147312691 0.0008641376852359887 -0.0008500824146290484; 0.0025192474278289056 -0.0024929264758820346 -0.003536702541561551; 0.00048048156289428766 0.0007455168630712194 -0.004059811299549717; 0.0039698459077125645 0.002548345835816313 -4.0610424277304213e-5; 0.000512168815272808 0.004741692965184984 -0.0001605692931797428; -0.003081013642271362 -0.0002502347971273088 -0.0020573538296123485; 0.0021991049772115447 -0.0003144269448603484 0.0002285179680018021; 0.0009105024310636105 -0.004588314709157099 0.0023730495350760767] %
+
+Mass Used: 105.16170369443262 kg
+Launch C3: 94.6858948973809 km²/s²
+||V∞_in||: 0.0001113386632626201 km/s
diff --git a/archive/ES_0.5635790675571779 b/archive/ES_0.5635790675571779
new file mode 100644
index 0000000..04c8ea4
--- /dev/null
+++ b/archive/ES_0.5635790675571779
@@ -0,0 +1,22 @@
+archive/ES_0.5635790675571779---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T14:17:39.035
+Launch V∞: [6.40308935145682, -7.365114115501985, 0.1302278915984609] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0230922244298094e-5, -2.921877230946537e-6, 4.500082026205278e-8] km/s
+ V∞_out: [2.393739876849513e-6, -4.511235547167574e-8, -1.0367018586328783e-5] km/s
+ time of flight: 1.8749577786998558e8 seconds
+ arrival date: 2029-04-08T16:27:16.035
+ thrust profile: [0.3979331121928458 -0.09272891326970631 -0.11931762740196905; 0.05893196964319367 0.01842410060366841 -0.061200009657262994; 0.11989422712923481 0.06986762559057265 -0.18485915273906317; 0.04705232599625511 0.037946915834739324 -0.11237665581667175; 0.04035577042771365 0.03989101900492063 -0.12262386381765895; 0.030316059589890483 0.034835338617194754 -0.11237724600030405; 0.010611515871190493 0.012117475189801774 -0.05091050455968992; 0.007280939538787336 0.009826623882741609 -0.038007761869312554; 0.01095997759601521 0.01939094364651145 -0.08047652218269137; 0.0024461405481899317 0.005214905115910247 -0.019142425701614837; -0.0007873996963884833 0.00010373815408418316 -0.00057671187538591; -0.0006504495752547746 0.0029864473855599114 -0.0017904374241269798; 0.00029995285801549956 -0.0011390998121414034 -0.0007503089719480884; -0.0043455777519209 0.001666491300967306 -0.0021306248100878052; -0.001959983568060074 0.0023016301496666 0.0030143417093447572; -0.0004931298233573226 -0.00015381761055480766 -0.0004479114399170694; -0.000994364177935091 0.0009266295983220174 0.0006740840458983645; -0.000483221551653652 0.00204781988718332 -0.0022805346625772395; 0.008975299795469207 0.005885150256488782 -0.007651314680592607; -0.0007354825052799116 -0.0027834937413949903 0.004325608570550248] %
+
+Mass Used: 101.8173043450447 kg
+Launch C3: 95.26141848085649 km²/s²
+||V∞_in||: 1.064007338299044e-5 km/s
diff --git a/archive/ES_0.563579892198238 b/archive/ES_0.563579892198238
new file mode 100644
index 0000000..c8440a4
--- /dev/null
+++ b/archive/ES_0.563579892198238
@@ -0,0 +1,22 @@
+archive/ES_0.563579892198238---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T02:37:38.656
+Launch V∞: [7.71829126383014, -5.707261111632099, 0.5375287336546669] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.877836974608414e-7, -1.2336346603193374e-6, -1.0931255790662464e-7] km/s
+ V∞_out: [8.816089303452289e-8, -4.4720022994505374e-7, -1.3412676464242584e-6] km/s
+ time of flight: 1.8460741506175828e8 seconds
+ arrival date: 2030-03-15T18:27:53.656
+ thrust profile: [0.5367877070611997 0.01495280319163655 -0.10755066906461176; 0.20675211264246926 0.14182882317251372 -0.1566090595110735; 0.11226294588646717 0.1292913477486359 -0.1612274162916347; 0.06985303621678789 0.11266208414786029 -0.15787061831566065; 0.017913499486833268 0.036957210962953596 -0.058682230805956484; 0.01230764317524116 0.031157005289535904 -0.052909579938060516; 0.009322427407905698 0.029080873236724356 -0.05191348305956362; 0.008161609604931949 0.029523288545591487 -0.05702878275571925; -0.0001343299730548072 0.00102287363410874 -0.0027086821092822096; 0.0012670491445393491 0.0057464741804905935 -0.010831269657407827; 0.00012242296650224883 -0.00016025337186812046 -0.0014986322463745516; -0.0006879755832714961 -0.0012656941922121706 -0.003883544988253637; 0.003378842792572341 0.001278885474832059 -0.0016604427627714795; 0.0008923314646659831 0.0038213391685535105 -0.00013851201942454588; -0.0034155655719037997 0.008497973584469777 -0.0016408248458253797; -0.0005987271527715542 0.0003763918684048285 -0.004001283091555077; -0.00032715906261900177 -0.0035822199415805173 0.000677867279617195; 0.00041428494493778287 0.00918381383360924 -0.0125234587379871; 0.0026573413523300507 -0.0015585018613566862 0.0001435379905903348; 0.0006715686495378236 -0.001017635033694578 0.0002817857831461123] %
+
+Mass Used: 118.31278591112459 kg
+Launch C3: 92.4337865691691 km²/s²
+||V∞_in||: 1.4166333770422756e-6 km/s
diff --git a/archive/ES_0.5635850981366021 b/archive/ES_0.5635850981366021
new file mode 100644
index 0000000..1c45d2a
--- /dev/null
+++ b/archive/ES_0.5635850981366021
@@ -0,0 +1,22 @@
+archive/ES_0.5635850981366021---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:37:50.194
+Launch V∞: [6.294082041594735, -7.387501688694207, 0.05485027930017953] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.702496384088792e-6, 0.001195641241496202, -0.000807730940794826] km/s
+ V∞_out: [-0.0005702271403488664, -0.0012965857538085777, 0.0002740732695437381] km/s
+ time of flight: 1.874957778741756e8 seconds
+ arrival date: 2029-04-08T21:47:27.194
+ thrust profile: [0.4642762332730352 -0.12034323525016155 -0.12401503222654416; 0.0922827223869673 0.028211899239894582 -0.10446019351880258; 0.1101352447959205 0.06846023731062129 -0.18080179243345032; 0.06801320260370419 0.05986447268177693 -0.1651309624495161; 0.02000916131364914 0.018858620908800208 -0.062325678944894686; 0.021772827853920713 0.02524990684595499 -0.0802007420405911; 0.009392236733820867 0.012798534178335014 -0.05051880020459336; 0.0057314265874800485 0.007988886188026057 -0.031270861273066844; 0.014744907052195654 0.024574860677376843 -0.09127540157563453; 0.004288559947228753 0.007520037152848526 -0.02817347457713201; 0.0012052639044231653 0.0015293096514673876 -0.008918376252296207; -0.0009697369659812992 -0.0004025978471675502 -0.001619240783467798; -0.0004362829310696556 0.0014802150509261101 -0.002274121596394896; 0.000553017623244466 -0.00011888311682636056 -0.00016776880804620633; 0.0002957439706582828 -0.0004433507890373241 0.002430562912151135; -0.0004901714982464371 -0.0008692755962582509 0.0023360548509126174; 0.0021946515310367607 -0.004127451120051546 0.0021981045202624522; -0.0012143153086799112 -0.0033477003453232087 0.0015004572590528406; -0.0012008997465096768 0.002527004334754404 0.0021771631316707127; 0.0006282479707026676 -0.00029654488764047174 -0.0006808075970522161] %
+
+Mass Used: 108.05293990981 kg
+Launch C3: 94.19365849992441 km²/s²
+||V∞_in||: 0.0014429140513430967 km/s
diff --git a/archive/ES_0.5635872973309539 b/archive/ES_0.5635872973309539
new file mode 100644
index 0000000..a936c29
--- /dev/null
+++ b/archive/ES_0.5635872973309539
@@ -0,0 +1,22 @@
+archive/ES_0.5635872973309539---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T09:59:49.738
+Launch V∞: [7.706564551756967, -6.170452648613826, 0.01922405978750182] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.914692777156307e-7, -2.7732177192010462e-6, 5.8235214838012906e-5] km/s
+ V∞_out: [2.430954793897674e-6, -5.816801338323041e-5, 7.061687798760043e-7] km/s
+ time of flight: 1.7110332145109853e8 seconds
+ arrival date: 2029-10-12T18:41:50.738
+ thrust profile: [0.2715199030908129 -0.033298728727806204 -0.096606398934872; 0.06921088981810165 0.02693752971641648 -0.08181968435036141; 0.046280397915403726 0.03029379780899625 -0.09378495166662912; 0.03255794333988888 0.02755513164733954 -0.09387531054076799; 0.02678039017783642 0.026818489905897927 -0.1007618749045007; 0.01953058852154983 0.02297353789654348 -0.09745712191560513; 0.014605247607771097 0.018189702481910635 -0.08600798963470854; 0.014806908727737 0.018902316809959983 -0.08722663465646945; 0.027355098737941435 0.03680419528066862 -0.18295219103636945; 0.0032224024137055933 0.007023852862914414 -0.0334427927826013; 0.0021347485013243064 0.005341120322130895 -0.027610703240443478; 0.0011493981154492422 0.0028502062518671618 -0.013949162297964078; 0.002358008074224064 0.0029653089660609546 -0.01942782219922628; -0.00013460635016492094 -0.00025562137848517976 -0.0012584739807231342; 0.00042095906689018165 -0.0007499819405183257 0.0024464816800976803; -0.00024937786673949377 -0.005748541155916862 0.0012269897605486977; -0.0018495540328664134 0.0002632136034530226 0.0026889187338337154; -9.587885396630051e-5 0.002059840457072999 -0.0007929900430395079; -0.0006380217642446775 -0.00039400432765169467 0.0009728667550110192; -2.6834277595481454e-5 -0.001780467811771057 -0.0013767431392219037] %
+
+Mass Used: 88.96688979811279 kg
+Launch C3: 97.46599264365716 km²/s²
+||V∞_in||: 5.83025233754338e-5 km/s
diff --git a/archive/ES_0.5635912926280163 b/archive/ES_0.5635912926280163
new file mode 100644
index 0000000..4a10d24
--- /dev/null
+++ b/archive/ES_0.5635912926280163
@@ -0,0 +1,22 @@
+archive/ES_0.5635912926280163---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T11:32:38.534
+Launch V∞: [7.605435469029863, -5.897762965839219, -0.043633498466503405] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3732885911762003e-6, 7.96774360933607e-6, -0.000202904601151563] km/s
+ V∞_out: [-8.982500241574068e-6, 0.00020323568487641073, -1.5837509767156052e-6] km/s
+ time of flight: 1.8429638381676257e8 seconds
+ arrival date: 2030-03-13T12:59:01.534
+ thrust profile: [0.3867269003292255 0.010396610882086028 -0.08685951137363589; 0.3519955904989331 0.22841537988438865 -0.22552710223684258; 0.07515837564615326 0.0882118147286815 -0.11302540999878065; 0.03642338100588464 0.065827202139832 -0.09153749684004243; 0.024627507903395626 0.060075061140798476 -0.09010359462527794; 0.014050462688020253 0.043768107212890366 -0.07351709084318998; 0.012209013448134522 0.04780212982573523 -0.0832641617535697; 0.004546153008008319 0.024859931812219255 -0.04543074521821145; 0.002946363485815842 0.024520551965251124 -0.04530172725852811; -0.00024065898623800049 0.002682672789690059 -0.0033906082511474694; 0.0015002078204027582 0.0003561594643657322 -0.002342940797373934; -0.0006369172306695632 0.0032500413446758056 -0.009568581538391567; -0.0016731600008294272 -0.001327623509225804 -0.0009496373727679578; 0.0013252900019774716 -0.0005677118684908228 -0.0007686347474572018; -0.0016238188372974278 -0.0023896729202611757 0.0020381006488678372; -0.0006559035038251244 0.0040217919461022576 0.0007019778918322317; 0.001441440553604311 -0.0015546467713956902 -0.0032498828568122647; 0.004707232114158882 0.004596939001387395 0.0009702796630298148; -0.0011387175991405397 -0.0034771923008056664 -1.8758735960005407e-5; 0.0006108214811034984 0.0002596168651684911 0.002392683068103112] %
+
+Mass Used: 117.19223815024088 kg
+Launch C3: 92.62816055699055 km²/s²
+||V∞_in||: 0.0002030656249301039 km/s
diff --git a/archive/ES_0.5635915424035074 b/archive/ES_0.5635915424035074
new file mode 100644
index 0000000..d882428
--- /dev/null
+++ b/archive/ES_0.5635915424035074
@@ -0,0 +1,22 @@
+archive/ES_0.5635915424035074---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T20:05:12.727
+Launch V∞: [7.955232103441572, -5.7224966067402985, 0.12144312429621189] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.08519024290707e-6, -0.00014658819548616725, -2.5041779230839674e-6] km/s
+ V∞_out: [-0.00014266099547741517, 2.2082948046478412e-5, -2.9093674850724382e-5] km/s
+ time of flight: 1.874957778742257e8 seconds
+ arrival date: 2030-04-23T22:14:49.727
+ thrust profile: [0.39069438456287375 0.002974956462438328 -0.12169501884648923; 0.0757847043111089 0.04646795343524908 -0.08803058750905661; 0.032768504242015405 0.03175008351812637 -0.07064182911141413; 0.03101997422886579 0.03873514087017009 -0.09812212952003871; 0.014606592197843219 0.02230689238735733 -0.06373409841625234; 0.009462643909638541 0.01610770115415697 -0.05164820981215959; 0.006734832136096074 0.013945601910232405 -0.0459784823628857; 0.0030675600103780678 0.00802793877964949 -0.02817835410331417; 0.012557249205468279 0.035347777723920344 -0.1203943176732966; 0.004323624664178914 0.019778977830548203 -0.06692793776875915; 0.0023763401883160327 0.01894125868130899 -0.06704767583772603; -0.0036343006964332254 0.00042627085796174535 -0.009335307499186932; 0.0007820520464430897 -0.002728355672331208 -0.003048663423008509; 0.004043657179549453 0.003823492835795205 0.0015979587021055655; 0.013529333231454095 0.006052829510951357 -0.004776678030063575; -0.007861022153723501 0.00380562289993798 0.008089739201002068; 0.0034372391475796867 0.0074750570491910525 -0.011072432779420695; 0.004938147025047227 -0.00790573371596142 -0.011196514526519395; -0.006230103998119799 0.014244217490381185 -0.003099193126536044; -0.01201126584402308 0.006496626442951119 -0.005613186969611624] %
+
+Mass Used: 97.24676975113925 kg
+Launch C3: 96.04743366622047 km²/s²
+||V∞_in||: 0.0001466244112735337 km/s
diff --git a/archive/ES_0.5635942626630206 b/archive/ES_0.5635942626630206
new file mode 100644
index 0000000..b8071a5
--- /dev/null
+++ b/archive/ES_0.5635942626630206
@@ -0,0 +1,22 @@
+archive/ES_0.5635942626630206---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T15:52:49.561
+Launch V∞: [6.53852974744044, -7.3931569320268755, 0.16150307684688026] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.123232995288819e-7, 2.2408247045122268e-7, 1.0353924815064809e-7] km/s
+ V∞_out: [-8.708996323379625e-8, 1.3644156582215443e-7, -2.1802702917506416e-7] km/s
+ time of flight: 1.8413042750909474e8 seconds
+ arrival date: 2029-02-27T19:13:16.561
+ thrust profile: [0.22693467581753055 -0.06082931622965167 -0.08025032533612639; 0.10848767197174425 0.02985632479706035 -0.11622984902603614; 0.057369701049408146 0.031798300428598124 -0.10670173066498503; 0.04177100240266693 0.02863106781595664 -0.10446209141253687; 0.03928771641049183 0.0324682010752798 -0.12083584793033635; 0.036720287418540824 0.03633797805559695 -0.1411785511183784; 0.018075319084690303 0.019535798375055292 -0.08490285476170488; 0.011628408519925882 0.015567392475279114 -0.07017552211926796; 0.009341577525864503 0.012031521182196818 -0.06351312916472461; 0.0034575492970658054 0.005820800524534465 -0.028688239569570156; 0.00046752352169746503 0.0001903290153536805 -0.0009772472526658337; 0.0029558539211993087 0.0008057833418673303 -0.0032841342658055305; -0.0006218951140532971 0.00040265977087093553 -0.0018247190051484835; -0.0006834211819425044 -4.505694930009559e-6 0.00117875554722124; -0.0010480125851659618 -0.0006665501477020433 -0.0014582967071574853; 0.0013351194514530675 0.0012240485483298155 -0.0007300755819449206; 0.0013508314535405658 0.0002567549001913655 -0.0015091370008000807; -0.00019580166365715907 0.0005520271005992949 0.0007280680874725155; 0.0021147106301844226 -0.003600681931370365 0.00656925520242445; -0.0026806973322482984 0.000519082512818239 -0.0007115377843240373] %
+
+Mass Used: 89.14283355268981 kg
+Launch C3: 97.4372239235716 km²/s²
+||V∞_in||: 2.712007615921819e-7 km/s
diff --git a/archive/ES_0.5635955067801411 b/archive/ES_0.5635955067801411
new file mode 100644
index 0000000..b89f535
--- /dev/null
+++ b/archive/ES_0.5635955067801411
@@ -0,0 +1,22 @@
+archive/ES_0.5635955067801411---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:27:40.564
+Launch V∞: [6.599725824539215, -7.395456124508067, 0.055355320753868203] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010723598280465345, -0.0005391953027175888, 0.006621007223458746] km/s
+ V∞_out: [-0.012126611000612686, 0.00011982591324449118, 0.0034719450533578352] km/s
+ time of flight: 1.8749577787493238e8 seconds
+ arrival date: 2029-04-10T20:37:17.564
+ thrust profile: [0.23224271664171509 -0.0649609773103385 -0.09287758947289632; 0.045613414504970105 0.00887354308194409 -0.058287220826593364; 0.03407774125881838 0.013936153531507702 -0.07447606601392606; 0.03558621038846121 0.019584954021452185 -0.10731840333518994; 0.03095142047582841 0.020103396645227752 -0.11863057777383275; 0.016422769052741478 0.012869354210272837 -0.08027892794863238; 0.02830862343348507 0.018770738457796258 -0.12681128909622624; 0.01447082813424427 0.013014853945869773 -0.0921224589342214; 0.011011056827500278 0.009479552481190581 -0.07590316941198043; 0.0009494828861383518 0.0007980768417006321 -0.007518148822924923; 0.005162125766201061 0.0047122530034573356 -0.04205174911053782; 0.0015847404151441628 0.0014321882300733625 -0.013553030995113027; 0.0006934825192101083 0.0003318601653147183 -0.0014382244540524448; -3.580342672022718e-5 -0.00018049856854181982 -0.0008047474251101636; 0.002027135787896917 0.0022217532842869316 0.0017267541770336178; 0.0012157780003172905 -0.0020755509873553175 -0.002056420276307715; 0.0028986652605376027 -0.0005272181488911275 -0.0035023978133897657; -0.0037524895308138177 0.0002049464774466721 9.024686637834313e-5; -0.00022060775194472892 0.000608931935280876 -0.004248695773969581; -0.0015205402218658242 0.0015892972655498264 0.003281312565512556] %
+
+Mass Used: 84.39016189262611 kg
+Launch C3: 98.25221646014947 km²/s²
+||V∞_in||: 0.012614437296541011 km/s
diff --git a/archive/ES_0.5635960402027596 b/archive/ES_0.5635960402027596
new file mode 100644
index 0000000..b905797
--- /dev/null
+++ b/archive/ES_0.5635960402027596
@@ -0,0 +1,22 @@
+archive/ES_0.5635960402027596---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T18:11:26.735
+Launch V∞: [6.3205017144492155, -7.544602868864145, -0.015184946506301682] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.710962046268654e-6, 1.0142062314686932e-6, -1.8292139163975974e-8] km/s
+ V∞_out: [-1.3162670095732936e-6, 2.936950507370392e-8, 6.6115450687434795e-6] km/s
+ time of flight: 1.8749577784182197e8 seconds
+ arrival date: 2029-04-11T20:21:03.735
+ thrust profile: [0.2718145854305888 -0.07815274855378039 -0.10169951766094308; 0.14743871035420567 0.03001758515195895 -0.1709717191608909; 0.08955771155961575 0.037281388928682706 -0.17781729512031474; 0.02704424462884835 0.015464708440558647 -0.07784121492896856; 0.03339732271955743 0.022181930447154354 -0.12038943974913656; 0.02030175439796562 0.015267071573847376 -0.09029951070178525; 0.01598648612225156 0.01291677265027695 -0.0829192790939921; 0.007634132595533359 0.006766479224272016 -0.04696950340248128; 0.00465485297193016 0.004306363770093316 -0.031717067101362906; 0.0006704502366824108 0.0014157917382021231 -0.0071142188379771905; 0.0012041401225341335 0.00185886814438213 -0.007104243906218303; 0.00047502372717693123 -0.0007368232002266659 -0.0038562883627019013; -0.00028609983962493636 0.0002503934742294305 -0.0018581652369718316; 0.0007760241166745157 -0.0002914842563711145 -0.002616380326007501; 0.0017074187929871048 0.00048788103085586193 0.0013158238096139636; -0.0004046252538790774 -0.000345892893777794 0.0004713704857901721; 0.002024241165820486 0.0015800322620836845 -0.00044357059863659896; 0.0006546462154680909 -0.001417695821450017 -0.00042594553217524663; -0.0011800215969209162 -6.0650845060018215e-5 0.004655620714128232; -0.0004085344708256971 -0.00015419691777638058 0.0017813795752878495] %
+
+Mass Used: 92.45368467255048 kg
+Launch C3: 96.87000495382897 km²/s²
+||V∞_in||: 6.787190911471658e-6 km/s
diff --git a/archive/ES_0.5636043118119299 b/archive/ES_0.5636043118119299
new file mode 100644
index 0000000..6f07048
--- /dev/null
+++ b/archive/ES_0.5636043118119299
@@ -0,0 +1,22 @@
+archive/ES_0.5636043118119299---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T19:17:28.715
+Launch V∞: [6.629853780396786, -7.280805959693073, 0.23725895912415607] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.1262705259576504e-8, 4.866957996172952e-8, 3.252146437034533e-8] km/s
+ V∞_out: [-1.5851460781258303e-8, 3.565257641961333e-8, -5.4349244531157114e-8] km/s
+ time of flight: 1.874957778748358e8 seconds
+ arrival date: 2029-04-06T21:27:05.715
+ thrust profile: [0.24333149640811563 -0.045158860818874054 -0.07680633562172436; 0.10682659297344334 0.04209694984746059 -0.10333840230708638; 0.0879351095524707 0.0639186862175941 -0.14775480703608895; 0.06970144812590943 0.0687113232788422 -0.1650444719771385; 0.048338974886932486 0.05947033837779902 -0.1522648002020155; 0.01785758245871595 0.02427604632548109 -0.06780142368494912; 0.010311310330828355 0.015393827441475562 -0.045002079361077356; 0.009102552054580808 0.01604282144148488 -0.04779426149961307; 0.006886748394867064 0.014284477538201727 -0.05046684345004358; 0.002661833817470923 0.006276941570340247 -0.016687976995676458; 0.00053088500562886 0.0015322668655884946 -0.00468322364856187; 0.0003266087823351235 0.0008801418135883236 -0.002509997422450107; -0.00015392935913189243 0.00036188465254342054 5.197941896849072e-5; -0.0006498215806359415 -0.00011140600635009182 -0.0019898593632436063; 0.00026671903695138505 -0.0005656913868453263 -0.0006519633286486328; 0.0010394175752206974 -0.002405881367591113 0.00014688178079435774; 0.0006913075635376964 0.0021600958733911774 -1.1329843627204579e-5; -0.002953506557257422 -0.0008428580306637243 0.00034132502776952004; -0.001382058593791638 0.001380420976623348 -0.0006922945201105498; 9.22746586214485e-5 -0.0006335307000884304 -0.0009487469184949394] %
+
+Mass Used: 91.58026486325252 kg
+Launch C3: 97.02138838582842 km²/s²
+||V∞_in||: 6.636060878706566e-8 km/s
diff --git a/archive/ES_0.5636056273700931 b/archive/ES_0.5636056273700931
new file mode 100644
index 0000000..ca7e3b6
--- /dev/null
+++ b/archive/ES_0.5636056273700931
@@ -0,0 +1,22 @@
+archive/ES_0.5636056273700931---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T20:06:43.454
+Launch V∞: [6.453547275568544, -7.346386581345672, 0.11301027098891846] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.300743107203265e-6, -8.430149753908604e-7, 1.7914899167228206e-8] km/s
+ V∞_out: [1.1934440352451655e-6, -2.2484004997138507e-8, -6.236746701197873e-6] km/s
+ time of flight: 1.874957778888096e8 seconds
+ arrival date: 2029-04-07T22:16:20.454
+ thrust profile: [0.3465638841331272 -0.07236409132912096 -0.10221445582689397; 0.10175559117383727 0.034544791408770585 -0.09125363533834732; 0.07191981751154453 0.046519957516254686 -0.10857927123501457; 0.05287919064698635 0.04542204402472988 -0.11068074137257772; 0.04719192813807312 0.05146951496614416 -0.13036812570786396; 0.041409554881399545 0.052604727789827145 -0.13948454217084924; 0.031235877092967285 0.044906454238562175 -0.127125488719595; 0.003740767826464956 0.006586906282809478 -0.02032885322049087; 0.0031425849681181034 0.006065249010514714 -0.014693287972710769; 0.006954127332697871 0.006582434725530515 -0.02343214724240541; 0.0006491139819181233 0.0009781296225387242 -0.0038987199883353287; 0.0045404082609073575 -0.0001546816946385223 -0.006386936585592585; 0.0022316043844400075 0.003580007824759644 -0.012931833568075935; 0.002486027451535818 0.0017918538246626005 -0.004167006413654364; 0.0017636887936044099 0.002065313522902692 -0.004024185436483218; 0.0016086394147960814 -0.0018108352061049198 -0.00011974606603433859; 0.0011767020879056983 -0.0027761543233306646 -0.00020614158074723363; -0.003041873266722931 -0.0033407971913961693 -0.004747812080959672; 0.0002989746252525993 0.0007814229870063754 -0.00012970951855894013; 0.0024633283067634093 0.0026570665875823357 0.002053838784005769] %
+
+Mass Used: 99.69566782055836 kg
+Launch C3: 95.63043956192291 km²/s²
+||V∞_in||: 6.356914258924285e-6 km/s
diff --git a/archive/ES_0.5636090755148206 b/archive/ES_0.5636090755148206
new file mode 100644
index 0000000..755cb88
--- /dev/null
+++ b/archive/ES_0.5636090755148206
@@ -0,0 +1,22 @@
+archive/ES_0.5636090755148206---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T22:13:33.202
+Launch V∞: [6.435917811380872, -7.532254621426514, 0.24271099679905658] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.089843024834701e-9, 6.204881898358832e-10, -5.584590492322443e-9] km/s
+ V∞_out: [-1.84712515849543e-9, 4.288409957798532e-9, 5.499432634544527e-9] km/s
+ time of flight: 1.7843319947438204e8 seconds
+ arrival date: 2028-12-23T03:00:12.202
+ thrust profile: [0.17841889417140125 -0.05989719876639507 -0.06851946638891976; 0.0837663684165128 0.014554016787650758 -0.09465143643248286; 0.05841557314976169 0.022982312281418 -0.10910060178938505; 0.046540434637360725 0.024802910452475214 -0.11997154530979462; 0.05007998902933093 0.03287005858763902 -0.1662197761381205; 0.03914230428944557 0.029249981186572887 -0.15698377431892116; 0.026137458503708237 0.021006159901242678 -0.11863681371076684; 0.010465754474283618 0.009019568847545078 -0.054846331343671055; 0.007259463814777735 0.006628568054423202 -0.042627196562093586; 0.003615975981213427 0.0033377869254629247 -0.023015788039792297; 0.0009049552225333092 0.0006810181440409317 -0.0056395056258056325; 0.0001208505452498348 0.00019945412721084153 -0.003603006907188909; -9.80992458284275e-5 -0.00035851772097205586 -0.0005022750465747577; -8.058790141695721e-5 0.00016026228315965885 -0.0006144179661585643; 0.0005896496368251003 -5.129312115759437e-5 -0.0015405161706989886; -4.515343198165134e-5 0.0007211703773331823 -0.0004896947497142379; 0.0001393358426757358 5.3296376090592574e-5 -0.0005492345318784275; -0.001892803597648067 -0.0004529157435851031 -0.0003918113761635477; 0.00021015854983661946 0.0018891774956680755 -0.0002067231460310201; -0.0005054008916884466 0.000560170174227736 0.00010379697752989749] %
+
+Mass Used: 84.62421752252021 kg
+Launch C3: 98.2148063848178 km²/s²
+||V∞_in||: 6.949782192878644e-9 km/s
diff --git a/archive/ES_0.5636105182139806 b/archive/ES_0.5636105182139806
new file mode 100644
index 0000000..8c054c4
--- /dev/null
+++ b/archive/ES_0.5636105182139806
@@ -0,0 +1,22 @@
+archive/ES_0.5636105182139806---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T11:38:07.807
+Launch V∞: [6.458738993768261, -7.354478085982469, 0.1680584032475697] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.228742274279864e-7, -9.178948425718886e-8, 1.4185773864549573e-7] km/s
+ V∞_out: [-4.4839836768619105e-7, 4.0938020314327493e-8, -5.5792380897402036e-8] km/s
+ time of flight: 1.874957778747071e8 seconds
+ arrival date: 2029-04-08T13:47:44.807
+ thrust profile: [0.34425525172038013 -0.07862335150288217 -0.10991182739306338; 0.10877162172115297 0.03406198964110064 -0.10428781484988862; 0.06975293760081558 0.041315816911552346 -0.11362776959478232; 0.044403630881556244 0.03605170795173328 -0.10406784872296837; 0.040078767018763846 0.038983195138367586 -0.11859063345672766; 0.02243531197661441 0.027812013761004322 -0.08726149817388172; 0.02345206025102789 0.03072734297099396 -0.10341808351128608; 0.009877072455451937 0.015650815151858684 -0.05155545300636301; 0.012112630401996383 0.0171023054817991 -0.06177849896849548; 0.004323476873426567 0.0061425079716112795 -0.0260466219859087; 0.0013631310499641175 0.002902790806676016 -0.011016499177455534; 0.0010474691601828397 0.0023627075165056446 -0.0073542270053934804; 0.0013969797623521781 0.0021835857159860535 -0.009367265710912728; 0.0003449803361013401 0.0012763401752555268 -0.004236807633273909; -0.00037913764677961 -0.0031849067064549747 -0.0020684563593892516; 0.0005535144537496343 -0.0004885446278987157 0.0018126393605996855; -0.0026584755790698225 0.005010919156917752 -0.0015021576907919575; -0.0011921313247559777 0.0013015193771853686 0.0027897367135365204; -0.0005841438593527603 0.000560217842010359 0.002286141017602135; -0.00034542722161083037 0.0021915470000996584 0.002444894507004817] %
+
+Mass Used: 98.52618246960401 kg
+Launch C3: 95.83190093372114 km²/s²
+||V∞_in||: 4.5538065358184777e-7 km/s
diff --git a/archive/ES_0.5636109577420454 b/archive/ES_0.5636109577420454
new file mode 100644
index 0000000..b3cb123
--- /dev/null
+++ b/archive/ES_0.5636109577420454
@@ -0,0 +1,22 @@
+archive/ES_0.5636109577420454---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T13:38:21.310
+Launch V∞: [6.5234140760548955, -7.354658562614577, 0.11911836353344842] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001462061746028822, 0.0012821337370055833, 0.0015536488427064577] km/s
+ V∞_out: [-0.0016965217854509045, -0.0008510423465318834, 0.0016097752357735302] km/s
+ time of flight: 1.870191516125545e8 seconds
+ arrival date: 2029-04-03T03:24:12.310
+ thrust profile: [0.30160225131237534 -0.07152600552396596 -0.09665705466397757; 0.06556511478914329 0.019128505273341603 -0.06547274593044786; 0.0786949830419665 0.04440346567851447 -0.12876534392054945; 0.04769226485248683 0.036480868122346854 -0.1135447091110407; 0.03735025394729055 0.03419564194711821 -0.11320517155738621; 0.03288277126656956 0.03743770098314924 -0.12599367630251893; 0.016174594138169608 0.02113926065755688 -0.08082456542875635; 0.010557844482202107 0.01522343082356889 -0.06037160151021199; 0.0034504622714767396 0.0056104452722468365 -0.01872858077320047; 0.011995305208913133 0.014403552079929827 -0.06094470429760739; 0.00032904876715057177 0.00360786579918463 -0.014073320342670859; 0.0009767647337739526 0.002882088623410463 -0.008059424979574951; 0.0014145803434764148 0.0016281066124577484 -0.007318533978697787; 0.000405522855365222 0.0017153570971134464 -0.007080451600888833; -0.001344960853006333 -0.0011729710471256227 0.00027877408510816604; -0.0010989420453721558 -0.0013413732729287374 -1.4820383476211313e-5; 0.00056425137464012 -0.0016024261832388422 -0.003642844786958549; 0.001134571812585598 -0.0008146956336653704 -0.004803524501311485; -0.003430707334079109 0.004235596585053111 -0.006714922889736107; -0.0012919438765429344 -0.002004770085903825 -0.0006700732619224626] %
+
+Mass Used: 93.69540007080832 kg
+Launch C3: 96.66012296484195 km²/s²
+||V∞_in||: 0.002489039211264432 km/s
diff --git a/archive/ES_0.5636121336155061 b/archive/ES_0.5636121336155061
new file mode 100644
index 0000000..f857e9b
--- /dev/null
+++ b/archive/ES_0.5636121336155061
@@ -0,0 +1,22 @@
+archive/ES_0.5636121336155061---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:45:03.061
+Launch V∞: [7.9371020476338305, -5.78233431598595, 0.5784494090968283] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0261128164520907e-9, -5.523176462518122e-13, -1.5996677279192803e-9] km/s
+ V∞_out: [5.699838812887677e-10, 1.2324933218509267e-9, 2.881576465862965e-11] km/s
+ time of flight: 1.827538967901147e8 seconds
+ arrival date: 2030-02-25T09:43:19.061
+ thrust profile: [0.2934204284048073 -0.014941713227946324 -0.07102562403954218; 0.08982528864059865 0.058164477266621675 -0.09915727202210828; 0.07231884550989548 0.05902180428772035 -0.10896913486706032; 0.04120650595813785 0.048756007889198955 -0.0881337335712205; 0.017138469275515794 0.03696614118533779 -0.09005272996283416; 0.030634672718547716 0.056356756452363245 -0.1448982425599641; 0.0064550045031255675 0.018422170550323677 -0.057806327496327754; 0.006973052994112154 0.019502063422928782 -0.047747915134167256; 0.002290093558530878 0.013006741759222566 -0.045322806122767345; 0.00219280961439441 0.011365824459172405 -0.041380326989492296; 0.0005887945753570085 0.008329425006854865 -0.030151555080670467; -0.00259946523360037 -0.004183971338125161 -0.004876911302436944; -0.005493483784514856 0.008429021869898868 0.001725397519526827; 0.0001694580076743672 -0.0030397334432906075 0.0037141848369209567; -0.0006365099114538817 -0.0015634330500253362 -0.006942382144841237; 4.429585132005088e-5 -0.0006491051146691443 0.0016094808441405252; 0.01533027410562601 0.0031403675939871375 -0.0021854436540223693; -0.004921018975362543 0.012692350027320184 0.010602233034295677; 0.0002445848145913724 -0.0008841886025479429 0.003031951264879913; -0.001422359428097329 -0.014107994688816627 -0.013546460038075026] %
+
+Mass Used: 93.069923029037 kg
+Launch C3: 96.76758277526632 km²/s²
+||V∞_in||: 1.9004853740264503e-9 km/s
diff --git a/archive/ES_0.5636126479627316 b/archive/ES_0.5636126479627316
new file mode 100644
index 0000000..0d70f12
--- /dev/null
+++ b/archive/ES_0.5636126479627316
@@ -0,0 +1,22 @@
+archive/ES_0.5636126479627316---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T22:24:35.196
+Launch V∞: [6.47311045885029, -7.3115847089777, -0.07912623613440288] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003633791574501332, 5.586767965962057e-5, -0.002529765836847304] km/s
+ V∞_out: [0.00424879702187319, -4.3181542142728766e-5, -0.0012331716490770275] km/s
+ time of flight: 1.8749577787473822e8 seconds
+ arrival date: 2029-04-08T00:34:12.196
+ thrust profile: [0.3990104566764262 -0.09055069933319124 -0.12633410318482466; 0.0863549061328134 0.028814084746665306 -0.08658853704841314; 0.06399613175362072 0.040145658188024416 -0.10771311539713223; 0.05555523527023659 0.04761795734111374 -0.13187162728260876; 0.034567681223384626 0.03652086117726857 -0.10788260246772023; 0.020520819349383816 0.02505633932117619 -0.07899492397368797; 0.01580452288872855 0.021557698463643176 -0.07187811184790759; 0.012876916518657406 0.02000841771645085 -0.06791964967560024; 0.014010310387639216 0.02372390918796778 -0.08310382803760946; 0.008601283439621753 0.015845368218717074 -0.05966853740805268; 0.00024309901939834728 0.0006159950653078885 -0.0024487169027524263; 0.00013437834020559812 0.0002454724471147909 -0.000235821297038263; -0.00027744130011132686 0.00034162680620909686 -0.00020099072343518964; -0.00020563359282147056 0.0010634907627264897 -9.42198331734471e-5; -5.928622632901475e-5 -0.0007090062026601075 -0.0014701303046094863; 0.0006127893855750633 -0.000711531204201266 -0.0008443774636552267; -0.0003930246744752006 -0.001324636477281837 0.0015035873571236625; -0.00020455484462856974 0.0014199568895168226 -0.00014848141118048192; 0.0009739079299543119 0.0017403271585384218 -0.0037534185472866983; -0.0013131126092086175 -0.0009127181715326452 0.0007947572173861027] %
+
+Mass Used: 101.24239219656329 kg
+Launch C3: 95.36669093027832 km²/s²
+||V∞_in||: 0.0044280105683960555 km/s
diff --git a/archive/ES_0.563613698758569 b/archive/ES_0.563613698758569
new file mode 100644
index 0000000..6eb8dfe
--- /dev/null
+++ b/archive/ES_0.563613698758569
@@ -0,0 +1,22 @@
+archive/ES_0.563613698758569---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T02:49:11.825
+Launch V∞: [8.039835421094228, -5.4644231675094055, 0.29382735038933894] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.15927623219368e-6, -0.00018364848153712722, -3.3377270601389843e-6] km/s
+ V∞_out: [-0.00017716064228556977, 2.5820744753996524e-5, -4.155596013007106e-5] km/s
+ time of flight: 1.8749577787490922e8 seconds
+ arrival date: 2030-04-20T04:58:48.825
+ thrust profile: [0.5109213869038249 0.0018495109218014114 -0.14348110381783294; 0.07033203675516049 0.04257108517535527 -0.06749996510946199; 0.0716518337101126 0.07105899382810088 -0.1263897362284123; 0.04088617225422712 0.054204077812765886 -0.1077302685922236; 0.02188091061256843 0.03665973610871716 -0.07956430827584032; 0.0326863930541137 0.06521311589718445 -0.15454291053309627; 0.002554165521800443 0.005151758088503556 -0.013036548787420615; 0.002078831245499748 0.004921811247293952 -0.012984926902717466; 0.005420047787200547 0.004563968239482904 -0.00856284211625488; 0.002705157090288229 0.011957731467778924 -0.03384297308335119; 0.0012970484633825642 -0.007095571848657272 -0.03153966615443235; -0.0011070074595315583 0.0003949553960990702 -0.006832047192435085; -0.002037664952694926 0.004267450027327249 -0.007042086074696934; -0.0009042361900113626 0.01490357997448938 -0.03951129894427152; 0.001354772170393857 0.002309233059132945 -0.0069500020933945675; 0.0037753900867603433 0.010173027233968786 -0.0067536588954800695; 0.0008126235801465113 0.0025267787475085346 -0.0022794109342090907; 0.008292357093307917 0.005886668679874729 0.004042620920241406; -0.003301266922805755 -0.0040359762060728395 0.003978790465807035; 0.020242432912578396 -0.0019842956045593523 0.011115062715959412] %
+
+Mass Used: 105.80226467989542 kg
+Launch C3: 94.58520866373175 km²/s²
+||V∞_in||: 0.00018385994392867028 km/s
diff --git a/archive/ES_0.5636216062630423 b/archive/ES_0.5636216062630423
new file mode 100644
index 0000000..f78611b
--- /dev/null
+++ b/archive/ES_0.5636216062630423
@@ -0,0 +1,22 @@
+archive/ES_0.5636216062630423---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:54:48.789
+Launch V∞: [7.601555803762525, -5.97412536982838, -0.3021723665700688] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008387361069845127, -0.0005801770615047801, -0.03494749156712051] km/s
+ V∞_out: [0.03229425776888632, 0.012967338180890456, -0.0033809247648148395] km/s
+ time of flight: 1.8749577782977203e8 seconds
+ arrival date: 2030-04-22T02:04:25.789
+ thrust profile: [0.3505001540565666 0.03502349604336641 -0.0793588721338927; 0.2526989115232967 0.20383076293372357 -0.1763838283744803; 0.08502372492491916 0.10524892240314436 -0.12864699388132528; 0.05384783883858078 0.09673131611667372 -0.12888460986409245; 0.03193821144553839 0.07716655787528114 -0.11260443592081897; 0.016044587016193636 0.04897448752442069 -0.08044421479256855; 0.009411231765419205 0.036675409778497314 -0.06498876031126286; 0.0006704173013212353 0.004152723719432057 -0.008375361911940032; 0.003054444036460487 0.02059579150181207 -0.03983224086171102; 0.0004678820933404496 0.005435537220025334 -0.011246310561573018; -0.000430744768118067 0.00080083300324162 -0.0013990586909334224; -0.000205753588749627 -0.0001441046814336218 0.0009968917055335426; 0.0013394842897911682 -0.0015032766910626338 0.00018828424176286834; -0.00017061089916843155 -0.0004762067500083475 0.0017451359344594374; 0.001432128042382042 0.001001380559017982 0.0022648652657246133; -0.00015774757615651008 -0.0038500743898052556 0.0021712615180224763; 0.004884528037306018 0.004921155336698447 0.0020926402032904255; 0.0006071357363713176 -0.004925017776923818 0.0021761937802408293; 7.160669263425206e-5 -0.0026157270097669117 0.004004002587607135; -5.946960205844442e-6 -0.00028679275051724266 0.00072467422479789] %
+
+Mass Used: 111.76193315785804 kg
+Launch C3: 93.56513271126136 km²/s²
+||V∞_in||: 0.03496236906323447 km/s
diff --git a/archive/ES_0.563626594056883 b/archive/ES_0.563626594056883
new file mode 100644
index 0000000..2fc2426
--- /dev/null
+++ b/archive/ES_0.563626594056883
@@ -0,0 +1,22 @@
+archive/ES_0.563626594056883---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T16:32:36.367
+Launch V∞: [6.5272233831760875, -7.309044978997079, 0.12766469359637972] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5423134455423384e-6, 4.2309573913575516e-7, -9.910468916439528e-9] km/s
+ V∞_out: [-6.012599524608977e-7, 1.1391015488087758e-8, 2.5452329855571337e-6] km/s
+ time of flight: 1.8749577791090667e8 seconds
+ arrival date: 2029-04-07T18:42:13.367
+ thrust profile: [0.28048509904584484 -0.06693924866539269 -0.09455353675102185; 0.16357576074873573 0.050563171476326316 -0.16515165474841612; 0.10032353653909536 0.05858710911755785 -0.17277498086951018; 0.05816220304804018 0.04595650846314187 -0.14295238293630752; 0.03447404532274765 0.03322386503281201 -0.11095650374523833; 0.026306523153459237 0.030012351866908336 -0.10785441198256206; 0.01078731756814004 0.014195527949658731 -0.05471738485738606; 0.005797991045146424 0.008349943107217655 -0.034331192868773064; 0.0027387250760119897 0.004493201604497355 -0.01980939703911699; 0.0013508466044395602 0.0029926176388925365 -0.014581174032170846; 0.0006458135877212084 -0.0003066205926539284 0.0017378267443228061; -0.0005052008077101974 -0.00010080743052359742 0.0010210837532662201; -0.00023620099882157438 -0.0004647828133885364 0.0008305279136563547; -0.0005396680960579514 -0.0002257974254659806 0.0017186847365271976; -0.0011141117876771163 -0.00183435061489686 0.003535196276053762; -0.0010636717201721127 -0.0012465423643970392 0.005327225315641162; 0.000980182994779389 0.00042463933530564033 -0.0006564879408529036; 0.00024074925819390165 0.0009512165072159645 -0.0013263454265565401; 0.001042811423328174 -0.000520015398154044 -0.00034825052189524255; 0.00826590068888669 -0.0004481495568044586 0.002169014819454884] %
+
+Mass Used: 97.31304880793095 kg
+Launch C3: 96.04308187287415 km²/s²
+||V∞_in||: 2.577298173912815e-6 km/s
diff --git a/archive/ES_0.5636312100767568 b/archive/ES_0.5636312100767568
new file mode 100644
index 0000000..3361b1f
--- /dev/null
+++ b/archive/ES_0.5636312100767568
@@ -0,0 +1,22 @@
+archive/ES_0.5636312100767568---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T06:19:38.092
+Launch V∞: [7.523152010033041, -6.3053748340019595, 0.10717666218201019] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002676145685809217, 0.0002055018998635427, -0.0001332105441362544] km/s
+ V∞_out: [6.005230019911561e-5, 0.00035746281652874383, -1.5373133245814007e-5] km/s
+ time of flight: 1.678718769223962e8 seconds
+ arrival date: 2029-09-04T05:24:14.092
+ thrust profile: [0.3228922990305293 -0.041773339288071344 -0.1051235307344153; 0.08836328527727945 0.03644101082651668 -0.09317785851141923; 0.03025251888290046 0.02097918249204667 -0.05581794303884754; 0.10605570191818224 0.09620533641031478 -0.2548694458133388; 0.043614760795374435 0.04840010300469419 -0.14434424065569315; 0.028221755682786176 0.036043604027563424 -0.11602654438498303; 0.011582850296754349 0.01614157048625844 -0.05796957235607702; 0.023203023337814217 0.036121394139920646 -0.12378778427716894; 0.004348947261333676 0.00680910758634628 -0.02851489872545391; 0.0046881016757088865 0.007711250747309328 -0.03190828226436282; 0.0008657589791579831 0.0006658514253375415 -0.011041244449450486; 0.0010258930802055375 0.0023734637757025214 -0.009750682051516276; -0.0011016521527195317 -0.00036077566386250254 -0.00032108517698181465; 0.00016930370097485467 0.00017458169103985434 -0.0037291258684089834; 0.0011706587802077276 0.0013424588869453819 -0.004304308857184974; -0.004169169590136156 0.0009883435127040299 0.0015474228773842825; -0.004018775365446498 -0.0023003977532263732 0.003849195606764296; 0.0013368545755839162 0.0002463372308316974 -0.002910849709012213; -0.0016083037524200262 -0.0038332315886586803 -0.0019444832417354924; 8.26830908662917e-5 0.002184751340315308 0.004972742887010034] %
+
+Mass Used: 95.42859208811524 kg
+Launch C3: 96.36705480024588 km²/s²
+||V∞_in||: 0.00036275837307132603 km/s
diff --git a/archive/ES_0.5636335693998182 b/archive/ES_0.5636335693998182
new file mode 100644
index 0000000..298785b
--- /dev/null
+++ b/archive/ES_0.5636335693998182
@@ -0,0 +1,22 @@
+archive/ES_0.5636335693998182---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T21:19:21.963
+Launch V∞: [6.492416493906001, -7.583410534606794, 0.20830005163230655] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.521709127231457e-10, -3.350308001830356e-9, -6.903599332730175e-9] km/s
+ V∞_out: [1.9790942557670335e-9, 2.7932526796162457e-9, 1.3379412403691392e-9] km/s
+ time of flight: 1.8749577787429518e8 seconds
+ arrival date: 2029-04-12T23:28:58.963
+ thrust profile: [0.12367243128793202 -0.03538591744178315 -0.04921388117572069; 0.04076293032179644 0.007410378470415984 -0.051107459867532415; 0.057591952946110817 0.020866122018675944 -0.11715306935635895; 0.05488155973655695 0.025751329452866848 -0.1545271747789774; 0.05129350338066104 0.02772060187551933 -0.18267369675404382; 0.029012092778153305 0.017377279714063377 -0.12574908442557967; 0.012783871214101218 0.008319655879810922 -0.06664328073861628; 0.006546920723250601 0.005127852892314741 -0.04403067130856801; 0.005658798382318911 0.004096608570253671 -0.038218817391983864; 0.0018535659012984436 0.00166484023351391 -0.012665053321878122; -0.0004609702489093096 -0.0010273805158104044 -0.0038086828707707384; 0.0015946636953346562 -0.00047165713789154616 -0.0031424207206187512; 0.0016874125243411665 0.001001398319655553 -0.0019011452032423374; 0.0011740030001417523 -0.0014732553446602146 -0.0009074596318275965; -0.0012208671872274376 0.0010280081167572171 0.0022791608578748893; 0.0008485532847198159 -0.0005395200880646445 0.0011656324275712625; -0.0011614160743310471 0.002499668582827649 -0.0022858888159800307; 3.6393292288621e-5 0.0011294625694836776 -0.0012819903205945375; 0.0038169131583032116 -0.0023176141603858777 -0.000585459554731592; -0.002184888948728739 -0.0010416260513712071 0.0006207217041412173] %
+
+Mass Used: 75.97180326006628 kg
+Launch C3: 99.702976178238 km²/s²
+||V∞_in||: 7.732456071717256e-9 km/s
diff --git a/archive/ES_0.5636370725520096 b/archive/ES_0.5636370725520096
new file mode 100644
index 0000000..cd803db
--- /dev/null
+++ b/archive/ES_0.5636370725520096
@@ -0,0 +1,22 @@
+archive/ES_0.5636370725520096---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T00:10:36.335
+Launch V∞: [7.393513406398529, -6.33675274685358, -0.1227293351026166] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00013210899132234277, 8.472317136675939e-5, -3.928991250920451e-5] km/s
+ V∞_out: [-6.347756408609691e-5, -0.00012248977610117162, 8.431199578433399e-5] km/s
+ time of flight: 1.6508451346736673e8 seconds
+ arrival date: 2029-08-01T16:59:09.335
+ thrust profile: [0.42727497130678804 -0.0646066515497641 -0.14859200182160462; 0.12266961703536504 0.04496039900716025 -0.1304235161535198; 0.10957447708132015 0.07092769003209319 -0.19733169116466923; 0.07686653690114809 0.06557964196414597 -0.19750776739504766; 0.045413829138339946 0.046147882433919166 -0.15278934184856977; 0.03218256060713766 0.03724775558859943 -0.13239523587403237; 0.02006679707226216 0.02629507149471743 -0.10024386193062482; 0.0027818540283433306 0.0027118204586705705 -0.012884680129935598; 0.003560169026520224 0.005304165160316211 -0.02339463667258427; 0.0009176582867708783 0.0015378007378582075 -0.007445115440326759; -0.0005046464522043355 -0.0005206288845001231 -0.001333946091017826; -9.975718557042735e-5 0.0009307178693593247 -0.0004694832964208576; 0.001751203360669837 0.0004191708261852363 0.00164097999772318; -8.469172909270279e-5 0.0004183786931117397 -0.0013732725942034586; -0.0032025259386787713 -0.0041748763479079395 0.0009036503135550764; 1.1056312675280076e-5 0.0031541116428487528 0.0006821175242797755; -0.00102476016916439 0.00043075060363147985 -0.0006260026668977044; 0.0033661572306360604 0.00029802066369686794 0.00041712009893799147; 0.001382902733987983 0.0009915364820541226 7.763807252320586e-6; -0.0010618835947216253 0.0038717937711942596 -0.007352562500742567] %
+
+Mass Used: 104.38094423957682 kg
+Launch C3: 94.83353835504589 km²/s²
+||V∞_in||: 0.0001617853472340096 km/s
diff --git a/archive/ES_0.5636395472268675 b/archive/ES_0.5636395472268675
new file mode 100644
index 0000000..ba41db2
--- /dev/null
+++ b/archive/ES_0.5636395472268675
@@ -0,0 +1,22 @@
+archive/ES_0.5636395472268675---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T19:38:13.410
+Launch V∞: [7.952318047148558, -5.8560695828158345, 0.15524336968689184] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.608125374651906e-7, -9.579293051132967e-7, -9.3158838846347e-8] km/s
+ V∞_out: [7.995530519917303e-8, -3.9715322981911664e-7, -1.099230675048766e-6] km/s
+ time of flight: 1.8749577791904485e8 seconds
+ arrival date: 2030-04-25T21:47:50.410
+ thrust profile: [0.2947621442782801 -0.004953664446023073 -0.10345523425368693; 0.04531571697286466 0.022890752749606273 -0.05699796263391253; 0.05202596628577848 0.04160151278795934 -0.11488063760096873; 0.04234592342692374 0.043954282029155765 -0.13722957152168888; 0.026088681819202375 0.031306049574781385 -0.11274465369350994; 0.018494097701281683 0.02478410858587295 -0.09995478452064344; 0.015627009569626447 0.023287418093385512 -0.10170028238980039; 0.004188661447009836 0.006526697513221915 -0.03327516654217426; 0.0021980006079621783 0.002311480232687688 -0.013483026170708127; -0.00035628912791590235 0.002553815515684566 -0.009752744841177809; -0.0026502402584165493 0.00222303886235833 -0.0010622642316194851; 0.0016661631228765317 -0.0018813621294266607 0.001315803083694635; -0.0012651258510807033 -0.0038792322564933897 0.0030572951516698813; -0.00011905146460330744 0.003873751515627665 0.0035212226985768345; -0.006486135259092219 0.011507317462907026 -0.004392195538905041; 0.0029477895992106266 -0.003961982566221982 -0.008124112946518; -0.0037984786043034797 -0.001878246993671862 -0.004351030555545728; 0.024098756687072193 0.012794312923112856 0.0021428169806177303; -0.017386070253939886 -0.014217336976146213 -0.012503616679194354; 0.0009593869572341216 -0.021313904608572062 -0.01506247872892239] %
+
+Mass Used: 88.49689134857817 kg
+Launch C3: 97.55701378561723 km²/s²
+||V∞_in||: 1.1674674867083995e-6 km/s
diff --git a/archive/ES_0.5636397499511372 b/archive/ES_0.5636397499511372
new file mode 100644
index 0000000..b618b6a
--- /dev/null
+++ b/archive/ES_0.5636397499511372
@@ -0,0 +1,22 @@
+archive/ES_0.5636397499511372---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T22:34:08.126
+Launch V∞: [7.7699507363942555, -5.77478125828738, 0.09529496473328065] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9228510181504637e-9, -1.7243325496631941e-9, -3.1777655004791474e-9] km/s
+ V∞_out: [-2.1857832766180074e-10, 7.36654678565479e-10, -1.1270692533456993e-10] km/s
+ time of flight: 1.839135527188054e8 seconds
+ arrival date: 2030-03-09T13:40:00.126
+ thrust profile: [0.508029073747424 0.013155024933452825 -0.1013069452694393; 0.09714802318884437 0.06787172604435016 -0.08921540177228499; 0.07841596601951596 0.09119845810829721 -0.1258675808847058; 0.036024426459158015 0.06018705672316912 -0.09375332080389541; 0.020072875731909506 0.041955897882429094 -0.07334623052167315; 0.016257698476635957 0.04336544143583253 -0.08181796528768938; 0.006347398459772604 0.02169106433606752 -0.043733088894504064; 0.016362767387893502 0.07663101347899563 -0.15352052777538777; 0.0034447732503974154 0.014011103168986374 -0.032447943575175255; 0.0010092413855609245 0.026498031389324172 -0.059116051044353336; 0.0014483857177439547 0.0016614522109241177 0.0008527682386764227; 0.0006623298537164352 -0.0026114175009007 0.001270876303573623; -0.001861219485376946 -0.0020523956318962873 0.002712848946256996; -0.0041454184471255906 -0.004723881605233038 -0.0023219399856505884; 0.0004394278976806411 -0.002252699815406402 0.0047969871088205645; 0.0021750198346595045 0.0008163158766041433 0.004783722057280161; 0.0026516628065360367 -0.00023957788733639058 -0.004771326311642143; -0.0025935865492718634 0.0035351884627826615 0.004279135604794662; 0.0008732456112515246 -0.0015167695605229309 0.005326506489872322; -0.004949744666422618 0.007635844300625517 0.00025492492604845365] %
+
+Mass Used: 110.82537569170154 kg
+Launch C3: 93.72931415736431 km²/s²
+||V∞_in||: 4.094981362090154e-9 km/s
diff --git a/archive/ES_0.5636404308148875 b/archive/ES_0.5636404308148875
new file mode 100644
index 0000000..430880a
--- /dev/null
+++ b/archive/ES_0.5636404308148875
@@ -0,0 +1,22 @@
+archive/ES_0.5636404308148875---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T18:14:35.978
+Launch V∞: [6.645008628244228, -7.398070863299833, 0.17389434746382945] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.202950842363792e-7, 3.8430753813750315e-6, -2.0336642339236654e-7] km/s
+ V∞_out: [1.3880933724275856e-6, -3.1495613163320184e-6, 1.7978959450669647e-6] km/s
+ time of flight: 1.874957778737803e8 seconds
+ arrival date: 2029-04-09T20:24:12.978
+ thrust profile: [0.14922283091129415 -0.03443307342020972 -0.05211153583061813; 0.030671240120862652 0.009677699075849894 -0.03271830006641326; 0.0759325541844433 0.042964887035791856 -0.13105149431450433; 0.041155710144941446 0.03192618437030073 -0.1022420844136176; 0.024356125345503042 0.022924386762031942 -0.07844421792074276; 0.016807537539229707 0.018070847160329948 -0.06589179333867064; 0.009487284006794999 0.011152806778163656 -0.042430167722705754; 0.034747857560340906 0.042985120934046085 -0.16013008558713424; 0.008680136657333113 0.012180972217841203 -0.05373456644557245; 0.02154575843975648 0.03577931365236416 -0.1363903296592581; 0.0006890759641722407 0.0026430462759643703 -0.012687229395736112; 0.0005810052872747462 0.0010921276052998738 -0.0068872788214619195; 8.239698556919032e-5 0.0006935019723292913 -0.0010323132955508485; 0.00020717533812947086 -1.387347575327241e-5 -0.0006765532778633291; 0.00017627436978993291 -7.821167221693662e-5 0.00042115236775396026; -0.0007736481233395912 0.0003485220072561254 -0.0005425895612067779; 0.00040254554737451635 -0.00032249462084017424 -2.973164681693678e-5; -0.0014755953170144348 0.0003763393707102077 -0.0017330537143960146; -0.0005646671905654325 -0.00014198753719357236 0.0011449752407652295; 9.252211679969576e-5 -0.0021456128309041474 -0.002576939982773281] %
+
+Mass Used: 80.55981938113337 kg
+Launch C3: 98.91783141192604 km²/s²
+||V∞_in||: 3.8834640804022884e-6 km/s
diff --git a/archive/ES_0.5636429684641224 b/archive/ES_0.5636429684641224
new file mode 100644
index 0000000..173937d
--- /dev/null
+++ b/archive/ES_0.5636429684641224
@@ -0,0 +1,22 @@
+archive/ES_0.5636429684641224---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T07:04:25.586
+Launch V∞: [7.45100242339691, -6.429961696276168, -0.12442756774013314] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006595510848548027, 0.00044183637464521836, -0.0002157968653681734] km/s
+ V∞_out: [-0.00035297501630962455, -0.0006288804175543485, 0.00039571193849382235] km/s
+ time of flight: 1.6440505980300868e8 seconds
+ arrival date: 2029-07-26T03:08:44.586
+ thrust profile: [0.29326591074659286 -0.04717504106302081 -0.10737132677795087; 0.06583097482583053 0.022739380842060262 -0.07517387217862453; 0.09742860659183841 0.06116412892287817 -0.1843776168554945; 0.06792660476913773 0.054126362641421295 -0.18196521983429587; 0.048784448079960206 0.04702703717916826 -0.16868134090357742; 0.03789082724006734 0.0407708221925381 -0.1582943642578358; 0.017464875836596394 0.020335525504829942 -0.08890017974310337; 0.008232531616804432 0.010730377305573583 -0.04952958822106085; 0.0018453659038582665 0.0023483516585865484 -0.012205704550785776; 0.004293207194417788 0.006313260415731923 -0.032553256721171826; 0.0010417796148788937 0.0013228050870789502 -0.007830045583963764; 0.0003549790883981903 0.0006006546053089731 -0.0023187936250278927; 0.0008678206615975648 -0.0005832686490428161 -0.0018262301911401554; -0.00010366159886030651 0.0007062052446513403 -0.001655721191054328; 7.343385564382676e-5 0.00012478329767663166 -0.005201127141092613; 0.00015380872975552864 0.0005837398071358341 -0.0018022978226396667; -0.00216596481463224 0.003903524268955099 -0.0013549675833102503; 0.0002851286274171182 0.0001320755289755276 -0.0009456328956239188; 0.0006198515853453024 -0.0034653882349927195 -0.0032152905066516364; -0.001506726897766127 -0.0004959654336725203 0.003153613800505488] %
+
+Mass Used: 92.46572384096498 kg
+Launch C3: 96.87732674865906 km²/s²
+||V∞_in||: 0.0008226756970978944 km/s
diff --git a/archive/ES_0.5636509289771567 b/archive/ES_0.5636509289771567
new file mode 100644
index 0000000..dc3dfcc
--- /dev/null
+++ b/archive/ES_0.5636509289771567
@@ -0,0 +1,22 @@
+archive/ES_0.5636509289771567---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T11:08:22.510
+Launch V∞: [7.87512358511974, -6.105184800400839, -0.09500130037528862] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6427227031787135e-7, -1.6970434544532567e-6, 4.0212297643750135e-5] km/s
+ V∞_out: [1.419917136050736e-6, -4.027399864382143e-5, 2.8941742124929955e-7] km/s
+ time of flight: 1.854208221812214e8 seconds
+ arrival date: 2030-04-03T12:55:24.510
+ thrust profile: [0.21858592194474807 -0.00796596689368261 -0.07917406104104496; 0.055250250283724454 0.026734162465153602 -0.07372291262088167; 0.02025222163963216 0.016579197488448546 -0.05375364910950596; 0.03790823005496208 0.03748185844544665 -0.12905652253578367; 0.011979421908126694 0.01770838127931374 -0.06409179325935253; 0.013898492921200174 0.020282227956305063 -0.08270910246690549; 0.011134264245527348 0.019060838342524786 -0.08000221905793566; 0.02040565436704794 0.02939320534519003 -0.14747265805652895; 0.004886732771930572 0.008007674242677084 -0.03841861721089138; 0.002829283029141076 0.00504515767132121 -0.03190069151862825; 0.0020635023783036914 0.004805639166292799 -0.03214136491600191; 0.0012132891169227195 -0.0005548195447711618 -0.005368322678971808; 0.0010115764524212542 -0.0020181140519713783 0.0028229856786687905; -0.0026181141245200067 0.0005573206576855992 0.0034052835654234106; -0.0014338167381133164 0.0011060953350701648 0.0023311294612875988; -0.0011495661166903172 0.0014806846396131462 0.003926817818208301; 2.555534188514277e-5 -0.0012298840656827766 0.0024718417712157746; -0.0027586049208828635 0.00416974874312645 -0.0008467868640963507; -0.005731913805401988 0.0010590370408314624 -0.002042058254512035; 0.003812894506514771 -0.0006632067060176041 -0.0034864280384313837] %
+
+Mass Used: 78.34346111902187 kg
+Launch C3: 99.29987817502762 km²/s²
+||V∞_in||: 4.024895872080064e-5 km/s
diff --git a/archive/ES_0.5636536430534779 b/archive/ES_0.5636536430534779
new file mode 100644
index 0000000..ac4aa4c
--- /dev/null
+++ b/archive/ES_0.5636536430534779
@@ -0,0 +1,22 @@
+archive/ES_0.5636536430534779---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T21:27:40.981
+Launch V∞: [6.467290200584627, -7.368212760035047, 0.1303433045925883] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009632434844539926, -0.0002896571864315634, 0.00644153686778358] km/s
+ V∞_out: [-0.011250285032299493, 0.00012093309009098955, 0.0027891185564952146] km/s
+ time of flight: 1.8749577787493753e8 seconds
+ arrival date: 2029-04-08T23:37:17.981
+ thrust profile: [0.34244430514262014 -0.07420578438105394 -0.11085138895970399; 0.09193819152117538 0.029796762346096555 -0.09328541254578869; 0.05478728813158066 0.03365952832771139 -0.09478114912380868; 0.038363870750697845 0.03119273790526535 -0.09299889632924989; 0.03390575607170527 0.03455095064706971 -0.10645459402736109; 0.025441313983554828 0.028934694186986763 -0.09673132648672704; 0.02314894850747663 0.030235277574086807 -0.10453897175624088; 0.0203347445118451 0.02987616029226908 -0.10636062411730669; 0.006263280870281044 0.009626453957653752 -0.03975763724274875; 0.006093081020488631 0.011353582693633178 -0.04732389771158382; 0.002683151945155324 0.0023977213113083114 -0.0038006898183612072; 0.0014438007018356981 -0.0016412833841394424 -0.003044963373987452; 0.000997823164540107 0.0011576984216822657 -0.004007753923410886; 0.0006573691633666929 0.0006417366286679792 -0.0025097771669897635; -0.0013455730958263814 0.0030091897254696924 -0.0022579428951040787; 0.0009395122001331626 -0.000810953031141994 -0.003943045929138115; -0.0003934082340750049 -0.0016456145013222503 0.0036303314144811765; -0.004067899271483655 -0.00010699949727182121 0.0031963940601126345; 0.0026837359499527836 0.0007565654767919844 -0.00047255898225036924; 0.0027574462998268888 0.0023219770231489587 -0.0015860828917680769] %
+
+Mass Used: 96.81780160454628 kg
+Launch C3: 96.13339119277336 km²/s²
+||V∞_in||: 0.011591423533758633 km/s
diff --git a/archive/ES_0.5636547318138416 b/archive/ES_0.5636547318138416
new file mode 100644
index 0000000..be3be54
--- /dev/null
+++ b/archive/ES_0.5636547318138416
@@ -0,0 +1,22 @@
+archive/ES_0.5636547318138416---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T19:55:36.082
+Launch V∞: [6.525174726283663, -7.363380795773494, 0.25417725354213183] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.873239134225585e-8, 6.053361169847948e-8, 3.348451364243676e-8] km/s
+ V∞_out: [-1.8837874431228397e-8, 3.860007799675279e-8, -6.201381570196554e-8] km/s
+ time of flight: 1.8389309343408552e8 seconds
+ arrival date: 2029-02-23T05:20:29.082
+ thrust profile: [0.22157577782097912 -0.05440254918487352 -0.06883067531383733; 0.14539387874096293 0.04608357129883673 -0.13200005908044354; 0.09558624048081306 0.05828000782435531 -0.14559663474278767; 0.07600437162942121 0.063471754764354 -0.16281597895721947; 0.05324531541111606 0.05505221420053832 -0.14930623242359453; 0.02487767265999587 0.035559862966206335 -0.10222460687097223; 0.0161270773517461 0.02657114261235965 -0.0816091512401934; 0.0064510906825551865 0.010988566665094712 -0.03805083631267255; 0.0025450904169699636 0.0038778997585429235 -0.01416593835331254; 0.0020068091287406523 0.003604327419453101 -0.013453324220642783; 0.001007369647851553 0.002061989704275879 -0.007577998959197408; 1.9685509112659222e-5 -0.00010276217476251455 0.00013075012464972154; 0.0004645665357584794 -0.00030232327268478096 0.0001496160000529271; -3.881228682176855e-5 2.1297138913942343e-5 0.0008209796202330877; -0.00023905191345980617 -0.00019536601600101566 0.00029729374533880913; 0.0004204972051081234 6.575326743468542e-6 0.00014973615554538894; -9.658714002300787e-6 -0.00031665168063214704 0.0008512699538504643; -1.706387247020445e-5 -0.0004825362729175762 0.0012301132118783939; -4.0558105154486423e-5 -0.00022591950234305543 -0.0005018581207751444; -0.0004758278361299518 -0.0005136473159531462 0.0013358376171689235] %
+
+Mass Used: 92.56950695097657 kg
+Launch C3: 96.86188802831519 km²/s²
+||V∞_in||: 7.49071499349519e-8 km/s
diff --git a/archive/ES_0.5636577073867626 b/archive/ES_0.5636577073867626
new file mode 100644
index 0000000..3a4417f
--- /dev/null
+++ b/archive/ES_0.5636577073867626
@@ -0,0 +1,22 @@
+archive/ES_0.5636577073867626---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T13:07:54.644
+Launch V∞: [6.256254195880828, -7.5308350042101155, 0.03193671108418214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008839918834049312, 0.0010674224517410878, 0.0009189359044361289] km/s
+ V∞_out: [-0.0010148385109422027, -0.0005521767263193876, 0.0011962618380835569] km/s
+ time of flight: 1.8336657393776378e8 seconds
+ arrival date: 2029-02-20T20:17:27.644
+ thrust profile: [0.39781574634522665 -0.12018562904267119 -0.14482719030792096; 0.05200562021046712 0.011300348984614034 -0.05865091203221397; 0.05142015097413917 0.024123075767958215 -0.0964344029332907; 0.050554371762499925 0.03110334146924994 -0.12782505115202467; 0.03348745432235624 0.025193602818052357 -0.10973892397219895; 0.048627930749480325 0.03542954854056482 -0.17978816151644345; 0.010929771185667918 0.010165435869267108 -0.05361574652101792; 0.005401210070626202 0.005662205573773759 -0.03037479164831087; 0.0032838597282278535 0.003646692199328392 -0.02111471975626053; 0.01609174789204918 0.020474971736768006 -0.09748173694840735; 0.006826777607339092 0.0072155152401337545 -0.046714863822872654; 6.787010606402072e-5 0.0004656080476560213 -0.0017846710086704375; -0.0003211798242172093 0.0003127216222015508 -7.503168241763773e-5; 2.6445407607465082e-5 -0.00016908705743284472 -0.0004259105532149912; -0.00027298122357517036 -0.00010099641864212374 -0.000818002680359184; -2.8932400700289166e-5 0.000627085928740978 -0.0009414705155403177; -8.190378802372747e-5 -0.00020777161418936488 0.00042679563996792034; 0.0020063611805542577 -0.0004174072750035903 -0.003072969655072353; -0.0005137291934672012 -0.001016339086957489 -0.0004623176061364435; -0.0004431770183830862 -0.0003817253409439307 0.001464027649000994] %
+
+Mass Used: 98.44525308172797 kg
+Launch C3: 95.85521237762771 km²/s²
+||V∞_in||: 0.0016629117646070697 km/s
diff --git a/archive/ES_0.5636581165784301 b/archive/ES_0.5636581165784301
new file mode 100644
index 0000000..4ad2b4c
--- /dev/null
+++ b/archive/ES_0.5636581165784301
@@ -0,0 +1,22 @@
+archive/ES_0.5636581165784301---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T06:24:02.511
+Launch V∞: [7.564923647305983, -6.2257867051630775, -0.05342387997743259] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0014466421361385045, 0.0015701639122923338, -0.0009828260198924564] km/s
+ V∞_out: [0.0004159847360261072, 0.0023086143936598045, -0.0001416893646432268] km/s
+ time of flight: 1.6856514173943213e8 seconds
+ arrival date: 2029-09-12T06:03:03.511
+ thrust profile: [0.4040800742180742 -0.05835585242271473 -0.11966968809107623; 0.035759883475365704 0.012807708688848361 -0.041199123331694495; 0.03813679897680534 0.029762825450237267 -0.0776803701649423; 0.0848693154014169 0.05744015769159597 -0.19879918751352257; 0.020606520696389515 0.023685691528863753 -0.08036256141414232; 0.06939488541435598 0.07431139443344831 -0.23868826928696815; 0.009187263266104558 0.011028665367976693 -0.04345176854491444; 0.007844782110534632 0.014131544410909077 -0.061572121199919436; 0.006800255982990021 0.01161900875867751 -0.04959467945235718; 0.002666243154267233 0.009427710208938551 -0.04124941646646689; 0.0010254782958957838 0.0013925635569918102 -0.005843688172520517; 0.006064871336875333 0.016230516062840452 -0.06916341216164561; -0.0009907255324811506 -0.001187953290986873 -0.003985766350027148; 0.0049287286892056945 0.0035762143420077323 -0.007873465319685191; 0.0012841325923382055 0.0009468417805740233 -0.006110095517311261; 0.002313269005508708 0.002679734784426847 -0.001217318374015001; 0.0024886863954482205 -0.001449734248644191 -0.00014373376705411126; -0.00030686274300407556 0.0006190344488385202 -0.0026212249073291785; -0.001649050498691688 -0.0004660957892004113 -0.0006083037270088997; -3.968728090047958e-5 5.860921751482738e-5 -0.00016630290933243867] %
+
+Mass Used: 97.65162934904765 kg
+Launch C3: 95.99134399870643 km²/s²
+||V∞_in||: 0.002350347882100475 km/s
diff --git a/archive/ES_0.5636626971873429 b/archive/ES_0.5636626971873429
new file mode 100644
index 0000000..9188306
--- /dev/null
+++ b/archive/ES_0.5636626971873429
@@ -0,0 +1,22 @@
+archive/ES_0.5636626971873429---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T08:28:52.947
+Launch V∞: [5.967683974740242, -7.6944826346898205, -0.15629007290331867] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.382046095219419e-9, -2.4259495887394776e-9, 5.550490012938623e-9] km/s
+ V∞_out: [4.947200143588945e-10, -1.202698209305558e-9, -1.5692134340088082e-9] km/s
+ time of flight: 1.7982108643064815e8 seconds
+ arrival date: 2029-01-09T14:46:58.947
+ thrust profile: [0.4012480470894323 -0.10687491671932323 -0.12190481644677076; 0.135281133588189 0.038518844316706144 -0.12832509252620536; 0.08024459531994924 0.04575985004117532 -0.13079704251345445; 0.061427057059263 0.04877501322337736 -0.143618037925143; 0.04547776639848366 0.04546947415566001 -0.13947300810421484; 0.03504058544580005 0.04298980262404126 -0.13548999772564796; 0.029513802399911124 0.032938039320959185 -0.11092375827920246; 0.00422594052113264 0.005526632752789393 -0.02221986362356299; 0.005653348983610077 0.009100388465286628 -0.034053204543840726; 0.0020284616468274536 0.003750848143147637 -0.016981848200695666; 0.0019165145037218204 0.002822709065073186 -0.012630715858119835; 2.2012212497076933e-5 3.837500528437661e-5 -0.00020223698091693742; -1.674625584717223e-5 -3.071104166714846e-5 -7.284738582847265e-5; 5.582239351431371e-5 -7.740217852808467e-5 5.398563369264208e-5; 8.625328708723512e-5 0.00024886337759302205 -0.0001249054518621057; -1.6311270455748238e-6 -0.00027494052577450384 -0.00030396149662263055; -2.767877173807915e-5 6.782149701042159e-5 -0.0001055765856899538; -4.3568397013132656e-5 8.084632448472132e-5 -5.482750253727279e-5; -2.5808076450073967e-5 0.00010859845460453325 6.688037494906107e-5; -3.6009982490769636e-5 5.618669484989467e-5 4.676970012732166e-6] %
+
+Mass Used: 104.3571539072168 kg
+Launch C3: 94.84274162480283 km²/s²
+||V∞_in||: 6.937680201697507e-9 km/s
diff --git a/archive/ES_0.563669269238861 b/archive/ES_0.563669269238861
new file mode 100644
index 0000000..2414fc9
--- /dev/null
+++ b/archive/ES_0.563669269238861
@@ -0,0 +1,22 @@
+archive/ES_0.563669269238861---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T16:31:28.985
+Launch V∞: [6.617439250035655, -7.294553024298494, 0.2294559184810287] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.588246971826608e-7, 0.00024805680399800584, -0.00017805078852633054] km/s
+ V∞_out: [-0.00015355079215866846, -0.0002582187046862596, 5.392429058813781e-5] km/s
+ time of flight: 1.8570111843242332e8 seconds
+ arrival date: 2029-03-17T00:10:06.985
+ thrust profile: [0.2555347195379544 -0.06469575513587171 -0.08342303063477297; 0.09226353003044184 0.02724022033064763 -0.09098659270609867; 0.07612390044590614 0.04329578266497817 -0.1254197169406481; 0.09085643606123711 0.06997455981918763 -0.207416696489269; 0.03977517212925036 0.03756217707841706 -0.11914270476139138; 0.023867592627152507 0.02641418229160565 -0.088445673663038; 0.00878166670883044 0.01125997695070014 -0.03946405836223973; 0.01823580420057027 0.025317242400400723 -0.09215325972957111; 0.0029781831979661505 0.004094701646713413 -0.018622175221903625; 0.003514505259239577 0.005755865703995423 -0.02319183476143732; 0.0001398939663665607 0.0018404892606303188 -0.004639953347628791; -0.00020224293754222462 0.0005222916770666111 -0.0009668835193943394; 0.001204440328147328 9.863612548365895e-5 -0.0036506651877118734; 0.0007562607521860558 -0.0028769608919660085 -0.0015709940882334143; 0.00012263703049306902 0.0019792511138829647 -0.0017447916752248826; -0.00024099684056682382 -0.0002147191318746252 0.000597716243460154; 0.0012038752255580465 0.0031327472556691664 -0.003238990887188139; -0.0008199259332108059 -0.0020514986954111537 -0.00010005618679757096; -0.0011467184189708698 -0.0037202997376682935 0.0006174960318820499; -0.0009250949466760076 -0.00027996758139014165 0.0011382230487641974] %
+
+Mass Used: 91.4678203660169 kg
+Launch C3: 97.05365607074073 km²/s²
+||V∞_in||: 0.0003053438015081921 km/s
diff --git a/archive/ES_0.5636731246057971 b/archive/ES_0.5636731246057971
new file mode 100644
index 0000000..6b0d815
--- /dev/null
+++ b/archive/ES_0.5636731246057971
@@ -0,0 +1,22 @@
+archive/ES_0.5636731246057971---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T16:42:49.360
+Launch V∞: [7.581744995099974, -6.3474382934770555, -0.08860547886422837] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.161324932173121e-5, -0.00032486426776393506, 0.005238523393389466] km/s
+ V∞_out: [0.0005693027092341398, -0.005216630836333127, 6.667229340826786e-5] km/s
+ time of flight: 1.660951508568659e8 seconds
+ arrival date: 2029-08-15T02:15:19.360
+ thrust profile: [0.22571545369234522 -0.035987246409782826 -0.08690289809310878; 0.0631209801530937 0.021157305548437793 -0.07547236498311682; 0.0788307928056819 0.04517671440037978 -0.1562252762291537; 0.06354833269344626 0.04685135231815325 -0.1772530448405757; 0.04913224491309707 0.04353680766427702 -0.17897157353567816; 0.01973387652991136 0.01921725464068708 -0.08817174869309746; 0.016832895082728876 0.019317203622308873 -0.09153054579924147; 0.015162209055405785 0.01775676998750865 -0.09062516915636985; 0.004523793531746643 0.0030223653239048296 -0.034716953564951046; 0.00685907643208853 0.008737002395773555 -0.05118095427969071; 0.0011552896331849906 0.0014563297297206105 -0.00948444277307696; -0.0002558024839544213 0.0032818981133999462 -0.008982908650680592; 0.000163606812366452 -0.001216922239683341 0.00010362848052868534; -9.355492431326783e-5 -0.0017182137355571353 -0.001022371661801704; -0.00011220438401261421 -0.000535006303344574 -0.002684007213636096; 0.0004899989875092093 -0.00022458779353883409 0.0009269179335307264; 0.002743824989962363 0.00465435129925962 0.0043777437529653376; -0.00030677486655443097 -0.0004886505423440928 0.0008424816112305657; 7.280957586041194e-5 0.00032048104768562266 -0.0014651861363048939; -3.822595215206446e-5 0.002035743987801163 0.0035570706344736844] %
+
+Mass Used: 87.23133959197139 kg
+Launch C3: 97.78068099110718 km²/s²
+||V∞_in||: 0.005248751832395736 km/s
diff --git a/archive/ES_0.5636991726396553 b/archive/ES_0.5636991726396553
new file mode 100644
index 0000000..3135143
--- /dev/null
+++ b/archive/ES_0.5636991726396553
@@ -0,0 +1,22 @@
+archive/ES_0.5636991726396553---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T04:18:18.118
+Launch V∞: [6.44995898884534, -7.324919831819151, 0.121715180987415] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.244759493652837e-6, 1.6798061134617133e-6, -3.4747622089985286e-8] km/s
+ V∞_out: [-1.6625898879572773e-6, 3.9043588033280854e-8, 8.246423295444967e-6] km/s
+ time of flight: 1.874957778749919e8 seconds
+ arrival date: 2029-04-08T06:27:55.118
+ thrust profile: [0.39875624764686984 -0.08960647952607162 -0.12559121881216517; 0.096071998470014 0.030584193046369286 -0.09742661338421557; 0.07622854636452751 0.0450151990182442 -0.1277878498450547; 0.0485252819830941 0.03959919630502635 -0.1174555141005886; 0.035624993512327584 0.03530944367939157 -0.1104590816737495; 0.02272355741045448 0.02593377274627069 -0.08986059576679256; 0.026076746821104148 0.032831349433985815 -0.11666958636813501; 0.015016787936650159 0.021977073482693628 -0.08040824569513713; 0.001628787878700839 0.002441684006946665 -0.010747681995201533; 0.0032619989727186594 0.0055093086920363615 -0.022915762056140866; 0.0006436208645240099 0.001032764862465528 -0.00392053358759256; 0.0017187848844304066 0.002969332743865217 -0.01362831571454958; -0.0035389098914687367 0.0009168915057971946 -0.003310042234190187; -0.0001472807189566289 -0.0003886773904193619 0.0013075747125163035; -0.0008461246004724441 -0.0010810022540434193 0.0020679765587498307; -0.00160885219861046 3.393481003313389e-5 0.0029173222188096774; 0.0002730598100191611 -0.0004842614780740805 0.0011444946157647732; -0.00022146339749839594 -0.00044059082922640166 0.0008137486963175978; -0.00031645984953863773 -0.0010805913722143675 0.006131955286833031; -0.0062563884602921446 0.005915937465922136 0.000627202935927842] %
+
+Mass Used: 101.90015757998981 kg
+Launch C3: 95.27123608564709 km²/s²
+||V∞_in||: 8.414215060493927e-6 km/s
diff --git a/archive/ES_0.5637007809199992 b/archive/ES_0.5637007809199992
new file mode 100644
index 0000000..2d5697a
--- /dev/null
+++ b/archive/ES_0.5637007809199992
@@ -0,0 +1,22 @@
+archive/ES_0.5637007809199992---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:08:09.453
+Launch V∞: [7.965646499251109, -5.946028414303854, -0.03488269157110462] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.560500783175452e-6, 4.907440586250724e-5, -0.0008776796236911611] km/s
+ V∞_out: [-0.00010896159397778505, 0.0008684239346626689, -1.43516297808735e-5] km/s
+ time of flight: 1.8087505012036934e8 seconds
+ arrival date: 2030-02-06T03:12:19.453
+ thrust profile: [0.18508978671893334 -0.011285534825603807 -0.06522598580898063; 0.03170096506840763 0.01418427191591767 -0.03988316851102859; 0.04928949441139422 0.03601626187570737 -0.11230875929162429; 0.028763641401256857 0.020205246202971962 -0.07891430144856082; 0.024834881281431014 0.02455809657590207 -0.09487041863326631; 0.015192971545604344 0.019490936371490138 -0.07649016806454335; 0.006337552673714681 0.009346631943226373 -0.0420491666103285; 0.004173415122690694 0.006441209148529161 -0.04025219998304199; 0.012404711177010967 0.022988954483057624 -0.10491472983365172; 0.030260347529280782 0.037816622965423236 -0.19700806139194316; 0.0036115653866614274 0.0048882401146115514 -0.03195766218149021; -0.0007970272568029119 0.00018790588629833852 0.0001442544619229165; -0.0015314181265027574 -0.0016411053248073587 0.0019894534537400204; 0.00018847018092392278 0.003787780505686007 0.0047480626135883285; 0.0008531744440194774 0.0002995057113045644 0.009084096364423316; 0.00558599191886547 -0.005111070650517458 0.0021133234227194023; 0.0039420876765413225 -0.0009382414463978829 0.000982638991558374; -0.00014732908262194512 0.002023458989146575 -0.004058075189899027; 0.00406835405127275 0.002495152942978444 0.007050880488027394; -0.007725454317930468 -0.0013492522354832518 -0.007853166300486486] %
+
+Mass Used: 81.27094107468201 kg
+Launch C3: 98.8079948569115 km²/s²
+||V∞_in||: 0.0008790750021038833 km/s
diff --git a/archive/ES_0.5637013020935046 b/archive/ES_0.5637013020935046
new file mode 100644
index 0000000..d61147d
--- /dev/null
+++ b/archive/ES_0.5637013020935046
@@ -0,0 +1,22 @@
+archive/ES_0.5637013020935046---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T02:38:27.794
+Launch V∞: [6.356670862997989, -7.44725805863955, 0.2675874845187969] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005286868987072554, -0.0034287006381592483, 0.004738829956134531] km/s
+ V∞_out: [-0.004103698558626963, -0.0033224898361913285, -0.0025646797088797525] km/s
+ time of flight: 1.8451172619910914e8 seconds
+ arrival date: 2029-03-04T15:53:53.794
+ thrust profile: [0.3451601714563651 -0.07958638022075613 -0.10786852513042278; 0.10110366678165655 0.03200747739969281 -0.10209219013956054; 0.06016107972860027 0.03544496767882556 -0.1027485163152842; 0.060399320697050736 0.0493207313086139 -0.14276973974695656; 0.030864868967132062 0.029862354835579946 -0.09459081000216484; 0.027923688753327975 0.031922007881418524 -0.10528919800298087; 0.013884686984529106 0.017239686900352186 -0.060793277699241866; 0.016194645998780063 0.022822131688896945 -0.08531123190990333; 0.00576858609883351 0.008372041660542118 -0.03352699894837103; 0.002524694778427335 0.0037299019326112667 -0.014834409662759692; 0.012653503222729396 0.024997901021879747 -0.08867856585737592; 0.00038484951137708915 0.00026684246821318436 -0.0021945026563356903; 9.016940915739646e-5 0.0008627950805771627 -0.003594150567210798; 0.0004995956609814831 -0.00013327068518690158 -0.0013213294789043513; 0.00037713685712593287 -0.0003917884504810519 -0.000706112349754405; 0.0002442803131360375 -0.0007506425177084182 2.8585846463483966e-5; 0.0003907886360503311 -0.0005635831610425802 0.0015151318979476417; 0.0008731666403824471 0.0007617081218615266 -0.00034296790097004424; -4.296033714505345e-5 0.001264665456738051 -0.000286756803343283; 0.0005049483619242671 0.000562022490469863 0.0003448558023262946] %
+
+Mass Used: 97.99848510882794 kg
+Launch C3: 95.94052011433041 km²/s²
+||V∞_in||: 0.005872989635282556 km/s
diff --git a/archive/ES_0.5637028229107246 b/archive/ES_0.5637028229107246
new file mode 100644
index 0000000..7e7c058
--- /dev/null
+++ b/archive/ES_0.5637028229107246
@@ -0,0 +1,22 @@
+archive/ES_0.5637028229107246---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:01:32.152
+Launch V∞: [7.665155839920847, -5.643224466426418, 0.0356668982595124] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7076012610904344e-9, 3.210425297494553e-10, 1.1503468590033836e-8] km/s
+ V∞_out: [2.168444761752356e-9, -7.422760354438892e-9, 1.1904165270800276e-9] km/s
+ time of flight: 1.8749577787282622e8 seconds
+ arrival date: 2030-04-17T18:11:09.152
+ thrust profile: [0.632418915244542 0.032101226090473986 -0.12348578558702526; 0.22908385154718675 0.16216957956839206 -0.16191991670873787; 0.13768010943035874 0.17123091955951092 -0.18528051590238825; 0.05923834765230858 0.10414486387527319 -0.13296170677059935; 0.026724597111696502 0.0661308210357728 -0.09452434501261824; 0.011949631824490388 0.034992491464009144 -0.05513602897767341; 0.004354143654868647 0.0187369092394744 -0.030789685357029337; 0.006482550148893004 0.029166779049251933 -0.04848527619852698; 0.00047810693332718144 0.0028424090485853885 -0.005754390122891142; 0.00015996727902040656 0.0015677001797975293 -0.0038164116588206196; -0.00014990586584813663 0.0004954818977774417 -0.0011180551740641704; 3.639436844836164e-5 0.00016478915659064544 -0.0003761368926177374; 8.352960869724695e-5 0.00022713644389261192 -0.0003594945365011122; -9.020474693343575e-5 0.00023822001342026065 -0.0001944614271836687; -4.656894486877299e-6 -0.0003270922666462125 0.00015725224189363666; -0.0005777940307007635 0.00020112073308487508 -1.9738833360125963e-5; -0.0002727788607109411 0.00024566169805273046 -0.00047479572150633295; 0.0003764455646421426 0.00045912482616392773 -0.0008702498316238959; -0.0001738072605845187 -0.0001367412810572734 0.00022625548336367997; 5.396363600210348e-5 0.00018721354797299569 -7.78102987422111e-5] %
+
+Mass Used: 129.14239348364117 kg
+Launch C3: 90.60186855637785 km²/s²
+||V∞_in||: 1.163394859773244e-8 km/s
diff --git a/archive/ES_0.5637133379158732 b/archive/ES_0.5637133379158732
new file mode 100644
index 0000000..02fc9f2
--- /dev/null
+++ b/archive/ES_0.5637133379158732
@@ -0,0 +1,22 @@
+archive/ES_0.5637133379158732---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T14:58:49.379
+Launch V∞: [6.2872692687894105, -7.386350861059166, 0.0017706025731259731] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.7813392163252434e-6, 9.247825849073135e-7, -2.022179299678625e-8] km/s
+ V∞_out: [-1.403653090317047e-6, 3.266200118215265e-8, 6.698366680276421e-6] km/s
+ time of flight: 1.8749577787470898e8 seconds
+ arrival date: 2029-04-07T17:08:26.379
+ thrust profile: [0.4314503725201323 -0.08625446747299344 -0.11647665992046183; 0.14231997759617715 0.053618290251355366 -0.12236458098585935; 0.06697960346503752 0.0463409153415524 -0.09853890955880124; 0.07781393371202175 0.07385377751096345 -0.15840751684893098; 0.06170822430666307 0.07457614124961988 -0.1646889159106121; 0.03153317224023627 0.04413339005181096 -0.10659637894762931; 0.0093603087533297 0.014881661642697367 -0.03896961314259933; 0.008063689316754026 0.014532398398327274 -0.039469196160745325; 0.006021396297092417 0.011721645474728003 -0.03298345086183473; 0.001192682885859775 0.0028515618617255666 -0.008828109797316632; 0.001209669438898828 0.00535822584055477 -0.019048127573723588; -0.0006349687722337555 0.0013728992870710686 -0.0040510362546029525; 0.00046291330936561637 0.0004176831376826418 -0.0016688370003002267; -0.0008895613795208029 0.0010672299033793304 -0.0030668334802539396; 0.0006058183209362343 -0.0004197632384187859 -0.003259446085496998; -0.0008438008110395656 -0.0007675948095704774 -0.0014015869756745774; 0.0003353286296957996 8.534071756324986e-5 -0.0035879808446821673; 0.00019134504379167666 -5.003477689969721e-5 0.002922273049373379; -0.002057158984461444 -0.0011390794712038313 -0.00030229285708322905; -0.002820643254626748 -0.0018897069856328341 0.0012399361965168077] %
+
+Mass Used: 108.81926152537972 kg
+Launch C3: 94.08793703596669 km²/s²
+||V∞_in||: 6.844135688100472e-6 km/s
diff --git a/archive/ES_0.5637168536098188 b/archive/ES_0.5637168536098188
new file mode 100644
index 0000000..4d14df0
--- /dev/null
+++ b/archive/ES_0.5637168536098188
@@ -0,0 +1,22 @@
+archive/ES_0.5637168536098188---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T17:08:56.818
+Launch V∞: [6.567335252456077, -7.502391070863271, 0.15483052497695302] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.39192854250598e-8, 1.4419136002484353e-8, -1.948759564250752e-8] km/s
+ V∞_out: [6.522578868340916e-8, -6.070280810451447e-9, 7.767414914784099e-9] km/s
+ time of flight: 1.8749577787454584e8 seconds
+ arrival date: 2029-04-11T19:18:33.818
+ thrust profile: [0.13294815199869162 -0.03500874358605863 -0.0500929112640035; 0.02634916059229818 0.00603995471845827 -0.031535176394478184; 0.0480974946003903 0.0208626958798862 -0.0923813883646252; 0.045794218374229735 0.025895982116428812 -0.12079449280766473; 0.05956071762606641 0.04168621966178896 -0.19871325193449554; 0.027219915922336975 0.022436424708136084 -0.1159791294303828; 0.014579137783874306 0.011966119281671645 -0.07032743663364598; 0.011260007770254245 0.0101502580158897 -0.06345169766449646; 0.006809988649678858 0.005056251692877611 -0.03914999454266769; 0.007549877958894183 0.006486756324485735 -0.05418689070986708; 0.000903569702173789 -0.00025574971342383476 -0.007103034905683382; 0.00012727720191845816 0.0020862481611943254 -0.006636439097020341; -0.0025397386240473383 0.0023357258662824072 -0.0010062088968335083; -0.00048160813696761765 -0.0008410424075574296 0.003207732627366719; 0.0011308716531664913 -0.001076514936548547 -0.0004863758107018512; -3.1370939358156004e-5 -6.537550853394225e-5 0.0007142122357055142; -0.0012070212025060262 0.00020197218073826506 -0.003067803448548985; -0.001828660400109195 0.001097504313593261 -0.0011183822732522208; 0.003971255730337901 -0.0027481573792755543 -0.008142169394174621; -0.007170688944789394 0.004005380799013096 0.0036784747768141245] %
+
+Mass Used: 77.60453243770417 kg
+Launch C3: 99.4397365897859 km²/s²
+||V∞_in||: 6.836192592543222e-8 km/s
diff --git a/archive/ES_0.5637243385442647 b/archive/ES_0.5637243385442647
new file mode 100644
index 0000000..d177dab
--- /dev/null
+++ b/archive/ES_0.5637243385442647
@@ -0,0 +1,22 @@
+archive/ES_0.5637243385442647---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:03:03.920
+Launch V∞: [6.329407423172713, -7.536442491870221, 0.0689215412496289] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7599095070290765e-7, 4.858160494767723e-8, -5.7672471379548254e-8] km/s
+ V∞_out: [1.8369796635215783e-7, -4.8925490810262784e-8, 2.349128440776117e-8] km/s
+ time of flight: 1.8477115593221888e8 seconds
+ arrival date: 2029-03-10T00:22:18.920
+ thrust profile: [0.30305904352410984 -0.0837694134530794 -0.11529592548614535; 0.08124986657514346 0.015971354817364013 -0.09654419039271027; 0.06595490711399875 0.02813342914908197 -0.13886347017208894; 0.0684337109160644 0.03826416334288038 -0.1863603783027355; 0.02357945462573408 0.013889293939173396 -0.08075182368536597; 0.017725482284271343 0.013405360217866718 -0.07283468975337459; 0.010656017505075286 0.008903595628402417 -0.05347232691908374; 0.007175857185397604 0.005234795170476404 -0.04781260020372191; 0.012161067487668183 0.011710993004192224 -0.08015671239736902; 0.008936411112428135 0.0078042683476876925 -0.061010218414048134; 0.0010458023420627397 0.0009417795155553689 -0.0072864556158789475; 0.0001500179520694927 0.0005047658008354461 -0.0019741038297067513; -0.00017371510957996778 0.0014012163629221674 -0.0012474640778818678; 0.0024482972303729506 0.0001341192613759617 -0.0017026160820030917; 0.0008895792792738997 -0.0009127111745320788 -0.002382469170334683; 0.001193747516397081 -0.002135963710748017 -3.310176000119783e-5; 0.0004361889006465709 -0.0015611159562043512 -0.00041976975303367357; 0.00015903942267993828 -0.0010502510461694282 -0.0006779524810223703; -0.0009259622788978325 -0.001329681575496853 -0.0011387175633132654; 0.004462627779685995 0.0015935484068518853 -0.0007647875016362966] %
+
+Mass Used: 92.63773031463916 kg
+Launch C3: 96.8641139406291 km²/s²
+||V∞_in||: 1.9146566539103104e-7 km/s
diff --git a/archive/ES_0.563737653366458 b/archive/ES_0.563737653366458
new file mode 100644
index 0000000..a7c5f19
--- /dev/null
+++ b/archive/ES_0.563737653366458
@@ -0,0 +1,22 @@
+archive/ES_0.563737653366458---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T00:23:40.761
+Launch V∞: [6.489954362017618, -7.281615068978195, 0.22773070949421972] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01664123228566674, 0.007668053048668954, -0.0189834278199067] km/s
+ V∞_out: [0.017257116897643098, 0.006847048645269807, 0.01873276906703726] km/s
+ time of flight: 1.874957778795233e8 seconds
+ arrival date: 2029-04-07T02:33:17.761
+ thrust profile: [0.3650338809245643 -0.08162336196005106 -0.11176653135250113; 0.14520142677599351 0.048904961932066005 -0.13667166655508406; 0.07907821295034184 0.05063421334899339 -0.13083532238270873; 0.07369762145052372 0.06269038195067017 -0.16514487117499446; 0.04677779545560952 0.04948423657795828 -0.1437776041471367; 0.02876816873233181 0.03520999907791329 -0.10660430079070526; 0.011985504184633903 0.01697928675685089 -0.054464341845588855; 0.004890234430305873 0.00768004861603207 -0.024625304772132102; 0.0025245086138236516 0.003610738228381135 -0.010625817609548933; 0.0021563907572888816 0.004647262231382527 -0.016419655137851336; 0.0011156238765992923 0.00021703483550196114 -0.0026791741486624264; 0.0012888069104071863 -0.0012999748485993858 -0.002010297899191665; -0.0008358322706211936 0.000575755787524689 9.840292869882708e-5; 0.0005653248367328347 -0.0011569477358366483 0.0007064124933043496; -0.0008278645320376217 -0.0008309176668840651 0.0015100517215320968; -0.0034022210174770007 -0.005447527093465245 0.004070668496538924; 0.00024476035668923935 3.224310033457771e-5 -0.007049144320139921; 0.00011522894017881543 0.0006266676756031934 -0.001787349363062995; 0.00016729159148542853 -0.007888279924077979 0.0019443800439539348; 0.00023437434891145428 -0.00037016948290839367 0.0001674409095571575] %
+
+Mass Used: 102.39975528651757 kg
+Launch C3: 95.19328690988857 km²/s²
+||V∞_in||: 0.026383710530104097 km/s
diff --git a/archive/ES_0.5637421412009661 b/archive/ES_0.5637421412009661
new file mode 100644
index 0000000..8929e54
--- /dev/null
+++ b/archive/ES_0.5637421412009661
@@ -0,0 +1,22 @@
+archive/ES_0.5637421412009661---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T10:42:43.340
+Launch V∞: [7.556522575322576, -6.283659985803671, -0.09241611435148002] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007029432294077214, 0.0005742821304481111, -0.0004438003813633917] km/s
+ V∞_out: [0.00016326371525054474, 0.0009962500914508319, -4.0868220180768734e-5] km/s
+ time of flight: 1.6853473010290822e8 seconds
+ arrival date: 2029-09-13T01:54:53.340
+ thrust profile: [0.36765981884982324 -0.05656488045538168 -0.14007341359537467; 0.05518741031280314 0.018852073621778757 -0.06909063354256705; 0.05296442690017737 0.031975993376860204 -0.11591832427275048; 0.04003085700080923 0.031048204418316686 -0.12217993751803567; 0.033031177194934994 0.029956191158253632 -0.1315774056056292; 0.018405649285825353 0.017293973792955226 -0.08640132847684635; 0.017749225482604578 0.016457309188826215 -0.09399806277370552; 0.02612857391417519 0.023942075963396446 -0.13922093025010104; 0.011129689197398093 0.013209702065493767 -0.07329486046844468; 0.008690597982240672 0.011367670564173114 -0.06952463992355688; 0.00033532444571836544 0.0013261017628189756 -0.004627768964612186; 0.0005108159989928896 -0.00018184235457385442 -0.006102227681312713; 0.0032669373161311765 -0.0019730990832089925 0.00042190479512705607; -0.0024547277867275137 -9.253345216059369e-5 0.0012347418548611885; 0.0005043029709361688 -0.002507249587268406 -0.00047757470358130837; -0.0037359291221710964 5.3246026614455524e-5 -0.002708937523697407; -0.0013488632136973173 6.31921592783596e-6 0.0003428187652094682; 0.001529890808032586 0.0026069384576517395 0.0009978528767495538; -4.3361460645973196e-5 -0.0003047208666552394 0.002022275171673238; -0.0015177637196932341 -0.001422923715764247 -0.004883056852175067] %
+
+Mass Used: 94.2344156451336 kg
+Launch C3: 96.59395698674176 km²/s²
+||V∞_in||: 0.0010103899878860982 km/s
diff --git a/archive/ES_0.5637429677099859 b/archive/ES_0.5637429677099859
new file mode 100644
index 0000000..1f67455
--- /dev/null
+++ b/archive/ES_0.5637429677099859
@@ -0,0 +1,22 @@
+archive/ES_0.5637429677099859---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T04:27:28.892
+Launch V∞: [6.465415242742649, -7.346075168433503, 0.32242629501974174] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5022110664993425e-7, -3.2075205203915734e-8, 4.117723746764371e-8] km/s
+ V∞_out: [-1.5825179148865698e-7, 1.4368498006251669e-8, -1.8783431797342244e-8] km/s
+ time of flight: 1.8461117464698955e8 seconds
+ arrival date: 2029-03-04T21:20:22.892
+ thrust profile: [0.3773070896312836 -0.09680763406386551 -0.11244471301047193; 0.06799620824633194 0.017792618937061376 -0.06900075845554048; 0.061278439134515965 0.03196476603086393 -0.10094756133095635; 0.05534717909601549 0.040037017469226006 -0.12744943189385782; 0.05262313859035092 0.04694608945362086 -0.15646544404657994; 0.0347210844951656 0.03555792863816008 -0.12701953041416858; 0.022779214292628292 0.026753705137424123 -0.10533761178596451; 0.009688258192617033 0.013035617361268103 -0.05078942124682103; 0.004626405731865452 0.007577907521285752 -0.02962780804476862; 0.0031079094332867128 0.003952702570008145 -0.01763616853518682; 0.0027395626786194324 0.0022744375667491197 -0.01457012468064401; 0.0037171616687279208 0.001825441975166781 -0.003382144500823722; 0.002314542526777406 0.00014910507660985753 -0.0008234878312234828; -0.0007394577425859229 1.4040981517799973e-5 -0.002327295580949458; -0.002506489665585708 -0.0038031841175571665 0.0023365742087351534; 0.0009071740044031554 -0.0020733984011419406 -0.001219337540987006; 0.0012566630525423063 0.0023599092594578505 0.0019346179711988139; -0.00031131192035857786 -0.000615960501696913 0.0021362676273445624; 0.0027077010495263265 -0.002796557135253238 -0.0016485446649587788; -0.001221382274808387 0.0011156277285624824 -0.0037682087940144595] %
+
+Mass Used: 98.45628441199096 kg
+Launch C3: 95.87037335708445 km²/s²
+||V∞_in||: 1.5903070319114778e-7 km/s
diff --git a/archive/ES_0.5637479270979902 b/archive/ES_0.5637479270979902
new file mode 100644
index 0000000..8dfc70e
--- /dev/null
+++ b/archive/ES_0.5637479270979902
@@ -0,0 +1,22 @@
+archive/ES_0.5637479270979902---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T14:32:20.347
+Launch V∞: [6.313651682316435, -7.351871466566208, 0.1977053040249058] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001734397384179411, 0.0018283901945327682, 0.0017345737948985217] km/s
+ V∞_out: [-0.0006138253256056852, -0.001330425082584522, 0.002685555943530084] km/s
+ time of flight: 1.874957778749483e8 seconds
+ arrival date: 2029-04-07T16:41:57.347
+ thrust profile: [0.42009176274679544 -0.0931898566200786 -0.12578344435683936; 0.19644901039974627 0.06672023127909132 -0.1788743765765793; 0.10434861303914274 0.06705870311741036 -0.1628470002246231; 0.05648914866914864 0.05008853991856139 -0.1275523065398195; 0.04011198015595908 0.04465530600911273 -0.11811947291612278; 0.013079335048494362 0.015812640719148733 -0.04821575849197137; 0.010254348960718652 0.013812125402086962 -0.044590666467566785; 0.005091239086559236 0.0073905205246776896 -0.024809803727775782; 0.00445225414284658 0.00755056153140946 -0.026172359550047944; 0.0048335670388692355 0.005353117645091916 -0.023126656394542828; 0.0039030798096013133 0.00871415677447762 -0.03104724250459224; 0.004259616324665387 0.005264326100674499 -0.029718922348418674; 0.0013931370836067366 0.0005617134402686659 -0.0024860320608249293; 0.0005691717906366547 0.0010715703930505673 -0.002603891251930669; 0.0010133574520945548 0.0022188518411273184 -0.002838073305935572; -0.00040617465126845066 0.0004041361116563551 -0.0019743246612666764; 0.002385839853300228 -8.949683421173967e-5 -0.0005850693576420224; 0.0022056047640431195 0.0007771305474878595 0.00031539540932250926; -4.965185907456431e-5 0.0003031522046951317 -0.001794318813178034; 7.241770367480231e-5 0.00015042674672119936 -0.0015066327388304687] %
+
+Mass Used: 109.65667070068048 kg
+Launch C3: 93.95129901376708 km²/s²
+||V∞_in||: 0.003059393933389523 km/s
diff --git a/archive/ES_0.5637481604374007 b/archive/ES_0.5637481604374007
new file mode 100644
index 0000000..5cb8fdd
--- /dev/null
+++ b/archive/ES_0.5637481604374007
@@ -0,0 +1,22 @@
+archive/ES_0.5637481604374007---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T01:36:55.584
+Launch V∞: [6.483078816951895, -7.557433707787402, -0.015577499808963677] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012523381632625244, -0.0003602965836578574, 0.008344609642947714] km/s
+ V∞_out: [-0.01433695473650993, 0.00012228635316928534, 0.004584152075811078] km/s
+ time of flight: 1.8292800437783778e8 seconds
+ arrival date: 2029-02-16T06:56:59.584
+ thrust profile: [0.15104444512215714 -0.043946472920062915 -0.05860826594797817; 0.03802305626102297 0.007497983758339205 -0.044650447576356916; 0.03667472656122936 0.015237651982372114 -0.07250474929987719; 0.036879585703087844 0.020772333748136793 -0.1011793179244056; 0.027802900088052102 0.018538195477113127 -0.09708170317842856; 0.016959450610839547 0.012567886761435946 -0.07183707952505974; 0.04692688168360562 0.027361761483764555 -0.17695241444961632; 0.012498651145330619 0.010715983044335091 -0.06577313196052441; 0.029012015201175603 0.025646193847682172 -0.17073181879213659; 0.006807347838115463 0.007331806862915033 -0.05017260880466529; 0.00012794747894972623 0.0004819615452892892 -0.001601623028142894; 0.00029769329627592553 0.0003282852392329262 -0.0019516186220748632; 0.0001952292532289981 0.00021998258465630622 -0.0021998059092283345; -2.248788059304994e-5 0.0003933886413938156 -0.0017930702232422462; -7.180105026587547e-6 0.00039615549285325455 -0.001999243900887406; 0.00012112506752015779 -2.147545121378798e-5 -0.0008708194256285214; 9.103440790725806e-5 -0.0013445781360126726 -0.0012566851612851562; -4.9861653203300534e-5 0.0003014827414322582 0.00017881922972125524; -0.00038660488265294555 0.00023897570292920898 -0.00024035382996361238; -8.494536381597768e-5 -2.958040190712463e-5 4.9367667291644064e-5] %
+
+Mass Used: 79.35826636831462 kg
+Launch C3: 99.14535785291193 km²/s²
+||V∞_in||: 0.015053152867015827 km/s
diff --git a/archive/ES_0.5637499097489407 b/archive/ES_0.5637499097489407
new file mode 100644
index 0000000..3445c44
--- /dev/null
+++ b/archive/ES_0.5637499097489407
@@ -0,0 +1,22 @@
+archive/ES_0.5637499097489407---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:56:20.868
+Launch V∞: [7.878036007797216, -6.042305352112364, 0.09608786469933085] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0726209217322625, -0.41593810386977953, -0.5772267061605858] km/s
+ V∞_out: [0.3013342162874978, 0.141721303270902, 0.632804925278861] km/s
+ time of flight: 1.7606442063572162e8 seconds
+ arrival date: 2029-12-10T10:43:20.868
+ thrust profile: [0.1742233057415076 -0.014221329043419294 -0.05882567575056897; 0.03102954367887457 0.01449686205119885 -0.036318558448064565; 0.05296975895842369 0.04029412957335359 -0.09792827179956665; 0.055672110006602854 0.03730327285597058 -0.14278756082498453; 0.02566209151539845 0.03310280953084511 -0.12735544472742705; 0.016447807040934 0.020017200809770177 -0.06406724253569582; 0.031508661762526674 0.044737153331746216 -0.16470735062644254; 0.012123077653251463 0.029288794028136562 -0.07621547988430008; 0.0009088205685241122 0.0027599951733533502 -0.010129722127757243; 0.012420831339036424 5.781497172847004e-5 -0.043668225509010866; 0.006273546651016543 0.003939461208031887 -0.05938715424582215; -0.00021340672249934613 0.00026659521719813416 -0.0018190069508963592; -0.0005827685222167152 0.004669643427192805 -0.006153540639435962; 0.009866132556786075 -0.0015464255757263227 -0.0025622270919372922; 0.0006502192991828457 0.0038957070875465004 -0.009370998528050435; 0.005241061585820919 -0.001654274561182236 0.0011429695089029473; -0.012841691653327363 0.003309362972542222 -0.010150837667403219; 0.001966528257559685 0.004533351195110788 -0.021591564280954906; 0.00020057990466030174 0.0013232748608150305 -0.006381487765986755; -0.006237096935550898 0.0024071923986807168 0.010245449500156448] %
+
+Mass Used: 82.64575528842761 kg
+Launch C3: 98.58213818605769 km²/s²
+||V∞_in||: 0.715170591417901 km/s
diff --git a/archive/ES_0.5637548803263887 b/archive/ES_0.5637548803263887
new file mode 100644
index 0000000..77e0d08
--- /dev/null
+++ b/archive/ES_0.5637548803263887
@@ -0,0 +1,22 @@
+archive/ES_0.5637548803263887---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T18:19:35.635
+Launch V∞: [6.416775085628216, -7.5761493251931205, 0.09333988120837027] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.969135210865111e-9, -8.486669385665706e-10, -4.567698164001496e-9] km/s
+ V∞_out: [-8.215669325510104e-10, 1.874024632414203e-9, 2.8777154260573623e-9] km/s
+ time of flight: 1.8089704064407125e8 seconds
+ arrival date: 2029-01-22T11:30:15.635
+ thrust profile: [0.14784589456272026 -0.04429427536937729 -0.06057793709311054; 0.08086387562987435 0.016845906550633966 -0.09553192357881209; 0.054511940296509444 0.02335978139217837 -0.10433755185604135; 0.061819424342114425 0.03702483881833081 -0.16605050105124147; 0.03253342875726169 0.023362588961077256 -0.11423460162266663; 0.026069744402218653 0.020500709975110554 -0.10750160088995817; 0.016633179423743625 0.014236691090234059 -0.0798844298853969; 0.01111825050358698 0.010515868910927553 -0.0616191240900414; 0.01083931452253894 0.010707753616186451 -0.06904719283351474; 0.008478167740561052 0.008993424110027482 -0.05714783625737872; 0.0011579855820342852 0.0011952384473044358 -0.008148969215165237; 0.0034317832884054903 0.003891058767766195 -0.027861415116012665; -7.956710345381602e-5 -4.9009009692588025e-5 -0.0016013253012010713; 6.13640131379187e-5 0.0002273549578557796 -0.0006776523037708593; -0.00022812734919349438 0.00028451726116612136 0.00021244855625182928; 0.0005922001725684751 -0.0005265420390779878 -0.0006378955875760316; 0.0002727327504862305 0.00027346469227585915 -0.001422899696356966; 0.0013358224689566872 0.00046125439857241295 -0.00031282680463460123; 0.0004548081403881151 -0.0008854764840991056 -0.001371405459661327; 7.478321304593596e-6 1.479072783351171e-5 0.0002617322242521394] %
+
+Mass Used: 82.65379870236166 kg
+Launch C3: 98.58175343058716 km²/s²
+||V∞_in||: 6.802676446362714e-9 km/s
diff --git a/archive/ES_0.5637614689373467 b/archive/ES_0.5637614689373467
new file mode 100644
index 0000000..6799f26
--- /dev/null
+++ b/archive/ES_0.5637614689373467
@@ -0,0 +1,22 @@
+archive/ES_0.5637614689373467---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T12:16:35.931
+Launch V∞: [6.675571228501513, -7.192487383919903, 0.45267076092912356] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007099020179334568, -0.004719984634469799, 0.0061984111874982045] km/s
+ V∞_out: [-0.005781940356167551, -0.004596718537916642, -0.002568733613710838] km/s
+ time of flight: 1.8749577787475395e8 seconds
+ arrival date: 2029-04-06T14:26:12.931
+ thrust profile: [0.32215270993083434 -0.07928490965453959 -0.10488805651253606; 0.11351128078751553 0.03352205332395941 -0.11339198682010379; 0.07290469080130427 0.04082826559310978 -0.12264474829605604; 0.0643688450663758 0.04887095462738533 -0.15200231319133967; 0.05038292097480433 0.04638003884397075 -0.15421437635839438; 0.029554176694212793 0.031898605586493226 -0.11280655237549725; 0.013539300801614727 0.016345065057830212 -0.06189867816595476; 0.004952286679756739 0.006404376924706551 -0.026842918185785936; 0.0004695376227158874 0.0008368935274869534 -0.004189091159161483; 0.0009257375035560062 0.0021807818405659447 -0.011215675946272714; 0.001368336714753558 0.0003983917678688001 -0.005883690238844719; -0.001598967862292557 0.002342474349458611 -0.005286070404465063; 0.002840605981781858 0.0016979069280305848 -0.0041649043416476135; 0.002744263143536813 -0.0008757698449623017 -0.0011752373273429067; -0.00032912153034537583 0.0008350279630497872 -0.002610699393969175; -0.0005853650791493505 0.0010786066469558255 -0.002884798649833543; -0.0005333250326518791 -1.3563227941083223e-5 -0.00021262964378670904; 0.00454635433827011 -0.00023421006895096364 -0.0024677421750951825; 0.0015708140424742865 -0.003337292312394343 -0.0010242104030668768; -0.0003308697743338656 -6.570975790014521e-5 -0.002570791541105679] %
+
+Mass Used: 94.80483235431257 kg
+Launch C3: 96.50003681244432 km²/s²
+||V∞_in||: 0.007823203760225085 km/s
diff --git a/archive/ES_0.5637628406154263 b/archive/ES_0.5637628406154263
new file mode 100644
index 0000000..2e7ef64
--- /dev/null
+++ b/archive/ES_0.5637628406154263
@@ -0,0 +1,22 @@
+archive/ES_0.5637628406154263---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T20:34:32.872
+Launch V∞: [7.761533371903277, -5.676092445495771, 0.2618376103527567] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.943800661073555e-9, -2.3836295972858784e-9, -1.5910370736397404e-9] km/s
+ V∞_out: [-1.9243454714390008e-9, 1.7473443064330207e-9, -6.848223144881279e-10] km/s
+ time of flight: 1.8143950494543183e8 seconds
+ arrival date: 2030-02-05T20:26:16.872
+ thrust profile: [0.5551113619434551 -0.012870003330029035 -0.13607519310643942; 0.2772128709870726 0.16787150568378675 -0.23088377489426212; 0.07356706307129755 0.07396941117314837 -0.11656787645475558; 0.04103522595153083 0.05629490393161986 -0.09874766863946798; 0.014429065490951687 0.025986009977061564 -0.05145517330467427; 0.015169145898355819 0.03357660752105746 -0.06877353899775547; 0.01751076760398731 0.04504586046685521 -0.09685576454795257; 0.010173659381294733 0.030350701367040735 -0.0690721962983663; 0.002751465393013957 0.008887138027263122 -0.02191098219570836; 0.0013664306213817237 0.0050301109809500885 -0.011763618285727662; 0.0008137094997587582 0.004317078916541861 -0.015126308250985522; 0.0003253166864206946 -0.0003463117460884497 -0.00046263436446385804; 0.00019339274088896486 0.0005928878033705548 0.0006149969658382826; -0.00023529657307872474 0.0010317028676304937 5.021125564720727e-5; -0.000727654031716026 -0.001060604525140619 -0.0006189353181734285; 0.0011692081941172558 0.0004567453542959569 0.0006604391336497896; 0.0005826336893732509 0.00010947920864367639 -0.0011082514561903988; 0.00014501781342009625 -0.0003332880836545303 0.0007550377921910236; -0.0014139520071858609 0.000988199909731321 -0.0012645937896233136; -0.0002617629352997792 0.001103123108012966 -0.0018248972748103052] %
+
+Mass Used: 117.97673682612776 kg
+Launch C3: 92.52798466717765 km²/s²
+||V∞_in||: 4.108412267396062e-9 km/s
diff --git a/archive/ES_0.5637658987049774 b/archive/ES_0.5637658987049774
new file mode 100644
index 0000000..f000114
--- /dev/null
+++ b/archive/ES_0.5637658987049774
@@ -0,0 +1,22 @@
+archive/ES_0.5637658987049774---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T10:47:26.856
+Launch V∞: [7.666173173053599, -6.247285311982243, -0.14088972729452362] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0012608108206479986, -0.0008536125585717114, -0.051884023286823275] km/s
+ V∞_out: [0.04759391930478086, 0.018684645052315083, -0.009078480707506161] km/s
+ time of flight: 1.8749577781475195e8 seconds
+ arrival date: 2030-04-28T12:57:03.856
+ thrust profile: [0.2973434879343995 0.0020885557295290654 -0.1053032379984903; 0.17644054195492587 0.09776161310631372 -0.20222809343620662; 0.039364427442917745 0.03389320007459798 -0.08598588700030764; 0.0409984932900429 0.04639453396242333 -0.13108186171180153; 0.026377065189000307 0.035989646955404374 -0.11435297517335248; 0.013584438669109503 0.02103910951105985 -0.07541670791210553; 0.0069608596792277 0.012132469290301892 -0.04787735479444287; 0.005641817873888067 0.011452485145176912 -0.04770067711943694; 0.00042315158185303296 0.000953287195228956 -0.004088213980614909; 0.00025237974714667217 0.0004956166987993363 -0.0024874428058504696; -0.00024633102841302565 0.0006002336325706916 -0.001933038455369924; 0.00026529843758946224 4.713325163062599e-5 -0.000634172756578604; 0.0005469969505360686 0.00027856308349219873 -0.001316567069904242; 0.00016673173443396778 0.0006558989550499931 -0.0017941956078767684; 0.0005980663642219397 8.535776549204073e-5 -0.00107470296925748; 0.00012890380822211907 -0.0003417401838918901 -4.166742580127142e-5; -0.00010922195611948014 0.0003757226166758715 -0.0002802878165525714; -0.0004374632764250889 -0.00034025239531742927 -0.0006051346779131145; -0.0018202208003439304 -0.00081175161176846 -0.0022200408561754313; -4.033515428993295e-5 9.696603143905446e-5 -0.00010740874241072645] %
+
+Mass Used: 87.11817880023182 kg
+Launch C3: 97.81863480381288 km²/s²
+||V∞_in||: 0.051906359636881054 km/s
diff --git a/archive/ES_0.5637760552093656 b/archive/ES_0.5637760552093656
new file mode 100644
index 0000000..482a288
--- /dev/null
+++ b/archive/ES_0.5637760552093656
@@ -0,0 +1,22 @@
+archive/ES_0.5637760552093656---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T13:58:03.076
+Launch V∞: [6.822489342832012, -7.259833449536298, 0.14865879464754742] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001044001368474558, 0.0011550237956077737, 0.0011183087173657063] km/s
+ V∞_out: [-0.0012898151510281522, -0.0006586189971887542, 0.0012557240279149795] km/s
+ time of flight: 1.8749577787493983e8 seconds
+ arrival date: 2029-04-08T16:07:40.076
+ thrust profile: [0.1262709122650944 -0.03531055331384626 -0.04932846437205514; 0.06883813282997818 0.015923401091628812 -0.08196207281188161; 0.05545548228871609 0.025410839373606487 -0.1115528072779148; 0.04529705174897201 0.027811349358441775 -0.12781852566710492; 0.03623801595908524 0.026373081032064025 -0.1306801497027648; 0.027521429599055968 0.022691128068814716 -0.1209923231022176; 0.019616072961092874 0.017981121366642278 -0.10166235193935413; 0.012769563357762297 0.01250098805179042 -0.07632842922751505; 0.006410649970768779 0.006604755459617858 -0.04381353426787746; 0.0008340993136191471 0.0008511465044120441 -0.006779248557912207; 0.0015850964372968283 0.0019838091237829414 -0.012127572180618103; 0.0010974065558303856 -0.0001279635599695547 0.0006995214139132806; -0.0029277316521798633 0.000979099764596555 0.001964590468376217; -0.0001954432086081982 0.0006431481671296553 0.0012760226625356673; -0.002548465404404112 -0.0020305196562400455 0.0003612672563202534; 0.0007591783711537231 -3.353523217892426e-5 0.001033517487159488; 0.0025462698296664773 -0.0013537034994104435 0.003891199920962379; -0.004146550377589659 -0.003167192318491183 -0.0011417498307658436; -0.0017222764411368085 0.0026422498200925353 0.0020428984786329133; -0.0007075575831180939 -0.0008348658259282576 0.0025270435919014177] %
+
+Mass Used: 78.64248616341001 kg
+Launch C3: 99.27364198528855 km²/s²
+||V∞_in||: 0.0019169332834329603 km/s
diff --git a/archive/ES_0.5637855218630328 b/archive/ES_0.5637855218630328
new file mode 100644
index 0000000..5a49e6a
--- /dev/null
+++ b/archive/ES_0.5637855218630328
@@ -0,0 +1,22 @@
+archive/ES_0.5637855218630328---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T16:14:03.962
+Launch V∞: [6.448419090524474, -7.274280499871501, 0.18108842879094447] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009119807641674202, 0.0012110590151022044, 0.001017887300510317] km/s
+ V∞_out: [-0.001230573112142791, -0.0006115182581495648, 0.0012025046543526039] km/s
+ time of flight: 1.8749577787448353e8 seconds
+ arrival date: 2029-04-07T18:23:40.962
+ thrust profile: [0.47994513936957334 -0.11829859659949712 -0.15317583907728513; 0.08605670702042957 0.028154821316502543 -0.08785439424972348; 0.05676134548068529 0.035127041382429725 -0.09682365883210534; 0.05290879092424255 0.04399085497134675 -0.1263186447927301; 0.02906573685546235 0.03036153855078471 -0.09303634154514898; 0.022373864863053643 0.027094362665587637 -0.08650799637229925; 0.01911498827147641 0.025017559455158506 -0.08560030912712391; 0.017435578884963554 0.02450427458889719 -0.08960493138306345; 0.0030251290892859724 0.004822826235767594 -0.0192627294881279; 0.010357865741735599 0.017196344179368613 -0.07005187221753115; 0.000723485711615013 0.0015800158059639743 -0.0062524207535143254; 0.00029461538184934774 0.001181061482435246 -0.006075812693704386; 0.0017701926134477484 0.003733521870872265 -0.016876321043762212; 0.0007887720500983686 0.00017922084149979466 -0.0011238083101770048; -0.00019009118821467635 0.00044307294413916494 0.0022324635374876287; 0.0009689661678133862 0.00032001609336887893 0.002812815794080068; 0.001064325864006155 -0.0003559181006775792 -0.0011010322759246371; 0.000176048859891089 0.0007761498521894657 -0.0031655493507640586; -0.0011091254315188717 0.0008146583287103803 0.0011045969808711684; -0.0002709626894344254 0.0006799852478938561 0.0013765813018177732] %
+
+Mass Used: 106.32443380832774 kg
+Launch C3: 94.53005857689323 km²/s²
+||V∞_in||: 0.001826052411299274 km/s
diff --git a/archive/ES_0.5637859768021649 b/archive/ES_0.5637859768021649
new file mode 100644
index 0000000..5ecf44e
--- /dev/null
+++ b/archive/ES_0.5637859768021649
@@ -0,0 +1,22 @@
+archive/ES_0.5637859768021649---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T17:07:00.274
+Launch V∞: [6.382369222926161, -7.351124860197941, 0.22389790003022025] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.814640963698474e-9, -4.659337887122072e-9, 1.3576768665877698e-8] km/s
+ V∞_out: [4.510407999572171e-9, -9.921306680734027e-9, -1.3542464151562554e-8] km/s
+ time of flight: 1.8749577785584092e8 seconds
+ arrival date: 2029-04-08T19:16:37.274
+ thrust profile: [0.4379807851356724 -0.1027829215604753 -0.1430108612374304; 0.10515694763831572 0.03143771219188677 -0.10753557407992534; 0.05810764951297081 0.032819675831945776 -0.09912375222727002; 0.06386499194620218 0.049273508805787174 -0.1541856635664029; 0.03213652402843543 0.028480667195938822 -0.09579176331342193; 0.029958039196890836 0.031979403631697226 -0.11385019811585653; 0.013169396548838098 0.016634611072247767 -0.06427323304530994; 0.008968105821796706 0.012087144467682037 -0.048782035583663154; 0.00884973559295411 0.01298740418811859 -0.05491534056929748; 0.0028460312487195863 0.0030146349941368115 -0.020001556200476264; 1.0265061994059813e-5 0.0024961543556189644 -0.014186484059215377; -0.0016572696684624775 0.0031591675996462017 -0.005192068109226606; -0.0005191639573828908 -0.0006032355551961291 0.0015288204855207718; 0.0010427799266344157 0.004260716908270568 -0.00038336909983517154; 0.0008644220002305268 -0.006283849308053962 -0.00042971543680577363; 0.0015221198366893573 0.0008844754333676338 -0.004301938852903949; 0.0001069591036961027 -0.0024868106458709556 -0.0036949540517798645; 0.0007845310859647055 0.0011354148675116406 -0.004797204220885153; 0.008599884198183414 0.00010818793426334896 0.0013308901864431443; -0.00032190849058185735 0.002623362767627972 -0.0006702851321915707] %
+
+Mass Used: 104.61145031644855 kg
+Launch C3: 94.82380387761323 km²/s²
+||V∞_in||: 1.6844464143214555e-8 km/s
diff --git a/archive/ES_0.5637909658384163 b/archive/ES_0.5637909658384163
new file mode 100644
index 0000000..ed9de95
--- /dev/null
+++ b/archive/ES_0.5637909658384163
@@ -0,0 +1,22 @@
+archive/ES_0.5637909658384163---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T00:39:15.380
+Launch V∞: [7.706691835256926, -5.590837663343892, 0.15695688218825302] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.711655918239027e-6, 4.379197282210775e-6, -3.153732970899242e-6] km/s
+ V∞_out: [9.156072797488258e-7, 7.094222809261348e-6, -3.233571407000773e-7] km/s
+ time of flight: 1.8749577787468848e8 seconds
+ arrival date: 2030-04-18T02:48:52.380
+ thrust profile: [0.7210467182099257 0.026515934830826315 -0.1308766060028087; 0.16080145113892108 0.11750205692717915 -0.12366749122989854; 0.061321504439582696 0.07708369667874536 -0.09249765272147221; 0.08635328207391263 0.14975858787384982 -0.1859041308595653; 0.027757298271507313 0.0651482308845959 -0.09459657535186108; 0.01494097481906706 0.045993182982605206 -0.0722143368513054; 0.005466948125128236 0.021144869308351435 -0.03599623031407876; 0.0027761740753831123 0.011630345025760838 -0.02097965909248336; 0.003939991904020343 0.02524190974135579 -0.04600420181156787; 0.0006460365198490043 0.006324705716387059 -0.01205179622120235; 0.00044505460174351055 0.0005928871240450302 -0.002633032467735403; -2.8873058515155835e-6 0.0020330152049438943 -0.0033280664281730085; -0.0016353344342490274 0.001255275070956963 -0.002309063198885784; -0.0009401349282844801 0.0013591361291411443 -0.0011661314841773904; 0.0004583234082972291 -0.0015181498784786352 -0.0017945724297528359; -0.0001330795901250142 0.000751259231475271 -0.0014570767296221347; -0.00048306850679604124 -0.0009706687395547487 0.00039570683543183787; -0.0012143411075499118 -0.002368123687896759 0.0016862503222528193; 0.003929250867726248 -0.003850760584037175 -0.0013283113658206645; -0.0023347922457919567 -0.003941895567749373 0.0027734815035171598] %
+
+Mass Used: 128.81745848613036 kg
+Launch C3: 90.67520028434662 km²/s²
+||V∞_in||: 7.164014376041972e-6 km/s
diff --git a/archive/ES_0.5637916525397748 b/archive/ES_0.5637916525397748
new file mode 100644
index 0000000..f65cf60
--- /dev/null
+++ b/archive/ES_0.5637916525397748
@@ -0,0 +1,22 @@
+archive/ES_0.5637916525397748---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:54:24.356
+Launch V∞: [6.5300991087808296, -7.5335504281936085, 0.14328595687721146] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.660768803743272e-5, -2.4296024541454442e-6, 5.297998977999061e-8] km/s
+ V∞_out: [3.1386069228025813e-6, -7.201259607632176e-8, -1.6488653812076458e-5] km/s
+ time of flight: 1.8271753841799545e8 seconds
+ arrival date: 2029-02-13T01:46:42.356
+ thrust profile: [0.08996340821549365 -0.027263240373839693 -0.034344243691153575; 0.051090947417821886 0.00978641072602383 -0.056264869829178034; 0.06089515744569652 0.02563802008080343 -0.1140251711756801; 0.06032147465352177 0.0344033889664183 -0.15734573506573885; 0.048582694505578575 0.03309657192374114 -0.16116922698792363; 0.033778542437090116 0.025874656623335376 -0.13499528435062308; 0.02234689218237109 0.018390800894094884 -0.10308148655126256; 0.012630297693372641 0.01023288899625872 -0.06266575180015474; 0.0044097517790069336 0.0042285068620233025 -0.022322742412387138; 0.0013706408725420861 -0.00037722191957284025 -0.008146697875828345; 0.0034981256894292745 0.0033537434820410253 -0.02454134700011827; 0.0016352601928163763 -0.00011061097900271323 -0.0024352644468628305; 0.004457648952986207 0.0010457724069505574 -0.006638418845733557; -0.0005518398863334471 -0.0008371955952937295 -0.00569992758613245; -0.0032973389447602474 -0.0009296031006328481 -0.0021701236316315525; 0.0012117536558854955 0.000824084960361805 -0.0021548801718172693; 0.007396188500984193 1.6301095131490933e-5 -0.002570414603507555; 0.00109855074700241 -0.005283907696757108 -0.007098420380769934; 0.002325525530031706 -0.0013678051707205544 -0.000268127883438847; -0.004874803665035057 0.0005999447741656469 0.0003855321178923755] %
+
+Mass Used: 77.82380210430256 kg
+Launch C3: 99.41710729007451 km²/s²
+||V∞_in||: 1.678454875512573e-5 km/s
diff --git a/archive/ES_0.5638014292518135 b/archive/ES_0.5638014292518135
new file mode 100644
index 0000000..d9351c8
--- /dev/null
+++ b/archive/ES_0.5638014292518135
@@ -0,0 +1,22 @@
+archive/ES_0.5638014292518135---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T08:05:13.192
+Launch V∞: [6.511881786132343, -7.5143826030996665, 0.10679567236815793] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.334126075107828e-7, -8.53230284888172e-8, 1.6893870652428308e-9] km/s
+ V∞_out: [1.0073414406031763e-7, -2.638487305454299e-9, -6.363685760733993e-7] km/s
+ time of flight: 1.874957778743262e8 seconds
+ arrival date: 2029-04-12T10:14:50.192
+ thrust profile: [0.20955799249075105 -0.058066443452777304 -0.08385402275581055; 0.0380358047586097 0.008375614328648508 -0.05565914559775056; 0.024590561376370862 0.009252194846292713 -0.054962385636327944; 0.024878164749512807 0.012631308984646651 -0.07661957493269071; 0.04670221386013496 0.027322035039335002 -0.1733912121903577; 0.027770816117952627 0.019632806206172675 -0.12794322493247826; 0.006972387510477282 0.004830958647519359 -0.0409034928847089; 0.01624951069172827 0.012102481036147195 -0.10275637154265335; 0.01814082704251478 0.01270997645210885 -0.11663115675081633; 0.001400732405277767 0.0007742430213033348 -0.012088788755005546; 0.0034604103481923622 0.0024878150776630912 -0.02460395879281595; 0.0006460194448323954 0.0004619239589501306 -0.004520623413113432; 0.0004066447657081252 0.0003621046110900974 -0.0027563666522430466; 0.0006014016440630107 -0.00026680914160262027 -0.0035806966687450207; -0.0009603473435551668 0.0006404362893938269 -0.0018978413273944882; 0.00027764149777333505 0.001166785415513774 0.00017504706690646583; -0.00016372065600314518 -0.0036859256451814947 -0.0032159535490964776; 0.0011578565515130168 -0.0005737519820062521 -0.00010738428085575827; -0.00011750895869174448 -8.305917376223726e-5 -0.002562291544276366; 0.0006069769336811337 0.0004171248770748182 0.001017828509518569] %
+
+Mass Used: 80.95692635564956 kg
+Launch C3: 98.88195561796564 km²/s²
+||V∞_in||: 6.391356699267916e-7 km/s
diff --git a/archive/ES_0.5638074040917858 b/archive/ES_0.5638074040917858
new file mode 100644
index 0000000..ba25363
--- /dev/null
+++ b/archive/ES_0.5638074040917858
@@ -0,0 +1,22 @@
+archive/ES_0.5638074040917858---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T01:59:55.399
+Launch V∞: [7.624992285521234, -5.775267822339258, 0.13399388924536756] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.59455369267397e-6, 0.00018120891240417842, 3.1936334490795554e-6] km/s
+ V∞_out: [0.0001747799049414345, -2.826405779700927e-5, 3.823486126122867e-5] km/s
+ time of flight: 1.8580352653233644e8 seconds
+ arrival date: 2030-03-30T14:05:21.399
+ thrust profile: [0.5715980152493966 0.026043725055255377 -0.11781625903762921; 0.21627367958451255 0.15524149046366392 -0.1644702935306937; 0.08903822305067222 0.10735340405264356 -0.13121601281176326; 0.056625205259611795 0.09522189548459238 -0.12909870189908726; 0.04651545774614073 0.10332958064768562 -0.14992492562145102; 0.006579123139006541 0.01818904312147605 -0.03288951262090691; 0.008889756697834837 0.031116132854531974 -0.05590569709160584; 0.005945593583596319 0.025679005459705653 -0.04899790903997514; 7.156946772673414e-6 0.0027906158965695657 -0.0068248208653566384; -0.00021513738372944135 0.003815739061933735 -0.00647380243935209; 0.0014018815790834077 0.00034485690689293764 -0.0013587437296865767; -0.002360179290507209 2.553524319861948e-5 0.0007293220238001081; -0.006300212508731166 -0.0012495187107653132 -0.0008971731936837965; 0.00529259335218687 0.0010293622933462499 0.0025030001763760856; -0.0021009993117030957 0.0010984827767756547 0.00037038717027754273; -0.006043891088959733 -0.0010905281338167818 -0.0049736759630762154; 0.0029782074260237853 -0.0008813784776925416 -0.005100368150334685; 0.0006695436956588751 0.0004564255719340717 0.0010632463205150029; 0.0005130181814777143 0.007021158195481642 0.013318498189772213; 0.004584059219033619 -0.0028754859646458017 0.0023148974331022483] %
+
+Mass Used: 123.95425397831286 kg
+Launch C3: 91.51218013636067 km²/s²
+||V∞_in||: 0.0001812556231904998 km/s
diff --git a/archive/ES_0.5638080658309372 b/archive/ES_0.5638080658309372
new file mode 100644
index 0000000..9924db5
--- /dev/null
+++ b/archive/ES_0.5638080658309372
@@ -0,0 +1,22 @@
+archive/ES_0.5638080658309372---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T04:59:01.179
+Launch V∞: [7.750909172774557, -5.973031155045321, 0.21502914439574028] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003813649146675065, 0.0022907188982657805, 0.0001738842726539323] km/s
+ V∞_out: [-0.0030704840958601515, -0.0019262620868739848, 0.0025957127484280374] km/s
+ time of flight: 1.7370831216062486e8 seconds
+ arrival date: 2029-11-09T17:17:33.179
+ thrust profile: [0.3384799279305832 -0.032375881529507586 -0.1027600362843631; 0.14308504146885062 0.06739304982807426 -0.14493540526320484; 0.09026895167363032 0.07323400572034887 -0.1602663512252759; 0.03885348214384983 0.04095363252667886 -0.10460260198585827; 0.029832109122895713 0.037877425126474185 -0.10559021415481148; 0.024240992888325007 0.038153023649090144 -0.11271187595360571; 0.013069132972396529 0.022121111408050457 -0.06740429521709432; 0.010531231265269704 0.01673311351911349 -0.05976673747378651; 0.004901356863074556 0.01213469500752284 -0.03762056301371634; 0.006024244341822936 0.009583620882605788 -0.03988492496145578; 0.004979021911544032 0.012992421946719285 -0.04638596130491164; -0.00017824576286538295 -0.0004077726949781762 0.002232331826776619; -0.00024387937264334306 -0.0013280590639361488 -0.00404382519914585; 0.00016137650058921176 0.0037127090669709147 0.003219779171419272; -0.001412297615942212 -0.00419442424153141 0.0030392423414509163; 0.000875606960445655 -0.00010330728369801166 -0.0011353681481061286; 0.00014188283800819465 0.0005815662814563664 -0.00252859434789688; 0.0034608290916798073 -0.0008036144733108779 -0.004939756047180952; 0.0038329747667531 0.006197306344473427 -0.007759376779009865; -0.00205896859636554 0.003154591909473925 0.0012081413975244973] %
+
+Mass Used: 98.94314178877949 kg
+Launch C3: 95.7999317166824 km²/s²
+||V∞_in||: 0.004452139780496995 km/s
diff --git a/archive/ES_0.5638099765173756 b/archive/ES_0.5638099765173756
new file mode 100644
index 0000000..5ea4a4b
--- /dev/null
+++ b/archive/ES_0.5638099765173756
@@ -0,0 +1,22 @@
+archive/ES_0.5638099765173756---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T13:45:11.696
+Launch V∞: [6.364527308164853, -7.465059363607196, 0.17063695234239673] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008820694012336538, 0.0009305950441734299, 0.0007602281337283874] km/s
+ V∞_out: [-0.0010111470136954773, -0.00042194315194835395, 0.0010103189160269913] km/s
+ time of flight: 1.8374932734960353e8 seconds
+ arrival date: 2029-02-23T07:13:58.696
+ thrust profile: [0.277248332769818 -0.06765937842254643 -0.08530045646899911; 0.15165057124224002 0.047351667325679705 -0.13934594493771754; 0.06850162497918266 0.04400451952855558 -0.11743855247219706; 0.04962151881167189 0.042700014759707035 -0.12137690090874748; 0.02367255320419092 0.02408952846270447 -0.07456299844840587; 0.029247395399349712 0.03319198822481415 -0.10635172544337664; 0.020113212281446174 0.029331780930020233 -0.0978736867685957; 0.018369282219267504 0.030183419222914894 -0.09495847106409101; 0.012800894917454059 0.021716381637523565 -0.07567105143974824; 0.0018853695059598745 0.0036082542006339764 -0.013951969384839967; 0.0016130017782786529 0.003406850716763667 -0.01403891982625431; 0.00013040528677312933 -0.0005823826693677007 0.0007336894342789712; -4.9842269200513404e-5 -0.0003690930267971352 0.000998860663712753; 0.0004282892643697583 0.0006362258327310246 -0.0014414988555432123; 0.0007822734935134122 -0.0005028175958274659 0.0016852609150996263; -0.0005805051980438863 -0.0012579949928484217 -0.00018587769608370395; 0.0005909382158259702 0.001663870958611957 0.00073123409880767; -0.0013275168150909174 -4.1296141216299036e-5 0.0014864214042621122; -1.2478273045889526e-5 -0.0014307870719315304 0.0014860693132868485; 0.0004234015511588158 0.0005098760032910327 -0.0008961814741227775] %
+
+Mass Used: 96.24159518991974 kg
+Launch C3: 96.26343612806032 km²/s²
+||V∞_in||: 0.001490637575048003 km/s
diff --git a/archive/ES_0.5638157476099009 b/archive/ES_0.5638157476099009
new file mode 100644
index 0000000..dc4e0e1
--- /dev/null
+++ b/archive/ES_0.5638157476099009
@@ -0,0 +1,22 @@
+archive/ES_0.5638157476099009---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T15:55:25.934
+Launch V∞: [6.461532505729429, -7.503273617595711, 0.0627932194466003] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.830131453880804e-7, -0.00016786163679412698, 0.00011401031817917698] km/s
+ V∞_out: [9.420641157096336e-5, 0.0001811830224701397, -3.6780415664466785e-5] km/s
+ time of flight: 1.843848170519839e8 seconds
+ arrival date: 2029-03-04T17:55:42.934
+ thrust profile: [0.20475527282988304 -0.05797072227199032 -0.0771777683231252; 0.060457282408721114 0.013984173994355647 -0.06967451664635507; 0.05411765158420394 0.02530341002237735 -0.10332766896436225; 0.055266722476238844 0.034878597750101006 -0.14574395613623758; 0.04131444267822124 0.03136190942943908 -0.1397694129748185; 0.02808053624773211 0.02419721096104752 -0.11597035860920527; 0.01648153070192445 0.015609815461395104 -0.08129653859002607; 0.012597635041156302 0.012871838232230284 -0.07084091259340293; 0.007862324252096141 0.008586920094211413 -0.05079840833521304; 0.0034179469569314376 0.004077123015140032 -0.023166412542341256; 0.004861044131319258 0.006332625044147384 -0.03921899964398304; -8.403383165798978e-5 0.0009350406534298157 -0.0021428129121628878; -0.0004653842895543097 -0.0007101753640276434 0.001447989800760543; -0.0018625747772914474 0.0009130549551024216 0.0028324422327007954; -0.0012905928390467775 0.00025147694089986875 0.00427808692403347; 0.00028948867968207957 0.0005304129806362745 0.0013184850120996358; 0.005284187768136419 0.0036682556669793303 -0.0005955823848272288; -0.0011372621375102393 -0.0010699304386204253 0.0003964377367312833; 0.0009010784631767515 0.002615888014998356 -0.0008980423703178093; 0.0007202730550957662 -0.0009151610243114299 0.0002772773359836587] %
+
+Mass Used: 85.80068717771746 kg
+Launch C3: 98.05446029151433 km²/s²
+||V∞_in||: 0.00020291898644587004 km/s
diff --git a/archive/ES_0.5638159481019496 b/archive/ES_0.5638159481019496
new file mode 100644
index 0000000..7e9c161
--- /dev/null
+++ b/archive/ES_0.5638159481019496
@@ -0,0 +1,22 @@
+archive/ES_0.5638159481019496---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T16:03:20.112
+Launch V∞: [6.24306445279748, -7.490648230903849, 0.1210738686887472] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006721079245212433, 0.0044887156706836465, 0.006622773837422923] km/s
+ V∞_out: [-0.004387465855667932, -0.0078009432711447, 0.005364276438788474] km/s
+ time of flight: 1.7943781546316835e8 seconds
+ arrival date: 2029-01-03T11:53:35.112
+ thrust profile: [0.4360028883056282 -0.1349168522111024 -0.154736051723817; 0.063467855986418 0.013576601900899158 -0.06879498045253783; 0.06915976176047021 0.03165738762389616 -0.12331622885306709; 0.05270699269376834 0.03293154304924552 -0.13009296265130602; 0.05612950022455638 0.042928060220880034 -0.17559191742949026; 0.025982623618535036 0.022725341676033812 -0.09999124310736528; 0.022827507828400387 0.022215406531141915 -0.10218543817305749; 0.012886771325179264 0.013819876883723357 -0.06657538831402215; 0.003999321780615015 0.005510491170730921 -0.02284666084102296; 0.004262408661352713 0.004659791154139931 -0.02546938579869183; 0.004137065409624481 0.005703842576955767 -0.02959030479756624; 0.0005151194384520038 0.00048029642154579936 -0.003679150229692285; -0.00025843598832504854 0.0005230728320148513 -0.005360870037291831; 0.0005670246273035032 0.00020461349775050339 -0.0017650145776903661; -0.00016850512677859522 0.0008615212631446622 -0.00021803654343120098; -0.002205957572517728 3.73118030231309e-5 -0.001432911725838086; 0.0006812757320137282 0.0007913644657037792 -0.0008573580904698342; 0.0009022947472800435 -0.0018004027626830799 -0.004485575310902698; 0.0011805080402112005 0.001664002298573573 -5.914605222611226e-5; 0.0006829339339690505 0.0002970039271959798 -0.0016621913452067108] %
+
+Mass Used: 103.03338533707438 kg
+Launch C3: 95.10032356260572 km²/s²
+||V∞_in||: 0.010449048181261288 km/s
diff --git a/archive/ES_0.5638177868977235 b/archive/ES_0.5638177868977235
new file mode 100644
index 0000000..c6fc53e
--- /dev/null
+++ b/archive/ES_0.5638177868977235
@@ -0,0 +1,22 @@
+archive/ES_0.5638177868977235---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T08:23:32.800
+Launch V∞: [6.610968555237465, -7.454146872865886, -0.10715718453535712] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.351681267888184e-9, -1.7971158916511575e-9, 1.0997309020335542e-9] km/s
+ V∞_out: [9.951764108010773e-10, -2.2645843465004348e-9, -3.003276154737361e-9] km/s
+ time of flight: 1.874957778748369e8 seconds
+ arrival date: 2029-04-11T10:33:09.800
+ thrust profile: [0.14437347317322016 -0.03878781750134415 -0.05943892721956644; 0.0589833092609058 0.013328216187955252 -0.07330423736397564; 0.024839625273515558 0.010909545153357611 -0.05262798690260376; 0.038349052992950904 0.022202303513142573 -0.11173547178317943; 0.030052548260617075 0.02097945846176154 -0.11199082450782694; 0.018120295163311623 0.014168991675728927 -0.08313054362968342; 0.019359640520355204 0.016727857193105947 -0.10287163186641936; 0.022858049942852423 0.01872536357060051 -0.1262621166912998; 0.01602492866787921 0.014043065459675805 -0.10062545122173366; 0.005386301190527875 0.005065020745223809 -0.0418037749801996; 0.0008074796440443654 0.0013845480372773077 -0.009092316119257707; -0.001557824827986398 -0.0015346331812785823 -0.0011006158094869817; -0.0009066053298807691 0.0006686760113547737 -0.00023982372097587547; -0.00025259186718253653 0.00012742474285073945 -0.0021132279964791723; 8.645675749528216e-6 1.8802232601402224e-6 0.0022840036966804635; -0.002278059299176041 0.0004768790886103445 0.0013114944244779023; 0.0003047494474212833 -0.0005736563731186694 -0.001815296261893455; -0.00031366073738578807 -0.0004076433728112999 0.003454432282206704; 0.001219005418008769 0.001160264482553469 -0.005278964068267389; -0.001545114707905549 0.00046550770671606093 0.0014688938232860138] %
+
+Mass Used: 78.65003928105534 kg
+Launch C3: 99.28069350279236 km²/s²
+||V∞_in||: 2.5032131021693856e-9 km/s
diff --git a/archive/ES_0.5638198699260211 b/archive/ES_0.5638198699260211
new file mode 100644
index 0000000..c0b5d0f
--- /dev/null
+++ b/archive/ES_0.5638198699260211
@@ -0,0 +1,22 @@
+archive/ES_0.5638198699260211---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T22:35:26.947
+Launch V∞: [6.498411901842929, -7.290150275300213, 0.1880002685354251] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003462734195567827, 0.00035901469049064177, 0.0003401986647587119] km/s
+ V∞_out: [-0.00039708572894480814, -0.00019820029685156467, 0.0004098483856572914] km/s
+ time of flight: 1.8749577787523845e8 seconds
+ arrival date: 2029-04-08T00:45:03.947
+ thrust profile: [0.41606387549335394 -0.09816875569351552 -0.12819329446972158; 0.07572482616085377 0.023217921509173768 -0.073938432125492; 0.054902664590977174 0.031887893130225886 -0.09017861484611836; 0.04068570276712604 0.03183700715269489 -0.09393929664265152; 0.0264617611698077 0.025041417319989427 -0.07866007828153429; 0.019643689666423634 0.02151070807656578 -0.07150873721456981; 0.0592955659253594 0.0787614391133101 -0.2539190447051312; 0.00876685869795907 0.011726545777809348 -0.04321916003078055; 0.005008938105978504 0.007583613355182311 -0.027924657200762346; -7.582226066447917e-5 0.00242220403833656 -0.006253174631166037; 0.002209921654139948 0.0007400699696992613 -0.013225684980453985; 0.0010102616054802579 0.002726209741708307 -0.01043721783769707; -0.0007643899087939809 0.004251653424674174 -0.01098738346734781; 0.0007195598844903226 0.0008943923418499438 -0.004437960818295587; 0.0006328835241575017 0.0007898245933682325 -0.004558550889284245; 0.00040454716806494727 0.0004686135400131889 0.0006672358614552101; 0.0016907823261502776 -7.782754261122108e-6 -0.0006021687844811495; -0.0006093325581238568 0.0009493736389264464 -0.0018530003257282816; 0.007963178922324322 -0.0028036459982932957 -0.0016146369899388041; -0.0038356074300939917 -0.004594954070861199 -0.0034540140494298023] %
+
+Mass Used: 101.22572601027377 kg
+Launch C3: 95.410992383443 km²/s²
+||V∞_in||: 0.0006037648222472468 km/s
diff --git a/archive/ES_0.5638269208507296 b/archive/ES_0.5638269208507296
new file mode 100644
index 0000000..ab9f630
--- /dev/null
+++ b/archive/ES_0.5638269208507296
@@ -0,0 +1,22 @@
+archive/ES_0.5638269208507296---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T05:59:51.740
+Launch V∞: [6.206937023834187, -7.590448366723374, 0.09395005013516836] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00024122343271061985, -3.932945558974887e-5, 6.901303070931199e-7] km/s
+ V∞_out: [4.2598625867572484e-5, -1.1103493158144809e-6, -0.00023968190533375333] km/s
+ time of flight: 1.7758025843013623e8 seconds
+ arrival date: 2028-12-13T13:50:49.740
+ thrust profile: [0.35905136636844953 -0.11671247603013919 -0.13481031891494247; 0.05640923187220887 0.010191164424615446 -0.06286364598315708; 0.052302704539630894 0.02090423357849879 -0.09612939917363632; 0.05951937358290671 0.033567143403634564 -0.1505922695696269; 0.050454537097689385 0.03453147247120183 -0.16166657463680467; 0.036167601521044104 0.028157017055436113 -0.14046398338191124; 0.024506291365750978 0.021179172966788968 -0.11217507681937168; 0.006898418323700258 0.006121387304519743 -0.03646122824665278; 0.015601876152501028 0.016260910303622315 -0.09102375503110532; 0.002517909557442137 0.0025219035443621056 -0.01459844053804126; 0.0003004277451333336 0.0009153148112695305 -0.0018482685693320402; 0.0010879737182290495 0.0008140017695455509 -0.00575504876853573; -0.00010919082942297833 0.00041431413414252065 -0.0017558949601722625; 0.0008139983356395919 0.0006454458919574627 -0.004586348930001945; 0.00016764261592450082 0.00014026186399705853 -0.000831532246271055; 0.001567813152709257 -0.0001919835724988398 0.0010208252374269465; 0.0010509127518878514 6.0464673107934945e-5 0.0011811065987218773; -0.0009004444958718816 0.0020231859825053443 0.0010560318145160506; -0.0005934382916810506 0.0001186500056034731 -0.0005741842890124345; 0.0016782014861235787 0.0011009852536458381 -0.0005584027218302249] %
+
+Mass Used: 96.92423960618225 kg
+Launch C3: 96.14980023765753 km²/s²
+||V∞_in||: 0.000244409547369823 km/s
diff --git a/archive/ES_0.5638350590225232 b/archive/ES_0.5638350590225232
new file mode 100644
index 0000000..4bb1bc5
--- /dev/null
+++ b/archive/ES_0.5638350590225232
@@ -0,0 +1,22 @@
+archive/ES_0.5638350590225232---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T21:27:13.738
+Launch V∞: [6.595564333959015, -7.365592919074555, 0.11648500487907745] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.4416217583007965e-8, 8.855748364104034e-8, 4.6936223858179476e-8] km/s
+ V∞_out: [-2.853194117520785e-8, 5.6948900112293114e-8, -8.924365348167824e-8] km/s
+ time of flight: 1.8749577787493938e8 seconds
+ arrival date: 2029-04-09T23:36:50.738
+ thrust profile: [0.24560725405890266 -0.06617953777991366 -0.09249427123662071; 0.05858072278011514 0.01426448785216621 -0.06828015334930489; 0.04494974293212408 0.021522352985450938 -0.08880352514617398; 0.043266388892942355 0.027447761888600843 -0.11961391445397344; 0.03805694811363727 0.02878988630560602 -0.13552360482925976; 0.02776443992732725 0.02372582015716956 -0.11770847445902194; 0.016368454854513676 0.015412539946664333 -0.08201722822750843; 0.015003016672970798 0.015390054868331476 -0.08665209458656822; 0.007809662500376461 0.007950744614737947 -0.04816081315396646; 0.0009704492418145398 0.0005658581207140039 -0.006332279685558759; 0.0017911586473896874 0.0010187975576258098 -0.015027404431497478; 0.001652097994503611 0.0007511268908972834 -0.01151152671344093; 0.0007457201682667223 0.0009157444847261432 -0.00856854431942751; -0.0021081471737260395 0.005085805111473837 -0.006899359957446866; 0.0004959260273060288 -0.00018007767638043674 -0.00409797730379757; -0.0002108983656987015 0.0002463787223419961 -0.0010690032379174121; -0.007324391353255438 0.005226404735922229 -0.00089371128727088; 0.0031032788169530388 -0.003174268913651832 -0.0051881534942849; 0.004917386963203539 -0.0019576090592203495 0.0045425172055864795; -0.00011275762520140042 0.0022097429051871546 -0.008501490712189051] %
+
+Mass Used: 87.50008817217213 kg
+Launch C3: 97.76699668927512 km²/s²
+||V∞_in||: 1.09627721873983e-7 km/s
diff --git a/archive/ES_0.5638361638405747 b/archive/ES_0.5638361638405747
new file mode 100644
index 0000000..44ba494
--- /dev/null
+++ b/archive/ES_0.5638361638405747
@@ -0,0 +1,22 @@
+archive/ES_0.5638361638405747---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T01:12:26.773
+Launch V∞: [7.647813354468308, -5.593387563021782, 0.33097014696531035] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.31660869221701426, -0.6104409106775761, -0.8989094587405372] km/s
+ V∞_out: [0.5092538136205869, 0.2230037711921716, 0.9840095751337903] km/s
+ time of flight: 1.863665639006104e8 seconds
+ arrival date: 2030-04-04T01:41:49.773
+ thrust profile: [0.7696601044361125 0.011310869155980556 -0.1450108235576182; 0.24029890997314104 0.16398996594467188 -0.16614899147306114; 0.06377782317225378 0.07858103439158833 -0.09234987981931032; 0.048159296193661175 0.08229417829303431 -0.1063004508613059; 0.023223475903194964 0.050905112485856815 -0.0739300335607526; 0.028448241542763153 0.08304955999635452 -0.12296934613871369; 0.013271165277214517 0.04962786868516549 -0.07873714707628568; 0.004221697616588296 0.0220434667405588 -0.037634728389376926; 0.0004952133694525655 0.003018892762831385 -0.005902041415573462; 0.00036112981172951517 0.002355362603613627 -0.004705388345482235; 0.00020010573661350469 0.0005909985117384193 -0.0005858208655491096; -6.912253912434675e-7 0.00018865027624831204 -0.00025760575146330163; -0.00021897802519167615 0.0006383573817265277 -0.000573323026431874; -0.0003193364567247443 -0.0003072172936648775 -0.0006442567551397031; 0.00039196397699803136 -0.00014069098680462246 -0.00013800086954596176; 0.0001593239133598489 0.0005096695833203579 -0.00012572101787025082; 0.00024389864084332203 0.00010727971587192551 -0.0007209259991121244; -0.0001561049548609708 0.00012387130074237486 3.3819746538585977e-6; 0.0009168590474598515 0.0007436051128189332 4.21028907378202e-5; 0.0003210590769525428 -0.0007180851725780783 0.0007232645189264882] %
+
+Mass Used: 133.48217163739582 kg
+Launch C3: 89.8845747731328 km²/s²
+||V∞_in||: 1.131776207750208 km/s
diff --git a/archive/ES_0.5638459511705199 b/archive/ES_0.5638459511705199
new file mode 100644
index 0000000..cf25ff7
--- /dev/null
+++ b/archive/ES_0.5638459511705199
@@ -0,0 +1,22 @@
+archive/ES_0.5638459511705199---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T07:05:41.040
+Launch V∞: [6.597497074391769, -7.392950610859738, 0.17020161819928134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.15197179772902e-6, -2.054924993434895e-6, -2.394346720143555e-6] km/s
+ V∞_out: [-3.2739262718049517e-6, -2.0706396477291434e-6, -6.251930103012537e-8] km/s
+ time of flight: 1.8749577787474006e8 seconds
+ arrival date: 2029-04-10T09:15:18.040
+ thrust profile: [0.22880033902177202 -0.059470468462277444 -0.08248662241904728; 0.020469411692108537 0.005033616408044182 -0.024320145358090888; 0.05650279746286256 0.02731076666813005 -0.10949598115762525; 0.04531434617876363 0.02879327146637453 -0.12291097610590841; 0.037634561165808295 0.02884591039561922 -0.1299415518135048; 0.03000760072272334 0.026166426085527238 -0.12626571957069313; 0.017875869542427435 0.017149331780535685 -0.09022544447643856; 0.005701827858150393 0.005638770978270815 -0.03332974957077263; 0.0059029526429121085 0.0068882166140441774 -0.042319111240251464; 0.013163596536019395 0.01501473818624279 -0.09462239436097546; 0.002116785791428981 0.0026835496821405354 -0.01938723613101516; 0.0007134557454265366 0.0019618783150363497 -0.0018290862224044986; 0.00178263136374437 -0.001213525977207414 0.0017648118008881594; 6.852626169196661e-5 0.0008653042084444508 0.0013029103301785867; 0.000557990207053161 0.0003393273346200886 -0.004199074016507404; -0.00025154921000313923 0.0004946538196783511 0.000632899145237462; -0.008900376715224163 -0.0005739608524321667 0.004173044423783268; 0.0028135708642935318 0.0012680772124851265 -0.0011686430190417348; 8.510605207265929e-5 -0.0003940952236453887 -0.005425870734911128; 0.001681764979421749 0.003292340622882096 -0.004053891193332795] %
+
+Mass Used: 84.91895569527424 kg
+Launch C3: 98.21165497205698 km²/s²
+||V∞_in||: 3.819240181387742e-6 km/s
diff --git a/archive/ES_0.5638586388902914 b/archive/ES_0.5638586388902914
new file mode 100644
index 0000000..103c18d
--- /dev/null
+++ b/archive/ES_0.5638586388902914
@@ -0,0 +1,22 @@
+archive/ES_0.5638586388902914---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T13:53:25.881
+Launch V∞: [6.387825467773845, -7.4290398616668405, 0.5165546230023481] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007744141526167607, -0.0034846337344536763, 0.008490303913240222] km/s
+ V∞_out: [-0.007864428342079037, -0.003241256803227699, -0.008471063629176875] km/s
+ time of flight: 1.8749577787403372e8 seconds
+ arrival date: 2029-04-10T16:03:02.881
+ thrust profile: [0.3933380329778646 -0.09554870337645106 -0.14128902186579478; 0.04298667515662655 0.009960153847297318 -0.04983510733856168; 0.06286567243473333 0.028680377672399598 -0.12077327736997208; 0.05432596492592223 0.03426851999465329 -0.14859326454817115; 0.04049956765350779 0.02915405716953861 -0.13850029043115017; 0.01976503281835864 0.015912386718760375 -0.08290225230219395; 0.016354447231534154 0.014449338156383475 -0.07993236750081431; 0.014144538109207388 0.013629842584028145 -0.08209919664586167; 0.0026938511584096163 0.0059444663401640825 -0.027050705445033844; 0.003326957036573298 0.004049285888655749 -0.022152506483237824; -0.000168718784817064 0.0016571457067817408 -0.008372968618397886; -0.0025076860525068837 0.0008192641535862689 -0.003948318419922417; 0.0013485669849829746 -0.0013079787332954118 -0.0011724510346151004; -0.0004612694745835574 -0.00032371363749314377 -0.0008303545376890176; 0.00419651306857002 0.001634807490930408 0.002550518893459515; 0.0002786443627081436 -0.00010700496285984297 0.004023715446488464; 0.006198266073959407 -0.002258732426139805 0.003166429609764196; 0.00032363110171225733 -0.0010474688166293921 -0.0024367201079313313; 0.0009652359455824106 -0.0017909375825226968 0.00452314606219161; 0.0008644810732375514 0.0007757232577554234 -0.0003529951510206292] %
+
+Mass Used: 96.30805115480598 kg
+Launch C3: 96.26177615152011 km²/s²
+||V∞_in||: 0.012008316317443856 km/s
diff --git a/archive/ES_0.5638644011827746 b/archive/ES_0.5638644011827746
new file mode 100644
index 0000000..a29a875
--- /dev/null
+++ b/archive/ES_0.5638644011827746
@@ -0,0 +1,22 @@
+archive/ES_0.5638644011827746---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T05:13:17.332
+Launch V∞: [6.604176224375799, -7.456822444428203, 0.13403813009696364] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9986007071319625e-8, 5.7874978144742856e-8, 3.08730436020303e-8] km/s
+ V∞_out: [-1.8725730076095615e-8, 3.723141483641799e-8, -5.970446589210912e-8] km/s
+ time of flight: 1.8749577787479165e8 seconds
+ arrival date: 2029-04-11T07:22:54.332
+ thrust profile: [0.13252453140520581 -0.03550390585033915 -0.054052080939185586; 0.061626657559503945 0.012970099825325168 -0.07522553153470089; 0.047266406353267565 0.020070228177598688 -0.0994031937343705; 0.042729137522014966 0.025585753199833142 -0.12562699348648984; 0.032919451999338795 0.02330342539235615 -0.12391349222353838; 0.0269989054927121 0.021123669307639197 -0.12110553291326809; 0.020334046236930418 0.015960136386489535 -0.10184394572659393; 0.009875994558921096 0.008798793058137735 -0.059136099448188185; 0.013398149378463618 0.011959943571156397 -0.09029137943597323; 0.00035912374006928454 0.00072504963360866 -0.008706220543393862; -0.0006868288450664569 0.0011328640063202975 -0.002128496344193574; 0.001776912661759146 0.0015461637573311545 -0.00024621920714314725; -0.004013623277636089 -0.0024641550778923263 -0.002153417520059833; -0.0017285179270593763 0.0035049984309919527 0.0008674784923272763; -0.004729122745655406 -0.004862288538844815 -0.003087320487264604; -0.0032018165472996016 -0.0006608124448496215 0.0008146490318873912; 0.000983627541141239 0.002307845305396208 0.0011512407088704153; 0.0020248095646193433 0.004288452096283036 0.003633150994365581; 0.0029508956432854677 -0.0024011104171479166 0.007119373955254842; -0.00017590882923803643 0.0001090364651493489 -0.0006132756930185166] %
+
+Mass Used: 78.95748843439469 kg
+Launch C3: 99.23731079065868 km²/s²
+||V∞_in||: 7.212363368957889e-8 km/s
diff --git a/archive/ES_0.5638719517888426 b/archive/ES_0.5638719517888426
new file mode 100644
index 0000000..6dc6e21
--- /dev/null
+++ b/archive/ES_0.5638719517888426
@@ -0,0 +1,22 @@
+archive/ES_0.5638719517888426---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T02:01:30.008
+Launch V∞: [6.073697277334345, -7.4907454558713, 0.14014249233628803] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.823514121793697e-9, 1.8820278402851584e-9, -5.297451507313513e-9] km/s
+ V∞_out: [-2.3385311690991757e-9, 5.282893138470021e-9, 7.375544317367588e-9] km/s
+ time of flight: 1.799909870448503e8 seconds
+ arrival date: 2029-01-09T07:31:17.008
+ thrust profile: [0.5436327765554544 -0.14802797203456805 -0.1702551719046489; 0.15541119135047188 0.041238773914493626 -0.15015260752484805; 0.08063348340551918 0.04341855436316713 -0.13198406728168735; 0.05657870884904003 0.041817766138788424 -0.1301810232732519; 0.03109937989829881 0.028113092206317424 -0.09191479031831666; 0.03653741656923124 0.0388928978460417 -0.13060832165482583; 0.026837082836406626 0.029398331351639932 -0.1109984982477058; 0.009540235134700202 0.012205751236737542 -0.04713744677506382; 0.006652501534577137 0.009377875386647005 -0.03736787890791419; 0.0006472827839701864 0.0008826962566161546 -0.0050251657017014485; 0.0012205920786991786 0.0036312504520101064 -0.01939417747502793; 0.0010148069491163808 0.0008888876842210087 -0.004737294213795369; 0.0003876255485737908 0.0003753166202839319 0.000636779680723312; -0.00030722164758764317 -0.0008132521505088401 4.757497380437079e-5; -3.125055169826643e-5 0.0008373619791496633 -0.0012988440593092033; -0.00029470515051169163 -0.0003933981723790253 -0.00042311926385740756; 9.843153619035873e-5 0.0003786922156542118 -0.0006451527532860867; 0.0017852314670759335 0.0008728323807557505 0.0010347871120999477; -0.0015405665774883008 -0.0001231527352143811 -0.001951832377581168; -0.00023358024745630444 0.001461402086238176 -0.002126164403490356] %
+
+Mass Used: 115.22982530648824 kg
+Launch C3: 93.02070601951341 km²/s²
+||V∞_in||: 6.798844129960802e-9 km/s
diff --git a/archive/ES_0.5638763469134197 b/archive/ES_0.5638763469134197
new file mode 100644
index 0000000..3fc7a95
--- /dev/null
+++ b/archive/ES_0.5638763469134197
@@ -0,0 +1,22 @@
+archive/ES_0.5638763469134197---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T12:20:56.987
+Launch V∞: [6.418712141813285, -7.410200402184725, 0.1628796282274803] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3848226550522397e-6, 8.821705560460045e-6, -5.583773247996738e-7] km/s
+ V∞_out: [3.214373332147004e-6, -7.284084972522378e-6, 4.07109551089563e-6] km/s
+ time of flight: 1.8749577787694588e8 seconds
+ arrival date: 2029-04-09T14:30:33.987
+ thrust profile: [0.31488555163902526 -0.07563837574232893 -0.10648707082382804; 0.14649097090455693 0.043647511393353614 -0.1500612459110626; 0.052213607058238326 0.03024734844117352 -0.09488154473560742; 0.037932385126914485 0.029605580283977622 -0.09708101260012221; 0.031962701372223526 0.030285526774109055 -0.10504868773999823; 0.022314720269826296 0.02439466220119587 -0.09080870646378385; 0.00608646640995604 0.008889048774337226 -0.03482003402149968; 0.012506946849979664 0.01582964204487053 -0.06825529144865747; 0.015240710137605779 0.021015413852962347 -0.08429284283710915; 0.009320654803639337 0.014023999662873751 -0.06280625906510047; 0.004785469996360701 0.003933525822634181 -0.019216922843102106; 0.0027546088205086007 0.004043135252555447 -0.015046426871395971; -4.942977005775837e-5 4.283411955888835e-5 -0.0006009241158064779; -0.0005023495912149343 0.00046637136722683166 0.0006595679642103388; -0.0013980032222256395 -0.00011529371195194681 0.0009871635873531597; 0.0017925952261086556 -0.0017637358860202624 0.0018403425210484093; 9.359870495988956e-5 -0.0006329913096644232 0.0008947545248447043; -0.0008002922411788813 0.0014292146908147902 0.0027083950130189095; -0.0007611504686248706 0.0023353564462980266 -0.0028542644817322656; -0.0009001243087127377 -3.847175746998733e-6 -0.002050472238877855] %
+
+Mass Used: 97.05385695478935 kg
+Launch C3: 96.13746533329147 km²/s²
+||V∞_in||: 8.947178774242083e-6 km/s
diff --git a/archive/ES_0.5638866797335786 b/archive/ES_0.5638866797335786
new file mode 100644
index 0000000..8cd9d4c
--- /dev/null
+++ b/archive/ES_0.5638866797335786
@@ -0,0 +1,22 @@
+archive/ES_0.5638866797335786---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T18:23:20.961
+Launch V∞: [6.568961660723386, -7.390166227542383, 0.026351946966442687] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004758787779958256, 0.003194216727622264, -0.004192123236038357] km/s
+ V∞_out: [0.003774084303478494, 0.003001870932528573, 0.002186809015622191] km/s
+ time of flight: 1.8589747173129842e8 seconds
+ arrival date: 2029-03-21T08:34:31.961
+ thrust profile: [0.20230989377210767 -0.054379476109482607 -0.07381545175761818; 0.0837988560112258 0.021601700912803817 -0.09397177345770232; 0.08964603773341043 0.04522354336955426 -0.16415180375153773; 0.03517111880924053 0.02433021436491883 -0.09466592033391612; 0.054472270492166866 0.044633340695066234 -0.17988592717107824; 0.01734504560396523 0.016784735388330647 -0.07542704439390349; 0.011698054352815762 0.013661138897323415 -0.06368535775521253; 0.00566992920631257 0.007057054170080049 -0.03338486761301342; 0.010439941036909919 0.012359347792799003 -0.06502445351825262; 0.0025822542744320487 0.005322135237636296 -0.04099352912157011; 0.0016546646094928233 0.002542973846524228 -0.018883934480071772; 0.00014616875967265463 0.0005733947622042625 -0.0012624799177208092; 0.001036195940732631 -0.0016785028147579034 -0.008054996274801258; -0.002162233402425392 0.0033822972138927033 -0.0001506666604251005; 4.274632693378492e-5 -0.0002912159157970047 -0.0008721264766994412; -0.0013662278588923015 0.006920041021295525 0.004436574890651333; -0.0022627894295583315 -0.00266495032727445 0.0010447582984626832; -0.0018621952203557782 -0.0014906942327751738 0.00406972279455241; -0.000158013693300175 -0.00027236139239605525 0.003421024296073656; 0.0007349617915660832 -0.0007209856085478229 -0.0008044767535271297] %
+
+Mass Used: 87.56315954659613 kg
+Launch C3: 97.76650859587068 km²/s²
+||V∞_in||: 0.005291821835672606 km/s
diff --git a/archive/ES_0.5638891514236115 b/archive/ES_0.5638891514236115
new file mode 100644
index 0000000..70ad07f
--- /dev/null
+++ b/archive/ES_0.5638891514236115
@@ -0,0 +1,22 @@
+archive/ES_0.5638891514236115---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T10:34:01.313
+Launch V∞: [6.418582909213082, -7.612182146435248, 0.08628023413159969] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.59627712618994e-7, -0.0001660217109568968, 0.00011454413660765525] km/s
+ V∞_out: [0.00011024834676255727, 0.00016377025714751193, -4.3558870581195924e-5] km/s
+ time of flight: 1.8358306894849104e8 seconds
+ arrival date: 2029-02-25T05:51:49.313
+ thrust profile: [0.1741841405927429 -0.05626640859418052 -0.07425003043254777; 0.02590068977124646 0.003852381485366673 -0.033730853414834075; 0.05377901900969819 0.016135155391475246 -0.11149064709562825; 0.035091060175611664 0.015389634266009925 -0.10559930140080465; 0.04053743314651341 0.0196936025284829 -0.15281915248578617; 0.028826140578146118 0.014229815824918406 -0.12626819932363634; 0.018945649875643764 0.010289046039481015 -0.10698067258794725; 0.020268916805748778 0.011927963384824694 -0.11949642760963466; 0.0035324346283824473 0.003737555712999165 -0.03533413764936917; 0.003104647792861042 0.002669159781076527 -0.031821564940138936; 0.001098601109341346 0.0003674623253749717 -0.005909924846814819; 0.00028834214711272155 0.00011198710635214397 -0.002126591015307152; 0.0002627267537159085 0.00010636634297164608 -0.0020991286417956483; 0.00025975966562412193 0.0005841415102295492 -0.0009469581021892364; -5.224103305595171e-5 3.9990151536258966e-5 0.0001711092067839292; 0.0016000352177100842 0.0005543001635627959 0.002403044656275166; -0.0008088075730791817 0.00014562266821346214 0.0017064665152019508; -0.00017746794489520966 4.598336506310345e-5 0.002615796942514234; 0.00048748579486514263 -6.0108624681003446e-5 -0.0003088323223185991; -0.001973078070916162 -7.399136931166518e-5 0.0003943756260557775] %
+
+Mass Used: 79.49003074232905 kg
+Launch C3: 99.1509678717516 km²/s²
+||V∞_in||: 0.0002017024564139597 km/s
diff --git a/archive/ES_0.5638918610300788 b/archive/ES_0.5638918610300788
new file mode 100644
index 0000000..b046623
--- /dev/null
+++ b/archive/ES_0.5638918610300788
@@ -0,0 +1,22 @@
+archive/ES_0.5638918610300788---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T21:41:55.744
+Launch V∞: [6.509857782014956, -7.408128561275599, 0.17159791649012] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0587738670106813e-9, -1.3954139652531996e-9, 1.6065624184684032e-9] km/s
+ V∞_out: [6.639928992374158e-10, -1.522419485826175e-9, -1.994861741710673e-9] km/s
+ time of flight: 1.8749577787469527e8 seconds
+ arrival date: 2029-04-10T23:51:32.744
+ thrust profile: [0.29177652304341917 -0.08943192781942426 -0.10963017009074116; 0.06995837850030383 0.012311960010881622 -0.08784859466978331; 0.04487389919098768 0.016982434057245227 -0.0980896337919014; 0.04696276116619204 0.02264026645317773 -0.14057744877266298; 0.03347554769576325 0.019033513962239085 -0.12883822959340338; 0.024226165780755034 0.015728639554449864 -0.11448959052463499; 0.014172705322572674 0.010144617669535406 -0.07864186025048014; 0.004083502582362415 0.0032313168851653023 -0.025627247033063127; 0.005411789226187267 0.004204976183950475 -0.035929396146457314; 0.0009555742279767408 5.981047373664126e-5 -0.006404409630095243; 0.007522436608970788 0.0059465972722665345 -0.05793900720080179; 0.004208418727203136 0.0032333923710954286 -0.03258984596904484; 5.6025761907740464e-5 -0.0004254088555562092 0.0008620257987354979; 0.0003023197074820063 -0.00034641194224740605 0.0014112421588044393; 0.00264317091208199 -0.002694167075311081 0.00206319343865172; -0.0002048380875268589 -0.00016864081019087615 0.0011700374327069368; -0.0009484679775554333 -0.0007994094031777263 0.0018915075913363963; 0.004256242966518314 -0.00043643249490702503 0.005809225458273762; -0.00023608705185201352 0.00022929935056662627 -0.00026899254003443407; 0.0016415367126451487 -0.00010554066680847112 -0.0011971544437644325] %
+
+Mass Used: 90.36013722530697 kg
+Launch C3: 97.28806296739171 km²/s²
+||V∞_in||: 2.9608736505202e-9 km/s
diff --git a/archive/ES_0.5638940969880548 b/archive/ES_0.5638940969880548
new file mode 100644
index 0000000..4a55bfb
--- /dev/null
+++ b/archive/ES_0.5638940969880548
@@ -0,0 +1,22 @@
+archive/ES_0.5638940969880548---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:01:40.501
+Launch V∞: [7.965689808391153, -5.802036155013386, 0.06010456358330123] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0235823388995987e-8, -1.866525265237025e-7, 9.236411877434769e-9] km/s
+ V∞_out: [-2.7388026806085997e-8, 1.1311976711625465e-7, 1.4916318846536598e-7] km/s
+ time of flight: 1.76329289034966e8 seconds
+ arrival date: 2029-12-09T19:23:09.501
+ thrust profile: [0.3059845131104925 -0.019588625411603992 -0.0925377681494782; 0.06231855551576348 0.03239640156705868 -0.06332115972999187; 0.0391945699042798 0.03436982671455866 -0.07084604379519847; 0.04570478980419496 0.05336522740798875 -0.11860997986128488; 0.04416634307990966 0.06351458962187927 -0.15198399655024242; 0.05911042845066327 0.09816331090701363 -0.2443384628332286; 0.006746233217213406 0.013172721029529436 -0.03770321478529659; 0.0033801012378431717 0.007225238562728068 -0.02159269845337054; 0.0023045344276111076 0.00530166830249452 -0.01745829103428388; 0.010214846392750247 0.027257039539902748 -0.08379651033502197; -0.00041290196061306026 0.00017949763331707568 -0.001182311552060476; -0.0002173634103738763 0.002446279027270713 -0.004396523743183392; 0.0010859485049511562 0.0011654738660525363 -0.004174383331769484; 0.0005181917102231894 0.0008454067220334555 -0.0028319127787348264; 0.0015451057351421249 -0.0024145158293730996 -0.0023842124465000315; -0.0003258623428074787 -0.007504444396168987 -0.004499224679447831; -0.0008730565663721988 -0.00042776840822062183 0.0060539842338458855; -0.006986212151885525 -0.005857563894522086 -0.0013521423336076217; -0.0002002951456262865 0.0016063419837540616 -0.0003523651672477534; -0.0008995385576803662 -0.0002802461824413671 0.0059735578288356225] %
+
+Mass Used: 91.34632016683963 kg
+Launch C3: 97.11945022615275 km²/s²
+||V∞_in||: 1.8797331063287075e-7 km/s
diff --git a/archive/ES_0.5639072837688943 b/archive/ES_0.5639072837688943
new file mode 100644
index 0000000..356b6c4
--- /dev/null
+++ b/archive/ES_0.5639072837688943
@@ -0,0 +1,22 @@
+archive/ES_0.5639072837688943---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:48:38.793
+Launch V∞: [6.5154970523271825, -7.3409444494832305, -0.018383296446087945] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.33809261026143e-7, 0.0003151627962036668, -0.00019049041804848784] km/s
+ V∞_out: [-0.00016528425535881992, -0.0003221697860570875, 6.713288223862035e-5] km/s
+ time of flight: 1.874957778747918e8 seconds
+ arrival date: 2029-04-09T02:58:15.793
+ thrust profile: [0.34116120169802294 -0.08104688893378281 -0.11941823195919055; 0.09297413843145994 0.027086680612796954 -0.1008887456034973; 0.03871246703712383 0.021669180680542383 -0.07454041802850712; 0.03250486364607488 0.024864949425761968 -0.087490533962089; 0.03126228596501814 0.0294641237942105 -0.10846147344785523; 0.03292052410645625 0.03657315685822078 -0.13962910935219985; 0.015756373808541547 0.018944414232571212 -0.08058398137688719; 0.018413648240745078 0.02603663135081682 -0.11343026280511455; 0.0092334441339568 0.014061178063135074 -0.0660508517035171; 0.0015497980944797487 0.0024593935969410355 -0.011676484447427363; 0.0005897915834606091 0.0031076773839440407 -0.015693450728335858; 6.434838226187096e-6 0.00041836516436714833 0.0009661606712747651; 0.0003180732478905478 9.507879196358457e-5 0.0009024806699060818; 0.0005145184413504634 0.0002854098982571602 0.0012696566212269194; -0.00200965435474181 -0.002913586638613577 0.003544913993719606; -0.0023500558472573504 -0.0028088135094687097 0.004426679689615282; 0.001244409201080045 0.0004128353397176807 -0.0003288907489045986; 0.003203885366822231 -0.0031495153056597504 -0.0019073202624302127; -0.0013153054726413862 -0.003135736999387723 -0.002238288913618168; 0.0018629077578132137 -0.00175792173202452 0.002265050798301565] %
+
+Mass Used: 95.89971742696207 kg
+Launch C3: 96.34150519487108 km²/s²
+||V∞_in||: 0.0003682595001883015 km/s
diff --git a/archive/ES_0.5639126612308274 b/archive/ES_0.5639126612308274
new file mode 100644
index 0000000..ab42988
--- /dev/null
+++ b/archive/ES_0.5639126612308274
@@ -0,0 +1,22 @@
+archive/ES_0.5639126612308274---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T22:53:06.522
+Launch V∞: [7.792046940785573, -5.580906885870836, 0.31187167043905856] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.923090832429618e-5, -0.0011562097100516761, -2.0045511015245055e-5] km/s
+ V∞_out: [-0.0011156473308100855, 0.00017026251052128038, -0.0002522667330816325] km/s
+ time of flight: 1.8749577787256765e8 seconds
+ arrival date: 2030-04-19T01:02:43.522
+ thrust profile: [0.6189056864828378 0.02311001101208408 -0.13661321701645168; 0.16554021145961426 0.11522009592182025 -0.13527217408342695; 0.10875934359917519 0.12747331154828465 -0.16413942491393088; 0.0368180512516821 0.061706169708384266 -0.09149583227913631; 0.016655845526473156 0.03683945814864262 -0.06054562975604418; 0.008816475941804711 0.024884258366720945 -0.04469123446748844; 0.006960942707221174 0.022800674994292548 -0.04119539792974192; 0.0036591221136657442 0.016253373423094294 -0.03185724277850811; 0.00511738410321862 0.030980314966951816 -0.06304710439298189; 0.003328430962813217 0.02004952312549218 -0.041706432429854806; 0.002428951567062502 0.005790345011573039 -0.01605554220815634; 0.002438732705155363 0.003127255409318565 -0.0028860173198137153; -3.919295594915703e-5 0.0021587998328805747 -0.0004162565176940823; 0.0033830356254381877 -0.0007887177492021495 -0.00889925824189303; 0.0021746450329669475 0.0026090487645637666 0.006153112810807005; -0.0037732210614027997 -0.002834766809962332 -0.004075331127427844; -0.002465228443000886 0.0021768687264523147 0.0018705311479941386; -0.000490383657044585 0.0009096974108569208 -0.015521357060373293; -0.0003424973967066085 0.0004029369493577054 -0.002388978417166389; 0.004553179293046633 -0.001277377181466063 0.0013987008098527366] %
+
+Mass Used: 121.46604814853072 kg
+Launch C3: 91.95978113498877 km²/s²
+||V∞_in||: 0.001157430947600797 km/s
diff --git a/archive/ES_0.5639250012462531 b/archive/ES_0.5639250012462531
new file mode 100644
index 0000000..4a27c89
--- /dev/null
+++ b/archive/ES_0.5639250012462531
@@ -0,0 +1,22 @@
+archive/ES_0.5639250012462531---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T15:05:24.406
+Launch V∞: [6.472122295967592, -7.43181270185061, -0.027444025384807356] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.2622299715176446e-6, -3.1406065270248563e-6, -3.591095715427585e-6] km/s
+ V∞_out: [-4.690416846315865e-6, -3.3237992341958156e-6, -9.480305317527102e-8] km/s
+ time of flight: 1.8749577786532104e8 seconds
+ arrival date: 2029-04-10T17:15:01.406
+ thrust profile: [0.31109794197044394 -0.07995847027147202 -0.11749500522427245; 0.037287460961263515 0.009149717693593117 -0.0440771225201579; 0.04801337864600503 0.02368417590066617 -0.09438539308349644; 0.04178644700530266 0.026959827070303644 -0.11560341182541542; 0.037202717272425065 0.029233768527883883 -0.13230236378718765; 0.04028725308753131 0.036847423153285146 -0.17311137385100808; 0.015636523366306304 0.015635459124867777 -0.08051271005798301; 0.0061813426551364774 0.005976290857316597 -0.0374194769636871; 0.006452296284412258 0.007183381168474512 -0.042961838225738055; 0.005180532800610238 0.004951088950193131 -0.03441727198797083; 0.0018107954681995423 0.0005985586998525029 -0.008648160987537172; 0.00045978962028495334 0.0011979274225991845 -0.006827730816383764; 0.0008713981870674643 0.0016058785866606608 -0.0076602692500653356; 0.003477266840923177 0.001880978067438518 -0.003110415388936463; -0.003370631709511381 0.004346095036667006 -0.000260554083441084; 0.001624763881790627 0.0030065063571281915 -0.0008521623662156863; -0.0034642115098826903 -0.00046130024914921113 -0.0029198730130051784; 0.004187139389792209 0.005332517079210577 -0.0016177217693365987; 0.0020867500913174988 -0.0033803241966838806 0.0029630836729142673; 0.010400749072539423 0.005241302252891869 -0.0013332423291745055] %
+
+Mass Used: 91.37356681467236 kg
+Launch C3: 97.12096022387821 km²/s²
+||V∞_in||: 5.779405002422092e-6 km/s
diff --git a/archive/ES_0.5639327802800096 b/archive/ES_0.5639327802800096
new file mode 100644
index 0000000..acfa8c9
--- /dev/null
+++ b/archive/ES_0.5639327802800096
@@ -0,0 +1,22 @@
+archive/ES_0.5639327802800096---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T09:04:43.974
+Launch V∞: [7.875911926005751, -5.604457656635264, 0.12322779523593463] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.615302230376559e-9, 1.8406900085999137e-9, 2.1158820059487187e-8] km/s
+ V∞_out: [3.8254024877486325e-9, -1.3487777034881637e-8, 2.129391734702524e-9] km/s
+ time of flight: 1.8596866165453967e8 seconds
+ arrival date: 2030-04-02T19:02:24.974
+ thrust profile: [0.5512287317524965 -0.0006613968314870479 -0.15638435692612837; 0.13316388800909204 0.08206466063741238 -0.13762764757044615; 0.054472608814459714 0.05585046156397659 -0.1065940954653267; 0.03833462580778401 0.0530453774494862 -0.1133727526594723; 0.013659653727339419 0.024247455227194133 -0.05759917549317067; 0.023566104126078468 0.04956092821407772 -0.12612148909946108; 0.0059137499434752504 0.010841514953504806 -0.031468033594726656; 0.005534836495985847 0.02234069300761574 -0.05909016976408358; 0.004456770864427477 0.011950553294218822 -0.024755713083949346; 0.0029413790062485772 0.007003689579544287 -0.01475205963922448; 0.000662430257970281 0.002499111200837843 -0.01617881786321656; 0.005487081192998306 0.00097685116214041 -0.018673092376034008; -0.0037682593072269 -0.008421969942182788 0.0009604397242537217; -0.00019686659213946915 0.0008185595588716692 0.0004549490591707868; 0.003819371474323757 0.016277764807135452 0.0012419988890892209; 0.021271470238644827 0.003050570934451303 -0.007199657646019342; -0.00741103877075562 -0.01009990621300435 -0.010473985755988787; -0.004639806584546121 -0.0021391483895183217 -0.00012056083062387743; -0.014097265411592029 0.008639436838515667 -0.016118106019315445; 4.276903467998437e-6 0.00038077466107897787 -0.005242149199032823] %
+
+Mass Used: 112.76671393905144 kg
+Launch C3: 93.45511938073597 km²/s²
+||V∞_in||: 2.1734415582095502e-8 km/s
diff --git a/archive/ES_0.5639355608019826 b/archive/ES_0.5639355608019826
new file mode 100644
index 0000000..bb8098c
--- /dev/null
+++ b/archive/ES_0.5639355608019826
@@ -0,0 +1,22 @@
+archive/ES_0.5639355608019826---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:55:51.765
+Launch V∞: [6.538169910361676, -7.456500985169395, 0.12747400229215985] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005906915591502034, 0.0007005605049702257, 0.0006020064838854669] km/s
+ V∞_out: [-0.0006997554468028324, -0.00036011091787578365, 0.000763457990840086] km/s
+ time of flight: 1.8435583263002053e8 seconds
+ arrival date: 2029-03-04T05:53:03.765
+ thrust profile: [0.17926988311202205 -0.05452754057166909 -0.0716919686979495; 0.10480949824805083 0.020164709015955764 -0.12682314829791871; 0.03395782252961153 0.01402635800812402 -0.07151326213697921; 0.03786927799616908 0.020819799391242563 -0.10974988070212498; 0.028662681002530704 0.018682490826457513 -0.10606245936533225; 0.020392412250865008 0.015244201067638304 -0.09271989774355467; 0.014054499584869061 0.01121002674115449 -0.07367910838692489; 0.01269235434090558 0.010551967903102973 -0.06703441143551157; 0.022891582414055305 0.01998642024741376 -0.14661522732021076; 0.0052404046212629184 0.004950927228708181 -0.03706451828849274; -0.00035280116535008727 0.0006165534972517278 -0.001475392476694996; 0.0026323830605802815 0.002493298246241126 -0.021471257387069252; -0.0002745845607054774 0.00019040132059974194 -0.0023054979397004963; -0.0005539916630976584 -0.0019311287782079283 -0.000762722479968587; 0.00011004536992348084 5.3432236136763856e-5 -0.001200348977799541; -0.00026471053544212665 -0.0004393177910807923 -0.0011586920102004685; 0.0014725265766829558 0.000441582530288071 -0.0031715473612938415; -0.00018245995513202547 0.001305103205037373 -0.0009238539515412738; 0.00016146037081419618 -0.00025957064734975186 -0.0011357277938472167; -0.002866373083631143 0.0033023960110381305 0.001965424202275019] %
+
+Mass Used: 84.13877395318013 kg
+Launch C3: 98.36332233985135 km²/s²
+||V∞_in||: 0.0010964092966659754 km/s
diff --git a/archive/ES_0.5639448169834456 b/archive/ES_0.5639448169834456
new file mode 100644
index 0000000..3ad1e84
--- /dev/null
+++ b/archive/ES_0.5639448169834456
@@ -0,0 +1,22 @@
+archive/ES_0.5639448169834456---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T07:24:42.904
+Launch V∞: [6.3762717517841185, -7.321787497434913, 0.14746040037047137] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.3392383188765605e-8, 5.264655598400204e-8, 3.821043069332124e-8] km/s
+ V∞_out: [-2.01778245188933e-8, 4.532572174044134e-8, -5.421626927893459e-8] km/s
+ time of flight: 1.8593872938601953e8 seconds
+ arrival date: 2029-03-19T09:03:31.904
+ thrust profile: [0.47309720439014075 -0.10180681141090075 -0.12112957868376238; 0.08362509598152132 0.03193971363066701 -0.07639223004267182; 0.07737067636340317 0.05305677977741496 -0.11408962067777743; 0.05400309626587757 0.051294765985349856 -0.11510797897986116; 0.05904557765041001 0.069543570550639 -0.15684462204671454; 0.02522740949807633 0.03348953111835016 -0.08346220552367924; 0.015974623370727803 0.02456681001343718 -0.0634380423401544; 0.019251253094168475 0.03255128814457084 -0.08708243283272583; 0.01296847824130483 0.027881083968115998 -0.07600949114074666; 0.003437232136895537 0.008005347100015341 -0.023286594005330234; 0.00033968533610363006 9.251814499374779e-5 -0.0013940234722558897; -2.473727258461475e-5 -0.0002851414038082547 -0.0007157170014446125; 0.0002865595112928901 -0.0005283661354377663 0.0003277917064439604; 0.0004047947080449723 0.0005860028964150846 -0.0008029336754436696; -0.0004242670094231927 -0.001010191966853778 -8.331527076371303e-6; -1.1328768707967625e-5 0.0005002074733158424 -0.0008035533887564191; -0.0014106317551241382 0.000161793845450531 -0.0003280092186060672; -0.0010581235322578428 -0.00011900950010238471 -0.00022610526023673092; 0.00041110739307746296 0.0008944827271264082 -0.00024083156455228312; 6.680473062622148e-5 0.00023669693157393442 9.499519899328404e-5] %
+
+Mass Used: 107.92719709810126 kg
+Launch C3: 94.28715817987174 km²/s²
+||V∞_in||: 7.312146145811859e-8 km/s
diff --git a/archive/ES_0.5639629530919683 b/archive/ES_0.5639629530919683
new file mode 100644
index 0000000..78d56d8
--- /dev/null
+++ b/archive/ES_0.5639629530919683
@@ -0,0 +1,22 @@
+archive/ES_0.5639629530919683---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T08:56:29.269
+Launch V∞: [6.528058319365237, -7.238574861836078, 0.3376016038015709] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3831467529036093e-7, -1.3119170791287224e-8, 4.336570542344714e-8] km/s
+ V∞_out: [-1.4421005796188142e-7, 1.4388744585051902e-8, -2.0214505118639323e-8] km/s
+ time of flight: 1.874957778748194e8 seconds
+ arrival date: 2029-04-07T11:06:06.269
+ thrust profile: [0.45548953473953346 -0.10965713561148428 -0.14103220390331012; 0.0478045175446225 0.01406353879164825 -0.05035817869837484; 0.07366825031291918 0.04206254204382825 -0.12486044934485765; 0.06485147606108034 0.05009329169303257 -0.15311584893874677; 0.03913996714460081 0.03652211786049787 -0.12193853754359302; 0.026567298676384556 0.028664226102942815 -0.10302682439217163; 0.008581581867124707 0.011165238823502038 -0.045259514357206286; 0.014692576608567383 0.019284381084645013 -0.08315255524924872; 0.008889026570522575 0.014167755996684862 -0.05260705338396584; 0.0050502220541141715 0.005168846707596349 -0.017456912391553264; 0.0022543501368687048 0.001143059630780979 -0.003273249649360819; 0.0033370280262498544 0.001276290037194178 -0.0046038307281461984; 0.000998552038192277 0.0015796465895582252 -0.006019510658189355; -0.002792619016972903 0.0020616516416726975 0.002440295176951022; 0.0015558532885049925 0.0036232145270095246 2.5376678244013818e-5; 0.000786846135558386 -0.00019509069877729712 0.0003735225563855603; 0.00022824662213481598 0.0006442506882005823 -0.002525590443440957; 0.0018788904008107672 -0.003006371135584286 0.001482665705595451; -0.0001660252803439826 0.0006194566460281166 0.008322489389070355; -0.0034180604484918223 -0.0014206089206731112 0.0013768823523594425] %
+
+Mass Used: 103.05227522371479 kg
+Launch C3: 95.12648629432827 km²/s²
+||V∞_in||: 1.4554602862944127e-7 km/s
diff --git a/archive/ES_0.5639685646002535 b/archive/ES_0.5639685646002535
new file mode 100644
index 0000000..0f1dbe4
--- /dev/null
+++ b/archive/ES_0.5639685646002535
@@ -0,0 +1,22 @@
+archive/ES_0.5639685646002535---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T14:15:44.714
+Launch V∞: [6.44506261521095, -7.312899144197846, 0.19911845106788503] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.391711169379383e-6, -9.804770666775806e-7, 2.5641107053547956e-8] km/s
+ V∞_out: [1.8478468240867998e-6, -4.145228631177485e-8, -9.262232562106988e-6] km/s
+ time of flight: 1.8480274097119403e8 seconds
+ arrival date: 2029-03-06T12:21:24.714
+ thrust profile: [0.4197976632198425 -0.11016033919396416 -0.1376315743571163; 0.09703555927698627 0.026916564327481032 -0.09700686223696543; 0.0640562119088049 0.034869852301883025 -0.10751400224052658; 0.0634978344780491 0.04734482802641734 -0.14927085632609038; 0.0651811371264754 0.059017119550725625 -0.19588868317778516; 0.023178364355471544 0.024262167054523005 -0.08619985329074759; 0.02566357702709002 0.029924917037840688 -0.1107098157927789; 0.0033856600226601493 0.0043596471914811525 -0.018528657569409475; 0.0014715914390736168 0.0017960848359612413 -0.009884470931032284; 0.0009562438313555864 0.0021285283071796226 -0.0079447567260558; 0.0009355285414041447 0.0015934914868880202 -0.006380999038128152; 0.0005344407364075674 0.0007763213303378448 -0.005759282602548463; 0.000926229938303087 0.0010119646575771244 -0.007330244856140436; -0.0008628846639199885 -0.0015273350808324973 -0.001750784889802035; -0.0012029470083378883 -0.002577920515638759 -0.0015584548380866143; -0.0007000589749377398 0.0010700107273121538 0.001846663264234472; -0.0024223446017602305 0.003540695047864154 0.00510627630993416; -0.00365122905975584 0.0007119086342197874 0.0034203962741317486; -8.681968393351933e-5 8.023353206945759e-5 -0.00025513299658611044; -0.006979996994624531 0.0018909483910989303 -0.006268657429598928] %
+
+Mass Used: 103.46430940589107 kg
+Launch C3: 95.05697416475508 km²/s²
+||V∞_in||: 9.442787270382463e-6 km/s
diff --git a/archive/ES_0.563972583515112 b/archive/ES_0.563972583515112
new file mode 100644
index 0000000..1f23d3a
--- /dev/null
+++ b/archive/ES_0.563972583515112
@@ -0,0 +1,22 @@
+archive/ES_0.563972583515112---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:31:05.129
+Launch V∞: [6.176866931281132, -7.7441148865318095, -0.023396147634636027] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3918407464372643e-9, 7.726291118828958e-10, 6.454855672192992e-9] km/s
+ V∞_out: [-3.765283955712524e-9, -5.64320649130123e-9, -2.8080851235985427e-9] km/s
+ time of flight: 1.7592644842843723e8 seconds
+ arrival date: 2028-11-25T19:58:33.129
+ thrust profile: [0.19919636583671674 -0.07266065004944389 -0.08299226739456557; 0.05991358442519395 0.007277088877242127 -0.07281988099428936; 0.06639343641303017 0.02139093500196896 -0.13224680862610216; 0.06274050235315211 0.02787163079412291 -0.17091945120938062; 0.049380449115015324 0.026079297083961436 -0.16993431266254141; 0.03242581741885214 0.019262819470014823 -0.1354069972244104; 0.01980262802518778 0.012598747786928296 -0.09599365915851119; 0.011732240407722246 0.008031196961119607 -0.06470374113366124; 0.005657967874989879 0.003789645312549871 -0.03328287377829609; 0.004101195710293701 0.0052646428164755885 -0.039470472443735; 0.00015486058612154273 0.00011564788088149586 -0.0012183297222106513; 0.00015702847994926908 0.00011091630831642551 -0.0009690101039384149; 0.00015405650825598143 -4.7765032329144056e-5 -0.0011570006982690251; 2.3182942378573894e-5 -4.290646475013497e-6 -0.0007954988756248571; -1.8833712682285366e-5 8.450624889003633e-5 -0.00032173576107822276; 8.066205482921924e-5 0.0001778228611081298 -0.00013980267685926554; 9.056000561263292e-5 9.42350663622143e-5 0.00022793647216821564; -0.00010707807754336228 -0.0001248135968275932 0.0009361884300425458; -0.00015442779828049764 -0.0008162833414642452 0.000221771593180983; -8.540540800043182e-5 -0.000151078494301414 -3.245040682472219e-5] %
+
+Mass Used: 85.56898502098511 kg
+Launch C3: 98.1255478422821 km²/s²
+||V∞_in||: 6.64825827994175e-9 km/s
diff --git a/archive/ES_0.5639986711481667 b/archive/ES_0.5639986711481667
new file mode 100644
index 0000000..1942664
--- /dev/null
+++ b/archive/ES_0.5639986711481667
@@ -0,0 +1,22 @@
+archive/ES_0.5639986711481667---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T20:06:21.375
+Launch V∞: [6.483038453152036, -7.424493610339795, 0.1764342435060734] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6532116373972954e-5, -4.056596565260101e-6, 6.903584376618988e-8] km/s
+ V∞_out: [5.263878598722742e-6, -1.1779413844237777e-7, -2.6317150904791015e-5] km/s
+ time of flight: 1.8488650288828138e8 seconds
+ arrival date: 2029-03-09T17:28:03.375
+ thrust profile: [0.2868249624206282 -0.07795099996263363 -0.10060104102564416; 0.037203883693473896 0.009448991688063221 -0.04168643161120776; 0.047566648387412674 0.023938196874757917 -0.08797199723526769; 0.06930771814798474 0.04687779572117509 -0.17260757031066123; 0.04415985667943569 0.036230351367949956 -0.14325575449641467; 0.029452651002865888 0.02768424240634606 -0.1172387993387378; 0.011409473418870417 0.011574734742834866 -0.05405980421041547; 0.01927303429721662 0.022023340234714327 -0.10351191167505844; 0.004387455627431899 0.005676167718045487 -0.030732696697384976; 0.0058004815944874945 0.007850004819924053 -0.042073941143560376; -0.0002708301927838248 0.0009135717762343849 -0.002175789407906233; -0.0006362427938491368 0.0007924106988125186 -0.003966808013384714; 0.001016298900277913 0.0012926648204242316 -0.007127013179035259; 0.0020422984861008567 0.00042971339363940815 -0.0002858325594217075; 6.125369719222376e-5 -0.0016578225108292055 0.002823144604143622; 0.007576486518040129 0.003577585528944324 -0.0042601621228188545; 0.00016085342238203758 -0.000876930093353346 0.001083310038004146; 0.002756497088283307 -0.0005419057912215731 -0.005079223829657097; 0.0007531929060758131 0.0026017686033422047 -0.015187930288442895; 0.0020959490125216796 0.0034120374094648697 5.627724432933799e-5] %
+
+Mass Used: 91.09165468857645 kg
+Launch C3: 97.18402199730595 km²/s²
+||V∞_in||: 2.684052795537093e-5 km/s
diff --git a/archive/ES_0.5639989050494698 b/archive/ES_0.5639989050494698
new file mode 100644
index 0000000..c0c6248
--- /dev/null
+++ b/archive/ES_0.5639989050494698
@@ -0,0 +1,22 @@
+archive/ES_0.5639989050494698---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T18:48:40.495
+Launch V∞: [7.342113794876153, -5.9592649674527784, -0.09052651231450984] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.32468739013915e-6, -9.814519609618556e-6, 0.00020802019943731945] km/s
+ V∞_out: [6.762361876883622e-6, -0.00020776444313027947, 2.1533580485017885e-6] km/s
+ time of flight: 1.842554088975094e8 seconds
+ arrival date: 2030-03-12T08:52:08.495
+ thrust profile: [0.5520266797588692 -0.001115834985252552 -0.11466076243183419; 0.3936036204635016 0.2477869792600258 -0.27634286987323975; 0.22475584568688636 0.23892735240389612 -0.29721902125361027; 0.04224214909849424 0.06462553139405837 -0.09701358464433385; 0.018760484531716352 0.036530210071049445 -0.060938477212570195; 0.0070121613455288775 0.016570557220044066 -0.03004409277266577; 0.0018053846488180082 0.005678065686227996 -0.011045053589412813; 0.000885500340258474 0.003004059102185275 -0.004303261055940687; 0.0017863197997857083 0.006107134750601811 -0.011965870376462403; -0.0003231788228922829 0.0008877675923075496 -0.0032276599410513604; 0.0003373791634772468 0.000680266192223941 -0.0018821771329352041; -0.0007727934047580863 0.0017743421944960524 -0.0040937735703915875; -0.0007019527581601055 0.000215466741542335 -0.0021959562973899163; -0.0011030899043447677 0.00255152239328318 -0.0030832095288521664; -0.0019268684857701689 0.0002562909606984463 -0.0038669809239992607; -0.001076407090874236 0.0017757278445663493 -0.0052828847872151115; -0.001304329580041637 0.0019354403944245278 -0.0037675034694999235; 0.0004001045349701671 0.0034187905278470253 -0.003517377020479498; -2.323415737073717e-5 -0.0021053966367272025 0.0035412451446784083; 0.0004460619166568059 0.006917913279798529 -0.0009693868694379106] %
+
+Mass Used: 136.3373201822419 kg
+Launch C3: 89.42766897865249 km²/s²
+||V∞_in||: 0.00020825581136139115 km/s
diff --git a/archive/ES_0.5640003731246866 b/archive/ES_0.5640003731246866
new file mode 100644
index 0000000..c83a4e1
--- /dev/null
+++ b/archive/ES_0.5640003731246866
@@ -0,0 +1,22 @@
+archive/ES_0.5640003731246866---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T06:17:21.912
+Launch V∞: [6.584899336836157, -7.514341845444319, 0.07294556580349862] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2989206597996358e-8, 4.711922094317641e-9, -1.882298694202973e-8] km/s
+ V∞_out: [-4.808781717170403e-9, 1.0875618662556627e-8, 1.5147647971396847e-8] km/s
+ time of flight: 1.8749577784168172e8 seconds
+ arrival date: 2029-04-12T08:26:58.912
+ thrust profile: [0.11290667335133463 -0.032719804799545976 -0.04721588660938819; 0.038619606494741845 0.007067712155739231 -0.049216636881737066; 0.041084617310124104 0.015124209540488546 -0.0869115837740336; 0.04023931085251133 0.019555934926011785 -0.11742555313388711; 0.04159505895715908 0.023618841657920005 -0.15419120566511874; 0.027995127254856634 0.017527021743179542 -0.1252883958332809; 0.02340731652414116 0.017161776325273236 -0.12956138138227477; 0.008535328333971852 0.006066841884749317 -0.05233134771534389; 0.004378886158333453 0.003582487697094836 -0.032465227771644546; 0.0013693738129664853 0.0010212169130397206 -0.011635875165797165; 0.004992323848173197 0.003986854586564164 -0.040539646591593086; 0.0007565613968318616 -0.0005922761602046975 -0.0011935750750613444; 0.0025842927521460175 -0.0010133523369315295 -0.003294247223494165; 0.002357875948390472 -0.0010835427997418863 -0.0002248491672946721; 0.00037192565107943646 -0.0013124964329987079 -0.004041824890712081; -0.0021547382108958674 0.004452931493385043 -0.002531750332400688; 0.00033933004182071393 -0.0004128766761314196 -0.005309305258797122; -0.0001283318167890487 0.00010141533009365265 0.0025942617372169737; -0.0041808739908567 0.00024062924527171466 0.006795785635388076; 6.562653870408335e-5 0.00035331843436421585 0.0035459834094396687] %
+
+Mass Used: 75.64970538361922 kg
+Launch C3: 99.83155370203119 km²/s²
+||V∞_in||: 2.335008640858043e-8 km/s
diff --git a/archive/ES_0.5640007460344055 b/archive/ES_0.5640007460344055
new file mode 100644
index 0000000..dc3a04f
--- /dev/null
+++ b/archive/ES_0.5640007460344055
@@ -0,0 +1,22 @@
+archive/ES_0.5640007460344055---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T02:43:38.374
+Launch V∞: [7.574459704813602, -6.298470455910129, -0.08207958810726437] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.804651009768497e-7, -1.185523407963461e-5, 0.00024126105492319898] km/s
+ V∞_out: [1.0186202125809985e-5, -0.00024132037174027742, 2.3531391274063883e-6] km/s
+ time of flight: 1.7006478731453398e8 seconds
+ arrival date: 2029-10-01T10:56:45.374
+ thrust profile: [0.30091487743615963 -0.043187079249355664 -0.10964636229731262; 0.08193472480447449 0.028657930755971756 -0.09526264579543231; 0.048571668790267176 0.026803582974096338 -0.09677372355723653; 0.05130061163175575 0.03885875546217573 -0.14350429734778297; 0.024651408011648463 0.02244415153983185 -0.09582924979525494; 0.03979715452053865 0.04081572039872482 -0.1760805398365952; 0.02250891208327938 0.026334508676358476 -0.12433462978660874; 0.005379106886219192 0.008563934523830847 -0.04817231021057636; 0.005736372200535223 0.008205970778898675 -0.028223215378669553; 0.005864809539225689 0.008585676403293633 -0.049489245181077404; 0.005334692165637828 0.006436390185358772 -0.043193549823483834; 0.0005373707722067869 -0.003887802653905726 -0.0031908983316144743; -0.0009419756520945687 -0.0004907700380262815 0.0003858682700847004; 0.0006485276440476735 -0.0026702498929851663 -0.0018103537129513958; 0.0001646746817005818 -4.332430389557512e-5 -0.005980495184572319; -0.0069639522601701994 0.007713434331598261 0.004097206342982618; -0.000882182958638534 -0.0003119151428563668 -0.0002684618512495589; -0.0003049789651761165 -0.003134378671878642 0.0046124449445346435; 0.003944325705418475 0.0020109370903609613 0.005004232826926042; 0.003270504475913241 0.003308780513405306 -0.004766743088474796] %
+
+Mass Used: 91.87641309163064 kg
+Launch C3: 97.04990696260157 km²/s²
+||V∞_in||: 0.0002415528516442545 km/s
diff --git a/archive/ES_0.564003739337264 b/archive/ES_0.564003739337264
new file mode 100644
index 0000000..4627e9d
--- /dev/null
+++ b/archive/ES_0.564003739337264
@@ -0,0 +1,22 @@
+archive/ES_0.564003739337264---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T17:29:38.602
+Launch V∞: [7.762957723692413, -5.363056023319509, 0.5257916724320212] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2337733079512228e-9, -3.6013630889343142e-9, -2.8152936455775355e-9] km/s
+ V∞_out: [-7.241487445987619e-10, 6.349670478357929e-10, 5.170116559016652e-10] km/s
+ time of flight: 1.8749577782360446e8 seconds
+ arrival date: 2030-04-16T19:39:15.602
+ thrust profile: [1.0 0.007091376986758266 -0.2233150596685726; 0.12116518575649021 0.08020615572286588 -0.10618891071969498; 0.07733306655214578 0.08603063234862353 -0.1255909418186787; 0.027690144692917668 0.04336959969570029 -0.0724399817216362; 0.02429128784826399 0.04908517481101814 -0.0882039376561153; 0.01878550992729851 0.05011625242795705 -0.095053318038853; 0.007267256221503503 0.023188389239616844 -0.050210891220317466; 0.004242095063782876 0.018445289170146567 -0.042390524110674586; 0.0022484003032279464 0.010772041263418351 -0.025458202768431384; 0.0006984257947274313 0.005734268363324217 -0.015398700901203956; 0.000285825414185698 0.001183534440401906 -0.0027959478880182176; 0.0009974458087902895 -0.00020041151861637738 -2.6332453090887242e-5; -0.0003543643982801109 6.815427979489001e-5 0.0005985007420322917; -0.0001632680810707383 -0.00028345155784188596 -0.0011745274522821506; 0.00026847057660997 -0.0004562411869680872 -0.0012725725784418602; 0.0011555939863403253 -0.000349367519346331 0.000257164990401083; -3.286996244510434e-5 0.0003204393220678501 0.0015136150421245155; -0.0004596948620513413 0.000691406405535766 -0.0005484915737157272; 0.000709410453395489 0.0007883633050818102 -4.568646662340718e-5; 8.20772557050546e-5 4.582179606421393e-5 -0.0002533829031415211] %
+
+Mass Used: 137.07404932406826 kg
+Launch C3: 89.30233941189823 km²/s²
+||V∞_in||: 4.734753529443814e-9 km/s
diff --git a/archive/ES_0.5640106521534674 b/archive/ES_0.5640106521534674
new file mode 100644
index 0000000..48d7c56
--- /dev/null
+++ b/archive/ES_0.5640106521534674
@@ -0,0 +1,22 @@
+archive/ES_0.5640106521534674---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T17:01:06.685
+Launch V∞: [6.262477080767197, -7.581435319864793, 0.24634889886505945] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0054551983582712075, 0.004191445031648108, 0.005230278788395545] km/s
+ V∞_out: [-0.0036554097903476043, -0.006499473096330514, 0.004367191835534343] km/s
+ time of flight: 1.7769628094839543e8 seconds
+ arrival date: 2028-12-14T09:05:46.685
+ thrust profile: [0.27459648350353494 -0.0871452458061029 -0.09618172761732191; 0.08894467699545999 0.018330756957820347 -0.09154648864089159; 0.07484371379245339 0.03345155470130417 -0.12626604890479262; 0.05958965464947642 0.03647518801459198 -0.1387434077875152; 0.050264644587463665 0.03731551784100027 -0.14811045573370704; 0.028925423321586867 0.024705079105037657 -0.10408618332139954; 0.016651535794802594 0.015923741089577614 -0.07098931727879564; 0.03713548244871898 0.03884219743922555 -0.18393631355329937; 0.0028365944766134453 0.0030798468853481392 -0.01596455930219463; 0.002199296998355471 0.0026917684756575812 -0.013562843644266328; -4.2269102954706444e-5 3.674105501891631e-5 -0.0010674153906844802; -0.00042358654168958527 -0.00013354167720582873 -0.0007984557484647305; 0.000500273332392314 0.000424949390066572 -0.001583246993694601; -0.0016158791643992362 -0.000762410848316022 -0.001665327436218748; 0.00026554611597437894 -0.00011179899009855002 0.00019685678990616004; 0.0008159551084457444 0.0006625235497822094 -0.00039411271598778345; 0.0017156626032437067 -0.000918408768254938 0.0012845761159214527; 0.000214913688057399 0.0003835358085999414 0.0008629098536318959; -1.2244648393764529e-5 -0.0017457300258304621 0.0012983340693353146; -8.651311629938224e-5 0.0004364220197390624 0.0026853385792052625] %
+
+Mass Used: 93.59386140004608 kg
+Launch C3: 96.75746847639985 km²/s²
+||V∞_in||: 0.0086419451968728 km/s
diff --git a/archive/ES_0.5640232636046507 b/archive/ES_0.5640232636046507
new file mode 100644
index 0000000..28d302e
--- /dev/null
+++ b/archive/ES_0.5640232636046507
@@ -0,0 +1,22 @@
+archive/ES_0.5640232636046507---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T21:28:36.143
+Launch V∞: [6.540626712828583, -7.318250073429939, 0.2715110915935849] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6048056034758155e-9, -1.8518255386882444e-9, 2.1608945831550514e-9] km/s
+ V∞_out: [1.107100752662009e-9, -2.567216010529279e-9, -3.4974507919600476e-9] km/s
+ time of flight: 1.8749577787422106e8 seconds
+ arrival date: 2029-04-07T23:38:13.143
+ thrust profile: [0.28433173401923867 -0.0689952310792563 -0.08356268732412236; 0.14979656032229308 0.04779079628115135 -0.13814264612826166; 0.04258656083664275 0.02596340780911524 -0.0690377679587283; 0.055069509682898 0.0456589069561661 -0.1232835849878906; 0.03469790591361931 0.03559555167847807 -0.10183317859880309; 0.01604025410393723 0.01856901261259953 -0.05860656059973569; 0.014932492343759707 0.020012826412417226 -0.06399863644515758; 0.03498781560165957 0.04787767195900935 -0.1501748951903035; 0.011287040010456292 0.018259457946480272 -0.06354312295092195; 0.004642890941802007 0.006392053969285969 -0.02347242999128622; 0.004396039840875526 0.003881723986697324 -0.021636143510134185; -0.0016724873596427963 0.0002017682136724124 -0.0005473046251949657; -0.00015991303007238954 0.00024212207494416632 0.0008912409432807206; 0.001605242342551294 0.0009748734829435777 0.0008146640823380319; 0.000832075977537057 -0.0006289801422244331 -0.0013569696059083595; -0.0016309861328497692 0.0006018100363658864 0.0026412465527381685; 0.0007940144048523027 -0.0008651616277934282 0.001766416700406399; 0.00040783275417495313 0.0018848539730465417 0.0017080936295051081; 0.0019838004173997116 -0.0009513051522827152 -0.003064664679626995; -0.00023396848047956578 5.4018131385820704e-5 -0.00016064438414348952] %
+
+Mass Used: 95.633722999778 kg
+Launch C3: 96.41030020668249 km²/s²
+||V∞_in||: 3.8579444600908724e-9 km/s
diff --git a/archive/ES_0.5640328459054298 b/archive/ES_0.5640328459054298
new file mode 100644
index 0000000..95968e6
--- /dev/null
+++ b/archive/ES_0.5640328459054298
@@ -0,0 +1,22 @@
+archive/ES_0.5640328459054298---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T01:41:27.184
+Launch V∞: [6.594456760990534, -7.455334128977098, 0.023657302951094618] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.39910283282271e-10, -1.7288465171729513e-9, 4.897993142660417e-10] km/s
+ V∞_out: [8.085827770179213e-10, -1.7069882285341744e-9, -2.547097324845965e-9] km/s
+ time of flight: 1.8749577787473476e8 seconds
+ arrival date: 2029-04-11T03:51:04.184
+ thrust profile: [0.151858569355992 -0.03810989172191025 -0.06016713490013901; 0.046556575038740076 0.012436137191437263 -0.06100579955616959; 0.04323739014771267 0.021669248925884076 -0.088970221252358; 0.04549466422029578 0.029962376748017532 -0.12914690096018455; 0.02991843745729204 0.023865212516194927 -0.1087809541114849; 0.0209499976123528 0.018727637578644617 -0.09373864959672855; 0.028242857499916365 0.026576533034227558 -0.14038660011164905; 0.012070375457380876 0.011456452670468343 -0.07162732405422861; 0.004644169653662103 0.004757278569581016 -0.0316309686812406; 0.0052065867548022355 0.006426066720413837 -0.04177414916357839; 0.0031260243335163537 0.0039651475295952405 -0.028407777150181186; 0.001918130406925741 0.0027188797856362206 -0.018870335632417162; -0.0009288307789422205 6.197730995656276e-5 -0.0013545777334986993; -7.154236514738841e-5 -0.0012296639073332573 -0.0030470133735115614; 0.0028213601099721206 0.00023573044739305345 0.0033610345961390094; -0.00029456128408634824 0.0037723103178648795 0.0008978673670916996; 0.0013996022285102635 -0.0015289359915407314 0.002182806316806095; 0.0017174834429819802 -2.257488562657764e-5 -0.0003838892997280606; 0.004288041805170445 -0.0014494515312921288 0.00023978646503339317; -0.006293285975084445 -0.00484888115124578 0.0033574041905867335] %
+
+Mass Used: 80.13333163405832 kg
+Launch C3: 99.0694266152474 km²/s²
+||V∞_in||: 1.9432655185288956e-9 km/s
diff --git a/archive/ES_0.5640359596660192 b/archive/ES_0.5640359596660192
new file mode 100644
index 0000000..54014c7
--- /dev/null
+++ b/archive/ES_0.5640359596660192
@@ -0,0 +1,22 @@
+archive/ES_0.5640359596660192---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T21:00:21.363
+Launch V∞: [6.240087992656974, -7.632748840959221, 0.14147174339226268] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5387982220243366e-8, 5.028758392155307e-9, -7.852288845552702e-9] km/s
+ V∞_out: [2.4927863819096936e-8, -2.2652950450096344e-9, 2.933167867087282e-9] km/s
+ time of flight: 1.8238263353606254e8 seconds
+ arrival date: 2029-02-09T18:50:54.363
+ thrust profile: [0.25777992609204264 -0.07300502930446166 -0.09380603906242845; 0.09082679082661171 0.021789777223190927 -0.10044959856976081; 0.06315562205044356 0.030470643711785553 -0.11816192685335557; 0.05230558063167846 0.03613613112338162 -0.13769789712558766; 0.04395688251006905 0.034521990720731074 -0.13902882514404946; 0.02604858052164477 0.02407022958531734 -0.1067380920911532; 0.01850787547471627 0.017939671281832336 -0.08609915794193707; 0.011579246400905574 0.011363902204220684 -0.059318507405200935; 0.007220587075411266 0.00850134967644411 -0.04324829540756156; 0.007396835743207798 0.010277222457000634 -0.052872352137900876; 0.0021993556969172323 5.547437477222613e-5 -0.0016114662688062598; -0.001049494576382442 0.0014190909875725943 -0.0007156754689901153; 0.0007725131099250767 -0.0001027278352920573 -0.0005667472218916954; -0.0005045618380798474 0.0003729895851580558 -0.004378456563269853; 0.0006821787321879982 -0.0004376424115276668 -0.006565409317954608; 0.0002847464295894278 -6.61467299680799e-5 -0.0025414142646565975; -1.0571330734208267e-6 0.0007228452656387382 -0.0025801608730890335; 0.00011900041855379727 0.001103910408211277 -0.0026439422186263746; -0.0008189418294229046 -0.002281355705521605 0.0025143302770849986; 0.0003211222150250751 0.00021150194932573608 -0.0010939637151400703] %
+
+Mass Used: 90.93947714692922 kg
+Launch C3: 97.21756727944452 km²/s²
+||V∞_in||: 2.704619182613436e-8 km/s
diff --git a/archive/ES_0.5640360497315282 b/archive/ES_0.5640360497315282
new file mode 100644
index 0000000..e2f6c91
--- /dev/null
+++ b/archive/ES_0.5640360497315282
@@ -0,0 +1,22 @@
+archive/ES_0.5640360497315282---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T12:56:30.577
+Launch V∞: [6.207197059997433, -7.634056876449424, 0.04243290187201332] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00017041286740604813, 0.001106414184069169, -0.0014521875243631633] km/s
+ V∞_out: [0.0012076208318620102, 0.001138400082888703, 0.0007783323185971898] km/s
+ time of flight: 1.7950691862916613e8 seconds
+ arrival date: 2029-01-06T03:58:28.577
+ thrust profile: [0.27250697201402835 -0.08386104835376929 -0.10310679817706506; 0.09557234169723167 0.01885704028738739 -0.10789694558137605; 0.09822425061175355 0.04371285263338628 -0.18024878145816; 0.03467306477296498 0.020057463532151838 -0.09097105480443358; 0.0433207889528308 0.03098488427641282 -0.1448022127407283; 0.025879404544219185 0.02067471796882263 -0.10423908931676705; 0.015335089549893117 0.013325873287071275 -0.07230286904645515; 0.016787102397745106 0.01605630222371318 -0.09017162431506415; 0.005846460927698342 0.005900297505366719 -0.034024708769917845; 0.003104251020990119 0.0032389388448009282 -0.020685464585196406; 0.0005540190130244745 0.0009105777707352124 -0.005183497809753411; 0.005732591612081815 0.006599153736542745 -0.04360334161661975; -0.00022743118175814624 5.538617355622626e-5 -0.0005850378694792203; 0.00010489676927970162 9.030495798672738e-5 -0.0011850624856374198; 0.00030959027640528494 0.0002226099100824622 -0.001157223804461401; -0.00010469969967996109 0.00035201668236707314 -0.00017339512267547038; -0.00015811240237270175 6.258164086802827e-5 -0.0011857339764205796; 3.400038143429513e-5 2.0186737436281472e-5 -0.0014711970876319902; 0.0003167484022470065 0.00015464124432203609 -0.0020830119595907975; -0.0015298624880513059 -0.0006061582320423724 -3.3423639829095395e-5] %
+
+Mass Used: 93.31752302039331 kg
+Launch C3: 96.80992028566679 km²/s²
+||V∞_in||: 0.0018335870576558424 km/s
diff --git a/archive/ES_0.5640372635927948 b/archive/ES_0.5640372635927948
new file mode 100644
index 0000000..d681b08
--- /dev/null
+++ b/archive/ES_0.5640372635927948
@@ -0,0 +1,22 @@
+archive/ES_0.5640372635927948---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T14:06:58.012
+Launch V∞: [6.619830243547411, -7.253745553475195, 0.0976394259103016] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.8860263326218765e-9, -1.028351822338567e-10, -5.3268271687552134e-9] km/s
+ V∞_out: [-1.1089669810856666e-9, 2.5080211454255966e-9, 3.4043307512340747e-9] km/s
+ time of flight: 1.8749577777662528e8 seconds
+ arrival date: 2029-04-06T16:16:35.012
+ thrust profile: [0.28050112020376333 -0.061448391449035265 -0.08677902377513906; 0.10929203165423815 0.037787950457655234 -0.10383392027709075; 0.13665880996046656 0.0895581535978136 -0.21724223924674183; 0.041486579503308786 0.036276065291980034 -0.09443527324265333; 0.02884842961990909 0.031205179119865728 -0.08590939443878082; 0.02302453356964812 0.02913590048736738 -0.08447911002160566; 0.017086083081121903 0.02490719938722413 -0.07586691345171923; 0.007545849342106414 0.011996428888117437 -0.0391681709073234; 0.010711035484108088 0.019338910496516752 -0.06372037609789297; 0.007645391650748146 0.014607666773215447 -0.0500593985458822; 0.0001720679840146916 0.00022998558809320742 -0.0005153238208413091; 7.872530512557767e-5 0.00027165841845324523 -0.0016254566334003152; -0.0002195119656047879 0.00019946594283247446 -0.0005530034721404542; 0.0005533345907623198 9.120214652612256e-5 -0.0008140793483012753; 0.0005342357308270348 -0.00011094540250765496 -0.0017296609838258147; 0.0004894218041614316 0.0008935031657382537 0.0001945711112394809; -0.0010492501259768696 5.116840833591042e-5 -0.0002403205075198362; 0.0005022337154410987 0.00013002237506145437 -0.0005153912129789795; -1.0573945017520145e-5 7.384073967019004e-5 0.0004060935073084565; 0.00017022273878460975 -6.209272296992321e-6 0.0010788002090509037] %
+
+Mass Used: 95.42716314320433 kg
+Launch C3: 96.44851046543823 km²/s²
+||V∞_in||: 7.939204541313436e-9 km/s
diff --git a/archive/ES_0.5640453687010499 b/archive/ES_0.5640453687010499
new file mode 100644
index 0000000..e113106
--- /dev/null
+++ b/archive/ES_0.5640453687010499
@@ -0,0 +1,22 @@
+archive/ES_0.5640453687010499---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:45:32.485
+Launch V∞: [6.589602761424919, -7.4291283682155616, 0.2258145423041744] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.737405148370191e-7, 0.00019005487990969187, -0.0001390603166861705] km/s
+ V∞_out: [-0.0001182902493413594, -0.00019915512546990255, 4.185879031034244e-5] km/s
+ time of flight: 1.8749577787430203e8 seconds
+ arrival date: 2029-04-10T20:55:09.485
+ thrust profile: [0.18818157259890783 -0.047344072390193455 -0.07193034111148029; 0.061371658489976805 0.013881367933372682 -0.07073373010433986; 0.03244940131414047 0.01709209731631606 -0.06743276745351692; 0.027499032817128715 0.018851106654342715 -0.07871932845848217; 0.0297625632252075 0.02565119380817988 -0.10705204631840409; 0.01873464475723241 0.015396975003224055 -0.0813758976332955; 0.036434005699059004 0.03797799102245264 -0.1882374911825704; 0.009045008670765898 0.010280432938699296 -0.06088070771193098; 0.00898872453299512 0.0071772924293237355 -0.04471832883201508; 0.010593891673034986 0.01198251273691267 -0.07702969040161262; 0.001845733585431043 -0.00013430102301066724 -0.003309917373439203; 0.0021758233501468723 0.004836699103556108 -0.01886163316810415; 0.0033117423620995135 0.0016762146333334812 -0.0055454061519540875; -7.638789575378996e-5 0.0010101426357181794 -0.005486621572129554; 0.0016400900038122967 -0.0005253595246176347 -0.0026758246403541866; 0.005447953736832149 -0.00146653730817736 -0.0019442522532861616; -0.00035759691589586106 -0.0044028214281904504 -0.0034515387934825545; -0.004641518801186145 0.0030067451483585133 0.0031344727688829895; -0.0016752209623111922 -0.0005689348398757404 0.001645013323417643; -0.00030767515915739764 -0.00017863854177120402 0.00010058730858205711] %
+
+Mass Used: 82.50240056269058 kg
+Launch C3: 98.66580507232017 km²/s²
+||V∞_in||: 0.00023549725737792319 km/s
diff --git a/archive/ES_0.5640478783497895 b/archive/ES_0.5640478783497895
new file mode 100644
index 0000000..f993dd9
--- /dev/null
+++ b/archive/ES_0.5640478783497895
@@ -0,0 +1,22 @@
+archive/ES_0.5640478783497895---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T22:23:27.018
+Launch V∞: [6.3505090034192895, -7.623605011226313, -0.057294900917272365] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.022612422491110343, -0.009809702008701895, 0.025608561908763632] km/s
+ V∞_out: [-0.022503877229369966, -0.00892876391824352, -0.026015279423762607] km/s
+ time of flight: 1.7600496750315952e8 seconds
+ arrival date: 2028-11-25T00:39:34.018
+ thrust profile: [0.13752017190958588 -0.05331097273428221 -0.057056745575879406; 0.09032466320822628 0.011432440862372077 -0.10251853189875874; 0.07529693143157745 0.025010491714275766 -0.14111210477651492; 0.06330759737718246 0.028985617114822695 -0.16376626230999525; 0.04792659998481582 0.0264131783943666 -0.15779393966081806; 0.0344326691711356 0.02141992934891224 -0.13653454552460878; 0.02145827154979882 0.014705659262892027 -0.09968462405824295; 0.009399483350862362 0.007013742702566135 -0.05028004028770521; 0.005970919564844315 0.004746840703137653 -0.03571145922452878; 0.004695997249236956 0.0038887059079975262 -0.030661777576008773; 0.0022107432729603443 0.0019171173155722995 -0.015910417883105994; 0.00021419028360260481 0.0006669265761569862 -0.0057398189028138496; 0.00016246832352460885 0.0002582547696500364 -0.0014812311815417703; -0.00015598964975377304 -8.625029301068907e-5 0.0001653706938773826; 3.439167395241032e-5 -0.00017603171097490254 -0.000556528081963009; 0.00012911514432936455 4.4232421231334894e-5 -0.0003360025612436665; 0.0007340099109547796 7.92736714907023e-5 0.00026839835840972647; 0.000629542679953997 0.0004429690243439037 0.0009207234859508924; 9.664739941290975e-5 0.0005695301010674465 -0.0007837798391612847; 0.00043057449187305994 0.00014704904751199202 -0.00015252597919214038] %
+
+Mass Used: 83.75485413506385 kg
+Launch C3: 98.45160067537553 km²/s²
+||V∞_in||: 0.03554364004222109 km/s
diff --git a/archive/ES_0.5640588899455761 b/archive/ES_0.5640588899455761
new file mode 100644
index 0000000..138201a
--- /dev/null
+++ b/archive/ES_0.5640588899455761
@@ -0,0 +1,22 @@
+archive/ES_0.5640588899455761---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T18:09:49.298
+Launch V∞: [6.383545063811219, -7.244331284510195, 0.16101798884992588] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.276218695760804e-5, -3.431375223347374e-6, 5.81014989999201e-8] km/s
+ V∞_out: [4.55209659314789e-6, -9.785126777189198e-8, -2.256277649989422e-5] km/s
+ time of flight: 1.8749577787335575e8 seconds
+ arrival date: 2029-04-06T20:19:26.298
+ thrust profile: [0.5741236971715851 -0.1356667820737412 -0.14308477984749463; 0.09709847303659494 0.03285711174797787 -0.0905456946890133; 0.06976114019474791 0.04448614149720309 -0.10995987098449474; 0.026041164706744297 0.023673436945784436 -0.06259178772324274; 0.03788476022430253 0.041283925068663824 -0.1117663873590286; 0.023756646307596347 0.03037966941986565 -0.09085881304738663; 0.04632513456549115 0.0691353018843801 -0.18129015956061928; 0.009169025400715387 0.0142183574634955 -0.04850574385414972; 0.0035643677122297493 0.006353469075600519 -0.021691702837613517; 0.001407454037633799 0.002627499913005189 -0.009640846527426675; 0.006422001513442996 0.01413896985396244 -0.047035106377649266; 0.0011169897137224727 -9.086488424208164e-5 -0.0014566290033065045; 1.6978640968633678e-5 0.0007915273915877491 -0.0032713350763609547; 0.0023153846567467587 0.000705241734432851 -0.001955490196434393; -0.0007029714862580201 0.0010659944916296526 -0.00041090203046486706; 0.000986376850357966 0.0023793637040768045 -0.00030259482465717734; -0.0003691485048844868 0.0006443514570771766 -0.00045923871994271617; -0.0018684894976972852 -0.0005759716689967554 0.0004926637907418565; -0.0001404508478446072 -0.0010701567832890149 0.0008164814333793055; -0.0008658832851984226 -0.0004514378160086962 0.0006073129903737011] %
+
+Mass Used: 114.07589582048467 kg
+Launch C3: 93.25591013417498 km²/s²
+||V∞_in||: 2.301944540601901e-5 km/s
diff --git a/archive/ES_0.5640616009123496 b/archive/ES_0.5640616009123496
new file mode 100644
index 0000000..b1ef6ee
--- /dev/null
+++ b/archive/ES_0.5640616009123496
@@ -0,0 +1,22 @@
+archive/ES_0.5640616009123496---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T07:45:08.947
+Launch V∞: [6.594321512017348, -7.41660190193157, -0.4447381810219444] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.068486153699382e-7, -3.7873158468366354e-6, 2.1656902822589589e-7] km/s
+ V∞_out: [-1.4947278784617289e-6, 3.317972204623495e-6, -1.165438959452281e-6] km/s
+ time of flight: 1.8592124596368083e8 seconds
+ arrival date: 2029-03-22T04:32:33.947
+ thrust profile: [0.15332546891714552 -0.04110465557913083 -0.061741803789099894; 0.07010226889988544 0.018373558258820425 -0.08539892781800788; 0.06368247689997987 0.03260592671463216 -0.1276539651859941; 0.05608605997355387 0.03906909740224403 -0.1573810789437334; 0.04187098150737875 0.03441832159025581 -0.15187301581594972; 0.025084757952030225 0.024362669032756277 -0.11303060573447997; 0.012988094303184925 0.014446095977566265 -0.0709811644448936; 0.005080743458050931 0.006547222075799495 -0.03534331831845947; 0.006282665628778887 0.008827853352093422 -0.047451733345781545; 0.004731308136033809 0.008774412553956116 -0.04631238923478213; 0.0002733375187258976 0.0005660604064179962 -0.004194590991009061; 0.00033751746296238594 0.0002397395170236176 -0.001855596567401664; 0.0017828276530129114 -0.002979122212901161 -0.0028701602628311155; -0.00028430203592603933 -0.0001458080511117139 0.0013112113082538344; -0.0012316379015269692 0.0004691526464801011 0.0009947996903650518; -0.0002508487768296528 0.00011340373901426058 0.00012348131677219847; 0.0017330210439903846 -0.0011275383052124586 0.004457341759875669; -0.0012628791478101896 0.0005591694145691469 0.0012784629021525662; 0.0003617366257623594 -0.0001257442190837468 0.001172279525676759; 0.00017255584012187053 -0.0047926231969286515 0.0017847141686638433] %
+
+Mass Used: 82.38689758379178 kg
+Launch C3: 98.68885202524847 km²/s²
+||V∞_in||: 3.82721295286649e-6 km/s
diff --git a/archive/ES_0.5640742877146614 b/archive/ES_0.5640742877146614
new file mode 100644
index 0000000..ff0481f
--- /dev/null
+++ b/archive/ES_0.5640742877146614
@@ -0,0 +1,22 @@
+archive/ES_0.5640742877146614---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T15:32:16.099
+Launch V∞: [6.407629593864739, -7.396512016794931, -0.13616705087792563] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9761366034049372e-5, -2.786321428521858e-5, -3.067108838871358e-5] km/s
+ V∞_out: [-4.270093773696331e-5, -2.7884628188444763e-5, -9.022589086033898e-7] km/s
+ time of flight: 1.874957778754638e8 seconds
+ arrival date: 2029-04-09T17:41:53.099
+ thrust profile: [0.3781649732742117 -0.09278684032049898 -0.12782100956017958; 0.09273104529075846 0.027047578423358625 -0.10302751306930023; 0.03763850888550503 0.020578959366804317 -0.07218279766654842; 0.06083412400938838 0.04526178474846787 -0.15820321841690532; 0.026627094278581325 0.023924269118625933 -0.09224324546368164; 0.03279231346599286 0.03455751716559756 -0.13797484285093767; 0.021031274497460426 0.024362767620108264 -0.1053859823592349; 0.009620170862597678 0.012161914553382188 -0.05615392861034951; 0.002817369963547074 0.003515320726694293 -0.02022200137390667; 0.0038244010233992537 0.004658814775093549 -0.02309239604745412; 0.003139799212082652 0.005091113543513516 -0.024298425225623255; -0.0013272928450142575 0.00039416972896321747 -0.0022888465547571406; 0.00044846415734871097 -0.0010684259923745341 -0.00033638070137271327; -0.0002966628383278396 0.0004684853922394285 0.0014643150632646707; -0.0022005850122350777 -0.0007272212885380317 0.0015718788194686688; 0.003677449637963193 0.0012159007040059397 0.002182697865760597; 0.007160884812914994 0.0015004553011035272 0.0010849785821761217; -0.004675111366912562 -0.0019691487771536973 0.0022668918609363266; 0.0036226606682507228 -0.002380250801695841 -0.0012447307641340088; 0.0009897409429820592 0.0013607648441320052 -0.006837191634736186] %
+
+Mass Used: 99.34288612747605 kg
+Launch C3: 95.78464849250781 km²/s²
+||V∞_in||: 5.101777417199772e-5 km/s
diff --git a/archive/ES_0.5640770611649363 b/archive/ES_0.5640770611649363
new file mode 100644
index 0000000..a126397
--- /dev/null
+++ b/archive/ES_0.5640770611649363
@@ -0,0 +1,22 @@
+archive/ES_0.5640770611649363---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T19:35:40.623
+Launch V∞: [6.5271182011520175, -7.548191486468986, -0.02484579628156945] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010488164345899853, -0.0003439440272939692, 0.004332891103193977] km/s
+ V∞_out: [-0.010876163518667692, 0.00011172566709996238, 0.0032541329132978326] km/s
+ time of flight: 1.840724994974878e8 seconds
+ arrival date: 2029-03-02T06:50:39.623
+ thrust profile: [0.10310439512511879 -0.03239133305809724 -0.0469840306875757; 0.07170087099418472 0.010146723503452035 -0.09791862246294557; 0.043807882308213475 0.015428973883552292 -0.10398709329910598; 0.03836223391321025 0.017312241668378414 -0.12612677561294935; 0.040148915600118094 0.023340559935826996 -0.1651036008883576; 0.023036031987074972 0.013616681481741577 -0.11772089645694553; 0.025745585512520968 0.014985084812666943 -0.14548341632672374; 0.008570466595954796 0.005469653524701094 -0.058709171408578696; 0.0030339235650663847 0.0025897359360390667 -0.02090558620259316; 0.001993157297351838 0.0008343305921750547 -0.011503337190888464; 0.0006051473441442388 0.0005107830563590026 -0.0024932154771905787; 2.5588515112271793e-5 0.0004937169904905589 0.0003585307276176711; 0.0009676400043934242 -0.0015044617336311197 0.0033637191401333687; 0.0024148383849398533 -0.002598673114070768 0.0011460286822289945; 0.000928078333584648 -0.0011606862290973895 0.00014308438807524937; 0.0013332516869760406 -0.0021084861923079392 0.0012790337748584285; -0.003135324668067938 -0.0038760593220047526 0.0027797332585525036; -0.0003113124939404932 0.004191490339332884 0.0012297802792997417; -0.0012261415277118831 -0.004138205100028004 -0.0016564211991458861; 0.002894920781137687 -0.0010358505777912411 -0.0023441851824260664] %
+
+Mass Used: 77.21191444855913 kg
+Launch C3: 99.5790840418057 km²/s²
+||V∞_in||: 0.011353142038777355 km/s
diff --git a/archive/ES_0.5640827304218567 b/archive/ES_0.5640827304218567
new file mode 100644
index 0000000..61d167e
--- /dev/null
+++ b/archive/ES_0.5640827304218567
@@ -0,0 +1,22 @@
+archive/ES_0.5640827304218567---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T06:40:12.490
+Launch V∞: [6.53162444648191, -7.184214554600599, 0.25961040202331254] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.923511140709069e-8, 5.9505989794044766e-8, 3.3742494210919705e-8] km/s
+ V∞_out: [-1.9292233097427106e-8, 4.024852189570082e-8, -6.023255430025979e-8] km/s
+ time of flight: 1.8749577787482104e8 seconds
+ arrival date: 2029-04-06T08:49:49.490
+ thrust profile: [0.4918706909136068 -0.12039034649393135 -0.15461829958987194; 0.10076384798986833 0.030993680730471693 -0.1012710052333492; 0.0830264420121426 0.04876277568323525 -0.14033930027978647; 0.06093419429317897 0.04852907200310056 -0.14559873435467297; 0.042593416095124854 0.041444108955454535 -0.13240440537332104; 0.02716861002938457 0.030588395591236706 -0.10422516611803; 0.008455006822118485 0.01157627644301262 -0.04041520764050387; 0.004888858554845208 0.0077639183441881605 -0.028594790297651496; 0.003932030833257962 0.006672012736007662 -0.026161202616653417; 0.004058871054953782 0.007078791926674244 -0.028579394394696585; 0.0026993674223442896 0.00045728046860412454 -0.015162341142989737; -0.00046644917089732696 0.0034057704822127565 -0.004553546801655387; 0.000877545494178698 0.0018701070820905594 -0.0010223271884867602; -0.00020143499705247434 -0.00031122365823601584 -0.0033089049264798265; -0.003544675087551406 0.0005270149346268753 -0.0033379816344500535; 0.0003992708369493376 -0.0005006929972991165 -0.00013837308221261108; 0.003190895665033778 0.0007584479063093736 -0.0015473054318090311; 0.0005191815509538017 8.14735231389925e-5 -0.004443696388360842; 0.003725835784503589 -0.002045942526886929 0.00010355183479663428; 0.0007872502555526582 -4.8039205183907725e-5 7.150521327481266e-5] %
+
+Mass Used: 107.76553577485174 kg
+Launch C3: 94.3424542372539 km²/s²
+||V∞_in||: 7.439227430269835e-8 km/s
diff --git a/archive/ES_0.5640930749246753 b/archive/ES_0.5640930749246753
new file mode 100644
index 0000000..775f0a5
--- /dev/null
+++ b/archive/ES_0.5640930749246753
@@ -0,0 +1,22 @@
+archive/ES_0.5640930749246753---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T19:44:26.779
+Launch V∞: [7.971476193215301, -5.771900552148006, 0.19517227152608538] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6824863633729213e-6, -2.5021843510213203e-6, -2.449159432942545e-7] km/s
+ V∞_out: [1.4671022435771354e-7, -8.046591031415728e-7, -2.909932986553821e-6] km/s
+ time of flight: 1.790975240959225e8 seconds
+ arrival date: 2030-01-11T17:03:10.779
+ thrust profile: [0.3062825999270646 -0.0070350593883877635 -0.08326822942961062; 0.08180035206546332 0.05232041867319175 -0.0843402360862352; 0.04689709732166677 0.04906067593373359 -0.0859443842968228; 0.03265734697575214 0.04759773770631109 -0.09084611103306749; 0.024057015604924514 0.04585591661083703 -0.09432307789533396; 0.017561216312349234 0.03585959774514635 -0.08666039036655021; 0.018998039659380423 0.04780048434802932 -0.12207861689044934; 0.008532280038197367 0.02425568354645239 -0.0687038459923063; 0.013075130238739513 0.04513955010262265 -0.1140060798143528; 0.0038940080673832717 0.004545140923290681 -0.016381305710920877; 0.0007398329535229166 0.007799271020063298 -0.029840320276602373; -0.002468881782446852 0.0010617359465082306 -0.007753560070592907; 0.0006125149011704531 -3.8129895899283606e-5 -0.0032892211022764713; -0.0028200749707357827 -0.0029911824648150244 0.0029225066866620394; 0.0004095728283669336 0.004809000198387476 -0.0014149654577115516; 0.004013132791500004 0.007002272748668113 0.0013691021657903889; 0.001097806313978135 0.00018447431537713934 -0.006195335327024416; -2.3976986217103848e-5 -0.0007482677783592381 -0.0038895067557175866; -0.0016689773642068655 0.0006428597690334931 -0.0005625538766840312; -0.01586904724767256 -0.0035539229480338885 -0.003676564676941013] %
+
+Mass Used: 92.87398217111968 kg
+Launch C3: 96.8973608984574 km²/s²
+||V∞_in||: 3.025172839477364e-6 km/s
diff --git a/archive/ES_0.5640947980833085 b/archive/ES_0.5640947980833085
new file mode 100644
index 0000000..0f38c63
--- /dev/null
+++ b/archive/ES_0.5640947980833085
@@ -0,0 +1,22 @@
+archive/ES_0.5640947980833085---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T11:08:27.250
+Launch V∞: [6.642708480155754, -7.265197389809125, 0.31361773754661887] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.868528714784667e-6, 4.062542695570741e-6, 5.075156628875213e-6] km/s
+ V∞_out: [6.646422067404424e-6, 4.6650146842112845e-6, 1.504466036506955e-7] km/s
+ time of flight: 1.8749577787334847e8 seconds
+ arrival date: 2029-04-07T13:18:04.250
+ thrust profile: [0.26700477981777393 -0.06137076374721456 -0.09357065804400332; 0.08435723608200602 0.026341364504988037 -0.08870639795268892; 0.100669136400886 0.06058257091147558 -0.1769390379947019; 0.0457315473913161 0.03569747940202966 -0.11243279606222892; 0.055186385377608345 0.05512836123965052 -0.18049744567302659; 0.02828329046392476 0.03135013981768618 -0.11143014726347904; 0.012306408783191069 0.015415081731996426 -0.0586660682498524; 0.006378333541924213 0.008658773662785663 -0.035538755264586615; 0.002337529726680892 0.003381277607520672 -0.013239058708721501; 0.001347805498890299 0.0020531746366506416 -0.009744525686180689; 0.0008845463080845165 0.0010530779236318356 -0.003818802945543946; -1.5423404239696226e-5 -0.0011256932656932154 0.0040136962472257405; 0.0001269261202100018 0.0009903606707895645 -6.230156028532233e-5; -0.0006145561845251545 0.0017242671485007213 0.0032908516159554117; -0.0006460868149960516 -0.0015154711840768707 -9.849000741401007e-6; -0.0012069780848988037 -0.00421703036256194 -0.0009226392876792062; 0.0004392018451481589 0.005190731074485025 -0.003905531930780954; 0.0008363486947245778 -0.004959629705620592 0.0016955241369736348; 0.0046274687725751 -0.008480036182657729 0.004541016926247799; -0.0010136106260991823 0.0010334003907063035 -0.00013631154783296353] %
+
+Mass Used: 92.23628438578953 kg
+Launch C3: 97.00702515052636 km²/s²
+||V∞_in||: 8.12182490624084e-6 km/s
diff --git a/archive/ES_0.5641009406900314 b/archive/ES_0.5641009406900314
new file mode 100644
index 0000000..4924154
--- /dev/null
+++ b/archive/ES_0.5641009406900314
@@ -0,0 +1,22 @@
+archive/ES_0.5641009406900314---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:52:18.901
+Launch V∞: [6.447622433796157, -7.463513458512962, 0.16221984506423678] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.77887614061141e-7, 4.981384737005594e-6, -2.421676434150568e-7] km/s
+ V∞_out: [1.8657164785269015e-6, -4.0399505405900525e-6, 2.325826062219001e-6] km/s
+ time of flight: 1.829557553003994e8 seconds
+ arrival date: 2029-02-16T03:54:53.901
+ thrust profile: [0.298314020194168 -0.11064197634555768 -0.12579347176401393; 0.06810033966228327 0.006302302621738008 -0.08883977771990648; 0.045416747111990854 0.011529614141251284 -0.10331557943578548; 0.022974300279062478 0.007680283939756871 -0.07122939459585186; 0.023749828130498248 0.009112591917259015 -0.09397563237981477; 0.037220780965963804 0.015923549360251383 -0.19628035586267778; 0.025029443451705307 0.010844767456164856 -0.14462391654324788; 0.008087683541233926 0.0033596925472633176 -0.04696591858290778; 0.004034819191508233 0.0017795879957887772 -0.02649873250530335; 0.0028593134085622743 0.0013146431468654186 -0.02125070568383278; 0.0034322374904896817 0.0014040791179198622 -0.026624029901833258; 0.0011375807437322958 0.00045903971122012506 -0.0073542599786016565; 4.089143823132849e-5 -8.367488957564551e-6 -0.000522817438010081; -0.001290145930028017 -0.001907658919346666 -0.0011111258605153891; -0.0014030992090782542 0.00044266299858766815 0.0011952837145645925; -0.001182211024204402 -0.00021033870481239876 -0.00479756345096106; -0.0011049909236358125 -0.0020170010668404117 -0.0014307858909453621; 0.0008912611248332338 -0.0004052429001545302 0.00019978714526367987; 0.0007843185957573667 -0.0006547130513921799 -0.002195201122163495; -0.006941361847612747 0.004265151691132642 -0.0006082386306349597] %
+
+Mass Used: 90.52169388312177 kg
+Launch C3: 97.30218347232827 km²/s²
+||V∞_in||: 5.0206367285509484e-6 km/s
diff --git a/archive/ES_0.5641036274459091 b/archive/ES_0.5641036274459091
new file mode 100644
index 0000000..fb44e58
--- /dev/null
+++ b/archive/ES_0.5641036274459091
@@ -0,0 +1,22 @@
+archive/ES_0.5641036274459091---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:48:00.845
+Launch V∞: [7.348273945951938, -6.460766348678764, -0.054926928404966706] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004953739306779527, 0.00030795457567501584, -0.00014191676276925177] km/s
+ V∞_out: [-0.00024502568894280125, -0.0004561662100450902, 0.00030285234707163634] km/s
+ time of flight: 1.635897703725428e8 seconds
+ arrival date: 2029-07-16T13:24:10.845
+ thrust profile: [0.39774932212714786 -0.061861688761675214 -0.143228676112201; 0.11846366885276091 0.04226669403949576 -0.13394514812898187; 0.05967159052253965 0.03664463033751842 -0.11598094110883661; 0.050724598061590576 0.041752986524995005 -0.141364717364935; 0.05163695620027536 0.051172882647427226 -0.1872630097689002; 0.03437274937491379 0.03723238936751126 -0.14388720303379302; 0.015693042539878355 0.018851596869001685 -0.0821528304610904; 0.013842116937751623 0.01758964483923526 -0.08121540391668752; 0.01035829175815624 0.01412631116497893 -0.06401551414013743; 0.003105585224477411 0.0037681611948442583 -0.02226141691602891; 0.0002099554339309204 0.00018890498197158488 -0.0015660894642700331; 0.00021105716280219833 0.000484078576161919 -0.0021060931335466293; 0.00024302374281704605 0.00025748414441342066 -0.002158460162436247; -0.00010491285637160338 0.0003921981165140283 -0.0010337398643660192; -0.00040101801210110685 0.00026261202352814163 -0.0002778105650228786; -0.00021693129182821043 0.000305144383661632 0.0004015982104277672; -6.185021730370076e-6 -0.0003401582948448856 -0.0015055930911589918; 0.00018220842516012266 -0.0003873440663555343 0.0007663301976013695; 0.00177236901434784 0.000801556023489155 0.0013832393922604646; -0.00010875031218826646 -0.00024340990717436188 0.0015194754642257743] %
+
+Mass Used: 99.62794756099402 kg
+Launch C3: 95.74164876444 km²/s²
+||V∞_in||: 0.0006003096862698521 km/s
diff --git a/archive/ES_0.5641049380456489 b/archive/ES_0.5641049380456489
new file mode 100644
index 0000000..3cf6099
--- /dev/null
+++ b/archive/ES_0.5641049380456489
@@ -0,0 +1,22 @@
+archive/ES_0.5641049380456489---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T08:28:12.332
+Launch V∞: [7.406614639676723, -5.835740903092739, 0.40694187960483885] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.432024112319213e-6, -3.0793808674847407e-6, 3.7618386479976534e-6] km/s
+ V∞_out: [-7.502905481514022e-7, -5.890676546001928e-6, 2.755952969418992e-7] km/s
+ time of flight: 1.8117996295046648e8 seconds
+ arrival date: 2030-02-03T08:14:14.332
+ thrust profile: [0.8688427821911628 -0.013273120163424558 -0.15165704961655405; 0.1817697963184269 0.12249659224685756 -0.14289762668567196; 0.07252915880845248 0.08320845521195072 -0.10930842256011396; 0.040210712281384196 0.06834201457251984 -0.09799719500011239; 0.040902115587617444 0.08408530589308955 -0.12592122063771047; 0.02778056273769051 0.07232732763462406 -0.11806381656070204; 0.013553283983121054 0.043746265245283536 -0.07874225749355618; 0.005257286670512628 0.02217459331291634 -0.04320120358806743; 0.0021031263114823498 0.008905879980515716 -0.019773513932179757; 0.0006044588358142854 0.0006948821462937206 -0.0024649051956412977; -0.00016049139411694293 0.0004371414020753516 -0.00021157032925277685; 0.0007874352084549532 -0.0009593432323538043 0.0020669959227931634; 0.00023085196248414747 -0.001348746676643022 -0.0008348560716608878; 0.0023503741318158197 0.0005482991797981651 0.000157477373511744; -0.0013631215991071093 0.0013525415677385771 0.0017965562441880564; -0.004104090174643606 -0.0009423574879178174 0.0008806415574085623; -0.003373228501998041 -0.005625665769132812 0.0011975093555343693; 0.0005033132633104029 0.0003142883765834949 -0.0005289969269109615; -0.004847679688686318 0.0014772481207572066 0.005497936544639; -0.0001148257469504157 0.000776546155056423 0.0031948768305867146] %
+
+Mass Used: 138.49251270779314 kg
+Launch C3: 89.07941400207953 km²/s²
+||V∞_in||: 5.95086599144531e-6 km/s
diff --git a/archive/ES_0.5641108442838277 b/archive/ES_0.5641108442838277
new file mode 100644
index 0000000..519ba2d
--- /dev/null
+++ b/archive/ES_0.5641108442838277
@@ -0,0 +1,22 @@
+archive/ES_0.5641108442838277---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T07:35:13.154
+Launch V∞: [7.5552757193707984, -6.3393210621067535, -0.06469674945061378] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.870866112589435e-9, -4.619400890263314e-9, 1.6288281062805902e-8] km/s
+ V∞_out: [4.555977911173451e-9, -1.4678902831965297e-8, 2.2767136016014763e-9] km/s
+ time of flight: 1.6391094774606353e8 seconds
+ arrival date: 2029-07-19T10:24:20.154
+ thrust profile: [0.2596193610415938 -0.04770629085268989 -0.09737167422812196; 0.06583593050261377 0.021173737656731164 -0.07545750844919462; 0.08192150710738383 0.04668048518010182 -0.1561749800827251; 0.08795792859649793 0.06537480142474324 -0.23393363082171897; 0.05333962677696659 0.04700138793762766 -0.1846696976391216; 0.03500451548147785 0.03471622227222937 -0.14711893545561036; 0.01721174714700398 0.018530119894995565 -0.08718957988542424; 0.005730579564539583 0.00665934915548127 -0.035369666055267625; 0.004654986386824402 0.005568067456537104 -0.030948507401698647; 0.00014218324439185099 0.002478950600748836 -0.004692462401689113; 0.00232160318602052 0.00334634539483935 -0.016617825588021842; -0.0002424995285709685 -0.0001358303537029443 -0.0041620525713902045; 0.002108355917658187 0.00037220330258161253 -0.002072420283142211; 0.0010711081359655067 0.00021326462707242207 -0.0005155961312378727; -0.0019479508690723036 0.0014147247247490533 0.0010011833769716658; 0.0011422464851163629 0.0019895675241257795 -0.0010205774115371008; -0.004180985871360353 0.0029661217048277465 -0.0006769348012088134; -0.0009101542994690878 0.0003517052507181261 -0.004318294479541749; 0.002067132627334229 0.002017890351376506 -0.0009596922686565144; -0.0002842210811255096 -0.0034855494291455807 0.0030112584602125215] %
+
+Mass Used: 90.70133603528575 kg
+Launch C3: 97.2733683935737 km²/s²
+||V∞_in||: 1.703370495744136e-8 km/s
diff --git a/archive/ES_0.5641181765353954 b/archive/ES_0.5641181765353954
new file mode 100644
index 0000000..71684b1
--- /dev/null
+++ b/archive/ES_0.5641181765353954
@@ -0,0 +1,22 @@
+archive/ES_0.5641181765353954---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T01:32:31.515
+Launch V∞: [6.410461663624322, -7.530081990809689, 0.062022252265686584] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.256505464322492e-9, -4.815557507055808e-9, 1.3804683866767938e-8] km/s
+ V∞_out: [4.4820896896121506e-9, -1.0137871799833259e-8, -1.3359176894122823e-8] km/s
+ time of flight: 1.786125821901683e8 seconds
+ arrival date: 2028-12-25T08:08:53.515
+ thrust profile: [0.23164772331612704 -0.07668994301704611 -0.0893774384342413; 0.04753381499161748 0.00915896699538019 -0.0546074589366334; 0.042505836440821045 0.017563884639349943 -0.08141695409803859; 0.053509963997808434 0.03005859476394403 -0.13949621595876596; 0.06431691267784825 0.0433653318076429 -0.20277720440242497; 0.036163465404280455 0.02818382244940555 -0.1443192282736444; 0.02526717788952381 0.022429470500910004 -0.12273756014855411; 0.008649183215155553 0.008368194292708476 -0.04618598483384489; 0.01103484556140641 0.010559454743815484 -0.06754796264633768; 0.0007072663621299788 0.0005345990393654038 -0.006942133064532663; 0.0006771695139424802 0.0008772218378250568 -0.0037541967589671383; 0.0015699852744660832 0.0014828597889114154 -0.004209162818717779; 0.00024150311249788629 8.82827177498181e-6 -0.0003847404589159187; 0.001141024098754871 -0.002201844985965804 -0.0014602433337328694; 0.000734489400228743 0.0004219034947329644 -0.003021469380509528; 0.00015788290708339286 6.752605361544936e-5 -0.00122294685341046; -0.0017382517314838868 0.003361294711481065 0.0009745250649569747; -0.0006586832292696353 -0.0001692800934668025 -0.0005688930644932187; 0.002470892227521016 -0.007474629889797124 -0.002021204001744916; 5.123929546555059e-5 -0.0016505584490205411 0.004057349988089417] %
+
+Mass Used: 87.63787093943847 kg
+Launch C3: 97.80000028888963 km²/s²
+||V∞_in||: 1.730438626985068e-8 km/s
diff --git a/archive/ES_0.5641193830061901 b/archive/ES_0.5641193830061901
new file mode 100644
index 0000000..4370d31
--- /dev/null
+++ b/archive/ES_0.5641193830061901
@@ -0,0 +1,22 @@
+archive/ES_0.5641193830061901---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T20:59:43.151
+Launch V∞: [6.538814003951022, -7.419214083757594, 0.2160127928885222] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002600366624702003, 4.261957479668634e-6, 4.76616653027136e-6] km/s
+ V∞_out: [0.0002194313093123933, 0.00013960424115428116, 4.514417587872786e-6] km/s
+ time of flight: 1.8575890004591522e8 seconds
+ arrival date: 2029-03-19T20:41:23.151
+ thrust profile: [0.17693236119124753 -0.0486091717449235 -0.06401275555883985; 0.05152767039749928 0.012786184365006083 -0.056163762311565814; 0.1787146865310236 0.08474193669531624 -0.3179414686457044; 0.03722540820357955 0.024572705206368593 -0.09502406530289532; 0.03463833316406646 0.027438407056464498 -0.1126480552677961; 0.024024150678977375 0.02173106859383753 -0.09505514564029584; 0.015726209540795684 0.01582219621225916 -0.0736548508699582; 0.004753948067425629 0.004997008400072846 -0.02587501314140612; 0.002265246799386837 0.001959025989793365 -0.01526046440550029; 0.00036431545309672153 0.0059894026138155206 -0.005860611330600559; 0.00019354871737840813 -0.0004997190028353232 -0.0021614538112212783; 0.0011602914693354892 0.004387448666516024 -0.018061383125577306; -3.20508209348334e-5 0.0003355423030929319 -0.002635212663058474; -0.002928186957962978 -0.0006631419395494151 -0.005997877863484051; 0.0005885685294897529 0.00046852064714123583 -0.0036311796902515525; -0.0001019798127115725 -0.007577835822153808 -0.008688148392512113; 0.011845057796258206 0.0031473681111499952 -0.003119347597500388; 0.0033457515853595604 0.0007632920166408807 -0.009562857438618637; 9.533650949109678e-5 0.00012926843401226123 -0.0009249086075401132; -0.002559498928798382 -0.0023480621551666835 0.011231237342592569] %
+
+Mass Used: 87.36226844131215 kg
+Launch C3: 97.84748772558451 km²/s²
+||V∞_in||: 0.00026011525609543484 km/s
diff --git a/archive/ES_0.5641267574152299 b/archive/ES_0.5641267574152299
new file mode 100644
index 0000000..d293c89
--- /dev/null
+++ b/archive/ES_0.5641267574152299
@@ -0,0 +1,22 @@
+archive/ES_0.5641267574152299---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T10:56:33.728
+Launch V∞: [6.620923270091344, -7.363680009866871, 0.16957086118124323] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9036739177764725e-5, -2.6952685909193734e-6, 4.774977722506051e-8] km/s
+ V∞_out: [3.762667252241901e-6, -8.53594452514974e-8, -1.8855155486861947e-5] km/s
+ time of flight: 1.8749577787493348e8 seconds
+ arrival date: 2029-04-09T13:06:10.728
+ thrust profile: [0.21028111215908707 -0.05179214019892952 -0.07430479392096413; 0.05247210565727179 0.01475415674019874 -0.05839757530444007; 0.062445752852383456 0.03335613765209295 -0.11463059004255725; 0.04497618112935446 0.032823235025732624 -0.11961894685061064; 0.03249244552916564 0.029131663932382115 -0.11022309065548504; 0.034837843287420504 0.03453118617487818 -0.14038189093280823; 0.01554669718111552 0.01715377772637569 -0.07451865090398835; 0.007467221428490347 0.0088269531155654 -0.04314069880834536; 0.0062961711988812515 0.008969833360607549 -0.04302035938722725; 0.011959196727057177 0.017043632254586112 -0.08366461532332604; 0.001189117017743487 0.001066313203569261 -0.006263279792667805; 0.001456777915050591 0.0016343778006304502 -0.005030311470514479; -0.0022346821210998905 -0.0008647992832948825 -0.003126314411768011; 0.0002569799131795198 0.0006253708447925466 0.0024494046865362975; -3.5587020440253456e-5 -0.0001620768210102188 -0.0009360860346235582; -0.003609359912134769 0.00615670804008625 -0.010734523276722821; -0.006210611126618799 0.00039576971237109763 -0.0007209490717232043; -0.00619361895324165 0.0021052432094739336 0.003968354727047322; 0.0021209534232848708 -0.004282520631477153 -3.3604064479255606e-5; -0.0034833653484662324 0.0007807405376025554 0.0024744808336553126] %
+
+Mass Used: 85.96110232461615 kg
+Launch C3: 98.08916251311179 km²/s²
+||V∞_in||: 1.922665314974668e-5 km/s
diff --git a/archive/ES_0.5641279507314239 b/archive/ES_0.5641279507314239
new file mode 100644
index 0000000..caa2b99
--- /dev/null
+++ b/archive/ES_0.5641279507314239
@@ -0,0 +1,22 @@
+archive/ES_0.5641279507314239---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T21:32:36.667
+Launch V∞: [6.284049420067361, -7.2840600639466375, 0.23159410683089876] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.5652333005464e-9, 6.62330282536911e-10, -8.559714018367129e-9] km/s
+ V∞_out: [-1.8711216024954295e-9, 5.036187668545062e-9, 6.084666563247647e-9] km/s
+ time of flight: 1.8749577782983327e8 seconds
+ arrival date: 2029-04-06T23:42:13.667
+ thrust profile: [0.6071923945774459 -0.1348432355192808 -0.1591055820045334; 0.10518296365038605 0.03774589038707594 -0.09474707562815506; 0.06821776652494227 0.04568455552378015 -0.10432313672735169; 0.05857035376830896 0.05286694669096663 -0.12476763896045445; 0.0504171588837525 0.056844531626981165 -0.13905992202661763; 0.02135481349118263 0.02846854650803043 -0.07357532593761358; 0.015673824933689462 0.024769532243361984 -0.06881044028081335; 0.017254369834050785 0.03083206167851204 -0.09020845801775453; 0.004046481327054702 0.004892115771558467 -0.01713642258467718; 0.002782782577332919 0.004363646054162461 -0.014994284500203988; 0.005115558123359517 0.01139834625276415 -0.037230372467476874; 0.0022743568428546983 0.0024031830240484726 -0.0025428989387401846; 0.00031840328171541974 0.0003058088521384429 -0.004385216004175771; -0.0009769294458462589 0.0010810185005597258 -0.0014807847919164215; -0.002257386431266923 0.0005035094174929886 -0.0010669131683479034; -9.603694191563975e-5 -0.0012032171956549338 0.0010433926105413922; 0.0004568264282624981 0.0015644479600216655 0.00040870484533151396; -0.00015269736365839637 0.003252300235580972 -0.00021541505476068887; -8.94398495705928e-5 0.00038572484986339303 0.001693320819348974; -0.0008926874986838871 0.0022515639062345165 -0.0039001203516923627] %
+
+Mass Used: 117.98001942378596 kg
+Launch C3: 92.60044395935003 km²/s²
+||V∞_in||: 1.2853056973859486e-8 km/s
diff --git a/archive/ES_0.5641351089849155 b/archive/ES_0.5641351089849155
new file mode 100644
index 0000000..8ad9333
--- /dev/null
+++ b/archive/ES_0.5641351089849155
@@ -0,0 +1,22 @@
+archive/ES_0.5641351089849155---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T14:43:29.525
+Launch V∞: [6.522686860474448, -7.303719270785493, 0.20752884443336791] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3805127421052763e-6, 0.00024737443564946536, -0.0002449445603655258] km/s
+ V∞_out: [-0.00016309598032515608, -0.00030146653825243504, 6.0633819957878824e-5] km/s
+ time of flight: 1.8749577787399128e8 seconds
+ arrival date: 2029-04-08T16:53:06.525
+ thrust profile: [0.3950294948595612 -0.09226303318934716 -0.12148002826969329; 0.06031908545723868 0.01760061117348057 -0.06568707842473731; 0.04489035806712857 0.025004809668862326 -0.08220633775864052; 0.0503815711696321 0.038282891169486154 -0.12682526834224225; 0.02978027110701726 0.027035102011789523 -0.09815151624175845; 0.015544533612208112 0.016050047826259527 -0.0655417704708903; 0.016852217065576727 0.019799078712061352 -0.08210411173632129; 0.0229619213812455 0.02863405155890403 -0.12057186113963282; 0.010996004127612322 0.014949101498050808 -0.06703403727955613; 0.0016730863493400945 0.001671853649336853 -0.01087210763377618; 0.009037321161990115 0.012465936605485417 -0.06578541877431414; 0.000752034526622584 0.0013982035615054413 -0.002486501165265765; 0.0022290553685028833 0.0003000775888454799 -0.0030735859213336623; -0.0012860557200389039 0.0017382725354072941 -0.003026536112126742; -0.0006569026919425853 0.0006857700691438521 -0.00044225393575732285; 0.0026324269005162815 0.0001343233237560299 0.0009269063027467577; -0.0006755888932251535 0.000775276741862362 -0.0008915501640538754; 0.00043935815729416016 -0.0008593967388233284 0.00514916016446512; 0.00297760499037446 -0.0025844326377891355 0.00026609669224890095; 0.005940551552795099 0.00039288589276309207 -0.0022420200572196127] %
+
+Mass Used: 98.54946797186085 kg
+Launch C3: 95.93282728752123 km²/s²
+||V∞_in||: 0.0003481290779021243 km/s
diff --git a/archive/ES_0.5641422763728199 b/archive/ES_0.5641422763728199
new file mode 100644
index 0000000..e0625af
--- /dev/null
+++ b/archive/ES_0.5641422763728199
@@ -0,0 +1,22 @@
+archive/ES_0.5641422763728199---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T11:09:24.437
+Launch V∞: [6.375823696631521, -7.4748110498388245, 0.14262417370302802] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3779483140655222e-7, 2.3786377797691054e-8, -4.653079643731244e-8] km/s
+ V∞_out: [1.432932988452466e-7, -3.213300397174519e-8, 1.7480450841304106e-8] km/s
+ time of flight: 1.874957778748408e8 seconds
+ arrival date: 2029-04-11T13:19:01.437
+ thrust profile: [0.3837223825787537 -0.10350380121898663 -0.11474416157629308; 0.028798522665546528 0.006025512472845571 -0.036235739412602504; 0.02867106979809917 0.01186204600667871 -0.06013328232242803; 0.07583127469534558 0.04121936209890074 -0.19787217489832334; 0.03019168984043807 0.01985908576325291 -0.11313725790456358; 0.02334902260561773 0.016340584030072963 -0.11046863358274026; 0.020187311270166163 0.01662836766362439 -0.10784194119345945; 0.0061748191891105 0.005997150220272597 -0.04062672485793983; 0.007094225766646873 0.006062880458322589 -0.04790962556742397; 0.005764251039900324 0.004444854196989535 -0.03936389380888737; 0.0018088789262888996 0.0027846508301348103 -0.010022409687388933; 0.001618210069753425 0.004649488528274659 -0.0015473938215725559; -0.0004071729446457413 -0.0037112067042078313 -0.0037871534535863197; 0.004395416941721151 0.0019815781951803696 -1.4740679558934797e-5; -0.0006426205220704043 0.0016953814206599816 -0.003512391591553859; 0.0009334783788347424 0.0009410005613267589 -0.0021767062140481508; -0.004139456795370877 0.004957128721998818 0.0011635915519751312; 0.003504162085211827 -0.00419933883073552 -0.009891808361286274; 0.0010364468208640455 -0.00029566073274246544 -0.0031579428279046333; 6.844781236411837e-5 0.00033448382190050035 -0.0005986786171894402] %
+
+Mass Used: 94.99108254019347 kg
+Launch C3: 96.5442696962451 km²/s²
+||V∞_in||: 1.4737137560661245e-7 km/s
diff --git a/archive/ES_0.5641470143309303 b/archive/ES_0.5641470143309303
new file mode 100644
index 0000000..45d66d8
--- /dev/null
+++ b/archive/ES_0.5641470143309303
@@ -0,0 +1,22 @@
+archive/ES_0.5641470143309303---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T06:47:01.571
+Launch V∞: [6.209029592974181, -7.55098217353452, -0.034348835868343565] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.55283799387937e-8, -1.4853715747644729e-8, 2.983329140572321e-8] km/s
+ V∞_out: [1.2888151497485893e-8, -2.8725334026996225e-8, -3.8124080360715654e-8] km/s
+ time of flight: 1.7699529877743134e8 seconds
+ arrival date: 2028-12-05T20:08:39.571
+ thrust profile: [0.37806476300218184 -0.12992607082557497 -0.14562862784336666; 0.06717643665178252 0.011697607970730715 -0.07620688405511679; 0.09357116441399436 0.03764755026584181 -0.17288442828354542; 0.07316735262475486 0.040750702831461795 -0.18730001273266295; 0.05236646158990602 0.03544809931328823 -0.1709294441562132; 0.030374826824464275 0.02361665477103375 -0.12068197079900501; 0.018903388911589394 0.016248333011583585 -0.08835478646082319; 0.009022400546476362 0.008466408506245127 -0.04860740384750441; 0.001184340077667531 0.0018828411162743698 -0.007105927546155134; 0.0003157394983866478 0.0013479228753173057 -0.007756494243106609; 0.0003625033207132853 0.00013050264047952478 -0.0041163155288117545; -0.0009529993239806472 -0.000582282958606874 -0.0029265190632719136; 0.0011037554667940367 -0.0018337233348675508 0.0009809743052354187; 0.00044358250366853427 0.0008704091470540423 0.0027380625493850955; -0.0009331357165082307 -0.00109813669822015 0.002707687518037345; -0.000791108662623249 -0.0006198468172066986 -0.002927773333039321; 0.0005677124982734901 -0.0002108927385506424 -8.852383912018856e-5; -0.0005083679292329279 -0.0011970056122803975 0.00206707794132673; -0.00014895713877448338 0.0011162357996821783 0.0035816744487592632; -0.0037178334428003518 3.625717548389124e-5 -0.00028244157901701367] %
+
+Mass Used: 100.67658272113931 kg
+Launch C3: 95.57056011399075 km²/s²
+||V∞_in||: 4.871266702497314e-8 km/s
diff --git a/archive/ES_0.5641500953731028 b/archive/ES_0.5641500953731028
new file mode 100644
index 0000000..c791a21
--- /dev/null
+++ b/archive/ES_0.5641500953731028
@@ -0,0 +1,22 @@
+archive/ES_0.5641500953731028---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:05:24.825
+Launch V∞: [8.009906172320397, -5.823394217608092, 0.09646757959513491] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8023958924483341e-6, -2.0205996387606122e-6, -1.9396688513693385e-7] km/s
+ V∞_out: [1.2454322679357961e-7, -1.280259570484213e-6, -2.3904435085953984e-6] km/s
+ time of flight: 1.8445488593362248e8 seconds
+ arrival date: 2030-03-19T20:33:29.825
+ thrust profile: [0.20443123284227144 -0.007998895003247998 -0.07217244650101354; 0.06201863824883017 0.029971747800125893 -0.07317980911443189; 0.06087109700867961 0.04705898855509596 -0.1298807406891784; 0.05998112338585742 0.05951481862464908 -0.1858525399222054; 0.024860671787806918 0.028656969849965207 -0.10203311500775; 0.015189643931912574 0.019583964233001076 -0.07727426875244663; 0.008117098753513519 0.010208879096925139 -0.04726478731306515; 0.005091414041381336 0.006814543544759131 -0.03341247247887247; -0.0028352645361230805 -0.007070777132723028 -0.02185557574596777; 0.0011371466470232335 0.0005316866700909164 -0.007448058054613565; 0.014990151495146145 0.01993616147551537 -0.017293269656641373; 0.00020944503107447657 0.003174470083147801 -0.005181397839057378; 0.0035919669655184398 0.003233767496296798 -0.014757494119691765; -0.00046471993067005734 0.0033211240318496873 -0.013049653463217166; 0.0007301040288371519 0.0030340505428268915 -0.0067787616030664235; 0.023232361636551582 -0.015302805408381227 -0.02710218158587992; -0.006410478016638488 -0.02286635076878389 -0.02555176542621007; -0.00794340512057021 -0.005875528376544257 0.006204049293578238; 0.002285321433556782 0.016578392726903216 -0.019475286047420118; -0.008737762206835949 -0.0010443279924397776 -0.006145996028352762] %
+
+Mass Used: 86.04280986968251 kg
+Launch C3: 98.07982309696071 km²/s²
+||V∞_in||: 2.714604392135964e-6 km/s
diff --git a/archive/ES_0.5641515252052075 b/archive/ES_0.5641515252052075
new file mode 100644
index 0000000..e015d0e
--- /dev/null
+++ b/archive/ES_0.5641515252052075
@@ -0,0 +1,22 @@
+archive/ES_0.5641515252052075---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T21:06:21.413
+Launch V∞: [6.490477241357076, -7.61088928958961, 0.12372456069385661] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1455663200584723e-7, -2.527446330544807e-7, -1.0638134634070205e-7] km/s
+ V∞_out: [7.569780088453387e-8, -1.5292516651065535e-7, 2.4334536972131627e-7] km/s
+ time of flight: 1.851142519803065e8 seconds
+ arrival date: 2029-03-15T09:43:52.413
+ thrust profile: [0.07483011361151859 -0.02146604910229175 -0.03090571054855119; 0.06272838463072382 0.011437634198690467 -0.07536646595951216; 0.028450602303985145 0.01151246683690463 -0.05959845865437232; 0.06100562225370553 0.028511260484089262 -0.1693663953890896; 0.048697927706975924 0.026790297760217952 -0.1728187089103953; 0.03366682374013262 0.02125201573644336 -0.14536826895753494; 0.011609117740321074 0.008840673312355399 -0.060341501754470644; 0.0031338436893076816 0.0021719494960264585 -0.018352197891981843; 0.0035706967058843253 0.0033692910676538777 -0.02671841503676655; 0.011186382368370907 0.007525383812758374 -0.05947091425895301; 0.006856930312987871 0.0059451680285990665 -0.051232031706290995; 0.0007828534915549875 0.0007233253801071263 -0.006371162796916599; 0.00033266849689631776 0.0006335500693732153 -0.0037514619836008733; -0.0008693184148264666 0.0010079968559301683 -0.0014491474105215547; 0.00013918866465314223 -0.000469260148797219 3.868677442093972e-5; 0.00033369402368452303 0.00021938393730339364 -0.0019939912024457994; 0.00014949680625314134 -0.00039752345889033366 -0.0020005604848805387; -0.00032372459687576274 -0.000832944919289354 0.0023171364031278436; -0.0007823786560322887 -0.001852364255101433 0.002337706394067991; 0.002271552331268537 -0.0009113493851484182 0.0009494975059981945] %
+
+Mass Used: 74.45122227175852 kg
+Launch C3: 100.0672383658829 km²/s²
+||V∞_in||: 2.971869147920675e-7 km/s
diff --git a/archive/ES_0.56415889084599 b/archive/ES_0.56415889084599
new file mode 100644
index 0000000..4660f68
--- /dev/null
+++ b/archive/ES_0.56415889084599
@@ -0,0 +1,22 @@
+archive/ES_0.56415889084599---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T22:00:39.990
+Launch V∞: [7.583985360207082, -6.1036362184775905, 0.07790041197758214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0453749955893303e-5, 1.1170185632083393e-5, 1.032809271242781e-6] km/s
+ V∞_out: [-8.568949819232064e-7, 2.6432525924379276e-6, 1.5080775653105253e-5] km/s
+ time of flight: 1.7306941581032506e8 seconds
+ arrival date: 2029-11-04T00:50:54.990
+ thrust profile: [0.5037580465466766 -0.05521738028290687 -0.1549103729165426; 0.05853175885493406 0.0264071063547786 -0.06428625573392943; 0.046344393360794794 0.03542332572771562 -0.08944429824866615; 0.024579745436353946 0.02531581975167155 -0.0694615555231669; 0.03305709928380336 0.040827640836029765 -0.11723246392623479; 0.03047544519890707 0.04215314422452186 -0.1328914338156697; 0.030562675524960597 0.04548307925833579 -0.1515273443392648; 0.02239547956189226 0.03821968475257809 -0.12879078552912798; 0.004722102672079484 0.009247665960481991 -0.03350021408981908; 0.004803329184707267 0.010303472216358248 -0.040731913079180046; 0.0026202444974484347 0.003609841560217601 -0.004507258731145011; -0.0027520858018517053 -0.002137419167412992 -0.006108455815138686; -0.0024296081400732978 -0.0013951003502419763 -0.00017949905672655754; 0.003581197203298471 -0.003263085254894542 0.0034885716938360756; 0.0005287089469397364 -0.0055094835978025305 -0.0033026179297126965; -0.000664920669098609 -0.00022166452979627835 0.005049277688111477; -0.008265756239154466 -0.006549357770069514 0.0005200082014128063; -0.0032956424357569866 0.00011341485594127971 -0.0008258233993328483; -0.01313265518206734 -0.010972466973697689 -0.01464773907811969; 0.0019621871873794503 0.0011390608151038274 -0.006322952798915631] %
+
+Mass Used: 105.31792053804566 kg
+Launch C3: 94.77727750553304 km²/s²
+||V∞_in||: 1.5333643734817453e-5 km/s
diff --git a/archive/ES_0.564168376957333 b/archive/ES_0.564168376957333
new file mode 100644
index 0000000..c88b4b9
--- /dev/null
+++ b/archive/ES_0.564168376957333
@@ -0,0 +1,22 @@
+archive/ES_0.564168376957333---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T09:27:15.909
+Launch V∞: [6.508558118664757, -7.542285799328738, 0.032916414951872544] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.124085154265307e-9, -1.7629962451531617e-10, -6.171963221113353e-9] km/s
+ V∞_out: [-1.104554676744999e-9, 2.6545956833279334e-9, 3.56689888841827e-9] km/s
+ time of flight: 1.809785562127621e8 seconds
+ arrival date: 2029-01-23T01:16:31.909
+ thrust profile: [0.10245800050155826 -0.03207091913910213 -0.04022873242521822; 0.04553074444412189 0.008838816558024864 -0.05166226799324708; 0.04582086613383768 0.01955402485556457 -0.08630540039513811; 0.09569281769526668 0.053415869033139 -0.24257539688484225; 0.04035160697183288 0.027270507230946282 -0.13346567817631735; 0.030134600584872655 0.023496399159726844 -0.12323254124914541; 0.017288608855337177 0.01485626096027181 -0.08394685216839455; 0.010717137014442019 0.009753191485855708 -0.05637481113385047; 0.010849714970642313 0.010734254310061836 -0.06559898313842197; 0.002058337142430794 0.003618570914833239 -0.020682708557858833; -0.0007970296684175981 -0.00027877984659028187 -0.005283060670697338; -0.0003889928050453541 -0.0017743913018094823 -0.003353550017220166; 0.0003819374213557572 0.0008172558254334853 -0.0018489662623410825; 0.0008905881699385841 0.000803115163387263 -0.0029257778149238394; 0.0026461633045219116 -0.0011255001848312696 -0.0030470622803654823; 0.000611754317533045 0.003706391642350949 0.0005474943911373351; -0.0021891734460897892 -0.005251709905266954 0.0005221203665692498; 0.0041180406965120415 0.004502205585748264 0.006016487517702564; 0.00012610838074998123 0.0005860508717211879 -0.006135785734659963; -5.4226372761656265e-5 -0.0004759251324544774 0.002156078344124971] %
+
+Mass Used: 79.24693022341944 kg
+Launch C3: 99.24848735316614 km²/s²
+||V∞_in||: 8.69647230416293e-9 km/s
diff --git a/archive/ES_0.5641700386408275 b/archive/ES_0.5641700386408275
new file mode 100644
index 0000000..2dbc336
--- /dev/null
+++ b/archive/ES_0.5641700386408275
@@ -0,0 +1,22 @@
+archive/ES_0.5641700386408275---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T21:44:36.848
+Launch V∞: [7.602188440161492, -5.657857419288432, 0.2510955435696445] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1290863926579886e-6, -3.8783416275469056e-6, -1.1155635979019294e-5] km/s
+ V∞_out: [-1.086720593654847e-5, -1.2887779482476677e-6, 4.571043268032056e-6] km/s
+ time of flight: 1.8444305195201132e8 seconds
+ arrival date: 2030-03-13T15:55:27.848
+ thrust profile: [0.8431128004942959 0.0003420768372455901 -0.16472850832853925; 0.15011106656260145 0.10205785759501312 -0.11979985841045818; 0.0534750718332628 0.06249009216521422 -0.08472949983292394; 0.02967985800502251 0.04772509416290628 -0.07554491018967904; 0.05381382948824906 0.11470478757640389 -0.17783995620807638; 0.011791665310708337 0.030434667250716554 -0.055061385413384165; 0.0071964464908520825 0.03140947219203327 -0.05929106543686528; 0.0027408964414759257 0.007993991230665186 -0.018629239412255326; 0.0013611753491884987 0.012423457351484875 -0.026496468583554793; 0.0027341955976295023 0.016522429785322864 -0.035912770070806295; 0.0037599287548372626 0.024490756287742204 -0.05240251955109946; -0.002392448161233306 0.00024356751524128029 -0.0008657029636573799; 0.0017637512389544212 -0.000550755570869236 -0.004371317454262478; 0.0029823239028410184 0.002720032926583411 -0.0015125258571859037; 9.979084609980214e-5 -0.0001816940115874936 -0.001793329111761833; -0.0025699720104042506 -0.0051101442915238915 -0.0026067110156898807; 0.0005285389655088438 0.003159366663157502 0.0013330865559545105; -2.9675193924589843e-5 -0.00020404953675948092 0.0008667993532017583; -0.002940923921874053 0.008111282379992216 -0.002729974967538732; -0.0038538529782692474 0.0019452687075129683 -0.0025997773834439135] %
+
+Mass Used: 133.9703114134163 kg
+Launch C3: 89.86766862872271 km²/s²
+||V∞_in||: 1.1864425142350488e-5 km/s
diff --git a/archive/ES_0.5641712330776913 b/archive/ES_0.5641712330776913
new file mode 100644
index 0000000..fe6ea01
--- /dev/null
+++ b/archive/ES_0.5641712330776913
@@ -0,0 +1,22 @@
+archive/ES_0.5641712330776913---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T14:58:50.685
+Launch V∞: [7.5781837817336895, -6.479626634949491, -0.2951538425024304] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00037372737690605294, 0.001027878113647334, 0.0023177408501714692] km/s
+ V∞_out: [0.0023512696466250374, 0.00027349824676960513, -0.000981916189274331] km/s
+ time of flight: 1.659951275606851e8 seconds
+ arrival date: 2029-08-15T20:44:17.685
+ thrust profile: [0.1202598052456951 -0.023367779869901337 -0.050156639358134476; 0.0631469056411467 0.016810321595224335 -0.07893719907622157; 0.05309409334447046 0.024908522383058056 -0.11304133848560728; 0.0643050346488405 0.03848907758712511 -0.19064671782696951; 0.03493507627627675 0.023527886955493255 -0.13284639451966074; 0.03125971467345718 0.023066334481528873 -0.1427771407641189; 0.008878425187187285 0.006552924793375126 -0.04812654420077611; 0.03212471384182449 0.026013404776273456 -0.1910810892879041; 0.004721414712787235 0.003587871285967612 -0.03169889296605919; 0.0023563454716862826 0.002178119225997152 -0.020700121861273665; 0.0010857278202165502 0.0007500420069458283 -0.0017569840134957955; -9.47063033064769e-5 -4.889193466351007e-5 -0.0023575291521269436; 0.00010047875847321499 -3.105705260775119e-5 -0.003229177870337658; -1.6571971330325147e-6 0.0012178023263501683 -0.0026758803522659615; 0.0002566861643546512 0.00010667528587877083 -0.0019495286007727075; -0.00035530962698120355 0.00018104049044694384 0.0003041428999090087; -0.0040734129955416355 0.0007303515320869986 -0.005067291543495565; 4.68469415679882e-5 0.0005710209812531822 -0.0015679687883537758; -0.00023470553141392093 -0.0008353408083834733 -0.00032178141925222293; 0.0006758421853753855 0.0017085422422232965 0.00030062051738787184] %
+
+Mass Used: 77.77408372250966 kg
+Launch C3: 99.50154654882233 km²/s²
+||V∞_in||: 0.0025628359715982305 km/s
diff --git a/archive/ES_0.5641714751881283 b/archive/ES_0.5641714751881283
new file mode 100644
index 0000000..b029898
--- /dev/null
+++ b/archive/ES_0.5641714751881283
@@ -0,0 +1,22 @@
+archive/ES_0.5641714751881283---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:48:21.748
+Launch V∞: [7.7781855811028375, -5.861544346810419, -0.7974111741547102] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012897827791188957, -0.07630978742745836, -0.09792068506646269] km/s
+ V∞_out: [0.04945425397684552, -0.04436157489628055, 0.10566207068333147] km/s
+ time of flight: 1.8749577774606687e8 seconds
+ arrival date: 2030-04-22T09:57:58.748
+ thrust profile: [0.29597885193828627 0.01697166581676028 -0.08316181094998966; 0.16577700785577873 0.11909624864680061 -0.146825181524361; 0.09121729370031421 0.1102124483782284 -0.14944154318678649; 0.05320797306689426 0.09017695955595077 -0.13601593880991375; 0.029808216891514406 0.06677399775752746 -0.11031261399214426; 0.018663404492505 0.054009545286142074 -0.09586135974973539; 0.00878914486505469 0.03322943094444311 -0.06328431714521231; 0.001748001026977612 0.009478646977751068 -0.01771772463612945; 0.001545550134697754 0.014045557680247206 -0.030983926587230887; 7.178633968570524e-5 0.0001700211777427177 -0.0012484755686976; 7.631126099853749e-5 0.0011918836626285552 -0.0008495532799012726; -0.0004386801186435698 0.0008023588634762718 -0.0013001093316578009; 0.00014349603036704992 -0.0005932280843529848 0.0002897807681720183; 2.2494813566164448e-5 5.3639705817404596e-5 0.0019420272213895365; 0.0014289434839179643 0.0006809217058230206 -0.0033165346972400117; 0.0024984926553250813 0.005580755277784741 0.0014578912122873646; -0.001148550037888343 -0.006404039245446606 -0.005046619758437355; -0.0012840342402366577 -0.005506919369713933 -0.005730522737512005; 0.0004300349856172364 0.006441609599104323 -0.00569722862692397; 0.0009740342854985811 -0.0002279193937002935 0.0049051350457389] %
+
+Mass Used: 101.15325146066925 kg
+Launch C3: 95.49373764436807 km²/s²
+||V∞_in||: 0.12481185113137462 km/s
diff --git a/archive/ES_0.5641747172164814 b/archive/ES_0.5641747172164814
new file mode 100644
index 0000000..5b4ea82
--- /dev/null
+++ b/archive/ES_0.5641747172164814
@@ -0,0 +1,22 @@
+archive/ES_0.5641747172164814---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T01:28:30.608
+Launch V∞: [6.657457367874075, -7.259663579601966, 0.26412756798439374] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.0614369754221355e-9, -1.408677121629048e-9, 2.7249841971097353e-9] km/s
+ V∞_out: [1.1477365170467167e-9, -2.765638453047597e-9, -3.8871387518398605e-9] km/s
+ time of flight: 1.8749577787484384e8 seconds
+ arrival date: 2029-04-07T03:38:07.608
+ thrust profile: [0.24719010641451974 -0.05554594326428659 -0.08382228635156475; 0.1075438707254855 0.03722828433991988 -0.11292831685050742; 0.07910848592441855 0.05045422270698991 -0.13902086264971814; 0.074014514859577 0.06400168892940919 -0.1789181737078302; 0.03957793238911505 0.04188915331788645 -0.12812241632507151; 0.030439928179779193 0.037682125925077206 -0.11765314405086565; 0.011732861243393098 0.01624301063204281 -0.052778906696197184; 0.006288348383296277 0.010164922068739092 -0.038576999928241235; 0.0023220514464653333 0.004223505103722237 -0.017335716406237392; -0.000264590635326488 0.000731018513718768 -0.003972611957390094; 0.0010593126355275392 0.002314034158521448 -0.010491178541414369; 0.000162559617925907 0.0005786189788409392 -0.0026966536944642906; 6.86708065130598e-5 0.0006241277899808249 -0.00014992515915503575; -0.001450759516070891 -0.00021350060376271982 -0.000805244722875227; 0.0006892588620047702 -0.0012643870089876247 0.0027274021776967174; 0.0029548758559326677 0.0008788137753423278 0.0024903116355094214; -0.0007535009667127945 -0.0016444475902138377 0.0031305076791053785; 0.003713373003499076 0.001768764869845256 0.00020840527618843935; -0.002596395900205605 -0.008113381172806284 0.008093536760721215; -0.0008686287709706753 -0.0016400086758947409 -0.0008042702343687713] %
+
+Mass Used: 91.82090269955688 kg
+Launch C3: 97.09421726622939 km²/s²
+||V∞_in||: 4.333855842316484e-9 km/s
diff --git a/archive/ES_0.5641776240733896 b/archive/ES_0.5641776240733896
new file mode 100644
index 0000000..0ffcee9
--- /dev/null
+++ b/archive/ES_0.5641776240733896
@@ -0,0 +1,22 @@
+archive/ES_0.5641776240733896---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T02:43:25.202
+Launch V∞: [6.414690673026299, -7.548065925128721, 0.09700226562651526] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.470260176794377e-8, -9.470288622302613e-9, 3.139846673802793e-8] km/s
+ V∞_out: [1.0717287144531205e-8, -2.39353316215673e-8, -3.176251267378959e-8] km/s
+ time of flight: 1.7898976762779105e8 seconds
+ arrival date: 2028-12-29T18:06:12.202
+ thrust profile: [0.16839805600916932 -0.0529282306234034 -0.06433514769235524; 0.08881862514174126 0.0184432852622202 -0.09897194128763233; 0.06616728761402342 0.029658618959957854 -0.12318904491060209; 0.053984660813677116 0.032144751644004495 -0.13516506232320347; 0.04457232007983585 0.03207963153538172 -0.14243261167194401; 0.0358517909854601 0.030896939684311273 -0.14106474339577493; 0.022883794665471618 0.022109436800534253 -0.10859172612399011; 0.014073479237509545 0.014022430660448833 -0.074038936818469; 0.008642257134688285 0.00848883828497967 -0.04785030432725029; 0.003066739803052123 0.0033625383467429265 -0.020505388786202942; 8.674842572441938e-5 0.000276380372201988 -0.0011793232380791908; -0.0003020427927103919 0.002296809400092457 -0.00457517802861623; -0.0008517741640015212 0.000988385601020528 -0.003045912344045693; 0.0014990209450960865 -0.0011261481735002751 -0.0006119694025433758; -0.0017342716186769976 -2.1322616810561933e-5 -0.0006449612137361177; -0.00011000580340913397 0.00010977260746994431 -8.410571333720442e-5; -0.000476895721089735 -0.0004777044199428134 0.0002410147207196258; -0.003252559578955123 -0.0023901948051272405 0.005733380226175796; 0.0019997023043979703 0.0010666652216865255 0.0015533289552462429; 0.0016457930762404267 0.001733354949286066 -0.002718751902839541] %
+
+Mass Used: 85.77659845090784 kg
+Launch C3: 98.13096508023658 km²/s²
+||V∞_in||: 4.105811264773844e-8 km/s
diff --git a/archive/ES_0.5641881207086705 b/archive/ES_0.5641881207086705
new file mode 100644
index 0000000..4499953
--- /dev/null
+++ b/archive/ES_0.5641881207086705
@@ -0,0 +1,22 @@
+archive/ES_0.5641881207086705---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T17:22:49.556
+Launch V∞: [6.627522089438277, -7.435024591560174, 0.10230494376072148] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.385819066690253e-7, 3.629595247469954e-8, -4.510665108130882e-8] km/s
+ V∞_out: [1.4519626590963523e-7, -3.6282376474612334e-8, 1.7807746040686624e-8] km/s
+ time of flight: 1.8749577787494648e8 seconds
+ arrival date: 2029-04-10T19:32:26.556
+ thrust profile: [0.14024229289174933 -0.034132599011399437 -0.05354619774355602; 0.045124792820389614 0.011998158241665561 -0.05305170085576186; 0.039817682307391015 0.020158925020898374 -0.077567815438931; 0.04334964539467525 0.029626655195263446 -0.11743800007526953; 0.025862790910363642 0.021320587920733776 -0.0914112360489593; 0.02510188405949726 0.024651132202708703 -0.10782376469220463; 0.02122849732233067 0.02267787140610436 -0.10767582992793578; 0.015810192708886443 0.017038486287127966 -0.08919424253870835; 0.009461908995229282 0.011065939974098823 -0.061637933431149636; 0.008260046807081626 0.010718862825866352 -0.059830318740228504; 0.004604234590427833 0.005469278112770868 -0.03436179645475186; 0.003081258983386955 0.0033271068614855424 -0.02042640946461108; -0.0005437504951969392 0.001196403110992525 0.0031535097959255673; -0.001502679193471305 -0.0014909310930978133 0.0020945134033816364; -0.001133690615841487 0.0011531347439527205 -0.0008833624544388788; -0.003890194747023755 0.0007087777144866061 -0.0024710317541561293; 0.0025038933229648164 0.002495243208036164 -0.002133703346838444; 0.0019478780216029825 -0.0020639997494485535 -0.0014744406893266683; 0.003885745499152729 0.0003404188535197368 -0.0025340433247485594; 0.0004171028805736379 0.0004489072858852271 0.0009079618708602573] %
+
+Mass Used: 79.47052234986313 kg
+Launch C3: 99.21410602461472 km²/s²
+||V∞_in||: 1.5018971667141205e-7 km/s
diff --git a/archive/ES_0.5641888602493891 b/archive/ES_0.5641888602493891
new file mode 100644
index 0000000..771027b
--- /dev/null
+++ b/archive/ES_0.5641888602493891
@@ -0,0 +1,22 @@
+archive/ES_0.5641888602493891---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T11:30:30.504
+Launch V∞: [7.8818029325032075, -5.896344437057142, 0.06798796211598425] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0003903947220899418, 0.00024110559601167033, 1.5710616878269766e-5] km/s
+ V∞_out: [-0.00029675005715307137, -0.00018396883956591547, 0.00030471202157933343] km/s
+ time of flight: 1.8190603122474292e8 seconds
+ arrival date: 2030-02-17T20:57:41.504
+ thrust profile: [0.3467767034914098 -0.02274014249550783 -0.12636977893524462; 0.05022666485828521 0.023675565625828152 -0.06522249104545122; 0.028496147291131 0.021737800271502506 -0.06687917461208633; 0.03545318922293338 0.0328924797516634 -0.11662508333799389; 0.022477005987842785 0.024710818976782366 -0.09847788307191635; 0.020883758604505816 0.025844264709477375 -0.11215235500853625; 0.014635154764151207 0.020102924511022885 -0.09480042438394203; 0.011660502603357426 0.017515054611290572 -0.0868262309631537; 0.0028118068771483297 0.007447886274815505 -0.03246518826730396; 0.0028584114614523815 0.006067459218640292 -0.03921656179280308; -0.00012848088273469983 0.003679227794129567 -0.016036636820772027; 0.004575460663125599 0.003125069461482903 -0.016423424595147076; 0.0054121112804943776 0.002166146121841558 0.003930234703047286; 0.0007408614379088656 -0.0006538254688610808 -0.004812822344577965; 6.910806404581771e-5 -0.004511388629695448 -0.004021600241720636; 0.009143011530479382 -0.0011825265275145031 0.004977670814895831; 0.019927840326879193 -0.013360814779255745 -0.030308294852782705; 0.002211209725087979 -0.004878776470911228 0.014748029198191173; -0.010276489049558904 -0.020296651540516738 0.012376194780728548; 0.00019729123761019914 0.00027383702830668325 0.002374474307419612] %
+
+Mass Used: 93.00348458131657 kg
+Launch C3: 96.89431755022355 km²/s²
+||V∞_in||: 0.00045911520443840827 km/s
diff --git a/archive/ES_0.5641895716372177 b/archive/ES_0.5641895716372177
new file mode 100644
index 0000000..cb14b4c
--- /dev/null
+++ b/archive/ES_0.5641895716372177
@@ -0,0 +1,22 @@
+archive/ES_0.5641895716372177---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T07:15:07.172
+Launch V∞: [7.819127822703728, -5.684024765273453, 0.31315869871345114] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0016800085587290899, 0.0009852861084584511, 7.212129958969327e-5] km/s
+ V∞_out: [-0.0013890995193792596, -0.0007630215103736211, 0.0011354138238519813] km/s
+ time of flight: 1.839952743999832e8 seconds
+ arrival date: 2030-03-07T21:03:01.172
+ thrust profile: [0.48114994461386573 0.012835448262960555 -0.09233582977389339; 0.11157569869807478 0.07816687159401758 -0.08480167133240697; 0.12030352481903173 0.13622613335993286 -0.15531952421797485; 0.07667533551327385 0.12047755241697679 -0.14922051807119285; 0.061091233000167985 0.1223605994616287 -0.16267593574372308; 0.024291931925602566 0.06623314716639261 -0.09608642555001308; 0.006926853300756017 0.023932897759371553 -0.03905979248996034; 0.0037161033931443635 0.013080488484335039 -0.022914896630973895; 0.00023157704122409527 0.0048339194421021 -0.01063850066096347; 0.0005094348764573359 0.0003164225577316569 -0.0011761128819560208; -0.0005724418082242037 2.5109987812284166e-5 -2.6794806140201157e-5; 0.00034712090455402345 0.0005130852736082545 -0.002968855702902481; -0.00028375677978769137 0.0001174759623692177 -0.001361990207397812; 0.0015028994761247833 -0.0007674221653971093 0.0009145404797896843; -0.0009193484450615512 -0.000910710335570313 0.004121449979261286; 0.0024965958659282487 0.001142274709373668 0.0013666007119152181; -2.3181095898143776e-5 0.00046449955617825054 -0.0007929401351523815; -0.0006447510326498156 -0.0017058677719727793 0.0014525271962683615; 0.0010262254996108514 0.0019509494638465384 0.0020818177142257815; -4.410718877382389e-6 -0.0013478694717110613 -0.0008728494677824493] %
+
+Mass Used: 112.5421996815794 kg
+Launch C3: 93.54496581060137 km²/s²
+||V∞_in||: 0.00194895329722872 km/s
diff --git a/archive/ES_0.5642025757959662 b/archive/ES_0.5642025757959662
new file mode 100644
index 0000000..14e0dfc
--- /dev/null
+++ b/archive/ES_0.5642025757959662
@@ -0,0 +1,22 @@
+archive/ES_0.5642025757959662---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T18:03:40.814
+Launch V∞: [6.362198601614551, -7.3758768373917905, 0.3032582615894704] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.263888089311678e-8, 1.9086564624033395e-7, 8.360601325095514e-8] km/s
+ V∞_out: [-7.361107413272118e-8, 1.1584773643991981e-7, -1.8293218090183728e-7] km/s
+ time of flight: 1.8557213065783936e8 seconds
+ arrival date: 2029-03-15T13:52:30.814
+ thrust profile: [0.37658015778671305 -0.08134617226937912 -0.10576639057929964; 0.1305848344232297 0.04739938600574329 -0.11577023362171471; 0.10593269005842493 0.07335896844404748 -0.15976351503422598; 0.05787763176294404 0.05320847380647256 -0.12313639490644909; 0.029012932299556135 0.030744227790617806 -0.07934774429483156; 0.03261147092647106 0.043487879806615726 -0.10931810174773389; 0.025918857227304824 0.03922204469052072 -0.1045305979471389; 0.0097706073761636 0.014121588533670626 -0.04376347442199024; 0.006696324552708355 0.012631897523750194 -0.039723426744185525; 0.0014253900013294941 0.002247197527413061 -0.0035910312242335533; 0.0038796717271811763 0.007938636052402023 -0.025763855587786495; 0.0005854255867532609 0.0038280346346471713 -0.009068390257837873; 0.0005785179626528969 0.00011259567961943273 -0.0026212084463295704; -6.500670363766971e-6 0.00013690365813799426 -0.0002822959942451874; -0.000607228300050695 -0.0009137705537019666 -0.00034235125463828774; 0.002519632165865563 -0.0015079785788071716 -0.0018171532950869522; 0.0006287611829777291 0.00029731717262672776 0.001553470309589963; 0.0006806087378098238 0.0003250150165977193 -0.005931586598794492; -0.0015090379832666868 -2.3281089831006995e-5 0.0002276354898068482; -0.0004800038646990765 -0.0028624432202539385 -0.0035540891871341297] %
+
+Mass Used: 104.2266132787372 kg
+Launch C3: 94.97309573998115 km²/s²
+||V∞_in||: 2.2803864282087865e-7 km/s
diff --git a/archive/ES_0.5642076683033134 b/archive/ES_0.5642076683033134
new file mode 100644
index 0000000..d026541
--- /dev/null
+++ b/archive/ES_0.5642076683033134
@@ -0,0 +1,22 @@
+archive/ES_0.5642076683033134---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T18:48:23.057
+Launch V∞: [6.32446417151688, -7.428785490968607, 0.0728934806542681] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.20304310080166e-8, -2.814263063757594e-6, 4.928055011101032e-8] km/s
+ V∞_out: [5.331452054820362e-7, -1.1709770867169379e-8, -2.7648540910241273e-6] km/s
+ time of flight: 1.8543524749489287e8 seconds
+ arrival date: 2029-03-16T00:35:50.057
+ thrust profile: [0.4187718518983826 -0.10368595196658664 -0.1386278372619673; 0.09682584152707417 0.027219148453715557 -0.10292948712216259; 0.042848310104857984 0.023329709900598326 -0.07800219099127349; 0.06205277390975798 0.04528081293935031 -0.15247408754512656; 0.04349205098135144 0.03887419856154503 -0.13991890858535927; 0.0207553490869931 0.021338832776845385 -0.08359013674433192; 0.010436702754359449 0.012374011290939102 -0.05070000970820307; 0.01203727253879021 0.015020988252359691 -0.06600776421727267; 0.012847441134146717 0.019323845586097795 -0.08485219022103396; 0.002136753515174136 0.002986396109588579 -0.015208136109556562; 0.0037714463808723327 0.006206212742851324 -0.026990475320379452; -0.0031342816022043784 0.0002105552673087033 -0.0026619793995296304; 0.000393786551848344 3.983615603584904e-5 -0.001855969092485865; -1.2066117981905227e-5 -0.0019532260859654958 -0.005889676364494733; 0.0008881766660521605 0.001030024649561 -0.0027353791350818515; -0.0008112411288161711 -0.004210999104862046 0.0037598310542439066; -0.0010518870799553128 -0.00018201804292681222 0.0007817002168067242; 0.0019830852473378337 0.0037457748773606133 -0.002888366568846853; 0.0021841690688444203 0.006822327446561034 -0.004701700969404339; 0.004527027391819873 -0.000709537678653073 -0.0012761947138691658] %
+
+Mass Used: 102.96136242883404 kg
+Launch C3: 95.19101438714827 km²/s²
+||V∞_in||: 2.81619863732675e-6 km/s
diff --git a/archive/ES_0.5642085925708975 b/archive/ES_0.5642085925708975
new file mode 100644
index 0000000..f733a8d
--- /dev/null
+++ b/archive/ES_0.5642085925708975
@@ -0,0 +1,22 @@
+archive/ES_0.5642085925708975---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T05:09:02.589
+Launch V∞: [6.419506410789959, -7.569901314981379, 0.08275226547201024] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0721496156191895e-9, 1.6706028257993796e-9, 8.53261451509217e-9] km/s
+ V∞_out: [-4.721273177642139e-9, -6.810102756180863e-9, -3.6155908450247677e-9] km/s
+ time of flight: 1.798191684970895e8 seconds
+ arrival date: 2029-01-09T10:55:10.589
+ thrust profile: [0.15626868699123656 -0.05132243425023689 -0.06085237155702408; 0.07276363590845744 0.013083313678726727 -0.08487722608312939; 0.03994334143694143 0.015854501892148154 -0.0759027095600761; 0.04907205836791221 0.026419126002020062 -0.13116354255504276; 0.07572086921367688 0.04774736994314722 -0.2491065331502229; 0.033008583801774176 0.02416361172949775 -0.13494527245490595; 0.019299839775104292 0.01642057023230262 -0.09564438802016112; 0.009382529212630856 0.006247251042394607 -0.0429564112210667; 0.0043759401044181 0.0033174486927628503 -0.027119279896562307; 0.0011810191384053126 0.0008991061609061733 -0.010675985095567827; 0.002510455689452825 0.0013662051603900776 -0.013778493376730651; 0.001811281018058808 0.0014466459447479306 -0.011407826232917266; -0.0006950791027329666 0.002693385528337509 -0.002725790048284287; 0.00045795309793244046 7.531917021637537e-5 0.0025667465869033497; -0.00014436397947063025 0.0002204867262490702 -0.003844668345443826; 0.0005785819965712083 -0.0002889204412176999 -0.00023108403564313297; -0.0016456155387247692 0.003046800602229595 0.001419335998911931; -0.0012572608115486628 0.0002032927048358189 -0.0046908823880085024; 0.002581070624948288 0.0022477545326028423 -0.008867110056367842; -0.003369219055546502 -0.0034145378033200568 -0.0046629896898092715] %
+
+Mass Used: 83.54151225004989 kg
+Launch C3: 98.52031641417095 km²/s²
+||V∞_in||: 8.93813337863344e-9 km/s
diff --git a/archive/ES_0.5642123318755418 b/archive/ES_0.5642123318755418
new file mode 100644
index 0000000..76667fe
--- /dev/null
+++ b/archive/ES_0.5642123318755418
@@ -0,0 +1,22 @@
+archive/ES_0.5642123318755418---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T07:24:03.540
+Launch V∞: [5.913773544645053, -7.520479771218698, 0.06544213225326062] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.015773143559347506, -0.006597108502601704, 0.015542193945527995] km/s
+ V∞_out: [-0.015083315784227612, -0.006287999091256951, -0.016339073749331565] km/s
+ time of flight: 1.827952424413423e8 seconds
+ arrival date: 2029-02-10T23:51:25.540
+ thrust profile: [0.5591923512026563 -0.1281821168544298 -0.15102375730252923; 0.2690259496278616 0.09193121719747037 -0.21234037951204177; 0.0933324593770021 0.06047202885770455 -0.1308404181407478; 0.07565726431353735 0.06678820038964778 -0.14625518773936583; 0.037898917131209645 0.04236415954725939 -0.10021805198999074; 0.02254024248568374 0.030169710135275904 -0.07381657139698952; 0.01885453302788418 0.02898972905252379 -0.07581369129283724; 0.02017029303595676 0.034602680372352035 -0.09112799456648796; 0.0035298133292031952 0.00642920897064295 -0.018589493592263005; 0.00021534383920342686 0.0004257022171962701 -0.0012570507077701559; 0.0001703013567524521 0.00036239296753088875 -0.00047722605296661745; 0.00045048612513562186 0.000720979031864051 -0.001552331461659502; 0.00041119352448672545 8.456500413879194e-5 -0.0006579564203915435; -0.0003595622189112974 -4.73646195522987e-5 -0.00013998950258438001; 0.000346789656430278 0.00020753713102748605 -0.00042064092772804755; 0.00012839889455145074 0.00034894293224569577 -0.00013509069098192238; 0.00013128699794632973 -0.0001274863342669415 7.259850905857643e-5; -1.0364140038919762e-5 -0.0007742112413261169 -0.0004072190753166379; -2.541075290096403e-5 0.00032366781142484537 -0.0009998907102664433; -0.0011133501254723937 -0.0004325790270866348 0.00020544848646428503] %
+
+Mass Used: 124.2957926920567 kg
+Launch C3: 91.5346161993272 km²/s²
+||V∞_in||: 0.023105706892005976 km/s
diff --git a/archive/ES_0.5642136396372859 b/archive/ES_0.5642136396372859
new file mode 100644
index 0000000..acbbb99
--- /dev/null
+++ b/archive/ES_0.5642136396372859
@@ -0,0 +1,22 @@
+archive/ES_0.5642136396372859---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T12:23:54.659
+Launch V∞: [6.50598132454608, -7.5109417820667295, 0.09250403946775658] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.911484784053401e-9, 2.810963441029997e-9, -1.5123890079122246e-8] km/s
+ V∞_out: [-5.06222863338889e-9, -2.7076308425668487e-9, 1.6120694297914535e-8] km/s
+ time of flight: 1.8338413811063042e8 seconds
+ arrival date: 2029-02-21T00:26:12.659
+ thrust profile: [0.16011426253503155 -0.04736955357480804 -0.062392848041291506; 0.05298610884369064 0.010965600904860814 -0.06183205751100555; 0.049349188613854095 0.02043465901042573 -0.09654037884595652; 0.04752652933503382 0.027121550651416776 -0.12667931853389966; 0.03474412373021521 0.02377741389517095 -0.11817208598416183; 0.03532238133930479 0.027326129658682956 -0.14839219948279767; 0.021624842438702028 0.018471607990858514 -0.10428810032842141; 0.0033607255699663347 0.0024607707974899323 -0.018279425513882147; 0.01856220802625462 0.018247551709024132 -0.11605200306954737; 0.007227629808898933 0.007879327313446703 -0.04924693206808467; 0.0002451630013560722 0.0010497138117863945 -0.006522440448660256; 0.0002224747535253206 0.00013788410230392294 -0.00319660009718026; -0.0009583545100705158 -0.001472180738720413 -0.0014981128849223036; 0.003384089399298157 0.0009601250999855996 0.000794686452371093; 0.0011325624362890985 -0.0015900602468772002 0.0009429500206856673; 0.0020252754307981662 -0.0036733587210908175 -0.0013581126698597062; -0.00015639203687903443 0.00336036548019937 -0.0017579076859458194; 0.0005361776401221028 0.001956570800106046 0.0007834037001856154; -0.005224080170368468 0.0026539253050308406 -0.0011685780279190264; 0.0010583569163036134 -0.0028077931830914845 -0.005384175261212415] %
+
+Mass Used: 82.20410030700714 kg
+Launch C3: 98.75059644625595 km²/s²
+||V∞_in||: 1.829948352322277e-8 km/s
diff --git a/archive/ES_0.5642216561392988 b/archive/ES_0.5642216561392988
new file mode 100644
index 0000000..7f3e8b2
--- /dev/null
+++ b/archive/ES_0.5642216561392988
@@ -0,0 +1,22 @@
+archive/ES_0.5642216561392988---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T01:19:29.388
+Launch V∞: [6.344153802092125, -7.395457618547838, 0.16552899196941953] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.015386505963132154, -0.007538318396701022, 0.01789104945330757] km/s
+ V∞_out: [-0.01592260361990124, -0.006779230834735079, -0.01772214536837772] km/s
+ time of flight: 1.8499078224285495e8 seconds
+ arrival date: 2029-03-10T03:39:11.388
+ thrust profile: [0.4180218730318461 -0.11246871824546026 -0.13769540297694993; 0.1388192960028055 0.03640977141491789 -0.13741848744540547; 0.03324591399202884 0.017848229154759192 -0.05992996166015125; 0.0427135085577713 0.031503346322146825 -0.1050648280037045; 0.03563282285072771 0.03190856690282094 -0.11203041099823413; 0.03962468405268309 0.039840556360080624 -0.14675823072619001; 0.007196363994467482 0.011256263374124895 -0.04912785995733258; 0.010657843108704278 0.012491049045518256 -0.05523476891670452; 0.02103671069957616 0.026219957911869998 -0.10953652456107443; 0.0027392872857202617 0.003119114154841576 -0.017867513881478177; 0.0073007166780407595 0.004457051311604074 -0.025781793467538304; -0.002019575699692658 0.0005447907474960365 -0.0015113917725122234; -9.793897216379402e-5 0.0011381883850267198 0.000902819329258718; -0.0007618773233543721 0.0017665923788370826 -0.00273266441784242; 0.0009981704542914118 0.002948831645303976 0.0006886630033468484; -0.0018849317890357834 0.00040731089387916483 0.000824850162257534; 0.0005158946324924528 -0.0009830920650217955 0.0013759877628150797; -0.0006125771989205574 -0.0011927205641093781 0.0023608379786910763; -0.0010738852874784233 -0.0011903644506404262 0.007434302679330525; -9.730190015925209e-5 0.0016048606945460522 0.0007746691683466257] %
+
+Mass Used: 104.2757947486507 kg
+Launch C3: 94.96848069951963 km²/s²
+||V∞_in||: 0.024772171090646042 km/s
diff --git a/archive/ES_0.564235335603724 b/archive/ES_0.564235335603724
new file mode 100644
index 0000000..0eacebb
--- /dev/null
+++ b/archive/ES_0.564235335603724
@@ -0,0 +1,22 @@
+archive/ES_0.564235335603724---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T12:33:21.404
+Launch V∞: [6.261760625557406, -7.224238432457777, 0.1520482838059837] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.712638600358661e-7, 7.466608909003605e-8, -1.642161864087555e-9] km/s
+ V∞_out: [-1.0957127255722367e-7, 2.564642258781749e-9, 5.674096152910348e-7] km/s
+ time of flight: 1.8749577787475076e8 seconds
+ arrival date: 2029-04-06T14:42:58.404
+ thrust profile: [0.7389372747066383 -0.16997310988526818 -0.17093980484750101; 0.06328035594963484 0.021214609212457373 -0.05858833747025658; 0.03250514307434152 0.02095671975387968 -0.05269938589079231; 0.030209415319807052 0.025861200059332675 -0.06659545877411495; 0.15506138308097428 0.11141584710013624 -0.30739791960662843; 0.01982936715465988 0.023913315353704005 -0.06691582465781476; 0.010030099274136282 0.014675145895489917 -0.041695493054262366; 0.012586543381291575 0.019277054379676226 -0.05763229144699825; 0.012417804644490818 0.02372855895217448 -0.07177116073104851; -4.3510073418020004e-5 0.0045978814416816755 -0.017039677371050013; -0.0014648138414205918 -0.0007025985972317372 -0.003480430809935794; -0.0009145945138410788 -5.249964357860633e-6 -0.00369814809663667; -0.0005790289639198917 0.0010632181742556894 -0.001904377982942144; 0.0008378805627781905 -0.0002655289429433266 -0.0008205082087605312; 6.865794522403399e-5 0.000966636506927825 -0.0018499772526205545; -0.0026052193782534826 0.001140927057087277 0.002507429319035268; 0.0017462308610371592 -0.0004296103572469349 0.0013868391632975928; 0.004419099035077109 0.001704394657406039 -0.0010686122445991398; -4.8090629877485926e-5 -0.0008154972983729436 0.0008822950051558935; -0.0012300814508501086 -0.0003275385564128695 0.001988369235429531] %
+
+Mass Used: 124.97730804623961 kg
+Launch C3: 91.42238574138942 km²/s²
+||V∞_in||: 5.761250900096843e-7 km/s
diff --git a/archive/ES_0.5642517579156444 b/archive/ES_0.5642517579156444
new file mode 100644
index 0000000..3b197b8
--- /dev/null
+++ b/archive/ES_0.5642517579156444
@@ -0,0 +1,22 @@
+archive/ES_0.5642517579156444---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T05:31:23.924
+Launch V∞: [6.108366569230805, -7.732217733148591, 0.02866549741231831] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.897426126773252e-10, -2.584066088502999e-9, -8.157260160104393e-9] km/s
+ V∞_out: [2.8064346374393555e-9, 6.188162330046125e-9, 3.098655186049396e-9] km/s
+ time of flight: 1.7251959928298813e8 seconds
+ arrival date: 2028-10-14T23:38:02.924
+ thrust profile: [0.22271321328045252 -0.08368227877408772 -0.08736443941404365; 0.10192019359235209 0.01399698386998251 -0.11234812468610031; 0.08969961241003621 0.03191643596261923 -0.16122440991858752; 0.07469266187129267 0.03714921731381534 -0.184242258980329; 0.08664152022816067 0.05244041699461939 -0.26565043055172616; 0.02763828409700214 0.019349302143689368 -0.10610387472935001; 0.013982842275397334 0.01096606290318404 -0.0634989890265053; 0.0036064318432446917 0.002997381803578319 -0.01937059487912939; 0.002041262183737186 0.0022890594592423364 -0.014457605908297847; 0.002590136271723998 0.0016936763192162154 -0.014104509904558065; 0.0034220453779891745 0.0034672029999251123 -0.02274438489517935; -0.00045808808954115427 3.991289187758229e-5 -0.0009034543686750721; -0.0003717201345364624 0.00032772905222864596 -0.00011176130967537523; -0.00038528945968040353 0.000552829443009937 -0.00046238450012273385; 0.0006221539371053101 0.00040927388686232217 0.0009032193166996148; 0.001150746109657473 -0.00044971343207078 0.0002399727772024895; 9.606416044357773e-5 0.0002190965246790515 0.00047495357486470295; -0.0003896461400922348 -0.0001924334445823646 0.00016783336264811473; 0.00014391035058355112 0.0002680517157001166 -0.00019889998907868074; 0.00015774607316688708 -0.0020410724323741084 -0.00011855465440931923] %
+
+Mass Used: 91.87614715692553 kg
+Launch C3: 97.10015492765594 km²/s²
+||V∞_in||: 8.570772351197384e-9 km/s
diff --git a/archive/ES_0.5642539096073271 b/archive/ES_0.5642539096073271
new file mode 100644
index 0000000..a0f59d9
--- /dev/null
+++ b/archive/ES_0.5642539096073271
@@ -0,0 +1,22 @@
+archive/ES_0.5642539096073271---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T23:44:29.233
+Launch V∞: [6.171874348417226, -7.75981111125419, -0.029154986645948306] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5254255342464067e-8, -6.560852380929707e-9, 2.0921957334367427e-8] km/s
+ V∞_out: [6.644999727337004e-9, -1.6391422924880513e-8, -2.1008808486124707e-8] km/s
+ time of flight: 1.7936912318651643e8 seconds
+ arrival date: 2029-01-06T00:29:52.233
+ thrust profile: [0.1836433727235789 -0.05888193462388977 -0.06386264943907205; 0.05847772317803748 0.011140240282508528 -0.06458801422176588; 0.06433603511428708 0.02819631878875394 -0.11551486329719304; 0.03867196532631143 0.02258145768419573 -0.09898232797983667; 0.07267328738594508 0.04473225735208279 -0.18398408750603382; 0.04921797311206535 0.03381375329457586 -0.165479195919749; 0.03000655860110835 0.025047544235322083 -0.13305170696473478; 0.008072814657471044 0.008801964452741633 -0.038859693899282795; 0.012597385025169092 0.012671356217872074 -0.07104157502121906; 0.0009481603821449175 0.0011089910541107874 -0.005860537069152467; 0.0006322599337266655 0.0009178138893310142 -0.0048005293645131215; -0.00023203579705872844 -5.449592848275211e-5 0.000290201339512855; 6.885891478273769e-6 0.00016633464791244716 0.0015587726362863647; 0.0006001566039077383 -0.0005041702180736334 -0.0011435626797461221; -0.000693721215217568 0.001020089399175866 0.0014793408711884976; -8.873797229605481e-5 -1.58278278411769e-5 -9.39813070341155e-5; -0.0006933099000711511 -0.00018441012296626378 -0.0011549933396762105; 0.0005819778206425494 5.907687499914108e-5 0.0005552348190505249; 0.00013410299953332485 0.001393405952906408 -0.0012398088731764277; -0.0008906429154617314 -3.700022825957331e-5 0.0008846611608755088] %
+
+Mass Used: 84.83551097714326 kg
+Launch C3: 98.30755146824086 km²/s²
+||V∞_in||: 2.6710772896315366e-8 km/s
diff --git a/archive/ES_0.5642573147951144 b/archive/ES_0.5642573147951144
new file mode 100644
index 0000000..3ef025e
--- /dev/null
+++ b/archive/ES_0.5642573147951144
@@ -0,0 +1,22 @@
+archive/ES_0.5642573147951144---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T12:14:24.800
+Launch V∞: [6.328953192393752, -7.446079104648289, 0.01444677130211083] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.014652643361785e-7, -9.831845233541689e-5, 6.621928580806628e-5] km/s
+ V∞_out: [5.69382465370392e-5, 0.00010478239666316693, -2.1037612937869167e-5] km/s
+ time of flight: 1.8509979185947332e8 seconds
+ arrival date: 2029-03-12T20:50:55.800
+ thrust profile: [0.41816891899126885 -0.12136641653155687 -0.15255750961118944; 0.06038816709931021 0.012205313590288546 -0.06741284572632444; 0.07489329936037122 0.030497967875450303 -0.13898650579828956; 0.042352337995499194 0.024608506820864233 -0.115077607322492; 0.03496719330889239 0.024349208616730088 -0.12244059893568723; 0.023235666395236103 0.018681748174036925 -0.09955710093410176; 0.021165040015605645 0.01803985709311877 -0.10482416384415504; 0.006549251582293659 0.006434876430302442 -0.038481238675526906; 0.006994632223525196 0.007258605877451909 -0.042246244479223975; 0.001169617913787615 0.0013495617005157396 -0.011695306329271222; 0.005720839841547949 0.006085349535630526 -0.04210815550662589; 0.0007149146246272949 0.0024229767691234996 -0.012829043476968836; 0.0016076097829158236 0.002673341687716819 0.0002090099144326221; -0.0009700342150718369 0.0006554195029334365 -0.006435159742637794; 0.0011684071808801487 0.002173598373832643 -0.004874326761902069; -0.0004749581505293539 0.0005353967376784056 -0.004447770107994273; 0.0012199082979872128 0.0004719307752899071 -0.0032450466955840315; 0.0039002373658567828 -0.0011869129730320087 0.0014051973406183377; 0.0012784295818539342 0.00020078655145214404 -0.005615128932242896; -0.0054407112634240334 0.003829191421060053 0.005524864346250264] %
+
+Mass Used: 101.21715161618022 kg
+Launch C3: 95.499951253392 km²/s²
+||V∞_in||: 0.00011853945656981735 km/s
diff --git a/archive/ES_0.5642582354487204 b/archive/ES_0.5642582354487204
new file mode 100644
index 0000000..ba147b0
--- /dev/null
+++ b/archive/ES_0.5642582354487204
@@ -0,0 +1,22 @@
+archive/ES_0.5642582354487204---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:08:12.845
+Launch V∞: [6.497792922131684, -7.369845844608145, 0.10740021541015767] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1805952502158806e-6, -2.9915090938378946e-6, -3.488985161823768e-6] km/s
+ V∞_out: [-4.322098143613938e-6, -2.673140164897525e-6, -7.023579426414507e-8] km/s
+ time of flight: 1.874957778748869e8 seconds
+ arrival date: 2029-04-09T02:17:49.845
+ thrust profile: [0.31317412512297804 -0.07760946859014384 -0.08985418291915805; 0.08995614324219459 0.0282488600676835 -0.08691445949959208; 0.04931135861021432 0.029502093447569787 -0.08169411721302677; 0.025025710990066032 0.020456781203895255 -0.059706166987636505; 0.027186281502837095 0.026908498396981916 -0.08244534665505963; 0.025360966152178928 0.02873361217805834 -0.09170723597227894; 0.02303448152561535 0.029130041818896526 -0.09940971834811549; 0.0072088896558643 0.010255991363787704 -0.03873399336472272; 0.04764126391251894 0.06927537254676579 -0.22639302022196134; 0.005089469548692478 0.00835147216255466 -0.03315742561036381; 0.0007479092733362709 0.0012677730385327515 -0.005332827024269375; 0.0004532426943446654 0.0007366630912393416 -0.003089937662049167; -0.0009942466295048647 0.0015545367562270849 -0.000780025734781795; 0.00011058906070893025 -2.113525520622641e-5 -0.0012944999056570918; 0.0006062027116337995 0.0001194803112801226 -0.001050836800205946; -0.003834801292543173 0.000610793724103229 -0.003993386310918601; 0.0003016586434489744 -0.0004430295705696228 -0.0010230087243188529; 0.0032007822320536386 -0.00013778497163781863 0.0013475431016012152; 0.00036813397563849657 0.0016647755685736047 0.0027506705726663; 0.0022250822643595865 -0.000886948361661991 -0.0019318587697155312] %
+
+Mass Used: 95.1076679658081 kg
+Launch C3: 96.5474754384627 km²/s²
+||V∞_in||: 5.086957810244282e-6 km/s
diff --git a/archive/ES_0.5642611193969427 b/archive/ES_0.5642611193969427
new file mode 100644
index 0000000..8305f5a
--- /dev/null
+++ b/archive/ES_0.5642611193969427
@@ -0,0 +1,22 @@
+archive/ES_0.5642611193969427---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T05:59:43.500
+Launch V∞: [7.577912527592514, -6.245246178460718, -0.09333309056169438] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007395505959239028, 0.0004971770828842845, -0.0002355157675790134] km/s
+ V∞_out: [-0.0003870237405902543, -0.0007079910784097631, 0.00044642731376551487] km/s
+ time of flight: 1.6724041252821818e8 seconds
+ arrival date: 2029-08-27T21:39:55.500
+ thrust profile: [0.3811077070674411 -0.05874043561424263 -0.13812115905889097; 0.046908054230089286 0.01655085872903542 -0.057299934081502635; 0.04919408731675595 0.030184678520506547 -0.10156378678639863; 0.05790428881073467 0.04703186268160586 -0.16647673579117406; 0.03011771649197465 0.028192628135841464 -0.11410766963060541; 0.019817184922563284 0.020787399491286624 -0.09166720253322286; 0.006937640861597884 0.0076088809088526495 -0.03696561908891514; 0.03140498155473723 0.03787389168106341 -0.1771757680245596; 0.005079242070070914 0.006213599826100001 -0.036498969351120056; 0.007876424992323912 0.00995268168178443 -0.058641305468938545; 0.0029560808085410555 0.004125569458595882 -0.024885083566623636; 0.009886719532931484 0.014593158458512239 -0.08407530212922049; 0.00011124730255539396 0.00011278505081994164 -0.000853384753596329; 0.0002848828121078298 0.0001159071404297371 -0.0004709932517203273; -0.00011094999149952116 0.00015747092492937408 -0.0006530276775332425; -1.693590160042877e-5 0.0010670516859221024 -0.0004157601642043474; 5.039070620813265e-6 0.0003320092428115134 -4.885894535557568e-5; -0.00030629032444443526 1.7046295893097966e-5 -0.0005903431522013625; 5.7398306942803106e-5 -4.636066527359062e-6 -0.000159802331543526; -0.0003224577572128722 -0.0003507389647602186 1.753285468959352e-5] %
+
+Mass Used: 95.7579857976757 kg
+Launch C3: 96.43656917121557 km²/s²
+||V∞_in||: 0.000921730878540509 km/s
diff --git a/archive/ES_0.5642624187409208 b/archive/ES_0.5642624187409208
new file mode 100644
index 0000000..afc8763
--- /dev/null
+++ b/archive/ES_0.5642624187409208
@@ -0,0 +1,22 @@
+archive/ES_0.5642624187409208---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T17:39:36.837
+Launch V∞: [7.697144608259772, -6.000978991476535, 0.007411812280554687] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.260816880327386e-7, -3.1883421441737498e-6, -9.294675838887136e-6] km/s
+ V∞_out: [-8.92034548746701e-6, -1.0426824736214268e-6, 4.097433040731204e-6] km/s
+ time of flight: 1.7814821262756872e8 seconds
+ arrival date: 2030-01-03T15:16:28.837
+ thrust profile: [0.4720785696120338 -0.035054069855056304 -0.15781958411434788; 0.04618970639129718 0.021137733588985092 -0.052586963061438646; 0.05450483120687266 0.04348911233951291 -0.10986211086198437; 0.022576573576199913 0.02297495632709504 -0.06871812633152524; 0.028969852080434566 0.03342861323611952 -0.10898987663787141; 0.015705889423763886 0.02190405246524963 -0.08566306920826766; 0.017836724518039727 0.03615271004500866 -0.12604561414125448; 0.007353311587969754 0.010650040960714334 -0.04074406678813233; 0.006176523035175969 0.015584609740207868 -0.062126261174978284; 0.00750918791423822 0.017433249476183826 -0.07483387281978947; 0.004864641076133599 0.008563856043408239 -0.04534600032837011; 0.0031385608643130208 -0.008486287096190039 -0.004704493856407365; 0.002638130406173998 0.009505666082874809 -0.002836811158150711; -0.002382592410513202 0.006189499514546907 -0.0035139922484851214; -0.003590960748005241 -0.003691807807604532 -0.005785911727717378; -0.0013011348332947724 0.016854919329832702 -0.008520802605805924; -0.0012957980212053456 -0.004170309064723972 -0.003059755540124642; -0.0025725701232133893 -0.0022345274202616146 0.0023649408457674533; 0.006044937695735647 -0.02004857868787834 0.002064087082516658; -0.006162013772810446 0.00922797431192247 -0.00695643693798931] %
+
+Mass Used: 102.63542821360306 kg
+Launch C3: 95.25783891156648 km²/s²
+||V∞_in||: 9.869860782767725e-6 km/s
diff --git a/archive/ES_0.5642628046704565 b/archive/ES_0.5642628046704565
new file mode 100644
index 0000000..68a9270
--- /dev/null
+++ b/archive/ES_0.5642628046704565
@@ -0,0 +1,22 @@
+archive/ES_0.5642628046704565---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T13:50:07.421
+Launch V∞: [6.459455632834019, -7.4356943743500565, 0.13713238624982654] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.939470788475787e-6, 5.37254557250385e-6, 5.130069689483246e-6] km/s
+ V∞_out: [7.539275021809296e-6, 4.765965605261857e-6, 1.504259524824404e-7] km/s
+ time of flight: 1.8507992336147785e8 seconds
+ arrival date: 2029-03-10T16:55:30.421
+ thrust profile: [0.21763627315707515 -0.051745185851369904 -0.06509463420892557; 0.09579838983355504 0.032532449422818674 -0.09010485686600153; 0.1062766474701415 0.06516002266307781 -0.16198395103709076; 0.07126386897140237 0.0710488659141267 -0.15979410932035829; 0.017857879375742014 0.020137791526763982 -0.05541722741684392; 0.02309446098699001 0.029858901720143802 -0.08489673316595935; 0.031117553616703757 0.03974964288281184 -0.11346042454493381; 0.015257491209201252 0.024022991929724607 -0.06873515430615833; 0.006245214500923541 0.012458360330736669 -0.040536676166663975; 0.007844659529437062 0.019150455456833294 -0.057996804793774594; 0.0016614397926919887 0.0007838563791393806 -0.00047405522304632807; -0.001112739704633482 0.00024718840654340893 -0.009308592803290664; 0.00039411678069791416 0.002095578248778946 0.0006749433171206213; -0.0021852498492188387 0.0012289537369946952 0.0008244410793884246; 6.407619800680495e-5 -0.000994240367709094 0.0006696275660954985; -0.0008532633773623833 -0.000883130250314502 -0.0049996910040489145; 0.0015100227276318844 0.0035241398972615245 -0.00133943162729073; 0.0029489744912314917 0.0014324151373463095 -0.0003956659836426178; 0.00033720651422389876 0.00019441617647194653 -0.0010897634468525503; 0.0008791924780416399 0.001399627075338733 0.0009537722791030678] %
+
+Mass Used: 92.2812201584029 kg
+Launch C3: 97.0329231926508 km²/s²
+||V∞_in||: 8.920775337255784e-6 km/s
diff --git a/archive/ES_0.5642887991641435 b/archive/ES_0.5642887991641435
new file mode 100644
index 0000000..71269cf
--- /dev/null
+++ b/archive/ES_0.5642887991641435
@@ -0,0 +1,22 @@
+archive/ES_0.5642887991641435---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T20:09:29.242
+Launch V∞: [6.580826699791038, -7.457128412685127, 0.0996191310359808] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00092158263701888, -0.005998724083220211, 0.007895486991601629] km/s
+ V∞_out: [-0.007177978737381849, -0.005608988290602195, -0.0043909109705106315] km/s
+ time of flight: 1.8513970501091695e8 seconds
+ arrival date: 2029-03-13T15:51:14.242
+ thrust profile: [0.12996903565450207 -0.03781139913310626 -0.05095529530522386; 0.09643112174283189 0.019621086103021972 -0.11427944735153753; 0.0485573715193263 0.02025691885965425 -0.09890943056992695; 0.03928624470062488 0.023390794302803084 -0.11357249151906515; 0.04138217208379871 0.028493963222285028 -0.1506508159773193; 0.01851872751131883 0.014947148554021034 -0.0866476856107079; 0.006648413818201971 0.007948195210575233 -0.043605498818286514; 0.015958835685042316 0.014532941845095092 -0.08918319886791022; 0.007903112800551547 0.0026135868140842503 -0.041701421386050465; 0.004976213190435906 0.0046426131117448186 -0.05926434805113297; 0.0008953421396968624 0.004993466340262681 -0.03630261765355797; 0.0018206038453500014 0.0023870732304824577 -0.018536737849257412; -9.191570736771424e-5 0.0005183916092533537 -0.004359134090850658; 0.0005096791835776475 0.0009751558534052869 0.00020539781010670715; -0.0009566869537366945 0.0004741545738069634 -0.001133743761393856; -0.0005864893634716715 -0.003011666033050872 -0.0013434032083240628; -0.0030895029529760345 -0.00036376332676568246 -0.001602929788321774; 0.003141412434062049 -0.0024974840722224835 -0.007309250099027543; 0.0007626565886774518 0.0012996235696393819 -0.00034341441068807654; -0.004513914248998773 -0.0032108861457701976 -0.0018047149727506233] %
+
+Mass Used: 81.2687845993446 kg
+Launch C3: 98.92596818722677 km²/s²
+||V∞_in||: 0.009958550096174211 km/s
diff --git a/archive/ES_0.5642993513115102 b/archive/ES_0.5642993513115102
new file mode 100644
index 0000000..67eb860
--- /dev/null
+++ b/archive/ES_0.5642993513115102
@@ -0,0 +1,22 @@
+archive/ES_0.5642993513115102---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T07:06:29.849
+Launch V∞: [6.669039619761935, -7.307765384654268, 0.15868339859561506] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.932715486834837e-8, -1.9684341049876091e-7, -7.525623795629434e-8] km/s
+ V∞_out: [5.961879777797103e-8, -1.1709142987349114e-7, 1.8802220553939759e-7] km/s
+ time of flight: 1.874957778741387e8 seconds
+ arrival date: 2029-04-08T09:16:06.849
+ thrust profile: [0.2082727687010011 -0.051304830446323064 -0.0679873514022153; 0.06860458741207434 0.020753373361650024 -0.0756954870500983; 0.0707383343082667 0.040673889079783816 -0.11417177539291652; 0.04772199588624946 0.03386388393490063 -0.10784627792849687; 0.036704413779968456 0.038013926395263145 -0.1111586567000342; 0.025086248148122953 0.028274937946814994 -0.10055373256223207; 0.023011192016069985 0.02774835477630851 -0.10211771193509192; 0.01563189327390816 0.026107859240804096 -0.09847932602432957; 0.004596827705262452 0.008493981597121877 -0.03649639050893923; 0.0012908227647121782 0.0010601409045916188 -0.013080704378358454; 0.00543548928098786 0.010358004504529648 -0.04057214265427465; -6.93641773480279e-5 0.0033400288086197806 -0.006323291384965177; -0.0005493812074844613 -0.0002055020650840189 -0.0009453693089387199; 0.0038033581107748743 -0.0003243013328429384 -0.0027821049164524205; -0.0007959516732483408 0.00031453178974101244 -9.662937286022619e-5; -0.00334687905973726 0.00132347441780453 -8.447591541171137e-5; 0.0016693228737642341 -0.0004907004406659638 -0.0006791530465210787; -0.000857582175030892 -0.0006748284646467924 -0.0006315090220925198; 0.0009368790043262978 -0.0006530813900759196 0.0017355704823586245; 0.0010034998047305627 0.004576040419078753 -0.01790591174922681] %
+
+Mass Used: 87.23846526620537 kg
+Launch C3: 97.90470478809542 km²/s²
+||V∞_in||: 2.2888899100872454e-7 km/s
diff --git a/archive/ES_0.5643020693769174 b/archive/ES_0.5643020693769174
new file mode 100644
index 0000000..3279497
--- /dev/null
+++ b/archive/ES_0.5643020693769174
@@ -0,0 +1,22 @@
+archive/ES_0.5643020693769174---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T09:53:57.215
+Launch V∞: [6.589621178931784, -7.50203988843021, 0.1610570978951235] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0016264662689453326, 0.010373453872339011, -0.013821947549894407] km/s
+ V∞_out: [0.01203393856904019, 0.009879583173010494, 0.008362424712464374] km/s
+ time of flight: 1.8527948846149457e8 seconds
+ arrival date: 2029-03-15T20:25:25.215
+ thrust profile: [0.06957166381663114 -0.02069865494958039 -0.025366568563956814; 0.04650753070431153 0.008680852929836351 -0.05040310928268599; 0.0860666273887255 0.03459917986023881 -0.1630675155715638; 0.05344374559099257 0.028313800734612288 -0.1402992509966099; 0.04634070663401304 0.02901340846477142 -0.15508712648124726; 0.023868025189846966 0.016746911705788004 -0.09489848425578587; 0.015408064528187486 0.011882381640537763 -0.07096043337597141; 0.004166116188558807 0.0036386859185672804 -0.022818909019777605; 0.01247163687633199 0.005958924492752659 -0.04936616665408353; 0.0033195624065944828 0.0014370890114436142 -0.02186421952905096; 0.004673047774942086 0.0022250909399501714 -0.03440498904677801; 0.0015113047110324172 0.001941527625461926 -0.01378325164343315; 0.002905614487807683 3.4844337261124864e-5 -0.0329447573910716; 0.0007071829074420401 0.006208829242517334 -0.005447477023426243; 0.00047296121850104575 0.0022819758673271106 -0.0066506159058507255; 0.002392989811423515 0.0006645557839395945 -0.00200056490342013; -2.8788643318128013e-5 0.0015266565706028232 0.0005060436202770939; 0.0016198903357999526 -0.001154048414162956 -0.0053986596986585885; -3.888359099025779e-5 0.005479468419428718 -0.007259219687094765; -0.0004945626976421433 0.0005743979217179081 5.224167481012072e-5] %
+
+Mass Used: 76.59612751686473 kg
+Launch C3: 99.72964915820668 km²/s²
+||V∞_in||: 0.017358000225763167 km/s
diff --git a/archive/ES_0.5643021672507705 b/archive/ES_0.5643021672507705
new file mode 100644
index 0000000..fde9b79
--- /dev/null
+++ b/archive/ES_0.5643021672507705
@@ -0,0 +1,22 @@
+archive/ES_0.5643021672507705---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T01:15:25.340
+Launch V∞: [6.623581250349563, -7.376743535706094, -0.07855826791661653] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.523745577717867e-9, -1.6985381601724445e-9, 3.868747526333461e-9] km/s
+ V∞_out: [9.536748402382542e-10, -2.150351939751221e-9, -3.0040594426111313e-9] km/s
+ time of flight: 1.8749577785246637e8 seconds
+ arrival date: 2029-04-10T03:25:02.340
+ thrust profile: [0.23555655885512913 -0.05556566806475396 -0.08258923089907785; 0.027925522903333583 0.0077615906334767525 -0.03256978206043848; 0.02733068806205665 0.014630670117188634 -0.05243235714009756; 0.030220965170843567 0.022534153375762398 -0.08109323488259594; 0.019800902571814667 0.01738597071015496 -0.06807904011937868; 0.02064113590697822 0.02084749513755809 -0.08860970839528921; 0.007810909399557309 0.010031072618442818 -0.049615049156833145; 0.05905209912351142 0.06311732789265842 -0.26976546225336334; 0.007679333751429565 0.009545890906555356 -0.05071614581629263; 0.008506465380968766 0.009721727902047636 -0.07143739041036998; 0.0019972169926451536 0.005117239281525823 -0.032034943908589304; 0.0015282155554390737 0.003988177963980704 -0.015513005822428557; 0.00016872903477175162 0.0003500241572133827 -0.0008216324360190539; -0.00019634311263311396 0.0008328655169584902 0.0015770064207358435; -0.0006033586713041338 0.0017068758517365843 -0.002705278180404236; -0.000247267606654842 -0.001788032000246631 0.0007867086347639195; 0.00031639180870775784 0.00035891747690542123 0.0010590166472385265; -0.0012072738145121585 7.644547472870141e-5 0.0028142168965721156; 0.00014594525820372617 0.00029999225101298623 0.0006354804095481971; -0.0011840410183783267 -0.0006730792061714085 -1.9431845878171202e-5] %
+
+Mass Used: 84.96884828327075 kg
+Launch C3: 98.29434517302198 km²/s²
+||V∞_in||: 6.190033388924105e-9 km/s
diff --git a/archive/ES_0.5643084867495379 b/archive/ES_0.5643084867495379
new file mode 100644
index 0000000..d9306c5
--- /dev/null
+++ b/archive/ES_0.5643084867495379
@@ -0,0 +1,22 @@
+archive/ES_0.5643084867495379---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:13:14.303
+Launch V∞: [6.650889845864882, -7.43576280043107, 0.16047758823529998] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4955621607887946e-9, -2.5210309553433417e-9, 4.478463870769484e-9] km/s
+ V∞_out: [1.046883092583034e-9, -2.947410412901911e-9, -3.9020674426301615e-9] km/s
+ time of flight: 1.874957778747647e8 seconds
+ arrival date: 2029-04-10T12:22:51.303
+ thrust profile: [0.06187585673274299 -0.015636088291828363 -0.025700760113543955; 0.09588583256016325 0.024294120748775263 -0.10618035083379611; 0.07374512476715638 0.036430216615280064 -0.13850007385928112; 0.043125716557833045 0.026876711523862205 -0.11528132407454228; 0.03998013336725889 0.030902800301273663 -0.1347545043591809; 0.012007421966203977 0.010147478740276127 -0.061785677815006684; 0.018180284052369537 0.014056101501223486 -0.08262782840406911; 0.006199511813934966 0.012858086939096045 -0.054591478277491674; 0.020072057425888384 0.023414639507310236 -0.12355021113468917; 0.002295334880758571 0.0023360821405968664 -0.008415572018098408; 0.0003019962126214397 0.0019180294193443944 -0.005434997884637867; -0.0004574240492960721 0.0003929588476538266 -0.0016109011812013249; 0.0011525047829334181 0.001312986377962642 -0.0012629768762242276; -0.0008345286023388841 0.00039073202831312276 -0.0080997507165971; -0.0016832638684092316 -0.00038642283389052 0.00030001715030975734; -0.001061937189169263 0.0009696940477194238 0.007696725974379803; -0.00014297713991027574 -0.0011924062568238248 0.004968120431648909; 0.0018512688950323725 0.0050211508478695275 -0.0009263089564242703; -0.003395373295179812 -0.0016957894382953363 -0.0012909207548289087; 0.007526977055380284 0.005148447309340838 -0.005932900612186496] %
+
+Mass Used: 77.64773407695884 kg
+Launch C3: 99.55065722242892 km²/s²
+||V∞_in||: 5.713148538060934e-9 km/s
diff --git a/archive/ES_0.5643134598669958 b/archive/ES_0.5643134598669958
new file mode 100644
index 0000000..655b2d4
--- /dev/null
+++ b/archive/ES_0.5643134598669958
@@ -0,0 +1,22 @@
+archive/ES_0.5643134598669958---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T19:57:52.801
+Launch V∞: [6.370411235469535, -7.2374722470241455, 0.35508096607917183] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4222118091393257e-5, -2.1775712449299503e-6, 3.8882339964292485e-8] km/s
+ V∞_out: [3.176695194367047e-6, -6.217708951833083e-8, -1.4026741278585644e-5] km/s
+ time of flight: 1.8588022464128977e8 seconds
+ arrival date: 2029-03-18T05:21:36.801
+ thrust profile: [0.576505992402562 -0.1499013308142395 -0.17113504741475588; 0.10331051060968838 0.030730554883757748 -0.0950411540623056; 0.09497395686941074 0.054111079470695045 -0.14503607485888007; 0.07374203834283098 0.057611890523814595 -0.15925979186277786; 0.050886461111683316 0.048797909239197065 -0.14231893933884882; 0.010265440618643781 0.012469183138422171 -0.040036058358669455; 0.00884869813259665 0.011672092734829173 -0.03832590304306541; 0.006669604571826688 0.01368965547857061 -0.04968671610965951; 0.018406331465122213 0.02536175301101047 -0.09130228751059166; 0.0006711559637645048 0.0012129668204886525 -0.006066430006244681; 0.0009637592553051656 0.0019084928306158534 -0.00720663901896784; 0.0009974495995000165 0.0022874007403541037 -0.009074709262346705; -3.112746623384845e-5 -0.00025042464609129463 0.0009604620310151282; 6.5020011971163905e-6 -0.000283471877114023 0.0014415086788133046; -0.00016094582072707898 -0.0008823800311707521 0.001132380750740153; -0.0007779149110128498 0.0002124737891125861 -0.0007697765301997735; 0.00020541932183926122 -0.0008461587738909751 0.0017843960677601707; -0.00029282205393307235 -0.0008059100914354989 0.0030185414198354464; -0.00033958413515758275 -0.000876752014779693 0.0023434639540035624; -0.00015317445948376224 -0.00017226510840943375 -0.0012151852223251896] %
+
+Mass Used: 115.34521626533615 kg
+Launch C3: 93.08922632791295 km²/s²
+||V∞_in||: 1.4387910597742893e-5 km/s
diff --git a/archive/ES_0.5643221920460123 b/archive/ES_0.5643221920460123
new file mode 100644
index 0000000..1920bbd
--- /dev/null
+++ b/archive/ES_0.5643221920460123
@@ -0,0 +1,22 @@
+archive/ES_0.5643221920460123---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T05:25:37.547
+Launch V∞: [6.737631491195215, -7.27671998391536, 0.47311850042751263] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.5268193668761624e-9, -7.167841716505825e-10, -2.4512837768562886e-9] km/s
+ V∞_out: [-1.452938305550084e-9, 3.2838933354329604e-9, 8.352373050781279e-11] km/s
+ time of flight: 1.8749577787709922e8 seconds
+ arrival date: 2029-04-08T07:35:14.547
+ thrust profile: [0.17454126449179028 -0.042518949410060576 -0.06011596979380889; 0.08082535611799756 0.023603155077286716 -0.08726390512914586; 0.070948656587943 0.03798308221641459 -0.12759726795091575; 0.03808895601574616 0.028739099207352414 -0.09751915531935369; 0.03117292858485981 0.02869556134536441 -0.10426105838560112; 0.02978513280286671 0.03097645803837877 -0.1202562062333686; 0.014413206777320421 0.017110171178240645 -0.07155865124106743; 0.0176558418772531 0.021705945012272163 -0.09472454656721006; 0.005733194634153206 0.007808326948338709 -0.03642527864945804; 0.0029730782075903343 0.003421856551477727 -0.020452721975492964; 0.0054838411977426735 0.006799128670268665 -0.0323469629928344; -0.0012269291662262611 0.002582138705788364 -0.005181789964628259; 0.0009201327053435511 -0.0002711663725957273 0.001402746662579678; 0.0040398438529526655 -0.00234443175151818 -0.003791952658970923; -0.0016163419118357582 -0.001113851577773293 0.0009589438794870746; -0.0015737488625906352 0.0024426213684067997 -0.006838752110715846; -0.00040802387817625923 0.002970732638918657 -0.003908009756499901; 0.004939322759546446 0.0014617788750818346 -0.004191613451490347; 0.0014522865118779499 0.0005343108966539101 -0.0035172465775231837; -0.0008542644893251325 0.0005387390896951002 -0.0016515651197601825] %
+
+Mass Used: 83.38321517339955 kg
+Launch C3: 98.57017295090539 km²/s²
+||V∞_in||: 3.5926853210694773e-9 km/s
diff --git a/archive/ES_0.5643349008617896 b/archive/ES_0.5643349008617896
new file mode 100644
index 0000000..ad098af
--- /dev/null
+++ b/archive/ES_0.5643349008617896
@@ -0,0 +1,22 @@
+archive/ES_0.5643349008617896---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T18:19:18.656
+Launch V∞: [6.352777981579001, -7.4130216657726455, 0.14399724031514352] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.9832120112412775e-6, 6.039282204724708e-6, 6.494816196668856e-6] km/s
+ V∞_out: [9.018177136510962e-6, 5.750071557829371e-6, 1.7724815537817478e-7] km/s
+ time of flight: 1.8749577787637827e8 seconds
+ arrival date: 2029-04-08T20:28:55.656
+ thrust profile: [0.3322070428800294 -0.07401038932222168 -0.09958610797464112; 0.19167090791949312 0.06827571042280044 -0.17800864406737307; 0.060467581258698215 0.037650511522674714 -0.10092718299765634; 0.04519537785382407 0.03866884544817897 -0.10760062681155491; 0.03677906075355355 0.03816864205866574 -0.11206393629958421; 0.03064455441972545 0.03734570196109196 -0.11476295521305005; 0.011087926142529089 0.01477164917890918 -0.04991028921781185; 0.007247823585435943 0.010576569908754177 -0.03797419347700104; 0.009559917628923283 0.01592419064291876 -0.058114740944426424; 0.0038713062953214038 0.008926270511999403 -0.035934017848978525; 0.0024909986388229497 0.0032345226529096917 -0.011988665879831625; -0.002449990826184964 0.0020340070950234375 -0.009142350058733595; -0.0019517610555325165 0.0004525463498373333 -0.0015485941440579033; -0.0009774298691023185 0.0004755481397215346 -0.0016989911083065718; 0.0008515856417778539 0.002669786354291455 -0.0007319902904645375; 0.003176208368284132 -0.0019448173659668637 0.002008915280828959; -0.0006152797530961088 0.007277984324726838 -0.0011324211665965818; 0.006992236957363078 -0.0018142777862087812 -0.008933201888771294; -0.00027069312586390417 -0.00023959667820258905 -0.001222735556740578; -0.0010250174544622704 0.0022143891910242934 -0.0037362040296650737] %
+
+Mass Used: 102.29080555569135 kg
+Launch C3: 95.33141350566798 km²/s²
+||V∞_in||: 1.0698335989689169e-5 km/s
diff --git a/archive/ES_0.5643457147747682 b/archive/ES_0.5643457147747682
new file mode 100644
index 0000000..10c096b
--- /dev/null
+++ b/archive/ES_0.5643457147747682
@@ -0,0 +1,22 @@
+archive/ES_0.5643457147747682---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:33:20.385
+Launch V∞: [6.556355770583496, -7.374081907064136, 0.14490245780396205] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00021800195905677543, 0.000268129634807018, 0.0002280678762132498] km/s
+ V∞_out: [-0.00024878308427949157, -0.00012481222249853075, 0.00027979529293365406] km/s
+ time of flight: 1.8749577787489823e8 seconds
+ arrival date: 2029-04-09T08:42:57.385
+ thrust profile: [0.2313517367104982 -0.056012628572114906 -0.07995068942808148; 0.08976267812427675 0.02575088184705182 -0.09571696843371041; 0.06996139543677614 0.038333979544332625 -0.12471158510499751; 0.06338214944602553 0.04672334278186824 -0.1567684077473873; 0.036324351635698256 0.03249778536277904 -0.11902031981089063; 0.024814686284439228 0.025690044469153267 -0.10224353328302493; 0.01176566647241755 0.01370532408126831 -0.05873552065679395; 0.00911891458093552 0.011895173507542626 -0.05274566493130472; 0.0038681791609973515 0.005211008251433339 -0.024713755633581583; 0.0025526322188685916 0.0035106990366935804 -0.013242083582360951; 0.004498218974580085 0.011750458304288969 -0.059142202977491336; 0.001503185665165037 0.0017199897688116015 -0.010979250261055007; 1.894560529077039e-5 0.0016999009109423579 0.0015243487747409034; -0.0008334397681314811 -0.0032106337862657626 -0.0006798325188327368; -0.001151901019237096 -0.00011594998886585802 0.004634331112300865; 0.0008089538360365254 -0.007148123561030614 0.0008355700731717568; 0.0029242743350738594 -0.006628625195313575 0.0023529030672305713; -0.0021037396981183243 0.0036323386518944613 -0.0006575280542250412; 0.0002646693134486882 -0.0005739173626204922 -0.0017930568395116957; -0.0012380548483949345 -0.002699066008083118 -0.004960192178226284] %
+
+Mass Used: 90.33069074237756 kg
+Launch C3: 97.38388168483178 km²/s²
+||V∞_in||: 0.00041404505959467635 km/s
diff --git a/archive/ES_0.5643499012258224 b/archive/ES_0.5643499012258224
new file mode 100644
index 0000000..9a8837e
--- /dev/null
+++ b/archive/ES_0.5643499012258224
@@ -0,0 +1,22 @@
+archive/ES_0.5643499012258224---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T04:41:24.708
+Launch V∞: [6.22199418332685, -7.587737551927004, 0.33769190135038935] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0027673404363945625, 0.0020345403287697493, 0.0029364223071593762] km/s
+ V∞_out: [-0.0029714796769654364, -0.001822386752113232, 0.0028736086119303997] km/s
+ time of flight: 1.7564381633543244e8 seconds
+ arrival date: 2028-11-19T02:38:20.708
+ thrust profile: [0.25653331876099955 -0.0828430416639876 -0.08813257001629339; 0.15401808121935992 0.032915952253595886 -0.15107834170842474; 0.09028380296495653 0.04216033494795691 -0.14687792708003583; 0.07922416935326522 0.050872366466543195 -0.1764819090619148; 0.050149719333578584 0.03870189806223662 -0.1422194498495477; 0.02942933882303559 0.027202983572986575 -0.1041353073859577; 0.01792689403996893 0.017558452166762235 -0.07412076798499898; 0.0179312719476454 0.02016855290606858 -0.08760690357578534; 0.003571019687724856 0.004381830339185754 -0.01888166263165643; 0.0046975184451175786 0.005257533828996827 -0.025085381613563586; 0.0015301981121884202 0.001689978439515498 -0.0084234375351596; 4.677631026575601e-5 1.6186413145325833e-5 -0.00013092508956978366; -0.00013198546902697697 7.328303983440134e-5 -0.0004391800139278235; 0.00020189436821616783 0.00012784430762182743 -0.0002569418981000041; 9.140918343390164e-6 0.00019346279566679434 -0.00020265755327149594; 2.332069837562091e-5 4.512729946274348e-5 -0.0002870823693103143; -0.0002177846988969523 1.5953924876410092e-5 -0.00036298085326548404; 1.4932763720530771e-5 -2.3161558835035448e-5 -0.0004469514512911442; 4.190145855274897e-5 3.914538010111316e-5 2.0323146607915574e-5; -5.047314960405014e-5 4.770728550465182e-5 3.38022363956989e-5] %
+
+Mass Used: 96.06900129546102 kg
+Launch C3: 96.40100859451401 km²/s²
+||V∞_in||: 0.0045188608527236334 km/s
diff --git a/archive/ES_0.5643544768665486 b/archive/ES_0.5643544768665486
new file mode 100644
index 0000000..d0e3745
--- /dev/null
+++ b/archive/ES_0.5643544768665486
@@ -0,0 +1,22 @@
+archive/ES_0.5643544768665486---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T05:24:35.051
+Launch V∞: [6.549696061617996, -7.3981457027706305, -0.0681036477108024] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.026019336599149533, -0.00039531836717167086, 0.020905214942805082] km/s
+ V∞_out: [-0.032724622245780564, 0.0002577898443199581, 0.006579004147606104] km/s
+ time of flight: 1.8749577787493476e8 seconds
+ arrival date: 2029-04-09T07:34:12.051
+ thrust profile: [0.19595025813703915 -0.04791544735567595 -0.06900822324688759; 0.07577740386763342 0.024957976321317275 -0.08263358923385139; 0.11785797895467662 0.06756736202352141 -0.20068962238372762; 0.03299304639927464 0.02361583130721258 -0.07683621728838946; 0.035035820905903584 0.028305201760752078 -0.10213618022071114; 0.023613380037946576 0.025886449231697962 -0.09019163035010276; 0.03205962780912669 0.041140744444828924 -0.1473417945989669; 0.007030927226234283 0.00883596940120902 -0.03493615819670854; 0.0010765011130245122 0.0029093978951643274 -0.012385713493045191; 0.003000314237210669 0.002049897906522903 -0.008831219185788443; 0.007477631374981973 0.020219662352229318 -0.054817722199815185; 0.0007778388567533218 -0.002269722824728177 -0.004168260221948949; 0.0013722247680241601 0.003512412650843028 -0.003917382977270352; -0.001334556166960841 3.446586407000274e-5 -0.004375135592874749; 0.00949818629897332 0.001478523513618304 -0.006168456605589674; -0.001239181280909216 0.005471126179657932 -0.000540010547282214; -0.0011025348022585919 0.00093914505292389 -0.0026712815394465137; -0.0006150308748369542 -0.0014026401977274268 0.0046584719027724045; -0.004654105662186045 -0.0006467886412001094 -0.006181762159971759; 0.0006679456529272727 0.002766953336980891 -0.0002592586326914195] %
+
+Mass Used: 88.87187707696876 kg
+Launch C3: 97.63571644582936 km²/s²
+||V∞_in||: 0.03337948719612311 km/s
diff --git a/archive/ES_0.5643636957703713 b/archive/ES_0.5643636957703713
new file mode 100644
index 0000000..7a7b57c
--- /dev/null
+++ b/archive/ES_0.5643636957703713
@@ -0,0 +1,22 @@
+archive/ES_0.5643636957703713---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T07:02:48.607
+Launch V∞: [6.295411671692523, -7.508746438365969, 0.07522029999204816] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0050418176079578625, 0.0033847339904223466, 0.0052262126970070025] km/s
+ V∞_out: [-0.005631906088797171, -0.002836473013485068, 0.004941830580122297] km/s
+ time of flight: 1.804204881402316e8 seconds
+ arrival date: 2029-01-15T11:50:56.607
+ thrust profile: [0.3398627015318442 -0.10205125374898023 -0.12193464064277648; 0.10020973538741208 0.023273786694565018 -0.1092221796438699; 0.05159727846091107 0.02510497776471289 -0.09708100806351809; 0.06345168206019293 0.04165787169915104 -0.1588195608428564; 0.04214888838522365 0.03380122835332564 -0.1369483404622355; 0.033928187507180595 0.031031360886171564 -0.13180906240418988; 0.014376262906674278 0.01429751910389535 -0.0630336659747166; 0.007625679660943368 0.009929012828829386 -0.04774397562615639; 0.00994948920440792 0.010449844044038245 -0.06523578471523396; 0.009325608058148561 0.009451286050074028 -0.0473378097706891; 0.0020386357789524854 0.0006965744502888231 -0.005122265573287671; 0.0010832049902057255 0.0009102308203346745 -0.005007989267750416; -0.002023074619341164 0.0007365839119769729 -0.0016873935897532522; -0.00023231446497924734 0.0005354363605402495 -0.00261156089117898; 0.0004706432497287036 4.5616723343237364e-5 -0.000808969265465467; -0.0011910112294217638 -0.0005853053376859239 0.003185403327372906; 0.0020859694373689796 -0.0019615345495866653 0.0009068318673625371; -0.00024132658995075745 -0.0010253023231118598 0.0065070431287267225; 0.0011282653996276316 0.0011163315933822424 -0.0012929833891859323; -0.0012608552522115652 -0.0033946097919305253 -0.0012504434445321172] %
+
+Mass Used: 98.31266590125915 kg
+Launch C3: 96.01913928528695 km²/s²
+||V∞_in||: 0.008011844240385077 km/s
diff --git a/archive/ES_0.5643762806034506 b/archive/ES_0.5643762806034506
new file mode 100644
index 0000000..0388e2f
--- /dev/null
+++ b/archive/ES_0.5643762806034506
@@ -0,0 +1,22 @@
+archive/ES_0.5643762806034506---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T23:25:28.348
+Launch V∞: [6.285218507478523, -7.410131920520238, 0.15357035097643243] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008996325619909265, -0.005803213658472468, 0.007768954010811991] km/s
+ V∞_out: [-0.006479676807457291, -0.005668508540596438, -0.004552083680216461] km/s
+ time of flight: 1.8589032288127986e8 seconds
+ arrival date: 2029-03-19T11:37:30.348
+ thrust profile: [0.3916462446364966 -0.08133219222177968 -0.10691235529285419; 0.1505617211264913 0.05473669313086647 -0.12572801796494687; 0.08426269252173994 0.05660637857668992 -0.11865351509752216; 0.08031515336369488 0.07619107917990575 -0.1588599976829343; 0.05891616446477765 0.06670418898861274 -0.14723321789687277; 0.026922568589377336 0.03740859417382567 -0.08980355945396588; 0.007978013817452369 0.012726017162129864 -0.03357868019767659; 0.007598334677080567 0.012356422061381482 -0.036652634754692735; 0.0055204926908763085 0.012578763956729924 -0.03745629297416401; 0.005733845520127047 0.011372991846764937 -0.03300095127425266; 0.005490647302631103 0.012582155478031529 -0.03748243581853495; 0.0008973756758219496 0.000911446801852534 -0.001626472793536397; 0.0012879418334833781 0.0002953885359281128 -0.001924343319509646; 0.0003106394258853355 0.0005157805671417925 -0.0028359953364422803; -0.0006732757309905373 -0.0008547564698677178 0.0016146335976864922; -0.00125902685027433 0.0008443187554139387 -0.0007009872826972425; 0.0003905340180035444 -0.000996803521805127 0.0017832975049114465; 0.000991172413474879 -1.4949160179112374e-5 -0.001066470784787426; 0.0004127940209244552 0.00043730600638748206 -0.0035427195977848444; -0.0010934177793723739 0.001622302083946261 -0.0024530068271207575] %
+
+Mass Used: 107.55293209341107 kg
+Launch C3: 94.43761061896251 km²/s²
+||V∞_in||: 0.009738751148611792 km/s
diff --git a/archive/ES_0.5643774398365109 b/archive/ES_0.5643774398365109
new file mode 100644
index 0000000..0b9fd9a
--- /dev/null
+++ b/archive/ES_0.5643774398365109
@@ -0,0 +1,22 @@
+archive/ES_0.5643774398365109---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:20:32.332
+Launch V∞: [6.634699955046302, -7.399662407327474, 0.2059140568902225] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.345626194097915e-6, -2.0867215769834283e-6, -2.568422788233262e-6] km/s
+ V∞_out: [-3.530127982091643e-6, -2.0297925300469746e-6, -7.307730276761695e-8] km/s
+ time of flight: 1.8749577787472224e8 seconds
+ arrival date: 2029-04-10T12:30:09.332
+ thrust profile: [0.17280893108792653 -0.04493181336949451 -0.06664900233319004; 0.051617194295619034 0.012725525323833092 -0.06253153116262883; 0.04886773084333811 0.023309232170928784 -0.09876102870177748; 0.03422855580810459 0.022229468242946457 -0.09922980898389573; 0.027174565020590638 0.021057824351685742 -0.10052055193138436; 0.020579910306503184 0.017909007840232503 -0.09244238564836259; 0.020555797875498265 0.019282312338233767 -0.10664195643704318; 0.015356551251712527 0.01611786140937708 -0.0935127041465604; 0.011467980995133839 0.013001114604491932 -0.08048477221892333; 0.006118214873664514 0.006789006141227577 -0.04517367667983735; 0.0013937868795358564 0.001841124691801811 -0.011086227956857654; -0.0005405966295228058 0.0002794167015123816 -0.0007262874295826926; 0.0006989157991000724 -0.0006917199789067492 0.000846738583910972; 0.004866553537631059 0.008815325202278304 -0.012564616313457287; 0.0007378669909474911 -0.000305215349887213 0.001293797132129161; -0.0003944570131711572 0.00043154043680910907 -0.009792906792323896; -0.0009640476562457756 0.00658964237325362 -0.010514150321883266; -0.0018331768912527298 -0.00039540150749234955 -0.006417526303148114; -0.0014881313455601193 0.00038492544426445193 -0.0027260328550700245; 0.00158001332255261 0.0026589080291722984 -0.004102715656487337] %
+
+Mass Used: 82.00990077332699 kg
+Launch C3: 98.81664783473182 km²/s²
+||V∞_in||: 4.056250091081959e-6 km/s
diff --git a/archive/ES_0.564378614189407 b/archive/ES_0.564378614189407
new file mode 100644
index 0000000..c26ab19
--- /dev/null
+++ b/archive/ES_0.564378614189407
@@ -0,0 +1,22 @@
+archive/ES_0.564378614189407---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:24:45.095
+Launch V∞: [6.418943825424663, -7.560404250324768, 0.06594254290205] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4629882575133958e-5, 1.4376316901522787e-5, 1.5645628510882604e-5] km/s
+ V∞_out: [2.1814292716960024e-5, 1.3748305136208609e-5, 3.9097139967543864e-7] km/s
+ time of flight: 1.8282431379653862e8 seconds
+ arrival date: 2029-02-14T14:56:38.095
+ thrust profile: [0.1872023633051809 -0.052366028072574435 -0.06855469613526233; 0.06910397683593683 0.01661335049151026 -0.07905379871603622; 0.05032002010319244 0.024858389080545808 -0.09849406900465736; 0.031093010848384218 0.020388035826074305 -0.08344908604831601; 0.03395949518913379 0.02500516001202437 -0.11698129165729004; 0.012349126689671114 0.010353169901916641 -0.04863231424296717; 0.020371607293677912 0.01715924894885584 -0.08923403845505942; 0.03060610462777169 0.032513460901649666 -0.15814353989545515; 0.018397100436043326 0.022923117189661075 -0.11140392412201654; 0.007716446911793573 0.011020114483459686 -0.06455734198829945; 0.001859993189906034 0.002570276942055658 -0.014564678578565492; -6.617256985423165e-5 -0.0002035152849250247 -0.0028384292772930812; -0.0007355274750324063 0.00016017600283340866 0.0002465860281531784; 0.00040563433904790606 0.000319134754037247 -0.0017238820827456434; -0.00018218243438208325 -0.0004553439714228161 0.0012367555008154527; -0.0009549269510515214 -0.0002261246742254156 -0.0021283832469687824; 0.0013172609925464853 -0.0005706066983961508 -0.0003679869342989206; -0.0004656982164409011 0.00044443903053121035 -0.0015817492599497834; 0.0003413383997074395 0.0003306211794091312 -0.001104554283146669; -0.001316492782852153 -0.0023945473269800636 -0.0007310309244410499] %
+
+Mass Used: 84.63479591367968 kg
+Launch C3: 98.36690068125061 km²/s²
+||V∞_in||: 2.5797241002009507e-5 km/s
diff --git a/archive/ES_0.5643789434280245 b/archive/ES_0.5643789434280245
new file mode 100644
index 0000000..ba62518
--- /dev/null
+++ b/archive/ES_0.5643789434280245
@@ -0,0 +1,22 @@
+archive/ES_0.5643789434280245---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:23:12.814
+Launch V∞: [8.101287262546073, -5.641332138435818, 0.3497152411870013] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5340710436944373e-8, -7.746026723549806e-8, 1.2415643589725916e-8] km/s
+ V∞_out: [-1.9270302706502452e-8, -3.696387237496783e-8, -1.0065583967963905e-9] km/s
+ time of flight: 1.8749577787126127e8 seconds
+ arrival date: 2030-04-23T09:32:49.814
+ thrust profile: [0.2534352724109066 0.0014124562823811663 -0.08010741044520894; 0.07792424331692824 0.04641976493110455 -0.08666897881867601; 0.05630376333967259 0.05407238495905269 -0.11466191619499624; 0.024808523659726477 0.030145749184453462 -0.07525383872746984; 0.01619368683968433 0.023011937754752312 -0.06881666092182928; 0.017453799708264172 0.027026988900678096 -0.08168309546021955; 0.008369189350305239 0.024350487645801784 -0.0861182253734524; 0.009620785938275651 0.015834807773514932 -0.05953991479962458; 0.00791703091244401 0.008046923066412748 -0.048776691921639075; -0.001831359859299378 0.0050636819769914925 -0.023014548757104777; 0.0009659043708493786 0.011484685835926423 -0.0486113956926857; 0.0015205919292504268 0.006112741136556103 -0.032413858634327934; 0.002081838547855307 0.0037839442670183666 -0.012645505297007833; -0.002372085338563888 -0.0030409659217605625 0.004914676463669602; -0.008049585009576272 0.00016871622786087922 0.0022363459893730477; -0.002142109672289068 -0.003572118378088549 0.010966539832295483; -0.002859226075074574 -0.0013210711396157266 -0.0006896978421514054; 0.0052234691632848 0.019295627281371054 0.014865149517772458; -0.001637863503694408 0.00959356236601767 0.014534205455748522; -0.005476955279281672 0.011464408784652031 0.020538314348901934] %
+
+Mass Used: 89.23835858727034 kg
+Launch C3: 97.57778435635856 km²/s²
+||V∞_in||: 7.993483972994537e-8 km/s
diff --git a/archive/ES_0.564389969428874 b/archive/ES_0.564389969428874
new file mode 100644
index 0000000..4ff56a7
--- /dev/null
+++ b/archive/ES_0.564389969428874
@@ -0,0 +1,22 @@
+archive/ES_0.564389969428874---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:06:23.112
+Launch V∞: [6.508564974716482, -7.37248417765429, 0.08586636125527831] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00026858501807699916, 0.0003230795756852108, 0.00027534063509607556] km/s
+ V∞_out: [-0.0003337945839527528, -0.0001502590272068424, 0.000325494111100553] km/s
+ time of flight: 1.8749577787487993e8 seconds
+ arrival date: 2029-04-09T06:16:00.112
+ thrust profile: [0.3117916066838506 -0.07305212920902124 -0.09451832014545598; 0.06083004009720888 0.020018384474188335 -0.06551009445675414; 0.05910337212892969 0.03595598138335229 -0.1047736937390418; 0.0348525428801597 0.02887336413256581 -0.08795786136332832; 0.03861978862274072 0.0382882254083298 -0.12052597504234334; 0.019744584260604586 0.023547221929873918 -0.0797327821947123; 0.014832949957694195 0.019030730590391228 -0.07088318502173398; 0.033439232549783836 0.04907813557352157 -0.17116835555388282; 0.007648671915642433 0.011274691439238163 -0.04663162842622977; 0.0016903409990519811 0.003073219031149716 -0.011836368506985597; 0.004313897318393183 0.008027222091657333 -0.034548837352265556; -0.002058697032878536 0.0008687466581740966 -0.0006214834695471794; 0.004239639730344113 -0.0039018360683539845 -0.003979148672248961; 0.004675213377645737 0.0021874953807613762 0.0008600748418739375; 0.001357308388017322 -0.00011686015818122473 -0.004156519245693329; -0.0003722139147660052 0.0007534144774201672 -0.001269544708731727; 0.0016662969423549175 -0.002175110885096542 0.0008324129150540601; 0.0004346213087411821 -0.0011473412597229108 -0.001713869749275015; 0.0005220458491092786 0.002330600077164723 -0.0032832173951170334; -0.002583899773559768 0.003794419858311561 0.011566432536280433] %
+
+Mass Used: 94.24146593114483 kg
+Launch C3: 96.72231401186426 km²/s²
+||V∞_in||: 0.0005023253820935869 km/s
diff --git a/archive/ES_0.5643999388773007 b/archive/ES_0.5643999388773007
new file mode 100644
index 0000000..09e4672
--- /dev/null
+++ b/archive/ES_0.5643999388773007
@@ -0,0 +1,22 @@
+archive/ES_0.5643999388773007---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T00:10:24.237
+Launch V∞: [8.050641560916652, -5.582536225930336, 0.09549062058273851] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6543380813727797e-9, 7.202680021841308e-9, 3.515965314503975e-9] km/s
+ V∞_out: [4.284802254281796e-9, -4.020592930845045e-9, -3.382008638519899e-9] km/s
+ time of flight: 1.8749577787484032e8 seconds
+ arrival date: 2030-04-22T02:20:01.237
+ thrust profile: [0.36633876272950316 0.007556856414636612 -0.10908177839750523; 0.08882086423886171 0.05483958267149641 -0.09736606264408099; 0.0459964203009345 0.046042439511285845 -0.0926166324647024; 0.03256754124138007 0.043624253935043725 -0.09758079328449151; 0.023042184546971465 0.03739726989951144 -0.0949935731091168; 0.019644753232814494 0.039540630054514005 -0.1060538411345155; 0.013022824074659206 0.029511103856909342 -0.08558779899468617; 0.006453653694089385 0.0160031114121656 -0.050401115205450805; 0.004445435210033899 0.012058592110943398 -0.03948210793576308; 0.011039570657627269 0.01304631133092751 -0.015967879525523847; 0.0036210016322019245 0.0070701044009361 -0.02499600616062048; 0.0002651332697528754 0.0009081892206178302 -0.004984108262783293; -0.004331818521105767 -0.0055807385402362256 -0.001544060096802379; -0.005866051395832797 -0.01299094702794404 -0.0038273924379808185; 0.007895910652783802 0.010178596605159256 0.002593038630655585; -0.0005787159658422804 -0.003135043274486912 0.00595418709826352; 0.00457184267360769 0.0028304319476784396 0.0024546166478061782; 0.014077481845683436 -0.012293772324841388 0.014588417630155521; 0.00919022555583127 -0.015156154301643378 0.015555283322868294; 0.0022784884890546878 0.0029313230617673347 0.01387435734666805] %
+
+Mass Used: 98.5444195205041 kg
+Launch C3: 95.9866587148023 km²/s²
+||V∞_in||: 8.443110933776286e-9 km/s
diff --git a/archive/ES_0.5644098605185898 b/archive/ES_0.5644098605185898
new file mode 100644
index 0000000..1731b37
--- /dev/null
+++ b/archive/ES_0.5644098605185898
@@ -0,0 +1,22 @@
+archive/ES_0.5644098605185898---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T00:45:49.220
+Launch V∞: [6.653615244137381, -7.433392654317281, 0.06379744408661508] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3219526811744962e-10, -1.4932089185201952e-9, -2.57734279934755e-10] km/s
+ V∞_out: [4.674392489160192e-10, -1.0701854070600186e-9, -1.7284900060760059e-9] km/s
+ time of flight: 1.874957778746853e8 seconds
+ arrival date: 2029-04-11T02:55:26.220
+ thrust profile: [0.11813634169862894 -0.03305203457846374 -0.04670680192271652; 0.028024130061776897 0.005765183719564479 -0.034192578482130274; 0.05556821399107677 0.022587614450539823 -0.11070862679699925; 0.051199228887849085 0.027625669527470816 -0.14389017306128138; 0.04188851116618036 0.02662508527762601 -0.15006805612953306; 0.026044554853239265 0.017941990297805053 -0.11328934730612841; 0.016366125514306044 0.012897678951734019 -0.08294962075334418; 0.022295648703379783 0.017424643428460593 -0.1279115202253284; 0.0033963063581336442 0.002125598522717976 -0.019006897882533274; 0.0010742291180610188 0.0013821380426426316 -0.007973496476108554; 0.0005186467842963634 0.002889212807753585 -0.004550387934024677; 0.0007309855833753952 -0.0005391238337202571 -0.0032875439278330304; -0.005911276046026578 -0.00220590965941399 -0.0022084041282695033; 0.005287387478508749 0.004799234597007708 0.002001910076331186; -0.00218944530112711 -0.001691007110345192 0.00030115106836919045; -0.009009664205817572 0.0013984983271758142 -0.000877952868621667; -0.00023323893354724757 -0.001697596482664264 0.0018143226190209132; -0.0018266663672944516 0.0034537866818052467 -0.004033419500654359; -0.0013831663361261344 0.009054636120012427 -0.0028077648843167985; -0.003666856713123701 -0.0026194392010744664 -0.013147265156689802] %
+
+Mass Used: 77.8865489474947 kg
+Launch C3: 99.52999228414744 km²/s²
+||V∞_in||: 1.5210441881531193e-9 km/s
diff --git a/archive/ES_0.5644111842910263 b/archive/ES_0.5644111842910263
new file mode 100644
index 0000000..dd5a505
--- /dev/null
+++ b/archive/ES_0.5644111842910263
@@ -0,0 +1,22 @@
+archive/ES_0.5644111842910263---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:21:49.410
+Launch V∞: [7.597367285785043, -5.796107625980628, -0.028494662395469935] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3423935002844208e-9, -7.182610677625787e-9, 9.313814984566617e-10] km/s
+ V∞_out: [-2.159991921477572e-9, -4.293486404406118e-9, -1.0898060338788217e-10] km/s
+ time of flight: 1.8749577782764176e8 seconds
+ arrival date: 2030-04-24T00:31:26.410
+ thrust profile: [0.829506505453038 -0.016642961938921022 -0.21290844980769583; 0.05106095265598745 0.02763674098407594 -0.06286967761234001; 0.036468407699031945 0.03172146386652874 -0.08052568386486544; 0.029695336331473574 0.03317620544688341 -0.0957723421890755; 0.018991335393186277 0.02515989665047184 -0.0825730388575493; 0.012578908940881215 0.018687284822749294 -0.07193539151496259; 0.02014612291468438 0.03821758022560434 -0.14010711625724; 0.005629482966861049 0.011440658021082021 -0.05122905556509469; 0.00472913073977527 0.009617721661908074 -0.04455863043905271; -0.00026633747198243833 0.001220992960637991 -0.009921706309275318; 1.5540633467681227e-5 0.0009573091273333995 -0.0037402859699269307; 0.0032557239292196286 0.005347938446376638 0.002866129306113235; -0.005654431993374285 -0.007096991001467638 -0.0013699664960450855; 0.00159890055763259 0.0008288835108850169 -0.00020990719875248914; -0.0044790480704472455 0.0059111365072741775 -0.009955289854936213; -0.0019240588320648278 0.0031579949969369426 0.003694921458468287; -0.0010983724136501775 0.003774860861082001 0.008598003744440565; 0.005845975004676094 0.01985348466165827 -0.013768344133319682; 0.012218327011475048 -0.0019974498046649663 -0.019801801369277786; -0.00416397069719252 0.0026941569364201715 -0.026890506398001404] %
+
+Mass Used: 125.80500114789038 kg
+Launch C3: 91.31566523285262 km²/s²
+||V∞_in||: 7.612107129578908e-9 km/s
diff --git a/archive/ES_0.5644150647066617 b/archive/ES_0.5644150647066617
new file mode 100644
index 0000000..be35684
--- /dev/null
+++ b/archive/ES_0.5644150647066617
@@ -0,0 +1,22 @@
+archive/ES_0.5644150647066617---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:38:16.655
+Launch V∞: [7.500898859185387, -6.005168517530791, 0.0898217055519091] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.562864257809844e-5, -0.00027102569657733145, -0.0005079388526712402] km/s
+ V∞_out: [-0.0005352191139095563, -6.789749651404095e-5, 0.00023026025284833974] km/s
+ time of flight: 1.794068272883839e8 seconds
+ arrival date: 2030-01-15T14:52:03.655
+ thrust profile: [0.5558437327398392 -0.006548987466429366 -0.1292310134020001; 0.13972510015635792 0.08522301058996025 -0.11272834940811727; 0.11968138442108024 0.12256032179119597 -0.16801912100149963; 0.06319160010536432 0.08921670928861905 -0.13763578640188007; 0.0357281583284381 0.06705470154549771 -0.11249284220223124; 0.019009300283083005 0.04061835904112013 -0.07813951080546211; 0.014131989556382882 0.03172726639178828 -0.06696134413172396; 0.002561949694641969 0.00952219761970859 -0.01854075183521406; 0.002797620635817721 0.016113116811220945 -0.0380733589145008; 0.0034037967825705294 0.018025541745099082 -0.03706338964404363; -0.0032782256727405977 0.0016700582665738718 -0.002289028161607572; -0.0029946281420322306 0.00403886136991678 -0.005203174627762676; 0.0002972597646334704 0.002529385887531727 -0.009915250943513212; -0.00405340313731877 0.003374541409859795 0.0014320093887662264; -0.0033561259683752725 0.0034096476612250947 0.0019659575633905104; -0.000507478587253258 -0.0056187283909961225 -0.01033825983015443; -0.000491434442319458 0.0015144199386148078 -0.0050001975174652595; -0.008812388396704155 -0.008282755849201667 -0.0027863751198664837; 0.0013296637600881819 0.000513435995052453 -0.01379049043623991; -0.01149409635782336 -0.0030994257686432457 -0.0015817507132973494] %
+
+Mass Used: 119.87157223342274 kg
+Launch C3: 92.33360055845986 km²/s²
+||V∞_in||: 0.0005806690088479059 km/s
diff --git a/archive/ES_0.5644152901617425 b/archive/ES_0.5644152901617425
new file mode 100644
index 0000000..0d6b3b4
--- /dev/null
+++ b/archive/ES_0.5644152901617425
@@ -0,0 +1,22 @@
+archive/ES_0.5644152901617425---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T14:23:27.604
+Launch V∞: [6.448172548937218, -7.4242345383264094, 0.1318043799194211] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.024920054299754153, -0.011016190554208176, 0.026299217863841092] km/s
+ V∞_out: [-0.023191936974389107, -0.00965120503839515, -0.028333397637971828] km/s
+ time of flight: 1.8437413063244766e8 seconds
+ arrival date: 2029-03-03T13:25:37.604
+ thrust profile: [0.2983279150024791 -0.08461109287926542 -0.10604742951586407; 0.0909311170393989 0.026540062463185684 -0.10634582502435129; 0.05305405747449945 0.025926416936319096 -0.10310816956898226; 0.05653288211073051 0.03733079971329946 -0.14300155385768243; 0.03317380288945887 0.02578232915727097 -0.11608674346585274; 0.027912649657182265 0.02335163295332015 -0.11035602162976564; 0.012902125538153276 0.011061268140071728 -0.06477756838018668; 0.008808705299813806 0.008627782656028317 -0.04866223747749356; 0.012605107299374294 0.010826438852098332 -0.06535122068739425; 0.007070961522033776 0.005817440355904211 -0.04241690874400454; -0.0011330511453110964 -0.0008867921646815078 -0.00292705462161961; 0.0012887890637121742 0.0014920667443190324 -0.009160151275949666; 0.003808365851630042 0.0035321414323252224 -0.02323521370627795; -0.0010516333062952985 0.0010690138544889357 -0.0016299732789763631; 0.005822715476745646 0.0002276447650251191 -0.004413100712001165; 0.002455836762875164 0.0004314406837546672 0.001889008938672054; -0.0036431254517742618 -0.0024886212572141934 -0.006570161613998961; -0.0008163134858224173 9.258510161602069e-5 -0.0012252381721221811; 0.002611387578108677 -0.0026809358728716 0.0006128493858117876; 0.006392618211457236 -0.0030967812056829965 -0.002330534571983612] %
+
+Mass Used: 94.31040463154523 kg
+Launch C3: 96.71556009551219 km²/s²
+||V∞_in||: 0.037868382865909385 km/s
diff --git a/archive/ES_0.5644163736201533 b/archive/ES_0.5644163736201533
new file mode 100644
index 0000000..174a0ef
--- /dev/null
+++ b/archive/ES_0.5644163736201533
@@ -0,0 +1,22 @@
+archive/ES_0.5644163736201533---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:43:35.005
+Launch V∞: [7.657312018052324, -6.1439549800222775, 0.7145025446904119] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004179811563982668, -0.0030008948346570584, -0.00019113555856435147] km/s
+ V∞_out: [0.003750834033048823, 0.0018375314115166607, -0.00300505815771397] km/s
+ time of flight: 1.7771873769438544e8 seconds
+ arrival date: 2029-12-31T21:02:32.005
+ thrust profile: [0.41836532213145866 -0.04588219208315166 -0.13946337314903035; 0.0435783328956959 0.014986657493018661 -0.055849149146261344; 0.026662711608731713 0.014629989781541284 -0.0588642387097772; 0.025123468383184303 0.016394373740453702 -0.07671401437480929; 0.053556164696588596 0.041748729091619516 -0.21128552779484594; 0.021259495844135057 0.016304658480158152 -0.09915833336242144; 0.025318783163172428 0.022131680103821175 -0.14091121277439947; 0.01009289208684494 0.008831028153236237 -0.06402523147882438; 0.007870559729294558 0.006511171881218074 -0.05053537213093381; 0.000833416729876727 0.003017154854497392 -0.018040020402736525; 5.285345869266247e-5 0.0013681765345611111 -0.002778568414976451; 0.003203311829647784 0.00016426900603551338 -2.851683623541351e-6; -0.0008638803333762383 -2.808955465923027e-5 0.0030676356798861977; 0.0008467393025047407 -0.0027264856807206472 -5.903475144445952e-5; 0.0012796622587576624 -3.2097452462947454e-5 -0.00031998029703562145; 0.002166405103822633 -0.001179279771851414 -0.0029746790992491853; 0.004161700043888703 -0.0027345931336700356 0.003701117275634669; 0.0010951791002405725 0.0023618093821293267 -0.008710554126395901; 0.0005858729969154332 -0.00037781994552664607 -6.530358688204406e-5; 0.0028067372616439137 0.006772156548118936 -0.013492320184042741] %
+
+Mass Used: 93.27587907932275 kg
+Launch C3: 96.89312402471818 km²/s²
+||V∞_in||: 0.005149051108779399 km/s
diff --git a/archive/ES_0.5644211327058775 b/archive/ES_0.5644211327058775
new file mode 100644
index 0000000..660c301
--- /dev/null
+++ b/archive/ES_0.5644211327058775
@@ -0,0 +1,22 @@
+archive/ES_0.5644211327058775---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T08:13:11.259
+Launch V∞: [6.4490747809303794, -7.35466725547923, -0.04200148324015091] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.598643648920694e-6, -3.502652524735346e-7, 6.874497914960179e-9] km/s
+ V∞_out: [5.174952048178439e-7, -8.855779690739352e-9, -2.5701356660602636e-6] km/s
+ time of flight: 1.8749577786927912e8 seconds
+ arrival date: 2029-04-08T10:22:48.259
+ thrust profile: [0.3452526484657931 -0.08343707406239953 -0.10332434470062601; 0.11511604680274257 0.03737580216647228 -0.10863756923765115; 0.054238790703429185 0.032698590115752366 -0.08715957536273707; 0.06136715623214387 0.04976849605402373 -0.13673948343627365; 0.04423088918222479 0.044813333924494374 -0.13002908536791957; 0.03557842377088783 0.04173370343471128 -0.12816165547104313; 0.013314753819952058 0.017546781997346897 -0.05709354940988801; 0.021773381193510025 0.03112268340852212 -0.10513237230528803; 0.0012762177955053676 0.0007706437831430644 -0.007910805754729053; -0.0031468549979798074 0.004248735069541612 -0.006939110188372746; 0.0008143445918007055 0.0018701016599307297 -0.006640124178522086; 0.00036963405994231563 0.0019218091377439393 -0.005591565349729177; -0.002651985130734511 0.0039919190321956064 -0.019566712997480144; -0.0015088498807656774 -0.0012928195011946944 2.1303031402299458e-5; 0.0031182360132324745 0.001032800208647361 -0.004274873669736359; -0.0030058328080235326 -0.0019873309876228757 0.0001570963567470553; 0.0013584987647749219 -0.0025053036067835153 -0.0021603851310867963; -0.0005012422605653994 0.002981933845881038 -0.01112127416062822; 0.004255444330570811 -0.0022834661367496204 -0.0012069866428933962; 0.0006713633926924618 0.00040496849971127216 -0.007984841453903418] %
+
+Mass Used: 100.33780427842794 kg
+Launch C3: 95.68346009344499 km²/s²
+||V∞_in||: 2.6221521351530675e-6 km/s
diff --git a/archive/ES_0.5644260574521859 b/archive/ES_0.5644260574521859
new file mode 100644
index 0000000..b2b38d2
--- /dev/null
+++ b/archive/ES_0.5644260574521859
@@ -0,0 +1,22 @@
+archive/ES_0.5644260574521859---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T17:00:10.849
+Launch V∞: [6.700530689477556, -7.34781143508696, 0.13150090761391636] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01185006995523372, -0.006135764748557832, 0.01357020511128381] km/s
+ V∞_out: [-0.012339868808045412, -0.0049706468673828465, -0.013610259858732026] km/s
+ time of flight: 1.874957778745167e8 seconds
+ arrival date: 2029-04-09T19:09:47.849
+ thrust profile: [0.1651262565625416 -0.04091354115571009 -0.06302156877166262; 0.051859344122529245 0.013567794175434399 -0.06041645404553477; 0.043452561242529594 0.02211809480701719 -0.08524436188922999; 0.03694060933538578 0.025290475776250418 -0.10170569453155096; 0.025896057768480953 0.02090218831508899 -0.09092247322884922; 0.016461536350404742 0.015142218352319744 -0.07044935044894426; 0.02075508269991308 0.019809649271486148 -0.10035067867605729; 0.0111704056301408 0.011882929884145492 -0.06244182824876692; 0.010948723002389136 0.011740590928207846 -0.06593479963940231; 0.0217578754835481 0.029195596540690053 -0.15206873076302907; 0.0036550920087582003 0.00558948023417543 -0.03194752730478491; 0.00043860270318217667 0.00046547373996072875 0.0011961809935228608; 5.790421037961429e-5 8.328109945063655e-5 -0.0004218801153460844; -4.756053520582767e-5 0.0002716903561323351 -0.0008426232471827416; 0.0027513650091224853 0.0007106854376339832 -0.001246993694473822; 0.0009644421968923198 0.0007730664979328284 -0.00674546590832961; 0.0028947051931709784 -0.0005826033362392833 0.00024105399569658136; -0.002358809958303624 -0.0011129618366617403 -0.0004166767767304256; 0.0014357373285936404 -0.0013968187373871723 -0.0010451214544028072; -0.0004527586476992093 0.0022666966662218974 -0.0030302830149426937] %
+
+Mass Used: 81.55276847380037 kg
+Launch C3: 98.90473689492855 km²/s²
+||V∞_in||: 0.019032136867832027 km/s
diff --git a/archive/ES_0.5644294954968871 b/archive/ES_0.5644294954968871
new file mode 100644
index 0000000..4ec95d6
--- /dev/null
+++ b/archive/ES_0.5644294954968871
@@ -0,0 +1,22 @@
+archive/ES_0.5644294954968871---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:19:23.702
+Launch V∞: [6.459570266180409, -7.41628999929658, 0.206413873648594] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.875868342824446e-5, -7.396390686972296e-6, 1.2768779764923302e-7] km/s
+ V∞_out: [9.699299242567782e-6, -2.209539092029471e-7, -4.834128736436728e-5] km/s
+ time of flight: 1.8580522212146544e8 seconds
+ arrival date: 2029-03-20T07:53:05.702
+ thrust profile: [0.24356491850722545 -0.06632214526253735 -0.08251657544912167; 0.18473669927982647 0.045878075111430425 -0.18512530403140298; 0.03687323257436202 0.018734731604849942 -0.06758489886903037; 0.04989758267871694 0.035051257421929924 -0.12760695381038786; 0.023795784003636758 0.01903814197436725 -0.07643213054219142; 0.028319539603979305 0.027310869163931568 -0.11023803287851262; 0.01284732617876487 0.012553842639348136 -0.05847783636814356; 0.01563496954043671 0.019293064147984096 -0.08544007269111463; 0.007186024693791252 0.0086115014991683 -0.04334797845648949; 0.005885371135754252 0.007662037197317639 -0.040939571742209725; 0.0018124304629781732 0.0041559626445575905 -0.01535346991676883; 0.005064777873985795 0.00722168915860022 -0.03394706727557362; -0.0016988505248150783 -0.0012752136055008186 -0.0011911339965277059; 0.0008808038505585228 -2.832144693784008e-5 0.001823893080938966; -0.0035275809332627004 0.0011694517721433841 -0.00803529499194269; 0.0015383233131374089 0.004082173539225102 -0.004134889018029791; -0.0008516004043488901 0.00010732262389746136 -0.0014141375346979625; -0.0019968374023503275 0.0015822711366642365 -0.0015047676718679837; -0.0020051565355041203 0.0002930186083722338 -0.002617871770661343; 0.0021243840314659466 -0.0025269927917214788 0.0026256611328910324] %
+
+Mass Used: 94.00934103606687 kg
+Launch C3: 96.77001206462312 km²/s²
+||V∞_in||: 4.931665143766109e-5 km/s
diff --git a/archive/ES_0.5644295967551184 b/archive/ES_0.5644295967551184
new file mode 100644
index 0000000..8acb14c
--- /dev/null
+++ b/archive/ES_0.5644295967551184
@@ -0,0 +1,22 @@
+archive/ES_0.5644295967551184---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T16:34:15.924
+Launch V∞: [7.508292215739288, -5.861147137285423, 0.040642868190236284] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.46971817736021e-5, -6.118784139672726e-5, -0.0038791025936709407] km/s
+ V∞_out: [0.003731825627695331, 0.0009565132789294543, -0.0004207258272715349] km/s
+ time of flight: 1.7594519868039203e8 seconds
+ arrival date: 2029-12-03T02:14:13.924
+ thrust profile: [0.7240858702500873 -0.04090850840124288 -0.17744273942670044; 0.2314181449338619 0.12795972387746024 -0.19607539962655354; 0.09334793004875226 0.08655914446196729 -0.14691275667244952; 0.06487810700582226 0.08246637235180526 -0.15664862619344117; 0.04897351133529767 0.07778873318176482 -0.15319724563394507; 0.016485846463420946 0.03249594862767861 -0.07125914975179864; 0.008831091096049314 0.02037883171998687 -0.04805672787123954; 0.0025355778170340795 0.00679173124730816 -0.017714431857804084; 0.002226676371069056 0.006221391131092497 -0.01762304061292812; 0.0011902140736680916 0.004259289169626594 -0.012229395430782818; 0.0008720394825161099 0.003961333722062638 -0.01061653732866722; 0.00010483002807374686 0.0005903441984689457 -0.0021042784445419057; 0.00017345134119380469 -0.0003517782931868458 0.0001573402732954279; 0.00028271866620111066 0.0003279892891183613 0.00017057125941677152; 0.0009959856194630646 -0.0010530877147646226 0.00012179353108797533; -0.000694245231671793 0.0008150733651756498 0.0003946919615212738; -0.0007880284108290809 0.00028182156875730804 0.0014532610502658333; -3.63915743141188e-5 -0.0006308914167238877 0.0012541683106253665; 2.7238345325600606e-5 0.0011193934141286617 -0.00020727892871786387; -0.0020023258958075914 -0.0008023518806069178 -0.00039395315827488235] %
+
+Mass Used: 129.24782352095053 kg
+Launch C3: 90.72914960457501 km²/s²
+||V∞_in||: 0.00388050956663681 km/s
diff --git a/archive/ES_0.5644447340248583 b/archive/ES_0.5644447340248583
new file mode 100644
index 0000000..c3ded1a
--- /dev/null
+++ b/archive/ES_0.5644447340248583
@@ -0,0 +1,22 @@
+archive/ES_0.5644447340248583---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T01:51:25.549
+Launch V∞: [6.79557556307775, -7.242550314830561, 0.23102297261803761] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.3143648773500217e-8, 5.909098377264723e-8, 4.106836235847094e-8] km/s
+ V∞_out: [-2.013983900753207e-8, 4.374529751056636e-8, -6.89460473452192e-8] km/s
+ time of flight: 1.8749577787456504e8 seconds
+ arrival date: 2029-04-07T04:01:02.549
+ thrust profile: [0.14656709523678813 -0.03261497082912318 -0.04800402893991085; 0.10287836115274933 0.03443392700225329 -0.10094877203737193; 0.059986022589170365 0.039251583997254175 -0.10527099469381977; 0.040325084063541274 0.0346201063014657 -0.09995969157620237; 0.03455474432067924 0.03698049153255664 -0.11178450113598518; 0.04958660021828459 0.05706844474407268 -0.17653503336630064; 0.019605504093751874 0.02901313819928519 -0.09447030570506872; 0.009147069613606111 0.01395471902390742 -0.04849252152058465; 0.00507738642876511 0.008971639216805678 -0.03125691691431692; 0.0004907731820341578 0.0026153368034793753 -0.007424713587387464; 0.0028344248976375757 0.00874754649973995 -0.03352101670504512; -0.0005942730763946422 0.0015868183105337346 -0.00276116332850511; 0.0002940272310313755 -0.0017414432706424688 -0.0013053203753837861; -0.0002686429355983382 -0.0010730708426501619 0.0005939090330228582; -0.000917459820002342 0.0003244576460501872 0.00031622899875798755; -0.0003984248804533533 -0.0018892723140393728 0.0025807205644813743; 0.00041708631351106444 0.00015512355848121878 -0.0007136165449621052; 0.0028917418790851165 -0.002937509048041868 -0.0026525596546895557; -8.19647690250753e-6 -0.0004270082389583378 0.0006634404214363132; -0.0017675900044738188 -0.002099383761569161 0.0019498695678028673] %
+
+Mass Used: 82.8402918859988 kg
+Launch C3: 98.687753910229 km²/s²
+||V∞_in||: 8.39030939805981e-8 km/s
diff --git a/archive/ES_0.5644461782300451 b/archive/ES_0.5644461782300451
new file mode 100644
index 0000000..1f04fe3
--- /dev/null
+++ b/archive/ES_0.5644461782300451
@@ -0,0 +1,22 @@
+archive/ES_0.5644461782300451---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:54:55.792
+Launch V∞: [7.79818141753822, -5.508609917479655, -0.002860946734358309] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.738943404807483e-5, -4.921874837913675e-5, -3.6711952623729216e-6] km/s
+ V∞_out: [3.368960844034761e-6, -1.6505887696565857e-5, -5.387259292119604e-5] km/s
+ time of flight: 1.874957778754161e8 seconds
+ arrival date: 2030-04-19T06:04:32.792
+ thrust profile: [0.7515936695483735 0.01638507575843124 -0.1947742343026688; 0.1244620957017011 0.08111602624893975 -0.12489448647811932; 0.07641659662079611 0.08320231287175953 -0.1421240765212403; 0.027517824505043774 0.04143410031511691 -0.0820717556335716; 0.033980806216904025 0.06506916989297601 -0.13664742209790326; 0.012785944105324298 0.0309484537759749 -0.07301858333009606; 0.008508714594911171 0.022233722191924942 -0.05483406056170825; 0.0028948913726647607 0.008720632428375615 -0.024581468291136298; 0.002605082626631726 0.013586378104320678 -0.036439530543039084; 0.000860322292885828 0.007840365105873525 -0.005637308667969302; 0.002904499559402071 0.004647863587784275 -0.003629812393870115; -0.002060982039405549 -0.0014724098860122619 -0.005152393471552682; -0.000141357443762745 -0.0009437313495397013 -0.0028094667902850284; 0.002194793821049885 -0.007712330439774526 0.0038837110080400285; 0.00023218519352843453 -0.0005509657502230438 0.009404282578517715; 0.003461355991112829 -0.005354972475294308 0.0018460046402327657; 0.0011115188214050084 -0.0014811053997701076 -0.00208631262340856; -0.01006672922445273 0.007513232975821303 -0.004813087147535328; -0.0011252670421621827 -0.003768589231482615 0.002868865583735393; -0.008860369936777666 0.009829345146181834 0.012704998064550943] %
+
+Mass Used: 126.77472976699528 kg
+Launch C3: 91.15642482880982 km²/s²
+||V∞_in||: 5.644593842020068e-5 km/s
diff --git a/archive/ES_0.5644553195286078 b/archive/ES_0.5644553195286078
new file mode 100644
index 0000000..dc95239
--- /dev/null
+++ b/archive/ES_0.5644553195286078
@@ -0,0 +1,22 @@
+archive/ES_0.5644553195286078---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T01:24:01.651
+Launch V∞: [6.271225886554584, -7.303079674373265, 0.3024103124954184] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0395501706290544e-7, -4.591783529715273e-8, 6.276573295410806e-8] km/s
+ V∞_out: [-2.162607489764175e-7, 2.0117932495748426e-8, -2.402150057584107e-8] km/s
+ time of flight: 1.8749577787172222e8 seconds
+ arrival date: 2029-04-06T03:33:38.651
+ thrust profile: [0.505298901245586 -0.10372239341330103 -0.129468382593997; 0.23343477257392584 0.09337636924283389 -0.18798713365614103; 0.07587648258073934 0.05539793460512486 -0.10913986960818386; 0.04940160323349981 0.048772763143022896 -0.10186963743546719; 0.055954335504904744 0.06998889937019077 -0.1424800119182049; 0.0152012286024211 0.022138754058356466 -0.05445298981100049; 0.023423550094890524 0.03812858859472493 -0.09668542038295656; 0.005753226789400161 0.010109866514194297 -0.02683158140706054; 0.012439501852854128 0.027088352010969697 -0.06758534119804584; 0.0009142679743626484 0.0008741528266850786 -0.0021901156030220467; 0.00044458064824303486 0.0006954356327341399 -0.001785519450858118; 0.000818493105948697 0.0008410029209136925 -0.0013553464231366664; -0.0004422156297977781 0.0001845525026004151 -0.000985980184973638; 0.0005269257109180462 0.000660399217021509 -0.001265678358142367; -0.000686759813709656 -0.0012052351594982538 -0.001699564387201531; -0.00010298791961600967 0.00047929607373724357 -0.0013528165887496365; -0.0015880644383784075 0.0013875214439131225 -0.0030762795184244096; -0.00013794958702621624 -0.00044954632277956663 0.0014274985117581887; -0.00044326164026881336 0.0005172113355077929 -0.0008079960550977565; 0.001494827306928427 0.0011827470694977514 -0.0019998378573272083] %
+
+Mass Used: 117.46212950606014 kg
+Launch C3: 92.75469884753983 km²/s²
+||V∞_in||: 2.182787983675302e-7 km/s
diff --git a/archive/ES_0.5644589199983351 b/archive/ES_0.5644589199983351
new file mode 100644
index 0000000..099e1aa
--- /dev/null
+++ b/archive/ES_0.5644589199983351
@@ -0,0 +1,22 @@
+archive/ES_0.5644589199983351---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T08:53:46.855
+Launch V∞: [6.350730951992071, -7.5621924134342695, 0.04265221570742416] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.775081326550073e-10, -1.4198194710721935e-9, -6.62596555910231e-9] km/s
+ V∞_out: [2.091626021335974e-9, 3.153602296393443e-9, 1.5983390231321672e-9] km/s
+ time of flight: 1.801944514274705e8 seconds
+ arrival date: 2029-01-13T22:54:37.855
+ thrust profile: [0.26423920100654336 -0.08208766358030946 -0.09728699890939427; 0.032469936426905655 0.006366155243011132 -0.037359339848344456; 0.051646948785860465 0.021973812126537633 -0.09518599567130191; 0.0467417843497149 0.027061444846155466 -0.11847052147449427; 0.05968937477710568 0.041960440047460114 -0.18714293119092215; 0.02165252886657989 0.017168007308371567 -0.08653263076720057; 0.02621858797726596 0.022966638875358443 -0.1208855011623454; 0.009053020274788002 0.008318327928047044 -0.04866852277428258; 0.007629680697263796 0.007346486956517377 -0.04703890265617258; 0.01405208233198265 0.011869335817712883 -0.0817828563284926; 0.004723660806280805 0.005162709562529832 -0.033697418476845785; 0.0011401729327426848 0.0013715414225053532 -0.0074232827629163636; 0.0013853945081977793 0.0010522217749426202 -0.001268091067807621; -0.0006315395148465868 -0.0004924274932960092 -0.0033833332628609627; 0.0006715437505232859 0.0006360873739187621 -0.004270023890023165; 0.0007140059641800053 0.0007330909224902025 -0.004464676182588436; -0.00047653393509429644 -0.0018646513967367087 -0.001041786162204523; 0.00022091196857627286 -0.0006867045004317657 -0.00032833900779307974; 6.13341982092612e-5 -0.00026973006954516426 0.0012154144117434028; -0.0019881015203205635 -0.0026193223880038932 -0.003978547926885743] %
+
+Mass Used: 89.66665788365435 kg
+Launch C3: 97.5203569338977 km²/s²
+||V∞_in||: 6.7868858330655886e-9 km/s
diff --git a/archive/ES_0.5644601658927109 b/archive/ES_0.5644601658927109
new file mode 100644
index 0000000..5c4fbef
--- /dev/null
+++ b/archive/ES_0.5644601658927109
@@ -0,0 +1,22 @@
+archive/ES_0.5644601658927109---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:47:10.870
+Launch V∞: [6.628506446367785, -7.325105697631175, 0.1642231465537721] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9071447882151826e-7, -4.343182105574081e-8, 6.214520209017098e-8] km/s
+ V∞_out: [-2.0343709995516106e-7, 1.748082432073872e-8, -2.3602399975264987e-8] km/s
+ time of flight: 1.874957778749331e8 seconds
+ arrival date: 2029-04-08T21:56:47.870
+ thrust profile: [0.240767959389042 -0.05794933688951957 -0.0807066690181457; 0.054865406496570936 0.015565276782753424 -0.06158218621746654; 0.061727746410130305 0.03314176125178969 -0.11227859642747813; 0.06273746418635144 0.04482303642254307 -0.15465833957740407; 0.043740107781697776 0.037649540597688734 -0.14060269200730588; 0.02489296577092368 0.024763150431528488 -0.10095603006461243; 0.019562469066205512 0.021392777531407167 -0.09274367388821067; 0.010948809950916495 0.012779397841557903 -0.06022203721589321; 0.0043045413175796104 0.005690585891246671 -0.02892035758361912; 0.003669817755601488 0.005369589900204579 -0.0291683741057823; 0.00023118492817611285 0.001142488541523717 -0.008701760261341934; 0.003179887484158836 -0.00014599308125637608 -2.731110498812835e-5; -0.0057276148748980965 0.00404697828656958 0.0017727114780908817; 0.0020199274829064123 -0.0014858674451849745 0.0017808462035427404; -0.008384159253909926 -0.0002812332422437499 -0.0031599305297473805; 0.00024708914113673677 -0.0015203053817724813 -0.0029430089605837137; 0.0018467572328812274 -0.0019312714039218645 -2.6081270376542183e-5; -0.0002297692861089936 0.0017012251139225383 -0.004046136697383093; -0.005614928769798003 0.003733097971592072 -0.0115795715685141; 0.007214335809073726 0.006567789096540589 0.003391618461205987] %
+
+Mass Used: 89.07962434974252 kg
+Launch C3: 97.62124043287201 km²/s²
+||V∞_in||: 2.0523245760651364e-7 km/s
diff --git a/archive/ES_0.5644612593947855 b/archive/ES_0.5644612593947855
new file mode 100644
index 0000000..afb3000
--- /dev/null
+++ b/archive/ES_0.5644612593947855
@@ -0,0 +1,22 @@
+archive/ES_0.5644612593947855---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T05:47:36.275
+Launch V∞: [6.229935445742533, -7.614989738863479, 0.07599406085078782] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2008519258379217e-7, -2.645560432273918e-8, 3.253887397193047e-8] km/s
+ V∞_out: [-1.264569710623723e-7, 1.3106909317339842e-8, -1.6190688910413623e-8] km/s
+ time of flight: 1.874957778743644e8 seconds
+ arrival date: 2029-04-12T07:57:13.275
+ thrust profile: [0.32724900545744184 -0.07916683946325502 -0.10735983842818672; 0.08966738821677767 0.022986188468125678 -0.0969811945757746; 0.06721961189260461 0.032640641459649705 -0.11888120798283583; 0.023450587835830834 0.01620676114166185 -0.061310397195663884; 0.05843116432049799 0.04644495448955664 -0.17321928133859388; 0.011933190742750217 0.011904378487138673 -0.0502129892057227; 0.04342606852646739 0.04276104191151236 -0.17815457397573262; 0.005756863955764813 0.006609155781253128 -0.03263175221933017; 0.008368560043345241 0.009516897215764646 -0.05040250961029371; 0.002265191838895805 0.003088242177688306 -0.018086497770147612; 0.0018231041201376553 0.001653110671339224 -0.011427124356375865; 0.000250283083279237 0.001021692247090255 -0.002968599211217181; -0.0005054262668441013 -0.000775868928636778 0.0005739049026920163; 0.0007348057525632995 -2.180011076943544e-5 -0.0014504431401873115; 0.0005612316245916846 0.0011628242793640254 0.0008654905965468499; 0.0012183491849030062 0.0012831493664094697 0.0008392617760296173; 0.0006475116743188241 0.0002848710545809776 -0.0006177597708655944; -0.001776298254084863 -0.0009837502308195282 0.000861500942068259; 0.0005341048730655965 -0.0018249916394049782 0.0013125281936366636; 0.00041107574886986944 0.0004469334651759801 -0.0004232659831538447] %
+
+Mass Used: 93.83682233658374 kg
+Launch C3: 96.80593947839989 km²/s²
+||V∞_in||: 1.2719721222310244e-7 km/s
diff --git a/archive/ES_0.5644624269752156 b/archive/ES_0.5644624269752156
new file mode 100644
index 0000000..4a2f211
--- /dev/null
+++ b/archive/ES_0.5644624269752156
@@ -0,0 +1,22 @@
+archive/ES_0.5644624269752156---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T10:27:11.104
+Launch V∞: [6.505823253580027, -7.469036742736736, 0.10090425882744096] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.809518039360635e-6, -2.0484170860897496e-6, -3.787326946400182e-6] km/s
+ V∞_out: [-4.946979382523661e-6, -2.8028178834336375e-6, -8.961656815862926e-8] km/s
+ time of flight: 1.8541092079245687e8 seconds
+ arrival date: 2029-03-16T09:29:11.104
+ thrust profile: [0.17627318331649083 -0.04606224275839632 -0.062021609459055334; 0.07386957132425033 0.019457366803080016 -0.07917702844450751; 0.08514321494013527 0.04356372011916436 -0.14674369033134482; 0.037795903743982597 0.02598249460433964 -0.09577876472084776; 0.03778514307136041 0.03160835781848159 -0.12083826556132499; 0.033562991135971915 0.03221015900364381 -0.12984836098620886; 0.0179169429934193 0.019464825732658626 -0.08523403876060151; 0.012645358138544392 0.015091966721385464 -0.0693815922242332; 0.0064629685681406495 0.009720974435821686 -0.04601075452421032; 0.007242671666927193 0.009574517295192025 -0.04716411920596303; 0.004072865502824355 0.0037692285436821795 -0.015721789237956918; -0.0005231455761272202 -0.0010149778208159044 -0.0017361304633353438; -0.00011380797447399087 0.0019472736822291996 -0.0018834522732231866; -7.811712399896501e-5 0.0009207351279791325 0.0007358416657158836; -0.001380286275996237 -0.006041217974953822 0.003627931660531036; 0.00023420827606091552 -0.0043503872837907485 0.0032302249711221647; 0.002995494072521984 0.006491528411362811 0.00019095161173425263; 0.0007447498414039516 -0.0029566973587136025 0.0009529363298854429; -0.00649255190690182 -0.0023826305815117742 -0.00452229671295731; 0.0008058173496071922 -0.003201395182031274 -0.0007625185143413232] %
+
+Mass Used: 86.15866965078112 kg
+Launch C3: 98.12242774062351 km²/s²
+||V∞_in||: 5.7491117270172655e-6 km/s
diff --git a/archive/ES_0.5644728194259196 b/archive/ES_0.5644728194259196
new file mode 100644
index 0000000..f3c76c1
--- /dev/null
+++ b/archive/ES_0.5644728194259196
@@ -0,0 +1,22 @@
+archive/ES_0.5644728194259196---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T23:58:25.365
+Launch V∞: [6.614415171771761, -7.189444461589768, 0.24511646776960655] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.179717547771277e-7, 0.00024810791953779504, -0.00017812454029998833] km/s
+ V∞_out: [-0.00014610192178341624, -0.0002621965995859413, 5.579161975739483e-5] km/s
+ time of flight: 1.874957778748393e8 seconds
+ arrival date: 2029-04-06T02:08:02.365
+ thrust profile: [0.38097825679449193 -0.09165935766607523 -0.11727433317075807; 0.12134302918801097 0.03800710799999787 -0.11526057319395884; 0.08948917552624146 0.053383790514710955 -0.14347272771033376; 0.05930610643455493 0.04803514662396649 -0.13464909779645004; 0.04249606543171947 0.04217080449499776 -0.12491781741234347; 0.0284009335065367 0.03288170766476906 -0.10265255989816333; 0.024169534561692633 0.0313669232826863 -0.10257261559296114; 0.006812945427049036 0.009729421610030256 -0.03401079222974635; 0.002902627041845566 0.0050242852517446875 -0.01733909222131731; 0.0004932201759439188 0.0011429550457798185 -0.0029988745872531167; 0.0006178208059783151 0.001134207686541056 -0.004692593859261626; -0.0004314855466321465 0.0011967969709065097 -0.0002412129424698317; 0.001981884346686049 -0.0007698418129389252 -0.0008602743175560647; 5.789479478510623e-5 0.0027573049637864716 0.00031520829391023337; -0.0004381632406435569 -0.003113351977037998 -0.002736730895334548; -0.0005031056889219938 -0.00014762768951861094 0.0017486550311097565; -0.0014173036562719708 -0.0014994086452359517 -0.0006032461082437299; -0.00034831652592139757 -0.00017773572491716025 0.001379100697588012; -0.002760894200863313 0.002097434015223287 -0.003788672872942929; -0.0024581305655335156 -0.0003149514305324651 0.0017091875406438964] %
+
+Mass Used: 101.47597875078918 kg
+Launch C3: 95.49868181362008 km²/s²
+||V∞_in||: 0.0003054284870018623 km/s
diff --git a/archive/ES_0.564475095168066 b/archive/ES_0.564475095168066
new file mode 100644
index 0000000..b7b7d97
--- /dev/null
+++ b/archive/ES_0.564475095168066
@@ -0,0 +1,22 @@
+archive/ES_0.564475095168066---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T19:38:51.268
+Launch V∞: [6.24227973836538, -7.633905651337561, 0.06495897315943824] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.023816714622712624, -0.010637700807075434, 0.21796628548250283] km/s
+ V∞_out: [-0.14095763581828363, -0.05572248666389857, -0.1587647327525509] km/s
+ time of flight: 1.7665576488029292e8 seconds
+ arrival date: 2028-12-02T10:41:35.268
+ thrust profile: [0.20540991383832738 -0.06817211510456742 -0.07908618807681816; 0.11626291554648534 0.02102453452715225 -0.1264434691254862; 0.09852466192185146 0.0415098242285739 -0.17849170881839485; 0.04956943824751696 0.02896862764252979 -0.12401795511622253; 0.05173904033456244 0.036886543138904576 -0.16322058654238075; 0.039648166135346316 0.0323507173991075 -0.15080757371150932; 0.020016269968542666 0.017901466798862856 -0.08894981008047062; 0.009575888847146108 0.009112317876177119 -0.0486401102393413; 0.0030396539972627696 0.003020884339913322 -0.016949605020377952; 0.002707381686546836 0.0018369608131970812 -0.010745486419216597; 0.0009123668462688965 0.002312417138299782 -0.006675017862319635; 0.0005358138523801105 0.0004882515241559056 -0.004647050547378013; -0.0009566556065265419 0.0020056290240852504 -0.003601321911667273; 0.00017753147389579633 -8.529179494395542e-6 -0.0015417751424056606; -0.00048541377136424534 0.0004944204583664991 -0.000519597700461321; 0.0006781607747620438 0.001327804774370911 -0.0022245384667245087; 0.0021441117208877733 0.001081861566651045 -0.0018243587763471635; -0.002460506386775102 -0.001227596134902499 -6.550317591206135e-5; 0.002877795391996709 -0.006767385496187214 -0.007136156518222762; 0.002583357381601343 0.000408684114358902 -0.0052419451296214] %
+
+Mass Used: 91.28132731601772 kg
+Launch C3: 97.24679149372444 km²/s²
+||V∞_in||: 0.21952152099719177 km/s
diff --git a/archive/ES_0.5644809151286215 b/archive/ES_0.5644809151286215
new file mode 100644
index 0000000..1d1e62a
--- /dev/null
+++ b/archive/ES_0.5644809151286215
@@ -0,0 +1,22 @@
+archive/ES_0.5644809151286215---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T12:21:03.176
+Launch V∞: [6.299185287321208, -7.625857033288085, 0.08895285990217788] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.21363234222519e-7, 3.5983957126998612e-6, -2.378294395190541e-7] km/s
+ V∞_out: [1.3094202542136028e-6, -2.9694505740446435e-6, 1.6579540625160873e-6] km/s
+ time of flight: 1.8001006706011224e8 seconds
+ arrival date: 2029-01-12T23:08:50.176
+ thrust profile: [0.2434258177985111 -0.08616384937628145 -0.09722644318437898; 0.060654490225431276 0.008446457435672811 -0.07525977387170156; 0.029539446471118162 0.011960430372878975 -0.06390239674040887; 0.058569060236968506 0.024978267950743715 -0.1648710414434337; 0.04825574344471235 0.023684907413189425 -0.17114822406638194; 0.029523001682176694 0.020021849140626276 -0.13786986655385028; 0.014998455381762208 0.010125861377154308 -0.07788966404153658; 0.016638051026193354 0.013512684864898294 -0.10723073492570029; 0.002513000503108158 0.0020544350140452106 -0.017163315389107887; 0.005151626138350973 0.0032246771389383092 -0.032993010646029594; 0.0008492032228159243 -0.0007186854640139645 -0.004128889904217984; 0.0011975530416749943 0.0010483077910724207 -0.00970886041732886; 0.0002577070909772532 0.0003785766736291142 -0.004184991086612714; 0.002551435243665239 0.0013648045141903759 -0.00021847160511137163; 0.0008384685258420991 -0.0027525723298122496 7.7991657649293e-6; 0.003373777593697431 -0.0010214428813301265 0.0007872195094249653; 0.003632547082809457 -0.00032297137564488577 -0.0009752016384284619; 0.0004701326850995867 -0.00044608206861686153 -0.0023403023458159846; -0.0028332382407816386 0.0001525335730724726 -0.0005309151708111361; -0.0045865254583703045 -0.0017691926360338447 -0.001562187114471441] %
+
+Mass Used: 87.81989789000272 kg
+Launch C3: 97.84134338743812 km²/s²
+||V∞_in||: 3.6437390369615735e-6 km/s
diff --git a/archive/ES_0.5644829629777285 b/archive/ES_0.5644829629777285
new file mode 100644
index 0000000..2f276b7
--- /dev/null
+++ b/archive/ES_0.5644829629777285
@@ -0,0 +1,22 @@
+archive/ES_0.5644829629777285---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T02:19:17.507
+Launch V∞: [7.37839925784857, -6.439839544187723, -0.04378612967720081] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0012662969926492444, -0.00077516336246283, 0.0003622208982876307] km/s
+ V∞_out: [0.0006702092906340223, 0.0012496018426741782, -0.0008073726365085143] km/s
+ time of flight: 1.688015555695526e8 seconds
+ arrival date: 2029-09-16T19:38:32.507
+ thrust profile: [0.27564861088904186 -0.038435637747590255 -0.10021900784310998; 0.28007285615504796 0.0828899850559192 -0.2667335230782029; 0.08744141158684192 0.049821065701075196 -0.172861236505268; 0.03915666793585772 0.031370511487828365 -0.11801126596517668; 0.026166521021893478 0.02369651869415557 -0.10676614146141022; 0.01792061487800061 0.01588069267150188 -0.08468731456339476; 0.013562088199665815 0.012147637963724665 -0.06418496512022188; 0.004509809841137241 0.007165094190677662 -0.03652284427863748; 0.003952995474002208 0.009311672804831122 -0.04684026890231459; 0.005318270034749479 0.007748538845600088 -0.06275005452407993; 0.0006356575255311125 -0.0009400360404381259 -0.00138613595557202; -0.0015906829655618201 0.0010131090096717377 -0.0031739889961373384; -0.0006285646342080713 0.00020557966478351923 -0.000729268576173385; -0.00036066101024203516 -0.0014621222710731602 -0.0005267462918299012; -0.0016314386005756478 0.0031465977008315917 -0.005324221568275981; -0.0015706419961346975 -0.0010490521002274958 -0.001838657948638375; -0.0010980619833130462 0.0007037956958605538 0.0015238788589020487; -1.4187967758035633e-5 0.009268360168322708 0.000763046385478148; 0.0016060560576159027 -0.0011499729719612467 -0.005455477988821128; -0.0036296597154536698 -0.0004371590090102315 0.0015624047174339242] %
+
+Mass Used: 99.06380404252104 kg
+Launch C3: 95.91422618825638 km²/s²
+||V∞_in||: 0.0015282638159864609 km/s
diff --git a/archive/ES_0.564485389070073 b/archive/ES_0.564485389070073
new file mode 100644
index 0000000..5b8bd6e
--- /dev/null
+++ b/archive/ES_0.564485389070073
@@ -0,0 +1,22 @@
+archive/ES_0.564485389070073---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T20:51:59.048
+Launch V∞: [6.632749699781666, -7.3074313652901814, 0.16899126371327564] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.011643970240161804, -0.006143517288852501, 0.015297459222070165] km/s
+ V∞_out: [-0.01302097539930864, -0.00527558160831708, -0.014491299223329463] km/s
+ time of flight: 1.8749577787493163e8 seconds
+ arrival date: 2029-04-08T23:01:36.048
+ thrust profile: [0.23893080688377336 -0.06638815264101351 -0.08556020189809836; 0.10115881152776572 0.02388894754389007 -0.11046417594607383; 0.04922416781368959 0.022975513852710985 -0.0903830632177997; 0.046470206761021454 0.02890413590664402 -0.1199783861957897; 0.0551827031891547 0.04087534083146825 -0.18278939346063752; 0.03404283851435844 0.028692614956395517 -0.1368959677049837; 0.019982270595845526 0.018611757121039105 -0.09394293997631536; 0.0031696874465870716 0.004422454763975735 -0.01631460816671221; 0.0014089030338465193 0.0036084788474603563 -0.004970016796755857; 0.0012730428297105434 -0.0011517418247736447 -0.011117873359028231; 0.0006731978651940661 0.00043148921736483475 -0.00422758831338323; 0.0029334070367612332 0.0008250878066416569 -0.0010941642398569738; 0.0005769187938387735 0.0010247808343358564 -0.0029554946785803845; -0.0009947565309216975 0.0011207432395030277 -0.003329238543397793; 0.004301310228139252 5.4428317361341553e-5 -0.011136307621013142; -0.008259283131155943 -0.0003798082340024599 -0.007622375140291444; -0.002383554472642028 -0.007846866170060876 -0.018321061551992816; 0.013299386919971002 -0.005312117819762757 -0.008172722007263947; 0.001649368592909528 -0.0007834108434575418 -0.001146114768096367; -0.0022411978130643913 0.0030869591322909805 -0.009064279633382123] %
+
+Mass Used: 90.28015516579899 kg
+Launch C3: 97.42047978559191 km²/s²
+||V∞_in||: 0.020182594141564234 km/s
diff --git a/archive/ES_0.5644884355559058 b/archive/ES_0.5644884355559058
new file mode 100644
index 0000000..2ae4c02
--- /dev/null
+++ b/archive/ES_0.5644884355559058
@@ -0,0 +1,22 @@
+archive/ES_0.5644884355559058---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T19:15:55.744
+Launch V∞: [6.453022105647363, -7.313083890020826, 0.1526829123199879] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2654138144370234e-6, 8.81794138990839e-6, -3.95939922999301e-7] km/s
+ V∞_out: [3.219976069187292e-6, -7.197181352345098e-6, 4.160939049532942e-6] km/s
+ time of flight: 1.874957778751637e8 seconds
+ arrival date: 2029-04-07T21:25:32.744
+ thrust profile: [0.3512620986441006 -0.08771654974511242 -0.11399879293397382; 0.1828048215217773 0.05304031876835837 -0.18184544102628625; 0.07724164478600393 0.04482193381714666 -0.1349752055391526; 0.059926477213029634 0.0464648324753865 -0.14625090559984047; 0.030031780676548617 0.028821782636128057 -0.0972523484397304; 0.02427978399047542 0.02717349774451205 -0.09664586718004997; 0.011884616428121008 0.012045575469356399 -0.047367390958420526; 0.014334784633340203 0.02001872077902082 -0.07000853649145766; 0.006600807006955544 0.006669938196344268 -0.027606146599433664; 0.0005987105504520146 0.0005329070464973383 -0.003862664531235512; 0.0001452449607490466 0.0012535371094677993 -0.003775730848572316; -0.0009757676250004477 -0.00019746988221818113 -0.0037366999786163; -1.5332059045380193e-5 0.00034360772140794717 -0.0013009040252650239; -0.003154256645809442 0.00021133018635176217 0.002588559735833695; 0.0019062537767411225 0.0005123562649341424 0.0005971776242124276; -0.0032738561374179853 -0.001598067765197104 0.0018779101333596766; -0.007999811265163883 -0.0027828619530988596 0.004071841628452607; -0.0007514891522223972 0.00020549428865760104 -0.0016561493062928843; -0.0020112791136875675 0.0017867699496637256 -0.006579863294582964; -0.005420508534950416 -0.0006756365882976164 0.011933120297392151] %
+
+Mass Used: 103.55149443923074 kg
+Launch C3: 95.14600235017016 km²/s²
+||V∞_in||: 8.917069636391332e-6 km/s
diff --git a/archive/ES_0.5644940080408848 b/archive/ES_0.5644940080408848
new file mode 100644
index 0000000..96ffd51
--- /dev/null
+++ b/archive/ES_0.5644940080408848
@@ -0,0 +1,22 @@
+archive/ES_0.5644940080408848---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:43:40.276
+Launch V∞: [6.659605890402569, -7.3061404817627285, 0.158034051495291] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.192597787494758e-7, 2.3930743065949306e-7, 1.0487024225408151e-7] km/s
+ V∞_out: [-9.393558660072443e-8, 1.326257930597747e-7, -2.3709242932736705e-7] km/s
+ time of flight: 1.8749577787493688e8 seconds
+ arrival date: 2029-04-08T21:53:17.276
+ thrust profile: [0.2314648305722427 -0.05861237443773169 -0.08233715445543852; 0.0843964995296192 0.023258872489346202 -0.09353101134396732; 0.04358837666548232 0.022055707727189167 -0.08149844873751608; 0.0458896463120082 0.03227343585509888 -0.12061954145794403; 0.02459487825581906 0.021125934635846052 -0.08633495855413513; 0.03340061902783676 0.033095573502539305 -0.1368231985967916; 0.02303313252378601 0.024756096241005724 -0.11207348049817471; 0.009963174922701077 0.011127973640447573 -0.05739824913835059; 0.008342077238952266 0.008908712441476037 -0.04911325182295924; 0.006651635258252596 0.009607346304290368 -0.04492061666271054; 0.0003712867275191105 0.0013428635291446284 -0.0052094964228876885; 9.385766016199422e-5 0.0008780104926815779 -0.010782295276599397; 0.00039635077234487996 0.0026342152442525996 -0.005189025607295873; 0.00509631178656625 -0.001257005219823205 0.003030141575755557; 0.005664662531365566 -0.0034540106530822215 -0.0019855912526522503; 0.0022737779993238683 0.00239783018186819 -0.0075060499647244235; -4.324664189138145e-5 0.0003886227696425356 -0.0016079609154735185; -0.0028044958437295486 -0.0006153716057607313 0.004844678894094498; 0.006375373480227586 -0.004355335624421825 -0.004018468104667208; 0.0038795344691915077 0.0016586018670870855 -0.0026617668645358182] %
+
+Mass Used: 88.33876037004802 kg
+Launch C3: 97.75501411616872 km²/s²
+||V∞_in||: 2.872084763837094e-7 km/s
diff --git a/archive/ES_0.5644968104044382 b/archive/ES_0.5644968104044382
new file mode 100644
index 0000000..a84924d
--- /dev/null
+++ b/archive/ES_0.5644968104044382
@@ -0,0 +1,22 @@
+archive/ES_0.5644968104044382---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T15:15:17.928
+Launch V∞: [6.435233089598003, -7.329924295308124, 0.11800778373365191] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4130065680657348e-6, 1.0596062582416601e-5, -6.312524194393643e-7] km/s
+ V∞_out: [5.048216840166131e-6, -6.769384800115907e-6, 6.5801318565778605e-6] km/s
+ time of flight: 1.874957778751001e8 seconds
+ arrival date: 2029-04-06T17:24:54.928
+ thrust profile: [0.34262734120166166 -0.06885317905066077 -0.09038315680581122; 0.12507657236333466 0.04984777458700892 -0.10410605052718233; 0.11198734285126098 0.07875174359696892 -0.14912478615810185; 0.06938346589448761 0.06703980880642338 -0.13393689052359806; 0.05280956889006464 0.06325410413318866 -0.133160464742021; 0.013777597669823265 0.019856134385498665 -0.046039179711155974; 0.032710663055005126 0.049781691720704464 -0.11964204163210665; 0.008502417101659974 0.015154583795899533 -0.03926121095476657; 0.007895846191397896 0.016074066675271666 -0.04203609254538083; 0.0048443693151237754 0.011055406287797073 -0.02921875988340755; 0.001509296004146235 0.0018372410740091268 -0.006678020635777662; -0.0011067795329956828 0.0011786248984310091 -0.0020458122134139655; 0.0015971344769444824 -0.000467337324887585 -0.0004450711449568496; 0.0005063689140214889 0.0006723200650651249 -0.000593977113208426; 0.00041752334648111387 0.0007986469544968315 -0.0014013758181333994; -0.002792006337252413 -0.0019478363400462783 -0.0007711301451858757; -0.0004046933093575873 0.00018114410982727447 -0.000423262208705666; -0.0004445877346668096 -5.375016093611581e-5 0.0006825787374158258; 0.0012730205751452237 0.00221412691571038 0.0013938472628090628; -0.00019660753449002048 0.0033887047454117863 0.00013324695047702633] %
+
+Mass Used: 103.51495671685325 kg
+Launch C3: 95.15394092942708 km²/s²
+||V∞_in||: 1.0708483059188829e-5 km/s
diff --git a/archive/ES_0.5645019316766067 b/archive/ES_0.5645019316766067
new file mode 100644
index 0000000..48c7e84
--- /dev/null
+++ b/archive/ES_0.5645019316766067
@@ -0,0 +1,22 @@
+archive/ES_0.5645019316766067---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T02:55:18.777
+Launch V∞: [6.498167176011766, -7.457863361295802, 0.08726412714844638] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.015669907179835, 0.0002448319999104827, -0.01073910107173743] km/s
+ V∞_out: [0.018355674526359507, -0.00017798804136308932, -0.004888066994029792] km/s
+ time of flight: 1.862026572005059e8 seconds
+ arrival date: 2029-03-26T05:52:55.777
+ thrust profile: [0.22153634195671731 -0.06016757600815707 -0.08255350407350982; 0.06223733822193649 0.015060933148618873 -0.0703202036035404; 0.05599778172238743 0.026548330414072254 -0.10614750437090825; 0.06065883596784982 0.03814545353232677 -0.15960773431208425; 0.042266023269033164 0.03187369222866469 -0.14279602830405547; 0.024902900603509397 0.02168636301706661 -0.10300814472819148; 0.01780849263358935 0.017255065784426402 -0.08660675225211713; 0.01684077088378492 0.01769052093500696 -0.09375691244652717; 2.8497397993026063e-5 0.005262405270302349 -0.015002040027166298; 6.181268191799132e-7 -0.0003043306766405062 -0.0011586168426604908; -0.00043808055089772266 -0.000723407484494676 0.00023359236084641774; 0.003666847526542021 -0.004505669354224637 -0.011933974307727583; -0.00045787820332006374 -0.002085606456880054 0.0007898779673831631; -0.003320375301075807 -0.00239146628946904 0.0010428752348869792; 0.0001791767094638571 0.0005030369319928812 -0.019609878001106307; -0.00013349339190091725 0.0034993691418127165 -0.01017608607507046; -0.001204715715868378 -0.002740027087331544 -0.007952651939204866; 0.0005946168218096363 0.00405009912083913 -0.005042773487221512; 0.0028979715710657147 0.005855572436588805 -0.0024083841707262014; 0.0048566565333312915 -0.0007772103022692015 0.0079799943926647] %
+
+Mass Used: 87.77340100829588 kg
+Launch C3: 97.85351759104203 km²/s²
+||V∞_in||: 0.018998269014881768 km/s
diff --git a/archive/ES_0.5645042461885547 b/archive/ES_0.5645042461885547
new file mode 100644
index 0000000..e210f57
--- /dev/null
+++ b/archive/ES_0.5645042461885547
@@ -0,0 +1,22 @@
+archive/ES_0.5645042461885547---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:42:10.209
+Launch V∞: [6.5846524442158145, -7.33860749402445, 0.6027523987355698] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000951400167018692, -0.0063130005107148056, 0.008724833969350166] km/s
+ V∞_out: [-0.003128050487351451, -0.008152424459627687, -0.006372551156312227] km/s
+ time of flight: 1.8749577787267572e8 seconds
+ arrival date: 2029-04-09T04:51:47.209
+ thrust profile: [0.25096793998634587 -0.061519725416546676 -0.08229472718089408; 0.09857768121909917 0.026411253467735853 -0.10404915111702599; 0.035476064388068954 0.018153827031776516 -0.062184760751357725; 0.05679221940752469 0.03962441306661577 -0.14213180090435817; 0.05618474763778611 0.047976228517329 -0.17664510060672647; 0.019659280770839196 0.017882444453972142 -0.07899441965080221; 0.013347023196862711 0.013717182858764559 -0.06823112416088134; 0.009515873911960442 0.012811693316041598 -0.05666756284254939; 0.008811829879357507 0.008914914407466805 -0.04656175004708405; 0.0037194243202471433 0.005380975635882808 -0.02618535738149891; 0.0009966796853510015 0.0018459517293176438 -0.007577487847940923; -0.0003817952108215914 0.0004934237889027767 -0.009622564018630389; 0.0023606788988440293 0.001567149386329801 -0.011326859650591433; 0.0008228192882159123 -0.001029887632321683 -0.001185559767684923; 0.0008360345008558482 -4.512835331302187e-5 0.003960780793246788; 0.0018625857261816473 -0.003618709568676078 -0.0006325866562283341; 0.0007458426911066759 0.001461623363748996 -0.005672492698952914; 2.0738999508143315e-5 0.0012763568471857267 -0.0014790471161245495; -0.0023205931235130497 -0.003149472624644702 -0.008786225043189499; -0.0017818255927059981 -0.004537816843082345 0.011087383015030221] %
+
+Mass Used: 89.39426428951856 kg
+Launch C3: 97.57611821665061 km²/s²
+||V∞_in||: 0.010811191678941557 km/s
diff --git a/archive/ES_0.5645047314044094 b/archive/ES_0.5645047314044094
new file mode 100644
index 0000000..69665cb
--- /dev/null
+++ b/archive/ES_0.5645047314044094
@@ -0,0 +1,22 @@
+archive/ES_0.5645047314044094---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T23:47:36.724
+Launch V∞: [6.51168998972622, -7.191152696923362, 0.2576385675920688] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.4856691498066444e-7, 0.00021602249844587785, -0.00014851512818920572] km/s
+ V∞_out: [-0.00013250900066790077, -0.0002212375586721135, 4.677936270192776e-5] km/s
+ time of flight: 1.874957778756477e8 seconds
+ arrival date: 2029-04-06T01:57:13.724
+ thrust profile: [0.4923451705757029 -0.11565876678541034 -0.1467312851143405; 0.10914788091068628 0.03549127048924521 -0.10359633842335614; 0.09338281565161022 0.057536685058980366 -0.14796693629022387; 0.06293409672525181 0.052711813381790415 -0.1418054524953179; 0.036343295388657666 0.037372767730941954 -0.10818347710762583; 0.028038469271738448 0.03371545304983014 -0.10304524069754356; 0.014041737652174363 0.01915283806652653 -0.0630123214129438; 0.004595250137755807 0.007006622166403199 -0.02394193396478048; 0.006801077235806868 0.011672723303584166 -0.04179264550415298; 0.0029209190946280473 0.0051996666701885005 -0.01946088183618521; 0.002411438647111445 0.004198694820414156 -0.018459747477919848; -0.0018049679262721109 0.0008948911494129726 -0.0017579364265865177; 0.00010174561409966094 0.0006870698297692892 -0.0024978204649461454; -0.0015880509273064295 0.0048332872865168575 -0.003024353647439985; -0.0003579644770255001 -0.0003246605460936585 1.857970036668805e-5; -0.000125326329990165 -0.0007543578657513479 -7.709979355084723e-5; -0.00012674887037521376 -0.00043366426965131403 -0.0016138250918264806; -0.0003538007784483261 -0.004750990878204462 -0.0008326754984528428; -0.0007590609963786664 -0.0007196309533030478 -0.0015611553413927065; 0.0024531638733849685 -0.003003083701492549 0.002091075383092101] %
+
+Mass Used: 109.19874593017948 kg
+Launch C3: 94.1811612642797 km²/s²
+||V∞_in||: 0.0002621499277794097 km/s
diff --git a/archive/ES_0.5645127677553429 b/archive/ES_0.5645127677553429
new file mode 100644
index 0000000..c0f4be7
--- /dev/null
+++ b/archive/ES_0.5645127677553429
@@ -0,0 +1,22 @@
+archive/ES_0.5645127677553429---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T08:16:47.528
+Launch V∞: [6.558588615036072, -7.354664168702798, 0.22087160821372162] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.465990697232099e-7, 3.867368521261881e-8, -4.616170267667957e-8] km/s
+ V∞_out: [1.5271548546197642e-7, -3.9867394447756474e-8, 1.8640515212225384e-8] km/s
+ time of flight: 1.8749577787499896e8 seconds
+ arrival date: 2029-04-09T10:26:24.528
+ thrust profile: [0.306661243542438 -0.07317528970815719 -0.10141215739104606; 0.036544590829450066 0.011337374836891668 -0.039067158746349556; 0.0434576420995899 0.025140305860011612 -0.07758885537292103; 0.045640579389525114 0.03592876043555544 -0.11388704082329733; 0.032004912380188544 0.03015683133350652 -0.10298401258248913; 0.028505785895764964 0.030052946698562524 -0.11093283690211984; 0.012249322573890187 0.014891812056885638 -0.05713738735805056; 0.02378110256019503 0.035376351108433596 -0.13738384243553092; 0.010412152442085867 0.01425588082263672 -0.060619708402636405; 0.008537208260748077 0.013297094143819868 -0.05911794101336215; 0.0030328184627608054 0.006049005468144817 -0.024975825498409425; -0.0010349325162619218 -0.002154220159411721 -0.0027986919397537937; -0.00182460817423833 -7.199801582096974e-5 -0.0031247629537012244; -0.004808351234284738 -0.0012631071527502502 -0.001105532839133087; -0.00022887742728671344 -0.0004288930365600733 0.001669599609382263; -0.0009353530274745005 -0.007139549360900893 -0.00022331216575525797; -0.0023159885127296068 -0.0086210979406578 0.0007044534295165581; -0.0004710618604786696 -9.668442695162161e-5 0.0010002285491987912; 0.0009022049556895795 -0.003546790086727104 -0.002031410007476791; 0.0002472219962053775 -0.0005368545705560909 -0.0039039016666094118] %
+
+Mass Used: 91.86099783042027 kg
+Launch C3: 97.15495392299653 km²/s²
+||V∞_in||: 1.5848610022852306e-7 km/s
diff --git a/archive/ES_0.564523063789044 b/archive/ES_0.564523063789044
new file mode 100644
index 0000000..c23d6fa
--- /dev/null
+++ b/archive/ES_0.564523063789044
@@ -0,0 +1,22 @@
+archive/ES_0.564523063789044---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T17:16:10.642
+Launch V∞: [6.47844679589086, -7.492961661275946, 0.12921771014290642] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.370360112678349e-8, -6.0463725760642225e-9, 1.9151987232789917e-8] km/s
+ V∞_out: [6.058063758767657e-9, -1.4680030555910323e-8, -1.960101553560325e-8] km/s
+ time of flight: 1.8353952694840187e8 seconds
+ arrival date: 2029-02-22T00:28:16.642
+ thrust profile: [0.1825120367756995 -0.04828289551911266 -0.06389326009109213; 0.08951278535587123 0.02330887771189826 -0.09248067500523131; 0.039971027836098016 0.020962808662509033 -0.07066717186989918; 0.03141132522829765 0.022371894573194714 -0.07861058334655976; 0.05061349308561156 0.04358716321704065 -0.15488901381476147; 0.02780974883445391 0.026997694960450215 -0.10540725367352194; 0.03160418504856959 0.035059721024047835 -0.13814209619537252; 0.012024585450051578 0.01458749663267582 -0.06225304972747294; 0.005888601534894278 0.0074776653802920085 -0.036955010486787364; 0.00995175267842954 0.013872125318767522 -0.06390139616459543; 0.0056402899061756715 0.011511282939405372 -0.04591943216971702; 0.0010472328694028376 0.0012712658101842857 -0.006354717191384683; 0.0014724476075920847 0.0009067786159504112 -0.0019460928798214882; 0.0008767658605303342 -0.0003355053274230964 -0.0010372475256452858; 0.0021911141113713614 -0.0030257677836132667 -0.001735730241074074; 0.00010136117367364654 0.0005253158953811638 -0.0024530023300842483; -0.00018175971202773704 -0.00038877118871944035 -0.002167834879673812; 0.003612092152778511 -0.0014308597119046026 0.0012948918966344133; -0.003253183057277828 0.001843334149312641 0.0030339054624595775; -0.0012262915604859363 -0.0016568028993615251 0.0048899823356952955] %
+
+Mass Used: 86.17681448048461 kg
+Launch C3: 98.13144456115431 km²/s²
+||V∞_in||: 2.4313492553220553e-8 km/s
diff --git a/archive/ES_0.5645367950965174 b/archive/ES_0.5645367950965174
new file mode 100644
index 0000000..30d6c2d
--- /dev/null
+++ b/archive/ES_0.5645367950965174
@@ -0,0 +1,22 @@
+archive/ES_0.5645367950965174---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:00:57.951
+Launch V∞: [6.65402302186258, -7.412977521658178, 0.09167198161459131] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.454767940427186e-7, 6.347745245671222e-8, -7.982924740266571e-8] km/s
+ V∞_out: [2.559808185780429e-7, -6.564431409651035e-8, 3.0192137158377556e-8] km/s
+ time of flight: 1.8577166293641046e8 seconds
+ arrival date: 2029-03-20T17:15:19.951
+ thrust profile: [0.08734390642795985 -0.02519584250342512 -0.03585717170172322; 0.1350559533982235 0.0329999212301206 -0.171160870082884; 0.04578658857144391 0.018501878927463307 -0.09251017407246648; 0.0346770627446688 0.018603741181455788 -0.09690109564288277; 0.017937417153778747 0.011957646881647684 -0.067176638649516; 0.01755611674055565 0.012909087506451294 -0.07775669462147715; 0.019597458671699243 0.015139923555424185 -0.09850343643549621; 0.01610431755729365 0.013298524753016839 -0.09227445316923735; 0.013351265235157733 0.011552537674356175 -0.0847159927676349; 0.005930959778245872 0.0053480161181956145 -0.041057987515670406; 0.005774631663177882 0.005749330345737449 -0.04497220768266803; 0.0009014191067432203 0.002239020962629404 -0.008881156970549238; 0.0005668839735777625 -0.0005619702698723184 0.0008250056178549076; 0.0003836836461436478 -0.0005455094897586045 -0.00039974175167187276; -0.0011574302854550718 -0.0017654495136004268 0.0007009263027683761; -0.0013182848231088084 -0.001603550680068792 -0.0016080002608990038; -0.0016904136358630174 -0.001996385137686318 0.0015925580037753982; 0.0007203994827445959 0.003855351077965692 0.002340801528198435; -0.00026430128755219775 0.001447414407037207 0.002074749019251311; -0.002280081323535073 0.0009617735733938331 0.0009705453873418257] %
+
+Mass Used: 79.74573340418829 kg
+Launch C3: 99.23666186429978 km²/s²
+||V∞_in||: 2.6582127854022794e-7 km/s
diff --git a/archive/ES_0.5645393486931725 b/archive/ES_0.5645393486931725
new file mode 100644
index 0000000..5b4aae0
--- /dev/null
+++ b/archive/ES_0.5645393486931725
@@ -0,0 +1,22 @@
+archive/ES_0.5645393486931725---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T03:25:36.969
+Launch V∞: [5.953652705093693, -7.460539485851331, -0.08767554894081118] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.177423299078445e-5, -1.7678181243844684e-6, 3.2510366579333725e-8] km/s
+ V∞_out: [2.338755032900368e-6, -5.3759343939948907e-8, -1.1673784612539829e-5] km/s
+ time of flight: 1.7828912459082043e8 seconds
+ arrival date: 2028-12-18T16:11:00.969
+ thrust profile: [0.6682137063113106 -0.19135756195269013 -0.19540193215131463; 0.16997711655196165 0.04553861134436969 -0.15125196873155497; 0.10866992541164308 0.0598170862186663 -0.16013425750205382; 0.07130310091852748 0.054211815033413005 -0.14691058964747908; 0.058545081779687924 0.055005268572704054 -0.15425756049556788; 0.043183726095875355 0.04752646006475923 -0.13934121697892543; 0.021978567030078913 0.02731066187943068 -0.08426830584496615; 0.0027331601493141263 0.003979739783782924 -0.012354157690443941; 0.0016730068556725743 0.002631240946535884 -0.008856490019249479; 0.0007331883713925482 0.0012755337673433682 -0.0047948067881013095; 0.00025669760942984986 0.0006829360237607846 -0.0020525875176305927; 0.000998253907663748 0.0020674098108608863 -0.007350683379468807; 0.0002414569622256102 0.00043997060213821275 -0.0016381443572967712; 8.063753804735487e-5 0.0001769947244818148 -0.0006641486310019158; 0.0004311046145775016 0.000254296503265685 -0.000521566204004717; 8.54879601176356e-5 0.00014296217028780827 -0.0006088051418117405; -0.0001463865576569075 -1.5318794621794422e-6 -0.0003675343045882937; -5.075999231924336e-5 -0.00038609632494498764 0.0007239062131187426; 6.002965007288698e-5 3.9652399895623606e-5 -9.34957507873833e-5; -0.0007764260890104038 0.00030718014394107607 0.000232899709280243] %
+
+Mass Used: 127.13489123962745 kg
+Launch C3: 91.11331695469836 km²/s²
+||V∞_in||: 1.1906250474692452e-5 km/s
diff --git a/archive/ES_0.5645463228022704 b/archive/ES_0.5645463228022704
new file mode 100644
index 0000000..9cc1cb2
--- /dev/null
+++ b/archive/ES_0.5645463228022704
@@ -0,0 +1,22 @@
+archive/ES_0.5645463228022704---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T11:13:50.829
+Launch V∞: [6.019836410215823, -7.62645822561329, -0.2309868665890301] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7129546619263522e-7, 9.621617218942034e-8, 1.5155364937577318e-7] km/s
+ V∞_out: [-7.432180534360557e-8, 1.125340698241614e-7, -1.9637061992201233e-7] km/s
+ time of flight: 1.806492765875905e8 seconds
+ arrival date: 2029-01-19T07:35:06.829
+ thrust profile: [0.4504428491471518 -0.1269763175059584 -0.13102760828377466; 0.13691756868270236 0.03749404186614058 -0.14587381320928777; 0.08857094072391614 0.05079483644224842 -0.1603808968230119; 0.03074520883127818 0.020863925656447978 -0.07702082057656726; 0.025653909085989027 0.02136525046159973 -0.08189702579780549; 0.044829315401188334 0.04545510664329023 -0.1768061617391734; 0.02123731780295903 0.023881852133654975 -0.10317901662128975; 0.010509870279037645 0.012367876589150041 -0.05705170427446573; 0.007564814847663893 0.009902505636644143 -0.04698687471968946; 0.002126017039422351 0.002868684201312907 -0.013729389406246266; 0.00209065971012748 0.0009244153486148536 -0.006148256968538561; 7.867555995947706e-5 -0.00012994277601582855 -0.00045893128211693733; 5.670112457590386e-5 0.00010632202676406032 -0.0005120965900366854; -0.00019098824997415553 0.0006187728377167673 -0.0014860714234844036; 0.0006399078736318445 0.0009253086277652559 -0.0004908057823211127; 0.0014368893228703626 -0.0008795135846685416 -0.0015699661410601168; -0.0023889920284884633 0.0005672711960132469 -0.0004270761990573381; -0.0023302338674492822 -7.587954424129515e-5 -0.00011319889539127036; -0.0002674023316661403 0.0023330891220925193 0.0014150903912995222; -0.0010721008149973308 0.0009581702438624877 0.004312436383034456] %
+
+Mass Used: 107.65191590494078 kg
+Launch C3: 94.45465040532136 km²/s²
+||V∞_in||: 2.4812939601758437e-7 km/s
diff --git a/archive/ES_0.5645502350622138 b/archive/ES_0.5645502350622138
new file mode 100644
index 0000000..19b8321
--- /dev/null
+++ b/archive/ES_0.5645502350622138
@@ -0,0 +1,22 @@
+archive/ES_0.5645502350622138---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T22:52:50.812
+Launch V∞: [6.341534009313411, -7.686821672134053, -0.3302136020178066] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.85647147595221e-9, -3.764576731525179e-9, 8.866616136941818e-9] km/s
+ V∞_out: [1.7822363366233223e-9, -4.0022735934006385e-9, -7.092044608991683e-9] km/s
+ time of flight: 1.8633768211841884e8 seconds
+ arrival date: 2029-03-30T15:20:52.812
+ thrust profile: [0.16279050026011357 -0.0400657600841723 -0.06371620316209918; 0.035330522200335314 0.00871682133208147 -0.0427693236379627; 0.05958271098518685 0.02737897112052736 -0.11160994464673289; 0.04778899796221185 0.03029833120512179 -0.12658806844410325; 0.04240534645028575 0.030681000330308298 -0.13983088997349005; 0.029855286923581765 0.024304059251326386 -0.12035205531310361; 0.023657493725003573 0.019051303996567456 -0.1098687987140733; 0.01563579049001485 0.017685483641209476 -0.09285699754732205; 0.004875805914117741 0.005157581114610427 -0.03111981667855253; 0.0016878713006506826 0.0026708351940564613 -0.01503869515518427; 0.0015297029702708745 0.002061976728597336 -0.01366815631699026; -0.0001730830306490139 0.00028813341255850514 -0.0029476411488541508; -2.0377973230060396e-5 -0.0001570044845012002 -0.0001052908318003755; 8.55171836505408e-6 0.0004042538649963815 0.00022506048539106785; 7.998499489365925e-5 -0.00027625705644034005 0.00021911064698719267; -0.000915719674401556 -0.0015039989558457618 -0.00033518680357706477; -0.00035354760560683753 0.0014138376464799662 -0.0003275450476800028; 3.6209610945059955e-5 -0.0011395364398202388 -0.0007282126426635505; -0.000292926781105655 -9.001679086325222e-5 -0.0007855422716589885; 0.0006677298541608155 0.0009548503566213183 -0.000973575435075883] %
+
+Mass Used: 78.742562377598 kg
+Launch C3: 99.41132203342596 km²/s²
+||V∞_in||: 1.0787689042800375e-8 km/s
diff --git a/archive/ES_0.5645549481326992 b/archive/ES_0.5645549481326992
new file mode 100644
index 0000000..06c42e6
--- /dev/null
+++ b/archive/ES_0.5645549481326992
@@ -0,0 +1,22 @@
+archive/ES_0.5645549481326992---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T04:45:48.740
+Launch V∞: [6.578265203578189, -7.472256061482407, 0.14420698036338467] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.683600808150247e-7, -9.155970815435941e-5, 6.191574773947082e-5] km/s
+ V∞_out: [5.845597096045598e-5, 9.488401188253015e-5, -1.746885887672695e-5] km/s
+ time of flight: 1.8544992657656077e8 seconds
+ arrival date: 2029-03-17T14:37:54.740
+ thrust profile: [0.1374901680310723 -0.03980281663416279 -0.053619151908270865; 0.029971962055607367 0.005998583113913778 -0.03703161613866508; 0.05233417426768506 0.021755676337286006 -0.1041603672870098; 0.0676789442357805 0.03739494231028905 -0.18477352382033585; 0.05164804388455136 0.033778032557400445 -0.18003063573728295; 0.026877193559036144 0.019731573914957935 -0.1149218196976028; 0.01916391554970053 0.01537346905301817 -0.09622517879577117; 0.00718643377581689 0.0060367907291977866 -0.04276823367599799; 0.006375504435762072 0.0055927393360930815 -0.041996396644215554; 0.0017639875100721235 0.0009834058823226129 -0.0049568083564480985; 0.0015131864657651698 -0.00012219037705607028 -0.011141113477141912; 0.0011669651007696616 0.0021394399373838805 -0.0019002902178185655; -0.001546615128167157 0.0002667846996909484 0.0029478111332418948; -0.0033754346767082893 0.0019731532368891577 -0.0023595247440865398; 0.001121398357664567 -0.0020980550739346723 0.006437373241251713; 0.0018873299077134848 0.0012813381155213903 0.003316104478301211; -0.003871401545173236 7.10155007746687e-5 -0.0032154805474696804; 0.002033859098477406 -0.0043763859769999185 0.0025139413798026377; -0.0007812220148078811 0.016528427420440563 -0.002303355829852524; -0.003996433819687692 0.0030820723385133514 0.005387147132746494] %
+
+Mass Used: 80.39505971225253 kg
+Launch C3: 99.1289793901537 km²/s²
+||V∞_in||: 0.00011052968828591814 km/s
diff --git a/archive/ES_0.5645605651759527 b/archive/ES_0.5645605651759527
new file mode 100644
index 0000000..433276d
--- /dev/null
+++ b/archive/ES_0.5645605651759527
@@ -0,0 +1,22 @@
+archive/ES_0.5645605651759527---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T02:43:14.193
+Launch V∞: [6.069142530492021, -7.575310824248149, 0.22540832727593493] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0015806226902111162, -0.0013786577333586626, -0.0016159302789647573] km/s
+ V∞_out: [0.0017986975777000843, 0.0009433008384809036, -0.001693900080795311] km/s
+ time of flight: 1.7966303446486568e8 seconds
+ arrival date: 2029-01-05T13:07:08.193
+ thrust profile: [0.3722578643442268 -0.10942542614158222 -0.08025405072634707; 0.18876685188050707 0.049835935946539664 -0.14596873278266984; 0.07157594560457432 0.03778432845457953 -0.09719943134373775; 0.10679500122538718 0.07839912135784055 -0.18530040776698417; 0.06540957269625851 0.05675762459250638 -0.14946111129440354; 0.030598474862277764 0.0336089184457429 -0.09449271967222336; 0.02673099597214386 0.03308565995715454 -0.09491029615422641; 0.019549876239655508 0.02611700935184704 -0.07937807940101456; 0.0038970260349028597 0.005920092140538991 -0.01824804408299334; 0.003489529662298445 0.004907359165958092 -0.014952021237916639; -0.0003847044081685524 0.0007292037889458945 -0.004635820801058887; -0.00014275696850871988 0.0009775553014307486 -0.0006031948392032684; -0.0007971573782586954 -0.0007119851339002588 -0.0020490159300972236; -0.0007568058602231569 0.0010593659577264288 0.0006238327941093553; -0.000704556086326598 0.0004186914192083422 -0.001889741331674571; -0.0008427784694398429 -0.0031676142162678994 0.0005047387409763374; 0.0008904872721646343 -0.003427544860697958 -0.0010244430180416945; -0.0008806317533641056 -0.0005131184236188205 -0.0006552797019761915; -0.00139030279358668 0.000945305496576618 0.00047355727820098123; 0.0009273815748416576 -0.00030963831832972336 -0.0001713097627290734] %
+
+Mass Used: 108.74196072709037 kg
+Launch C3: 94.2706340534036 km²/s²
+||V∞_in||: 0.002647696338524301 km/s
diff --git a/archive/ES_0.5645684018397408 b/archive/ES_0.5645684018397408
new file mode 100644
index 0000000..dfce8e6
--- /dev/null
+++ b/archive/ES_0.5645684018397408
@@ -0,0 +1,22 @@
+archive/ES_0.5645684018397408---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T01:04:42.510
+Launch V∞: [6.2383804926364474, -7.2453668505563185, -0.03840222753062577] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.434770791778286e-7, 5.598601280850148e-8, -1.2308208207094228e-9] km/s
+ V∞_out: [-8.088609540151739e-8, 1.956367206514795e-9, 4.413751329782608e-7] km/s
+ time of flight: 1.8599968302761117e8 seconds
+ arrival date: 2029-03-19T19:39:25.510
+ thrust profile: [0.7295942150868836 -0.17359969782491733 -0.2151277303524762; 0.07819303109694557 0.023872730554893504 -0.07740773296082147; 0.08093450269370482 0.04878127744254746 -0.1336932988854955; 0.056184141604355003 0.0459568962130654 -0.1316506336614647; 0.050310739994683315 0.05167170328030154 -0.15194619584094626; 0.028357585376280307 0.034299312033543736 -0.10746618732919899; 0.015245627380749985 0.02013243081228924 -0.06858466449332848; 0.008441062081215358 0.011665250612166334 -0.04296488792950973; 0.00318818984419548 0.005712076802729777 -0.01995239945622059; 0.0007821071696215038 0.0010687153843751893 -0.00533631248352016; 0.00279810629201197 0.004680836398389719 -0.016268696906640033; 0.0012050544602178455 0.00201446862430758 -0.005798893967771375; 0.00012435405468320897 0.0007942727539662292 -0.003228582681184986; -0.00039064559647753404 0.0013269843648098943 -0.0017141861699281164; 0.0006937284661705321 0.0010633722418232502 -0.005347615113742263; 0.0002615612729529829 0.0007808764483764859 -0.003985308506399957; -0.0034468247304756316 0.0029938142486816526 -0.0025801990987249605; 0.002999184687220685 -0.0005615752202622306 -0.003748356143083158; 0.0008469874359631833 0.0014442655896427386 -0.002266452452351927; -0.0011910103697313895 -0.005463692159372346 0.0009342374081996548] %
+
+Mass Used: 125.41359638979202 kg
+Launch C3: 91.41420670112667 km²/s²
+||V∞_in||: 4.4699873412145635e-7 km/s
diff --git a/archive/ES_0.564574051181311 b/archive/ES_0.564574051181311
new file mode 100644
index 0000000..7dd2d89
--- /dev/null
+++ b/archive/ES_0.564574051181311
@@ -0,0 +1,22 @@
+archive/ES_0.564574051181311---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:23:45.862
+Launch V∞: [6.411460891162661, -7.510706493655844, 0.0805200557139783] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.213100234312863e-8, -8.447991442169921e-8, -5.8081903458579484e-8] km/s
+ V∞_out: [2.647363852821877e-8, -5.845380808270177e-8, 8.77071293487223e-8] km/s
+ time of flight: 1.842357631119666e8 seconds
+ arrival date: 2029-03-02T10:59:48.862
+ thrust profile: [0.22533999559523435 -0.05747051129946559 -0.07796812207337893; 0.07217247961821288 0.02064537941073706 -0.07505357399257315; 0.04282040842208645 0.022917535044268137 -0.07541047240083118; 0.07128384611725021 0.051646504533227056 -0.16644569645263355; 0.05762164477759175 0.050158621651479746 -0.171073386363003; 0.024195701487270262 0.025084204340782054 -0.09277943168634348; 0.02678952224601577 0.03005530951262473 -0.12147168716644209; 0.011905037688478464 0.015659836291982154 -0.0616017480282867; 0.005388033060144513 0.00820520306201565 -0.037454163419359976; 0.003331942127920539 0.00288298745505381 -0.014190128321931986; 0.0012694387983766136 0.0014958662808740733 -0.0042122270367264915; 0.00038626516521360745 0.0005398945375262754 -0.0020705239590073673; 0.0003079068092336582 0.0002862526468610893 -0.0027964444655873607; 0.0030150239508527255 -0.0006221565612780804 -0.0013243438011317837; -0.0008972224766374836 -0.0027456768972047574 -0.0060108921160896825; 0.0018526250072814954 -0.0007966606961800102 -0.0048972295101123095; -0.0014364641172974705 -0.005405881236474511 0.005659149598223536; -0.008797385006239713 0.0001682280369891306 0.005366705567868371; -0.00288209929554466 0.003994948756947314 -0.007539453736385228; 0.0021489521822001556 0.008504434178915747 0.0035912938741142785] %
+
+Mass Used: 89.77957312413628 kg
+Launch C3: 97.52402627212454 km²/s²
+||V∞_in||: 1.150130638465416e-7 km/s
diff --git a/archive/ES_0.5645774087687623 b/archive/ES_0.5645774087687623
new file mode 100644
index 0000000..b63cb87
--- /dev/null
+++ b/archive/ES_0.5645774087687623
@@ -0,0 +1,22 @@
+archive/ES_0.5645774087687623---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T15:21:24.776
+Launch V∞: [6.292440528069578, -7.530252058333944, 0.08767220060133563] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003832687658276287, 0.002701885587020795, 0.004091235674511407] km/s
+ V∞_out: [-0.004281505235938212, -0.0022694989870890104, 0.0039033927472083224] km/s
+ time of flight: 1.8051228893913168e8 seconds
+ arrival date: 2029-01-16T21:39:32.776
+ thrust profile: [0.32358358875044346 -0.09656751274522099 -0.11644506614203572; 0.06936575944268399 0.015009769424044807 -0.07383840418582244; 0.06489168590515113 0.03006386800656213 -0.11472189284161996; 0.06889806518181944 0.04311911938023882 -0.16697284493082248; 0.0503965389673553 0.03794353273736804 -0.15514931012767388; 0.025626244498534404 0.022465643920331613 -0.09846208796698996; 0.024943468849096748 0.022448440966524232 -0.10349659172582286; 0.012967679169793127 0.013644705658417978 -0.06624667350984807; 0.006375244798104685 0.007348092101977526 -0.037144355086203854; 0.0016753120603245162 0.0011279938006817083 -0.007448313908247777; 0.003038453627097917 0.005665982697588416 -0.025211666254260204; 0.0025192348278867214 0.002061532692333325 -0.009911937830468436; 0.0015026398283150815 0.0007684604850152906 -0.0022966401643153855; 0.0016855998879915415 0.002084067518929982 0.0014199949552930195; 0.0007026826246787337 0.0009442864773254109 -0.0014479021817497893; 0.00047412319210751573 0.0005775175695789025 -0.0011557604342487874; 0.0028915360620077827 -0.001253265081870102 0.0032530795088263863; 0.0002894263233798266 -0.00854660242358627 -0.001975823934270246; -0.003269043684462531 -0.0005173887757776345 0.0016816642831919198; 0.008293393388707264 -0.0035011373635724903 0.002306720594632876] %
+
+Mass Used: 96.88170028634431 kg
+Launch C3: 96.30719027609344 km²/s²
+||V∞_in||: 0.006223173608027409 km/s
diff --git a/archive/ES_0.5645792144794106 b/archive/ES_0.5645792144794106
new file mode 100644
index 0000000..1fbe504
--- /dev/null
+++ b/archive/ES_0.5645792144794106
@@ -0,0 +1,22 @@
+archive/ES_0.5645792144794106---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T02:57:00.669
+Launch V∞: [6.348472765697439, -7.441250961615659, 0.13869082704812058] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.808389074321892e-8, 7.324576573088811e-8, 4.0165856829555935e-8] km/s
+ V∞_out: [-2.318704518349107e-8, 4.927602706460842e-8, -7.433922277871012e-8] km/s
+ time of flight: 1.8104299602833626e8 seconds
+ arrival date: 2029-01-21T12:40:16.669
+ thrust profile: [0.34548570266593803 -0.0956539597875894 -0.11547895013062859; 0.112505075943994 0.029478237368713498 -0.11301871574208514; 0.06865365339753607 0.0361739051462227 -0.11508602997448347; 0.07509626219773238 0.05492501052523108 -0.17354458666699113; 0.05356543151547791 0.04766118444922024 -0.15883631470547868; 0.02926587062097385 0.029651003079097082 -0.10653575511876984; 0.01691877307537908 0.019070160777507707 -0.07244489426264852; 0.007758519224745762 0.009534294367958303 -0.037728664477470884; 0.009959166906316026 0.013348889244974361 -0.05521442818548992; 0.0021535116585490142 0.002793479301776031 -0.009237956312769824; 0.0012648324953986175 0.0024361050081385394 -0.00974791965774289; 0.0014886684352427644 0.003233476993275632 -0.003498366186840415; 0.0005434163463379149 0.0002837381514214089 -0.0015489916352476902; 0.0004680696228616288 0.0002435027058506396 -0.0007206215072425234; 0.00019878063336128878 -0.002622758454364492 0.0014735490682039835; -0.00013612291352322172 -0.00026494192880459106 0.0003139510948167979; -0.003279868204055647 -0.0017934015347921845 -0.008195030037922019; 0.004742497025719699 -0.0010934813067928159 -0.0024957826556026774; -0.0002447552746932424 0.0031747502811463723 -0.0016531291147864864; 0.001168036090843775 -0.005322593680863441 0.0045621495785856505] %
+
+Mass Used: 100.45749828232283 kg
+Launch C3: 95.69455747605535 km²/s²
+||V∞_in||: 9.180752140482806e-8 km/s
diff --git a/archive/ES_0.564581086562879 b/archive/ES_0.564581086562879
new file mode 100644
index 0000000..b89bd50
--- /dev/null
+++ b/archive/ES_0.564581086562879
@@ -0,0 +1,22 @@
+archive/ES_0.564581086562879---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:24:38.531
+Launch V∞: [6.50214853689265, -7.292286403875224, 0.17583914286883398] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010165178444803435, 0.0010997141289369385, 0.0009482827937416608] km/s
+ V∞_out: [-0.001095735702196492, -0.0005661878341043293, 0.0012723324383038523] km/s
+ time of flight: 1.8749577786380956e8 seconds
+ arrival date: 2029-04-08T17:34:15.531
+ thrust profile: [0.42393239137788813 -0.10689043650174383 -0.14572913627257367; 0.07222596298998595 0.019082043687733547 -0.079501165234287; 0.061209519501138045 0.03167828775543123 -0.11390195299988007; 0.03057619260118884 0.020762626919799052 -0.08072678085965038; 0.022176041640587493 0.01817687165151593 -0.07587712381354636; 0.03230074976437097 0.030769027195423997 -0.13107148886169312; 0.020399021055479433 0.021758335772493642 -0.0987711422129065; 0.02410525396553524 0.029161799855297425 -0.1314866981694406; 0.0018263727234843802 0.005968194464235565 -0.023112772488435903; 0.0012206548238141784 0.001246339182257864 -0.01800699074524658; 0.004574755807567036 -0.0017653225720628152 -0.009242783478980119; 0.00039039455640658114 0.0017317601814143704 -0.006530971923926775; 0.00476226222966072 0.0022497774831859146 -0.006845867721158768; -0.0011836790915846695 -0.0005604206746356768 0.0039795039506924906; 0.0014467009209270486 0.00047602970298006326 -0.002697444812082799; -0.004179959478807284 0.0033246958359822 0.00115209062259479; -0.008784910829574938 -0.0054969325121070525 -0.005740859229782553; -0.000490451069588456 0.0017930144278070653 -0.004425727699785482; 0.001389113901883665 -0.010113191223515231 -0.0028962398830063283; -0.0014549365585675613 0.0020025027271073814 0.0004625985646368324] %
+
+Mass Used: 101.6745410126382 kg
+Launch C3: 95.48629599612353 km²/s²
+||V∞_in||: 0.0017725461772368533 km/s
diff --git a/archive/ES_0.5645851637728729 b/archive/ES_0.5645851637728729
new file mode 100644
index 0000000..d30e740
--- /dev/null
+++ b/archive/ES_0.5645851637728729
@@ -0,0 +1,22 @@
+archive/ES_0.5645851637728729---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T10:17:25.031
+Launch V∞: [6.284788700061887, -7.276044368349196, 0.1637533309948584] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4531094903118574e-6, -0.0006621622051122944, 0.0005525703293142284] km/s
+ V∞_out: [0.0004472805500705066, 0.0007227448839247674, -0.00014602415749502467] km/s
+ time of flight: 1.8749577787283874e8 seconds
+ arrival date: 2029-04-06T12:27:02.031
+ thrust profile: [0.5947554736448137 -0.12885485734682298 -0.14745398055932277; 0.13708315800216997 0.05045121234544656 -0.11834125745662405; 0.06345048950233341 0.04346876715892896 -0.09492746137005846; 0.05628671875454142 0.05340498402285369 -0.11916816599154177; 0.04023337626461364 0.04750647320813171 -0.11136961362830775; 0.04524628085469982 0.06273551027752831 -0.14988380301771442; 0.02867194089978644 0.0465082229872236 -0.11886165319658658; 0.005797665284386469 0.01083052052392617 -0.029776307589200402; 0.00295672458870312 0.006403257243949602 -0.01856134321682116; 0.0012902596317467428 0.00035787540945601457 -0.0027009153211771074; 0.0015367918909671948 -0.0007607726753062923 -0.0028459758723471985; 0.0015961641771003645 -0.0023652998112462533 -0.003423708441313631; -0.0027049193665124936 0.0009506445742176954 -0.0007316940411022863; -5.763552268625189e-5 -0.0014366473447894959 -0.0028857359693459706; -0.001899651985713865 3.553908045743717e-5 -0.0010693351837705123; -0.0014401107002386115 0.0036743854612300564 -0.0020753312008216576; 0.0005521544600045795 -0.004075932548031911 0.005222730786026322; 0.0008478776101039318 0.002697187287861835 0.001358036549201986; 0.0017705511061614533 0.0006064472003733175 -0.005210411931564079; 0.0007557679286862421 -0.0007894881231406332 -0.0006545341942313563] %
+
+Mass Used: 119.29649052154764 kg
+Launch C3: 92.46620580802356 km²/s²
+||V∞_in||: 0.0008624376919312968 km/s
diff --git a/archive/ES_0.5645909166654386 b/archive/ES_0.5645909166654386
new file mode 100644
index 0000000..edcd815
--- /dev/null
+++ b/archive/ES_0.5645909166654386
@@ -0,0 +1,22 @@
+archive/ES_0.5645909166654386---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:01:00.124
+Launch V∞: [7.445282847924464, -6.232654123887064, -0.1448680834325728] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007845794154676186, -0.0023915751150436586, -0.004303705729954879] km/s
+ V∞_out: [-0.004481343629125718, -0.00048232260822210206, 0.0021314558456814875] km/s
+ time of flight: 1.6662717655578697e8 seconds
+ arrival date: 2029-08-18T19:20:36.124
+ thrust profile: [0.43945537281466607 -0.06074218430402709 -0.14717858156992916; 0.18432742193976237 0.0726512706150095 -0.17975790383145268; 0.098015564271553 0.06548268526001072 -0.1696586954206518; 0.07196301040943155 0.06357768826062042 -0.17929073448764626; 0.048701480637457745 0.05136854762235789 -0.16093133059114967; 0.02726999992716318 0.032707755442458256 -0.11443065723872597; 0.012307657765267335 0.017822980356563375 -0.06554700099111958; 0.009332790924932145 0.01452877361755572 -0.05738532359441464; 0.0016237200528303746 0.0027476270567206806 -0.010505179509517298; 0.0005727756244586501 0.0014080475967780334 -0.015568082754999919; 0.0016290925751733926 0.0009767173758297811 -0.006726370455887595; -0.001275466801319297 2.6888475715261106e-5 0.0011994918565197315; 0.0017989321573660016 4.4285188051477195e-6 0.0034446076919252633; -0.0024095163927539895 0.0011434191553737656 -0.0009170684354152534; -0.0013240512834791485 -0.00024591370710628645 0.0021474158173695724; 0.0013749401100052246 0.00020658442463705287 0.004474059183260841; -0.0014074398809215496 0.0013293340927758549 0.005776398874283611; -0.0007174668841612421 -0.0016327107130987074 0.0005847979249860402; -0.005763839087719056 -0.0020189770272465227 0.0023291862800188324; 0.0005842739986341529 -0.0005573444838624436 0.0011225018329444132] %
+
+Mass Used: 108.61073100433305 kg
+Launch C3: 94.29920087520206 km²/s²
+||V∞_in||: 0.004985687455117706 km/s
diff --git a/archive/ES_0.5645960711900239 b/archive/ES_0.5645960711900239
new file mode 100644
index 0000000..b1eb3cc
--- /dev/null
+++ b/archive/ES_0.5645960711900239
@@ -0,0 +1,22 @@
+archive/ES_0.5645960711900239---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T06:31:51.942
+Launch V∞: [7.801832197597587, -6.199560395010751, -0.22020425439676095] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.595442396789598e-6, -0.0001763530829762293, -3.2884900065187483e-6] km/s
+ V∞_out: [-0.00017127792463874828, 2.6318210664799415e-5, -3.56329285791278e-5] km/s
+ time of flight: 1.8749577774246833e8 seconds
+ arrival date: 2030-04-29T08:41:28.942
+ thrust profile: [0.2786082083585344 -0.00031081862724273765 -0.10733853241534667; 0.055808654968349206 0.02719074520920103 -0.074397975163806; 0.033015509665227455 0.024190213138355628 -0.07798542873647887; 0.038679647027340024 0.03586820328555139 -0.1298452442813738; 0.02876038154096872 0.03080776877647543 -0.12797917459822808; 0.020970200428761916 0.023960180982092304 -0.10754341658516793; 0.012526177551798285 0.017597767227536296 -0.08654959731645072; 0.003839750374240852 0.004724700658332276 -0.028955137479577134; 0.0006803099778470525 0.001415625913393701 -0.010313719402219583; 0.00321020274825781 0.0033147926473160497 -0.02388421619059933; 0.0020571707445859477 0.0022847974426242665 -0.008079366776780457; -4.503061691922174e-5 0.00011930530969732551 -8.355377533392715e-6; 0.00026621614419958814 -0.0016529193210794116 3.8976043438323984e-5; 0.0006500442548468883 0.0018800016663974252 -0.0009645098786043079; -0.0027169788083980795 0.00030532246343213307 -0.004333220693122171; 0.0005713819452158528 0.0009774509419541754 -0.006038293296137576; -0.004161031416411864 -0.00028985559421921766 -0.005714554278175276; -0.0005990265318673912 -0.0003059759473543514 -7.328141264266409e-5; -0.000738589708094128 -0.00010135678486825235 -0.0015867202691735318; 0.00022774363183277174 -0.0024553762661721464 0.00044022687091813264] %
+
+Mass Used: 79.1442726287155 kg
+Launch C3: 99.3516246445107 km²/s²
+||V∞_in||: 0.00017654720271628984 km/s
diff --git a/archive/ES_0.5646000682022235 b/archive/ES_0.5646000682022235
new file mode 100644
index 0000000..8c79eed
--- /dev/null
+++ b/archive/ES_0.5646000682022235
@@ -0,0 +1,22 @@
+archive/ES_0.5646000682022235---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T00:41:11.290
+Launch V∞: [6.447127690476297, -7.4694987110506545, 0.13458304223017548] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.553295782854861e-11, -1.2281208710432508e-9, -8.941304650171834e-11] km/s
+ V∞_out: [8.397124781699448e-11, -1.944668684298352e-10, -2.659782910435212e-10] km/s
+ time of flight: 1.874957778746357e8 seconds
+ arrival date: 2029-04-11T02:50:48.290
+ thrust profile: [0.2665076542134075 -0.07246861013946887 -0.09497225231142796; 0.10516653666530873 0.02727511724101714 -0.11919823891529777; 0.031035622126946067 0.01540145553135721 -0.06368407380462293; 0.030760827775685888 0.021719907020203252 -0.0908039641328847; 0.028420721265555976 0.0246573684590017 -0.10775562954754336; 0.02815048465536341 0.026037381755544733 -0.123406748963119; 0.026019034444360243 0.0237660869652305 -0.12600256179750285; 0.009556302260827862 0.009450800379324366 -0.05466680995579075; 0.007153132469063968 0.00868508692158401 -0.04532093855413158; 0.004989628398206016 0.0056256814456151025 -0.03802106762076895; 0.0035179812030798224 0.004541807397305249 -0.02922991677108976; 0.0015222343007601107 0.0016760898611805379 -0.011039317308254198; 0.0004125611969672267 0.0010955267110796178 -0.005867137801861825; -0.000679722429112131 -0.004735928705024571 0.001151568145021777; 0.00010376772960869445 -0.0002937947677905999 0.0022219062119336304; 0.0007228164563898944 -0.001066199675720877 0.002045325318161719; -0.0004957253883766852 -0.00019722475235490382 0.005588021773506931; -0.004536556262268815 -0.00010311562356641541 0.0005560079298685632; 0.0024423392599782056 0.0032756706315129882 0.00394278261399958; 0.0005786075626377866 -0.000513183368893061 -0.0016761679041533881] %
+
+Mass Used: 90.66770179538844 kg
+Launch C3: 97.37697904694954 km²/s²
+||V∞_in||: 1.235071703508838e-9 km/s
diff --git a/archive/ES_0.5646022159645948 b/archive/ES_0.5646022159645948
new file mode 100644
index 0000000..464398c
--- /dev/null
+++ b/archive/ES_0.5646022159645948
@@ -0,0 +1,22 @@
+archive/ES_0.5646022159645948---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T10:53:55.037
+Launch V∞: [7.69953801034952, -5.813363119929581, 0.10499216765016835] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00019057590572053477, -0.0005349291918253694, -0.0011581643986563507] km/s
+ V∞_out: [-0.0011830393115777012, -0.0001418963457337384, 0.0004973129175707316] km/s
+ time of flight: 1.7741389584691858e8 seconds
+ arrival date: 2029-12-22T20:32:10.037
+ thrust profile: [0.6434243920382646 -0.04585529837511872 -0.1980749133710302; 0.0669798797115842 0.033349123908773065 -0.0738766349812654; 0.05849189127064459 0.048912180904624805 -0.11282107646345019; 0.054349629129060884 0.0604175117505071 -0.1511406313639282; 0.035560501424007976 0.04832253400334343 -0.13355662995833853; 0.024111776868206522 0.03837133670024722 -0.1155325248308982; 0.009399395629862483 0.017041262503705468 -0.055897387810682674; 0.006222522756982556 0.012360763341486935 -0.043082623309433514; 0.002932529800576267 0.006207441775138671 -0.02603986517650717; 0.001237565268459642 0.0026189137254321385 -0.010550254200179805; 0.005645114218451494 0.013248352146055164 -0.053448653873785924; 0.00191209381526697 0.000640343308709764 -0.004025068808319426; 0.0055601916544883185 0.0023610143376945505 5.001506620435931e-5; 0.008625075458665431 0.006348388592069811 0.00046024052591777005; 0.005025337141924376 -0.012349562522478623 -0.003101553770145782; 0.0004403829653228592 0.003648032981259088 0.0031757404468168056; 1.654905008032867e-5 -0.0005921743042658316 0.0044507984213415855; -0.005771290442583298 0.012362250249819691 0.002419474214358295; -0.006641843731222041 -0.0066115171903992215 -0.0016429467162114703; 0.0023683417324159004 -0.007963142042189699 0.011244321272721583] %
+
+Mass Used: 115.6828370872804 kg
+Launch C3: 93.08909969224231 km²/s²
+||V∞_in||: 0.0012898888287070213 km/s
diff --git a/archive/ES_0.5646098703502913 b/archive/ES_0.5646098703502913
new file mode 100644
index 0000000..7823afa
--- /dev/null
+++ b/archive/ES_0.5646098703502913
@@ -0,0 +1,22 @@
+archive/ES_0.5646098703502913---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T19:17:57.349
+Launch V∞: [7.912541083103784, -5.796647326259173, 0.1410918686728438] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.721355916045519e-6, 6.497896826529542e-5, -0.0012636619857607115] km/s
+ V∞_out: [-5.519919044422864e-5, 0.0012640810556078495, -1.3395269064003923e-5] km/s
+ time of flight: 1.8373188549302933e8 seconds
+ arrival date: 2030-03-10T07:56:02.349
+ thrust profile: [0.3746449294217034 -0.019599580289648255 -0.12396701949543792; 0.057463767125285954 0.02924737112139813 -0.06849567296728415; 0.06483430029049274 0.05135068425350601 -0.1326795747368455; 0.017029058975479242 0.01633610224762586 -0.05276194764803424; 0.02805344072043728 0.03916796955149817 -0.11844472347171989; 0.012952248060755425 0.025146832014311005 -0.09147915977921751; 0.01381767141752601 0.017094808983375162 -0.07304321183229483; 0.01379342046493527 0.024839178210598993 -0.09946534650858033; 0.004738590752602608 0.009431299753774469 -0.04396400714997449; -0.0011019389440238814 0.0006754049656571008 -0.01613951098181334; -0.0017762860573171547 0.01006707610535053 -0.025928510756212657; -0.002584281918539376 0.001856286647340697 -0.0032678088014273347; -0.0037196726637707435 -0.0004655776510460539 0.0068451034886481705; -0.0011322569313351096 -0.00041135041519780756 0.002790877731589676; -0.0011855124907267298 0.0034823617645468293 -0.011004437269803404; -0.010308917224016435 0.013138872300396204 -0.0022432667926445956; 0.021428317297449175 -0.0020618958986559637 -0.01737670748062329; 0.003545552607711714 -0.01218852023171232 0.010233207755797676; 0.007745041046352007 0.015480068108702135 -0.02659731375375524; -0.009935869967000726 -0.00025204903818452007 0.01184012359016998] %
+
+Mass Used: 97.37373647061577 kg
+Launch C3: 96.22933353223841 km²/s²
+||V∞_in||: 0.0012653615857226507 km/s
diff --git a/archive/ES_0.564616864537854 b/archive/ES_0.564616864537854
new file mode 100644
index 0000000..8dddeee
--- /dev/null
+++ b/archive/ES_0.564616864537854
@@ -0,0 +1,22 @@
+archive/ES_0.564616864537854---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T05:52:57.006
+Launch V∞: [7.844160776463345, -5.75903303310965, 0.1447459112174354] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003173672580468977, 0.002052709932958694, 0.000135533632893882] km/s
+ V∞_out: [-0.002734899818801752, -0.0013113736433467446, 0.002265130236276142] km/s
+ time of flight: 1.81226098251239e8 seconds
+ arrival date: 2030-02-06T18:27:55.006
+ thrust profile: [0.4938063807246066 -0.02406345450440812 -0.1356724532478948; 0.058840383642930656 0.03344481835074325 -0.06603447221410709; 0.05873172083143201 0.054936751258174384 -0.11609096192381418; 0.04537451373568675 0.05566210809593241 -0.1305004419333469; 0.026752018914926637 0.04141386203114067 -0.11449136386618135; 0.02174985029477291 0.0341538739438068 -0.1048400665814302; 0.012677617459514727 0.02288066356024928 -0.07805108694556062; 0.009832706310768083 0.02665439069570893 -0.08586248403334744; 0.0012591558670443717 0.005266625461229069 -0.02072553110203884; 0.002735195363023335 0.011923670102733177 -0.042632615393584185; -0.002219017324489689 -0.005148365782042266 -0.004231252341207124; -0.00040251198452216164 -0.004494042103840719 -0.00046612277594578703; -0.00010048647346090736 -0.00022047472081886729 0.0031074156896714836; 0.00324820007304821 0.003813280338680172 0.004751126647234675; 0.0015704473324641127 0.0009999219426868882 0.002928120474331429; -0.007074092364580663 -0.011874133489487921 0.007717819413084495; -0.002488790908688655 -0.0022112123872473073 0.00901794228146628; -0.020421336114170238 -0.003516625346029074 0.008087916154398168; -0.010897414008977766 -0.014024238969464638 0.013375817315974628; 0.001221654539080745 0.0008488137871399713 -0.003356699977570332] %
+
+Mass Used: 106.19642696426445 kg
+Launch C3: 94.71827114226832 km²/s²
+||V∞_in||: 0.0037820873975271 km/s
diff --git a/archive/ES_0.5646175052506845 b/archive/ES_0.5646175052506845
new file mode 100644
index 0000000..38cc607
--- /dev/null
+++ b/archive/ES_0.5646175052506845
@@ -0,0 +1,22 @@
+archive/ES_0.5646175052506845---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T15:03:03.025
+Launch V∞: [6.301198679876696, -7.342086448939956, 0.11384923752081698] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005516317454821604, 0.0009297803989373499, 0.0008819383934816625] km/s
+ V∞_out: [-0.0009315701002203048, -0.0004717630272355377, 0.0009252589011155191] km/s
+ time of flight: 1.8749577787495518e8 seconds
+ arrival date: 2029-04-07T17:12:40.025
+ thrust profile: [0.46143089217923866 -0.10204016782763325 -0.12653906102735157; 0.21786012030997773 0.06749088751405502 -0.185469264668067; 0.048666942869434064 0.030511307515052658 -0.07802217593523998; 0.03196411486506615 0.026679112938287057 -0.07272995214079729; 0.04981389712752774 0.05130245683952787 -0.13512961599970158; 0.027652739513803003 0.03225033634104266 -0.09628117563588881; 0.013292703217405184 0.01829530222091593 -0.05906142229685188; 0.02501475761828826 0.03900173201033985 -0.12076373808031589; 0.0073634022870704635 0.015922557044495717 -0.03922005251194739; 0.0015715218112559032 0.0011922936800637138 -0.012528816976800495; 0.00016440741134471788 0.0001464872999386276 -0.0014014642862477547; 0.0004545203911086841 0.0006115647862330971 -0.0003371780747172277; -0.0016494729406028924 0.0024546358825383256 -0.0007415826122126492; 0.00042543598765787036 -0.0007943389380365699 -0.004482414542729533; -0.0012092241765696982 0.004762172594455492 0.000529174494259765; -1.0516169005216416e-5 -0.00030809448388812794 0.0006556962572174159; -0.000967364205400525 0.00010458821481597672 -0.00291544961548581; 0.0036894596700661436 -0.004464960414330275 8.631039594076567e-5; -0.002613032891602058 -0.000226590719227642 0.0036236963246579447; -0.00527483157476475 0.002767045712573163 -0.00645332050651001] %
+
+Mass Used: 112.5786735165475 kg
+Launch C3: 93.62429987587163 km²/s²
+||V∞_in||: 0.0013952076916247302 km/s
diff --git a/archive/ES_0.5646226765603133 b/archive/ES_0.5646226765603133
new file mode 100644
index 0000000..a19ace1
--- /dev/null
+++ b/archive/ES_0.5646226765603133
@@ -0,0 +1,22 @@
+archive/ES_0.5646226765603133---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T21:22:03.195
+Launch V∞: [6.565532832512303, -7.170939688070493, 0.4502254549983168] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0861760906421652e-5, -1.5837719731787448e-6, 2.828717196635303e-8] km/s
+ V∞_out: [2.1910752210616745e-6, -4.783312902810591e-8, -1.0751520888827393e-5] km/s
+ time of flight: 1.8749577787482333e8 seconds
+ arrival date: 2029-04-05T23:31:40.195
+ thrust profile: [0.4797497517182076 -0.10952282386522945 -0.1348341580088057; 0.09054599092538265 0.029526079443923926 -0.08760571005744962; 0.08539830123703894 0.05233275986667736 -0.13666698782308326; 0.06065954644829325 0.05001872700951856 -0.13614681839320628; 0.04007657465220103 0.04110203215708906 -0.11962858923336096; 0.03298779946235583 0.03940797080702191 -0.12077965253567041; 0.014546864325969083 0.021284028826415217 -0.06746860448605821; 0.0053603551240410325 0.00803217589969372 -0.028480416543900676; 0.005181638322206027 0.008224127676465808 -0.03094992624566324; 0.0004337436113883216 -7.424054715918075e-5 -0.0016280197828319745; 0.00335089772912206 0.006283732770313687 -0.02497265000902306; 0.0011601494358824019 0.0010847596380006716 -0.00651626160860937; 0.0006075614194767475 3.18350044177598e-5 -0.0038382279581469295; -0.0003682047356285375 0.0006810134991914877 -0.0001424309114962264; -2.8371948042468304e-5 0.0004748689528031557 0.00027469987043630137; -0.001542914671711516 0.0010526077216939848 0.0025914463656819585; -0.002140147030710751 -0.004314771443996104 -0.003832879962998897; -6.359508447273187e-5 0.0009307154519481119 -0.0017520521080436715; 3.0844572952086577e-6 0.0007620705842351918 0.00012120123190949381; -0.0027841565318592054 -0.0038395227767017387 0.0008735198229683446] %
+
+Mass Used: 106.12720397412386 kg
+Launch C3: 94.73130034507 km²/s²
+||V∞_in||: 1.097665631307613e-5 km/s
diff --git a/archive/ES_0.5646228136905828 b/archive/ES_0.5646228136905828
new file mode 100644
index 0000000..d03daa5
--- /dev/null
+++ b/archive/ES_0.5646228136905828
@@ -0,0 +1,22 @@
+archive/ES_0.5646228136905828---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T00:20:31.469
+Launch V∞: [6.521634621218826, -7.527987812795048, 0.07799636122034131] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.843639185209711e-8, 7.606220213007901e-8, 4.001098513824095e-8] km/s
+ V∞_out: [-2.4007295543070756e-8, 5.2303533896849936e-8, -7.48560991170364e-8] km/s
+ time of flight: 1.842026121085267e8 seconds
+ arrival date: 2029-03-02T23:44:03.469
+ thrust profile: [0.1435780945313529 -0.03723262431093516 -0.0542239578352134; 0.03287456279664443 0.008271393528773544 -0.03730009793120645; 0.04095460389786282 0.02022777726534726 -0.0770571891615283; 0.03494099780730389 0.02334040977866276 -0.09129540613214464; 0.026094747375234536 0.020985634130186403 -0.0873198649937364; 0.018527587446931462 0.016968217640304033 -0.07547040455368999; 0.020969395566715416 0.0212279042932919 -0.09800735735365763; 0.03654561509222373 0.03940904849476255 -0.1739131167044003; 0.0070522491054029295 0.008180241903792258 -0.0427906397130933; 0.02021903879341502 0.025827215199655 -0.12758091334637303; 0.0032147037734597057 0.00399923120767352 -0.02291892073822816; 0.0020366818399058734 0.0027270412419963864 -0.01600746882865807; 0.0007868949646658715 0.002008568533101129 -0.007337633322134959; 0.0003862237830863545 0.00012143796323004725 -0.001031599156106153; 0.00011213024068567679 0.0009472689817115578 -0.0026245028975273184; 4.684409618116187e-5 0.0002608244005921015 -0.00220437764904225; 0.0002254548682863881 0.0013410196990866954 -0.000837131569730015; -0.0009896671450205963 0.0004255926693690905 -0.0004288866895730567; -0.00047264286964065344 0.00036468332909889113 -0.0010795860685076377; 0.0010022124602061646 -0.00015874112277749293 -0.0009935340893023675] %
+
+Mass Used: 80.01093720364588 kg
+Launch C3: 99.2084020746344 km²/s²
+||V∞_in||: 9.414719190298504e-8 km/s
diff --git a/archive/ES_0.5646232751278945 b/archive/ES_0.5646232751278945
new file mode 100644
index 0000000..22fa524
--- /dev/null
+++ b/archive/ES_0.5646232751278945
@@ -0,0 +1,22 @@
+archive/ES_0.5646232751278945---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T20:50:52.200
+Launch V∞: [6.583174984324081, -7.478130592380632, -0.01578225261440106] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011352433909040767, -0.00037635244518137667, 0.00800107545904041] km/s
+ V∞_out: [-0.013303731408497775, 0.00012927347895014152, 0.0039985023321215665] km/s
+ time of flight: 1.846742243908187e8 seconds
+ arrival date: 2029-03-08T07:14:36.200
+ thrust profile: [0.11455406241726714 -0.03384384025763535 -0.04646608027142819; 0.04864999140152002 0.009829352318789493 -0.059017246603720604; 0.0534068467288367 0.022252185212588847 -0.10812143494885341; 0.057250028736728874 0.031827073465860486 -0.16059644494414577; 0.04320400714593683 0.028546644771367966 -0.15486241348491156; 0.031377294565785176 0.02337574525716995 -0.1363860907792148; 0.01919580604208915 0.01566522506720908 -0.09799703859917812; 0.0067265922887151 0.006025235582943536 -0.04000424505435384; 0.008645142059730984 0.007742369672098108 -0.05385002883511744; 0.0009570530725296663 0.0009074940253674075 -0.0056574593460012; 0.003680510869606135 0.001548738021985275 -0.0096076362196054; 0.0026080153022862234 -0.00017234051098387337 -0.0012012460734983038; 0.004389265714823559 0.0037360989133344603 -0.0034032702168322365; 0.00981855080828012 -0.0017999862396951877 -0.007077812567782638; 0.0003577448905353175 0.0004458401842136672 -0.0028032721648037482; 0.003994009334246663 -0.0012220654397310116 -0.00738464512633454; 0.001792122806617964 0.0007420982140560826 0.005839390879171713; 0.009249539786461543 -0.005306784865789572 0.006250545629975439; 0.010576482889320166 -0.0003244937478426521 -0.0009520689749592903; -0.0007610997624019256 -0.001053703468535743 -0.0010826076108022367] %
+
+Mass Used: 79.70535950505246 kg
+Launch C3: 99.26087911042704 km²/s²
+||V∞_in||: 0.013893761381403934 km/s
diff --git a/archive/ES_0.5646343884946567 b/archive/ES_0.5646343884946567
new file mode 100644
index 0000000..efdc4d3
--- /dev/null
+++ b/archive/ES_0.5646343884946567
@@ -0,0 +1,22 @@
+archive/ES_0.5646343884946567---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T01:36:29.276
+Launch V∞: [6.412183962339828, -7.608341344048776, 0.08386004177708878] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1472214594757233e-6, 1.5587919029014777e-5, -9.298840666694862e-7] km/s
+ V∞_out: [5.616044269293003e-6, -1.2768677656633641e-5, 7.341690297686912e-6] km/s
+ time of flight: 1.7841370850357336e8 seconds
+ arrival date: 2028-12-24T00:58:17.276
+ thrust profile: [0.11980046397507982 -0.04201811937155043 -0.04672263238783339; 0.042851317033505094 0.005816127452034621 -0.048386352688330754; 0.06460258862227773 0.022231707769700227 -0.1210182764469326; 0.07097900041770905 0.03347327722807382 -0.18433051419299862; 0.06322597777037285 0.03554840840414394 -0.2077689908277521; 0.03904684910439738 0.024527529038241007 -0.1535237871614666; 0.020579282282197908 0.013831772503556189 -0.09356740172947545; 0.004898111023555542 0.003292577484744932 -0.026859640454515256; 0.0036451000218909965 0.0010446600886583556 -0.017553876831173064; 0.0036772289452182607 0.003480445455412475 -0.012078645915349826; -0.004819929312914196 0.0001927871858208594 -0.009387629934719817; -0.00014336943095438455 0.000884419843346875 -0.006625033678724488; 0.000606611702174068 -0.001061416285883886 -0.011255727957209704; 0.0049525140056918245 -0.0005888637437897263 -0.008640455816755903; -0.0031896000727536233 0.0047972379741094235 0.0008963455551040662; -2.052118941307888e-5 0.001191291777137637 0.00039151098084886857; 0.00013378733671115788 0.001699195740110078 -0.007356800221470669; 0.0010476508417964691 0.0007289414985283387 -0.0005206479112422049; -0.004023647170152694 -0.0006055667682776764 0.0037651005888428273; 0.0027856863651712924 0.006727863006373529 0.0014137528812533473] %
+
+Mass Used: 81.181823437601 kg
+Launch C3: 99.0099936810569 km²/s²
+||V∞_in||: 1.5762565274364446e-5 km/s
diff --git a/archive/ES_0.5646390342268269 b/archive/ES_0.5646390342268269
new file mode 100644
index 0000000..30b7bff
--- /dev/null
+++ b/archive/ES_0.5646390342268269
@@ -0,0 +1,22 @@
+archive/ES_0.5646390342268269---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T14:24:12.821
+Launch V∞: [6.2959305510988415, -7.597661578070238, 0.0687697179747265] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.578436053889911e-9, 8.655130558607273e-10, 7.53248819612926e-9] km/s
+ V∞_out: [-4.302069158458321e-9, -6.360242409369258e-9, -3.1790732513145667e-9] km/s
+ time of flight: 1.7981544076351714e8 seconds
+ arrival date: 2029-01-08T19:08:12.821
+ thrust profile: [0.19640030883116932 -0.05643666702952971 -0.06935684093713503; 0.10495624832976877 0.02585224147188596 -0.10699192092494256; 0.08176527929710711 0.041293099538094256 -0.13725084932745896; 0.07692953043918081 0.052744258177176075 -0.17653643985736722; 0.047808419955656274 0.04029518418595576 -0.14280975142450666; 0.02579770104857768 0.02435487592265273 -0.09385742453343825; 0.015989674546968063 0.01840342488538103 -0.07361409418232659; 0.010465544737517667 0.01245147694121043 -0.05410542390901682; 0.015287021148251246 0.01990520485761076 -0.08466813836668986; 0.0016017946990886964 0.0030154451767729867 -0.01506206237077898; -0.0009481444275548237 0.0017783399284872568 -0.004301712293946405; -0.0019133252652037119 0.0010475920691847334 -0.00810117560740566; -0.0022197804389792325 -0.0021861139592464275 0.0026168621969443317; 0.0005196772315127641 -0.0005405247197321125 0.0006090229293342748; 0.0007447661945868965 0.0017430186308449991 -0.0011054201186310715; 0.0004580170336876533 -0.0033145647081757315 0.0005737117508786403; -0.0019893089379470937 0.0022259435332595947 0.0017080184750806644; 0.0003308377140313479 0.0002940375759112029 -0.0018786439126661416; -0.0033361950464047504 0.0019023942689836196 -0.006371638853731913; 0.0006033927439529571 0.0021616112800861764 0.003898635746442501] %
+
+Mass Used: 90.76593523731162 kg
+Launch C3: 97.36793223325482 km²/s²
+||V∞_in||: 7.744607908145613e-9 km/s
diff --git a/archive/ES_0.5646468045985222 b/archive/ES_0.5646468045985222
new file mode 100644
index 0000000..3eff94e
--- /dev/null
+++ b/archive/ES_0.5646468045985222
@@ -0,0 +1,22 @@
+archive/ES_0.5646468045985222---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T14:24:58.030
+Launch V∞: [6.540868114127168, -7.4435320269563485, 0.1264437377024074] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0503044727209432e-8, 4.126137786709383e-8, 2.15109481918853e-8] km/s
+ V∞_out: [-1.357061993351754e-8, 2.6249899532220488e-8, -4.292561480947325e-8] km/s
+ time of flight: 1.8749577787472638e8 seconds
+ arrival date: 2029-04-10T16:34:35.030
+ thrust profile: [0.2021970743057298 -0.0496839833925748 -0.07530402213505981; 0.06695362325421833 0.01789062895458129 -0.077963783886396; 0.039874622662642405 0.01959891798790785 -0.07781131798053073; 0.04076255605621638 0.02934182925083627 -0.1154937059357809; 0.05029381518630402 0.04284507289379181 -0.17613593583164627; 0.023202796048411935 0.021485494893946754 -0.09974625343838883; 0.025575363817167848 0.026677705413144886 -0.12710332647352773; 0.005680864202076325 0.005284265177348239 -0.035229552138030626; 0.012517234586524475 0.010968012409330449 -0.05105499588238609; 0.001414737056349118 0.0015045966346578753 -0.006192480318947705; 0.0035340992955871825 0.004504934956595869 -0.030654220294774683; 0.002787706689700661 0.0012348304927263997 -0.0010525537861927022; 0.0017848396997348392 -0.0007900769666343644 0.0002374934541634218; 0.00297704119499925 0.002468034821083003 -0.00015589259514507182; 0.001431849613091893 -0.0028982081489515674 -0.0008587079004864647; 6.62343574940865e-8 -0.0012738611993162014 0.00406270886652183; -0.005870693470663331 0.009931729167588927 0.0015359355917709402; -0.0016532680438553116 -0.008661893867604083 -0.006372260317413389; 0.0014302804005560282 0.013555534601861149 -0.007601088489762006; 9.702294699921382e-5 3.0132711218586942e-6 -0.0017768225407998525] %
+
+Mass Used: 85.89144770599114 kg
+Launch C3: 98.20511274153453 km²/s²
+||V∞_in||: 5.084876634384579e-8 km/s
diff --git a/archive/ES_0.5646531191595692 b/archive/ES_0.5646531191595692
new file mode 100644
index 0000000..42da54e
--- /dev/null
+++ b/archive/ES_0.5646531191595692
@@ -0,0 +1,22 @@
+archive/ES_0.5646531191595692---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T15:31:59.299
+Launch V∞: [6.06962279553541, -7.529917811788297, 0.22469609905028057] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.46130540008799e-6, 7.458180410306051e-7, -1.564260304414727e-8] km/s
+ V∞_out: [-1.1409995664860922e-6, 2.4191456040185848e-8, 5.391606091442558e-6] km/s
+ time of flight: 1.7686686672555095e8 seconds
+ arrival date: 2028-12-02T17:13:05.299
+ thrust profile: [0.4627207920429425 -0.14329482142443467 -0.139614508532038; 0.1775447911679182 0.04324221504969359 -0.16103686755756194; 0.10260625052369929 0.052428349747578415 -0.15554927454598158; 0.07783477045741911 0.05468074264772393 -0.16328885633441176; 0.052142596989026464 0.04499112647286507 -0.14033309153677462; 0.026982428158576512 0.027288742279939493 -0.08969229142150176; 0.026717559403575706 0.030296453194393363 -0.10319878307497939; 0.009952988421501972 0.012614025251257132 -0.04741447300588464; 0.0028671189009374055 0.005217517805120026 -0.017994820311835483; 0.0022056608692454737 0.0030848991372175883 -0.013470701581230196; 0.0005191498754246768 0.0004493989832753398 -0.0019049376629516911; 0.0006105003315665274 0.0012704266380820042 -0.005294714670278167; 0.0010758390736183817 -0.0015332947824064527 -0.0005585356313217253; -0.0016888428275915039 0.0009092046728747432 -0.0027971699842177754; -0.0003333634619885602 -0.00010360493470508913 -0.003039744368526468; 0.0004391051019711361 0.0010633158053026072 -0.0025514400957041736; 0.00010973027506451062 0.0005763217773165167 0.0006998098639178414; 0.0013226512236885945 0.0003733660481756052 -0.0020651705520918053; 0.00039533830052934714 0.00019399360838136113 0.0005365785222041818; 0.00035906547069595703 -8.820671074477604e-6 0.0011084695324768612] %
+
+Mass Used: 112.81755544859152 kg
+Launch C3: 93.59047146929815 km²/s²
+||V∞_in||: 5.512018315860984e-6 km/s
diff --git a/archive/ES_0.5646550020755132 b/archive/ES_0.5646550020755132
new file mode 100644
index 0000000..a81a80e
--- /dev/null
+++ b/archive/ES_0.5646550020755132
@@ -0,0 +1,22 @@
+archive/ES_0.5646550020755132---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:27:15.449
+Launch V∞: [6.607557308637433, -7.408865312661301, 0.1653817223977415] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.017661504566022272, -0.008875450782266673, 0.02094398653391596] km/s
+ V∞_out: [-0.018297044594530354, -0.007721251300185608, -0.0208536532780828] km/s
+ time of flight: 1.8461215869291186e8 seconds
+ arrival date: 2029-03-06T08:36:33.449
+ thrust profile: [0.15265331452177267 -0.04327191970270766 -0.05865866662945027; 0.08424812354883357 0.019294682451561827 -0.09567819162522341; 0.061713434991273707 0.02854953137156847 -0.11766737872896091; 0.04738971383847568 0.02948622977292906 -0.12647257554190022; 0.03577649655625548 0.027123122668441985 -0.12382648202372014; 0.020091643760572802 0.017133399314787443 -0.08325836524846025; 0.021152738809909144 0.019902302454451747 -0.10289469252205917; 0.008517712108262347 0.008769642099003048 -0.046646757796522276; 0.011695506692425974 0.014136376993827644 -0.0723065987032594; 0.009345827478670611 0.009845920649015377 -0.06429746706944575; 0.0035920145575174065 0.0016590079406720282 -0.007649361662293902; 0.0007267264409564983 0.0006546607876029627 -0.004024253202604879; -0.0016936473964244316 -0.004795916931294088 -0.0002142642965516344; -0.0006569741773881341 -0.0006477359337388838 -0.0026025216390043147; 0.0014689560003750507 0.0010017731693672664 4.395368975182359e-6; -0.0005474087381895183 0.0004936756706290645 -0.00455263574056233; -0.0003547383167616399 -0.002102510974880108 -0.005721117311567712; -0.0005317534788497605 0.0013318943274473278 -0.0015269886514301771; 0.004440860368018221 -0.004221074106924216 0.005369509503742734; 0.0009938614493383178 0.002937181787711646 0.008267439490514596] %
+
+Mass Used: 83.72321120867446 kg
+Launch C3: 98.57844992218703 km²/s²
+||V∞_in||: 0.028798488537715255 km/s
diff --git a/archive/ES_0.5646553599198615 b/archive/ES_0.5646553599198615
new file mode 100644
index 0000000..26ccf68
--- /dev/null
+++ b/archive/ES_0.5646553599198615
@@ -0,0 +1,22 @@
+archive/ES_0.5646553599198615---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T07:48:10.540
+Launch V∞: [6.177470081011915, -7.51506051807631, 0.0400378032791625] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8640207658881653e-7, -3.921319135339572e-8, 4.8229565029929856e-8] km/s
+ V∞_out: [-1.9444852739964979e-7, 2.0274187107112458e-8, -2.3100375941109627e-8] km/s
+ time of flight: 1.8164628817808202e8 seconds
+ arrival date: 2029-01-28T17:06:18.540
+ thrust profile: [0.33291932524540946 -0.08585512869178441 -0.09276314488393302; 0.22153262079133715 0.06520621072737125 -0.17956956888023923; 0.08534982708412978 0.052130345298204595 -0.13574285831735472; 0.07601991604081536 0.06226553264640176 -0.14581150738720466; 0.04506442242162266 0.04481413471672929 -0.11388163374173424; 0.021521569015036015 0.02353746216752405 -0.07000860977003767; 0.035256274413831924 0.03590161183606798 -0.11807585575186112; 0.009185177916803886 0.013908953842595311 -0.04375407809671005; 0.005509180332445682 0.010703007482442635 -0.03371500230617058; 0.0011547743229099142 0.004481845543807996 -0.018664148563609644; 0.003623775772158129 0.007089378947165078 -0.022913550286888518; -0.00018073663307752256 0.00014176558201247144 0.0015332874003733735; 0.0007834414339167697 0.0009657143414211495 -0.0062411867516548565; -0.0012075420934947985 0.00024035205687992665 -0.0020650895929638455; 0.001514488007548731 -0.00046218547750180236 -0.0006599406215888593; 8.85899195030795e-5 0.00043955804662039954 6.477618826838461e-5; 0.0006760734791259706 -0.00014912840388218193 0.0021133331280365876; 0.000390350394829195 -0.00015558349061663176 0.00048712680007147397; 0.0027088219784397287 -0.0012114439429714015 -5.369389915200134e-5; -0.0018425699445290768 0.0008906363108824756 2.365541772358199e-6] %
+
+Mass Used: 106.7044869691158 kg
+Launch C3: 94.63887421783815 km²/s²
+||V∞_in||: 1.9649300108583328e-7 km/s
diff --git a/archive/ES_0.5646606346197812 b/archive/ES_0.5646606346197812
new file mode 100644
index 0000000..9d80560
--- /dev/null
+++ b/archive/ES_0.5646606346197812
@@ -0,0 +1,22 @@
+archive/ES_0.5646606346197812---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T22:37:01.303
+Launch V∞: [6.460417649190199, -7.444178339399443, -0.15158773822837004] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.9504594759726766e-9, 9.510432822173421e-9, 5.387924649634116e-8] km/s
+ V∞_out: [-3.499228682594132e-8, -3.4983695618232185e-8, -1.491610821794486e-8] km/s
+ time of flight: 1.8587038250683254e8 seconds
+ arrival date: 2029-03-20T05:16:43.303
+ thrust profile: [0.1773594091632511 -0.03985531233781899 -0.05742339635304118; 0.12090283190686103 0.04124462825858836 -0.11239249868240929; 0.1097481432491102 0.07181094694098183 -0.16890876707217403; 0.085617398369052 0.0750592254761946 -0.18692560338294487; 0.036666454210627926 0.03953014546418426 -0.10731398219117055; 0.02781451053891222 0.034114637620551495 -0.0983461147166533; 0.010141258723118043 0.013699056201540502 -0.04360594815909833; 0.010607439533473156 0.01590156278315221 -0.051765826808831274; 0.008250238300202202 0.013511526690522005 -0.047339184142105584; 0.002246019658615568 0.0038309101512802282 -0.01357346509199021; 0.00027024895477649165 0.001279769593649305 -0.0034992659134150993; 0.0004250759149498581 0.0006840174411293876 -0.0020776856102121457; 0.0005706242884858363 0.0014511801464346886 -0.004507853044307141; 0.0017234558482791401 0.001343583281389105 -0.003244880350606302; -0.0019719268212327304 0.008060814057686863 -0.005528251620264739; -0.003790633996239007 0.0012276565323846608 -0.0025368471726354876; 0.002892530606634144 -0.0040808802693327005 -0.004601440405807481; -0.004701863980667818 0.0005560800201255772 -0.005874619756415188; 0.002676084526426749 0.004935201501922209 0.0019459763083829263; -0.0015254294972838482 -0.003564047909565913 0.00262440456627196] %
+
+Mass Used: 91.9121042631341 kg
+Launch C3: 97.17576619313326 km²/s²
+||V∞_in||: 5.515188503039314e-8 km/s
diff --git a/archive/ES_0.5646630940282743 b/archive/ES_0.5646630940282743
new file mode 100644
index 0000000..e8c6012
--- /dev/null
+++ b/archive/ES_0.5646630940282743
@@ -0,0 +1,22 @@
+archive/ES_0.5646630940282743---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T22:42:42.486
+Launch V∞: [6.663037445759148, -7.425306708984568, 0.10776644896690073] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000490691055493139, -0.0031389432130375077, 0.004127749687913031] km/s
+ V∞_out: [-0.0033465561852868983, -0.002651658729385793, -0.003399399276142795] km/s
+ time of flight: 1.8749577787463826e8 seconds
+ arrival date: 2029-04-11T00:52:19.486
+ thrust profile: [0.09524515669596012 -0.02699971910827098 -0.04035442629327225; 0.08951753378847885 0.01903588283475146 -0.11172896739288282; 0.043197012273437536 0.017537933934528977 -0.09302614612349235; 0.034615245105948524 0.018198315837315245 -0.10545683715972996; 0.024271698168753915 0.014970729943857463 -0.09514346219986428; 0.034341434708294094 0.02456227270521374 -0.15206018420353448; 0.014743177483870704 0.011559718605711939 -0.08405273724544475; 0.011109760958539171 0.009785841407518701 -0.07873397431841614; 0.009036690669379056 0.007568806169423432 -0.05481263619759362; 0.00537366477254197 0.004415028020520418 -0.04022780080954278; 0.0018600730128823934 0.0011558904040727524 -0.013301410260612184; 0.0007031977353794883 0.00016666331049937778 -0.0012659363882852148; 0.0014535469441017638 -0.0002901992435104129 0.00030214606464980384; 0.0004577225951533619 0.0002936672537565449 0.0030306812060056838; 4.210964125668732e-5 0.00018630942913409808 0.004156486201160847; -0.0011812641407643722 0.0003815913119872664 0.0012043328010662984; -0.006919970885671643 6.039396102081217e-5 -0.0023605266068145838; 0.002696547303056529 0.006072589218727314 -0.00887642875698641; -0.0015566668451046646 -0.00017131427978571472 0.01218050345113034; -0.000349702149759735 -0.0018510871158476474 0.0005391564591642178] %
+
+Mass Used: 78.10691858697055 kg
+Launch C3: 99.54286133360276 km²/s²
+||V∞_in||: 0.005208844372092655 km/s
diff --git a/archive/ES_0.5646700937858697 b/archive/ES_0.5646700937858697
new file mode 100644
index 0000000..ce262e2
--- /dev/null
+++ b/archive/ES_0.5646700937858697
@@ -0,0 +1,22 @@
+archive/ES_0.5646700937858697---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:30:13.138
+Launch V∞: [6.341982748851332, -7.577932803215325, 0.05863948589444832] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.708093096810917e-7, 0.000273292274835986, -0.0001745132863497184] km/s
+ V∞_out: [-0.00015213385494005025, -0.00027973687597495625, 6.115332605278682e-5] km/s
+ time of flight: 1.8094757336450073e8 seconds
+ arrival date: 2029-01-22T22:43:06.138
+ thrust profile: [0.24477223497357556 -0.06928206583133563 -0.08568747130057791; 0.04959461231683979 0.011910407030216365 -0.054869553249870015; 0.04915045445872489 0.024446639857599522 -0.08739924412191152; 0.0438726414066319 0.03019778602103436 -0.10935068332954412; 0.04152106926555604 0.03223649905411747 -0.13591481726426832; 0.030280692382640098 0.02642088865056263 -0.12157283816922261; 0.01351448903216759 0.014079724063458275 -0.06471770505243736; 0.026052062556355587 0.029491275426237282 -0.13363892679536968; 0.016225671487051372 0.0201700782132064 -0.09642817031100105; 0.005963470815620625 0.007984039655494492 -0.04177980053840849; 0.0008119904642005418 0.0014034914530980502 -0.007480837428985537; 0.002205996075452711 0.0029615683186786507 -0.017485829411650854; 0.0006831803039276598 0.0014002805989167405 -0.00046797954311910165; -0.00020281172603559645 -0.0012156406807870765 -0.0005897612334902404; 0.0010924904164453376 0.0011304028647194917 0.001949598994806804; 0.0004083877886544157 0.0014950430922182952 -0.0018530036089813853; 0.0013370040669683143 0.00276805557141507 0.0009260616193334887; 0.002062683447418333 -0.003776389214360699 0.0008772182302519624; -0.0005452619894109203 9.015474390206295e-5 -0.0007469993209045041; 0.0004721937642173919 0.000810720370884892 0.0037171074778664147] %
+
+Mass Used: 89.1611548980436 kg
+Launch C3: 97.64924934608075 km²/s²
+||V∞_in||: 0.0003242596381088167 km/s
diff --git a/archive/ES_0.5646735592184182 b/archive/ES_0.5646735592184182
new file mode 100644
index 0000000..dc88c8e
--- /dev/null
+++ b/archive/ES_0.5646735592184182
@@ -0,0 +1,22 @@
+archive/ES_0.5646735592184182---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T14:09:21.132
+Launch V∞: [6.615723311977789, -7.592235019319295, 0.1040475999194184] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.993804617362961e-7, 3.626136120067935e-6, -2.602169531525363e-7] km/s
+ V∞_out: [1.2722482324021784e-6, -3.0007989729155492e-6, 1.6874321660382265e-6] km/s
+ time of flight: 1.8749577787492633e8 seconds
+ arrival date: 2029-04-13T16:18:58.132
+ thrust profile: [0.020551317617164767 -0.006626870043085767 -0.00887474860830269; 0.007814116649559976 0.0008131921712704543 -0.010372715339624911; 0.04377131656220557 0.011287619055625184 -0.09568244950807248; 0.05345169196236873 0.01773226167616232 -0.16132128991544706; 0.047530618277125576 0.017503709731119515 -0.18084725642353056; 0.034829378355339495 0.013308948834653245 -0.15796058660496354; 0.02040509062172273 0.007706751511970285 -0.10683499985596603; 0.0070624478949942796 0.0024753504653615053 -0.04245476676551995; 0.0022025267939315835 0.0006253055102688617 -0.014361885503612674; 0.00118981274806154 0.0004281770238341875 -0.005244623429386365; 0.0028234090103057964 0.0007866125644898645 -0.019648951734113376; 0.0006794146512474182 0.0016791359708564061 -0.002402784792476754; 0.0007961286733992922 0.0001524286576514451 -0.0021071694105149466; -0.0014401945560805025 0.0021675698310161867 -0.0037549871413401588; -0.0007836479094342637 0.0017150188809620538 -0.0021940713956192254; 0.0011414874913382553 -0.0019193421122832678 8.097942617259842e-5; 0.0012325181394870603 -0.0038020296159699237 -0.0028392463528764834; -0.003599785344188913 0.003356381732186567 -0.0024416077537812806; -0.0009894700830030533 0.0006108030547753749 -0.013370405191643972; -0.0009908129923467902 0.00158860170927107 0.005422658045561536] %
+
+Mass Used: 67.1653407332251 kg
+Launch C3: 101.42065343227362 km²/s²
+||V∞_in||: 3.669599006640001e-6 km/s
diff --git a/archive/ES_0.5646786561383559 b/archive/ES_0.5646786561383559
new file mode 100644
index 0000000..32dfecd
--- /dev/null
+++ b/archive/ES_0.5646786561383559
@@ -0,0 +1,22 @@
+archive/ES_0.5646786561383559---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T07:42:34.974
+Launch V∞: [6.468385147997573, -7.458055743038762, 0.19042037328799302] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.010107316096395e-8, -5.998215332915172e-8, -4.945678918038662e-8] km/s
+ V∞_out: [1.9920005138453978e-8, -4.1084720000702306e-8, 6.513735382384237e-8] km/s
+ time of flight: 1.8749577786781552e8 seconds
+ arrival date: 2029-04-10T09:52:11.974
+ thrust profile: [0.25345489508428604 -0.06232863036024276 -0.08233841870918505; 0.08056057187930764 0.02517070667319099 -0.08528942150807618; 0.03949614774005433 0.02274195984175695 -0.07194657668127959; 0.03431635594442277 0.02774841118882314 -0.08705824390370007; 0.024013723018719898 0.023447673796419644 -0.07880641610619242; 0.01381351591054535 0.015412889530891746 -0.05596595689642836; 0.029506950591524053 0.03864678354425003 -0.12960288107128382; 0.0344527216255497 0.05001481766307704 -0.17672673128171368; 0.01425814518329977 0.026633390797389606 -0.09073734554842237; 0.0020592048779226936 0.005119285597084457 -0.024401621905400798; -1.184572500082567e-5 -0.000496931356741786 -0.0009696220137936731; 0.0013290104713905857 -0.002540178625774799 -0.004368111522592133; -0.0001812488533216578 -0.0003126645414015342 0.000131610680162706; -0.0010369494704307136 -0.0034728839793950307 -0.0002002227510496642; -0.005201941516658554 0.0039245749874787395 0.0010715805072825982; -0.0004245276960366559 -0.0005294422664030049 0.001029646116436137; -0.00027126316599529086 0.00020100135467423618 -0.002030097771413882; -0.006639027212583777 0.005632070094522807 0.00379508711355979; -0.006069207247321169 -0.0013803952647948557 -0.00016491665662764145; -0.00244374675406231 -0.0002706537132559065 1.303478092253593e-5] %
+
+Mass Used: 90.04840494999416 kg
+Launch C3: 97.49886180767217 km²/s²
+||V∞_in||: 8.336610413997272e-8 km/s
diff --git a/archive/ES_0.5646838435450188 b/archive/ES_0.5646838435450188
new file mode 100644
index 0000000..b4083a9
--- /dev/null
+++ b/archive/ES_0.5646838435450188
@@ -0,0 +1,22 @@
+archive/ES_0.5646838435450188---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T17:32:32.512
+Launch V∞: [7.327355652242866, -6.293764726491528, -0.07280472359375327] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3777465445332362e-9, 4.0463570090442613e-10, -1.1526845231409236e-8] km/s
+ V∞_out: [-3.732895186472029e-9, 1.1747880051537884e-8, -1.927067620994452e-9] km/s
+ time of flight: 1.673163199384369e8 seconds
+ arrival date: 2029-08-26T06:17:51.512
+ thrust profile: [0.4507043731077677 -0.047236961000541165 -0.1232535811447416; 0.20879889927518494 0.09821642841376947 -0.17638416522325912; 0.15160064605682091 0.12344335128613888 -0.2109759415263807; 0.0886386651342436 0.0934008941015076 -0.18448604664524643; 0.029567624763244937 0.040436830374769674 -0.08907296375968989; 0.023238661331228268 0.03730386876706895 -0.08767554862940347; 0.017598788400282585 0.032432327463069066 -0.08083342401933571; 0.009519524757137382 0.019474830026676937 -0.05184967140219976; 0.0025530510452612537 0.005742442341312569 -0.016424716467827862; 0.008207508947658464 0.021118371315800556 -0.05824134698044806; -0.000598049989104888 0.0014237559873451727 -0.006956256890232447; 0.00022202421193690704 0.0004464800565300305 -0.0015097095596632287; -0.00016749147485834118 0.0005816554512750049 0.00020374854095412407; -0.0005429511399693259 0.0008590803544227568 -0.0006610608296819757; -0.0005148566704436763 -0.0011096984797802736 -0.0009474746889764924; 0.0010400347270711986 0.0003874027762715794 0.00041477548378215435; -0.0005715001240390646 -0.0004571771521894389 -0.0015004192391763183; -0.0011866710506338721 0.0007665354680121004 -0.0007058390631726119; 0.0009958135606960728 0.0008892441647532658 0.00325914932697899; -0.00041825504068851275 -0.0003737128988018489 9.192137088079972e-6] %
+
+Mass Used: 114.5074752169935 kg
+Launch C3: 93.306915814662 km²/s²
+||V∞_in||: 1.1615940623999485e-8 km/s
diff --git a/archive/ES_0.5646850884246604 b/archive/ES_0.5646850884246604
new file mode 100644
index 0000000..fda0614
--- /dev/null
+++ b/archive/ES_0.5646850884246604
@@ -0,0 +1,22 @@
+archive/ES_0.5646850884246604---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T19:58:30.614
+Launch V∞: [6.503112970474432, -7.515869327944588, 0.16394537672061132] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000364426770230559, 0.003520642372482084, -0.003516433772928262] km/s
+ V∞_out: [0.003497383269412158, 0.002846475729276158, 0.002197264784590129] km/s
+ time of flight: 1.8533083637312323e8 seconds
+ arrival date: 2029-03-16T20:45:46.614
+ thrust profile: [0.17782178700912643 -0.05129086813386093 -0.07061715265058048; 0.049438856898466284 0.009478458226645097 -0.059891736359241894; 0.03977500606858301 0.015823973523662584 -0.08156011960119038; 0.04242990567086597 0.022605204416428642 -0.11907095935913828; 0.03262264987234842 0.020504585522132895 -0.11706995466641361; 0.026299942942642957 0.018179055073859262 -0.11082212875814461; 0.031462714757576345 0.026091796723252483 -0.15913850935993937; 0.017329680782193713 0.01267498283549904 -0.09050229811072033; 0.004445845714174919 0.003923134718447888 -0.029689867459600557; 0.004221168564287955 0.001642909302984314 -0.01670262045442316; 0.002496071958627082 0.0020653211557811304 -0.01787319123718771; 0.0018408448854624919 0.0011261875545267675 -0.014524085368220491; -0.0035541194547898756 0.004183884865279696 -0.006290077198845381; -0.006572345553736394 -0.0014490421385689527 -0.002631209372552718; 0.0013203633259589922 0.0017568440267559573 0.0020965367054299293; -0.0048735404625021754 -0.0023353328254585365 0.0012681942299667662; -0.0008791348858258252 0.002848317418623428 -0.0014406053831547434; 0.000590928656504714 0.0021912623709487962 0.00048678017467282744; 0.0016101627421464156 0.0016647137987888003 -0.0006012130205404927; -0.0013821946191079726 0.002928611723301412 -0.011193899517649281] %
+
+Mass Used: 82.432988965209 kg
+Launch C3: 98.8056481480391 km²/s²
+||V∞_in||: 0.004989292140691648 km/s
diff --git a/archive/ES_0.5646913793190925 b/archive/ES_0.5646913793190925
new file mode 100644
index 0000000..d8d634d
--- /dev/null
+++ b/archive/ES_0.5646913793190925
@@ -0,0 +1,22 @@
+archive/ES_0.5646913793190925---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T02:42:13.299
+Launch V∞: [6.297845554324099, -7.346488831179479, 0.15393198703795502] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.548391862171469e-5, -8.497883294837252e-6, 2.0785764588175626e-7] km/s
+ V∞_out: [1.1369129706336567e-5, -2.50266264181894e-7, -5.495940610885713e-5] km/s
+ time of flight: 1.8749577787528056e8 seconds
+ arrival date: 2029-04-07T04:51:50.299
+ thrust profile: [0.4130991269557325 -0.09243528947990338 -0.11695164549049693; 0.22335506487022264 0.08181001248522574 -0.1915159411629099; 0.11530110155447379 0.07436534249761756 -0.17547342860071025; 0.06597466818428016 0.05772128332110824 -0.14558121618978562; 0.02690060796627057 0.029549883270266405 -0.0788070356635792; 0.027766726383385898 0.03525824561674046 -0.0979939713611894; 0.013120347822988206 0.018257235678691162 -0.05649421181194058; 0.004634288106489639 0.007525521755693978 -0.024592114379592408; 0.004678861109408449 0.008445210014215589 -0.028279672267291996; 0.0016631666709132978 0.00310569077078055 -0.01151407542866643; 0.0006302837177290593 0.0026648013000306354 0.00036369960634586185; 0.0011253900637567414 -6.34341340311859e-5 -0.002820107788563447; -0.000591819811383528 0.0012820039270135136 0.001926938170413259; -0.002918650540398424 0.0010810579248329965 -0.000878536016362848; 0.0037327188628247143 -0.002931114149338052 -0.00263906937754296; -0.00010044993248677282 -3.5510196357069754e-5 -0.00014748306194926875; 0.0050255690879835 0.0018950676443513473 -0.0028057687417569993; -0.004285737956321479 0.0011952917438150517 -0.00022959382407174806; -0.0030398519376426472 4.8302502903641344e-5 -0.008102587893079338; -0.0014986729997050828 0.003864799617843288 0.006873318999328039] %
+
+Mass Used: 112.47147353411901 kg
+Launch C3: 93.65745182939811 km²/s²
+||V∞_in||: 5.6131296536911415e-5 km/s
diff --git a/archive/ES_0.564698424590657 b/archive/ES_0.564698424590657
new file mode 100644
index 0000000..a939f38
--- /dev/null
+++ b/archive/ES_0.564698424590657
@@ -0,0 +1,22 @@
+archive/ES_0.564698424590657---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T18:09:20.366
+Launch V∞: [6.302930835685802, -7.303135318085574, 0.20530181959421773] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.494889954477737e-7, -1.3081508331054992e-7, 1.62486081532873e-7] km/s
+ V∞_out: [-6.716582316966644e-7, 5.965052336707791e-8, -8.208075755262684e-8] km/s
+ time of flight: 1.8505633169866553e8 seconds
+ arrival date: 2029-03-08T14:41:31.366
+ thrust profile: [0.5749110900538278 -0.14985656042208623 -0.13569031126352477; 0.0687238163058708 0.0244862924023156 -0.06326418570496081; 0.10087882352014284 0.07095992768228565 -0.1507876459005371; 0.045249896576129545 0.04113260617110467 -0.09714223260134809; 0.05751233898841074 0.06336980279230887 -0.1491570962731987; 0.017294699077989466 0.023239800651216787 -0.060440410485521644; 0.031994997537074694 0.04920177242508933 -0.12838633200985042; 0.01138388449463319 0.01897420340571502 -0.055209385265332145; 0.010572693132033815 0.020258086991198593 -0.05886159899833818; 0.0035754050553096235 0.006400820410997909 -0.021916465153742286; 0.0019438421862790567 0.003829073553477397 -0.013873678681241541; -0.0007919064387709092 0.00045269761632076456 -0.00033631599080384815; -0.0006094827261104276 0.0010279593940270507 0.0002852280790068592; 7.092941459058274e-5 0.0014435808514347646 0.0005236294695581407; 0.0009790142906173456 -0.0007257004290076696 0.000866319986346392; -0.0005124520060758953 -0.0005349741959196728 0.0006711794321036023; 0.00012110653709985239 -0.00031751485523903765 -0.00011474176954572501; 0.0010450161576509806 -0.0005222292215456435 0.0018408006045083228; -0.003364195633959138 0.001621659127075714 -0.0020223211028214307; 0.0005110051087839163 -0.0010308157481427858 0.0002687439639780816] %
+
+Mass Used: 115.7030786758869 kg
+Launch C3: 93.1048714308365 km²/s²
+||V∞_in||: 6.821658654031377e-7 km/s
diff --git a/archive/ES_0.5647004768694155 b/archive/ES_0.5647004768694155
new file mode 100644
index 0000000..2e1b575
--- /dev/null
+++ b/archive/ES_0.5647004768694155
@@ -0,0 +1,22 @@
+archive/ES_0.5647004768694155---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T23:12:08.926
+Launch V∞: [6.617340602408469, -7.425414209473867, 0.14981725138049048] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0898186365758164e-5, -1.7459313732395836e-6, 2.9746575752534787e-8] km/s
+ V∞_out: [2.519764024108314e-6, -5.704601676224312e-8, -1.074721037689424e-5] km/s
+ time of flight: 1.8749577787481105e8 seconds
+ arrival date: 2029-04-10T01:21:45.926
+ thrust profile: [0.11660643326860823 -0.0274582464649679 -0.04184823759920852; 0.07329776238669525 0.021353413744804563 -0.07804579647540022; 0.06962675742507336 0.03829775104113051 -0.12490688778263427; 0.038130363821053316 0.02875069215727159 -0.09720064005954945; 0.0433285709836628 0.03923129663479923 -0.13904039782098615; 0.02616455232645954 0.027337226315969583 -0.10271939462395183; 0.01876088239115885 0.021778700637858247 -0.08706942323268052; 0.012726224512786176 0.0175695568249891 -0.0717868666437228; 0.010857089060561004 0.01688327505083888 -0.06843166869229166; 0.004761045443510036 0.007212079772432351 -0.028326544552940282; 0.0021969492813268274 0.0025958143040434967 -0.011928248761751166; -0.00017481959894219976 0.000413091821687099 -0.00594246117389876; -0.00011877030945440137 -0.00039365514813565134 -0.0012984378091682623; 0.0032481817148290563 -0.0005532600208463581 -0.0030305741896409313; 8.754653162517366e-5 -0.001870670487437857 0.001284429065100551; -0.008672655138769797 0.0015505579273753494 0.0026825727965905355; 0.0011672124698452937 0.0030178246177099436 0.0008815220805344021; 0.007696308162149794 0.010022187770366415 -0.011971332145697854; 0.0008891589855802345 0.0015863238324574887 -0.005637864470883431; 0.005618292138132933 -0.006689036333382716 -0.005867863223992922] %
+
+Mass Used: 81.61811778476886 kg
+Launch C3: 98.9484180393513 km²/s²
+||V∞_in||: 1.1037192907692988e-5 km/s
diff --git a/archive/ES_0.5647049502046776 b/archive/ES_0.5647049502046776
new file mode 100644
index 0000000..e5cab47
--- /dev/null
+++ b/archive/ES_0.5647049502046776
@@ -0,0 +1,22 @@
+archive/ES_0.5647049502046776---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:59:38.037
+Launch V∞: [6.472384887847012, -7.338491900999727, 0.2317779441985278] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004073027907838714, 0.0027007037198586957, -0.003590372700749405] km/s
+ V∞_out: [0.0032568521669132577, 0.0023625682355902476, 0.002031851593072234] km/s
+ time of flight: 1.8749577786120567e8 seconds
+ arrival date: 2029-04-09T14:09:15.037
+ thrust profile: [0.3989975733054399 -0.10665154611020385 -0.1461239029604283; 0.09442487696202345 0.022874599034024844 -0.11085920887099862; 0.03714983260368494 0.017889349557781386 -0.07536575738294261; 0.03338746742509109 0.021550486673306127 -0.09475260247292058; 0.02902459546047265 0.022480160464752662 -0.10506779174586521; 0.025755796852115792 0.022714171990616 -0.11354288050708815; 0.015545252215133486 0.015097487465863231 -0.08030502619634552; 0.013586049230775898 0.014348137463344296 -0.08082577415359732; 0.005837829599103768 0.006662596566871035 -0.0384769342456815; 0.005464753116256285 0.0061584674410311456 -0.04019298539847711; 0.0025813282620557026 -0.00012047169059119667 -0.01242668784669519; -0.0014750614848310338 0.00011002818512857471 -0.00270665709283399; 0.002078613812509205 0.0017882737645068517 -0.028454318580020208; 0.0031775387438850652 -0.0013526508036589835 -0.0017423503637264137; -0.0006338765196897686 0.003962170335148329 -0.005048395475984907; -0.00351465758279789 0.004247815309383725 -0.0023249852505243768; 0.0009706235383002482 0.0012981102560362847 -0.0024447386473885626; -0.004195590116492476 0.009720922423633024 -0.00516193734836534; -5.0743880095451064e-5 -0.008162670003463112 -0.0020095443946413606; 7.368661731729689e-5 0.0034557088837830884 -0.0030423444907943793] %
+
+Mass Used: 99.9952304636231 kg
+Launch C3: 95.79895053288585 km²/s²
+||V∞_in||: 0.004511149773187042 km/s
diff --git a/archive/ES_0.5647097178020514 b/archive/ES_0.5647097178020514
new file mode 100644
index 0000000..b3e4ed2
--- /dev/null
+++ b/archive/ES_0.5647097178020514
@@ -0,0 +1,22 @@
+archive/ES_0.5647097178020514---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T11:46:21.879
+Launch V∞: [5.890555716341702, -7.654113108299419, -0.4650934462307722] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.458746937742977e-9, -2.693024969672495e-9, 4.702218831615393e-9] km/s
+ V∞_out: [2.390263723325932e-9, -5.364989053976809e-9, -7.500387094784625e-9] km/s
+ time of flight: 1.76310630682188e8 seconds
+ arrival date: 2028-11-28T02:56:51.879
+ thrust profile: [0.5087799454909951 -0.1685140948849994 -0.16915670183581105; 0.1368261771867144 0.031260858150887826 -0.13673161406193107; 0.06912018036659404 0.03403059200349303 -0.11580533260310064; 0.10124578708431323 0.06859602487342048 -0.22532249983665234; 0.06195561243462475 0.053427440822104884 -0.18632730230904448; 0.02850508654503692 0.027229042237718288 -0.10135125283523536; 0.012364398438738176 0.013837042792243516 -0.05449549440598667; 0.00459737903863485 0.005605641451474374 -0.024175480514235122; 0.007698226665755497 0.010323087473702704 -0.04367814505742944; 0.0007584365236549683 0.0009436310672837602 -0.004425329207318581; 0.0013078623669067267 0.002051832658919118 -0.006875027842204456; -2.7328582301460597e-5 -9.790617394052586e-5 4.5032876392828614e-5; -2.1048636631873052e-5 -0.00021231617468095074 -0.00022403150414266302; -0.0003873589105916165 0.00023379502047693858 -0.0007725807386102173; -0.0010872925966470062 -0.000382634598679566 -8.804993160643445e-5; -0.0003050104566869583 -0.00048734673237501886 -6.338269613578661e-5; -0.0006197680455810969 0.0007621336390993647 -0.0006432334103648049; -0.0016127261027185234 0.0004553512347176046 0.0007990318659953474; -0.0018178699162914663 -0.0007609957306742187 0.0013991663331891513; 0.0006055086710691261 -8.773568240315408e-5 0.000785357945500421] %
+
+Mass Used: 113.4089688941799 kg
+Launch C3: 93.50040603569371 km²/s²
+||V∞_in||: 7.691629447522566e-9 km/s
diff --git a/archive/ES_0.5647129324835499 b/archive/ES_0.5647129324835499
new file mode 100644
index 0000000..d35b2d5
--- /dev/null
+++ b/archive/ES_0.5647129324835499
@@ -0,0 +1,22 @@
+archive/ES_0.5647129324835499---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T20:24:52.566
+Launch V∞: [6.494001560803294, -7.508717423714728, 0.05915385451306258] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.378495298637633e-6, 1.0240636685804232e-6, -2.234916164383666e-8] km/s
+ V∞_out: [-1.428234271749411e-6, 3.1489613225203944e-8, 7.31090795575378e-6] km/s
+ time of flight: 1.8236553941734746e8 seconds
+ arrival date: 2029-02-08T13:30:31.566
+ thrust profile: [0.15374143974019513 -0.047544823793378495 -0.059626742241775686; 0.0633244642880114 0.011556795733959874 -0.07151211830904904; 0.06634843024864266 0.02661895453296479 -0.12667922467615977; 0.06009173882845044 0.03250707132712648 -0.16003079410435; 0.044802701150768245 0.028701120786382216 -0.15154185138295953; 0.033051008582217344 0.023554814469519684 -0.13322285400874584; 0.02091845444978538 0.014889287831955665 -0.09345263828570644; 0.012129700449731098 0.009086100250778436 -0.0610247168539502; 0.0017916723124756096 0.0013099283539510737 -0.01259429765011708; -0.0012455524333265767 0.0005081042453168602 0.0003155923884125499; -0.0011336124893836788 0.0002590841845450374 -0.0007079254126411993; 0.002494708200386241 0.005783893136319905 -0.020833467065474533; 0.0015242672214701475 -0.00011668615486304856 -0.00799657943126129; 0.004477736551371996 -0.00920291674899225 -0.022649970352249943; 0.0004588480720662952 0.0023188649234819883 -0.013139151673847917; 0.00042306548209800846 0.001034232453528359 0.0008943272332461172; -6.02828661102877e-5 0.0007774086639870067 0.0011952412580347876; 0.001452638583299369 -0.0017382333686053165 0.002020671682642009; -0.0013308646939966715 0.005407029774968124 -0.01681286602874653; 0.0012076485547341705 5.9783895899322495e-5 -0.0007813626210500949] %
+
+Mass Used: 83.91946323421189 kg
+Launch C3: 98.55639279941653 km²/s²
+||V∞_in||: 7.449254912697661e-6 km/s
diff --git a/archive/ES_0.5647270837549305 b/archive/ES_0.5647270837549305
new file mode 100644
index 0000000..63123e2
--- /dev/null
+++ b/archive/ES_0.5647270837549305
@@ -0,0 +1,22 @@
+archive/ES_0.5647270837549305---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T18:09:18.872
+Launch V∞: [6.342920235643871, -7.250917563406169, 0.14813617525048534] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.041265053724188e-6, 1.0930963559042015e-6, -2.302455009676616e-8] km/s
+ V∞_out: [-1.5740143783438697e-6, 3.6588039636248275e-8, 7.959508285636826e-6] km/s
+ time of flight: 1.8599331830358577e8 seconds
+ arrival date: 2029-03-20T10:57:56.872
+ thrust profile: [0.6408770492124031 -0.1638328702809932 -0.20177733998202566; 0.06310382869465661 0.018857927224041587 -0.0665853591019474; 0.06739428002426293 0.0391402271785477 -0.1179253843101868; 0.04718273154676559 0.03721443043932424 -0.11686108050100982; 0.03249448521684018 0.031292548095926395 -0.10444137605203568; 0.021133212094958265 0.023240494377976928 -0.08286098057682519; 0.016760472447341298 0.021187213003222596 -0.07920479445327167; 0.014675649137554703 0.02045326980865591 -0.07940453535861698; 0.005691918269663968 0.008228989198119187 -0.03593183913069494; 0.007126520180565789 0.012005094429622293 -0.049879361635011076; 0.0040678128158870485 0.007033899680485573 -0.030786951252540114; 0.0008583630489086356 0.0012320469822523035 -0.00469975260036519; -0.0011677155177327743 0.0009134628794871392 -0.002401409067960528; 0.002110237891673617 -0.001566983556573843 -0.000970459813904452; 0.0027124740290923833 0.0025797566755637906 -0.004201485049824089; 9.270565658146606e-5 -0.0017159365094058607 -0.002538734178103811; -0.0005663305201481521 0.002943251518668606 -0.0024057709925059904; 0.0012730881198856543 -0.001023664631764586 0.002251987779445703; 6.84366390024492e-5 -0.0003909302416890542 -0.002870772409978757; -0.006163638616286157 -0.0024002524168993226 0.003025839122397766] %
+
+Mass Used: 117.33767381884172 kg
+Launch C3: 92.8303869534704 km²/s²
+||V∞_in||: 8.115253134526616e-6 km/s
diff --git a/archive/ES_0.5647278674912162 b/archive/ES_0.5647278674912162
new file mode 100644
index 0000000..e35030b
--- /dev/null
+++ b/archive/ES_0.5647278674912162
@@ -0,0 +1,22 @@
+archive/ES_0.5647278674912162---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T14:21:07.453
+Launch V∞: [7.5535525849305705, -6.248549533066277, -0.1268141281798116] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.471038438578726e-9, 5.830693918490507e-9, -7.64902919585079e-9] km/s
+ V∞_out: [6.176015523579249e-9, 1.2099871008890988e-8, 3.868735015623004e-10] km/s
+ time of flight: 1.6442594880781204e8 seconds
+ arrival date: 2029-07-24T16:13:35.453
+ thrust profile: [0.3940283430591204 -0.06938246362479572 -0.1392525091550364; 0.06624141075682685 0.021695363794322842 -0.07375854992682533; 0.05241756348783126 0.03125103802059839 -0.0987164645080344; 0.06458788150501484 0.04744550625337737 -0.16776872198005546; 0.05989326610847214 0.05169779742563166 -0.19793345816077332; 0.041166461804118065 0.04391320801306358 -0.17525808743811802; 0.013630076074527672 0.014724508299453777 -0.06648494369497757; 0.013173009367585378 0.016721292630343148 -0.08512580287895978; 0.00506858543597598 0.008328650922189557 -0.038152155258344374; 0.005398325487191978 0.00745333093140368 -0.03521088722027168; 0.001284462766155965 0.003386961065558234 -0.0023708135811458093; 0.0016195841441826318 0.001063858649819522 -0.009521555930287537; 0.00039606103135530357 0.005015082939240802 -0.005253976198084013; -3.25688795215974e-5 -0.0004341568855530664 -0.0013228003522376616; -0.0019527307053221073 0.002507783635651293 -0.0024987653798402166; 0.0009106937124962143 -0.0007733762453678407 -0.002175891244782542; -0.001237763583052554 -0.0018774030682278753 -0.003191857692669938; 0.002516918336879604 0.00030413525728278636 0.0056672287702654875; 0.0006341968495585269 8.869036520420975e-5 0.00011960443497790844; -0.0006112802973356718 -5.718708025842967e-6 -0.0005898625472059139] %
+
+Mass Used: 98.16895523541825 kg
+Launch C3: 96.11660974360011 km²/s²
+||V∞_in||: 1.3498340946765856e-8 km/s
diff --git a/archive/ES_0.5647281144062901 b/archive/ES_0.5647281144062901
new file mode 100644
index 0000000..155df42
--- /dev/null
+++ b/archive/ES_0.5647281144062901
@@ -0,0 +1,22 @@
+archive/ES_0.5647281144062901---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T04:04:02.617
+Launch V∞: [6.5148069743272945, -7.515685982032404, 0.05149521872448991] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.830940502713264e-7, 0.000281708607444552, -0.00019474268073811052] km/s
+ V∞_out: [-0.00018565197428017807, -0.0002813851721563727, 5.993906830416224e-5] km/s
+ time of flight: 1.847384598906915e8 seconds
+ arrival date: 2029-03-09T08:18:21.617
+ thrust profile: [0.13729223355218045 -0.038065995906974764 -0.05346893196815618; 0.07458840241779914 0.01695171378691258 -0.08633665748450715; 0.04242677634217259 0.019121987311667712 -0.08253893446900522; 0.041495291965082545 0.026108530440733947 -0.11507644630511843; 0.04168030343189231 0.030648695271005968 -0.14356898077139751; 0.024548418513307545 0.020328284564682907 -0.10338908243240472; 0.02675016349012651 0.02483472793097563 -0.12669143678824615; 0.009825935133731683 0.009520206771577958 -0.054899613063611394; 0.011211247286329011 0.011189219622923022 -0.06752815158979075; 0.004740925444294658 0.005807828559377153 -0.037308615751295335; -0.0022173857556963047 0.001369469095599104 -0.0037815174732593075; 0.0020386045483873337 0.0028786754710964056 -0.019591177592199333; 0.0008619978901062957 -0.0015526384433467923 0.0016157573709882616; 0.0006921392383015775 -0.0005509534370868267 -0.009239024714461494; -0.0018152971088089779 -0.0013974532730763297 -0.0037243433155211923; 0.005803811746220993 -0.0017615564090428444 0.002206350765061849; 0.006913654837701146 0.0023922332054340844 0.001409484292293879; -0.0031310242906809373 -0.002624119686068108 0.0015232209469070637; -0.00258055677803398 0.0004929787164273365 -0.0012639375053978864; 0.0023916023852469798 0.0007866603594910509 -0.00503237373024777] %
+
+Mass Used: 81.7525650109269 kg
+Launch C3: 98.93089745081342 km²/s²
+||V∞_in||: 0.00034246931404801213 km/s
diff --git a/archive/ES_0.5647310648588211 b/archive/ES_0.5647310648588211
new file mode 100644
index 0000000..c4ad9e5
--- /dev/null
+++ b/archive/ES_0.5647310648588211
@@ -0,0 +1,22 @@
+archive/ES_0.5647310648588211---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T10:58:49.871
+Launch V∞: [7.738857848746164, -5.835479703274394, 0.16639833944011068] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.764985140116566e-7, -6.917407680847051e-6, 0.00014404024574527004] km/s
+ V∞_out: [2.0686809577105114e-8, -5.894791100271614e-7, 6.184676736188856e-9] km/s
+ time of flight: 1.7517532381640255e8 seconds
+ arrival date: 2029-11-24T22:47:32.871
+ thrust profile: [0.5468518065265383 -0.03465996314443928 -0.1445090550072326; 0.13622395809874094 0.07583158110004189 -0.11966876538888958; 0.06088956743192308 0.05666592778506961 -0.09851637335993775; 0.025127764977914788 0.030859528756089227 -0.06357110045872537; 0.027030195135415477 0.04656328049145449 -0.10368881258032381; 0.027652625555233852 0.05008428924850205 -0.11932685765696463; 0.04503643278149839 0.10107320317603882 -0.219532311515193; 0.0053219994738344266 0.013592436316884504 -0.03474856934433723; 0.0014369936544571806 0.003514987095874178 -0.009659181368372719; 0.0028571755236601495 0.008318322021333122 -0.023306414859182716; 0.002327390716242346 0.007989239631580216 -0.027490200694262737; 0.000690698562402762 0.0017156780160135635 -0.006703034355389961; -0.0004498101942586787 -9.189583836019733e-5 0.00047863611822083563; 0.001051985419787173 -0.0011239651149870962 0.00028063648699421526; 9.213184914346731e-5 -0.00024079123096959937 -0.0006496977726792375; 0.00075853894584319 0.0009132478019127275 -0.0005664569636899641; -0.00034678139288853843 -0.0002266086568247866 0.0006989610911552827; -0.0005958642682256927 0.0013343742239394821 -0.004603103331193794; 0.0016307397735127569 0.002341361040062647 -0.0007951480440155156; -0.00037405757952886046 -0.0023115763979670158 0.0022409547330299547] %
+
+Mass Used: 110.69205229814816 kg
+Launch C3: 93.97043257779595 km²/s²
+||V∞_in||: 0.0001442074036723409 km/s
diff --git a/archive/ES_0.564738479646665 b/archive/ES_0.564738479646665
new file mode 100644
index 0000000..3326352
--- /dev/null
+++ b/archive/ES_0.564738479646665
@@ -0,0 +1,22 @@
+archive/ES_0.564738479646665---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T13:53:56.113
+Launch V∞: [7.590603448909897, -6.352468444565711, -0.13808503891305188] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.299311232976124e-9, -1.3348723900358712e-9, -9.850470834354319e-10] km/s
+ V∞_out: [9.244402770521337e-10, -2.976298798433163e-9, 4.349137654509741e-10] km/s
+ time of flight: 1.6550864340814537e8 seconds
+ arrival date: 2029-08-08T04:31:19.113
+ thrust profile: [0.23512550970851698 -0.039289234896881034 -0.08896013692308258; 0.042202229614350315 0.014409855907319472 -0.05072933241392474; 0.05740835295011576 0.034966836751056336 -0.11524730268946595; 0.06272571778331153 0.050022601345154905 -0.17259926377623727; 0.037491455702054956 0.03556950044828797 -0.13647498954556075; 0.026991111752031755 0.02871862798214384 -0.12113512280769596; 0.013934302491791258 0.015563564350354582 -0.07420340484620679; 0.004666566632524504 0.0056648522890451695 -0.028953389869768056; 0.014550304731894023 0.019912989658267266 -0.10231728504220511; 0.018755789116832906 0.025276460575056527 -0.12909787782895368; 0.00423049979553384 0.006924013521891946 -0.03918900891830691; 0.0007598999872883346 0.0012971878745584794 -0.009251746940899003; 0.0006526399231988902 0.00014102676501804136 -0.0010434926637707485; -0.0006640249462214212 -0.0007364236708229184 -0.0017504520275522211; 0.0002547186395845457 -0.00018671380430129475 -0.00019922359293886695; -0.00014234431510227937 -0.0002087663122442169 8.527306720852409e-5; 0.00015178727174621702 -0.00018765120716358972 -0.0021754446472792436; 0.0001934949734735572 -0.00021522070508095664 0.00014925654027355187; -0.0024678039869210624 -0.0008131990973126869 0.00042307911186579823; 0.00021550519522314652 -0.0013387143232286571 -3.2811277142579497e-6] %
+
+Mass Used: 87.25215562907351 kg
+Launch C3: 97.99018353577753 km²/s²
+||V∞_in||: 2.1072284485557483e-9 km/s
diff --git a/archive/ES_0.5647390845461828 b/archive/ES_0.5647390845461828
new file mode 100644
index 0000000..9071235
--- /dev/null
+++ b/archive/ES_0.5647390845461828
@@ -0,0 +1,22 @@
+archive/ES_0.5647390845461828---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T06:45:40.353
+Launch V∞: [6.063445081078443, -7.764774159710829, 0.005765900747058452] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009805853198795497, -0.006281544980340776, -0.009657605087953155] km/s
+ V∞_out: [0.0063700491150660635, 0.011288859685541556, -0.0077993978798785255] km/s
+ time of flight: 1.7151267396051297e8 seconds
+ arrival date: 2028-10-03T09:10:13.353
+ thrust profile: [0.2514037411732549 -0.09353143046677731 -0.0982320694206637; 0.07309375535585728 0.009733964585129321 -0.08019841890973363; 0.07847281365480831 0.027800259800344715 -0.14036255979426632; 0.08377328730707506 0.041805360330371376 -0.20331416908780978; 0.05684125216784456 0.034651232920346574 -0.17540057101382875; 0.043019029074208 0.02973402318935656 -0.15932948683771178; 0.0330799239737687 0.0252066072532689 -0.14165457194745057; 0.006114905950705876 0.004829777586057254 -0.030025708713760525; 0.003007048622180754 0.00248240376382082 -0.014936083581505047; 0.00035258599739487013 0.0003399946675115693 -0.0030098368752810595; -0.00021029336655118108 0.0006112264927606809 -0.002185897429484589; 0.0004292448303672581 0.00033519005757561655 -0.0021840696140892324; 0.00026403745619478806 0.0003473089011890823 -0.0018032703842847699; 2.3485851679077262e-5 0.00020581431265341284 -0.0015679724947503717; 0.00020799599469861318 -0.0006375994700353145 -0.0016893550168554997; -0.0002310864859381039 0.0008417022292299303 -0.0022217518581624934; -0.0023748002233746754 0.0020025279324674848 -0.002464020949436001; -0.0009407894044478819 -0.001011845545446107 -0.003302590852503176; 0.0005062648758274221 0.0004624421791008896 -0.00018340552163040942; 0.0015666322227174366 0.00013824679042086555 0.002300177333237229] %
+
+Mass Used: 92.69574802283705 kg
+Launch C3: 97.05711724817878 km²/s²
+||V∞_in||: 0.015128843324300471 km/s
diff --git a/archive/ES_0.5647586784949894 b/archive/ES_0.5647586784949894
new file mode 100644
index 0000000..ac961ad
--- /dev/null
+++ b/archive/ES_0.5647586784949894
@@ -0,0 +1,22 @@
+archive/ES_0.5647586784949894---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T08:31:07.322
+Launch V∞: [6.331903840386725, -7.545420114736284, 0.16865487185743971] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.06402376631565e-10, -2.249068182832458e-9, -6.973727399145964e-9] km/s
+ V∞_out: [1.5519536975196397e-9, 2.3605727097164033e-9, 1.2361074628033912e-9] km/s
+ time of flight: 1.7934283853428262e8 seconds
+ arrival date: 2029-01-01T01:58:25.322
+ thrust profile: [0.1822460707859498 -0.0453254916194183 -0.0567547701571024; 0.10296469515192094 0.03273318467050823 -0.09032531255187651; 0.1535102871405524 0.09548532996501159 -0.20924025582938233; 0.06309416519515641 0.052732283771812376 -0.12392413386948035; 0.04124707619178296 0.042859634702949824 -0.10641970426500431; 0.044425955822404765 0.05380439187245643 -0.13578718093419795; 0.01855913176008796 0.024969442031301487 -0.06898280152805557; 0.012194580082840583 0.018262802190499396 -0.05257736800306906; 0.021114504155677342 0.036673290042127486 -0.10155767048141243; 0.0022324667309560806 0.0034613942203860666 -0.01062725687160233; 9.363725266046946e-5 0.0007717571313070041 -0.0015703981925170635; 0.00024546497325361413 0.0005168827060577578 -0.0015928131103025585; 0.00021278888773431607 0.00021597741576096614 -0.0007815710572903607; 0.00021910416621428986 -2.806918809058188e-5 -0.00047481643767392724; 0.0005053487936961167 0.00023435632668055258 -0.0005691452790334668; -0.00016126012084023006 1.5160086485721861e-5 -0.0004642572125316165; 0.0003578944557865414 0.0002365563661485252 -0.0005707937299143446; -0.00015637784770878454 -2.5021441582394094e-5 0.0002873912935015136; -1.081995595894321e-5 2.5841975020266645e-5 -0.00028213351168925786; -9.628445305562196e-5 0.00017477555997587704 5.4571372300767855e-5] %
+
+Mass Used: 92.73203497498253 kg
+Launch C3: 97.05481541757231 km²/s²
+||V∞_in||: 7.344904689353466e-9 km/s
diff --git a/archive/ES_0.564761106774319 b/archive/ES_0.564761106774319
new file mode 100644
index 0000000..6533264
--- /dev/null
+++ b/archive/ES_0.564761106774319
@@ -0,0 +1,22 @@
+archive/ES_0.564761106774319---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T10:34:22.106
+Launch V∞: [7.417454525550476, -6.150881830374266, 0.18108291102206076] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.331000428613837e-9, 1.1804318421350779e-8, -4.599742099652758e-8] km/s
+ V∞_out: [-1.4768798817032056e-8, 4.7602325474219336e-8, -7.808365055103697e-9] km/s
+ time of flight: 1.6602023670847195e8 seconds
+ arrival date: 2029-08-09T23:18:18.106
+ thrust profile: [0.5644923647668181 -0.08446067005192417 -0.173010266824658; 0.2184834254625433 0.08700494023912711 -0.20620285890100135; 0.10108907349496855 0.07055155019281403 -0.16709298977644735; 0.10240280083604311 0.0952860720880668 -0.23822429940339765; 0.04254789362394527 0.04774271163005471 -0.1336267111616708; 0.020512916666981518 0.02633671384450501 -0.08233316790494719; 0.010356294502245397 0.01583184946596119 -0.05203447028349728; 0.005204354213725251 0.008420135369551525 -0.02873216355724016; 0.00420187216014385 0.00784340961224303 -0.027394396326951096; 0.0011332390179320663 0.0024262271340308784 -0.008469216861712866; 0.001648702216265664 0.00214948459808324 -0.009725675790421873; 0.0005180530024019017 0.0005588183999224548 -0.0021909753866002765; 8.609788866636203e-5 0.0006320809819845094 -0.0002083205474998609; 0.00031731535534427157 -0.0005764417638054381 -0.00036144066154602747; -0.00010443636187130626 -5.5480230048941164e-5 0.0006631104388457646; 0.0002258424678394186 -5.563596059629525e-6 0.0002681214567658493; 3.1409663298392825e-5 -0.00035613247647822244 9.152760179673039e-5; 0.0002446882707291951 -0.00036263779071372444 0.00024213892476793088; -0.0010556714002815635 -0.0004827191798885017 0.0005549972623244929; -3.843910234392145e-6 6.332724236359947e-5 -0.0002055498950976482] %
+
+Mass Used: 117.06013319211206 kg
+Launch C3: 92.88476995050175 km²/s²
+||V∞_in||: 4.790810200948839e-8 km/s
diff --git a/archive/ES_0.5647628702435273 b/archive/ES_0.5647628702435273
new file mode 100644
index 0000000..84e5902
--- /dev/null
+++ b/archive/ES_0.5647628702435273
@@ -0,0 +1,22 @@
+archive/ES_0.5647628702435273---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T08:58:23.666
+Launch V∞: [6.515091501357688, -7.473903442995473, 0.14681387416386754] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010409262868197003, 0.0011561721067820945, 0.0010640148682310498] km/s
+ V∞_out: [-0.0012491182114110495, -0.0006022546628712918, 0.0012762752924461898] km/s
+ time of flight: 1.833017277399423e8 seconds
+ arrival date: 2029-02-18T22:07:10.666
+ thrust profile: [0.16967443232405416 -0.045880357193390266 -0.05968852389096676; 0.08732872533596298 0.022557435963821305 -0.09040431737050164; 0.031030402584937455 0.0150107514393059 -0.0533257671733335; 0.056545351309395954 0.04034392818967525 -0.13805951812726422; 0.03969752093492428 0.03427848592968064 -0.12456115605897736; 0.020915214322134387 0.019606141395471493 -0.07937484281071709; 0.009083315627209466 0.008431321196620564 -0.0389509598432801; 0.017860019884567382 0.020029473986680806 -0.09609418119228216; 0.03770768631893715 0.048651223382443556 -0.19627300283609306; 0.006177388837936423 0.008088298127422953 -0.03927618727034385; 3.546134176914324e-5 0.0010994649956377282 -0.0062327118811665765; -0.0003052235222607547 0.0015317757646894983 -0.0003881769408606244; 9.847388532634887e-6 -8.789852431055406e-5 -0.0006939382199217009; -0.0007040016171251839 0.002873551246305304 -0.0008754699099252158; -0.0003271811285938976 7.286926385001165e-5 0.0009486513451138917; 0.00025754032536669713 -4.89510244655337e-5 0.0016978548492957808; -0.0014466482107082018 0.0002122730097975184 -0.0005171348779769737; -0.0006556999636016638 -0.00012104107745955424 -0.0010443687843398391; 7.104818380406964e-5 -0.0036228216424276987 -0.003771557507947865; 0.003517737758607549 0.004382765643696808 -0.006459695023546961] %
+
+Mass Used: 85.31465710119164 kg
+Launch C3: 98.32720425992976 km²/s²
+||V∞_in||: 0.0018847782667756796 km/s
diff --git a/archive/ES_0.5647677684606803 b/archive/ES_0.5647677684606803
new file mode 100644
index 0000000..5278491
--- /dev/null
+++ b/archive/ES_0.5647677684606803
@@ -0,0 +1,22 @@
+archive/ES_0.5647677684606803---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T20:25:48.706
+Launch V∞: [8.065732858499672, -6.049608929497405, 0.06137928347124824] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0543286399746387e-6, 1.695447299374871e-5, -3.117667975206961e-6] km/s
+ V∞_out: [2.6809428775302765e-6, -9.867692410258092e-6, -1.4185368116177491e-5] km/s
+ time of flight: 1.8749577786880606e8 seconds
+ arrival date: 2030-04-29T22:35:25.706
+ thrust profile: [0.11367459515256198 -0.013369043542301968 -0.05081414328959648; 0.02555922087127929 0.006497291350389676 -0.04257148199262253; 0.018276071599037807 0.004891065996660272 -0.048410100500582; 0.04888865169700986 0.012386629239138226 -0.17717008637822995; 0.015971788258942538 0.004905053414835345 -0.07765163919749242; 0.018218404582748808 0.004188727319480356 -0.1017696959366769; 0.01632203122353004 0.003228264534802086 -0.10134840768125318; 0.01465180946627576 0.0019759399823183208 -0.09941162695803402; 0.004153460424234228 2.9183495592686608e-5 -0.02562401215393424; 0.0009309328263994855 0.0005540838003878519 -0.01718717553898231; 5.4830604791208395e-5 -8.181531327022301e-5 -0.002379101478144297; 0.002068946737432569 -0.00012878227695683868 -0.01399609514473025; 5.1495754166753875e-5 0.0003893444371901552 -0.0005220550330731922; 0.0020132822031893845 0.00038626644702734593 0.000598940492158675; -0.00033490008399433857 -0.0006110304976251565 0.0015624682316568474; 0.0022000529001268403 0.003729594140549238 -0.0014994230909240404; -0.00026797192685207495 -0.0002622040991580028 0.003608580448011668; -0.00016485092078939696 -0.002356548255852936 0.00241180233550838; -0.004108642727085965 0.0005936217786665085 0.007165573331781934; -0.0004254008186550434 0.00027644160776314227 0.0007511125670282608] %
+
+Mass Used: 65.89316726510333 kg
+Launch C3: 101.65758216097548 km²/s²
+||V∞_in||: 1.7360710649636593e-5 km/s
diff --git a/archive/ES_0.5647696300686091 b/archive/ES_0.5647696300686091
new file mode 100644
index 0000000..efcd8ae
--- /dev/null
+++ b/archive/ES_0.5647696300686091
@@ -0,0 +1,22 @@
+archive/ES_0.5647696300686091---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T13:11:07.186
+Launch V∞: [6.586337031401532, -7.461100944570326, 0.12981714814607695] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010994316435527854, 0.0010828980658138976, 0.0011250884137714082] km/s
+ V∞_out: [-0.0012991639551116218, -0.0006076178131209137, 0.0012608952721463967] km/s
+ time of flight: 1.8214117122609922e8 seconds
+ arrival date: 2029-02-05T15:57:18.186
+ thrust profile: [0.1346242137822591 -0.04374538423896403 -0.055440702798270944; 0.06619519677720012 0.009654370010147285 -0.08406193030831725; 0.05397337362488032 0.01854532119400445 -0.11490927666678513; 0.04530852027756795 0.021032282428678033 -0.13298365219591496; 0.03611945294510108 0.019558653434745547 -0.13461583528888596; 0.028105419047545255 0.016956843247924347 -0.12628607644222933; 0.02102717837581413 0.013788451171678831 -0.1093760930405928; 0.013666468646968428 0.009294245345021728 -0.08151357064244659; 0.007744004056249038 0.005517991654409556 -0.05170373686910958; 0.002550473750634948 0.001887920093667901 -0.02099353990503897; 0.0007813466274969499 0.00041264482070378205 -0.002924432977964654; 0.0003331904195638574 0.00029716534107460633 -0.002738092522306012; 0.00152673706133481 -0.0015906470667360925 -0.0026692308985063855; 0.0013778106681328504 -0.001099883278387412 -0.0016414985245974444; -0.0018121142760309556 0.00237834785823239 0.00035655503668817; -0.0056948205959943 -0.00041325233664637627 -0.00036811235638046147; -0.0032223779081702745 0.003493883065820606 0.0037125373832593584; -5.642094332271872e-5 -0.0007981511537727773 -0.002187659033282387; 0.0017729675960111834 -0.0018247167985715525 -0.004692169538316612; -0.004814062524338891 -0.010355318892599254 0.005639955426543313] %
+
+Mass Used: 81.02039589868991 kg
+Launch C3: 99.06471528823214 km²/s²
+||V∞_in||: 0.0019097754052744848 km/s
diff --git a/archive/ES_0.5647717736027369 b/archive/ES_0.5647717736027369
new file mode 100644
index 0000000..cf7ef5d
--- /dev/null
+++ b/archive/ES_0.5647717736027369
@@ -0,0 +1,22 @@
+archive/ES_0.5647717736027369---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T08:31:59.255
+Launch V∞: [6.297675089478074, -7.510119626950714, 0.12470487259395399] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001049740071436111, 0.0013457494246607751, 0.0010462580065641824] km/s
+ V∞_out: [-0.0013894170109197159, -0.0006718563035420262, 0.0012750396603802383] km/s
+ time of flight: 1.80647380828525e8 seconds
+ arrival date: 2029-01-19T04:21:39.255
+ thrust profile: [0.3586933151445227 -0.13718620254002806 -0.12935584592815985; 0.07981222544005691 0.01127720610693528 -0.09696633266778058; 0.0552090202729917 0.01797879223481662 -0.11209246642274737; 0.056503798184485365 0.02553155904114331 -0.15863871280705655; 0.040154977651497475 0.020438126356907352 -0.1411151089417319; 0.027351231461042142 0.015424776146677952 -0.11844350630458313; 0.022848686226994357 0.014381606556373605 -0.11523370878101098; 0.012171277191705849 0.008513511685492175 -0.06983683509346382; 0.003522754091454491 0.0023051663067104864 -0.022909021980312697; 0.0016513033592162423 7.102418613026435e-5 -0.010122935890348106; -0.0026112178984582135 -0.0003566587548229652 -0.0023515822138330117; -0.0027198014794217896 0.003722273021821182 9.702501302214059e-5; -0.00016939104448030688 -0.002574909489982196 0.0006003074620758195; 1.832672333034824e-5 0.0019304995449962784 -0.0019963443273487602; -0.0018860705870732616 0.0011182350057915768 0.0005432885877061045; 0.005238640662171838 0.0029175855712359603 -2.2074658547105864e-5; -0.002579598394603473 -5.429466121675708e-5 0.004521745858860149; 0.0033845655916852173 -0.0004237636693798138 -0.007631894528609589; -0.004308229589771795 0.006319239870048467 -0.0016256199316481762; -0.0012470166766973118 -0.001819232030818102 0.002722363967997754] %
+
+Mass Used: 98.44447125074157 kg
+Launch C3: 96.07815964899167 km²/s²
+||V∞_in||: 0.00200191197305305 km/s
diff --git a/archive/ES_0.5647827416764486 b/archive/ES_0.5647827416764486
new file mode 100644
index 0000000..77f54a9
--- /dev/null
+++ b/archive/ES_0.5647827416764486
@@ -0,0 +1,22 @@
+archive/ES_0.5647827416764486---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T14:22:39.274
+Launch V∞: [7.706099128609502, -5.569501466278842, 0.7577753710553716] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5832371879069656e-9, -7.093008352523046e-10, -9.92723515712238e-10] km/s
+ V∞_out: [5.635799345990887e-10, -5.352876017732892e-10, -4.266244852957412e-10] km/s
+ time of flight: 1.855862036802504e8 seconds
+ arrival date: 2030-03-28T14:06:02.274
+ thrust profile: [0.8615202200101926 -0.0073562591599234325 -0.21545119881236655; 0.059422167667665116 0.03581285889650717 -0.06229098518307989; 0.07436569755552828 0.07372509388928951 -0.13586716870066012; 0.03962737940303425 0.05258427155807027 -0.11118639128066755; 0.021690559296669396 0.03627277375800101 -0.08471914332379797; 0.014720020696414551 0.029729142957907892 -0.07549486366596274; 0.011516841684041067 0.02898429529740283 -0.07817608487213433; 0.004181099784980872 0.009102584443590696 -0.030552743914354197; 0.0033011912466615768 0.009199316235300644 -0.02234508811378278; 0.0012679682670144717 0.008743614867886532 -0.026431756748390215; 0.0004157296707865099 0.0038718596511210755 -0.004023761231868726; -0.0014181694096897738 -6.428310976398311e-5 -0.009677460740455467; -0.003643197193811041 0.0037328930730560167 0.005817612746871063; 0.0012971778543164948 -0.0014797405526141823 0.0009293381237658889; 0.001878290359384058 -0.004126048590903392 0.0031743494522752666; 0.0016811843937580007 -0.006592666252312956 0.006884419507151862; 0.005540087798110762 -0.013598048312307648 -0.009895922493673857; -0.01834861227703181 -0.001355944432721341 -0.005383859265433679; -0.00699923313635555 -0.01032381074739092 -0.004559429174137159; 0.0035284429420423765 0.006241427080913446 0.014767673231490242] %
+
+Mass Used: 128.210917680261 kg
+Launch C3: 90.97753387581639 km²/s²
+||V∞_in||: 1.998811558579057e-9 km/s
diff --git a/archive/ES_0.5647839511188827 b/archive/ES_0.5647839511188827
new file mode 100644
index 0000000..88ef7c1
--- /dev/null
+++ b/archive/ES_0.5647839511188827
@@ -0,0 +1,22 @@
+archive/ES_0.5647839511188827---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T05:46:55.065
+Launch V∞: [6.535122969138391, -7.470878486343564, 0.10911698070847052] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.079550095760828e-6, 0.00029008014273361325, -0.0002387578934446524] km/s
+ V∞_out: [-0.00020267912376503074, -0.0003054958300250564, 8.203023430251687e-5] km/s
+ time of flight: 1.8418604997160232e8 seconds
+ arrival date: 2029-03-02T00:34:24.065
+ thrust profile: [0.16622918661415373 -0.046839364622483115 -0.06427845493897841; 0.06461073434545443 0.014808869102905419 -0.07559882197759378; 0.05593495534078198 0.026197563912533934 -0.10988701175299674; 0.05342080141423662 0.034203234617256204 -0.14643138481565565; 0.0306900489030616 0.023140223918813117 -0.10813888494079126; 0.02800374225597695 0.0242548281981479 -0.11941081031157075; 0.018257760906561633 0.017256599508567033 -0.09123483234928934; 0.00871867046169676 0.009129305200135975 -0.05212523535837534; 0.014855593908696106 0.017626927145665765 -0.09939489164618008; 0.00595553522030945 0.006972719240446557 -0.04358142356170623; 0.0011769477070174047 0.00046637232672124045 -0.0017766088141347378; 0.0005051225419254835 -0.001296855683808901 0.001164167382776917; -0.00065276543185216 -0.0005200400807706233 0.002038378464894447; -0.002466386888252657 0.00026387755482837035 0.0014205246668436478; 0.00028169516017760294 -0.0043676365899473005 -0.002479438650550472; -0.0011566641762527652 0.0011440273428746086 0.0018198927933539397; 0.0035019045877230344 -0.0015002734075071837 0.005200410585721866; 0.0005346371674536796 0.007213405557693798 0.0005603761479970929; -0.0031402785193000017 -0.0012138588103693887 -0.0049540053854959945; -0.0025115370181419843 0.005286409564611438 -0.0003673307670578668] %
+
+Mass Used: 84.13431908482016 kg
+Launch C3: 98.53376409495021 km²/s²
+||V∞_in||: 0.0003757033222090147 km/s
diff --git a/archive/ES_0.564785521577207 b/archive/ES_0.564785521577207
new file mode 100644
index 0000000..54ed3fa
--- /dev/null
+++ b/archive/ES_0.564785521577207
@@ -0,0 +1,22 @@
+archive/ES_0.564785521577207---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:48:11.381
+Launch V∞: [6.497271701064009, -7.5251289845676235, 0.08273116112736617] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7649876654332499e-9, -1.6283914918980342e-9, 1.389791957983502e-9] km/s
+ V∞_out: [7.563307243779348e-10, -1.636636691982867e-9, -2.5017552454749084e-9] km/s
+ time of flight: 1.8233190259009477e8 seconds
+ arrival date: 2029-02-08T14:33:13.381
+ thrust profile: [0.14982404995860238 -0.0476011546573826 -0.060469697209188066; 0.048044937292061114 0.008198116420760309 -0.0571992667176343; 0.051951645031400116 0.019488293888397817 -0.10312088736117882; 0.060562906581233374 0.030798783506637752 -0.16714554741974277; 0.04350934552582437 0.02606025330092147 -0.1522291567438181; 0.030865020507488808 0.02061807849884489 -0.1299729544887842; 0.01778536183804991 0.01292459851756987 -0.08773059505000462; 0.013284333067616207 0.010236064820771962 -0.07393780290683069; 0.008191735312371403 0.0066393686085334 -0.050658156034869874; 0.0008484762669379755 0.0015740519161297154 -0.015782151751763437; 0.00553814402449317 -0.0028139617935548297 -0.003943118369166948; -0.0015210212284281393 0.0018829377199640473 -0.0033976381018016874; 0.0004908814153174297 0.002472779734652453 -0.002282222166622429; -0.0009776442494248841 -0.0007799192912830982 0.0019823526573945318; 0.0038091806698134245 -0.002843992733967598 -0.0015943384680310278; 0.0017600940600501058 -0.0033651867551983106 -0.010281647399387254; 0.0018920817514591572 -0.0002371210555431145 -0.001338197036527245; -7.207402197593809e-5 -0.0003035025386905999 -0.002407032310082149; 0.006588272298147712 0.012760462096662635 -0.008785456337217279; 0.0021427611607933578 -0.00349029383136625 -0.006952641762229906] %
+
+Mass Used: 82.29756545845885 kg
+Launch C3: 98.84895023684844 km²/s²
+||V∞_in||: 2.7745922216594343e-9 km/s
diff --git a/archive/ES_0.5647873039645623 b/archive/ES_0.5647873039645623
new file mode 100644
index 0000000..f418566
--- /dev/null
+++ b/archive/ES_0.5647873039645623
@@ -0,0 +1,22 @@
+archive/ES_0.5647873039645623---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T23:19:53.916
+Launch V∞: [6.416767233737806, -7.391426907775409, 0.11236249767334178] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00664453000189971, -0.00020044114534042564, 0.0043961682575204795] km/s
+ V∞_out: [-0.006359201422369313, 0.00016528634245783239, 0.0048074375986913425] km/s
+ time of flight: 1.859699554633778e8 seconds
+ arrival date: 2029-03-21T09:39:08.916
+ thrust profile: [0.3282499392724471 -0.07829496510629652 -0.10492885402437631; 0.12430303603127973 0.03666495591672312 -0.11859380214323104; 0.07468464492852905 0.04442376590264339 -0.12122340278377358; 0.050671813386663545 0.041426584783739985 -0.11586754759498026; 0.03240253829777021 0.03100749304813536 -0.09651713313138674; 0.028571350256628353 0.03333668381539375 -0.10417203274536418; 0.018927900383965208 0.024702003956056585 -0.08054273210707483; 0.00959327201692208 0.01715046649485944 -0.05016388051857864; 0.014355310014621262 0.02260969503575206 -0.08260549374491383; 0.008572998635330746 0.0148215622609082 -0.05660392279713526; -0.00011088626828160216 7.212626139259197e-5 -0.0015058804398870047; -0.0005787575956130297 -0.00043902349991235107 0.0019454011618249378; -0.0007322143231881493 0.0006967562169752022 -0.0025839944477960004; -0.0009590480716558055 -0.0006031644055050834 -0.0001819138079440178; 0.0010526031895759889 0.0005154780277277505 0.0006032790492845655; 0.0001683302082374344 0.0006504134194499002 0.004155471130623624; -0.002750565186410408 -0.003067530504537571 0.005507032463203417; -0.0008048281040113552 -0.00020270283940879185 0.006530230716297445; 0.0005837368088368255 -0.0014565385976866175 0.0010988753194885372; 0.0022162718862757834 -0.0030144112134765986 0.0025914023733407546] %
+
+Mass Used: 99.96432831625089 kg
+Launch C3: 95.82071879584088 km²/s²
+||V∞_in||: 0.007969708335147617 km/s
diff --git a/archive/ES_0.5647885990142105 b/archive/ES_0.5647885990142105
new file mode 100644
index 0000000..6d9b77b
--- /dev/null
+++ b/archive/ES_0.5647885990142105
@@ -0,0 +1,22 @@
+archive/ES_0.5647885990142105---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T20:13:34.321
+Launch V∞: [6.561487534988026, -7.496707858274876, 0.09686580766660557] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.253872177220006e-8, 8.751465760251653e-8, 4.587367729814321e-8] km/s
+ V∞_out: [-2.7962387607124626e-8, 5.7399957784142505e-8, -8.670031202650248e-8] km/s
+ time of flight: 1.844001333279298e8 seconds
+ arrival date: 2029-03-05T02:29:07.321
+ thrust profile: [0.11930515942395874 -0.03237603672394093 -0.045995109237597274; 0.08795334164736811 0.019606891401400508 -0.09744309626632154; 0.027138397782321064 0.012426283696589005 -0.05249086123164246; 0.023952094737443953 0.014582198229507059 -0.06433942386408645; 0.017211455307342444 0.012685539028029522 -0.058816144889107524; 0.027496173736742457 0.02072266905266835 -0.1008165064254798; 0.013774610213240987 0.014851138858898534 -0.07265375258772538; 0.02807173050842679 0.029340931793360517 -0.152504433555612; 0.012234595753188257 0.015345916086356706 -0.08469657610829838; 0.021905208701047802 0.02649569303885713 -0.1385346871190335; 0.0047046160550313606 0.004894819675573548 -0.02992957602835079; 0.0038340940729247653 0.005314419090572237 -0.028010617277413823; 0.00012438497976127093 3.261243883375838e-5 -6.79910791015696e-5; 9.91086512656505e-6 -1.0513885279823189e-5 -0.00010341708863062879; 3.462160316520572e-5 9.012717669032276e-6 -0.0002969515720606591; -1.543068822957755e-5 -0.00015531398564651246 0.00015528170218572003; 2.4560502978771906e-5 -3.65381166846709e-5 -0.0001307940241862104; -0.00012999416164285088 -5.986099776627833e-5 -3.9152384153127474e-5; 0.00010232480544356223 -5.869659307376608e-5 0.0001394700067944855; 2.0677776051216486e-5 -1.0606129165047012e-5 3.261239659894999e-5] %
+
+Mass Used: 79.88510503180487 kg
+Launch C3: 99.26313036881842 km²/s²
+||V∞_in||: 1.0757672803237944e-7 km/s
diff --git a/archive/ES_0.5647997605266213 b/archive/ES_0.5647997605266213
new file mode 100644
index 0000000..d88833e
--- /dev/null
+++ b/archive/ES_0.5647997605266213
@@ -0,0 +1,22 @@
+archive/ES_0.5647997605266213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T01:21:56.660
+Launch V∞: [7.471854168079045, -6.318794953925658, -0.020390672231811884] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0028905327611319334, 0.0020009502249212353, -0.0009268825264134993] km/s
+ V∞_out: [-0.0015587856537808732, -0.002788405787728689, 0.0017328355871995484] km/s
+ time of flight: 1.627535876250797e8 seconds
+ arrival date: 2029-07-04T18:41:43.660
+ thrust profile: [0.403146111316746 -0.06310783574698381 -0.14156628000009705; 0.08628099179684888 0.031121593562442575 -0.09362504348983054; 0.07344888122265228 0.047233400011339674 -0.13466219167662172; 0.07476640885415661 0.06383930975848465 -0.18773100221465666; 0.052523007463784674 0.05396565488072553 -0.17160018119009224; 0.0228938915767583 0.026827044530574003 -0.09534585725269029; 0.027375701415350475 0.03438890788677604 -0.1270305444533056; 0.01900432597148701 0.02670484185836268 -0.10675653272734781; 0.004538995400145234 0.006799894799397681 -0.033884403793712436; 0.002214633377825205 0.0033514685015261867 -0.015717526828666364; 0.0025952195896901094 0.004331161841428489 -0.019128193672042087; 0.0001000230908712551 0.00018539011161726343 -0.0004818609492670383; 6.139678628921013e-5 6.347564551738633e-5 -0.0006165139209715311; 8.645845704302776e-5 0.0001513874880993904 -0.0005805953091445378; -0.00010832004956636346 0.00030936483682667313 -0.0009745436978139542; 0.0001028780082936221 0.00027636147822561366 -0.0013181655777057683; -0.0006093000766372003 0.0004269871031714127 -0.000750790550934801; -0.00012013622109458959 -6.924507815871898e-5 9.571927407094679e-5; 0.00020677743983833416 0.0004466755590021753 -0.0007416440138088587; -0.0003042935041648765 -0.0006429168825499112 -0.000495002199497838] %
+
+Mass Used: 100.35527802424622 kg
+Launch C3: 95.75619015831063 km²/s²
+||V∞_in||: 0.0036356694931690384 km/s
diff --git a/archive/ES_0.5648003985887231 b/archive/ES_0.5648003985887231
new file mode 100644
index 0000000..e29bf0c
--- /dev/null
+++ b/archive/ES_0.5648003985887231
@@ -0,0 +1,22 @@
+archive/ES_0.5648003985887231---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T05:37:29.666
+Launch V∞: [6.520344403239505, -7.475838472407441, 0.12180610384088496] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9021226212434746e-8, -2.936477299870362e-8, -2.0319133971832973e-8] km/s
+ V∞_out: [9.113467478160665e-9, -2.0267322560129116e-8, 3.013423086761891e-8] km/s
+ time of flight: 1.8749577787451702e8 seconds
+ arrival date: 2029-04-11T07:47:06.666
+ thrust profile: [0.19104338075468777 -0.050208275094728604 -0.07108018357375157; 0.07159524206167801 0.017057353924671437 -0.0835760788179143; 0.027676513761591325 0.013049795692159666 -0.05592502511408105; 0.07071977699692404 0.04327262862381584 -0.18676328179546658; 0.04679748710196843 0.03401578404181768 -0.15960452612325232; 0.01684405141406711 0.014055046362633359 -0.07396820884776296; 0.008734406033109451 0.008336489434727446 -0.0456243798081816; 0.003063173080607817 0.002639431065932777 -0.017525167791169968; 0.010858784208245738 0.012196947137538125 -0.07847077859013325; 0.008545654630299994 0.009104630163985624 -0.06532761604604373; 0.003543378794687758 0.0035409717498772883 -0.026913254552380465; 0.002110548645375864 0.0030890474514995844 -0.01490771681521368; 0.0027904532452510174 -0.000369265093946451 -0.004356238995459302; -0.001909528126275499 -0.0012407229147988889 -0.0005555131315216233; -0.0028359822872774513 -0.003572027339917787 -0.0020168431505108776; 0.00037019074998389124 0.00021358663935092158 -0.003034798722599115; 0.006454536030850222 0.004766517493696435 -0.006025324697512912; 0.0010286221481058608 -0.001947248162030267 0.005309895825819482; -0.00031300383751228127 0.00016016163164558458 -0.0007012356760098483; -0.001639805068169083 -0.012006514393985371 -0.005198514856175446] %
+
+Mass Used: 84.82944743249527 kg
+Launch C3: 98.41788872931686 km²/s²
+||V∞_in||: 4.045941355550404e-8 km/s
diff --git a/archive/ES_0.5648092016017632 b/archive/ES_0.5648092016017632
new file mode 100644
index 0000000..ee4427d
--- /dev/null
+++ b/archive/ES_0.5648092016017632
@@ -0,0 +1,22 @@
+archive/ES_0.5648092016017632---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T08:52:26.458
+Launch V∞: [6.48470512087083, -7.566618503201537, 0.15335190039349755] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.781396910056527e-9, -2.9610074335656475e-9, 7.651457239463886e-9] km/s
+ V∞_out: [2.9202777054444865e-9, -6.6500370268061156e-9, -9.009403294367475e-9] km/s
+ time of flight: 1.8322524711730033e8 seconds
+ arrival date: 2029-02-20T00:46:33.458
+ thrust profile: [0.14322128992657485 -0.04343321071056218 -0.05730071741205527; 0.016700464358970275 0.0032742489784406102 -0.02126280289335362; 0.03867824303442478 0.015411327163063876 -0.07791650799439254; 0.04762553656151777 0.02509280904725788 -0.13120792875165616; 0.06221708652832118 0.037911602470254775 -0.21348350409557285; 0.02854342969682681 0.02028881979427058 -0.12162046443957353; 0.027416904925352825 0.020312345058968794 -0.132371254058996; 0.003508804882817888 0.002739317510124181 -0.019709856587695803; 0.006775876113895247 0.006241832285896443 -0.050193428564927964; 0.007117378056156478 0.006495122422280787 -0.049769129230617624; 0.001872970028336171 0.001648626233288297 -0.014714279989641928; 0.0013380373052842224 0.0012209253272565048 -0.010038757729554213; 0.0009382999012777709 -0.0012193339943519844 -1.4599795772085502e-5; -0.00034657489608055903 -0.0004385716450287021 0.0003377490315152648; -0.0013043472234987364 -0.0018829955320984462 0.00345781101272877; -0.0003147449503485671 -0.00046446621752367515 0.004632915652976296; 0.00032141485478194906 -0.002585564819297107 0.005648442599628849; -0.002713223742252967 0.0019480720380075697 -0.00639139003603729; -0.0017945105963049943 0.0018569046956777883 -0.0033698635919382405; 0.0026213306814864114 0.004785373269090279 -0.00557400558253328] %
+
+Mass Used: 79.52704338458898 kg
+Launch C3: 99.32863288299453 km²/s²
+||V∞_in||: 1.0036778025869979e-8 km/s
diff --git a/archive/ES_0.5648232125768946 b/archive/ES_0.5648232125768946
new file mode 100644
index 0000000..7e4100d
--- /dev/null
+++ b/archive/ES_0.5648232125768946
@@ -0,0 +1,22 @@
+archive/ES_0.5648232125768946---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T07:48:36.211
+Launch V∞: [6.212996020678536, -7.482812818769782, 0.11099476308642427] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.714345829611048e-6, 2.3299733723852256e-6, -1.6959823861735916e-6] km/s
+ V∞_out: [1.6467941638519997e-6, -3.8073350869474576e-6, 2.214920252102881e-6] km/s
+ time of flight: 1.769631943622731e8 seconds
+ arrival date: 2028-12-03T12:15:10.211
+ thrust profile: [0.4192994059567082 -0.13022367969334087 -0.12311457110037106; 0.12926093266315453 0.03163563044590938 -0.11899667536121247; 0.0837978656247748 0.042653066507758616 -0.12854676581155722; 0.06132346697391935 0.04176254203193599 -0.13197019287398296; 0.10687151917413586 0.07579664253898849 -0.28472949288133886; 0.02840461458247752 0.028072878311265394 -0.09675389644495404; 0.020311421044338304 0.022552969575084153 -0.0818921873082612; 0.004283601746735733 0.005079888017781226 -0.019906573907539856; 0.004097553535535791 0.005172220046019611 -0.021226318353432538; 0.0002610044318116584 0.0007908070977028789 -0.003574866462244033; 0.0020040027519115907 0.00014236317224032937 -0.0013586168642377577; 6.75248213747959e-5 0.00018612776215530018 -0.0006421056446307147; 0.0013906952821904751 0.0013936283589822403 -0.0003888248987076854; -0.000832968554438493 0.00022768214753384353 -0.0012462387767257716; -0.0010632963362572825 0.0009903558592252594 -0.0011399002056263576; -0.00021734760424810533 -0.0002736389093748314 -0.00031584396250426846; 0.00041698216863185955 0.0008180143742358881 -0.005053620360847406; 0.0007911166101875868 0.00010826193569265296 0.001571603551345916; 0.00035617350176576077 0.0005063577052018705 -0.0017567484195179792; -0.0043873575643260014 -0.0012345100018006487 0.0004947043533387064] %
+
+Mass Used: 107.09134009136278 kg
+Launch C3: 94.6061270711453 km²/s²
+||V∞_in||: 4.701222937936919e-6 km/s
diff --git a/archive/ES_0.5648345637412502 b/archive/ES_0.5648345637412502
new file mode 100644
index 0000000..c637405
--- /dev/null
+++ b/archive/ES_0.5648345637412502
@@ -0,0 +1,22 @@
+archive/ES_0.5648345637412502---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T14:39:22.717
+Launch V∞: [6.5319186351456215, -7.3132136813190645, 0.3213350624028617] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008369473042805336, -0.0010696108318615572, -0.0008408130787267847] km/s
+ V∞_out: [0.0010771127369830762, 0.0005747611300646585, -0.0010300434479892523] km/s
+ time of flight: 1.8749577788425848e8 seconds
+ arrival date: 2029-04-07T16:48:59.717
+ thrust profile: [0.2728788833479555 -0.06538592337030838 -0.082630254118972; 0.15338914145005136 0.04823435892853766 -0.13936161830865532; 0.08037921199525751 0.047863085956124145 -0.12728517565741443; 0.08994059099684104 0.07117324234906708 -0.19275033442522313; 0.028714354127567506 0.02879065787506267 -0.08590383075611846; 0.017057246609394047 0.02011391716431764 -0.06357015343032651; 0.008394156664232969 0.011900381576666902 -0.041304225647704106; 0.0101291463657895 0.01571178290009578 -0.054654449838246785; 0.0075438704141738665 0.00956414673714077 -0.03891892854112062; 0.004576617353811021 0.005089696333688868 -0.026474777741109626; 0.004433451662781012 0.004757553434211712 -0.020414362865187295; 0.003842872448507448 0.005222858172350239 -0.019968849588947932; 0.00011850502143538475 0.0044183913018113075 -0.00853854481657307; -0.0016820535266796905 -0.006165976975403711 0.003583439013139107; -0.0008016563898202986 -0.0006872928987931653 0.0006468919102125071; -0.001034121469989074 0.004897613260638034 -0.0019962361152042023; 0.0016713297440589994 0.00301197857235734 -0.0005484310133760475; -5.638435994158032e-5 0.0009075698062045585 -0.006127197524083419; -0.0013716072645034237 0.003790227835948641 -0.0048525878510814096; 0.00011230191601822122 0.00027568829579916127 -0.0028563051700498778] %
+
+Mass Used: 97.50183987323271 kg
+Launch C3: 96.25231162712443 km²/s²
+||V∞_in||: 0.001597346160084294 km/s
diff --git a/archive/ES_0.56483510209538 b/archive/ES_0.56483510209538
new file mode 100644
index 0000000..9b86c9e
--- /dev/null
+++ b/archive/ES_0.56483510209538
@@ -0,0 +1,22 @@
+archive/ES_0.56483510209538---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T22:15:31.431
+Launch V∞: [6.5771010896042945, -7.28064670331804, 0.22519847424903772] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.669049212699144e-8, 1.5030996618917063e-7, 8.915807146934762e-8] km/s
+ V∞_out: [-6.131485410936302e-8, 9.474104548312278e-8, -1.6533210126506012e-7] km/s
+ time of flight: 1.8436049481335062e8 seconds
+ arrival date: 2029-02-27T17:30:25.431
+ thrust profile: [0.2901806960060438 -0.07008856183098998 -0.09055260708534572; 0.14487991940711675 0.047244290884383505 -0.13561696497051204; 0.09742130807164018 0.06022364302537853 -0.15120057808793222; 0.07590348300310391 0.06482037898540341 -0.1702669638295835; 0.046938748555022926 0.04877786363726019 -0.12990105080251024; 0.025519769221435208 0.03229424133118593 -0.09478923957209452; 0.014253164405745833 0.02118859693558135 -0.06163784163020621; 0.009586720179625292 0.015322027279173622 -0.048717869250330656; 0.006084366115153462 0.010769227094967219 -0.03602686484779141; 0.00116171543974636 0.002404839246661011 -0.008309959985465132; -0.00011640028617407838 6.19359681349925e-5 5.8882536038001485e-5; -2.2554732906725585e-5 -9.720059273361672e-5 8.431754494372186e-5; -9.686686985837525e-5 -0.00031681153483744274 0.0013359107119688836; -9.708880322278078e-5 -3.750704171027886e-5 0.000413845267156883; -7.709659611841466e-5 -0.00016810761434893576 0.000226150437931838; 0.000135744467182282 -0.0005073593776794313 0.0003369758673253521; -6.881917784327138e-5 -0.00010605823846205985 0.00025829519315010254; -3.651731430628734e-5 0.00036233599692329986 -9.928103252884774e-5; -0.0001324126482266832 -0.0005190767811754432 -0.000140243760181028; 0.00014133065052793735 -0.00012311605217236432 0.00048364417099535636] %
+
+Mass Used: 97.12634694502867 kg
+Launch C3: 96.31678951421394 km²/s²
+||V∞_in||: 1.9972806240406657e-7 km/s
diff --git a/archive/ES_0.5648496778198562 b/archive/ES_0.5648496778198562
new file mode 100644
index 0000000..8d9d0b1
--- /dev/null
+++ b/archive/ES_0.5648496778198562
@@ -0,0 +1,22 @@
+archive/ES_0.5648496778198562---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:52:14.336
+Launch V∞: [6.415365240697378, -7.329384372423079, 0.13877744725031904] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.831213264879384e-7, 0.00030759713017049233, -0.00021817760076610405] km/s
+ V∞_out: [-0.0001698545664488274, -0.0003302840481151275, 6.55576492044182e-5] km/s
+ time of flight: 1.8749577787493548e8 seconds
+ arrival date: 2029-04-08T18:01:51.336
+ thrust profile: [0.4303539965733348 -0.10819513401391218 -0.13628749620486463; 0.10005273103204451 0.027702635682446474 -0.102945714545189; 0.08132215177933123 0.04347008056702112 -0.1404183142158046; 0.04965411694107643 0.035819711997131076 -0.12166250481098673; 0.02724936280834673 0.02279618959349439 -0.08583046114079629; 0.01882460583036513 0.018723060868178012 -0.07387976719469984; 0.031941828527302166 0.03610977184761646 -0.14622878705476072; 0.008473777470837452 0.004411584596095291 -0.03798610578514927; 0.004514031275442125 0.009162913062070921 -0.041864777070242117; 0.0031210115094028783 0.006934701934932452 -0.009877441694700149; 0.004100522152993477 0.004711633912552958 -0.017280025212082953; 0.0007462546774173167 -0.003738021555290051 -0.007442752798094256; 0.0020484666606424068 -0.0028972654731257218 -0.0002657845078777826; -0.004975755268459442 -0.0038166449289855618 0.0027021229744000107; 0.0026509372785215074 0.0028130884471464 0.0027865322731499362; 0.00013815775855185878 0.000523054106889022 -0.002202192896034697; 0.000862804644132794 -0.005116518027633056 -0.007610790249497637; 0.0003760534776466563 -0.00031109272018120526 -0.0012886956580815622; -0.010228992733479929 0.002287500638486148 -0.01207361830839391; -0.005054176876238763 0.004079759446850123 0.001796473260719356] %
+
+Mass Used: 105.43102461405579 kg
+Launch C3: 94.8960456301331 km²/s²
+||V∞_in||: 0.00037711858412536355 km/s
diff --git a/archive/ES_0.5648536686818371 b/archive/ES_0.5648536686818371
new file mode 100644
index 0000000..11c2f1c
--- /dev/null
+++ b/archive/ES_0.5648536686818371
@@ -0,0 +1,22 @@
+archive/ES_0.5648536686818371---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T03:39:40.938
+Launch V∞: [6.6114421561559, -7.220748408313412, 0.2233288548356176] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.003236125848315e-8, 5.000508639094881e-8, 3.6726675475892545e-8] km/s
+ V∞_out: [-1.73292968324594e-8, 3.5378305371442134e-8, -5.716443597925032e-8] km/s
+ time of flight: 1.8749577787483698e8 seconds
+ arrival date: 2029-04-07T05:49:17.938
+ thrust profile: [0.38188555285143805 -0.09555635131336597 -0.12563031794550206; 0.07383896230577178 0.021145501261976538 -0.07563937376602531; 0.07056196232875557 0.038902774662240826 -0.1213867505080129; 0.04107189068581904 0.030494649704028647 -0.10012454973717692; 0.03739147960642051 0.03372907544145585 -0.11711541477947589; 0.05291844916368855 0.0554972593406701 -0.20025070966742092; 0.025866385659115882 0.030353917409066008 -0.11694791226833459; 0.00258222822791362 0.0036410816264579016 -0.014999478913704437; 0.0011556905151542437 0.0011336740216425182 -0.0036395019757975333; 0.0007231123888095369 0.0006149748332635508 -0.007995497824026232; 0.0014550246225487858 0.002304975379238701 -0.013533247087157228; 0.0006320512201642986 -0.000980458025807161 -0.0018385587183440354; -0.0010416220179133458 -0.0002948547136604201 0.003659513355057826; -0.0028689961789603933 0.0052421443659085454 0.004604941826906961; 0.0007150189673527133 0.0011106192415156681 0.002865733290797882; 0.0031944807710204168 -0.0019725713539694443 0.00019891173570426614; -0.0015788587252850885 0.00039791016040964435 -0.003685661632374009; -0.0031333944724347006 0.001851403707417289 0.002764118131611467; 0.0017462065752928894 0.004113322972045924 -0.015732254116704834; 0.00025419407717764097 -0.0020490730355046246 0.0008852380575244223] %
+
+Mass Used: 99.57781749188689 kg
+Launch C3: 95.90025073775824 km²/s²
+||V∞_in||: 6.89296748812717e-8 km/s
diff --git a/archive/ES_0.5648575310907298 b/archive/ES_0.5648575310907298
new file mode 100644
index 0000000..364c504
--- /dev/null
+++ b/archive/ES_0.5648575310907298
@@ -0,0 +1,22 @@
+archive/ES_0.5648575310907298---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T19:32:22.928
+Launch V∞: [6.0431400457228595, -7.668901468268721, 0.049569388214728276] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008349344802085767, -0.005174088537417741, -0.008216180073659657] km/s
+ V∞_out: [0.005561741119834006, 0.009504302087538849, -0.006523821687288131] km/s
+ time of flight: 1.7311418353537837e8 seconds
+ arrival date: 2028-10-21T10:48:45.928
+ thrust profile: [0.3909277348064352 -0.1407773089753359 -0.147964341054328; 0.08647105639132152 0.013986096560496793 -0.09539513969122011; 0.08637623142554147 0.034316651645989155 -0.1537902313876511; 0.08035796467762611 0.044478826552466 -0.19444800661266345; 0.043012565425091735 0.02879015787507658 -0.13542289447673034; 0.03492112657737194 0.02679782207300854 -0.13185631636870543; 0.017213972514105003 0.014675120600026412 -0.07735739273609965; 0.00726241333105323 0.006993440266292778 -0.03806605196280493; 0.004868869875856451 0.004459983737063701 -0.028129336718755154; 0.0130005187916358 0.013067659459005562 -0.07855472952793437; 0.00047489460807572466 0.0005032795210390893 -0.0012478893823696336; -4.662565632298791e-5 0.00015765873806388212 -0.0019861420840115683; 0.0003105535500877605 -0.00015532040054003817 -0.00260312897750052; -0.00012116316176651885 -0.00017051158040667038 -0.0011295709922047297; -0.0006459917952107831 0.0009530172976658122 -0.0002037030807972296; 0.0010955961786344374 0.000647816638372415 -0.00031244193593506865; 0.00103905462618446 -0.0005603560394242296 -0.00029530416344110736; 0.0004325572513307357 -0.0005623900315499449 6.846354655735249e-5; -9.02807786255473e-5 0.00017724840265107028 0.0011484936780396982; 2.4262536784688444e-5 0.00037156000713342444 0.0008419703682297284] %
+
+Mass Used: 102.88517021804319 kg
+Launch C3: 95.3340484664814 km²/s²
+||V∞_in||: 0.012805794228393499 km/s
diff --git a/archive/ES_0.5648649529850593 b/archive/ES_0.5648649529850593
new file mode 100644
index 0000000..be76bed
--- /dev/null
+++ b/archive/ES_0.5648649529850593
@@ -0,0 +1,22 @@
+archive/ES_0.5648649529850593---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T17:57:45.398
+Launch V∞: [6.413070279605613, -7.482832588144851, 0.1794258769486296] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.829856314218131e-6, 3.6871468406164154e-6, 4.185998957993848e-6] km/s
+ V∞_out: [5.666246194349562e-6, 3.6945380987250834e-6, 1.1804293939922e-7] km/s
+ time of flight: 1.8749577789394796e8 seconds
+ arrival date: 2029-04-10T20:07:22.398
+ thrust profile: [0.27549809231770456 -0.07207040868934367 -0.0861464942063037; 0.0851029818147075 0.024441704060100135 -0.09520706388250649; 0.05843028416054266 0.0324269098031937 -0.11097751516970124; 0.02906471674842297 0.024772655049718026 -0.07930434502014393; 0.04579125713555522 0.04135115713071209 -0.15917969518338354; 0.019368201067628512 0.023164186200666143 -0.08247788069985122; 0.024341305313254076 0.028173607308836078 -0.1179952267589387; 0.010571597179379392 0.013230821582681901 -0.059242780246759524; 0.0027639931566790102 0.00469043904503408 -0.027729905478617433; 0.010751137754540905 0.015427665448662402 -0.0773037157886254; -0.0007204690651152753 -0.000355327374215287 -9.723606715642203e-5; 0.001341412012254207 -0.0007833378577616626 -0.0016893442988941748; -0.0009224342366677305 6.42507868772805e-5 0.0029595528124803793; -0.004094755998338306 0.00022799684066218646 0.0009643688602349334; -0.0002846784601930242 -0.0013095228214991983 0.003563121021009904; 0.0010969301110220894 -0.00042025187741733937 0.002228109711723545; 0.0009623780468673753 -0.0005572785269924012 0.003975778887126216; -0.0033539744891117607 0.0007000552926216689 0.0036442253176439997; 0.00128688712916786 0.0022757431639145996 0.004119758326850209; -0.0001236225612942224 -3.825646316008626e-5 -0.008543756940494807] %
+
+Mass Used: 92.2865008235899 kg
+Launch C3: 97.15244759868217 km²/s²
+||V∞_in||: 6.7664938105454356e-6 km/s
diff --git a/archive/ES_0.5648796174355584 b/archive/ES_0.5648796174355584
new file mode 100644
index 0000000..f2fcc81
--- /dev/null
+++ b/archive/ES_0.5648796174355584
@@ -0,0 +1,22 @@
+archive/ES_0.5648796174355584---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T21:45:55.979
+Launch V∞: [7.6757265444883105, -5.491682245671845, 0.45294233505462184] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.254063974528267e-9, -2.728748983157911e-10, -6.190449309965719e-10] km/s
+ V∞_out: [8.276326960827742e-10, -7.448626779081723e-10, -6.654772883323519e-10] km/s
+ time of flight: 1.8576048952832606e8 seconds
+ arrival date: 2030-03-28T21:54:04.979
+ thrust profile: [1.0 -0.01343240604502063 -0.2588233003905733; 0.08543560222702407 0.05793023154048169 -0.08368225745059132; 0.04241516881629683 0.04686207750753955 -0.07169303820458736; 0.03225428044294903 0.04783309351688668 -0.08125198896016796; 0.02007200525273753 0.038207920279460926 -0.07252274663079519; 0.023272387723305313 0.05675948176127485 -0.1121116890288445; 0.010680226462046765 0.029770064047565672 -0.06460825973916241; 0.01029670105918232 0.0350631244241419 -0.07964282749625198; 0.0034362191791125945 0.013852132089053882 -0.034488188572954756; -0.0001391886962614576 0.00017438770951904987 -0.007383277810759364; 0.0014776767618254855 0.004609542561549683 -0.006710667807810056; 0.0007841337354640715 0.0019158014370127135 -0.005498592321271004; -0.002682020329065167 0.0030384353204090846 -0.004626429984531037; -2.1330377581293015e-5 0.001092122721298435 -0.003872295265972655; 0.0034153635559078903 0.002833623715062048 -0.005620645402110906; 0.012615217385683879 0.0068149144839275205 -0.0038236565698825673; -0.0008863913339049575 0.001785275503626765 -0.002946962307279601; -0.00020960599482320675 0.004603218896835132 0.00013982833826776074; 0.011029776912165109 -0.0064313961929341554 -0.017380639620498742; -0.008290926897811515 -0.011599231698945892 -0.00471088865794358] %
+
+Mass Used: 138.22325332104992 kg
+Launch C3: 89.28050863207454 km²/s²
+||V∞_in||: 1.4249048350444453e-9 km/s
diff --git a/archive/ES_0.5648804830164132 b/archive/ES_0.5648804830164132
new file mode 100644
index 0000000..ee84c50
--- /dev/null
+++ b/archive/ES_0.5648804830164132
@@ -0,0 +1,22 @@
+archive/ES_0.5648804830164132---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T01:10:36.355
+Launch V∞: [6.03152771952163, -7.3783041874024455, 0.06059433318194016] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.860035792258668e-7, 4.639804106011067e-6, -3.103847947076007e-7] km/s
+ V∞_out: [1.745173560922323e-6, -3.7933211873294417e-6, 2.157888553506153e-6] km/s
+ time of flight: 1.874957778739016e8 seconds
+ arrival date: 2029-04-06T03:20:13.355
+ thrust profile: [0.6212419395332285 -0.11949501495796519 -0.145550881865982; 0.2227583447691549 0.09294000375670287 -0.16287679457780707; 0.1029087216356881 0.07829247412476015 -0.13046173563649982; 0.06976872822128206 0.07301143728134825 -0.12637962572496975; 0.04856421820472052 0.06388309454514603 -0.11642646717890474; 0.04965326437083251 0.07883587553113089 -0.1474458126796992; 0.014870707927135931 0.02623461443587498 -0.05379250155127336; 0.007518129415447085 0.01511819977085026 -0.032991280058931365; 0.0025826601163650206 0.0060070855838330805 -0.013487252476972108; 0.00024601604323005755 0.0005114362206548856 -0.0012215066409381671; 0.00019534778030919542 -0.00016508842086034438 -0.0001433433474508182; 0.001248774106875504 0.0032725705261738955 -0.00747386743725113; -0.0001847730715148254 0.00047391875758385024 -0.0009108680580054125; 0.0004079439922884899 0.0005272681416763655 -0.0008353617969207596; 8.595515514513518e-5 0.0002908406866422562 -0.0007693596409539824; 5.489695896287448e-6 0.00010009764449052295 0.00015511746131804645; 0.0005456328574027394 0.00018144915764139866 -0.0003172973211890193; -0.00014300435889761694 0.00018435644442035002 -0.0007395666201116901; -0.00026488345549786435 -0.00032829930171487064 0.00042141141530593147; -0.00041396886296680524 -0.00021054495100375525 -0.00030423908178343667] %
+
+Mass Used: 129.23006609841195 kg
+Launch C3: 90.82237098641203 km²/s²
+||V∞_in||: 4.700502289506254e-6 km/s
diff --git a/archive/ES_0.5648881303968899 b/archive/ES_0.5648881303968899
new file mode 100644
index 0000000..48686b0
--- /dev/null
+++ b/archive/ES_0.5648881303968899
@@ -0,0 +1,22 @@
+archive/ES_0.5648881303968899---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T20:21:17.906
+Launch V∞: [7.834604596371028, -6.203013523933002, -0.3300667677305718] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5717565980371244e-6, 1.5622289547174425e-5, -0.00035919273747912647] km/s
+ V∞_out: [-1.0595760107205889e-5, 0.00035944139687503306, -3.849312817473002e-6] km/s
+ time of flight: 1.788020157462422e8 seconds
+ arrival date: 2030-01-15T07:34:52.906
+ thrust profile: [0.15924019481446583 -0.033535203341937554 -0.0633181875932863; 0.03861623668883604 0.01075770425479878 -0.05747357770914667; 0.04410420672196134 0.02334171252597748 -0.12268441016490382; 0.027507170195613148 0.01477015583035365 -0.10050033971093272; 0.021811950131368347 0.012217851898488251 -0.10100876701653504; 0.01852797908891351 0.010577880084446323 -0.10208385557181023; 0.01691076674782755 0.016736048674467346 -0.14695295326104385; 0.006924880763617789 0.0036159760831060623 -0.0505831555416587; 0.005397123842058027 0.0074077103760140225 -0.02959327769628959; 0.0072544305731350595 0.004975094708254213 -0.04605237625953275; 0.002730577921994859 0.0019189280218663987 -0.027443508320687263; 0.0006240613774366599 -0.002546394279131418 -0.005959862699697086; -0.0006924854377085617 -0.0028944545104403734 -0.006047832006077919; -0.0013056875471417716 0.003442770421759702 0.0002861077849905429; -0.0010696103486098787 -0.004279132465452813 -0.0018536438432791382; 0.004072064545464457 -0.0005948571106072125 -0.005813833366862187; 0.008068013961090397 0.009545878087831085 -0.0011089012879334998; -0.0015184811726099519 0.005052741237769861 -0.009959210890799748; -0.0017402139371313413 0.0002928456863975126 -0.009771710447094394; -0.0005222981917114476 -0.0037653137104652658 -0.00597128410354153] %
+
+Mass Used: 75.89327695042402 kg
+Launch C3: 99.96735003073387 km²/s²
+||V∞_in||: 0.0003595357409316185 km/s
diff --git a/archive/ES_0.5648965956176054 b/archive/ES_0.5648965956176054
new file mode 100644
index 0000000..aca4c60
--- /dev/null
+++ b/archive/ES_0.5648965956176054
@@ -0,0 +1,22 @@
+archive/ES_0.5648965956176054---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T03:10:56.953
+Launch V∞: [6.309668362391616, -7.228775039881893, 0.21480921227420316] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5391790457449978e-6, 4.067140815375596e-7, -5.258292221896925e-7] km/s
+ V∞_out: [1.4438490622864116e-6, -3.8480473509781343e-7, 4.101944497152316e-7] km/s
+ time of flight: 1.874957778780121e8 seconds
+ arrival date: 2029-04-06T05:20:33.953
+ thrust profile: [0.6396796851918579 -0.14159934004928826 -0.17673068373401762; 0.15284283886076674 0.05475786757124364 -0.13392680825665587; 0.059967686231631026 0.03959791015895963 -0.09194883967230173; 0.04595611329002312 0.04174418218760098 -0.10021641456042019; 0.03176342621105239 0.035337953469874284 -0.09063293007397598; 0.019846731045323605 0.02662126998531094 -0.07148165071620786; 0.02769274921482614 0.04185272556272493 -0.10885308884071322; 0.011696253568868525 0.019979455201346464 -0.0586027784148248; 0.0074796870714973285 0.014573869476599756 -0.04488575086772564; 0.007289174122392991 0.014569305034852634 -0.04874038064094616; 0.003365242815866051 0.007868151035576858 -0.026097432178936175; -0.00018878062085288358 0.00023389552306190075 -0.0006260678469429716; 0.0004792533590059762 -0.0004146526928834474 0.00041108165146961045; 0.0008833544784725955 0.0013522543525198779 -0.002876411660364244; -0.0002758812530704561 -0.0011932822695039634 0.0011517601690860428; -0.0009000306276641806 0.0008355812132435581 -0.0009416636459077674; 0.0011218221960291193 0.0005244266409802038 -0.0013024065833031292; 0.0003376985745443015 0.001193719314461853 -0.0009958674201941942; 0.0021219628245022727 0.0010217036512910505 -0.0024252058650943687; -0.0006638186021956593 0.0008207179999163863 -0.0007295854060903697] %
+
+Mass Used: 121.7187574473387 kg
+Launch C3: 92.11324641826302 km²/s²
+||V∞_in||: 1.6765991917837847e-6 km/s
diff --git a/archive/ES_0.5649034767744845 b/archive/ES_0.5649034767744845
new file mode 100644
index 0000000..8738a39
--- /dev/null
+++ b/archive/ES_0.5649034767744845
@@ -0,0 +1,22 @@
+archive/ES_0.5649034767744845---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T17:24:29.738
+Launch V∞: [6.516602821982749, -7.3070092429176405, 0.25527722960967425] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0038189307320520274, 0.0025592607694749393, 0.004115206966398637] km/s
+ V∞_out: [-0.0025901002295680787, -0.004569008229521027, 0.003237056598707652] km/s
+ time of flight: 1.8581365718608055e8 seconds
+ arrival date: 2029-03-18T08:18:46.738
+ thrust profile: [0.298034058228898 -0.08334209123926892 -0.09119968428227118; 0.15569466544583674 0.04047397280357361 -0.14086828172338584; 0.09487577949951531 0.050306814473627136 -0.14961017178971947; 0.06592093061886338 0.04844289565572095 -0.14961580154162973; 0.044905747921368526 0.04182995469204967 -0.13603722130920756; 0.028266850329882805 0.032020708989856046 -0.10780894601784105; 0.0171452728688243 0.02096675744140745 -0.07634366326135512; 0.005609555433983562 0.007453944397175698 -0.02953942254112028; 0.00229873859046793 0.0033813155608348735 -0.015459160394423781; 0.0019888945892815426 0.0036549638891665882 -0.014195402167406801; 3.7311552450423674e-5 0.00027157459058241664 -0.005556573070951205; -0.0008153050792103886 -0.0010471342030087135 0.0007310690896473195; -0.0006039747868901116 0.00035943308930361706 -0.00043570847224581486; -0.0017552881944212795 0.001366114573536587 0.0019182335651029853; 0.00048318301024387783 -0.00139777023467104 0.003629840181070013; -0.0013755232345419558 -0.0007367937175346167 0.003577777154664227; 0.00017337052514400248 0.0026614541904083325 0.00011995486062237146; 0.002218502526216374 0.008608373116657813 0.0032459693225218734; -5.34443030670522e-5 -0.00870637895884844 0.0015589271047892388; -3.7723473278825965e-5 -0.0011378916485475237 0.005924446136175786] %
+
+Mass Used: 99.49935610639704 kg
+Launch C3: 95.92366287951455 km²/s²
+||V∞_in||: 0.006170006158723082 km/s
diff --git a/archive/ES_0.5649057865187427 b/archive/ES_0.5649057865187427
new file mode 100644
index 0000000..e9df52e
--- /dev/null
+++ b/archive/ES_0.5649057865187427
@@ -0,0 +1,22 @@
+archive/ES_0.5649057865187427---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T10:35:07.673
+Launch V∞: [6.45737556301965, -7.464167560250479, 0.13681628941835083] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.060909956841561e-5, -3.2470837316070767e-6, 5.428892083478743e-8] km/s
+ V∞_out: [4.125083091570784e-6, -9.234954108952861e-8, -2.0452415930341143e-5] km/s
+ time of flight: 1.8405312376621073e8 seconds
+ arrival date: 2029-02-27T16:27:10.673
+ thrust profile: [0.19496266158305084 -0.05484692144993761 -0.06808059496031778; 0.16036349619459767 0.03862674912217008 -0.1608271952846763; 0.041243903666240166 0.021802318809257547 -0.07697888266496015; 0.0504535844018797 0.03653504049157966 -0.12761871625157323; 0.03741130749965153 0.03201016818028579 -0.1253364633103025; 0.027482764607662816 0.027046095431180982 -0.10548438409629045; 0.01261073486786307 0.015039390848396323 -0.05984418507328305; 0.01337276377563504 0.015501191413565325 -0.06880365523748226; 0.007550981873297675 0.010320545312471606 -0.05033759786032918; 0.009350521092214821 0.009988747353995004 -0.05492496182129146; 0.0024260344729636622 0.003167358639190174 -0.019044932707366784; -0.0010203660730437498 0.0010757536608727836 -0.008408395902158559; -0.002378966519214285 -0.0002943954331356218 -0.0021292409882142024; 0.0002790835822884962 -0.00043453093555656584 -0.0024768083518204647; 0.00254668908629351 0.006480322324704859 -0.008446825443103484; -0.004438317816068229 -0.0018135057048884714 -0.0028343768989770304; 0.002169887396660138 -0.0023709383808787113 -0.0004481247028270258; 0.0002656077582111137 0.0016285925344867594 -0.00227434552837416; 0.0019911179691506674 -0.003393744278971769 0.003328411839267619; -0.004939175460617979 0.004674613530602392 0.007285928834900913] %
+
+Mass Used: 90.71382878436316 kg
+Launch C3: 97.43021522642913 km²/s²
+||V∞_in||: 2.0863400611306423e-5 km/s
diff --git a/archive/ES_0.5649064803266926 b/archive/ES_0.5649064803266926
new file mode 100644
index 0000000..3ecad27
--- /dev/null
+++ b/archive/ES_0.5649064803266926
@@ -0,0 +1,22 @@
+archive/ES_0.5649064803266926---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T06:23:52.322
+Launch V∞: [6.180041969250723, -7.560722874766941, 0.0240334436360373] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3550870301902431e-7, 2.767709721372184e-7, 1.2322120572167704e-7] km/s
+ V∞_out: [-9.175183879430121e-8, 1.7356611150528484e-7, -2.575925855936841e-7] km/s
+ time of flight: 1.8179337578471753e8 seconds
+ arrival date: 2029-01-31T08:33:27.322
+ thrust profile: [0.28797131503859863 -0.07303321727644373 -0.08898145383250114; 0.24003903362709283 0.0657268827526955 -0.2064837107728615; 0.04559004073648025 0.027725914715491455 -0.07282389231948586; 0.06467399162049917 0.05768631321504071 -0.14783767973359088; 0.04436994631691518 0.04804112336953787 -0.13253869523567027; 0.03232103575904187 0.03979917783489442 -0.11689000229878266; 0.011973052329409569 0.01637318411303277 -0.05268554621144818; 0.009643698360163483 0.017029729828593212 -0.058105967107711376; 0.015090890060291982 0.02500774309449373 -0.08562645312021715; 0.0016911824935443456 0.0026906085061314962 -0.011385976790419302; 0.0008057876591512228 0.0008294252013865649 -0.004535537786115221; -0.0016733226384946205 0.0006686030140358113 0.00042455035910366054; -0.0028186716296856804 -0.0005553268414095606 0.003299770375595865; 0.0021356170984611093 -0.0005439614391622816 0.0006502875489962875; -0.0003144047653957115 0.0005377010995469033 -0.0019831467935605123; 0.002422712321053778 0.0009442501663125642 0.0013326258533371445; -0.0003610227737248343 -0.002558689634686244 0.0006118219083867664; 0.0004185537743039299 -0.004107059930901309 0.0036065490625133466; -0.00022324009752837712 0.0005994967160166515 -0.0013476151379924733; 0.0004324250576429097 -0.0005044942810713598 -0.0015293634638710637] %
+
+Mass Used: 102.80240441450633 kg
+Launch C3: 95.35802673713744 km²/s²
+||V∞_in||: 3.318858917627909e-7 km/s
diff --git a/archive/ES_0.5649117966004618 b/archive/ES_0.5649117966004618
new file mode 100644
index 0000000..77e87cb
--- /dev/null
+++ b/archive/ES_0.5649117966004618
@@ -0,0 +1,22 @@
+archive/ES_0.5649117966004618---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T12:24:32.674
+Launch V∞: [6.440088419235104, -7.278942833116861, 0.15878594597612886] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012641215096916297, -0.00597483158543557, 0.014421297362238274] km/s
+ V∞_out: [-0.012812200410408666, -0.005197272924796808, -0.014566103978690445] km/s
+ time of flight: 1.8749577787394193e8 seconds
+ arrival date: 2029-04-07T14:34:09.674
+ thrust profile: [0.47072529767895144 -0.10480402538961694 -0.14469503316804574; 0.09503370213204511 0.031192309275184998 -0.0954786508681824; 0.07698542797629895 0.047797762971574016 -0.12923884395599908; 0.05024686697699967 0.04177205588842523 -0.11983423705427557; 0.03272821648328199 0.03331281452607519 -0.10191491252775546; 0.01968498253918934 0.02384028469837107 -0.07689929798870715; 0.0184609775224742 0.024729067837422177 -0.08439946847219879; 0.007850534898841216 0.011616958261595332 -0.04313086085691365; 0.013600881124577465 0.020956031656204563 -0.08023288588707737; 0.002698183226379533 0.005026993140073463 -0.01937667255648371; 0.0024969233603088317 0.0048936266025735 -0.02000679254846709; 0.0019631906889856906 0.0028498462945074137 -0.009951076180502626; 0.00045769481141511465 0.00048196470078892454 -1.6939326801482246e-5; -0.0003495571195547961 0.0006815132060001066 -0.003306769056313522; 0.000763472780801099 0.0015186025777407914 -0.0065284686113268806; -0.0004763093428787397 -0.002523484980200408 -0.0017529237576039047; -0.0018340298887775065 -4.411524131168565e-5 -0.001517902213330645; 0.006713517163702306 0.003193750804463185 -0.001770807184304665; 0.007922020736406422 0.00267417247093613 0.00030469322858637593; -0.007092588074300684 -0.0004066369430336715 0.00877301719305917] %
+
+Mass Used: 107.91315924726996 kg
+Launch C3: 94.48296059198894 km²/s²
+||V∞_in||: 0.020086631106557506 km/s
diff --git a/archive/ES_0.5649140150784663 b/archive/ES_0.5649140150784663
new file mode 100644
index 0000000..a6a98e8
--- /dev/null
+++ b/archive/ES_0.5649140150784663
@@ -0,0 +1,22 @@
+archive/ES_0.5649140150784663---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T20:18:42.757
+Launch V∞: [6.493671190766329, -7.294137183930939, 0.2581228336643211] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3229706685292928e-8, 2.2275480435399582e-8, 1.1712539546562638e-8] km/s
+ V∞_out: [-6.687421901275086e-9, 1.4375074340738227e-8, -2.272974498240984e-8] km/s
+ time of flight: 1.8749577385173824e8 seconds
+ arrival date: 2029-04-07T22:28:15.757
+ thrust profile: [0.4227472493462054 -0.09545067124574871 -0.12839330496974447; 0.06039864311871576 0.020127113774538206 -0.05984306261841469; 0.05061794407285235 0.03279504796099529 -0.08391663445454284; 0.04638273148640629 0.03974326874988165 -0.10648344831315866; 0.032672678362575897 0.03456809002909834 -0.09748866165888821; 0.031317966422941566 0.03900850339661543 -0.11447961625607936; 0.022057974317909224 0.03110362362166084 -0.09683727810607091; 0.022574118375621247 0.03593789327811841 -0.11302017057607397; 0.008191870104105454 0.016653086708693147 -0.05503788164445563; 0.0034900906523500507 0.006628739711096822 -0.023765059355336602; 0.0017614162487611623 0.0010531007728812542 -0.01988573886964873; 0.0011428510238266254 0.002726331809022726 -0.003433461598111463; 0.004789615731604737 0.0009339024445101991 -0.0008557553516955656; -0.00019844287018141708 -0.0005086998735791531 0.0015030465399344809; -0.00043432856590967935 7.436084644498082e-5 -0.0019377161389638733; 0.0024066974001813934 -0.0002832543236981084 0.002548128617329169; 5.067376760182279e-6 0.0011125820897319673 0.0008659817997129257; 0.008038066392692358 -0.0034831991525867824 -0.001811315126311439; 0.006959369156321526 -0.0023610553886784557 -0.003188253480319973; 0.0033174436610857033 0.0022631320682608954 0.008197101038663532] %
+
+Mass Used: 102.33984148874379 kg
+Launch C3: 95.43883018905146 km²/s²
+||V∞_in||: 2.8432477033078697e-8 km/s
diff --git a/archive/ES_0.5649151119464034 b/archive/ES_0.5649151119464034
new file mode 100644
index 0000000..d64b653
--- /dev/null
+++ b/archive/ES_0.5649151119464034
@@ -0,0 +1,22 @@
+archive/ES_0.5649151119464034---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T22:02:04.573
+Launch V∞: [7.578960912522031, -6.361250521353218, -0.0862568784281087] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1822743700378117e-10, -3.452728809644234e-11, 9.839638069672237e-11] km/s
+ V∞_out: [8.130699835328759e-10, 1.913032958212423e-9, 4.46339119122941e-11] km/s
+ time of flight: 1.661952630810605e8 seconds
+ arrival date: 2029-08-16T11:23:07.573
+ thrust profile: [0.2282780131686688 -0.03608833234380379 -0.08757464115243596; 0.037481504191020386 0.01313507127543553 -0.04469457575060373; 0.10563307493977475 0.06411565930144476 -0.2073390819979889; 0.03264231771092284 0.025723684128634607 -0.09452426946500278; 0.02723287280918255 0.02527405234989939 -0.10073089119524709; 0.03046564181328372 0.033664035022255845 -0.1405639756190473; 0.034254626302299106 0.03667368868561614 -0.16410484869261244; 0.022438997604867374 0.02698190792982387 -0.12628590530317388; 0.004130335841982419 0.0050319782231694945 -0.02439340294184363; 0.0036554414510913706 0.005313664345954083 -0.025236193933533636; 0.0016408708085314276 -0.0003973157947809035 -0.004569116568869661; 0.0023787394282559536 0.0036366390456665848 -0.02122957376795215; 0.003437549958970951 -0.0011627271090180675 -0.001139480003218036; -6.748888398142442e-5 0.00018684791336786552 0.0008385732762135551; -0.004683492357252841 -0.006284854204340103 -0.002992845211847753; -0.0010110401883163065 0.003506936525463437 -0.00479308409895144; 0.005450558768247437 -0.0013329816810695838 0.0033922028441416953; 0.00013519810201790086 -0.007999787387505477 -0.0042297195718077; 0.0033398416179722203 -0.004810522039256464 -0.0007804541893702056; -0.00015533809991144076 -0.0005309588188636104 -0.00014059618918978384] %
+
+Mass Used: 87.90498168229851 kg
+Launch C3: 97.91359695802952 km²/s²
+||V∞_in||: 1.576442457497009e-10 km/s
diff --git a/archive/ES_0.5649157544105051 b/archive/ES_0.5649157544105051
new file mode 100644
index 0000000..842da32
--- /dev/null
+++ b/archive/ES_0.5649157544105051
@@ -0,0 +1,22 @@
+archive/ES_0.5649157544105051---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T22:37:13.712
+Launch V∞: [6.436212794608795, -7.4728912050359915, -0.12994900893747205] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.02933356595318553, -0.019859853769583623, 0.030501896849116136] km/s
+ V∞_out: [-0.02953105257272254, -0.012431295730440968, -0.03403795813440837] km/s
+ time of flight: 1.8080063392972663e8 seconds
+ arrival date: 2029-01-19T13:01:06.712
+ thrust profile: [0.23327782094141367 -0.07028082634317043 -0.08991045808051966; 0.09184961282114629 0.02096274328225591 -0.10283562008160137; 0.07382129869787447 0.0350140092257722 -0.1364244003207359; 0.061013170591784585 0.039260253396455086 -0.1555452564804627; 0.04572533106423705 0.035712625164356325 -0.14952531714009562; 0.03130880310124153 0.02847451494502374 -0.1265299264897128; 0.017778923604797783 0.018777496848600382 -0.08813695380062402; 0.008559422870866227 0.00981505766386006 -0.049270993200862596; 0.005996384160582868 0.007396770724609137 -0.038965294050468495; 0.001429610676910883 0.0014847611921538677 -0.009810251361149288; 0.0029147331948760767 0.003205631070686351 -0.019516023011557117; -0.0005853570233543216 0.0010965502467814815 -0.0013557873565252466; -0.0006780243789938939 -0.00011370992713575535 -0.0017526106661613708; 0.00039414726643111883 0.0007908904489350324 -0.003397391756615054; -0.0029144912582376495 0.0013765076501378855 0.00274171456290692; 0.003165537647709426 0.00457292721416193 -0.0028929327634124656; -0.0002605605878888852 -0.0002445631325644418 0.00573423031343764; -0.0005247780130043594 -0.0003587609895702897 0.002992847382276601; -0.000490489993379784 -0.0014090570516978463 0.005233743501832768; 0.002492464981498272 -0.0018867868382848147 0.0012039521853199151] %
+
+Mass Used: 91.56773521809055 kg
+Launch C3: 97.28582484471407 km²/s²
+||V∞_in||: 0.046746524947564295 km/s
diff --git a/archive/ES_0.5649250762014535 b/archive/ES_0.5649250762014535
new file mode 100644
index 0000000..f31602b
--- /dev/null
+++ b/archive/ES_0.5649250762014535
@@ -0,0 +1,22 @@
+archive/ES_0.5649250762014535---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T17:17:49.724
+Launch V∞: [6.608711690362955, -7.425798913953589, 0.15897274754139856] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.1615063653965196e-8, 9.91947934578537e-9, -1.2937229704108906e-8] km/s
+ V∞_out: [4.259916866527351e-8, -3.739510054943441e-9, 5.035711681581183e-9] km/s
+ time of flight: 1.874957778746737e8 seconds
+ arrival date: 2029-04-10T19:27:26.724
+ thrust profile: [0.1628210639035448 -0.043729777589587945 -0.06177428426939726; 0.0517271047436543 0.012154354966556176 -0.06112958350208847; 0.040882016677040355 0.018470498507741472 -0.08115462110787267; 0.052792020213088174 0.03153676765843484 -0.1445016900441102; 0.03870030592790859 0.02781538227844404 -0.13676780681012643; 0.023918339924262136 0.018698943519759672 -0.09966699247839918; 0.023446966957672424 0.0203245522289494 -0.11474728941586425; 0.009280224291369337 0.008416712660716466 -0.05193746772635255; 0.004984631936472501 0.0046874408384390874 -0.03255576113114967; 0.00503215654536048 0.009209073509759629 -0.041255957372788095; 0.006980699452099719 -0.0022932635968077554 -0.019703982260211382; 0.00840498189085489 0.006456865150388233 -0.012191875356633792; 0.0028212505664547255 0.0009988052959493839 -0.004572484389593132; -0.0003702149078416983 0.003212758233784606 -0.003834994216918158; 0.0015018425275143909 -0.0007366390864747486 -0.00339846389183882; -0.004165706586140333 -0.0026539919435459866 -0.0027590066728552303; -0.010480910316632813 0.008279783067544861 -0.005856812197808067; -0.0014110502354968404 0.0032571768323062895 -0.004891066722798846; -0.0003135832632103694 -0.005833802193871896 0.0016380190232977948; -0.004281220475778255 0.005739126779660585 0.011668842486346073] %
+
+Mass Used: 82.49606860259064 kg
+Launch C3: 98.84283205127515 km²/s²
+||V∞_in||: 4.469431178384913e-8 km/s
diff --git a/archive/ES_0.5649255691595256 b/archive/ES_0.5649255691595256
new file mode 100644
index 0000000..dc81a0e
--- /dev/null
+++ b/archive/ES_0.5649255691595256
@@ -0,0 +1,22 @@
+archive/ES_0.5649255691595256---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T15:55:21.991
+Launch V∞: [6.30846101030624, -7.7010741350263725, -0.14140295954048032] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8077321632742559e-6, -1.3455352134213909e-5, 8.329182730533916e-7] km/s
+ V∞_out: [-4.891840759295902e-6, 1.0984245030432173e-5, -6.382243691571227e-6] km/s
+ time of flight: 1.736369002772227e8 seconds
+ arrival date: 2028-10-28T08:23:41.991
+ thrust profile: [0.10095184892539874 -0.0374812627163545 -0.042468280898292195; 0.05019869330329653 0.006970722545634626 -0.05825877114066391; 0.07032696872171242 0.023967594117666517 -0.13251982945825905; 0.07426279345435327 0.035040835829161614 -0.1931236695514094; 0.06396908414173327 0.036438867809115406 -0.21001078796511435; 0.040410660499462 0.02611300899704209 -0.15802687747184613; 0.020757492297889403 0.015067440832353268 -0.09401246759066667; 0.007888501535779795 0.006345545887956027 -0.04223344333465376; 0.004012343655146661 0.003232303520586099 -0.02493746323302371; 0.003249541735451911 0.002704371640713187 -0.01990162981776517; 0.0023569675835380054 0.0007862053863177373 -0.00942579845264751; 0.002549004194226116 0.0003403756302628757 -0.011591100840325615; 0.00017215524217130653 0.0008508785090587453 -0.00022558195257337509; -0.0010500064446952566 0.0018491235508193804 -0.001328782869222252; -0.0008701306011745096 0.0010282028435715193 -0.0014981644055799092; 5.133237261565989e-5 0.000803382408849384 -8.516672108537958e-6; -0.001991571988380897 0.001754235465569832 -0.0010286937147365395; 0.0018062247380825074 0.0008347705321591105 -0.003974791123583477; -0.0008284425240216486 0.0019489018675607596 -0.0022396553822238508; -0.001596800098527599 -0.000572712363119209 0.001274645676495752] %
+
+Mass Used: 80.86105931873726 kg
+Launch C3: 99.12321794869302 km²/s²
+||V∞_in||: 1.360177008625779e-5 km/s
diff --git a/archive/ES_0.5649343184824483 b/archive/ES_0.5649343184824483
new file mode 100644
index 0000000..026d13b
--- /dev/null
+++ b/archive/ES_0.5649343184824483
@@ -0,0 +1,22 @@
+archive/ES_0.5649343184824483---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T22:04:38.555
+Launch V∞: [6.237068673173598, -7.446247173404043, 0.110760424728393] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.211022839928824e-9, -3.8238824952117085e-9, 1.1335077553070846e-8] km/s
+ V∞_out: [2.7571458353730906e-9, -1.1452475980196026e-8, -8.85480372587145e-9] km/s
+ time of flight: 1.8749577787409776e8 seconds
+ arrival date: 2029-04-10T00:14:15.555
+ thrust profile: [0.49519356177532725 -0.11917735964586562 -0.15011540835637296; 0.08995724214119663 0.027057295858504107 -0.09185644934894663; 0.0467454725770358 0.026914819760752398 -0.08296812559596667; 0.04701529753538987 0.037450323669403485 -0.11810342070696472; 0.058527440604119095 0.052896828642269016 -0.1712768076261603; 0.02053323365136032 0.023783907654739426 -0.08309891700303851; 0.0214675694520207 0.028342632931191734 -0.10003857070370836; 0.0073067432676136015 0.009668960384489724 -0.04398474232605541; 0.0043777368342738775 0.004529192275218298 -0.0222544411751566; 0.0012014710505033857 0.0017765719445886037 -0.008776097733460568; 0.00037109284980828337 0.006101694180509535 -0.021228612607883557; 0.0025291063347005526 0.00424996810127351 -0.020353605616946928; -0.0038114589459417375 0.0023929521285212 -0.011394602656924064; 0.00138258178995238 0.001353882891319148 -0.004448065814841926; 0.0038547377654159706 0.0036172613143298955 0.0016332560081568307; -0.0016683092154211542 -0.0033691411613681966 -0.0020013056112777616; -0.0010789694020561175 0.0006913235824270196 -0.0032503789764821355; 0.0015515181208983846 -0.0001597769831825051 -0.0023986630594666682; 0.0007392662289714563 -0.005015840245425092 0.0002887366904637679; 0.008655345308839704 -0.01331774057169216 -0.010036825061386239] %
+
+Mass Used: 108.65734380370623 kg
+Launch C3: 94.35989047299718 km²/s²
+||V∞_in||: 1.3967995950360675e-8 km/s
diff --git a/archive/ES_0.5649382019635835 b/archive/ES_0.5649382019635835
new file mode 100644
index 0000000..dd301c1
--- /dev/null
+++ b/archive/ES_0.5649382019635835
@@ -0,0 +1,22 @@
+archive/ES_0.5649382019635835---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T01:04:39.579
+Launch V∞: [6.6096196877984275, -7.449999618547184, 0.2601261340931027] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.517222554140898e-6, 1.2462029892680306e-6, -2.7204666511545164e-8] km/s
+ V∞_out: [-1.9004681205056774e-6, 4.194123268870458e-8, 9.400642391995123e-6] km/s
+ time of flight: 1.874957778738466e8 seconds
+ arrival date: 2029-04-11T03:14:16.579
+ thrust profile: [0.11701891957651224 -0.030849719406990113 -0.045999752557201984; 0.09440892402537521 0.02205939620141003 -0.11052760680260625; 0.04239133502401302 0.019063091044564513 -0.08737210972039364; 0.04277468416901339 0.02579996511075612 -0.12747336548522217; 0.023606809024168625 0.016850256630242953 -0.08553108205172728; 0.017424745845912352 0.013389454791306907 -0.07775109073995445; 0.0232883177878403 0.020604657248633786 -0.12031626117616478; 0.012557053145447665 0.011823851595699807 -0.07264106981597344; 0.01011708317742759 0.010049451079236757 -0.06881560524661957; 0.0050020781277937175 0.004804904980139032 -0.033570537338009146; 0.0021444855007107287 0.002275457935434795 -0.018577699331470306; 0.0035724165983950554 0.004179942864005417 -0.030936144135187117; -0.002481875830124698 -0.00231343148353213 -0.0025667971381392227; -0.0008495833521308858 -0.0015915028275261744 0.0027174064536130173; -0.0005774251031085956 -0.002207851629890516 0.0009911098832330574; 0.00037147967968280914 0.0051621685132791665 -0.005108640881582679; 0.0013309442286126311 0.0017314727405049134 0.0024029988220898384; -0.0017824047571209452 -0.0007708144311144303 0.005321357872492192; -0.0006122369167533801 -0.00015607222569267017 0.006286012228759765; -6.465321618171391e-5 -0.0030363163674330825 -0.0004233804624969675] %
+
+Mass Used: 80.09404697812397 kg
+Launch C3: 99.257232339324 km²/s²
+||V∞_in||: 9.598504421491339e-6 km/s
diff --git a/archive/ES_0.5649528006928507 b/archive/ES_0.5649528006928507
new file mode 100644
index 0000000..8d15e89
--- /dev/null
+++ b/archive/ES_0.5649528006928507
@@ -0,0 +1,22 @@
+archive/ES_0.5649528006928507---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T05:24:29.638
+Launch V∞: [6.251556614691675, -7.416491997215271, 0.2943917170555047] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00035530058980274827, 0.0007787468932770934, 0.0003429728370542461] km/s
+ V∞_out: [-0.0006300718856210496, -0.000313674939372629, 0.0005927135550628344] km/s
+ time of flight: 1.813183507941962e8 seconds
+ arrival date: 2029-01-24T19:36:59.638
+ thrust profile: [0.5227054604150171 -0.147089354223581 -0.15982839889717063; 0.0393622149994536 0.010753994841915436 -0.039707614690429896; 0.07419040065573082 0.03613107692687628 -0.11838591138779286; 0.07194266352642646 0.05286827151504289 -0.15851635801045313; 0.049615143331192775 0.04550335047170232 -0.1412864995782793; 0.020362902044798174 0.02135758890552567 -0.07277318679397123; 0.02550271733751843 0.030482954909565006 -0.1052813265347785; 0.015616762266739668 0.020406890280732976 -0.07588275848043402; 0.008650765563384712 0.012389961462204868 -0.04789910559308079; 0.0024806051670209716 0.005153937915948467 -0.0199254464522268; 0.004163037584786772 0.0070095331775995775 -0.029535256592103015; 0.0009951701700198436 0.002142443923809189 -0.007358006321543408; 0.0016708978034876783 0.000989958394885176 -0.004559231661569239; 0.00019800370087833322 0.002235240356916519 -0.0025783960573703664; -0.0017172074027453355 -0.0005628617337571932 -0.0005053145536503575; 0.00039866370462461327 -0.00047231091126351656 -0.0027924660281375214; 0.0021830750703814177 -0.0021199230464230205 -0.0020604288192967004; 0.0022144080514164477 1.339291696775811e-5 0.0008589534970787252; -0.0020927799789992978 0.0037633424766333086 -0.0037433757120813277; 0.0002462623098071033 0.0022392948769729506 0.008999588391448812] %
+
+Mass Used: 109.76921669026751 kg
+Launch C3: 94.17298013452428 km²/s²
+||V∞_in||: 0.0009221255879000127 km/s
diff --git a/archive/ES_0.5649739287507354 b/archive/ES_0.5649739287507354
new file mode 100644
index 0000000..7005709
--- /dev/null
+++ b/archive/ES_0.5649739287507354
@@ -0,0 +1,22 @@
+archive/ES_0.5649739287507354---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T21:16:08.647
+Launch V∞: [6.411461335761406, -7.568985325398707, 0.06918502316857628] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.651348329159579e-5, -2.6672574051749596e-6, 4.635679163740376e-8] km/s
+ V∞_out: [2.9769705985006366e-6, -7.076945326365374e-8, -1.6458501305947475e-5] km/s
+ time of flight: 1.8091586647148558e8 seconds
+ arrival date: 2029-01-22T19:40:34.647
+ thrust profile: [0.17495583556701397 -0.056497993779295805 -0.06870590164762787; 0.041364233225096345 0.007169085666914793 -0.04773322248113163; 0.07046373252244725 0.027063293641808792 -0.13443146965038333; 0.06822954241187638 0.03552765258550465 -0.18045073402158893; 0.05384419658243569 0.03340172637057669 -0.18078866224963297; 0.031713310303641315 0.021983124357257012 -0.12849761243840835; 0.01590606706390204 0.01197115307715011 -0.07557350512607362; 0.008969900808243775 0.007431835923640739 -0.04805661773221759; 0.0041908271107752425 0.0033976059102427663 -0.023773364423465972; -0.0002551276118571353 0.0014453824426332626 -0.0054733052585968075; 0.0019664369096851187 -0.0009597864325185997 -0.008965260072693786; 0.004571594713067152 0.004379286219067217 -0.018370620354506276; -0.0011881339398491283 -0.0018566591087522046 -0.007519794276905157; 0.0011498670207315907 -0.0005343097199411543 -0.003988111442284354; 0.0010504046267704322 0.0007839502221415134 -0.0014429227527383388; -1.4549552450242656e-6 -0.00010369547492503669 -0.0010819589083934198; -0.014764739807444095 -0.010053165172237461 -0.01025185724454361; -0.000507193795344841 -0.0006934677242885128 -0.0013698127911298545; -1.8892267396203766e-5 0.00029018621122432634 -0.0007075975811953474; -0.0019138589742391657 -0.014099060414114926 -0.0160701086047969] %
+
+Mass Used: 85.12947255546896 kg
+Launch C3: 98.40116188349525 km²/s²
+||V∞_in||: 1.6727568306224455e-5 km/s
diff --git a/archive/ES_0.5649758604241615 b/archive/ES_0.5649758604241615
new file mode 100644
index 0000000..5522c42
--- /dev/null
+++ b/archive/ES_0.5649758604241615
@@ -0,0 +1,22 @@
+archive/ES_0.5649758604241615---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T23:19:56.862
+Launch V∞: [7.658586456642932, -6.334263607109908, -0.12336182226980773] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.771234172486328e-7, -1.2308954162216518e-6, -1.0904825821841566e-7] km/s
+ V∞_out: [9.287971273808616e-8, -4.173705404553611e-7, -1.3967344165120348e-6] km/s
+ time of flight: 1.7358509102548057e8 seconds
+ arrival date: 2029-11-14T01:24:47.862
+ thrust profile: [0.23251130568596212 -0.03161036354115077 -0.09671483496820396; 0.03319837924723464 0.011025021399404197 -0.042170664775398034; 0.03704510208016121 0.0198880683591785 -0.08608537572857804; 0.04125439625012474 0.027140241894943067 -0.12613174533748997; 0.02934768223109163 0.021851907951807917 -0.1186531055989969; 0.025511731835594343 0.019975800504915403 -0.1239163225853582; 0.016475381159799005 0.013929549764509741 -0.09321564075171722; 0.021002051295649606 0.018974128157077507 -0.1296399248383329; 0.008560855294980086 0.005421077937992954 -0.045805808161271624; 0.009826695434729932 0.0013251080114752057 -0.03012584951820756; 0.011330428776121448 -0.0023269398083880168 -0.02183477294457501; 0.0005180010936583681 0.001982591075175068 -0.0130670818572262; -0.001727361380968047 0.0015329550676332416 -0.011286297515402534; -0.001863524761270224 0.001907736911592162 -0.012532209272243187; -0.002189387741493899 0.0011276699364667674 0.0017153244171630574; -6.062198097990003e-5 0.0009556919947828952 -0.004349472444030798; 0.0005385641796195224 0.0013547959568582014 -0.003841321633084648; -0.006784905699084735 -0.0001449486389295718 -0.011049416287494339; 0.0044336881310706585 0.006420728437519903 0.0030067235650318353; 0.0011395610595313918 -0.0016977417748811462 -0.0038952256382242863] %
+
+Mass Used: 82.85148659320748 kg
+Launch C3: 98.7920600974253 km²/s²
+||V∞_in||: 1.4597656845987771e-6 km/s
diff --git a/archive/ES_0.56498520107397 b/archive/ES_0.56498520107397
new file mode 100644
index 0000000..6a06d8b
--- /dev/null
+++ b/archive/ES_0.56498520107397
@@ -0,0 +1,22 @@
+archive/ES_0.56498520107397---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T07:37:28.615
+Launch V∞: [6.512966447183749, -7.529784190265531, 0.1213231863446648] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.8289247028949225e-9, -2.1752244191495592e-10, -5.280838031362808e-9] km/s
+ V∞_out: [-1.640545565050262e-9, 3.4857958782550107e-9, 6.603127226263375e-9] km/s
+ time of flight: 1.840229308051466e8 seconds
+ arrival date: 2029-03-01T05:06:18.615
+ thrust profile: [0.14992136816133356 -0.04583445421945481 -0.05986600422383551; 0.03516512061290594 0.007252542429928207 -0.04293875872852836; 0.040836630960025634 0.015590121274778901 -0.08240101859320861; 0.047981483456487284 0.024136683443895898 -0.13339632457627768; 0.03624746696931526 0.02148199609129977 -0.1281083189469663; 0.0482091496823689 0.03213135708014498 -0.20298571765085394; 0.02241100141181613 0.015532625526063448 -0.11013939040436266; 0.010313926907834775 0.007514533842735619 -0.05906464490407857; 0.005568455876178624 0.00484596068812548 -0.03885226420338805; 0.0024509135313285006 -0.0011715858432510028 -0.003990098113448073; 6.898782315254142e-5 9.168715240274866e-5 0.000330130666508114; -0.0065675442915524495 0.0019085744070589084 0.0006219388785176725; 0.0005432088723461236 -0.00010148550896911458 0.0002308541514987316; -0.0021434905145370094 0.0026593239049190775 -0.009647776581319142; -0.002647944810112551 0.004913457435656368 -0.006624570226225772; -0.005817571604064518 0.005309392049022597 -0.02143305586076306; 0.006953899350708484 0.006107240110884676 -0.009825389379980357; -0.004071351007667396 -0.0023864927498856475 -0.00897757474290147; -0.0008346909527306432 0.0028563266903786507 -0.00196090279086862; -0.0002587587938652516 0.0016840468940560991 -0.001042754316278102] %
+
+Mass Used: 80.8846441966216 kg
+Launch C3: 99.13110120965887 km²/s²
+||V∞_in||: 7.868349859928898e-9 km/s
diff --git a/archive/ES_0.5649858273137778 b/archive/ES_0.5649858273137778
new file mode 100644
index 0000000..daad69c
--- /dev/null
+++ b/archive/ES_0.5649858273137778
@@ -0,0 +1,22 @@
+archive/ES_0.5649858273137778---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T08:25:49.041
+Launch V∞: [6.440204521866287, -7.419071634142184, 0.1490794650845293] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.429309703024685e-8, -1.4836128415854438e-7, -1.0903208762784763e-7] km/s
+ V∞_out: [4.96261667248457e-8, -1.0547483908233656e-7, 1.629845856921028e-7] km/s
+ time of flight: 1.8749577787484816e8 seconds
+ arrival date: 2029-04-10T10:35:26.041
+ thrust profile: [0.3537362567114553 -0.09064103600947147 -0.12454311000260981; 0.06722693677548233 0.01857932571317077 -0.07555280170881544; 0.034832656327532775 0.018104174254182256 -0.06742966798814072; 0.03553421289361439 0.025245017977667067 -0.09483818418009995; 0.025850972006214726 0.021865904816322487 -0.08941515086235964; 0.015128685182976387 0.01492033529014014 -0.06324829471820914; 0.022421012043409873 0.024423423749714 -0.10910273329309987; 0.008635635543866734 0.009775723470808573 -0.04481104466454197; 0.007179543440321019 0.009186494059906724 -0.04807344648039713; 0.02255524038304875 0.04061572292710043 -0.16179452379461975; 0.0027006374683510802 0.0037024347508604963 -0.02154604908047059; 0.0030994672284704945 0.004854109834638952 -0.026041263531110595; -0.0003506434855942889 7.109012295555459e-5 0.0005569678087439026; 0.000771923318444653 -0.001268046987377793 -0.007453876763936636; 0.0014165423002446957 1.1800008909922944e-5 0.00034388368894466685; -0.0017602450959095539 -0.004979525761707681 -0.0021753170643626935; 0.00032062981654728195 0.0019206000763099785 -2.4037344447707743e-5; 0.0006922928409327393 -0.0004696292547634424 -0.0039522959869980456; -5.770553273602491e-6 -0.0009710095067301996 2.6565446854171382e-5; -0.00043647817093615837 -0.0027270748137006528 0.00044458535874028135] %
+
+Mass Used: 95.99381504909888 kg
+Launch C3: 96.54108288291003 km²/s²
+||V∞_in||: 2.0685805499717565e-7 km/s
diff --git a/archive/ES_0.5649875966596176 b/archive/ES_0.5649875966596176
new file mode 100644
index 0000000..fc6a4b2
--- /dev/null
+++ b/archive/ES_0.5649875966596176
@@ -0,0 +1,22 @@
+archive/ES_0.5649875966596176---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T07:06:24.779
+Launch V∞: [6.337330865541133, -7.401408401002008, 0.11037608247751567] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005270403561990089, -7.569797849545376e-5, 0.0038758645575491645] km/s
+ V∞_out: [-0.00640682722602759, 5.0122141180805e-5, 0.0012690512116902825] km/s
+ time of flight: 1.8262285817928976e8 seconds
+ arrival date: 2029-02-08T23:40:42.779
+ thrust profile: [0.41212458021843584 -0.1120385829130914 -0.1318331236501116; 0.08101027801845193 0.022889595392674413 -0.07799780169744655; 0.09982652326446911 0.0550261022945213 -0.15659225654920272; 0.061406348376891795 0.046428324336112575 -0.13569316571833753; 0.06020444492060818 0.055649771436766436 -0.1686470570584496; 0.02333641789425545 0.025789806360527905 -0.08351637050039336; 0.01636789659753371 0.02050254876577602 -0.0701203888693675; 0.009428937798572961 0.013286911129351339 -0.04795142847408603; 0.0035050856112340805 0.005189620828680099 -0.022356101953003672; 0.0032368873721027487 0.005054156111007509 -0.020620421763222204; 0.0048295375944930235 0.009724551205006295 -0.0365598830972217; 0.001491329093863907 0.00021814689795472014 -0.006113897220043606; 0.000549577985170941 0.0009963123262926644 -0.0033045549754088365; 0.004235068412094174 0.0017261485226231401 -0.005052328976670441; -0.004360351914735886 0.003504519235492415 -0.0023881987452547973; 3.0401871870814907e-5 0.002122599228174664 -0.0036518036891508682; 0.0009407395146578313 0.0014610595572159095 -0.0055171165999573476; 0.0007167036930146216 0.0018490492682882043 -0.0045379557133567745; -0.0028611104012000585 0.0005835649982080525 -0.0031993823283324885; -0.007363450772670849 0.0017374875708317937 -0.000836329434872469] %
+
+Mass Used: 105.24924453503263 kg
+Launch C3: 94.9547916973465 km²/s²
+||V∞_in||: 0.0065425690641102065 km/s
diff --git a/archive/ES_0.5649893764474064 b/archive/ES_0.5649893764474064
new file mode 100644
index 0000000..9893bac
--- /dev/null
+++ b/archive/ES_0.5649893764474064
@@ -0,0 +1,22 @@
+archive/ES_0.5649893764474064---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T19:12:55.160
+Launch V∞: [6.661120508622595, -7.405109334641902, 0.16506698239825685] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9501578754088094e-8, -8.009385773518074e-9, 9.164570384363401e-9] km/s
+ V∞_out: [-3.0646994893590366e-8, 8.080082639220122e-9, -3.728814744940724e-9] km/s
+ time of flight: 1.8749577787474805e8 seconds
+ arrival date: 2029-04-10T21:22:32.160
+ thrust profile: [0.14340966122202128 -0.03981473279430603 -0.05695256473722992; 0.03719703221776387 0.007067129907696887 -0.04823268321678954; 0.04881073015075518 0.019273006653335607 -0.1045296442062382; 0.05344134008111393 0.029023541801939518 -0.15479419381187634; 0.03883288956432464 0.02432101401309659 -0.14572564609711808; 0.02624185163687574 0.017778764731898627 -0.12209123476020314; 0.015215437360756041 0.010554625003203394 -0.08272435082343714; 0.008120041401472879 0.006394927167871685 -0.0531052904264005; 0.005949410360828835 -0.002722603875423194 -0.027066335627197197; 0.005129418473238229 0.004091210612227796 -0.0028879138427922047; 0.005716717006454988 0.004644252676440997 -0.040373124681034836; 0.002921416588594176 -0.0008557001639503212 -0.00818507453820075; 0.0003465596800566091 0.007243923952325159 -0.00707189116256437; -0.008465974134506454 0.0017895143563788094 -0.002221596114022506; 0.003995066857456861 -0.001346988981765817 -0.011325850683639685; 0.0024899503814490367 0.006564458075081518 -0.004101046682404686; 0.0010822446462504455 -0.0007142938407743061 -0.0037277051705042925; -0.006726486956603428 0.006193076475894636 -0.00032983733347248956; 0.0034117172682305566 -0.005063530734892864 0.007931200150714898; 0.0012770473322452308 -0.006288881115562396 -0.0013761206908208127] %
+
+Mass Used: 80.29266870572519 kg
+Launch C3: 99.23341779707124 km²/s²
+||V∞_in||: 3.19136766885711e-8 km/s
diff --git a/archive/ES_0.564989900739262 b/archive/ES_0.564989900739262
new file mode 100644
index 0000000..b09b252
--- /dev/null
+++ b/archive/ES_0.564989900739262
@@ -0,0 +1,22 @@
+archive/ES_0.564989900739262---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T11:23:13.582
+Launch V∞: [6.176378225133139, -7.449936429497017, 0.10279612952006886] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.010673595958136294, 0.007280176020024945, 0.00993766003839575] km/s
+ V∞_out: [-0.006678820408316115, -0.012415720812056653, 0.008176595309769032] km/s
+ time of flight: 1.7748875376234782e8 seconds
+ arrival date: 2028-12-09T17:49:06.582
+ thrust profile: [0.5266205540939636 -0.16890356570960244 -0.17721376195748695; 0.07689486753781775 0.016638812077618366 -0.07574307004954033; 0.0813183747045281 0.038441221695511334 -0.13183517209681622; 0.10563700441658878 0.06963826782119487 -0.23512798724128983; 0.07793331252766918 0.06276612890203119 -0.22136586277662648; 0.026888792246506834 0.02481703133077929 -0.092633723172267; 0.012721841317785875 0.013414695715543122 -0.05167338510961802; 0.004431888506107393 0.004994089639065201 -0.02195310283545853; 0.0006098871051358925 0.0022233655867321305 -0.0036068961164443985; 0.0017823638821291006 0.0030839720903457534 -0.004594292739772847; 0.000542507124765855 0.001607204872642797 -0.007287969405032839; 0.003050446296397183 0.002743629999108902 -0.01468404322145576; 0.0003011942086210079 0.0005528896461539845 -0.0031362966856333463; -0.00026659536403369534 1.5035280395460046e-5 2.335597613635455e-5; 0.00027854403542778585 0.0010051908552046712 -0.004244471173675; -0.0016848492557399496 -0.000958504514011065 0.0031417572068394286; 0.0006760255937468911 -0.0003261280191923744 0.003048902983224665; 0.0012028982670649906 -0.0011504923045834296 -0.0023221927759414476; -0.006618490178175021 -0.0033628004451370236 0.0008306512104221588; -0.00024488781273577045 -0.0003183632625089474 0.0013470895708540902] %
+
+Mass Used: 112.80623853428142 kg
+Launch C3: 93.65976782768986 km²/s²
+||V∞_in||: 0.01629980676568951 km/s
diff --git a/archive/ES_0.5649993677791569 b/archive/ES_0.5649993677791569
new file mode 100644
index 0000000..01727e0
--- /dev/null
+++ b/archive/ES_0.5649993677791569
@@ -0,0 +1,22 @@
+archive/ES_0.5649993677791569---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:18:59.650
+Launch V∞: [6.4722128586833785, -7.460544763803478, 0.1644938781207167] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3205800007012575e-6, -1.016619889255317e-5, 6.244145067345765e-7] km/s
+ V∞_out: [-3.423646232608654e-6, 8.48190633016066e-6, -4.479428507892156e-6] km/s
+ time of flight: 1.85277901069458e8 seconds
+ arrival date: 2029-03-14T21:24:00.650
+ thrust profile: [0.23502533404337125 -0.06151659917633069 -0.08549444207147727; 0.08117965296469586 0.02064174226348926 -0.08912033952580195; 0.0530274234700449 0.02630575357113095 -0.09809213691653507; 0.056465074967024645 0.03689649008798416 -0.142473319405469; 0.026055469873626853 0.022629993996324958 -0.09108986959069529; 0.026465302884669993 0.023440568655138775 -0.10417031040645662; 0.023546821709833365 0.024538758153799047 -0.11337905326707068; 0.017596696095685597 0.01997677781261947 -0.09626546064123247; 0.004896446731036803 0.007698216789313378 -0.03825861178449919; 0.002372462026290099 0.0029344727764670695 -0.017569759565414615; -0.0007790084221549543 6.125571202966979e-5 -0.00038695970282146116; 0.003513048248268928 0.006556103505902695 -0.034250497889991315; -0.0005586864407480851 -4.5949354866048144e-5 0.0020971851454892614; 0.0002651464117637483 -0.0012461248493044093 -0.002841961855630633; 0.0001222520105071545 -0.007812162225377292 -0.00527617733402742; -0.001002938539419811 -0.0008027493009265104 -0.0006793153656005663; 0.0037768487665782754 0.008304514034558308 -0.004724582075489684; 0.0004205967615357618 5.018893931250172e-5 0.004027531828383031; -0.002947757074348219 -0.00849211818568079 0.0012105000406576404; -0.00657592730481044 0.005767187539014406 0.0021739636964388962] %
+
+Mass Used: 89.97069584457631 kg
+Launch C3: 97.57632569676116 km²/s²
+||V∞_in||: 1.02706097646353e-5 km/s
diff --git a/archive/ES_0.5650117562897803 b/archive/ES_0.5650117562897803
new file mode 100644
index 0000000..44cc459
--- /dev/null
+++ b/archive/ES_0.5650117562897803
@@ -0,0 +1,22 @@
+archive/ES_0.5650117562897803---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T13:34:54.684
+Launch V∞: [6.641857042051145, -7.342694412230446, 0.08892534612791025] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009778854831442814, -0.0002890292931707255, 0.006528362546980653] km/s
+ V∞_out: [-0.011277635792272424, 0.00010950620246591982, 0.003316412392858195] km/s
+ time of flight: 1.8749577787483868e8 seconds
+ arrival date: 2029-04-08T15:44:31.684
+ thrust profile: [0.17431680448760167 -0.04176441097203346 -0.05908544502195798; 0.069390986040397 0.01989811777418745 -0.0682670193420096; 0.07709908148464197 0.042737765959599126 -0.12810301640262436; 0.06457446722023936 0.04787536866037427 -0.14797163223358786; 0.056056068188067354 0.05028803711541609 -0.1625993427746123; 0.03576901518780513 0.03521073497442765 -0.1212153365827561; 0.012884158836863023 0.020001959945255658 -0.05823325938676115; 0.004071584372422746 0.00853843787885133 -0.029502082917042934; 0.00757170817587902 0.012218231212635058 -0.03938920483068942; 0.005750112268380684 0.004550189164889187 -0.01910662876357168; 0.0008476659161366694 -0.0010710740788114244 -0.010128564476232777; 0.0015105394900769109 0.003189710981956118 -0.012513452625592425; 0.003548145176426214 -0.0025567241919159382 -0.005185135907461184; -0.0004857953277653935 -0.0007916713105497622 0.0022870581635773763; 0.004438032759544429 0.003793003756042758 -0.0069279227515909175; -0.00688530035942535 0.0022260915985163852 0.0017006189050458014; 0.0034687100687843357 -0.00433788663596487 -0.011519443419041743; 0.00817247572642714 0.0029896246900799357 -0.009042444590233392; -0.002793238910097407 0.0018084797433586314 -0.00840361478635135; -0.0016490261970687464 -0.0034482674390600068 0.006166256108593031] %
+
+Mass Used: 87.29593449691038 kg
+Launch C3: 98.03733391562857 km²/s²
+||V∞_in||: 0.011761337393832512 km/s
diff --git a/archive/ES_0.5650147869427633 b/archive/ES_0.5650147869427633
new file mode 100644
index 0000000..9db17a6
--- /dev/null
+++ b/archive/ES_0.5650147869427633
@@ -0,0 +1,22 @@
+archive/ES_0.5650147869427633---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T19:55:39.532
+Launch V∞: [6.57753176701597, -7.483624851512429, 0.12318485592721592] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.218344431981063e-7, -8.009146579371746e-7, -6.338725196734886e-7] km/s
+ V∞_out: [-9.900248709026051e-7, -6.917683288995774e-7, -2.2514725346856367e-8] km/s
+ time of flight: 1.874957778744363e8 seconds
+ arrival date: 2029-04-11T22:05:16.532
+ thrust profile: [0.1466076792820573 -0.040704333587612045 -0.060569283738679855; 0.05355519607605975 0.010665685542602273 -0.06817349288122994; 0.0427339679099217 0.016751002794899925 -0.09167734348803402; 0.0415547153142672 0.02133611220471035 -0.12449288155914431; 0.03374700057779464 0.02012702505840387 -0.1286847189737962; 0.0237751877512583 0.015590982307579571 -0.10919692909728028; 0.01458999042287748 0.011021957892450682 -0.08045067803539219; 0.009555784881660435 0.007317118382455977 -0.05874477384500667; 0.016182294727305854 0.013297181475333895 -0.10631454883668363; 0.0011912966487678295 -0.0004860928028010739 -0.011291158130325336; 0.0039972684320093805 -0.0002112820659760184 -0.020500992260375973; 0.0016747598933097416 0.0015540848130302452 -0.009436040004106708; -0.0015464581220848033 -0.003585299656482109 -0.00023104090049353657; 0.0021263125690274666 -0.0005544060669731252 -0.006595933084005001; -0.0009095698695230419 0.0011538725066452165 0.001747797879315251; 5.745044008347073e-5 0.002837741761942316 0.001708129573068293; -0.00026936888120573466 0.0024684970529030544 -0.0007659618108274858; 0.0038870347243980946 0.002934182674877647 0.0005849035438493071; -0.007251240081819549 -0.0029163710608382317 0.00614733605459821; 0.004612768661627021 -0.00646599259074274 -0.007945720100960781] %
+
+Mass Used: 80.02877059067441 kg
+Launch C3: 99.28373957300848 km²/s²
+||V∞_in||: 1.1957996216939265e-6 km/s
diff --git a/archive/ES_0.5650149064125383 b/archive/ES_0.5650149064125383
new file mode 100644
index 0000000..387e107
--- /dev/null
+++ b/archive/ES_0.5650149064125383
@@ -0,0 +1,22 @@
+archive/ES_0.5650149064125383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:45:16.161
+Launch V∞: [6.190227716569008, -7.71603414699837, 0.30521427970882586] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.274033716669503e-7, 2.05236676733113e-7, 1.4123155018787136e-7] km/s
+ V∞_out: [-6.280265014782793e-8, 1.4288793933324046e-7, -2.1361974403848182e-7] km/s
+ time of flight: 1.794324941636908e8 seconds
+ arrival date: 2029-01-06T06:06:50.161
+ thrust profile: [0.21494149623994052 -0.06457020722696193 -0.07747924095625183; 0.06162636569506552 0.012462957290898118 -0.06695320159965874; 0.058636738905804425 0.025521872139777756 -0.10418449385191293; 0.06172280075021344 0.03687521765874508 -0.15044698226117226; 0.055348642428883335 0.040080693638642105 -0.1707996856261092; 0.0388276644826461 0.032118160902407926 -0.14521485673398013; 0.012655462372266025 0.011253106781434619 -0.057456825203211305; 0.016434312044404095 0.01570439014966481 -0.08223707476070367; 0.0077903944565699615 0.008009652411308965 -0.04491929302533417; 0.007371208539397635 0.00775722618273158 -0.04577066217506785; 0.0005872648790011368 0.0014080729405635244 -0.005525669016495476; 0.000341903222720337 0.001168643640732762 -0.0025255270327846644; 0.001462612319959601 0.00012917234942958584 -0.0057736489415050295; 0.0007123120680289237 0.0002324898598350146 -0.002139506932713628; 0.0010258550511870518 0.0011741028117508167 -0.0015463511168584939; 0.001546660273098825 -0.001407355810907072 -1.5252879301146539e-5; 0.0027573574731431477 0.0006997015439413569 -0.0010676608672826702; 0.00016058410528525295 0.0010610232594078003 -0.0008123495177867861; 0.0008856984765059217 0.003801687114449087 -0.00427771931872145; -0.0017537876028474793 0.0019263298701289251 0.0021404202011743] %
+
+Mass Used: 87.81338641451521 kg
+Launch C3: 97.9492578971622 km²/s²
+||V∞_in||: 2.798214848024158e-7 km/s
diff --git a/archive/ES_0.5650181627923483 b/archive/ES_0.5650181627923483
new file mode 100644
index 0000000..58fbfea
--- /dev/null
+++ b/archive/ES_0.5650181627923483
@@ -0,0 +1,22 @@
+archive/ES_0.5650181627923483---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T10:50:24.380
+Launch V∞: [6.574866840780801, -7.224515501759259, 0.2704262869247684] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.933504388699276e-9, -3.1364121178884903e-10, -4.477842976998156e-9] km/s
+ V∞_out: [-1.5088479570240401e-9, 3.7020565848661687e-9, 5.157338615193128e-9] km/s
+ time of flight: 1.8749577787483093e8 seconds
+ arrival date: 2029-04-06T13:00:01.380
+ thrust profile: [0.39116576649878865 -0.08555904263086941 -0.10772117803930877; 0.11847832782585442 0.04231994778342303 -0.11404157247390777; 0.062192603558757116 0.04014867212062704 -0.10151198837766913; 0.05625036882482535 0.05078644731198627 -0.13035183276142503; 0.026130425323104632 0.027988747788732022 -0.07869145984458494; 0.025486109964586917 0.03220725039064821 -0.09220825161927375; 0.022820881034040612 0.032843483075101834 -0.09494578920873539; 0.019625355192573746 0.032993106198274814 -0.09855031817205176; 0.007882268185644095 0.012271445860893933 -0.042253991333747416; 0.00272068331804105 0.0048029028690182414 -0.01612655773023752; 0.0027877140324035826 0.0038889835829428562 -0.015664144716482167; -0.00025093943325978996 0.0010897044346278586 -0.0030745900737698248; -0.0003035774320789375 0.0007194072343719606 -0.0018822977063961618; 0.0005641748981616485 -0.0002810271619128038 -0.0029046118329118737; 0.000737880287477297 7.304088377463867e-5 -0.002803873455616865; 0.0012579349016296616 -0.001080315908092524 -0.00390958088507683; -0.000894187001219134 0.0003979962354900984 -0.0010483470142937624; 0.00018508850947532773 -0.00019104093969653777 -0.0006081758385834907; -0.0009965600453910057 -0.002026728008175047 0.006583940809659274; -0.0011854258252952722 -0.0033262562888361795 0.006303795154940753] %
+
+Mass Used: 102.13002317379733 kg
+Launch C3: 95.49562858581868 km²/s²
+||V∞_in||: 6.6700010561992495e-9 km/s
diff --git a/archive/ES_0.5650244724103487 b/archive/ES_0.5650244724103487
new file mode 100644
index 0000000..65b27b5
--- /dev/null
+++ b/archive/ES_0.5650244724103487
@@ -0,0 +1,22 @@
+archive/ES_0.5650244724103487---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T10:03:20.587
+Launch V∞: [7.630880729156872, -6.149514119819654, 0.0416554831910075] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.098293891261728e-6, 1.531672612237194e-5, 1.522770456236775e-6] km/s
+ V∞_out: [-1.175108936558874e-6, 4.284990104946428e-6, 1.594839597182637e-5] km/s
+ time of flight: 1.736441713671114e8 seconds
+ arrival date: 2029-11-10T04:32:51.587
+ thrust profile: [0.24351907260592748 -0.01674161759183629 -0.07592465508710432; 0.16745494872823308 0.08477052106046526 -0.16284611558614667; 0.10167549109718788 0.0872445680902561 -0.17553249591360012; 0.06586198095332411 0.07570251042789743 -0.16721386269162794; 0.041475315950597294 0.0589845942496878 -0.14194671522480884; 0.0234723727970407 0.0390145812154166 -0.10214370230942141; 0.009831596404558222 0.018671203760751133 -0.052733842336997155; 0.00433768188011584 0.01051483703195945 -0.027177060064020084; 0.002551339327075937 0.006439964830455514 -0.02138695954119048; 0.0037923898665298368 0.0049038353868297215 -0.00753449174722439; 0.0005084719397712979 0.0017051902149774643 -0.0013343490139224399; 0.002370200707358288 0.004355538480934563 -0.0045650149125556275; 0.0009046185217982504 0.0053368984812262946 -0.009611382008554055; -0.003942729814993649 -0.011595271733093057 -0.009295433966319419; 0.0010695570049902865 -0.0008238468208495207 -0.005528125245234598; -0.000423945089675614 -0.0002009460743545231 0.00411335367697711; -0.0074159955396156255 0.004450398522157337 -0.033198796439014126; -0.007318781137178675 -0.008341501088021997 -0.0035391455873530478; 0.0007642061499918314 -0.00291586330688019 0.013716796477245548; -0.0026430649758819634 -0.0014274185296255372 0.015552903742779497] %
+
+Mass Used: 98.91171902681344 kg
+Launch C3: 96.04859979175887 km²/s²
+||V∞_in||: 1.6556271239453002e-5 km/s
diff --git a/archive/ES_0.5650369948685505 b/archive/ES_0.5650369948685505
new file mode 100644
index 0000000..b4c25d2
--- /dev/null
+++ b/archive/ES_0.5650369948685505
@@ -0,0 +1,22 @@
+archive/ES_0.5650369948685505---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T18:40:25.509
+Launch V∞: [6.318112695562761, -7.416011826026132, 0.08249962417051042] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.798658780506725e-9, 5.722134370928869e-10, -7.763011678874065e-9] km/s
+ V∞_out: [-3.4202795312302354e-9, 7.882000349013734e-9, 1.0993964741876162e-8] km/s
+ time of flight: 1.851938431646379e8 seconds
+ arrival date: 2029-03-12T05:24:28.509
+ thrust profile: [0.39549638798271536 -0.09541495757290461 -0.12292877883271035; 0.14330085217590544 0.04414871258599085 -0.134259218950064; 0.06429698177826984 0.03772148258280126 -0.105856478827521; 0.044768253785162006 0.03552885138405608 -0.10357788859968979; 0.040924493366888935 0.04012215745849202 -0.1212219268391148; 0.03129183756748431 0.035537859122511936 -0.11363813104899845; 0.01583265665463817 0.01793303965185706 -0.06584630651603873; 0.007010299569101084 0.008991604183148228 -0.038007641822949974; 0.0030945551131633625 0.010619550967604884 -0.019502488499015546; 0.01328397878982288 0.026186630533375426 -0.09456836006096195; -0.0017887694938263084 0.0074792123227284315 -0.010376081438002834; 0.0012812708610097537 -0.0003788758489514989 -0.0016212187774414463; -0.0007309478864922271 0.001749156266948802 -0.0033751587527431712; -0.00392568707373798 0.009011217562593425 -0.01816003093327334; 0.0008260125331666072 0.00048221375128231197 -0.006707638663870049; 0.002638739729556236 0.0021708607181456147 -0.00595738146520554; 0.0021389906991137668 -0.0011748850014523197 -0.00041741985475289393; 0.0025755142074892733 0.0005657880562727517 -0.0029742114502826064; 0.0005079217122900942 0.001890462123098729 -0.005330307322439701; -0.002231796394899017 -0.0013410759980176867 -0.0011533861715089645] %
+
+Mass Used: 105.49474453076436 kg
+Launch C3: 94.92258562557906 km²/s²
+||V∞_in||: 1.1747688065305144e-8 km/s
diff --git a/archive/ES_0.5650456574285904 b/archive/ES_0.5650456574285904
new file mode 100644
index 0000000..893bc54
--- /dev/null
+++ b/archive/ES_0.5650456574285904
@@ -0,0 +1,22 @@
+archive/ES_0.5650456574285904---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:02:31.338
+Launch V∞: [6.667487228488288, -7.338524008032058, 0.11740103072873904] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012672141818451054, 0.001375814026976321, 0.0012299555658711284] km/s
+ V∞_out: [-0.0014857164355432213, -0.0007153142298915137, 0.001513796296706377] km/s
+ time of flight: 1.8749577787495387e8 seconds
+ arrival date: 2029-04-09T02:12:08.338
+ thrust profile: [0.17801208368847354 -0.043708446043339885 -0.06028639704347576; 0.07250239658471729 0.02006086968019777 -0.07400216260994695; 0.06570082348027224 0.035990885698882716 -0.1151839596072272; 0.02895828419291181 0.02153521179943868 -0.07300709581278823; 0.04011244566683127 0.03450532772119104 -0.1276912270893621; 0.02902281833210338 0.03034437977112914 -0.10877904842650665; 0.01864841668031113 0.020367225350560948 -0.08057353421971312; 0.021796842187314168 0.0265946826605483 -0.1125806518123119; 0.00654994026393413 0.009512259497230266 -0.04250709472933224; 0.004615296126543023 0.007739570580991154 -0.03494137745186765; 0.0028739645346859957 0.004894563855182603 -0.023173509238867997; 0.00021751992132730568 0.0005871173668350375 -0.010071938546932007; -0.003724267076449035 -0.00011514397046160545 -0.0015444636872274614; 0.0032467756938432627 -0.003715672531485351 -0.004273415044583442; 0.001917767195636724 -0.0015792247614838063 -0.006802690332650187; 0.003499398468423601 0.0019594676586240233 -0.005119019977717921; -0.005053388037546004 0.00550181251142383 -0.003583819710416934; 0.0062792730502847175 0.0038573889040822854 -0.012042377452905793; 0.0030431717167542995 0.005615053542820334 0.003267651699390989; 0.0017620392000226438 0.0029289592838739552 0.0028659299774766176] %
+
+Mass Used: 85.66849623024336 kg
+Launch C3: 98.3231035605335 km²/s²
+||V∞_in||: 0.002238635011231516 km/s
diff --git a/archive/ES_0.5650666794698552 b/archive/ES_0.5650666794698552
new file mode 100644
index 0000000..5d49fba
--- /dev/null
+++ b/archive/ES_0.5650666794698552
@@ -0,0 +1,22 @@
+archive/ES_0.5650666794698552---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T14:30:19.284
+Launch V∞: [6.356860855133272, -7.653445997386996, 0.06799690016309733] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8140720029529367e-7, -1.6501938086078813e-7, -2.610390911116311e-7] km/s
+ V∞_out: [1.7871701328603338e-7, -2.5285731538349486e-7, 2.813226547009918e-7] km/s
+ time of flight: 1.757502625192196e8 seconds
+ arrival date: 2028-11-22T18:01:21.284
+ thrust profile: [0.1231990969163212 -0.04877031500744722 -0.05148505035995062; 0.06663447739602221 0.006003947897946524 -0.0803909510841471; 0.06012332807832143 0.016817680079496 -0.1206313034371558; 0.05444976957283388 0.021192390041155834 -0.15088005428322185; 0.04540757100183072 0.020986285190758323 -0.15868722809060082; 0.03557542861914702 0.018230484311863866 -0.14860817831350873; 0.026002157006792523 0.014231243772506782 -0.12528074538308995; 0.016588897248140076 0.00957379303623603 -0.09078982312507085; 0.007938061982159376 0.004957370544890645 -0.049503724583980314; 0.000521068087381307 0.00039457608907385436 -0.0038297890880703506; 0.001479406432562097 -0.0001432336670067339 -0.006432110208539765; -0.0007274727782112421 0.00040501622828905017 0.001480381811151576; 0.0005896748300932455 0.0005426590468777064 -0.002364827011111869; 0.0008432846078494173 -0.000582314288192365 -0.0005447103397597537; -0.0004356207877416467 -1.5724370026228835e-5 0.002247642797962613; 0.0007956435459697435 -0.000828313403677365 0.0015401240188945818; -0.0008006063801935406 -0.0003472891820123416 0.0061860646180927565; 0.0027079092392907063 0.000164761348839831 -0.0008941773165221122; 0.00038363945258133533 -0.0003973365484923677 -0.0005340286943142977; 0.0003599471225952528 0.0005407293449455145 0.002383106427132229] %
+
+Mass Used: 81.80548103638466 kg
+Launch C3: 98.98953914487653 km²/s²
+||V∞_in||: 4.1780715111891013e-7 km/s
diff --git a/archive/ES_0.5650781662032586 b/archive/ES_0.5650781662032586
new file mode 100644
index 0000000..21d2d9e
--- /dev/null
+++ b/archive/ES_0.5650781662032586
@@ -0,0 +1,22 @@
+archive/ES_0.5650781662032586---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T02:45:02.449
+Launch V∞: [7.928043852574249, -5.622994906257982, 0.0357971623289443] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005321946071849566, -0.0033435899590950917, -0.00024041544762180421] km/s
+ V∞_out: [0.004492808733028205, 0.0025590641574841826, -0.003562323209494654] km/s
+ time of flight: 1.874957778463295e8 seconds
+ arrival date: 2030-04-22T04:54:39.449
+ thrust profile: [0.4708548269630896 -0.0054470198619729895 -0.1481910974150751; 0.11349969238501122 0.06281179658775157 -0.12302923745592007; 0.05156283257464463 0.04498820300964499 -0.09988173122548244; 0.04036870079503506 0.04607820783346643 -0.11662799537264913; 0.03875737063704942 0.05493490280592113 -0.1530209243033341; 0.012566893444458029 0.01907717818201759 -0.05820200618390989; 0.0066475372144261385 0.011271480880560047 -0.03541280914583453; 0.003880723897126014 0.00712262866618659 -0.022680728271612653; 0.005841243500730384 -0.00015534355308830625 -0.006839444087138884; -0.0071023195345306135 0.010156799925970053 -0.027162124803936354; 0.002227364110684607 -0.0014471413210276473 -0.005701240865537776; 0.0035554986417684308 0.007218184208669372 -0.026270795096963524; 0.009252503180678065 0.0005083311569297393 -0.006959116909841146; -0.0005298453156903923 -0.0004387159566861063 -0.0010181847081863937; -0.009942974317088581 0.0006031392791276478 -0.0031033063870927412; 0.0006941786152723379 0.016864074888007036 -0.012854565044046437; -0.00020027652830956064 0.0009129902561535346 0.0010035041416509302; -0.015441564772029775 0.043280961479699336 -0.035248164745347706; 0.004250917853667615 0.02973725017522875 -0.030219675894351886; 0.009198014488014293 0.00825807958023961 -0.004146160591249269] %
+
+Mass Used: 108.1640044314513 kg
+Launch C3: 94.47323248097436 km²/s²
+||V∞_in||: 0.006289714094749596 km/s
diff --git a/archive/ES_0.5650807610592214 b/archive/ES_0.5650807610592214
new file mode 100644
index 0000000..deede45
--- /dev/null
+++ b/archive/ES_0.5650807610592214
@@ -0,0 +1,22 @@
+archive/ES_0.5650807610592214---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T15:15:54.023
+Launch V∞: [6.350191917718392, -7.2837290804480235, 0.13452950466861843] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5541043844983579e-7, -4.0972097634960057e-8, 5.065229572904853e-8] km/s
+ V∞_out: [-1.6070814600663575e-7, 4.071311798547813e-8, -1.961352696231519e-8] km/s
+ time of flight: 1.8749577789452428e8 seconds
+ arrival date: 2029-04-07T17:25:31.023
+ thrust profile: [0.557646054495088 -0.12475629307983925 -0.16979073440403297; 0.10198528254263363 0.03196477220713478 -0.10161144104340583; 0.07355732949709978 0.04374825407538247 -0.12345843856824365; 0.04271194832992093 0.033922341490374916 -0.09963272597889922; 0.04047443173955626 0.039873429668803834 -0.12333671092615615; 0.02775322337392861 0.03170132849820704 -0.1021639203679535; 0.018766389360416705 0.026501836665622214 -0.08887907088857729; 0.009249830902569785 0.01304717873217968 -0.04671920443586917; 0.004930460254211906 0.007817506123313644 -0.026075501364508168; 0.0015438403208704017 -0.0006874961177871363 -0.0208260731965063; 0.0013946139515530224 0.0027228091930811826 -0.011670342479701465; 0.0005455134112857943 2.873826999891119e-6 -0.007358643063170538; -0.009243176473021732 -0.00041055207487782075 -0.007959061804348192; 0.0017136494270487941 0.0035784071169426756 -0.01038241180634688; -0.0004988494669186689 0.0008277529067173676 -0.0036075759661808953; 0.0009293103678934475 0.0023848004398881635 -0.01053925146616962; 0.0005460438351386735 0.001498233805564038 -0.008005877539784293; 0.006788763091609666 -0.010283228528819471 -0.0008973212949514075; 0.0029106221505946924 -0.0010183089669653137 0.00026463623080529844; -0.00313714296492413 0.0007192402617236092 0.00479215417290877] %
+
+Mass Used: 114.4523760041534 kg
+Launch C3: 93.39574489684657 km²/s²
+||V∞_in||: 1.6851341853514777e-7 km/s
diff --git a/archive/ES_0.565094205627817 b/archive/ES_0.565094205627817
new file mode 100644
index 0000000..2e1dd5b
--- /dev/null
+++ b/archive/ES_0.565094205627817
@@ -0,0 +1,22 @@
+archive/ES_0.565094205627817---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T13:03:43.351
+Launch V∞: [6.380355991180289, -7.455129615662278, 0.037422350270549354] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.059170860164548e-8, 2.905409834980731e-8, 1.974622821548479e-8] km/s
+ V∞_out: [-7.077825937528994e-9, 1.5305991405192274e-8, -2.416967863453237e-8] km/s
+ time of flight: 1.8533608173980203e8 seconds
+ arrival date: 2029-03-14T15:18:24.351
+ thrust profile: [0.3186255451329666 -0.07345046566855712 -0.09954832761141183; 0.06734479579707271 0.02120594346275435 -0.06778959244570172; 0.08131258556821198 0.049851167602393234 -0.1301303706782677; 0.04632914098917851 0.03810807742292259 -0.1041334946744305; 0.04587862331213575 0.04613458000212838 -0.13157754785758097; 0.028341703316519293 0.034634925159221015 -0.1049299796260435; 0.011893998704083822 0.016807307325396616 -0.05183341934458627; 0.023454215866240736 0.037451986982567735 -0.11992067284081152; 0.009769206371938515 0.010749486300764532 -0.05147357877209012; 0.003915996893170594 0.004084511407586074 -0.017416274315291122; 0.001959364264215399 0.003963064800869635 -0.018620128073267146; 0.001250640180827245 0.003454027667842862 -0.01853906634631924; 0.0005645230328146188 0.001150641203113245 -0.002118778943941857; -0.0008688422698656307 -0.003256837601570291 0.0024801793800532856; -0.00020640002474880178 -0.0002704313558544269 -0.0005044644396605749; -0.005006518309910334 0.0033280057230305037 -0.0011073106828119392; 0.004207786198955501 0.002300324501006692 -0.012965181069047125; -0.0037791127999103192 0.0033506363184766562 -0.007422150702231801; -0.005909116762034171 0.0011346748292154812 -0.0020801385974090255; 0.00042163364856929216 0.004321200165387301 0.0001053759449182231] %
+
+Mass Used: 97.58898644103374 kg
+Launch C3: 96.28930059281477 km²/s²
+||V∞_in||: 4.071943789878937e-8 km/s
diff --git a/archive/ES_0.5651009649882082 b/archive/ES_0.5651009649882082
new file mode 100644
index 0000000..5b1a385
--- /dev/null
+++ b/archive/ES_0.5651009649882082
@@ -0,0 +1,22 @@
+archive/ES_0.5651009649882082---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T16:51:11.008
+Launch V∞: [6.422615943502143, -7.3747695444857415, 0.1237238783380335] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.504039859331903e-8, -9.935969931450627e-9, 2.95883555519686e-8] km/s
+ V∞_out: [1.0328938744562901e-8, -2.274897641892489e-8, -3.1390937218661624e-8] km/s
+ time of flight: 1.8516844489667824e8 seconds
+ arrival date: 2029-03-11T20:31:55.008
+ thrust profile: [0.3780817139809952 -0.09275631708056734 -0.12723436550979336; 0.09700606627861467 0.03244010648251216 -0.10604389425715183; 0.06207003111950564 0.03938278619328009 -0.11406899587719901; 0.04450773342672317 0.03940102475940336 -0.11474348361656284; 0.02854282639205312 0.03083546663887865 -0.09697565979248139; 0.02764666802927481 0.03409555014163457 -0.1170755232845725; 0.018065124930104717 0.02261425830324574 -0.0810749381347796; 0.00831650355047584 0.013229287083079582 -0.053468090752630794; 0.0073374919868144685 0.008298924271033622 -0.04337435126067866; 0.004531267780018479 0.007369975105822554 -0.03700194048198947; 0.005730891529846207 0.011023753810788515 -0.045365880843576976; 0.004011962561743476 0.002764740946914648 -0.01990502736130955; -0.0021501901801135427 -0.00030682257765235607 0.000178610259083941; -0.0005313244578625151 -0.0002367014966909734 0.0018834359411004792; 0.0011013988175761712 0.00031617915731225625 0.001458664869117316; -0.0053760026654357685 0.0016430591515877906 0.001987015741347928; -0.0024105729841906024 0.0010021064804995746 0.0009328790718816959; 0.003821055769243689 -0.0007472429616038895 -0.002559776316361346; 0.0031756745269075045 0.0012646438928805345 0.003869858478107161; 0.003451935229023955 0.00025943535797806074 -0.003393284242691668] %
+
+Mass Used: 101.31137337748169 kg
+Launch C3: 95.65252899007335 km²/s²
+||V∞_in||: 4.001519516959396e-8 km/s
diff --git a/archive/ES_0.5651010299076125 b/archive/ES_0.5651010299076125
new file mode 100644
index 0000000..83415bf
--- /dev/null
+++ b/archive/ES_0.5651010299076125
@@ -0,0 +1,22 @@
+archive/ES_0.5651010299076125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T05:43:53.443
+Launch V∞: [6.263748991810774, -7.603533865246449, 0.038087083752152015] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008583264911781864, -0.0041249868938763, 0.009700960393554794] km/s
+ V∞_out: [-0.008831307596558289, -0.003479949508213905, -0.009725339546325986] km/s
+ time of flight: 1.7942325845982322e8 seconds
+ arrival date: 2029-01-04T21:31:31.443
+ thrust profile: [0.23143922945143086 -0.07781989796532 -0.09170524822297348; 0.1174776211937703 0.019378175066045326 -0.13614117384572885; 0.09792439462909895 0.03717058633898747 -0.18857330331741562; 0.042962280280084524 0.02237380365402549 -0.11595490685290684; 0.06312430528377688 0.03833825671502257 -0.2116755752166084; 0.025819793555066115 0.018335229622604678 -0.10700986917295806; 0.012247681585174537 0.009620385542357465 -0.05956901543338124; 0.008195584317793067 0.007038925671091582 -0.04551953080957299; 0.0021213345266072763 0.002259452235655476 -0.014601059995375898; 0.0016308821081963867 0.002216839387288742 -0.013464855864489167; -0.0003275956582837855 0.0008067973359730329 -0.0037622316251544044; -5.200918263610941e-5 -0.0012793186869381034 -0.001045484613414597; 0.00015245533068698898 -8.870191269766838e-5 -0.001535446242420531; 0.0004939429371169576 -0.0002775955865790508 0.001073222585473483; -0.0031746210345464697 -0.0038000444369147377 0.003182888296588705; 2.0350120704818245e-6 -0.0006079308197192072 0.0007429267449926699; 0.008057610745849602 -0.005753760433159467 0.007314413713181731; -0.00010640904204156691 -0.001889208706707924 0.0005220093191961655; -0.010742388780814346 0.0005055968260835311 0.010308032651012974; 0.0002648731549194221 -0.003787143996449454 -0.00010414496221421545] %
+
+Mass Used: 93.16111398541307 kg
+Launch C3: 97.04972929830883 km²/s²
+||V∞_in||: 0.013593990803947006 km/s
diff --git a/archive/ES_0.5651018999576068 b/archive/ES_0.5651018999576068
new file mode 100644
index 0000000..52d9aa3
--- /dev/null
+++ b/archive/ES_0.5651018999576068
@@ -0,0 +1,22 @@
+archive/ES_0.5651018999576068---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T06:16:34.536
+Launch V∞: [6.477729493195538, -7.263350955100967, 0.14741297960757918] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0016542164053959937, 0.0019513300391190206, 0.0017476911869680456] km/s
+ V∞_out: [-0.0018499484744421012, -0.000988634815020832, 0.002279848647539352] km/s
+ time of flight: 1.8749577787506595e8 seconds
+ arrival date: 2029-04-07T08:26:11.536
+ thrust profile: [0.4526351251388091 -0.10877173810862792 -0.13587300894761867; 0.0780906414898752 0.023249925698847363 -0.07568954621166211; 0.06569374135417444 0.03793232157415433 -0.10770977679203446; 0.06999873958166054 0.056219333339342654 -0.1614129658533437; 0.0531586332416524 0.05186327090442374 -0.15923440811655107; 0.02452632281286743 0.026544949785938972 -0.08937372638794835; 0.011776211052897605 0.013454761969153529 -0.04945860609371328; 0.01335435858731326 0.017249380714841347 -0.06520211224961353; 0.003231322953243732 0.004156020355796067 -0.019894200923952523; 0.0017369357541843421 0.01802182600953636 -0.02016174144352089; -0.002291837508371916 0.006332565872904044 -0.003853373012686485; 0.0008614581273609852 -0.0014359880166971827 -0.0027134776177001664; 0.0007687228644631652 -0.0005492387607231623 -0.0005515160527090591; 0.002887192134282106 0.006138309272945388 -0.00974551487165329; 5.228626957759524e-5 -0.00015466751027305416 0.0004562181723435653; -0.0060122795222949214 0.005747507231309512 -0.020281336804567694; 0.004344788247132222 -0.004740903768744139 -0.0074227513527084146; 0.0015372168656422028 -0.002451124853022121 -0.002332117077683102; -0.00820547425611561 0.0003780511691810113 -0.011595604985993952; -0.00040298414191390717 -0.0001338546713919894 -0.00040209732528484726] %
+
+Mass Used: 106.64151703906828 kg
+Launch C3: 94.73897707053824 km²/s²
+||V∞_in||: 0.0030981519204931283 km/s
diff --git a/archive/ES_0.5651094991084779 b/archive/ES_0.5651094991084779
new file mode 100644
index 0000000..b1d0955
--- /dev/null
+++ b/archive/ES_0.5651094991084779
@@ -0,0 +1,22 @@
+archive/ES_0.5651094991084779---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T13:11:18.329
+Launch V∞: [6.563694276920465, -7.429648799428459, 0.12389098313620353] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007580726590065919, -0.0038623832513651674, 0.006467009161104326] km/s
+ V∞_out: [-0.005355700147546528, -0.0042150398580826035, -0.0032949475809121035] km/s
+ time of flight: 1.8476135487147242e8 seconds
+ arrival date: 2029-03-08T23:47:12.329
+ thrust profile: [0.23281532453810258 -0.0673457518582605 -0.08466956561772768; 0.022579235704255143 0.0053323243385549664 -0.027087484084846087; 0.028176413617177546 0.012497303022282405 -0.05774209793386501; 0.04514228010507822 0.02494285791014815 -0.121821561473602; 0.021346622247861463 0.014756975857085047 -0.0775221860011858; 0.044125466854905815 0.033210543570028485 -0.1744990261259997; 0.025732919654072366 0.022111685252006946 -0.12372686886869808; 0.016530098149125184 0.015648866637942908 -0.09404077823645535; 0.007804017520206809 0.007630964881265104 -0.0470967206186307; 0.007936262342654134 0.008228401910557992 -0.05702383510351195; 0.0006398144672438268 0.0006346139458017217 -0.010794960050462807; 0.0023899041076769502 0.0023453563273093756 -0.019249505880558772; -0.0003572526867825197 -0.00060706286426943 -0.0034129707440470674; 0.0001732751455177802 -0.00024050829101269827 -0.004908828796983856; 0.0014564110000766738 0.0045584995497529425 -0.0041485803222942865; 0.0034156179706123857 -0.00843728885966634 -0.0022268940685110377; -0.0042217139992164416 -0.0006178992492550089 0.004482620403277592; 9.117160051326186e-5 0.00022775538675758717 -0.0025245769761217444; -0.002079810011037234 -0.010236631324962182 -0.005236918694170137; -0.001667303873846106 -0.0018159027290742431 -0.0056484275276546475] %
+
+Mass Used: 85.89459084655118 kg
+Launch C3: 98.29711281942966 km²/s²
+||V∞_in||: 0.0075706595503012 km/s
diff --git a/archive/ES_0.5651175578325808 b/archive/ES_0.5651175578325808
new file mode 100644
index 0000000..0fdd3b8
--- /dev/null
+++ b/archive/ES_0.5651175578325808
@@ -0,0 +1,22 @@
+archive/ES_0.5651175578325808---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T02:59:59.685
+Launch V∞: [7.586236522823566, -5.657193498790375, 0.16486046370346588] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.899357571386206e-5, 0.00013580360687470054, 0.008082770309136825] km/s
+ V∞_out: [-0.007662694227725427, -0.00224719404562564, 0.001122572190230475] km/s
+ time of flight: 1.813714530742744e8 seconds
+ arrival date: 2030-02-05T07:57:32.685
+ thrust profile: [0.9293358387273518 -0.03382379588230857 -0.2302606351168464; 0.10034080970312685 0.05857221650510065 -0.09290822043583495; 0.07996600348240884 0.07853995046821337 -0.13086476946153025; 0.042128331982250515 0.056485389585628695 -0.1070779775374523; 0.023935065051491917 0.03749215724856755 -0.07684322744984831; 0.01716841649793876 0.03561295894944706 -0.07494067021875869; 0.027540268584522864 0.06744206925626206 -0.1528421433193967; 0.00617727064061887 0.013919626335546938 -0.03148605143016219; 0.0033954392663708157 0.009014380846886848 -0.02509591566652775; 0.0004572654817785364 0.0020150376114769475 -0.003953448964910932; 0.0005168220383685172 0.0022408436081077783 0.0011301825842264558; -0.0003594293926850044 0.0024923951577717745 -0.004309197628863441; -0.0007256632580528444 -0.0005847641279394652 -2.9266130655240113e-6; 0.00026442556209093244 0.0014122045219800753 -0.00942554685269488; 0.0013265407004376824 0.003201811371735041 0.00016591699360341862; -0.0004573574022511021 0.0018736615647339558 -0.004686977351492301; -0.017823705346157195 -0.003208442135809705 -0.01268432849823259; 0.010089507677290105 -0.009553482388184282 -0.014220734279138659; -0.0006299225173958217 0.0003824480325003223 -0.0010194326021712688; 0.0058268641144643245 -0.00043016009631621565 0.004129018814320442] %
+
+Mass Used: 136.7421400977646 kg
+Launch C3: 89.58200183547079 km²/s²
+||V∞_in||: 0.008084126343141818 km/s
diff --git a/archive/ES_0.5651221044887245 b/archive/ES_0.5651221044887245
new file mode 100644
index 0000000..aacd82a
--- /dev/null
+++ b/archive/ES_0.5651221044887245
@@ -0,0 +1,22 @@
+archive/ES_0.5651221044887245---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T01:35:14.407
+Launch V∞: [5.949869936616507, -7.423801053526834, 0.14409461593322828] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.71578275308649e-8, 6.387894760533811e-10, -1.704628757549856e-8] km/s
+ V∞_out: [-3.523712026741594e-9, 8.03290544043256e-9, 1.1148809516356289e-8] km/s
+ time of flight: 1.8387670275916797e8 seconds
+ arrival date: 2029-02-22T06:26:56.407
+ thrust profile: [0.6587307774673699 -0.15295398549136857 -0.14926064015043253; 0.18281193914564833 0.06762171914539357 -0.13714567017618223; 0.1589365760214345 0.11142808532859803 -0.19407708651588232; 0.04834201773989017 0.04542585924237356 -0.08732477655420483; 0.04575988305529003 0.05386540403928689 -0.1061642677640426; 0.059828947928379915 0.08359912832414715 -0.16546217762959148; 0.020185050126070365 0.03236026177548015 -0.07019189488676394; 0.010865040497320717 0.01976836369122399 -0.04509532152631128; 0.0014863311228067153 0.00401184892488157 -0.009968621193856598; 0.0007436265804084866 0.0017279568197853272 -0.00462032784632062; 0.00020803275764590375 0.00018370161895259782 -0.0005514581538435317; 0.00012837765636409594 -0.0001721386498372766 -0.00033081447509630065; -5.838862921114197e-5 0.0003417355332869635 -0.000652752685193672; 0.000718964385677799 7.657950778925554e-5 -0.00026241559310420724; -9.066567003658543e-5 0.00023855158860211316 0.0006053228247773396; -0.0003274098685548718 0.0003436661186100393 0.0005812626056891418; -0.0002591902183847715 0.000758158647138787 0.000983858667622364; -0.0003778803463607617 -0.00028894858214155634 0.001024199341101184; -0.00016159942027464116 0.00029641384997821307 -0.0005531723961681974; 0.0013119622846800491 0.00013096911640805243 -5.239364170009673e-5] %
+
+Mass Used: 131.19098588402858 kg
+Launch C3: 90.53453760333998 km²/s²
+||V∞_in||: 2.4194524539246866e-8 km/s
diff --git a/archive/ES_0.5651246214739835 b/archive/ES_0.5651246214739835
new file mode 100644
index 0000000..7ef92f6
--- /dev/null
+++ b/archive/ES_0.5651246214739835
@@ -0,0 +1,22 @@
+archive/ES_0.5651246214739835---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T03:11:45.616
+Launch V∞: [6.397211286362951, -7.618501280637881, -0.44999270791703305] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.009930652161201006, 0.00031317126262642554, -0.008754879415811908] km/s
+ V∞_out: [0.012750558407826691, -0.00013069490084715929, -0.0035826534516818272] km/s
+ time of flight: 1.8511425569379765e8 seconds
+ arrival date: 2029-03-15T15:49:20.616
+ thrust profile: [0.1583322927151261 -0.050549429768169014 -0.0699819794789512; 0.08844512787850763 0.013499204728371182 -0.11733694075006729; 0.049864943107614426 0.016961540804853254 -0.11367181544677747; 0.04030934189095171 0.018150646976502725 -0.12865891188745945; 0.030708599486292638 0.016147034801964187 -0.12582529383750332; 0.02169228542512923 0.012620686402036245 -0.1084093156465234; 0.01438221893895135 0.009031108069682863 -0.08241449093408677; 0.013749393200747114 0.009161525022187688 -0.08936663915982587; 0.0015747658945943503 0.0011847903638919832 -0.011535715478997264; 0.006053453518285929 0.00426008156885819 -0.0490449080088582; 0.0006336179971978858 0.000564554788892801 -0.0047382085845081015; 0.001745399199062358 -0.0016018982219777667 -0.00253125090601405; -0.0013808382732789942 0.00108900425810878 -0.001249824808729262; -0.00019135570737809679 0.0003176754786831659 2.6227252009900447e-5; 3.750095137549091e-5 -0.0009469047735296797 0.0006684436076599934; 0.002113978683647124 -0.0027589981141136095 -0.0061029301083273604; 0.0007874414202914235 0.002675791117791762 -0.00286049099271403; 0.001590080121835904 -0.001931234802632846 -0.0030957689921864316; 0.00041500694051092727 0.000704678003445508 -7.028043995304582e-5; 0.0007032035681550225 0.00021192269528969238 -0.001247888247306872] %
+
+Mass Used: 80.82991497097782 kg
+Launch C3: 99.16836744262906 km²/s²
+||V∞_in||: 0.013242501356311363 km/s
diff --git a/archive/ES_0.565128708587251 b/archive/ES_0.565128708587251
new file mode 100644
index 0000000..2aae46a
--- /dev/null
+++ b/archive/ES_0.565128708587251
@@ -0,0 +1,22 @@
+archive/ES_0.565128708587251---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T15:14:33.730
+Launch V∞: [6.595731462585813, -7.417376296045265, 0.09754315414183813] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.331878181633888e-9, 1.1965953597710997e-9, -8.146709285553504e-9] km/s
+ V∞_out: [-2.428322900365313e-9, 5.670578636822378e-9, 7.629335374022525e-9] km/s
+ time of flight: 1.8661937230751714e8 seconds
+ arrival date: 2029-03-30T13:57:25.730
+ thrust profile: [0.160364396330146 -0.042352217632794655 -0.05795909001731857; 0.04657052678539798 0.01188167296416519 -0.05244149259295977; 0.07470641359925706 0.03688431449136493 -0.135599292516872; 0.059928452593788394 0.03979213018767028 -0.1521075869690321; 0.05188018301083998 0.04125403896316634 -0.1684612190935743; 0.01820621597665033 0.016541545299338475 -0.07659500555247449; 0.015395129281158573 0.014866689622886653 -0.07278050460614038; 0.008801929130364339 0.007587064958252119 -0.04762104147785446; 0.005554312509731486 0.005955269345069888 -0.03428342286045005; 0.008768261067785318 0.010533758569017188 -0.04689872715731357; 0.004106084794947078 0.0064843932385753675 -0.03252881539671514; -0.0008455378699693694 -0.0011506969696416518 -0.00046963734297643964; 0.0005166843615310232 0.0025496722143368445 0.001775496967123443; 0.00043292206138517605 0.003531732077023702 -0.0007221856370256009; -0.0025619650254512702 -0.0036535689923083235 0.0010856286177917769; -0.0016156867262981946 0.008335954316473937 0.005330168337453152; 0.005763504236368683 0.0019307207074656732 -0.009931746351349729; 0.005670804959357017 0.0056610857794600735 -0.004310815709474015; -0.000772236886346726 -9.844462749250939e-5 0.00036470161841894544; -0.0036667288825422565 0.0014776667984327232 0.014714000645669866] %
+
+Mass Used: 84.55464737330158 kg
+Launch C3: 98.5306593105985 km²/s²
+||V∞_in||: 9.80967061537404e-9 km/s
diff --git a/archive/ES_0.5651459043694274 b/archive/ES_0.5651459043694274
new file mode 100644
index 0000000..be61a16
--- /dev/null
+++ b/archive/ES_0.5651459043694274
@@ -0,0 +1,22 @@
+archive/ES_0.5651459043694274---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T22:58:00.004
+Launch V∞: [7.6774822730680246, -5.758816341375492, 0.17399980735854134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.174431027958936e-5, -2.5656425407041438e-5, 1.829205558630462e-5] km/s
+ V∞_out: [-6.026483112700417e-6, -4.4299544070615286e-5, 2.1050405319091555e-6] km/s
+ time of flight: 1.874957778768671e8 seconds
+ arrival date: 2030-04-19T01:07:37.004
+ thrust profile: [0.5029174756520545 0.03787241648399186 -0.09522816770478201; 0.19934115185606688 0.1545385844037517 -0.1358184016808366; 0.07462118120196391 0.09714747008209244 -0.0986854258973017; 0.08270463808961129 0.15665845216151988 -0.16576039548872007; 0.028269179317221397 0.06994221731102954 -0.0847026148037453; 0.02204154595959856 0.07565136622160304 -0.09730471320670177; 0.014317979100785886 0.06000687620718965 -0.08171067894166548; 0.002769039963363995 0.013789715989174741 -0.020480919928717853; 0.0005475354785056206 0.002504670464826503 -0.003626185150896754; 0.0002618359307269392 0.0005023306765323883 -0.0018398282086625145; 0.0018913212722431417 0.0017663736083676769 -0.004637990824022319; -0.0011389185545836612 0.001346902916441457 -0.003213621895387495; -0.006199988995545445 0.0031358692472125763 -0.0010849153688425829; 0.0013764090812798183 0.002487367723264102 -0.001800641440600487; -0.001220323444250108 0.0029049893104388675 -0.001802017658199559; 8.61485680424391e-5 0.0008915609964485348 -0.0005085072012130706; 0.0038798201807529594 -0.0009858750337979824 -0.0019449354148801052; -0.0021050492807206935 0.00629603849596912 -0.01367805896786705; -0.006180320825423951 -0.0031669167533850935 -0.0036939130584811037; 0.004454672513841444 -0.005841294970516626 -0.004971974285275295] %
+
+Mass Used: 121.865363864752 kg
+Launch C3: 92.13797563992797 km²/s²
+||V∞_in||: 4.472753846755243e-5 km/s
diff --git a/archive/ES_0.5651496399760065 b/archive/ES_0.5651496399760065
new file mode 100644
index 0000000..2ecc12a
--- /dev/null
+++ b/archive/ES_0.5651496399760065
@@ -0,0 +1,22 @@
+archive/ES_0.5651496399760065---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T09:22:51.435
+Launch V∞: [6.412917764949987, -7.489910727876928, 0.12400121671436384] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5570257051377297e-9, -2.039373933103225e-9, 2.5879589676729796e-9] km/s
+ V∞_out: [1.0815819025015423e-9, -2.7202126249544555e-9, -3.635747318421939e-9] km/s
+ time of flight: 1.8086094256928858e8 seconds
+ arrival date: 2029-01-20T16:31:53.435
+ thrust profile: [0.2488069423961358 -0.07671316459240331 -0.09141765973412004; 0.05432648874544575 0.011288055775391912 -0.058080013054015625; 0.08346956608136542 0.036872804348165714 -0.14865302055732202; 0.08920761677993619 0.054036929146783784 -0.2202619693371892; 0.03555115790433485 0.02556591628009753 -0.11223862916381; 0.027158514605005065 0.02231990550716899 -0.10335560087056149; 0.016193423815297734 0.015302638502054454 -0.07463621399645656; 0.016140601145717092 0.015384958933616934 -0.07892618109077848; 0.004683868955410019 0.004791520800868656 -0.025667255844438318; 0.0022579528008509044 0.003920223852312246 -0.01586138499897787; 0.0012079623380252585 -0.0010193017236012616 -0.006984341993636657; 0.001667159070726022 0.0009842271747575607 -0.00933232162480966; 0.0006434909576295889 -0.0006049258206457069 -0.007373228972465613; -0.0012890266978675352 -0.0015730567902419812 -0.000820362891597615; 0.00019251607014546745 0.001064770611360466 -0.0036187457156666237; -0.002306567221550383 -0.004342437907242539 5.6619904537908924e-5; -0.004928463575671812 0.0024384617667732676 0.002858078932315995; 0.00677423186389442 0.007083111998114148 -0.001510887337035539; 0.011172426372955051 -0.008439264783324938 -0.009596046620438085; -0.0024834568711605024 0.002115736836472519 -0.002181584216323256] %
+
+Mass Used: 92.10993587761959 kg
+Launch C3: 97.23965327332367 km²/s²
+||V∞_in||: 4.170726329323828e-9 km/s
diff --git a/archive/ES_0.5651605430529593 b/archive/ES_0.5651605430529593
new file mode 100644
index 0000000..d9aa543
--- /dev/null
+++ b/archive/ES_0.5651605430529593
@@ -0,0 +1,22 @@
+archive/ES_0.5651605430529593---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T02:43:25.939
+Launch V∞: [6.636856790566113, -7.4004524508444005, 0.20599018303988262] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4570555469319918e-9, 8.2287337657864e-10, 7.606370744547401e-9] km/s
+ V∞_out: [-4.374755654312418e-9, -6.466541337080921e-9, -3.1669981083109853e-9] km/s
+ time of flight: 1.8749577787485206e8 seconds
+ arrival date: 2029-04-10T04:53:02.939
+ thrust profile: [0.16658200263227127 -0.039265351554954094 -0.06265156640782824; 0.04016889736621522 0.010950495708040592 -0.04629929579011288; 0.04049944037172288 0.021603527510116554 -0.08127283927076481; 0.038240579718336595 0.027132660184803356 -0.10692127834000678; 0.05403398141493524 0.047708812739288835 -0.17934397662268914; 0.027772526473420055 0.02777802547637442 -0.12274881128929924; 0.016655769977418675 0.020688238993928763 -0.09210654565746051; 0.010813502826830107 0.014626883413254018 -0.06401827110060547; 0.004569843166007344 0.0068819153719792405 -0.035384279866162265; 0.0024357461353455715 0.004888738202906458 -0.02588831117702812; 0.004549876476720192 0.0066326811582009815 -0.036744742645903675; -8.504826916933363e-5 0.00041721613649995217 -0.01457267849644839; 0.0013667866337988652 0.001413737747211799 -0.0005944544095064067; -0.0029147527177949928 -0.0018166949945998202 0.002985554595707686; 0.005170167572492445 0.003847625919973337 0.0007824880690325932; -0.0012463999398306773 -0.00154713306624363 0.0008500563175337213; -0.0028221364177963247 0.0006292233124172622 0.004313728602796429; -0.014830372478269137 -0.0004327924328154477 0.006085170521624757; 0.0019978906184373794 0.0018959605415444644 -0.0028664090326081175; -0.001801215568490506 -0.004200759140509987 -0.012066732070216184] %
+
+Mass Used: 82.68815402977862 kg
+Launch C3: 98.85699649120123 km²/s²
+||V∞_in||: 7.788260869040905e-9 km/s
diff --git a/archive/ES_0.5651648394918256 b/archive/ES_0.5651648394918256
new file mode 100644
index 0000000..fb90603
--- /dev/null
+++ b/archive/ES_0.5651648394918256
@@ -0,0 +1,22 @@
+archive/ES_0.5651648394918256---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T14:32:59.440
+Launch V∞: [6.511537903564224, -7.530970467262936, -0.01949520945982477] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.018034425007349704, 0.000287826198622966, -0.012595713784996439] km/s
+ V∞_out: [0.021065588596044068, -0.00022373621782387237, -0.006333336516027929] km/s
+ time of flight: 1.8586962925509083e8 seconds
+ arrival date: 2029-03-22T21:00:08.440
+ thrust profile: [0.1293522024429491 -0.030593293602240945 -0.047146131967811006; 0.05269153628889532 0.0160607916471153 -0.056995152530207864; 0.05551202881560298 0.03038880040926373 -0.09767967055066913; 0.04375176399734053 0.03092144742534262 -0.10476142271997106; 0.02668998190050381 0.024172354533818413 -0.08719452715211373; 0.016986199668091482 0.018111420359709977 -0.07015895255436115; 0.03211433787028003 0.0366380165479461 -0.1624148890490996; 0.016995373668483395 0.022046708605110335 -0.09411997174485287; 0.011683111240569501 0.014750954898309021 -0.06443014483134013; 0.005128686050603959 0.010398912154403854 -0.040471225005787294; 0.00703662230057095 0.00994445493452995 -0.0495228519525745; -0.000945945188749798 0.0022583185333404044 -0.013058564747726195; 0.0011126817907683231 0.0005289624810151891 -0.0043396742799387995; -0.003940403061550204 -0.0023896440510174865 -0.001452336031243963; -0.0004057409505338191 -0.005025128701356689 0.001401727387835143; -0.0004277478713706542 -0.001717201099885152 -0.0026273903747985354; 0.002206747453261627 -5.575167870538675e-5 0.0033866278052304567; 0.00013655509376172322 0.0008795382152778251 0.0037733129692889837; -0.004209399817970746 0.002074653600062641 0.0031554001922578733; 0.0008374477686251906 -0.0008653465360003909 0.0002580897123123133] %
+
+Mass Used: 81.18218375652668 kg
+Launch C3: 99.11602211153198 km²/s²
+||V∞_in||: 0.021999439425128164 km/s
diff --git a/archive/ES_0.5651705658761781 b/archive/ES_0.5651705658761781
new file mode 100644
index 0000000..43212ba
--- /dev/null
+++ b/archive/ES_0.5651705658761781
@@ -0,0 +1,22 @@
+archive/ES_0.5651705658761781---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T18:51:56.405
+Launch V∞: [6.382513047255863, -7.62236889959326, 0.040357138866785026] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.083775036244456e-10, -2.751956455147397e-9, -8.50970895065195e-9] km/s
+ V∞_out: [3.0578945972835495e-9, 4.2598193669244595e-9, 2.2087512887495072e-9] km/s
+ time of flight: 1.797136035413277e8 seconds
+ arrival date: 2029-01-08T19:18:39.405
+ thrust profile: [0.1309990226796151 -0.04181775377376593 -0.052779351522456164; 0.05263723086838424 0.009502042740293745 -0.06075654851375984; 0.07677192272407633 0.031206889921278326 -0.14602272689603576; 0.04890115468539071 0.026588339085096883 -0.1292817094111576; 0.05539617370064303 0.03576658565890482 -0.18095356704071505; 0.03309113045109173 0.024526694280037065 -0.13435681761418256; 0.018013899592772564 0.014577631677425968 -0.0853201638061464; 0.009397165962079648 0.008077615830022864 -0.050152012836880734; 0.008405825469109085 0.007702281262977375 -0.04997694703653496; 0.0049608646894149944 0.004252659694190902 -0.024894720413823273; 0.0015057160893308065 0.00245545485554471 -0.01251831999862467; 0.0010661567178274758 -0.0025492721841214724 -0.0024000976731729635; 0.00014349450043815498 0.0011204950639201717 -0.0043551615860829025; -0.0008038161590633842 0.0006529753693650751 -0.00475548010474139; 0.00039979351654530144 0.00040446479143603855 -0.003082219515622751; 0.006854646337126045 -0.0028244885166938075 -0.007762209126306136; -0.0027798300794804813 -0.0006316867253957237 -0.0035110220348631453; -0.0014389947582907929 -0.003086193395581787 -0.0006855299057356263; 4.6697569789765775e-6 -0.0009564612887130652 -0.003864926588807634; 0.008212546602365546 -0.0042169581486939285 -0.015872236621389268] %
+
+Mass Used: 82.80710688075123 kg
+Launch C3: 98.8386091385354 km²/s²
+||V∞_in||: 8.958061087200999e-9 km/s
diff --git a/archive/ES_0.5651706023523843 b/archive/ES_0.5651706023523843
new file mode 100644
index 0000000..b852573
--- /dev/null
+++ b/archive/ES_0.5651706023523843
@@ -0,0 +1,22 @@
+archive/ES_0.5651706023523843---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:05:52.396
+Launch V∞: [7.5497398573755214, -5.875839622595359, -0.013674515039173116] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.976739575340029e-8, -5.993235475059172e-8, 4.3758819417382996e-8] km/s
+ V∞_out: [-1.2786437450827016e-8, -1.0206540950090812e-7, 4.795155943653687e-9] km/s
+ time of flight: 1.7729108013566515e8 seconds
+ arrival date: 2029-12-20T04:37:12.396
+ thrust profile: [0.6950101760696329 -0.038324084033894465 -0.16606939356475214; 0.18369072670367917 0.10208133968592444 -0.15313974230271205; 0.05139881682777309 0.04981594873481981 -0.08172421336160693; 0.026663294259398996 0.034838806096898364 -0.06304244183410426; 0.01739381710700345 0.028397606242588972 -0.05655345398870546; 0.036855458118811336 0.10262949609292801 -0.18979120912376893; 0.01111406501367687 0.025911036276542447 -0.056954613611511926; 0.008649257215976454 0.0235278016610672 -0.05430095264779018; 0.017726109275757688 0.05602075049964784 -0.12762264739452742; 0.0004904149716492412 0.0017191064232423016 -0.005281979270172774; 0.0027321980745761707 0.003437101070244533 -0.010011877895528666; 0.000331176548500843 0.0031964970086927925 -0.002810682742790408; 0.00026212706938860117 0.002030551891332356 -0.002631986166260134; 0.0004637783386320885 0.001899920126459054 -0.006826437247930893; -8.892738005897684e-5 0.004344215818378967 -0.00275943531237304; 0.005268675880187354 0.010104986975947524 -0.0031530061717125256; 0.001155948358068138 -0.00033280445997713225 -0.002382443696495642; -0.005462844424377318 -0.0028366336634322153 -0.0092580807339263; 0.00020091821143338313 -0.0009585484277745398 -0.0013396952800220595; 0.0035980324542581018 0.0007831688117123758 0.0021899898935272702] %
+
+Mass Used: 125.47424337938673 kg
+Launch C3: 91.5242501768677 km²/s²
+||V∞_in||: 1.0185387048593434e-7 km/s
diff --git a/archive/ES_0.5651733788404983 b/archive/ES_0.5651733788404983
new file mode 100644
index 0000000..22df256
--- /dev/null
+++ b/archive/ES_0.5651733788404983
@@ -0,0 +1,22 @@
+archive/ES_0.5651733788404983---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T04:17:29.628
+Launch V∞: [8.03362971798757, -6.0424801004310815, 0.12432021262763189] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.14916721151403e-5, 5.8968471664018235e-5, 4.3462908906465294e-5] km/s
+ V∞_out: [9.307416897403568e-6, -6.090216650126274e-5, 8.181613467528455e-5] km/s
+ time of flight: 1.8749577777191728e8 seconds
+ arrival date: 2030-04-29T06:27:06.628
+ thrust profile: [0.13168899051035451 -0.009280374428953703 -0.05593522466420901; 0.015043035763330099 0.005138902555639942 -0.022890872567411964; 0.03366745270668896 0.01679191107521014 -0.08701802127877274; 0.03876143964245278 0.022326868889277016 -0.13785770010002962; 0.03446418827835923 0.021230282020972963 -0.15528298724833167; 0.026111521806429033 0.016269645913226577 -0.14085128458106225; 0.007960601892075352 0.004204809506393438 -0.051960814343049; 0.00909089157335094 0.004766236165486594 -0.06244763067796003; 0.0026001668378952242 0.0015732974769060157 -0.021627624597195534; 0.001528903587128439 -0.0011276007611947794 -0.009155146751495431; 0.0001377491942337486 0.0010398852222941503 -0.009882605263006205; 0.004178043899880226 -0.0004844346286062661 -0.003205068760346032; -0.0009815575935723203 0.0002726302551336491 -0.0025469996982213127; 0.00037932816116437043 0.000933578724415751 0.00348058697805648; -0.00554100745728953 0.002722057182485238 0.0030556207573945423; -0.004014055036810692 0.005097602199917155 0.002871088530136026; -0.0002048977975176111 -0.007043585452427346 0.005864289668296105; 0.0024465517236730346 -0.0028085465961528973 0.005758110500069309; -0.007960713787047515 -0.006411951352761987 0.00813700820469061; -0.0021703263117478695 -0.004198284862517117 -0.005985151754607381] %
+
+Mass Used: 69.81594691746068 kg
+Launch C3: 101.06622772510642 km²/s²
+||V∞_in||: 0.00010235899707803194 km/s
diff --git a/archive/ES_0.5651801264961549 b/archive/ES_0.5651801264961549
new file mode 100644
index 0000000..3f28d70
--- /dev/null
+++ b/archive/ES_0.5651801264961549
@@ -0,0 +1,22 @@
+archive/ES_0.5651801264961549---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T23:56:11.487
+Launch V∞: [5.924047363171005, -7.639977800314076, 0.16589883843962575] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2005538181809165e-5, 7.295158934138304e-6, -5.508437233053194e-6] km/s
+ V∞_out: [7.885296351705355e-6, -1.074258956774816e-5, 7.05276509877572e-6] km/s
+ time of flight: 1.7312174518627653e8 seconds
+ arrival date: 2028-10-19T17:18:36.487
+ thrust profile: [0.4779492423914894 -0.1481403639349366 -0.1417068049570426; 0.14732513592115076 0.03613511811250986 -0.1295001103580742; 0.10334597164913788 0.05288790639562143 -0.1474363872889256; 0.08759371835416144 0.06284645873112135 -0.17126737442642; 0.07034341721156047 0.06309693045014238 -0.1748043867196303; 0.039971059336250774 0.040583760452685726 -0.12310231942934931; 0.028310681445467435 0.03183225091890953 -0.10047745618225658; 0.016755565943285946 0.020762924749070735 -0.06981527971274445; 0.0006023581519147678 0.0010175147721419688 -0.003606282058902228; 0.00029313157991397206 0.0009442020603470411 -0.0019473849202244198; 0.0018013299490881594 0.00300174125616756 -0.01053840011614096; 0.00037134818891666884 -0.0002890275972594319 -0.000935839497778818; 0.00018877806437071981 0.0004115481454486534 -0.0014927700938059932; 0.00018243577136507858 6.424825758526381e-6 -0.0004785895234162849; -0.0004305612642220429 -0.0001265078419060879 -0.0006583883599029827; 5.445177768490238e-5 -0.0001954480113715558 -0.0014849999143654775; 0.0014771458549135746 0.0005348177312990768 -0.0008514418040187714; -0.000537427132963201 -4.248639026342173e-5 0.00048527623796613967; -4.396630931227533e-5 -9.727881952539439e-5 1.9937847519178843e-5; 0.0009371958658317328 0.000199368828219519 0.0003056193862610451] %
+
+Mass Used: 114.011945391459 kg
+Launch C3: 93.49112037498087 km²/s²
+||V∞_in||: 1.508957161948948e-5 km/s
diff --git a/archive/ES_0.5651820747410401 b/archive/ES_0.5651820747410401
new file mode 100644
index 0000000..ec5b4a6
--- /dev/null
+++ b/archive/ES_0.5651820747410401
@@ -0,0 +1,22 @@
+archive/ES_0.5651820747410401---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T09:43:17.495
+Launch V∞: [6.605940405474, -7.454002938319022, -0.3100002163061831] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.780290315524973e-9, -2.241560923926325e-9, 3.447469067227246e-9] km/s
+ V∞_out: [1.3968786462811786e-9, -3.3156950698894918e-9, -4.494978827242286e-9] km/s
+ time of flight: 1.8581184332201752e8 seconds
+ arrival date: 2029-03-22T00:07:20.495
+ thrust profile: [0.13359660141845855 -0.039202514020654375 -0.054542339729789835; 0.07953324497669452 0.016652230133557856 -0.09916570275787906; 0.03628667376583277 0.01760935057665194 -0.08763838264961968; 0.024668510353767756 0.016318539595812174 -0.08584436849525348; 0.019644113362650477 0.015825019614868343 -0.08798715829256755; 0.01544175232809971 0.014077384652930718 -0.08456946807075624; 0.014850131654167778 0.014532794369555747 -0.09241649074380943; 0.017314879287197365 0.016393431345756944 -0.11071885487692681; 0.011718252950199102 0.012273618716389094 -0.08747411166468924; 0.007870201310871941 0.008886476534657337 -0.06657445507741123; 0.003934828185829997 0.004735852611603679 -0.037403273205316764; 0.0007459695495227991 0.0006841803545001579 -0.006262457724561263; 0.00040173107668006226 0.000561469376798065 -0.0048669195435226305; 0.0038612537928955793 -0.0007560623882450679 -0.0028666156977343047; 0.0006900603798735935 0.00048022716561641333 -0.0040214002709268865; 0.0009129802306219749 0.00020679442716799873 -0.004251840687118058; -0.00018515780533562873 0.0001623156129253447 -0.0004926515248252347; -0.0039841758511850595 0.002628943056326923 -0.00389398871339289; -0.001357686653631166 0.0003695614745380047 0.0012745531380479345; -0.0037270768527186667 -5.289034360272211e-5 0.0006517034642255475] %
+
+Mass Used: 80.14828715224075 kg
+Launch C3: 99.29670857925247 km²/s²
+||V∞_in||: 5.585716893543212e-9 km/s
diff --git a/archive/ES_0.5651845064118078 b/archive/ES_0.5651845064118078
new file mode 100644
index 0000000..04aea70
--- /dev/null
+++ b/archive/ES_0.5651845064118078
@@ -0,0 +1,22 @@
+archive/ES_0.5651845064118078---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T23:02:42.224
+Launch V∞: [6.4322382825805775, -7.306711939354993, 0.1884417929697916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0463788228169104e-8, 6.250313244574408e-10, -9.003047900087926e-9] km/s
+ V∞_out: [-2.8072263079753376e-10, -1.3857688259576776e-8, 8.87207412704868e-10] km/s
+ time of flight: 1.874957778753614e8 seconds
+ arrival date: 2029-04-07T01:12:19.224
+ thrust profile: [0.42292581597050904 -0.07782075632980767 -0.11789583248666174; 0.10926279710027469 0.041834667145700076 -0.09543473184185278; 0.07044179949670193 0.048589607370801695 -0.10237835297178527; 0.051046205913808464 0.04860302102635653 -0.1068899875020204; 0.05118589100204354 0.06012207310015548 -0.13700689470349964; 0.023884227233272104 0.032870705207720376 -0.08195071212424891; 0.014779890352137441 0.02322981178582615 -0.06193863873921919; 0.024367455354657445 0.04456853098076774 -0.12198541723925757; 0.011390986778878173 0.02121115039131902 -0.061886098400955734; 0.000903980901908839 0.002994684562596995 -0.00847534269217708; -0.0001951368027964795 0.0005017758492246286 -0.00017807130283394338; 0.0006081570014426814 -0.0005992400715856066 -0.0019345593094628262; -0.001645506531349987 -0.0010029776576589875 -0.001045647758927323; 0.0002754371779942654 0.0037364318431220467 0.002272314669789394; -0.006017831429017517 0.003015692750347729 -0.0032850181690782044; 0.006335680030910243 -0.0028621055696738656 -0.00641101296209165; -0.0026765698650572135 -0.004075641934700881 -0.0051128463633791634; 0.00044368583119560744 0.0015603275049944538 8.905796428008029e-5; -0.0033954266727156453 0.0020260318061752942 -0.0014164477179369806; 0.0019888783189683057 -0.0017984322825185953 0.0004330116007229734] %
+
+Mass Used: 106.39802999242647 kg
+Launch C3: 94.79723899794561 km²/s²
+||V∞_in||: 1.3817973792557322e-8 km/s
diff --git a/archive/ES_0.565188467978634 b/archive/ES_0.565188467978634
new file mode 100644
index 0000000..53e9fea
--- /dev/null
+++ b/archive/ES_0.565188467978634
@@ -0,0 +1,22 @@
+archive/ES_0.565188467978634---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T09:51:26.681
+Launch V∞: [6.453089661225103, -7.500389093495669, 0.06513064856880071] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1691717602140792e-8, 2.1130396475963233e-8, 1.426546026800784e-8] km/s
+ V∞_out: [-6.996382648098937e-9, 1.714523940017274e-8, -2.624721133478437e-8] km/s
+ time of flight: 1.85292316310854e8 seconds
+ arrival date: 2029-03-15T23:56:42.681
+ thrust profile: [0.2314691257367697 -0.06723615575183114 -0.08665014964676765; 0.06380301552165746 0.012986896004193275 -0.07031498433650948; 0.04284504507173584 0.01796582758507442 -0.07944729129029915; 0.04695832178926163 0.026321441486681824 -0.1213430454315123; 0.04641811096890038 0.03093304492845857 -0.15374635788336044; 0.020547717803819483 0.015065883744451645 -0.08158358185885911; 0.014508115082441202 0.010720438945997316 -0.0676911192635953; 0.02413497595992372 0.022204936295311766 -0.1325790008636327; 0.00218005920813475 0.0033763908880397966 -0.016178851770305456; 0.00878162068862097 0.004937948069459703 -0.054041877713356334; 0.004376349863557929 0.006051340931469776 -0.0353090997360823; -0.001106262143864259 2.1064561848854388e-5 -0.0034981003048594733; 0.0027673196675612383 0.003971564389252174 -0.016065244490939306; -0.000627279299814328 -0.0012085039720088342 0.0034330494213511437; -0.001799838441094175 -0.0010919157184248983 0.0013567420529274057; -0.0011856774867801915 0.0004359368452715187 -0.0050547237095268935; 0.0015365453783349663 0.0012288532158192247 -0.0008996289227204577; 0.0006695041965497238 0.001829405450291546 -0.003055588168222838; -0.001212660552353854 0.00010289058260484502 0.010251213769705421; -0.0008614040832569493 -0.005275832695035391 -0.006636473911795841] %
+
+Mass Used: 88.28895171077738 kg
+Launch C3: 97.9024447310221 km²/s²
+||V∞_in||: 2.8048052915981863e-8 km/s
diff --git a/archive/ES_0.5651935313821119 b/archive/ES_0.5651935313821119
new file mode 100644
index 0000000..e39e4d6
--- /dev/null
+++ b/archive/ES_0.5651935313821119
@@ -0,0 +1,22 @@
+archive/ES_0.5651935313821119---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:07:11.845
+Launch V∞: [6.317790459779531, -7.5884281056074805, 0.10288157126210366] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.368827253935705e-7, -0.0001740200994274006, 0.00011997073149909356] km/s
+ V∞_out: [0.00010894599444016138, 0.00017764640107804241, -3.796232292195228e-5] km/s
+ time of flight: 1.839797028349592e8 seconds
+ arrival date: 2029-02-28T20:35:33.845
+ thrust profile: [0.24983907285026896 -0.07006686772538442 -0.09384557577944792; 0.07749394916121753 0.017920915070957437 -0.09011032814274048; 0.0558980993406067 0.024918611127204136 -0.10802123826566627; 0.05438638183508408 0.03271147606345728 -0.1446918774544528; 0.045524634903405845 0.03279140197752759 -0.15396140716603512; 0.02948844826044446 0.023995956371973857 -0.12209481834455356; 0.019210317393352796 0.017658847539156877 -0.09433674254342232; 0.008832127670985844 0.006844844959192818 -0.04487914591364472; 0.008053995188865523 0.006379706149085982 -0.04385769675290068; 0.0024823887876921887 3.3284074923339846e-5 -0.0064442431222785914; 0.00019822494682358188 0.0026654155096837028 -0.007216074111410851; 0.0034229586545828044 -0.0028088648434919797 -0.004223156688528188; 0.00027325796741764854 -1.5684310000981774e-5 -0.0035063825720992765; -0.0014930073376501498 0.008316124921853598 -0.006287093906476962; -0.0047685887228125865 -0.0009755029482983205 0.0001748010097834059; -0.00046598436813200157 0.0026837703126828833 -0.0006114277498673161; 0.0011723194139647123 -0.00040093961519870443 0.0011441755340887412; -0.006653718996938135 -0.006385382913217715 -0.015510452999870793; -0.0070399167026690655 -0.0018095381263483895 0.0019752655210675575; 0.004391114394675211 -0.005116301242270416 -0.0036434871542632427] %
+
+Mass Used: 90.5881914645297 kg
+Launch C3: 97.50930202536016 km²/s²
+||V∞_in||: 0.00021136759369451793 km/s
diff --git a/archive/ES_0.5651970091345873 b/archive/ES_0.5651970091345873
new file mode 100644
index 0000000..b2345c4
--- /dev/null
+++ b/archive/ES_0.5651970091345873
@@ -0,0 +1,22 @@
+archive/ES_0.5651970091345873---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T21:56:32.207
+Launch V∞: [7.519832182633027, -5.654543386120506, 0.15957222136376364] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004780877994402316, 0.0032538270710169796, 0.0001985102294708909] km/s
+ V∞_out: [-0.0041324889046065495, -0.0013358650075529807, 0.0038294127931890022] km/s
+ time of flight: 1.8206543216572902e8 seconds
+ arrival date: 2030-02-13T03:40:24.207
+ thrust profile: [0.953208204426231 -0.02354251059232325 -0.23964330900393305; 0.22123414204588485 0.13328790906860077 -0.20168535311760488; 0.05543764268014199 0.05614593238085362 -0.0979625206309428; 0.032411400569372424 0.04483578264037318 -0.08596527637330707; 0.02445949715694486 0.04392525198116605 -0.08932220349538153; 0.013978469229602239 0.02837628934238794 -0.06591871705867515; 0.00989848648383258 0.024755302547081994 -0.05989527147039737; 0.003182176249346566 0.009492744181577122 -0.025421714743054644; 0.010358569019813958 0.03458164344376063 -0.09044133852140518; 0.002714040033810472 0.006463581081030407 -0.02031177753076951; 0.00023368294933756104 0.0022803955644868775 -0.00563134243272725; 0.0007426495548139872 0.002031568731848663 0.00187950538713768; -0.00019183166603622915 -0.0006702806122511264 0.0009638766080049144; 0.000109565168116466 -0.003000118453260207 -0.0010088812749098658; 0.001538720243894983 0.004371606135960857 0.0011360974311057548; 0.00048573112579019775 -0.0002214953267615017 0.0004450759845910806; 0.002391857879989955 -0.006023575613110044 0.004480272554096337; -0.0016110121007324024 0.0036723729551310694 0.004104651549545913; 0.000962330943493893 -0.0012876626129164344 0.006143384764888859; 0.0011498307423341634 -0.0011734094705880289 0.005515152995855525] %
+
+Mass Used: 142.8711758401896 kg
+Launch C3: 88.54720025431351 km²/s²
+||V∞_in||: 0.005786500783431022 km/s
diff --git a/archive/ES_0.5651991927212052 b/archive/ES_0.5651991927212052
new file mode 100644
index 0000000..1d6da72
--- /dev/null
+++ b/archive/ES_0.5651991927212052
@@ -0,0 +1,22 @@
+archive/ES_0.5651991927212052---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T09:47:15.971
+Launch V∞: [6.419270298592986, -7.2202904025269055, 0.23511779723515885] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.07293064046448e-6, 1.4787589142604633e-5, -8.597888273818033e-7] km/s
+ V∞_out: [3.304517615928711e-6, -1.3963254407367441e-5, 4.2014603079521985e-6] km/s
+ time of flight: 1.874957778756454e8 seconds
+ arrival date: 2029-04-06T11:56:52.971
+ thrust profile: [0.544626790303823 -0.13984519526825953 -0.13609679504139552; 0.10612180294806768 0.03234885011762932 -0.0986950479332631; 0.08855645164852714 0.05186956628285142 -0.13018446880182022; 0.06258442922311858 0.05097757357618495 -0.12836122292056681; 0.03791574375114674 0.04182823160684155 -0.11491540650207754; 0.020094706665862903 0.024525221672254228 -0.07325845283785232; 0.01824722766490514 0.027855734152581375 -0.08667864833557638; 0.01827199543923799 0.025323880707462446 -0.08855944608615098; 0.003024279899766737 0.00565739357655762 -0.018284259024215734; -0.0009541131932050153 0.0008641084397850498 -0.004271974959282412; 0.004157444726981659 0.006597407402004706 -0.0251231049163142; 0.0001771413630460468 0.002256324550578319 -0.0019059234599381404; -0.001765346869603758 -0.0012127155888081308 -0.002552823117408193; -0.0030788801657258297 0.00023066142306094506 -0.00223415188079408; -0.0009896741191008497 0.0037940788489667756 -0.004376755499334937; -0.0004936937305418184 -0.0005144284899111511 -0.006476763150970584; -0.0016471360969270577 0.006559399106158677 -0.0014748491398729434; 0.0034450468983912045 -0.004133477270595914 -0.0035606516317480954; 0.0032171827108370753 0.0011497211764151954 0.005110412677954476; -0.00017701265889275355 -0.0023673647889745917 0.0028564017342405093] %
+
+Mass Used: 114.59544543092397 kg
+Launch C3: 93.39490504179693 km²/s²
+||V∞_in||: 1.4956907130765554e-5 km/s
diff --git a/archive/ES_0.5652055982721644 b/archive/ES_0.5652055982721644
new file mode 100644
index 0000000..51c01f9
--- /dev/null
+++ b/archive/ES_0.5652055982721644
@@ -0,0 +1,22 @@
+archive/ES_0.5652055982721644---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T07:12:49.764
+Launch V∞: [6.2765539081489345, -7.42693920731718, 0.12039396629098835] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.291396083647353e-9, -2.9372090244970725e-10, -3.90466241238156e-9] km/s
+ V∞_out: [-1.5308495719806946e-9, 3.3073560318860817e-9, 5.042305746959765e-9] km/s
+ time of flight: 1.854335105170119e8 seconds
+ arrival date: 2029-03-16T12:31:19.764
+ thrust profile: [0.5154435189859512 -0.137583930564383 -0.17864145179967933; 0.039719966915016267 0.009869607081046039 -0.04529705977208998; 0.06429715909471478 0.03230772337553847 -0.12053231394766342; 0.03527152608155041 0.023100539908380194 -0.09319844651351643; 0.037639472979957525 0.029858790338783206 -0.1255193783621121; 0.029409565350760693 0.02747547592946052 -0.12215301931693305; 0.01312778320070304 0.013116766395487308 -0.06411548401207424; 0.010824319989666282 0.011839051695170731 -0.06082644895558511; 0.011451365579377506 0.013332449815090663 -0.07073993275737002; 0.003407974474093401 0.004267694192130063 -0.024550312429542902; 0.0018744116327521357 0.0024433740199344104 -0.014700210215731833; 0.0036279678656193533 0.005397274660763066 -0.027077075045791616; 0.002312394933626241 0.0010199580807314982 -0.0040582731700528965; 0.00029248947384215166 0.0007848877004376299 -0.009218640038963144; 0.0024568162054958414 -0.0016693766780944957 0.00021746456664875147; -0.00019277736422021116 0.0007640259321136466 -0.0036044321240770497; -0.00512105551305805 0.007550352797333801 -0.017680392390010558; -0.0023793886795507556 0.00028935069956465226 -0.004039014506843677; -0.0034567299974868283 -0.0015705146568363066 0.002131784899578313; -0.008983673583012485 -0.001793380499075124 -0.0034253814488344127] %
+
+Mass Used: 107.75374164466803 kg
+Launch C3: 94.56904965820408 km²/s²
+||V∞_in||: 5.8093666496396226e-9 km/s
diff --git a/archive/ES_0.5652258322363258 b/archive/ES_0.5652258322363258
new file mode 100644
index 0000000..60bc830
--- /dev/null
+++ b/archive/ES_0.5652258322363258
@@ -0,0 +1,22 @@
+archive/ES_0.5652258322363258---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T16:46:16.507
+Launch V∞: [6.231850605336456, -7.715224946375363, 0.3345445762035339] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00021777843534460646, -0.001516547672324408, 0.0018567771541919593] km/s
+ V∞_out: [-0.001668108647216327, -0.0013581576074285385, -0.0010765972135510682] km/s
+ time of flight: 1.822077458108814e8 seconds
+ arrival date: 2029-02-09T14:02:01.507
+ thrust profile: [0.21018060626109708 -0.06990947720615247 -0.08987164595816362; 0.06706354992155575 0.008051781395062794 -0.08928871387602363; 0.10636104526452986 0.032062546385082435 -0.22334311039677268; 0.04052374636363153 0.015106883808335518 -0.12496587067629804; 0.030924274912041444 0.012887877748941708 -0.11886031908448584; 0.01861358561674541 0.00819357575677384 -0.08782552041239525; 0.014948964352148514 0.00710559441088218 -0.08223419634666093; 0.008273994321299799 0.003494172600378706 -0.04887363331971062; 0.009567689793693395 0.004968263089530965 -0.06560012014397049; 0.002442340102799163 0.0011587512316010623 -0.017306539825535962; 0.00011052023872048288 -1.1446500481656632e-5 -0.0009130667576590926; 0.00012618864270101373 2.1267927015238154e-5 -0.0005785879374690726; 0.00028243828833076566 0.00034648445448001226 -0.0010339774980208567; -0.001110097051044998 -0.00011323710446756627 -0.0012565887676633625; 0.0003070418554033821 0.00010305117530206459 -0.0008726887335415594; 0.0001324144535718671 -0.00032839221395104806 -0.0005065420872449981; 7.121647572757818e-5 -8.304020574646028e-5 1.6424165067669078e-5; -0.0003725044305537986 -0.0008562219174788688 -0.00047649406571939547; 1.244993527558711e-5 -6.7660470296051e-5 -0.00041280679703950074; 0.00026688768156003144 -0.00012687682626844716 6.804942631123104e-5] %
+
+Mass Used: 85.00676586145846 kg
+Launch C3: 98.47257801387228 km²/s²
+||V∞_in||: 0.002407273497063206 km/s
diff --git a/archive/ES_0.565227323666669 b/archive/ES_0.565227323666669
new file mode 100644
index 0000000..fcb0e32
--- /dev/null
+++ b/archive/ES_0.565227323666669
@@ -0,0 +1,22 @@
+archive/ES_0.565227323666669---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T14:54:35.775
+Launch V∞: [7.671744839496231, -6.111084431404726, -0.182206201544168] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0002935756802558263, -0.00023653710218361898, 0.00017740981042808256] km/s
+ V∞_out: [-6.188477205854813e-5, -0.00041193818752439525, 1.6187063436796478e-5] km/s
+ time of flight: 1.6833985576964375e8 seconds
+ arrival date: 2029-09-07T23:58:50.775
+ thrust profile: [0.3524839453234105 -0.05140269878253945 -0.1211366222581303; 0.07865998404755999 0.03013393230090932 -0.08694219691200451; 0.0833412537249829 0.05572587264790501 -0.1555187421322303; 0.06529838116140224 0.05743204100979455 -0.17394399564338361; 0.04689294018189056 0.04938864620851576 -0.16380695743021365; 0.02277353561386218 0.027271926327210455 -0.10042581661722547; 0.009060625858272378 0.011464926707557176 -0.048221446032101156; 0.020254438434121794 0.029685219124361534 -0.12033251511876886; 0.007362732537119677 0.010798246951081449 -0.0466734271440538; 0.001736073209626949 0.0011676781531958671 -0.009214915796925483; 0.00011572626853304825 0.001271200724224584 -0.007063241115803941; 0.004090634230977305 0.005471609007540632 -0.006271284903059945; 0.0007941936372479193 4.5528276752614723e-5 -0.002662884348448875; 0.0018749985644098523 0.001458414331582163 -0.007017798392309494; -0.004057276779488037 -5.1424861285489544e-5 -0.002424205040299501; 0.002687700038781227 0.0037534956438665303 -0.003495670670484784; -0.0009712351749628224 -0.0007180216060871801 0.0035599331624681096; 0.00017476398441011428 0.0012077328230836832 0.00042691042826821166; -0.0008629391802189135 -0.007323922670120164 0.009729963172679832; 0.005325873630548224 0.008294234865926516 0.009860777551203055] %
+
+Mass Used: 98.06558896959041 kg
+Launch C3: 96.23422090997543 km²/s²
+||V∞_in||: 0.00041666619923293896 km/s
diff --git a/archive/ES_0.5652372416764279 b/archive/ES_0.5652372416764279
new file mode 100644
index 0000000..66aa2fb
--- /dev/null
+++ b/archive/ES_0.5652372416764279
@@ -0,0 +1,22 @@
+archive/ES_0.5652372416764279---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T17:20:05.540
+Launch V∞: [6.470670760156412, -7.395200940332589, 0.22502533212262274] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6887547282894614e-9, 2.2369733841982e-9, 1.3799759731845776e-8] km/s
+ V∞_out: [-7.444955814321868e-9, -1.0192007529961766e-8, -5.189235735646165e-9] km/s
+ time of flight: 1.871747577690876e8 seconds
+ arrival date: 2029-04-04T02:19:22.540
+ thrust profile: [0.2055563064493174 -0.045209871672312205 -0.05713843615972891; 0.09972357531746463 0.03977542993916564 -0.0895407198264872; 0.21733063170964848 0.1387705258388455 -0.30264553232274144; 0.021862427541473644 0.018792617053660147 -0.04704010136446584; 0.05742408497226715 0.05194014634745678 -0.12949597839933139; 0.021210293980070325 0.028668676151198117 -0.07491062663672333; 0.012846585663308544 0.02228651515117424 -0.05413497111714262; 0.005040269334805393 0.007492682407826237 -0.022608148043087355; 0.011376035201758809 0.017295294398099098 -0.04523491979013526; 0.003763985508610636 0.009870447508970596 -0.03616856252182326; 0.000655224146942715 0.0009695697881788809 -0.007253965612524064; 0.0031708334871955674 0.0016069894198162244 -0.00829041803098756; 0.0015005375406776638 0.0003041470399523455 -0.004400882552887139; -0.0033173005288213413 0.005699814425527795 -0.0041829284432493095; 0.004141125765726024 0.00024591955805179937 -0.008104906628001682; 0.006441357789035613 -0.0017222147484165374 -0.005439465233888628; -0.0014240363852351039 -0.0064978338278868075 -0.0046222837936440485; -0.0025494292473831996 -0.006455243340725542 0.0001225993254049011; 0.007198268400245641 -0.0034707253342039154 5.151865976166215e-6; -0.0001771381945038016 0.00025184467404048986 0.000716250683282336] %
+
+Mass Used: 95.88970358887218 kg
+Launch C3: 96.60921343433606 km²/s²
+||V∞_in||: 1.4081523749601935e-8 km/s
diff --git a/archive/ES_0.5652435141866625 b/archive/ES_0.5652435141866625
new file mode 100644
index 0000000..a009fcd
--- /dev/null
+++ b/archive/ES_0.5652435141866625
@@ -0,0 +1,22 @@
+archive/ES_0.5652435141866625---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T14:59:32.455
+Launch V∞: [5.966955201326111, -7.408299216230515, 0.0583177072635143] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.242891148241597e-7, -2.6421883492360343e-8, 3.334336563138705e-8] km/s
+ V∞_out: [-1.3097058685618476e-7, 1.130730511566779e-8, -1.4431360192705436e-8] km/s
+ time of flight: 1.8460630838472152e8 seconds
+ arrival date: 2029-03-04T06:31:20.455
+ thrust profile: [0.6918402833326789 -0.1656707906661921 -0.19722929862250402; 0.25714325486202866 0.0830429380403059 -0.22410482498449874; 0.04853364452862593 0.029434184777654505 -0.0769823550262162; 0.05755120826045176 0.04908720538193619 -0.1281115485586865; 0.034392134101332975 0.035812696761343174 -0.1001198592469836; 0.04691337787813727 0.05686727986550089 -0.16111077833525472; 0.00944156345647964 0.012588700513808077 -0.03964116573932702; 0.007188529867724694 0.01039356721709126 -0.033463737833153484; 0.005587423280561843 0.00934806636003675 -0.031356309797610074; 0.001805734973446417 0.0024073319139287196 -0.007249447384719292; 0.0016717544433307602 0.0010778476417652794 -0.0025407304367771762; 0.00012734422988551724 0.0029725872944360993 -0.006915933066930091; 0.0006144493600841352 0.0007312194314215961 -0.0036784935264080445; 0.0005186342501740404 -0.000859352833286784 -0.0006293304098255129; 0.002285492251160119 -0.0004795792564590128 -0.004864900569053117; -0.006353349705192619 -0.00313051037707224 0.0016298964225484845; 0.0033301677498278268 0.004835465187968334 -0.0003387207172804675; 0.00019243426186325404 -0.00014660085881042922 -0.0016861078613013094; 0.001812380527361764 -0.0020322112311998305 -0.0006077124285155334; 0.0026278619191342934 0.004827385389020597 0.007389903613199416] %
+
+Mass Used: 131.5874596780195 kg
+Launch C3: 90.49085260681487 km²/s²
+||V∞_in||: 1.3136848945879443e-7 km/s
diff --git a/archive/ES_0.5652458952246794 b/archive/ES_0.5652458952246794
new file mode 100644
index 0000000..3fcc7a1
--- /dev/null
+++ b/archive/ES_0.5652458952246794
@@ -0,0 +1,22 @@
+archive/ES_0.5652458952246794---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T06:37:09.211
+Launch V∞: [6.278394166213676, -7.236703262087256, 0.036905412351746235] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.030590913218541835, 0.0009146350723170842, -0.02090814525265122] km/s
+ V∞_out: [0.03535092257081892, -0.0003561668164054079, -0.010877631807819471] km/s
+ time of flight: 1.8749577821569425e8 seconds
+ arrival date: 2029-04-05T08:46:47.211
+ thrust profile: [0.5439443342497728 -0.1260475703157938 -0.1543988864865852; 0.28370541959235207 0.09857918382597824 -0.24271423332009656; 0.11678770167858535 0.076007060942437 -0.17379597565521662; 0.0516082083696797 0.045662291935636506 -0.11048165538536746; 0.035152804066851534 0.03764773997793786 -0.0969696161112909; 0.03169464463365778 0.040341738572242124 -0.10801443351353356; 0.012013814321765301 0.01744850004540646 -0.04966708958163336; 0.002486945232937354 0.0038243998412041736 -0.011910734575958865; 0.0013121819012920637 0.002414951739660154 -0.008229244016100729; 0.0005231967992047927 0.00031963579737551834 -0.0030267669709125892; 0.0006922452824230991 0.0018511758712555294 -0.004741523993993739; 0.0012261589280887376 0.0013420992870855233 -0.0034038306715169033; 0.0018909137146163554 0.0013655467207891066 -0.002264352556412134; 0.00046620669077832065 0.0010885028609211693 -0.0021289897751909366; 0.0012796409293886987 -2.2704325162106352e-5 -0.0007114787481272734; 0.0007024830325521427 0.0012740004087195443 -0.002079188048469246; 0.000329573804349508 -0.00034348296989292714 -0.0048050442643748515; 0.0021272418619120454 -0.000526955832196907 -0.005982477349071256; 0.0008986032002339463 0.0025682319971742284 0.0008931967937271499; 0.00111994195495266 -0.0010412108731394985 0.001294918038008418] %
+
+Mass Used: 124.01497281614456 kg
+Launch C3: 91.7894694193111 km²/s²
+||V∞_in||: 0.03706468759838442 km/s
diff --git a/archive/ES_0.5652466156064215 b/archive/ES_0.5652466156064215
new file mode 100644
index 0000000..d3b8f3b
--- /dev/null
+++ b/archive/ES_0.5652466156064215
@@ -0,0 +1,22 @@
+archive/ES_0.5652466156064215---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T00:44:29.609
+Launch V∞: [7.5440183307691955, -6.364327100877076, -0.26373638690493195] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.239284315915184e-9, 1.1911058025185633e-8, -4.635875791515353e-8] km/s
+ V∞_out: [-1.1042835999999815e-8, 3.6252863314032416e-8, -5.627536064137512e-9] km/s
+ time of flight: 1.6249915654271337e8 seconds
+ arrival date: 2029-07-02T19:23:45.609
+ thrust profile: [0.24245256513919075 -0.04971695225976795 -0.09103126295193086; 0.08875167751253193 0.027666313729579818 -0.10392175101637209; 0.10347121401153067 0.05669530832682906 -0.197337755021531; 0.06143065827970566 0.04390466389671683 -0.16773003449425733; 0.039287831233967535 0.035773045352339335 -0.1448902430027528; 0.025714067771936088 0.026358502528634985 -0.1190090714020522; 0.01904163355899578 0.021705944072027705 -0.10143196029029605; 0.006801946467161474 0.00909251913750445 -0.045162837279879804; 0.009097518308490636 0.014746491465426096 -0.07531460288592877; 0.007050235360577596 0.00913933346928693 -0.05090182444216531; 0.0004170439882335337 0.0005920264337209749 -0.0025827949973356345; 0.00027324282627642503 0.0004275964591668825 -0.0024434911292889306; 0.00044062104382001563 0.0006840055126279946 -0.003812320534528857; 0.00048432218571505805 0.00023877015618211446 -0.003164512066523208; -0.00014035831636365466 0.00044797642761375825 -0.0007045478204317512; -1.7731647466170302e-5 0.0005244592399731669 -0.000874020031964297; 0.00011293919846989205 -0.0004614666177067614 -0.001443611641717175; 0.0024288942048974445 0.002363282101307617 -0.00012265212476738003; 0.0002281931612617391 0.0012741558237738299 -0.0018359591920556874; 8.325571268782316e-5 -0.003629989585885034 0.0023079887921939367] %
+
+Mass Used: 90.7835496024718 kg
+Launch C3: 97.48642890371771 km²/s²
+||V∞_in||: 4.8269414824399664e-8 km/s
diff --git a/archive/ES_0.5652543058932085 b/archive/ES_0.5652543058932085
new file mode 100644
index 0000000..6ff2b1a
--- /dev/null
+++ b/archive/ES_0.5652543058932085
@@ -0,0 +1,22 @@
+archive/ES_0.5652543058932085---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T09:35:11.748
+Launch V∞: [6.4418014842467555, -7.4557210184405704, 0.11329270020330945] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.152045563140129e-6, 3.3003159076438434e-7, -5.711690925394931e-9] km/s
+ V∞_out: [-3.8667403964204975e-7, 9.16213749793056e-9, 1.967547330695801e-6] km/s
+ time of flight: 1.8749577787454548e8 seconds
+ arrival date: 2029-04-11T11:44:48.748
+ thrust profile: [0.3366579640207298 -0.09621902556933697 -0.12396744451120366; 0.029514878523375664 0.006264078801438877 -0.0366427815347443; 0.05364644820168356 0.021264796262683967 -0.10526795242462854; 0.030745822679110194 0.018019169488129563 -0.0865598584995188; 0.02584123941599064 0.016190918009969472 -0.09175671599879738; 0.029497726589188415 0.0213187296643984 -0.12686412011380413; 0.012627165993959376 0.009980062817739098 -0.06567342315721772; 0.026919084756016922 0.0207536061563467 -0.1469445972454237; 0.003585582667142137 0.002919269564394769 -0.031022257161612124; 0.010357134842487457 0.008204320712281658 -0.06821460177845942; 0.0021654386210405788 0.0002714542992779505 -0.018280032813432465; -0.0014159095118619336 -0.0007265637600788134 -0.0036402067780397576; 0.001102663423164794 0.0011800624111575088 -0.006203213717130694; 0.0009040393040057665 0.0010715031421642917 0.0008364731200151973; -0.0006606732350949735 -0.0003544904917098242 0.0018273891451546075; -0.0007015768029130099 0.0097891097930223 0.0007033060094068832; 0.00874828027633245 -0.0031647282048979978 0.0009845141989052422; -0.00023581786989260666 -0.001747001121506992 0.0035599413988142673; 0.003394903285619888 0.005527221412393535 -0.0003195566069651226; 0.002838494407169942 -0.00254270881834286 -0.0008629859693407545] %
+
+Mass Used: 93.06175477352917 kg
+Launch C3: 97.09741750317956 km²/s²
+||V∞_in||: 2.1772123415383287e-6 km/s
diff --git a/archive/ES_0.5652602427932027 b/archive/ES_0.5652602427932027
new file mode 100644
index 0000000..d81bb59
--- /dev/null
+++ b/archive/ES_0.5652602427932027
@@ -0,0 +1,22 @@
+archive/ES_0.5652602427932027---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T20:08:07.173
+Launch V∞: [6.149902409005303, -7.507152667112172, 0.0941559471468744] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7530913521777872e-7, -3.644444586680503e-8, 4.7288411350142134e-8] km/s
+ V∞_out: [-1.829087965743618e-7, 1.6520345383261222e-8, -2.7541518534449442e-8] km/s
+ time of flight: 1.7807065359846172e8 seconds
+ arrival date: 2028-12-17T20:12:20.173
+ thrust profile: [0.4748577699231646 -0.15081260151806422 -0.16127269234001726; 0.12444300473192511 0.026907635560716323 -0.12551217477192664; 0.051669560698594866 0.024152631544625075 -0.08760889866760722; 0.0583209328173919 0.03738326012265471 -0.13542940494578556; 0.05648228961612916 0.04474301129654152 -0.16582953387140892; 0.028017550108347573 0.025502878778556618 -0.10156131536403251; 0.03608959185501274 0.036553084236575745 -0.1503452611660986; 0.005625289170923335 0.007005357122980661 -0.029716868498322252; 0.007690046802268024 0.009453405406529947 -0.04227626450491718; 0.0030636461312789614 0.0026279488391648806 -0.01862516487499087; 0.0014124018906482706 0.0021056886574996802 -0.012573389871489527; -6.531384682461293e-5 0.00046216062348416326 -0.0017239537901392523; 0.0003518045089336508 7.489845423284508e-5 0.0013353103183799202; 0.0019687783207523245 0.0008984608216956204 0.000882303710884188; 0.0012860520838276156 0.00161690808657381 -0.002616694968138237; -0.00018110586974051868 -0.0005505847120517896 -0.0029919951870020106; -0.0004914550681235494 7.503393333734327e-5 -0.0011693247162543872; 0.0066612759032570554 -0.0006592001906948516 -0.0012087818797523744; 0.004296479570585871 0.0036792118385831542 -0.007697709711333193; -0.004903774231039068 0.001671042307548967 -0.006497867167320278] %
+
+Mass Used: 110.04316405039299 kg
+Launch C3: 94.18750615000177 km²/s²
+||V∞_in||: 1.851963400647112e-7 km/s
diff --git a/archive/ES_0.5652693436459226 b/archive/ES_0.5652693436459226
new file mode 100644
index 0000000..dbd692e
--- /dev/null
+++ b/archive/ES_0.5652693436459226
@@ -0,0 +1,22 @@
+archive/ES_0.5652693436459226---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T16:23:43.288
+Launch V∞: [7.5819859649267585, -5.842598559076756, 0.10759997447982916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.258371205835529e-9, -1.5316116599463352e-9, -1.0698757235390145e-9] km/s
+ V∞_out: [-8.847543536278288e-11, -1.7565225052978576e-10, -4.537225880894482e-12] km/s
+ time of flight: 1.8535663829748803e8 seconds
+ arrival date: 2030-03-26T00:21:01.288
+ thrust profile: [0.5638139026190526 0.026544557022901875 -0.12672639393678012; 0.21721015221230716 0.1576280240064272 -0.1636471119022604; 0.0856040343791364 0.10603843541432466 -0.1305058651065359; 0.03355507124329585 0.058970711331007314 -0.08327902255996388; 0.03425370642622787 0.08094629739309524 -0.11953997362515484; 0.017253196097295607 0.05172845870880024 -0.08595376066476616; 0.017283349415022894 0.0581447845300523 -0.09753888201384232; 0.004116890779805144 0.015966700521973787 -0.03024285897336033; 0.0016225992339186288 0.002751329440402606 -0.004099338277882359; 0.0030481470009221683 0.002407896454205634 -0.012280636062558239; -0.0004476808898651025 -0.0013228917216411013 -0.008615447727485466; -0.00156434465164783 0.0022603052184963198 0.0017928911666871862; 0.0035979280359917207 0.0022514689192182687 0.0005994357947607335; -0.004355819329098885 0.006582296566969891 0.0006499699322057742; 0.002593541572922938 0.000755995451113509 0.003557925286899952; 0.003772505477028686 0.009463598431983376 0.00295519801610915; 0.0016189539448368813 9.56696966819204e-5 0.0020361871196508457; 0.0024893914689629454 -0.010979854697230822 -0.00040246197062956176; 0.0076666025985695834 0.011647775649572293 0.005495327204176174; 0.0006989163755736317 0.009533287932950319 -0.015572401090537098] %
+
+Mass Used: 124.9489609655252 kg
+Launch C3: 91.6340468493802 km²/s²
+||V∞_in||: 2.2525466548725825e-9 km/s
diff --git a/archive/ES_0.5652725782001254 b/archive/ES_0.5652725782001254
new file mode 100644
index 0000000..4acf0a0
--- /dev/null
+++ b/archive/ES_0.5652725782001254
@@ -0,0 +1,22 @@
+archive/ES_0.5652725782001254---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T13:35:46.394
+Launch V∞: [6.392851590389669, -7.341513530907547, 0.46716621570146943] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1358014120342298e-8, -3.376635553588639e-8, -2.3272713761892845e-8] km/s
+ V∞_out: [1.580596374207379e-8, -3.456546759827715e-8, -2.4470944621868307e-9] km/s
+ time of flight: 1.8569076242073113e8 seconds
+ arrival date: 2029-03-17T18:21:48.394
+ thrust profile: [0.4379267352976709 -0.1135245819426807 -0.12009354995585382; 0.12494800937983398 0.03782810598171346 -0.11817747279292445; 0.04215929408009378 0.023278762383211898 -0.06826388344673046; 0.033788687100067355 0.025669544608028377 -0.08038172490413958; 0.03287053323817287 0.03134358371336627 -0.09630547147106673; 0.019449560338210648 0.022917524971201805 -0.07342634645282338; 0.01920095235288769 0.023780460523165348 -0.08171810877479418; 0.03362477554000883 0.04584684968500881 -0.15742097022473497; 0.014210196554141777 0.02067299804090146 -0.07754320119749543; 0.005417476490124142 0.008375113596059969 -0.03450566447542567; 0.002215740871970569 0.0023676198444662878 -0.011379784672016054; 0.00031253109545338587 0.0025733117746836237 -0.0009657312111841796; 0.001728987306061441 -0.0005627300513774023 -0.0008301746576796637; 0.00029031118785052454 0.0002041619139325282 -0.0015742786465924525; -0.00038558601516019395 0.0026947315600607197 -0.005801764816543372; -0.0018547244637771559 -0.003441461876916464 -0.0015923973332460587; -0.00022530651242756434 -0.00047430578302346026 -0.00016025979083833161; -0.00037918136460627375 0.003895956194806559 0.004449307061010659; -0.0013016005315770484 0.00938988564756614 0.002638341490897056; 0.0020145284173393053 0.0027897133953575038 0.0019668721597951655] %
+
+Mass Used: 105.40774408316793 kg
+Launch C3: 94.98461665433916 km²/s²
+||V∞_in||: 4.62379794020416e-8 km/s
diff --git a/archive/ES_0.5652726904330798 b/archive/ES_0.5652726904330798
new file mode 100644
index 0000000..44e15f1
--- /dev/null
+++ b/archive/ES_0.5652726904330798
@@ -0,0 +1,22 @@
+archive/ES_0.5652726904330798---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T12:27:12.505
+Launch V∞: [6.587453714778532, -7.321170222736059, 0.06798024537033746] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7949398308269136e-9, -1.9990448892172868e-9, 2.386727349952705e-9] km/s
+ V∞_out: [1.2281457090789187e-9, -2.6210914001468578e-9, -3.708551056554441e-9] km/s
+ time of flight: 1.8749577787483457e8 seconds
+ arrival date: 2029-04-07T14:36:49.505
+ thrust profile: [0.24899639241077812 -0.05013802503095233 -0.0738657723612692; 0.08278535407316341 0.02912707424895367 -0.08267521676905264; 0.08491120186954143 0.05953267945082037 -0.1454090755070826; 0.0612470005504358 0.05725795645182288 -0.14918692025038108; 0.0414547840709383 0.04835359477342316 -0.1332573982430779; 0.03827685355589039 0.05145603755968222 -0.1421566321685534; 0.013292523890436808 0.01949788857915944 -0.06302673524795599; 0.010872950594037789 0.018909491224925842 -0.05117935365246766; 0.0008320274739191409 0.004210817486879819 -0.013216607825686665; 0.0024329731373878005 0.00439487787359898 -0.007404983467730357; 0.000668260162187948 0.0011868498790897932 -0.0012200550934124508; 9.707474326070987e-5 0.0008902877197976798 -0.0017390298017410898; -0.002409584723845064 0.00047841282982483363 -0.0020847455816849956; 0.002059163183560569 -0.002185668108266214 -0.004623834998873569; -0.00425563675752247 0.01044964017260185 0.0011541924766334218; 0.0010742193163099495 0.00316912088107799 -0.007603580338407419; -0.0029707014939477127 0.012146433962364887 -0.006155163285004063; -0.0035691179556628515 -0.0032165198518210995 -0.001639625552980157; 0.0021840283930846895 0.006007723658695128 -0.01516676324793726; -0.0005582848321164003 -0.00025057417627597335 0.0025298524427168267] %
+
+Mass Used: 93.65904857300075 kg
+Launch C3: 96.99870118838726 km²/s²
+||V∞_in||: 4.183818419824263e-9 km/s
diff --git a/archive/ES_0.565286059609635 b/archive/ES_0.565286059609635
new file mode 100644
index 0000000..368fb82
--- /dev/null
+++ b/archive/ES_0.565286059609635
@@ -0,0 +1,22 @@
+archive/ES_0.565286059609635---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T22:19:53.213
+Launch V∞: [7.988242072384396, -6.136743937127558, 0.13909477148794322] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000722418877416963, 0.004104622841716175, -0.00687063513087425] km/s
+ V∞_out: [-0.0026772964801814662, -0.0022375611092277092, -0.0017587369517585345] km/s
+ time of flight: 1.8525859998236772e8 seconds
+ arrival date: 2030-04-03T03:03:12.213
+ thrust profile: [0.08059184542275102 -0.008605178194323562 -0.03524953883772876; 0.04289745581089866 0.011899413854085023 -0.06353975029851931; 0.06567144448857493 0.02708259985274456 -0.16379746416169227; 0.028184781621341366 0.013830056880751264 -0.0990035919601012; 0.01577647043677322 0.0036482962593418246 -0.0775100295791379; 0.024190111867317458 0.009986849693082476 -0.12175961170878716; 0.011888204001741587 0.002993439438032184 -0.06211274042841895; 0.013135501158700016 0.004911420703069978 -0.09444453455970261; 0.002340704427096998 0.001155798601241886 -0.04109169050750235; -0.00010913611602385938 0.001826499826865855 -0.012356156152088085; 0.0012634940159711142 0.000942160889078144 -0.006781930270156799; -0.0006503076446184378 0.00048631101078151453 -0.006993311071807642; 0.0026933973319200784 0.0005707551070614288 0.0013098119114508208; 0.0006853767884122972 0.001216167314745018 -0.005247649223327992; 0.0021016020242639356 0.0023988458990130256 -0.0002539478579637604; 0.002292837650105782 0.0002739694402897636 0.0006636208942377396; -0.001804981266140693 0.0007564652547552685 -0.00045397726880425093; -0.0011780857199761615 -0.0006375974546955188 0.010347297528263417; 0.004544074375100427 -0.0012871583339337806 0.0015448454406063808; -0.003364194434561334 0.0005132804904531693 -0.003056594728855845] %
+
+Mass Used: 67.46965755592828 kg
+Launch C3: 101.49098491233927 km²/s²
+||V∞_in||: 0.008035884818039017 km/s
diff --git a/archive/ES_0.5652933997638618 b/archive/ES_0.5652933997638618
new file mode 100644
index 0000000..a6dafed
--- /dev/null
+++ b/archive/ES_0.5652933997638618
@@ -0,0 +1,22 @@
+archive/ES_0.5652933997638618---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T23:39:05.357
+Launch V∞: [6.361902547769098, -7.382460061118089, 0.1277682529725017] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007276589645917352, 0.0032253915727337625, -0.008100045065928714] km/s
+ V∞_out: [0.007418360660585972, 0.0030261802684442623, 0.008042797737438868] km/s
+ time of flight: 1.874957778623691e8 seconds
+ arrival date: 2029-04-07T01:48:42.357
+ thrust profile: [0.351875712747304 -0.06880726196007221 -0.08638610570650714; 0.12575453462430353 0.051741170207525944 -0.09992614566707027; 0.08597292111210307 0.06424914521174982 -0.11296621144953349; 0.051400764582301854 0.055626068639728715 -0.1018870649963087; 0.06261241965283497 0.07998933417051488 -0.1564267174522776; 0.04734629863626617 0.07376824700999349 -0.14154709635192092; 0.031743441013028055 0.059928459391322804 -0.11834231731507627; 0.0059369901599415935 0.012059440152182781 -0.027925580540837252; 0.0028995367457780416 0.006824212082568317 -0.01621424334407478; -0.001464003803943847 4.661347073938154e-6 -0.009281006001972866; 0.0006900005747125346 0.0001303688917209092 -0.0028094214745709375; 0.0027072844854692086 0.0021442545451404002 -0.000817803413398076; 0.007541397006590681 0.0030397144036639783 -0.0029561855623824597; 0.0008160309118132787 0.0007682618596472047 -0.00043278121418062476; -0.00397435460699821 0.00267876260026761 -0.00123178790719003; -0.0023474296472634033 -0.000508855897740691 -0.002094438264546732; -0.005724813091441939 -0.0059534856071737615 -0.006087468417471621; -0.0008328491787398786 0.000292103800760892 -0.0031076800912930034; -0.0028269462210862486 0.0008602031373920165 0.0030507715513712393; 0.00074583437832959 0.00017061961095167293 0.001378138834413807] %
+
+Mass Used: 105.3957020957755 kg
+Launch C3: 94.99084530778228 km²/s²
+||V∞_in||: 0.011356171790819726 km/s
diff --git a/archive/ES_0.5652939140783093 b/archive/ES_0.5652939140783093
new file mode 100644
index 0000000..7b33aee
--- /dev/null
+++ b/archive/ES_0.5652939140783093
@@ -0,0 +1,22 @@
+archive/ES_0.5652939140783093---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T16:22:55.230
+Launch V∞: [6.315859186761994, -7.375905988002819, 0.2432728233926148] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.018716796616308908, 0.0005804595313474872, -0.012074372623476892] km/s
+ V∞_out: [0.021437497057295567, -0.00020780855376709023, -0.006093192670383462] km/s
+ time of flight: 1.8397863191237935e8 seconds
+ arrival date: 2029-02-24T01:33:26.230
+ thrust profile: [0.41701284681352535 -0.10361609871395443 -0.10596320470834296; 0.11211740736565746 0.039212741186442 -0.0997484314041141; 0.1318928747525347 0.08410024122564526 -0.18142915232554524; 0.08779752423436803 0.07762393084307846 -0.17344877324613006; 0.03042298057013668 0.03258303911658534 -0.08082955450558703; 0.022748340556410434 0.028829824146385682 -0.07502893678637573; 0.02729170785801186 0.039108921029012256 -0.10363729171477103; 0.007840976278384046 0.013147840266095546 -0.03769675588239281; 0.007672469980147978 0.013656493521923507 -0.040002541592517794; 0.0061269440045136165 0.012623136048504771 -0.037984878674444535; 0.0007343678044155915 0.0015157013944598178 -0.004900490180825211; 0.00023607251058327676 0.0004844439304632149 -0.001116407125715797; 1.5966688831160585e-5 -0.0014498410303372474 0.0013607266756061878; -0.0003976112602776705 -4.326451425424888e-5 0.002126557876726434; -0.0002127524105347391 0.0007888225068983295 0.00031193453357744594; 0.0002862905541558525 -0.0013831032916563684 0.001898390281988576; 0.002967756471023107 -0.004913530151158257 -0.0003742377053562746; 0.00018199155992507934 0.0037699131321072277 0.0019546209215162624; -0.0011121065869705076 0.0007299761593114744 0.0005209131272753689; 0.00010946049214766287 0.0016996839081735962 0.003167524272104887] %
+
+Mass Used: 109.11561930615926 kg
+Launch C3: 94.35324807746314 km²/s²
+||V∞_in||: 0.022281065573584512 km/s
diff --git a/archive/ES_0.5653179942911326 b/archive/ES_0.5653179942911326
new file mode 100644
index 0000000..e9af47b
--- /dev/null
+++ b/archive/ES_0.5653179942911326
@@ -0,0 +1,22 @@
+archive/ES_0.5653179942911326---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T18:51:27.594
+Launch V∞: [6.448732732098999, -7.368072677535572, 0.24347683133816253] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9207927852698942e-8, 6.000045604178065e-8, 3.299732965309467e-8] km/s
+ V∞_out: [-1.992096988478666e-8, 3.6806658508769834e-8, -6.228726748505258e-8] km/s
+ time of flight: 1.825185598908082e8 seconds
+ arrival date: 2029-02-07T06:27:26.594
+ thrust profile: [0.3368827743761706 -0.08992740509230242 -0.10751715711203705; 0.11454366940514761 0.031629389228601125 -0.10967416260943644; 0.06442492075695591 0.03579235142463199 -0.10255097891379471; 0.05456045174475742 0.04181080125316135 -0.12276685962103362; 0.08050915666841142 0.0776178419919161 -0.2388090538143359; 0.028691547664712845 0.03021599708921165 -0.09863566253965232; 0.018808552928263694 0.022622684472860893 -0.07838070064301773; 0.003585640624500012 0.00473575462983166 -0.017542380676220364; 0.007318746662533251 0.009949249669114518 -0.03926563113079754; 0.0009244962627590716 0.002899856335235188 -0.006174778631380102; -3.855104000375265e-5 1.735607117102876e-5 -0.007539543294491997; 0.0016825196778982184 0.0014215496282005437 -0.0057150025185894356; -0.0008960201597747949 -0.003713655542133411 -0.0017807638532378503; 0.0017808844341710129 0.0027322129763217135 -0.005354632842468374; -0.0023966820575863235 0.0018992326323392593 -0.0032563662998246834; 0.0004152280094516847 -0.002828215891499914 -0.002532651726849542; 0.007570624047100122 0.005932593861479759 -0.0038622380605540406; 0.0031538876370732615 0.0004618846388496302 0.00013194213656009138; -0.005649756974884335 -0.0013966698483200322 -0.005831003853946495; 0.0004948656695557024 -0.005056806283205581 0.0032415826891742505] %
+
+Mass Used: 99.92306951279807 kg
+Launch C3: 95.93392979888972 km²/s²
+||V∞_in||: 7.444448628948365e-8 km/s
diff --git a/archive/ES_0.5653295486627805 b/archive/ES_0.5653295486627805
new file mode 100644
index 0000000..5d2d7d4
--- /dev/null
+++ b/archive/ES_0.5653295486627805
@@ -0,0 +1,22 @@
+archive/ES_0.5653295486627805---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T06:39:37.788
+Launch V∞: [6.356584191468404, -7.581998693106673, 0.0801103144049952] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.109952210691476e-10, -1.5553063861721588e-9, -9.750435588137737e-10] km/s
+ V∞_out: [4.5163054668829395e-10, -1.0075745212436521e-9, -1.4006701964340001e-9] km/s
+ time of flight: 1.8386383958676606e8 seconds
+ arrival date: 2029-02-27T07:56:56.788
+ thrust profile: [0.20199071254643605 -0.057223465329891664 -0.07463484192313721; 0.08861914732628877 0.02170064594240203 -0.09615899673806014; 0.06099274986523803 0.027134825772028588 -0.1183060094017254; 0.058982288515833044 0.035930057630091536 -0.15291321175968414; 0.035171338740658635 0.024682464097568035 -0.11298636242488787; 0.0342789342816814 0.028260102422087655 -0.1291635090490212; 0.01516104392869845 0.01445040141422973 -0.06753560339091416; 0.01668368749220335 0.016205631474471033 -0.08777774662360793; 0.0058370846604736204 0.006651831352232093 -0.03503457489204254; 0.003113573510370594 0.0041157021653026055 -0.023427602189705153; 0.001031392847146834 -0.004078919634440609 -0.005984999601535528; 0.0025248745416672344 -0.0024315707629740287 -0.011620685049537272; -0.0018323019805199705 -0.0019458181813111234 -0.004891224550298922; 0.003683277574880042 0.003003680516847516 -0.004302242547057938; 0.006676035298972947 0.002555975159906871 -0.003971729190332203; 0.0007185354655856066 -0.007229252577176229 0.0027326185950236953; -0.004766005306617062 -0.005227214436361807 0.005142209201814933; 0.0075472947095514015 -0.0023026880576695772 -0.0019123548068828641; -0.0007193790292233781 0.0014026995820166704 0.001775231348265619; 0.0009791743433941627 -0.00029750537737045237 -0.0035551379582584603] %
+
+Mass Used: 88.47198094341093 kg
+Launch C3: 97.89928442797138 km²/s²
+||V∞_in||: 2.0492926070385738e-9 km/s
diff --git a/archive/ES_0.5653321066029318 b/archive/ES_0.5653321066029318
new file mode 100644
index 0000000..cc8d77d
--- /dev/null
+++ b/archive/ES_0.5653321066029318
@@ -0,0 +1,22 @@
+archive/ES_0.5653321066029318---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T10:45:45.011
+Launch V∞: [6.133712106150652, -7.610232074386011, -0.10862228918428474] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0013617976698773835, -0.0009179037689017394, -0.0014631943087531534] km/s
+ V∞_out: [0.0014950867589293873, 0.0008224045466869091, -0.0013920995992155055] km/s
+ time of flight: 1.7592721224424902e8 seconds
+ arrival date: 2028-11-23T15:25:57.011
+ thrust profile: [0.386526985898585 -0.13505528842457215 -0.1448969885255599; 0.0780525492225787 0.015012854071218974 -0.08475200057847578; 0.06471360278366095 0.028199883535037436 -0.11639156178373432; 0.06237478410590715 0.03779536310704559 -0.1545191797301546; 0.053390234686578636 0.041031371578819975 -0.16796881712001338; 0.031281159524798874 0.026797695028905406 -0.11926470494360472; 0.018582906931474276 0.017416689634167544 -0.08272103053501671; 0.006651402703792067 0.006728161232196794 -0.033313898523537354; 0.0008336374099197344 0.0011751544237948233 -0.00471552148573914; 0.009522274672682329 0.01111326541232749 -0.06671776582512932; 0.010809509654192074 0.01461667059986184 -0.07684605534997523; 0.0006107151809539227 0.000758304499390646 -0.0038066863379766108; -0.0014404888746326985 0.00016640433929737735 -0.00117756373820466; -0.001638788554158917 -0.0005739935134463766 -0.00395338510672043; -0.0015542697110245435 -0.00016851631004611873 -0.0025951523994183785; -0.0009131957070186944 0.0008737272119038382 -0.0008581749974417088; -0.0002204075462050476 -0.0013600113795500138 -0.0022558845135282743; -0.0009556651907905377 -7.911797343291519e-5 0.000163860773131476; 0.001145448533326497 -0.00026977258039956537 -0.0012349766861499477; -0.00013007353505298003 0.0002642429403939576 0.0005105611478970016] %
+
+Mass Used: 102.17996886840183 kg
+Launch C3: 95.54985522886031 km²/s²
+||V∞_in||: 0.002199540362852 km/s
diff --git a/archive/ES_0.5653423639682773 b/archive/ES_0.5653423639682773
new file mode 100644
index 0000000..d049c54
--- /dev/null
+++ b/archive/ES_0.5653423639682773
@@ -0,0 +1,22 @@
+archive/ES_0.5653423639682773---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T09:00:32.238
+Launch V∞: [6.719689724107299, -7.219624661218872, 0.2582138537692281] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.667069811562496e-9, -1.0536993679280932e-8, -5.4645806856533463e-8] km/s
+ V∞_out: [3.8250852481371724e-8, 3.7132683171442275e-8, 1.8480382270752133e-8] km/s
+ time of flight: 1.8595697905781683e8 seconds
+ arrival date: 2029-03-18T15:43:31.238
+ thrust profile: [0.22859907243888863 -0.05815297315818799 -0.07272612167828718; 0.10774131123347933 0.032785927121727794 -0.10417262011510847; 0.15113464734915713 0.08829307521447473 -0.2382903033246215; 0.06102494629836063 0.04865032636591255 -0.13942835913556298; 0.028192272761761304 0.027415403248049915 -0.08408438950108407; 0.022186859962243816 0.02520137494022547 -0.08128301080802534; 0.022982196755487745 0.02992398444229396 -0.10079514825328273; 0.007719476061682236 0.011695295363515516 -0.04179427358935738; 0.003476408567178109 0.005579315582324385 -0.022900992473363586; 0.0006565286147920363 0.001043206283939144 -0.004207943410376391; 0.0001447067888465729 0.0011646815016929624 -0.005251595730068257; 0.0005131338747488604 0.001085894587659406 -0.004784572939285186; 7.434997659513473e-5 0.00025406748211677344 -0.0003944660845026859; -0.0007116194359366014 -0.0005096738203984774 0.0021691153202260593; 0.00015143035235728433 0.0007619399919260454 0.00019010285728091525; -0.0002489884536055288 -0.0007604230677613837 0.0018199777703439585; 0.00023478876198037267 0.00014105195549663635 -0.0013949820187659483; -0.0004633490926697996 -0.0006961064267600313 0.002871560714814561; -0.00019848095890050117 -4.77108683508357e-5 0.00030693273713014533; 0.000680439546217296 0.0008466134731797374 0.0012941251522655187] %
+
+Mass Used: 91.72676427964097 kg
+Launch C3: 97.3438846314313 km²/s²
+||V∞_in||: 5.605035470602317e-8 km/s
diff --git a/archive/ES_0.565345519821593 b/archive/ES_0.565345519821593
new file mode 100644
index 0000000..0aed537
--- /dev/null
+++ b/archive/ES_0.565345519821593
@@ -0,0 +1,22 @@
+archive/ES_0.565345519821593---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T17:46:20.194
+Launch V∞: [7.8386011592321445, -5.478270788688764, 0.2845121463717499] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.555939334178074e-6, -8.858924373787059e-5, -1.528190068843021e-6] km/s
+ V∞_out: [-8.674837443395059e-5, 1.2961187724818754e-5, -1.8951145289719446e-5] km/s
+ time of flight: 1.8496974246238098e8 seconds
+ arrival date: 2030-03-19T14:15:22.194
+ thrust profile: [0.8047687180508053 -0.008049667367060885 -0.19303024322122986; 0.08375497918690683 0.05200650534544874 -0.08057430219691086; 0.05146914459327079 0.053967212255010284 -0.09127434083191678; 0.04392334184195442 0.06202665987263236 -0.11579711769798136; 0.0330312197961651 0.0593629590806835 -0.12063313650049796; 0.021447112402417003 0.04647945433330354 -0.10468455547241695; 0.003272333685793283 0.009629986786409011 -0.023965644605721682; 0.004392262315024267 0.014604396069871375 -0.037203438083651307; -0.0003601925574087437 0.004776007245584439 -0.013852506109321632; 0.0038022865152116635 0.01825269563060473 -0.04911770348154885; -0.0007964392752056694 0.0063699489623815185 -0.018031332127026102; 0.001197418254157728 0.007360245951986027 -0.024123684859055926; -0.0006821735593985682 0.0013137063353119021 -0.001068957431656149; -0.0022602211632518775 -9.664508918668562e-5 -0.008158848042246536; -0.008750499216382523 -0.0029085138561665753 0.0003652928447047312; 0.006369854808771891 0.0006310126792662017 0.0008310726169184221; 0.000992363071686222 -0.0031233094680592046 0.004037728690304658; -0.000609228089606247 0.008769583472503867 -0.013575885351179689; 0.004285308452127905 0.009021277885251602 -0.0038040838611153203; -0.0006669546197076481 -0.003168814223028276 3.3639772205990796e-5] %
+
+Mass Used: 125.60938737182141 kg
+Launch C3: 91.5360661291492 km²/s²
+||V∞_in||: 8.861608442120423e-5 km/s
diff --git a/archive/ES_0.5653482436809578 b/archive/ES_0.5653482436809578
new file mode 100644
index 0000000..74e1a5f
--- /dev/null
+++ b/archive/ES_0.5653482436809578
@@ -0,0 +1,22 @@
+archive/ES_0.5653482436809578---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T05:32:19.702
+Launch V∞: [6.381023318769254, -7.319820288011548, 0.13819077145984698] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.919379836134652e-9, -1.61692408001842e-10, -5.127928847983032e-9] km/s
+ V∞_out: [-2.0544070705884477e-9, 4.664401583396943e-9, 5.831778001729628e-9] km/s
+ time of flight: 1.8749577787555432e8 seconds
+ arrival date: 2029-04-08T07:41:56.702
+ thrust profile: [0.4857128265004691 -0.10984013291355305 -0.15513626932073654; 0.08187075389109165 0.02349859673692297 -0.08477571459272987; 0.07714435383234937 0.04444278595141064 -0.13560785804953962; 0.05683493470116466 0.04347804676107108 -0.1399514666493799; 0.03872701723835507 0.03840141560645749 -0.1248801156772348; 0.02135396388902127 0.022654133065195606 -0.0851715782571837; 0.02257528275746401 0.02646917967182344 -0.1012982398123981; 0.010350879525939709 0.014380938111782824 -0.05914928145242534; 0.0021560325636807835 0.004486596166630619 -0.01341312016913623; 0.0028758719353456 0.003560006662693944 -0.009605697180031706; 0.0034990015115226297 0.0022132935250883615 -0.01109591750588705; 0.0015738184587969959 0.0038132229217998958 -0.013805330631467664; -0.0035607691295432703 0.0021291309028813286 0.0007505721281364413; 0.0036136862215096427 0.0005361188034585824 0.004247888571808994; 0.00033913876896440626 0.0014941292248035918 -0.001457960275875066; 0.002912733090717559 -0.002896295193839339 0.0012308833945088044; -0.0021327842338706637 0.0009889988852016555 -0.003643792365230854; 0.0006625639166414831 -0.0021671754307698225 0.009003085154659828; -0.002387153433180213 -0.0042603858067127316 0.0018622601932553728; -0.006314423499122243 0.0028277106244157147 0.020901082595347613] %
+
+Mass Used: 109.39439235323925 kg
+Launch C3: 94.31632433277912 km²/s²
+||V∞_in||: 7.833317071919119e-9 km/s
diff --git a/archive/ES_0.5653566122022405 b/archive/ES_0.5653566122022405
new file mode 100644
index 0000000..b84502f
--- /dev/null
+++ b/archive/ES_0.5653566122022405
@@ -0,0 +1,22 @@
+archive/ES_0.5653566122022405---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T00:15:19.279
+Launch V∞: [6.553601456210008, -7.300833878870676, 0.20046911846096116] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0199645876861854e-5, 9.637916158747019e-6, 8.980083213574823e-6] km/s
+ V∞_out: [1.4037355940132655e-5, 8.961621694942869e-6, 2.8810509316365914e-7] km/s
+ time of flight: 1.8749577787496874e8 seconds
+ arrival date: 2029-04-08T02:24:56.279
+ thrust profile: [0.3400859641956831 -0.08038660185193158 -0.10340172565273906; 0.08527268350377555 0.027238800689298927 -0.0835291226181628; 0.04685006098760613 0.02881612747377579 -0.07875534981423922; 0.03973838034479488 0.032167548110280046 -0.09197197083484092; 0.046764603016703335 0.04623524048272434 -0.13872157308865127; 0.02151575719907161 0.02553629683350744 -0.07890169950032748; 0.02109959721535286 0.042646501376580215 -0.13587012984179755; 0.008975485174530829 0.014597419658586913 -0.04578774207482133; 0.013480916533192356 0.01891698144224741 -0.0637563373817355; 0.005134551489436699 0.00907736517937528 -0.04574174649628477; -0.000844366242478765 0.004496500376232818 -0.018133738829804756; 0.002810988427588061 0.004025974751984876 -0.005616054016845157; -0.004287049534093657 0.0008638450853508396 -0.0009692505368447003; -0.0005809891310355784 -0.0002907537557471883 -0.0008294037862415563; 4.648525829046982e-5 -0.0002651144921909576 -0.003287970544940186; -0.0018930543728412194 -0.001024020308832639 -0.0020869465986561035; 0.01293065303337241 -0.0019396459569556404 -0.0018263971468793663; 0.006855936749468928 9.94078219341241e-5 0.0011872129887649644; 0.0012731160343030729 0.0019065108115100611 -0.016290099026368823; -6.136153634832259e-5 0.0005015590348813562 -0.0013427001377857828] %
+
+Mass Used: 97.8790586625123 kg
+Launch C3: 96.29205524116028 km²/s²
+||V∞_in||: 1.666025505264401e-5 km/s
diff --git a/archive/ES_0.5653707625121045 b/archive/ES_0.5653707625121045
new file mode 100644
index 0000000..2d7f418
--- /dev/null
+++ b/archive/ES_0.5653707625121045
@@ -0,0 +1,22 @@
+archive/ES_0.5653707625121045---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T20:28:14.949
+Launch V∞: [6.088568897952268, -7.615780410454521, -0.373122513220308] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.531829593716792e-10, 1.2423193262091976e-10, 4.675724315353559e-9] km/s
+ V∞_out: [-3.0553087700729317e-9, -4.395945472990462e-9, -2.2396471603198624e-9] km/s
+ time of flight: 1.8111227742484686e8 seconds
+ arrival date: 2029-01-26T01:26:11.949
+ thrust profile: [0.4869881978711412 -0.16272825764359813 -0.20213460085179294; 0.01856680458851358 0.0031202638282971477 -0.023226804410311355; 0.06559280314352928 0.024235352182887186 -0.1340833331717921; 0.05786993834989632 0.028900397697649266 -0.16505646418568415; 0.055835315464878355 0.033312825447326555 -0.20331513795746753; 0.03428695347214791 0.02312462417927876 -0.1509122220634198; 0.013554094254679832 0.010210916428276583 -0.07058056165607045; 0.005586526093832331 0.004484139931526355 -0.03335640894315471; -6.033306497140638e-5 0.0004956576152135178 -0.00674202955153884; 0.0005600297886305697 8.927072343005362e-5 -0.0034688494501587423; 0.0011873910856358143 0.002701840481772497 -0.008002736397975932; -0.000469443523589627 -0.0004828503838116596 -0.00037875155092722884; -0.0005093918229212988 -0.001086478661837785 -0.001956642839782296; 0.0006881996224558529 -0.0011593836795873477 0.004064740414194504; 0.0019149022904272899 0.0012251635684798507 0.0018646232447384315; 0.0021812849404410943 -0.006931644170251679 -0.00583025188457882; 0.0036921419559807736 0.005458284955151791 0.004344426249571992; -0.007712075212235162 -0.0027985976073632056 0.001861938614327038; 0.00010355417850986114 0.0001635056467298333 2.5431933369098395e-5; -0.0005276953910218041 -0.0011573055425870022 0.0029433350624052633] %
+
+Mass Used: 104.20753937518475 kg
+Launch C3: 95.21000289524636 km²/s²
+||V∞_in||: 4.754550726244642e-9 km/s
diff --git a/archive/ES_0.5653727559039341 b/archive/ES_0.5653727559039341
new file mode 100644
index 0000000..1edf5fb
--- /dev/null
+++ b/archive/ES_0.5653727559039341
@@ -0,0 +1,22 @@
+archive/ES_0.5653727559039341---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T15:31:57.834
+Launch V∞: [5.9932842052938895, -7.761560771572579, -0.03352456058351624] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.804817371139924e-6, 2.870929403751279e-6, -2.1959247879432604e-6] km/s
+ V∞_out: [3.148717462385653e-6, -4.327496587205086e-6, 2.7401171291741373e-6] km/s
+ time of flight: 1.710189004393013e8 seconds
+ arrival date: 2028-09-28T00:46:57.834
+ thrust profile: [0.37099478309901246 -0.14471817137044013 -0.1516206078069334; 0.04633399600731018 0.004550989142818871 -0.05541850771678684; 0.07179570543459302 0.021605922007103706 -0.13940346223728323; 0.05488826207537685 0.02421720109442472 -0.1477364890670328; 0.0537723202466698 0.02857455255292177 -0.17948142595072802; 0.04039511746905152 0.023620869571117455 -0.1639575836511267; 0.018230273449731778 0.011667325258566187 -0.08533580345262386; 0.01708584848604276 0.011587748469482894 -0.09006328986300383; 0.007802569485949448 0.005586301069691227 -0.04505415693384771; 0.004638372970807686 0.003378642215929489 -0.029213699512690355; 0.0006082304118860129 0.0005586908596295512 -0.0035689071651335575; 0.0002004628950857681 0.0002993881294937505 -0.0023973549007185596; 0.0001651898657117193 0.0004525331572907218 -0.0007793383130815424; 0.0005246738362982334 0.00034273322232002693 -0.002010703156609379; -0.00011220751717237656 -0.00018386695481251527 -0.0006315764357814346; -0.0003855758465426322 3.982925660722179e-5 -0.0007686681970175532; 0.0003793146789969915 0.0005269140958276829 -0.00020729147114523184; 0.00022054230499612008 -0.0012294641968425557 -0.00045965333295295543; 0.0011677263534771738 0.0012026662579992956 0.00023912532468449953; -0.0010318940764418834 -0.0013913480365810187 -0.000576857499710348] %
+
+Mass Used: 98.65418563224557 kg
+Launch C3: 96.16240507240185 km²/s²
+||V∞_in||: 6.012536177490767e-6 km/s
diff --git a/archive/ES_0.5653833365370812 b/archive/ES_0.5653833365370812
new file mode 100644
index 0000000..5691ad4
--- /dev/null
+++ b/archive/ES_0.5653833365370812
@@ -0,0 +1,22 @@
+archive/ES_0.5653833365370812---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T09:58:42.530
+Launch V∞: [6.300647174851247, -7.542525992683934, 0.00022958698376628143] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.861677919026451e-8, 4.962186111759525e-8, 7.846922431520244e-8] km/s
+ V∞_out: [-4.3577353270963104e-8, 5.867188093630881e-8, -1.0669160817699654e-7] km/s
+ time of flight: 1.7898229704987058e8 seconds
+ arrival date: 2028-12-29T23:16:59.530
+ thrust profile: [0.33060418621462584 -0.10446321164777204 -0.1249860117831298; 0.055140331391278385 0.009953614828349043 -0.06482578577127891; 0.05630947489220134 0.026902325394305995 -0.11595853933360284; 0.03691804005946569 0.02271645974276848 -0.10113477065325581; 0.05544254535754843 0.04159357671754032 -0.19217642781832947; 0.026949103299313264 0.02530189917403427 -0.12030596828780715; 0.02250163595230143 0.021643891675821134 -0.11415789975623486; 0.011348487016157306 0.010806612791704591 -0.06224091723836811; 0.010002581919459757 0.009007829122983958 -0.07248274751275784; 0.0023554484823843733 0.002664613573928556 -0.017275388747832257; -0.00020843229327601246 0.0008794802223570256 0.0001413757379524717; 0.0014721595506451488 0.0012130906505037732 -0.011923277119156198; 0.0007101144022294757 -0.00151454116043042 -0.0038891681447842863; -0.0030047403070189056 0.0003838094358270019 -0.0003962510168332141; 0.0005312943029823734 -0.0007005537176514811 0.0028177701052418684; -0.0003763430354226821 -0.0027240280249925166 0.005157675965318199; 0.0031175917444645892 -0.0016665847285225416 0.0031779233231423107; -0.0019173160352137044 0.006751136535268204 0.005111798110339939; -0.00044546215973883293 0.003932865170601335 -0.00027684803938506753; 0.0002035168311094728 0.0014954681966016883 0.0027304973482989324] %
+
+Mass Used: 96.18474881418842 kg
+Launch C3: 96.58785322498393 km²/s²
+||V∞_in||: 1.2834594586296666e-7 km/s
diff --git a/archive/ES_0.5653912136415178 b/archive/ES_0.5653912136415178
new file mode 100644
index 0000000..57cf02e
--- /dev/null
+++ b/archive/ES_0.5653912136415178
@@ -0,0 +1,22 @@
+archive/ES_0.5653912136415178---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T04:47:33.175
+Launch V∞: [7.914433076977376, -6.144545560258394, -0.15538906336301506] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.826199352901122e-7, 7.852183871212752e-6, -0.00015325981284144562] km/s
+ V∞_out: [-6.08010628689561e-6, 0.00015390882287109406, -1.5826695216958526e-6] km/s
+ time of flight: 1.8173296171745464e8 seconds
+ arrival date: 2030-02-19T14:10:14.175
+ thrust profile: [0.16017456537998329 -0.022842381507292592 -0.06965849309528782; 0.01818100691911554 0.00489410324190551 -0.03101446417636127; 0.02974988711074786 0.01190337318059769 -0.07937775588815929; 0.034597569729485765 0.014942796166433498 -0.12252798647125847; 0.027973335715458427 0.012248257535168549 -0.12470321350373825; 0.022917135977049346 0.009853743677145895 -0.12114955575827895; 0.014116977093225383 0.006277103976400598 -0.08974008719075452; 0.011513413596530415 0.00422891224130209 -0.08029467454545439; 0.007904069701464662 0.0005855961527697017 -0.04935043438260043; 0.00426104149066992 0.002055299432576872 -0.03337235401217408; -0.0009765575045561866 0.0022985354344839458 -0.007961281386627791; -0.001292402287621376 -0.004042497145469349 -0.00415290895516881; 0.0023331931894563273 -0.0031738328729420794 -0.009798528701179381; 0.001103142836929446 0.006571421357249358 -0.0023333914034601284; 4.133289823249342e-5 -0.00039354210964295117 -0.005891191063871686; 0.01205573003941951 -0.005100899034704593 -0.00429920008463998; -0.0021367910008975068 0.0019296682037285053 -0.0027821373044265582; -0.006815404755177241 0.0028435335228873286 0.006386801897513349; -0.005956265396734784 0.014669953496424627 0.0012254590708506287; 0.0016876417420258534 0.00018410675425738362 0.004751981212085103] %
+
+Mass Used: 73.85236772226835 kg
+Launch C3: 100.41783683305756 km²/s²
+||V∞_in||: 0.00015346282780434286 km/s
diff --git a/archive/ES_0.5653971644523668 b/archive/ES_0.5653971644523668
new file mode 100644
index 0000000..5e228bf
--- /dev/null
+++ b/archive/ES_0.5653971644523668
@@ -0,0 +1,22 @@
+archive/ES_0.5653971644523668---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:21:57.495
+Launch V∞: [6.574421672137035, -7.515028585357984, 0.05122691144841967] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.65356853599414e-8, 1.5199306931833602e-8, -1.798870100049718e-8] km/s
+ V∞_out: [5.896414421631339e-8, -1.9060399959960304e-8, 8.57562453301313e-9] km/s
+ time of flight: 1.8403859393408006e8 seconds
+ arrival date: 2029-03-01T13:11:50.495
+ thrust profile: [0.09853931948871106 -0.03118215992025294 -0.04219429926657606; 0.07739986715350365 0.011365147023898415 -0.09971522688035749; 0.026026364252763695 0.008705187005926108 -0.05768123016868441; 0.03596528455368839 0.01617448202806678 -0.1093697440013747; 0.02953579440467078 0.015419620508379995 -0.11364282663272803; 0.017725583478978117 0.010052625588370272 -0.08260555378498095; 0.015510403424789487 0.009582094716863483 -0.08503015784042951; 0.010652609620234241 0.006779132438101578 -0.06461178731267682; 0.03114373565436864 0.021124932505787855 -0.19867467542168527; 0.007632203224381518 0.0051106813281485055 -0.05561578239044293; 0.00060579739170432 0.000639897780165531 -0.007138896148368348; 0.0010214242934711844 0.0004956990830306166 0.0005655072162982604; 0.0010582356952695772 -0.0003821432199675048 0.001109418066843137; 4.070872203187654e-5 -0.00013884218076793997 0.00012175372096652514; -0.0004614594383335842 -0.0012832435729998484 0.004487903986271991; 0.0009524940865878512 0.00044386744922453997 0.005151290152698091; -0.0021612668515625304 0.0009815048726427617 -0.000904020096246231; -0.00044165170059585844 0.0006528229003123366 0.0004235846115665119; -0.0033175695786158707 -9.098146211319134e-5 0.002298937124879997; 0.0033186345307750654 0.001966173601398102 0.00016756413865659303] %
+
+Mass Used: 78.03911343785694 kg
+Launch C3: 99.7012991582693 km²/s²
+||V∞_in||: 6.124455905639019e-8 km/s
diff --git a/archive/ES_0.5653987857158209 b/archive/ES_0.5653987857158209
new file mode 100644
index 0000000..0dd6b1b
--- /dev/null
+++ b/archive/ES_0.5653987857158209
@@ -0,0 +1,22 @@
+archive/ES_0.5653987857158209---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T23:57:38.353
+Launch V∞: [5.948145327998948, -7.481254688291869, 0.18783963615870175] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.914601339624158e-5, -2.9862620671037016e-6, 5.120267142855487e-8] km/s
+ V∞_out: [3.746760515172692e-6, -8.47886159131236e-8, -1.9010319797597836e-5] km/s
+ time of flight: 1.797196163948309e8 seconds
+ arrival date: 2029-01-05T02:04:34.353
+ thrust profile: [0.6793889232591721 -0.18782807843903498 -0.17619489360132087; 0.12434586342247197 0.040097964716098486 -0.10332649757139545; 0.08923174543423085 0.0560518524327707 -0.12207464255249652; 0.04620141568538404 0.03843834024147925 -0.08515843139411554; 0.04952690389107524 0.05252373098842053 -0.12165864113119709; 0.03683750175392825 0.04584381136202994 -0.1087609937134314; 0.022730162973595817 0.0324465193837598 -0.08227973899438633; 0.029001442533562495 0.04602863177448441 -0.11372490152676866; 0.01609494865405571 0.029733845573626728 -0.07546468803404724; 0.006030773118338679 0.010784054572142016 -0.03136187637055717; 0.0008517379522829555 0.0016962481656596204 -0.005118466646393136; 2.5191277536181757e-5 3.875123206216089e-6 1.8299398467614694e-5; 0.0005655546688898238 0.0006782741839074357 -0.0007764194922028712; 0.00021564508074473386 -3.2529156400444895e-5 -0.0003601076234426317; 6.38616003921684e-6 2.6841894179758337e-5 -0.00013758612898706146; -0.00041217281380915584 -5.580043108037777e-5 -0.0004983211143716465; 0.0002189323444585101 -0.0005795029499280021 0.00017325636618184342; -0.000657109640640936 -7.288635879779706e-5 -0.00045863238964202274; 0.0001054069135740074 0.0003967529308436656 -0.00012116079089759485; -0.0004146622594528871 0.0007450742884803816 0.0007686956171226464] %
+
+Mass Used: 126.55340168430848 kg
+Launch C3: 91.38488828299701 km²/s²
+||V∞_in||: 1.937756981192549e-5 km/s
diff --git a/archive/ES_0.5653994344616884 b/archive/ES_0.5653994344616884
new file mode 100644
index 0000000..95589ff
--- /dev/null
+++ b/archive/ES_0.5653994344616884
@@ -0,0 +1,22 @@
+archive/ES_0.5653994344616884---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:15:13.780
+Launch V∞: [6.430535735664193, -7.447211006363647, 0.124602289028002] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3926091735087176e-7, 3.419260512938952e-8, -4.436648609734233e-8] km/s
+ V∞_out: [1.4461727141915262e-7, -3.825785675780887e-8, 1.8232718433152682e-8] km/s
+ time of flight: 1.8456322944575083e8 seconds
+ arrival date: 2029-03-06T05:49:02.780
+ thrust profile: [0.2817945929889097 -0.0806173353401246 -0.1020398764423566; 0.13067969125912426 0.02865580498967447 -0.1448817087551979; 0.030699429586691553 0.014953815912871808 -0.06286102380458822; 0.04481810579942814 0.027177118534091844 -0.12096898294442184; 0.018086305531411287 0.014701202185304187 -0.06537311527649523; 0.016532741184007528 0.014353776207640135 -0.07417028905614281; 0.05052388701012058 0.04042836092033122 -0.22125750214852768; 0.010680842521105148 0.013170343494201436 -0.07009691385570589; 0.008668447950640529 0.011355903328015586 -0.06479208880073933; 0.0017260918442281083 0.0027797036023673597 -0.014254414843507162; 0.0005252599424286359 0.001374256306632013 -0.001917855601294201; -0.002075106206987361 -0.0019410129475084617 0.0006012419153787517; 8.514592504311121e-5 -0.0014416227934617991 0.0016833750974026; -0.002079389302706952 -0.00033978312153472653 0.0027401594294705033; 0.0030577528677763056 0.0004692939958792785 0.004641296944003238; 0.004902081946929667 -0.00753187836495021 0.0023484614032523556; 0.0018240407127933925 0.0005204620108807173 -0.00010101030719275421; 0.0027472295300453595 0.005337489768968022 0.003960412293522429; 5.689330194938173e-5 -0.0007397133176337187 -0.0012717482216890944; -0.003586472884563879 -0.011054192171257388 -0.003876955787688524] %
+
+Mass Used: 94.80111398886675 kg
+Launch C3: 96.82826735138909 km²/s²
+||V∞_in||: 1.5010370560238132e-7 km/s
diff --git a/archive/ES_0.5654114845058504 b/archive/ES_0.5654114845058504
new file mode 100644
index 0000000..4b4cce2
--- /dev/null
+++ b/archive/ES_0.5654114845058504
@@ -0,0 +1,22 @@
+archive/ES_0.5654114845058504---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T21:26:54.855
+Launch V∞: [7.496844696106728, -6.257502876705621, -0.054764743096804916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003415309216814914, 0.002346709673938824, -0.001090521024089403] km/s
+ V∞_out: [-0.001830006640737154, -0.003264152147375318, 0.002088470775014334] km/s
+ time of flight: 1.6420080156487906e8 seconds
+ arrival date: 2029-07-21T08:46:55.855
+ thrust profile: [0.4393402962160066 -0.0649102803087462 -0.14821583224352874; 0.0845105038534408 0.03227743255441139 -0.09154851064656704; 0.06218443897905919 0.0422874754437195 -0.11560066572189505; 0.07811380540515542 0.07325062465736197 -0.1985835610516061; 0.059739518596629335 0.0683970195176195 -0.19787113255916988; 0.019628519928085068 0.02445166869030816 -0.08217961289392607; 0.023217326250800894 0.03447518382940623 -0.11964789589834676; 0.007998088595265608 0.012716727830331573 -0.050080593597938136; 0.0029969968602243345 0.005196789670573173 -0.024437679906368175; 0.0015469908111510325 0.004478442391311468 -0.014141103818308434; 0.010619667155496587 0.018804303755404792 -0.07336200772062489; 0.00226407753501997 -0.0013337489153585555 -0.004587124435690131; 0.0009765442840448694 0.0009148263902510316 -0.0020983466857909744; -0.000451615482205258 -0.00017232169075432702 -0.0001773877782736931; -0.00016110570476769796 -2.172105374866236e-5 0.0012578699132574636; -0.0004974940069299306 -0.0016297484443082294 0.00022796607917485587; 0.0023175505945189677 -0.0009687411722609222 5.90908286814192e-5; 0.00018245716940465308 0.0005001131637422248 -0.0004248666018860736; 0.0012372257185441875 0.00010778899374491561 -0.002106329972705388; -0.0017504249094129373 1.5139176118053116e-5 -0.0017179291200220318] %
+
+Mass Used: 103.36827126827211 kg
+Launch C3: 95.36202182660917 km²/s²
+||V∞_in||: 0.004284929339464067 km/s
diff --git a/archive/ES_0.5654141838767668 b/archive/ES_0.5654141838767668
new file mode 100644
index 0000000..99fb2ea
--- /dev/null
+++ b/archive/ES_0.5654141838767668
@@ -0,0 +1,22 @@
+archive/ES_0.5654141838767668---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T09:34:14.155
+Launch V∞: [7.8169385618354115, -6.126599973565273, -0.09229373629655448] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.0245632656620256e-6, 2.7143584495459853e-6, -1.950544125628373e-6] km/s
+ V∞_out: [9.875065084588064e-7, 4.4010689827801584e-6, -1.9909952098490268e-7] km/s
+ time of flight: 1.874957778153756e8 seconds
+ arrival date: 2030-04-29T11:43:51.155
+ thrust profile: [0.3547311784894423 -0.03303629478973681 -0.11551873142448983; 0.057273917645993294 0.019466595378860765 -0.08332105820453838; 0.03450125282749835 0.0184324297345502 -0.08887172142366735; 0.033381437250445775 0.019770911995622163 -0.12148696732346928; 0.016338903643603523 0.01028591320311694 -0.07533663771712337; 0.014598456688593676 0.009027132987705433 -0.08573294196311736; 0.008425261024436363 0.00546217233596777 -0.05763532727663861; 0.011976086279153683 0.006550951571521519 -0.08381822061594167; 0.004122915003723408 0.001963304310586741 -0.037616711789047214; 0.0051377467240278 0.003172591035077764 -0.04382683540455842; 0.0014169096696379452 2.3046176598243715e-5 -0.012687108695778713; 0.0013943875661614335 -0.0009897628183969099 -7.627885184283189e-5; 4.6395080420918425e-6 -0.00012795472393908777 -0.0004397787331626034; 0.0006588972325328307 -0.00011786570943900911 -0.001313666560348834; 0.0020250257881648157 -0.001995491647269921 -0.002547303679817716; -0.001027364522728179 0.0014456688308350607 0.0016785112403938766; -0.001043482425347843 0.0004130179374066481 0.0007870220235219128; -0.0001571326658825256 -0.0025210817841388035 -0.0007420122741776136; -0.0004787297491591864 0.0026901573047755463 -0.0030858804082496637; 0.0018186968390971274 0.0011979645062858957 -0.003513655467903273] %
+
+Mass Used: 84.20161706830004 kg
+Launch C3: 98.64827384935906 km²/s²
+||V∞_in||: 4.5078095708045585e-6 km/s
diff --git a/archive/ES_0.5654182453673648 b/archive/ES_0.5654182453673648
new file mode 100644
index 0000000..5f94ea2
--- /dev/null
+++ b/archive/ES_0.5654182453673648
@@ -0,0 +1,22 @@
+archive/ES_0.5654182453673648---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T06:38:17.071
+Launch V∞: [7.250058857840835, -6.375280947015451, -0.028019025862766056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8522739971541866e-9, 1.491235319985401e-9, -2.9520385115742193e-9] km/s
+ V∞_out: [2.3850445386031982e-9, 4.811413011560943e-9, 1.489733081821899e-10] km/s
+ time of flight: 1.6235635405171895e8 seconds
+ arrival date: 2029-06-29T09:37:31.071
+ thrust profile: [0.5555748700290416 -0.08018609667206093 -0.17506040084768942; 0.17578177444021686 0.0748761182325531 -0.17287589041844736; 0.09646451280767811 0.07138075421433407 -0.15846307518677602; 0.09078507255447729 0.08816667611141409 -0.22544303602245172; 0.0526346589323952 0.0687810057083646 -0.17553485208528358; 0.023645428171947796 0.03252549891835859 -0.09403754923735069; 0.007510528743999726 0.011209268087161535 -0.0359147612812586; 0.00888460924385908 0.015686950771646016 -0.05025273566100901; 0.01002058406091174 0.018207286996488794 -0.061384337416046195; 0.0011680443418240194 0.0021812012438297947 -0.008362378167076518; -6.544314785165661e-5 0.0005005129044130804 -0.0011927036817433602; 0.0017983791170099112 0.00389965590676224 -0.015423206764655202; 0.0010406107716159334 0.0007378444905729525 -0.0011442238594033068; 0.00024171475776762084 -0.00033044936171774 -0.0008576884296465335; -0.00010138078210707608 0.0009867637032349471 -0.0015379649369265348; 0.00024831659995327434 4.533657111647441e-5 -0.0006810627495428562; 0.00018990050086372182 6.960991441849182e-5 -0.0005859171891316268; 0.00039371657766383713 -8.083689456675242e-5 -0.0009002458063901843; 0.0012993339386181907 0.0006687554464802211 -0.0007031392912753771; 0.0006647807622083613 0.0006168072802377689 0.0010036536856262053] %
+
+Mass Used: 115.93926990408045 kg
+Launch C3: 93.20834566134488 km²/s²
+||V∞_in||: 4.367354016819705e-9 km/s
diff --git a/archive/ES_0.5654205234360743 b/archive/ES_0.5654205234360743
new file mode 100644
index 0000000..0362f73
--- /dev/null
+++ b/archive/ES_0.5654205234360743
@@ -0,0 +1,22 @@
+archive/ES_0.5654205234360743---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T05:29:50.477
+Launch V∞: [6.309063347949476, -7.659021388728032, 0.07374325805371858] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.525529120949306e-9, 1.1345474162628524e-9, 8.622280402994284e-9] km/s
+ V∞_out: [-4.86263899798679e-9, -7.1081314023732246e-9, -3.508908907650863e-9] km/s
+ time of flight: 1.7587504896942368e8 seconds
+ arrival date: 2028-11-23T19:40:38.477
+ thrust profile: [0.13710839614169112 -0.048880123673135906 -0.05510756346460855; 0.0965364463305801 0.014123377009900427 -0.10941707366043878; 0.05106804766903709 0.018323110128191065 -0.09638138673575945; 0.07008884657005097 0.034802228494981956 -0.1799479713552912; 0.061953884427797354 0.03757252914447317 -0.20389767582641646; 0.027998648922973077 0.018663626163965604 -0.1096233395734236; 0.022605983729035425 0.016504244413323085 -0.10252975677061113; 0.006096109816351866 0.005317274181605856 -0.03258248920859258; 0.00741181709954094 0.005839612495656164 -0.04123056549815613; 0.006023256108959858 0.005285238015671607 -0.037381508117144004; -0.00018418664671004817 -5.562886760598825e-5 -0.00328011194392897; 0.0017225180494930814 0.001838971652280183 -0.013422465740865398; 0.0013790517528016748 0.000678488780863321 -0.00903250754499926; 0.0010505181631069844 -0.0004343304892074891 -0.00665491309632989; 0.0007717293222442286 -0.002188386624877875 -0.0009725902774766005; -0.003083666286180032 0.0035790763098771756 0.0006104670604939526; 0.0020583503603617665 -0.00232161497139142 -0.0030080927320873165; 0.0006997897209359465 -0.0015616563256266012 0.0018358198370398687; -0.00011871113250586074 -0.00032905362847499096 0.0013180921348630455; -0.0028208196686278276 -0.007671703902819675 -0.0020185083982746294] %
+
+Mass Used: 85.24703633642912 kg
+Launch C3: 98.47032702954131 km²/s²
+||V∞_in||: 8.829391614741775e-9 km/s
diff --git a/archive/ES_0.5654301160814303 b/archive/ES_0.5654301160814303
new file mode 100644
index 0000000..94d2c61
--- /dev/null
+++ b/archive/ES_0.5654301160814303
@@ -0,0 +1,22 @@
+archive/ES_0.5654301160814303---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T17:32:46.855
+Launch V∞: [6.396651072017287, -7.507790183072163, 0.09292392822075614] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.15061784831946e-8, 1.6701681043853423e-7, 7.033671294131378e-8] km/s
+ V∞_out: [-6.285620085604105e-8, 1.0044703223788612e-7, -1.6033548796408473e-7] km/s
+ time of flight: 1.8749577787437528e8 seconds
+ arrival date: 2029-04-10T19:42:23.855
+ thrust profile: [0.2526705371972205 -0.05919301711872817 -0.07742319153891088; 0.09519672703721227 0.02844124498305664 -0.09529868696984606; 0.06326923224723353 0.03742306420678045 -0.11380652844389509; 0.03723607840685119 0.029678567870554524 -0.0930098358788261; 0.026928332289578395 0.026075241183584518 -0.08667028780510284; 0.03087565053371181 0.035047464102771465 -0.12295998440407238; 0.010570685273163337 0.015551108350562266 -0.0641751536846952; 0.015388539819457474 0.02461765171615734 -0.08898333356087862; 0.01089253776889454 0.02118721251300703 -0.08114838476542022; 0.007177043523622989 0.011000585362618009 -0.0470877343735676; 0.002507979527863688 0.005425693535632204 -0.02573346943930553; -0.0021258794489694534 0.00038561149803428873 0.0010718272738453219; -0.0005014992282837502 -0.0013830726499486135 0.0006055062918160032; 0.000942365535128074 0.0009806630252058145 0.0022371359877364147; -0.005217768385533344 -0.003404672835273276 0.0003675668148808602; 0.0010947212101755353 0.003466826602336489 0.000676180968983717; -0.006029344302436709 0.0046677855372687605 1.5656021348431446e-5; -0.004133357063971397 6.691382396113707e-5 -0.0019209060281935339; -0.0010910657576860211 0.00017393103915731948 0.0005397612496806871; 0.0032329082607720095 -0.0035630789341631105 0.007886705671336456] %
+
+Mass Used: 92.12775827310679 kg
+Launch C3: 97.29269322661062 km²/s²
+||V∞_in||: 1.987086442190788e-7 km/s
diff --git a/archive/ES_0.5654365796502374 b/archive/ES_0.5654365796502374
new file mode 100644
index 0000000..1f0dcdf
--- /dev/null
+++ b/archive/ES_0.5654365796502374
@@ -0,0 +1,22 @@
+archive/ES_0.5654365796502374---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T09:10:00.790
+Launch V∞: [6.2489242490261425, -7.576599242692235, -0.14024867936879326] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8490140904183698e-6, -0.0006104947928521046, 0.00041322362491744803] km/s
+ V∞_out: [0.00031678126723268333, 0.0006540183303977684, -0.000123267415338744] km/s
+ time of flight: 1.7544720800813156e8 seconds
+ arrival date: 2028-11-17T00:30:08.790
+ thrust profile: [0.28731038470687126 -0.0916425668752852 -0.10332980187950129; 0.12304936478002035 0.02659424471261762 -0.1313159982643997; 0.07554273019410965 0.035847682905637036 -0.13571446661617156; 0.051181189727229556 0.0322316313805295 -0.12434606585073851; 0.04172275275791469 0.03237866655145532 -0.12856112058283362; 0.024676756068775767 0.02104988157170581 -0.0892228767046493; 0.026143333414133954 0.023483293997944344 -0.1038936172987668; 0.01572555926973643 0.014590552705891671 -0.0694131395221379; 0.01636219123922634 0.01908959299290604 -0.09592827868362218; 0.01042984875267493 0.012840708058102012 -0.0652979379925914; 0.00017799887557329444 0.0002250627888989047 -0.0011366286350288468; 0.0001813214535768768 0.0003968066127356172 -0.0023955364061722098; -4.0806783243668574e-5 7.410627101130878e-5 -4.676781403634492e-5; 6.59261868033542e-5 1.9016240880707778e-5 -0.00031083800304007776; -5.317950954380957e-5 -8.51290316844524e-6 5.32244628503571e-5; -0.00019808604515341295 -5.9616973770107456e-5 -0.0001870093522530843; 0.00015418979785645478 7.376389811011594e-5 -0.0006400823489036271; -0.00021423740497184522 -0.00020887324113093395 -0.00035308279417097844; 0.00021258321516308062 0.00017048168639780193 0.00021221348208841454; -9.095117353858832e-5 -1.0691595242175818e-5 -0.00019933135316283556] %
+
+Mass Used: 96.9134593207159 kg
+Launch C3: 96.47358004649618 km²/s²
+||V∞_in||: 0.0007371981247551817 km/s
diff --git a/archive/ES_0.5654561364811311 b/archive/ES_0.5654561364811311
new file mode 100644
index 0000000..b391ee3
--- /dev/null
+++ b/archive/ES_0.5654561364811311
@@ -0,0 +1,22 @@
+archive/ES_0.5654561364811311---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T08:20:38.784
+Launch V∞: [7.812896770919729, -5.843576723930903, -0.10856273391275192] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8773434025103947e-8, 1.5746675222078294e-7, -2.9468799128001845e-8] km/s
+ V∞_out: [2.1523522269460283e-8, -8.31308993943018e-8, -1.3728667811747159e-7] km/s
+ time of flight: 1.754063777865118e8 seconds
+ arrival date: 2029-11-28T12:20:15.784
+ thrust profile: [0.4123336418978629 -0.03163547250585236 -0.13129491811231703; 0.12014546851973193 0.058636450156869135 -0.12366617008297702; 0.09002917279483846 0.07455885006022576 -0.16311861161317612; 0.06412158570494321 0.07073300061035362 -0.1700456097115818; 0.04151589237790065 0.05609444047534088 -0.14780807971115262; 0.022178735194164818 0.03520828303361599 -0.10107118772740264; 0.00804563314468598 0.014240023331380228 -0.04560716798470563; 0.007072478161838736 0.01446691060589681 -0.047529273447600426; 0.002571120248073851 0.00690791169445815 -0.023961693464404996; 0.0014604635664681803 0.0035950894488054595 -0.014911361145915715; 0.0016965429714419957 0.0019144290087075271 -0.012216691986582536; 0.003446264934699045 0.0007366305989642368 -0.0014921851218389968; 0.00020095277735622633 -0.0005107971142998043 -0.004119093319489178; 0.00023423846835033183 -0.0009744963120508555 0.0023405299655953143; -0.0028363762526296948 -0.0010833342790267653 0.0026975217770154125; -0.007224876813991645 0.0012291321262186312 0.006789096158653234; -0.003666984237585399 -0.0045018003662173935 0.007262694342260928; 0.00012734000932495995 0.00039886062437557675 0.002229313407949805; -0.0029772059066121553 0.007559992410301353 0.011748535550509333; 0.0013799128573919648 -0.0005026978096987187 0.007577679102442129] %
+
+Mass Used: 104.36239652718041 kg
+Launch C3: 95.20053074870958 km²/s²
+||V∞_in||: 1.6129671417019908e-7 km/s
diff --git a/archive/ES_0.5654649889548067 b/archive/ES_0.5654649889548067
new file mode 100644
index 0000000..ac87406
--- /dev/null
+++ b/archive/ES_0.5654649889548067
@@ -0,0 +1,22 @@
+archive/ES_0.5654649889548067---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:58:12.618
+Launch V∞: [7.655942024533932, -5.430892682132975, 0.2542828197044758] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6074251234412547e-9, 1.6299545789102535e-8, -2.774314318085606e-9] km/s
+ V∞_out: [5.765414489930544e-9, 9.72748140896333e-9, 3.088416294494532e-10] km/s
+ time of flight: 1.8749577787392417e8 seconds
+ arrival date: 2030-04-16T11:07:49.618
+ thrust profile: [1.0 0.01544653637901852 -0.23088888559548176; 0.1813956829738063 0.12321859842042593 -0.1556468887896818; 0.09759881335089403 0.11211963073986837 -0.15735427636954302; 0.04434529826086432 0.07098533619809753 -0.11295828176959705; 0.031439994678067865 0.065603968772033 -0.11359654435352559; 0.010773157469986042 0.028811266842581798 -0.05500783076001977; 0.0030500891694473387 0.010600557865296307 -0.022108422625878667; 0.0037412679333813726 0.015806720007827863 -0.034306404876852034; 0.0005058185092142644 0.0017439321010418963 -0.0044960308651120695; -3.0732641090259116e-5 0.001883547593165757 -0.0051058085971565905; 0.0003772097410756081 0.00013900983157102214 -0.0008907660485313496; 0.00024401491471638778 -0.0002297508355074857 0.000553449101839631; -0.0010661469959917745 -0.001078876561790405 0.002139322823243755; -3.367154028449475e-5 0.0013488951194152452 -0.0029605654821009525; -0.0001295231465498113 -0.0010066945208843366 0.0009971185760486155; -0.0035426423803430742 -0.0015989311680992902 0.0017249864712604852; -0.0002624638500144692 0.0005294423311829994 -0.0011153724758763202; 0.0001498831384925332 0.000218332950878437 -0.00011365339634005053; -0.0005364126649270076 -0.0010986211054393653 0.004454065349492867; -0.0021023501162730014 0.003491097436126105 0.0018820729828774969] %
+
+Mass Used: 145.36838417904983 kg
+Launch C3: 88.17270336026708 km²/s²
+||V∞_in||: 1.673829975358721e-8 km/s
diff --git a/archive/ES_0.5654743507214596 b/archive/ES_0.5654743507214596
new file mode 100644
index 0000000..bf73b98
--- /dev/null
+++ b/archive/ES_0.5654743507214596
@@ -0,0 +1,22 @@
+archive/ES_0.5654743507214596---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T16:01:52.241
+Launch V∞: [7.806861022182315, -5.44159600766655, 0.6575096249033531] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.133594483687249e-9, -5.714735804876342e-8, 1.7561865694644456e-8] km/s
+ V∞_out: [-7.498053237313274e-8, 2.8176067942239853e-7, 3.9376938745054303e-7] km/s
+ time of flight: 1.8749577787647784e8 seconds
+ arrival date: 2030-04-16T18:11:29.241
+ thrust profile: [0.7026010890689688 0.015412543179930264 -0.14791276856683822; 0.30345238070687747 0.20620377110849375 -0.2405031637299829; 0.08855130797623456 0.09982010754158005 -0.1374088784365454; 0.04078987941077683 0.06533719226464339 -0.10374937033705174; 0.02101417930502339 0.044481769629334714 -0.07846511388604778; 0.00967299776219084 0.027284452468278472 -0.05244544613699897; 0.0057015424866501616 0.014121837665333287 -0.02805525200421342; 0.003942333544497781 0.01095424464499671 -0.02322150891817894; 0.0004819214394308662 0.0023672636596805277 -0.0048633651308222555; 0.000244174773149376 0.0010725024940300924 -0.0017705770085259958; -0.00015920877063082278 0.00036704849678873534 0.00024965535341079845; 0.00011215078275502975 -0.0017711808441385757 -0.002179784789906299; -0.0004121231501493222 -3.936270234137238e-5 -0.0011708134093214393; 0.00022727121512514803 0.0013548208600217809 0.000898015722540097; -7.890895546765437e-5 -0.0007856624149378808 0.0010189066194198086; -0.0017320890828838814 -0.0012263576019116579 0.0011276595703366102; -0.00024126988624223046 -0.0008056274350881107 -0.0085754828666128; 0.0005429300005563026 -0.00014479439568937784 -0.004417334111983154; -6.194888605791463e-5 0.0006846455158745817 -0.0007919678700472014; -0.00015315150605031073 -0.006018224936148036 0.004603245572672922] %
+
+Mass Used: 128.94294645825448 kg
+Launch C3: 90.99036503716258 km²/s²
+||V∞_in||: 6.033568610578124e-8 km/s
diff --git a/archive/ES_0.5654770663254166 b/archive/ES_0.5654770663254166
new file mode 100644
index 0000000..6984774
--- /dev/null
+++ b/archive/ES_0.5654770663254166
@@ -0,0 +1,22 @@
+archive/ES_0.5654770663254166---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T04:31:33.949
+Launch V∞: [6.026573429412798, -7.845870831839663, -0.1315506106063018] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5341881015313685e-6, 9.577963694481099e-7, -6.80915595328385e-7] km/s
+ V∞_out: [7.775367411599452e-7, -1.5212764465824845e-6, 9.052480599656603e-7] km/s
+ time of flight: 1.725630713639902e8 seconds
+ arrival date: 2028-10-17T10:42:44.949
+ thrust profile: [0.21542829427439816 -0.08246994321276999 -0.09063856167710975; 0.07855608129814698 0.00867611379983552 -0.09245050624050234; 0.04760590423046847 0.014817385988956997 -0.09265344613399662; 0.07467261982098053 0.03282382450076153 -0.19632666854724198; 0.059863960828789295 0.03170498299928848 -0.19847973579520073; 0.035814575463128516 0.02143953206346226 -0.143328953486291; 0.00973091751217266 0.006421873759923521 -0.04734973892606173; 0.026033892636266404 0.018113916263478386 -0.1348130886982649; 0.0025598138513978253 0.001997503003499712 -0.018501987508667554; 0.0005286102072200231 0.00029638375798650516 -0.0036050786920309836; 0.0006461446671430001 0.0007254395466414606 -0.006241355646014462; 0.002211904225993247 0.0008375892989072261 -0.013245867785671148; 0.0006749767030262974 -8.23002104537898e-5 -0.003151112352805217; 5.405449835021005e-5 0.0006397009175637434 -0.001560896436111737; 0.00013758903880975443 0.0009508384437772554 -0.002624045150068695; -0.00070398983905459 -0.00017813200076720337 0.0004450633052639709; 0.0006368089718593898 0.00019820034094376784 -0.0015573811195736512; 0.0010921176580129313 3.660750275647168e-7 -0.0034344751426942342; 0.00018861840601178907 4.7062841801293824e-5 -0.0004993703665996953; -0.00019540008801699927 -0.00022064670239451507 9.987218999504919e-5] %
+
+Mass Used: 88.67151586950831 kg
+Launch C3: 97.89458197316762 km²/s²
+||V∞_in||: 1.9325509214946483e-6 km/s
diff --git a/archive/ES_0.5654794081293362 b/archive/ES_0.5654794081293362
new file mode 100644
index 0000000..f3f573f
--- /dev/null
+++ b/archive/ES_0.5654794081293362
@@ -0,0 +1,22 @@
+archive/ES_0.5654794081293362---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T09:27:36.589
+Launch V∞: [7.37471598561881, -6.039736331212267, -0.1824935888715304] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0035030599487024684, 0.00275828953201976, 0.1573252422393202] km/s
+ V∞_out: [-0.14523197831660542, -0.054827928472540886, 0.026600040017684956] km/s
+ time of flight: 1.7617230084740564e8 seconds
+ arrival date: 2029-12-06T10:12:36.589
+ thrust profile: [0.603844589089698 -0.015518814429375234 -0.13461299547279912; 0.25710437571521266 0.15783592109453534 -0.18754068426275516; 0.11812739402350332 0.12394779751826951 -0.15982697050700678; 0.06880462527562846 0.09924487116631178 -0.1419676006677661; 0.059754854025616845 0.11256872337637193 -0.1675985268792616; 0.0180642433763413 0.040885283557170346 -0.07006626724463372; 0.00653468732526929 0.019298141059529914 -0.03651011155654962; 0.005405213987353643 0.018088257853714197 -0.034381383383964535; 0.004495366742999051 0.018016052601370073 -0.035950744574740366; 0.001402597251647298 0.0066996946269953376 -0.016980200102474276; 9.992109159553206e-5 0.00040064006432975367 -0.000369054539203955; 8.227671078665335e-6 0.0019426731535035218 -0.0002534203432322103; 0.0020048929053819702 -0.0011601368964651044 -0.002260108617872982; -5.986394201991789e-5 0.00028790269989988087 -0.0013237373673731822; -0.0003520607223797801 0.0002500146004598405 -0.0017735150230172782; -0.0006355128200647658 0.0008598382851716857 -5.20033469672207e-6; 2.7145149015235113e-5 0.00010275798896942036 -0.0002086374503661888; 0.0029491422355321685 -0.0009791670538794235 0.00032716224448944614; -0.0013771964407198263 -0.00016359848323203266 0.0021827637373447143; 4.430070455291795e-5 0.001173169696033979 0.0012897626151372934] %
+
+Mass Used: 129.48674023122248 kg
+Launch C3: 90.89815472908624 km²/s²
+||V∞_in||: 0.15738840947098817 km/s
diff --git a/archive/ES_0.5654835408211963 b/archive/ES_0.5654835408211963
new file mode 100644
index 0000000..f067430
--- /dev/null
+++ b/archive/ES_0.5654835408211963
@@ -0,0 +1,22 @@
+archive/ES_0.5654835408211963---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:28:31.291
+Launch V∞: [6.5286773430951195, -7.451459169502393, 0.1831264017890728] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.701056150036118e-7, -1.1483932740468738e-6, -4.864632660647928e-7] km/s
+ V∞_out: [4.18307292805048e-7, -6.773718902275785e-7, 1.1048439926905124e-6] km/s
+ time of flight: 1.8511756248861918e8 seconds
+ arrival date: 2029-03-12T20:01:13.291
+ thrust profile: [0.1802188225471006 -0.048435860871998616 -0.06436781508528465; 0.07763073853807051 0.01845205704067059 -0.08369410004535043; 0.06618208910477344 0.032194878240602395 -0.11857487936636249; 0.04564484835467754 0.03024689969847446 -0.11527491236641572; 0.03806773704999717 0.030074591075142345 -0.1258416863865483; 0.0291044621304089 0.0273650337195896 -0.11173501903202841; 0.02242424487424117 0.019794901445719045 -0.09314726669491485; 0.013011820539591582 0.012697554493807078 -0.07404478266817055; 0.004158444940817108 0.008184188725381694 -0.03238208087320732; 0.007927784634364676 0.007763569299274432 -0.0481461422908869; 0.00401644605519536 0.0035286086682141 -0.009655231155443835; 1.6100052803809297e-6 0.000889874574256211 -0.006336485575475887; 0.001333872967374513 0.002702392796075259 -0.018266219590767227; 0.0002554582669320601 -0.003009774160465382 0.0031314051536388433; 0.0013944269314645923 0.0010220030583622322 0.0005662647183050808; 0.00048457500166250455 0.001466443989981969 -0.004105510611027219; -0.0025820508179995685 -0.004621012725288917 -0.0057428351200684725; 0.0021744334261086717 0.001868032654743545 -0.0009491109929297168; -0.0037464475952921133 -0.011848416308205637 -0.011817614714601368; -0.0019018732777725872 -0.011281180056262774 -0.009661067676758853] %
+
+Mass Used: 87.00592413451295 kg
+Launch C3: 98.18140688403705 km²/s²
+||V∞_in||: 1.3713037713669316e-6 km/s
diff --git a/archive/ES_0.5654877726200134 b/archive/ES_0.5654877726200134
new file mode 100644
index 0000000..8bfd6dc
--- /dev/null
+++ b/archive/ES_0.5654877726200134
@@ -0,0 +1,22 @@
+archive/ES_0.5654877726200134---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T14:13:27.079
+Launch V∞: [6.013538627796042, -7.6986548699879025, 0.02835600542401281] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006937559619698838, -0.00417851265758694, -0.006489765820078391] km/s
+ V∞_out: [0.004300700292332423, 0.0077581059267027635, -0.005386970648693238] km/s
+ time of flight: 1.7307199897667995e8 seconds
+ arrival date: 2028-10-20T17:46:45.079
+ thrust profile: [0.3549847400018176 -0.13167011800430198 -0.1131581606974424; 0.1010212466104725 0.018567280442771915 -0.10324818759173393; 0.047013459054165915 0.020739370776716812 -0.07943920130241855; 0.12186995997777032 0.07807352788781509 -0.22284551299885647; 0.05859908181152971 0.04241371599876171 -0.17086698612527815; 0.054748976776690356 0.0520728498176747 -0.19867593748952544; 0.010639670809081327 0.011026820611377417 -0.04633540647040061; 0.0072685918157880764 0.007545589471964788 -0.03258239091750899; 0.012635400565821483 0.014508923625448696 -0.06579116617302354; 0.0005700002279017205 0.0009208806649950002 -0.004175573934213533; 0.00017017471913837975 0.00015966220239108998 -0.000948165412530446; 0.0029914712790554917 0.004120214591819638 -0.020417446371558474; -0.0008397495106168666 -0.00036402469510003445 0.0005776305075015543; -0.0015593708515780002 8.4717901314689e-6 0.00037170968553995316; -0.0024224998793099285 -0.0008260499890579344 0.0009952428032328914; 0.001042173885469647 0.0003564187379149847 0.0021212705466634655; -0.0018919510306069785 -0.002331114931358309 -0.0013590165726465812; 0.0010177645235749904 -0.003520141476235827 0.0013296631969761494; -0.0007053797463246106 -3.561836375765319e-5 -0.0021812987415552655; -0.000345682080939937 -0.0002629393580032038 -0.0006389054669529887] %
+
+Mass Used: 103.04476481702386 kg
+Launch C3: 95.43273769822716 km²/s²
+||V∞_in||: 0.010378186831327903 km/s
diff --git a/archive/ES_0.5654969742331261 b/archive/ES_0.5654969742331261
new file mode 100644
index 0000000..76bd552
--- /dev/null
+++ b/archive/ES_0.5654969742331261
@@ -0,0 +1,22 @@
+archive/ES_0.5654969742331261---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:33:50.072
+Launch V∞: [7.729168646337956, -6.280374227944911, -0.03227058105561845] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.939870847108626e-6, 0.00018527183865201747, 3.2096027558671653e-6] km/s
+ V∞_out: [0.0001806008123870972, -2.6278943429182424e-5, 3.30477948881407e-5] km/s
+ time of flight: 1.7369704090513453e8 seconds
+ arrival date: 2029-11-15T07:44:30.072
+ thrust profile: [0.19093278409806497 -0.03461638416222495 -0.08217026009694099; 0.03236957348501548 0.0077243860352854314 -0.045032213015671424; 0.045067002898900185 0.01769071659590846 -0.10749994072639663; 0.046072279287167395 0.021286112714046384 -0.15377729270980123; 0.03931060757631764 0.019317327021793982 -0.16555974565533457; 0.02941495482108055 0.01471467085406183 -0.14720340039358193; 0.018658617109568634 0.009071178214184657 -0.10631708898571467; 0.007877368274961986 0.003636682021294179 -0.05070678487234967; 0.001370268297288168 0.002504044730498892 -0.020955246892696365; 0.0038315955648931138 0.0014327364533959384 -0.02605667452594184; 0.008910383430784173 -0.0021039930652629367 -0.0070595622053641624; 0.0030367882936557086 0.0035422121215629796 -0.0020005027955761036; -0.005160826951770257 0.0036116455173270715 -0.007071228018363089; 0.009761345754491804 -0.0037280191925264223 -0.0014802263251418378; 0.005603325172233488 8.706952016417221e-5 -0.009122673852667483; 0.004933421558116583 -0.0015907906104369682 -0.008891210333698739; -0.01025044585546888 0.0018061171459611324 0.0073396821605246874; -0.005614571290588185 0.004457744433256067 -0.010289678785076379; 0.002297369630978255 0.003035661427710319 0.002586642666439892; 0.0037822231057160084 0.0025826508207986176 0.009039985562310868] %
+
+Mass Used: 81.17202945632198 kg
+Launch C3: 99.18418979697002 km²/s²
+||V∞_in||: 0.00018546966678251845 km/s
diff --git a/archive/ES_0.5654971069658157 b/archive/ES_0.5654971069658157
new file mode 100644
index 0000000..1c74d62
--- /dev/null
+++ b/archive/ES_0.5654971069658157
@@ -0,0 +1,22 @@
+archive/ES_0.5654971069658157---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T21:11:32.590
+Launch V∞: [6.2772905620589885, -7.382903441132903, 0.08258711221178296] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.582896958867248e-5, 3.5079442176302375e-6, -7.562806207642843e-8] km/s
+ V∞_out: [-5.257034953027963e-6, 1.1966561492061558e-7, 2.5527645190761865e-5] km/s
+ time of flight: 1.874957778752756e8 seconds
+ arrival date: 2029-04-06T23:21:09.590
+ thrust profile: [0.3826870217518064 -0.06778156459823154 -0.09871692871916928; 0.2539082072068639 0.10462621969199465 -0.1990623163319668; 0.06832026012461484 0.04904385339794948 -0.0985466029267193; 0.049651462398101094 0.050836079073292594 -0.10421130359448273; 0.034338465968271614 0.04175989641780687 -0.09151524919710813; 0.04720406168636408 0.07464994203553914 -0.154988622641828; 0.015625365841616813 0.02686039916691112 -0.06520514055171467; 0.011427638756015882 0.020807215328081954 -0.05115670293771571; 0.00401824055598677 0.008650053406480831 -0.024154019870995757; 0.0020851035613357084 0.005012178049151151 -0.015070360126441298; 0.0020732551854470887 0.003453101686168975 -0.013400714688216357; 0.0017504025503040956 0.004436835237137167 -0.010519143921999312; 0.0015943991109553578 -0.0012307585333145524 0.001333646967363967; 0.0013239380035927329 0.00039554293082042294 -0.0010420356825314701; -0.0007907922589382925 -0.0014070937929663743 0.0016668394120562028; -0.000828365658065129 0.0002049366270868517 0.0024282898175657054; 0.00010619025737221841 0.0016972713717078288 0.00281911755793923; 0.0024106219823472356 0.002902838204852645 0.0019802199650072595; -0.0010814873133502332 0.0034930568979895 0.0014949296678825202; -0.0011147628537350475 -0.0008611910491785705 0.00025817444006121795] %
+
+Mass Used: 111.88893765264083 kg
+Launch C3: 93.91846065271041 km²/s²
+||V∞_in||: 2.6066205367301677e-5 km/s
diff --git a/archive/ES_0.5655018910193597 b/archive/ES_0.5655018910193597
new file mode 100644
index 0000000..5f197c1
--- /dev/null
+++ b/archive/ES_0.5655018910193597
@@ -0,0 +1,22 @@
+archive/ES_0.5655018910193597---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:44:10.448
+Launch V∞: [6.639676515553571, -7.414796208026319, -0.06656862483770327] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.611251440973388e-9, 8.916697285012792e-9, 5.102770381157753e-8] km/s
+ V∞_out: [-3.424204364757297e-8, -2.991430008668672e-8, -1.4841198646706794e-8] km/s
+ time of flight: 1.8749577785415795e8 seconds
+ arrival date: 2029-04-10T20:53:47.448
+ thrust profile: [0.14599488963230026 -0.041722988481942565 -0.05900234354075515; 0.058184617319974756 0.013192399647831258 -0.07868410144933564; 0.047492941973260455 0.020941991777469936 -0.1054254601181368; 0.040708036340320795 0.023292526209336972 -0.12576616679483066; 0.035236071447382875 0.023937534461885058 -0.13890705429428168; 0.024789557246409723 0.019435012858554278 -0.12018879588954642; 0.026551401287231803 0.02245345052000352 -0.14487040784975797; 0.005819267629171901 0.006921205142462798 -0.048943404958011874; 0.0013930034791259163 0.0031856520429256762 -0.022938351851638825; 0.0020906743019584563 0.004091831675592801 -0.018346275967935918; -0.0008779802044145738 -0.001050639835949059 0.0011321295805328717; 0.0038048556672082073 -0.0006597643484022625 -0.003246327937508917; -0.008140220351988588 -0.0016458264593007732 0.004328311313217302; -0.004890874125433158 0.00036231860459609274 0.0062084195898022; 0.0016659886576438343 -0.0013000527810904934 0.0023443912666326235; 0.001015772735379099 -0.001302583718101426 -0.0002994307855903981; -0.001834302757923815 0.010006412225156905 -0.011785214666711778; 0.0027926758616999793 -0.0008924713036947538 -0.007065984058410432; 0.00779839529918237 -0.006702453785302432 -0.00824197491402966; 0.003756270746211263 -0.0003894310918112886 -0.006123154230567278] %
+
+Mass Used: 81.85006540844051 kg
+Launch C3: 99.06893841956786 km²/s²
+||V∞_in||: 5.222109432375399e-8 km/s
diff --git a/archive/ES_0.5655155946510998 b/archive/ES_0.5655155946510998
new file mode 100644
index 0000000..bd9e72f
--- /dev/null
+++ b/archive/ES_0.5655155946510998
@@ -0,0 +1,22 @@
+archive/ES_0.5655155946510998---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T17:36:50.897
+Launch V∞: [6.273319965636948, -7.59340518548721, 0.029246384627926416] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008270288247734663, 0.0010158286568609275, 0.0009271819854085638] km/s
+ V∞_out: [-0.0009162990726586593, -0.000387028940629668, 0.001258969366710758] km/s
+ time of flight: 1.8048171022692132e8 seconds
+ arrival date: 2029-01-17T15:25:20.897
+ thrust profile: [0.26469207084335866 -0.08146728119994295 -0.09838944360653654; 0.11411082954893359 0.022819564698065946 -0.1265487958539183; 0.04859911719351681 0.020302999340815638 -0.09150694870708002; 0.049591110901995125 0.028190403486209655 -0.12853523487600657; 0.029747548051192264 0.020550180103961313 -0.09954657457949384; 0.021869576269435243 0.017146940326879558 -0.08854141546135803; 0.01707904288013656 0.014494994354887231 -0.08061614415386417; 0.04065413728373113 0.03683733157681012 -0.20294535345748013; 0.0026617408272853627 0.0022394391811254135 -0.01385986530725365; 0.0014454549798870665 0.001448748877319694 -0.008730723144110223; 0.002453573838097511 0.003317913738280201 -0.01759862520531216; 0.0031815207448240524 0.00048750460037063313 -0.006811926420213382; 0.0028459297470970622 0.0007008327792157403 -0.00668469326269433; 0.0003006940496286816 0.003936387943507531 -0.002923100568832552; -0.007591914657859616 -0.0032159745384542516 -0.008978501810070469; -0.00354192197138017 -0.009631619945709092 -0.009941308131513489; 0.0009196107912648648 0.0010669638240386747 -0.0037123869862136644; 0.00027424695675910414 -0.0005614459636553914 -0.0022852715840245806; -0.00155329275995928 -0.0009316219953077161 0.005896918141118111; -0.00046823158341546605 -0.0009387768691970894 0.00045174968573569174] %
+
+Mass Used: 93.84618761561705 kg
+Launch C3: 97.01520105325703 km²/s²
+||V∞_in||: 0.001604852320673844 km/s
diff --git a/archive/ES_0.5655198511551601 b/archive/ES_0.5655198511551601
new file mode 100644
index 0000000..957aa93
--- /dev/null
+++ b/archive/ES_0.5655198511551601
@@ -0,0 +1,22 @@
+archive/ES_0.5655198511551601---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T21:07:35.341
+Launch V∞: [6.290904422290604, -7.437107084398742, 0.24357545542014838] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.415266666507652e-6, 8.562056823000481e-7, -1.8362303272790766e-8] km/s
+ V∞_out: [-1.5267768107857225e-6, 3.5086526466268486e-8, 6.2884175374867434e-6] km/s
+ time of flight: 1.8439605352135956e8 seconds
+ arrival date: 2029-03-02T02:15:08.341
+ thrust profile: [0.360571481640261 -0.08303244829609074 -0.0993909731543122; 0.17358836360093688 0.055724829440660435 -0.14995494165866793; 0.06797903222343415 0.04330302623413286 -0.0989362270025685; 0.030554817864461063 0.027445192205771053 -0.06728369678062321; 0.05040582634476041 0.055182894637266285 -0.13221702485141817; 0.052471501933122805 0.06840924512378613 -0.16331890609478003; 0.021476986231702085 0.031456293444775955 -0.08309756622106199; 0.021700914425838835 0.03536883915841589 -0.0971067975677616; 0.00189859037036171 0.005133995854252753 -0.013894013208185002; 0.0006673711518363019 0.002169237084820108 -0.011841256279210566; -0.0005881397219372388 0.008050676831729595 -0.012851375683740774; 0.00023276161182834743 0.001501989354564809 -0.0003165803891902758; -0.00038392815996176986 -0.0008434805523066534 0.0012101485136787457; 0.004466648814935154 -0.003529318550505683 0.0018711563429224063; 0.0016007722066246008 0.002108133123089491 -0.0021824822994654194; 0.002264480526123725 0.002411893993601758 -0.0011694117013106198; 0.0017052214247673782 -0.00046314396428756094 0.003403059753132766; 0.0007423643702827877 -0.0002767201365583943 -0.002741981179323222; 0.00487878338525833 -0.011172672806962977 -0.008497945640644319; -0.0013840351560456383 -0.0033566955742304035 -0.0007872632756504276] %
+
+Mass Used: 105.92517246114676 kg
+Launch C3: 94.94536923769257 km²/s²
+||V∞_in||: 6.472176739474021e-6 km/s
diff --git a/archive/ES_0.5655267107824472 b/archive/ES_0.5655267107824472
new file mode 100644
index 0000000..e3561f5
--- /dev/null
+++ b/archive/ES_0.5655267107824472
@@ -0,0 +1,22 @@
+archive/ES_0.5655267107824472---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:17:56.371
+Launch V∞: [7.412671940915033, -6.433054534696698, -0.1899766438870779] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0397236241889511e-8, 6.138796317283262e-9, -8.128921608156865e-9] km/s
+ V∞_out: [7.819278483612194e-9, 1.53537971518549e-8, 5.045958389919904e-10] km/s
+ time of flight: 1.621203723308831e8 seconds
+ arrival date: 2029-06-27T20:44:08.371
+ thrust profile: [0.2873628971241162 -0.0422432045496121 -0.10050940870529698; 0.1313756089647208 0.05223700302250446 -0.13547119990215403; 0.09639335057002092 0.06613604679938766 -0.16678958239947805; 0.07732791229335428 0.07116367671176016 -0.18801383537423316; 0.052516932607139494 0.05723508484227322 -0.16489082932048896; 0.0236993462008269 0.030279421650974376 -0.09627341070414229; 0.036151700397276436 0.05087559923949923 -0.1564101300845035; 0.007948439102982903 0.011854013904945091 -0.043434234811400296; 0.008310235564840321 0.014298613446372779 -0.05216904346496377; 0.0012622232125305834 0.002328138311554503 -0.009338517190601036; 0.0013020327743189118 0.0009695594205586647 -0.003977575846616378; -7.353302639610376e-6 -0.00026898065925448335 0.0005572168014655456; -0.0015561847098062083 0.0013677990260545806 0.0008445094843018818; -0.00013116997000195353 -7.033136489059341e-5 -0.0007306094634256897; -0.002886116434270508 -0.0008157650718083377 0.0001073677963711019; 0.00021899355786437368 -0.0032867401296615487 0.0008472487066562423; -0.0007696825448590561 -0.0003602393110643366 -0.002512173196127808; 0.00027749916661043075 0.0018252792331208334 -0.002195682999172837; -0.0002698463726831589 -1.2637322531383065e-5 -0.00012750308726909478; -0.004835922425399068 0.0015115247985140654 -0.0023574149301394025] %
+
+Mass Used: 97.63457130732695 kg
+Launch C3: 96.36798707523339 km²/s²
+||V∞_in||: 1.455564179987646e-8 km/s
diff --git a/archive/ES_0.5655274718484358 b/archive/ES_0.5655274718484358
new file mode 100644
index 0000000..730b30f
--- /dev/null
+++ b/archive/ES_0.5655274718484358
@@ -0,0 +1,22 @@
+archive/ES_0.5655274718484358---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T16:04:30.555
+Launch V∞: [6.560451242863986, -7.31058714074588, 0.1883968395729805] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00101106245472317, -0.006708610052143524, 0.0089193889674473] km/s
+ V∞_out: [-0.007687379632133162, -0.006471144174270465, -0.004958955450418494] km/s
+ time of flight: 1.8749577787479526e8 seconds
+ arrival date: 2029-04-08T18:14:07.555
+ thrust profile: [0.33726401456432303 -0.08500090651496858 -0.10872707184075506; 0.05210949681594429 0.014707378560473433 -0.05447604344650241; 0.06803295517427765 0.03811461608070342 -0.11742593108277932; 0.049646155957927894 0.03451674218699326 -0.11718956134899876; 0.035336607705997905 0.032055061027224524 -0.12170790562227582; 0.02232005015008027 0.022250309592703153 -0.09065721560546872; 0.01043118657816618 0.011718611957962801 -0.050673528429285575; 0.014938923026251553 0.01870561394090248 -0.07825491493686129; 0.01932948775171188 0.02278235818002837 -0.10924218904607251; 0.0023294644353460577 0.003320244851815059 -0.01751646678435295; 0.0005146955161287235 -0.0006851142598495473 -0.009117208481401587; -0.0035970107274950285 0.005306958315360114 -0.004055780862332622; -0.00024341229967834348 -0.0011122240604400854 -0.006695624922233587; 0.0013704401281539413 0.003054931560717378 -0.009774598682731341; -0.0028216380248142748 0.004795473718226233 -0.0050907296440591485; 0.009445331415795098 -0.004783867164112396 -0.007055549185641295; -0.008214539267890054 0.007626390757116639 -0.006726511286552537; 0.001344924951085852 0.0031065426656564257 0.0040303196338958465; 0.00016929893937717069 -0.006210649559281767 0.001745261668572042; 0.009061365883587826 0.0008419653972740935 -0.0044038456923726] %
+
+Mass Used: 96.75047753053332 kg
+Launch C3: 96.51969822159573 km²/s²
+||V∞_in||: 0.011206390840573632 km/s
diff --git a/archive/ES_0.5655326063518934 b/archive/ES_0.5655326063518934
new file mode 100644
index 0000000..45944ec
--- /dev/null
+++ b/archive/ES_0.5655326063518934
@@ -0,0 +1,22 @@
+archive/ES_0.5655326063518934---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T13:05:07.724
+Launch V∞: [6.487155564648749, -7.330533048698427, 0.2563016869185473] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.9576204779272964e-8, -7.475253979768297e-8, -4.9414308295915156e-8] km/s
+ V∞_out: [2.4869209234734068e-8, -5.281446198516072e-8, 8.15741456929828e-8] km/s
+ time of flight: 1.8500437181206006e8 seconds
+ arrival date: 2029-03-08T19:11:18.724
+ thrust profile: [0.3405375333375924 -0.08235191107844157 -0.1051964662689523; 0.10718682218143824 0.033098572440114084 -0.101191734931456; 0.06604642255512429 0.039008970017549056 -0.10612073919947546; 0.07569923604870232 0.06168298322612183 -0.16653527735869517; 0.056612095607812274 0.05636715449635293 -0.16217908818132828; 0.024151515272090043 0.02755970837425641 -0.08702595454327615; 0.009573834374522553 0.012096083567870721 -0.04215758943847132; 0.008165077321571965 0.011870446364925595 -0.04294993751403247; 0.012633132166181895 0.021709559911508847 -0.07692435816671607; -6.781382137377489e-5 0.0021588735307968526 -0.007683514237712032; 0.00041261488092223355 0.0008136022586532046 -0.0028964010550942203; 0.0033324263307484563 0.006344430364090547 -0.02223155577132921; 0.0011383880433742904 -0.0033715477812034556 0.0006049235319652733; 0.003851242656246626 0.002402281540579947 -0.0009430853282536506; 0.00022057427687219126 0.0007015529424999208 -0.001598117136936065; -0.006561115126097978 0.0013878801841906967 -0.0019137162104907908; -0.0029331940978306694 -0.00024502265105438614 0.0013173055152555092; -0.0028940388572359444 -0.0023038177976969177 0.005488833730892096; 0.00010161467436324638 0.0015058112053516484 -0.004886068838437984; -0.0027772911119826474 -0.009387941043904988 -0.0025812793869790605] %
+
+Mass Used: 100.45541693628184 kg
+Launch C3: 95.88559265273037 km²/s²
+||V∞_in||: 1.0240857459648745e-7 km/s
diff --git a/archive/ES_0.5655478212115105 b/archive/ES_0.5655478212115105
new file mode 100644
index 0000000..d989c46
--- /dev/null
+++ b/archive/ES_0.5655478212115105
@@ -0,0 +1,22 @@
+archive/ES_0.5655478212115105---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T15:24:46.143
+Launch V∞: [6.128203578254339, -7.686343729407135, -0.03500972098868396] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2887990751935201e-6, 0.00039874169529633807, -0.00025955064601353547] km/s
+ V∞_out: [-0.00039410492639327936, -0.00020534506195747727, 0.00016976760879803578] km/s
+ time of flight: 1.745445239920196e8 seconds
+ arrival date: 2028-11-07T20:00:09.143
+ thrust profile: [0.28044112674956456 -0.09566806823797479 -0.10269323102436277; 0.09142465217261386 0.015764228832547984 -0.10081662507818318; 0.0739018276910412 0.030931546095104623 -0.13506427487548536; 0.04990847447007657 0.027442454677229545 -0.12414136525794796; 0.08399684599634542 0.05805460876409924 -0.26090220432340977; 0.026120862533180314 0.020493507637248855 -0.09809686177865354; 0.020848223390251455 0.01791513321821064 -0.0910715644121864; 0.01257204340215564 0.010896823832691842 -0.06210556979597466; 0.006418855694108041 0.006692723437044422 -0.03706601141209105; 0.0021270067286035532 0.0024054554712513903 -0.015010875401455698; 0.0010854550130022559 -0.00022118405560285785 -0.0008760035903036139; -0.000475324305713376 0.0005148568200567165 -0.0009137503654855445; -0.00037327423507824375 0.00048300518411515775 -0.00038513762113480713; -0.00040271592903911365 -0.0018244240684215153 0.0013790479654447975; 0.0004120171738210784 0.0005735333216489417 -0.005278156030340447; 0.0013635824476862391 0.0006009781061589142 0.0012733720737184207; 0.004196261463953211 -0.00045336813977548676 -0.0007637759699019261; 0.00563827500080199 -0.004090705401608233 -0.008254758017550854; 0.0012586480945702794 -0.0010197960950297737 0.0017120432256820357; -0.007395879607503165 0.0015268446943400363 -0.008470942825710377] %
+
+Mass Used: 96.09588064190757 kg
+Launch C3: 96.63598470368937 km²/s²
+||V∞_in||: 0.00047577635336037614 km/s
diff --git a/archive/ES_0.5655496163478178 b/archive/ES_0.5655496163478178
new file mode 100644
index 0000000..833ae55
--- /dev/null
+++ b/archive/ES_0.5655496163478178
@@ -0,0 +1,22 @@
+archive/ES_0.5655496163478178---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T00:10:54.071
+Launch V∞: [6.072778466099559, -7.6855059550920615, 0.09669056059730485] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.096564952234233e-10, -1.2221750385036506e-9, -3.181523658013412e-9] km/s
+ V∞_out: [3.32351990919789e-10, 4.821608519880747e-10, 2.4619523896388745e-10] km/s
+ time of flight: 1.76009943008302e8 seconds
+ arrival date: 2028-11-25T03:49:57.071
+ thrust profile: [0.2983436953649241 -0.09936437323778469 -0.10921742492430905; 0.10760624343165315 0.019699534675386116 -0.11509445863443855; 0.14376099533544706 0.06213506875468629 -0.24021977424418806; 0.06510555184266846 0.03831433648780284 -0.15526316310922805; 0.037100398960900526 0.02575344067629116 -0.11239275564196724; 0.02971270428599692 0.023696651312230782 -0.10759106524382865; 0.022717494109164394 0.019519834938475634 -0.09391552354609672; 0.009051312174798544 0.008593014683273281 -0.0426539752091571; 0.006315262677218175 0.00644417932713054 -0.033038385183002054; 0.0011136482881297508 0.0020260583782409644 -0.00587670512960927; -0.0002076876287434049 0.0019047894660523862 -0.0031779959732280184; -0.0001812634022784628 -3.652354447129108e-5 -0.004676956696670264; 0.0007282540119585661 -0.0014745172013272583 -0.006900184820158765; -0.0007548064435984804 0.0002473484380283771 -0.0015680179958929286; 0.00501438652688269 -0.006641818612388817 -0.009303899716107643; -0.0010902158601047707 0.0008683768389031763 0.001282665264206256; -2.2020444005011993e-5 0.00025792287646316035 0.0002493689921204993; -0.0112077942060849 0.0042101589127532014 -0.00480025048531054; 0.0012357870939835535 0.0045669907427287465 -0.003153537760886285; -0.005117568405312904 -0.004969986688255188 -0.0017855638544634986] %
+
+Mass Used: 100.0704490390317 kg
+Launch C3: 95.95498914858669 km²/s²
+||V∞_in||: 3.462294853620724e-9 km/s
diff --git a/archive/ES_0.5655637336695545 b/archive/ES_0.5655637336695545
new file mode 100644
index 0000000..480283e
--- /dev/null
+++ b/archive/ES_0.5655637336695545
@@ -0,0 +1,22 @@
+archive/ES_0.5655637336695545---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:00:07.411
+Launch V∞: [7.7715422031833965, -5.799621922802392, 0.1555735359528037] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.152085544422221e-9, -1.2820174618824262e-9, -1.4169637762938499e-9] km/s
+ V∞_out: [4.963409744026773e-10, -4.6461413219743193e-10, 1.699177195382202e-10] km/s
+ time of flight: 1.87495777874489e8 seconds
+ arrival date: 2030-04-23T18:09:44.411
+ thrust profile: [0.5071560650069659 0.006651070749599274 -0.15149611748171005; 0.11179363974833315 0.06469177488088389 -0.12278831983136902; 0.05726714975831232 0.052862324038628256 -0.11520621113491417; 0.049547202939469556 0.060853450992853046 -0.1479746857891154; 0.022025601372189677 0.031978896317286815 -0.0899783290516424; 0.012756069565630175 0.021120790957513454 -0.06567743450187197; 0.011989546333282617 0.023161651466226695 -0.07680618148954545; 0.004524541168821855 0.008217785228337503 -0.021936097173741193; 0.0023734084418285005 0.005750678749899139 -0.023901464564730465; 0.005709675301423023 -0.0017637741466835124 -0.01722133162985633; -0.0004912976736048854 0.0025030458934236395 -0.01163079014091714; 0.0008180213905627921 0.0037372115782259353 -0.0070004662387254364; -0.0012674054539263532 0.0018791545668752883 -0.005162929272688028; -0.0010522491113779525 0.0031453062531379295 0.002574801041052996; 0.010928280440663686 0.005110840998950775 0.001193588476613181; 0.00032965531315294004 -0.004694494611123286 0.008946488260622186; 0.000772884493951867 0.03489605873127456 0.004503482869981489; -0.0006496018514631929 -0.004756941506280891 0.007101560991261685; -0.00029553639840694356 -0.005106701773875881 0.03021057951060649; -0.03155565030783519 0.004425800568654024 0.0055724271306364995] %
+
+Mass Used: 111.16035551548248 kg
+Launch C3: 94.05668578839962 km²/s²
+||V∞_in||: 2.2312902584753585e-9 km/s
diff --git a/archive/ES_0.5655740201227861 b/archive/ES_0.5655740201227861
new file mode 100644
index 0000000..8e050aa
--- /dev/null
+++ b/archive/ES_0.5655740201227861
@@ -0,0 +1,22 @@
+archive/ES_0.5655740201227861---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T15:40:17.762
+Launch V∞: [7.782819898875424, -5.784835376573534, -0.24441691243293978] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0300418344762272e-5, -1.579467484431353e-5, -1.622596182535459e-6] km/s
+ V∞_out: [1.407450064005205e-6, -5.759657143461496e-6, -1.7957148126321743e-5] km/s
+ time of flight: 1.851797582572277e8 seconds
+ arrival date: 2030-03-24T22:29:35.762
+ thrust profile: [0.4049865343153764 0.010903380531146076 -0.11034450145821095; 0.1760657714252795 0.1159035575223276 -0.15928605569102025; 0.0697025441759536 0.07592597244257138 -0.11767189880323987; 0.053192578035009444 0.07981602346827096 -0.13601941485365734; 0.03527733074541656 0.06781670317770688 -0.1263120780318965; 0.027045718845135926 0.0653884754806089 -0.12992289774273288; 0.0034538203008638467 0.010181645397200347 -0.021931454508690756; 0.000796921154853325 0.004545059148418599 -0.011049313990837677; 0.005692643478105578 -0.0018068424645276784 -0.0044439629207210455; 0.0019583372973033717 0.005531127775231163 -0.0031578796834341805; 0.0004806038020115774 0.0028879849039699732 -0.00693396982351675; -0.00010859679512836493 0.0026762577203870664 -0.004594213278317768; 0.0009333742453144038 0.0015440996928497413 -0.009953804654559952; -0.006774986264442271 0.0037496280454463408 -0.0009305027536873995; 0.003977480700375699 0.003702906055231035 -0.004055930789754631; -0.0035282288811065037 -0.00667148678808058 -0.02770275869182873; 0.01666565591577182 0.026177816004083945 -0.03113911172984385; 0.0019898049713660427 -0.0006707681956340441 0.004767286173132026; 0.002295551085659236 0.017876629502845874 -0.009986513979316068; -0.00043835533689390034 -0.0036288053431486394 0.015029756504776455] %
+
+Mass Used: 110.9410078296687 kg
+Launch C3: 94.09634553947117 km²/s²
+||V∞_in||: 1.8926256626345433e-5 km/s
diff --git a/archive/ES_0.565575354867164 b/archive/ES_0.565575354867164
new file mode 100644
index 0000000..c0de0cd
--- /dev/null
+++ b/archive/ES_0.565575354867164
@@ -0,0 +1,22 @@
+archive/ES_0.565575354867164---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T20:22:55.022
+Launch V∞: [6.470973042763541, -7.450669223699247, 0.13097992434517758] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010799371564499214, 0.001206249607916004, 0.0010936482297357524] km/s
+ V∞_out: [-0.0012912889284863412, -0.0006214304934565134, 0.0013278081123809424] km/s
+ time of flight: 1.8423896896926874e8 seconds
+ arrival date: 2029-03-02T05:52:23.022
+ thrust profile: [0.2659105207481746 -0.07526020846273251 -0.09333642213735972; 0.039611912215969505 0.009502690567400721 -0.04302961229234961; 0.06145929870862551 0.02957530949909049 -0.10949027596552587; 0.053627036706465875 0.03460734386118544 -0.13253736493214024; 0.044338646953902994 0.034410155486010036 -0.1397877462472501; 0.02348752444699638 0.021100094036643955 -0.09179321206881366; 0.029637411057052043 0.029146406979879948 -0.1327120101742753; 0.0007608028122865346 0.001215669841801628 -0.020167727183620025; 0.014467686420400798 0.015407898682750752 -0.08390475432905653; 0.009309533113827838 0.012972010585829561 -0.06221653573483423; -0.002391715779468994 0.001902403811376868 -0.006965635808627364; 0.0024755011731193268 0.001629398606242853 6.588421020648936e-5; -0.005518356632248232 -0.0020302191644902302 0.0010425393428596776; 0.004429824289125693 -0.000628592130587576 0.004312274852645497; -0.002111927304057643 0.003977269676592231 -0.004508792534022777; -0.007271046967789935 0.002145241145021205 -0.008370642305253598; -0.008546522856403302 -0.0023262806519520982 0.0006183312417751361; 0.0027542916945267368 0.000667280874689806 0.0008059656098791234; 0.0036167380093030674 0.006975202829323315 0.0013598004740970277; -0.0012378119217148129 -0.002987426987685908 0.0028376213917101095] %
+
+Mass Used: 91.65304885158184 kg
+Launch C3: 97.40311974173306 km²/s²
+||V∞_in||: 0.0019538088004927194 km/s
diff --git a/archive/ES_0.5655771560419189 b/archive/ES_0.5655771560419189
new file mode 100644
index 0000000..839cf59
--- /dev/null
+++ b/archive/ES_0.5655771560419189
@@ -0,0 +1,22 @@
+archive/ES_0.5655771560419189---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T20:33:59.835
+Launch V∞: [7.697489445336432, -5.645151954008118, 0.29125186492576094] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4843709657300004e-5, -4.182448732353407e-5, -0.00010609421107864357] km/s
+ V∞_out: [-0.00010684739731396083, -1.287481750288749e-5, 4.002804161750918e-5] km/s
+ time of flight: 1.8749577785369384e8 seconds
+ arrival date: 2030-04-17T22:43:36.835
+ thrust profile: [0.6385042425910422 0.027323120684571506 -0.10681666735174382; 0.15496494108453704 0.11289771892651138 -0.11162698278006204; 0.12850701223196123 0.1747730491440172 -0.16661738832933848; 0.04730693867110683 0.09578443454356551 -0.10619923142974681; 0.02959471197531019 0.09410252463737272 -0.11756878116035216; 0.015133987382137152 0.0507371283509157 -0.07217537195661326; 0.007790527359208873 0.028432562169698535 -0.042594526373455066; 0.004926837211542632 0.03647532006551495 -0.05588014901755072; 0.0007640369128587503 0.006744810536997588 -0.008874680071140437; 0.0005946417387707794 0.00342484210541444 -0.006917741829674636; 0.0007964490029074334 0.0013801588264886393 -0.0038834854302306683; 0.0017975631611658566 -0.00045152981951407964 -0.003506333978364333; 0.0002816021131249473 -0.0022467308612716137 -0.001078987458051499; 0.0010404372854572919 -0.0015354449113889961 0.0021784560033645535; -0.0015682429880205045 -0.003266517468517867 0.0022664267971600717; -0.002196590101603608 -0.0005675773751397927 0.0032842390153696903; -0.0018288057080810154 0.001752722719413673 0.0013506685834466597; -0.0032878968492553715 0.00015464617851730493 -0.001204382852234597; 0.0026402803485836963 4.122455535291545e-5 0.00397769503163907; 0.004265351458685304 8.631673946600128e-5 0.0013312940940189452] %
+
+Mass Used: 127.81719541881284 kg
+Launch C3: 91.20391199373017 km²/s²
+||V∞_in||: 0.00011500263075541558 km/s
diff --git a/archive/ES_0.5655788717157356 b/archive/ES_0.5655788717157356
new file mode 100644
index 0000000..36d0686
--- /dev/null
+++ b/archive/ES_0.5655788717157356
@@ -0,0 +1,22 @@
+archive/ES_0.5655788717157356---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T12:27:59.468
+Launch V∞: [6.469126838125918, -7.459439375204, 0.13222284780921342] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.6813470482622235e-5, 6.298595633630082e-5, 5.800015909902238e-5] km/s
+ V∞_out: [-9.106446849656391e-5, -4.512904405739033e-5, 7.391447651360228e-5] km/s
+ time of flight: 1.8425377285034397e8 seconds
+ arrival date: 2029-03-03T02:04:11.468
+ thrust profile: [0.2752399447950911 -0.07931542574920841 -0.10623991601539418; 0.04347035040174506 0.008771345099523774 -0.04686769659358966; 0.04677572439059813 0.020292223927264375 -0.08772294281031674; 0.04522753352847575 0.02345494061976268 -0.11710552888650383; 0.039690897888091284 0.02289890644958155 -0.1286163596937744; 0.032066400326526 0.02072928917785505 -0.12485001987830134; 0.01549982386932811 0.016265210231670647 -0.07613122918601332; 0.013804185549573954 0.015214580824206252 -0.07877180679692235; 0.007940841146558606 -0.0017226539430286662 -0.03405710201693332; 0.008480659380945428 0.011072033176032869 -0.06627196860059258; 0.005570938694020342 0.007045918604475197 -0.043454494737886894; -0.0023278856274062927 -0.0029928181771794026 -0.009966713899111678; 0.002562408230612938 0.0003553726039861333 -0.011418637384970481; -0.0018337772040967761 -0.0020620260034759728 -0.0019346838369127938; 0.002771345684581311 0.002157822413925659 -0.005368800332791048; 0.0018177318825825337 -0.004883163607739517 0.003814567686536152; -0.0029178497318394867 0.0033644476878404213 -0.012868230487264534; -0.0017397624004318645 0.001021590459958274 -0.00010050294513013868; -0.002920323931769299 -0.003614407551512136 0.006709308083242265; 0.004125080506157685 0.0004060730793659922 -0.00021291952604832296] %
+
+Mass Used: 91.03181279243017 kg
+Launch C3: 97.51032072158766 km²/s²
+||V∞_in||: 0.00010275709016603229 km/s
diff --git a/archive/ES_0.5655795231234919 b/archive/ES_0.5655795231234919
new file mode 100644
index 0000000..0ee5df6
--- /dev/null
+++ b/archive/ES_0.5655795231234919
@@ -0,0 +1,22 @@
+archive/ES_0.5655795231234919---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T15:23:40.996
+Launch V∞: [7.240937802551998, -6.5163565976367455, -0.2923479497323159] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.068904971711154e-9, 8.169299261402096e-9, -3.147362227599349e-8] km/s
+ V∞_out: [-9.633894575565202e-9, 3.167443933295428e-8, -4.7428216827975865e-9] km/s
+ time of flight: 1.595442900054987e8 seconds
+ arrival date: 2029-05-30T05:15:10.996
+ thrust profile: [0.5422110146258157 -0.1232302558436199 -0.21949089596478616; 0.05146931878203369 0.013588097955351012 -0.06516300010837427; 0.0967976677183123 0.047382353947958845 -0.19868380208501046; 0.056039189764608616 0.03594044123971553 -0.16381832397038967; 0.040444895696789135 0.03047271931268273 -0.15183415193594962; 0.03006979822550908 0.02530306729150136 -0.13697321374174498; 0.020095167133547705 0.018214436298197918 -0.10722485740510561; 0.01316887275618365 0.012777720394285982 -0.08152929606816327; 0.005059806327404566 0.0055115278787348995 -0.03363995428247417; 0.0035721327381221532 0.0034549926537853896 -0.026218861564759253; 0.0026915909349803703 0.0026409540397849653 -0.02096305255061234; 0.00010495547116800582 5.298533153626223e-5 -0.00024528865725832337; 2.00538956326962e-5 -4.937301535207065e-6 -4.104038899756032e-5; -2.0815175480863005e-5 3.254776121876281e-5 -5.149252962146115e-5; 7.361121031677114e-5 -4.8394700935263524e-5 -9.064739934937371e-5; 8.360926759494453e-5 3.995249144119571e-5 -2.3065973831733877e-5; -6.590849183280874e-5 -0.00010153824842877755 -0.00016022458538513353; -2.7982746223110015e-5 -3.8491728478988376e-5 -0.000236998103140367; -1.9955803416704795e-5 -9.360932088104063e-5 0.00011043370673583024; -3.21377890643409e-5 -0.00012315477176808785 7.394992424496227e-5] %
+
+Mass Used: 105.79539677580533 kg
+Launch C3: 94.97955089170318 km²/s²
+||V∞_in||: 3.2770143992101624e-8 km/s
diff --git a/archive/ES_0.5655800941805544 b/archive/ES_0.5655800941805544
new file mode 100644
index 0000000..cd03c54
--- /dev/null
+++ b/archive/ES_0.5655800941805544
@@ -0,0 +1,22 @@
+archive/ES_0.5655800941805544---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T00:11:49.669
+Launch V∞: [7.682590349636599, -6.234502619691033, -0.13413895612375706] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.117761145625634e-6, 1.0376878535653936e-6, -7.491597884163039e-7] km/s
+ V∞_out: [1.9694190894482825e-7, 1.687685111527768e-6, -6.736664405811546e-8] km/s
+ time of flight: 1.7743860085783973e8 seconds
+ arrival date: 2029-12-29T16:41:49.669
+ thrust profile: [0.31281713441143216 -0.04837878913579524 -0.10408043698801929; 0.051638525610383436 0.016282068113653306 -0.07625802432695958; 0.053205872643540104 0.02578916085587391 -0.13146426389927635; 0.028267724255624314 0.017156133939150834 -0.10171612247201683; 0.03458194565810765 0.02121714723497552 -0.15142885326127264; 0.01632058372681476 0.013949360602923433 -0.10561390508354296; 0.011984810745955254 0.009949786739405612 -0.08327434267539088; 0.007355920352459254 0.005641561724104894 -0.052391076282682865; 0.007019012260323998 0.005893769327963886 -0.06421473812534056; 0.002241295550716194 0.001957130961382811 -0.0163054998265085; 0.002888125941897515 0.0032791737488381744 -0.03006399536450298; 0.0015810233105472235 -0.00015308232723170654 0.0011516326946401714; 0.00285722798175516 -0.0028566909208558216 0.004292508169081356; 0.0004960376553653125 -0.0006736843917185675 0.0036510267365266304; 0.0009473792374523385 -0.001070627531514488 -0.002402405097463837; 0.00023306994555144273 -0.008239614688481153 0.003988165636094771; -0.005414339210256062 0.0017152096387515522 0.0011083169600911384; -0.0007062354967585316 0.005948233343934357 0.0017467145147025335; 0.005464765485554764 -0.011825592905935094 -0.004743985075527571; -0.005453721835711278 -0.012672724069028205 0.0018977781715598888] %
+
+Mass Used: 88.70638105756689 kg
+Launch C3: 97.90921065481372 km²/s²
+||V∞_in||: 1.6992429045570395e-6 km/s
diff --git a/archive/ES_0.5655870328004489 b/archive/ES_0.5655870328004489
new file mode 100644
index 0000000..4f07141
--- /dev/null
+++ b/archive/ES_0.5655870328004489
@@ -0,0 +1,22 @@
+archive/ES_0.5655870328004489---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T09:23:36.519
+Launch V∞: [6.450604339098398, -7.48040691246839, 0.13508953741100735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7550525677647606e-7, -6.142695194577125e-8, 7.748114173569855e-8] km/s
+ V∞_out: [-2.8909612379990777e-7, 2.6122737705728668e-8, -3.4446562704505344e-8] km/s
+ time of flight: 1.820922679266863e8 seconds
+ arrival date: 2029-02-04T22:34:43.519
+ thrust profile: [0.2618365264201173 -0.07891723595416361 -0.09851474889926953; 0.03478923172966827 0.0074734981039744205 -0.04043999479667703; 0.044718347426221515 0.019630961557884578 -0.08484757548210102; 0.057667099980135056 0.03396780686346421 -0.14924048884613242; 0.036736470470601204 0.02600968755673235 -0.12199625793414658; 0.02575638395671267 0.02103604752713647 -0.10451914476911632; 0.04134729414241524 0.035026336085579104 -0.18440077570600635; 0.016587021854078447 0.016572409868686515 -0.09124850325887565; 0.001685158896621685 0.0008746659796912055 -0.0191582491488679; 0.002785792837801352 0.005619566080264997 -0.016675639441877638; 0.004073626975073411 -0.0020476740938797653 -0.0042724866412148736; 0.0006850420437576809 0.001056332871547672 -0.00703597895135985; 0.0007877622147648644 -0.0076543649763456635 -0.0068074547059792274; 0.009120741400206085 0.008447216845180195 -0.0002933167858986518; 0.006843307524056959 -0.0031112942482896225 -0.0011571058317446405; -0.003944250978966307 -0.0011164932029394626 -0.0034232866789874602; 0.001358890011245461 0.0013203091816192864 -0.009280607452999062; 0.00020092674484496628 -0.00016505414052236716 -0.0016738414639209291; -0.005664251730447477 0.004924576381001879 -0.005837932988494084; -0.004142990599344644 0.009569718396150966 0.0023101449207180687] %
+
+Mass Used: 90.60551185741951 kg
+Launch C3: 97.58503309881786 km²/s²
+||V∞_in||: 2.9271102517924995e-7 km/s
diff --git a/archive/ES_0.5656001543315292 b/archive/ES_0.5656001543315292
new file mode 100644
index 0000000..94e0164
--- /dev/null
+++ b/archive/ES_0.5656001543315292
@@ -0,0 +1,22 @@
+archive/ES_0.5656001543315292---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T07:26:52.120
+Launch V∞: [6.182155228605818, -7.614488930758931, 0.06394381856835413] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008500868123263022, 0.0009539917589885866, 0.0008658677334398644] km/s
+ V∞_out: [-0.0010058287518620412, -0.0005050202387657998, 0.0010560724751874412] km/s
+ time of flight: 1.7817065035224044e8 seconds
+ arrival date: 2028-12-20T11:17:42.120
+ thrust profile: [0.30499372683724124 -0.09568996041165476 -0.10971064773746333; 0.1099544128035362 0.024217903085891307 -0.11699828329768146; 0.058532932511610895 0.027192236832972144 -0.10453777960490453; 0.07425338266793736 0.04669362272082369 -0.17670842156367292; 0.05118286900185553 0.038238579541083374 -0.15501925030976357; 0.0341456414673147 0.032394390306329825 -0.12552434574163696; 0.019214839656193694 0.019264193329447846 -0.0808724056087221; 0.0117682816769095 0.015208369500086194 -0.06383063063873437; 0.007441811534290799 0.008280753293768872 -0.03606640984950045; 0.0004825435858930216 0.0005596911491985092 -0.00770452746426307; 0.0013922033926748723 -0.0007656502705767206 -0.002361329339603091; -0.002102537214329808 -0.0032761331626690016 -0.005045369899587538; 0.0012216416370048652 0.001585649371898523 -0.010134577205259199; 0.0031027462950993187 -0.0011837145789504063 -0.005482719413563951; -0.001200123141172647 -0.0002650143953245829 -0.005488948049157235; 0.00168843279798482 -0.0006767953583016136 -0.0029813175542504236; 0.0035337221398284357 0.00038251852341366754 -0.004121921556591575; 0.006802923496627849 0.0010447158394203118 -0.003186960797989379; -0.006823356786317257 0.0016709972393250349 -0.002703400193849948; 0.00744337501584073 -0.013674983875165553 -0.0011034941622510264] %
+
+Mass Used: 98.67933312500782 kg
+Launch C3: 96.20357375916164 km²/s²
+||V∞_in||: 0.0015435267398142213 km/s
diff --git a/archive/ES_0.5656046504083709 b/archive/ES_0.5656046504083709
new file mode 100644
index 0000000..8988bdb
--- /dev/null
+++ b/archive/ES_0.5656046504083709
@@ -0,0 +1,22 @@
+archive/ES_0.5656046504083709---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T03:39:28.145
+Launch V∞: [6.357601633184473, -7.317079317692776, -0.03603322807409289] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1011493728826465e-8, 1.7440733149625453e-8, 8.452732632704966e-8] km/s
+ V∞_out: [-5.759942639036411e-8, -5.3661091235032974e-8, -2.7383272511001678e-8] km/s
+ time of flight: 1.8749577785533196e8 seconds
+ arrival date: 2029-04-07T05:49:05.145
+ thrust profile: [0.47419514449624833 -0.1167048869231272 -0.1302370421791166; 0.13240772080250574 0.04642131978540583 -0.1152867995804275; 0.03541496678363544 0.024721840678357566 -0.055852114741090024; 0.04119213490594108 0.04005145591520012 -0.09146627619610452; 0.03924451025695613 0.049013272686604485 -0.11324193367515575; 0.08599640507905057 0.1133251909915859 -0.25008693092712647; 0.011053092542380927 0.015672422007670713 -0.045466508868779336; 0.005713531697764188 0.009257096225809754 -0.029774464131286944; 0.006687041554257373 0.013861278036475114 -0.03934148561912452; 0.002639949568455259 0.006072049475595134 -0.02302332637047547; 0.0018516434372459227 0.007852390931738654 -0.024122869841522187; -0.0005450225906193481 0.003378896086343817 -0.003254633905326155; 0.0005006190049142247 0.00011367949786464176 -0.001732599646713131; -8.316152040848735e-5 0.002157683199456197 0.00010402087607790339; -0.0021529805104755734 0.0007083403866145101 0.001005117668725294; 0.002895221481207952 0.005897564517402831 0.0014126379367987425; 0.004699244362846961 -0.00486107777078881 -0.002779811148710873; -0.0036768190605405834 -0.0009299129588713744 0.002608990250845436; -0.003761815920990681 -0.004049815153574681 -0.0001512044209881437; 0.0019150344459392924 0.004975352542453899 0.003260483934373106] %
+
+Mass Used: 111.77181995275032 kg
+Launch C3: 93.9600466612027 km²/s²
+||V∞_in||: 8.700747705189463e-8 km/s
diff --git a/archive/ES_0.5656082693493839 b/archive/ES_0.5656082693493839
new file mode 100644
index 0000000..fdffe11
--- /dev/null
+++ b/archive/ES_0.5656082693493839
@@ -0,0 +1,22 @@
+archive/ES_0.5656082693493839---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:25:43.547
+Launch V∞: [6.248609060153668, -7.668213146018595, 0.010064836522826578] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.912903679805769e-9, -3.6253200097719846e-10, -4.356109596278411e-9] km/s
+ V∞_out: [-1.5737400874942726e-9, 3.4789531040453425e-9, 5.0661598050837885e-9] km/s
+ time of flight: 1.7826011000845554e8 seconds
+ arrival date: 2028-12-23T11:07:33.547
+ thrust profile: [0.24215800754090694 -0.08965510507541727 -0.09858191787938143; 0.07389200783044464 0.008132772853794192 -0.09417498292621766; 0.038584572486637686 0.011075676437401493 -0.0830976637261194; 0.03976249901576087 0.015646826699290642 -0.11532548456749267; 0.03695982148927781 0.018309407837607178 -0.13978579974556085; 0.021392508050508244 0.012386825908343077 -0.0975232160615311; 0.027548146025020228 0.017273182562386902 -0.14715988520622122; 0.020136275801380173 0.012289645388033094 -0.11795613948970511; 0.006058876570180356 0.0034167662885971847 -0.040240538684716505; 0.005634769268864362 0.004498061501166271 -0.04791121257402469; 0.0006893568310877159 0.000687920248856723 -0.007785847941324697; 0.0023225631458624538 0.0007362598215559973 -0.004946123378127876; 0.0020295672618542283 0.0008418933196123606 -0.001978320491121975; 0.00015783415005530006 0.0001038739048452215 0.001401764450340791; 0.00019535005549210015 -0.00019804008303700237 -0.0015191406235434996; -0.00016836838505039222 -0.0025001190262244266 0.0038034245114469006; 0.0030369410597853356 -0.0006593911197984825 -0.0016170471091679773; 0.0012259769500473196 0.001998019161925951 0.004821096309149166; -0.0004067426279193661 -0.0014382401816928285 -0.0012619573591349763; 0.0009515332052782801 -0.0006047469817415919 -0.0020812889629681125] %
+
+Mass Used: 89.103843088958 kg
+Launch C3: 97.84670934034114 km²/s²
+||V∞_in||: 6.575997478221114e-9 km/s
diff --git a/archive/ES_0.5656088129371041 b/archive/ES_0.5656088129371041
new file mode 100644
index 0000000..d890cb6
--- /dev/null
+++ b/archive/ES_0.5656088129371041
@@ -0,0 +1,22 @@
+archive/ES_0.5656088129371041---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T14:31:29.501
+Launch V∞: [7.4737853603345545, -6.365622826786243, -0.052775070072211314] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0363454602261779e-8, -6.91414641102579e-9, 5.188231994866241e-9] km/s
+ V∞_out: [-4.571421394069967e-9, -8.583111101521187e-9, -2.7676268551282375e-10] km/s
+ time of flight: 1.6593945197043976e8 seconds
+ arrival date: 2029-08-13T04:49:00.501
+ thrust profile: [0.3982544162905184 -0.06826060825302199 -0.11930717088409926; 0.026852090827052363 0.01036628253199794 -0.03038326567158089; 0.03999990923142866 0.028250630068498872 -0.07584299542813891; 0.022959708061137517 0.02087058614502586 -0.06575963901346886; 0.05220943441742878 0.050719243201971326 -0.1705130710779443; 0.031127930799979237 0.03727768341556637 -0.12623534637472647; 0.03541647786468855 0.04404702543966673 -0.14488779106312033; 0.012749682673927856 0.01868666398934925 -0.07373560938982321; 0.036729778091614484 0.04727572511183925 -0.18681036462720582; 0.007525628563248578 0.008539199227687498 -0.033501587506348254; 0.004490481752170175 0.00653484299101558 -0.03368703888997624; 0.0014405437749685957 0.0010845891029375144 -0.004014180267045167; -0.00057292496323235 0.0005004022688050723 -0.0018675104146050486; 0.0006872851869594306 -0.0012708640843733172 -0.00031189439931648055; 0.001933850332596877 -0.0006140003637105178 -0.003224701608435387; -0.005533414839685281 0.0005036034177164113 -5.968285182011979e-6; -0.0021546252512308593 0.0010454548178060405 -0.0014390323922980452; -0.0013356548316265943 0.0005468930721975698 0.0008046761748414194; -0.001348811393349662 -0.004495858782584808 0.0006333205316930452; -0.0018365803104498225 -0.004625374667360516 0.00303213417839702] %
+
+Mass Used: 97.65207546585452 kg
+Launch C3: 96.38140679327432 km²/s²
+||V∞_in||: 1.3495345979958994e-8 km/s
diff --git a/archive/ES_0.565612041946955 b/archive/ES_0.565612041946955
new file mode 100644
index 0000000..5f55ee8
--- /dev/null
+++ b/archive/ES_0.565612041946955
@@ -0,0 +1,22 @@
+archive/ES_0.565612041946955---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T14:37:05.625
+Launch V∞: [7.617199158843039, -6.077433017618617, -0.2730684578204187] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.503523530802447e-6, -7.560305706181158e-6, -6.083121417327273e-6] km/s
+ V∞_out: [-1.3164482505137375e-6, 8.906031710869905e-6, -1.0157302513764892e-5] km/s
+ time of flight: 1.8749577787426522e8 seconds
+ arrival date: 2030-04-22T16:46:42.625
+ thrust profile: [0.24706950103168615 0.028952331955518485 -0.0635527753737683; 0.17039580266340915 0.14187095971740973 -0.12725288634471368; 0.09796501626039038 0.13745028518650146 -0.13604932699700287; 0.06044301358716032 0.12100932820319557 -0.131053694815414; 0.04855620700060682 0.13358961588117244 -0.145721569453928; 0.019891321063688384 0.06989646217412614 -0.09298809392822475; 0.00988677255227137 0.04414218168713727 -0.06332532743178627; 0.0033752814023085094 0.018371078722019145 -0.028824920554022318; 0.000740552017796243 0.0025287781605094805 -0.004154219117901032; 0.00013993130982951782 0.004002817232767889 0.0014965302710328553; 1.3278272126567107e-5 0.0021477658156285485 -0.0019554076658864243; -0.0005069076641351061 0.0010374823775010013 -0.001831797104248573; -0.000344343645207628 -5.195472804003288e-5 -0.0010467649775648847; 0.0010795473962884547 -0.0028066679586084644 -4.9232586048195614e-5; -0.005416681359806275 0.005058682217609011 -3.0563262285001605e-5; -8.082924241758927e-5 -0.0068687843851182135 0.0006818393655584616; 0.002697499957386189 0.002300895503627223 -0.002236051076659758; -0.0010358768920165056 0.0033711450163014757 -0.002102970162336977; -0.00023182722966420702 -0.011427744714423614 -0.0015869429541363745; -0.0046380747519071145 -0.0028999995712055155 -0.00799651777337953] %
+
+Mass Used: 105.53040690275157 kg
+Launch C3: 95.03148149177646 km²/s²
+||V∞_in||: 1.3582324839635405e-5 km/s
diff --git a/archive/ES_0.5656224107763604 b/archive/ES_0.5656224107763604
new file mode 100644
index 0000000..eedaf23
--- /dev/null
+++ b/archive/ES_0.5656224107763604
@@ -0,0 +1,22 @@
+archive/ES_0.5656224107763604---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T05:36:43.270
+Launch V∞: [8.038933596166302, -6.147955821552678, -0.09016690034013546] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3060076053535517e-8, 1.943002872568467e-7, -3.585465441427411e-8] km/s
+ V∞_out: [2.8884169026236803e-8, -1.1543370604513625e-7, -1.559147882980159e-7] km/s
+ time of flight: 1.8608742222027668e8 seconds
+ arrival date: 2030-04-14T00:33:45.270
+ thrust profile: [0.07023734985850105 -0.010820236301619879 -0.03321356610933114; 0.02663653773477778 0.004472334099819988 -0.043877786780785764; 0.06107324579931441 0.009010579760913587 -0.17202373798267837; 0.023256782605692673 0.0032295000677397415 -0.08992516139344181; 0.013143192313307957 0.0003861890099825538 -0.06322585526591966; 0.01183969016248165 -0.0004910486603125554 -0.06175134911051707; 0.02925093775921988 -0.0024043939687518863 -0.16631227049552372; 0.007695818872049882 -0.0009212716694864627 -0.04848153157654403; 0.009671466141311555 -0.000328053980843756 -0.05482143318211164; 0.0023198896781470753 -0.000662154771723579 -0.015716183962517262; 0.0017114022054825217 -0.000846264919395595 -0.013570064531849977; 8.924809067004059e-5 -2.268447477207894e-5 -0.001723470598145647; 0.00015502057435165648 -0.00018319177881715603 -0.0003375348814247325; 0.00019113665467348278 -0.00022045707132575703 -0.0007347176443685666; 6.968872875336466e-5 -3.6763181143812176e-5 -0.000522308370148679; 0.0002898659795303502 -0.00016256626579902006 -0.0003048150919037584; 5.882697087015595e-5 -9.972433111562878e-5 -0.0006367044274405212; -7.432452710782306e-7 9.856607156579473e-5 0.00041086766167709493; 3.6453575683416164e-5 2.773671068330262e-5 -0.00024740286816775684; 5.510936432759491e-5 0.0001812979869122704 0.0002396191502342035] %
+
+Mass Used: 62.38480463845235 kg
+Launch C3: 102.42994421725169 km²/s²
+||V∞_in||: 1.9892190673441427e-7 km/s
diff --git a/archive/ES_0.5656318919458854 b/archive/ES_0.5656318919458854
new file mode 100644
index 0000000..2e4a98a
--- /dev/null
+++ b/archive/ES_0.5656318919458854
@@ -0,0 +1,22 @@
+archive/ES_0.5656318919458854---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T11:26:50.133
+Launch V∞: [6.801249158576139, -7.164221208361966, -0.20139543678908628] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5159712962324358e-7, -3.906061881736378e-8, 4.9877171321908124e-8] km/s
+ V∞_out: [-1.5272723310754315e-7, 4.076810452714763e-8, -3.907059726486791e-9] km/s
+ time of flight: 1.8749577784859926e8 seconds
+ arrival date: 2029-04-06T13:36:27.133
+ thrust profile: [0.26688594181570857 -0.06783928549399068 -0.09610082523228398; 0.08585572768021166 0.025000030921855713 -0.09409264904645555; 0.05011556347383327 0.028175366131781596 -0.09366415121776868; 0.0503382085997942 0.038386068840181545 -0.1324794777591383; 0.041427932727718206 0.040346622371516025 -0.14218570126556354; 0.036231112522750346 0.039660200816823976 -0.1527676718889515; 0.014501342835617645 0.017360067115293663 -0.07206970423812327; 0.012254552307270307 0.016309433153300093 -0.07063254568369222; 0.003897854874180987 0.005450873756483766 -0.02511822957502231; 0.002096952609001236 0.0030350921864929613 -0.015088568834353734; 0.00017822605275980696 0.0006864256431083968 -0.002180565845110942; -0.0004092645619534507 0.001555989147955442 -0.0024388157281943473; -0.00012607719092153275 0.00017901499299290624 -0.0017850921646472692; 0.00046518386015274133 0.0010065152047265633 -0.00323036146075951; -0.0013327536305031797 0.0008377156928908024 -0.0006928076537745299; 9.051124284833491e-5 0.0013416065262417452 -0.002605537364239441; 0.00046799032698465945 0.002320883170037838 -0.0019499385008292032; -0.0003339074272884386 2.1502412087370793e-5 0.0016391273903721298; 0.0016200058906725657 0.0029023550730484828 -0.002113159898481802; -0.0017657061755024508 0.0015963183908782406 -0.0022915590021072556] %
+
+Mass Used: 90.43278199574252 kg
+Launch C3: 97.6236157613355 km²/s²
+||V∞_in||: 1.6430202029030832e-7 km/s
diff --git a/archive/ES_0.5656454347393535 b/archive/ES_0.5656454347393535
new file mode 100644
index 0000000..91cb764
--- /dev/null
+++ b/archive/ES_0.5656454347393535
@@ -0,0 +1,22 @@
+archive/ES_0.5656454347393535---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:20:21.046
+Launch V∞: [7.728122429140452, -5.602649290237379, 0.21183992173161462] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6212434909284065e-6, 1.7098546610995343e-5, -0.00042497981803420073] km/s
+ V∞_out: [-1.7563619641685487e-5, 0.0004256244432850386, -3.1443704986307556e-6] km/s
+ time of flight: 1.8111362470327675e8 seconds
+ arrival date: 2030-02-01T23:40:45.046
+ thrust profile: [0.8138513167862973 -0.03635184758990619 -0.21419232584620856; 0.10440750462164858 0.05992874084150588 -0.10006859567975396; 0.0573669268384033 0.056026470966157774 -0.10273385156350226; 0.08208607433383094 0.10867486066724336 -0.19979714518885036; 0.02034370494523369 0.03249145978656693 -0.07097605906655556; 0.01322987754321691 0.028520678608893252 -0.06806741120292192; 0.006831048287498443 0.01389703017206118 -0.03512365583718846; 0.011874595053860473 0.024114761439067007 -0.06977855668074341; 0.004751946916787912 0.01533173057862125 -0.04571592318691169; 0.0007670246440726889 0.002388646579317529 -0.009013281805049152; 0.002135728730920692 0.008889147077913035 -0.026690816919964087; 0.0004441027157831031 0.0003737634069891747 -0.0013425919211082927; -0.000843643778010564 -0.0016482541148755423 -0.00017728506451175022; 0.00373554244453873 0.00015126945159495668 0.0010804258804281812; -0.0025331346065984106 0.008042768114585255 0.00284310050092692; -0.00484098167816681 -0.0048861760506472415 9.285385552231787e-5; 0.002319973972273323 0.0023554944037366965 -0.0004360981597236948; 0.0035349712152466578 0.006421572991016207 -0.009430354542155295; -0.004721327640132021 0.0006285336935936504 0.005622052285842708; 0.0005800022874794435 -0.004089974157158978 -0.003838015222454743] %
+
+Mass Used: 128.16215676979346 kg
+Launch C3: 91.15843150162038 km²/s²
+||V∞_in||: 0.000425331725774165 km/s
diff --git a/archive/ES_0.5656575741448574 b/archive/ES_0.5656575741448574
new file mode 100644
index 0000000..8b7d3bf
--- /dev/null
+++ b/archive/ES_0.5656575741448574
@@ -0,0 +1,22 @@
+archive/ES_0.5656575741448574---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T14:51:28.512
+Launch V∞: [6.518777544331289, -7.677947547573857, 0.26197371865754954] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.013347322478010681, 0.007414326578321844, -0.015688816134223772] km/s
+ V∞_out: [0.014347380408247498, 0.005533082811861717, 0.015602661198678622] km/s
+ time of flight: 1.8496530185445422e8 seconds
+ arrival date: 2029-03-15T10:06:29.512
+ thrust profile: [0.022123200749267855 -0.008039710194972615 -0.010346489236184876; 0.05059177151164425 0.0013651877285744186 -0.07153301070108864; 0.040388424576371484 0.005026633588999455 -0.09672859407855186; 0.0298186106490272 0.004376208744322689 -0.09813786136098976; 0.024055578016023503 0.0033487366811472403 -0.09881154411532878; 0.03982338202979327 0.004130894861292811 -0.19122899280907554; 0.021764461157244182 0.0017342677761398807 -0.11940287122947593; 0.012805676787449283 0.0007574325690198866 -0.07779843370839624; 0.013721821146180566 0.00025924607444452425 -0.09006660583174889; 0.0005071859563429384 1.549178709340928e-5 -0.0037213108924639355; 0.00013680144740496345 2.16645158574952e-5 -0.0013852172512434854; 0.0002244914006373633 4.6029419043122045e-6 -0.0005809979756160974; 2.4487379005921927e-5 6.17041670429668e-5 -0.0006997349802103563; -0.00027921973304210156 -0.00028164289373789416 -0.0004944253258789893; 0.0008241681795176606 6.301127009307906e-5 -0.0005008625650021451; -7.71079747157063e-5 -0.0001789816870087481 -0.00017010272820877393; 0.00015770198235474635 0.0005495407532878467 2.689210048028494e-5; 0.00010807916797938788 0.00043662874418249855 -0.00030730715893828803; -0.0003071171272674353 -0.0006288629874578339 0.0007781286055874546; -2.5972865806358385e-5 5.104461110664915e-5 0.00021977502532647222] %
+
+Mass Used: 67.76901473959697 kg
+Launch C3: 101.51396944504056 km²/s²
+||V∞_in||: 0.02189205809501471 km/s
diff --git a/archive/ES_0.5656582389607862 b/archive/ES_0.5656582389607862
new file mode 100644
index 0000000..6b76e07
--- /dev/null
+++ b/archive/ES_0.5656582389607862
@@ -0,0 +1,22 @@
+archive/ES_0.5656582389607862---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T12:31:48.227
+Launch V∞: [7.501216817873034, -6.223474456707456, 0.019738123489436828] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007334260248645713, 0.0005609135973561538, -0.00042439488091486224] km/s
+ V∞_out: [0.00016799926368532233, 0.0010011682021995112, -4.2883638016109063e-5] km/s
+ time of flight: 1.6730683634691492e8 seconds
+ arrival date: 2029-08-27T22:39:04.227
+ thrust profile: [0.4852141633867371 -0.07070694821467509 -0.16516738252090613; 0.0525006668014496 0.01931232208554062 -0.061387158042877595; 0.06998843132431566 0.044426439438399905 -0.13438294117723448; 0.08481955122268404 0.07097433006457457 -0.22390472730375066; 0.033898173089010726 0.03324403122859085 -0.12182950712257555; 0.01766627653389531 0.01963773986172472 -0.07996606764825887; 0.017577476470385274 0.021753388592851333 -0.09187771933583921; 0.0011660103703056827 0.009858911591987849 -0.041386091665272386; 0.00703688542595259 0.007857618982812538 -0.04566517896086735; 0.011429843805959704 0.01633900409539043 -0.0793663452438991; 0.005620758514429303 0.009376916351020292 -0.04103115837182496; 0.000991364325052705 0.001548658148187008 -0.013919671879367544; 0.004809103943713847 -0.00046172440440832665 0.002837084935132711; -0.002164358606345276 -0.0007816705353687317 0.0020443381589034457; -0.0039191987048396 -0.0020237917016810046 0.0019272272834385323; -0.00340537028894238 -0.0026457793019148065 0.005724017506966069; -0.0018600652899391358 -0.003069896863610537 0.0043162032291582195; -0.004508052845092312 0.0004492202347953397 0.005271958411338545; 0.00033415233922108535 -0.0006582719532687558 -0.0022389262082127327; -0.00421874445918941 -0.0026926207701357145 -0.0012639492402815888] %
+
+Mass Used: 105.76632579687384 kg
+Launch C3: 95.00027765555029 km²/s²
+||V∞_in||: 0.0010161932948973872 km/s
diff --git a/archive/ES_0.5656584962730732 b/archive/ES_0.5656584962730732
new file mode 100644
index 0000000..d3d777a
--- /dev/null
+++ b/archive/ES_0.5656584962730732
@@ -0,0 +1,22 @@
+archive/ES_0.5656584962730732---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T14:20:09.191
+Launch V∞: [7.411042078466391, -6.203334994848626, -0.1417486770568867] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006164019806589364, 0.0004815171486134261, -0.0003765536234896947] km/s
+ V∞_out: [0.00014011884650171129, 0.0008559244809589382, -3.593773154622557e-5] km/s
+ time of flight: 1.667390668737999e8 seconds
+ arrival date: 2029-08-20T10:44:35.191
+ thrust profile: [0.6010779007741536 -0.09342269182962896 -0.19819599956044934; 0.10145326247765359 0.03865788006491725 -0.11346788330059325; 0.07645227320901374 0.05162663255741935 -0.14572880621843387; 0.06044077946013159 0.05356849997738495 -0.16557363033484254; 0.04615054533433635 0.04917998167103983 -0.16608680311684162; 0.022069352518284485 0.028260914194736572 -0.1028789236553973; 0.013683491426383768 0.01856864120048593 -0.07340446364098703; 0.014923646897521698 0.02267373048893578 -0.09316037526355875; 0.0025265140284225123 0.005934402086563549 -0.02809228492550269; 0.005375759857072143 0.007727496614164375 -0.031537179514137426; 0.0006969411153680701 -0.0004358801803248534 0.00013020415632551859; -0.0017047745615071251 0.0013352055889100265 -0.0028499717527584283; 0.00010829500169338873 -0.001662637437627376 0.0016515091610261156; -0.0009568030721211544 -0.001151378628415178 0.005945779527284483; 0.0047960560790409204 -0.00435473047075977 0.001018271631237741; -0.0027072669355840424 0.0005800395516492432 0.009300215785608475; 0.0008998589526805486 -0.0031439651782608404 -0.0007243694788396534; 0.0007342336836690978 -0.003244439211082379 -0.006279121367165931; 0.0016211258259799213 -0.0054044195131962135 -0.000700167384512335; -0.00401433417960206 -0.005091915717630213 -0.005806377642400614] %
+
+Mass Used: 114.9557314503163 kg
+Launch C3: 93.42500243456041 km²/s²
+||V∞_in||: 0.0008681029878604742 km/s
diff --git a/archive/ES_0.5656618102509928 b/archive/ES_0.5656618102509928
new file mode 100644
index 0000000..49d7c04
--- /dev/null
+++ b/archive/ES_0.5656618102509928
@@ -0,0 +1,22 @@
+archive/ES_0.5656618102509928---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T06:00:28.473
+Launch V∞: [6.448653861871963, -7.485322305576425, 0.10982300079847541] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0579414674451376e-7, -1.670639244610568e-7, -1.2336435680583952e-7] km/s
+ V∞_out: [5.681762861098413e-8, -1.214264703090118e-7, 1.8212509031188577e-7] km/s
+ time of flight: 1.8554970811158067e8 seconds
+ arrival date: 2029-03-18T19:35:36.473
+ thrust profile: [0.25347649761797736 -0.0709387360603699 -0.09571141000266895; 0.0658107130301214 0.015078191395889467 -0.07740234758548208; 0.03566429444438426 0.016153629433094487 -0.07182067357127223; 0.036748654003668564 0.02245030925722785 -0.10174920251979448; 0.06406217525385284 0.045621527259795056 -0.21610231298109012; 0.028147914348905845 0.023298679515118548 -0.11951590705137674; 0.01677044838746259 0.015312722843012952 -0.08511298763722673; 0.007964232673871767 0.00813177898124743 -0.046226551211833; 0.0023670435939197685 0.003959099906764837 -0.021918397200265602; 0.003731270587807682 0.0015113468558286126 -0.025911473372231986; 0.004593553437767627 0.00256838700842557 -0.01708289099700256; 0.0041685738791661636 0.002521340279702738 -0.029953557722799194; 0.0020872299700936056 -0.0018046765891223731 0.003667604033724647; 0.0002990881219019271 6.825750405326132e-5 0.0014427420020220482; 0.001126334224428267 0.0048788192420422365 0.0003671114409911562; -0.005050125913392737 0.0025277734510109704 -0.0033037564164531048; -0.0002826589459658849 0.0018455560232081836 0.0002808951264314809; -0.004314192431945067 0.007229817874061519 -0.013844475861883676; -0.0044085207985045515 0.004993267722869646 -0.01022189655279233; 0.007227091441789756 0.003107168864891296 0.01119882814725991] %
+
+Mass Used: 90.44650014223862 kg
+Launch C3: 97.62724774010051 km²/s²
+||V∞_in||: 2.330697768305618e-7 km/s
diff --git a/archive/ES_0.5656635395475118 b/archive/ES_0.5656635395475118
new file mode 100644
index 0000000..ecf6711
--- /dev/null
+++ b/archive/ES_0.5656635395475118
@@ -0,0 +1,22 @@
+archive/ES_0.5656635395475118---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T03:37:47.528
+Launch V∞: [6.506167294108336, -7.329996498167685, 0.21918071750747833] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0274583731809644e-7, 2.0519591596705923e-7, 9.282599536144068e-8] km/s
+ V∞_out: [-7.970663743700535e-8, 1.242271544573901e-7, -1.9915233142830916e-7] km/s
+ time of flight: 1.8331431328070098e8 seconds
+ arrival date: 2029-02-15T20:16:20.528
+ thrust profile: [0.3341850530878233 -0.08618820763067343 -0.09282919851775107; 0.05379281862659381 0.01732863292727409 -0.05026070934922586; 0.11335816406101404 0.06864132737874748 -0.16364780209012142; 0.08983621893308374 0.07325426774579873 -0.18025550602427484; 0.05345489538262889 0.054517204986147566 -0.14222240726336763; 0.0328795803639049 0.0399484306491414 -0.10965793502207227; 0.010859191980151993 0.014730580852631495 -0.04608278673460581; 0.018366885944452297 0.029617661921752584 -0.08581480131232462; 0.005941028325900952 0.010259031205291475 -0.03280018170062335; 0.00019688538269763676 0.0028704604212899465 -0.006674288795745887; 0.0008310966067705233 0.0015677048276157917 -0.00532312960328449; -0.0003168477717843117 0.002184436743484396 -0.005124290115365304; -0.000311119150624786 -0.00011007007155040913 -0.0006141885437955484; -0.0008983129931693517 0.00024126740619694493 0.0026352346115489068; 0.00031367071133108686 0.0004931541457384014 -0.0009165768265539693; -0.0007209864595247908 -0.005066344209659684 0.0005758521587492739; 0.0016658706247687333 0.00023303981164068716 -0.004290585020862302; -0.0008494569883808652 0.0005076251641756642 0.0028526834372378496; -0.0014030879494512458 -0.001427782420778778 0.004675195285817954; -0.00010456143182782369 -0.0006379936603176776 0.0019408359441987393] %
+
+Mass Used: 99.31603616958182 kg
+Launch C3: 96.10710170900262 km²/s²
+||V∞_in||: 2.475454229643509e-7 km/s
diff --git a/archive/ES_0.5656661676564458 b/archive/ES_0.5656661676564458
new file mode 100644
index 0000000..5c5aca0
--- /dev/null
+++ b/archive/ES_0.5656661676564458
@@ -0,0 +1,22 @@
+archive/ES_0.5656661676564458---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T06:42:20.949
+Launch V∞: [6.315290423019312, -7.358710284922364, 0.14886198010316626] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013727601214200016, -0.006332289923668199, 0.013970877711332522] km/s
+ V∞_out: [-0.013106488431248838, -0.005358961971345188, -0.014934949279675062] km/s
+ time of flight: 1.874957778833418e8 seconds
+ arrival date: 2029-04-08T08:51:57.949
+ thrust profile: [0.5056265278487008 -0.10875621844692729 -0.14422588718679447; 0.060356505120773875 0.021675797453560214 -0.058981724586706606; 0.08663636308486589 0.0546929424410848 -0.13467970284848757; 0.05168665808675559 0.04502656213098166 -0.11617998119015985; 0.047629921743308226 0.05010634370537829 -0.13628643142618543; 0.03168516413583036 0.04025022613908475 -0.11676447215935863; 0.013074519798943156 0.021723690090994997 -0.06609568826557341; 0.017121728399280917 0.02260155864263946 -0.07381681431661521; 0.004119956817315107 0.006473445527483732 -0.026765706509049678; 0.004625628144562934 0.011573119570674502 -0.0392516774804134; 0.005811718445226157 -0.001014993358921973 -0.0017373147342055312; 0.002787805618291987 0.0011613392440389745 -0.004662656004416713; 9.073488706681755e-5 -0.0007020406233922749 0.00019390100153915315; -0.0011558231993157113 -0.001992853948534571 0.005509856586576911; -0.007579559414425674 -0.005506569580683719 0.0026606453030032437; -0.0017399074761858218 -0.0007875503290643339 0.0004503519472139161; -0.0003453647856296769 0.001592815218000968 -0.0027118760074343762; -0.0031208149906380225 0.009168141833112323 0.0064935337715900324; 0.010544164271717076 -0.005161107474081257 -0.0059498530719127194; -0.00487219766025041 -0.001458259223871262 -0.0003804697063487764] %
+
+Mass Used: 111.28578683639262 kg
+Launch C3: 94.05567007362185 km²/s²
+||V∞_in||: 0.020584711676351054 km/s
diff --git a/archive/ES_0.565667964791674 b/archive/ES_0.565667964791674
new file mode 100644
index 0000000..8d101f9
--- /dev/null
+++ b/archive/ES_0.565667964791674
@@ -0,0 +1,22 @@
+archive/ES_0.565667964791674---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T20:39:11.023
+Launch V∞: [5.96267075797282, -7.510498669697487, 0.14677241499888077] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7462223882496595e-8, -7.537726061853019e-9, 2.376052973414738e-8] km/s
+ V∞_out: [7.683856813774538e-9, -1.8025081743495836e-8, -2.4066893748770384e-8] km/s
+ time of flight: 1.750141865622071e8 seconds
+ arrival date: 2028-11-10T11:42:17.023
+ thrust profile: [0.6265161129809692 -0.20187081507224122 -0.19543595896322333; 0.1569315115751736 0.034233175029056005 -0.14822826274430945; 0.11269781625805404 0.05312299084823215 -0.17415345411765945; 0.05905633896306351 0.03934407245300674 -0.12941324100067342; 0.06222639744581581 0.051009869506321165 -0.17108064560942587; 0.02541132905391349 0.024276895490736885 -0.08746305990855127; 0.008369531810493045 0.009419076740259328 -0.03617520240434305; 0.01222599461654563 0.014593912313934837 -0.05724185456339487; 0.008688871870513148 0.009248067795868793 -0.04379119892110653; 0.00975584841435907 0.013371325945509367 -0.056103487684214526; 0.00043695388887837896 0.001202610799288263 -0.004534876806620674; 0.000497470213265709 0.0007158924112766587 -0.0030131252943776223; 0.0005567434482261644 3.361495443658793e-6 0.0003212302186634986; 0.00016928277434562127 -2.0192508112789026e-5 -0.00196300203212415; -4.779172366690454e-5 0.00025672425957050973 -0.0008130278118785423; -0.0011826788600401462 0.001044281561393729 0.0010641922946548867; -0.0009775610482865306 0.0006163547393109297 0.00034996063873984543; 0.000486545226035638 -0.0004014260694874261 0.0018300182681396978; -0.0006708551095559476 0.0001357108746357837 0.0005909870724492893; 3.684539411507726e-5 6.288662419739299e-5 -0.00021066391861394884] %
+
+Mass Used: 123.3809382226068 kg
+Launch C3: 91.98257497731649 km²/s²
+||V∞_in||: 3.0435330626646304e-8 km/s
diff --git a/archive/ES_0.5656769019406248 b/archive/ES_0.5656769019406248
new file mode 100644
index 0000000..7477e65
--- /dev/null
+++ b/archive/ES_0.5656769019406248
@@ -0,0 +1,22 @@
+archive/ES_0.5656769019406248---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T22:06:59.026
+Launch V∞: [6.305813745276205, -7.738711173562777, 0.0036093492368449533] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.683558375348939e-9, 1.3536059423179147e-9, 1.0357197453947333e-8] km/s
+ V∞_out: [-5.657273696787805e-9, -8.341452710367432e-9, -3.974645085927601e-9] km/s
+ time of flight: 1.7641812888448575e8 seconds
+ arrival date: 2028-12-01T19:09:07.026
+ thrust profile: [0.09520147200147386 -0.03419168641311985 -0.0412792315427303; 0.03487978399781713 0.004913828679692458 -0.044925273384726586; 0.05620907846090092 0.0184808532326866 -0.11236742858233952; 0.04638527944598881 0.020960692310550134 -0.127205210633059; 0.05248681278314422 0.028226003678304405 -0.17873999007043695; 0.024645578244122158 0.01513486319943602 -0.1048693792464699; 0.01995852757915767 0.01354174713843524 -0.09581575458284956; 0.027676338038215925 0.020450077458024015 -0.15074555467299258; 0.009911681817028456 0.007950446168564709 -0.06142774336078383; 0.005414772359903561 0.0045444376667720865 -0.03777807258877372; 0.0017665513216640577 0.0018272867510357395 -0.016175159744628836; -0.00011581011138291574 -0.001105886494674663 -0.0010407442944013866; -0.001170091661072084 -0.0004953808007881541 0.0003216034724701207; -0.001956178520835954 -0.0006113400416344373 0.0003610877161931512; 0.00034348561236369744 0.0006601967956372471 -0.0015532929788633295; 0.0017925828489960753 -0.0008321151868256615 0.00048771305219583335; 0.0006407464924379433 -0.000338466249557337 -0.0001922552208772695; -0.0004781931501059117 -0.00015314894416602063 0.00484267420044522; 0.0028977118467248455 -0.0017192825688316072 -0.000988835186790163; 0.002784581999044938 0.0018643862483415925 0.000702646453775003] %
+
+Mass Used: 78.65917349956953 kg
+Launch C3: 99.65095064534161 km²/s²
+||V∞_in||: 1.0580083031353726e-8 km/s
diff --git a/archive/ES_0.5656778450046895 b/archive/ES_0.5656778450046895
new file mode 100644
index 0000000..cecf651
--- /dev/null
+++ b/archive/ES_0.5656778450046895
@@ -0,0 +1,22 @@
+archive/ES_0.5656778450046895---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:44:58.490
+Launch V∞: [7.528803394218295, -5.607150718948696, 0.2372403101879216] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.840599710493783e-7, 3.464231309637352e-6, 7.893258280103145e-6] km/s
+ V∞_out: [7.913310534041444e-6, 8.897472168329393e-7, -3.439017444755601e-6] km/s
+ time of flight: 1.87495777871182e8 seconds
+ arrival date: 2030-04-16T17:54:35.490
+ thrust profile: [0.8921406560864477 0.03522700171590061 -0.15749187934226697; 0.19669142964263564 0.1453315869432337 -0.14031663962318022; 0.1325088780465242 0.16739953741906657 -0.17465561320787445; 0.042234575559658254 0.07512237699819169 -0.091321911226816; 0.020392293114992553 0.04802319541689045 -0.06454633676886964; 0.03976014956422098 0.12409483494339446 -0.1624474837926876; 0.005182186026647217 0.020326388602240023 -0.03162029619498605; 0.0002968670749672659 0.001815173503518195 -0.003032803980210339; 8.892708955143144e-5 0.0010006454118601628 -0.0018853911227489709; 0.00023959298247256433 0.0011853656673523846 -0.0028241049365313737; 0.00030951700356245717 0.0043685784267728945 -0.007459101449355557; 7.029858623791357e-5 0.0003709582784304776 -0.0005141864153168468; 0.00026094703440052066 0.0010971998135071888 -0.0013397415758350341; 0.0007560245172127591 0.0006327835877068026 -0.0009704135720204662; 0.00013880155422534227 0.0006532186524265758 -0.0010992354929388595; 0.00031250225125293635 -0.00013331984975393032 0.0013869162373974086; -0.0004035750241651627 -0.0005378003909731803 0.0013918987119132364; 0.0009496488705759938 0.0008098305964917176 -0.0006516418748796184; -0.0015494257488440984 -0.0019888775355002613 -0.00046285749880554424; 0.0004566228889507244 -0.001152802809194861 -0.0004744719267986892] %
+
+Mass Used: 145.57822009710026 kg
+Launch C3: 88.17930269857786 km²/s²
+||V∞_in||: 8.655586339543412e-6 km/s
diff --git a/archive/ES_0.5656843717925183 b/archive/ES_0.5656843717925183
new file mode 100644
index 0000000..2ecdee3
--- /dev/null
+++ b/archive/ES_0.5656843717925183
@@ -0,0 +1,22 @@
+archive/ES_0.5656843717925183---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T06:15:28.957
+Launch V∞: [6.0740899995356195, -7.406187598474327, 0.1073888808837251] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.47169778164105997, -0.34091374890590065, -0.4773018831639117] km/s
+ V∞_out: [0.00077497695746198, 0.0003757124396482357, -0.0007938992832454086] km/s
+ time of flight: 1.8749577787141186e8 seconds
+ arrival date: 2029-04-06T08:25:05.957
+ thrust profile: [0.5309507602607335 -0.09822851115650243 -0.12035791172735619; 0.23506078818589066 0.09926016916224488 -0.16961443085718764; 0.08808917339086014 0.06815248106174172 -0.11331937493004494; 0.08348342490937735 0.09007891928287426 -0.15102771481815191; 0.06900132816114278 0.09181572777295652 -0.15747037296684835; 0.03184174652509196 0.05064460439567878 -0.09614094601653937; 0.015589652273891114 0.028016530077598495 -0.05668587401525576; 0.011789720841978515 0.02470729632618587 -0.05139405809033237; 0.00020286829417108038 0.0009528859962084732 -0.001599260658265163; -0.0001224322252933905 0.0003071271400773546 -0.0011695227339067289; 0.0002123808305584067 0.0009168623216737155 -0.0021268932641567836; -4.228350928068284e-5 -7.730140066638921e-5 -6.109857941704382e-5; 0.000560922416963082 -0.0020797804405019785 9.245890062635263e-5; -0.002357081007814193 -0.0010384025171077714 0.0006021748133017751; 0.0022195317586431056 -7.221305483454902e-6 0.0013579999547686723; -0.0004300236078651845 -0.0003710454956628831 0.0023299462833899806; 0.00036288273651704177 6.919707135574471e-5 -0.0005308947287709996; 0.000649467093684381 -0.0020037765748059403 -0.003508626544055922; 0.00041498003999403983 0.0015090464725014184 -0.002799752760979615; -0.0009793453738942254 -0.0014328315859819688 0.0017992111185945038] %
+
+Mass Used: 124.71175453632395 kg
+Launch C3: 91.757716437991 km²/s²
+||V∞_in||: 0.7526872319031251 km/s
diff --git a/archive/ES_0.5656912912159532 b/archive/ES_0.5656912912159532
new file mode 100644
index 0000000..0446604
--- /dev/null
+++ b/archive/ES_0.5656912912159532
@@ -0,0 +1,22 @@
+archive/ES_0.5656912912159532---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T11:55:25.528
+Launch V∞: [6.395391428862471, -7.423415124376746, 0.15443025976377303] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008538157491548342, 0.0009066644246419571, 0.0008531780671612453] km/s
+ V∞_out: [-0.0009806906006912396, -0.0005241495069747947, 0.0010205627362074145] km/s
+ time of flight: 1.8352227802494064e8 seconds
+ arrival date: 2029-02-20T14:20:03.528
+ thrust profile: [0.3304371388952853 -0.0997078571489215 -0.10016932708755744; 0.08102756175605207 0.02240177096557388 -0.07926646350345967; 0.07314289516509107 0.0377523563006734 -0.11225839315388239; 0.0716245753007913 0.04707333577190828 -0.1448821187638162; 0.03010459469997689 0.02969900195194475 -0.09501466205102417; 0.041132714640211 0.03784616083072763 -0.1322750790090375; 0.007679764303619976 0.008676318624302277 -0.03366666617601919; 0.020946362328651935 0.02622396938606482 -0.10114813538223541; 0.01997651447527513 0.022087314645269137 -0.0967217951859869; 0.0034391778190556123 0.0073392654993087855 -0.026372635996981638; -0.0005323744184200864 0.000639060414249299 -0.0023354089764461216; 0.001644830878369322 0.0036216344943311397 -0.009707735700831631; 0.00041833200028276214 -0.0004237683091847383 -0.0036378014438177677; -0.000546237476206454 0.004094985069906811 -0.004306293077746451; 0.0032398554007717025 -0.0014466659622838242 -0.001375668622097379; 0.006841393810989226 -0.0024650161521185985 -0.003636101689306083; 0.00040256018754946743 9.605317584018185e-5 0.0027140354899089884; 0.004875248641848415 -0.009663677504606769 0.005336726795248685; 0.003677898891254321 -0.006249009168552629 0.001055047104423487; -0.0025000137287055912 -0.003075201562752745 0.006669397442290796] %
+
+Mass Used: 99.78666775505735 kg
+Launch C3: 96.03197234232367 km²/s²
+||V∞_in||: 0.001509620656556196 km/s
diff --git a/archive/ES_0.565694562888508 b/archive/ES_0.565694562888508
new file mode 100644
index 0000000..56f9b5f
--- /dev/null
+++ b/archive/ES_0.565694562888508
@@ -0,0 +1,22 @@
+archive/ES_0.565694562888508---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T08:53:49.204
+Launch V∞: [6.477179558179326, -7.281419664871369, 0.005393657824805439] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003112845733019383, -0.000890535281022391, -0.002065619139633407] km/s
+ V∞_out: [-0.0020622033387313297, -0.00025346400062740276, 0.0009102630492230147] km/s
+ time of flight: 1.8749577781744254e8 seconds
+ arrival date: 2029-04-06T11:03:26.204
+ thrust profile: [0.39719211878605926 -0.07933642953388413 -0.10616363748842532; 0.10047653327491934 0.038966771351379284 -0.08886884514700173; 0.06971063300690736 0.04992743270977706 -0.1039418015758313; 0.10834445082588647 0.10258167592191263 -0.20664811260214788; 0.04444685719743235 0.05487301232124932 -0.12540436843721173; 0.01149078822017016 0.016459979678854077 -0.043015068139328025; 0.017553367375043066 0.027374392654008338 -0.07204195473990178; 0.007850193979900607 0.014907702577376647 -0.04122231565296825; 0.004797508473970224 0.010495500259915467 -0.029499248691942908; 0.00822779511015776 0.020047870057890337 -0.058143132667716674; 0.004231057355514327 0.010704572635643526 -0.030054773922197194; 0.0006275529940249832 0.0018111417125243963 -0.004072016401772847; -0.0007435438025703974 0.0006324557783033534 -0.004332599777241208; -0.0002857416483889741 -0.0004890957160657761 0.00012952339735055685; 0.0011551052870503937 -0.0006636738913878385 -0.0038488998029939546; 0.004944558045460351 9.776743585093785e-5 -0.0006363743284192838; 0.0011623103608571802 2.0531538488635257e-5 0.0025309915956034323; 0.0004430462739216654 0.0010470461755574254 -0.003177810860772259; -0.0005196417294200434 0.001312521386814668 -4.0792971879606305e-5; -0.00275563907925876 -0.003086289650236801 -0.0011787922099649234] %
+
+Mass Used: 105.96807737416384 kg
+Launch C3: 94.97295645641636 km²/s²
+||V∞_in||: 0.0022708442488073143 km/s
diff --git a/archive/ES_0.5657003106791471 b/archive/ES_0.5657003106791471
new file mode 100644
index 0000000..96cbb50
--- /dev/null
+++ b/archive/ES_0.5657003106791471
@@ -0,0 +1,22 @@
+archive/ES_0.5657003106791471---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T22:48:22.450
+Launch V∞: [6.686885245024341, -7.314707069262385, -0.6198273101538085] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6684763230192175e-5, 4.071640645956002e-6, -7.283610978432158e-8] km/s
+ V∞_out: [-5.690681479807488e-6, 1.2101349569287882e-7, 2.6390226057583032e-5] km/s
+ time of flight: 1.8749577782736784e8 seconds
+ arrival date: 2029-04-10T00:57:59.450
+ thrust profile: [0.2306650227783556 -0.06547097180090665 -0.0873873389351843; 0.03407510117908508 0.006354986989888169 -0.04144347633969647; 0.03844257532764572 0.01474978263515701 -0.08468944617220246; 0.032948829611634575 0.016834305230086055 -0.10356901775644155; 0.03547067796380299 0.020183107784594288 -0.13482956864162127; 0.03280585612943182 0.02396932069794574 -0.16483460360542768; 0.012955638487513575 0.009344632011486062 -0.06952273453561685; 0.013253629927246427 0.01009582386346762 -0.08461423202440346; 0.01117201125874514 0.008927876262406697 -0.0797370228780993; 0.0009612672142967651 0.0009762939439640051 -0.006981981700441608; 0.0006917175678956178 0.0001594488604973552 -0.004121683950281024; 0.0005117187803766782 0.0028824538428516527 -0.02083849832310131; 0.004116972381419637 -0.004684743240871598 -0.006516328509846322; 0.0004440589766894818 -0.0005758343652786666 -0.003663509818079072; 0.0032182996015341367 0.0015203828775518765 -0.00575426110889061; 0.002553802913635753 -0.00022132128251789278 -0.00760452787131106; 0.0006003849325958818 0.00013445139530093332 -0.0034540062409107943; 0.0014334967034369804 0.0005361404875223149 0.0018376848431751296; 0.0001540730967709114 0.0001634575596943501 0.006320481886709745; -0.00044955693231493645 -0.0004947374909050391 -0.0008311224620084455] %
+
+Mass Used: 84.79626430435746 kg
+Launch C3: 98.60355968365384 km²/s²
+||V∞_in||: 2.6993705771903675e-5 km/s
diff --git a/archive/ES_0.5657043321299875 b/archive/ES_0.5657043321299875
new file mode 100644
index 0000000..7f941e9
--- /dev/null
+++ b/archive/ES_0.5657043321299875
@@ -0,0 +1,22 @@
+archive/ES_0.5657043321299875---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:32:24.649
+Launch V∞: [6.494402173748479, -7.532960647144659, 0.0035521093011455056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.290418407002891e-8, -6.313778664788113e-8, -3.418299325915552e-8] km/s
+ V∞_out: [2.2483923222652864e-8, -4.389123436404794e-8, 6.821164265222401e-8] km/s
+ time of flight: 1.8151198621025005e8 seconds
+ arrival date: 2029-01-29T15:32:10.649
+ thrust profile: [0.1439777042048434 -0.04355319195120849 -0.05880678044702651; 0.05675834162880215 0.011096053881563567 -0.06808894480110995; 0.05130046101328 0.021500488363445102 -0.10241749735509455; 0.041687218400105794 0.02382743816219907 -0.1157389210970438; 0.04128779363602867 0.02924088352723329 -0.14714822943797826; 0.023630205452359273 0.018187592847283704 -0.10120205865768486; 0.016597344100155786 0.01430750134747677 -0.08465641475208857; 0.012242927549514896 0.011036156748954227 -0.0702919971649493; 0.01069924018231216 0.00974365084794724 -0.06805746475003265; 0.007683287012737339 0.0076571207484616675 -0.051393879347584; 0.0026583453996362892 0.001984146897147211 -0.01167294004760816; 0.009830258563518676 0.009585204937960046 -0.0703532229363168; 0.0002500576159130624 -0.0006942088763347921 -3.96388892375454e-6; 0.0006205005613453968 -0.0003805964806352954 -0.0024981988521535258; 0.0021663819904986907 -0.0012125666889854286 -0.0030171935316114147; -0.0028302895762977913 0.0006958982881415912 -0.0031253508081358723; 0.002963426061495358 0.0015018358442821702 0.0008972656120599381; -0.00231595352134835 0.00039405282463596074 0.008004464467310866; 0.000150937073788563 -0.0002204165779895422 0.0011371579427417104; 0.0035982994092793657 -0.0005538049454142839 -0.0005736065788830198] %
+
+Mass Used: 82.9389055990714 kg
+Launch C3: 98.92276832329954 km²/s²
+||V∞_in||: 9.545571488635402e-8 km/s
diff --git a/archive/ES_0.5657148034217127 b/archive/ES_0.5657148034217127
new file mode 100644
index 0000000..d24b8d9
--- /dev/null
+++ b/archive/ES_0.5657148034217127
@@ -0,0 +1,22 @@
+archive/ES_0.5657148034217127---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T17:18:03.930
+Launch V∞: [6.577033409815005, -7.445048158749895, 0.11276930958377548] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009413860408319217, -0.0060708723577045836, 0.008271978706425888] km/s
+ V∞_out: [-0.006946363712155656, -0.00612431161222684, -0.004516796590135894] km/s
+ time of flight: 1.8597344745683217e8 seconds
+ arrival date: 2029-03-23T04:35:30.930
+ thrust profile: [0.14022867240224576 -0.03729251582848321 -0.052312132266922454; 0.06469019373247521 0.016006455787636764 -0.07206947158082848; 0.0878087540291306 0.04277320582949801 -0.16189525639668936; 0.04271916315144179 0.027817515410614616 -0.11150074379737429; 0.031164777664186117 0.024366831367192966 -0.1043124974379355; 0.022896953594332053 0.02051711865470456 -0.09331036832343355; 0.021898607171404363 0.02182160261430303 -0.10426596925354693; 0.009951471077200612 0.011009085609472015 -0.0554295207156388; 0.01839080998122255 0.02148027838154236 -0.11296264422979004; -9.130544429898526e-5 -0.0007712063937229739 -0.009845660449833782; 0.002452252458881245 0.0042731925152485395 -0.0034858755751323665; 0.0002760146239078119 0.0007897579619689644 -0.0009114615262305055; -0.0013544489076918026 -3.684983366827551e-5 -0.0006007577824236041; 0.004364085319916643 3.389125137549158e-5 0.0007023405021598073; 0.0009175174365676109 0.0005551073410522988 0.006147835738298187; 0.0037873362900880106 0.0016911610660792155 -0.006725572580782333; -0.0011614122896675628 -0.014308099995268855 -0.00031720215414384346; -0.012070436693890971 -0.008127644446388593 -0.009134191267334193; 0.002019453960299555 -0.00042572648456420275 -0.000136905732924869; -0.007881238417680667 -0.0040407892863001255 0.0056933748755131144] %
+
+Mass Used: 84.25744370884468 kg
+Launch C3: 98.698827477112 km²/s²
+||V∞_in||: 0.010303753227876631 km/s
diff --git a/archive/ES_0.5657196981510605 b/archive/ES_0.5657196981510605
new file mode 100644
index 0000000..0472f82
--- /dev/null
+++ b/archive/ES_0.5657196981510605
@@ -0,0 +1,22 @@
+archive/ES_0.5657196981510605---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T20:21:54.134
+Launch V∞: [7.583040684216794, -6.093649800052297, 0.11780110441419142] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0028365806054794006, 0.017878033568032484, 0.019610761317881278] km/s
+ V∞_out: [-0.004586463350364125, 0.004152417018132447, -0.025944014408484758] km/s
+ time of flight: 1.8216348840178546e8 seconds
+ arrival date: 2030-02-21T05:20:02.134
+ thrust profile: [0.4697670491142758 -0.011831462571341081 -0.144867055926169; 0.14608391802781395 0.07548564815886998 -0.15353434056620507; 0.03674102942746151 0.029546582899857038 -0.06813554214143291; 0.03445443344441164 0.03612399421320884 -0.09441201892219808; 0.0477473468472438 0.062262198021157296 -0.17606727697261187; 0.018853546256245853 0.027352390315439446 -0.08593147181120964; 0.008195534375244014 0.014154327002161023 -0.047202130148242; 0.006473422901854134 0.012156760425517842 -0.04085839164010206; 0.005993009666493102 0.0029047301189990622 -0.005663206567808049; -0.006762710570657344 0.005335851303745165 -0.021927094694994022; 0.0006733941032724487 0.005039470037152868 -0.019178061455534627; 0.003915306993064065 -0.004401961927850204 -0.01419732211758682; 0.004948820774548251 -0.0009465779971676667 -0.0025109688382503013; -0.008870735878509723 0.015740208165490405 -0.01920921390049382; -0.0074801152431484665 0.00787591484505782 -0.007001779279109785; 0.0233864254565965 -0.003294597344980464 -0.019672707142827338; 0.008640049397442425 0.007744487068739431 -0.012066187036724463; -0.0011281350960663204 -0.0009891935855096106 0.0029029037235995567; -0.001387522379764894 0.0057189605647384525 0.001799291740433106; 0.007807764402819351 0.032719144353159584 0.0021750322912958897] %
+
+Mass Used: 107.88743365077062 kg
+Launch C3: 94.6489510043657 km²/s²
+||V∞_in||: 0.026688054130228133 km/s
diff --git a/archive/ES_0.5657266555368381 b/archive/ES_0.5657266555368381
new file mode 100644
index 0000000..a5873d8
--- /dev/null
+++ b/archive/ES_0.5657266555368381
@@ -0,0 +1,22 @@
+archive/ES_0.5657266555368381---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T17:15:26.566
+Launch V∞: [6.390256732490131, -7.60075621558592, 0.0930468496034348] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009618571742181429, -0.007012886608941504, 0.009510639615257173] km/s
+ V∞_out: [-0.008094035906940853, -0.006810451877103108, -0.005352383530742729] km/s
+ time of flight: 1.814654047186895e8 seconds
+ arrival date: 2029-01-30T00:18:50.566
+ thrust profile: [0.16941567221645448 -0.053891902135307125 -0.06724045045244408; 0.07527658947514758 0.013416721596064383 -0.08957077844165505; 0.04779087976224052 0.018559549684447108 -0.0955442218467054; 0.03819128540359874 0.01985451139596026 -0.10573044053181087; 0.029326596880492592 0.018309709313500455 -0.10372703558958606; 0.02579626924369504 0.01804212829509678 -0.1090849084134074; 0.01993158161631152 0.015153495504552611 -0.0980243989767952; 0.009360368789638215 0.007371444674724689 -0.051991302589770895; 0.021155241182112268 0.017997413462848548 -0.12767352141643443; 0.00023851998339762854 0.00010572710310580456 -0.0026694029898328346; 0.014593664978626627 0.012469884649732204 -0.09763095239419785; 0.0015960159430156075 0.0008797012530082539 -0.004639715461686808; 0.00026656968975342444 0.0006370494845222611 -0.00563037083199505; -0.00018665821948228578 0.0004530677213523274 -0.0032683746808168292; -0.00021692403620151435 0.0002896039996160589 -0.0010475512210532758; -0.00117313011075101 0.0026595215254934528 0.0011536598586807945; -0.0016080086551883825 -0.00020563946433835105 0.0031822293198444174; -0.00045318475486891795 -0.0010106156834970119 0.0009162043585076115; 0.0002644791887368415 0.004285361580044819 -0.005441995939311606; 0.0006265979572653265 -0.0014113790595736923 -0.0015538274013779559] %
+
+Mass Used: 84.75715053891781 kg
+Launch C3: 98.61553387212457 km²/s²
+||V∞_in||: 0.011855716499004397 km/s
diff --git a/archive/ES_0.5657282157016452 b/archive/ES_0.5657282157016452
new file mode 100644
index 0000000..2216c5e
--- /dev/null
+++ b/archive/ES_0.5657282157016452
@@ -0,0 +1,22 @@
+archive/ES_0.5657282157016452---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T20:06:34.587
+Launch V∞: [7.813310641764986, -5.778966234090957, 0.19150966451647033] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2004373116533605e-7, 7.050035198691296e-7, 2.1036608256471395e-6] km/s
+ V∞_out: [2.04942609912485e-6, 2.1152408403790554e-7, -8.63903789340961e-7] km/s
+ time of flight: 1.8179252539447024e8 seconds
+ arrival date: 2030-02-13T22:01:59.587
+ thrust profile: [0.4860264008902649 -0.025722354272621283 -0.15483666455767522; 0.10577759721904101 0.05177186845278621 -0.11696884929746601; 0.056337527742315846 0.04387407242236238 -0.11175564787297103; 0.03146796377490654 0.031551187687424306 -0.09106666124297552; 0.027613782018308223 0.033279345320030865 -0.10539425172191391; 0.029091116179816332 0.04022352146303781 -0.13700550746395945; 0.013362337841823526 0.018243790743854574 -0.071806057099116; 0.008580741449088568 0.013069562046791472 -0.05408332224583864; 0.0009885539440801893 0.004937579843655912 -0.014381921799421531; 0.002711407529028631 0.015685023232097247 -0.013766857851577169; 0.005544191031381591 0.004944178889751632 -0.011966055020394351; -0.0027670367797268704 0.003089214169373379 -0.018655851166807513; -0.004381052187267983 -0.003130901065807753 -0.011222013188566136; 0.0007334754210642267 0.0019077281719470983 -0.0032243010969008855; 0.018601433781298894 0.004723773050976695 -0.0013701545773200285; 0.005875215801337735 -3.95176136337203e-5 0.010072839350503229; -0.00521945674000346 0.0026854436289147215 0.003074357334251328; -0.0037401153021653015 0.019995275529443322 0.013405808228469677; 0.00028356115917722554 -9.273010871504528e-5 0.0021129918792118967; -0.012985062663012751 0.04551145269818795 0.02238902393863819] %
+
+Mass Used: 108.87737740392595 kg
+Launch C3: 94.4809498710846 km²/s²
+||V∞_in||: 2.2295376372726765e-6 km/s
diff --git a/archive/ES_0.5657309096548279 b/archive/ES_0.5657309096548279
new file mode 100644
index 0000000..e789bd4
--- /dev/null
+++ b/archive/ES_0.5657309096548279
@@ -0,0 +1,22 @@
+archive/ES_0.5657309096548279---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T07:18:05.561
+Launch V∞: [7.7429329074170035, -5.910922809678835, 0.1818590960034814] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.481062771016907e-9, -2.1453758278312244e-9, -1.5172700350217335e-9] km/s
+ V∞_out: [-7.721272970532905e-10, 8.707483023024959e-10, -2.8976811427256233e-10] km/s
+ time of flight: 1.7654987098150358e8 seconds
+ arrival date: 2029-12-13T16:55:55.561
+ thrust profile: [0.47302864337633166 -0.03193935274604721 -0.14385032536782597; 0.06539093089499047 0.032519659461126664 -0.06931164782033676; 0.052537754048508994 0.04265985244358544 -0.09584580537921124; 0.05544426908204043 0.060247794056628785 -0.14642471199082946; 0.033698858666785035 0.04438580506306787 -0.11971947515248478; 0.017975063797265968 0.02702843621341535 -0.07860822220474654; 0.013234129152002566 0.02297579842100675 -0.07085811820699989; 0.012911201979216684 0.024476846839954942 -0.0798964074993693; 0.004242854858351229 0.008788353252883959 -0.030193726162253357; 0.010493077800139904 0.024472598284000932 -0.08387499666115211; 0.005844879469453123 0.001863281230080228 -0.011578870403631869; 0.0006671133742618485 0.0007323097786466051 -0.013106452048688563; 0.002170957584361934 0.0018542831636454084 -0.004529994801432407; 0.00018784556570102307 0.0035121966126502634 -0.0019556078173826735; -0.00039702906711074017 -0.0005069301171799301 0.0027503833387841964; 0.00565302355245918 0.007284067277609495 -0.00038323698127865546; -0.0185002421112337 0.002472788155325572 0.006912848914683752; 0.018690413486393727 -0.00017892354748738626 -0.03308892008371983; -0.006438339624727462 0.007955356222050155 -0.018406404949833467; 0.00017402061890359796 -0.00700240301945136 -0.00042567889254283226] %
+
+Mass Used: 106.28969592163821 kg
+Launch C3: 94.92509120154187 km²/s²
+||V∞_in||: 3.6139200704419928e-9 km/s
diff --git a/archive/ES_0.5657319825337964 b/archive/ES_0.5657319825337964
new file mode 100644
index 0000000..f706aa3
--- /dev/null
+++ b/archive/ES_0.5657319825337964
@@ -0,0 +1,22 @@
+archive/ES_0.5657319825337964---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T05:37:58.158
+Launch V∞: [6.179314866578535, -7.681344492612755, 0.13873091521925696] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.6117651663798424e-8, 8.617548747922887e-8, 6.207011773510498e-8] km/s
+ V∞_out: [-2.9645448897497882e-8, 6.696902527191751e-8, -9.44460157612102e-8] km/s
+ time of flight: 1.7258035995639443e8 seconds
+ arrival date: 2028-10-14T16:37:17.158
+ thrust profile: [0.216358872269259 -0.07477105377994159 -0.08003835849326012; 0.10984467657121122 0.020251522160300354 -0.11377180764054018; 0.09503385292551483 0.040765113773010175 -0.15913879220794708; 0.058502337728448185 0.034745141720717354 -0.13624899119707487; 0.05259111353448415 0.03826016406636412 -0.1537287416775447; 0.025771686732004764 0.021321309415234836 -0.09232187252417846; 0.03511245486806086 0.03277289581066269 -0.14309895676934978; 0.010049594398266705 0.010122661864739776 -0.046602629190022775; 0.018808745496606317 0.02039026686336338 -0.0988278927895389; 0.004690244482087564 0.005328581211081995 -0.026620854752277677; 0.000554745354737169 0.0002032046705976484 -0.0037719047144268983; 0.0008093041244030385 0.0005094767353441628 -0.0008723756442907446; -6.750131104601932e-5 -0.00016367153915642355 0.0007980982865211575; -0.0006840589526757271 0.0009096317699117682 -0.0025803466650116272; 7.179898506182191e-5 0.0003404104101071184 -0.0004340073528628053; 0.0003880194273466987 0.00015135275173609936 0.0013798491777975554; 0.00014092389040336494 -0.0008768003405903766 5.582886300435912e-5; -0.0010155422545809094 -0.00012388958522650264 -0.0001215957409791854; -0.00029132837256923955 0.0003264111870127833 -6.569125866733293e-6; -0.0006710141128400699 -0.0006162856255986821 -0.0003421643664210023] %
+
+Mass Used: 92.98429469823031 kg
+Launch C3: 97.20623170134837 km²/s²
+||V∞_in||: 1.2011704702577376e-7 km/s
diff --git a/archive/ES_0.5657333162039024 b/archive/ES_0.5657333162039024
new file mode 100644
index 0000000..a3a880d
--- /dev/null
+++ b/archive/ES_0.5657333162039024
@@ -0,0 +1,22 @@
+archive/ES_0.5657333162039024---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:22:13.698
+Launch V∞: [7.52871928012377, -5.697157708497235, 0.09858672938359561] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.426807530089206e-7, 2.196355944016472e-6, 6.099805725277961e-6] km/s
+ V∞_out: [5.807709609354657e-6, 7.008935798956e-7, -2.8584202713592847e-6] km/s
+ time of flight: 1.843561822137789e8 seconds
+ arrival date: 2030-03-12T13:25:15.698
+ thrust profile: [0.8209819337465554 8.037094590254744e-5 -0.1756213578933609; 0.22113119836602713 0.14141771149794538 -0.16910295639471343; 0.10278344746020962 0.11113983988641013 -0.1450978874651649; 0.04450802693718343 0.0676243508291459 -0.1044317128816157; 0.01230058876885995 0.023139755375021845 -0.043668800762915835; 0.02786296290048754 0.05346825244312165 -0.10477056670829951; 0.006841841390267736 0.018542823832401845 -0.03992802188790405; 0.004243754525678913 0.0132476853236679 -0.026656403519050582; 0.003642116388326374 0.008754794750982219 -0.01720782797523708; 0.0036758215577364257 0.02193418144748539 -0.049235484531272605; 0.00232478888817115 0.009290806228705324 -0.007168270653867711; 0.0022595848366962342 -0.000889971371524753 -0.01185303948411221; 0.002728028961528111 0.00538015961262638 -0.00941039367323148; 0.00014121760348033034 -0.0024168362566855174 -0.004683263894671363; -0.005465912864083825 0.002910968881641281 -0.005342221039428832; 0.0012173220838073034 0.002119038657397396 -0.0177221590110069; 0.0028972875868334695 -0.0020996658627283685 0.0023851785448662; 0.002553758329705272 -0.0009202543660710532 0.004465063556601876; -0.006562307220433616 0.007148850905626388 -0.00540769059967737; 0.0009490452692486596 0.00451975948322109 0.0038390673538695186] %
+
+Mass Used: 139.98672300184307 kg
+Launch C3: 89.1489392976074 km²/s²
+||V∞_in||: 6.514955707388838e-6 km/s
diff --git a/archive/ES_0.5657400431016592 b/archive/ES_0.5657400431016592
new file mode 100644
index 0000000..9f9e2ed
--- /dev/null
+++ b/archive/ES_0.5657400431016592
@@ -0,0 +1,22 @@
+archive/ES_0.5657400431016592---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T22:30:53.116
+Launch V∞: [6.454343517563503, -7.421068832829034, 0.21944661811764807] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.8461972000140016e-9, 1.979572191065648e-9, -9.48709179141109e-9] km/s
+ V∞_out: [-2.1665505569032895e-9, 5.01704518017269e-9, 6.70083903952334e-9] km/s
+ time of flight: 1.874957778747116e8 seconds
+ arrival date: 2029-04-11T00:40:30.116
+ thrust profile: [0.3558954749833722 -0.10333923095698298 -0.13393206061180327; 0.03521795964427868 0.0076974237284648805 -0.0421912583943219; 0.05549373402071439 0.023320752021006124 -0.1123084087732677; 0.0319762750800697 0.019140412933462407 -0.0948683830115425; 0.02746377799520858 0.01903602516000285 -0.1001759923345272; 0.03128420804990568 0.022162629038264336 -0.13351958485830362; 0.02124852373100614 0.01810915746556105 -0.11337286013453737; 0.0043736017498332115 0.004408126738855878 -0.027525565710415867; 0.00454265494540729 0.003355588471205693 -0.025583118987258617; 0.007629923645013429 0.006871864011115182 -0.053482889719020224; 0.007792514825245712 0.012702174816408946 -0.08153210864361707; -0.0014104159643365428 -0.00016928288938733793 -0.0006942637657988693; -0.0016568383715230427 -0.0013987447481142465 0.0033053268872203674; 0.00045199917215952114 0.00040898554512244203 0.0006072390803941946; -0.0003411279100064225 -0.0002288034290481145 0.004290825137348875; -0.002447858018151631 0.0015134683827362607 -0.003972946709515287; -0.0017936958125481406 -0.006808205031647283 -0.0008650559252178384; 0.004394696447267895 -0.005694868654663293 -0.004120210124530189; -0.0005837660658364724 -0.001379813029234764 0.00036157991795623696; 0.012681166542735722 -0.005113011404101912 -0.004805811711301463] %
+
+Mass Used: 95.48606047066369 kg
+Launch C3: 96.77896968250377 km²/s²
+||V∞_in||: 1.1318199433644544e-8 km/s
diff --git a/archive/ES_0.5657488361901479 b/archive/ES_0.5657488361901479
new file mode 100644
index 0000000..4b5c86c
--- /dev/null
+++ b/archive/ES_0.5657488361901479
@@ -0,0 +1,22 @@
+archive/ES_0.5657488361901479---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:04:15.879
+Launch V∞: [6.4557828796979955, -7.382625383437429, 0.03756929974582307] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004455434854981125, 0.0021030180992791235, -0.004915945290274902] km/s
+ V∞_out: [0.004491087204059419, 0.0018239556100851822, 0.004996814912825689] km/s
+ time of flight: 1.8749577787247005e8 seconds
+ arrival date: 2029-04-09T06:13:52.879
+ thrust profile: [0.34001934710204695 -0.07714740613768356 -0.11335392721928025; 0.08183042635937135 0.024678707005857975 -0.08366177035246808; 0.05788178235554814 0.032895834427306925 -0.09923950825671173; 0.04758337620436531 0.03571690639447736 -0.11368535363597103; 0.030434183168512336 0.027261333553108006 -0.0942648589592628; 0.028547043239482976 0.029355536451690433 -0.10572498847221731; 0.03520156703848997 0.04478840805840213 -0.16176138134818732; 0.007235611698855359 0.009006296430879185 -0.03764247040245316; 0.009772211410548393 0.013950750047684644 -0.05934969949685324; 0.0018483927086772568 0.0033506316719278733 -0.017922625298817194; 0.001188481812895313 0.0011467679881954308 -0.004236453160902203; 0.00029624680988244703 0.0001181147369839011 -0.0028544527033469713; -0.007822552570691534 0.005696244944898853 -0.006236340853645795; 0.0009593240009377176 -0.0012593020998148908 -0.001028565673651365; -0.00017822043414475615 0.002001941103335663 -0.005620650486978334; -0.00381147804333327 0.007126768148888766 -0.00362084021563785; -0.0003234716197228546 0.0013560167510898924 0.003758505505564807; 0.01676626027670365 0.007115461794499892 -0.0011493526378132989; 0.0001742378841640891 0.0024582350801985475 -0.003908731473968057; -0.014121079607902461 0.012555167575596916 -0.01153081883623832] %
+
+Mass Used: 98.98038292199044 kg
+Launch C3: 96.18170159425979 km²/s²
+||V∞_in||: 0.006959892453899863 km/s
diff --git a/archive/ES_0.5657591726874239 b/archive/ES_0.5657591726874239
new file mode 100644
index 0000000..76871fc
--- /dev/null
+++ b/archive/ES_0.5657591726874239
@@ -0,0 +1,22 @@
+archive/ES_0.5657591726874239---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T09:13:54.997
+Launch V∞: [6.302201292759959, -7.70139819108994, 0.3064553895008882] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.017332843819947184, -0.007155055100200915, 0.018690407608097065] km/s
+ V∞_out: [-0.016759292173538175, -0.006676242641393704, -0.019376975123308875] km/s
+ time of flight: 1.824529965390573e8 seconds
+ arrival date: 2029-02-13T02:37:10.997
+ thrust profile: [0.22256450033272593 -0.07967313647567968 -0.09811366168578023; 0.023522653144497706 0.0016814800226277423 -0.03251416296966754; 0.0342235778211872 0.006233451065174104 -0.0798570202906673; 0.039323465999224184 0.009392553022744627 -0.12646980159338786; 0.04003023780607063 0.010381998806152967 -0.15886412803333422; 0.041813349621203345 0.010769219640947672 -0.19635458379639842; 0.02315497642053556 0.00573663232912809 -0.12264574197732393; 0.007116577076780474 0.001649750450100653 -0.04378988595746871; 0.002596475784843862 0.0005440102662051027 -0.01806756916634421; 0.003588147072310581 0.0007382184402246487 -0.025893983348839626; 0.002189415219801784 0.00037954663813766513 -0.01765701658211894; 0.000256879616748989 0.00047864542329736014 -0.004755053436568513; 0.0004078799911084337 -0.00017213437091591468 -0.0026086290041599713; -4.2101976323650895e-5 -0.0006062040564083562 -0.0010523076800088376; 0.00015847862817106983 0.0002398840407134581 -0.0005116145190652178; -0.0007503967869934586 -9.696352406895228e-5 0.00038389978786007085; -0.0001562711922910071 -0.0001301066012068751 0.00010251078973329584; -0.0013913098184539282 5.99922628829371e-5 -6.292075874830957e-5; 8.06134498384865e-5 -4.982175075468663e-5 -0.0014035883113688952; -0.00012065364174817723 -0.0004961848043227872 -0.00016707940086918734] %
+
+Mass Used: 81.833758997328 kg
+Launch C3: 99.12319013794284 km²/s²
+||V∞_in||: 0.026475528794160187 km/s
diff --git a/archive/ES_0.5657694118464424 b/archive/ES_0.5657694118464424
new file mode 100644
index 0000000..6adef27
--- /dev/null
+++ b/archive/ES_0.5657694118464424
@@ -0,0 +1,22 @@
+archive/ES_0.5657694118464424---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T18:54:52.755
+Launch V∞: [6.567189899513897, -7.385844799716881, 0.15792997432438313] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008547803983641, -0.00033615662609823375, 0.00593267538066322] km/s
+ V∞_out: [-0.010106944267801402, 0.0001085706683735397, 0.0024824158593338493] km/s
+ time of flight: 1.8525066165050757e8 seconds
+ arrival date: 2029-03-13T21:25:53.755
+ thrust profile: [0.2598322845602576 -0.06900524653064355 -0.09200057487861445; 0.0445171442336143 0.010794065604497353 -0.04983538938150971; 0.045316232977406244 0.02236603311708671 -0.08693637706953847; 0.04250514734553872 0.027922566423555662 -0.11265316862007667; 0.033865121641759345 0.02678306866106224 -0.11506230934600914; 0.016242312586081453 0.014200825816928284 -0.06676607363267513; 0.02278455383895744 0.02608543516465537 -0.11458598068479584; 0.010517131929295221 0.011319603464705242 -0.05855933571580697; 0.026944777376182023 0.0327538994973984 -0.15998260833594646; 0.0026825730994483993 0.003228121087657517 -0.01906528672910825; 0.004943733176749158 0.006157330581598058 -0.03782729708888366; 5.6919379069167875e-6 0.003057147708587341 -0.007917068009293916; -0.0019624614699567384 -0.0013654984542281958 0.0004735738862172282; -0.0013220435286056323 -0.0002565152101535096 0.0032145685309496793; -0.0008415480410528954 0.0012693425443619042 -0.000803800522637737; -0.0015423892372146946 -0.0030857044051617595 -0.0044156503036068585; -0.00419037498298296 -0.000894982885886146 0.00926585982226337; 0.00011044662254983045 0.0016107327400981704 0.004322823924644171; 0.001051022283841284 -0.004361522352356916 0.0052751022330956715; 0.0016764429828177597 0.003423222759033055 -0.003716815990860564] %
+
+Mass Used: 90.12648114584408 kg
+Launch C3: 97.70362845857234 km²/s²
+||V∞_in||: 0.010410311781706932 km/s
diff --git a/archive/ES_0.5657847139559575 b/archive/ES_0.5657847139559575
new file mode 100644
index 0000000..fb4b17d
--- /dev/null
+++ b/archive/ES_0.5657847139559575
@@ -0,0 +1,22 @@
+archive/ES_0.5657847139559575---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T08:23:05.530
+Launch V∞: [6.591402312793161, -7.4852707131810226, 0.11003550836111617] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.835803525534266e-8, -2.7804720297913098e-8, -1.970675732546174e-8] km/s
+ V∞_out: [8.254123113980456e-9, -1.93508435514516e-8, 2.9282666484396693e-8] km/s
+ time of flight: 1.8510517367160776e8 seconds
+ arrival date: 2029-03-13T18:29:18.530
+ thrust profile: [0.11087675915360654 -0.03286937072070066 -0.04450544515048128; 0.059481414347928224 0.011231232833031408 -0.07094619796837827; 0.043957666884483056 0.01724533643205434 -0.08825656978229664; 0.036470444865770404 0.018981436745917193 -0.1020409556793617; 0.029349480175182508 0.017972105333149434 -0.10438595649965485; 0.02906107657552595 0.02008852699144038 -0.12439345272973237; 0.022862467469154747 0.01707757466066496 -0.11451493793517135; 0.013645690120509826 0.0104259125066631 -0.07622468327357694; 0.016957876864694226 0.014499982394378663 -0.10838670323568396; 0.005083659479401384 0.004356811567084853 -0.036327588055834824; 0.00010653819719864542 -0.0005645821458273192 -0.0038053728037413794; 0.0012154449187211282 0.0005296316943944633 -0.007809566668060217; -0.001688035796127205 0.0005467753017543913 0.0019335487770849227; -0.001475141718967198 0.0003240065972609452 0.0029509219771933727; 0.00439589774718564 0.001816501449175959 -0.009124681241927059; -0.00939641765017412 0.011099221997126683 -0.009549988326200017; 0.001431235405466756 0.003980580516683564 -0.0037135171043905764; 0.0003252800087503769 -0.0019839696499506514 0.0046163063435590524; 0.0020353824918671773 0.007909602071639495 0.000132935352712421; 0.0029621680371107423 3.2451568610618054e-5 0.006674628393408198] %
+
+Mass Used: 79.73567512977888 kg
+Launch C3: 99.48796991180085 km²/s²
+||V∞_in||: 3.8710156465276975e-8 km/s
diff --git a/archive/ES_0.5657881045423062 b/archive/ES_0.5657881045423062
new file mode 100644
index 0000000..8851316
--- /dev/null
+++ b/archive/ES_0.5657881045423062
@@ -0,0 +1,22 @@
+archive/ES_0.5657881045423062---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T17:12:15.111
+Launch V∞: [6.048258856363886, -7.756542290659954, 0.15012521686378968] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.025669070522916743, -0.011802133286305238, 0.028547616953914803] km/s
+ V∞_out: [-0.027309757536771916, -0.011202456462101528, -0.027232801473037783] km/s
+ time of flight: 1.741481366863581e8 seconds
+ arrival date: 2028-11-04T07:41:11.111
+ thrust profile: [0.2868031962948561 -0.10432240839345934 -0.11217487287296603; 0.1047072456872412 0.015236624864459715 -0.12036864245724832; 0.05339483416925077 0.01895984103255241 -0.10058136955035922; 0.06652288250848734 0.03178531391536626 -0.17029842435632306; 0.05430326624106219 0.03126425151151387 -0.1745796613763504; 0.025079747757995815 0.015282476886909948 -0.09799422052929953; 0.024429347630452427 0.01705547404063272 -0.11080565099187599; 0.015016731806623 0.013307797608910748 -0.08691872509596178; 0.007559208882212915 0.005452232523035572 -0.04551755010243607; 0.0023599508013587072 0.0011229250841690891 -0.011985290939158219; 0.0015298430188493764 -8.062704599568957e-5 -0.0032645220930020017; 0.0017383932723882653 0.0018645940088869882 -0.00894076712696747; -0.0001367523180193884 0.0002739123876739814 -0.004415406224580393; 0.0013620881642410878 -0.001045339908239333 -0.004546124748291904; 0.001283544505590283 0.0007760521935313842 -0.003667913513086194; 0.0004188891064480535 -0.0002041463338012516 0.0003997096827698468; -5.880689832905861e-5 -0.00028912327715629755 0.0009609419803986866; -0.0019128543411607182 0.0037103913260191613 0.0014491546524890778; -0.0007742019199822752 -0.0011869219068879249 -0.001764048544039806; 0.006794413253455122 -0.0022874817114728074 -0.0017732954410963526] %
+
+Mass Used: 95.60658232616333 kg
+Launch C3: 96.76792108111896 km²/s²
+||V∞_in||: 0.040164137801845454 km/s
diff --git a/archive/ES_0.5657898125111257 b/archive/ES_0.5657898125111257
new file mode 100644
index 0000000..184b27b
--- /dev/null
+++ b/archive/ES_0.5657898125111257
@@ -0,0 +1,22 @@
+archive/ES_0.5657898125111257---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T07:08:52.149
+Launch V∞: [7.6863836507146885, -5.687586416646838, 0.403741606065663] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.734460707624214e-10, -1.1193338149928358e-9, 1.3839006570053067e-9] km/s
+ V∞_out: [6.149776300487471e-10, -1.986201186820832e-9, 3.258173318320386e-10] km/s
+ time of flight: 1.8749577787492102e8 seconds
+ arrival date: 2030-04-18T09:18:29.149
+ thrust profile: [0.5837262414327687 0.031153329713502202 -0.09674912397922202; 0.2147582868639132 0.16745279574681937 -0.13834576190799086; 0.08002159526148754 0.10775597549898255 -0.10907579742104247; 0.052045277792489575 0.10198555562783407 -0.11373784101080427; 0.022991797271181665 0.05992723001240052 -0.07227633820358362; 0.01582670416252411 0.054430212163136815 -0.0692561688675051; 0.0075222929395194075 0.03601683430130079 -0.05018080673897339; 0.005566780011933689 0.0731329550053179 -0.0998793408421157; 0.002412632345764946 0.01543579707932091 -0.0263457722803267; -0.0002688236602642716 0.0006147417790994827 -0.0019198025251638568; -0.002540419096619725 0.003506862603465632 -0.003266615322220174; -0.0013368997701449531 -0.0016022606879371737 0.001496026578295867; 0.0016435145579600575 -0.0034758043203747192 0.0016520166971829933; 0.0015373224225002009 0.0012181715229973172 -0.009480368016946999; -0.0027444779031705903 0.0022387682751377667 0.0006782161825318596; 0.0021620334632758455 0.004145523378332031 -0.007687946578286551; 6.543455536726301e-5 0.004709332245310249 -0.0024604251229342917; -0.0005598600267563503 0.00152257942354291 -0.0023073667579423286; 0.00023329757775361571 0.001580416829074538 -0.0036130847254032894; 0.00044499071412077963 -0.0005605440498633813 -0.0009502566941413317] %
+
+Mass Used: 125.80063034558225 kg
+Launch C3: 91.59214015726818 km²/s²
+||V∞_in||: 1.9406978235222413e-9 km/s
diff --git a/archive/ES_0.5657972782299101 b/archive/ES_0.5657972782299101
new file mode 100644
index 0000000..967579b
--- /dev/null
+++ b/archive/ES_0.5657972782299101
@@ -0,0 +1,22 @@
+archive/ES_0.5657972782299101---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T01:16:56.401
+Launch V∞: [7.3075110377914, -6.43829454475096, 0.254387362353164] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6868910767354994e-5, -4.705241428426204e-5, -3.6433030330673347e-6] km/s
+ V∞_out: [3.162935202177813e-6, -1.617304549379666e-5, -5.171200321326409e-5] km/s
+ time of flight: 1.6309532882747093e8 seconds
+ arrival date: 2029-07-10T17:32:24.401
+ thrust profile: [0.4848769226191405 -0.09738123084639863 -0.17668208814102368; 0.10064110038545454 0.02750584214460962 -0.11287480283074815; 0.0823403158514641 0.03998519921679431 -0.15586403830826645; 0.07405285247871439 0.04739568226878764 -0.1996733613515048; 0.0618222351292469 0.04572180528030232 -0.2134909648175021; 0.029160852071327795 0.02329513994774094 -0.11639424220433182; 0.011319972692331471 0.010380027399080975 -0.05621377303047424; 0.012375983403733462 0.011398496700887998 -0.06352626249870011; 0.004809059664576253 0.00458827933232713 -0.02974797725639961; 0.0008782813984866398 0.0008252822387747647 -0.004743619058510852; -0.001208480572837451 0.0009999591116286028 -0.003322875966338385; 0.0011311032345026808 0.0012474698939579265 -0.008011308135575488; -4.787197605404933e-6 7.958289247861957e-5 -0.0039958074830011864; 0.0002678943501570766 0.0002496289390456362 -0.0032028708564104513; -0.0018008106220136477 0.00020336267234885355 -0.003943881160976689; 0.0002161499446954924 -0.005191022432700686 -0.004553586450013697; 0.0010242201675348377 0.0010005996159885965 0.003754638015558802; -0.003479384555623013 0.002515136882436601 -0.001245220093763131; -0.0053216308926234916 -0.0019042175004608986 -0.005087066248765592; -0.004454300657447449 -0.0008771847515132742 -0.003797523794092078] %
+
+Mass Used: 106.41976627008944 kg
+Launch C3: 94.91606714253811 km²/s²
+||V∞_in||: 5.430600070703669e-5 km/s
diff --git a/archive/ES_0.5657982599269262 b/archive/ES_0.5657982599269262
new file mode 100644
index 0000000..a1cb5fa
--- /dev/null
+++ b/archive/ES_0.5657982599269262
@@ -0,0 +1,22 @@
+archive/ES_0.5657982599269262---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T11:13:43.534
+Launch V∞: [7.533241085100956, -6.348167116770249, -0.08331683689705878] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005969187924732292, -0.0017681236395110133, -0.00325154737762555] km/s
+ V∞_out: [-0.0033793644174211334, -0.00037828857975701394, 0.0015773284393683998] km/s
+ time of flight: 1.6740091332334673e8 seconds
+ arrival date: 2029-08-30T23:28:56.534
+ thrust profile: [0.3043413577713626 -0.05402250872970167 -0.11900029201916831; 0.05345407056976408 0.017117065014086646 -0.06712624112948343; 0.09778713255717833 0.05283894347009245 -0.2026356569434241; 0.04613493973221218 0.031915143041227695 -0.13752816224129583; 0.04200704572553944 0.03348498483453803 -0.15981689921569536; 0.029857675654007283 0.026538295084143425 -0.13871360923635884; 0.019094535030114164 0.01856066004274187 -0.10462169733459331; 0.00892155436220733 0.007461735470287221 -0.050480511263108846; 0.0031745044153755598 0.0038968634498783663 -0.026470558244484577; 0.0014900117086650193 0.0017438836527246201 -0.015771714389072326; -0.0007365529883578371 0.001808091786818718 -0.01114987433850917; 0.002957894697374867 -0.0012859055485925906 -0.021831075599964077; -0.0019736838850615652 -0.0009742642749569978 0.0016315442296250475; -0.010058099926557054 -0.0012571007957021619 0.0012100067564267637; -0.0018917863423033373 0.00025384133511379965 0.005839704113411925; -0.0006712797876729145 0.0018059143138857085 0.002978438504859726; -0.008761978689489568 -0.002846761920031277 0.006789478687420345; 0.007837114734535435 0.010436254189671382 -0.0013794211553282048; -0.00029394380189483153 0.0005477358816812191 -0.00037998682791865043; -0.011378438434338785 0.007385078457895627 -0.0034278466563174275] %
+
+Mass Used: 93.93861925804185 kg
+Launch C3: 97.05588868400665 km²/s²
+||V∞_in||: 0.0037490176844540172 km/s
diff --git a/archive/ES_0.5658055816034347 b/archive/ES_0.5658055816034347
new file mode 100644
index 0000000..82a5ac1
--- /dev/null
+++ b/archive/ES_0.5658055816034347
@@ -0,0 +1,22 @@
+archive/ES_0.5658055816034347---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T23:50:19.557
+Launch V∞: [6.152791912634972, -7.25305945487787, 0.27934398492226664] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.280200167471791e-6, 4.228209192848664e-6, 4.49450782000326e-6] km/s
+ V∞_out: [6.274462999102008e-6, 4.122217740885214e-6, 1.304806873516414e-7] km/s
+ time of flight: 1.8393755233011407e8 seconds
+ arrival date: 2029-02-22T21:36:11.557
+ thrust profile: [0.771776997804592 -0.20437133249774952 -0.224692272992409; 0.16370644499874507 0.047610900251795055 -0.15494208258017925; 0.0770450030851192 0.04365475342328262 -0.12415393562696261; 0.03816510887177193 0.029272078774996102 -0.08684627042315649; 0.0370092048337421 0.034975013088791314 -0.10826218728558926; 0.027273386871471718 0.030204995009935315 -0.09843805792873872; 0.01679134369683046 0.020882149021529493 -0.0715539556251097; 0.021124386242303863 0.029496235385559132 -0.10365121143098222; 0.002877729711179815 0.0038907841999836577 -0.01515939879893044; 0.00025018480659854444 0.0001650056299808589 -0.0024527043734296258; -0.0002307576050472359 0.0038746863927293733 -0.0033568433005520676; 0.0014935169995456126 0.002112097201447146 -0.011291219159925798; 0.0005398837682851135 0.0008152983171726321 -0.0042083658313530345; 0.001915269824183011 0.0003686495488147406 -0.004603729969821023; 0.0042164421007158635 0.005745128162502253 -0.004042826907246273; 0.0010652367303267654 -0.00046700994705254186 -0.0061648384859594365; 0.00422389327664751 -0.0014751675844562875 0.0008678808094202341; 5.659079863741903e-6 -0.0026596602290232642 -0.0043090899070118045; -0.00046324227020093606 -0.0014952887023951195 0.00119835229892549; -0.006534845058256659 -0.002762009232641087 -0.00024571773581616636] %
+
+Mass Used: 131.94628698180486 kg
+Launch C3: 90.54175283809182 km²/s²
+||V∞_in||: 7.509891277254682e-6 km/s
diff --git a/archive/ES_0.5658057547250406 b/archive/ES_0.5658057547250406
new file mode 100644
index 0000000..55e084e
--- /dev/null
+++ b/archive/ES_0.5658057547250406
@@ -0,0 +1,22 @@
+archive/ES_0.5658057547250406---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T15:01:40.817
+Launch V∞: [6.5633228559534835, -7.487237770379872, -0.004363735208302211] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012011737789744764, -0.0003831115645167021, 0.00838153270234645] km/s
+ V∞_out: [-0.014058363942362574, 0.00013910769805242838, 0.004122305659573976] km/s
+ time of flight: 1.854434889042016e8 seconds
+ arrival date: 2029-03-17T23:06:28.817
+ thrust profile: [0.14165055838056212 -0.041479937489733505 -0.058471756024862896; 0.05107401145080157 0.009780581272682854 -0.06349394604813617; 0.047707678701774475 0.01907859999557706 -0.09956237144455629; 0.04528864952892515 0.024114559858959442 -0.1315048809105659; 0.03768127332890295 0.023664732422721636 -0.13927487707112346; 0.01942482239888037 0.01360847655667645 -0.08710457824582961; 0.027801626519672728 0.020643593321225402 -0.1429646373838103; 0.011699021928113585 0.00923945448914932 -0.06837871294259759; 0.009706191587892155 0.008078079588053438 -0.06338655657647096; 0.0017085293481779134 0.001983030736069638 -0.012023769040214596; 0.0011165509082000022 0.0009474880479463819 -0.011700642019697626; 0.001213811365879612 0.00011653297068704992 -0.001942320533649847; -0.0002332423298699439 0.0010647727106707853 -0.0040828264357905325; -0.0039544686631689824 0.004450137425238716 -0.0004643715098064799; -0.0015216665637091042 -0.00026073149582911653 0.001509284301835344; 0.003954075851517133 -0.0006722018933546833 -0.0036311561207837384; 0.0070588867924868265 -0.0070043338357191716 -0.00019958714005285406; 0.0033601872770944482 -0.016049822974593148 -0.00677566823546109; -0.00040216364757726837 -0.008116114416599261 0.004327637665747233; 0.009580601075749151 0.003068452828999834 -0.010683506050493738] %
+
+Mass Used: 81.81364077330954 kg
+Launch C3: 99.13595538386933 km²/s²
+||V∞_in||: 0.01465191829218795 km/s
diff --git a/archive/ES_0.5658064737418916 b/archive/ES_0.5658064737418916
new file mode 100644
index 0000000..9d0e349
--- /dev/null
+++ b/archive/ES_0.5658064737418916
@@ -0,0 +1,22 @@
+archive/ES_0.5658064737418916---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T02:27:18.005
+Launch V∞: [6.542180088529309, -7.431387544478317, 0.0937008768335409] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2272101438182963e-9, -2.8455106775485177e-9, 4.804577886742855e-9] km/s
+ V∞_out: [8.793027010427673e-10, -1.9654082273542143e-9, -2.6088203119624153e-9] km/s
+ time of flight: 1.8749577787483025e8 seconds
+ arrival date: 2029-04-10T04:36:55.005
+ thrust profile: [0.18420275101531838 -0.0438607224995951 -0.06900188468215357; 0.09910431785097878 0.028560978907061215 -0.11012241286823; 0.05734898405200621 0.031031515791225362 -0.1062966566303529; 0.04521183714865414 0.03254420052465282 -0.11834718565775959; 0.031624218127210175 0.027658873830880948 -0.105286761308482; 0.03419547933513062 0.03541108291062381 -0.14202467661877388; 0.013061811503901396 0.015238982176778198 -0.06434806923461435; 0.006654469815157579 0.008661425020033614 -0.038579789816851506; 0.014209458268161577 0.018940355482229214 -0.08841149822736696; 0.003004342636737164 0.005392470322338196 -0.024265000776564336; -0.000329594466225697 0.00030984547096470197 -0.0016210814218552867; -0.0006777191747817481 0.004803541411679438 -0.011904951523694035; 0.0006749106411007515 0.001079198337059751 -0.006853080552280096; 0.0011033834511394477 -0.0030510848485531712 0.003097585794665599; 0.0066475488612213526 -0.007592250442827899 -0.0006921716374899026; -0.003238984136002372 -0.0012804266222118386 0.0022972904827409588; -0.0006673745376857736 0.013339397874274508 -0.009182426462260864; 0.0008953310626855294 -9.92768440758327e-5 -0.005780315127657618; -0.006430304244939372 -0.001261378798752373 0.0076661876766662; 0.01373746706370661 -0.0014059796230049136 -0.0006528240635103543] %
+
+Mass Used: 88.2400968579791 kg
+Launch C3: 98.0344210012962 km²/s²
+||V∞_in||: 6.011768850392385e-9 km/s
diff --git a/archive/ES_0.565812411562571 b/archive/ES_0.565812411562571
new file mode 100644
index 0000000..ed24885
--- /dev/null
+++ b/archive/ES_0.565812411562571
@@ -0,0 +1,22 @@
+archive/ES_0.565812411562571---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T04:30:50.978
+Launch V∞: [6.452548119927482, -7.583826683967991, 0.08660530007934021] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.7498556992719035e-8, 5.940798320322717e-8, 4.072071491612141e-8] km/s
+ V∞_out: [-2.0239275735947533e-8, 4.122277277722133e-8, -6.736597439697562e-8] km/s
+ time of flight: 1.8180770227802536e8 seconds
+ arrival date: 2029-02-03T10:39:12.978
+ thrust profile: [0.14282535146509215 -0.05082683175829674 -0.060005349672201946; 0.042392653850797844 0.004513910644086575 -0.05355690983107503; 0.049963591830211124 0.013639527958031326 -0.10648588259023883; 0.0547029982744765 0.01974542034904127 -0.16158698112234057; 0.047102856461397634 0.019598843422306205 -0.17575434225098419; 0.03387215530349658 0.015368023176494404 -0.15136442689467874; 0.020194386878306533 0.009663501097211438 -0.10424605116997802; 0.010231022238721587 0.004740735229941442 -0.0587084682995996; 0.0028257416318729486 0.0029787478916892592 -0.02487808790951806; 0.001080426357557873 0.0016669605463232628 -0.00740556596415788; 0.0031774841488209737 -0.0027121476476436313 -0.00634016491346534; -0.0020263456489445454 0.0032000114637497105 -0.0005687253910285155; 0.0014642393589394359 -1.1393077074672658e-5 -0.007737063013592957; 0.003472464496284888 -0.0038681248904882735 0.000368610543330883; -0.001333844909849467 -0.000213279931183635 -0.004007373247031114; 0.00039335901760885613 -0.0007664371802637335 0.010884382982369576; 0.00018091202000989758 -0.0018500721046066412 -0.002421319631897709; 0.0018477076738220742 -0.000997974239458597 0.005235485954811098; 0.00438826592810179 -0.0026366847349900573 0.001350090829129274; -0.0007863457211818143 -0.008869590689439412 0.012134038842052186] %
+
+Mass Used: 81.69686829539523 kg
+Launch C3: 99.15730489044645 km²/s²
+||V∞_in||: 8.120115065743312e-8 km/s
diff --git a/archive/ES_0.5658146585966002 b/archive/ES_0.5658146585966002
new file mode 100644
index 0000000..f84566b
--- /dev/null
+++ b/archive/ES_0.5658146585966002
@@ -0,0 +1,22 @@
+archive/ES_0.5658146585966002---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T02:22:30.112
+Launch V∞: [6.395672030188579, -7.499286902048253, 0.10088285565814264] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.12640861159893e-9, -1.944594701899676e-9, 2.499315026120964e-9] km/s
+ V∞_out: [1.1889797185411056e-9, -2.7939545858220594e-9, -3.844850762551323e-9] km/s
+ time of flight: 1.823701579919075e8 seconds
+ arrival date: 2029-02-06T20:45:07.112
+ thrust profile: [0.2233553700402731 -0.05634966022209345 -0.06646651284260055; 0.06696347884449397 0.022116118559771757 -0.06381701358559584; 0.13147619737960872 0.08536676514086147 -0.1905143274197373; 0.04063108510061142 0.03333333601249973 -0.08995575850267186; 0.020055748881857596 0.019419394053858445 -0.05633642806450573; 0.02276291258939944 0.02736106038715675 -0.07407515360146881; 0.019821509239052522 0.02800594440440223 -0.08329667589673773; 0.0411300313838087 0.06171124629261972 -0.1777874520166212; 0.01421633508192712 0.024063330839937776 -0.07772623881593681; 0.003732143022955087 0.007424706755853579 -0.02635472128827261; 0.004427151578151576 0.00937360018598771 -0.03154673539323782; -0.0003429169254088768 -0.00033167904935558557 -0.0009188867755276916; -0.0015909927251490286 -0.0021972870847428334 -0.0012915973935223421; -0.0016171526217859445 -0.003350700943311054 -4.401174252545003e-5; -0.00020970904541501483 0.00045436476299091704 -0.0015998990097829072; 0.00024636517002467155 -3.252821588989991e-5 -0.0004272692609234807; -0.0033106903633928603 0.008265813763828789 -0.003032178152323266; 0.002382902366457556 0.00024063559522804855 -0.0008874308530343639; -0.0011381740602477842 -0.0008899989732751665 0.0051683428458546; -0.00014792509019133842 0.0015837374708837732 -0.0006978198286947865] %
+
+Mass Used: 93.38483940208107 kg
+Launch C3: 97.15410210753471 km²/s²
+||V∞_in||: 4.4499949394499625e-9 km/s
diff --git a/archive/ES_0.5658220202611646 b/archive/ES_0.5658220202611646
new file mode 100644
index 0000000..f6c0862
--- /dev/null
+++ b/archive/ES_0.5658220202611646
@@ -0,0 +1,22 @@
+archive/ES_0.5658220202611646---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T02:00:10.678
+Launch V∞: [5.900820760574823, -7.684078327993536, -0.021626626753506885] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.9853009959873635e-7, -2.145815714485665e-7, -3.599799122678099e-7] km/s
+ V∞_out: [2.457081378213536e-7, -3.5750890318595504e-7, 3.8247287224528777e-7] km/s
+ time of flight: 1.7366006988004687e8 seconds
+ arrival date: 2028-10-28T00:54:39.678
+ thrust profile: [0.4773230059096041 -0.1651049810985121 -0.17248228353912212; 0.19102939801072705 0.037593010106696814 -0.19951265085700437; 0.05823329797425824 0.025443293645817273 -0.10619652033049845; 0.04281054708477046 0.025851010047054937 -0.10747992558045273; 0.033367185386307195 0.024351173489366853 -0.1034580774516903; 0.026596856791959812 0.022990234259556288 -0.10215424908282032; 0.03358130814452016 0.029970623959581087 -0.14155760545332993; 0.008179294872162603 0.007985777706431033 -0.040417797742834105; 0.00955932203860434 0.010129774072541307 -0.05275187669546481; 0.008463778106071636 0.009623613082990272 -0.05208082437218412; 0.004370082799333873 0.005194910193600545 -0.029182515781031648; 0.0023557384791899312 0.0035283481136207055 -0.018303727255260274; 0.0001807212815036536 -0.000263851196468699 -0.0013887037607256381; 0.00010991993004005575 0.0005234141649449823 -0.0014533037004347852; 0.0002058789263104416 0.0001435709130452021 -0.0008113816747071568; 0.0003055748675759957 8.987353940919746e-5 0.0001851196934871172; -0.00011781468729514717 -2.0742652053619892e-5 0.00022733944894699377; -0.00038083750362072235 0.00024659008051572027 0.0007060691699515447; 5.9195561675215403e-5 0.00012024606986534687 -0.0006408201728977793; -0.00014354209270694247 -0.0002458670824791063 -0.0002705582538792984] %
+
+Mass Used: 112.57861382878491 kg
+Launch C3: 93.86521311015551 km²/s²
+||V∞_in||: 5.783225988389655e-7 km/s
diff --git a/archive/ES_0.5658308186511349 b/archive/ES_0.5658308186511349
new file mode 100644
index 0000000..cc4759c
--- /dev/null
+++ b/archive/ES_0.5658308186511349
@@ -0,0 +1,22 @@
+archive/ES_0.5658308186511349---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T20:58:51.424
+Launch V∞: [6.201172636231491, -7.6999942180100165, -0.08084101263079989] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1347592146892864e-6, 0.0003576571742632803, -0.00014706970002229374] km/s
+ V∞_out: [-0.00032224610091427573, -0.00016352136558449984, 0.00013448203694691274] km/s
+ time of flight: 1.7240203559990737e8 seconds
+ arrival date: 2028-10-13T06:26:06.424
+ thrust profile: [0.19751064199939392 -0.07299222858308568 -0.07872919692259345; 0.0851157398642044 0.012679497306024393 -0.09504727504915701; 0.07410011177274158 0.027789839918684802 -0.13465231285398432; 0.0623211049147581 0.03267500471553035 -0.1552497046473903; 0.049588210643813475 0.03146710385439563 -0.15562976163667158; 0.03756341317861469 0.027335968030485738 -0.1420268731582895; 0.03131695497255216 0.025373669335246783 -0.13738639267978595; 0.00837250787970951 0.007299009008264647 -0.04310193273446875; 0.006633126553459077 0.006196278532626823 -0.03795129937729591; 0.0029999017677821115 0.003708864578781377 -0.024358516242537778; 0.0067905200946782995 0.007081675184496897 -0.045256958734394594; 0.00044564967521689363 -0.0001396704398450753 -0.0010150156103057406; -0.00047400713880723077 -3.1156070247548844e-5 -0.0013802921963630664; -0.0004251287419634451 -0.0005869598856519087 -0.0017535269639654977; 0.0002728550478390859 -0.00014147370339336117 0.0012239317226876486; -0.0017740491451392324 0.0021318774261610794 -0.0015464130670726818; 0.0006465131336322997 -0.00016195193189212943 -0.001870130624197424; 0.001166697115398543 0.001927946363475456 -0.000981052387917218; 9.79734313115157e-5 -0.0010230595154730883 -0.0012761123855889464; -0.0007080830539397272 -0.0009406988299089588 0.001106749607339035] %
+
+Mass Used: 89.9218567284911 kg
+Launch C3: 97.75098829105708 km²/s²
+||V∞_in||: 0.0003867162249571606 km/s
diff --git a/archive/ES_0.5658329627565251 b/archive/ES_0.5658329627565251
new file mode 100644
index 0000000..bd831dd
--- /dev/null
+++ b/archive/ES_0.5658329627565251
@@ -0,0 +1,22 @@
+archive/ES_0.5658329627565251---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T07:38:38.584
+Launch V∞: [6.166932185761697, -7.505971964840549, 0.1043991167728543] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.303606241937945e-9, -1.9030391844730906e-9, 1.7429572938492553e-9] km/s
+ V∞_out: [9.62896936396658e-10, -2.2891339124658744e-9, -3.3130646351515087e-9] km/s
+ time of flight: 1.790015983416254e8 seconds
+ arrival date: 2028-12-28T02:18:36.584
+ thrust profile: [0.42427823323194436 -0.11921057164900654 -0.12098015265660926; 0.1441705925878782 0.04315020439102394 -0.1308014688359683; 0.09841818325019071 0.05769178864333692 -0.14746672412903392; 0.047265364783173475 0.0371828796672511 -0.10135098293893914; 0.04259965994601896 0.0473270625059763 -0.1278802094152833; 0.024273572700965605 0.028398814170003905 -0.08405279855443827; 0.01931371297868141 0.0260100604699133 -0.07783502243550346; 0.010006622890400298 0.01744740949784954 -0.05689656573173161; 0.018141271707183715 0.03221640951597695 -0.09899629159176503; 0.008428046744653894 0.014808242492480278 -0.050944907437330544; 0.0035272607259635206 0.005635026726660596 -0.021989335982499237; 0.0005072109337836285 -0.0006233949326527711 2.8685230817948604e-5; -0.0006252382041349034 0.0008402216574024109 -0.002218930458743285; -0.0002067353816493298 0.0002473013977450256 -0.0006757607240951663; -3.953530985173915e-5 0.0002601076180430407 0.0007313657854990934; -0.000820087774530081 0.0001106278651674935 0.0003782292651295055; -0.0006438722568035946 -0.001639654773739455 0.0014715957130025186; 0.002481142911131485 -0.002153162224956145 0.0004899447132743514; 0.0007268348539255837 2.6432775228983662e-5 0.003043623187372002; 0.00018062175287009198 0.00027604102598733385 0.00019989078214344608] %
+
+Mass Used: 109.57931632063628 kg
+Launch C3: 94.3815668963388 km²/s²
+||V∞_in||: 3.459199326971169e-9 km/s
diff --git a/archive/ES_0.5658353898555306 b/archive/ES_0.5658353898555306
new file mode 100644
index 0000000..ecc39a2
--- /dev/null
+++ b/archive/ES_0.5658353898555306
@@ -0,0 +1,22 @@
+archive/ES_0.5658353898555306---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T08:58:57.593
+Launch V∞: [6.297362159846241, -7.37822583173693, 0.12194769399481657] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.604026379991091e-9, -1.6317428463128073e-9, 1.2678643545999577e-9] km/s
+ V∞_out: [9.201125890531261e-10, -1.8907732204178717e-9, -2.7996185327957854e-9] km/s
+ time of flight: 1.8129661123746082e8 seconds
+ arrival date: 2029-01-23T17:09:08.593
+ thrust profile: [0.49116292009660617 -0.13932615842546023 -0.15305143270798252; 0.07722323325075149 0.020931188321651865 -0.07775670831497863; 0.10054665612061854 0.054904123136682415 -0.16401728102823424; 0.08915388421598898 0.06553029469361826 -0.19975504049036336; 0.03799507360314754 0.03445862631383237 -0.11420679979686693; 0.02618990270367341 0.027331743331537144 -0.09520097791182686; 0.020150638338217418 0.023644954855924667 -0.08646426665455172; 0.008296399599917187 0.010434792231399242 -0.04028503865243012; 0.00836880216939503 0.012066161906459573 -0.04690517443556751; 0.0012551072287132045 0.002267567452733161 -0.011651020111012676; -0.00034761480710488796 -0.0005502712523784602 -0.0010377353183058503; -0.0014936305545596338 0.00028160989097140326 -0.002597718242024088; 8.704807562632437e-5 0.0006374014438357827 -0.000134138523029645; -0.001383188982668299 -0.003914647087906252 0.0006034586318403195; -0.0030875155424180413 -0.0006116546629401814 0.001117974300354845; -0.005229722988121828 0.002577169754533906 0.0007822720792374244; 0.0005505259559431821 -7.653491098559892e-5 0.005618681061231072; 0.00032237298844946184 0.001901553570481906 0.001824240461912961; -0.002354952705378017 -0.008907633050474366 0.0006073562202518865; -0.0005854825371207262 -0.0018333745783855812 0.007815463176179826] %
+
+Mass Used: 111.16711745219527 kg
+Launch C3: 94.10985783644406 km²/s²
+||V∞_in||: 2.6159062226818288e-9 km/s
diff --git a/archive/ES_0.5658417779903163 b/archive/ES_0.5658417779903163
new file mode 100644
index 0000000..e863f49
--- /dev/null
+++ b/archive/ES_0.5658417779903163
@@ -0,0 +1,22 @@
+archive/ES_0.5658417779903163---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T00:35:10.666
+Launch V∞: [6.4622087210106764, -7.44058442979128, 0.11682885272092776] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012728160533580929, 0.0008180120368769267, 0.0004975815145123429] km/s
+ V∞_out: [-0.0010087733476706168, -0.0004826263707816277, 0.0011340340161433825] km/s
+ time of flight: 1.83195379128733e8 seconds
+ arrival date: 2029-02-17T08:11:29.666
+ thrust profile: [0.2713868661593183 -0.07646195839834447 -0.09581268772118845; 0.06318148623807636 0.014987436074228509 -0.07054609758286855; 0.06685535012470059 0.032815052936975515 -0.12426922993888971; 0.03765776210947043 0.02506599352602159 -0.09706809441462759; 0.059258199193584056 0.04784006142276204 -0.1920566147111132; 0.029264890449780884 0.02604077235511257 -0.1180685678357989; 0.019631620749483984 0.019905047531389084 -0.09502775191276941; 0.012221471777180738 0.012965579073741778 -0.06477719222713173; 0.004775037096461928 0.005217297230808356 -0.028845448361771366; 0.0040558554759697295 0.004799000019359398 -0.02706911931528027; 0.0020540847677536457 0.0025027694303132817 -0.01290405830813797; 0.0015641579769655567 -9.203759106636667e-5 -0.002921584579244665; -0.0010863561857784201 0.0025025302375686065 -0.0014940788228966662; 0.0009798319196123834 -0.0021952134047899924 -0.002170357273927753; 0.0011569909173963038 0.01033689806136988 -0.0007712782365893044; -0.006424619481183395 -0.0012070044027526687 0.00038851840083623597; -0.005367274727039631 0.00013075221102909409 0.0044508689932408665; 0.008050102600298705 -0.014635771017301898 -0.0039855465503249796; -0.00152083562231093 0.00691469661193739 0.003583945407179647; 0.002238261747626387 0.004774763594184644 0.008090654440331427] %
+
+Mass Used: 93.52156570444504 kg
+Launch C3: 97.13608719158697 km²/s²
+||V∞_in||: 0.0015927309131633022 km/s
diff --git a/archive/ES_0.565846542032701 b/archive/ES_0.565846542032701
new file mode 100644
index 0000000..041e078
--- /dev/null
+++ b/archive/ES_0.565846542032701
@@ -0,0 +1,22 @@
+archive/ES_0.565846542032701---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T23:47:58.467
+Launch V∞: [7.791884918321834, -5.700861594088046, 0.9957350266430115] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2272774123962822e-9, 7.900984584112912e-9, -2.4031234704945446e-9] km/s
+ V∞_out: [4.266531022591932e-9, 8.782753478801856e-9, 2.1381355456897655e-10] km/s
+ time of flight: 1.8531302149616525e8 seconds
+ arrival date: 2030-03-24T19:38:19.467
+ thrust profile: [0.4158718505852578 0.0034837122449625866 -0.07333746415445393; 0.25825876900942196 0.16208820255373213 -0.15846064144927155; 0.07018109916705977 0.08398653388831447 -0.09813240541340801; 0.03895894920573875 0.06562934786459756 -0.08593212645298547; 0.028283364208966624 0.0626880235783079 -0.08870591306145317; 0.014867845997077052 0.0411487450080025 -0.06364451753826848; 0.011508013154912672 0.03811356907348632 -0.06316999301308472; 0.007491331888547267 0.03165867516125173 -0.054906726900510426; 0.003177165015447048 0.019383387456135548 -0.0364825577847637; 0.003990561165425175 0.012139998049412477 -0.02619842423468015; 0.0019939292994885175 0.010491042648006951 -0.023253710496661077; 0.004686879349363409 0.0017098665578949555 -0.00033325649581804817; 0.0011915154444384788 -0.002847358123977225 -0.0020456882322345948; 0.0007144547572275031 -0.005287640955015719 -0.0003638864416354592; -0.0004696421476482965 0.004586079883059311 -0.0012768105463187586; 0.003546424365186621 -0.005418152319688611 -0.00023811678131203506; -0.006784005569648159 0.005392561263926739 0.002867342996745078; -0.003683645913867313 -0.0020905367063696993 -0.0014355050630593315; 0.00021035597980704427 -0.005029846936167459 -0.004729403365902809; -1.8720271795513136e-5 0.0009319060440505656 -0.0010237035191093605] %
+
+Mass Used: 110.62640556296628 kg
+Launch C3: 94.20478173860312 km²/s²
+||V∞_in||: 8.349058010327257e-9 km/s
diff --git a/archive/ES_0.5658550104812201 b/archive/ES_0.5658550104812201
new file mode 100644
index 0000000..a37b3c3
--- /dev/null
+++ b/archive/ES_0.5658550104812201
@@ -0,0 +1,22 @@
+archive/ES_0.5658550104812201---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T07:01:53.365
+Launch V∞: [6.66906831472619, -7.3893437814350165, -0.05446688871631223] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.976171842708742e-9, -2.302927264675721e-9, 3.366993981984027e-9] km/s
+ V∞_out: [1.613400149435707e-9, -3.5882304382063987e-9, -6.355627043103837e-9] km/s
+ time of flight: 1.874957778747012e8 seconds
+ arrival date: 2029-04-10T09:11:30.365
+ thrust profile: [0.12457060668596878 -0.03429154460690589 -0.05085912203257439; 0.07423557685356337 0.016118252330910587 -0.09422798046401532; 0.06559142241783796 0.029148930655157727 -0.1435276970500297; 0.041503714406935635 0.023765524166808646 -0.12356302567894009; 0.03791112763649482 0.026040788643700713 -0.14257507071185332; 0.026861225960389885 0.020640162694560475 -0.1249817356411458; 0.013164395831283577 0.010498312450274994 -0.07340791758060299; 0.006570659602491935 0.0050773605571679285 -0.045799827495729785; 0.0006874510969470354 0.00288022843406652 -0.02406559418367401; 0.005167405135363692 0.005374867542640587 -0.03784599831333689; 0.0020345751195326896 -0.0001355065551801567 -0.006717612259207201; -0.001049327672874815 -0.0014247255357538562 -0.0033016774548672674; -0.004885531402238162 -0.0010999361148581594 0.00036332921869449255; -0.005162156688992484 0.003851843966067979 0.004375802295700731; -0.0017254100611075076 0.0011184594954517276 -0.004618587972355591; 0.00011692057805395308 -0.00011130504036873236 -0.0019654425724087514; 0.004258360179174627 0.0015108609142219951 -0.0019589284815016653; -0.00020424634739913062 -0.0004054284842539523 0.0025888384552507516; -0.003177045963554439 0.0209365524129261 -0.008758397456402667; -0.0049092836882543775 0.00029252083428410875 0.02238067911342943] %
+
+Mass Used: 82.18677686076899 kg
+Launch C3: 99.08184034868361 km²/s²
+||V∞_in||: 7.2356583912376804e-9 km/s
diff --git a/archive/ES_0.5658608978994226 b/archive/ES_0.5658608978994226
new file mode 100644
index 0000000..763a3be
--- /dev/null
+++ b/archive/ES_0.5658608978994226
@@ -0,0 +1,22 @@
+archive/ES_0.5658608978994226---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T20:48:10.266
+Launch V∞: [6.515013147522038, -7.471415992112421, -0.020875543797744447] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.016537289822289365, 0.00029140655543647635, -0.012384906415018758] km/s
+ V∞_out: [0.019856883528108105, -0.00019021082815325627, -0.005701713743641862] km/s
+ time of flight: 1.874957778749388e8 seconds
+ arrival date: 2029-04-10T22:57:47.266
+ thrust profile: [0.19096401636859572 -0.046439292711461126 -0.0709776685313096; 0.07365596539003723 0.021354771331619577 -0.08598209834500196; 0.05116383897383847 0.02736236284662846 -0.10108292584753716; 0.049888116136188876 0.0344001469625137 -0.12999548158755397; 0.029145421997085287 0.028285616838763353 -0.11369328761691602; 0.025850258623958157 0.02716746133264404 -0.11567230083488364; 0.013128680725470762 0.010999325871375894 -0.06829358236030954; 0.02130030563332777 0.019612773863945467 -0.08636619564946767; 0.009689787298982623 0.006192287067714446 -0.045742628839868835; -0.00022470860602545 0.008308431701478085 -0.05069206132325957; 0.00332829707434187 0.0026366689963358884 -0.017037244158725588; -0.0006744100730619082 -0.0011650613498376378 -0.0036382630154141466; -0.0026730110323502933 -6.522950582537527e-5 0.0017757152249726574; -0.0014201152791218493 -0.000561873728459116 -0.003504960329518205; 0.002658793732243381 0.0011530309238105487 0.007803816049090853; 0.0017710200319110366 -0.0007881980487768316 -0.0038474342160383698; -0.00039861770674311724 -0.00010857000868927944 0.004685453413784262; 0.0034360080874586787 0.004202126347245987 0.0054416082831343845; -0.002299161227270188 0.0005347653683968881 0.006698944372365691; -0.003976055623123772 0.0003861075654819553 -0.016948533606868432] %
+
+Mass Used: 86.94169488653506 kg
+Launch C3: 98.26788902790709 km²/s²
+||V∞_in||: 0.020662835704610333 km/s
diff --git a/archive/ES_0.5658640292521155 b/archive/ES_0.5658640292521155
new file mode 100644
index 0000000..911afa0
--- /dev/null
+++ b/archive/ES_0.5658640292521155
@@ -0,0 +1,22 @@
+archive/ES_0.5658640292521155---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T17:46:19.534
+Launch V∞: [6.409231564630884, -7.235115266346872, 0.20010600540250179] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0020368791389206893, 0.002199830865958887, 0.0020697139278543553] km/s
+ V∞_out: [-0.0023884922512835342, -0.00119669405202382, 0.0024764313573019583] km/s
+ time of flight: 1.8749577787503722e8 seconds
+ arrival date: 2029-04-05T19:55:56.534
+ thrust profile: [0.5047943680482854 -0.12463538343505016 -0.12889433692299573; 0.11125792102384875 0.04036305158137442 -0.0935774442095444; 0.1308575512634234 0.08539292631896248 -0.17955389841014371; 0.053446527139554 0.046655772664380965 -0.10328867132099004; 0.021782487914055834 0.027394755157969804 -0.06359155683880817; 0.07102995678616143 0.08926607784390059 -0.20142486552947111; 0.014066514575649077 0.02209062324066217 -0.05457556949659583; 0.007146740796089055 0.01503386866723812 -0.04042403444912498; 0.0024213107363150314 0.00583795105378967 -0.014589153149088027; 0.004069428192094774 0.004338609080834641 -0.015011695773055467; 0.0009621171284366883 0.004829967886920933 -0.011527401382685475; -0.002471905879372737 0.0008639778528921548 0.00027245739964099373; -0.0003163042597723914 -0.002935232530175966 -0.001397686754034501; 0.00112799431561983 -0.0013731985483064742 0.0009831004013737396; -0.0028400521968010646 -0.005045632916066592 -0.00029359919730309256; 0.0002436450381006909 0.0008938858075489408 -0.005730166222438464; 0.0015614640201992683 0.0012173560499665512 -0.001576067318015858; 0.001483126623768189 0.0004280287929012247 -0.0019325907588400326; 0.005842525494281909 -0.0031850981716808552 -0.0010042109242620863; -0.003983196067858104 -0.004063070626225904 0.0007823777502522827] %
+
+Mass Used: 114.96112407872488 kg
+Launch C3: 93.46518457978456 km²/s²
+||V∞_in||: 0.003643054790769694 km/s
diff --git a/archive/ES_0.5658733476280237 b/archive/ES_0.5658733476280237
new file mode 100644
index 0000000..5c8334c
--- /dev/null
+++ b/archive/ES_0.5658733476280237
@@ -0,0 +1,22 @@
+archive/ES_0.5658733476280237---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T01:05:22.659
+Launch V∞: [6.4502762679357755, -7.461498232440605, -0.3418784453244735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0003039886470138381, -0.00037303464566671823, -0.00033609902897711934] km/s
+ V∞_out: [0.0003685133397473228, 0.00020050027702572814, -0.0004150855319323221] km/s
+ time of flight: 1.8749577776760012e8 seconds
+ arrival date: 2029-04-11T03:14:59.659
+ thrust profile: [0.28580919251537656 -0.07344212870991296 -0.10435918898075904; 0.07529963430223714 0.0171041078168856 -0.08981242678828043; 0.038405524333934814 0.01707504593657665 -0.07694042901943046; 0.03916508113874536 0.024498032644737388 -0.11251973656903846; 0.029793333026099798 0.021611653961184186 -0.10812797830471407; 0.025446515454739544 0.020903369487362176 -0.11443669314217911; 0.02163692685039197 0.022405849535615363 -0.11374750219873607; 0.008878661048178242 0.008605847607426692 -0.054794193601868706; 0.008389733668986066 0.0069037179797659595 -0.04684747884335811; 0.006938558621839051 0.007100847377468935 -0.05269964298723921; 1.3714223704057568e-5 8.777745792709076e-5 -0.0038436593540127997; -0.0040366261598262605 0.0035266673737790223 -0.005917976472737065; 0.003395909716552612 0.007758983705314815 -0.006693017633302493; -0.0001494402668157446 0.00014442089722365356 0.00020291629076406206; 0.00823145862653362 0.0056144614004022845 -0.025760840746960275; 0.0004080765352506609 -0.0019181809923873362 0.0008844059406148407; -0.0038927177196674463 -0.003048782519031636 -0.008748003616156175; -0.0021756436343013308 0.009579721191546011 -0.013058970549703834; -0.0001926832240542383 0.0007553681452882855 0.00017871847721277442; 0.0023109825197764637 -0.0019252300696185744 4.1890252592795794e-5] %
+
+Mass Used: 92.03698495143544 kg
+Launch C3: 97.39690067678723 km²/s²
+||V∞_in||: 0.0005869637992758671 km/s
diff --git a/archive/ES_0.565879201960495 b/archive/ES_0.565879201960495
new file mode 100644
index 0000000..c8e3f64
--- /dev/null
+++ b/archive/ES_0.565879201960495
@@ -0,0 +1,22 @@
+archive/ES_0.565879201960495---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T14:59:56.979
+Launch V∞: [6.26880013706195, -7.3299191775902095, -0.1094762358193462] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4794240418889986e-7, 8.307949919958648e-8, 1.2971263117729996e-7] km/s
+ V∞_out: [-6.913622931723041e-8, 8.645111779815196e-8, -1.8293450397167261e-7] km/s
+ time of flight: 1.869004625860319e8 seconds
+ arrival date: 2029-03-30T19:47:38.979
+ thrust profile: [0.48884460832823673 -0.10780953582403961 -0.1431680264813015; 0.19541281238812014 0.0700504038557237 -0.17432031737782694; 0.10046878153752264 0.06789870061243575 -0.15511598809910118; 0.06153605297032116 0.057447390320633514 -0.13649881556058813; 0.041679768774409036 0.04737908566149941 -0.1198878759321614; 0.02274774611618299 0.02966081825824958 -0.08117819800072497; 0.01582268707329602 0.025644872830392722 -0.07238270018494987; 0.004657604805906284 0.008729585939177522 -0.026258288154325047; 0.003322982457191169 0.004882255128103511 -0.01769522899319648; 0.003475171501294428 0.00709993711089799 -0.02449689394804256; 0.002957958533337776 0.0008969730496603362 -0.007436807913467014; 0.0014075987777234676 0.0014509767285376895 -0.007049314312616434; -0.0013847555404882298 0.00025391987078618125 -0.003760656615810077; 0.0028044268889948665 -0.0013871931281534949 0.0034665762170805582; -0.0019169121920493684 0.0022109067037528055 0.003414635571060931; 0.0024577160022550594 0.0021624813749751928 -0.000393861422484861; 0.0013309484117437463 -0.0045370816541616 -0.002470047982421646; 0.005671802584481546 -0.002237342944035982 0.0034010159269155745; 0.0002475240276004795 -0.0017217773706990481 0.001774956692391313; 0.004387391589358435 -0.0043922791111981295 0.0034459941889832387] %
+
+Mass Used: 117.47332938516683 kg
+Launch C3: 93.03755535464184 km²/s²
+||V∞_in||: 2.1357557171030622e-7 km/s
diff --git a/archive/ES_0.5658832912892968 b/archive/ES_0.5658832912892968
new file mode 100644
index 0000000..075ead8
--- /dev/null
+++ b/archive/ES_0.5658832912892968
@@ -0,0 +1,22 @@
+archive/ES_0.5658832912892968---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T22:16:31.089
+Launch V∞: [6.3447756675560925, -7.358824180619245, 0.34362842053247533] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.89856930581946e-6, -1.419068354293409e-6, 2.7006068716201713e-8] km/s
+ V∞_out: [2.011720863651825e-6, -4.43308087727596e-8, -9.79219224434068e-6] km/s
+ time of flight: 1.8404597016001195e8 seconds
+ arrival date: 2029-02-26T02:09:21.089
+ thrust profile: [0.47386252372160037 -0.12508459783821624 -0.148141962244127; 0.07907691255770731 0.02232690976078561 -0.08040357338201333; 0.07924092785133621 0.04302735943558204 -0.13100676894207625; 0.0667845140245411 0.04913233069788861 -0.1534810643084068; 0.042507247591415144 0.03853677391491614 -0.12839802798250136; 0.027098556832575012 0.02878864848028949 -0.1014444352260999; 0.012538365233129905 0.015488634873592515 -0.057617855392462995; 0.010300993356230054 0.013908423308800648 -0.0538596147946673; 0.0049547724232446725 0.006620712787781871 -0.025934987046532028; 0.008113961674211159 0.012918752274596398 -0.05344069777704912; 0.0022908016562759484 -0.00046939875858349365 -0.008562326950629048; -0.0018922002011207487 0.0016142897826206984 -0.0025913519806487462; 0.00041686698624303353 0.004202272401834554 -0.006784540462731392; -0.0014543924493884827 -0.006490977300902346 -0.0004307278320462289; 0.003872659859962631 -0.008944092401853662 -0.0019023040556979906; -0.0037070358940953234 0.0003189072993950086 0.0021269216202324786; 0.000774975421619496 -0.0003800202298723642 -0.002778294832349628; -0.005114909850631054 0.0034280893237865428 0.0003146741300742019; 0.004332179562810054 0.003596147317798349 -0.016320723204346087; -0.0007328935413790436 0.005941794578871924 0.002622654371480284] %
+
+Mass Used: 108.79228601256955 kg
+Launch C3: 94.526552084276 km²/s²
+||V∞_in||: 9.999807929356226e-6 km/s
diff --git a/archive/ES_0.5658889087757847 b/archive/ES_0.5658889087757847
new file mode 100644
index 0000000..dbbc352
--- /dev/null
+++ b/archive/ES_0.5658889087757847
@@ -0,0 +1,22 @@
+archive/ES_0.5658889087757847---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T04:38:57.605
+Launch V∞: [7.481802885854957, -6.325457954589025, -0.09637067102353901] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0003389839331935043, -0.0002147137656394332, -0.014092865914586326] km/s
+ V∞_out: [0.0037960572397382603, 0.01287456176269777, -0.004288811688602131] km/s
+ time of flight: 1.653638934544327e8 seconds
+ arrival date: 2029-08-06T03:03:50.605
+ thrust profile: [0.3693723625896046 -0.07373103492049075 -0.14575077243566523; 0.16483913570748618 0.04742625620462933 -0.19698615733478844; 0.04307690268578556 0.02324901558481533 -0.09172780813217306; 0.03209102813960003 0.023208448928930422 -0.1002597453928049; 0.019290715564413627 0.016226872693930573 -0.0764261277205447; 0.027988253851989005 0.025925545923326 -0.13087059643201; 0.012575921859200286 0.013673534654947375 -0.07263033513170303; 0.008221599412004822 0.008663431827887202 -0.052110877220019336; 0.009060308762372264 0.010284453943226942 -0.061018073561807364; 0.01977622614952428 0.029424759505499536 -0.16738449761941362; 0.00028951666628483744 0.00035833633735557425 -0.004100014356031375; 0.004985164232955772 0.005559610429141295 -0.04209859415760405; 0.0003692874431784142 0.0010666965101844813 -0.005621285704794943; 0.0004727612219399227 0.000405901440234659 -0.0023431994399422964; 0.000241155842199701 0.0005681038339042067 -0.0012478538213502837; -0.0007603707045190696 -0.0016343484283774848 -0.0005757457165778959; -0.0017318239806693933 -0.0008235537175067503 -0.0024367232782154195; 0.0018678927414909588 -0.00018633023010451263 0.0004745721477326841; 4.386805267878415e-5 -1.7327639837385798e-5 -0.00020758059517948942; -9.534805504982156e-5 0.0002909328518857894 0.0026540713764775644] %
+
+Mass Used: 100.21492653002997 kg
+Launch C3: 95.99808006429465 km²/s²
+||V∞_in||: 0.014098577296827772 km/s
diff --git a/archive/ES_0.5658972426706004 b/archive/ES_0.5658972426706004
new file mode 100644
index 0000000..ea4c5df
--- /dev/null
+++ b/archive/ES_0.5658972426706004
@@ -0,0 +1,22 @@
+archive/ES_0.5658972426706004---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T18:42:02.359
+Launch V∞: [7.8553232824295876, -5.9665855512095245, 0.2238087773225407] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7152808335520007e-9, 3.7301906167482073e-10, -2.4667343973613663e-10] km/s
+ V∞_out: [1.1147050397267336e-9, -1.025777955974556e-9, -8.425686417853359e-10] km/s
+ time of flight: 1.8561137860938823e8 seconds
+ arrival date: 2030-04-04T01:25:00.359
+ thrust profile: [0.33258280580026234 -0.017007790786879414 -0.09812589555510388; 0.027261841761143435 0.01366198938698264 -0.030036125735742658; 0.07518712043313905 0.05671089079421305 -0.1440447813647325; 0.024490740887069998 0.027632209687936914 -0.08339478444696485; 0.017136214230039394 0.024623741612814446 -0.08187829361278445; 0.025642196955417314 0.04222030177262362 -0.15767691833943254; 0.006028095678450212 0.012939619778639194 -0.055146364423123685; 0.004811197522729205 0.012776833176922311 -0.04814776864805692; 0.0034800472165802216 0.009470369590946902 -0.045621636893927286; 0.0031309653005505244 0.006239317905712729 -0.027276704127085265; 0.005417263026024088 0.007979457067343118 -0.03871340420967351; 0.0013632600953432416 -0.00014709872846343478 -0.005458994053172038; -0.0030098908583941495 0.006441056105357738 -0.000321372412327194; 0.004706677060195712 -0.002127615141053095 0.006627239018211522; -0.01155399199955304 -0.010622216715312244 0.0014588245808482073; -0.0002702380774045171 -0.019674957027238645 0.0005530576550341663; -0.0010310352159706867 -0.0013986856839811894 0.0061480178401343765; 0.0020934806075177627 0.015954486073465002 -0.008692172246922742; -0.015591653349191673 0.004963672404545424 -0.008309711043314487; 0.002313689037206252 0.011390706689422068 -0.018365665499068096] %
+
+Mass Used: 92.30148173126327 kg
+Launch C3: 97.35633738018923 km²/s²
+||V∞_in||: 1.772619345543444e-9 km/s
diff --git a/archive/ES_0.5659004657678063 b/archive/ES_0.5659004657678063
new file mode 100644
index 0000000..9cbb45d
--- /dev/null
+++ b/archive/ES_0.5659004657678063
@@ -0,0 +1,22 @@
+archive/ES_0.5659004657678063---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T11:05:53.999
+Launch V∞: [6.329583756949594, -7.343839193818359, 0.12193457054396142] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.6103217850726247e-7, -7.929224432336087e-8, 1.008063975436148e-7] km/s
+ V∞_out: [-3.7746082231336006e-7, 3.38230628615429e-8, -4.870331248035376e-8] km/s
+ time of flight: 1.855897541988334e8 seconds
+ arrival date: 2029-03-16T11:48:27.999
+ thrust profile: [0.5100142170924019 -0.12671791947305108 -0.14956292277917516; 0.10259295191925687 0.03191243953798148 -0.0997772042469217; 0.040903791908725826 0.026156928795549633 -0.07140410573266817; 0.03623019920034946 0.030216176832335608 -0.0865856342864938; 0.0780011184272211 0.06911165862190564 -0.21636807950740453; 0.021081629996324854 0.027526176734413096 -0.0849634392542505; 0.014365967983917502 0.01781881714858471 -0.07286634026119973; 0.007202474165715162 0.008331377800448628 -0.035216796709588306; 0.011637454090727938 0.012049190706501728 -0.057327443936936305; 0.007953995781026105 0.009915614297201171 -0.04697432976263949; 0.0015250393206034006 0.001441677263938496 -0.0077168787393373205; 0.0004816448529322344 -0.000420120659447595 -0.004824459402278755; 0.0010000381838058494 0.005030841506464517 -0.001378068236668261; 0.0004225803691851474 0.003545320700034086 -0.008832428324037753; -0.0008476754004438868 -0.0024099333482193786 -0.003235175335452723; 0.002053853505114232 -0.0016814436956492395 0.010967264316681819; 0.0014479985685253946 0.0030546160116196428 -0.01631447824022901; 0.001032149047349065 0.0036774709699410515 -0.012168532938361558; -0.00034188587383355174 0.002365626420146341 -0.004455627292661393; -0.003273513432437732 0.002309858889363173 0.00042601256428412976] %
+
+Mass Used: 111.82278609346076 kg
+Launch C3: 94.01047268039656 km²/s²
+||V∞_in||: 3.8313629913290217e-7 km/s
diff --git a/archive/ES_0.5659041568078296 b/archive/ES_0.5659041568078296
new file mode 100644
index 0000000..6d5dd9d
--- /dev/null
+++ b/archive/ES_0.5659041568078296
@@ -0,0 +1,22 @@
+archive/ES_0.5659041568078296---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T17:51:33.382
+Launch V∞: [6.43125043625115, -7.58828695454113, 0.11721480709273929] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7166956724729687e-7, 2.662520520431943e-7, 1.1904995396573884e-7] km/s
+ V∞_out: [-1.1062660289110939e-7, 1.7622109420577238e-7, -2.6693336620020074e-7] km/s
+ time of flight: 1.7893493002431187e8 seconds
+ arrival date: 2028-12-30T18:00:23.382
+ thrust profile: [0.14302421116978228 -0.055167842162167656 -0.06212025893174362; 0.06127350485403113 0.003908607898392189 -0.08105616611536931; 0.05380506283444214 0.013430331961601436 -0.11790194114613249; 0.05058444207166749 0.01655050741089431 -0.1522197303838372; 0.042401711409545996 0.015928886590668604 -0.16051639462968365; 0.03284163633378986 0.013521272072153302 -0.1487393349276746; 0.024623058197911205 0.010792291367551082 -0.12902062254279464; 0.011962453943973803 0.006475465647966654 -0.0724170534021706; 0.0028256083389771912 0.0010137629006509055 -0.019415307542193325; 0.0010191089244369442 0.0003251651252471835 -0.006183164421446544; 0.0011588090660321511 -0.0016254474121369742 -0.005282292274754323; 0.0009747557709993061 0.0023290716593621025 -0.0021356328149787665; -0.0005425545724057345 0.002046858427265405 -0.004435629225303063; -9.664911823849873e-5 0.00040405705417853187 0.0018221817358788789; 0.00033485669541471054 -0.0026165331453363587 0.005688914620183668; 0.00023036545789155628 -0.00032437851435965464 0.0043520688333062146; -0.0006377639059720924 0.0003706197735926087 0.003994947956339173; 0.00122996684430388 -0.0012684775241735544 0.010386684413256068; -0.00019743793300212734 0.0006476185226162194 -0.007169427319790688; -0.002736892497349009 -0.0014140440555920743 -0.005856617092636379] %
+
+Mass Used: 82.97339733855915 kg
+Launch C3: 98.9568203892415 km²/s²
+||V∞_in||: 3.384279643813888e-7 km/s
diff --git a/archive/ES_0.5659108989065487 b/archive/ES_0.5659108989065487
new file mode 100644
index 0000000..4a31851
--- /dev/null
+++ b/archive/ES_0.5659108989065487
@@ -0,0 +1,22 @@
+archive/ES_0.5659108989065487---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T02:07:47.703
+Launch V∞: [6.130573024275095, -7.845552621377055, -0.0784052096622607] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.191062965339578e-9, -1.8046421126041933e-9, 8.544374173151941e-10] km/s
+ V∞_out: [-2.7984497927319573e-10, -1.7442711188519315e-9, -2.4951158685662304e-9] km/s
+ time of flight: 1.7694476176972374e8 seconds
+ arrival date: 2028-12-09T01:27:08.703
+ thrust profile: [0.10818507486569905 -0.03809316479708489 -0.043720791485564896; 0.10307778492726181 0.01352557740931132 -0.11731586707681559; 0.06195263594655784 0.019949952728823054 -0.11662381587940501; 0.05297869602816711 0.02353476513691385 -0.13843890419234145; 0.061298622311652916 0.033057676118460576 -0.2013002559070188; 0.019673451178396344 0.011633483438533977 -0.07711606875839097; 0.037698609678500486 0.02458703188352249 -0.171274109502593; 0.008147490165463006 0.006282353098485129 -0.040332080263287634; 0.0005720174783977606 -0.000837833410127161 -0.008638688969456245; 0.00020312422519466159 0.0039825108814279826 -0.008420668113839149; 0.0031950133147769675 0.0051422035695298015 -0.027934732659926506; 0.002145191677209643 0.0018566753790509485 -0.014866560513057415; 8.147160141281024e-5 -4.6912422321934016e-5 -0.003482804450103539; 0.0015955819342073092 0.001353568115889105 -0.006053705227419227; 0.000357106489459012 0.0015212847390728198 -0.005306730644261629; 0.002837240898201708 0.001480119771185666 -0.0035315089235800562; -0.0012691834599596586 -0.0014693255592946844 -0.001612331148765286; 0.0006302200569341903 0.00015539312106710793 -0.0002615899074700865; 0.00022394527057350623 0.00027833650250818666 -0.0015121383190778333; 0.0002005126026011451 0.00015530593762424615 -0.0002563893422634746] %
+
+Mass Used: 81.89656337124325 kg
+Launch C3: 99.14276891766805 km²/s²
+||V∞_in||: 2.3249575140411264e-9 km/s
diff --git a/archive/ES_0.5659140252585807 b/archive/ES_0.5659140252585807
new file mode 100644
index 0000000..b8babdf
--- /dev/null
+++ b/archive/ES_0.5659140252585807
@@ -0,0 +1,22 @@
+archive/ES_0.5659140252585807---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T13:36:44.247
+Launch V∞: [6.5460223314999455, -7.38438458498507, 0.1878565284740245] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.693654683621254e-8, -1.9914233481258416e-8, 2.5296075183256148e-8] km/s
+ V∞_out: [-8.34165389490077e-8, 1.5537960158691845e-8, -7.074478861440923e-9] km/s
+ time of flight: 1.8749577787430903e8 seconds
+ arrival date: 2029-04-09T15:46:21.247
+ thrust profile: [0.22974702814780879 -0.05644635167211078 -0.08227603934389849; 0.1022823089390459 0.02781961888751792 -0.11136410412207483; 0.06230109855018473 0.03231852350108511 -0.11404618755842945; 0.0535035964080807 0.03698543727296956 -0.13773847580306492; 0.03673396833253616 0.0304498281832083 -0.12146843488766774; 0.02107622174011749 0.019726506595292924 -0.08463257232991189; 0.017380208503318062 0.01807462034876734 -0.08223587044854976; 0.015832896222644947 0.01829054188766135 -0.08639341297005573; 0.005354782697870311 0.005960289792503243 -0.03220075231037639; 0.0012376341869145128 1.8204078008595206e-5 -0.006422854452371796; 0.0025726302425507375 0.0003397961835542411 -0.011111132970333303; 0.0002764689419183325 0.0002904181374360411 -0.0038020663396039272; 0.002788276172997795 -0.0006395273559553176 -0.004545027647636247; 0.007362108415962666 0.006913626973692633 -0.005135109855898966; 0.0011587047940113113 -0.0004186838867108616 -0.015818628714621665; -0.0005588923824944746 0.007468497562882289 0.005848705794267303; 0.00026518388783734016 0.0007507076827523853 0.005209398338465482; 0.0012236927412249514 -0.009851311457609079 -0.014209137254079355; 0.0067812570437621325 -0.0011265173724403015 -0.000890451858800918; 0.009673240853597512 0.006369721540080987 -0.015518432946638572] %
+
+Mass Used: 91.97983032562752 kg
+Launch C3: 97.41483413875142 km²/s²
+||V∞_in||: 9.270615562425182e-8 km/s
diff --git a/archive/ES_0.5659224076844829 b/archive/ES_0.5659224076844829
new file mode 100644
index 0000000..cf05511
--- /dev/null
+++ b/archive/ES_0.5659224076844829
@@ -0,0 +1,22 @@
+archive/ES_0.5659224076844829---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T19:59:52.930
+Launch V∞: [6.504422462410621, -7.2340439974288815, 0.19259615573606936] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3249688278743684e-7, -2.9656729351129526e-8, 3.965809815195607e-8] km/s
+ V∞_out: [-1.40498662149804e-7, 1.3434040357796125e-8, -1.717311594656106e-8] km/s
+ time of flight: 1.87495777872304e8 seconds
+ arrival date: 2029-04-06T22:09:29.930
+ thrust profile: [0.42709067360138175 -0.10333070219192061 -0.13584301173391677; 0.1472135356342259 0.045029734105446646 -0.1469177998837353; 0.08843712348998209 0.051849118092276776 -0.15107215800894558; 0.05054975471141392 0.04014509148034922 -0.12438097020096321; 0.034283931453949666 0.033454434633912164 -0.11047240545038607; 0.020271159695815884 0.023238859639150473 -0.08227954346399312; 0.009302320312982395 0.01151570407096397 -0.04523689758623475; 0.008990771425044106 0.010245427289152422 -0.03891799164100216; 0.009316843438649317 0.013931456226888905 -0.05606149790150922; 0.0016032422989245253 0.00430122191645468 -0.019291820677925554; 0.0014103288234087786 0.0010134926150473914 -0.009934596838630936; 0.001849356218270541 0.0005916280223453724 -0.006756871063707644; 0.0005122462369005817 0.0011075704456461088 -0.007765973459191602; -0.0017183193861122058 -3.853582888104279e-5 -0.00023844422600181794; -0.00035446765694699726 2.3669082829908873e-5 0.0019019326123691652; -0.005254732528033311 0.004770051251944549 -0.0003797276337921202; -0.0015204504761837613 -0.0005544265310773958 0.0015306834762304116; -0.021768221262947418 0.005859017543204819 -0.011230769924429241; -0.008728423378135924 0.0042157540938566294 -0.004795726051975332; -0.0004518409331381672 -0.0001645604002623877 0.0011501703606996822] %
+
+Mass Used: 107.9661574334209 kg
+Launch C3: 94.67599740545299 km²/s²
+||V∞_in||: 1.414486136136516e-7 km/s
diff --git a/archive/ES_0.5659236569157846 b/archive/ES_0.5659236569157846
new file mode 100644
index 0000000..2c4addc
--- /dev/null
+++ b/archive/ES_0.5659236569157846
@@ -0,0 +1,22 @@
+archive/ES_0.5659236569157846---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T14:32:19.812
+Launch V∞: [6.5411193648200205, -7.358795650596363, 0.10265355881209069] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1696841063020184e-6, 0.0003677148753489316, -0.00024785229251054417] km/s
+ V∞_out: [-0.00020364494980026196, -0.00038564501686629124, 8.02251552221582e-5] km/s
+ time of flight: 1.8749577787493983e8 seconds
+ arrival date: 2029-04-08T16:41:56.812
+ thrust profile: [0.24799511465417934 -0.05649944828897732 -0.09124680590280715; 0.09643074078526176 0.030234523071305013 -0.09939027298402754; 0.0819537529462533 0.04890737572756142 -0.14246929578007833; 0.0659380208189583 0.05301146409985279 -0.1613929631464937; 0.04176670964762573 0.04106491296454309 -0.13277921839589285; 0.029270753626931174 0.03386054202064786 -0.11637465742717219; 0.015064099285071922 0.019628976659747086 -0.07220740503177289; 0.0034183043202595377 0.004845718210281688 -0.01893113799454484; 0.003434654768150598 0.005862079079373046 -0.02480004313037936; 0.0025565212796579786 0.004797962386918241 -0.020514981339160458; 0.0006810719559125645 0.002502026207843657 -0.007627458072366053; 0.0005138853898889134 0.004063056697707298 -0.00529016239381354; 0.002633776443080324 0.0007982701659196486 0.0019769723610475855; -0.0055316226457146475 -0.001654467492424273 0.002436794003257385; -0.0020424390103844885 -0.007976017752851065 0.004913675045593411; 0.0009849060767746416 0.000832154817202341 0.001134394264803209; 0.001617323773723062 0.0043902459657809 -0.019070666740103843; -0.0004088478549392412 -0.0004033851856402769 -0.001724056003503414; -0.013142198578931275 -0.002945536803385282 0.006693025197439241; 0.014958832646291166 -0.00876339538359375 -0.003976290185036584] %
+
+Mass Used: 94.7104530047709 kg
+Launch C3: 96.94865372519621 km²/s²
+||V∞_in||: 0.00044344825697765594 km/s
diff --git a/archive/ES_0.5659488360280694 b/archive/ES_0.5659488360280694
new file mode 100644
index 0000000..cfe57a4
--- /dev/null
+++ b/archive/ES_0.5659488360280694
@@ -0,0 +1,22 @@
+archive/ES_0.5659488360280694---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T15:45:28.690
+Launch V∞: [5.946265450602775, -7.7474446739309455, -0.0711347186894537] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3798570481583242e-6, 8.504332138407613e-7, -5.807513337653145e-7] km/s
+ V∞_out: [5.448589006932714e-7, -1.4126352044374185e-6, 8.22213006100327e-7] km/s
+ time of flight: 1.7526216651003823e8 seconds
+ arrival date: 2028-11-16T03:41:34.690
+ thrust profile: [0.29297537894634146 -0.09281128106159567 -0.09384170662949991; 0.19025273728162534 0.04088716069492528 -0.16750180609225132; 0.06837369742232989 0.03348006028996877 -0.11107883302498547; 0.13309379362190404 0.07984539414466627 -0.2532592944619155; 0.05012097829035004 0.04371934240477823 -0.13701036066819633; 0.026532135258729026 0.028452784974754296 -0.09769187057053677; 0.012449089035895486 0.014211201658781515 -0.05249946682107497; 0.005290294064775033 0.006380353624740617 -0.024819376956511846; 0.007283097630570064 0.010624882058614978 -0.040063899815661046; 0.004040010594002796 0.006201594695101979 -0.030375027286905602; 0.004735483318451068 0.006364819941633256 -0.020760346631483535; 0.0024158681149401237 0.004713097835301739 -0.01878071538839702; -0.00014456864393412746 -0.0006456258569168887 -0.0012345552776847307; 0.002160658101146403 0.0026444098813038865 0.0019980621501410256; 0.00019201746635779922 -0.0013801123439986407 -0.0011213959088262795; -0.0004252556897708275 -0.0005788659889627102 -0.0005216687480924748; -0.00012183967892510558 -0.0014039164707445049 0.002945092876216395; -0.00032185799424818686 0.0004252988236958686 -0.0044947101140329175; -0.0018730125486337151 -0.0030919927466189004 0.0017333695308270987; -0.0038031249743246337 -0.0001181075920755096 -0.0013365453739578026] %
+
+Mass Used: 103.85512242441973 kg
+Launch C3: 95.38603193285623 km²/s²
+||V∞_in||: 1.7217764768476544e-6 km/s
diff --git a/archive/ES_0.5659490205966428 b/archive/ES_0.5659490205966428
new file mode 100644
index 0000000..c26df21
--- /dev/null
+++ b/archive/ES_0.5659490205966428
@@ -0,0 +1,22 @@
+archive/ES_0.5659490205966428---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T07:56:45.430
+Launch V∞: [6.484888787817479, -7.585880930631674, -0.013332945485813204] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008098047640822907, 2.4268843773522334e-5, -0.0005434783629418015] km/s
+ V∞_out: [0.0009407890247794269, -9.306384762039548e-6, -0.00026578183500946043] km/s
+ time of flight: 1.8498092762724146e8 seconds
+ arrival date: 2029-03-13T07:32:12.430
+ thrust profile: [0.09521898447069935 -0.02700609570047487 -0.03939114607798364; 0.06446324109938113 0.013307454862666835 -0.07780078355356908; 0.05252628255184287 0.022176276509600305 -0.1086158880418635; 0.05077206010934356 0.028811136301424897 -0.1475116165229817; 0.04552881663781015 0.03087978008836202 -0.1695671120255805; 0.026478312273640822 0.020176024810501056 -0.11981509886355723; 0.011183291192899366 0.009481349874738575 -0.058464299396432745; 0.012545635816015439 0.012061291484121687 -0.07655194444020336; 0.0045066620808327275 0.004455826091148459 -0.02978183219791985; 0.003823211925885003 0.004124805767350693 -0.028745473442608454; 0.0013061447244675718 0.0019598034123391008 -0.0111756172656543; 0.0005010433002729953 -0.004372842920280104 -0.0051994109961158354; 0.007537134770083194 -0.0010730854677208652 -0.00580367334398617; 0.002635311860716442 -0.003844969819336397 -0.005347207732085191; -0.002607917808632585 0.0005702887130985555 0.003664673929084688; -0.0009816549629051165 0.003006340991372875 0.004520263902927848; 0.0006271503178208451 0.0008245052860493731 -0.009173031208433716; 0.010873900893469627 -0.0014320627459074554 -0.009176586023710376; -0.003789396239700163 -0.009093226007011672 -0.004433457998276714; -0.0029454076200506737 -0.001265268405501035 0.005199053047921969] %
+
+Mass Used: 79.27648322889809 kg
+Launch C3: 99.59954985151745 km²/s²
+||V∞_in||: 0.0009755723774761044 km/s
diff --git a/archive/ES_0.5659571622310493 b/archive/ES_0.5659571622310493
new file mode 100644
index 0000000..7b9371d
--- /dev/null
+++ b/archive/ES_0.5659571622310493
@@ -0,0 +1,22 @@
+archive/ES_0.5659571622310493---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T16:45:14.708
+Launch V∞: [6.679159147649568, -7.28681298154192, -0.8099525829590362] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.392371600176348e-6, -1.1694917955953718e-6, 2.5881590434474236e-8] km/s
+ V∞_out: [1.7942489440357914e-6, -4.228735485768458e-8, -9.290141881706471e-6] km/s
+ time of flight: 1.8749577781853852e8 seconds
+ arrival date: 2029-04-08T18:54:51.708
+ thrust profile: [0.23071844140599743 -0.05571685203570931 -0.08966839777138122; 0.04976377905372631 0.012106156198452745 -0.06099363246045732; 0.06488739107217885 0.034450667468778264 -0.13816292404428304; 0.05692415221752544 0.04234479998955754 -0.1662099732174803; 0.0335335071668874 0.028755768870682617 -0.13236370936132794; 0.02691908098655754 0.026583643486513292 -0.1308206411783683; 0.016236630841104938 0.01594064050149878 -0.0913757582365542; 0.006885611421372917 0.0072155161709772184 -0.041932965048359645; 0.005208363191779326 0.005941408168456387 -0.0361241886549585; 0.001195513187137846 0.0017737224526070158 -0.010650769438351202; 0.00020639143645764238 0.0010362794689476728 -0.0044468563536458556; 0.0003787642192352137 0.0006260433040944247 -0.003337875215551959; -0.0003058185010441014 0.0004703016502724582 -0.0023357244883228778; 0.0004117741748335805 -0.0012089947558328548 -0.0024766810037341047; -0.00042384544135073087 0.0007411983356575961 -0.002769595269893111; 0.00021293261587721445 -0.0002487587243250176 -0.000642332053974588; -0.0017863632701545437 0.001623956590920406 -0.001609278902401771; -0.0008632075731823472 0.0007941224536369214 0.0019272500859150144; -0.0021711430133162244 0.0015438818700871859 -0.002849732896882632; 0.0010975021760223948 -0.0003049962711056996 -0.0003509497601108865] %
+
+Mass Used: 86.488493653153 kg
+Launch C3: 98.36483353424077 km²/s²
+||V∞_in||: 9.464936618514014e-6 km/s
diff --git a/archive/ES_0.5659616992187686 b/archive/ES_0.5659616992187686
new file mode 100644
index 0000000..f999653
--- /dev/null
+++ b/archive/ES_0.5659616992187686
@@ -0,0 +1,22 @@
+archive/ES_0.5659616992187686---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T20:06:22.421
+Launch V∞: [6.2523364627749, -7.453126204570807, 0.2364402700131118] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.279827467862791e-6, 7.273802659129228e-7, -1.5552848497023665e-8] km/s
+ V∞_out: [-9.001780124609786e-7, 2.0367396041253674e-8, 5.2542551388134146e-6] km/s
+ time of flight: 1.874957778748782e8 seconds
+ arrival date: 2029-04-09T22:15:59.421
+ thrust profile: [0.45987867536671934 -0.11703437327531373 -0.12791660660346366; 0.09154217368775887 0.031230266164097787 -0.093185084549393; 0.06207019904587624 0.0374935697298386 -0.10301518237398888; 0.04171001150778752 0.03302258195423778 -0.09786739975457995; 0.04188059926813727 0.04306386402038405 -0.12763937606197692; 0.01967231999647512 0.022720534872670266 -0.07539929451014235; 0.018033749334838745 0.022943503534087622 -0.0796910601694187; 0.021106786570053427 0.029731025796751392 -0.10638613593402255; 0.012454277836282012 0.016628223540396163 -0.06539426138801843; 0.004525407520298864 0.006091404758499271 -0.02660602580901665; 0.002486769825443635 0.0034198749069012007 -0.015421617452366324; -0.001087100939971831 0.002018512802782847 0.001622128043230473; 9.486632743593927e-5 0.00395311063940249 0.001965960359041909; -0.0053276850742467186 -0.005008025226022724 -0.0006874849063943909; -0.0006753838413991221 0.0036014295722946515 0.004312618539911094; -0.00016220938127579118 0.00034960143688025566 -0.0018924524337410476; 0.0009972891287247433 0.0019134639114107084 0.0014613319898753889; 0.0019022086522822916 -0.0021860232182501485 0.005868055938000942; -0.012193624069984102 -0.0009260658199413751 0.001961460767681026; -0.005583493699401369 6.160258886128833e-5 -0.0031937564415524654] %
+
+Mass Used: 107.89120053521401 kg
+Launch C3: 94.69670546628846 km²/s²
+||V∞_in||: 5.329718757376821e-6 km/s
diff --git a/archive/ES_0.5659639034528638 b/archive/ES_0.5659639034528638
new file mode 100644
index 0000000..f090fc9
--- /dev/null
+++ b/archive/ES_0.5659639034528638
@@ -0,0 +1,22 @@
+archive/ES_0.5659639034528638---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T17:43:41.105
+Launch V∞: [6.410067549172536, -7.527963943931262, 0.10393551798313128] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6241854735980042e-7, -3.740007443955464e-8, 4.611752909552742e-8] km/s
+ V∞_out: [-1.7167525804886826e-7, 1.523863572975376e-8, -1.9733634881912122e-8] km/s
+ time of flight: 1.8170941338103545e8 seconds
+ arrival date: 2029-01-31T20:33:54.105
+ thrust profile: [0.22307114643813314 -0.06557321990671544 -0.08930628668452312; 0.07979749435704082 0.016476285091181698 -0.09455867947969641; 0.058196564503200356 0.024824375641892295 -0.11411098625019322; 0.0454962753924272 0.02503474571668455 -0.12078156450296705; 0.028260524915196466 0.019558368816259983 -0.09832086035049867; 0.02669326919809466 0.021463893421631203 -0.11567309999890324; 0.022468037056595676 0.019101593378872114 -0.1130974593835499; 0.015447010203059323 0.014095020319659285 -0.08716060546241935; 0.009506418486561221 0.008075714918291375 -0.05452827528934427; 0.006778890165691336 0.0065965161474652225 -0.04387767383540514; -0.001748012557185031 0.003535645141634554 -0.009802096412068492; 0.001324404958492985 0.0024614090281431552 -0.0026680324588984187; -0.002162713501870916 0.006057765631267975 -0.002777196704240032; 0.004210106407836105 0.0012603442354304365 0.00039071218673789303; 0.0038478052900666735 -0.00435050037726085 -0.007322651879864938; 0.002685401036645695 -0.009488971344178993 -0.00264844782260583; 2.7234176741928063e-6 -0.00736909277113681 -0.007579327378387393; -0.0012713153229891797 -0.004400955633192849 -0.010833063768307912; -0.0026874443306566216 -0.0005712638664248334 0.003771797363364769; 0.002690679482705986 -0.0008584704830910848 -0.0010837458822394682] %
+
+Mass Used: 89.96616400677749 kg
+Launch C3: 97.77000971798233 km²/s²
+||V∞_in||: 1.7293171075435752e-7 km/s
diff --git a/archive/ES_0.5659641173438936 b/archive/ES_0.5659641173438936
new file mode 100644
index 0000000..de4d699
--- /dev/null
+++ b/archive/ES_0.5659641173438936
@@ -0,0 +1,22 @@
+archive/ES_0.5659641173438936---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T01:55:34.619
+Launch V∞: [6.333212594488109, -7.3578482257138935, 0.20273296466855012] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3236314645993902e-7, 6.08386309045142e-8, -7.824809951252595e-8] km/s
+ V∞_out: [2.411549676451983e-7, -6.913104152597516e-8, 3.13540380054311e-8] km/s
+ time of flight: 1.8051702081707662e8 seconds
+ arrival date: 2029-01-13T09:32:34.619
+ thrust profile: [0.41620853880114883 -0.12437652499026224 -0.12865094838231647; 0.19183895858180963 0.04918705506691091 -0.17280549832047493; 0.10847640750532445 0.05725491005932936 -0.16356982869434342; 0.08421537199601006 0.06108849156890887 -0.17703129466105474; 0.045644720775426625 0.040732607116574594 -0.12461216827714201; 0.017311277503077076 0.017819853170923668 -0.06096101118265568; 0.012755688476790492 0.015731112531103108 -0.05481031235847792; 0.00640384336290043 0.008192124456749512 -0.02891902957266071; 0.01065172582077473 0.012770022502226409 -0.0514397450516193; 0.003683802998765957 0.004021215089371283 -0.01912430604942471; 0.0007750792640926075 0.0010600230483869724 -0.0032415414195265555; 0.001010542507493635 0.0037884464514370887 -0.01477052444116238; 0.0016000318133794257 0.0026041444073963966 -0.009994166280476858; 0.0012834256958305138 0.0003236219273262094 -0.0011757878005275461; -0.00048065164901879467 0.00019650329064073413 -0.0019096658579904704; 0.0004939973083485823 -0.0002624478962340856 -0.0007959828033684722; -0.0005849800205631955 0.0015140239374241214 0.000316673916993052; 0.00051368704154489 -0.0006372183472481677 -0.0002606269879896609; 0.001110226170378595 0.0019699249901026722 -0.0006998141870133703; -0.0015780656788061057 0.00031171222211786307 0.0009708267623883451] %
+
+Mass Used: 110.27456144945063 kg
+Launch C3: 94.28861293458719 km²/s²
+||V∞_in||: 2.526197457057167e-7 km/s
diff --git a/archive/ES_0.5659730781416151 b/archive/ES_0.5659730781416151
new file mode 100644
index 0000000..93d30c8
--- /dev/null
+++ b/archive/ES_0.5659730781416151
@@ -0,0 +1,22 @@
+archive/ES_0.5659730781416151---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:02:11.954
+Launch V∞: [7.916132094858807, -5.685715285599215, 0.24376660381427553] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.24199130012274e-9, 1.372690815515381e-9, -1.0767404745343922e-10] km/s
+ V∞_out: [2.4837000117661835e-9, -2.2620152878948344e-9, 8.247421727497386e-10] km/s
+ time of flight: 1.8198374588888234e8 seconds
+ arrival date: 2030-02-15T13:04:36.954
+ thrust profile: [0.48690121272446324 -0.02100234200636976 -0.15406366884125053; 0.05238227230346276 0.026675513553721757 -0.057933847768207654; 0.04945865366157005 0.04081082599489888 -0.09690366550712479; 0.05067799450490903 0.05590866834798164 -0.14722051505483133; 0.027071022017260866 0.03630128538253185 -0.10494063175454245; 0.015472223930210346 0.027046000345925688 -0.0781159085509268; 0.013801004190942696 0.024078964291862896 -0.0776520390801511; 0.0061975560448757055 0.00970933682713462 -0.03356079750465903; 0.012026267497748185 0.025612129603139345 -0.09711933793956161; 0.005723640676400638 0.007152892685466868 -0.01986551658123674; 0.0011741078349604371 0.005625812500469746 -0.009437303162856254; -0.000537604136807061 0.0015968880329451582 -0.011558004749828026; -0.0003744019316171657 0.0018617953368346637 -0.005574915080501617; -0.0078099068146616 0.003306175134953941 -0.008066156440445275; 5.603000640503567e-5 0.001060554611423159 -0.0003085576711726639; -6.913300588770556e-5 -0.0012038126873471868 -0.0019377922710213148; -0.0020380897083313305 -0.0214891201593376 0.010480942806376077; 0.006838259651831341 -0.040361910708524594 0.027821529615378853; 0.014238782059780998 0.005045732349797715 0.010942499559487204; 0.001487335495343755 -0.005860889786110301 -0.007910578012327849] %
+
+Mass Used: 105.83234561105292 kg
+Launch C3: 95.05192780928539 km²/s²
+||V∞_in||: 2.6310451849638277e-9 km/s
diff --git a/archive/ES_0.5660011176894992 b/archive/ES_0.5660011176894992
new file mode 100644
index 0000000..febca0f
--- /dev/null
+++ b/archive/ES_0.5660011176894992
@@ -0,0 +1,22 @@
+archive/ES_0.5660011176894992---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T04:26:56.639
+Launch V∞: [6.430678277040496, -7.44586712944434, 0.1769998828660056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4776228511540354e-9, 7.268136912205279e-10, 7.1965294851058045e-9] km/s
+ V∞_out: [-4.257084298666022e-9, -6.133864897111299e-9, -3.0610042229022015e-9] km/s
+ time of flight: 1.874957778748327e8 seconds
+ arrival date: 2029-04-10T06:36:33.639
+ thrust profile: [0.2655842308672802 -0.06705542759859419 -0.08676762856388981; 0.12442585358233525 0.03178431920232737 -0.12767461415432593; 0.07161507479449973 0.034100167450830686 -0.1268724872841189; 0.05186908270592546 0.036765312183463066 -0.14115050526192482; 0.025085843803501113 0.025271878748356336 -0.09342770886404897; 0.02608890938046651 0.01938944611825427 -0.0946779166871073; 0.016248934268673663 0.013714392764858498 -0.07586960359297676; 0.009055146579338567 0.01387007266014122 -0.059060612002107035; 0.0034482809933668924 0.00825368931286756 -0.03289023723867097; 0.00441106517211797 0.008418851484531188 -0.02590353813149351; -0.0017502784342067835 0.004085718562451357 -0.012124937396486355; -0.0015223730208785485 0.0006948088698243145 -0.008708649698643873; 0.0010987649956288033 0.0004842520347809814 -0.0024630728080704757; 0.0006528369231789613 0.003808472312643872 -0.00858976544592779; -6.749630679824095e-5 0.00822961087583204 8.21834966145598e-6; 0.010285448842540904 -0.00977577845690953 -0.006970890239018796; -0.0007498143611177881 -0.0006494052419052483 -0.0023255197856101345; 0.014964231924083894 0.0059695533970640065 -0.005811693145047131; -0.0076943227753059765 0.0017910354088279618 -0.018309575240534726; 0.0014982808424096835 -0.000803052993528189 -0.006839102303695035] %
+
+Mass Used: 95.51694930881285 kg
+Launch C3: 96.82588937067479 km²/s²
+||V∞_in||: 7.382524233756053e-9 km/s
diff --git a/archive/ES_0.5660011207689892 b/archive/ES_0.5660011207689892
new file mode 100644
index 0000000..7408d63
--- /dev/null
+++ b/archive/ES_0.5660011207689892
@@ -0,0 +1,22 @@
+archive/ES_0.5660011207689892---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T07:08:34.158
+Launch V∞: [6.501537383538298, -7.4197925195757755, 0.041065036991692644] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0422234256573307e-8, 3.5214308296578823e-9, -8.66194844993118e-9] km/s
+ V∞_out: [-5.911385008057297e-9, 1.4016906672543952e-8, 1.962150672161094e-8] km/s
+ time of flight: 1.837109635502702e8 seconds
+ arrival date: 2029-02-23T13:57:57.158
+ thrust profile: [0.27920067425127426 -0.07461509467718776 -0.09977703891669445; 0.0634466455641523 0.01590713477738051 -0.07517570232755451; 0.04202695331705649 0.0205899318430081 -0.08167820827242273; 0.03754550857033683 0.024956036245016407 -0.1018258266257134; 0.03091239664787392 0.026397299918153004 -0.1099681252617391; 0.02381785168114747 0.02256911847265503 -0.10119451151107908; 0.02254888342129262 0.02346912893436158 -0.11078691808267206; 0.01888363090311163 0.023231219362321698 -0.10628681270688858; 0.009886705780823 0.01092476051216627 -0.062378832051280045; 0.009364777093676172 0.01223678476395187 -0.06836489051396126; 0.001962622563672428 0.003350282268206919 -0.0187773999658804; 0.000607242316945757 0.000281339554566753 -0.011624420223554262; -0.0008465343549393908 -0.0014674155200320711 0.0013032074199098645; -0.003791866216914294 -0.001515650903189186 -0.0018014080207573045; 0.0009613155196149999 -0.002115429720659457 0.005195872047364819; 0.003939405736001639 0.003891856019037086 0.0010865800918671686; -0.004310425948761385 0.0013300852685443688 0.005313269843317498; -0.0032512814929729775 -0.003151781884735089 -0.002148145014722706; 0.0009411202996119425 0.00288114356842037 0.00660896048911121; 0.002190454640189297 -0.0007218706547260517 0.0024368348887585157] %
+
+Mass Used: 92.60549919504365 kg
+Launch C3: 97.32499572036178 km²/s²
+||V∞_in||: 1.4001885335061857e-8 km/s
diff --git a/archive/ES_0.5660019634303051 b/archive/ES_0.5660019634303051
new file mode 100644
index 0000000..7c05c66
--- /dev/null
+++ b/archive/ES_0.5660019634303051
@@ -0,0 +1,22 @@
+archive/ES_0.5660019634303051---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T02:20:10.985
+Launch V∞: [6.560275199460281, -7.364423529898475, 0.25942027218142005] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.06202074005853e-8, -1.4842308659023527e-7, -6.177884403046169e-8] km/s
+ V∞_out: [4.772727319614134e-8, -9.132641696311789e-8, 1.431947148003023e-7] km/s
+ time of flight: 1.8498287745950192e8 seconds
+ arrival date: 2029-03-08T02:28:07.985
+ thrust profile: [0.18547497153731746 -0.038569314278534245 -0.05634568720106668; 0.1371442579464769 0.050324649636226404 -0.11832010120495115; 0.09178662235019684 0.06253853562477811 -0.13277956299757052; 0.05941952353357243 0.05504789151215934 -0.12314901776234137; 0.04696938147111255 0.0538486243352057 -0.12468128707525118; 0.028942456703810297 0.03884903308888448 -0.09819267014499351; 0.024885051601699716 0.03845965534953155 -0.09734841539219323; 0.015264786304627314 0.026320266286269958 -0.0700976194068775; 0.009410745305801889 0.01793840886804651 -0.049629871764797724; 0.0022226675328817598 0.004526734664723244 -0.01353521353825268; 0.0008904529173864136 0.0024292533741858825 -0.0037772709343026276; -0.00078198452432497 -0.0003312344888832183 -0.0008995111122543321; 0.0001335681567920567 0.0007812855052771388 -0.0025255302663148163; -0.0008617495301028031 0.0021532745568203465 -0.0030718209661278174; 1.2516702456387722e-5 -0.0012009559947035184 -0.001564794685879212; 0.00047805779956579107 -0.0005169443161355495 -0.0018026597058560466; -0.0001760745316985409 -0.0012005442557854187 0.00473988044495319; -0.0019280524430310255 -0.000504371231148983 -0.002252377005447029; 0.0012187741614986345 -0.0014536708355790706 -0.012072234504891758; 0.00035705790121614813 0.003949616631471234 -0.007381115868371152] %
+
+Mass Used: 92.52337026372061 kg
+Launch C3: 97.33924349799462 km²/s²
+||V∞_in||: 1.755939973234116e-7 km/s
diff --git a/archive/ES_0.5660075551503174 b/archive/ES_0.5660075551503174
new file mode 100644
index 0000000..65c55f1
--- /dev/null
+++ b/archive/ES_0.5660075551503174
@@ -0,0 +1,22 @@
+archive/ES_0.5660075551503174---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T17:49:58.216
+Launch V∞: [6.150494773083787, -7.440390944762742, 0.1572204698714536] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.30775879904108e-8, 2.953539588015343e-7, -4.827565372737395e-8] km/s
+ V∞_out: [3.917471281685876e-8, -1.575665449765113e-7, -2.44749525428709e-7] km/s
+ time of flight: 1.8195033305791494e8 seconds
+ arrival date: 2029-01-30T15:35:31.216
+ thrust profile: [0.46292654692544244 -0.10406069932046393 -0.11994511990653171; 0.19346486640277719 0.06823333962802972 -0.155057185295025; 0.11178587781574004 0.07378095465430683 -0.14989011149704565; 0.07522910790048393 0.06900972820262273 -0.14492795911374137; 0.035957311835947296 0.04002592898893629 -0.08949507455892051; 0.04863215811245062 0.06535316897247581 -0.14645020853083726; 0.026479523359213174 0.03966904947163877 -0.09546027443829667; 0.005451448669097577 0.009073558454630934 -0.023840558371856852; 0.006001876140388225 0.01058296748566484 -0.028030557864353146; 0.001592387627793278 0.003594679331690067 -0.009778489912447669; 0.0016781563807158723 0.003819301201307567 -0.011059795203295157; -0.0003499918031584664 0.0002628595972770264 -4.9349682488530715e-5; 0.0009235402113487583 0.0010452998903338908 -0.000962775536463934; -0.0024801487436246603 0.0004412799898935234 -0.002560453493265449; 0.0002766993014303153 0.0007211775901501642 -0.0019392883336688625; 0.0017600550820224671 0.0026035535429000155 0.0014827363665221491; 0.0006259563335653997 -0.0006721058393757721 -0.002980950161918382; 0.0012246467380424256 0.004691812958369578 -0.000799327730868373; -0.00209241223779476 -0.0020948100561672626 0.0035590407249043; -0.0004155861357060851 0.0018394300162679956 0.0021585547546674] %
+
+Mass Used: 116.60127143745785 kg
+Launch C3: 93.21272164078499 km²/s²
+||V∞_in||: 3.0109570994919064e-7 km/s
diff --git a/archive/ES_0.5660398072987904 b/archive/ES_0.5660398072987904
new file mode 100644
index 0000000..b79b6cc
--- /dev/null
+++ b/archive/ES_0.5660398072987904
@@ -0,0 +1,22 @@
+archive/ES_0.5660398072987904---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T11:58:51.992
+Launch V∞: [6.212228112302816, -7.700617981463272, -0.13036561997522786] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.04537284043285304, 0.021379095774815796, -0.050055225631455876] km/s
+ V∞_out: [0.04635589174633903, 0.01936962381411871, 0.04996379392024736] km/s
+ time of flight: 1.753667846059168e8 seconds
+ arrival date: 2028-11-18T04:58:35.992
+ thrust profile: [0.18454273767030166 -0.06719544569335259 -0.07485073530924774; 0.07977978220358221 0.01090391227405699 -0.09162316520585762; 0.07897284662645127 0.027523540840533618 -0.14896310150406225; 0.06807499505745523 0.033048031120114646 -0.17776433850794338; 0.04817881828146205 0.02840451584499776 -0.161904567884673; 0.04266540282466456 0.028350559294482623 -0.16845573223939708; 0.024491283104021308 0.017718117010908255 -0.11344213205132164; 0.006417886692609448 0.005025778016480347 -0.033932420745886; 0.0029795065658164833 0.002167813790911797 -0.015533428953626806; 0.0005946218290970336 0.000419088924298585 -0.003729931475934879; 1.398934594436024e-7 -0.0002483135065424883 -0.0012779454624449833; 0.00033562787743168093 -0.0007807312657173706 -0.0023267347759111253; -0.0006738589469244973 0.000377573581975107 0.00031238371561527023; -0.0003449518628992165 0.0035867820153970796 -2.40577639128096e-5; -0.00232296576787338 0.0013330201916481987 -0.0018431862217315469; -0.010864417823590995 0.0053651912943539415 -0.009710710029941628; 0.0047491498067986325 -0.0006395431494855424 0.005109761784638402; 0.004125367072757439 -0.003938093419896019 -0.01972132966247257; -0.00139094040974771 -0.00545386037191838 -0.002876766219859686; -0.00044243755579424977 -0.0014407004145409407 0.0005971533416533869] %
+
+Mass Used: 89.24807995346646 kg
+Launch C3: 97.9082906105924 km²/s²
+||V∞_in||: 0.07086103300199516 km/s
diff --git a/archive/ES_0.566043731522905 b/archive/ES_0.566043731522905
new file mode 100644
index 0000000..2a2f4ee
--- /dev/null
+++ b/archive/ES_0.566043731522905
@@ -0,0 +1,22 @@
+archive/ES_0.566043731522905---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T18:33:20.094
+Launch V∞: [6.424930682982625, -7.406380366519174, 0.2029471100695017] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.0675842838882234e-9, 5.699536831987342e-10, -6.635534364112722e-9] km/s
+ V∞_out: [-1.8304091985069595e-9, 4.642389937383603e-9, 6.0420631928352915e-9] km/s
+ time of flight: 1.7979749474136555e8 seconds
+ arrival date: 2029-01-05T18:18:14.094
+ thrust profile: [0.3104527769575241 -0.09129145675589743 -0.1057893879344067; 0.12412559657070091 0.032753207736288974 -0.12517619279423786; 0.07894459014536423 0.042653123652442684 -0.1313010972053016; 0.08789070432087973 0.06532214113908928 -0.20525397121913008; 0.04734354790078847 0.042922330066269956 -0.13898426261431113; 0.028691084664659378 0.029487171153658995 -0.10318979924509174; 0.016651024245460725 0.018971212057603284 -0.07140775410693374; 0.005518001607795507 0.00659760139808331 -0.027801529403185154; 0.009616002889416957 0.013089320851813423 -0.05187898661481532; 0.002895715122727706 0.004880307625919285 -0.020584653008895747; -0.00035565212676988726 -1.9207190594243656e-5 -0.0014007933717350078; -0.0006844295029525302 0.000636422656402053 -0.0007246420188503327; 0.0002752023322040784 -0.0005399639008052202 -0.0002687904467753319; -0.001363053401202233 -0.0011918950449429826 -0.00037571635423043134; -0.00016945388144256007 -0.00015876018024997294 0.002027971019962049; -0.004191002053245635 0.0013268107453044535 0.0027294205040520676; 0.0020649099734765942 0.004672243832602707 0.001657416046231543; -0.0008396024932821103 0.0037286765239386115 -0.007393488701321864; 0.0006537486270151865 -0.001706049305261366 0.003917000554279235; 0.00011700335129386508 -0.0006447915575229976 -0.0012811622856553461] %
+
+Mass Used: 99.36123376901833 kg
+Launch C3: 96.17539194417785 km²/s²
+||V∞_in||: 7.803871180692766e-9 km/s
diff --git a/archive/ES_0.56605761728156 b/archive/ES_0.56605761728156
new file mode 100644
index 0000000..fbdd0ad
--- /dev/null
+++ b/archive/ES_0.56605761728156
@@ -0,0 +1,22 @@
+archive/ES_0.56605761728156---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T01:10:21.586
+Launch V∞: [6.088038831097581, -7.696946710907592, -0.00972754117339007] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6131935787592828e-9, 1.0587474108699247e-9, 8.217925591777589e-9] km/s
+ V∞_out: [-4.742705764450041e-9, -6.704916410239157e-9, -3.4685172105711414e-9] km/s
+ time of flight: 1.7043954565989184e8 seconds
+ arrival date: 2028-09-18T17:29:26.586
+ thrust profile: [0.22316444542980798 -0.0844270234891961 -0.08328117537557841; 0.20315369648885262 0.03187008254973004 -0.20353553159649393; 0.11010365887047295 0.043738476269202686 -0.18203691041410772; 0.0674045851870963 0.03763689672005673 -0.15468717486735248; 0.07922826081760281 0.054737591375053685 -0.22721638974086708; 0.028332760812329088 0.022334272981622546 -0.09930434767981637; 0.021339461799640934 0.018749122713243808 -0.08677618189010446; 0.0046428081429164565 0.004011692493861049 -0.020204285526066998; 0.004194242120680089 0.0044439569125587644 -0.01733950592135909; 0.0020812963148411213 0.003233986064390956 -0.008897030015381922; 0.001938533036020154 0.0012843877973909626 -0.006673318150994284; 0.0014718563015707756 0.001237681248999135 -0.00333043333872786; -0.0004205705757215423 -0.00021213388720619256 -0.001952909197738376; 0.00025659521791435776 -0.0008286541510184389 -0.0018434880482803384; 0.00043172259826722097 0.00030326443486232196 -0.00234634606040495; 0.00028385489895404255 -0.00010678729720297112 -0.001037155492075982; 0.0012530652365340025 -0.0006552802477620568 -0.0004292213544853596; -0.00011268835644659045 0.0007511520249168409 -0.001635410339463783; -0.00025445977948813394 6.814585986248214e-5 0.0015557236180003984; 0.0018171716005289393 0.0030642995621729336 0.002885824141422243] %
+
+Mass Used: 98.6079695518838 kg
+Launch C3: 96.3073001045605 km²/s²
+||V∞_in||: 8.441424088065176e-9 km/s
diff --git a/archive/ES_0.5660588348167352 b/archive/ES_0.5660588348167352
new file mode 100644
index 0000000..8e5830f
--- /dev/null
+++ b/archive/ES_0.5660588348167352
@@ -0,0 +1,22 @@
+archive/ES_0.5660588348167352---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T21:33:18.887
+Launch V∞: [7.496325429766003, -6.498103773291287, -0.02060918738668749] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00042980074797342006, 0.0014716853039217648, 0.0026735191924902608] km/s
+ V∞_out: [0.0027826872159589905, 0.00018659930065729178, -0.001318315340098743] km/s
+ time of flight: 1.682086689639535e8 seconds
+ arrival date: 2029-09-11T18:11:06.887
+ thrust profile: [0.2539410491780876 -0.044835951167716145 -0.10591592934938864; 0.05687540934204202 0.01559385156522943 -0.08079086007184141; 0.056267026738952224 0.026051702145510544 -0.1331967152167943; 0.052875860457715564 0.03028993361752687 -0.17177874012515842; 0.03773468456533306 0.024242083782508365 -0.15872596339529538; 0.020482657083778756 0.014023797049278933 -0.11262493323400552; 0.01337174456321498 0.0084117550540466 -0.08789468407169267; 0.0068709223582206 0.00450661304974736 -0.04506540450404166; 0.005904183001498511 0.004160477730829275 -0.04258329796035061; 0.007990164962112805 0.005843626937803314 -0.06282092414539156; 0.001969789751056217 0.0023903420133941713 -0.025169740639593277; 0.0016275834399453444 0.002069051877578381 -0.001914326096520457; 0.0007164661974863064 -0.0005560538324336957 0.00014946477792918437; 0.001308647610218686 0.003732589383590906 -0.001446165464701726; 0.0006070044825545629 -0.0030351339663161475 -0.002811776479817942; -0.0021304484208278527 0.00025879832970001043 -0.0014073591905254877; -0.0008504483741888129 6.656544188391627e-5 -0.0004101907373118248; 0.00037631314669951774 0.00044844067825883965 -0.0032701099078756794; 0.0027282898049873273 -0.0014457646849317701 0.0007703633354295683; 0.0049359920530449 -0.008715454151790923 0.0011613278834010185] %
+
+Mass Used: 86.28138532605317 kg
+Launch C3: 98.42067233602366 km²/s²
+||V∞_in||: 0.0030819297833259577 km/s
diff --git a/archive/ES_0.5660772771902858 b/archive/ES_0.5660772771902858
new file mode 100644
index 0000000..f8b504c
--- /dev/null
+++ b/archive/ES_0.5660772771902858
@@ -0,0 +1,22 @@
+archive/ES_0.5660772771902858---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T12:50:34.363
+Launch V∞: [6.287741974356525, -7.261637765836273, 0.3501489359335347] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.5386144454862158e-8, -6.1006549672399366e-9, 7.086575820672058e-9] km/s
+ V∞_out: [-2.842327507268354e-8, 2.57439761744661e-9, -3.3988147185995643e-9] km/s
+ time of flight: 1.8461673839880416e8 seconds
+ arrival date: 2029-03-02T07:16:12.363
+ thrust profile: [0.6298573211275723 -0.14806488886075742 -0.15481666074240072; 0.12857534288017997 0.04610164551974019 -0.10904673022467065; 0.06345403029323268 0.04275254373770307 -0.0917637358588795; 0.054397542055125536 0.05132813123698566 -0.11049980092991689; 0.06496848732287747 0.07466000279738193 -0.16393325097480765; 0.038969110766169685 0.05213395562328161 -0.12339238220202578; 0.020637588091278008 0.030465702147700353 -0.07842752444916316; 0.011312365467216765 0.019014322308559057 -0.05126929466205712; 0.005997816131071253 0.011755845586150284 -0.03268086404247676; 0.0010958098873316093 0.002433753382850221 -0.007031311308143293; 0.002495832172395044 0.005883479795071932 -0.017482155967704128; 9.34711706921342e-5 -0.00032547195453374147 4.471892359307508e-5; 0.0020688935020314507 0.0009631552294515739 -0.0007891634327955562; 0.0013050708205151749 0.0006396044396844363 -0.0010757977223988247; 0.0018816434806756405 -0.0003615037063054486 -0.001689708759117161; -3.615669245387432e-5 -0.00019410739024731504 0.0005474663546617138; 0.0011859597146577218 0.0012933395611390778 -0.0025200176817237853; -0.001953051624333311 -0.004051527446386717 0.0007093193571369736; -0.003540158896979132 0.0003728406335427413 4.488701943534262e-5; 0.0031608082905250365 0.0017359802829901888 -0.004594426787997933] %
+
+Mass Used: 121.48365239743407 kg
+Launch C3: 92.38968645563989 km²/s²
+||V∞_in||: 2.7053537258084603e-8 km/s
diff --git a/archive/ES_0.5660776968666412 b/archive/ES_0.5660776968666412
new file mode 100644
index 0000000..f2f851f
--- /dev/null
+++ b/archive/ES_0.5660776968666412
@@ -0,0 +1,22 @@
+archive/ES_0.5660776968666412---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:51:17.606
+Launch V∞: [6.347544725224467, -7.647968369260002, -0.04667955429338566] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0821963255162517e-7, 6.269656185171485e-8, 9.637376081083443e-8] km/s
+ V∞_out: [-5.265294582519781e-8, 7.171653003450403e-8, -1.3129412588382646e-7] km/s
+ time of flight: 1.7847620044321585e8 seconds
+ arrival date: 2028-12-26T07:34:37.606
+ thrust profile: [0.1636764036934882 -0.07311038491362899 -0.06747755767852728; 0.08062829255847993 0.001100435422205505 -0.10187501051393341; 0.04913229737669803 0.007251868376000884 -0.10834046129942604; 0.04113998562527979 0.008507958655269062 -0.12898820354982643; 0.0334263946783357 0.00787895119551025 -0.13348156405565054; 0.024908998933002045 0.0067955277088283415 -0.12210836112271642; 0.018739339707652722 0.0054188337644199966 -0.10610990285670492; 0.01277848685927263 0.0032683885094130956 -0.07887778771330214; 0.007616885633303936 0.001357638098250701 -0.050247995059010314; 0.00345956423633345 0.001992599750722044 -0.0305785445543912; 0.00360303855833814 0.001595042120591265 -0.03214972014068985; 0.0013378167764517626 -0.0007305417835090145 -0.012483789326929777; 0.0009683934705238466 0.0006216861891983035 -0.010208984969291224; 0.0015333977470901585 -0.001252515983940456 -0.001701864036510707; 0.0016727950097139453 0.00029984963321177277 0.0002990529178776146; 0.0023396799689053855 0.0001946669083854615 0.00034606761157031764; 0.0014650383749212213 -0.00039944919989297963 0.0018946456061169435; 0.0014770989300100564 -0.0008681283239233994 -0.004558454369811253; -0.0010321044892197561 0.0011833770237093804 0.005961705908478607; -2.8278681654280008e-5 9.340116464737718e-7 0.0005913673101938704] %
+
+Mass Used: 84.17859436357458 kg
+Launch C3: 98.78492319671547 km²/s²
+||V∞_in||: 1.5789315852961647e-7 km/s
diff --git a/archive/ES_0.5660918740819547 b/archive/ES_0.5660918740819547
new file mode 100644
index 0000000..55350cf
--- /dev/null
+++ b/archive/ES_0.5660918740819547
@@ -0,0 +1,22 @@
+archive/ES_0.5660918740819547---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T06:28:09.388
+Launch V∞: [7.622723002731972, -6.449409152023366, -0.2880403590091574] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01321466579106193, -0.1304054975835235, -0.08476442560736727] km/s
+ V∞_out: [0.026971699752169846, -0.025095502403138435, 0.15166883329660014] km/s
+ time of flight: 1.7553179497064096e8 seconds
+ arrival date: 2029-12-08T21:18:03.388
+ thrust profile: [0.22513543753081122 -0.030782534432170078 -0.0987675143451682; 0.04107290482660307 0.01097902791594303 -0.06160856492097275; 0.04150834759136833 0.018036762072438452 -0.10629027073883701; 0.04015889036041455 0.021333365979206608 -0.14354787090639526; 0.03146981769653102 0.018231717297205956 -0.14415901856540245; 0.023959282067306766 0.014389220585223735 -0.13244367020337472; 0.013079644800917466 0.007336395579114578 -0.08311120706349573; 0.011842604097316299 0.007743403516947706 -0.08563852494654076; 0.004433182176607299 0.0024616001061459154 -0.033174495953321614; 0.0019704375524882264 0.00023334474353965532 -0.013111789228859971; 0.00030901984057516205 -0.00046597677853888755 -0.0027530030133355076; 0.0006391913189187456 -0.0004024239828329092 -0.0029596703632615486; -0.0009280169337749493 -0.00138569867582216 -0.00023794597022650226; 1.588092116516791e-5 0.00011254668237032899 0.001407187442668411; -0.000449784970950234 0.0006758501977751942 0.00041282686424406806; 0.00013099116242479907 -0.0012810796734413752 -0.00010709283624231176; 0.0012915454443738713 0.0008077491985424661 -0.0023103585276185237; -0.00034752928830514317 -0.0011735595430297846 0.00224518184730387; 0.004890510919887725 0.004581512256192159 -0.004207217877143073; 0.0053497085973537705 -0.0015489502429912498 -0.002225463650264317] %
+
+Mass Used: 78.36863522478052 kg
+Launch C3: 99.783751635 km²/s²
+||V∞_in||: 0.15609365470935296 km/s
diff --git a/archive/ES_0.566094407927553 b/archive/ES_0.566094407927553
new file mode 100644
index 0000000..4ad902f
--- /dev/null
+++ b/archive/ES_0.566094407927553
@@ -0,0 +1,22 @@
+archive/ES_0.566094407927553---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T23:40:46.475
+Launch V∞: [5.909419854232968, -7.74933905288613, -0.30854449296258857] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1111517559748305e-5, -3.258564291822868e-6, 5.829803513398753e-8] km/s
+ V∞_out: [3.951986202604556e-6, -9.0673672877873e-8, -2.0982984863772045e-5] km/s
+ time of flight: 1.6991933822421497e8 seconds
+ arrival date: 2028-09-13T15:29:44.475
+ thrust profile: [0.4336086811507247 -0.15608235082914526 -0.14212779892239308; 0.04251292774787442 0.00788615105318473 -0.04421337143653269; 0.10615353685330675 0.04633681839707722 -0.16841953945250102; 0.06026223789429507 0.036726994066289466 -0.1412309174853631; 0.07156151720623743 0.05882101787359054 -0.2111031191907492; 0.03347153747502198 0.029595822432678876 -0.11540913093085844; 0.021216053876614783 0.020932841017006522 -0.0840512002890314; 0.018935905353990312 0.02173006384428165 -0.08597445000573661; 0.01108439190196588 0.01287367198918735 -0.05449308328703192; 0.011402764606891711 0.013696655177474083 -0.05824624922077483; 0.00028090066817661267 0.0003741876046149022 -0.0017530186416973175; 0.00014272078235569156 7.044521720809478e-5 -0.0006019729567560274; 0.00019364917102584274 0.00036524467995710736 -0.0002785293870197364; -2.39556603998536e-5 -0.00010867427534109604 -0.0003642468867803171; 7.631855365938334e-5 1.759696863833473e-5 -0.0004095880350471114; 0.0003057445762865272 -0.00021118564544208933 -0.0006226523757218122; 0.00015340361066765455 -0.00020647966505365502 -7.961257343196292e-5; -1.688534983865144e-5 -0.00012758221070090258 -8.46772709852747e-5; 0.00046162177292629865 0.0005346961245566789 -0.0009231338995931368; -9.68229095173618e-6 0.0002197830775061793 -0.00011225865381009933] %
+
+Mass Used: 105.87606814857418 kg
+Launch C3: 95.06869847432644 km²/s²
+||V∞_in||: 2.136159670016276e-5 km/s
diff --git a/archive/ES_0.5660986628200324 b/archive/ES_0.5660986628200324
new file mode 100644
index 0000000..27e91a8
--- /dev/null
+++ b/archive/ES_0.5660986628200324
@@ -0,0 +1,22 @@
+archive/ES_0.5660986628200324---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T03:02:48.427
+Launch V∞: [6.020930914525074, -7.39807905343625, 0.014254530070212724] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0019371548745102352, 0.01244124389207773, -0.01696307028706828] km/s
+ V∞_out: [0.014719789179215185, 0.012177761905928168, 0.008987804685154213] km/s
+ time of flight: 1.8749577786667162e8 seconds
+ arrival date: 2029-04-07T05:12:25.427
+ thrust profile: [0.5274393535549065 -0.1375475847671631 -0.12059190996552924; 0.39773474858662855 0.10842395563135193 -0.27558491849823513; 0.074517126653524 0.05065787389730275 -0.10961335418754166; 0.06341895101068666 0.06019338759579595 -0.1305870867349729; 0.02194140000611285 0.024802356172021756 -0.060750883055769124; 0.031916082293180326 0.04394419414017509 -0.10746804354394231; 0.009283927906997669 0.014535634217076685 -0.0403332503050516; 0.007352638303198653 0.012577760071422767 -0.03593394532659051; 0.008461390655153764 0.01501962260608293 -0.04418808358372624; 0.003958427780459077 0.008006820883334879 -0.02536121586484652; 0.00116528594526611 0.0016525247155145992 -0.004788726456062641; 0.0008615207682875481 -0.00017848221131023774 -0.0028917847934386348; 0.00015771445158609305 0.003632731996431236 0.0004401170194831532; 0.0007738259751028187 -0.0006209979127169759 -0.0024704155058956033; 7.320069934104108e-5 0.0005390435348409067 -0.0020213436037279666; 0.001462387374604295 0.0017958108096196566 -0.00024651316126528657; -0.0015267879122761792 -0.0017619577568096984 -0.00039373007116941337; -0.0013918828586603027 0.0009187774878672481 -0.0013395126804356637; 0.004261681764656609 0.0023031958003145846 0.003457260502701405; -0.0005573847919848543 -0.004583952352582104 -0.006794738952168252] %
+
+Mass Used: 129.71202191501743 kg
+Launch C3: 90.98338595000348 km²/s²
+||V∞_in||: 0.021125408212719084 km/s
diff --git a/archive/ES_0.5661113942035847 b/archive/ES_0.5661113942035847
new file mode 100644
index 0000000..f19cf85
--- /dev/null
+++ b/archive/ES_0.5661113942035847
@@ -0,0 +1,22 @@
+archive/ES_0.5661113942035847---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T19:41:16.731
+Launch V∞: [6.170161921059808, -7.662047416007094, 0.10858809142820104] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010892432321655607, -0.000304929966924384, 0.0073896978103098485] km/s
+ V∞_out: [-0.012633858218096016, 0.00012897478517199688, 0.0036560785462380215] km/s
+ time of flight: 1.825621680791074e8 seconds
+ arrival date: 2029-02-12T19:24:04.731
+ thrust profile: [0.36293944732240385 -0.10538273086925856 -0.12823755301313425; 0.04708673836514417 0.010744577978688833 -0.05640436062476361; 0.03449679219366677 0.01576561108311826 -0.06893300101835789; 0.03241450301216615 0.02029251810297491 -0.08973900235352297; 0.031817350798675474 0.02511109389424675 -0.11233289377808468; 0.04049424197946163 0.03520990480165073 -0.16619060226916657; 0.03005978819436073 0.0288656071799082 -0.14459652957933947; 0.010056603080256311 0.009896933753288923 -0.05709004328180546; 0.010055476032900013 0.010952235983295528 -0.06491273205945089; 0.005587146389034771 0.006540013415852466 -0.04099464208472948; 0.00266465176843936 0.0035632199931014547 -0.030663356675780292; -7.721967767494845e-5 6.742962074598877e-5 0.0002835848775067742; 0.0005282818185282813 0.0002057907015265051 -0.0004005599364911372; 9.941239925298509e-5 -0.003775784731136802 -1.0270738078752787e-5; -0.0036340875212622146 -0.0005930973783971731 0.0019401756318751123; -0.001471965539522504 0.0031903519104937023 0.0025385465735141355; 0.001947020061813121 0.00047284201840915003 0.0002314027985475429; 0.0029254566126723997 -0.0012510731290705816 0.0042884893421842995; -0.0017869323670561617 -0.00011938906655267813 0.004833228748326455; -0.00011787707837481484 -0.0003606300939240104 -0.0002461388039321649] %
+
+Mass Used: 95.85694259096363 kg
+Launch C3: 96.78966011083746 km²/s²
+||V∞_in||: 0.013166081341624562 km/s
diff --git a/archive/ES_0.5661142127572062 b/archive/ES_0.5661142127572062
new file mode 100644
index 0000000..02fb0af
--- /dev/null
+++ b/archive/ES_0.5661142127572062
@@ -0,0 +1,22 @@
+archive/ES_0.5661142127572062---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T08:18:10.815
+Launch V∞: [7.820000398415907, -5.590797219631064, 0.241502439856378] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6287930881942084e-9, 2.8395545766166628e-8, -8.21703056620793e-9] km/s
+ V∞_out: [8.819937449601762e-9, 1.6660537556759234e-8, 3.4697555930747203e-10] km/s
+ time of flight: 1.8333879639246312e8 seconds
+ arrival date: 2030-02-28T07:44:46.815
+ thrust profile: [0.6870320092755424 -0.00979749866063578 -0.1561846004842381; 0.10067765575283001 0.06781746276815805 -0.0859933587564185; 0.05203109090468015 0.06011261901331236 -0.08350564279776605; 0.05099702342765929 0.07987439760563915 -0.11915475171770154; 0.023371811363904753 0.04907157211232588 -0.08177440710677616; 0.014714588446278211 0.0370840818864391 -0.06654026729708752; 0.008576932667671072 0.0258971212989299 -0.04807558406723163; 0.008768557065508366 0.03895971269452489 -0.0753207492668902; 0.0016102440432901543 0.014532495607949067 -0.029137054506345336; 0.006842268901105429 0.048540957413384836 -0.09476623400188124; 0.002384403552407704 0.01565108848019482 -0.03550429904970185; -0.0008811390490052616 0.0005034937712605892 -0.002052556505288121; 8.907508386409306e-5 0.0020289747806605182 -0.007587349009958794; 0.0007453553950864426 -0.000247851007947078 -0.0002482166995795717; -0.0012628596938935041 0.0030153352542979612 -0.004011023364960652; 0.0003951397700783225 0.002518371247961652 -0.0024886566443500934; -0.001014837104676498 -0.0013695390905066637 0.004952965660552941; -0.0036079509485253364 0.002650672397290917 -0.0044072435577779045; 0.0009133672101706302 -0.0009811336669818217 0.0009685973195673507; 0.008564454986038467 0.0011959267170150404 -0.005295341442198687] %
+
+Mass Used: 121.07141282089742 kg
+Launch C3: 92.46774321071597 km²/s²
+||V∞_in||: 2.9677216240493255e-8 km/s
diff --git a/archive/ES_0.5661272140423022 b/archive/ES_0.5661272140423022
new file mode 100644
index 0000000..16df96c
--- /dev/null
+++ b/archive/ES_0.5661272140423022
@@ -0,0 +1,22 @@
+archive/ES_0.5661272140423022---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T00:56:26.025
+Launch V∞: [6.227448688967715, -7.635837511655531, 0.02746307864030862] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.049272937372817e-8, 8.100272974409022e-8, 4.315480316621778e-8] km/s
+ V∞_out: [-2.6491006256824917e-8, 5.069710662137395e-8, -8.263502369726159e-8] km/s
+ time of flight: 1.762975314036487e8 seconds
+ arrival date: 2028-11-28T12:28:37.025
+ thrust profile: [0.2669536002492909 -0.09069425953111633 -0.10170149440922727; 0.06764679143483814 0.013095742481929783 -0.07834852179145421; 0.05897893597601724 0.025137826863795006 -0.11247194040952474; 0.07731651875709111 0.044092042600545917 -0.19607734430640655; 0.040140870161838246 0.02846165005025508 -0.1340848275023896; 0.027264466136205152 0.02188645252449222 -0.11168519388207461; 0.01838187735405722 0.016033732801629123 -0.08956459526108951; 0.01952819056910497 0.018905054954016353 -0.10285090800793546; 0.0035725250990710083 0.0030614255560073435 -0.021465753082951164; 0.0053704390563364904 0.005699741598107485 -0.035117487292442205; -0.00012692598703257848 -0.0009074614948600135 1.0624961305138558e-5; 0.0031983025969499895 0.010360350733220936 -0.04058802700410592; -0.0013134820418343436 0.00033341454842470704 -0.0005732817004310885; 0.0036403482041209695 0.004676930749054172 0.0013618053796620947; -0.0024244224561521034 0.0017535931774364853 0.0038300051252665264; -0.0002802546238092153 -0.0002547985110236326 0.0022000667313259612; -0.002791304675544672 -0.003165979554613724 -0.0017259354692666668; -0.001691424123315298 -0.004406185894829362 -0.0023757584520532164; 0.00019184267211375626 0.0013061465078708166 -0.0011462344046314007; -0.0011897302020312639 -0.00038634190007706974 0.005791112007798551] %
+
+Mass Used: 94.13574863957001 kg
+Launch C3: 97.08788589881985 km²/s²
+||V∞_in||: 1.0031670047625724e-7 km/s
diff --git a/archive/ES_0.5661295953337632 b/archive/ES_0.5661295953337632
new file mode 100644
index 0000000..e2ef7c1
--- /dev/null
+++ b/archive/ES_0.5661295953337632
@@ -0,0 +1,22 @@
+archive/ES_0.5661295953337632---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T18:24:01.795
+Launch V∞: [6.330819131363203, -7.444693007841791, -0.045075742928142336] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002108985504869084, -0.0015739237217827198, -0.002150395189048669] km/s
+ V∞_out: [0.0021553258722760054, 0.001192273015503223, -0.002342357447882525] km/s
+ time of flight: 1.8078358922823402e8 seconds
+ arrival date: 2029-01-18T04:03:50.795
+ thrust profile: [0.3339876043572633 -0.09523472734327683 -0.113427666353578; 0.11742551530339514 0.030825845747242748 -0.11631256477816405; 0.12471044561121823 0.0674496861790411 -0.20371049233730304; 0.0689099569434208 0.050431336674782494 -0.1579810338996267; 0.049850208450937274 0.044541863389227006 -0.14605659337842739; 0.020498154053977407 0.02167647994409356 -0.07518399164971035; 0.01449534883898578 0.017219521686455103 -0.06250505529616898; 0.01004003709285814 0.013224700980654699 -0.04974863935372539; 0.0026073346096565472 0.004235705303131659 -0.015443534735047487; 0.003630456222305343 0.0013588632336940798 -0.01089863474814915; 0.002291679966949953 0.005900052461423436 -0.0261338501681942; -0.0007509473610866971 0.002325224857697506 -0.00700294524213059; 0.002415754309886861 -0.0031460025181122412 -0.0013817959443220259; 0.0016033244112633447 -0.000501822549609965 -0.007203617620104198; 0.002948627387571131 0.00029345661199235533 -0.0018160982626974076; -0.003197028918731335 -0.00014354688565022155 -0.005606377743889316; 0.0011916087322766744 0.0012616561245206931 -0.007423160241418295; -0.00401908383133431 0.0015616164926022542 0.00812227651668318; -0.0018687613645737267 0.010237112753918174 -0.002070307695203673; -0.00020108354896565496 0.0027715807026195945 -0.0017858150868736763] %
+
+Mass Used: 103.37344726980427 kg
+Launch C3: 95.50475667764333 km²/s²
+||V∞_in||: 0.003398419516602083 km/s
diff --git a/archive/ES_0.5661463028552626 b/archive/ES_0.5661463028552626
new file mode 100644
index 0000000..3a3f893
--- /dev/null
+++ b/archive/ES_0.5661463028552626
@@ -0,0 +1,22 @@
+archive/ES_0.5661463028552626---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:59:19.101
+Launch V∞: [7.781523213363427, -6.043262869941665, 0.022812154751764267] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.99373724082547e-6, 6.533631077630375e-5, -0.0013233965963400035] km/s
+ V∞_out: [-5.974000290385009e-5, 0.0013234972896262413, -1.7813589859884912e-5] km/s
+ time of flight: 1.7686158175204933e8 seconds
+ arrival date: 2029-12-19T16:12:20.101
+ thrust profile: [0.286313900806503 -0.026744336928463515 -0.08873392460256177; 0.046766075028808224 0.022203858572628514 -0.056867064951925846; 0.08751916935299216 0.07689575675083477 -0.18049369071855087; 0.030078810067878686 0.030829774048435395 -0.0906101835996288; 0.017298704908694826 0.02098996486191639 -0.07084193830557897; 0.01831122673136299 0.025983662627165872 -0.0914072101614609; 0.02204198574336631 0.03398080792247092 -0.12299335775238972; 0.006293121483194887 0.008734651786730496 -0.03586522361693323; 0.01149463571103629 0.01697536851595221 -0.0789239696460123; 0.002282844505461682 0.0036541693456387464 -0.016998467365417193; 0.006467419044242738 0.0125266485295022 -0.06341924475449233; 0.004019907368779755 0.003118878606340871 -0.014847993434102614; 0.009932114610715708 -0.004762381401333132 -4.318260177294496e-5; 0.003367576365306667 -0.011042763787160242 -0.010361874729167985; -0.0002275371090246026 0.001624436233501305 -0.008267624135437163; 0.0017098543131291617 0.0005965615132530536 -0.011457629037524961; 0.0005825521279426236 0.018542509449708335 -0.0012412339758903369; -0.005704499683735565 -0.012959064491705084 -0.006055890525882577; 0.012299670504220503 0.004632100377162829 0.007976859279352214; 0.016651127261312355 0.02368680552606058 -0.00756098660481664] %
+
+Mass Used: 94.24106149102545 kg
+Launch C3: 97.07365002973387 km²/s²
+||V∞_in||: 0.0013250389700004 km/s
diff --git a/archive/ES_0.5661493853736566 b/archive/ES_0.5661493853736566
new file mode 100644
index 0000000..b2dd6b7
--- /dev/null
+++ b/archive/ES_0.5661493853736566
@@ -0,0 +1,22 @@
+archive/ES_0.5661493853736566---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T10:51:40.562
+Launch V∞: [7.518555172978564, -6.421409312351947, -0.07709150501099656] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.524797432953679e-9, 3.686323778376672e-9, -5.421677051305503e-9] km/s
+ V∞_out: [4.435723042258674e-9, 8.769090395787662e-9, 2.762477392020497e-10] km/s
+ time of flight: 1.6024801630935344e8 seconds
+ arrival date: 2029-06-06T04:11:56.562
+ thrust profile: [0.19470816608683095 -0.04041090188254591 -0.07473742696198472; 0.11369255219770068 0.033549775641406605 -0.12670469259996606; 0.10037821656600751 0.05420963742708867 -0.1884242000959138; 0.08389726097549198 0.059301789798037956 -0.2205507041998926; 0.04134842834170254 0.03431548657393656 -0.14169194912414584; 0.03964917178059457 0.0371849278942399 -0.16244218811083092; 0.02595717096179443 0.026613089857267142 -0.12459087762020056; 0.006066958840517296 0.006649127777783291 -0.03404518592268245; 0.003106674000999643 0.00436864411667507 -0.025545750050564503; 0.001552914512508875 0.0009524306986607868 -0.014713748114536466; 0.003089201808343096 0.002008439364491558 -0.007856839827861653; -0.002520605634544738 0.0009150992222688347 -0.0030582271160731157; 0.002643652199118187 -0.0007063691678017769 -0.002723649379457622; -0.0004578703324918227 0.0008688052437775635 -0.0007415370654357252; 0.0011554241892007934 0.0010788323738996895 -0.0008201688520900426; 0.0011580125805351104 -0.0011451190776990278 -0.0018808286384504342; 0.0012072571487099638 0.001235859268786868 -0.001996566484208928; 0.0008249527213983187 0.0003306147789659356 0.002127896480475896; -0.0014306857525338247 -0.00190023269304404 -0.002749420199081592; -0.0025642727377417416 0.000586743338714073 0.0032615311579859293] %
+
+Mass Used: 90.1877930841033 kg
+Launch C3: 97.76911254602788 km²/s²
+||V∞_in||: 9.249678188388876e-9 km/s
diff --git a/archive/ES_0.5661514450469888 b/archive/ES_0.5661514450469888
new file mode 100644
index 0000000..284e232
--- /dev/null
+++ b/archive/ES_0.5661514450469888
@@ -0,0 +1,22 @@
+archive/ES_0.5661514450469888---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T17:32:00.172
+Launch V∞: [6.049141238305538, -7.732486212466329, -0.07761559087579221] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2217650424494593e-6, -0.000416903225670039, 0.00017092056764602624] km/s
+ V∞_out: [0.00036709569438438637, 0.00020576908478449416, -0.0001614339234182524] km/s
+ time of flight: 1.7418126393390217e8 seconds
+ arrival date: 2028-11-04T17:13:03.172
+ thrust profile: [0.3616220617804143 -0.13037193367660455 -0.1477128442083487; 0.04619406024291761 0.00567595882076307 -0.05738684103131372; 0.05083789366197069 0.01781924629277811 -0.10208915423305254; 0.07434070421650796 0.03611916667790532 -0.19775334235779335; 0.03126190873907834 0.017703776975657705 -0.11019474564231685; 0.02673220121451211 0.018042428128529152 -0.11258914615219946; 0.022808541713168262 0.017542629745828694 -0.11095629057050756; 0.016111646309376313 0.01295673335577222 -0.08906935411485296; 0.013915343639935993 0.013016210092247162 -0.09174346670244964; 0.0019526820148374957 0.002728933568489183 -0.02088729266120914; 0.0009962468330331597 0.0010122111812885788 -0.01004021338198264; 0.0008932189104298262 -0.0003130840182177662 -0.0013423259877694891; 0.0012187404736184529 0.0019409440081089749 -0.015802334121613488; 0.0006947449954947376 0.0010996565673517598 9.232466375161418e-5; -0.0028453437009946098 0.0009563637057139416 -0.0016068433475400477; 0.0002150492965122236 0.000313843606104216 0.0025331547572080434; 0.0002681740518959416 -0.00026039560501414215 0.0017602005683691035; -1.1429490748263724e-5 -0.00010363002115762677 -0.0006164710329050341; 0.0008615793263841119 -0.0023528695075065442 0.0027773418501327958; -0.00036699551236431873 -0.004087040625694033 -0.004127761976553189] %
+
+Mass Used: 98.23807048125127 kg
+Launch C3: 96.38947692689753 km²/s²
+||V∞_in||: 0.00045058143850844795 km/s
diff --git a/archive/ES_0.5661516689382727 b/archive/ES_0.5661516689382727
new file mode 100644
index 0000000..3361c26
--- /dev/null
+++ b/archive/ES_0.5661516689382727
@@ -0,0 +1,22 @@
+archive/ES_0.5661516689382727---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T16:04:46.340
+Launch V∞: [6.5056162379840226, -7.474966762940619, -0.7922685845048651] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1207656651105763e-7, -6.797136575566576e-9, 3.622242168720466e-8] km/s
+ V∞_out: [-1.0165789804915526e-7, 2.6897869383582905e-8, -4.624682671036612e-8] km/s
+ time of flight: 1.8474115882147282e8 seconds
+ arrival date: 2029-03-08T21:04:04.340
+ thrust profile: [0.17620727630036365 -0.05145139211171396 -0.07264565936299672; 0.06369479874354078 0.014474225007688793 -0.07846873265951322; 0.057487540322916135 0.02698457130607455 -0.11921614600421192; 0.05649221650097836 0.03578388893128733 -0.16371034146974806; 0.03895865530309629 0.03007037324954902 -0.14684977416365552; 0.026794828387966596 0.023754124000600736 -0.12421632566224367; 0.016644137170262283 0.016180715701418723 -0.0913554737485043; 0.007367613058945926 0.007407799513492516 -0.04654041592187264; 0.005153695371833639 0.006325518988952265 -0.03839815440953329; 0.004065065407899228 0.004995248870224883 -0.0332011279735382; 0.0001090266170101465 5.4428196950104596e-5 -0.001123847578807824; -0.0011917614121502663 0.0012973188641128286 -0.0025254559219731643; 0.0019231919683286316 0.000888044874691325 -0.0017489056707960175; -0.00012598320377442732 -0.00035444893294751887 0.0026657584922165534; -0.0021775397355054387 -0.0001384485001152289 0.0003588782585165432; -0.0009916912830669551 -0.0010885245604466862 5.454406883252769e-5; -0.001288628197149524 -0.003187895914577849 0.0025852023226350983; 0.001156828003354938 -0.0009143678056788567 -0.00021972015744396202; 0.0024669806949571076 -0.0004969866491788105 -0.0028831966233766795; 0.007633790645764407 0.003940421045510048 0.0012128065990190124] %
+
+Mass Used: 84.02609561892496 kg
+Launch C3: 98.8258602529817 km²/s²
+||V∞_in||: 1.179805986568135e-7 km/s
diff --git a/archive/ES_0.566168795170304 b/archive/ES_0.566168795170304
new file mode 100644
index 0000000..7047153
--- /dev/null
+++ b/archive/ES_0.566168795170304
@@ -0,0 +1,22 @@
+archive/ES_0.566168795170304---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T01:10:30.010
+Launch V∞: [6.502647627343337, -7.248863976708228, 0.3328209742616127] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.480893333927934e-5, -3.9773169097166655e-6, 6.953714689026605e-8] km/s
+ V∞_out: [4.909364326246387e-6, -1.1407090928103053e-7, -2.4640314296461606e-5] km/s
+ time of flight: 1.8749577787482023e8 seconds
+ arrival date: 2029-04-06T03:20:07.010
+ thrust profile: [0.4070690637633941 -0.0871270910175054 -0.10817676028796365; 0.10930120018292651 0.03980051987120812 -0.09338738697186674; 0.08345392474600283 0.05652361658012908 -0.1196213679570179; 0.0929194520922406 0.08526727604154923 -0.18200691671672856; 0.04002432495547758 0.0462033106069977 -0.1068450967798129; 0.028883890493914426 0.03959042997729084 -0.0950896449251549; 0.012131269306143829 0.01969929919244524 -0.048193249106015176; 0.011311723213184832 0.01905123146753283 -0.04890219417114908; 0.007440698963372998 0.012488355746925604 -0.03604304196038028; 0.005177365631161453 0.009136563762214755 -0.02801509940974241; 0.00024831271946918203 0.000831848933473369 -0.009144254924644308; 0.0017244747518810064 0.003927525825889112 -0.012606478946504483; 0.0011557632617344813 0.0024836413184196778 -0.00292972942382152; -0.0008215575994254714 -0.0010207031012166076 0.0006372875867004702; -0.005426440138242542 -0.0050763399925113665 -0.0014449106203284533; 0.00629002617573182 0.004710801353678311 -0.0010404642357573382; -0.002506497438911222 -0.0005123218526224539 -0.004601189759832237; 0.0018961810280616362 0.0005626241009038494 -0.005309931955713064; -0.00032053465172598663 -0.0033878710825935177 -0.0039888947280263655; 0.005028294292558277 0.0038624576444511224 -0.0012828325821844337] %
+
+Mass Used: 106.70644900381785 kg
+Launch C3: 94.9412249191206 km²/s²
+||V∞_in||: 2.512582453667783e-5 km/s
diff --git a/archive/ES_0.5661761207679898 b/archive/ES_0.5661761207679898
new file mode 100644
index 0000000..0e1250c
--- /dev/null
+++ b/archive/ES_0.5661761207679898
@@ -0,0 +1,22 @@
+archive/ES_0.5661761207679898---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T09:08:35.666
+Launch V∞: [6.22263525789121, -7.573445846274287, 0.42801474351323626] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.791359183230955e-6, -8.881106320042419e-6, -1.339418751319143e-5] km/s
+ V∞_out: [-1.5977993333858452e-5, -9.962892839749347e-6, -4.4204939832658573e-7] km/s
+ time of flight: 1.727603900376495e8 seconds
+ arrival date: 2028-10-15T22:08:25.666
+ thrust profile: [0.34769700204804876 -0.12961537831064243 -0.12622604497106382; 0.0741618638957754 0.011434688534857624 -0.07868558733424222; 0.07404649077193896 0.028094818173779457 -0.1284295350692975; 0.07148084067299326 0.037774603382942945 -0.16993503320717313; 0.06370255417595086 0.04090498871881173 -0.19049094285231885; 0.036847427880347026 0.02743009026761084 -0.13178314045773704; 0.037156589250081015 0.03037397002836397 -0.1525283072602576; 0.007973182581201603 0.007098334848230302 -0.038092822605648356; 0.0024666742964278687 0.002141542835510862 -0.012768153819741062; 0.0019808225311585105 0.0022133253992380098 -0.012859989779233649; 0.0009310503138500973 0.0010390586473952384 -0.006637572361184153; 0.0006409632585993145 -0.0004385941282859104 -0.003090575967816726; 4.595616376078726e-5 0.0003294737602533016 -0.0016085580910575091; 9.930055647188667e-5 0.0014533784554235348 -0.002531299731135531; 0.001253270984724692 0.0009038243916431638 6.494565622115842e-5; -0.00021147673679511723 -0.0022568973533068364 -7.963242395739095e-5; 0.0004486067552709246 0.00025536144274573353 -0.0010362453038987567; 0.0008510526225567285 0.00046161511830138737 0.0010726532118348173; 0.0004990361852372351 -0.004016761512422043 0.0020019855403616478; -0.00012046731236828426 -0.0002659065625519754 -0.0037150204185310036] %
+
+Mass Used: 99.01357663011049 kg
+Launch C3: 96.26146815986475 km²/s²
+||V∞_in||: 1.8818847554020726e-5 km/s
diff --git a/archive/ES_0.5661772522843169 b/archive/ES_0.5661772522843169
new file mode 100644
index 0000000..72006f7
--- /dev/null
+++ b/archive/ES_0.5661772522843169
@@ -0,0 +1,22 @@
+archive/ES_0.5661772522843169---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T00:58:40.869
+Launch V∞: [6.592331690077758, -7.413639782403467, 0.0992862422540946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.0959913081644036e-8, 8.158771095597398e-8, 4.1881108803565755e-8] km/s
+ V∞_out: [-2.6889548016844937e-8, 5.228081743835439e-8, -8.162160250464553e-8] km/s
+ time of flight: 1.874957778749381e8 seconds
+ arrival date: 2029-04-10T03:08:17.869
+ thrust profile: [0.18644474159991206 -0.043001097387585584 -0.06653678188199931; 0.05798546200736372 0.016849853276654364 -0.06381435385921422; 0.04037260332753798 0.02213442176003683 -0.07478287686944321; 0.03466933998536786 0.025565175470065617 -0.0896271290262689; 0.041225338245951565 0.03716968820145321 -0.1338707765970303; 0.03256176237661188 0.0339597592773962 -0.13031975022577444; 0.02451528672635972 0.028437266651805657 -0.11598931293004784; 0.01104163975725217 0.013829614033806035 -0.06178802977048406; 0.00545606320875954 0.00768641501211005 -0.036677173970034255; 0.012212017364608987 0.018966463833075455 -0.08728093336294276; -0.0028905427379179237 0.0021759644044901886 -0.010335527111648576; -0.0010741873482527481 0.0009749943567491379 0.0015225503444074038; 0.0017161743991841838 0.0021378094054669526 -0.011516821175681646; 0.003511007568079054 0.002739283695289894 0.0017175045904989001; -0.005407009559519947 -0.002140709294557944 0.0020273421789162626; -0.0006220014998756811 0.0028160968754711276 0.009271691402349971; -0.0004912366497336942 -0.003024602924267986 0.005266529625463539; -0.008759013479530571 0.003175726457968313 -0.011958977822018137; 0.0027699141020483004 0.0007279096324964328 -0.0007930148246320275; 0.00803192448687013 0.0016955713333719742 0.00819968900719141] %
+
+Mass Used: 86.36075445505458 kg
+Launch C3: 98.43074969313975 km²/s²
+||V∞_in||: 1.0044051141500378e-7 km/s
diff --git a/archive/ES_0.5661775066785784 b/archive/ES_0.5661775066785784
new file mode 100644
index 0000000..d2ef5e1
--- /dev/null
+++ b/archive/ES_0.5661775066785784
@@ -0,0 +1,22 @@
+archive/ES_0.5661775066785784---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T20:29:46.206
+Launch V∞: [7.694981082429265, -5.544737605447989, 0.1414069531004781] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0032229168875075424, -0.003306044964713325, -0.002651364689588578] km/s
+ V∞_out: [-7.966891829835522e-10, 2.2766702375749922e-9, -4.2709662264226954e-10] km/s
+ time of flight: 1.8589355995258263e8 seconds
+ arrival date: 2030-03-30T09:35:45.206
+ thrust profile: [0.8136706840950494 -0.0022850684253896384 -0.2044185682494005; 0.1611109137868781 0.10017641475068348 -0.14382267500771115; 0.12857270597674295 0.13430671179796827 -0.20960894632505714; 0.03736964960077789 0.052284235792261 -0.09191584234907878; 0.01648689281771028 0.02871191506656157 -0.05485079134700705; 0.012036248498235862 0.027006968040850846 -0.05257349804940063; 0.0021914465220539245 0.005953227399679178 -0.007088618216794539; 0.005044628696264187 0.019224663853800283 -0.046930957813831484; 0.008809143431335383 0.010099325298334213 -0.026043272776213298; 0.002160760782216571 0.012107301116761785 -0.03177716498090059; -7.331208792486733e-6 -0.012246862428144236 -0.01760122315406272; 0.0017608223496722421 0.005814014972298401 -0.008666763076276215; -0.000268363203582788 0.001592597345929734 -0.0027405029726145064; -0.00430024931182161 0.012119283218782074 -0.015198099844946895; -0.0029551658690450235 0.0010929355990430935 -0.003496451170187124; 0.011492472769175456 0.014963244608416377 0.00023405185884089758; -0.0006545249453417711 0.005138504728688545 -0.009640637831077123; -0.0004364897043337042 -5.484457876342441e-5 -0.010455430318695755; -0.0016307006706645765 -0.0015191444288131478 -0.004855624955626738; 0.002598123229786052 0.008432209980756063 -0.004464798368564463] %
+
+Mass Used: 135.67549588318343 kg
+Launch C3: 89.97684489859851 km²/s²
+||V∞_in||: 0.005324177052811521 km/s
diff --git a/archive/ES_0.5661814399031164 b/archive/ES_0.5661814399031164
new file mode 100644
index 0000000..dc97170
--- /dev/null
+++ b/archive/ES_0.5661814399031164
@@ -0,0 +1,22 @@
+archive/ES_0.5661814399031164---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T10:42:46.039
+Launch V∞: [7.741953545470719, -6.317661337578401, -0.21733146496394465] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009159667804921539, -0.0006443882582494747, -0.04022232243917678] km/s
+ V∞_out: [0.03699813191308788, 0.014364078380531081, -0.006936904943736869] km/s
+ time of flight: 1.8154732560250714e8 seconds
+ arrival date: 2030-02-17T16:31:31.039
+ thrust profile: [0.17576179194489472 -0.010991497510148628 -0.07043904727963225; 0.0774233587843894 0.03221548390756682 -0.09959522116069063; 0.04674754276973656 0.030468024919624907 -0.10586047368667516; 0.03984958161108309 0.03234668231512965 -0.1297570535993842; 0.029340712718906987 0.027150563725438465 -0.12418029383971864; 0.017701891416695252 0.017781416498280113 -0.09151138149478288; 0.010119435469619324 0.010643707370294176 -0.06100243777258891; 0.004282492765093323 0.004843882686423164 -0.030323463982446116; 0.007456976958191517 0.008686038020403953 -0.05815396717144063; 0.003717524472402253 0.00416958452806666 -0.030692885183244593; 0.0036588052372409554 0.0025591489482793125 -0.023774257949995537; -0.0016783647507710756 -3.9388044247352726e-5 -0.0011194250839359158; -0.0011192679567764254 -0.007390777625255644 -0.013333781789010658; 0.002077368217020415 0.00011180718191346065 -0.00961553805978311; -0.002402138858197494 0.0011526431328623176 -0.0019587329072517706; -0.0016486152857092145 -0.0011403048950742343 -0.0009806851617180498; -0.000648484680349603 -0.0026258827900079917 -0.006441271172030927; 0.0020848116041898603 0.012733543474966082 -0.007399373226090165; -0.004874949979859215 0.002400785816784931 -0.0034047025303737674; 0.0005272679697880455 -0.0012722325199108146 0.0021271365881392395] %
+
+Mass Used: 77.80713230733545 kg
+Launch C3: 99.89792244222292 km²/s²
+||V∞_in||: 0.040237910653653966 km/s
diff --git a/archive/ES_0.5661915300050187 b/archive/ES_0.5661915300050187
new file mode 100644
index 0000000..e9c6a65
--- /dev/null
+++ b/archive/ES_0.5661915300050187
@@ -0,0 +1,22 @@
+archive/ES_0.5661915300050187---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T23:18:33.102
+Launch V∞: [6.012629277350104, -7.696708747644439, 0.002949419876584461] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.302030006042218e-9, 1.3959183612773215e-10, -4.601579731354071e-9] km/s
+ V∞_out: [-1.3691824641826686e-9, 3.2127597692471585e-9, 4.312820487888378e-9] km/s
+ time of flight: 1.7085776685239092e8 seconds
+ arrival date: 2028-09-23T11:47:59.102
+ thrust profile: [0.3387211800563282 -0.1149380394230452 -0.112341166203567; 0.10180218087399816 0.020975383044063052 -0.09670457932636066; 0.1577818120456501 0.0740154905147262 -0.22705969764036532; 0.06404206797574603 0.04183483309555106 -0.13264831489078285; 0.050679869361120095 0.04344701791198251 -0.13653313754994745; 0.02478114599175808 0.023239191784998347 -0.08188939783505582; 0.03919013505811377 0.04141421585343514 -0.14147182262776878; 0.020967313451191856 0.02454523768662114 -0.08758714522161554; 0.01090456310423107 0.013115008245064175 -0.051427944746396004; 0.003596939880098206 0.00450981785713043 -0.017778379707983766; 0.001252965497090897 0.0025614069941014934 -0.010064005053785385; 0.00010943847134914453 0.00023670830958934453 -0.0003642847959009942; -9.829022249567779e-6 -0.00018555772402369157 -0.0007416129457857081; -0.00017027428682225566 -3.903720959757466e-5 -0.0001277784926005579; -0.00042083458125859814 -0.00025489613368344583 -0.00022301866173104335; -0.0002796141080426178 0.00012809422799422618 0.00016267955177430335; 4.062598279762747e-5 -0.00011820793931739305 9.362259382612131e-5; -0.0001448685194858784 0.0003727591809730347 -0.0007108302903612296; -0.0001198696374248838 -8.202170862170743e-6 0.0006794901339959047; -3.2767625579542404e-6 0.00010025223465582133 0.00015135048797177602] %
+
+Mass Used: 104.10902208590369 kg
+Launch C3: 95.39104507199167 km²/s²
+||V∞_in||: 5.66545885745588e-9 km/s
diff --git a/archive/ES_0.5662083802190785 b/archive/ES_0.5662083802190785
new file mode 100644
index 0000000..afd1a8a
--- /dev/null
+++ b/archive/ES_0.5662083802190785
@@ -0,0 +1,22 @@
+archive/ES_0.5662083802190785---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T07:49:14.162
+Launch V∞: [6.635697336073364, -7.448305696820132, 0.19362092674069245] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.1014225051937254e-9, -9.48806626616701e-10, -2.859817103402015e-9] km/s
+ V∞_out: [-2.6050628227110015e-10, 5.890837877289862e-10, 8.184825307226292e-10] km/s
+ time of flight: 1.8749577787394142e8 seconds
+ arrival date: 2029-04-11T09:58:51.162
+ thrust profile: [0.1271139465549499 -0.03483986545299174 -0.0508235108152073; 0.03927039229300535 0.007783483964206913 -0.050198546127443615; 0.04038332227291742 0.016679379520307413 -0.08374879031360667; 0.04428369558460406 0.024346185284310116 -0.12647087959152145; 0.03535379446970771 0.022828082891563687 -0.12866280227253096; 0.021122533684229575 0.015043011045135423 -0.09302192654392218; 0.01877953452344928 0.014617804893945124 -0.09670141521530773; 0.012842443205809193 0.01056445588348555 -0.07733924909274; 0.014143255367304985 0.012143813565245555 -0.09275467926157163; 0.0006391158189933326 0.001972164413506016 -0.020373968663650377; 0.001361631333685169 0.002401282315580209 -0.016694764183563505; -0.0012871980011696102 0.0023981810442070053 -0.0013396381108505934; 0.00027970329462804355 -1.8836717030890386e-5 -0.001013783556385189; 0.003966196413051433 -0.0013551184593638297 -0.0006061946461841169; -0.0012774807920028753 0.007423681366094423 0.0008971444414355128; 0.0028421212955646023 0.0014449152273589027 -0.02647058628816239; 0.0023509658131866534 0.0016976015884833553 -0.021528684976901226; 0.004264387129483944 0.00028286286426443404 -0.008057128205513417; 0.0018169300837865446 -0.00037323266058696976 -0.003173037434474407; 0.0013324886108085387 -0.002924022854195229 0.013764130623655963] %
+
+Mass Used: 79.88429219918817 kg
+Launch C3: 99.54722595252629 km²/s²
+||V∞_in||: 4.324073245834832e-9 km/s
diff --git a/archive/ES_0.5662095760188285 b/archive/ES_0.5662095760188285
new file mode 100644
index 0000000..2ae329d
--- /dev/null
+++ b/archive/ES_0.5662095760188285
@@ -0,0 +1,22 @@
+archive/ES_0.5662095760188285---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T07:51:57.642
+Launch V∞: [6.519278830933162, -7.421923769788834, 0.22685901703375036] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.207558871743603e-9, -4.9188252931203014e-9, 1.070128739934637e-8] km/s
+ V∞_out: [3.6695428747330918e-9, -8.843464753421451e-9, -1.153709418570176e-8] km/s
+ time of flight: 1.8749577788115826e8 seconds
+ arrival date: 2029-04-10T10:01:34.642
+ thrust profile: [0.21724606120697043 -0.05844846854082335 -0.07953058450919977; 0.11235050070491395 0.02638725199572443 -0.1264971678399169; 0.06797390861879078 0.031448881725358924 -0.130511359111658; 0.04371455108310928 0.025936708957229385 -0.11751146391005234; 0.03494567190586371 0.024643429006297558 -0.11995378894154463; 0.01799329594181335 0.014350703568438363 -0.07733345389703929; 0.011314073038049812 0.009808882843047846 -0.05626347097543325; 0.014115228140483885 0.013026017281753751 -0.08181196150716022; 0.007270327375760242 0.006682654369087014 -0.05029566628528207; 0.0020143800494104966 -0.0008056176767404452 -0.01821974787182387; 0.004257390696885023 0.005991377195988577 -0.02109032921638364; 0.0058353214730504435 -0.0009534243438776523 -0.01318405526280094; 0.0010092181085887906 4.8204370527564835e-5 -0.003490270373156525; 0.0008520643136587815 8.49624582805395e-5 -0.008209109707330181; -0.008333900233992442 0.00024153186639485285 0.0055285893541800355; -0.005794187255611165 0.01443747369152617 -0.004276002266253188; -0.0029222656680315076 0.0034770701224569166 0.006200156239313839; -0.0001834957502037245 0.006856275478874775 -0.0032859808060746653; 0.0007874157606949398 0.00024553470725552156 -0.001270127783107922; -0.004237380545629647 0.011556854807766257 -0.01494317416476956] %
+
+Mass Used: 91.02625740918756 kg
+Launch C3: 97.63741393361927 km²/s²
+||V∞_in||: 1.380801575742508e-8 km/s
diff --git a/archive/ES_0.5662149143146279 b/archive/ES_0.5662149143146279
new file mode 100644
index 0000000..d544bfa
--- /dev/null
+++ b/archive/ES_0.5662149143146279
@@ -0,0 +1,22 @@
+archive/ES_0.5662149143146279---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:04:40.535
+Launch V∞: [7.873109815357973, -6.022476192201201, 0.0372422173491493] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.098891595824285e-6, -1.657145869661753e-6, -1.6732253791176502e-7] km/s
+ V∞_out: [1.412507774145534e-7, -6.603149733505111e-7, -1.8779939220995266e-6] km/s
+ time of flight: 1.800517544840659e8 seconds
+ arrival date: 2030-01-27T12:27:14.535
+ thrust profile: [0.19558903388833865 -0.015274968415529524 -0.07309155521421325; 0.053666350261382605 0.02265306189995981 -0.06549180518234791; 0.07848508143709355 0.0541257898997603 -0.16643821351060473; 0.035907909378761954 0.03041383416810634 -0.1092870430107078; 0.039604910416107066 0.04044071244727948 -0.15895409436966584; 0.019621844480170268 0.019653530435333535 -0.09485611069452411; 0.00672282468055981 0.007902159867058854 -0.042137808274720565; 0.004235971985802711 0.012009642944588905 -0.07051320849219575; 0.004256710030587011 0.007768273023581509 -0.048130956296588465; -0.0006517543272338017 0.002715214226603085 -0.013535999066920625; 0.004403531898663545 0.010913923440795158 -0.02039135570548986; 0.0020198747351688035 -0.0022734705656918134 -0.00875231023850102; 0.007227867671417345 0.004724202219736098 -0.00031167166929211686; -0.0005868569429029012 0.0015233247128262936 -0.0003467188405280267; 0.01834109525191628 -0.001720037277216337 0.003797142221920565; -0.00014356940420026318 0.00010896623564802914 -0.004287549325164935; 0.0018601280027280974 0.008829945535943396 0.008170717552400477; 0.006592255694403077 -0.0012644416213521705 0.028108969419162074; -0.03059366106689239 -0.024492130602749525 -0.03282420947603397; -0.007288435901575216 0.0023398938089019203 -0.0005367606079669154] %
+
+Mass Used: 87.41552300749436 kg
+Launch C3: 98.2574646330694 km²/s²
+||V∞_in||: 1.995417751851347e-6 km/s
diff --git a/archive/ES_0.5662171542918231 b/archive/ES_0.5662171542918231
new file mode 100644
index 0000000..15890b8
--- /dev/null
+++ b/archive/ES_0.5662171542918231
@@ -0,0 +1,22 @@
+archive/ES_0.5662171542918231---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T04:59:43.307
+Launch V∞: [7.913750170750589, -5.777652638005858, 0.24471486541832074] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003224703712083144, -0.002190400427184992, -0.00013458484111210332] km/s
+ V∞_out: [0.0028847601728770596, 0.0012485161099076484, -0.002304436472867228] km/s
+ time of flight: 1.8557719586369416e8 seconds
+ arrival date: 2030-04-01T02:12:58.307
+ thrust profile: [0.33467876444695377 -0.013424028391861199 -0.10113530117932355; 0.11682929751306635 0.058294928122646875 -0.11994164298054662; 0.06110757911214776 0.049383090604717114 -0.11353915526658262; 0.04541107183838379 0.04408082318958945 -0.12078739145108909; 0.02793354625695042 0.02999104498489414 -0.09293738861987226; 0.012756490632531267 0.016268877471619213 -0.06064703076806104; 0.025550336702207598 0.03811284231609595 -0.13882800673454004; 0.0008554226951832059 0.0051601057322184715 -0.015872004325644493; 0.0019406373481589464 0.004634211586849034 -0.01296608870644661; 0.008799379097233509 0.003741957646005595 -0.017448048468849914; 0.00042739487839871075 0.0028177316375316147 -0.008188652214412912; -0.0013789394300995567 -0.0022644355404022086 -0.010491448649095673; 0.0001184982465242874 -0.00042026046016678184 -0.00962849489853243; 0.0004710388881283753 0.0024755281674239855 -0.0038182065853802453; -0.015625193466973122 0.016723890065005367 -0.01065276421867493; -0.01755060276175429 0.00026361076629502055 0.0011052863063782115; 0.002877542992235797 -0.021080680845475635 0.004327010070551052; 0.01420959262749891 -0.002701753859801422 0.003418682210349842; 0.02583709828632053 0.04223222025334454 -0.009858129757218934; -0.025582833293746533 -0.00999526994123895 -0.0064500231935184634] %
+
+Mass Used: 100.18653004789849 kg
+Launch C3: 96.06859713586772 km²/s²
+||V∞_in||: 0.00390060010018871 km/s
diff --git a/archive/ES_0.5662256363703712 b/archive/ES_0.5662256363703712
new file mode 100644
index 0000000..3e9a24b
--- /dev/null
+++ b/archive/ES_0.5662256363703712
@@ -0,0 +1,22 @@
+archive/ES_0.5662256363703712---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T20:07:12.903
+Launch V∞: [6.519800637504277, -7.269305808432339, 0.1789681183911434] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.312968128097634e-7, 6.208864405246915e-7, 6.899283269446192e-7] km/s
+ V∞_out: [9.600847732074166e-7, 5.606180952516382e-7, 1.7651272516798526e-8] km/s
+ time of flight: 1.874957778576714e8 seconds
+ arrival date: 2029-04-07T22:16:49.903
+ thrust profile: [0.4152520021051891 -0.09765754210788224 -0.13506482857628038; 0.06364979414687408 0.018981068735749656 -0.06606069293406128; 0.07896800832886415 0.044730424742109184 -0.1378813296854892; 0.05467706552278974 0.041541866329264904 -0.13426312604732313; 0.03992028495733383 0.03627437664850905 -0.1266431555507125; 0.029594918416310748 0.0308390640746399 -0.11283045404714677; 0.017754418045516293 0.021713428876717233 -0.0826176979020165; 0.014634845101623129 0.019493637930573352 -0.07979591797340486; 0.0021402347846115983 0.003778050805114155 -0.013504126757287677; 0.0005111378623164371 -0.004862094884334428 -0.008974886430434623; 0.0012092220297301149 0.0018109538903537982 -0.0039684831150560455; 0.00019361375887807098 -0.0009003857920143804 -0.0013212355749033927; 0.01002564871418115 -0.0009730696621610031 0.0027434074828246472; -0.00041871290019157483 -3.2243191028778634e-5 -0.0009117061404932387; -0.0013605720582185118 -0.01145329327655906 -0.0021007866717856257; 0.0001090021405667855 -0.0003058010771250149 0.0040680522638186535; -0.0017439406282102688 0.0025419210025182464 -0.003750409704116887; 0.006530331619870254 0.01996717690233182 -0.007710615544770738; 0.0010836085807661856 -0.0052705164288703345 -0.005037727428148119; -0.003913272692470559 0.0043347500634463715 -0.016240938802510506] %
+
+Mass Used: 104.19786065129256 kg
+Launch C3: 95.3826368767098 km²/s²
+||V∞_in||: 1.1225135786313624e-6 km/s
diff --git a/archive/ES_0.5662321374061432 b/archive/ES_0.5662321374061432
new file mode 100644
index 0000000..032c37b
--- /dev/null
+++ b/archive/ES_0.5662321374061432
@@ -0,0 +1,22 @@
+archive/ES_0.5662321374061432---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T18:27:18.460
+Launch V∞: [6.686735477227411, -7.274864919157432, 0.06865394526046877] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012059120530312101, -0.0003785784805598895, 0.008374277184533728] km/s
+ V∞_out: [-0.014066734408164328, 0.00014435368662134174, 0.004216002453830917] km/s
+ time of flight: 1.8749577787493947e8 seconds
+ arrival date: 2029-04-07T20:36:55.460
+ thrust profile: [0.2288915995140484 -0.05169683509988308 -0.07446980003865503; 0.10124306250372091 0.03295977802451384 -0.10260588961050104; 0.042986198881490724 0.025980162748200433 -0.0759600276133268; 0.045228792892352036 0.03801989959472701 -0.11122903646629831; 0.039648357932425125 0.041336504847608334 -0.12479296937448825; 0.020504991945164648 0.02344917558843061 -0.08098327772439816; 0.018460443382401794 0.02495028402860006 -0.09175862884323881; 0.012662833969739343 0.0191022536077736 -0.07256637371672191; 0.015682479482982688 0.028708004807558 -0.09997063226401613; 0.007793462055116218 0.011206241908872363 -0.044661213411637014; 0.0009832625200314755 0.0013795643153851362 -0.008644667844851173; 0.001043249655735831 -0.0009075915658516192 0.00011223807779633683; -0.003313668774021845 -0.0010054846888618292 -0.000697800812822696; -0.002194541253980489 -0.002571070605061516 -0.0028592288433669628; 0.0004729078785585066 0.0003750028270912639 -0.002626236840733193; -0.001836824513687252 -0.00027132014906871334 -0.003026880584037074; 0.0007850328397091164 0.0003192617298151003 0.01027160069401537; -0.001127752996538538 -0.005775739423156042 0.002108602907907105; -0.0021578682050890155 0.0002587909404175725 -0.0025696605614087173; -0.007624584846393728 -0.008639312237915897 -0.009586616701827103] %
+
+Mass Used: 91.03280189867291 kg
+Launch C3: 97.640804298599 km²/s²
+||V∞_in||: 0.014686532197695275 km/s
diff --git a/archive/ES_0.5662369364026315 b/archive/ES_0.5662369364026315
new file mode 100644
index 0000000..49f1854
--- /dev/null
+++ b/archive/ES_0.5662369364026315
@@ -0,0 +1,22 @@
+archive/ES_0.5662369364026315---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T15:49:22.530
+Launch V∞: [7.29117585022951, -6.109404807905493, -0.17728611423780158] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00014599758105109039, 0.00023813222376090388, 2.0937859368674972e-5] km/s
+ V∞_out: [-1.5238883250660999e-5, 7.598753378296057e-5, 0.0002693509241944174] km/s
+ time of flight: 1.684021752045622e8 seconds
+ arrival date: 2029-09-06T18:12:17.530
+ thrust profile: [0.7432172163461025 -0.09839697406485792 -0.22266469592475874; 0.2976898607667871 0.12977788454066067 -0.27883743732341637; 0.06678904117377077 0.05159033720160828 -0.1153679239142292; 0.046070762760078626 0.04813516217229778 -0.11585734906729689; 0.034179227229958725 0.04362195669070996 -0.11382691234953018; 0.04462634308420477 0.06666278680718916 -0.18043802759834432; 0.01133248270295917 0.020074316556926677 -0.06445776476695902; 0.004348389840043185 0.007983028454935415 -0.021325142776899696; 0.00048471699050016865 0.0007818050346147538 -0.004866972979886225; 0.0025498840148399354 0.009620400015286953 -0.03410619431269746; -0.0005860924672665076 0.0015023323162882602 0.0002102176001647321; -0.00020077293912709537 -0.00032444092666055065 0.0014337939108199829; 0.00010134934127360674 -0.0004124626250189467 0.0034939347094249487; 0.0017208467898182566 0.0012343830158632369 -0.00033642001138526234; -0.0005077903386929167 -0.0027062769833149673 -0.0020035358938461827; 0.0003873640205660548 -3.066718074428397e-8 0.0006298693532370858; -0.004823323181336485 -0.001839286532497123 -0.0017896537776998906; 0.0007009557632233726 -0.004850726924293544 -0.0034169846885952248; -0.0002703382577699721 0.0007177978280670732 -0.001517413850886943; 0.005573707134742031 0.002972056525657012 0.005498164698229905] %
+
+Mass Used: 132.59099308230998 kg
+Launch C3: 90.51750275213031 km²/s²
+||V∞_in||: 0.00028010827124707563 km/s
diff --git a/archive/ES_0.5662403062804201 b/archive/ES_0.5662403062804201
new file mode 100644
index 0000000..6470c12
--- /dev/null
+++ b/archive/ES_0.5662403062804201
@@ -0,0 +1,22 @@
+archive/ES_0.5662403062804201---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T14:13:06.527
+Launch V∞: [6.5436248644725685, -7.2865523441118984, 0.137330754969624] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.3711310508240656e-8, 6.372735698796594e-8, 3.478876295009662e-8] km/s
+ V∞_out: [-2.0148872721482487e-8, 3.929860861353391e-8, -6.464455908334412e-8] km/s
+ time of flight: 1.8749577787561032e8 seconds
+ arrival date: 2029-04-07T16:22:43.527
+ thrust profile: [0.3563081244488578 -0.08268373280597517 -0.10822675738539869; 0.09756351090307579 0.032509332818888154 -0.09496505024418377; 0.05519388390765771 0.03385489695478415 -0.09058852355367773; 0.046275620944816374 0.03862687757879102 -0.10644855466624688; 0.03142456053300084 0.03293023415229653 -0.10044287510483502; 0.03195284946695958 0.03822357556289125 -0.1175597538592788; 0.01770875643765957 0.02245367073696241 -0.07431084287883179; 0.01541120089698408 0.023678010052359744 -0.07979749730383259; 0.016968203737409343 0.029200837623808384 -0.09260362053372598; 0.0026932282334344963 0.0022340069865821313 -0.018733391024129672; 0.0019296168266217664 0.0015345068743780727 -0.004740562858225007; -0.002886059217299286 0.0023849873793347137 -0.007380887821262218; 0.0015482945736521366 0.0024446103492006127 -0.001615369351647816; -0.0009036953325095437 0.0002262348015100047 -0.010335501586096923; -0.003164992850349521 0.005231244203702655 -0.004153905853650579; -0.00011141957999489865 0.0074176744084956964 0.0016234528646338897; 0.0032501557521256953 -0.0031502511283560716 0.0032891210755258667; -0.0012778201442059133 0.0076528389321930115 -0.0004573011109646726; -0.001315177682711892 0.0020982990988637797 0.001210312367581623; 0.0028492620566046727 0.015975841821644896 -0.010970366365644905] %
+
+Mass Used: 101.01192552148405 kg
+Launch C3: 95.93173116668676 km²/s²
+||V∞_in||: 8.00492755273443e-8 km/s
diff --git a/archive/ES_0.5662491142666747 b/archive/ES_0.5662491142666747
new file mode 100644
index 0000000..e65ccd9
--- /dev/null
+++ b/archive/ES_0.5662491142666747
@@ -0,0 +1,22 @@
+archive/ES_0.5662491142666747---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T06:25:38.198
+Launch V∞: [6.501796066811516, -7.4970118454374, 0.030351103179633344] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00436300373015133, 6.66740422702198e-5, 0.00019627291511890187] km/s
+ V∞_out: [0.004192262934968868, -4.2113350036459624e-5, -0.0012294272892619928] km/s
+ time of flight: 1.8560264548347217e8 seconds
+ arrival date: 2029-03-20T10:43:03.198
+ thrust profile: [0.2140164224657328 -0.07179940245540892 -0.08709167152928442; 0.02701480258746079 0.0019700520654030466 -0.037106576497704415; 0.07329556720841778 0.02083389455737313 -0.15689861996375104; 0.03999006233851387 0.01512030266590349 -0.11653802668628777; 0.040746915790844634 0.01791035377283271 -0.155420379976394; 0.027630594153360503 0.013612498975802743 -0.12965925372345372; 0.009199365638503742 0.0030612220372083733 -0.047590348709668995; 0.009055556696975737 0.002759586637026568 -0.054377010171781134; 0.006447836389645717 0.005885630032993588 -0.04543430977627128; 0.003814270502825628 -0.0018727563511610704 -0.0287674367918433; 0.002149046298440048 0.0018955574832038385 -0.015948096264688547; 0.0009007187930179201 0.00042239875244647323 -0.007743959515784902; 0.003706860940190954 0.0024626776942136804 -0.005148755398725128; 0.0028626982496153365 0.0013842883194036936 -0.006784713919210473; -0.005919848211047596 0.00464787442081141 -0.009977308604287858; 0.0026475651696732136 -0.007160416566439696 -0.0018995835105183375; 0.0005595824678084993 0.001008572399866614 -0.00811278799690927; 0.0014774255579400669 0.004327166686391781 0.0037642866411045812; 0.002353328645778291 -0.01172670556897135 -0.017124595082418738; -0.011071847397204964 0.002837877294713428 -0.0022373448898179065] %
+
+Mass Used: 86.16045059321186 kg
+Launch C3: 98.47945989449862 km²/s²
+||V∞_in||: 0.004367925140663052 km/s
diff --git a/archive/ES_0.5662622346337174 b/archive/ES_0.5662622346337174
new file mode 100644
index 0000000..a67f7bf
--- /dev/null
+++ b/archive/ES_0.5662622346337174
@@ -0,0 +1,22 @@
+archive/ES_0.5662622346337174---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:34:00.476
+Launch V∞: [7.49777145415946, -5.784068648271616, 0.3633135848482237] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9461949897609533e-5, 1.3663179214623552e-5, 0.001000304830493363] km/s
+ V∞_out: [-0.0009111544537884101, -0.00020052574201629165, 0.0003460057764895862] km/s
+ time of flight: 1.8523900930501553e8 seconds
+ arrival date: 2030-03-22T04:50:49.476
+ thrust profile: [0.6697952718403456 0.023626976725268634 -0.12102897593066236; 0.23219209692057743 0.1646999442610144 -0.15163450819464946; 0.16289777387157559 0.19534767225957736 -0.19119303343559357; 0.07198446696641875 0.12140792574229241 -0.1357344896135271; 0.03559142416139913 0.07849360314911134 -0.0975396228287246; 0.01037783655034607 0.029115071917228775 -0.04069273075957551; 0.011302568568535877 0.03981361442746931 -0.057314596317108786; 0.00010476873688734189 0.002387857629744206 -0.001837255297200829; 0.001771832711395823 0.010114619009277818 -0.016921708712216557; 0.0016792253683302484 0.008541132422092085 -0.01496292488986888; 0.0018934831978748416 -0.0006808886227504646 -0.0037659343517169423; -0.0017856029386893028 0.00276752387560416 -0.003549877441522056; 0.0017186893260954421 0.0019144035506809614 0.0010004992882985493; 0.0006337307705649633 -0.0028181562105857594 -0.004170833455300842; 0.00021409099625348173 0.0023960894853130707 -0.003179228974162192; 0.000686595712111038 -0.0006773006302461071 -0.0009134303176036021; -0.005865182686126667 -0.00022278930726403533 -0.001194382082059588; -0.0012628250343303228 -0.003969300313286448 -0.0034038073514255788; 0.0007256388422919196 0.0016080899214214938 -0.0022188419262380178; 0.0021391494110409586 0.00795009124394886 -0.0006862442380729966] %
+
+Mass Used: 136.7824690113066 kg
+Launch C3: 89.80402366766236 km²/s²
+||V∞_in||: 0.0010005874293975631 km/s
diff --git a/archive/ES_0.5662654688785789 b/archive/ES_0.5662654688785789
new file mode 100644
index 0000000..1d57605
--- /dev/null
+++ b/archive/ES_0.5662654688785789
@@ -0,0 +1,22 @@
+archive/ES_0.5662654688785789---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T01:13:04.931
+Launch V∞: [7.427715550181951, -6.392482114639518, 0.06165906742647188] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.986920138318898e-9, 2.785328580953588e-9, -4.613652027189869e-9] km/s
+ V∞_out: [3.4547060966448313e-9, 7.251137677679289e-9, 2.1070295748072333e-10] km/s
+ time of flight: 1.620285471706519e8 seconds
+ arrival date: 2029-06-27T09:08:51.931
+ thrust profile: [0.3780403937980335 -0.07553405170443077 -0.13988938772416368; 0.08632677226257933 0.02612506414970696 -0.09596792960152015; 0.08518685420171022 0.04612988480666054 -0.15809195718058652; 0.07579859961188397 0.050146375624498106 -0.1969014563010698; 0.05108901618608875 0.03931549196007218 -0.16904414236268264; 0.027623516202156265 0.026192895794245764 -0.1203683914849869; 0.03247547558204771 0.03303846497481321 -0.15532312561729666; 0.005005192333298397 0.005116387132756513 -0.02886771550191238; 0.0031624190372185157 0.003972482924574068 -0.02379903793346503; 0.0026299488046821616 0.002258220544618238 -0.015318449535970079; 0.00035931972387812615 0.000355122251033062 -0.009284512397643224; 0.0021314651590489024 0.0031764923195582197 -0.01730237807130834; 0.0006964077846329809 0.00015893866751169762 -0.0037852961467674125; 0.001399120686646148 -0.0017484367108410712 -0.0032464771431746442; -0.0003631924479569372 0.0005310104521151727 -0.004178902731982269; 0.007912019762289134 0.00718826239905598 -0.0006445720853830873; -0.002781569734109964 0.0034357115473615165 -0.004357243792564658; 0.003619559678633848 0.005761351735200052 -0.0030172442691872477; -0.003552989711951119 -0.0036226818098970626 -0.0038406629960961213; 0.0016354137553823717 -7.299769000550593e-5 0.0031455968879453237] %
+
+Mass Used: 100.41795198586078 kg
+Launch C3: 96.03858772099677 km²/s²
+||V∞_in||: 7.342561732654394e-9 km/s
diff --git a/archive/ES_0.5662670278708793 b/archive/ES_0.5662670278708793
new file mode 100644
index 0000000..e350a71
--- /dev/null
+++ b/archive/ES_0.5662670278708793
@@ -0,0 +1,22 @@
+archive/ES_0.5662670278708793---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T01:39:55.268
+Launch V∞: [6.77316375691213, -7.250328220311386, -0.5778430962853209] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.401394607148933e-6, -7.081544627973352e-7, 1.5500532255866476e-8] km/s
+ V∞_out: [-2.526005165120362e-7, -2.3378118179416534e-8, -5.4402326674542875e-6] km/s
+ time of flight: 1.8577799858534938e8 seconds
+ arrival date: 2029-03-19T06:39:53.268
+ thrust profile: [0.2233907669699183 -0.056832764592476485 -0.08499461713956506; 0.04002027150844419 0.00648308338068741 -0.06499191678674067; 0.050602146155259015 0.023916568161303116 -0.13225387994993582; 0.048106872442790695 0.029139155783772703 -0.17214881565465884; 0.023918722866314763 0.015237226558652572 -0.12491700664613094; 0.02031941490458258 0.01091118261100036 -0.1254460358417471; 0.010462340610188647 0.006165698972306766 -0.07587082884728888; 0.007670833661734065 0.004379578321051832 -0.04593410390786107; 0.006379045430892319 0.0036529647805514077 -0.04621610567018895; 0.004914837620717313 0.003190348619878223 -0.02761332881922597; 0.003632030767143824 0.0024967252894473936 -0.01918269462935846; 0.001608422541635179 0.0013219249928170813 -0.006704146768888681; -0.0008254552687078818 -0.000525775872556269 0.0020792450394451737; 0.00041304710190774 0.0002828423776039591 0.0006615483647301121; 0.0014737656575999352 0.0007462238189650912 -0.0016871230692291762; 0.0014546796523493707 9.327736874497537e-6 0.0017524564854755947; 0.0005684401032747856 0.0004592279847207858 0.00013769304003110596; 0.00010630852241379354 0.00010045017498593768 0.0005819455952330169; -0.0001833276757039991 -0.0001433497920329075 -0.0032020873140754555; -0.0005018882321480593 -0.0001685639446538064 0.0011367281353493435] %
+
+Mass Used: 84.44622870868079 kg
+Launch C3: 98.77690922411631 km²/s²
+||V∞_in||: 5.4476404719674346e-6 km/s
diff --git a/archive/ES_0.566271536782522 b/archive/ES_0.566271536782522
new file mode 100644
index 0000000..127fd0e
--- /dev/null
+++ b/archive/ES_0.566271536782522
@@ -0,0 +1,22 @@
+archive/ES_0.566271536782522---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T10:34:33.475
+Launch V∞: [7.5072606383980105, -6.350116596222346, -0.17604881906521846] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3698738684857038e-8, 2.9715672145919723e-8, -1.0906698273966597e-7] km/s
+ V∞_out: [-3.411028973967394e-8, 1.0456196131891427e-7, -1.8539712964042605e-8] km/s
+ time of flight: 1.626189788556862e8 seconds
+ arrival date: 2029-07-03T14:30:51.475
+ thrust profile: [0.3185864160958903 -0.05072842423172202 -0.1118186795519223; 0.08059495255090554 0.028996208211253087 -0.08745990294753868; 0.05547859218025323 0.03535033545180441 -0.10195985780100136; 0.08900655891054694 0.07750384224016724 -0.22333039216944048; 0.039477009701975825 0.040132875554138484 -0.1317460607091713; 0.035770802370850306 0.04259469830058214 -0.14758196406272658; 0.03586020238497134 0.047591234975000965 -0.1732131153986931; 0.010828987457532663 0.014564504005133965 -0.059125123910608486; 0.0016289944469981882 0.0008231206333478044 -0.007721093481697808; 0.0009920292325589894 0.001101767916333091 -0.0052735475373672; 0.004582325939044139 0.008560161892341827 -0.03447380242347163; 0.00256872391827525 0.004739511074876211 -0.02079745485580202; 0.003965703911020146 -0.0008786196092170353 -0.0023782588490415166; 0.0011170657859859115 0.0006147680327391289 -0.002896016561388861; -0.003086851238131774 0.003619922265883683 0.0004829379059540849; -0.0055393395133540605 -0.0015540601979559896 -0.0014927977313907081; 0.00039561288646976765 0.0007955546086766587 -0.003371032485076254; -0.0005206333618692164 -0.0014715506177903842 0.00015149027181619173; -0.0011975569328793031 0.002433826240878195 -0.009228211113362217; 0.0017083869777228659 0.0014968021438576651 -8.569923862991255e-5] %
+
+Mass Used: 96.48549803288415 kg
+Launch C3: 96.71393626515284 km²/s²
+||V∞_in||: 1.1386958916486167e-7 km/s
diff --git a/archive/ES_0.566274975618521 b/archive/ES_0.566274975618521
new file mode 100644
index 0000000..a96be10
--- /dev/null
+++ b/archive/ES_0.566274975618521
@@ -0,0 +1,22 @@
+archive/ES_0.566274975618521---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:45:33.841
+Launch V∞: [7.332305474445906, -6.37814011450935, -0.16499632113277196] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8122795558176647e-8, 3.6102467223515016e-8, -1.4428207441455235e-7] km/s
+ V∞_out: [-3.927264566691537e-8, 1.389277704580317e-7, -2.10446820306356e-8] km/s
+ time of flight: 1.6429824099613386e8 seconds
+ arrival date: 2029-07-23T14:09:33.841
+ thrust profile: [0.5052275961794055 -0.07177644372726476 -0.15822500156540756; 0.10124131067820046 0.044222028837686445 -0.10773398886430818; 0.06115312169603134 0.046090183355133874 -0.11343532636441836; 0.07303782677998721 0.07614944976064003 -0.18849363229684818; 0.036145744484832716 0.04281781116256302 -0.12279668592520249; 0.02767029517274335 0.041546641804059856 -0.12335648401141397; 0.013139414933178523 0.018463725442452554 -0.06634739802229708; 0.008583817878019002 0.014318948786151283 -0.054727523326656695; 0.017865209756794433 0.03515726029641494 -0.11789402211951189; 0.0011530487649957478 0.002944239271819073 -0.009150431770491022; 0.006763645162835527 0.015099764716305558 -0.059528776747763516; 0.0007135288524139971 0.001572714739570301 -0.00918947783081308; 0.001995856980125714 -0.00031868539357272864 -0.0008202460884372759; 0.0020950081046312557 -0.0004147726189895143 -0.0013989415639860028; 0.0003423090645228499 0.0012698311478312558 -0.002066086198525558; 0.0032523585061708907 -0.0016882968805730536 -0.0008761997854612109; 0.0011277343081017516 0.0030610046219488266 0.0033939832897232312; 0.0007504737244420189 -0.004522966007568617 -0.003104417107070487; 0.0021756402846970606 -0.0027610310963903143 -0.0030338459712063344; 0.002610935243136277 0.0008982456404839058 0.006536409317551625] %
+
+Mass Used: 109.57564593974894 kg
+Launch C3: 94.47059867689009 km²/s²
+||V∞_in||: 1.4983037360907457e-7 km/s
diff --git a/archive/ES_0.5662904316513523 b/archive/ES_0.5662904316513523
new file mode 100644
index 0000000..ed373a3
--- /dev/null
+++ b/archive/ES_0.5662904316513523
@@ -0,0 +1,22 @@
+archive/ES_0.5662904316513523---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:39:41.699
+Launch V∞: [6.463342118856671, -7.542409191115915, 0.033412794106365426] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.223651153761223e-6, 9.194058278866952e-7, -2.054987224775705e-8] km/s
+ V∞_out: [-2.1667626307867186e-6, 5.2192229119923744e-8, 6.952184835196223e-6] km/s
+ time of flight: 1.8237137416237813e8 seconds
+ arrival date: 2029-02-08T21:22:35.699
+ thrust profile: [0.1293477580586018 -0.03659649498999898 -0.053333933575341615; 0.08973717614398954 0.01795833276218129 -0.10248044858761103; 0.07046526317046033 0.0288530653673403 -0.1308305156722957; 0.058381685320186144 0.03171908648362747 -0.15018244829317146; 0.03431190153062316 0.020680716075951715 -0.11088933897638036; 0.02306359463272757 0.01714144052003421 -0.093723691257706; 0.018488430878781794 0.015275123021392995 -0.08915879734386858; 0.021128406877567067 0.017568435462210586 -0.10890235849988064; 0.007244067248694005 0.007558128101711262 -0.04805617056270824; 0.00339729631005718 0.0038894127946523596 -0.02579215740403058; 0.00159669268084447 0.0025960066418825862 -0.01602040841762014; 0.004281978683442848 0.0019523756651736272 -0.0018312211147773413; -0.004232965814900932 -0.0019293569157856107 -0.0007160622475900469; 0.0008721942553048648 -0.001510522045400794 0.0032301005509120405; -0.00570733930409778 0.0004253106541917056 0.00239607763465031; 0.001662223113358099 -0.008913918820212668 0.004288209035130558; -0.0010581164359746767 0.0004470092294641053 -0.001831030007963328; 0.008479371799267566 0.007925806074765309 -0.0082451765819429; 0.012781476328224947 0.0010153334769472293 0.0029058834303570605; 0.0017020511914459715 0.0006407647811541291 -0.0025571510339994228] %
+
+Mass Used: 85.13307928908989 kg
+Launch C3: 98.66384416642647 km²/s²
+||V∞_in||: 7.281954776352107e-6 km/s
diff --git a/archive/ES_0.5662906037361493 b/archive/ES_0.5662906037361493
new file mode 100644
index 0000000..3565dde
--- /dev/null
+++ b/archive/ES_0.5662906037361493
@@ -0,0 +1,22 @@
+archive/ES_0.5662906037361493---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T01:27:15.444
+Launch V∞: [6.119952806666619, -7.434898596598426, 0.12410883959355071] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010697850139360931, 0.0009386769733496507, 0.001123864482615223] km/s
+ V∞_out: [-0.001238080601500184, -0.0006301953128626332, 0.001165460548231829] km/s
+ time of flight: 1.8109594510626847e8 seconds
+ arrival date: 2029-01-21T01:53:00.444
+ thrust profile: [0.5720453037307975 -0.15940630197473643 -0.13793342621793517; 0.08313871486169057 0.027804879679821412 -0.07308029042275284; 0.10687858925601047 0.06722748086726615 -0.14325790031444588; 0.06305993619198257 0.05523957169382722 -0.12536655176754957; 0.06348693995832506 0.06839163938840952 -0.15465132875928306; 0.03869721613831622 0.04969729811565039 -0.11947649190666854; 0.018939311633638493 0.024721664420399216 -0.06570399561012778; 0.01120650839925416 0.0182686865106466 -0.05024299750568626; 0.007301086943404541 0.014667173972765275 -0.04274395561740396; 0.00700955746654325 0.017152511641125082 -0.044035890448373874; 0.004229004187280979 0.008660503885948231 -0.02720160001648665; -0.002925308795917871 5.1692981294879114e-5 3.007780411295102e-5; 0.0016953377589372218 0.0005331286808863175 0.0005077520666267321; 0.004031436204502837 -0.0007580685857516698 -0.0009990952632984895; -0.00021351354379898655 0.0039673179102201256 -0.0013776586821120122; 0.000632770461457067 0.0002795426750698207 0.0013945699923088228; 0.0007978753438007409 -0.000477806919705832 -0.0012430795467756597; 0.0008525703931496847 0.0017412478414121967 -0.003261534327246461; 0.0001886041770274615 0.0018972156218049847 7.85862183228462e-5; 0.00511942710367018 -0.00147378417087439 0.003243667089621345] %
+
+Mass Used: 119.64853976621407 kg
+Launch C3: 92.74694250159314 km²/s²
+||V∞_in||: 0.0018134568678695093 km/s
diff --git a/archive/ES_0.5662920877568121 b/archive/ES_0.5662920877568121
new file mode 100644
index 0000000..2ed5775
--- /dev/null
+++ b/archive/ES_0.5662920877568121
@@ -0,0 +1,22 @@
+archive/ES_0.5662920877568121---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T07:04:04.217
+Launch V∞: [7.490933622967947, -6.023530050620871, -1.104873308689161] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1096296651746379e-5, 7.763703908365608e-6, 4.879609083746029e-7] km/s
+ V∞_out: [-9.89557096047222e-6, -4.37028114951202e-6, 8.200126003061932e-6] km/s
+ time of flight: 1.8749577787227467e8 seconds
+ arrival date: 2030-04-25T09:13:41.217
+ thrust profile: [0.6576482988279143 0.019911221645126723 -0.2068121547546138; 0.11663837779095163 0.07318846786239118 -0.13416064216776266; 0.08176708855297572 0.07999916800096786 -0.15736794834165727; 0.026882915992446774 0.03583697757250555 -0.09052891564416032; 0.012512236224618745 0.021324433280940323 -0.060746941100989355; 0.01846507227493348 0.0369060848924194 -0.1157159371341872; 0.006959831251754301 0.019186034258797037 -0.06268062172409263; 0.0035571523456158194 0.011225103983763005 -0.038460628000764226; 0.0012055460782068933 0.004953580888037195 -0.02012537220640166; 0.00025124071012759867 0.001111958468187462 -0.0052694380710215614; 0.0005694879606004533 0.0003214496107456835 -0.0020343592500921574; -6.271041940458105e-5 0.0014061550411542964 -0.005408205859185752; -0.000950899370149097 -0.0025757455122519665 0.0006353606769599421; -0.00030473951492629024 -0.00040142317407371235 -0.0012565553806974704; 0.004846909995768226 0.0003615825485301195 -0.0024394126885957886; -0.004122047660046545 0.0014601630965985816 -0.0018595679390917674; -0.00018764467498612363 0.0014297390013003214 -0.0036310801799250845; -0.0005722863907777999 0.0001760817185080429 -0.002446591627536729; 0.002465951469855317 0.0046496736604933805 -0.0005792782640351363; 0.0006671351041777475 0.0024387686022875354 -0.000280427133922433] %
+
+Mass Used: 114.57058496720856 kg
+Launch C3: 93.6177458426981 km²/s²
+||V∞_in||: 1.3551420722877402e-5 km/s
diff --git a/archive/ES_0.5662930686585494 b/archive/ES_0.5662930686585494
new file mode 100644
index 0000000..57ee1d1
--- /dev/null
+++ b/archive/ES_0.5662930686585494
@@ -0,0 +1,22 @@
+archive/ES_0.5662930686585494---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T01:31:52.139
+Launch V∞: [6.478765157259742, -7.236190715268668, 0.1880166319886586] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.568431310653836e-7, 0.0001891184379850661, -0.0001275617424976587] km/s
+ V∞_out: [-0.00011528584640341694, -0.00019246356218157777, 4.071878535432651e-5] km/s
+ time of flight: 1.87495777874566e8 seconds
+ arrival date: 2029-04-05T03:41:29.139
+ thrust profile: [0.41144595101991954 -0.0810217198079987 -0.1042521715044898; 0.18598516753697933 0.0732210117240092 -0.14668646022722215; 0.0833370772822901 0.05980913220517543 -0.11412256433996054; 0.06331074237225517 0.06085337900954787 -0.11993536503803662; 0.044143007687964655 0.05657038916694419 -0.11474431479435282; 0.03169769866189197 0.04625065927704221 -0.10131554353141164; 0.027248209762703403 0.045499481711537164 -0.10235403926249163; 0.008989553318743182 0.01697346230255237 -0.041484817863586765; 0.007130050993470985 0.01494887780276493 -0.03747529152348983; 0.003362246497771379 0.008064938681631507 -0.021085459604965755; -0.0007119947227851741 -0.00015093690198965956 -0.0016564893513654863; -0.00017209669153760593 0.0004620312443209058 -0.0006134327888715008; 1.08273416327327e-5 -0.00044392865516635575 0.00045417223098128973; 0.00037023030270167274 -0.00042833899486465003 0.0007152846591582798; -0.0008153545846075886 0.000610945766969368 -0.0005822726497696832; -0.0010037030603157484 0.0018214216501000339 0.0006766300778541033; 0.0032726018153348925 0.001627446287428958 -0.0004274026931449558; -0.001091349396338178 -0.0006999743068490001 -0.0013257645105526255; 0.0006840457839608243 0.0001419169863186709 -0.0004205037817912793; 0.002699094325908284 0.0014419616073743102 0.00215566367155705] %
+
+Mass Used: 110.17072177499631 kg
+Launch C3: 94.37220428456767 km²/s²
+||V∞_in||: 0.00022811859154664026 km/s
diff --git a/archive/ES_0.5662981691512404 b/archive/ES_0.5662981691512404
new file mode 100644
index 0000000..5752a2d
--- /dev/null
+++ b/archive/ES_0.5662981691512404
@@ -0,0 +1,22 @@
+archive/ES_0.5662981691512404---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T11:01:12.876
+Launch V∞: [6.6373343089634185, -7.431307745181781, 0.13094328240610933] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.340200805795266e-9, -1.0055076078841791e-8, -7.039244563728494e-9] km/s
+ V∞_out: [4.033391495689285e-9, 2.631704868774112e-9, 1.3276669575551895e-8] km/s
+ time of flight: 1.874957778739551e8 seconds
+ arrival date: 2029-04-10T13:10:49.876
+ thrust profile: [0.11087397784791532 -0.02681554063741048 -0.040546186744146014; 0.0689490570223792 0.01989162633816419 -0.07580619741650406; 0.042840900103495484 0.02181902668663501 -0.08001680936779194; 0.032262757600090446 0.023955604517851413 -0.08074542753177098; 0.03897436376363712 0.033519046576104106 -0.12798962318754661; 0.04237766047084811 0.041041377289959886 -0.16433803814464376; 0.01955477765632273 0.018577106831132586 -0.08778401672728943; 0.012536852935996467 0.0172956623622884 -0.06784693027015794; 0.005437845202611742 0.004180273300972733 -0.031486489211094; 0.00911306586019168 0.011495906716046868 -0.061018416240756206; 0.0002453307499167335 0.0032425084554199316 -0.01952175357918501; -0.0024894222704325416 -0.0006287045755597187 -0.003778173885057786; -0.0030725882042823725 0.005610761059807099 -0.010918504033742546; -0.0013219172039565983 -0.003401026531335156 -0.00851819401368765; 0.002773693000547769 -0.007138667478214015 -0.00232673495868267; 0.001287939159511582 0.008125964899201338 -0.0036286765196617762; 0.010182186333037094 -0.015660115404637222 -0.007286203986427942; -0.012098722110904896 -0.0004650355635703238 0.0017779238158569782; 0.005376012419156278 -0.007297032724934012 -0.001633525185329389; 0.0028933574779029343 0.0009614231653449336 -0.006081176648830951] %
+
+Mass Used: 81.45635256791184 kg
+Launch C3: 99.29568767574891 km²/s²
+||V∞_in||: 1.338556175980276e-8 km/s
diff --git a/archive/ES_0.5663143463172544 b/archive/ES_0.5663143463172544
new file mode 100644
index 0000000..19a8009
--- /dev/null
+++ b/archive/ES_0.5663143463172544
@@ -0,0 +1,22 @@
+archive/ES_0.5663143463172544---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T15:20:39.171
+Launch V∞: [6.62080363728513, -7.438728048123627, 0.055608901512022274] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011631431891771453, -0.000365367834391452, 0.00809239657844218] km/s
+ V∞_out: [-0.01380623040217772, 0.00010391015933423165, 0.0032042986089271907] km/s
+ time of flight: 1.8749577787493908e8 seconds
+ arrival date: 2029-04-10T17:30:16.171
+ thrust profile: [0.14324642401853915 -0.036113212062861395 -0.05564392005387026; 0.034284331499049844 0.008826698180154241 -0.03983033526300857; 0.036199734213970984 0.018336351849716416 -0.07179318034737636; 0.04462573828429956 0.030430878306780457 -0.1200670745469141; 0.04411268802791793 0.03431844011630041 -0.14864656493194894; 0.027562467707310863 0.025610207369424435 -0.11615867769353623; 0.027571088616305844 0.04480622180387142 -0.16603481897485103; 0.00642377916033904 0.007521235443658252 -0.039193439569865075; 0.008945028057056685 0.009691102299323863 -0.06021397572106797; 0.0025852874413041216 0.003775033672833903 -0.021705131245661726; -0.00019522866034867904 2.6939933310354115e-5 -0.00093509997114372; 0.0010258333461631256 0.0014792563975753884 -0.009006112802014863; 0.0015543876016702448 0.0007401721971129378 -0.004798426594863436; -0.0021773970337742097 -0.0008707122541709793 0.005170945810389082; -0.001808193127631832 0.0028436522888350383 0.0014110209903335307; 0.01008157424932905 0.0031060095456397208 -0.006314535597352053; -0.0024983029994885895 0.010201544119541639 0.0024965555422611194; -0.015562187955896395 -0.002799981578888108 -0.0006471147135353221; 0.007982244486537367 -0.006513845522972031 -0.017834715917721365; -0.00691787507217314 -0.009404319251582048 -0.003607882003838926] %
+
+Mass Used: 82.19202329388372 kg
+Launch C3: 99.17280812735653 km²/s²
+||V∞_in||: 0.014174293064915395 km/s
diff --git a/archive/ES_0.5663148955065705 b/archive/ES_0.5663148955065705
new file mode 100644
index 0000000..c2e3ec4
--- /dev/null
+++ b/archive/ES_0.5663148955065705
@@ -0,0 +1,22 @@
+archive/ES_0.5663148955065705---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T20:28:25.316
+Launch V∞: [7.469118934225349, -6.374713195093774, -0.351855840557983] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9585013830822242e-5, -2.429951172588807e-5, 8.55032555808231e-6] km/s
+ V∞_out: [1.801419785068322e-5, 3.097071291400525e-5, -1.9532298472450957e-5] km/s
+ time of flight: 1.6200705506612837e8 seconds
+ arrival date: 2029-06-26T22:26:00.316
+ thrust profile: [0.3302002872077492 -0.06871821095381189 -0.12689452942290488; 0.07892294315062384 0.022750662670847323 -0.08973558134040023; 0.10372182544194557 0.054830845261667004 -0.19977382689442577; 0.08184002544523107 0.056381111619876585 -0.22238169010902464; 0.05608204341228361 0.045369773303818764 -0.1956073716698722; 0.03652785684678085 0.033100087227963364 -0.1546893738741903; 0.013452651318465705 0.01358816666290877 -0.06799274449468788; 0.0016873852098017626 0.0041477529872557435 -0.010840638241804899; 0.0026451236016301616 0.003265983073110675 -0.013415731631750886; -0.001950013983699784 0.0012720256927685745 -0.0057310222880209375; 0.0021046841775339926 0.0032535239230913043 -0.019240650135392792; 0.0054752978290945695 -0.0038970409358236105 -0.008552493357247932; -0.002006443744502558 -0.0018977375991265405 -0.003184582508684745; 0.0018050048160430958 0.0040153685701922485 -0.005118099612765947; 0.001701326523419957 0.0008281974982317075 0.00016205986986440272; 0.0017255301215995957 0.00336384605735058 -0.0006398540456015438; -0.0025699214370365196 0.000516929678806553 0.0025751954091248795; 0.0029869477845787477 0.0017106592130855388 -0.010497729723560018; 0.00030832776389158964 0.0005201832735090193 0.004229839660451059; -0.010691880400648626 -0.001716622439435104 0.009664757957218464] %
+
+Mass Used: 97.50107847359277 kg
+Launch C3: 96.54850850584106 km²/s²
+||V∞_in||: 3.922814526122425e-5 km/s
diff --git a/archive/ES_0.5663182957689787 b/archive/ES_0.5663182957689787
new file mode 100644
index 0000000..1897dfe
--- /dev/null
+++ b/archive/ES_0.5663182957689787
@@ -0,0 +1,22 @@
+archive/ES_0.5663182957689787---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T15:35:40.394
+Launch V∞: [6.100638177898346, -7.438383016202471, 0.10915900523593865] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8565301932515397e-7, -3.943023723605345e-8, 5.342577466007109e-8] km/s
+ V∞_out: [-1.950816688188987e-7, 1.8687568910420568e-8, -2.522266059179099e-8] km/s
+ time of flight: 1.7903848775781888e8 seconds
+ arrival date: 2028-12-27T20:30:27.394
+ thrust profile: [0.5936598828271094 -0.1677080717942005 -0.17455888547672746; 0.12788010579269843 0.03500588500896 -0.11932568606941665; 0.10041031515579248 0.056070768453928485 -0.15021209021981974; 0.06658744397738778 0.051474932924192106 -0.1405294734535355; 0.02383617038015161 0.021940503213800394 -0.06789604640162421; 0.04088629663454882 0.04559450431937688 -0.14028869466127283; 0.01630575907197854 0.020312849889499437 -0.0663619042447988; 0.018782734953877857 0.022275404875588073 -0.07890407241798837; 0.012940451747109727 0.01969744359026328 -0.0682395340764734; 0.005700015800275767 0.006196165565538774 -0.02757986780552668; 0.00044961283546925384 0.00022687541884303087 -0.0030862094449245958; -0.0011383941733290632 0.0020124545710276413 -0.001339264931688634; -0.0022677644077744984 0.0018290177421892598 -0.00017805628772660925; -0.00275655193600188 0.0021716448236193432 -0.0022644598108138795; -0.0012142404817328957 -0.000806834734503589 -0.0009518449529428005; -0.00040777232179712295 -0.001558284009909663 -0.002006980800938807; 0.0009515011660615133 -0.00216164460530159 -0.0017179239424300772; -0.000504148881612837 -0.0015333255668226033 0.00259246144508814; -0.0021970750779232223 0.008745006301405709 -0.001799784896184342; 0.001238304783592018 -0.004348564534623194 -6.974465822776575e-5] %
+
+Mass Used: 120.77575645339994 kg
+Launch C3: 92.55924376178433 km²/s²
+||V∞_in||: 1.9717023251765503e-7 km/s
diff --git a/archive/ES_0.5663322401511072 b/archive/ES_0.5663322401511072
new file mode 100644
index 0000000..81ee067
--- /dev/null
+++ b/archive/ES_0.5663322401511072
@@ -0,0 +1,22 @@
+archive/ES_0.5663322401511072---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T08:53:46.238
+Launch V∞: [6.524810482372535, -7.427523685990371, 0.13995994674448645] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1621688240651729e-6, 0.0003582609705503363, -0.0002484284284291131] km/s
+ V∞_out: [-0.00019515350803199865, -0.00038230801693791357, 7.702393721591323e-5] km/s
+ time of flight: 1.8749577786995608e8 seconds
+ arrival date: 2029-04-09T11:03:23.238
+ thrust profile: [0.19965079483153578 -0.04152073768790288 -0.06448040566665249; 0.08525594383131738 0.02858632663599232 -0.08214032588658242; 0.0417179080049678 0.026121429876382364 -0.06862432710771421; 0.05001096840645332 0.04122478326480331 -0.11274793956977333; 0.039786379015173616 0.04076683836995635 -0.11523406554176917; 0.053641540718501926 0.06496544750662006 -0.1843338880294626; 0.014114664877003988 0.019654504001785242 -0.06263887069136377; 0.02720214901626314 0.04221074687078234 -0.13300793429215085; 0.004431639369323436 0.008355783433840528 -0.029241926647555525; 0.002684494104437251 0.0009719172534058277 -0.009583049251618929; -0.003754104624876854 0.0014807021202771996 -0.0037703156839789306; -0.0012006141239563413 -0.0008809973514584669 0.0019181763161837228; 0.0004968999513869613 -0.0023924434691797035 -0.0020022749811798466; 0.00042309183556910496 -0.0021316983295684333 0.0011363409152202381; -0.005605155423361274 0.0007690366831093611 -0.0032926498777691724; 0.009364073097651908 0.013285411851144256 -0.0007894609646450616; 0.001229452329083541 -0.00383042242404429 0.004590959432024128; 0.000560483101850524 0.0009435322584506745 0.0010584471578221576; 0.0036510087348070024 -0.009576067032983622 0.00843706386641423; -0.011612845260617566 0.015216308037147524 0.012341439017052563] %
+
+Mass Used: 90.44932928909611 kg
+Launch C3: 97.76084872351923 km²/s²
+||V∞_in||: 0.00043596898709404036 km/s
diff --git a/archive/ES_0.5663396050432679 b/archive/ES_0.5663396050432679
new file mode 100644
index 0000000..26207ce
--- /dev/null
+++ b/archive/ES_0.5663396050432679
@@ -0,0 +1,22 @@
+archive/ES_0.5663396050432679---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T04:18:09.957
+Launch V∞: [5.766110617662817, -7.5203053420072115, 0.19679694236374878] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01108039426574967, -0.00511388328654573, 0.012749714732737574] km/s
+ V∞_out: [-0.010998994380510245, -0.004935744137534692, -0.012873002110505379] km/s
+ time of flight: 1.7079902165729994e8 seconds
+ arrival date: 2028-09-21T00:28:30.957
+ thrust profile: [0.7976385548773928 -0.2960376637580536 -0.24958740559127687; 0.21638927027537752 0.03842542531698972 -0.20202295773640686; 0.08963409787358187 0.03837508490718571 -0.14111422788233843; 0.07510961901495605 0.04620697405586636 -0.1618852317793854; 0.04679743683358939 0.03433195670313722 -0.1284268858344777; 0.057038572874202415 0.04921513622097807 -0.1853089721981016; 0.01922797135637311 0.019236238475343226 -0.07570915236301697; 0.0040880303465208835 0.0044230334957698686 -0.018612217018356025; 0.0021178349355690717 0.0024400813129181543 -0.011089129112326103; 0.0007535465376179386 0.0007765800209568048 -0.004305152279722882; 0.0005238541998817119 0.0010272416222937154 -0.004332593945727079; -0.00011654809368985432 4.0084672779054246e-5 -0.0008464653882297112; -0.0003186560987369174 -0.0004456304250966815 -0.0007207130858858048; -8.626767624915062e-5 0.0003142773785135323 -0.00013391824708688092; -0.00041671432282008625 -0.0001405578541915488 0.00023587740269500452; -0.00014955042863937657 -0.0001704767405737346 -7.475822175669273e-5; -0.0007223714078394471 0.00041780970127407836 -0.000799793041007667; -0.0002776444820950584 0.00020351634387015018 -7.380496270240641e-6; -0.0007281672328182434 0.00046221396784015774 -0.0008496814878458251; -0.0005747370541991542 0.0006693342028279668 -0.000852237443181125] %
+
+Mass Used: 136.65264596657198 kg
+Launch C3: 89.8417531286698 km²/s²
+||V∞_in||: 0.017648857331823368 km/s
diff --git a/archive/ES_0.5663551290263107 b/archive/ES_0.5663551290263107
new file mode 100644
index 0000000..5349c31
--- /dev/null
+++ b/archive/ES_0.5663551290263107
@@ -0,0 +1,22 @@
+archive/ES_0.5663551290263107---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T04:47:07.956
+Launch V∞: [6.468395875051202, -7.355266001030065, 0.1117714435435262] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.17652507251108e-7, 3.5300414039419837e-6, -2.2202242196879665e-7] km/s
+ V∞_out: [1.1640760730177093e-6, -2.982624446911402e-6, 1.5895691049945562e-6] km/s
+ time of flight: 1.8528610390902936e8 seconds
+ arrival date: 2029-03-12T17:08:50.956
+ thrust profile: [0.34391591148651673 -0.08378613962772445 -0.10756510776642585; 0.08246943212257513 0.025181385360137996 -0.08016549457512143; 0.07321181574062051 0.04224960593786328 -0.11801528451107708; 0.06529436400518124 0.05199447315822911 -0.1480127551010035; 0.02781538412555234 0.027079137930527363 -0.08256675746428613; 0.04589767887279544 0.050593223135467096 -0.15994165645084607; 0.02538646939835103 0.03148624768390591 -0.104786338673427; 0.010034911456488016 0.016402172956380957 -0.0527897650447121; 0.0059810096548590696 0.011175530609958118 -0.03516721494085487; 0.002220913775447932 0.00380202764978219 -0.017010514933819828; 0.0006411457357737734 0.0008670744663300542 -0.010104797813136881; 0.0012243413382825486 -0.0023932790385071496 -0.0017451945615233888; -0.009302778223385837 -0.0026248275902892937 -0.0020058401913665104; -0.0061098625674841055 0.0033302417773698467 0.0006903379406960073; 0.0019994715795968268 0.0060233000963708875 0.0024819992103229634; 0.004592331193232947 -2.519667636307894e-5 -0.00232476585786601; -0.009536661235083125 -0.0022176122593320713 -0.004926297123404012; 0.0009799313541571989 0.0020564204333927837 0.002883696924796992; -0.0018895969674887188 0.00021787107211333528 0.006506269134257477; -0.003580547456135135 0.010618248543769936 0.008844963427222722] %
+
+Mass Used: 101.0242905430623 kg
+Launch C3: 95.95257599788002 km²/s²
+||V∞_in||: 3.5746958454762188e-6 km/s
diff --git a/archive/ES_0.566357664019779 b/archive/ES_0.566357664019779
new file mode 100644
index 0000000..893b0f9
--- /dev/null
+++ b/archive/ES_0.566357664019779
@@ -0,0 +1,22 @@
+archive/ES_0.566357664019779---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T19:56:12.997
+Launch V∞: [7.565313190507022, -6.370841006667332, -0.1752953840918118] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006210964677743578, 0.0003864127620119205, -0.00018436647199069077] km/s
+ V∞_out: [-0.00029615717624395185, -0.0005845190325288681, 0.0003736670683846764] km/s
+ time of flight: 1.6504954900394794e8 seconds
+ arrival date: 2029-08-03T03:02:01.997
+ thrust profile: [0.2436924331902289 -0.04589418972116413 -0.09527831874296999; 0.06817023039931977 0.02044824699942697 -0.08043232419027126; 0.0512281612186612 0.026705422776653404 -0.09888856156173331; 0.050162604538161584 0.03387796090317274 -0.13671498007959396; 0.04158972150656457 0.03189784631340478 -0.14603994913427049; 0.04105812264453594 0.036407703760294695 -0.1754374242846388; 0.023791500794138578 0.021766290077416248 -0.11918223658788198; 0.015469729425341857 0.015808393869865715 -0.09163791006478364; 0.007048652873995602 0.0010699466922837115 -0.03721451622734259; 0.003739044887382578 0.0044534408574213695 -0.02267909312806732; 0.0025123227409001416 0.0018583398574314924 -0.01690953561066117; 0.001457863710424525 0.0026375531648574857 -0.012570667102793687; 0.0014312467331103183 0.0006834849010083645 -0.0028668337563764303; 0.0024066556341354284 -0.004155303062894001 -0.024415492567398847; 0.00947962304225581 -0.007731327844101115 -0.013235027793083078; -0.0036112812943638974 0.002777534881352283 -0.00794773308345631; -0.0005004706373289809 -0.0001612898186591355 -0.0008789291853662146; 0.003659421571013368 0.0010173094613888545 -0.0037368822376084307; -0.0009885520464321847 -0.0031788478002458577 -0.007209438642608369; 0.007832568527021654 -0.01106553932108206 0.002101233553179876] %
+
+Mass Used: 89.94548225587369 kg
+Launch C3: 97.85230727437747 km²/s²
+||V∞_in||: 0.0007543650581262093 km/s
diff --git a/archive/ES_0.5663718429054283 b/archive/ES_0.5663718429054283
new file mode 100644
index 0000000..a638217
--- /dev/null
+++ b/archive/ES_0.5663718429054283
@@ -0,0 +1,22 @@
+archive/ES_0.5663718429054283---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T19:27:23.368
+Launch V∞: [7.562404497508174, -6.065520855368055, -0.5822577233965928] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00017408341462180733, -0.00011444415310928335, -0.007055588250191898] km/s
+ V∞_out: [0.0065771920695404384, 0.0023325293176834163, -0.0010631210530497254] km/s
+ time of flight: 1.8749577782604071e8 seconds
+ arrival date: 2030-04-21T21:37:00.368
+ thrust profile: [0.30913065195688355 0.03271976821538586 -0.07196146100418647; 0.152856635034958 0.12556864415693053 -0.10533229364931997; 0.1106618322020698 0.15486333190899182 -0.13892085644716606; 0.0716184012928483 0.14438158675091306 -0.14160961240733896; 0.03942311586515499 0.10973873245253415 -0.11648414582440055; 0.0213277289095877 0.0799501880944169 -0.09251458831454727; 0.013253897188105967 0.06788404422939463 -0.08307784509221153; 0.0047455544984253825 0.032843156392237824 -0.04462222530514052; 0.0009970022657000762 0.010619328144585499 -0.015318033974664184; 0.000446548635614544 0.00047580281182333755 -0.0009337055157223177; -0.0005148102225209284 -1.617159922682565e-5 -0.002324708691387429; -0.00022658777065159052 0.0007576145977738465 0.000740712564756417; -0.0003129359834149253 -0.0012955574887274805 -1.0065842572029446e-5; -9.158820964897699e-5 -0.0008895449650905261 0.0015320613459503612; 2.2209301922711262e-5 0.00019541528413607144 -0.00114911479906574; 9.374570151665873e-5 -0.0007921923935795058 -0.0015857953196873205; -0.0008045767399076187 0.00013849831017446028 -0.0013584678103140588; 2.61935267060273e-5 -8.784809985121276e-5 -0.001062919745388532; 7.391168388786015e-5 -0.0009846737224224829 -0.0014485879762215453; -5.36054939905517e-5 0.0005579460825485128 -0.0011146991746610584] %
+
+Mass Used: 110.56989704713169 kg
+Launch C3: 94.31952908729166 km²/s²
+||V∞_in||: 0.007058663333498295 km/s
diff --git a/archive/ES_0.5663735070962101 b/archive/ES_0.5663735070962101
new file mode 100644
index 0000000..180a136
--- /dev/null
+++ b/archive/ES_0.5663735070962101
@@ -0,0 +1,22 @@
+archive/ES_0.5663735070962101---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T00:08:54.008
+Launch V∞: [6.766374503665829, -7.178580182729692, 0.47837912465587307] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009721195918167901, -0.00014535445644626478, 0.006292304458588852] km/s
+ V∞_out: [-0.011355449748017879, 8.20366561975892e-5, 0.0023128326487531696] km/s
+ time of flight: 1.8749577779149508e8 seconds
+ arrival date: 2029-04-06T02:18:31.008
+ thrust profile: [0.2530082587918701 -0.061727168096464294 -0.07261993400641124; 0.10384851361779726 0.03359698548415082 -0.09861241360617311; 0.07715503249534979 0.04553559942845442 -0.12100396091790741; 0.06684315260306582 0.053194041221095195 -0.1452913311000915; 0.03717815767876296 0.036052085076919836 -0.10749828538699406; 0.0268445650806431 0.02980154524983575 -0.09525523913833031; 0.021854734063842866 0.03002362806526757 -0.09105720275160127; 0.006406807812662464 0.008960512384056868 -0.03166509556424469; 0.012640230222971387 0.017151235724919292 -0.06045432411087551; 0.002883632349678258 0.005377423764640063 -0.0190491249433943; 0.004053703360918495 0.007277535155524281 -0.02361362150582533; -0.0010772111947860213 -0.0005127871500566466 -0.002077360094786195; -0.001597857095419343 0.0011447413571354873 0.0013972847335413088; -0.002397457778722419 0.004535626769214485 0.0009246216971850255; -0.0019713544320327826 -0.0009929588448659027 0.0011042011339343913; -0.004378804554468135 0.0014341922376154377 0.005013015061528912; 0.0007984366118094959 -0.00012780344851141874 -0.00039292280655739225; 0.0020132923516875847 0.00022538615515613235 -0.0026684041055629448; 0.0012707200575214166 0.003015211734297839 -0.0005325563965061231; 0.0007720301992694985 -0.000296528677957336 -0.0017334748939322308] %
+
+Mass Used: 91.75843523348294 kg
+Launch C3: 97.54468395064497 km²/s²
+||V∞_in||: 0.011580840789726375 km/s
diff --git a/archive/ES_0.5663740952672771 b/archive/ES_0.5663740952672771
new file mode 100644
index 0000000..c9d03b3
--- /dev/null
+++ b/archive/ES_0.5663740952672771
@@ -0,0 +1,22 @@
+archive/ES_0.5663740952672771---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T17:55:55.403
+Launch V∞: [6.583334535087103, -7.427288338899205, 0.11382310149702253] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.907972380885023e-8, 1.0747350999082834e-7, 7.61955180432935e-8] km/s
+ V∞_out: [-3.5615785178365307e-8, 7.879324878210975e-8, -1.1850222185153701e-7] km/s
+ time of flight: 1.860001076632514e8 seconds
+ arrival date: 2029-03-23T12:37:42.403
+ thrust profile: [0.17177766302561517 -0.047779466832964114 -0.0654978740197048; 0.04991529262827161 0.010981929248579325 -0.0582815059057979; 0.061068386172672524 0.027540184109749625 -0.11874603835719369; 0.06080643825410009 0.03681400457351515 -0.16360316475170392; 0.04542418992809965 0.03272823946481818 -0.15653803201309066; 0.02750957047504217 0.022253672584880386 -0.11671759761836571; 0.011532826954948781 0.009990429275963095 -0.05789067354911983; 0.005879562029262534 0.005419971461820461 -0.03357212276089584; 0.007112176353615891 0.006813501584887533 -0.04425624123162434; 0.0056921099590958885 0.005199081145811089 -0.03419510423103766; 0.0028515898442818145 0.0023921876360134143 -0.017938184651648627; -0.0008234853933764138 0.0010415800701535295 -0.00667123220144056; 0.0011209183425556204 -0.0016047422965183638 0.0006560317392395355; 0.006617756224059108 0.012875060292201698 -0.004454779853044795; 0.009447120282848425 -0.0014294340684349476 -0.004721183955322417; -0.01282058335082275 -0.007127068100516965 -0.019609579151216715; -0.0005200639140423733 -0.0009046935945238141 0.0038288920031971756; 0.0008499508278294082 0.0052350024906229475 0.007443070625035671; 0.004715064200811622 0.007251162157120081 -0.014011364238889965; -0.0022962285131022287 0.003809422855117624 0.009020319540318341] %
+
+Mass Used: 86.08225316251401 kg
+Launch C3: 98.51786136845303 km²/s²
+||V∞_in||: 1.4875590933183654e-7 km/s
diff --git a/archive/ES_0.5663747814617652 b/archive/ES_0.5663747814617652
new file mode 100644
index 0000000..dbb2404
--- /dev/null
+++ b/archive/ES_0.5663747814617652
@@ -0,0 +1,22 @@
+archive/ES_0.5663747814617652---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T17:54:49.106
+Launch V∞: [6.56084457807351, -7.485248209854722, 0.11050065206213944] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.487480378220075e-8, -1.6308151631536746e-7, -6.800246764898221e-8] km/s
+ V∞_out: [5.979556337009193e-8, -9.912481143245202e-8, 1.4957185060433394e-7] km/s
+ time of flight: 1.8562007383393478e8 seconds
+ arrival date: 2029-03-20T03:02:42.106
+ thrust profile: [0.15702444592097908 -0.04606691453575567 -0.0632078487875532; 0.046651718868830225 0.008716432465559242 -0.05660070527683069; 0.04289871333581663 0.01707833394802533 -0.08737414992345686; 0.02862615280001299 0.014572478199508035 -0.08066065517945756; 0.028947397857635473 0.017544715830376093 -0.10384253925573379; 0.037291072337212475 0.02527057028292396 -0.16102683877774795; 0.035814399389836556 0.026593246720093073 -0.1799128873778462; 0.006963094290631787 0.005563012775310416 -0.04024458652058071; 0.011528873918391169 0.009476805338027344 -0.07244648478292834; 0.004346575252251546 0.0038012350772849614 -0.030567141237487664; -0.0007295346146850108 -0.0006220002601466262 0.00259730263223327; -0.0021472015369006555 0.0008594715365094746 -0.004122644533923759; -2.3585713136478918e-5 0.00023835114010003675 -0.0014636455147586745; 0.0016537220500364351 0.0038051625341571087 -0.004680188301060493; 0.0002915051730535586 0.00022367247221883859 -0.004472478577655932; 0.0023088586893934564 -0.006690856974940439 0.00026831307489043267; -0.0017208771094149925 -0.0007090565484769652 0.0012398187688626454; -0.005856065501438532 0.007132395524387796 0.0027697742094064306; -0.008978705691020508 -0.006524367796428961 0.014185105157188897; -0.011507927690852654 -0.008278434051812392 -0.014297375115551632] %
+
+Mass Used: 82.76988741861578 kg
+Launch C3: 99.08583273487606 km²/s²
+||V∞_in||: 1.9190141430300456e-7 km/s
diff --git a/archive/ES_0.566379503326529 b/archive/ES_0.566379503326529
new file mode 100644
index 0000000..31af3a9
--- /dev/null
+++ b/archive/ES_0.566379503326529
@@ -0,0 +1,22 @@
+archive/ES_0.566379503326529---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T14:51:42.429
+Launch V∞: [6.432649144269156, -7.242134844503197, 0.28900856929540064] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0172995044383532, -0.007545813519153344, 0.019752921500611816] km/s
+ V∞_out: [-0.018398314395262787, -0.006961098467228495, -0.018958637458222488] km/s
+ time of flight: 1.87495777873134e8 seconds
+ arrival date: 2029-04-05T17:01:19.429
+ thrust profile: [0.49142920724031913 -0.09838126933413176 -0.12228368586810874; 0.12038859286804242 0.04717518970652473 -0.1006458236975937; 0.06964956452183707 0.04846240139782306 -0.09758171218827785; 0.06669534480584868 0.06538345354096328 -0.131673904839614; 0.06323883100875788 0.07761251829244059 -0.16084258758605832; 0.02716321313273761 0.03892113960301191 -0.08833893884774485; 0.025325245920907936 0.04185795269856524 -0.09787023108055093; 0.006898507418267947 0.01322462887610707 -0.03258368834674218; 0.008040926762754861 0.014874757077940668 -0.039874987767107246; 0.0018347701961233173 0.0006826477061544715 -0.006155007591406775; 0.0008728717281040205 0.0018927049232530951 -0.007048261859913018; 0.001680094090185405 0.003787934439927207 -0.011367631061310881; -0.004088484323467579 0.003456562942199413 -0.0012386624013502638; 0.00046009871597426104 0.0019037395830612124 -0.0007707051780665296; -0.002491588844916686 -0.0009765213233342116 -0.0007430169500674986; -0.0026074495260272382 0.0007508050714955814 -0.00042270488409280145; 0.004213807829884521 0.0008543080425283115 0.0005250571021956458; 0.006376173951855303 -0.0012717533602689289 -0.002957992399357139; -0.0024060312359323864 -0.0017144079700936138 -0.0013291891886820515; -0.0019039216900796163 -0.009289189944901662 0.004516485306031256] %
+
+Mass Used: 112.96181512551584 kg
+Launch C3: 93.91101807236022 km²/s²
+||V∞_in||: 0.027320140250148277 km/s
diff --git a/archive/ES_0.5663821651977778 b/archive/ES_0.5663821651977778
new file mode 100644
index 0000000..33daabd
--- /dev/null
+++ b/archive/ES_0.5663821651977778
@@ -0,0 +1,22 @@
+archive/ES_0.5663821651977778---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T14:58:50.876
+Launch V∞: [5.742358011821634, -7.794540094033933, 0.05263134943951112] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.1942807288381396e-6, 0.0009833375794898866, -0.0006192613863087533] km/s
+ V∞_out: [-0.0009683330152731167, -0.0005070860157296422, 0.000394294415209668] km/s
+ time of flight: 1.7064585432057837e8 seconds
+ arrival date: 2028-09-22T16:36:24.876
+ thrust profile: [0.4425173132400772 -0.15806449499397965 -0.15215775645847002; 0.24316570737314924 0.04048038584417365 -0.22718641720904884; 0.056039162226553474 0.022294210388879982 -0.09115189855959296; 0.07755664897876707 0.04464079569907694 -0.16992621675091912; 0.051922031258919844 0.03657761255101156 -0.1444582004231516; 0.03651074116459404 0.029872592938258467 -0.12224178495928562; 0.03321247035165591 0.02981539452431925 -0.12791148961657356; 0.011705831523685336 0.011306761794493804 -0.053278714281128486; 0.0052647311864698915 0.0048111766939963885 -0.025971031725089615; 0.0003603661488845752 0.0013527522978816434 -0.00659733537655338; 0.0009864958458259277 -3.25505659021035e-5 -0.005282134480770429; 0.001535054114296671 0.0016706462652228984 -0.005996832341102989; 0.0006706607403971346 0.000917705346740247 -0.0030827530153995967; -0.0010952574342626385 0.0014182234935925376 0.0002677870012528246; -0.002773092771217449 -0.0019137329006303743 -0.0013670488107186774; -0.002587273084068547 -2.2443926938690005e-5 -0.001052453785929469; -0.0015009653488180818 0.0025490104343428833 -0.0022965456662901226; -0.002701612039914231 0.0034501774212253268 -0.0012991785077067536; 0.00022695119882347128 -0.0004888393193756299 9.56613842630356e-5; -3.2694446105587145e-5 -7.84372822820326e-5 -0.0014521592395273354] %
+
+Mass Used: 114.00743764186655 kg
+Launch C3: 93.73230087237845 km²/s²
+||V∞_in||: 0.001162087631480278 km/s
diff --git a/archive/ES_0.566401739375957 b/archive/ES_0.566401739375957
new file mode 100644
index 0000000..8f21579
--- /dev/null
+++ b/archive/ES_0.566401739375957
@@ -0,0 +1,22 @@
+archive/ES_0.566401739375957---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T07:17:28.711
+Launch V∞: [5.995870819446714, -7.352492304747246, 0.26799166767693383] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4360767175021845e-5, -2.2081249985541166e-6, 3.938263419434214e-8] km/s
+ V∞_out: [2.778932387725382e-6, -6.029200828214929e-8, -1.4257049126112084e-5] km/s
+ time of flight: 1.8148818569755077e8 seconds
+ arrival date: 2029-01-23T20:40:33.711
+ thrust profile: [0.7176384149412913 -0.18502940461889442 -0.17582823410569756; 0.25148534670854056 0.08288087624097826 -0.18938620843141882; 0.1025534065174206 0.06715110011893867 -0.13694302097639363; 0.06835237360374732 0.06204860201283204 -0.12976055483183094; 0.036877337230590106 0.04257294191024597 -0.09009506435106925; 0.017185230947731153 0.022736348200473933 -0.05339103578314546; 0.04442846281835254 0.06753705309501318 -0.1557799193994319; 0.0077013011450367454 0.013126021255715478 -0.03323679218646571; 0.00907364776330746 0.016691619891108712 -0.042929254432285166; 0.0015268800721247042 0.003058850635817344 -0.008364342824533596; 0.00010339691159518707 0.00027679794469197554 -0.0005401281293667377; 0.00018550128396245628 0.0004217028423002774 -0.0010820784861531572; -7.297454650710165e-5 0.00025856042550298475 -0.0007613899322125575; 0.0002444191447647507 0.0001432034877307908 0.0002129050620355941; 0.0007175285012021016 -0.0004559852478735072 -0.000895796837582712; 0.0004231300275608215 0.0004547174825659521 4.961416573799084e-5; 0.00020290163885872803 -0.00039307772563487703 -0.0001766657817693975; -0.0007079786120549136 -3.5189395064695996e-5 1.2074603816061434e-5; -0.0011063708678415059 -0.0006517902137248178 -0.0004578300759982512; -0.00012778551305747313 4.205442381697552e-5 -7.707314088180339e-5] %
+
+Mass Used: 135.32702380392448 kg
+Launch C3: 90.08142950880433 km²/s²
+||V∞_in||: 1.4529590526105702e-5 km/s
diff --git a/archive/ES_0.5664039427379558 b/archive/ES_0.5664039427379558
new file mode 100644
index 0000000..4126b89
--- /dev/null
+++ b/archive/ES_0.5664039427379558
@@ -0,0 +1,22 @@
+archive/ES_0.5664039427379558---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T12:50:20.858
+Launch V∞: [6.264926028394547, -7.450466725995844, 0.15936495089086603] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.004599631715719e-5, 0.00010851324449645141, -0.0001615695282566002] km/s
+ V∞_out: [0.00013700242385428988, 0.00011115899969659603, 8.61060890654855e-5] km/s
+ time of flight: 1.8266165135702658e8 seconds
+ arrival date: 2029-02-10T16:11:11.858
+ thrust profile: [0.4139487001479784 -0.11518614354875882 -0.1429988256033574; 0.1486807108892063 0.03518852569164627 -0.1570703333293018; 0.06385582252455593 0.03016444543043669 -0.1145548195080813; 0.05513001491147649 0.03535355053700077 -0.1377597951981717; 0.041778196670374176 0.032286765007716475 -0.13351802777671795; 0.02208055621330004 0.019492702771761083 -0.0864473789025335; 0.013284153248307631 0.01300700226031467 -0.06195744256423062; 0.006400195518855202 0.006749499142948756 -0.03590655623088623; 0.01627958574754448 0.018897942294974112 -0.09478961377071574; 0.0021620766357626896 0.0037642717475781223 -0.018472411635232253; -5.629502449456538e-5 0.0006164834908272466 -0.0006679034966964549; 0.0005840287475323998 0.0010926565458686693 0.0017757249855796485; 0.002046321459664268 0.00287762667008748 -0.0006317418807024063; 0.00045522945495564605 -0.0032310769982746078 -0.0044552759870017805; -0.0060368059395615676 0.005451611230830976 -0.010411589130073845; -0.0009374947951269984 -0.0002815766201265716 0.004560914648404773; -0.0008542591648103223 -0.0023437872965483206 0.013454622409795832; 0.0022234957582387286 0.00461768015884634 -0.011638376754082285; 5.091386647014607e-5 0.0001415319504066853 0.001831578171553356; 0.011765326777944844 -0.0005429237222843825 0.0038348757895512644] %
+
+Mass Used: 107.89705957095339 kg
+Launch C3: 94.78414976399915 km²/s²
+||V∞_in||: 0.00019565704347289533 km/s
diff --git a/archive/ES_0.5664074730100246 b/archive/ES_0.5664074730100246
new file mode 100644
index 0000000..d7aac3f
--- /dev/null
+++ b/archive/ES_0.5664074730100246
@@ -0,0 +1,22 @@
+archive/ES_0.5664074730100246---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T08:16:10.417
+Launch V∞: [7.347619693027553, -6.4614469157367225, -0.14102034739214583] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.3901238905031527e-8, 7.84811332212691e-8, -2.890147891831731e-7] km/s
+ V∞_out: [-6.226054744655923e-8, 2.907844146108768e-7, -4.3774558321969814e-8] km/s
+ time of flight: 1.6037421298038635e8 seconds
+ arrival date: 2029-06-07T12:39:42.417
+ thrust profile: [0.38664402042702006 -0.07281534985424908 -0.1277738529967681; 0.11984446755775367 0.04371929414363534 -0.1224339536171413; 0.06962403731094038 0.04509786277560297 -0.12102973960168963; 0.05037740900651583 0.042923078424896434 -0.12361195799891056; 0.0567927230627571 0.05968406836248668 -0.17872214347979218; 0.02506565822612963 0.02889840932704585 -0.09875420417879775; 0.020601804022363744 0.026188251071451552 -0.09509877013471277; 0.0577064045268668 0.07656551064644955 -0.23816982169800113; 0.0027136694547286525 0.0041892498675982996 -0.01757757988051707; 0.004687953361858048 0.006919335674236161 -0.03253542121285893; 0.00022605475781683538 0.0004514569483290703 -0.001622291543885338; -0.0001609919258039889 -4.515527057383044e-5 -0.001985993616812488; 0.0001124479823133555 0.0002638555781150014 -0.00043641609942958974; 0.0004992583601272759 0.00024239671689235657 -0.00018699843378976123; -6.253779529211974e-5 -0.0004636380277512745 6.365450417953038e-5; -0.0001510586278649214 -5.974381339179344e-5 0.0008769689331885308; -0.00021975490740301878 0.0009793472959157422 -0.0003196712777517245; 0.0002485784998884975 -0.0004444504146168272 -0.0011459504482754415; 0.00014084119675442547 0.000360303267698453 -0.0005347952184086125; -0.0017766451644128153 0.0009610897343353445 -0.0005629526528983846] %
+
+Mass Used: 102.22214604802912 kg
+Launch C3: 95.7576981366285 km²/s²
+||V∞_in||: 3.0139364730794277e-7 km/s
diff --git a/archive/ES_0.5664112395990893 b/archive/ES_0.5664112395990893
new file mode 100644
index 0000000..fc38c5c
--- /dev/null
+++ b/archive/ES_0.5664112395990893
@@ -0,0 +1,22 @@
+archive/ES_0.5664112395990893---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T00:16:50.783
+Launch V∞: [5.903249714534581, -7.788326438084997, -0.3645237129221337] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8815616819431484e-5, 2.4770642958970565e-5, 4.030472663141625e-5] km/s
+ V∞_out: [4.7494000544302365e-5, 2.8469576906934135e-5, 1.3007932629237244e-6] km/s
+ time of flight: 1.6828348418785498e8 seconds
+ arrival date: 2028-08-25T17:41:34.783
+ thrust profile: [0.3677414607127945 -0.14548761065048663 -0.14445280870995741; 0.07946790341994366 0.010105568980171793 -0.08558000602143061; 0.08862389206652234 0.03171040212318392 -0.15350008488624745; 0.08731320108117217 0.04446416067064298 -0.2057367971918143; 0.09487638288889759 0.06015981507856278 -0.27912682655588134; 0.036039675528813354 0.026120874487325283 -0.1301631508499845; 0.007267894858500086 0.005942666314009669 -0.031925753440067484; 0.013333500549065375 0.011662043503324003 -0.06335645613347975; 0.0016697278575721324 0.0030336839338384242 -0.012388168415555938; 0.0017054373981662994 0.001040561290756276 -0.00842881486050155; 0.0002284564976086647 0.001055450164708273 -0.00532543892163617; 0.0007838338462422095 -3.750132300960258e-5 -0.0010135631652071631; -1.0177857382592977e-5 0.0009148766953129525 -0.00526776563955577; -0.00035562833017783806 0.0009254426822862142 0.0017974433005810352; 0.0011130120901929894 -0.0034332967177831348 0.0022414671948227244; -0.0003015357177823675 -0.0002555592378877681 -0.0011568708493447373; 0.0019401844972944417 -0.0017758259210447877 -0.001080892451544234; 0.0004535710894406129 0.000642621398653367 0.00012340616882878402; 8.620956916806653e-5 0.0006747835558148618 -0.002351315963624041; 0.00019026103038400515 0.0020608315493350965 -0.0045204829099179215] %
+
+Mass Used: 102.91740949121913 kg
+Launch C3: 95.63926343560888 km²/s²
+||V∞_in||: 5.539309987821854e-5 km/s
diff --git a/archive/ES_0.5664146218495308 b/archive/ES_0.5664146218495308
new file mode 100644
index 0000000..cf0687f
--- /dev/null
+++ b/archive/ES_0.5664146218495308
@@ -0,0 +1,22 @@
+archive/ES_0.5664146218495308---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T08:26:47.043
+Launch V∞: [6.177485797831257, -7.69809798332749, -0.3348386327185401] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.014718837284351374, -0.009333280523314573, -0.014070296955961332] km/s
+ V∞_out: [0.009869219952396967, 0.016685950353854718, -0.011221781269278778] km/s
+ time of flight: 1.7906671141924122e8 seconds
+ arrival date: 2029-01-01T21:11:58.043
+ thrust profile: [0.22738771883304734 -0.07521653343771241 -0.09238463748005384; 0.12850861632813643 0.023306099203532382 -0.15126712482360513; 0.04642011223714988 0.018653782020585864 -0.09388320262852227; 0.05200378818261561 0.026590420964191994 -0.14031364431215168; 0.028189214812108482 0.01821077894795823 -0.09897381942012334; 0.024869471078097373 0.01913502054105499 -0.10824920331807882; 0.037278439146510904 0.031170634089000348 -0.17766094788911713; 0.011598009119365657 0.010078925058771986 -0.0625148803212961; 0.005750356980749913 0.006738672660869509 -0.036321728811235486; 0.001828655465586998 0.002275419934356509 -0.011116061413487208; -0.0003685741085969859 -0.0025625944085680766 -0.0027442042370233967; 0.001834106072347283 0.0004215933611689103 -0.002752886509710747; 0.0006054030631695768 -0.0008317760720617676 -0.005581610623474676; 0.0009807097861166323 0.000664702655275412 -0.004369179704674448; 0.006438123717091085 0.001196141928405284 0.0002416505766055315; 0.00047243307013715994 0.00046516505381304215 -0.005167993039371374; 0.0016417252038561554 -0.0008947878708617086 0.0016422176337594033; 0.0007831902166556346 -0.010202982698480278 -0.005873353945991919; 0.0027800336925228237 0.006624831738951811 -0.007844744171724892; 0.0024841568460652313 0.0003110703996514482 -0.00415036331143298] %
+
+Mass Used: 91.8677906803282 kg
+Launch C3: 97.53416025327847 km²/s²
+||V∞_in||: 0.022399275719518923 km/s
diff --git a/archive/ES_0.5664308914516696 b/archive/ES_0.5664308914516696
new file mode 100644
index 0000000..58dce7f
--- /dev/null
+++ b/archive/ES_0.5664308914516696
@@ -0,0 +1,22 @@
+archive/ES_0.5664308914516696---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T20:04:35.663
+Launch V∞: [7.509307833441803, -6.333121401248997, -0.1817210180696717] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.271428745364246e-9, 5.010121462946101e-9, -7.2623323414101975e-9] km/s
+ V∞_out: [5.225162103155902e-9, 1.1861270058684725e-8, 3.9334667813811057e-10] km/s
+ time of flight: 1.6055525817952424e8 seconds
+ arrival date: 2029-06-08T02:45:33.663
+ thrust profile: [0.2916904903694949 -0.05361393457749055 -0.1032484107511071; 0.14221341221855052 0.04954921077842634 -0.1470148792408471; 0.10872504681233194 0.06869094997573837 -0.18964991251883132; 0.08476282049123839 0.07124985491678776 -0.2084084436047515; 0.05734124749165038 0.058078525432764365 -0.18359786008893833; 0.028652525551532405 0.033156414088365 -0.11483862385421766; 0.02214286877454734 0.028600975913872947 -0.1047302623009569; 0.007491983914798436 0.010472132895069965 -0.041553247914474026; 0.004386033285067914 0.006382314173546623 -0.02613750751548277; 0.005209563757215502 0.006332197389276999 -0.02698821664749633; 0.00011054794274808919 0.0002295243302950653 -0.001051116581653552; -9.102277764512208e-5 0.00010648560226112049 -0.0004586066966632958; 0.0002029316952378265 -0.0002577239602447843 -0.0002301601439113197; 0.00038752939338218794 0.00036664295566437194 -0.00042704816720829785; -0.00021104419339617545 7.948466209983318e-5 -0.0005080101135874628; -0.000546564012270712 0.00011329577977599046 -0.00013820794984494; 0.00012201940002488465 -0.0001963310150273644 -9.791273385697873e-5; 1.3964816109789439e-5 0.00044058470172570505 -0.0001234971339450794; -0.0006102706543089674 0.00027389358979673493 -2.547171198839088e-5; -8.686339760961912e-5 0.00012986202195161385 -0.00035440785568486156] %
+
+Mass Used: 97.73764549253337 kg
+Launch C3: 96.53115334875677 km²/s²
+||V∞_in||: 1.2798522535469949e-8 km/s
diff --git a/archive/ES_0.5664375708622752 b/archive/ES_0.5664375708622752
new file mode 100644
index 0000000..81cc11e
--- /dev/null
+++ b/archive/ES_0.5664375708622752
@@ -0,0 +1,22 @@
+archive/ES_0.5664375708622752---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T13:17:18.373
+Launch V∞: [5.720631017964269, -7.511278444244092, -0.13644923663848896] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007758622439673582, 0.00021815797529135337, -0.0047424939917561715] km/s
+ V∞_out: [0.008703305662574571, -8.6173423530914e-5, -0.002673760488608389] km/s
+ time of flight: 1.8749577784137538e8 seconds
+ arrival date: 2029-04-08T15:26:55.373
+ thrust profile: [0.8530779965228171 -0.16455767718909714 -0.19945354603467658; 0.1500163470855251 0.05916131856828614 -0.12369601312645766; 0.09810245317486951 0.07173952531252688 -0.13634646729499533; 0.07457043832611576 0.07423868837305327 -0.14674489845817743; 0.04478766913013177 0.05573476530960777 -0.11792149200247258; 0.03572794936331869 0.052536815415963264 -0.11661465386008046; 0.010142600241131257 0.016895852740382383 -0.041544750584507066; 0.008445524995980525 0.015945294349903015 -0.04047415538399059; 0.0026226363144042993 0.006438675371246774 -0.01697413580242983; 0.002974022912488812 0.008069948534022426 -0.022819491083583703; 0.000360774551881215 0.0011941310329034397 -0.0034778328209290965; 0.000810221492363866 0.000736589992112215 -9.422998574930416e-5; 0.0004087488840196905 0.0012696255827578634 -0.0034617941311182727; 0.0005112982277281433 0.0010832774157705036 -0.003245021493512217; 0.0004960814765908086 0.0001337762519052292 -0.0007068335580733499; -8.91778208399124e-5 -0.0007705417057231692 -0.00038007000832206053; -0.001756590364932142 -0.0011430924663729791 0.0004952596197103214; 0.00033775737380437303 -0.0021089062208271203 -0.0019277533900046117; -0.0008881822384365597 -0.00028365347469463107 -0.0004008452088027139; -0.0023347997508298144 -0.002651405807885414 -0.00018620036247839327] %
+
+Mass Used: 140.7231738944206 kg
+Launch C3: 89.16354150484008 km²/s²
+||V∞_in||: 0.009095881723364318 km/s
diff --git a/archive/ES_0.5664426380797135 b/archive/ES_0.5664426380797135
new file mode 100644
index 0000000..63c378c
--- /dev/null
+++ b/archive/ES_0.5664426380797135
@@ -0,0 +1,22 @@
+archive/ES_0.5664426380797135---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:49:09.301
+Launch V∞: [7.376091419606102, -6.425847663241017, 0.13155970960662589] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.008637310714576e-6, 2.9714051384246607e-6, 3.371433233243831e-7] km/s
+ V∞_out: [-1.7921275596067548e-7, 5.680708803450067e-7, 3.551098531467505e-6] km/s
+ time of flight: 1.6100520378121245e8 seconds
+ arrival date: 2029-06-15T04:29:12.301
+ thrust profile: [0.38055692701824695 -0.07405750889185876 -0.13923541060610983; 0.15231555640187627 0.04655716179471547 -0.16604334948387794; 0.07430536502775092 0.040869057871396525 -0.13843318009701722; 0.04674338834364828 0.03327272152259762 -0.12487970377834688; 0.06791990432414377 0.05752863616678056 -0.2251655881590058; 0.041402908686105674 0.039491624103574006 -0.1670560826414333; 0.01695484905199888 0.017880714380992976 -0.08216359986044443; 0.010517610125070923 0.012672897229503181 -0.06024737712318678; 0.00343756331181963 0.0034779017936290785 -0.022713314477209673; -0.000985361518299027 0.002128423184106574 -0.014358819145352248; 0.0018827929080333298 0.002296019326925353 -0.011374861019801836; -0.0005340366928524788 0.0016945794257880761 -0.008203875793217965; 0.0029950536746007127 -6.427586933751986e-5 -0.010451012914863436; -0.00040901644253018296 -0.0008834261793553479 -0.0004883182545599718; -0.0008345770728653058 -0.0005119854118848081 -0.00017085945009169025; -2.8167678802606955e-5 -0.00030883491962807944 -0.00020095816705061097; 0.0006321056882672652 -0.000558860811478157 0.004392696805479645; 0.0016580651783432235 -0.004092183201876095 -0.004226594903643382; 0.000910468780047743 -0.004014655368120821 0.000645173100915481; -0.0018713765363709777 0.0009381529087222738 0.0036311807592002776] %
+
+Mass Used: 102.5090315502407 kg
+Launch C3: 95.71555077875857 km²/s²
+||V∞_in||: 3.6024350047035366e-6 km/s
diff --git a/archive/ES_0.5664460427601127 b/archive/ES_0.5664460427601127
new file mode 100644
index 0000000..d578cfe
--- /dev/null
+++ b/archive/ES_0.5664460427601127
@@ -0,0 +1,22 @@
+archive/ES_0.5664460427601127---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:20:04.911
+Launch V∞: [7.729370468527385, -5.927026393551302, 0.06360225404425775] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.160653789754887e-9, -1.716722879740984e-9, -2.0191356664452633e-9] km/s
+ V∞_out: [9.924514724301528e-10, -8.955963790276364e-10, -7.277625456469447e-10] km/s
+ time of flight: 1.794957201109318e8 seconds
+ arrival date: 2030-01-18T16:15:24.911
+ thrust profile: [0.4564321658177519 -0.027390546731576624 -0.1453435468789629; 0.07069077770362604 0.033229649103267776 -0.07616707743771899; 0.03412689652470096 0.025968476520527917 -0.06637554223776994; 0.08540580812136675 0.08981578285012748 -0.2342085540226177; 0.0352058132821379 0.04245663667854567 -0.12807996085804885; 0.023491546003178338 0.03301374661928837 -0.10955546431713596; 0.011648200934781463 0.017165246743821503 -0.06366163792206862; 0.00338911612097127 0.003939023350090936 -0.018568494539306507; 0.002655172965586256 0.004249254017987845 -0.01424659675006262; 0.008362117066239325 0.005251283790327064 -0.026173178661682794; 0.0022987066151098517 -0.0014502534766206619 -0.008928513365605814; 0.007452446181650545 0.004703870897316659 -0.015927063132244217; -0.00016637996725628323 0.00298230490900786 -0.008109533991860837; 0.007183554868127955 0.010208658789590803 -0.010966746452427428; 0.008157014439747493 0.017651477283962897 0.005365086611908279; 0.005743708361514695 -0.00531967680894822 -0.0011522774336896607; 0.0133755959469612 0.0031274049971295684 0.012007657885318768; -0.01104961527791437 -0.005617324014874666 0.03255944059254966; -0.0028697787990712544 0.012905727515900096 -0.04404022451913138; -0.0025249522533557726 -0.0020600551447200206 -0.002823335462834437] %
+
+Mass Used: 107.40539597495172 kg
+Launch C3: 94.87685495631652 km²/s²
+||V∞_in||: 3.4194255489072562e-9 km/s
diff --git a/archive/ES_0.5664709053060669 b/archive/ES_0.5664709053060669
new file mode 100644
index 0000000..cea6840
--- /dev/null
+++ b/archive/ES_0.5664709053060669
@@ -0,0 +1,22 @@
+archive/ES_0.5664709053060669---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T07:34:50.437
+Launch V∞: [5.938849295588237, -7.562583141725794, 0.08621063530071242] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.410898820565648e-5, 7.799581386344456e-5, 7.596455697752887e-5] km/s
+ V∞_out: [-8.725451887168473e-5, -4.270143599622814e-5, 8.894763674277241e-5] km/s
+ time of flight: 1.808233972546496e8 seconds
+ arrival date: 2029-01-19T04:18:07.437
+ thrust profile: [0.5235772960659024 -0.13950040742083783 -0.14265409480623842; 0.196749234019357 0.06097199118753076 -0.16033441179733515; 0.11039338073939324 0.06894941791961844 -0.15264127894822369; 0.04575929149343711 0.04083411013629864 -0.09579421691309921; 0.05957922863412367 0.06151475470095133 -0.1439937717301712; 0.028709313346601442 0.03918760854307673 -0.09902973512002915; 0.01843137775907437 0.02650750377988031 -0.07144028813474304; 0.018422536389554607 0.030183925828096574 -0.08302021150553858; 0.005680687111210476 0.006767717213117763 -0.022584454677594838; 0.006143320373511709 0.011924697286723206 -0.03628937117120186; -0.001393803382989096 -0.0008625604299471626 -0.003944835743625319; 0.0006661714374255963 0.0007348626850681669 0.00027196719173979735; -0.0011384793988017668 -0.0018224040675746897 0.0009475706810856584; -0.0038393826693671794 0.0045159467627812755 -0.000974824962580125; 0.005555724889683226 0.00402199563320633 0.0010460595865387163; 0.0017188956837330613 0.00162057124305201 -0.0018209641559604377; -0.001069053001230951 -0.005123033531530779 0.004083194614367163; -0.003537425572094084 -0.001535360187545359 0.0035911590111963134; -0.0012238050608535972 0.001552468112925465 0.0002450090697832168; 0.0010793497866221566 -0.0027181157800205296 -0.003452005170170306] %
+
+Mass Used: 121.47423199537707 kg
+Launch C3: 92.47002700486303 km²/s²
+||V∞_in||: 0.00013170460519617167 km/s
diff --git a/archive/ES_0.5664774165515959 b/archive/ES_0.5664774165515959
new file mode 100644
index 0000000..a3e5cdc
--- /dev/null
+++ b/archive/ES_0.5664774165515959
@@ -0,0 +1,22 @@
+archive/ES_0.5664774165515959---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T17:23:09.950
+Launch V∞: [6.207957118593612, -7.567149450276648, 0.08178863782949092] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.942863809128956e-6, 2.432383694105198e-6, -1.7238500482282313e-6] km/s
+ V∞_out: [1.7337016231775765e-6, -4.003546070487501e-6, 2.3247512229311565e-6] km/s
+ time of flight: 1.797264477961039e8 seconds
+ arrival date: 2029-01-06T21:23:56.950
+ thrust profile: [0.295417391773708 -0.08402659885439656 -0.09445112951400189; 0.12404908623290092 0.03085133022432951 -0.11691251988888247; 0.12058145009469208 0.06236312839072109 -0.18308502381243447; 0.05798477978442684 0.04023955128684078 -0.12731940209177325; 0.04231566293438806 0.03979000973075973 -0.12438014231663728; 0.047448386008365026 0.04963382604225118 -0.16280813031062874; 0.014990050482042312 0.016098375435755752 -0.0639464719157336; 0.006286649059364271 0.007913458585850274 -0.032401180976789845; 0.0058828507602064675 0.0073296199530784876 -0.03200770263522466; 0.004922944828202982 0.005960652021072773 -0.023097645399348266; 6.536180567868208e-5 0.00482665858907352 -0.009970719788516746; 0.00027162661823189414 0.0017534336596076593 -0.010779812437193777; -0.0007674579108307947 0.005125470197361784 -0.0004952238454401662; -0.0023423351854268137 -0.000444997647028502 -0.0022795375830972227; 0.0020304013509869043 0.0035013896492766556 0.003683269098643642; 0.007550289210813563 0.001495406602511803 -0.003797428350361224; 0.006147882675022409 0.0028569964168687193 -0.006968824458758963; -0.005764487038712162 -0.00191947358813114 0.0078043481615952155; -0.01178762666140317 0.0005687622973837276 -0.011146070344482416; -0.003745296751416049 -8.081527789097209e-5 0.0003801896587310159] %
+
+Mass Used: 102.01515064954447 kg
+Launch C3: 95.80717177039728 km²/s²
+||V∞_in||: 4.9431087830902754e-6 km/s
diff --git a/archive/ES_0.5664851511899136 b/archive/ES_0.5664851511899136
new file mode 100644
index 0000000..ff69415
--- /dev/null
+++ b/archive/ES_0.5664851511899136
@@ -0,0 +1,22 @@
+archive/ES_0.5664851511899136---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T08:26:48.694
+Launch V∞: [7.990553726115299, -5.896597789962502, 0.016610063743524844] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2425783070173505e-9, -5.486779960546815e-10, -1.6834991326938459e-9] km/s
+ V∞_out: [5.571739679957554e-10, 1.1153394892237861e-9, 2.7826114613200276e-11] km/s
+ time of flight: 1.8306321764718428e8 seconds
+ arrival date: 2030-03-04T03:20:25.694
+ thrust profile: [0.2056039641521522 -0.009016865305926536 -0.07619480386139083; 0.043019954240068006 0.018542200928096903 -0.04850381416974208; 0.038837969331550204 0.027973745004577524 -0.07725002073257112; 0.02943884528705998 0.0331361878348691 -0.09833189460723452; 0.022089850113602604 0.025392323883135486 -0.0935943465889209; 0.019406538457134494 0.02491163922511633 -0.09743805881682284; 0.013976941237722295 0.01697040503727097 -0.08113586730591982; 0.010456330362916712 0.0197940886058406 -0.08643775490067347; 0.005714608811619753 0.0105533409149199 -0.047012076842397034; -0.0025656238686917535 -0.00565609106769846 -0.02239905336470028; 0.007572462686455069 0.015095650459005091 -0.08333680020355815; -0.009195595883800912 -0.0030665489234551445 0.0015463812829145107; 0.007895333252938685 0.005915949446304483 -0.012123231395789694; 0.008449307625017357 -0.0021974331145024756 -0.02235414532455543; -0.0013090152488512642 -0.010031782489687635 -0.014652308012823662; -0.018986419508702893 -0.012030340303453766 0.00037916743900302807; 0.001031364567844516 0.0013143653189514604 0.0021604939008350744; 0.008412128363228296 0.014855052946768631 0.0016573834036286827; -0.0035506645040360796 -0.03257000581380109 -0.0018689865456025453; -0.007118701029522084 -0.005640925883411665 -0.01131799254480942] %
+
+Mass Used: 85.62131665056313 kg
+Launch C3: 98.61909024074332 km²/s²
+||V∞_in||: 2.1631499537030753e-9 km/s
diff --git a/archive/ES_0.5664917822543566 b/archive/ES_0.5664917822543566
new file mode 100644
index 0000000..fb1b7ce
--- /dev/null
+++ b/archive/ES_0.5664917822543566
@@ -0,0 +1,22 @@
+archive/ES_0.5664917822543566---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:44:32.925
+Launch V∞: [6.537680909678101, -7.490892226909861, 0.09139524503532669] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.933435585579936e-7, 0.00029771261211528283, -0.00020985151288784642] km/s
+ V∞_out: [-0.00018387041702403533, -0.0003075564502511682, 6.497195157097811e-5] km/s
+ time of flight: 1.8357760647432178e8 seconds
+ arrival date: 2029-02-22T22:31:18.925
+ thrust profile: [0.15004624417635623 -0.04272501964167602 -0.055945652056306486; 0.046954280030198706 0.010475488485492105 -0.05284789672207113; 0.05483995455010609 0.0253575462419084 -0.10273411038715403; 0.05370078106332921 0.033393658830109786 -0.13865466982601649; 0.033770393789824674 0.025259526264197033 -0.11292965990422696; 0.022878562505797142 0.01938811714742472 -0.09314448279259338; 0.015006044419299286 0.013636251887544604 -0.0701874238009434; 0.003187935105724473 0.0038308171980123056 -0.018102911493441617; 0.021447803117681092 0.022887751842258556 -0.12868372173945528; 0.014380458241457636 0.017828181744998832 -0.1006685315374314; -0.0007751865004519125 0.003114104080112692 -0.010735041229794452; 0.0009002168228631701 0.003995401082260546 -0.013132030436655466; -0.002333638511176762 0.0017261925847286558 9.280840456717815e-5; -0.0038157801897665024 0.0009523311403124559 -0.010399777963807382; 0.0024623030704942097 0.0006786900007288662 -0.006782540491569778; 0.009011240743590117 0.0014030033474937045 -0.021724188822396157; 0.006785473065178297 0.00039487890153136907 -0.00929652856610268; -0.0012061497129750836 -0.00011790791793075614 0.0008358191577973089; -0.004846321892896636 -0.0031512079690558543 -0.0016708073469820428; 0.003989586125734778 -0.00018591272016401338 -0.007431411608689466] %
+
+Mass Used: 84.20571441396442 kg
+Launch C3: 98.86309112276312 km²/s²
+||V∞_in||: 0.00036424065524943316 km/s
diff --git a/archive/ES_0.5664943658023852 b/archive/ES_0.5664943658023852
new file mode 100644
index 0000000..80a3d35
--- /dev/null
+++ b/archive/ES_0.5664943658023852
@@ -0,0 +1,22 @@
+archive/ES_0.5664943658023852---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T19:20:03.820
+Launch V∞: [8.037902691537896, -5.453859558735327, 0.3604414020048958] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.010823440370881104, -0.07366611456716914, -0.0719269136363833] km/s
+ V∞_out: [0.017256329632543525, -0.015718170701669743, 0.10096947706128917] km/s
+ time of flight: 1.8749577785678053e8 seconds
+ arrival date: 2030-04-19T21:29:40.820
+ thrust profile: [0.5399178615794877 0.001691895782404777 -0.13938234386719475; 0.08033912259011354 0.05418013189083967 -0.07809618154764246; 0.051198807013691464 0.05718297200771366 -0.09152096866862003; 0.028689394420356097 0.04232012918806482 -0.07742014786667509; 0.013779768589646208 0.02278284384075235 -0.050982083578220344; 0.012333874689010576 0.03500232047115753 -0.07163569798755921; 0.014587189030101751 0.04702289396945902 -0.10285175432279148; 0.005004967682875434 0.016803853288420125 -0.04740948565830553; -0.0007244579016638551 0.01289631454862675 -0.035394032232366965; 0.004788279690829788 0.021878569154066295 -0.05870507781096354; 0.003119757042312903 0.024353779753785554 -0.06658546330379952; -0.002361965254692078 0.0018668657681887547 -0.0028277637121246354; -0.006515553718804773 0.0014196349111269258 -0.006777873139465729; -0.003357983452333016 -0.0016525618518591675 0.002652134962199181; -0.0076444412318110964 -0.0007358825769768122 0.00027799050685927513; 0.011238402297036224 -0.007515902530782157 -0.0045251795755121655; 0.0018061881847857813 0.0015689713473898397 0.01223286828954492; 0.00972545530643391 0.0046133747044371076 -0.0029142425835891974; -0.004274072226699127 0.004056206989104409 -0.011096686554983193; 0.013846986382870644 -0.007599959762094252 0.01975269326639975] %
+
+Mass Used: 109.76286644841548 kg
+Launch C3: 94.48238176932011 km²/s²
+||V∞_in||: 0.1035245101516595 km/s
diff --git a/archive/ES_0.5665293655497684 b/archive/ES_0.5665293655497684
new file mode 100644
index 0000000..680cf3d
--- /dev/null
+++ b/archive/ES_0.5665293655497684
@@ -0,0 +1,22 @@
+archive/ES_0.5665293655497684---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:41:06.661
+Launch V∞: [7.8855949312072715, -5.834375559384948, 0.09805845009670985] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.824309553515195e-6, -3.5845608776174555e-6, 2.449299199085918e-6] km/s
+ V∞_out: [-8.394600713222499e-7, -5.7158603705085025e-6, 2.7874515629662134e-7] km/s
+ time of flight: 1.832968782556243e8 seconds
+ arrival date: 2030-03-05T03:29:04.661
+ thrust profile: [0.36714662932968456 -0.014635516167618696 -0.10941359977233629; 0.050275038331661644 0.02536716634687086 -0.053005505273895616; 0.06896362806844966 0.06142936193877646 -0.1381426367010303; 0.030963705237010253 0.038390592392834634 -0.09458040117789084; 0.018755686310007583 0.02641312538954379 -0.0841305247261073; 0.011430945839190068 0.01824152190332856 -0.06267914405513828; 0.018469471712906933 0.03750478020902087 -0.12282568318439624; 0.00612019524169265 0.01922530700073475 -0.06263542180272325; 0.0034038521132213366 0.006722757000222257 -0.020993719808637703; 0.00011088187442094381 0.005433444228988822 -0.017661931746121406; 0.007415918596325312 0.020425184298609043 -0.08090236002568797; 0.002030455665622935 0.0016009861822889873 -0.008562574005117918; -0.0019689001144789745 -0.011254310672373511 0.005764673191269677; -0.0037715316096348472 -0.00013120355401534563 0.0008394006940987695; 0.003545502296619288 -0.004451711266187223 -0.010630458936133137; -0.0014478025808197796 0.00025082964072679686 0.0060131137579038174; -0.027290024334902258 0.007631941178319851 -0.019446122817466147; -0.008283100219665827 0.007898406803132054 0.0008179757163429228; 0.020169151729071775 0.01420261208009377 0.002550256259304405; 0.004612577961079886 0.035953057749717486 -0.01690482312059057] %
+
+Mass Used: 99.59665370251378 kg
+Launch C3: 96.2321610466656 km²/s²
+||V∞_in||: 5.785627607537158e-6 km/s
diff --git a/archive/ES_0.5665356071389285 b/archive/ES_0.5665356071389285
new file mode 100644
index 0000000..63cf74b
--- /dev/null
+++ b/archive/ES_0.5665356071389285
@@ -0,0 +1,22 @@
+archive/ES_0.5665356071389285---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T03:00:33.189
+Launch V∞: [7.571103354428905, -6.1735410835634275, -0.7779549181145944] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.9083097678698206e-6, 3.351459727816931e-6, -2.5282701646370833e-6] km/s
+ V∞_out: [7.657533437319376e-7, 5.6754032818808535e-6, -2.6160184532530955e-7] km/s
+ time of flight: 1.8749577779212984e8 seconds
+ arrival date: 2030-04-24T05:10:10.189
+ thrust profile: [0.273342616983131 0.030513142309748824 -0.07087628573819904; 0.13368935543776359 0.10968162771247163 -0.10213403202385624; 0.07799861983806484 0.10933071307012637 -0.11122835388528825; 0.062420620880047246 0.12524433071660815 -0.13678629559226166; 0.0335515921662492 0.09421307753703197 -0.11294504165533177; 0.020595783447607343 0.07987329841968849 -0.10276286680240945; 0.010840705141706465 0.05941412498791152 -0.08307615278937029; 0.003888931700798909 0.02986050071073221 -0.04834572787224881; 0.0014640937810056264 0.015637509188399294 -0.02724582583509464; 0.0002057494005487553 0.0032388942670338603 -0.006026110041768678; -3.472953157590728e-5 0.0004483567896738927 -0.0018455312772451891; -3.434495904287606e-5 0.00029463520362132647 -0.00021810531403404542; -1.6426975215180672e-5 -0.0012709538762995178 0.0012084445625606924; -0.00026199928903573123 0.0002539440283948353 -0.00172730702648618; 0.0006014652340362748 0.0008179456475032304 -0.00010329992462248887; -0.00020665892305707606 -0.0009530532210398176 0.00023687685759628437; -0.0005631511396248084 0.0006889598949772972 0.0008046419120568259; -0.00011613638455288137 -3.3593283340223844e-5 0.00014071653940911366; 0.000660639255562077 0.0016865243752202516 0.0019268464819065204; 0.0006478245523146726 -0.00024353481473697006 0.001680382650547772] %
+
+Mass Used: 100.72820367911527 kg
+Launch C3: 96.03942936850879 km²/s²
+||V∞_in||: 5.735792671828316e-6 km/s
diff --git a/archive/ES_0.5665384587240233 b/archive/ES_0.5665384587240233
new file mode 100644
index 0000000..076d92d
--- /dev/null
+++ b/archive/ES_0.5665384587240233
@@ -0,0 +1,22 @@
+archive/ES_0.5665384587240233---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:37:46.509
+Launch V∞: [7.454760807005343, -6.0234296744843165, 0.03243457148194693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.886649863470508e-6, -0.00039416407871717147, -6.9248807688101905e-6] km/s
+ V∞_out: [-0.00038121601279259286, 5.733633455469349e-5, -8.28669463340441e-5] km/s
+ time of flight: 1.739976327685471e8 seconds
+ arrival date: 2029-11-11T12:18:18.509
+ thrust profile: [0.6037331446935688 -0.028745392057976313 -0.15111106595345952; 0.22888755481679804 0.1274869144499073 -0.18834434302596897; 0.08142612467626857 0.07686071434438373 -0.12470566954588327; 0.06001290143260824 0.07711699995983612 -0.13532844521780646; 0.031388987426326516 0.05064940856521506 -0.0989448665665781; 0.02818294078145693 0.054402285727393015 -0.11224180339954011; 0.017976708041070995 0.041465774905833946 -0.09074992228201145; 0.00652965859256226 0.017207644840732263 -0.04097142437073267; 0.002801973265911637 0.008583585969775298 -0.022139733866822425; 0.0027810735509651015 0.00954027680053141 -0.02510429421273048; 0.0029794069733378977 0.011540100184066872 -0.030646619090811827; 0.00020764112528411435 0.0030606567121163105 0.003412357431866451; -3.6624092934854765e-5 0.001045181634453044 -0.0018417262342909355; 0.0008960484519390862 0.0030646456703969536 0.00405621719382964; 0.001577485279251771 -0.002955837419276669 -0.0023514064413264505; -0.0038836027125139093 -0.005924276188808862 0.0026928969286715023; -0.004088737032506674 0.0007450634349953807 0.0025372516673631204; -0.0029279595987455726 -0.004794647489776959 0.001776392491513808; 0.0026878214988443764 0.007183028758014995 -0.008627474707553331; 3.6090430742942523e-9 0.002920085093578588 0.005885294948910998] %
+
+Mass Used: 125.13361005982824 kg
+Launch C3: 91.8562157345484 km²/s²
+||V∞_in||: 0.00039426885189072937 km/s
diff --git a/archive/ES_0.5665432445694298 b/archive/ES_0.5665432445694298
new file mode 100644
index 0000000..7a44cd5
--- /dev/null
+++ b/archive/ES_0.5665432445694298
@@ -0,0 +1,22 @@
+archive/ES_0.5665432445694298---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T08:01:04.220
+Launch V∞: [6.53869967917667, -7.4146424574432315, 0.14887751079427364] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009304994975068368, 0.00102130972640672, -0.0014058073083891053] km/s
+ V∞_out: [-0.0013364920609169654, -0.0006300726408582039, 0.0013046343517017509] km/s
+ time of flight: 1.8435201753524226e8 seconds
+ arrival date: 2029-03-03T00:54:41.220
+ thrust profile: [0.2426421794136654 -0.06811872244737394 -0.08489585096208965; 0.037704606261811456 0.010124123749955046 -0.04096550866960447; 0.04193964268123702 0.021637242592626633 -0.07638288377921655; 0.08164939944464836 0.051957208535974686 -0.195761146359923; 0.02020538913426084 0.01720968210603472 -0.06516155006082201; 0.02105730943981145 0.02047895195967512 -0.08389581632613562; 0.011912598459356103 0.008358585943332589 -0.04917173406959808; 0.03960794360875817 0.056406788376038186 -0.1859664756925854; 0.010930890914830276 0.013541097770106475 -0.06485507328269996; 0.004873862806307403 0.006698589993967867 -0.03341150320363316; 0.0006592018689382734 -0.001756785732567249 -0.007960442730628922; -0.0020310592613127787 0.0027507243259043542 -0.011107644349945817; 0.002735504711224713 0.004497036132835624 -0.02590337874867002; -0.0006364002082250211 0.0023324034836240868 -0.0042993736649847136; -0.0025654657188793686 0.00019612229883593732 -0.0003275515871460301; -0.002491464703241794 -0.0028978869184106467 0.0032918768871517882; -0.005860517201377133 0.0035744623954856794 0.003075043209025344; -0.0005388822683543273 0.001619950146649282 0.006165065762734497; -0.008029950926099887 0.006468651883382142 0.011161617335331098; -0.003964625983830459 -0.005823134909177033 -1.0236555745187122e-5] %
+
+Mass Used: 90.73731411780454 kg
+Launch C3: 97.75368077940519 km²/s²
+||V∞_in||: 0.001971090322748723 km/s
diff --git a/archive/ES_0.56654325260072 b/archive/ES_0.56654325260072
new file mode 100644
index 0000000..2cd45bf
--- /dev/null
+++ b/archive/ES_0.56654325260072
@@ -0,0 +1,22 @@
+archive/ES_0.56654325260072---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T07:10:46.448
+Launch V∞: [6.546354204657233, -7.486068184059556, 0.25370028936816497] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.8544115987650107e-10, -2.815847903002303e-9, -9.464334639237324e-9] km/s
+ V∞_out: [3.3890831409551955e-9, 4.997662064097917e-9, 2.446971076676821e-9] km/s
+ time of flight: 1.8749577787461564e8 seconds
+ arrival date: 2029-04-11T09:20:23.448
+ thrust profile: [0.15174939233143883 -0.03923295825506905 -0.055333899298792226; 0.033616513450682284 0.008576385986843882 -0.03585894870509554; 0.06816036068373046 0.03169288518020458 -0.12465531725366343; 0.06881962847464658 0.04157350701349383 -0.1731503750329255; 0.04901611725421311 0.036216753091235 -0.16090434623710795; 0.02824780535923846 0.0239728988049378 -0.11273336563419482; 0.00980697082212496 0.00950196018885752 -0.0464653684733167; 0.004395001834110048 0.005330214237155427 -0.022625124424636635; 0.014319522028255618 0.015555363186851346 -0.08107510835283936; -0.007312006545942948 -0.008576308110744026 -0.019049831949563167; -0.00022556987164024092 0.0008349483608083017 0.0010596294022576923; 0.005698898838973471 -0.004890358283715893 0.002790924665254445; 0.0003467651197161665 0.0004446221973098415 -0.004564688911839154; -0.009803927157938815 -0.0036347550124679797 -0.014748127290410461; 0.0033858837192404234 0.0013922469953039824 -0.009308863947564859; 0.0029246608246609324 6.324298587432692e-5 0.0026610550052663753; 0.01076964246306002 0.0005045837771219686 -0.011062183599565999; -0.008472284650370726 0.0032010213380084655 -0.008037605325650225; -0.006847866731793218 -0.001387310562409712 -0.020384635352394497; -0.0034436168004149765 -0.0029516092175898494 0.0009708425842098704] %
+
+Mass Used: 83.6985126488953 kg
+Launch C3: 98.96033406604766 km²/s²
+||V∞_in||: 9.881861892580613e-9 km/s
diff --git a/archive/ES_0.5665564658990728 b/archive/ES_0.5665564658990728
new file mode 100644
index 0000000..05da714
--- /dev/null
+++ b/archive/ES_0.5665564658990728
@@ -0,0 +1,22 @@
+archive/ES_0.5665564658990728---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T02:59:34.671
+Launch V∞: [6.141488734819277, -7.74099229347945, 0.012202374753054341] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1975236588263302e-9, -2.8576596674893365e-11, 2.92919623882942e-9] km/s
+ V∞_out: [-4.542958508691183e-9, -6.33866417649788e-9, -3.1588533327580053e-9] km/s
+ time of flight: 1.74286963010542e8 seconds
+ arrival date: 2028-11-05T08:02:17.671
+ thrust profile: [0.18315155715862372 -0.06399042168537215 -0.07073137356668502; 0.09250576023860724 0.01519179460514781 -0.09906017322165983; 0.09369303071877842 0.03669951713778996 -0.163707375109197; 0.07788537744036025 0.042267549260432045 -0.18693885639940797; 0.05629253758070973 0.037094454711166264 -0.17149164681849324; 0.03169347349036792 0.02390615383099289 -0.11645464228305655; 0.02457778462827015 0.020511281895738396 -0.1043689016186863; 0.010812723461099035 0.009953720229086438 -0.05269284595064252; 0.0050010465750946614 0.004857105119318805 -0.026556435163263246; -0.0010129566903945518 -0.0010141896396945278 -0.004842195851080256; 0.0022634005691381503 -3.1076732497776734e-6 -0.007596735255838819; -0.0013217962514451016 -0.004149160813193261 0.0018051499116159627; -0.0020303173829973498 0.00227864340280407 -0.008018674105970989; 0.0012133221348655339 0.0023162936993501287 -0.0035893315241918903; 0.0017565964672726507 -0.007469025415898799 -0.013030004135220036; 2.7657898431296098e-5 -0.0004769024613379278 0.00032983250118325935; -0.0028691418898589838 0.0014089681933440676 -0.0018873302377722452; -0.0008817718518396556 -0.0008017334095802037 -3.3046912159689044e-5; -0.011575397308837847 -0.009669528359992144 -0.000526136740840853; 0.0022530684358416705 0.0015323362490105806 -0.009824709630935085] %
+
+Mass Used: 91.41007583309374 kg
+Launch C3: 97.64099446556993 km²/s²
+||V∞_in||: 3.1646595616114444e-9 km/s
diff --git a/archive/ES_0.5665617721663763 b/archive/ES_0.5665617721663763
new file mode 100644
index 0000000..777edfa
--- /dev/null
+++ b/archive/ES_0.5665617721663763
@@ -0,0 +1,22 @@
+archive/ES_0.5665617721663763---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T01:58:23.748
+Launch V∞: [7.388366758513368, -6.261862231486398, -0.14257382045435418] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00023146710819014617, 0.00014496652932506371, 0.008980534531120875] km/s
+ V∞_out: [-0.003539106330718938, -0.007337877680729615, 0.0037783505559393265] km/s
+ time of flight: 1.667955890509297e8 seconds
+ arrival date: 2029-08-21T14:04:52.748
+ thrust profile: [0.5163911289072143 -0.0767133985316347 -0.18061642380737544; 0.18522173285091656 0.07212764409764888 -0.2029576117785787; 0.06504748057079442 0.04397418864739175 -0.12629304097945201; 0.040605116745982446 0.03592573815097015 -0.1129846590196572; 0.03748756906486447 0.040031647978820195 -0.13512914607911275; 0.03318835252689213 0.04165970339510834 -0.14858241698120547; 0.01325743553272014 0.01718053261983579 -0.06895708050056765; 0.005018499193489185 0.0066270207058486226 -0.034239464215627624; 0.013859340974579236 0.019256365430329093 -0.08740805031590301; 0.0029449244697518653 0.004945445705817092 -0.022823285111700176; 0.0033654036312181787 0.0024896055174004317 -0.011908349367421755; 0.0006438697519710046 -0.0011497836212743637 -0.0005836242411922047; -0.0004768258061521827 0.002354136732329243 0.004735295266173351; 0.002071917788863459 0.0009943677927895995 -0.002402411213390941; -0.0024545980628119207 -0.00344113458441474 0.001938672443814229; -0.00990854396301916 2.1163186624872362e-5 -0.0011381544823765638; -0.005567983393616873 0.0005632615039170337 0.009038621765774175; -0.007705417655295036 -0.005194954128140222 0.008211284656862007; 0.0009399678041188346 -0.0013453793096150132 -0.003158388702842488; 0.0014086011862954602 0.0014007920481299888 0.012163271022190355] %
+
+Mass Used: 113.71001351835503 kg
+Launch C3: 93.81920925870011 km²/s²
+||V∞_in||: 0.008984686571130508 km/s
diff --git a/archive/ES_0.566565601555085 b/archive/ES_0.566565601555085
new file mode 100644
index 0000000..7744448
--- /dev/null
+++ b/archive/ES_0.566565601555085
@@ -0,0 +1,22 @@
+archive/ES_0.566565601555085---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T04:25:44.901
+Launch V∞: [6.359638154074168, -7.66831753691977, -0.052994361955537986] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.280414876227051e-10, -2.2767335971784375e-9, -6.265070281625417e-9] km/s
+ V∞_out: [1.9933070914927794e-9, 2.8281477983986343e-9, 1.4340306828088043e-9] km/s
+ time of flight: 1.754417033000091e8 seconds
+ arrival date: 2028-11-18T18:14:07.901
+ thrust profile: [0.10187482033738954 -0.0354952869617428 -0.04261762188505962; 0.04652706283537359 0.007070348473523165 -0.054476094599457126; 0.05756216850827453 0.022013520263290367 -0.11210277188690772; 0.06051678555987511 0.03223826578710481 -0.1580203647291846; 0.06566608651744427 0.042354958972522186 -0.2128508336768823; 0.028025922953254505 0.01955341598030709 -0.11454159115448478; 0.0260597458192982 0.020616551076717244 -0.1207756828033996; 0.010824182145294584 0.007801445847498074 -0.049953732322337505; 0.006137466889946289 0.006679545488734999 -0.03865400780193603; 0.008715477255225042 0.007790156074095981 -0.052590942917410975; 0.00036678330557177283 0.00016541866329447606 -0.0060074376525963286; 0.0019769349695116087 0.0021533095325456768 -0.014536039292077278; 0.0006760830950128324 -0.004928168874899542 -0.003335213520061313; 0.0008815115211048862 0.0023280718705965984 0.00021047679396057938; -0.0068202347260456955 -0.0027988100112590905 6.42293511157084e-5; -0.00029008900244200124 -0.0007679720989325004 -0.0027663316986005645; 0.0011541625492974769 0.0017118247114545151 -0.005548738185531079; -0.0017939873620738693 0.0027325846945048787 -0.002658748782484551; 0.0003131675459156241 0.0010976613216588768 -0.011188446521601478; 0.0030454566810533138 0.007011896829631064 0.0031179552159507707] %
+
+Mass Used: 82.02962022984593 kg
+Launch C3: 99.25089970018625 km²/s²
+||V∞_in||: 6.705569768030673e-9 km/s
diff --git a/archive/ES_0.5665690874901219 b/archive/ES_0.5665690874901219
new file mode 100644
index 0000000..e68ec67
--- /dev/null
+++ b/archive/ES_0.5665690874901219
@@ -0,0 +1,22 @@
+archive/ES_0.5665690874901219---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T10:22:34.375
+Launch V∞: [6.241959527422062, -7.579030924591836, 0.06879858887810944] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4819942551533114e-9, -2.1109743955888137e-9, 4.408556501719002e-9] km/s
+ V∞_out: [1.1706897413637291e-9, -5.4022110840671775e-9, -3.6065832582156596e-9] km/s
+ time of flight: 1.7789068050205502e8 seconds
+ arrival date: 2028-12-17T08:27:14.375
+ thrust profile: [0.342509003025573 -0.1134429176456366 -0.13010924717868558; 0.05729576070324877 0.010099809967963351 -0.06719526968335084; 0.052493867660742266 0.02104237892314897 -0.10208804905223075; 0.06657367914441699 0.0366338178644466 -0.17470644695145204; 0.03209317333321911 0.021131293047156084 -0.112548507070416; 0.03032586152019082 0.02289694825112476 -0.12374636382447862; 0.017978844375247733 0.011983298055053888 -0.08594077279783345; 0.020629231584789458 0.02071918376860385 -0.12323891799674368; 0.009179657491726723 0.00945057866396575 -0.06970873966286886; 0.0018358561038167968 0.0013285504428592586 -0.012408777044251428; -0.000759872458006628 0.00036124442418516555 -0.00162189122568231; 0.007012939914474336 0.003433184538200694 -0.013454015660469918; -0.001077226274810894 -0.0007373365648670756 0.004775379485619985; 0.001017321113236091 0.002153094118015661 -0.0022765613632906956; -0.000345133483468843 -0.0030774862874716124 0.0011933937071193336; -0.0006220098091091525 0.0004961926198369524 0.001696732268445794; 0.0016381117696743545 0.009843147806105103 0.00488643603549676; 0.0013863206933336816 0.0010997940881764 0.0032612684616740266; 0.003922831259241949 -0.002410050714511052 -0.002070739654044318; 0.012395520657096067 -0.006422599093740822 -0.004372672357785892] %
+
+Mass Used: 98.61434190007367 kg
+Launch C3: 96.40850174372605 km²/s²
+||V∞_in||: 5.481959395170169e-9 km/s
diff --git a/archive/ES_0.5665727297399563 b/archive/ES_0.5665727297399563
new file mode 100644
index 0000000..3292dad
--- /dev/null
+++ b/archive/ES_0.5665727297399563
@@ -0,0 +1,22 @@
+archive/ES_0.5665727297399563---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T12:58:44.063
+Launch V∞: [7.457357584608836, -6.540583160824668, -0.2173713946017566] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005670419081705597, 0.0003616514559566143, -0.00016850817495104857] km/s
+ V∞_out: [-0.0002691912508929405, -0.0005614707218407725, 0.0003049074436759389] km/s
+ time of flight: 1.624765288751741e8 seconds
+ arrival date: 2029-07-04T01:20:52.063
+ thrust profile: [0.14150963685038495 -0.023806759001924038 -0.054633424775365515; 0.06726577847154663 0.02275516467148257 -0.07372775784163522; 0.08936994816170801 0.05280434219652584 -0.1601538780821975; 0.10442178813284979 0.07962245984546276 -0.25065976954278113; 0.07020120428403331 0.06322138924409562 -0.21946249504718218; 0.029637683063845354 0.03211499719429296 -0.12192410335215804; 0.017682850381001123 0.019915192918746234 -0.08579004044432423; 0.008635943262755621 0.01051061336539414 -0.04649363279884353; 0.0018369580974024987 0.002877272516896295 -0.010260678513920945; 0.00043660053489940015 0.002012851529640119 -0.004888527692742743; 0.004100210748548398 0.003398230641254247 -0.026772129782549937; 0.0021297233074890655 -0.001665321077854822 -0.00926005753767158; 0.0004453612259858462 -0.004678435863746676 9.435476793986887e-5; -0.0012876850240208172 0.0009914271311459917 -0.005865889409535561; -0.0013242372995892517 -0.0011883127184710417 0.0028047042681094655; 0.0023036620937757213 0.0045843033494674165 0.0005982951700362052; -0.0024058280987597743 -0.010055404391181163 -0.0034791257570848536; -0.000731004994966103 0.0031381183451430314 0.005053405430842019; 0.002904268774950697 -0.004505252656591901 0.007345836319463141; -0.005798440487294274 0.0012258462175078354 0.002630988922812958] %
+
+Mass Used: 86.77599814574842 kg
+Launch C3: 98.43866055157724 km²/s²
+||V∞_in||: 0.0006933421278435211 km/s
diff --git a/archive/ES_0.5665736612352807 b/archive/ES_0.5665736612352807
new file mode 100644
index 0000000..aa5f232
--- /dev/null
+++ b/archive/ES_0.5665736612352807
@@ -0,0 +1,22 @@
+archive/ES_0.5665736612352807---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T04:41:57.476
+Launch V∞: [7.839120902592396, -6.1855379588598565, -0.0008397539969874701] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011975050856396715, 0.06718787766704566, 0.069502501474597] km/s
+ V∞_out: [-0.013508527774378293, 0.013276931469813449, -0.09554546389358132] km/s
+ time of flight: 1.7979670197047257e8 seconds
+ arrival date: 2030-01-26T04:13:38.476
+ thrust profile: [0.1080203176902873 -0.00794233147308447 -0.04187305211443129; 0.06535487734727069 0.027601460118736963 -0.08111445627874375; 0.05009300402820613 0.03394711861207428 -0.10860855961823042; 0.03983585617925635 0.03405220329534241 -0.12367177086637873; 0.032546661249779195 0.03240062881609854 -0.13136595690735853; 0.0238546384716225 0.026567833681012856 -0.11942855370138188; 0.01734335186540984 0.021273061123929224 -0.10411832219875887; 0.010885893666726647 0.014851681187195109 -0.07795880645202774; 0.0051222326076074305 0.008674621954709342 -0.0464093621900349; 0.00033589318531075424 0.0034805561221481155 -0.013673085634053617; -0.0034000800196982905 0.003631654287842241 -0.00017812247382910699; 0.0011124346622159113 -0.0005625628608126242 -0.0012738181114225451; -0.010767867708617812 0.00444411402362957 0.002602366006652; -0.00015572349944246192 -0.0024172151812389547 0.0004591148206511316; 0.004986755967545456 -0.009431983462767194 0.009621629797752296; 0.0011798985668879935 -0.0026295549886453623 -0.001029363109633047; -0.002108173455902169 -0.0025999673520422867 0.013995914383815252; -0.013428855529440249 0.0029583501135914273 -0.002559043167018607; -0.002703505943316177 -0.00201998637742942 -0.024994700645056767; -0.00435769577373959 0.018580023785451212 0.007092475825035328] %
+
+Mass Used: 79.34520519282114 kg
+Launch C3: 99.71269707114396 km²/s²
+||V∞_in||: 0.09740744560679918 km/s
diff --git a/archive/ES_0.566578015905107 b/archive/ES_0.566578015905107
new file mode 100644
index 0000000..723f363
--- /dev/null
+++ b/archive/ES_0.566578015905107
@@ -0,0 +1,22 @@
+archive/ES_0.566578015905107---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T12:40:21.375
+Launch V∞: [6.5400597047970335, -7.2153603828261765, 0.24997312217858028] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5013717979460902e-5, -2.32251793111184e-6, 4.181147135109626e-8] km/s
+ V∞_out: [2.8033492388208245e-6, -6.830299213842768e-8, -1.4922140496106342e-5] km/s
+ time of flight: 1.8749577787483513e8 seconds
+ arrival date: 2029-04-05T14:49:58.375
+ thrust profile: [0.40297728505345165 -0.08744939807770477 -0.10796879083111453; 0.14728328611295327 0.052010857092035456 -0.12535647898583066; 0.07515038064694604 0.049730874463101225 -0.10901686749228072; 0.06993729642720449 0.06342003558714471 -0.1428188787120909; 0.05234835724146616 0.05847075837676915 -0.1385755230998412; 0.03422639597119142 0.044880249122685116 -0.11251255278605844; 0.01921992476899954 0.028913520519279926 -0.0761686849896431; 0.007784343651668332 0.013049807345628413 -0.03556646778192569; 0.001497063519244445 0.0010929275519808463 -0.0029823481200294474; 0.003365478590207171 0.004213519399147378 -0.006900015767514183; 0.0030487587785831076 0.007465050564029916 -0.024179863801002236; -0.0031794966043699035 0.0014982048435567825 -0.006596740878680467; -0.0014331349772609607 -0.0019034819514293776 -0.005869456786533589; 0.002192878416513903 0.006149286334582532 -0.003809234226771575; 0.0013082779295127656 0.004810415245469296 -0.003954527726024131; 0.0010719823687828293 -0.00265730241928365 -0.0026440358258740574; -0.0011596570067027197 0.0026565633820030948 -0.0004178538711730323; 0.00044029100129244444 0.000369512767834575 -0.00562309340196424; -0.004617196576065033 -0.006150622077589342 -0.001840138439258409; -0.0003610321331986391 0.0024718387308059592 0.006089604454299976] %
+
+Mass Used: 107.44597629991358 kg
+Launch C3: 94.89629295817907 km²/s²
+||V∞_in||: 1.5192352197940255e-5 km/s
diff --git a/archive/ES_0.5665837867488375 b/archive/ES_0.5665837867488375
new file mode 100644
index 0000000..ab617ed
--- /dev/null
+++ b/archive/ES_0.5665837867488375
@@ -0,0 +1,22 @@
+archive/ES_0.5665837867488375---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T22:08:49.352
+Launch V∞: [6.453464113514608, -7.223116635043339, 0.1637440238000356] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.706817408626912e-6, 1.0853494459437435e-6, -2.2263650603429016e-8] km/s
+ V∞_out: [-1.4818854646760762e-6, 3.2770667600250274e-8, 7.64077504394474e-6] km/s
+ time of flight: 1.8749577787454638e8 seconds
+ arrival date: 2029-04-07T00:18:26.352
+ thrust profile: [0.5477174278164396 -0.13131792413283505 -0.16513795135726184; 0.07559394639093411 0.023921057218629607 -0.07488511233421219; 0.05343940319591358 0.032087585303307915 -0.08929105110560571; 0.042121635379902475 0.034289727574806535 -0.09913576644539722; 0.045921040199809096 0.045798180268721 -0.13829416973700737; 0.027978070547341274 0.032545495305436274 -0.10455755142122823; 0.03527200671629414 0.046503594092121445 -0.15393098886328968; 0.00786888069834018 0.011352891331931543 -0.043708008127538375; 0.005173025810154588 0.008166485284596922 -0.03124659591584116; 0.004298100917839293 0.0010299330220712728 -0.005541013669493004; 0.002934428767182376 0.005132645657721268 -0.021039804607979256; 0.004345043512688752 0.002081629742496846 -0.0023807598851301424; 6.041413808352032e-5 -0.0020721312420375515 0.0032717496078661255; 0.0007117146599935511 0.0015146157161601964 -0.003219857899767578; 0.0072669769843641055 -0.0018524714867588737 0.002114172947140546; -0.007301226932987809 -0.0009982906816134657 -0.0023677334859228097; -0.004768194811344394 0.007327480967865912 0.0012687386842638658; 0.004132671687126542 0.0034277038110504254 0.0034120505874009393; -0.0018436477512092243 -0.0027052015311310614 0.015060782231968637; -0.0032775359654134578 -0.00029168458728735553 0.005431580003939443] %
+
+Mass Used: 113.57110483002998 kg
+Launch C3: 93.84742509319092 km²/s²
+||V∞_in||: 7.782898795427281e-6 km/s
diff --git a/archive/ES_0.5665858560534153 b/archive/ES_0.5665858560534153
new file mode 100644
index 0000000..d6f8237
--- /dev/null
+++ b/archive/ES_0.5665858560534153
@@ -0,0 +1,22 @@
+archive/ES_0.5665858560534153---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T00:05:42.948
+Launch V∞: [7.3119093981254855, -6.3563847876257284, -0.11516964878710845] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.178508244281387e-6, 9.146675056134427e-6, 8.050788434318633e-7] km/s
+ V∞_out: [-6.441617607290437e-7, 1.983831901401184e-6, 1.0863617271536491e-5] km/s
+ time of flight: 1.6164435290696988e8 seconds
+ arrival date: 2029-06-20T21:18:14.948
+ thrust profile: [0.48937488791220085 -0.08346694552889485 -0.16010447196556982; 0.15264659847323941 0.05569541828157948 -0.14936958427641248; 0.15565561019866134 0.10213853713404221 -0.2505716555680256; 0.087791071197402 0.07573592906934636 -0.20622606059091692; 0.05365666641937216 0.056051986003786684 -0.16479110878577533; 0.02625702436057213 0.031192379913432385 -0.09798255355770091; 0.02079509373110652 0.027662033554266302 -0.09170010589911272; 0.0030751445241819827 0.003940243143817873 -0.015736514756267923; 0.0015215040248382956 0.0005343360669333983 -0.0078319882031022; -0.0011954845362642185 0.002238942126010442 -0.005297875439536117; 0.0031825158703284017 0.003007614653092256 -0.012328149833399922; 0.00029349939038820605 5.200088620636791e-5 0.0008809273567079055; -0.0017262251842388452 0.0020622993362686146 -0.0017076872537091497; -0.0032602654098452554 -0.007095212541816169 -0.001525977046610453; 0.0031059116749486172 0.0025588495155562095 -0.008382498763282599; 0.002690236008913342 0.001744068719271862 -0.008789306587966596; 0.0013357208163389343 0.0021236713154221573 -0.0006814176631420388; 0.0012450015592295625 0.002693308085162796 0.0012792433428078873; -9.180105938731058e-5 0.0007785953335576611 -0.00019350072250206348; 0.0022968114480352124 0.002167928570245895 -0.0008945613339621052] %
+
+Mass Used: 113.37818652956685 kg
+Launch C3: 93.88091066275732 km²/s²
+||V∞_in||: 1.1067239070848083e-5 km/s
diff --git a/archive/ES_0.5666077466513756 b/archive/ES_0.5666077466513756
new file mode 100644
index 0000000..820f046
--- /dev/null
+++ b/archive/ES_0.5666077466513756
@@ -0,0 +1,22 @@
+archive/ES_0.5666077466513756---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T20:53:53.375
+Launch V∞: [6.193080032428587, -7.646746877729102, 0.3018884316109307] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3275782173382052e-9, 6.261811176447235e-10, 6.359470505157235e-9] km/s
+ V∞_out: [-3.848856183376282e-9, -5.5300194409648395e-9, -2.8322454781700066e-9] km/s
+ time of flight: 1.761775016396414e8 seconds
+ arrival date: 2028-11-25T23:05:34.375
+ thrust profile: [0.2096729494713049 -0.06156602708037824 -0.07195661066371377; 0.13326899291367883 0.033314397763273086 -0.12275293754855328; 0.09528125918301729 0.05012584051934897 -0.1584179153799263; 0.07175607952537026 0.05518220806437433 -0.16766482140259317; 0.06430919808523679 0.07325417411694303 -0.2220362723696662; 0.027861392946569266 0.03031682309244479 -0.09896949240507308; 0.017680318994335503 0.01863293884294842 -0.06814443196024254; 0.0076597484339063285 0.009302061764634112 -0.03517095491458308; 0.001883274087912438 0.0031301642468337465 -0.013343918258380928; 0.003383133563891127 0.004492078828460805 -0.016493702473941246; 0.004194226136600919 0.0048262309139980464 -0.016019937318481507; 0.0012979373134871764 0.0016927759883752684 -0.003702478480604875; 0.00017322290531834557 0.00025593857775005314 -0.0016345543348067054; -0.000924921011153888 -0.0004060531424008989 0.0003968560056137507; 0.0012580729481034348 0.0053645518181697415 -0.0018703380979932646; -0.0034613598725106312 -0.001395405186535538 0.0032433726876424994; 0.00180011526123706 0.0018333907811806938 -0.011527204666993833; -0.0025702780350803115 -0.004039244030699718 -0.0062446296115580705; 0.003457724747947209 -0.009705927361089915 -0.010300718222660992; 0.00010900902942530849 0.006777171986593095 0.0029331564548184304] %
+
+Mass Used: 95.68670186255349 kg
+Launch C3: 96.91811472526595 km²/s²
+||V∞_in||: 6.526670806867043e-9 km/s
diff --git a/archive/ES_0.5666113541986704 b/archive/ES_0.5666113541986704
new file mode 100644
index 0000000..405336d
--- /dev/null
+++ b/archive/ES_0.5666113541986704
@@ -0,0 +1,22 @@
+archive/ES_0.5666113541986704---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T19:56:22.422
+Launch V∞: [7.900742957102164, -5.552222324798963, 0.17451931363062817] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.132547014121761e-9, -2.1708676310610405e-8, -1.2710339449093058e-8] km/s
+ V∞_out: [-1.69103303947983e-8, 1.425911185380365e-8, 9.496311522611347e-9] km/s
+ time of flight: 1.8749577790511864e8 seconds
+ arrival date: 2030-04-20T22:05:59.422
+ thrust profile: [0.5994472813032884 0.004054320075580212 -0.16365297954754138; 0.08244757508160917 0.05031256828494317 -0.08250953830392127; 0.056184639470392955 0.056173507494593655 -0.1028228041601218; 0.024872511655747085 0.03333274966014758 -0.0685462206333265; 0.052379071610865746 0.08867998649310725 -0.1966036941108268; 0.011490202223981253 0.02326645446385315 -0.05718547329481916; 0.005754063474713394 0.015317246178402508 -0.04014463369837754; 0.003186275761681733 0.010083637116742896 -0.03172057230283802; 0.008801029503660011 0.001232354798748362 -0.003687819553587807; 0.0011489564573472612 0.008316183494885889 -0.021524314592644905; -0.001311928046243525 -0.0012413835312792127 -0.001428501902042128; 0.014025434429786527 0.010280432673501518 -0.02503162425809931; 0.0005443294929840908 0.0018505073803180682 -0.0027172966668991367; -0.015935134604793372 0.007482321086283962 -0.00914664189936141; 0.0032468728917850733 0.018925689102999445 -0.06513547607479857; -0.00017568766595194913 -0.010845656185623938 -0.0006585492132375702; 0.004449259552485573 -0.0047364566480202035 0.010601996799365458; -0.01726243683779803 -0.0005755830877873806 -0.012335508023800283; 0.004010301976972089 0.009431749274250605 -0.02509387864433209; -0.0005242564592162831 -0.003588951385994006 0.017337822541092184] %
+
+Mass Used: 116.91692734579965 kg
+Launch C3: 93.27936900902556 km²/s²
+||V∞_in||: 2.5493083393225608e-8 km/s
diff --git a/archive/ES_0.5666331541720689 b/archive/ES_0.5666331541720689
new file mode 100644
index 0000000..279aed2
--- /dev/null
+++ b/archive/ES_0.5666331541720689
@@ -0,0 +1,22 @@
+archive/ES_0.5666331541720689---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T18:07:28.367
+Launch V∞: [6.6065634227126315, -7.499201435210922, 0.2113726044681488] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00039941927620534286, 0.0025574920262335416, -0.003487368440956819] km/s
+ V∞_out: [0.0030032488430565794, 0.0025026729702913413, 0.0018530012689506993] km/s
+ time of flight: 1.8749577787450922e8 seconds
+ arrival date: 2029-04-11T20:17:05.367
+ thrust profile: [0.08899154933349088 -0.022475792979011575 -0.03649555095140519; 0.06140656961683461 0.01461061799590767 -0.07779215948988731; 0.044024303226200955 0.022152407863064952 -0.09294768599423785; 0.0291105194593497 0.018225346353528037 -0.08092705873340433; 0.02429904404672198 0.01740412837085529 -0.08692007503693747; 0.022560723388351387 0.02144735968722218 -0.10736136716592626; 0.017367550528908673 0.01815438568400633 -0.10133091345344052; 0.008173979489017835 0.007809568935646976 -0.04749149820818789; 0.013226866179101375 0.013839977089974094 -0.08432206381592057; 0.023261121901289032 0.02020984548658285 -0.12896790959909582; 0.002460035500374384 0.000635847366574504 -0.011520781700227849; 0.0020422068069795365 0.0017156179917624946 -0.003548668607172722; 0.004637900808291417 -0.00016957757924382073 -0.0014287796566348281; 0.003330091494828881 -0.004091833664741992 -0.012197949409617999; -0.00574604064385524 0.0058240997346174035 -0.005122160509232266; 0.0021700771155442077 -0.004351452839661055 -0.00045164980202393006; -0.0021609751476509317 -0.01001409173698842 -0.0027043106836433777; -0.0032275253438162374 0.00014318985418936632 0.004500442316846345; 3.183560513719002e-5 0.010660616773674487 -0.0031783994509974284; 0.0024781109477070564 -0.0003955316807021639 -0.000342648141610523] %
+
+Mass Used: 78.15062518841751 kg
+Launch C3: 99.92938080211364 km²/s²
+||V∞_in||: 0.004343044999241217 km/s
diff --git a/archive/ES_0.5666495451921495 b/archive/ES_0.5666495451921495
new file mode 100644
index 0000000..c3cf7ad
--- /dev/null
+++ b/archive/ES_0.5666495451921495
@@ -0,0 +1,22 @@
+archive/ES_0.5666495451921495---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T05:39:03.719
+Launch V∞: [6.630436119784487, -7.171628062454649, 0.2785769804837074] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.709951634599828e-6, 1.011856134113502e-6, -2.254771356058098e-8] km/s
+ V∞_out: [-1.5662078105957484e-6, 3.437196260613586e-8, 7.616168986373688e-6] km/s
+ time of flight: 1.8749577787084696e8 seconds
+ arrival date: 2029-04-06T07:48:40.719
+ thrust profile: [0.42310734664887034 -0.1056597599713735 -0.13503559656540398; 0.07295535578384531 0.022258289310970583 -0.07439596761123592; 0.08396731428471446 0.048640785886489624 -0.14238025942270063; 0.06261809680218389 0.04910211768348629 -0.14983470000006077; 0.047521359327219584 0.04553468821066681 -0.1471348387450356; 0.0215640579960037 0.02434073585958543 -0.08361857906613009; 0.014484352274398694 0.018981447721008116 -0.06750098805510422; 0.008562256400642416 0.012100459265667468 -0.0462095229954345; 0.005868644292482348 0.008924996183448013 -0.034986018053132555; 0.0031022171068452 0.004172745321070771 -0.021187185003327676; 0.000919303290826534 0.0017776363083439465 -0.0024545791254777785; -0.0002763970661168123 -0.00045733536010686263 -0.0016176177506838935; -0.002059216569538429 0.006761383310491803 -0.0022572885820687297; -2.2144442753750638e-7 0.00011944745288729641 -0.00018308852782743994; -0.002984286879167179 -0.0060829865374636 -0.0005952305380929056; -7.52812938850727e-5 -0.001006395648451575 -0.0012327788874588006; -0.002192760115770453 -0.0005487396532984625 0.004325871508083053; -0.01434089462602416 -0.0020905701918266916 0.005837902748569076; -0.0015520827155292923 -0.0003294702975927725 0.012305096605398188; -0.001079495250958113 -0.005531178510279182 -0.0041019324967300945] %
+
+Mass Used: 104.1680015812608 kg
+Launch C3: 95.47253733878519 km²/s²
+||V∞_in||: 7.776098986214006e-6 km/s
diff --git a/archive/ES_0.56665963466056 b/archive/ES_0.56665963466056
new file mode 100644
index 0000000..375f9e6
--- /dev/null
+++ b/archive/ES_0.56665963466056
@@ -0,0 +1,22 @@
+archive/ES_0.56665963466056---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T19:14:13.868
+Launch V∞: [6.331170432316695, -7.098229680574298, 0.26050284585857053] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.888184493282791e-8, 2.0245219032717624e-7, 1.1061060337490365e-7] km/s
+ V∞_out: [-6.952233807342323e-8, 1.2743858609701848e-7, -2.164510263930477e-7] km/s
+ time of flight: 1.8749577810405165e8 seconds
+ arrival date: 2029-04-03T21:23:51.868
+ thrust profile: [0.8254705238601255 -0.18504732005251262 -0.20682857021755457; 0.10396557086205165 0.03834696666171983 -0.08630725866366795; 0.07650051825431602 0.052875136582889656 -0.10671345506817274; 0.05127406011614926 0.04857952137570457 -0.10184862586272546; 0.028622789680606272 0.033795251648913886 -0.07561404559263939; 0.014600921086492398 0.02053801871843073 -0.04890457036399703; 0.06904610120897646 0.11659815887185132 -0.25369336132044173; 0.005544993165597369 0.010199853523073897 -0.02644173473598647; 0.006379053689377678 0.013103560449236678 -0.034984080778360065; 0.00037109395992867807 0.0008002648295521957 -0.0023949006131671617; 0.00011693445695850302 0.00011234518436369671 -0.00021185207789322876; -7.514364511591764e-5 0.0001347734459691614 -0.0003354154972515643; 0.00023633302799739734 0.00014861711595615083 -0.0007945173865695582; -1.764972654952693e-5 0.00012635114923545832 -0.0003275463217099624; 0.00013113043953764828 0.00023470567821412753 -0.00018851211528012372; 0.00011897686736479513 0.00019896816829219127 -0.0005718194349114672; 0.00024054117035452333 0.0005529995606547652 -6.375982224212512e-5; -0.0001695736714051464 0.0005866727772884187 0.00020552619913436236; 3.7279502450917224e-5 -9.688893923686802e-7 -0.0001537721025053325; 0.0004320647448684265 -1.1497548014474229e-5 0.0002129977886151771] %
+
+Mass Used: 132.97364242274307 kg
+Launch C3: 90.53644537392748 km²/s²
+||V∞_in||: 2.5099644261333917e-7 km/s
diff --git a/archive/ES_0.566660208433267 b/archive/ES_0.566660208433267
new file mode 100644
index 0000000..d3ca70b
--- /dev/null
+++ b/archive/ES_0.566660208433267
@@ -0,0 +1,22 @@
+archive/ES_0.566660208433267---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T03:12:40.657
+Launch V∞: [6.249697536696187, -7.6347521832392875, -0.12834747579293726] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2101722734997827e-10, -3.2267023537680095e-9, -1.138471054030397e-8] km/s
+ V∞_out: [4.212222327271077e-9, 6.260961991551913e-9, 3.030310487548594e-9] km/s
+ time of flight: 1.7347157221127862e8 seconds
+ arrival date: 2028-10-24T21:45:32.657
+ thrust profile: [0.2061363546969812 -0.07500139584650536 -0.07740777381827085; 0.08641100657920178 0.01403849391723832 -0.09006926410304805; 0.09519638607071387 0.03790028034523942 -0.16212872149815524; 0.07912193592145894 0.04398004251634266 -0.1857295014399546; 0.08767555636363215 0.05970247478602815 -0.2593343664809706; 0.02995103012449217 0.02330675283610865 -0.10766471049919471; 0.021415877083247204 0.018406205415707557 -0.08978978421619639; 0.004250925923235643 0.004506620834213277 -0.020044092393378826; -0.001339783141691371 0.0030454267568239455 -0.00932006063086529; 0.0021008795031727916 0.000438519109853928 -0.004990963325045733; 0.002652691595190165 -6.0134362816092264e-5 -0.010653681514920542; -0.0022067762630272095 0.002266355398014658 -0.006775058227479023; 0.0009357615247013476 0.0003827189980932738 -0.00016990035443821333; 0.0039078811793508625 0.0017479575012494092 -0.005344740905174429; -0.006595643286542021 -3.107537805044445e-5 -0.004085720205998572; 0.0015342274257516876 -0.004105660137057009 -0.0001560476646769854; -0.003100494202699447 -0.00161394388951979 0.002454106263705905; 0.009119620672686495 -0.004354377530140315 -0.004250908425697297; -0.0007945784560334118 0.007480870846400091 -0.007904669484684096; 0.00045698596443463765 0.0010775889367350446 0.0021102131361455598] %
+
+Mass Used: 93.14321573927737 kg
+Launch C3: 97.36463327420587 km²/s²
+||V∞_in||: 1.1835205565646326e-8 km/s
diff --git a/archive/ES_0.5666606080330524 b/archive/ES_0.5666606080330524
new file mode 100644
index 0000000..047c3ac
--- /dev/null
+++ b/archive/ES_0.5666606080330524
@@ -0,0 +1,22 @@
+archive/ES_0.5666606080330524---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:45:09.450
+Launch V∞: [6.560894654440069, -7.419458904022398, -0.022697114766479447] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.723936575122449e-6, 5.45142673838255e-7, 5.867748862703191e-9] km/s
+ V∞_out: [1.0807992279092e-6, -2.434235874610676e-8, -4.636552008645187e-6] km/s
+ time of flight: 1.8593936972866076e8 seconds
+ arrival date: 2029-03-22T08:34:38.450
+ thrust profile: [0.1877474786978581 -0.05025293417384218 -0.06969405239496537; 0.057328102767663626 0.01384469478073209 -0.06276033153622491; 0.0688216108233505 0.03339484199192914 -0.12724480490862927; 0.06591630026863461 0.043147087627015766 -0.17144295288870665; 0.044535542010988124 0.03490201491806956 -0.14802574046721048; 0.03357414728478947 0.03000082108392989 -0.1357114709014418; 0.01824832422532255 0.01794026281544005 -0.08603088333587226; 0.008304893922203281 0.008898503281454802 -0.04418691304662184; 0.0003405924873903436 0.00019912515778579645 -0.003055606998485489; -0.0035428479212945164 0.0030242153089058404 -0.007360914887141623; 0.007068362715993021 -0.0033114611353829556 -0.014178601734210941; 0.004348440304530363 0.0035414336841189985 -3.2369140490683785e-5; 0.0017578621123311427 0.002436505469023228 -0.008234229457059448; 0.0006454594497501119 -0.0033177854734525317 -0.005063907546107872; -0.004395246640717609 -0.011032871394229277 -0.00502890577107593; 0.012246745685630129 0.00932184883070858 0.0021126532924347803; 0.004220846151514795 0.01918173068961418 -0.0028242477430320445; 0.0010266601352988808 -0.0011586368102617798 -0.015150580201488776; -0.010326148878231106 0.0013273428172041483 -0.00024369057315752965; -0.007566731551012052 -0.0052226967589588036 0.0067430834130958114] %
+
+Mass Used: 88.88773455598312 kg
+Launch C3: 98.09422425415623 km²/s²
+||V∞_in||: 4.755290919712048e-6 km/s
diff --git a/archive/ES_0.5666681403296812 b/archive/ES_0.5666681403296812
new file mode 100644
index 0000000..a144d34
--- /dev/null
+++ b/archive/ES_0.5666681403296812
@@ -0,0 +1,22 @@
+archive/ES_0.5666681403296812---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T14:13:33.663
+Launch V∞: [6.462795949282218, -7.518132860919457, 0.2737169094415935] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2193962117619926e-7, -2.6045088804798046e-8, 3.257191963182614e-8] km/s
+ V∞_out: [-1.2827074806300574e-7, 1.2263293745697e-8, -1.53625490976935e-8] km/s
+ time of flight: 1.8207863438282767e8 seconds
+ arrival date: 2029-02-04T23:37:27.663
+ thrust profile: [0.18206097836147636 -0.05344573964021092 -0.06624407243270229; 0.03760471275945144 0.008109265641754517 -0.04218023947654344; 0.07004933990788013 0.03128384426305816 -0.1255411216062848; 0.0680375850570654 0.041038024826717874 -0.16977875687235697; 0.04917636280985293 0.035470767245438815 -0.15529294113425626; 0.019379053103230074 0.0159280322350881 -0.07557051856674211; 0.012827168243244586 0.011683336973627745 -0.05818493883337963; 0.01700400091187368 0.014986493825739968 -0.08625039800114771; 0.008867335822027466 0.009300478537323603 -0.054407580250349794; 0.004910094038298959 0.00435232587763969 -0.024548948737698677; 0.007820058970427703 0.009215669504613756 -0.053626616659974764; 0.0001445126033897883 0.00048576335686824736 -0.005923908891667165; 0.0027065126082048098 0.000922443690674093 -0.001024921201410887; -0.0035773626215685507 0.005318923688982237 -0.008365648768315791; 0.005407600381578946 0.0006697642297118824 0.003257164565934287; -0.0017687876132232148 0.0003526282920405623 -0.005025104511356629; -0.002161151807722591 0.0044708006484902914 -0.005334191073566205; 0.004318804442586373 -0.011285945351405353 -0.010967137467859527; 0.007657525970268151 0.003890632977726365 -0.00989337804603293; -0.006752121149338802 0.008927242703243262 -0.001266654517108827] %
+
+Mass Used: 87.3171478837371 kg
+Launch C3: 98.36497414300987 km²/s²
+||V∞_in||: 1.2887415494173742e-7 km/s
diff --git a/archive/ES_0.56666905749986 b/archive/ES_0.56666905749986
new file mode 100644
index 0000000..bcc824f
--- /dev/null
+++ b/archive/ES_0.56666905749986
@@ -0,0 +1,22 @@
+archive/ES_0.56666905749986---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T05:41:17.263
+Launch V∞: [6.438440893850522, -7.62052689331773, -0.006675823580616076] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.261928575903157e-9, -3.27750799352138e-9, 7.042041302852936e-9] km/s
+ V∞_out: [1.6918308675654154e-9, -4.181844253470391e-9, -5.238703960439917e-9] km/s
+ time of flight: 1.870746572480836e8 seconds
+ arrival date: 2029-04-08T10:52:14.263
+ thrust profile: [0.14515294069820628 -0.0420218757208502 -0.06310813796306954; 0.07987598736912793 0.013626807083038404 -0.10710373779739216; 0.03474445083840562 0.011745767473540506 -0.07942225503445034; 0.048150435022275 0.022915471194898382 -0.1598071981784837; 0.033515680189805594 0.01758511627841885 -0.13674426656645533; 0.023095702626589498 0.012625149480714618 -0.11061082597213372; 0.010981471174658277 0.0067246100490288545 -0.06524192958638668; 0.00822468110090912 0.0048993977155049485 -0.05414648481033816; 0.007762567207063957 0.004757845684017472 -0.05582835033884039; -0.000886070932304596 -0.00041299424292526635 -0.01179556251036914; 4.6560151883224816e-5 0.00047479379980503974 -0.003000113565677785; 0.004570790893687988 0.002944450985470108 -0.0419581291174202; -0.0033072770175383366 0.0002966120559385776 0.0014119221189497332; -0.0005213833087319569 -0.00016056772497780822 0.0033333582125347977; 0.0022575820656074827 -0.0015244639356149533 -0.0022750870376578524; -0.005229545224548424 -0.00388791095527638 0.0004931521823158115; -0.0018865801685807031 0.0021783680406266977 -0.0014250917400493864; -0.002906767690340769 0.0030720466564950048 0.002515984371123856; 0.006731361619690151 0.0040994590888503565 0.0003234087206001884; 0.0018863591912491322 -0.0026721511541293605 -0.0006983193299726481] %
+
+Mass Used: 80.54559133813518 kg
+Launch C3: 99.52599584200597 km²/s²
+||V∞_in||: 8.859821642944237e-9 km/s
diff --git a/archive/ES_0.5666721032326041 b/archive/ES_0.5666721032326041
new file mode 100644
index 0000000..e09f483
--- /dev/null
+++ b/archive/ES_0.5666721032326041
@@ -0,0 +1,22 @@
+archive/ES_0.5666721032326041---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T21:39:54.979
+Launch V∞: [6.480210431719866, -7.304891628002413, 0.17089148252990302] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01785831874035362, -0.007504665637291831, 0.018714149565881064] km/s
+ V∞_out: [-0.01590301320306551, -0.007329771821691897, -0.020463521873902463] km/s
+ time of flight: 1.8749577787477192e8 seconds
+ arrival date: 2029-04-07T23:49:31.979
+ thrust profile: [0.4164477621051888 -0.09308304834673516 -0.11766301313078671; 0.07111968097106008 0.024121433974835238 -0.0671118717741137; 0.057321448417370094 0.036064556576377936 -0.08942781998178828; 0.04623973560038009 0.039442471845136336 -0.10122555275254157; 0.03345099414598165 0.03444570734835183 -0.09417000658230926; 0.019160937758471407 0.023555916048240002 -0.06938090996387015; 0.033083430501215746 0.05328195249056691 -0.17688819258544536; 0.004104787032086321 0.007987617335351213 -0.025801099653120295; 0.015908159883013227 0.025200899314106174 -0.0828904613534484; 0.004418439099594232 0.008437777213527363 -0.032212224013374834; 0.002923033409815674 0.0016912228531765412 -0.009710655768596867; 0.0050006509967825685 0.009285392345004067 -0.03569491390446258; 0.0010404247950296184 0.003753343642866365 -0.004872682483001374; -0.0016613067140031058 -6.0500084784115716e-5 -0.0010374564677788842; -0.0016084777774713938 0.0016564196961594002 -0.0017082206498143025; 0.0006615687105865481 0.005026644854460419 0.006140048115479142; -0.0026819184298065043 -0.0029170817734675116 -0.008855543006962245; -0.0018927268547374255 -0.007930330380356084 -0.015803792095212196; 0.001556274658512243 -0.004399486136522504 0.007901245065735085; -0.0006860346346967635 -0.005666205044503981 0.005045387658536585] %
+
+Mass Used: 104.71211223368482 kg
+Launch C3: 95.38377283503199 km²/s²
+||V∞_in||: 0.026934345147669368 km/s
diff --git a/archive/ES_0.5666735913523809 b/archive/ES_0.5666735913523809
new file mode 100644
index 0000000..10f1d64
--- /dev/null
+++ b/archive/ES_0.5666735913523809
@@ -0,0 +1,22 @@
+archive/ES_0.5666735913523809---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T20:12:47.265
+Launch V∞: [6.290046342544382, -7.26267016115376, 0.2484311956301031] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3695371838430362e-7, 3.639998459803049e-8, -4.7284109737879597e-8] km/s
+ V∞_out: [1.4644899576977033e-7, -3.211139324115224e-8, 9.009406544791908e-9] km/s
+ time of flight: 1.8600007651131207e8 seconds
+ arrival date: 2029-03-18T14:54:03.265
+ thrust profile: [0.6186266810015466 -0.1355759792468542 -0.1375237727581987; 0.09417199042555177 0.036078837160409515 -0.07706267283930564; 0.10000250050982873 0.07239158875778497 -0.1355173036849951; 0.06776510112295626 0.06726899696801202 -0.12890367490270946; 0.054433280797249455 0.06793121846138786 -0.13673593718844787; 0.023721498071457597 0.03381891173942402 -0.07387442130416108; 0.03233099192902384 0.05637028652142243 -0.1225246298576023; 0.011140402488330193 0.020947740748572502 -0.049880742129974356; 0.0028774861521114244 0.006304023405251736 -0.01579496136769173; 0.006017850845070054 0.013099590367573216 -0.034032420160606904; 0.0008170101795237235 0.0017950918846594266 -0.005980282994323863; -0.0008455920147043771 0.0011720683610010364 -0.0031365452612187846; -0.0009187564381403614 0.0014826280186234072 -0.001625799906635497; 0.0021751199394820283 0.0009782464177763104 -0.0008692141063803306; -0.0016141801220302902 -0.000912551854466512 -0.001594642092491434; -4.2761080320464926e-5 -0.00034225372497537204 0.002043951882165102; -0.0002549151282661752 -0.0021315719599253008 -0.0011901554705562856; -0.0008355516276191823 -0.0034958436809094866 0.0041033226849503624; 0.0017012535133904755 0.001230466912820826 -0.00034607489749428856; -0.0030481144413461655 0.007495162351143014 0.0011110125188299879] %
+
+Mass Used: 122.2779795442616 kg
+Launch C3: 92.37277892003134 km²/s²
+||V∞_in||: 1.4938897848143898e-7 km/s
diff --git a/archive/ES_0.5666801958405926 b/archive/ES_0.5666801958405926
new file mode 100644
index 0000000..a6c6d3b
--- /dev/null
+++ b/archive/ES_0.5666801958405926
@@ -0,0 +1,22 @@
+archive/ES_0.5666801958405926---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:30:36.892
+Launch V∞: [7.480102359860277, -6.4814152296004215, -0.3020364808179663] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6535721831644374e-9, -4.939362018449627e-9, 1.8393457687795307e-8] km/s
+ V∞_out: [5.302192796282792e-9, -1.7415265474730206e-8, 2.634629101410489e-9] km/s
+ time of flight: 1.6117674038719672e8 seconds
+ arrival date: 2029-06-18T14:49:36.892
+ thrust profile: [0.24933011102842215 -0.050050844798224546 -0.10289922555393691; 0.054429818376554015 0.015573871962528501 -0.06831095406596159; 0.06429253876005019 0.03391596367941441 -0.13457804015662805; 0.05594758475277533 0.03848664805265722 -0.16348983637248324; 0.042385416560085605 0.034233891021160145 -0.15887831032539435; 0.03452985152637656 0.031113690652614056 -0.15621897012609887; 0.014810439539118123 0.014199924318217177 -0.08014638817872682; 0.006478293773030821 0.006173638347628284 -0.037774775738411474; 0.012819311159200202 0.013810074022277137 -0.08905018080585574; 0.00769038875133136 0.007796594084272375 -0.052725407364858014; 0.009617787055778267 0.01160104191372048 -0.07751159796300135; 0.0004835654428320818 0.0004309125682136751 -0.003797104065451898; -4.9222290482585886e-5 3.280747178271222e-5 -0.0008166925575226252; 8.662698341100765e-5 -0.00033893760714283046 -0.0009946762026973078; 0.00015812903815923886 0.0006980257069661075 -0.0007788354293077334; 0.0002125238865175118 0.0002291083881971657 -0.00241429032822955; 0.00023268088888030267 0.005747594914370255 -0.003849645072247406; -6.342573970555265e-5 -9.100775745358634e-5 -0.0005717738569313378; -0.00014507821207706954 -0.0004378960029813761 0.0001110575004240966; -0.0010728544206416836 0.0006418038316398278 -0.002310255123224002] %
+
+Mass Used: 89.15747423269204 kg
+Launch C3: 98.05190072822846 km²/s²
+||V∞_in||: 1.9116769701676963e-8 km/s
diff --git a/archive/ES_0.5666862148895373 b/archive/ES_0.5666862148895373
new file mode 100644
index 0000000..e74ebbb
--- /dev/null
+++ b/archive/ES_0.5666862148895373
@@ -0,0 +1,22 @@
+archive/ES_0.5666862148895373---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T07:16:24.474
+Launch V∞: [6.556824274829386, -7.452394190810035, 0.04894187284195824] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.82820672713822e-6, 4.681099019380773e-6, 4.948686038519606e-6] km/s
+ V∞_out: [7.259635869554857e-6, 4.1202361837016664e-6, 1.4271468165177258e-7] km/s
+ time of flight: 1.874957778744924e8 seconds
+ arrival date: 2029-04-11T09:26:01.474
+ thrust profile: [0.18813947556244567 -0.05196062216749538 -0.07302594937534912; 0.08795956888955735 0.01636094906648997 -0.10692789349356414; 0.03752837753032183 0.016394114099619723 -0.084140440844794; 0.030224545084336266 0.01579897031299663 -0.09234788614381644; 0.01200895388557915 0.007651954131648304 -0.0483952626986409; 0.011660947293681466 0.008164950814352756 -0.05422729530845475; 0.05736350570964115 0.040115027160434136 -0.25395761133279326; 0.004890639061250711 0.004412273890891853 -0.030382366753956603; 0.001535450739778263 0.004108006455073276 -0.011270774356150636; 0.012590967701518067 0.008897781525566808 -0.06939799560651823; 0.005161529133090811 0.009454512444557875 -0.05481110579752211; 0.0007974701544868685 0.00018187536575404973 -0.006537805923527485; -0.001635211673340071 -9.385451818787584e-5 -0.004631058248532557; 0.00048395872627500416 -0.002196583346384495 -0.005211598416400535; 0.0003311434393800627 -0.0037937501224940724 -0.006015837548792374; -0.0002878598969714936 -0.0033576790870308024 0.0019663811837239333; 0.009598195785504953 0.0006637772171568913 -0.006440519612267595; -0.006447838433401257 0.009125215430517478 -0.003676368069868127; 0.010216433592761847 0.008227858885306812 -0.0048095654564798175; 0.001981771617308074 0.0003069064981476772 -0.011136913072162635] %
+
+Mass Used: 86.36088956121148 kg
+Launch C3: 98.53251905312834 km²/s²
+||V∞_in||: 8.349476734327083e-6 km/s
diff --git a/archive/ES_0.5666897784757571 b/archive/ES_0.5666897784757571
new file mode 100644
index 0000000..d7597c1
--- /dev/null
+++ b/archive/ES_0.5666897784757571
@@ -0,0 +1,22 @@
+archive/ES_0.5666897784757571---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T02:20:47.543
+Launch V∞: [6.364373518599498, -7.293490840020673, 0.7793856457259719] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003827915324701152, 0.00043794946804109674, 0.00042334785285002327] km/s
+ V∞_out: [-0.0004927271024655183, -0.00022099365693495967, 0.00047707829339445503] km/s
+ time of flight: 1.8292050320977443e8 seconds
+ arrival date: 2029-02-10T05:35:50.543
+ thrust profile: [0.42283427229163123 -0.11014657388127261 -0.11686452353684336; 0.2513283861262624 0.0728318296567108 -0.20917804615236418; 0.0937855860980297 0.05391721889298003 -0.13632721238572673; 0.09128201654934912 0.06971034730210653 -0.18161965228443763; 0.04777916496747002 0.048219652726952146 -0.12935134974067958; 0.015204944501300539 0.016985499480191225 -0.05222019764715468; 0.005869768352372118 0.008146687846512436 -0.025180174423335377; 0.009123769471076975 0.01327520074881775 -0.04316228137756869; 0.006447787314689214 0.008957602837153083 -0.03206905128213748; 0.0031211702093372796 0.002773467224315953 -0.012630698925427722; 0.00019157616837200492 0.0012354583301273526 -0.002351565816884062; -0.00024272864187328906 0.00036400578591549765 -0.0003990383322990596; -0.000317141595349455 -0.00013374269196098076 -0.0025805665215889576; -0.00036597631906099546 -0.000318396568170057 0.001023245776283079; -0.0014084956536328708 -0.0017863377781158186 -0.00011801343520695482; 0.002304680256025775 0.0030679927750996176 -0.0025241738870100897; 0.00033017953316753524 -0.0005057905002161203 -0.001564612956067824; 0.0004929238237931753 0.0004088368794599329 0.00030156611666485385; -0.0006912590323635889 -0.005274129589237492 0.0051965411973725366; 0.0006888278642110267 0.00017132349885087963 4.525485137841156e-5] %
+
+Mass Used: 111.00981962391825 kg
+Launch C3: 94.30770090247971 km²/s²
+||V∞_in||: 0.0007194112164826343 km/s
diff --git a/archive/ES_0.5666999268782198 b/archive/ES_0.5666999268782198
new file mode 100644
index 0000000..0c9a7f7
--- /dev/null
+++ b/archive/ES_0.5666999268782198
@@ -0,0 +1,22 @@
+archive/ES_0.5666999268782198---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T00:46:17.364
+Launch V∞: [7.478461299921209, -6.475994858611877, -0.15261663664344935] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0002426082306553934, 0.01635263098567045, -6.250867422762392e-5] km/s
+ V∞_out: [0.01579473888156578, -0.0025245334379720885, 0.003417705659557926] km/s
+ time of flight: 1.5967720143783316e8 seconds
+ arrival date: 2029-05-31T03:32:58.364
+ thrust profile: [0.21602940650940536 -0.046430704394960706 -0.0850729205499445; 0.08694826460781468 0.0250801504939242 -0.09990063793165914; 0.08749072704752046 0.045423193302276885 -0.16678482318960242; 0.07538394889524071 0.050757038998806556 -0.20042864029458676; 0.05115444617269793 0.04075004103745883 -0.1746784247771448; 0.024992128325799817 0.022893743475185413 -0.10544666213496498; 0.013841918018008102 0.013369807851480743 -0.06524974677815357; 0.015685801463758545 0.018536447912295757 -0.09152150002925791; 0.019427777647756675 0.023009569067400246 -0.12066062897496332; 0.0034755580733513026 0.0038967682437462572 -0.023308519899320344; -0.0008717024932046598 -0.00011965725277265861 -0.0036902440680560825; 0.00141065561893024 0.0015710060253960605 -0.005437971814638612; 0.0010033945872333617 0.0010693602528430582 -0.0007479655708268079; -4.462023338035171e-5 -0.0008138905288623327 -0.00039115057313252044; -6.755043538579707e-5 -0.0005024393460572475 -0.0017935353586653858; 0.0010733283978769284 0.0020782655861337385 0.00012927937249547928; 0.0010324302701369204 -0.0014656231689664223 0.0020533941810080593; 2.6863831467465425e-7 6.1377315046469e-5 -0.0008528233796582119; -0.0005551401966804321 0.0008325652324560312 0.001424680315837748; -0.0001474193642682527 0.0016565501607237257 -0.0014526188357373458] %
+
+Mass Used: 90.12967083561534 kg
+Launch C3: 97.88918466096703 km²/s²
+||V∞_in||: 0.016354550016476906 km/s
diff --git a/archive/ES_0.5667017076220804 b/archive/ES_0.5667017076220804
new file mode 100644
index 0000000..e559e9b
--- /dev/null
+++ b/archive/ES_0.5667017076220804
@@ -0,0 +1,22 @@
+archive/ES_0.5667017076220804---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T10:22:26.386
+Launch V∞: [6.488629560015167, -7.31506776092247, 0.28039224334690843] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.267975239123516e-9, -4.2734932524236356e-9, 1.285786774261622e-8] km/s
+ V∞_out: [4.168933836884673e-9, -9.441457469826203e-9, -1.2854577870907233e-8] km/s
+ time of flight: 1.8389204469398e8 seconds
+ arrival date: 2029-02-22T19:29:50.386
+ thrust profile: [0.32672999926158086 -0.08598367459563125 -0.09803066014375156; 0.1753839240420577 0.0517186896805353 -0.1565528815062488; 0.08205570119953182 0.04744185618202378 -0.12395186787422552; 0.03850127376750586 0.03071286306971776 -0.08243797142431925; 0.0629184343861734 0.06075815018615313 -0.16990496417595163; 0.009535812878557726 0.011509377846119575 -0.03321395689424683; 0.006465555203152761 0.008623221673660931 -0.025448903324947626; 0.047540416388385374 0.062472106456344066 -0.19606640377317724; 0.003925549882060705 0.00818983041478548 -0.025398511296041856; 0.0018489662820677395 0.0014082413680176157 -0.017761612795741528; -0.0019536696853549836 0.00014076147611682271 -0.0031042375188118938; -0.003412575907558927 0.0014901020090769192 -0.0033088577505120983; 0.004202071327934382 -0.0016146980948115257 -0.002851127637150981; 0.004661256743088644 4.361983121922995e-5 -0.003880404145855611; 0.002453980929452591 0.0031913143036213162 -0.004361825558553056; -0.0001230739849642153 -0.0004892617567521941 0.0019688383470385998; 0.0006987873030642247 0.0014292649826825432 -0.0057668456600821795; 0.0014032999076563745 0.001718458906250208 -0.002564454562811214; 0.0069933235026086536 0.004631177340958651 0.004375645848917049; 0.0007720978550429581 0.0006141899820107083 -0.0031994036169140806] %
+
+Mass Used: 102.95361883506621 kg
+Launch C3: 95.69114972411901 km²/s²
+||V∞_in||: 1.587283597911478e-8 km/s
diff --git a/archive/ES_0.5667025529546332 b/archive/ES_0.5667025529546332
new file mode 100644
index 0000000..050fc15
--- /dev/null
+++ b/archive/ES_0.5667025529546332
@@ -0,0 +1,22 @@
+archive/ES_0.5667025529546332---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T10:27:48.978
+Launch V∞: [6.276372272069706, -7.5657651314325145, -0.35527887829023785] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.134441152835906e-8, -4.080293051037338e-8, -6.570902208057001e-8] km/s
+ V∞_out: [3.38525306497765e-8, -4.9968961445902264e-8, 8.149589933570881e-8] km/s
+ time of flight: 1.775022073744083e8 seconds
+ arrival date: 2028-12-11T20:37:55.978
+ thrust profile: [0.29176937382190743 -0.09471340639617966 -0.10607898076147013; 0.0759289989296374 0.01662714805800312 -0.07992822504409201; 0.051616798204069204 0.024349591773879107 -0.09093224934591652; 0.06924748704615692 0.04422238719503797 -0.16296898050236477; 0.059808098763474066 0.04686280387238111 -0.17974075291524294; 0.032637015436610774 0.03043371202561449 -0.12233061006896724; 0.020839044576285395 0.021876420787364816 -0.0924694067996679; 0.008700868395415768 0.008107890610514746 -0.04100886061168577; 0.00420615235434311 0.006844608418681318 -0.02800317202849756; 0.013199080779958362 0.02180430556665534 -0.10244437762252366; 3.506810283774946e-5 0.0006899721104146747 -0.008809354198063066; -0.004631110776797097 8.709405503871167e-5 -0.003312361118385137; -0.0006437681865760915 0.0001753790436540832 0.0008283701626904329; -0.002334814179773119 -0.0004942247304170335 0.0003309295676861856; -0.002065694877575348 -0.003307265128486392 0.0007189316749681629; -0.000517748700368051 -0.0005795989167301876 0.0018239979535721322; -0.000938000016472206 -0.003793004346275672 0.00110912929112038; 0.002225102748564129 -0.0022824720914838463 0.0017349786192952916; 0.0036154926412948715 -0.0010898105577913924 -1.9429271804231093e-5; -0.00070792716614579 -0.00033371229401736244 0.00699434102307981] %
+
+Mass Used: 96.72038009644484 kg
+Launch C3: 96.75987400296466 km²/s²
+||V∞_in||: 1.0522632644612778e-7 km/s
diff --git a/archive/ES_0.5667123219152685 b/archive/ES_0.5667123219152685
new file mode 100644
index 0000000..1224c5a
--- /dev/null
+++ b/archive/ES_0.5667123219152685
@@ -0,0 +1,22 @@
+archive/ES_0.5667123219152685---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T13:08:56.576
+Launch V∞: [7.272622201180129, -5.957642850714617, 0.45254093929939526] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6434568985522025e-7, -2.2810797961749564e-6, 4.182754253412682e-7] km/s
+ V∞_out: [-3.787687654924672e-7, 1.246887337396996e-6, 1.900451830841009e-6] km/s
+ time of flight: 1.7868918788628212e8 seconds
+ arrival date: 2030-01-03T17:02:03.576
+ thrust profile: [0.7428702589888141 -0.011770114444658647 -0.13526077228888025; 0.34214157594221567 0.21254579582640099 -0.2227441978201952; 0.16724224656470343 0.18540641607189548 -0.21010680293488915; 0.08872487680462089 0.132711485436654 -0.17220525614504908; 0.02280720020220077 0.044078025456253056 -0.06806271748264646; 0.009034840185260318 0.019506167995018437 -0.03466623955443016; 0.007284747379661608 0.020757359980178563 -0.036928232881377115; 0.00473474508978094 0.014682129999212368 -0.02772286376158569; 0.005082543553230877 0.01802272320461048 -0.03038697723483036; -0.00029707514685583635 -0.0004514385144637878 6.406803554286154e-5; -0.0007127145128118538 0.0004765267406369139 0.00047346158835416644; -1.5671772520011922e-5 -0.00046500831589204076 0.0004495600587908505; 0.0001936459031112724 -0.0008741325995589025 0.0010723984251206358; 0.0001264575666625563 0.00045786199460571344 -0.0008687268984829193; -0.00014448774122592442 -0.001483153927001399 0.002804376102514657; 0.00034264539049662455 -0.0026661928223381476 -0.0003736370582956784; 0.000998724443535436 0.0002948599621125857 -0.00032373098711098837; -0.00039217578001567995 0.00041160076489241907 7.101803948835774e-5; -0.0008871708172285991 -0.0030482646715552205 0.002502853028233442; 0.00010600253230971557 0.0007384638329048747 -0.0009084396137148061] %
+
+Mass Used: 144.3932528706655 kg
+Launch C3: 88.58933531951106 km²/s²
+||V∞_in||: 2.334128962098502e-6 km/s
diff --git a/archive/ES_0.5667150850083381 b/archive/ES_0.5667150850083381
new file mode 100644
index 0000000..087ad08
--- /dev/null
+++ b/archive/ES_0.5667150850083381
@@ -0,0 +1,22 @@
+archive/ES_0.5667150850083381---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T22:24:56.154
+Launch V∞: [6.57842068552691, -7.291246980208207, 0.21118814949843046] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.804547221020031e-6, 3.4955504772456314e-6, 4.179231032732687e-6] km/s
+ V∞_out: [5.684355895933197e-6, 3.442075570222526e-6, 1.0671764352225668e-7] km/s
+ time of flight: 1.8749577787493062e8 seconds
+ arrival date: 2029-04-09T00:34:33.154
+ thrust profile: [0.3648480794877507 -0.09639865890507972 -0.12938358299077038; 0.04000095732814677 0.010350949392176609 -0.0435708400291759; 0.043293838951095134 0.021497714830288513 -0.08053765091046282; 0.04912058723766091 0.03248550670550674 -0.1278942045367903; 0.037914454968779765 0.030091194747277252 -0.1266139948212368; 0.024909153406145766 0.02263464807255522 -0.10134134480766857; 0.01954803983953779 0.01987046166039587 -0.0925219398918508; 0.027903429584251235 0.030286904519876423 -0.15235642423875062; 0.0023805595887819594 0.0037802415543872125 -0.014183657735806616; 0.0013994861825520997 0.003281103106616083 -0.006557767322572863; 0.001546778248289239 0.002610408793531969 -0.00863787130419833; -0.00027502635842669375 0.0018759576242724097 -0.0055271229630158535; -0.003245322110124017 -0.0026620335318437607 0.0021133669226921104; -0.0018180497331716852 -0.002515764542518769 -0.005665582590534993; 0.00022855259121393559 -0.008544306421316629 0.005380167019630039; -0.008306932588723599 -0.01195690930940746 -0.008615083967627592; 0.013349549689794009 -0.008376059492618092 -0.003180621966075492; -0.01498738413255655 -0.004322443798514423 -0.008605423793847499; -0.00369462836067017 -0.0034107161019037557 0.0021581161871674776; 0.00809568165468147 0.0037700438970776676 -0.007997526161793514] %
+
+Mass Used: 98.35300606258988 kg
+Launch C3: 96.48250167665222 km²/s²
+||V∞_in||: 6.645255805527679e-6 km/s
diff --git a/archive/ES_0.5667170861138429 b/archive/ES_0.5667170861138429
new file mode 100644
index 0000000..54a9d79
--- /dev/null
+++ b/archive/ES_0.5667170861138429
@@ -0,0 +1,22 @@
+archive/ES_0.5667170861138429---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T14:28:21.258
+Launch V∞: [6.257166504562989, -7.4859738892632555, 0.23995004805094983] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0001301813878119319, 0.00013736539078632262, 0.0001301955968131704] km/s
+ V∞_out: [-0.0001533405975284423, -7.634051071777434e-5, 0.00015301740553855117] km/s
+ time of flight: 1.8284732508118844e8 seconds
+ arrival date: 2029-02-11T21:23:46.258
+ thrust profile: [0.3166199012642938 -0.07243288203325117 -0.09137511810034328; 0.19862699375928128 0.059982780465705154 -0.1666676361074742; 0.07944190767358465 0.051821865627284816 -0.12066865850381422; 0.03558220947344534 0.030742225174867358 -0.07604672877492254; 0.03826185424182153 0.04315313608500008 -0.10584441697154542; 0.05635352662311273 0.07416306131327044 -0.18080563583319637; 0.01963764997887998 0.02867767115469098 -0.08092105129272427; 0.014775863847017623 0.02214839203733316 -0.06526279503750458; 0.004485836995925868 0.007305835754815358 -0.0235671697775503; 0.00032699785481902577 0.0047331190788457165 -0.009141312902104364; 0.002799593020254254 0.005487881610485733 -0.01886908991610697; -0.0002111156993346401 0.0031740368494220204 -0.012420398612614346; 0.0021298840490293985 0.0006912065460245805 0.0022054756009455374; 0.000604813919391914 0.0008423831070195284 -0.003839682810962527; -0.00014610103085291315 -2.7506207085590054e-5 -0.0020218728130004505; -0.007161868686568445 0.005954175764161347 0.0009620976069766658; 0.00028884889317725305 -0.005787587722629366 -7.475505453549518e-6; -0.005322636014831015 -0.002933202286369558 -0.004286817313248082; 0.003023288457908796 -0.0067262193666887396 0.008009811834336656; -0.0037108417282953193 0.00296477267216013 0.008883683544524776] %
+
+Mass Used: 105.54777018714049 kg
+Launch C3: 95.24951376211591 km²/s²
+||V∞_in||: 0.00022971142276355649 km/s
diff --git a/archive/ES_0.5667228913320583 b/archive/ES_0.5667228913320583
new file mode 100644
index 0000000..1f196d5
--- /dev/null
+++ b/archive/ES_0.5667228913320583
@@ -0,0 +1,22 @@
+archive/ES_0.5667228913320583---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T02:12:39.577
+Launch V∞: [6.43016156824315, -7.2138167786469705, 0.30796268682245037] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.980221503859033e-6, 1.0970241862345389e-6, -2.039395354331714e-8] km/s
+ V∞_out: [-1.3778305305322674e-6, 3.120042706843773e-8, 6.940683420815257e-6] km/s
+ time of flight: 1.874957778588855e8 seconds
+ arrival date: 2029-04-06T04:22:16.577
+ thrust profile: [0.5114655680728775 -0.12519440200894322 -0.1514183564622669; 0.15537894142553843 0.04834626624959639 -0.14138717621905955; 0.09003564932014457 0.054052683517363656 -0.13917757407414183; 0.07327276926070132 0.05964704533588027 -0.15942707013824664; 0.03500246218830398 0.03607495377584032 -0.10098961510338167; 0.02183175079724329 0.026910147860108414 -0.07873453947475567; 0.0042022518234332154 0.006240838124539203 -0.020683415113626702; 0.008312517915464826 0.023063841586852697 -0.06191986083113687; 0.005662309801348846 0.010265215743473523 -0.030546188417461; 0.0059002052390248975 0.0038122961271977087 -0.011610317533780222; 0.00023225884032306075 -0.00032098087952563397 -0.0030188143373407776; -0.0008146932674786816 0.0012473062145447926 -0.012383323252908215; 7.562806535492319e-5 0.002275393662035322 -0.00871135672037289; 0.008404433140729814 0.005255258858730668 -0.017931028494534134; 0.0020121860293348735 0.0034273781904230636 -0.003907226534493444; -0.0005672921721282681 -0.009081249927561694 -0.005307383662294277; 0.0011904159770711217 0.005659228356734082 -0.0070643130004088735; 0.005173513311408988 0.002769163579547109 0.004918699628036623; -0.003586508186399026 0.000426594476285694 -0.00837834295296855; 0.007865037996167203 0.0008068381198255378 0.0017872857708024145] %
+
+Mass Used: 115.87104048529909 kg
+Launch C3: 93.48097132607467 km²/s²
+||V∞_in||: 7.065930244593471e-6 km/s
diff --git a/archive/ES_0.5667280118534229 b/archive/ES_0.5667280118534229
new file mode 100644
index 0000000..49734da
--- /dev/null
+++ b/archive/ES_0.5667280118534229
@@ -0,0 +1,22 @@
+archive/ES_0.5667280118534229---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T10:18:44.093
+Launch V∞: [6.257826064122974, -7.654028816959386, 0.03529920638454202] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1375147268991854e-7, 2.302727225294707e-7, 1.021744500299927e-7] km/s
+ V∞_out: [-8.782469437467271e-8, 1.4092586695622753e-7, -2.2134103259434204e-7] km/s
+ time of flight: 1.7854460413109964e8 seconds
+ arrival date: 2028-12-25T22:02:08.093
+ thrust profile: [0.22314061006559577 -0.07006959546123884 -0.0846753651143935; 0.08549526323804416 0.018016162196297123 -0.09490693907326063; 0.04031257519234377 0.018082471925146112 -0.07568347013903132; 0.041836585240247866 0.0260064949383866 -0.10768708920672497; 0.028546695449653645 0.021539162848539593 -0.09465839206271652; 0.03224778148902765 0.027609616064035038 -0.12543367866099797; 0.020335838023994822 0.018698783136941906 -0.09204676311214473; 0.010018564901383477 0.010766032516865151 -0.05482024342730423; 0.020284218656943413 0.021510373244606168 -0.10872762012995166; 0.02260461051232536 0.02359107562410601 -0.12635387292353162; 0.0041563823487434925 0.003332762606513975 -0.01927189221738655; 0.002058159733405421 0.0033913196814438396 -0.012917716367347242; 0.00044343132629328893 0.00010766242671242398 -0.002241446161979872; 0.0002316141134106228 0.00022020134245247336 -0.0017189755560152705; 0.005891635007866447 0.0010844321088795685 -0.0020832071923883337; -0.0004361631455906873 0.0008382400705034555 -0.0015376103511120047; -0.0026594928582525648 0.006242354711080126 -0.0022294258763317478; 0.0015574787824121426 -0.0023111089038675217 -0.002265396612141605; 0.003703839802724506 0.0018820202526912979 -0.0047441870092265834; -0.0035480202525579713 0.000545773454771338 0.001185482270199536] %
+
+Mass Used: 90.99890424946807 kg
+Launch C3: 97.74579021363292 km²/s²
+||V∞_in||: 2.7641371622839445e-7 km/s
diff --git a/archive/ES_0.5667306448152907 b/archive/ES_0.5667306448152907
new file mode 100644
index 0000000..58fff69
--- /dev/null
+++ b/archive/ES_0.5667306448152907
@@ -0,0 +1,22 @@
+archive/ES_0.5667306448152907---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T20:39:16.393
+Launch V∞: [6.745076355016234, -7.291736982592519, -0.7894087430014743] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.814862267093487e-7, -0.0002253786986265147, 0.00015265804438600552] km/s
+ V∞_out: [0.00012635246918063422, 0.0002356196513918851, -5.155965208602473e-5] km/s
+ time of flight: 1.8599753299570274e8 seconds
+ arrival date: 2029-03-21T14:38:08.393
+ thrust profile: [0.14845518860429355 -0.04274468347592668 -0.059443223292437425; 0.06715705768454897 0.016473162663041288 -0.07881873989156553; 0.05978047827818915 0.029647905541643135 -0.11913873171544906; 0.05061815415176844 0.034083235365301265 -0.14265355379089836; 0.039320195895561925 0.03215320241836776 -0.14317848362803623; 0.02958432289198864 0.027901728874934015 -0.1319785763313595; 0.020442473854680735 0.02158558277283701 -0.1078339168108192; 0.0121628795503699 0.014128775239653822 -0.07416613212962966; 0.004792172964557708 0.006106959926069187 -0.03396425856220845; 0.0011241151846404659 0.0014203166173432388 -0.009934465219481636; 0.0007100199867284691 0.00034054416554506396 -0.0023915034800194705; 0.0003542382319391105 0.0003979271725010715 -0.002355588659943224; 0.00045755323186733444 0.0006017542145975597 -0.004112578731449028; 7.876094596899043e-5 0.00029132245010692927 -0.0017511531586588572; -0.0012874737117114087 0.0006773854600605214 0.00038689067302674434; -0.00018001487258012002 0.00010082555101252735 -0.001292852085103302; -0.0015954917214033922 7.693922965036046e-6 -0.0023700984948638896; 0.0006891478859853109 -0.0002781406005922935 0.00113813906671592; 0.0017300336640872415 0.0008257526608876811 0.0001325540203784014; 0.0003847498374599611 -0.00023228255343627966 0.0019225669785602586] %
+
+Mass Used: 82.00196399047582 kg
+Launch C3: 99.28864942183371 km²/s²
+||V∞_in||: 0.00027221407152059235 km/s
diff --git a/archive/ES_0.5667457418720422 b/archive/ES_0.5667457418720422
new file mode 100644
index 0000000..849adbd
--- /dev/null
+++ b/archive/ES_0.5667457418720422
@@ -0,0 +1,22 @@
+archive/ES_0.5667457418720422---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T10:55:23.812
+Launch V∞: [7.7066023889382285, -5.548603990402533, 0.4970704930035837] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007016699652531714, -0.0003920300757615782, -2.8991275485303447e-5] km/s
+ V∞_out: [0.0005626014377459448, 0.0003514678152391739, -0.0004572164870245832] km/s
+ time of flight: 1.8749577785237885e8 seconds
+ arrival date: 2030-04-16T13:05:00.812
+ thrust profile: [0.6983217584685897 0.016559120228798584 -0.11711740972460617; 0.3159367622350063 0.22434909976097595 -0.19065088234015837; 0.0602298412549247 0.07772609236559504 -0.08273037049039848; 0.029892463280308024 0.055590187228787294 -0.06563294435195706; 0.02033388998540353 0.04809425859811529 -0.06389096121389402; 0.019595474426103324 0.07694123202517826 -0.09911257543165705; 0.012720711895706402 0.07800791117750365 -0.10621872843960622; 0.003525951956268891 0.02268978351964122 -0.03567494197646456; 0.0021414794247714324 0.0169196047255328 -0.028140326350788843; 0.0005423658336329164 0.004622640205010719 -0.007946624949495797; 7.900805526088497e-5 0.0006612241152079009 -0.0010918819824305432; -2.708672894409438e-6 0.0001082358557673946 -0.00019411623740741706; -0.0004265453826960899 0.000372750488103737 0.00038080993952794353; -9.902449812972526e-5 0.00017767928786798564 -0.00021423503719586868; -0.00015776191121870923 -5.3990213334483085e-5 -0.00010409459836805169; 2.541331222425871e-5 1.6923917709060945e-5 -0.00012987034498813493; -0.0006635293177344327 -0.00021416442793834142 9.82212425276814e-5; -0.00029330901215016505 -0.0001895075700679628 -0.0005299616298707708; -0.00020882152253698467 -9.609730350746575e-5 1.8030856861663426e-5; -9.880217472997118e-5 -0.0005008970661738593 0.00023363808356686506] %
+
+Mass Used: 133.71949894271665 kg
+Launch C3: 90.42580569851415 km²/s²
+||V∞_in||: 0.0008042815517555281 km/s
diff --git a/archive/ES_0.5667469061210563 b/archive/ES_0.5667469061210563
new file mode 100644
index 0000000..5bfbbdb
--- /dev/null
+++ b/archive/ES_0.5667469061210563
@@ -0,0 +1,22 @@
+archive/ES_0.5667469061210563---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T01:00:59.710
+Launch V∞: [6.399582766486822, -7.570268590552301, 0.1628348934660718] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7434525545751356e-8, 5.907711786907588e-9, -2.1397817047098475e-8] km/s
+ V∞_out: [-6.846660810835145e-9, 1.580074814003604e-8, 2.1424592031542356e-8] km/s
+ time of flight: 1.8749577787459958e8 seconds
+ arrival date: 2029-04-13T03:10:36.710
+ thrust profile: [0.28783278419577824 -0.08234590771644627 -0.11262276028945395; 0.01754411978674819 0.0029091378238244965 -0.023464463721014073; 0.03200424123581112 0.011646112105151978 -0.06930504226018015; 0.031622691769132315 0.01502978538727117 -0.09465493285304266; 0.043954606065288365 0.0254201995677598 -0.16089253392845365; 0.015393291160254965 0.00897501790874979 -0.07061140117600727; 0.020637361993547817 0.01383320471080371 -0.12345226127605695; 0.013217946948547658 0.007311720604712009 -0.07984687755700748; 0.012605926405854794 0.006490063899387852 -0.09225859588788422; 0.004244424053924027 0.004121736943216304 -0.03746029892882274; -0.00011098535383540235 0.0035136028367962822 -0.003603239552905496; 0.0029920356020448607 0.002927178513082588 -0.025071994946930132; -0.0006481371214053875 -0.0014487315132155195 3.784122481895972e-5; 0.0007549478776372182 0.002512840706180977 -0.0009612145703284721; -0.0025766304731164444 -4.783401568667848e-5 0.00228685982639375; 0.0023550089922755755 -9.206148961484384e-5 -0.004036099105104539; 0.0008630006358476476 0.0002569724022017674 -0.002497608423721478; 0.0002716784997805543 0.004444202473930937 0.0007520035823126699; -0.0013163999331366396 0.0006491997611842964 0.005969435042029618; 0.012603500421259645 0.0004056464205526792 0.002744690663064928] %
+
+Mass Used: 87.84556610353593 kg
+Launch C3: 98.29014132074795 km²/s²
+||V∞_in||: 2.822641163775023e-8 km/s
diff --git a/archive/ES_0.5667516928088556 b/archive/ES_0.5667516928088556
new file mode 100644
index 0000000..2dd60dd
--- /dev/null
+++ b/archive/ES_0.5667516928088556
@@ -0,0 +1,22 @@
+archive/ES_0.5667516928088556---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T11:28:52.631
+Launch V∞: [6.5213159453468155, -7.205822922162901, 0.2591146069447803] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008378287171813988, -0.005385739936788517, 0.007123239941256671] km/s
+ V∞_out: [-0.005905778275435369, -0.005351241074860665, -0.004107751991488819] km/s
+ time of flight: 1.87495777874835e8 seconds
+ arrival date: 2029-04-06T13:38:29.631
+ thrust profile: [0.4880320835145097 -0.11052089690940353 -0.14400344917455837; 0.09278455938542894 0.02960124018452025 -0.08960376823693651; 0.05294797409421506 0.031843213465897094 -0.08642972173185928; 0.07135810321499533 0.05932864215872087 -0.16368316103282085; 0.032527018102351486 0.0324767038081987 -0.09667537490012196; 0.03212531948952345 0.03746600782073649 -0.11692663098362169; 0.02540840910639365 0.03365410037782175 -0.10982106088205686; 0.006092482243097913 0.008723364994340852 -0.03191392703672463; 0.0054023824726876155 0.008739803333080574 -0.0311746313203072; 0.004959093989941011 0.008945098397159606 -0.03021129070706797; -0.0022791025305982696 -0.0009126746233882239 -0.005474853820238829; 0.0007708559368401141 0.0018867089008839134 -0.006704122017058046; -0.004000408511772495 0.004852624302919278 -0.0002813753112518888; 0.00023075663190893572 9.100349182468594e-5 0.0034940595634047225; -0.0002974330780832668 0.0003533457946844098 0.0030619190304887276; -0.003665190854670129 -0.009889861910167398 -0.005665169458817611; 0.0020780094369690625 0.005608136281140747 0.0026967626361595913; 0.0006365146425089253 0.0017580759296999611 -0.005256910977352102; -0.005146750618206981 -0.010695263152170504 -0.003090617278358409; -0.003361503991292112 -0.0022896902981203366 -0.010968256993314517] %
+
+Mass Used: 109.85188980287694 kg
+Launch C3: 94.51858602413508 km²/s²
+||V∞_in||: 0.008969319867568942 km/s
diff --git a/archive/ES_0.566756512587661 b/archive/ES_0.566756512587661
new file mode 100644
index 0000000..bb70800
--- /dev/null
+++ b/archive/ES_0.566756512587661
@@ -0,0 +1,22 @@
+archive/ES_0.566756512587661---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T01:53:46.914
+Launch V∞: [7.468335439223121, -6.231780169178618, 0.09060347313268471] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007463757066457206, 0.000585300796464883, -0.0004543494950046862] km/s
+ V∞_out: [0.00018016244754644634, 0.0010350796918244646, -4.360973293218351e-5] km/s
+ time of flight: 1.6696641685266426e8 seconds
+ arrival date: 2029-08-23T13:27:22.914
+ thrust profile: [0.500137969380581 -0.06835995949171111 -0.15559423448019374; 0.09225503871348761 0.03569106883202029 -0.09899520604650182; 0.06585761714909669 0.042044997044270636 -0.1194799311614224; 0.05916870958162986 0.0505812336416048 -0.14679498957304804; 0.03593699343647777 0.04509052244974644 -0.1348247533982554; 0.0195794360168679 0.025553132467899278 -0.09051774467379821; 0.021146863468414243 0.029050276618915676 -0.10061072940562263; 0.006159065559697233 0.009322976330485564 -0.03717961479045869; 0.009467804889454765 0.016328734690961615 -0.06435300720397946; 0.008219412794066233 0.0166853408768826 -0.06817710200924773; 0.011283445108840814 0.014857632562612438 -0.07061640479903608; -0.0004295480929530826 0.0004020865570321669 -0.0016117441135898582; 7.385940248816808e-5 0.0009245912822912982 -0.0021803979095400615; 0.0014539623410633274 -0.000532031644510971 -0.0044587858697423014; 0.008672884433070464 0.005178319020665482 -0.01021427041544571; -0.00572683265444166 0.00316218414147091 0.00801375200076479; 0.0016166465625610284 0.0011962460252591322 -0.006489752300230751; -0.003404283721823614 0.0005679391921824877 -0.017269781405540162; -0.0013083495824291168 -0.00302639258994809 -0.0002271415654729195; -0.005685089490010652 -0.0017973063216510901 0.0012353822194817016] %
+
+Mass Used: 109.26985544104355 kg
+Launch C3: 94.61932729906759 km²/s²
+||V∞_in||: 0.0010517067944176926 km/s
diff --git a/archive/ES_0.566760279673756 b/archive/ES_0.566760279673756
new file mode 100644
index 0000000..09f2fa3
--- /dev/null
+++ b/archive/ES_0.566760279673756
@@ -0,0 +1,22 @@
+archive/ES_0.566760279673756---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T07:40:03.925
+Launch V∞: [7.877374526437088, -5.56599407575053, 0.26639868977468034] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7577717470696285e-6, -2.6328998708831373e-6, -2.413239036119042e-7] km/s
+ V∞_out: [2.173011509668729e-7, -1.0421805967458895e-6, -2.9803344495308754e-6] km/s
+ time of flight: 1.8749577787380818e8 seconds
+ arrival date: 2030-04-19T09:49:40.925
+ thrust profile: [0.5238479812300112 0.02611267600462532 -0.1255919949443646; 0.1882124565356007 0.1337291708517877 -0.16731587198013267; 0.0726219461959275 0.08660718764580655 -0.1261513817363717; 0.045566047539548675 0.07567016941683886 -0.12368012069242777; 0.019596910063130985 0.04121729447074374 -0.07778889975408386; 0.01564145553433681 0.04238143980129872 -0.08313386959280201; 0.0063025352926484625 0.02389106597939904 -0.053448502515423615; 0.002118422758081619 0.011979931045291861 -0.02977980345671662; -0.0036374262891275895 0.004068581826994846 -0.010120096805014276; 0.009643300410681335 0.009863558003773405 -0.015181916917414835; -0.008536565063485237 0.007281773593661946 -0.019796393289759275; -0.0015136250312861124 9.717556278363796e-5 -0.0014506638087515462; -0.0041361383162045046 -0.004929805035900637 -0.0016369655356688008; 0.004782866702685415 -0.0022475083749124267 -0.007065415828068426; 0.001303578329201863 -0.002070494243845965 0.0051545833677335996; -0.003192664320851274 0.001308390175882875 0.012971824267667676; -0.002492956761672103 -0.0028110898230652927 0.011105757013025092; -0.008650633541712045 0.0035112241029190343 -0.01287205665128726; 0.009469182210135055 -0.016944745468258353 -0.003639081115883041; -0.0067706317285934296 0.003895854162547077 0.020039704038405083] %
+
+Mass Used: 118.11198111876092 kg
+Launch C3: 93.1042877429636 km²/s²
+||V∞_in||: 3.1749268450386604e-6 km/s
diff --git a/archive/ES_0.5667605017794548 b/archive/ES_0.5667605017794548
new file mode 100644
index 0000000..310cc02
--- /dev/null
+++ b/archive/ES_0.5667605017794548
@@ -0,0 +1,22 @@
+archive/ES_0.5667605017794548---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T02:13:23.674
+Launch V∞: [5.82583154347001, -7.762658070999488, -0.026145289212591214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3457978355565535e-6, 1.4658691775579926e-6, -1.0949080259633033e-6] km/s
+ V∞_out: [1.0328448313652787e-6, -2.401335648938794e-6, 1.4218355837400621e-6] km/s
+ time of flight: 1.7128497762130877e8 seconds
+ arrival date: 2028-09-30T13:23:00.674
+ thrust profile: [0.4632375246808376 -0.17418813674090822 -0.16607195660519636; 0.15063066856196697 0.02265066927198749 -0.15540535407853753; 0.07327580138843286 0.028960239237744004 -0.12880003266182488; 0.06125622869009082 0.03415849897930256 -0.14663958501293786; 0.05886458214308193 0.03894354283960371 -0.17331852402299194; 0.017542988783398585 0.013705372461991706 -0.06523323947317804; 0.02512942004416178 0.021739843020739544 -0.1070052769054431; 0.010669468712920436 0.01012539378228442 -0.0524023908918882; 0.006020122403438069 0.00601047421980511 -0.0346471865766398; 0.00156289182070793 0.0008854787969217218 -0.010710589542699744; 0.008792934258006367 0.01015332738269512 -0.05736292023662749; 0.0068877495393835945 0.009601187305078107 -0.05037263822100155; 3.393258695543396e-5 0.00024380453932333103 -6.554197528882514e-5; 0.00014494977170393194 5.170101276124261e-5 -4.056079850235357e-5; -4.072112136526421e-5 -7.233456406877434e-5 0.0002338015756506919; -2.5540915465754855e-6 7.492865698729649e-5 -0.0003190698027083624; 7.57337704343069e-5 -0.0008914723845312641 0.0004061146348953814; -0.0005122959786655063 -0.00044741752353830497 0.0012751865533958988; 9.02701749685382e-5 -0.0005238235687659101 0.00049354257786431; -0.0004914727361729448 -0.0005992420069234108 0.0006341612076609174] %
+
+Mass Used: 111.72141913099586 kg
+Launch C3: 94.19985707629166 km²/s²
+||V∞_in||: 2.9749560528409853e-6 km/s
diff --git a/archive/ES_0.5667611707635987 b/archive/ES_0.5667611707635987
new file mode 100644
index 0000000..9c84c82
--- /dev/null
+++ b/archive/ES_0.5667611707635987
@@ -0,0 +1,22 @@
+archive/ES_0.5667611707635987---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:40:39.448
+Launch V∞: [7.745591469600544, -5.757165907104566, 0.35397193044192776] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8375642598892507e-9, 3.277281023299353e-9, 1.3673232989685502e-9] km/s
+ V∞_out: [3.449021570290641e-9, -2.7391232279497655e-9, -2.0379932985391036e-9] km/s
+ time of flight: 1.857218913308618e8 seconds
+ arrival date: 2030-03-28T09:05:30.448
+ thrust profile: [0.3668600973200493 0.022575602774990836 -0.07092856778050077; 0.2660980108327801 0.1990025495610118 -0.1737635866385998; 0.11113547057058401 0.14124361665510315 -0.14196978610888075; 0.06175533133298067 0.1119762887266618 -0.12636563673843168; 0.04828710250827377 0.11578389870282779 -0.14039325048869244; 0.02243711663642516 0.06998531156304133 -0.09456372233042976; 0.002676358565399951 0.007385549099470464 -0.01138757142427743; 0.003800859092285096 0.019840780924193505 -0.031237237901444833; 0.00025972560738723305 0.001337284447745513 -0.001922217214873565; -0.00321534806479897 0.0028881612339637904 -0.0013305725091518194; -0.0033147650698765875 -0.0013561292883202 -0.0018176945286892776; -0.0006367104104887082 0.005589277441184924 0.0006659628915728594; 0.0002907844209505268 0.0014204163572518018 -0.006062377932898796; 0.0003249115021954948 0.001400881739590923 -0.000948441504856015; 0.004622761907370243 -0.005727473917964936 -0.005967029911704662; -0.0028106119100821717 0.006714498892576926 0.001736454770008545; -0.0011022281716266194 -0.003730140792030455 -0.005262656511707908; -0.0010390243200639063 -0.003932795067596648 0.00547773456111526; 0.001932435651000963 -0.0015110513998744823 -0.00101290890012172; -0.0010362797657972494 0.004873976866677067 -0.008461083960932455] %
+
+Mass Used: 117.17878392093462 kg
+Launch C3: 93.26444262341664 km²/s²
+||V∞_in||: 4.545537904206842e-9 km/s
diff --git a/archive/ES_0.5667751602477894 b/archive/ES_0.5667751602477894
new file mode 100644
index 0000000..95832fe
--- /dev/null
+++ b/archive/ES_0.5667751602477894
@@ -0,0 +1,22 @@
+archive/ES_0.5667751602477894---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:24:34.895
+Launch V∞: [7.643620814731639, -6.104127525154233, 0.32244580488378577] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004203321467142553, 0.0011381457539620902, 0.0026635444330856627] km/s
+ V∞_out: [0.002705913721361763, 0.0002933448507575778, -0.0010751483627216324] km/s
+ time of flight: 1.7046191783099186e8 seconds
+ arrival date: 2029-10-02T17:56:31.895
+ thrust profile: [0.3579225832285226 -0.04247663710968437 -0.0988356988423182; 0.1116869594881267 0.05691615356516518 -0.10681859923637876; 0.07394697897431626 0.060055095045469346 -0.1266828778328292; 0.05450615427234333 0.05873003676052297 -0.13430358879755874; 0.03993102351145984 0.052806831474838445 -0.12986621425618577; 0.020965887368041062 0.032669378531634395 -0.08696020149587583; 0.018222326660404867 0.031718567878675 -0.08955847319309354; 0.02466715585336376 0.04733120674355843 -0.13572453598064294; 0.002234622084488182 0.007608092222040335 -0.02214434023819955; 0.004764184294732557 0.012480807464533951 -0.042677672231682354; 0.0030569250652278794 0.0078530642473171 -0.021548489153439643; 0.00032502721744495384 0.0006131054356727592 -0.0015500478496497157; -0.001321662752473087 0.0005348922516726258 -0.0034939867436962; -0.002817316165715094 -0.0005193343861962903 -0.004555378077175891; 0.0008064909539103657 0.0028450568472180825 -0.0032678631271176126; 0.007640549394213792 -0.008907416012134881 -0.0006382171280140112; 0.004466119086841497 -0.006783929996412634 0.003680226064728438; 0.010514699474322778 -0.004196278867363715 -0.00852032202526129; -0.00313165897690577 0.016306911997399642 -0.006344809436146806; 0.0004425517518078215 0.013373582614542717 -0.00136716345570568] %
+
+Mass Used: 102.4668677067375 kg
+Launch C3: 95.78928329983145 km²/s²
+||V∞_in||: 0.0029268624528400672 km/s
diff --git a/archive/ES_0.5668272079876397 b/archive/ES_0.5668272079876397
new file mode 100644
index 0000000..e4f91fe
--- /dev/null
+++ b/archive/ES_0.5668272079876397
@@ -0,0 +1,22 @@
+archive/ES_0.5668272079876397---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T01:47:51.551
+Launch V∞: [6.768885639133171, -7.280719536852043, -0.6484668244404999] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01579106994480299, 0.007669256082963404, -0.019103268980322764] km/s
+ V∞_out: [0.016536142516594778, 0.006869140891849742, 0.018780338270964207] km/s
+ time of flight: 1.874957778323368e8 seconds
+ arrival date: 2029-04-09T03:57:28.551
+ thrust profile: [0.15364682214332795 -0.046059010122094755 -0.058677143864990795; 0.06605317109082 0.014335357586518301 -0.08056148348634252; 0.048315885996601436 0.021520198586803877 -0.10103199785959652; 0.039989807669813984 0.023699692501035693 -0.11753794075817747; 0.0321884217895308 0.02279430667711872 -0.12185490050894765; 0.023995151906526253 0.019577701272959352 -0.11212958637829532; 0.01740164274671309 0.015959356333776847 -0.09711603680946236; 0.01245781140791266 0.012566136493825604 -0.0806741546268649; 0.00800338789937348 0.008800390192158133 -0.05903461486645236; 0.004669784134677731 0.005406146107476685 -0.037746247046674786; 0.0015834278061879162 0.0015069954474334608 -0.01131778912346637; 0.0023057399860939684 -0.00021009895070243706 -0.0008807374869555765; 0.00022250749496242818 0.0008160507224345183 -0.00581174114695707; 0.0017051323560958384 0.0004920663086384247 -0.00617049930608211; -0.0017230313074704951 0.0004789750108874233 -0.00262467157921559; 0.004493011346521044 -0.00042283177009914117 -0.003485789187969608; 0.0016134590739394171 0.0022113839149455463 -0.018192498905109423; 0.0023852779810681545 -0.00043754946173763724 0.0011639266559353365; -0.0007151602183915191 0.00011911106448479086 0.0008306803601311778; -2.1287586604626894e-5 -0.0004943626495746869 0.003726575339163863] %
+
+Mass Used: 82.35641519679984 kg
+Launch C3: 99.24719899236226 km²/s²
+||V∞_in||: 0.02594436864913643 km/s
diff --git a/archive/ES_0.5668282228952732 b/archive/ES_0.5668282228952732
new file mode 100644
index 0000000..5de7af3
--- /dev/null
+++ b/archive/ES_0.5668282228952732
@@ -0,0 +1,22 @@
+archive/ES_0.5668282228952732---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T11:41:19.520
+Launch V∞: [6.360300494101561, -7.395474797075838, -0.2439852057325261] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1370465879404954e-5, 1.7993533286404359e-6, -2.896973760199155e-8] km/s
+ V∞_out: [-2.2637702108106287e-6, 5.213824356865879e-8, 1.1275142922449891e-5] km/s
+ time of flight: 1.8749577787919563e8 seconds
+ arrival date: 2029-04-08T13:50:56.520
+ thrust profile: [0.36460495186001357 -0.07975314826541281 -0.1034797469066528; 0.165412049457416 0.05208887045457433 -0.14678449003249527; 0.04708583666868084 0.03126178958447502 -0.07739329910123662; 0.030692113230457126 0.02667951606046038 -0.07010898648951981; 0.04724680899801683 0.058186816453992256 -0.14943370274696952; 0.022793300702096064 0.0320438964137353 -0.08880015147772904; 0.02619183568996185 0.03543327276067689 -0.10574964446300593; 0.01811732902394835 0.026768018338020835 -0.08634513503901663; 0.007617847040973126 0.014796203860087752 -0.047435019997162604; 0.001440219292120572 0.0031662054886431173 -0.0117683514695957; 0.002452422828983525 0.003312920611337576 -0.009747837111820395; 8.80080717820137e-5 -0.0006653352390216497 0.0006885605879076726; 0.003830353726570777 0.004243221875168826 -0.006169523506789945; -0.0026979656864739164 0.0010228935282742169 -0.007217313158589656; -0.0001151347796478868 -0.0002731913063075853 0.0008671582232568178; -0.004243712591001417 0.010153940810199828 -0.016192424101246407; 0.0035811507569079894 0.004262243609837437 -0.015372916239183108; -0.0014171384261896323 0.005230303955925209 -0.014684967423491492; 0.0003232764322753528 0.0009152117553163911 -0.0029904688650598736; 0.001608401463527485 -0.0016305853640415468 -0.010259515796799361] %
+
+Mass Used: 105.93126803575069 kg
+Launch C3: 95.20599863006882 km²/s²
+||V∞_in||: 1.1511994004589232e-5 km/s
diff --git a/archive/ES_0.5668314789409864 b/archive/ES_0.5668314789409864
new file mode 100644
index 0000000..9e7d2d4
--- /dev/null
+++ b/archive/ES_0.5668314789409864
@@ -0,0 +1,22 @@
+archive/ES_0.5668314789409864---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T21:01:34.881
+Launch V∞: [6.60767740391614, -7.432515463478882, -0.01136379049092653] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6038915268663166e-8, -5.2031347290111365e-8, -2.9525282688666994e-8] km/s
+ V∞_out: [1.4620437893037067e-8, -2.9215254523285016e-8, 5.0654141114104146e-8] km/s
+ time of flight: 1.874957778184789e8 seconds
+ arrival date: 2029-04-10T23:11:11.881
+ thrust profile: [0.16354248112344916 -0.04240577748890612 -0.06528968619683771; 0.055854748779444845 0.012741505183759367 -0.06826329157167883; 0.04333251003288168 0.019549000107200742 -0.08896135414661191; 0.025505105508170943 0.015154373879446868 -0.07681207917088068; 0.03756948372665673 0.027300902361852793 -0.1377855372084254; 0.03661834368727948 0.03226290490116123 -0.16860649496799432; 0.02234624709331315 0.020056098694554658 -0.11696117398921481; 0.009942757695673507 0.008042971359879624 -0.0559997848416588; 0.004655508550089406 0.004611144838363438 -0.037734373549737896; -0.0030968396746949064 0.006031384564182394 -0.021381382155149262; -0.000830100135025652 -0.0007612069557318038 -0.00404740716876143; 0.0031764119789305842 0.0038345905119369925 -0.009182920747930746; 0.00023655579515050344 -0.00042117827039893233 -0.006525735185994247; 0.001774054752107708 0.005923877318080678 -0.006585671538090693; -0.0014358979376615081 0.007174189449198396 -0.0079286899200793; -0.00034247796144722516 -0.0019048995628505256 0.0018509560753423187; -0.0017362780960971662 -0.0014237559266459749 -0.007733081240204422; 0.01663972859806081 -0.011937074384347305 -0.004385838557738334; -0.00024106293649868177 0.000980125840613355 -0.0010988273556968343; 0.03307729289689088 0.014811594339082131 -0.022215930090687064] %
+
+Mass Used: 84.36446586975353 kg
+Launch C3: 98.90381592481097 km²/s²
+||V∞_in||: 6.524590812486633e-8 km/s
diff --git a/archive/ES_0.5668431774026942 b/archive/ES_0.5668431774026942
new file mode 100644
index 0000000..afc00db
--- /dev/null
+++ b/archive/ES_0.5668431774026942
@@ -0,0 +1,22 @@
+archive/ES_0.5668431774026942---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T03:54:10.911
+Launch V∞: [8.041523148087633, -5.815316281392509, 1.1204904856325604] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7330496871419396e-9, -1.6065577770136723e-9, -2.471340026772477e-9] km/s
+ V∞_out: [-9.532487509488998e-11, 3.039527647670328e-10, -5.1729549028783045e-11] km/s
+ time of flight: 1.8749577787834382e8 seconds
+ arrival date: 2030-04-26T06:03:47.911
+ thrust profile: [0.21673983765374077 -0.004291045703046031 -0.07089564459785763; 0.024732658193073385 0.011987815007349556 -0.030320108957428493; 0.03011078013236418 0.023183096973415952 -0.0659427317235566; 0.04228335109013589 0.03889543649298406 -0.12444864532984717; 0.03128353121673848 0.033355061571890506 -0.12377340007788977; 0.027093847426002397 0.0316095105534275 -0.12952270355092668; 0.014123796629220541 0.016244817293018916 -0.07531811389863285; 0.007110417277892359 0.009335638178688047 -0.05001842810274034; 0.0017281252511090804 0.002772639123514273 -0.018208377010341836; 0.0034242968087495533 0.0071653676021451364 -0.027895111981977076; 0.0033708161531330575 0.0040509409144551456 -0.035443152764367006; -0.00011944756249740695 -0.005049919633789508 0.0012559695947107186; -0.00032005122577432785 0.00033565820484744664 -0.0012808894179658326; -0.008467240240350093 0.008640160362022432 0.005662981893075422; 0.0046786847081925174 -0.002880752797644238 -0.0007666003283850078; 0.012093062818145985 -0.00013325224123523398 -0.0018422814453113402; 0.0018952938711258732 -0.002300232707544014 -0.01778877326222295; 0.006513089100032824 0.0043826650166993025 -0.005783837230275595; 0.01664058203110476 -0.00694135069525483 0.005483856842831605; 0.004235421684476967 -0.008742417901621637 -0.014335398735600474] %
+
+Mass Used: 79.50330825667834 kg
+Launch C3: 99.73949692225112 km²/s²
+||V∞_in||: 3.4193582200339405e-9 km/s
diff --git a/archive/ES_0.5668461826306513 b/archive/ES_0.5668461826306513
new file mode 100644
index 0000000..dfa8d85
--- /dev/null
+++ b/archive/ES_0.5668461826306513
@@ -0,0 +1,22 @@
+archive/ES_0.5668461826306513---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T19:45:17.626
+Launch V∞: [6.3633597160088105, -7.319204706637107, 0.33791935643534526] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012371509312029568, 0.009841774985319946, 1.4740943469423744] km/s
+ V∞_out: [-8.970315357522198e-5, -3.722898258219917e-5, -0.00010692210841184725] km/s
+ time of flight: 1.854075073710969e8 seconds
+ arrival date: 2029-03-13T17:50:24.626
+ thrust profile: [0.5047296074671286 -0.1196864416401635 -0.1483222728721977; 0.07351971329545229 0.023062995673716523 -0.07139754798199177; 0.07575203214715928 0.04565165899139886 -0.12174697344946708; 0.059253450393145765 0.04801935191864283 -0.13402218218702244; 0.04347179889695919 0.043771974563863975 -0.12755204356800726; 0.046799467121146236 0.05452034329175426 -0.16447154229262487; 0.015701497551685234 0.02015720010551167 -0.0674687417905247; 0.005009021923685346 0.006981195958478111 -0.024953648243775974; 0.005036093238089819 0.008474579581998253 -0.02874821599261344; 0.0015684926085369015 0.003916386307028447 -0.013540874874157423; -0.0006101294958844922 0.0014936840946094842 -0.005424334592202032; 0.002060927957471715 -0.00023591769147877093 -0.0034189240812398593; -0.0042738761899764055 0.00194918514121049 -0.001026181958553224; -0.0002574768146715997 0.00037266289822180266 -0.0039559291713804415; -0.0001946745097987541 -0.012134789803298532 -0.014792837856069083; 0.015056488974002767 0.0037134862632830956 -0.009195721779679162; -0.003607334324316404 0.0034188516425079684 -0.0025740796891176726; 0.012634914093486426 -0.004548378169883199 0.008013272723625111; 0.0031478075036544444 0.005233983370664445 -0.018724716567107447; -0.002624330466595977 -0.0013135908721914021 -0.005625312418084265] %
+
+Mass Used: 111.95299862654883 kg
+Launch C3: 94.17729390443618 km²/s²
+||V∞_in||: 1.4741791134271929 km/s
diff --git a/archive/ES_0.5668527825065786 b/archive/ES_0.5668527825065786
new file mode 100644
index 0000000..1ca68b5
--- /dev/null
+++ b/archive/ES_0.5668527825065786
@@ -0,0 +1,22 @@
+archive/ES_0.5668527825065786---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T18:53:29.510
+Launch V∞: [6.287958956675009, -7.345166808599448, 0.32802133423195823] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.419998698204755e-8, 9.231939886609599e-9, -1.191394221466289e-8] km/s
+ V∞_out: [4.156594777318158e-8, -3.680430932794284e-9, 5.091968989071091e-9] km/s
+ time of flight: 1.8544590993460876e8 seconds
+ arrival date: 2029-03-13T03:38:38.510
+ thrust profile: [0.4038180897946332 -0.0918083942788599 -0.11643209026111762; 0.28571417854783987 0.09869712346764603 -0.24058151528616586; 0.09357521948299534 0.059301089158366904 -0.14110631014665578; 0.06339863930643477 0.05483893620795741 -0.13542268708794147; 0.031244068023039015 0.03305643070517795 -0.0880884334426448; 0.02494264764634683 0.030960478928584043 -0.08753834305935891; 0.014357616801452372 0.020281134888431373 -0.060439769173755355; 0.005847801283846731 0.009027414530264125 -0.02901895705674147; 0.007392733967246664 0.01330104876089818 -0.04388468689649908; 0.0018080825931141842 -0.00019402812430785503 -0.0014893868491770552; 0.0008500228262310944 0.004347798015500835 -0.012135803829106858; 0.0006499818149818921 -0.0005363143478066279 -0.00018805879987626728; 0.0015366288725410585 0.00020922864562967775 0.0018673085330194845; -0.0002678993066832998 0.0030349838158220148 0.004216388566351992; 0.002330602116745784 0.0020785069225452446 -0.0030337512251986734; -0.007569955549311678 0.007241822255450527 -0.000421228826085431; -0.0007104260699472369 6.595499261973069e-5 -0.0001842711648237605; 0.0008324243311176945 -0.0031946264066985554 -0.00012227320144989843; 0.0015771318917210705 -0.0019280258951123023 -0.004613194732800884; 0.0003538203703641786 -0.015364796518745666 0.01418545964294534] %
+
+Mass Used: 115.34282210863967 kg
+Launch C3: 93.59750128269178 km²/s²
+||V∞_in||: 4.669913898968023e-8 km/s
diff --git a/archive/ES_0.5668626306450293 b/archive/ES_0.5668626306450293
new file mode 100644
index 0000000..e1ed641
--- /dev/null
+++ b/archive/ES_0.5668626306450293
@@ -0,0 +1,22 @@
+archive/ES_0.5668626306450293---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T08:30:12.837
+Launch V∞: [7.781271616489701, -5.8760461462592115, 0.22800367732516755] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0026748662256687985, -0.027636811608022286, -0.03773233660048136] km/s
+ V∞_out: [0.01892753320724865, -0.016068685626054888, 0.03955794970847954] km/s
+ time of flight: 1.8749577781323406e8 seconds
+ arrival date: 2030-04-25T10:39:49.837
+ thrust profile: [0.4864453785184547 -0.0032379448648704335 -0.15479914971972436; 0.09325300923169358 0.04655972535720966 -0.10506791727990288; 0.0402363363749321 0.03247123378295228 -0.08220293092589545; 0.02940437370757312 0.0319230761699998 -0.0994912490600828; 0.02560705441786069 0.0358180277561074 -0.1086005384432299; 0.013100503283897119 0.018327856796608453 -0.08338606085569557; 0.009307470027651343 0.013248916441920458 -0.07011702696641565; 0.0016060794287022346 0.006807494653284902 -0.02726858748793013; -0.0025610366860671085 0.010968053437775172 -0.03948433377727968; 0.005765126664456278 0.0042747284186791905 -0.0340344970508146; 0.0027307362327081606 0.008040289366729793 -0.004522989143062677; 0.0013195185788400419 0.0017450258848409421 -0.014346349164805592; -0.00019952512230204315 0.0012648224465434004 -0.0021162686365216034; 0.0014057447870404823 -0.00032453580225305363 -0.006675643548254612; 0.005477099871071433 -0.004929287798784285 -0.012633313150805894; 0.012604918975400201 0.005186213104766952 0.001459834279838601; 0.000286169800337994 2.5262509800782172e-5 0.008923816725222047; -0.0025467711167027275 -0.002985791935940093 -0.004238179739445696; -0.0017340513529713524 0.05008474233043983 -0.027734315449625943; -0.023736883424792098 -0.02239683038196738 -0.035300602232566695] %
+
+Mass Used: 106.42586598919388 kg
+Launch C3: 95.12809195942977 km²/s²
+||V∞_in||: 0.04684738509793865 km/s
diff --git a/archive/ES_0.566863407082855 b/archive/ES_0.566863407082855
new file mode 100644
index 0000000..3b73358
--- /dev/null
+++ b/archive/ES_0.566863407082855
@@ -0,0 +1,22 @@
+archive/ES_0.566863407082855---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T12:41:15.394
+Launch V∞: [6.1254915910643986, -7.585403697222531, -0.012666621830976683] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008525107976267177, -0.0008861991140123809, -0.0008397419153580905] km/s
+ V∞_out: [0.0005497924286657042, 0.000935922789304238, -0.0006601912805859592] km/s
+ time of flight: 1.7404437908434582e8 seconds
+ arrival date: 2028-10-30T22:20:54.394
+ thrust profile: [0.392119846690703 -0.1292372594389727 -0.13624854578811305; 0.11595316073618273 0.02467154406536218 -0.11708731916481853; 0.10442902574454158 0.049701172244387554 -0.17116710296067789; 0.04982775128282106 0.032576837977700696 -0.11579752156770703; 0.056483189114432564 0.04589916306226945 -0.16512642206722794; 0.027449099691793977 0.025249824525318494 -0.09750677777988367; 0.02912019747044925 0.031043857574237665 -0.12296434274359341; 0.019557162370546166 0.021833173258229963 -0.08977532825391986; 0.0030326009591901165 0.003749387463955314 -0.017011201753961855; 0.004850481186773485 0.006422499086841048 -0.025889123170434177; 0.0013729134111610194 0.0004992925304393822 -0.0057754843396089165; 0.0012787202213398218 0.000974453183757096 -0.004132597426296111; -0.0004098023959050888 -1.562334069889074e-5 -0.0011988408770654026; 0.003486861298029015 0.0016513175456924947 -0.008343380477216568; -0.001094656251648979 0.0014748341336117282 0.00040191950710262957; 0.00010381125343557042 3.309643442574693e-5 0.002767240059314312; 0.005204725757477954 -0.0005909999868665903 0.0006963350244924048; 0.0005388729825893783 -0.004405947429919615 -0.0007466636474298249; -0.0020997389818326207 0.0023367520230442697 -0.0031159987239039876; 0.007152628975734587 -0.0046548722139073 0.0037123173680310385] %
+
+Mass Used: 106.8230595321429 kg
+Launch C3: 95.0601569253465 km²/s²
+||V∞_in||: 0.0014890567531681746 km/s
diff --git a/archive/ES_0.5668679347285605 b/archive/ES_0.5668679347285605
new file mode 100644
index 0000000..0d13b40
--- /dev/null
+++ b/archive/ES_0.5668679347285605
@@ -0,0 +1,22 @@
+archive/ES_0.5668679347285605---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T08:40:24.407
+Launch V∞: [7.87124946065423, -6.264946181573107, -0.3696032474917886] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.026071513725205e-7, 2.234642109311443e-6, 6.789353178143177e-6] km/s
+ V∞_out: [6.497921263478018e-6, 7.196655839257399e-7, -2.9956076973378556e-6] km/s
+ time of flight: 1.8749577779600278e8 seconds
+ arrival date: 2030-04-30T10:50:01.407
+ thrust profile: [0.16184731336408406 -0.002630535080258912 -0.0668773814114606; 0.06932527173223155 0.03295407108734363 -0.09715444031399487; 0.029554066870157828 0.02073904918592164 -0.07687275744646768; 0.02403801644619919 0.021832732910814775 -0.09018264014092857; 0.020986960199780667 0.02207468224814829 -0.10241348270217149; 0.01223029613258797 0.015979895289686467 -0.08104195046384526; 0.01079775587561704 0.014987564314246098 -0.086173843405933; 0.010038297388308446 0.01262971926312931 -0.08382256075499199; 0.0038506636335487584 0.004416628060867883 -0.03446267879675697; 0.0027326156397775624 0.0029882057290727495 -0.026810411046016957; 0.0025137452705131917 0.003080325872985221 -0.027213725834879843; 8.664159412433565e-5 0.00023735854925145168 -0.0005547843267518954; 0.00014180834279252833 -0.0002736880724670454 -0.0004309595192277216; -0.00016659344769417712 5.0427542931759755e-5 0.00041930912717516263; 6.678237411382709e-5 5.708027033238284e-5 0.00018643673818477153; -0.00045899113450067466 -0.0002919493767015868 -0.0010080919346408983; -0.0009398610869794418 0.0007454469983722585 0.00034006084636375295; 0.0010766514180172216 -0.0007991512411292596 0.0006223345253021092; -5.834267020668712e-5 8.168460764432974e-5 -0.00023247496999206582; 0.0007879698169520399 -0.00012467163122551833 -0.00047479941903596525] %
+
+Mass Used: 70.18002632257549 kg
+Launch C3: 101.34272529041344 km²/s²
+||V∞_in||: 7.182102668677925e-6 km/s
diff --git a/archive/ES_0.5669035785937827 b/archive/ES_0.5669035785937827
new file mode 100644
index 0000000..fbdcca8
--- /dev/null
+++ b/archive/ES_0.5669035785937827
@@ -0,0 +1,22 @@
+archive/ES_0.5669035785937827---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T22:43:06.930
+Launch V∞: [6.681013004628335, -7.275646258068781, 0.4627251228095851] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.540385960719595e-6, 6.004097338092385e-7, -1.3008439672138849e-8] km/s
+ V∞_out: [-7.037234922056701e-7, 2.0365521098266375e-8, 4.5247408696917565e-6] km/s
+ time of flight: 1.8209742147389704e8 seconds
+ arrival date: 2029-01-31T13:20:07.930
+ thrust profile: [0.23896076144001688 -0.06633334251769044 -0.07555036441115154; 0.10615829084888845 0.030209690194331406 -0.09665470708775302; 0.08232768538396941 0.04632465595137083 -0.12523663092405424; 0.07864662651277589 0.06152205582756151 -0.16877054808228975; 0.04026484623735032 0.03775787339818369 -0.10980840550528818; 0.05690267409248504 0.06178872554609915 -0.18551711493715453; 0.012603588781522812 0.015857256544886057 -0.051395337401263376; 0.010254370245441635 0.01580583687268281 -0.049141508766165264; 0.0034126708287958024 0.005318546249058151 -0.01726060528903383; 0.005961438741322298 0.009222753387989516 -0.033346817134855156; 0.00039631801915665445 -1.3078503704592873e-5 -0.0008378235298606259; 0.0006361665255977373 0.000142721605694472 -0.0005871448107390432; 0.0003025515261890459 -0.00019128240050196908 -8.395605997137508e-5; -7.549145441424881e-5 7.780970855751542e-5 -6.287159605686038e-5; -0.0005454429234301662 0.00028555911064207505 -0.00016060516672414596; -0.00010544646247661791 0.0006665084506737337 -0.0001689457495088005; 0.0005038234330267894 -0.0006539944790814839 -9.685764840996537e-5; -0.0006572121471519076 0.00041057272638004953 -0.00022252021025037714; 0.0007096177693837167 -0.0006184404528386101 -0.0020200815278982754; 0.00010292835980860849 -0.0003016635120779498 5.7775512579763934e-5] %
+
+Mass Used: 90.97455464366612 kg
+Launch C3: 97.78507777984234 km²/s²
+||V∞_in||: 4.579930757146355e-6 km/s
diff --git a/archive/ES_0.5669057863875924 b/archive/ES_0.5669057863875924
new file mode 100644
index 0000000..7034014
--- /dev/null
+++ b/archive/ES_0.5669057863875924
@@ -0,0 +1,22 @@
+archive/ES_0.5669057863875924---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T05:53:16.178
+Launch V∞: [6.371829262241352, -7.366747119977934, 0.42970773811280466] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0073950460614433024, 0.003597122246237988, -0.008360470042919607] km/s
+ V∞_out: [0.008309138262262412, 0.002878602252954959, 0.007741542649765771] km/s
+ time of flight: 1.8749577787507817e8 seconds
+ arrival date: 2029-04-08T08:02:53.178
+ thrust profile: [0.4070450210227759 -0.0827130414598559 -0.11223011700526658; 0.1274856355849594 0.045621914780739556 -0.11509683283156419; 0.05945801915766472 0.03906159970069974 -0.09439276623663324; 0.04631929413826152 0.0417483768926861 -0.10263633056863239; 0.03977222943924889 0.043205507490562255 -0.11265626798983945; 0.025800194102892277 0.03343117576125704 -0.09329902940737853; 0.01830504683452953 0.02566992425573557 -0.07622301096996394; 0.01345176327293152 0.016643431099644456 -0.05650830122076814; 0.013822243240987485 0.025236196644450072 -0.07635665816363281; 0.007873553206030125 0.009368358207463083 -0.04022463641027381; 0.003473982137698272 0.0052536278396669404 -0.01826126629089738; 0.001733959682280047 0.003440102004688181 -0.0063132038622400796; 0.0014074375479049368 -0.0015235520610145 0.005252617315747793; -0.0026546980345334833 -0.0015258261401752205 -0.00027810381174476866; -0.0006869790523562564 0.0018620482890232854 0.0028738192908802414; -0.011134625292640843 -0.0021891278552091083 -0.011146280091809097; 0.008182699564620855 -0.0007796783540777113 0.003842655139932904; 0.0009762632006416307 0.0025777827560091084 -0.001953332687909073; 0.0010696510282387549 0.004964384319195748 -0.007033360543107884; 0.000813289521373815 -0.008841444955333427 0.010481985488714709] %
+
+Mass Used: 106.90946735271882 kg
+Launch C3: 95.05382001705239 km²/s²
+||V∞_in||: 0.011727039440703033 km/s
diff --git a/archive/ES_0.5669158348194394 b/archive/ES_0.5669158348194394
new file mode 100644
index 0000000..f089365
--- /dev/null
+++ b/archive/ES_0.5669158348194394
@@ -0,0 +1,22 @@
+archive/ES_0.5669158348194394---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T00:56:13.325
+Launch V∞: [6.2053492614332715, -7.363524393668115, -0.06903331070750303] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3525731483086603e-5, 1.754878943511515e-6, -3.8512830964784074e-8] km/s
+ V∞_out: [-2.5844375483103e-6, 5.947783503548023e-8, 1.3390298581438864e-5] km/s
+ time of flight: 1.8749577787575626e8 seconds
+ arrival date: 2029-04-06T03:05:50.325
+ thrust profile: [0.48126200361239 -0.09146066619502041 -0.11567803409747543; 0.19018051924587132 0.07559010557107647 -0.1380052544568541; 0.09418927920537068 0.068579245204016 -0.11644566102976195; 0.08732171328684173 0.08672431723860943 -0.1499288276055342; 0.06413985399641266 0.08047015455840499 -0.1453743659046205; 0.0362570442840457 0.0540662030408851 -0.10425492956972397; 0.007827813922797095 0.014314776566426728 -0.03036000605284017; 0.010229724615739982 0.02074823263527359 -0.04558503174466352; 0.010946670988551873 0.03238238035402147 -0.06843660642823034; 0.0014361868184181786 0.0034798382333960766 -0.0073348148472699585; -0.0002947437139234417 2.3444199452329288e-6 -0.0010187003813618087; 0.0018165574789955393 5.331744024539146e-5 -1.675805372444543e-5; 0.0006376284840590028 0.0030499047914854787 -0.004900308109910095; -0.0002870516520727853 0.0007740677447685004 -0.002598113784102952; -0.002209611100196785 -0.0013919751432546399 -0.00020291103669759425; -0.0003504444567542898 -0.000860582301901242 0.0022021438146283285; 0.0020591716078818155 -0.0015133633625886793 -0.00031500272825787305; -0.0016238281618353773 0.003403493236637506 0.0024965071990881334; 0.0010400436017203453 -0.0015325032957234357 0.004319166843248679; 0.0006984655352816682 0.001236610061109202 0.004839152717310875] %
+
+Mass Used: 120.46154407807808 kg
+Launch C3: 92.73261655050308 km²/s²
+||V∞_in||: 1.3639153034447891e-5 km/s
diff --git a/archive/ES_0.5669285937510413 b/archive/ES_0.5669285937510413
new file mode 100644
index 0000000..da0007d
--- /dev/null
+++ b/archive/ES_0.5669285937510413
@@ -0,0 +1,22 @@
+archive/ES_0.5669285937510413---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T16:53:35.592
+Launch V∞: [7.678728215834349, -6.17753638595049, 0.6398845607309158] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.809134284418626e-8, 5.362380167809462e-7, -1.1561179263330903e-5] km/s
+ V∞_out: [1.5207286878016725e-6, 1.1464923799002302e-5, -1.3913137148331665e-7] km/s
+ time of flight: 1.7271798353758138e8 seconds
+ arrival date: 2029-11-01T18:06:38.592
+ thrust profile: [0.29380007245726675 -0.04198264937236405 -0.12159159364065274; 0.07796448925775237 0.023309617488371164 -0.09617750570734501; 0.04854119454435031 0.02363960265532498 -0.10252228364734566; 0.04927968876102569 0.02952281924920052 -0.14703340865508338; 0.053720258488778705 0.036581640095274294 -0.20423588874882156; 0.020085786196848292 0.013941837616503944 -0.09052135394661721; 0.013438151726101343 0.009655251533716774 -0.07043747526319129; 0.0162672765872332 0.012210189468929463 -0.09469831015064778; 0.0022605948407424642 0.0022617444167080487 -0.013198509630581714; 0.0018125021941431704 0.001970211859984956 -0.013884311784231843; -0.0005994316191439528 0.004212818673595902 -0.015088508209864352; 0.0017421160200906966 0.0012266428299234089 -0.005687530222232134; 0.008830630015651021 0.0026371492719073535 -0.010187188763330194; -0.009875433934883713 0.0020667733845623005 -0.009104096632706012; -0.00040931906451128965 -0.005479851635983482 0.002411142560549103; -0.013262815673837115 -0.007009123424385798 0.0012698969708428562; -0.004093650945105909 -0.003802005001939849 -0.004929313304877945; 0.010849526570996075 0.005276859684073665 0.007905446390511071; -0.023025211711127994 0.0011419902525552342 0.0018934454790623442; -0.00350268106747557 -0.0012345300030569615 -0.0011408856208661583] %
+
+Mass Used: 92.46675483939634 kg
+Launch C3: 97.5342750634546 km²/s²
+||V∞_in||: 1.1573872101735912e-5 km/s
diff --git a/archive/ES_0.5669339102932146 b/archive/ES_0.5669339102932146
new file mode 100644
index 0000000..9b58448
--- /dev/null
+++ b/archive/ES_0.5669339102932146
@@ -0,0 +1,22 @@
+archive/ES_0.5669339102932146---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T12:04:31.648
+Launch V∞: [6.395344083407324, -7.23863218096833, 0.4581822198832658] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1283651637146381e-7, -2.465748011258296e-8, 3.137891713707744e-8] km/s
+ V∞_out: [-1.1926255200983936e-7, 1.1233262190465383e-8, -1.4446823647510184e-8] km/s
+ time of flight: 1.874957778748135e8 seconds
+ arrival date: 2029-04-06T14:14:08.648
+ thrust profile: [0.5307652599036145 -0.12134449439752272 -0.1414951911505094; 0.13523425994778748 0.045490657775409116 -0.1241307635817385; 0.08485507659824561 0.05270885062706215 -0.13312616738580405; 0.060087369389324165 0.05040694179565581 -0.13263022745904965; 0.04007576685336013 0.04138523358929835 -0.11807020561870324; 0.02395266339077213 0.029172349091670147 -0.08871397203167065; 0.017764499683249304 0.023523438357187298 -0.07364869246945305; 0.010157575601917468 0.015569138420437625 -0.05263310358001774; 0.002029367327713067 0.002509840751155483 -0.009120901393016988; 0.0008462089040677821 0.002358487374642281 -0.008942799965389268; -0.001777131320037379 0.0046991538506230375 -0.004519276220403449; 0.0031991012588659918 0.005207839377941559 -0.02280628710647214; 0.0009513759924771713 0.0012628739013299728 -0.0030345419227453766; -0.002954579384520506 -0.002356237183855898 -0.008806509593322225; -0.0022993281741790915 -0.0016355657175637093 0.002547256820138742; -0.0008645525343142502 -0.005186008990622409 0.002138160404377474; 0.0025257539558784254 0.009287749076675837 -0.0016359731627909714; -0.005046242923367461 0.005815219998353701 0.007391960948970665; -0.0007369694795745048 -0.002940525154464386 0.005508941537457017; 0.005078290469337663 0.0075912730762843755 -0.017250460414501744] %
+
+Mass Used: 115.95867100709711 kg
+Launch C3: 93.50815274314056 km²/s²
+||V∞_in||: 1.1968586881100716e-7 km/s
diff --git a/archive/ES_0.5669433286139834 b/archive/ES_0.5669433286139834
new file mode 100644
index 0000000..5159530
--- /dev/null
+++ b/archive/ES_0.5669433286139834
@@ -0,0 +1,22 @@
+archive/ES_0.5669433286139834---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T20:43:24.630
+Launch V∞: [7.47572500836232, -6.598683067269156, -0.03523656005163485] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00020021333216554453, -0.013741698877457052, 5.135052399717994e-5] km/s
+ V∞_out: [-0.013315420042468749, 0.0020559565176505997, -0.00284480639727028] km/s
+ time of flight: 1.6679260058565167e8 seconds
+ arrival date: 2029-08-26T08:00:04.630
+ thrust profile: [0.15660047064953733 -0.024143002703220375 -0.06707570370243755; 0.04872397107022745 0.015262679893667584 -0.06225713257581229; 0.06754628940999877 0.035181519832703276 -0.14284593781431945; 0.06038302228232455 0.03973963757189697 -0.17652412439948004; 0.03847150169776422 0.02957374392194699 -0.14469445833555428; 0.02387965784225563 0.020973745701614727 -0.11059192302242013; 0.016954190552202583 0.016318240731402204 -0.0925341233140196; 0.012926327029608182 0.012106722430784467 -0.07207154165034733; 0.013845685769342331 0.014534522765830322 -0.09234026580769598; 0.0029007232716904987 0.0026364596045721223 -0.022630829721107998; 0.0039737825153022465 0.0036268593865250104 -0.027039816404765202; 0.0007547919675057984 0.00038815235498095924 -0.0018708103447884414; 0.0003277390803346422 0.0015818080021566135 -0.0018500988645719098; 0.0010302450259776024 0.00250545550861519 -0.004402345695452237; 0.0005542922601678224 -0.0013426326428601755 -0.005903952842251788; -0.0017738328593153215 0.0015671132043980325 -0.0031447784025966066; -0.00022921568832156083 0.0010174038629560268 -0.009185849998282307; 0.00023514910541957428 0.0020622532881812696 -0.0007435623882669595; 0.000622799045373699 -0.002391338975013586 -0.002162690585713313; 0.0018500150536886286 -0.00267450983022521 -0.002198872063934922] %
+
+Mass Used: 81.42365866083128 kg
+Launch C3: 99.43032423808276 km²/s²
+||V∞_in||: 0.013743253264543879 km/s
diff --git a/archive/ES_0.5669443401175023 b/archive/ES_0.5669443401175023
new file mode 100644
index 0000000..b9a9d15
--- /dev/null
+++ b/archive/ES_0.5669443401175023
@@ -0,0 +1,22 @@
+archive/ES_0.5669443401175023---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T21:08:10.935
+Launch V∞: [6.525346371346284, -7.510541147137229, 0.12533703521157197] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9267222425764154e-7, 2.0985028984247807e-6, -1.2569800449889963e-7] km/s
+ V∞_out: [7.620877859817739e-7, -1.7414562144583742e-6, 9.456859586533586e-7] km/s
+ time of flight: 1.8370271342942265e8 seconds
+ arrival date: 2029-02-25T01:40:03.935
+ thrust profile: [0.14559711974362782 -0.04342560072176552 -0.06133099170520052; 0.054383879703163336 0.009873678377412577 -0.06857469387452259; 0.05232511188097165 0.0207846463916445 -0.10979703294997119; 0.04321112651161738 0.022707476121080025 -0.12448920084227152; 0.041252676214158686 0.026609448879223025 -0.15227942635170683; 0.02630259821510073 0.01857235717145814 -0.11552429638626996; 0.02001403356212731 0.015220546503301614 -0.10025650200109647; 0.01655647723910191 0.013609886392179029 -0.09630394224914833; 0.005850121200763927 0.0050940082125918796 -0.036252191422337654; 0.0012890568338385434 0.0026787861483844174 -0.018651362855076146; 0.0033722643110123294 0.003619589641978117 -0.029953589544970224; -0.0030419319887029775 0.001480759692982348 0.0017390207230928937; -0.0002511704583760182 0.0018817299393928766 -0.0033847306545513123; 0.0016484231262068865 -0.004845050688841734 0.0029429898255848193; -0.005985925498672607 -0.007936101806645827 -0.0006968589245533775; -0.004548022940026949 -0.004564867385685824 0.006341191998022235; 7.918734395142765e-5 -0.0004810753462419566 0.004424655939623685; 0.0009718796106562825 0.0017888238053912313 0.004714764150699216; -0.007671633116238912 0.0003729851302779673 0.012211083151033829; 0.0048082192008314095 -0.00442849269266973 -0.011500981718937679] %
+
+Mass Used: 83.9112461962909 kg
+Launch C3: 99.00408296127915 km²/s²
+||V∞_in||: 2.122538912219073e-6 km/s
diff --git a/archive/ES_0.5669446438806317 b/archive/ES_0.5669446438806317
new file mode 100644
index 0000000..6492560
--- /dev/null
+++ b/archive/ES_0.5669446438806317
@@ -0,0 +1,22 @@
+archive/ES_0.5669446438806317---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T02:20:09.428
+Launch V∞: [6.2083761772656265, -7.639679290602462, -0.07816630475022046] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.913742016803e-7, -0.00016127253175887162, 0.00020736978901931763] km/s
+ V∞_out: [0.00026119857825418653, 4.204760551103423e-5, -3.600849033948988e-5] km/s
+ time of flight: 1.7629313030233496e8 seconds
+ arrival date: 2028-11-28T12:38:59.428
+ thrust profile: [0.2848801151778207 -0.09660020856485889 -0.10614455327527278; 0.0508107624104765 0.009232829367743495 -0.05734610740283667; 0.06381932882594064 0.026516892829878118 -0.1136979241850149; 0.08048231012860449 0.04565387879757817 -0.19365183552070095; 0.046202704453453744 0.03184888563887987 -0.1428226687941324; 0.03361043140628538 0.026332618503723315 -0.12574561896792344; 0.02244855440920707 0.017920818308230523 -0.09251664372380584; 0.0035543345813079026 0.0033047287456701136 -0.020319680614809942; 0.009253465576288552 0.009095505348499384 -0.052382291853009376; 0.01070508060921737 0.010376553183893883 -0.06420847223687733; 0.007730800794993388 0.008885276642181155 -0.05279291960055521; 0.001501880716360467 0.0015987174822395798 -0.0026082035917349656; -0.003616441391259851 -0.0019286971331940314 -0.0010558130021610336; -0.00118855249635445 -0.0004756028133630351 0.0006267667391273665; 0.0005750736939211503 -0.0008410885842827203 -0.0015139682125971637; -0.0011988341480938208 -0.0012645285502160995 0.004200922324972838; 0.0013875228472556012 -0.005185230756119038 -0.004450501731491499; -0.003664000362513565 0.0008965202566926378 0.008917683573380084; -0.00025734690785438334 0.005847209170090062 -0.005430782645878893; 0.004416993581374172 0.0035861999017493813 -0.0041946323087428215] %
+
+Mass Used: 96.09940890216649 kg
+Launch C3: 96.9147443928978 km²/s²
+||V∞_in||: 0.0002627004699198677 km/s
diff --git a/archive/ES_0.5669507945114978 b/archive/ES_0.5669507945114978
new file mode 100644
index 0000000..523035e
--- /dev/null
+++ b/archive/ES_0.5669507945114978
@@ -0,0 +1,22 @@
+archive/ES_0.5669507945114978---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T07:21:32.296
+Launch V∞: [6.323411570282988, -7.675827429535264, -0.3710435927963415] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.111796402288281e-6, -5.076828120891477e-7, 1.14061593951457e-8] km/s
+ V∞_out: [7.854322758935506e-7, -1.6063280540224253e-8, -4.056379895807465e-6] km/s
+ time of flight: 1.8425424209213653e8 seconds
+ arrival date: 2029-03-05T21:05:34.296
+ thrust profile: [0.21947361228357207 -0.06340310177981155 -0.0877499956989709; 0.027993636302665135 0.005335560377800346 -0.03417218284462458; 0.02578956652852844 0.01045456695882717 -0.05364752934960413; 0.029732296854362277 0.015952954370458218 -0.08598427526161095; 0.040537752786351536 0.02626868348745589 -0.14651434612599587; 0.031692521735676875 0.023206387158306294 -0.13907929029891955; 0.009317586055211984 0.007134076986981901 -0.047971141465570084; 0.0168500232921481 0.014602640135638207 -0.10022916083366112; 0.02190960447670319 0.019417201218877432 -0.1373367448129073; 0.007959076601041285 0.007358501017185518 -0.05653142528235971; 0.00227614460058562 -0.00010822134970370407 -0.006201365270321149; 0.0017697261620912446 0.0007270530997775743 -0.008328014821284176; 0.00025048278845381125 -0.003562707382421316 -0.003094965609700278; -0.00014698773929679295 0.0008695670848857313 -0.0038380606466057936; -0.000445753235372555 0.00015422996486081907 -0.004743560944884977; 0.0018157356596664451 -0.0021617100044288434 -0.002676095093669984; -0.0051535302462501565 0.0026529555773847674 -0.002946037332523376; -0.004444295078067394 0.0036223074579863996 -0.0009218757564144175; 1.956148819311527e-5 0.0016359443841686317 -7.644993243088166e-5; -0.002923251805094189 0.0018585758429421183 0.0007453896047208587] %
+
+Mass Used: 83.70031214620622 kg
+Launch C3: 99.04153396294991 km²/s²
+||V∞_in||: 4.143035311463534e-6 km/s
diff --git a/archive/ES_0.566952551777573 b/archive/ES_0.566952551777573
new file mode 100644
index 0000000..47d88d2
--- /dev/null
+++ b/archive/ES_0.566952551777573
@@ -0,0 +1,22 @@
+archive/ES_0.566952551777573---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T09:35:31.704
+Launch V∞: [7.634955079798778, -6.0760341734769385, -0.9167489448869082] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1233611860383877e-9, -3.7161993811412356e-9, -1.0070416609221629e-9] km/s
+ V∞_out: [-5.780725491022826e-10, -1.2378789111004773e-9, -3.0428774716918014e-11] km/s
+ time of flight: 1.827586865597997e8 seconds
+ arrival date: 2030-02-25T15:53:37.704
+ thrust profile: [0.26578519888868346 0.01395190306779939 -0.07261837962744433; 0.12801821799512467 0.0926896400248592 -0.10498873020220795; 0.08358476654247908 0.10269459755168425 -0.12359421031561241; 0.058894143493119264 0.10209156645754945 -0.1334306217966364; 0.0444142887438572 0.10141812195854262 -0.14265453141105924; 0.02670135650217934 0.0798192279359278 -0.11998242146300059; 0.0137564089840152 0.05311724302870315 -0.08745878845858188; 0.005406408375927129 0.025268468151004697 -0.04855313623109398; 0.0023737528935202606 0.012418396126430562 -0.02520903831442288; 0.0007409836050812268 0.0025909145710853185 -0.002410971775304479; 0.0016132217598410585 0.006832028352434466 0.0023907900468846752; 0.0011944262442541978 0.004061423080514444 -0.00022585824769342432; 0.004126520108077608 -0.0011896719946512119 -0.004390492506252886; -0.0011184799570578934 9.425282307625284e-5 -0.0028904643281618537; -0.0011340457403154996 -0.0010498581708504413 -0.0005801321083628809; -0.00023768839474218296 0.0008814639089425942 0.0006147092977371242; -5.9337536441716566e-5 0.004115861389818953 -0.0045364538307927525; 0.0011659747432893283 -0.0026719724129423343 0.007266194664279171; 0.0005720802065095096 -0.004062230990495734 0.0034389604468127197; 0.0006727819109500323 0.001753545482869459 -0.004574930984360571] %
+
+Mass Used: 101.14621638192511 kg
+Launch C3: 96.051158975756 km²/s²
+||V∞_in||: 4.396923182590494e-9 km/s
diff --git a/archive/ES_0.5669648004897456 b/archive/ES_0.5669648004897456
new file mode 100644
index 0000000..f9f490b
--- /dev/null
+++ b/archive/ES_0.5669648004897456
@@ -0,0 +1,22 @@
+archive/ES_0.5669648004897456---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:16:39.896
+Launch V∞: [7.2819054035496045, -6.613825328196146, -0.33177631984388745] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009857245669833029, 0.0019113054213988998, 0.0006925446041342327] km/s
+ V∞_out: [0.0008461235423839499, -0.0011773810021859586, 0.0017326081583644043] km/s
+ time of flight: 1.5840819884176168e8 seconds
+ arrival date: 2029-05-17T13:33:17.896
+ thrust profile: [0.37667219534857066 -0.08738066594342977 -0.1482218040075446; 0.05919473537406328 0.016807526578943726 -0.07366569061531086; 0.07559880142641409 0.0379624454977703 -0.15187246885587205; 0.03506250409368244 0.023799730844778405 -0.10130965046851471; 0.0524304093736426 0.04078515957863064 -0.18509118949653292; 0.04404419389217556 0.04874936351955977 -0.19979589527379676; 0.023732372390084494 0.022962049007871955 -0.12076749727419907; 0.011408478428120995 0.011510391726750778 -0.07027289962949745; 0.012123032955468854 0.01245202098651422 -0.0812756973460505; 0.004132799618195015 0.004912584860144729 -0.035198945502370016; 0.0003534793392878955 0.0004524825302102063 -0.002546331583813098; 0.0004947163564889365 0.00020604691473173568 -0.0010147560962641237; 2.987038681093602e-5 3.304737173722111e-5 -0.00036090524801566184; -0.0004743821047136952 -0.0002817888726801333 -0.00019915187460945328; -0.00039164732002483894 -8.272205409563734e-5 -0.0013323944809272175; -6.48462291069196e-5 0.0013445694153002101 -2.511490444493433e-5; -0.00038340667119091376 9.777514926905938e-5 0.0007890834819057311; 0.00033331835498412617 1.1609543699075376e-5 8.642747159350375e-5; -0.0005197942906537102 -0.00035736326793707777 -6.7724154240001e-5; -0.00038380749152586293 -0.0008480848657471621 0.00029936454060854934] %
+
+Mass Used: 96.33197462820272 kg
+Launch C3: 96.87890730454293 km²/s²
+||V∞_in||: 0.002259282931493682 km/s
diff --git a/archive/ES_0.5669661740355211 b/archive/ES_0.5669661740355211
new file mode 100644
index 0000000..5b5e50e
--- /dev/null
+++ b/archive/ES_0.5669661740355211
@@ -0,0 +1,22 @@
+archive/ES_0.5669661740355211---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T14:49:12.950
+Launch V∞: [7.821381238684813, -5.693522597257366, 0.04834618681209905] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.5645163740584026e-6, -0.00040435336382188493, -5.9943153195522855e-6] km/s
+ V∞_out: [-0.00039020413149129345, 5.874094045161766e-5, -9.059415936444675e-5] km/s
+ time of flight: 1.8574306979592445e8 seconds
+ arrival date: 2030-03-31T10:07:01.950
+ thrust profile: [0.5156614723995858 0.010441149141994429 -0.1305600960108501; 0.12890980678512304 0.08407610057294974 -0.12019856481299551; 0.0494670424212049 0.052869629719134795 -0.08494577581618197; 0.04824786869614906 0.07118275213909524 -0.12589364499853997; 0.032188637863972074 0.06042481354030148 -0.11714150707345777; 0.015124112148273996 0.03431750700780328 -0.0714191675577065; 0.01294073530640032 0.03701342513161506 -0.08098576786622451; 0.0012240804621468863 0.004682007318647938 -0.013937454560959265; 0.004841183639285788 0.018619338077430478 -0.04554659109777746; 0.003807343447034988 0.0027977706192361335 -0.00800531505797739; -0.000593195809748386 0.006263469742489635 -0.008647755651806307; -0.0035572775447343438 0.003987257681764561 -0.014095500208169189; 0.005512786197692255 0.0055351848085182995 -0.0039159549806565075; -0.0009027632248670855 -0.0005410184745512263 0.007336317043890098; -0.01668193715358058 -0.014838199910355544 -0.03231038118443828; -0.00828940105400652 0.006948420106820721 -0.017890645560510888; 0.0035063437527841205 -0.0021791844071292086 -0.008223055676930414; 0.0058370274013462425 -0.010510637442650544 0.006294614131884509; 0.002875828593965143 0.008801545588407702 -0.040639705218406486; 0.0016356285470774759 0.015261899165816308 0.01835115424219358] %
+
+Mass Used: 115.50404487413107 kg
+Launch C3: 93.5925414001103 km²/s²
+||V∞_in||: 0.00040446853593103783 km/s
diff --git a/archive/ES_0.5669746578628586 b/archive/ES_0.5669746578628586
new file mode 100644
index 0000000..13621d9
--- /dev/null
+++ b/archive/ES_0.5669746578628586
@@ -0,0 +1,22 @@
+archive/ES_0.5669746578628586---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T00:16:21.271
+Launch V∞: [6.29903454286789, -7.2982404734261355, 0.3760469640273712] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.166719876543115e-9, -2.8742960451746372e-9, 1.3239054064839243e-8] km/s
+ V∞_out: [3.553248967170807e-9, -9.431427712991782e-9, -1.1907634123982377e-8] km/s
+ time of flight: 1.8376781354130226e8 seconds
+ arrival date: 2029-02-20T22:53:14.271
+ thrust profile: [0.5990686778931973 -0.13831057017606987 -0.15608188292326602; 0.07427010899716754 0.024855522797390468 -0.0688038370862674; 0.09425314385280503 0.06082244505938622 -0.1401556368610865; 0.047894363229072624 0.04205918816158103 -0.1024146504572511; 0.052456529899620956 0.057067320129065596 -0.14204155634514193; 0.04972745987952607 0.06521274349725836 -0.1666904709372841; 0.010315751648695151 0.015037829937139422 -0.04388180959984325; 0.01833504725047602 0.028937892699607295 -0.08429987784055568; 0.0036058334736170598 0.00598338234838262 -0.018084300885746488; 0.0026941869418171498 0.006208978524986081 -0.018661890891202234; 0.0006198120325566645 0.0017241605359672209 -0.004162284150364593; 0.0012914831027320526 -0.0008217505130286855 -0.0012071290622708494; 0.002944119112493147 -0.0037497848885002533 -0.00031901565296300557; 0.00022050062100528503 0.0014427927638368861 -0.003952812465323998; -0.0005298127509436616 0.0021317634493154733 0.003111549489719344; 0.00013091386395645594 -0.00013795566644721527 0.0017567356166270569; -0.0005505514188677181 -0.001953621889274306 0.005505689048107896; -0.005766351894119904 -0.005934363911070762 -0.003902487533830319; 0.0007244797297717367 -0.002546584047142702 0.0063914219448829405; 0.00951651346308034 0.0073782846300327175 -0.0013329960371734895] %
+
+Mass Used: 118.4829920937791 kg
+Launch C3: 93.08356149935244 km²/s²
+||V∞_in||: 1.4499280139707238e-8 km/s
diff --git a/archive/ES_0.5669769926901171 b/archive/ES_0.5669769926901171
new file mode 100644
index 0000000..5c1f892
--- /dev/null
+++ b/archive/ES_0.5669769926901171
@@ -0,0 +1,22 @@
+archive/ES_0.5669769926901171---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T01:42:20.789
+Launch V∞: [6.595798636599028, -7.397144432090494, 0.03572214931100197] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.537230983022231e-5, -9.075326720559897e-6, 1.5924710070306108e-7] km/s
+ V∞_out: [7.143342882467819e-6, -1.5656135708308514e-7, -3.574249853556275e-5] km/s
+ time of flight: 1.8749577786520475e8 seconds
+ arrival date: 2029-04-10T03:51:57.789
+ thrust profile: [0.20411038745388677 -0.05098539949213173 -0.0756557772555091; 0.05784574076496233 0.014331125865577027 -0.06601513057217796; 0.04674156970370141 0.022512309126944578 -0.08913960675010589; 0.048096068251937726 0.032414839194856375 -0.128342398574254; 0.0339402713383258 0.02693945580957217 -0.11601011838295446; 0.02540801207243859 0.022800920479226817 -0.10632173127692911; 0.01581636272503195 0.016554616452715804 -0.07867142405179514; 0.008445179409669983 0.01093542636124833 -0.06638494602615716; 0.006889625728960032 0.006637613387544257 -0.04351390881208038; 0.010412307026857637 0.01566995417226142 -0.07477166326030135; 0.003385001154130638 0.004143849668354118 -0.015013507114477511; 0.0019879150478651396 0.006964567438320016 -0.002969422557538971; -0.0016732400733475987 0.0030424718308473334 -0.007787680182639858; 0.002747994670420028 -0.003957363463891221 -0.007782969891523138; 0.0014875188494075909 0.000936545443220641 -0.0004468605945149545; 0.0009883636195916205 0.016093583498704045 -0.020653393214226864; 0.0017760734133095844 0.0006459923116129956 -0.006696962697694493; -0.012439291639991742 0.0013745068631110112 0.005656111027574608; 3.4629887211981965e-5 0.0017917264416819807 -0.007893214106924059; 0.016951736030142515 0.010442824607070507 -0.013004021278721389] %
+
+Mass Used: 88.50226619676778 kg
+Launch C3: 98.22358147572038 km²/s²
+||V∞_in||: 3.651831345296812e-5 km/s
diff --git a/archive/ES_0.566979220437721 b/archive/ES_0.566979220437721
new file mode 100644
index 0000000..7fcd7e5
--- /dev/null
+++ b/archive/ES_0.566979220437721
@@ -0,0 +1,22 @@
+archive/ES_0.566979220437721---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:45:29.759
+Launch V∞: [7.4334145901749755, -6.233519684391334, -0.01883944449366637] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003962244343396871, 0.0002607599171482519, -0.00013192236561017536] km/s
+ V∞_out: [-0.00021387802537447599, -0.00037481080158296537, 0.00023660265208587256] km/s
+ time of flight: 1.6595538624086505e8 seconds
+ arrival date: 2029-08-11T01:28:35.759
+ thrust profile: [0.5115356618382455 -0.08023420833496157 -0.16939139658152275; 0.11764589121193281 0.04418055776321056 -0.12285787511129975; 0.08758514794685382 0.057794353340356326 -0.15701564750565009; 0.06998862432504013 0.06091956897946363 -0.17827498566542893; 0.0574706010617353 0.059829430422836734 -0.18917161368121224; 0.027444857861531235 0.03299315422552239 -0.11442382890635813; 0.016285996021339184 0.022401350447335627 -0.08275439934540142; 0.0016455193639339598 0.0027107097710341015 -0.015555216201916957; 0.005639011303259659 0.008950537062071863 -0.03725555577930801; -0.0006410575412850144 0.0014295055953714966 -0.007757789314894797; 0.0005138217222618095 0.006213605041185564 -0.021357271999434543; -0.0009950910255584618 0.000984608551151259 -0.008619531364844819; -0.0036371058994999856 0.000500089246060493 0.0006004536166278563; 0.003836667936953644 0.0004039640093795893 -0.001999962270248649; 0.0006780488428578083 0.0086580430708043 -0.0045957848065783895; -0.0027150600899944256 0.011573994886253103 0.0004397695453331376; 0.00910797762986596 -0.010269335884998454 -0.0007410565138049781; 0.004949450895125186 0.0013814407755170235 -0.00935658144487649; -0.0005521522603624067 0.00436229793917337 0.0017403893231608403; 0.02113738287293379 0.0021636178154975584 -0.009704185770105334] %
+
+Mass Used: 112.48456938690379 kg
+Launch C3: 94.11277504978926 km²/s²
+||V∞_in||: 0.0004923342841070008 km/s
diff --git a/archive/ES_0.5669811956656594 b/archive/ES_0.5669811956656594
new file mode 100644
index 0000000..6774cf0
--- /dev/null
+++ b/archive/ES_0.5669811956656594
@@ -0,0 +1,22 @@
+archive/ES_0.5669811956656594---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T23:49:30.480
+Launch V∞: [6.463131152928825, -7.521080045812693, -0.22751034970461878] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.822706686827749e-9, -4.6573307295272785e-9, 1.5869549388271927e-8] km/s
+ V∞_out: [4.313674561005231e-9, -9.691463977683775e-9, -1.1744979680582668e-8] km/s
+ time of flight: 1.7987757401878124e8 seconds
+ arrival date: 2029-01-08T21:49:04.480
+ thrust profile: [0.16593336672736153 -0.04887866982449635 -0.06257781644358738; 0.04300487107585532 0.010524510713174944 -0.0481034370549878; 0.061127256136670555 0.031428677477228044 -0.11056687948498627; 0.0911551985687885 0.06163580438342652 -0.22021560049637048; 0.047462308544056246 0.04061934046418254 -0.15078137201898872; 0.029524666386179142 0.02940592362379842 -0.11585383880644493; 0.011885669092229614 0.013003676926464676 -0.05602550122126331; 0.007663993281868396 0.009535136522506898 -0.04226501601455271; 0.0010965205106654144 0.002022055681881509 -0.008342798086677396; 0.021576285372220293 0.0317561342001967 -0.14145490660383803; 0.001514875174328886 0.0009149099510081097 -0.007387405542742682; 4.209108382235277e-5 -0.00030447688116194395 0.0017240087323919491; -0.0011425478752833543 -0.0015369481660552405 0.0007732520849703882; -0.005750922417567774 -0.0018733218316676367 0.0005435684091445753; 0.000709874831443634 -0.000845900077560224 -0.0005201811963685785; -0.0008168704196926837 2.2571462155036555e-6 -0.0033523988940557144; -0.0012872212759296856 0.005875315589582231 0.005719609947158371; -2.321543338319531e-5 0.0006693715291499877 0.00630503272083506; 0.0012835683691715147 -0.0036175539864178163 0.0007319972914915215; 0.009546047587977703 -0.004129977068648929 0.004694818546947855] %
+
+Mass Used: 87.53365144083136 kg
+Launch C3: 98.39047031470366 km²/s²
+||V∞_in||: 1.8744958804777246e-8 km/s
diff --git a/archive/ES_0.5669956372048124 b/archive/ES_0.5669956372048124
new file mode 100644
index 0000000..9b430c8
--- /dev/null
+++ b/archive/ES_0.5669956372048124
@@ -0,0 +1,22 @@
+archive/ES_0.5669956372048124---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T17:10:37.394
+Launch V∞: [6.379992822096605, -7.300608919221345, 0.12005522861168157] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.792795621021633e-5, -0.00012390337923698453, 2.180170924557334e-6] km/s
+ V∞_out: [2.8275123806285132e-5, -7.168956195188081e-7, -0.00015539240012696695] km/s
+ time of flight: 1.8148337542354062e8 seconds
+ arrival date: 2029-01-24T05:13:32.394
+ thrust profile: [0.5189847073312757 -0.14343675451047797 -0.14897440159691758; 0.0732614644212778 0.022201119224767255 -0.06653890582887731; 0.08729012126965989 0.05308788727274098 -0.12869854430183172; 0.09379225224909532 0.07731000216296019 -0.18707807086861086; 0.06705014580719484 0.0675061928781512 -0.16967000985678288; 0.03250605519747202 0.039095172704344545 -0.10780207564992325; 0.010045605910425729 0.013410989700843456 -0.040585834491893846; 0.01001993323054223 0.014774643945783098 -0.046571833923830144; 0.009821901711320243 0.01564489550416579 -0.0521044302158614; 0.0026440567696966815 0.005838472063424172 -0.019085970854596596; 0.00029455495530388725 0.000668267279744028 -0.0017149558396536283; 0.0010603413997946015 0.0022191103146691734 -0.009744656614481359; -0.0001600270953100978 0.0013632907324803143 -0.0008003225111120147; 0.00039082384775771857 0.0016328643477333024 -0.0041597274047138685; 0.0008038050085629313 -0.002490055702516928 -0.0015840318172502584; -0.0019906446240231545 -0.002554732834203462 0.003631069457045431; -7.169466175107838e-5 -0.0008382395953869222 -0.0010719826075298003; 0.0006093149393374917 0.0012171347163576845 -0.002285756936388536; 0.0009104226817770125 -0.0004422239913707926 0.00010023452251935769; -0.00021408581807790894 -0.00036524966607588585 0.003089156105136062] %
+
+Mass Used: 113.05883855949105 kg
+Launch C3: 94.01761225933544 km²/s²
+||V∞_in||: 0.00015794519663197846 km/s
diff --git a/archive/ES_0.5670104048290463 b/archive/ES_0.5670104048290463
new file mode 100644
index 0000000..cd97389
--- /dev/null
+++ b/archive/ES_0.5670104048290463
@@ -0,0 +1,22 @@
+archive/ES_0.5670104048290463---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T00:38:58.759
+Launch V∞: [6.64693746731244, -7.441130150042866, 0.06830149594791622] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0035044039279746976, 5.186748912788389e-5, -0.0023805629199034825] km/s
+ V∞_out: [0.0032289408560313066, -3.329850336816791e-5, -0.0009765589905698411] km/s
+ time of flight: 1.8749577787462917e8 seconds
+ arrival date: 2029-04-11T02:48:35.759
+ thrust profile: [0.1116705312902882 -0.029795754431944453 -0.04569358046384155; 0.0559048974812367 0.012639222136771298 -0.06805392176225061; 0.04328393784480347 0.019057993848006296 -0.09017645592814129; 0.03178614842426926 0.019554267665907597 -0.09106177686343228; 0.03143792783370694 0.020113387175091563 -0.10744099392807431; 0.028373955743505236 0.020421077281547812 -0.11196543211694836; 0.016879451502060435 0.013511262242681144 -0.08667024056163111; 0.014268206441189951 0.012871542508874375 -0.08116090093881928; 0.009962090630601685 0.01024062336293329 -0.06860038665942653; 0.013940051398257231 0.013113637228924373 -0.09109304938284808; 0.001837005864352119 0.0020863784538564002 -0.018266316639238073; -0.0007876530805486977 0.0027400921662809117 -0.0025778396302148583; -0.0006414504169075708 0.0008890598335439655 -0.0017341091458146687; -0.006871547042432275 0.010461929366487628 1.2060269077317437e-5; 0.0037554779895809364 -0.0002563343714060729 -0.0018797357149524284; 0.004920969189875444 0.0019404551500320838 -0.013765428582854324; -0.012023940957066251 0.002975048757336967 -0.003280766065829207; -0.009256698433236529 0.0007507507495569425 0.00764725158608324; 0.01121069687151769 0.00025287724699826335 0.00042630533501133896; -0.002453598726419553 0.0065853293733483 -0.006310530897657482] %
+
+Mass Used: 80.7637848921263 kg
+Launch C3: 99.5568606985876 km²/s²
+||V∞_in||: 0.004236816840795967 km/s
diff --git a/archive/ES_0.5670171901477108 b/archive/ES_0.5670171901477108
new file mode 100644
index 0000000..3d63553
--- /dev/null
+++ b/archive/ES_0.5670171901477108
@@ -0,0 +1,22 @@
+archive/ES_0.5670171901477108---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T15:19:39.206
+Launch V∞: [6.1753940490284895, -7.735850324236743, 0.10692349512258043] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0032887676874508802, -0.001845899799891635, 0.005475844847483997] km/s
+ V∞_out: [-0.004250110483768607, -0.001770142181712622, -0.0047921748274752495] km/s
+ time of flight: 1.7550717768918723e8 seconds
+ arrival date: 2028-11-19T23:19:16.206
+ thrust profile: [0.18729571589148522 -0.05878383191695514 -0.07139896994575091; 0.056058198173524 0.010703818692489417 -0.06323193819215289; 0.08711325382272828 0.03853693066227575 -0.15442199225200678; 0.06841922598265099 0.044318217274547635 -0.17764878772483655; 0.048472650237771364 0.0359670438736169 -0.15239681103252262; 0.020659737747864376 0.016665267536524246 -0.08049130893542272; 0.01786003150459361 0.016223995981629106 -0.08208572235211838; 0.022985129099690152 0.02221466283701669 -0.11321630178940283; 0.011581251063966928 0.013323718805375305 -0.0719332829959501; 0.003954640964218387 0.0057175252387871 -0.03189446221468881; -0.0012766790893586084 -0.0005638457323901104 -0.0007491601567853239; 0.0022284521181551225 0.0023178632029153034 -0.009469397712950025; -0.0030599744771766476 0.0018973411895012375 0.0009941119096059687; 0.002175090022279742 0.0002836876781283754 -0.005177585687069641; 0.0009384162941487764 0.001941978257212391 0.0026052753662088946; -0.007450058663335977 0.0024759733922096157 0.003290933540573698; -0.0018191935078837123 -0.0006899976805563045 0.005657180947755263; 0.0015959784950895046 -0.00029533850354559 -0.002036421385468506; -0.0033069228790344836 0.00258696634780164 0.0003947105830122734; 0.009931882807355748 -0.0007378062211161034 -0.005446196206874862] %
+
+Mass Used: 89.90994539311578 kg
+Launch C3: 97.99030453357945 km²/s²
+||V∞_in||: 0.006648925910775215 km/s
diff --git a/archive/ES_0.5670243593782687 b/archive/ES_0.5670243593782687
new file mode 100644
index 0000000..1888cd3
--- /dev/null
+++ b/archive/ES_0.5670243593782687
@@ -0,0 +1,22 @@
+archive/ES_0.5670243593782687---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T06:07:15.400
+Launch V∞: [6.047091516507545, -7.287506098340522, 0.1258960662006582] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.839549773216802e-6, 1.2437613833973614e-6, -2.2124331789281324e-8] km/s
+ V∞_out: [-1.7409613133472197e-6, 4.548675285619768e-8, 8.796850707436102e-6] km/s
+ time of flight: 1.8199148295007437e8 seconds
+ arrival date: 2029-01-29T15:18:37.400
+ thrust profile: [0.7518834332755524 -0.20723856144297081 -0.21193119365513644; 0.26985449285058755 0.08078393179055131 -0.2293014843573425; 0.08270980167399253 0.04982770286221271 -0.1238793249630766; 0.09623464445393551 0.08029687257879434 -0.19716703054486664; 0.04216254730969486 0.043421524725809735 -0.11522555257652954; 0.01582656124657203 0.019641413336897215 -0.055747838638327184; 0.012261218926424285 0.017465393213486655 -0.05166420681167291; 0.007464223671177191 0.009409409499103823 -0.0302161981499925; 0.0022565674212766625 0.003984762103971406 -0.012619224722921006; 0.0023480459490649364 0.006600553019123953 -0.020673997626550297; 0.00012063663142090501 0.0007829607916714512 -0.0009239278746457986; 0.00037562461641683724 0.0008390190814391277 -0.0026997767688721067; 0.0006832332113451163 0.0022606166064464885 -0.002592434840197783; 0.00011245735143356974 0.00021007481675953843 -0.0005261458851818183; -0.0011273613622832875 -0.0006569489162955406 0.0008810607411452735; -0.0021466137953050288 -0.0028983190322024784 0.0004888684540736452; -2.3439041711673114e-5 0.0029983538200461807 -0.00459322669844424; 0.0017736892952833721 -0.005798961412008821 0.0002044072600123027; 0.005246865417754235 -0.002043922401508679 0.0013252644654266573; 0.0002639668277780549 -2.721952677710391e-5 -0.001014843404578674] %
+
+Mass Used: 138.3314398305065 kg
+Launch C3: 89.69091076185262 km²/s²
+||V∞_in||: 8.926649542693207e-6 km/s
diff --git a/archive/ES_0.5670252643310392 b/archive/ES_0.5670252643310392
new file mode 100644
index 0000000..ea474a4
--- /dev/null
+++ b/archive/ES_0.5670252643310392
@@ -0,0 +1,22 @@
+archive/ES_0.5670252643310392---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T11:23:08.835
+Launch V∞: [7.3317585571682775, -6.114477309417035, 0.10230266122323099] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007077213361084568, 0.0005817735837283054, -0.0004615868019239408] km/s
+ V∞_out: [-0.00041871621374137255, 0.0009362040865916925, -3.897723677289713e-5] km/s
+ time of flight: 1.6771851417826146e8 seconds
+ arrival date: 2029-08-29T15:51:42.835
+ thrust profile: [0.718914942886825 -0.09138711090414148 -0.1942534048426262; 0.24257474100307352 0.10647456225830529 -0.2098096792308139; 0.1076986990260225 0.08344628856756947 -0.1688390370872135; 0.035863955777000855 0.03718913494539827 -0.08529621414912418; 0.02616972103159651 0.03154792848357552 -0.08249949214219289; 0.018795897437950897 0.024589532331808214 -0.07191123115086595; 0.009502580800508763 0.01638606812344138 -0.0486662155510879; 0.02876074244220949 0.05547949832516907 -0.15298471494904295; 0.013831310102531578 0.027919184647317807 -0.08202560864194611; 0.0028039681605069055 0.004392386457438196 -0.018751511793566877; -0.0005115341273829373 0.0020953984699862973 -0.0025920955500247835; 0.0009615968640765945 -0.0010864366510043473 -0.004658735782062262; -0.0005727709498575444 0.0002755645905840201 -0.0033904916254787042; 0.002446265638037872 0.002280973215593077 -0.003980379562280518; -0.0008009244420829776 0.001760990837286149 -0.007647468184574692; -4.2673072181594485e-5 0.0010736198186792575 -0.0025565514848690353; 0.00021809200230655688 0.0005956520734256739 -0.00373698804058464; 0.0002600162995566482 -0.00048452348840820943 0.00031457051176607236; -0.004193460310469032 0.004171911223479518 -0.0044471990534377115; -0.0029259869065881086 -0.0014533927021669587 0.002871934220902465] %
+
+Mass Used: 129.80957922174912 kg
+Launch C3: 91.15198214247941 km²/s²
+||V∞_in||: 0.0010258617684744792 km/s
diff --git a/archive/ES_0.56703062097097 b/archive/ES_0.56703062097097
new file mode 100644
index 0000000..a15a1e0
--- /dev/null
+++ b/archive/ES_0.56703062097097
@@ -0,0 +1,22 @@
+archive/ES_0.56703062097097---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T11:52:30.069
+Launch V∞: [6.488586575205925, -7.400515754920452, 0.17189620007641507] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.333020316447552e-6, 1.2011692584571838e-6, -2.6270650265588287e-8] km/s
+ V∞_out: [-1.542639381164044e-6, 4.039466043469367e-8, 9.281791481089112e-6] km/s
+ time of flight: 1.8533205924771962e8 seconds
+ arrival date: 2029-03-14T13:00:09.069
+ thrust profile: [0.2970327154937748 -0.07736110510513047 -0.10035758194856902; 0.047697161488965974 0.013840229397157296 -0.05092552618095935; 0.07045664712904419 0.03858623956989915 -0.12246023175537596; 0.05936610622161521 0.04359595352774992 -0.14333338767576403; 0.03718452557377038 0.03331966670678212 -0.11673322609618551; 0.023510402725827672 0.024411239001247056 -0.091951796737442; 0.01394095507552721 0.016512271304959743 -0.06338903387473616; 0.006553050608842423 0.010588330958855561 -0.044853210857642614; 0.008451113257434193 0.013564587471841342 -0.05541433169058845; 0.018124544335061984 0.0279707995366813 -0.11725933964674362; -0.003029618646962994 -0.0013047539975656417 -0.009627711232576101; 0.004031101987818864 0.005244124266625193 -0.009678104913956237; -0.00019212691985579801 0.0001234687517378502 0.003925912888537274; -0.0036619043173408646 -0.007725786405334804 0.0004157390745325; 0.0026918742478361183 0.0029115935517671394 -0.0008453321668005238; 0.009422553450841958 0.001902549602641035 0.00014926309371214022; -0.0027864450558248827 -0.005943168714817043 -0.004521372150926328; 0.0009452992094749729 0.0007023569355637564 0.0003505994588204964; 0.0010157798451694662 -0.009211003190293247 0.017019794097653404; -0.002390437553234411 -0.003567606450433171 -0.007269013127382059] %
+
+Mass Used: 96.29192246231196 kg
+Launch C3: 96.89893748636909 km²/s²
+||V∞_in||: 9.410035385786321e-6 km/s
diff --git a/archive/ES_0.5670341432905954 b/archive/ES_0.5670341432905954
new file mode 100644
index 0000000..ac472f6
--- /dev/null
+++ b/archive/ES_0.5670341432905954
@@ -0,0 +1,22 @@
+archive/ES_0.5670341432905954---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T20:07:01.980
+Launch V∞: [6.171721762547421, -7.291809444119019, -0.1022443817641729] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8612473497033646e-9, -2.5500526667211913e-9, 5.033050412636371e-9] km/s
+ V∞_out: [1.387616476565082e-9, -3.2391827901430723e-9, -4.3407693232884734e-9] km/s
+ time of flight: 1.8476019520237112e8 seconds
+ arrival date: 2029-03-03T06:23:36.980
+ thrust profile: [0.6249698975418265 -0.14121382007609837 -0.1527900616501051; 0.1952428123889172 0.07170358463558898 -0.15349424878714785; 0.11145995980312796 0.07683892242603507 -0.14747847649326634; 0.09480182695559111 0.09085832576893045 -0.1754447893987231; 0.05995833997368598 0.07105791725364198 -0.1457542205115487; 0.023531502146990457 0.03255258269085168 -0.0719480887564993; 0.022609931375591134 0.03609007270977294 -0.0824507073930893; 0.009548714605561729 0.01735291057858625 -0.04199037891031902; 0.0014915872458172992 0.0019771065011225724 -0.005840806785731344; 0.0006197702295473136 0.0013032038479225889 -0.003343082584475816; -0.0002410181122424868 -0.0004800093451977226 2.4235575993332187e-5; -6.231899853909732e-5 -0.0001382885707787574 0.00022890018862108097; -0.0003600567393108893 0.0010794699391174782 -0.0012339994822539776; 9.525861387973718e-5 0.0002911101163532158 0.0002301375120006399; 0.0002819983727021323 0.0004484923312720469 -0.0004986243941423272; -0.001359790623090473 -0.0009172826011342104 0.000959972131901045; -0.0001463557004176775 -0.00011501820830252067 0.0003529826575016568; -0.00151982084246629 -0.000754546575016276 -0.0012836436237323558; -0.00018869700978906603 0.0013101142509083466 -0.0021163061112032247; 0.0007191511361186484 0.00035299044742125783 0.003500792223324765] %
+
+Mass Used: 129.1251515217532 kg
+Launch C3: 91.2710883972471 km²/s²
+||V∞_in||: 6.3262233169068206e-9 km/s
diff --git a/archive/ES_0.5670628276027172 b/archive/ES_0.5670628276027172
new file mode 100644
index 0000000..6ebe8e3
--- /dev/null
+++ b/archive/ES_0.5670628276027172
@@ -0,0 +1,22 @@
+archive/ES_0.5670628276027172---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T10:09:29.117
+Launch V∞: [6.383448715613291, -7.394031332480268, 0.1835333168336738] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.011277213916529924, -0.00510659270461086, 0.013400794912086919] km/s
+ V∞_out: [-0.011741228741920984, -0.004779916853136632, -0.013110926981325701] km/s
+ time of flight: 1.8749577787471026e8 seconds
+ arrival date: 2029-04-09T12:19:06.117
+ thrust profile: [0.3929673860966532 -0.09816622444385904 -0.1145578138039098; 0.11087364362906799 0.03476062390883725 -0.1135522701724992; 0.04742586566422745 0.026453820429264044 -0.08103384045895526; 0.043889214542332605 0.03264429434447979 -0.10733826467412963; 0.035923210285436935 0.03324181491754227 -0.11075487039477211; 0.0218113722323985 0.02362142801622016 -0.08864649577388117; 0.020898188486681034 0.02607037901355305 -0.09135183567194857; 0.01037371829308597 0.015458586397357378 -0.059430809192783034; 0.017262249230135758 0.023900384055927017 -0.1036959762863152; 0.0012901772512620069 0.0022003832901168795 -0.01503696086848149; -0.0004954913155043252 0.003324697453501097 -0.0048741952105148326; -0.004574047476497378 -5.7873859153300105e-5 -0.005174535858843211; 0.004364992006205701 0.004402499171285665 -0.002423338450463182; -0.003231078041533027 0.00240942666320814 -0.007332786641165418; -0.0018686794483491493 -0.004894560860193924 -0.0057858188040646906; 0.001893468525469995 0.0023463767466147443 -0.00865876418879712; -0.0003116148890592171 -0.000325927305697832 0.00014645759706719778; 0.00864086150611293 -0.010573907234695121 -0.005427666245270248; -0.00623686498563489 -0.017969413095515065 -0.002594352164065522; 0.0031890046101994028 -0.02424525559235824 0.0024056139900429743] %
+
+Mass Used: 104.75945778427831 kg
+Launch C3: 95.45380132895288 km²/s²
+||V∞_in||: 0.01824374268196566 km/s
diff --git a/archive/ES_0.5670657512741428 b/archive/ES_0.5670657512741428
new file mode 100644
index 0000000..9bd1ed8
--- /dev/null
+++ b/archive/ES_0.5670657512741428
@@ -0,0 +1,22 @@
+archive/ES_0.5670657512741428---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T13:30:25.383
+Launch V∞: [5.8942824443790895, -7.937373437126494, -0.28302461538986884] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.96053745368907e-7, -5.959766846048777e-7, 4.759316239136359e-7] km/s
+ V∞_out: [-4.363804269132317e-7, 1.00913982434283e-6, -5.976793478864404e-7] km/s
+ time of flight: 1.6878699002671424e8 seconds
+ arrival date: 2028-09-03T02:46:55.383
+ thrust profile: [0.23886910997220262 -0.09677313292216214 -0.0993006783721173; 0.05255935746658894 0.004665849735287406 -0.06236689316104955; 0.04641962034816984 0.013699776237162098 -0.09013273014109861; 0.10495267556678473 0.04479798188945287 -0.25600887327110317; 0.05861208903758914 0.030725900262486953 -0.18977531077575713; 0.03567052834402154 0.021079012154412952 -0.13970173365206848; 0.02233865572004847 0.014096310092701951 -0.10217304121391366; 0.016990661347802898 0.011551002033818954 -0.08721098902977491; 0.0035227912729915863 0.002515139246981397 -0.021326906040069087; 0.0029764461664096753 0.0028118930249322674 -0.01920709217961243; -0.00011721897876068964 -0.0016792722938062446 -0.0032174639284838777; 0.0026172660525211077 0.0001529806022579308 -0.0026419320750458593; 0.0006660840973204611 0.00027134309490036015 -0.0021878949937214945; 0.0019965435980181354 0.0015242015212341615 -0.002244274953515796; 0.00014933532177938434 0.00015928938170885686 -0.0003555319098580349; -0.00254418593737535 0.00347678339453963 -0.0009057621514549667; -0.00011122585556563869 -1.6650140521293384e-6 -0.0005020559522569737; 0.0011817681937233487 0.0009587070828683004 -0.0025923126236740476; 0.0002535287986000119 -0.00011864718071575301 0.001794248009737986; 0.003209735438874932 -0.002340686340867297 -0.00461698778204144] %
+
+Mass Used: 90.93341079313859 kg
+Launch C3: 97.82456554743338 km²/s²
+||V∞_in||: 1.2545206984729747e-6 km/s
diff --git a/archive/ES_0.5670667038231234 b/archive/ES_0.5670667038231234
new file mode 100644
index 0000000..4359ea5
--- /dev/null
+++ b/archive/ES_0.5670667038231234
@@ -0,0 +1,22 @@
+archive/ES_0.5670667038231234---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T05:54:42.921
+Launch V∞: [7.438360340212719, -5.893807377906329, -0.06450452205271918] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01658124652414911, 0.10190364244063732, 0.12570841253676115] km/s
+ V∞_out: [-0.06780909108935346, 0.05744323073110756, -0.1366167008743838] km/s
+ time of flight: 1.8749577787307426e8 seconds
+ arrival date: 2030-04-18T08:04:19.921
+ thrust profile: [0.4951182466214266 0.023574147506026745 -0.08349736518065393; 0.37255102100186943 0.25584925640465894 -0.20256030811457792; 0.12481818800313123 0.16681740090116148 -0.14219140597251495; 0.05634839587353808 0.10777132188253934 -0.1073815169314239; 0.05437987287729945 0.1360986901427992 -0.14300087325936642; 0.007182465236308588 0.024267873380192553 -0.029251672064120878; 0.01992117754121125 0.09196940720550725 -0.10917491560275684; 0.0011506763274736049 0.0042983597632887515 -0.005092072532471246; 8.702535681573122e-5 0.001204790368388517 -0.0016618812401853135; 0.0004968194183818163 0.0028661174010601903 -0.004346316386634564; 0.0007443380308066334 0.00024077896844668415 -0.0007460126696798791; -0.000457567850602181 0.00020083151409528756 -0.0010796419022913743; 0.00011350769522722149 8.368189547504855e-5 -0.0004495048129331195; -4.332909043228719e-5 -0.0001845141533061354 0.00023384411205319033; 3.909558972757098e-7 -0.00012776250728420424 0.0004332320888308945; 0.0002280628834258471 -6.429922487301648e-5 0.00046093897193398765; -9.441233644452577e-5 0.00024002799068157277 -0.00042797663111476385; 0.00034275378804533743 0.0013804801602371188 -6.290898408782498e-5; 0.0013312368772176665 0.0012410177656036966 -0.0007569608192420604; 0.00012887760023242833 0.0016419629343101794 -0.0009911285662667427] %
+
+Mass Used: 136.16755817319017 kg
+Launch C3: 90.0703307920778 km²/s²
+||V∞_in||: 0.16267112546938498 km/s
diff --git a/archive/ES_0.567073716129383 b/archive/ES_0.567073716129383
new file mode 100644
index 0000000..6aaa9dd
--- /dev/null
+++ b/archive/ES_0.567073716129383
@@ -0,0 +1,22 @@
+archive/ES_0.567073716129383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:02:52.870
+Launch V∞: [6.184537126260828, -7.633084953694224, 0.2729245195187147] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.027258862301052608, -0.012808252464003444, 0.031881413415615956] km/s
+ V∞_out: [-0.021525962241108792, -0.012748359139877532, -0.036019812043859456] km/s
+ time of flight: 1.800318956450553e8 seconds
+ arrival date: 2029-01-12T20:54:27.870
+ thrust profile: [0.3413280822306814 -0.10854556901850454 -0.11454887538766294; 0.06254785709880986 0.012371524714775931 -0.07197045139935135; 0.05258757959215176 0.021471694525753003 -0.10064060108159656; 0.05254189285700088 0.03017767367465968 -0.13834795757318383; 0.041201013926244597 0.02936657019468059 -0.13890110508762382; 0.024665916647319343 0.019473575454441873 -0.10160315581355962; 0.02020407751135024 0.015235759403064758 -0.09079033057145384; 0.02263129203592502 0.02118187168868042 -0.11948838843576902; 0.006046213074169715 0.005268643860834736 -0.033045650337730895; 0.004569310479553515 0.005821580653932855 -0.03015409085553721; 0.003988436606793922 0.004223236644409103 -0.0268951725894898; -0.0022556089286554885 0.0020044291987744347 -0.0048585359936272636; -0.003617513653957021 -0.005942924700853594 -0.004878265958995903; -0.006428895932270643 -0.00029969915492103266 -0.005675341093916684; -0.008149385944956525 -0.0013298453412605802 0.002079541925198174; 8.116957775458665e-5 0.0031109623373466013 -0.0061464458742568045; 0.0004388739979825926 -0.0016875874295628514 1.4646175819510963e-5; 0.0036038784316582096 -0.0016855511393359854 -0.0026378506160645732; 0.0012761218441174988 -0.0076209458313890475 -0.005197739199693189; 0.008549167126592514 0.0002059015761727356 0.008480781118492193] %
+
+Mass Used: 98.16199199397715 kg
+Launch C3: 96.58697316976622 km²/s²
+||V∞_in||: 0.043857968791393136 km/s
diff --git a/archive/ES_0.5670780367313694 b/archive/ES_0.5670780367313694
new file mode 100644
index 0000000..c82f445
--- /dev/null
+++ b/archive/ES_0.5670780367313694
@@ -0,0 +1,22 @@
+archive/ES_0.5670780367313694---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T11:27:17.269
+Launch V∞: [7.5187491363351375, -6.292864275730039, 0.1987047098705135] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010046754818470532, 0.0008144800842810775, -0.00038391365953508415] km/s
+ V∞_out: [-0.0005756901494135745, -0.0010250129761100945, 0.0006617835848773334] km/s
+ time of flight: 1.6572309309024206e8 seconds
+ arrival date: 2029-08-09T13:38:50.269
+ thrust profile: [0.33301323779049496 -0.05616068535334059 -0.1203009093949639; 0.12120155005586632 0.040687757100749046 -0.13451319538959583; 0.08701197667132879 0.05104519934514705 -0.16506514406607492; 0.05674988570008664 0.04293481395876099 -0.15274981879168145; 0.04090943842108379 0.036318694917967576 -0.1419508141396318; 0.03612984648042571 0.03622332272591229 -0.15207007387061647; 0.02224726000957 0.024032011930500002 -0.10984684010767236; 0.0064812110215633914 0.006760807291890226 -0.03814571882687495; 0.005917079684010547 0.0067300683058759934 -0.03805461725491651; 0.0024766238704670364 0.004665110411323713 -0.016008999603125594; 0.0020758100296208648 0.001715148002538784 -0.014875897571533599; 0.0003214144194466612 0.000822895738009976 -0.002074883483661208; -0.005459457323590701 0.008988272037370452 -0.0021560505560284534; -0.0062057767166076375 -0.0016828939207624014 -0.002009019306928637; -0.0006296029089937507 -0.0025084002096312044 -0.0031430952927349286; 0.0010292960623790712 -0.008116959407358513 0.0078641051907566; 0.0015279490830440333 0.0018654738428772544 -0.004704083068107471; 0.0062807474872466655 0.005721281988812145 0.005972756452285833; -0.0017921058748501897 0.005221558292650147 0.008866327040649784; 0.01777623476652166 0.007975963978201722 -0.001173029121699955] %
+
+Mass Used: 100.59230076378844 kg
+Launch C3: 96.17121292962443 km²/s²
+||V∞_in||: 0.0013491257648910052 km/s
diff --git a/archive/ES_0.5670852650645426 b/archive/ES_0.5670852650645426
new file mode 100644
index 0000000..785a117
--- /dev/null
+++ b/archive/ES_0.5670852650645426
@@ -0,0 +1,22 @@
+archive/ES_0.5670852650645426---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T23:54:14.552
+Launch V∞: [6.55794175039751, -7.367393210940256, 0.19555061779473137] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.862718983532724e-9, -7.079182309839274e-12, -7.308904397627785e-9] km/s
+ V∞_out: [-2.633108793039871e-9, 5.806447479993981e-9, 7.423386353646291e-9] km/s
+ time of flight: 1.8749577787501833e8 seconds
+ arrival date: 2029-04-09T02:03:51.552
+ thrust profile: [0.25820389484758005 -0.05638084218404618 -0.08484776317192257; 0.06098028860953643 0.02085969899423013 -0.06508232237957323; 0.05982221364106486 0.038300618083732085 -0.10579096013820641; 0.04151788027343834 0.034515296779104296 -0.10007163067382151; 0.04151687640399183 0.04328441548327039 -0.12848329475988002; 0.0372885716132151 0.04473438828668905 -0.14243768476739768; 0.021945865269758575 0.02939490254940927 -0.10246104740815551; 0.006751697081070493 0.013145520586629697 -0.043078022550868074; 0.011325290281876151 0.016134677041012645 -0.06322502019183032; 0.004139982743742262 0.006104211045472368 -0.02038320036629561; 0.0006211435515187465 -0.005161736938870063 -0.008564375465092935; 0.0009849898647132512 0.0019068856514154893 -0.008397287077221482; -0.001296680879809266 -0.0007096875891464019 0.0019365629132613868; 0.0012573100693695765 -0.0010639684400346801 -0.0045754783858310165; 0.015601725818157395 -0.005456385572926143 0.0010369759344975196; -0.001808191433557879 -0.000692441142252217 -0.004167760939380375; -0.004955811031442726 -0.0038194656977499917 -0.006095577942846289; 0.004282173146599977 0.004172449893252955 0.0014121505339042945; -0.01417830226136918 0.015328946476563413 -0.011639095345771995; -0.006852284369147942 -0.01649423486365803 0.014919615968353648] %
+
+Mass Used: 93.88009308167739 kg
+Launch C3: 97.32332277033524 km²/s²
+||V∞_in||: 1.002581894188327e-8 km/s
diff --git a/archive/ES_0.567092253353665 b/archive/ES_0.567092253353665
new file mode 100644
index 0000000..74bbf76
--- /dev/null
+++ b/archive/ES_0.567092253353665
@@ -0,0 +1,22 @@
+archive/ES_0.567092253353665---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T00:48:42.876
+Launch V∞: [6.436136617443257, -7.58327483217747, -0.05689506696900792] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.941303708960154e-7, -4.150787815264866e-6, 2.591289915187054e-7] km/s
+ V∞_out: [-2.038415789563604e-6, 3.379180477851624e-6, -1.4006077911914034e-6] km/s
+ time of flight: 1.859718353144272e8 seconds
+ arrival date: 2029-03-25T11:39:17.876
+ thrust profile: [0.19334468896067797 -0.05426131869707096 -0.07804237841358841; 0.023645700364298725 0.005434278188032276 -0.030707679372251977; 0.05579978756666364 0.023362147154927675 -0.11555043605391017; 0.04306606023328575 0.02411086945186098 -0.12265426525132236; 0.0227719321393504 0.015084279900610528 -0.08470099359989686; 0.027880256539010065 0.020739536610175094 -0.12609735490784055; 0.011496712759207306 0.00937957229404302 -0.06122868634472229; 0.035097062965475975 0.02935601579293095 -0.19446300231816366; 0.005984468617292811 0.005633819846025274 -0.04025631681216188; 0.004111000535965464 0.004160822979950875 -0.030584859661057586; -0.00098068477028435 0.0013160861053865599 0.0027897977043912937; -6.749535290311102e-5 0.0001489090659800205 0.00017562377271185823; 0.002730403773748648 -0.0030121459742493877 0.0009376873477446434; 0.002125425950525606 -0.0025473363746485924 0.0034695319239242467; 4.015121778876726e-5 0.00030427549499005725 -0.0034291323713674525; 0.00534045810161329 -0.009289763842078429 -0.00667978827682812; -0.0008386110934996119 0.006959899475622669 -0.007796222929944129; -0.003898688658161558 0.002990653339654501 -0.0023622903203460773; 0.0014486645518844577 -0.005565620899852742 0.004835859508068826; -0.006665480272417824 0.00800741445602655 -0.013519726301016086] %
+
+Mass Used: 84.497594319585 kg
+Launch C3: 98.93314878737557 km²/s²
+||V∞_in||: 4.201092503054154e-6 km/s
diff --git a/archive/ES_0.5670923714231744 b/archive/ES_0.5670923714231744
new file mode 100644
index 0000000..d0eebdb
--- /dev/null
+++ b/archive/ES_0.5670923714231744
@@ -0,0 +1,22 @@
+archive/ES_0.5670923714231744---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:09:56.566
+Launch V∞: [7.730056480055061, -5.702864107760551, 0.23292134731027672] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0027911688346187935, -0.0042104634344025125, -0.00012058426820658031] km/s
+ V∞_out: [0.0036286992367418167, 0.0016621192426334193, -0.0030922687314132893] km/s
+ time of flight: 1.8365562940986183e8 seconds
+ arrival date: 2030-03-05T18:37:05.566
+ thrust profile: [0.6389493237894 -0.0034945087968824818 -0.16124073445880033; 0.12291151125069642 0.08000265674881327 -0.10770446225801739; 0.05221800361908882 0.05588051194327924 -0.08326334103012989; 0.05455547998785894 0.08177228667454538 -0.13220052767762797; 0.02459031187079935 0.046347064117288825 -0.08331233860203405; 0.012393525647454379 0.02829888461232118 -0.053054506969414154; 0.017867650762049693 0.051246672787949296 -0.1026933604404602; 0.012398735238596 0.0424834803384832 -0.08939828145659824; -0.00021011383295903145 -0.0004817199837052683 -0.019647797406281763; 0.00012598210952032577 0.0006461424916003821 -0.003984620713905829; -0.0009681740286098437 0.003519633987566365 0.0010690125459953236; 0.00015458788302175796 0.00224397082747615 -0.006973983057691981; 0.014483460888693704 0.004686021059112626 -0.008719143361910223; -0.0007279778940655298 -0.0005215898059653832 0.0004892399725308521; 0.0008702271419252105 -0.013635180306856082 -0.00012093739282375995; -0.008656565505023786 0.012180917933451175 -0.04322712464444209; 0.021465542707876522 0.011347917052299096 -0.015948656631345103; -0.0012822980297996786 0.0017467395127852723 -0.010768452152137615; -0.009286597376438017 0.013733716292082641 -0.008322995755144731; 0.005273166666818313 0.004650964119727867 -0.014625520373873102] %
+
+Mass Used: 123.01210666603401 kg
+Launch C3: 92.33068457045762 km²/s²
+||V∞_in||: 0.005053035361198925 km/s
diff --git a/archive/ES_0.5671153725685684 b/archive/ES_0.5671153725685684
new file mode 100644
index 0000000..1bd92c9
--- /dev/null
+++ b/archive/ES_0.5671153725685684
@@ -0,0 +1,22 @@
+archive/ES_0.5671153725685684---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T10:54:42.989
+Launch V∞: [6.216527408946084, -7.335453427431301, 0.1510720198541591] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.03929036808528e-5, -8.355503944852692e-5, -7.516582078791087e-5] km/s
+ V∞_out: [8.307130925627458e-5, 4.12367244236905e-5, -9.116359454603394e-5] km/s
+ time of flight: 1.829876370747729e8 seconds
+ arrival date: 2029-02-12T08:48:39.989
+ thrust profile: [0.5932520533568361 -0.15395850135305847 -0.1773319822551654; 0.18409429017374151 0.05597963188117004 -0.17263272237329838; 0.06083642643441017 0.036384238324800026 -0.10017202721502062; 0.04147611025493627 0.03380665459276594 -0.09683894673167008; 0.03798111083293263 0.03848537172789301 -0.11272479865864772; 0.030839748632346932 0.036283817269063184 -0.11657633793647317; 0.019552318490629602 0.02349794553185147 -0.07605534848048642; 0.010671495405032379 0.014081778227154057 -0.050394413892404885; 0.00585307357975145 0.009735877345573563 -0.03528505433603812; -0.0005462877648262717 0.000765496204527296 -0.001976338054660378; 0.0016076833969812005 0.0032426112022017227 -0.011732480076570984; 0.007261875789287724 0.014662307000361398 -0.053878729330098823; 0.0009591421266378753 -0.0020786508119433394 -0.008197150512835684; -0.0016464098127356 -0.004175078654223687 -0.0022557902886886604; -0.000749841232447054 0.0022874728574021966 -0.0012369604820779917; -0.004367538193157925 0.0018690734417236075 -0.008444563074566043; -0.002571354745142622 -0.0033239490636013482 0.0039057768614102974; -0.00425639793636415 -0.0046222579673791 -0.005439716041611618; -0.0019392201529175395 0.0063857263610110696 -0.007997055839129972; -0.0013531084382816185 -8.891697291577537e-5 -0.002031045808893751] %
+
+Mass Used: 122.18594352031278 kg
+Launch C3: 92.47691276737434 km²/s²
+||V∞_in||: 0.0001326141248909295 km/s
diff --git a/archive/ES_0.5671158684539195 b/archive/ES_0.5671158684539195
new file mode 100644
index 0000000..853b061
--- /dev/null
+++ b/archive/ES_0.5671158684539195
@@ -0,0 +1,22 @@
+archive/ES_0.5671158684539195---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T16:21:47.005
+Launch V∞: [7.617088816080197, -5.579256769949316, 0.2731632840335654] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7145857715407553e-10, 7.139885003262942e-9, -3.2466067964886973e-9] km/s
+ V∞_out: [4.153412898693045e-9, 8.076398665105535e-9, 2.1223758299167165e-10] km/s
+ time of flight: 1.8749577786993715e8 seconds
+ arrival date: 2030-04-16T18:31:24.005
+ thrust profile: [0.7723004175770494 0.020688942502183744 -0.14559778441724558; 0.2369218405440136 0.16849166154115322 -0.167007302310564; 0.17400322849380662 0.208592829750461 -0.22830977368912228; 0.03307612742268025 0.05547560129068929 -0.07122709297598093; 0.021143103994649855 0.04656763804036403 -0.06206036820263017; 0.020226022052638206 0.04904630274950429 -0.07276552023480823; 0.005982185106408706 0.024703931964017864 -0.03975224334090231; 0.0009457322191460521 0.01152790886323372 -0.01872938617934597; 0.001304565793836 0.01488866703807862 -0.02796044883669408; -0.000253074980868893 0.0048506384190801 -0.009926226431376984; -0.0012783464395481191 -0.0013090892095149037 -0.0031404556041267585; 0.00024365180689149088 -0.00015083257458712684 0.00012220050113290193; -0.0006295811335873959 -0.0006272991452127368 -0.0008491051420639573; 0.0007566527534539591 -0.0009201401561758055 -0.0018932687966909862; -0.0010109014529224134 -0.002501950085664865 0.002258571907850785; -0.003378399868201135 0.0034661408299090503 -0.0019216535785813722; -0.0051412786385614025 -0.002718251092913071 0.002647362433296227; -0.002851135200779946 -0.0006777841319752071 0.002414449508103678; -0.001446084046101016 0.004512243572626581 0.0031596552845018894; 0.0020894858267932756 -0.0019652483972655284 -0.002723180582793586] %
+
+Mass Used: 141.16904301477007 kg
+Launch C3: 89.2227663168233 km²/s²
+||V∞_in||: 7.848063666276936e-9 km/s
diff --git a/archive/ES_0.5671190940362447 b/archive/ES_0.5671190940362447
new file mode 100644
index 0000000..21aff91
--- /dev/null
+++ b/archive/ES_0.5671190940362447
@@ -0,0 +1,22 @@
+archive/ES_0.5671190940362447---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T18:50:59.173
+Launch V∞: [6.449503172970993, -7.512905623418815, 0.13491069872590733] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.364597233303258e-7, -2.8207304336017707e-5, -4.2407035637538497e-7] km/s
+ V∞_out: [1.0180545793849886e-5, -2.270536477197291e-5, 1.3293407918517373e-5] km/s
+ time of flight: 1.7621714756469473e8 seconds
+ arrival date: 2028-11-25T08:03:26.173
+ thrust profile: [0.1892726456691351 -0.06045243760102714 -0.06982879043753674; 0.07801258713346143 0.016079618388172106 -0.0835957182723491; 0.08307136477369675 0.040615904938426435 -0.14710901574625296; 0.06304448737648549 0.042485753504273034 -0.15527833597826207; 0.040961727592733706 0.03352025278179791 -0.12902976535690425; 0.03919396695247677 0.03879875990073643 -0.151024944613865; 0.02477349114504887 0.024953272616311948 -0.10487875766631574; 0.011960444380837465 0.013671421223150059 -0.0607881711923; 0.009528298455884933 0.011981789929536168 -0.05381492634307894; 0.00516286113425802 0.0067832024622454185 -0.03337567653514922; 0.0012710842321397825 0.0012827794408032352 -0.008281642099706108; 0.00041611152625404695 0.0013539528869165132 -0.002128797856583387; 0.0014248915257827593 0.0010733699352023479 0.0004317990989937213; 0.0016316623749225913 0.0039181073412043466 -0.00013557218490958377; -0.0002529182697264503 0.0013468135407469742 -0.00014447009103926494; -0.004765375434120467 -0.0034885140456630756 0.001294795571881658; -0.0046163460608815805 -0.0014104311422412376 0.001409876233356829; -0.0005300362943231848 -0.00035137798219302217 0.00011764988704432693; -0.0002556370026054511 -0.0010386806855599093 0.0043437592858902585; -0.001868519278991915 -0.0013056915735174316 0.004791344597444623] %
+
+Mass Used: 89.63369231866727 kg
+Launch C3: 98.05804298119169 km²/s²
+||V∞_in||: 2.822603072316934e-5 km/s
diff --git a/archive/ES_0.5671191045825708 b/archive/ES_0.5671191045825708
new file mode 100644
index 0000000..43e6992
--- /dev/null
+++ b/archive/ES_0.5671191045825708
@@ -0,0 +1,22 @@
+archive/ES_0.5671191045825708---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T16:54:10.588
+Launch V∞: [5.9171937003421515, -7.690272033922035, 0.01600424725348134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006782953133567025, -0.00021885739735596097, 0.006786505799901292] km/s
+ V∞_out: [-0.009216459997992884, 9.384271915809468e-5, 0.002632447848491869] km/s
+ time of flight: 1.7255335816868922e8 seconds
+ arrival date: 2028-10-14T20:23:28.588
+ thrust profile: [0.4818214822063107 -0.1655050091311038 -0.15922431133232526; 0.12980429002738067 0.024916615133763212 -0.13835575405322564; 0.08347794348056752 0.03632011115458329 -0.14135664910160756; 0.03436799302332654 0.019979598248552395 -0.0858327832932697; 0.03961116593490577 0.02758507336909917 -0.1251298722923161; 0.02357503435630384 0.018964271400472507 -0.08835507471898621; 0.054794675981777424 0.04621704651262992 -0.22512504272406253; 0.008173896855455946 0.007326412129674714 -0.03789480620784869; 0.013074877889167327 0.011750309367667367 -0.06331439004303889; 0.0025333174598771175 0.0025288475699372357 -0.01695771518610725; 0.0008378894417129402 0.00041694579952715623 -0.0054353147228633335; 0.0009144891248398341 0.003363447626005737 -0.013857692717837194; 0.0007722734534351919 0.0006143522522686285 -0.0067249606101489005; 0.00025336502654329135 0.0009837697177711826 -0.0014898598184003428; 0.0009394481309117075 0.0025588600054888503 -0.004096589477250343; -0.0006890721108684886 -0.0005279720694356886 -0.002149170357531806; -0.002332598667169493 0.007578212621871531 0.000280177711652996; -0.006622429476155467 0.006982529003054258 0.00011380790359396577; -0.00022368548405834 0.0012221781515504434 0.00225119212474965; -0.0036574557254295606 -0.003589055490158775 0.003394631482561224] %
+
+Mass Used: 112.40891396870211 kg
+Launch C3: 94.15372137902234 km²/s²
+||V∞_in||: 0.009597552435107506 km/s
diff --git a/archive/ES_0.5671321978160428 b/archive/ES_0.5671321978160428
new file mode 100644
index 0000000..e0d9668
--- /dev/null
+++ b/archive/ES_0.5671321978160428
@@ -0,0 +1,22 @@
+archive/ES_0.5671321978160428---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T15:17:25.144
+Launch V∞: [7.743257752122705, -5.801518218348592, 0.21269694817522986] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00020110352750800446, -0.0003399562918259329, -0.00012675184726760938] km/s
+ V∞_out: [-3.737064953758947e-5, 0.00025223097736226197, -0.0003198586816037251] km/s
+ time of flight: 1.833584948879558e8 seconds
+ arrival date: 2030-03-01T20:12:19.144
+ thrust profile: [0.45643811648295585 0.007082630067643813 -0.09052972944376664; 0.12128958631668674 0.08864455045663854 -0.09604159897342213; 0.1034693529738298 0.12236935285320025 -0.14013591265140762; 0.02947793038748508 0.05373580992776541 -0.0700777192376494; 0.040057862780703085 0.09480620478675501 -0.12828817743599172; 0.03648623336055091 0.10221414383961304 -0.14582358424791195; 0.01317080409466642 0.05549884969530555 -0.07144487094366797; 0.008428005022664657 0.020041927251009464 -0.03281503461875723; 0.004620539883205099 0.008988857303665262 -0.017474162243694354; -0.00045779401738379045 0.010348430860461697 -0.025370208380595363; 0.002102389408822741 0.003182611042092461 -0.0014994282626375592; 0.0024928623044363444 -0.0025812352641249475 -0.0024579237833853708; -0.004583345960211244 0.011755845386676608 -0.006418929112154449; 0.00811635420848331 -0.005690804897128992 0.0016427725155676778; 0.00129034697661013 -0.0052125146240778845 -0.00267753176108828; -0.0035302011007762282 0.001653042029127698 -0.00902697761593553; 0.003495551746391724 -0.011665897554974707 -0.010405207436963663; 0.01202288685087386 0.011340923268283579 -0.000765996821509401; -0.01894833437428127 0.00597567068554479 0.0059286040287211605; 0.0003353121849526432 -0.00307082681840933 -0.000355777602732219] %
+
+Mass Used: 115.29901435387137 kg
+Launch C3: 93.66089424540205 km²/s²
+||V∞_in||: 0.0004148239866665776 km/s
diff --git a/archive/ES_0.5671387898267812 b/archive/ES_0.5671387898267812
new file mode 100644
index 0000000..db25831
--- /dev/null
+++ b/archive/ES_0.5671387898267812
@@ -0,0 +1,22 @@
+archive/ES_0.5671387898267812---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T20:15:52.121
+Launch V∞: [6.254080907359473, -7.277766720363851, 0.2752447990158073] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.652502279644358e-8, 1.6545993928851649e-7, 6.917440065690247e-8] km/s
+ V∞_out: [-6.346750795265968e-8, 1.0097950156005618e-7, -1.5511521463480003e-7] km/s
+ time of flight: 1.8201490238168386e8 seconds
+ arrival date: 2029-01-30T11:57:34.121
+ thrust profile: [0.6595510112734189 -0.18184905014811723 -0.1851438202076422; 0.12452207353823637 0.03778116880429862 -0.10906649709831157; 0.0674997803792699 0.04072774772780149 -0.09969237296584488; 0.07663405913922801 0.06182825599866685 -0.1567844257981134; 0.05300579495133529 0.05382773966664924 -0.13896111599411007; 0.022353817859610943 0.027033963839825936 -0.07486361639685894; 0.013577066687746053 0.017903365221396666 -0.054426038383416114; 0.021545667451444005 0.03403156064770909 -0.09743830646482127; 0.007527302708902249 0.012387377532452995 -0.038892155193884136; 0.005993091559504502 0.010520665137234191 -0.03379527477746733; 9.121356294502028e-5 -1.2711823269263628e-5 -0.0005465552306079193; 0.001018447221205346 0.0005639337310416658 -0.003768136117180167; 0.0014487375602082598 0.0015960354970155407 -0.00025796725079975076; 0.00022428884382104527 -5.38668137813475e-5 -0.003371378151023199; -0.0011787193225270968 -0.00046087199875610653 -0.004293999880619939; 0.004201046562234619 0.0016282513370369433 -0.001699228654589486; -0.0013164107315266124 0.00017642634165957605 -0.003960400950989842; -0.00014014960457314228 -0.0014783656201819723 -0.0019637391871022356; -0.0004075614224575024 0.004725735939389565 -0.0019439605560812824; 0.0014400450330431707 -0.0013134219107214628 0.007420788787652146] %
+
+Mass Used: 124.09006069913312 kg
+Launch C3: 92.15517613121915 km²/s²
+||V∞_in||: 1.9498248210954091e-7 km/s
diff --git a/archive/ES_0.5671455215975704 b/archive/ES_0.5671455215975704
new file mode 100644
index 0000000..b00a870
--- /dev/null
+++ b/archive/ES_0.5671455215975704
@@ -0,0 +1,22 @@
+archive/ES_0.5671455215975704---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T17:33:00.641
+Launch V∞: [6.200738025064156, -7.468863910208111, -0.235879956585387] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.802246990760105e-9, -5.425593232733741e-10, -3.6139393387713117e-9] km/s
+ V∞_out: [-5.763004829130037e-10, 2.857347218601473e-9, 3.990164542134109e-9] km/s
+ time of flight: 1.7761102657364193e8 seconds
+ arrival date: 2028-12-10T09:56:46.641
+ thrust profile: [0.45004556451165345 -0.13048333667899842 -0.13282425704063164; 0.11485889055618212 0.033695888593979866 -0.10192009231396455; 0.08752965520351204 0.05227324971879727 -0.1274940300289389; 0.0773115408718039 0.06370950577369194 -0.1558260235290677; 0.06688435434831845 0.06777387862617 -0.16700158868997497; 0.029765508487758243 0.03468662248590615 -0.09427996272220636; 0.027114835774607028 0.03649343259346419 -0.10033551636758986; 0.0192321033825728 0.02844293823526498 -0.08397071193639394; 0.011005768732751216 0.018583228653183757 -0.05544527844898229; 0.0012706015733333635 0.002464546691723363 -0.007866703293848526; 0.0015539365347464159 0.002442349449159942 -0.008466158900267627; -0.0001764901163711069 -0.00016186898032111616 -0.0005538488396543003; -8.360532754737102e-5 -9.36787621530518e-5 0.00022276293702759597; 2.2030991928841966e-5 -0.00023551155140824924 -8.317299195256713e-5; -0.00027004535064601494 0.0002928546253831062 0.0009195157827454899; -1.405638444949374e-5 -0.0018837008036420894 -0.0012674281336417616; 0.002015681847768334 0.0005905124548326511 0.0005800290428364647; 0.00033692687812521364 0.0004932839428572984 0.00048144812081660486; -0.0016129622999369834 0.0007604871362108236 0.001542313193254968; -0.0007470883143407816 -0.0007486527955513189 0.001212323087790403] %
+
+Mass Used: 111.65224467197277 kg
+Launch C3: 94.28871951860445 km²/s²
+||V∞_in||: 5.273709353228898e-9 km/s
diff --git a/archive/ES_0.5671477069329363 b/archive/ES_0.5671477069329363
new file mode 100644
index 0000000..e169288
--- /dev/null
+++ b/archive/ES_0.5671477069329363
@@ -0,0 +1,22 @@
+archive/ES_0.5671477069329363---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T00:03:04.930
+Launch V∞: [6.399986718332122, -7.414551333009131, 0.18318101602746548] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008985954197416426, -0.00026225451496642314, 0.006151814129313068] km/s
+ V∞_out: [-0.010415502726269692, 0.00011080830173996518, 0.0031702557148221046] km/s
+ time of flight: 1.8040239553820726e8 seconds
+ arrival date: 2029-01-13T23:49:39.930
+ thrust profile: [0.3848953449279677 -0.112484272355872 -0.1289515311817751; 0.048611568221597255 0.011378532534606734 -0.0505997980787076; 0.06778487279739352 0.03411088470244252 -0.1158949804018627; 0.06298073026434367 0.04360801614711874 -0.14861505351408225; 0.03544970493574658 0.02935935894349238 -0.10801012408587046; 0.022006834901451 0.02059535798448368 -0.08137775534716249; 0.011839685206990884 0.012332529481494558 -0.05223524432336921; 0.013341593702639907 0.01239302700564972 -0.05672541795392805; 0.023143067977242176 0.031039350082639302 -0.1284141296493431; 0.01865039052012236 0.0258729941209904 -0.11219088186290538; 0.0010650852695925888 0.001346119362467942 -0.006901211892662153; 3.2683142386370203e-6 -0.0007267281579736089 -0.0011642488768418638; 0.0007584876585824937 0.0021201976107788644 -0.00014932442414441593; -0.0012612694953173644 0.001127729200495847 -0.0020461754594735455; -0.000182054242866718 0.000864513887693595 0.0034146556953642397; 0.0012072238181802118 -0.0005986393352702381 -0.0009462889462556086; -0.0009764307498860666 0.00481654219776172 -0.008939700250505186; -0.0017636492389550308 -0.0018690218534379499 0.002329361176471068; 0.0013077360973883258 0.004734677498251265 -0.00649138606969843; 0.0005534659825541332 -0.00592084415793474 0.008032793914528885] %
+
+Mass Used: 101.85341038424622 kg
+Launch C3: 95.9689567492879 km²/s²
+||V∞_in||: 0.01089316149473155 km/s
diff --git a/archive/ES_0.5671638489803492 b/archive/ES_0.5671638489803492
new file mode 100644
index 0000000..c3bab1a
--- /dev/null
+++ b/archive/ES_0.5671638489803492
@@ -0,0 +1,22 @@
+archive/ES_0.5671638489803492---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T07:57:39.152
+Launch V∞: [8.02799167953936, -6.21945078112879, -0.2480256607518069] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004122530908280575, 0.00277302635222581, 0.00017557330716542666] km/s
+ V∞_out: [-0.003627676612661042, -0.0016563441553418888, 0.0029820496369078846] km/s
+ time of flight: 1.8542558144880286e8 seconds
+ arrival date: 2030-04-06T11:04:00.152
+ thrust profile: [0.01238659047021895 -0.0017041265851715495 -0.005914924751124166; 0.059099857914449445 0.012665934483907047 -0.09631439166233294; 0.019709964460072373 0.006063796376019237 -0.05473801049106226; 0.018300992883413428 0.004820591263157671 -0.06897300961021403; 0.023833677844967382 0.0052983591589800755 -0.11173209431744943; 0.015882020148939947 0.0027452293320211485 -0.0862480265737424; 0.009417068728404872 0.0009751020930700582 -0.05787017336767542; 0.02428708727042855 0.005063480837427333 -0.1625645229032626; 0.0123560966070828 0.00016408092203597441 -0.0870413212022531; 0.000191421431992681 6.65768494336354e-5 -0.0038082841843931495; 0.0021366867324922054 -0.0001441455805661688 -0.016417436906795584; 0.0007513290137278542 0.0002833852540375084 -0.00458137387517342; 0.0006512179297833952 0.0005251273870885459 -0.0013819732108859195; -0.00018871021555624248 2.127141597313046e-6 -0.00047045740246799055; 0.00019501354215182122 2.4747211852259787e-5 -0.0014974800828377176; 0.00030196060106617707 0.00022525477285959667 -0.0005838200254834559; -0.0002766681552028913 2.4525549657394137e-5 -0.0005855899123335777; -0.0006718428585305565 -0.0006689028959147235 -0.0016885477480926537; 0.0003819922481899097 -1.8515067322701933e-5 -0.002282519488836446; 0.0020017328622556826 -0.0031000590571535085 0.0019666382211998555] %
+
+Mass Used: 59.73936874524361 kg
+Launch C3: 103.19173515402808 km²/s²
+||V∞_in||: 0.004971494968925992 km/s
diff --git a/archive/ES_0.5671685144122656 b/archive/ES_0.5671685144122656
new file mode 100644
index 0000000..e17bd86
--- /dev/null
+++ b/archive/ES_0.5671685144122656
@@ -0,0 +1,22 @@
+archive/ES_0.5671685144122656---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T08:01:49.668
+Launch V∞: [6.717728331554777, -7.232012919307759, -0.5832851974513762] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00998264026752094, 0.004749415517848824, -0.01108612351395637] km/s
+ V∞_out: [0.010638198077428097, 0.001961192995178387, 0.011326800786173513] km/s
+ time of flight: 1.8749577784847343e8 seconds
+ arrival date: 2029-04-07T10:11:26.668
+ thrust profile: [0.2605493671889769 -0.06637182368304295 -0.09668047596065123; 0.04864555917846944 0.015840543406325396 -0.05470783830520353; 0.051070169906113745 0.03139695244353855 -0.09549935284261571; 0.05946331547399349 0.0484013957569095 -0.1548363255324499; 0.06658052900024385 0.06141549510449005 -0.2085437656203628; 0.0318341419729632 0.03791525661483708 -0.13371707018212475; 0.012418358867895721 0.017554074438933698 -0.06525586153985102; 0.0027368428892225205 0.004457359137123062 -0.017166466023692335; 0.0019175197128349255 0.0036250497253946107 -0.014728680956744062; 0.001688565429739088 0.002683359048394338 -0.011958326302950548; 0.0066511207272979544 0.016624695237330896 -0.06834394818561113; 0.00045119772736803405 -0.0010069231291814473 -0.00015660912863911004; 4.386073868382787e-5 9.438979449749617e-5 -0.0008125819797465213; 0.0005385996950486254 -0.0008268225618910914 0.0011006997801537074; 0.0005369402334985748 -0.0020920316921727504 0.0017447674778123523; 0.00152444162617253 -0.00021959481258684987 0.0033120808227940835; -0.001733662477436934 -2.5658345540185905e-5 0.0031536635046679083; 0.0010358978374527112 -0.00019085978578248984 -0.0017602152838461773; -0.0005753089705594882 -0.0009568871418912464 0.005493176446368305; 0.00150693859509529 0.0005222208972242274 -0.0004828566993222384] %
+
+Mass Used: 91.37097934579515 kg
+Launch C3: 97.77010642317394 km²/s²
+||V∞_in||: 0.015656059179710906 km/s
diff --git a/archive/ES_0.5671731978572935 b/archive/ES_0.5671731978572935
new file mode 100644
index 0000000..832695a
--- /dev/null
+++ b/archive/ES_0.5671731978572935
@@ -0,0 +1,22 @@
+archive/ES_0.5671731978572935---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T01:55:40.543
+Launch V∞: [7.81261127403475, -5.950960113908177, -0.10625094182127157] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003315694512037243, 0.00952894016746995, 0.021889828951518395] km/s
+ V∞_out: [0.021978411778822864, 0.0027720615157401144, -0.009467134192927735] km/s
+ time of flight: 1.759307466355247e8 seconds
+ arrival date: 2029-12-06T07:34:46.543
+ thrust profile: [0.299052652877751 -0.015463885034983684 -0.09404616627729137; 0.07143132181201568 0.0370065173969515 -0.07585449350046683; 0.0843837970475119 0.07485630961189949 -0.1540307326751797; 0.05880556767838773 0.06732705851933957 -0.1520853562785961; 0.047080413248937254 0.066925416692536 -0.17337024379210697; 0.027009060419531133 0.04583653086357892 -0.12277667712820682; 0.01641936462594679 0.03034965945645758 -0.09250230340251855; 0.005934964259273062 0.006092551068091351 -0.02754108490584231; 0.0015046094956450914 0.007041125380205678 -0.027930198713121964; 0.00010361202351193849 -0.007363741522475625 -0.0043339475627415065; -0.0025883887829461086 -0.003549796561276126 -0.0019456361907808735; -0.015210105948249442 0.005104698226217903 -0.0043263973923345625; -0.0006355015619079797 -0.0003388155760683881 0.004994105466097643; 0.002817812461918409 0.0030724759691167502 -0.0066357377745210125; -0.0014691414573834514 0.006554790562348157 0.007576795688935503; 0.0017360264270435397 0.0006575237888824134 -0.006297879361628131; 0.002124030682934751 -0.0015925087960419475 0.006202519358949346; 0.007054370401387683 0.0263188592597871 0.00492641701239323; 0.0010992881952343865 -0.004176718947854376 0.011112099979640501; -0.006774912317685747 -0.029253393347113462 0.015300315599869198] %
+
+Mass Used: 99.00641982186607 kg
+Launch C3: 96.4621104591388 km²/s²
+||V∞_in||: 0.024103094040788812 km/s
diff --git a/archive/ES_0.5671880727619942 b/archive/ES_0.5671880727619942
new file mode 100644
index 0000000..4e7ea15
--- /dev/null
+++ b/archive/ES_0.5671880727619942
@@ -0,0 +1,22 @@
+archive/ES_0.5671880727619942---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T11:19:08.753
+Launch V∞: [6.342693137715226, -7.6080166095587, -0.06185057301670958] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.423623816949445e-10, -4.047393270920652e-9, -1.4781061372710698e-8] km/s
+ V∞_out: [6.418195697296448e-9, 7.836624956867761e-9, 4.649624371624603e-9] km/s
+ time of flight: 1.7590406869758812e8 seconds
+ arrival date: 2028-11-23T09:33:36.753
+ thrust profile: [0.1776994057659853 -0.061534803325235796 -0.069213670633859; 0.07871292705263527 0.013384054941004525 -0.08626797941530792; 0.07067246325918614 0.028258457510478067 -0.12816977018058304; 0.05467866405807189 0.030169166548374895 -0.13646033412660466; 0.039916737756559496 0.026486039196339982 -0.1263217917942872; 0.0224536395384894 0.017067074768056474 -0.08573857935695858; 0.024108022371244743 0.021026745602911037 -0.10738583290390864; 0.027492050055632867 0.026799139009227632 -0.13484812159758483; 0.007530633255073872 0.007188376516835832 -0.04348077112176105; 0.009924892887529914 0.008589003729330342 -0.058995885501026184; -0.00013965060851288424 0.00014345446672655096 -0.013759960757634835; 0.002334247573894109 -0.0006661841918131025 -0.01030773900307087; 0.004861483606940876 -0.0010243552112901596 -0.00492508941386949; 0.0017982257377687255 0.003091155909512548 -0.013803077368738547; -0.00038775179062920553 0.003436785408843057 -0.00020201268044332983; 0.0028144879575391305 0.003256093599912446 -0.0027287383548283578; -0.003718174632649736 0.0033266778920971784 0.00066464211513881; -0.004009160893558556 -0.00529542473965934 -0.0013576007862219853; 0.0021136925015353583 -0.00125693484597387 0.0029587544803392216; 0.0019096329356523395 0.005521698955352681 0.0026029519001394357] %
+
+Mass Used: 89.37901051610697 kg
+Launch C3: 98.11549846392336 km²/s²
+||V∞_in||: 1.53258420532464e-8 km/s
diff --git a/archive/ES_0.5672044739207753 b/archive/ES_0.5672044739207753
new file mode 100644
index 0000000..2149d20
--- /dev/null
+++ b/archive/ES_0.5672044739207753
@@ -0,0 +1,22 @@
+archive/ES_0.5672044739207753---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T00:19:34.964
+Launch V∞: [5.815422923540786, -7.8484020199687, -0.058155205606493454] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.505908484000098e-7, -1.3239977376792506e-7, -2.2673257673901488e-7] km/s
+ V∞_out: [1.150672017723775e-7, -2.4715001801484886e-7, 2.4056330400978556e-7] km/s
+ time of flight: 1.716930070505837e8 seconds
+ arrival date: 2028-10-06T04:49:41.964
+ thrust profile: [0.367264270098553 -0.12478435086201892 -0.12873169804008938; 0.1302115105200252 0.02296274796110921 -0.13226198488964092; 0.08039878111621655 0.03228744687878514 -0.1328317699250072; 0.06562258593611481 0.03673892192622995 -0.14673538945260844; 0.048204035493893196 0.032259771887201895 -0.13729703468021845; 0.05555062780964137 0.04567679608926835 -0.19100662911167576; 0.037244619570179306 0.0343088507168189 -0.1479360906562541; 0.005494249905520426 0.005368021370137286 -0.025753926253196516; 0.0030169579976449543 0.003356812716008679 -0.01693656571320995; 0.0011245136683809482 0.0023526234595090513 -0.013696483161027572; 0.002518100870960298 -0.0001865064335052327 -0.003541190156379695; 0.0008480504548933797 0.0024052220406641338 -0.004360951255827744; 0.0012945346686402388 -0.00048631010706913524 -0.0013248260785728083; -0.003265832803799315 0.0013536363042167894 -0.001626239847294772; -0.007553389388887476 0.00023999270849234358 -0.0015990223447190635; 0.0061727733987644315 -0.006869630272703419 -0.00100174527794465; 0.0007577120511587875 6.843118968687112e-5 -0.0015302756262683924; 0.0004253086656489741 0.0027414246173570462 -0.005447143958494612; -0.001558577538972207 0.0006946717332097432 0.0019002244331647773; -0.0016742401891619086 -0.003058789065945265 0.007195741675398087] %
+
+Mass Used: 105.12223580555383 kg
+Launch C3: 95.41994007463155 km²/s²
+||V∞_in||: 3.629505954676858e-7 km/s
diff --git a/archive/ES_0.5672214797120587 b/archive/ES_0.5672214797120587
new file mode 100644
index 0000000..c521f26
--- /dev/null
+++ b/archive/ES_0.5672214797120587
@@ -0,0 +1,22 @@
+archive/ES_0.5672214797120587---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T20:15:24.062
+Launch V∞: [6.303743430020732, -7.668101115093078, 0.006010515451184459] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7153716603281063e-8, -1.1605334025586496e-8, 2.3099696322448642e-8] km/s
+ V∞_out: [9.800118912472158e-9, -2.237011959301856e-8, -2.9019820846390685e-8] km/s
+ time of flight: 1.752611227281633e8 seconds
+ arrival date: 2028-11-16T07:54:06.062
+ thrust profile: [0.16832697784830616 -0.05632701319492146 -0.06306152748268336; 0.027749573152335665 0.00424299807480305 -0.03398506733352753; 0.04619502264719313 0.017420701817714167 -0.07468467083195383; 0.057919540816775236 0.03766523812383398 -0.14727007071185652; 0.07368695720987815 0.05856885208715002 -0.2243366763269987; 0.016653180744174316 0.011155008113152657 -0.059711121982691164; 0.04085383306314678 0.032557786638888114 -0.15680447595401076; 0.01607794403578634 0.015215398118535851 -0.07382560190862042; 0.007917186362509493 0.00835061258889943 -0.04307189740685185; 0.010633616357702429 0.010878926464492804 -0.06086505286661526; 0.003428228328022976 0.004037672454193357 -0.022044099714399155; 0.0047901422399279315 0.006348121165337409 -0.03652855919280557; -0.0012665900183417862 -0.00019287515928754812 -0.007123481317704004; 0.0014287571546153623 0.005261623769032739 0.001167742483225263; 0.004715247962848214 0.0024633972579967927 -0.0012364528589702255; 0.00046103842152805567 0.0006598243550832925 -0.002305322572609466; 0.008031900297982581 -0.00111232578856893 -0.0076535605737832755; 0.0047039558677091755 0.003474491816863048 0.001149495334613188; -0.000884791093157594 -8.891148996130233e-5 0.0014747854352000168; -0.00030912655759334634 0.005493552886789696 -0.00203601136008092] %
+
+Mass Used: 86.95927259421796 kg
+Launch C3: 98.53699206911725 km²/s²
+||V∞_in||: 3.7491386656218585e-8 km/s
diff --git a/archive/ES_0.5672431842514416 b/archive/ES_0.5672431842514416
new file mode 100644
index 0000000..1cd5c7a
--- /dev/null
+++ b/archive/ES_0.5672431842514416
@@ -0,0 +1,22 @@
+archive/ES_0.5672431842514416---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T04:27:26.107
+Launch V∞: [6.303003063539015, -7.560823671094732, 0.1671615548460693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2094582879851914e-9, 1.0379818040226402e-9, 8.212917536675083e-9] km/s
+ V∞_out: [-4.452697889166124e-9, -6.851554443747904e-9, -3.5155709244306602e-9] km/s
+ time of flight: 1.7423683784325746e8 seconds
+ arrival date: 2028-11-01T19:34:43.107
+ thrust profile: [0.261333692307659 -0.09163348717430339 -0.08419767576636955; 0.04708559898165769 0.009858234206206922 -0.04965034738680569; 0.12874884714747042 0.05479070067816028 -0.19131128208585213; 0.08386261421366495 0.052354797276305404 -0.1811621151007985; 0.06837494852396443 0.05034285658903121 -0.1825497699996171; 0.026264830807513517 0.023052455670995814 -0.09338434180670006; 0.02559103300510306 0.020285275214979696 -0.08202274227292947; 0.016934388852925992 0.01943919641405159 -0.07926403436367528; 0.015430868505216366 0.016354892667543135 -0.06480344671427989; 0.0005092556066624961 0.0007330687921940209 -0.003290372375077693; 4.289559753160903e-5 0.0019467298693344947 -0.0038894342367972574; -6.32800371584412e-5 0.0004353300497241618 -0.0021802812743490544; 0.0031548474598678353 0.0013734997490762674 -0.0003252616890263636; 0.0024253262824875783 0.005092455214823572 -0.0014740935722562278; -0.0019279226154723618 -0.0030100862238678708 0.0016711539497117854; 0.0013700172848128437 0.0005188257069453587 -0.000948418340693472; -0.0008299961488880986 0.0016328440037547986 0.003147223647333962; 0.0006045738920082129 -0.0010836345935429205 -0.003348140501213041; -0.0019227406728064005 -0.003158233583742251 -0.008930630907934417; -0.0014426861785468874 -0.0001565601589989577 0.004215656099161725] %
+
+Mass Used: 96.40628468625664 kg
+Launch C3: 96.92184518978719 km²/s²
+||V∞_in||: 8.366134713240235e-9 km/s
diff --git a/archive/ES_0.5672474861134541 b/archive/ES_0.5672474861134541
new file mode 100644
index 0000000..0b74c15
--- /dev/null
+++ b/archive/ES_0.5672474861134541
@@ -0,0 +1,22 @@
+archive/ES_0.5672474861134541---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T16:41:31.340
+Launch V∞: [6.38331390846599, -7.498296250530996, 0.17831859141289685] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008501588758735814, 0.0017591668643500147, 0.001527192367308423] km/s
+ V∞_out: [-0.001640864272768613, -0.0007628028557187445, 0.001695592649689432] km/s
+ time of flight: 1.8100622831366137e8 seconds
+ arrival date: 2029-01-21T16:11:59.340
+ thrust profile: [0.24863085597603243 -0.06799494188399594 -0.07586638190442395; 0.09560352984410782 0.028336744283861258 -0.09436091029697202; 0.05500561952097164 0.03161488712352215 -0.09026743176832139; 0.03568580237207411 0.02696716645771116 -0.07994204129364542; 0.06745228587329864 0.06284412055864712 -0.18166151550685608; 0.055789097574581246 0.05922208655803511 -0.17877003273178177; 0.02027254884360326 0.026540502799333232 -0.07195859883652882; 0.007116429397766081 0.010372181976051711 -0.03869689283295299; 0.013494653018249217 0.02071568543190202 -0.07635951010410999; 0.004157166552251311 0.0065573689721615 -0.029122102895211412; 0.0026985937078315312 0.005534917216839141 -0.020233378297187476; 0.000769040520957338 0.0012246578476696602 -0.006397971004595212; -0.004597359966764169 -0.0030125868061207832 -0.002490941918161627; 0.0001629069885250873 0.002007043780588283 -0.0008736758569716013; 2.1267270330514374e-5 -0.003306152958649407 -0.002617557728688415; -0.010446431982633269 0.004818065014774968 -0.00022677985442904561; -0.0020873935437666765 0.0033837300258581495 -0.0006941804655632867; 0.0032776724854830944 0.005950782370570066 -0.00465401210520601; 0.010422607076317736 0.0005476192346844437 0.01005866521157759; -0.008432951202120042 -0.010367714237936754 -0.00478144719125136] %
+
+Mass Used: 95.93824676277791 kg
+Launch C3: 97.00294063478603 km²/s²
+||V∞_in||: 0.0024798698953007194 km/s
diff --git a/archive/ES_0.5672492535601636 b/archive/ES_0.5672492535601636
new file mode 100644
index 0000000..e909cbf
--- /dev/null
+++ b/archive/ES_0.5672492535601636
@@ -0,0 +1,22 @@
+archive/ES_0.5672492535601636---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T10:11:13.986
+Launch V∞: [7.409118464977775, -6.4343414977741045, -0.23636728863685827] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2579275501806772e-8, 1.7299124925512847e-8, -7.280030711962608e-8] km/s
+ V∞_out: [-2.0979356124750083e-8, 6.969213809423789e-8, -1.189937412145027e-8] km/s
+ time of flight: 1.615968937242242e8 seconds
+ arrival date: 2029-06-22T18:12:46.986
+ thrust profile: [0.37801732344425937 -0.0685254747568838 -0.13793197604277116; 0.10581652862083936 0.03521964359417799 -0.12375083691199842; 0.05311391231083973 0.030362729396245396 -0.10649907708438607; 0.03744175224787354 0.028253468224351767 -0.10753139043690006; 0.03245565302682881 0.0275083216086299 -0.12014438342362749; 0.03367690346693412 0.0362929283438987 -0.14239813345631366; 0.02001341684304159 0.022305797578836682 -0.12419118928697168; 0.02664922454509634 0.033736305887096196 -0.14055404194080545; 0.008199752190386437 0.01394660405157808 -0.08100280352933784; 0.0022925179789121857 0.0028034062387655603 -0.015974041045311575; 0.003481458735927532 0.00827885740374075 -0.05046850105912605; 0.0007444424956718047 -0.0002507943944123003 -0.004335862860860287; 0.00010164711797642655 -3.387127644556353e-5 -0.0003810446344148096; -0.00023173115173061271 -0.0006419600966605563 0.0022130535715648085; -0.00012532482322520915 0.0006795139073409361 -0.0012531006074932994; 0.0009667382099907923 -0.0019830404551629925 -0.00013500359319086803; 0.00019863245699200413 0.006169930681145185 0.005804073127916106; 0.0015260529510286993 -0.001461294081562484 -0.006505555862451117; -0.00211575779018714 -0.0010968882457346703 -0.0001818517166637737; 0.0027243487025636723 -0.0014309348926663818 0.0015954545262332478] %
+
+Mass Used: 99.73946662658227 kg
+Launch C3: 96.35165643319006 km²/s²
+||V∞_in||: 7.587741832752836e-8 km/s
diff --git a/archive/ES_0.567251535059237 b/archive/ES_0.567251535059237
new file mode 100644
index 0000000..2e7849e
--- /dev/null
+++ b/archive/ES_0.567251535059237
@@ -0,0 +1,22 @@
+archive/ES_0.567251535059237---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T06:13:00.346
+Launch V∞: [6.000885827794194, -7.334970875838725, 0.48584375606530983] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.015328349591372385, -0.007570318444672166, 0.018327102399814905] km/s
+ V∞_out: [-0.016170985345681267, -0.006769918848994117, -0.017915067166213952] km/s
+ time of flight: 1.8598391869181505e8 seconds
+ arrival date: 2029-03-18T20:24:58.346
+ thrust profile: [0.6976105959770219 -0.1562385285380262 -0.15368935432911487; 0.28316734732130316 0.1029348673423278 -0.19745406566963003; 0.09806346342293848 0.06953590515593884 -0.12527737782030807; 0.0578743054815588 0.05507497176728481 -0.10948098927779894; 0.024318835715217917 0.028851772615501148 -0.06033037920018745; 0.025515776958688872 0.03674722088237096 -0.08128606597458116; 0.016905877926873134 0.032226663082111646 -0.06982008457050318; 0.009958248698462489 0.018760767319567544 -0.04292968584946043; 0.006661436398201078 0.012060917336099295 -0.030383724872757666; 0.015140195081698867 0.03431553005084459 -0.07969674933288849; 0.00023306061567052877 -0.00025821644059800277 -0.0002933309877167186; 0.00027009085412947424 0.0005673651838051467 -0.0014905618012691696; -0.0024485025702091455 -0.0014923751920962488 -0.0026296001154692823; 0.0013695428244630558 -0.0027632354180824434 -0.0014686024478896555; -0.0002571588396251374 0.006145672015152646 -0.0012909606855040308; -0.0004972466418103347 -7.365418812163213e-5 -0.0038679750746293757; -0.00044680631714306474 0.003233722164497049 0.0025431865154860868; -0.00019046026875311266 0.0017767309939472169 -0.0006659988133257311; -0.0008077527723412774 -0.00021602513040346389 0.0018061203509488401; -0.00020075325728275735 -1.9036931025464066e-5 -0.0030773326558343177] %
+
+Mass Used: 136.51070060201118 kg
+Launch C3: 90.04847262293119 km²/s²
+||V∞_in||: 0.025062934882458813 km/s
diff --git a/archive/ES_0.5672628660096307 b/archive/ES_0.5672628660096307
new file mode 100644
index 0000000..1e30606
--- /dev/null
+++ b/archive/ES_0.5672628660096307
@@ -0,0 +1,22 @@
+archive/ES_0.5672628660096307---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T20:13:59.639
+Launch V∞: [8.057746121396907, -5.77846777188363, 0.19961094393233494] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.172432931816913e-6, 0.00011877063358544141, 2.1623565798262666e-6] km/s
+ V∞_out: [0.0001147706918038035, -1.727811913662927e-5, 2.584498882817162e-5] km/s
+ time of flight: 1.8749577787469503e8 seconds
+ arrival date: 2030-04-24T22:23:36.639
+ thrust profile: [0.18868007064427597 -0.0005682719149177954 -0.05848452518952153; 0.057730697471649065 0.02846056291452507 -0.057029245804093395; 0.05826413800420259 0.05294411996192282 -0.11288388310601513; 0.027366322727954792 0.036278072684931745 -0.08404693262135453; 0.027700338750365226 0.03508725635845739 -0.10062384719320612; 0.032280751912510196 0.04625484285084566 -0.14291206895078856; 0.005340986155552468 0.014441378864183818 -0.048402546030297616; 0.005678536993299295 0.011725614881433005 -0.0534367546802813; 0.006368412568160915 0.007367174303020948 -0.05479844159767932; -0.0015031658617182145 0.0013915867795160968 -0.0009546613788259713; 0.000531819376989902 0.0041169964342761866 -0.00452270520680023; -0.0009416667817007328 0.0011107133656359427 -0.008602891924607083; -0.0022040566551300876 -0.0034562553500568334 -0.004650812976847786; 0.015722771262800046 0.020749219403743788 -0.003030247760160606; 0.03383141354817608 0.0256962129258739 -0.047616329727861714; -0.009844382332250151 -0.0010645865664698768 0.0029100646089544975; 0.01460835592169875 0.011587709443368795 -0.007933577595129863; -0.009822467544502469 -0.009999591194728598 -0.030918031661865814; -0.0007003362840527493 0.0076848672552068155 -0.014622636577726309; -0.01176588544138297 -0.0383438048026703 0.015737844067703375] %
+
+Mass Used: 88.05280356485628 kg
+Launch C3: 98.35780687652222 km²/s²
+||V∞_in||: 0.00011890287318101125 km/s
diff --git a/archive/ES_0.5672797001291133 b/archive/ES_0.5672797001291133
new file mode 100644
index 0000000..85e3e2d
--- /dev/null
+++ b/archive/ES_0.5672797001291133
@@ -0,0 +1,22 @@
+archive/ES_0.5672797001291133---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T23:58:41.468
+Launch V∞: [6.097749079619911, -7.549585575188985, 0.19527547088998123] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8302843310783213e-8, -6.106278515315363e-8, -2.5778091113879242e-8] km/s
+ V∞_out: [2.204956377669238e-8, -3.618391867162881e-8, 5.536048564401819e-8] km/s
+ time of flight: 1.7795827011542264e8 seconds
+ arrival date: 2028-12-15T16:49:51.468
+ thrust profile: [0.4576418797902315 -0.11806023947851273 -0.12349314984761318; 0.09488468426923685 0.02793916535426512 -0.08174102604475371; 0.07499113559457068 0.04408661763649011 -0.10483185011953661; 0.06879528355132196 0.05546088516304733 -0.1325496113450395; 0.06830556676478199 0.06908144602026185 -0.1654595839286606; 0.0374567245158458 0.04345794664245438 -0.11187953149774915; 0.048118843392693754 0.06604355433725467 -0.16502355227371648; 0.013654049243355388 0.018661974782402186 -0.054436517273531354; 0.004937158326741398 0.007757747981402394 -0.022216669521670732; -0.0015009748592101752 0.0006811723870034928 -0.010707707435752122; -0.0008154745787764968 0.005605248578906073 -0.008838060418895954; 0.004119809799596122 0.006293703742734462 -0.02001687870896697; 0.0004899138687820364 0.0032201353336273257 -0.0018662209002059445; -0.0036701139551234066 0.0037650917787737676 -0.004831006140224288; -0.005219645561317608 0.0028965272973746807 0.004161858195345396; -0.0003203542985246036 -0.0007801314205159492 -0.001972367179084199; 0.0003885702861213719 -0.002839720438808823 0.0027088836651817114; -0.0010013073652935251 -0.00011275500770227618 0.003578276717494995; -0.008600797578447273 -0.003335526268661584 -0.0034945492588780575; 0.005742329032338899 -0.0003129282018407624 0.0014428254235348903] %
+
+Mass Used: 112.22762437357505 kg
+Launch C3: 94.21691870463837 km²/s²
+||V∞_in||: 7.207096954815028e-8 km/s
diff --git a/archive/ES_0.5672821428116683 b/archive/ES_0.5672821428116683
new file mode 100644
index 0000000..cd0597d
--- /dev/null
+++ b/archive/ES_0.5672821428116683
@@ -0,0 +1,22 @@
+archive/ES_0.5672821428116683---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T02:24:32.332
+Launch V∞: [6.249989718171748, -7.841477336589981, -0.29262003105344425] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005479376775983144, 0.003722721332544434, 0.005678634631846554] km/s
+ V∞_out: [-0.0034864533807669952, -0.006589479076993034, 0.004532865019859938] km/s
+ time of flight: 1.7673124506310138e8 seconds
+ arrival date: 2028-12-07T14:25:17.332
+ thrust profile: [0.07556606074412137 -0.031564938956221276 -0.03725984542094064; 0.03366136257603171 0.0003972073967900845 -0.0486482688159656; 0.04325076464078841 0.005878954758357273 -0.1045096228765024; 0.0485099563330819 0.008774869223897065 -0.16079552022792268; 0.041550926150653866 0.008126134692598245 -0.17295034809934; 0.032330433126788155 0.0063608720810893115 -0.1599251753198976; 0.020357725354423328 0.0038774849548948312 -0.11600234873161858; 0.009364273446708144 0.0016261140529909616 -0.05980287151890272; 0.006744246145241856 0.00115284953338484 -0.046817084488737025; 0.0021389855701399985 0.000658206357033913 -0.017056737136704105; 0.002009300731040587 0.00017409097836482818 -0.013798428460410772; -5.023725715380288e-5 0.0008699487707604837 -0.005462675346475328; -0.0006435854597479198 0.0008418987519846583 -0.004703967460563328; 0.0003548257792001955 -7.613566824609796e-5 -0.002564283512681272; -0.00013168808088286727 0.00057268243838777 -0.0019116691833490822; 0.0013401674106994802 0.00027154642563595373 -0.0012446931317246937; -0.0012097140548265825 0.00047307278307025084 0.002833440278738576; -0.0010385251381153072 -0.0002064842945042858 -0.0007753213097388569; 0.0007532362345845977 -0.005614628384353046 -0.004689057343379756; -0.0011729522357755537 -0.0024333164136930065 0.0045632173898979295] %
+
+Mass Used: 74.78137206314295 kg
+Launch C3: 100.63676478008058 km²/s²
+||V∞_in||: 0.008725200012319023 km/s
diff --git a/archive/ES_0.5672876887603091 b/archive/ES_0.5672876887603091
new file mode 100644
index 0000000..dfd5967
--- /dev/null
+++ b/archive/ES_0.5672876887603091
@@ -0,0 +1,22 @@
+archive/ES_0.5672876887603091---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T19:45:07.276
+Launch V∞: [7.906136120226014, -6.23338356327919, -0.04529302829636021] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.137769012106168e-7, -2.647853049069001e-6, -7.86026392658456e-6] km/s
+ V∞_out: [-7.619961633929552e-6, -8.367092202397642e-7, 3.270073790359652e-6] km/s
+ time of flight: 1.874957778748373e8 seconds
+ arrival date: 2030-04-30T21:54:44.276
+ thrust profile: [0.18697404778451596 -0.01325681039537131 -0.07943262220565504; 0.05547394102412985 0.01791650750288282 -0.08266143210844848; 0.02859213548041886 0.012727630251132332 -0.07471388532332686; 0.02521282863795676 0.012491795109561481 -0.09239942831142009; 0.02076659720492857 0.010349315662176136 -0.09418208283679243; 0.015500703662312543 0.00756227789905466 -0.08457403301105948; 0.019140757805188032 0.008919250223845878 -0.11354376677151723; 0.011724985271777833 0.0049084970977768365 -0.08137728793868358; 0.006282065856910891 0.002353381438002093 -0.046813205664946594; 0.0024999770517731964 0.0009074868492022657 -0.019937892104111152; 0.0007992466334889666 0.00030236844686233556 -0.00684280834535993; -5.659424306857736e-5 0.00013427375943463916 -0.002185862691677484; 0.0002446639723131036 -3.6322582776649023e-7 -0.0012190892227563566; -0.00019076372401930595 -0.00015204946266809526 -0.0007744023649047486; 0.00019447629708969102 -0.00029978472360601255 -2.530090101885506e-5; 0.00025070285260082664 -0.00013551571321881425 -5.164487150588633e-7; 1.9156690564729732e-5 0.0001058834948118712 -0.0007332887806014062; 4.917777173796267e-5 -0.00031183848456171415 -0.0004292630453743132; -0.0003271558562662501 8.396565026005831e-5 -0.0004445346317483556; 0.00032504994017567874 -2.5178858928919412e-5 -0.00019966446840204464] %
+
+Mass Used: 70.5449925550297 kg
+Launch C3: 101.36411045691388 km²/s²
+||V∞_in||: 8.334093088631447e-6 km/s
diff --git a/archive/ES_0.5672886754688101 b/archive/ES_0.5672886754688101
new file mode 100644
index 0000000..aef8d2c
--- /dev/null
+++ b/archive/ES_0.5672886754688101
@@ -0,0 +1,22 @@
+archive/ES_0.5672886754688101---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-06T21:05:49.925
+Launch V∞: [6.5920881631072055, -7.607219652088443, 0.10898177724393508] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.603195191013112e-7, 4.283924405091234e-6, -2.7186951229742116e-7] km/s
+ V∞_out: [1.5499405167831597e-6, -3.5082865467978505e-6, 2.0073400054322833e-6] km/s
+ time of flight: 1.8749577787489066e8 seconds
+ arrival date: 2029-04-14T23:15:26.925
+ thrust profile: [0.07088708667382286 -0.02946324318151698 -0.035545059940204515; 0.04150512476657155 -0.004293754387245869 -0.0683990319282766; 0.04145062492923386 -0.004707084007656232 -0.11715164337527477; 0.030975620496494962 -0.005517319637558026 -0.12001232777832721; 0.01998904020908805 -0.004910784791723394 -0.09417911661518144; 0.023533831262519515 -0.006983514337096894 -0.13065783010677898; 0.012460241366284479 -0.0047842752781239554 -0.07547883686495883; 0.01007679367928848 -0.004588859258451785 -0.06715575543355792; 0.0054420269457838575 -0.002855528044909462 -0.04063627636897165; 0.014170947158829645 -0.008994658191542174 -0.10723245941379123; 6.357259648093704e-5 -0.0001988405422963425 -0.0005140073946488969; -0.0001797756919959335 -0.0002840435673683476 -0.0013506198636164296; -0.0003707608063058224 -0.00016423046899826524 -0.00041506759201395346; -0.00045028308096157663 0.00021994171151532856 -0.0002113525640646794; -0.00011108926405733327 8.930098467904897e-5 -0.0006186538047448554; 0.00036014436961540844 -0.0008849300061740615 -0.0009637440543346862; 0.0005346240399990239 -0.00080445815440301 -0.0022503963781133375; 0.0001290863415847565 -9.444014536258037e-5 -0.0008079440119473443; 0.0002329338021253163 0.00011639823540230125 -0.0010327439339113276; 0.00015810261471241923 -0.0007311842636858754 -0.00016858927663780502] %
+
+Mass Used: 70.70257180403678 kg
+Launch C3: 101.33729421307 km²/s²
+||V∞_in||: 4.328958223838508e-6 km/s
diff --git a/archive/ES_0.56730248422309 b/archive/ES_0.56730248422309
new file mode 100644
index 0000000..51dc352
--- /dev/null
+++ b/archive/ES_0.56730248422309
@@ -0,0 +1,22 @@
+archive/ES_0.56730248422309---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T15:59:11.848
+Launch V∞: [7.884388307458738, -5.6301449985495, 0.08899600742246994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0014910033500487928, 0.001042289388532478, 0.03777522732634516] km/s
+ V∞_out: [-0.03472674132734625, -0.01353900413753425, 0.006398144571755064] km/s
+ time of flight: 1.8749577787493455e8 seconds
+ arrival date: 2030-04-22T18:08:48.848
+ thrust profile: [0.589967540711551 -0.006910271581604019 -0.18623087461238402; 0.04236166842655336 0.023332194777714275 -0.053643693260155174; 0.0397451281614777 0.0360729539918998 -0.08884153303116976; 0.03518337102002671 0.04389550131047149 -0.12227739339692045; 0.024560359007767422 0.036784222325382046 -0.1171286047057198; 0.016997730116144978 0.0282680746980936 -0.09520779502721989; 0.010052078803625825 0.01873865281075739 -0.07518392630892641; 0.006398632489041671 0.011552889085019055 -0.046355908238715285; 0.0048614197323108566 0.014453299398794457 -0.058780705124422336; 0.004059192657077876 0.006259203110701318 -0.033969404056748614; 0.0008100863502755976 -0.004643714637637158 0.0015432675751133077; 0.0008194852501821639 0.006126579120517832 0.0034657476555039327; 0.0010600073861446136 -0.0025324723375311875 0.01056540318971091; 0.003480698499653041 0.0036626071210736685 0.012436327616067826; 0.008572319333291568 0.006174679138096049 0.014705003710628507; -0.008304169134349764 0.022928762733225035 0.013753592110223561; -0.002654156333599379 7.281502861957275e-6 0.0006369188016132836; 0.012133445605079576 0.00042717614124592466 0.006772720345203576; -0.001175137810670363 0.0013567948391134611 -0.0025111556217092407; 0.04797128051348026 -0.013691348149567727 -0.012089993579182907] %
+
+Mass Used: 114.27771172881512 kg
+Launch C3: 93.87003197682114 km²/s²
+||V∞_in||: 0.037819006567020745 km/s
diff --git a/archive/ES_0.5673213170171009 b/archive/ES_0.5673213170171009
new file mode 100644
index 0000000..c724065
--- /dev/null
+++ b/archive/ES_0.5673213170171009
@@ -0,0 +1,22 @@
+archive/ES_0.5673213170171009---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:18:33.709
+Launch V∞: [6.3782177770727015, -7.549509358213114, 0.17902450470615783] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.588799860469848e-7, 3.8376580739637045e-6, -2.344987879264331e-7] km/s
+ V∞_out: [1.5099364147676152e-6, -3.0596544753804027e-6, 1.8583928796503476e-6] km/s
+ time of flight: 1.85321311710738e8 seconds
+ arrival date: 2029-03-16T16:27:04.709
+ thrust profile: [0.25238547642213993 -0.06885180676848239 -0.09145228216260538; 0.05709290602805574 0.013523294743812482 -0.06663544621559113; 0.054275537019039775 0.02555683320605165 -0.10421248310038377; 0.045179362029651074 0.026994033542294186 -0.10987107428450796; 0.0456380836827696 0.034858601206683604 -0.14684326309147414; 0.01932410130394407 0.01846468721650183 -0.08369866786620417; 0.020581671252820812 0.020232369512574157 -0.10683533019959307; 0.021780205064758328 0.021525907962695025 -0.11468918196460812; 0.007242783907932102 0.005146583780244496 -0.04683203526894063; 0.0034544155811019064 0.002338910050457782 -0.02676192515668912; -0.00045715167199436926 0.0016259689912194624 -0.00788726571847259; -0.0003358588592396333 -0.001111288742435105 -0.0011466887817907243; -0.0048815959018109895 0.005252347303438414 -0.0009713739856093487; -0.00499271389226885 -0.000619989773331758 0.0024084522842948678; 0.0012501004694636065 0.0005739230210273683 -0.0057295830143380185; 0.0032273185310638204 0.005278372389383041 0.004693769817063125; -0.0016494809659070892 -0.01102941386840536 -0.003035341648833535; -0.011521230631638405 0.0008420284600720708 0.008054764964192565; 0.0019515303310222243 0.0004638312248596975 -0.002017554324147833; 0.010221563503286428 0.020420886102753513 0.0038523861854038183] %
+
+Mass Used: 91.90685040029075 kg
+Launch C3: 97.7088033347989 km²/s²
+||V∞_in||: 3.885222775208863e-6 km/s
diff --git a/archive/ES_0.567323009755076 b/archive/ES_0.567323009755076
new file mode 100644
index 0000000..863810c
--- /dev/null
+++ b/archive/ES_0.567323009755076
@@ -0,0 +1,22 @@
+archive/ES_0.567323009755076---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T16:48:53.518
+Launch V∞: [8.027752355477402, -6.098304570853546, 0.03951754549482684] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.260979513666427e-6, 0.00021387872164521646, 3.792846761657876e-6] km/s
+ V∞_out: [0.00020633041809620513, -3.208036907536587e-5, 4.7305823989720885e-5] km/s
+ time of flight: 1.8749577787488076e8 seconds
+ arrival date: 2030-04-29T18:58:30.518
+ thrust profile: [0.06602158266873896 -0.005004903322536913 -0.029974568846601; 0.10062829715998216 0.03489514857965239 -0.15104419146906267; 0.024163401195332796 0.011802064502253885 -0.06572699958346241; 0.021826086488827712 0.012006661699636007 -0.08376174367214133; 0.01499156804417752 0.008682351774830281 -0.07401898804162156; 0.009227777423306398 0.005019816231400206 -0.0515020129641593; 0.007277913521350879 0.003945216920156869 -0.04607964549324579; 0.029723334422215555 0.014102778034841586 -0.19580889294202536; 0.0029343383498411806 0.0017045213059186123 -0.024636463003028238; 0.006866607407370275 0.003124107337989374 -0.05692791941180389; 0.0037187487687346497 6.178447473597955e-5 -0.0012710974903991056; -0.0026065690250338435 -0.0012287143462797736 0.0005665808949910458; 0.0005090309183079572 -0.0016984566005112754 0.003371036944361817; 0.001802549935833214 -0.00044654677403194436 0.0024811725586921457; -0.0026458436638259965 -0.0019374462807729077 -0.0010860667927154815; -0.009197673888824566 0.001978466087107954 0.0032689684079135134; 0.006238505902402494 -0.0039685347937188625 -0.0006525148829210493; 0.004813270420938887 -0.002448012706698456 0.00024169819187957217; 0.00885702558148697 -0.0022067225785800493 -0.004547620360251699; 0.0005431957986990609 -0.00024363821572243413 0.0017656148068787025] %
+
+Mass Used: 69.00199713660777 kg
+Launch C3: 101.63568815616816 km²/s²
+||V∞_in||: 0.00021411272498546635 km/s
diff --git a/archive/ES_0.5673272210645528 b/archive/ES_0.5673272210645528
new file mode 100644
index 0000000..26cf879
--- /dev/null
+++ b/archive/ES_0.5673272210645528
@@ -0,0 +1,22 @@
+archive/ES_0.5673272210645528---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T03:51:29.358
+Launch V∞: [8.113031495184002, -6.005027820817126, -0.222580268013907] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0776192256215194e-6, 1.620539267504504e-6, 1.513745883253779e-7] km/s
+ V∞_out: [-1.211830195243672e-7, 8.132907929533018e-7, 1.7675353138660407e-6] km/s
+ time of flight: 1.874957778154782e8 seconds
+ arrival date: 2030-04-29T06:01:06.358
+ thrust profile: [0.05595079853054296 -0.0038835247002675486 -0.02376179159931583; 0.01772245880617805 0.009031375495758059 -0.025610035820047162; 0.030104713011074865 0.015318149114424189 -0.07567115238689119; 0.03277951879420967 0.019020053999902156 -0.12001736362373248; 0.02093320371414628 0.01276237344687449 -0.09892897802116425; 0.015577620406058963 0.01055429769468685 -0.09000610254174002; 0.00983957532897567 0.0062639218750096745 -0.06105365682307981; 0.009119416744755977 0.005542100825780638 -0.06306923007267938; 0.011444995040967389 0.006993425734000475 -0.08687534921429958; 0.004456410378487262 0.002988015375195929 -0.03554186208578954; 0.008305989585906962 0.0020596032909319995 -0.037844757480295844; 0.000920387879501685 0.00038870538992997767 -0.005227803665687642; 0.0014928127904478361 0.0004946832835785001 -0.006953361260340338; -0.0012090640946087747 -0.011533016163390492 0.0036592606351048395; -0.0004800225981187712 -0.001681383957669953 -0.005608966668802418; -0.0027008591940250112 -0.0003887876020048117 -0.012188666233992838; 0.003154307566221687 0.0022253658085644463 -0.0054782125485179365; 0.025504487546677786 0.003786230754264786 -0.027702788070773005; 0.012609950627276 -0.002050440670464736 -0.020470502704848452; -0.0011140150690578362 0.0039051428745613924 -0.0026347204975212804] %
+
+Mass Used: 67.28320122163586 kg
+Launch C3: 101.9311811463444 km²/s²
+||V∞_in||: 1.952005373697479e-6 km/s
diff --git a/archive/ES_0.5673307550458531 b/archive/ES_0.5673307550458531
new file mode 100644
index 0000000..add46e6
--- /dev/null
+++ b/archive/ES_0.5673307550458531
@@ -0,0 +1,22 @@
+archive/ES_0.5673307550458531---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T01:10:44.921
+Launch V∞: [6.298014843918789, -7.385158936752695, 0.10650261582593505] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9930487283258713e-7, -4.514261392485363e-8, 5.6420227377871954e-8] km/s
+ V∞_out: [-2.098079700700269e-7, 1.901306390858977e-8, -2.5485206630897386e-8] km/s
+ time of flight: 1.8536691258635688e8 seconds
+ arrival date: 2029-03-12T11:59:16.921
+ thrust profile: [0.4110120184277321 -0.0882618317000046 -0.1047874180837093; 0.12420725307613058 0.04578804259457569 -0.09649715932310649; 0.11169947269180051 0.07675286169668302 -0.14238017467301003; 0.05153176882355954 0.04857932800192528 -0.09384621664092246; 0.04881700733867688 0.05726834890578097 -0.1148400168678224; 0.05730772383268685 0.07928543315302924 -0.16276314901577082; 0.0425051168357054 0.06773775815446179 -0.1450697989429099; 0.006754373416861241 0.003327053813727054 -0.005683719547425354; 0.011245220916446511 -0.00017773067895336 -0.008592805435132408; 0.0012411255048975006 -0.007975192935294563 -0.012545188861254004; 0.0001226345084949295 0.001124142248953228 -0.0006482252138918352; 0.0029594657168732124 0.0037054439600313254 -0.008507035114938943; 0.0005358216560217566 0.001772190640740059 -0.0036767861049762838; -0.00012352227070441943 0.0014182518153455653 -0.002599551723668438; 0.0067701993046997665 0.013448898023183801 -0.0273765646756971; 0.0002394268723514496 0.0009107081794633501 -0.0009677604747204363; 0.005933738024017113 -0.0021103133394236424 -0.0031133801103515606; -0.0010049936017840493 -0.0029113020874252083 -0.004627185318009296; 0.003758181457472073 0.0008537047396959102 -0.003125341887592141; 0.005650263787070189 -0.0008536468295620374 -0.008753474141634106] %
+
+Mass Used: 112.28726078892714 kg
+Launch C3: 94.21690630249738 km²/s²
+||V∞_in||: 2.1199889146916048e-7 km/s
diff --git a/archive/ES_0.56734285119728 b/archive/ES_0.56734285119728
new file mode 100644
index 0000000..dacc115
--- /dev/null
+++ b/archive/ES_0.56734285119728
@@ -0,0 +1,22 @@
+archive/ES_0.56734285119728---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T20:51:06.488
+Launch V∞: [6.027868954839484, -7.590427266910793, 0.0068064317111388006] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000542675545620921, -0.006316513415615988, 0.004797645376406423] km/s
+ V∞_out: [-0.005392460862644162, -0.004523969413654738, -0.0036901981025355603] km/s
+ time of flight: 1.7655214200609928e8 seconds
+ arrival date: 2028-11-29T07:06:48.488
+ thrust profile: [0.43048177672020965 -0.12835008910380158 -0.12702157044937576; 0.1160102059674752 0.029215760131441643 -0.10225876535791888; 0.11079828001186173 0.05908542660776365 -0.15868936763829528; 0.13184318460036046 0.09762432863806854 -0.2510036634488428; 0.04779534429817291 0.042540324420519464 -0.12234529277996996; 0.04398330730197999 0.04590415406753981 -0.1357948955479145; 0.01165088952725101 0.012122505862344743 -0.03987322979088632; 0.011934855881092409 0.01452693719043718 -0.04785023631827008; 0.005559109124538212 0.0028912002119685244 -0.015443952425837685; 0.003666839338991922 -0.001085299592151959 -0.009458005897801238; 0.0028424078325692804 0.007892780210807804 -0.009155779302743255; 0.00013308189427607665 0.00011781774848427726 -0.0016629540533081495; 0.00045866612135923336 0.003402844485868455 -0.005293159441966756; 0.00017644479871556547 0.0027265910519941724 -0.0038519378515065573; 0.002724772421988447 0.0032291472483714713 -0.0034946657615982013; 0.004605784086636804 0.012832491137689446 -0.012724369190146773; 0.0008956806700593597 0.0007721702394713053 0.0051083097775015875; -0.010768668270789003 0.010382259738677251 0.000521353196944881; -0.00029647660363724473 -0.0003039652955747771 -0.0017610190495009129; -0.0077868253343341375 -0.009551313153498903 -0.0003267206218751837] %
+
+Mass Used: 113.85927980561655 kg
+Launch C3: 93.94983655849315 km²/s²
+||V∞_in||: 0.007950486754609786 km/s
diff --git a/archive/ES_0.5673504346227108 b/archive/ES_0.5673504346227108
new file mode 100644
index 0000000..8916846
--- /dev/null
+++ b/archive/ES_0.5673504346227108
@@ -0,0 +1,22 @@
+archive/ES_0.5673504346227108---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T16:12:08.030
+Launch V∞: [6.42178945983223, -7.329425556879817, 0.1174091625341899] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.046673192289896e-9, -1.7404440437771462e-9, 3.718969630731589e-9] km/s
+ V∞_out: [1.1224901347568515e-9, -2.6235641364461953e-9, -3.55586863456225e-9] km/s
+ time of flight: 1.8583266936911464e8 seconds
+ arrival date: 2029-03-17T12:23:17.030
+ thrust profile: [0.30882337432023294 -0.07006043024773982 -0.08811423631217188; 0.22004923111421884 0.07487405791165183 -0.18273418456746976; 0.1287028485425464 0.0843102000809608 -0.1821422540048859; 0.04854582826739305 0.04333094512367624 -0.10429085888407248; 0.05388278385319898 0.06046270583185206 -0.14656888397977702; 0.034207078893831226 0.046352752237508045 -0.1254866318687905; 0.011116954379072412 0.017196366991197715 -0.04872102018058863; 0.0069061063758872245 0.010998281819226819 -0.037895535946586255; 0.000793641061439306 0.0021418833496104125 -0.012016138027809806; -0.0018010849257929333 0.0014899934175762928 -0.002097063516810318; 0.0030788156889279897 0.0010040327157453178 0.001475175973481658; 0.0004512514295540307 0.0035763854856036637 0.0013339395480665506; -0.000576243953733909 -0.0008169836372357714 0.0038516834822110643; -0.0015048564210666377 -0.00044017437178908253 0.0013259467882048152; -0.0028707344746725784 -0.000913927990012475 -0.003433992059681142; 0.00019691127662595313 0.0005387674754334711 -0.0026724627210959837; 0.0004215461784731327 7.45460601475163e-5 -0.002278186798531852; -0.004396987471851681 -0.0016378853586408411 0.009892631510895263; -0.006280307481064346 0.011568367532501813 0.003949214449220706; -0.006933117647511066 -0.007588825149558692 0.0034117643766255097] %
+
+Mass Used: 107.89591839156583 kg
+Launch C3: 94.97364377170231 km²/s²
+||V∞_in||: 5.765019038044965e-9 km/s
diff --git a/archive/ES_0.5673596059613244 b/archive/ES_0.5673596059613244
new file mode 100644
index 0000000..29dda01
--- /dev/null
+++ b/archive/ES_0.5673596059613244
@@ -0,0 +1,22 @@
+archive/ES_0.5673596059613244---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T03:26:23.143
+Launch V∞: [6.011940847365822, -7.797195348891089, -0.03950923633916346] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.9174706522788113e-7, -1.961590172121235e-7, -3.4109774889579535e-7] km/s
+ V∞_out: [2.69291684204931e-7, -3.376054878899746e-7, 3.4915122494693055e-7] km/s
+ time of flight: 1.6967121500696588e8 seconds
+ arrival date: 2028-09-11T22:19:58.143
+ thrust profile: [0.2722421181311501 -0.10722118479515583 -0.10629337436069215; 0.08422635590498233 0.009915106834756182 -0.09581074359576153; 0.08129512159909649 0.02621767540673193 -0.16072327896311722; 0.05619456548524841 0.0238068058811783 -0.1473039788095569; 0.046704327322234215 0.02443786806688787 -0.16056603680825118; 0.04752936498283295 0.02976251157045654 -0.16749180550591883; 0.029160600099699483 0.02328268913534531 -0.131360113110877; 0.012416423294748869 0.010210661903766668 -0.06854354790903278; 0.006893002338445741 0.0053960163317042405 -0.037795587305389115; 0.003008920497117692 0.0016331426660217312 -0.012693883717727127; 0.002597017542768813 -0.0012139028802053858 0.00014560913246488552; 0.002566959052682294 -0.0033486479453934508 0.0012865722258139094; 0.00060541192117719 -0.00010590333108474449 -0.002539432719797256; -1.5964007137614974e-5 0.0012068258065817095 -0.0009370803679505098; 0.004340255981460851 -0.002352522776644746 -0.0035737360535650024; -0.0018662772094338003 -0.00047788585411933965 -0.003991128149613677; 0.0031364959692177304 -0.0005371219642430617 0.0024744849338928796; 0.002803373370082925 -0.0013289061208102723 0.007575329917945038; -0.004151980316261893 0.0030483405756143614 -0.0015878067244421358; -3.525422436040718e-5 -0.000680990506881942 -0.0023776019530765617] %
+
+Mass Used: 96.42892088383314 kg
+Launch C3: 96.94124904075062 km²/s²
+||V∞_in||: 5.552403060388025e-7 km/s
diff --git a/archive/ES_0.567367660415866 b/archive/ES_0.567367660415866
new file mode 100644
index 0000000..55ce4fc
--- /dev/null
+++ b/archive/ES_0.567367660415866
@@ -0,0 +1,22 @@
+archive/ES_0.567367660415866---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T23:25:14.314
+Launch V∞: [6.212353893062356, -7.625792388428856, 0.22997001301476463] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.17770586991781e-7, 8.058336087631978e-7, -4.770094207087845e-8] km/s
+ V∞_out: [2.529730360651024e-7, -5.870142666552158e-7, 3.365292889282369e-7] km/s
+ time of flight: 1.7562593328444865e8 seconds
+ arrival date: 2028-11-19T16:24:07.314
+ thrust profile: [0.24071113042367578 -0.07936290839765439 -0.08488263949595222; 0.1091372099738696 0.0215828440067603 -0.11353358137631471; 0.13554203524256508 0.06011696336455055 -0.22066191305323876; 0.03755985091827349 0.02294116141875109 -0.09496179386253996; 0.03713130040164549 0.02835803541261544 -0.11794896587952877; 0.03953126787634107 0.0346663157524989 -0.1462118463555023; 0.026698021506004248 0.02832095403163545 -0.12170036316480815; 0.010596019209099531 0.010005465320776227 -0.05020553666145993; 0.008454212411456453 0.010049141195898162 -0.04972464043030901; 0.00023849201501380908 0.000575664808216666 -0.0029732852425141073; -0.0005154946100031745 0.0007771253640403205 -0.0042855886460845954; 0.00014022860086968392 0.00045037302542396134 -0.005478923394626244; -0.000996533837936589 0.0024358587101234773 -0.0009792592310063995; -0.0012797083120769123 -0.003096324936803957 -0.00418169483253769; -0.00016675103902706584 0.0012129848108144354 -0.003708903849290305; 0.0021067983617661604 -0.0018599396076427663 0.004590967268668944; 0.005374881751617927 0.005300570954310109 -0.005026849209492156; -0.007635689287305555 0.008466700252421012 -0.0015920413145680437; 0.002164415572150364 0.004982964810663032 -0.021996638016633006; -0.0025281100756669363 0.0006901085857185447 0.006256777445817368] %
+
+Mass Used: 97.26847335462071 kg
+Launch C3: 96.7989366509525 km²/s²
+||V∞_in||: 8.157898602257548e-7 km/s
diff --git a/archive/ES_0.5673676947884623 b/archive/ES_0.5673676947884623
new file mode 100644
index 0000000..b06b8c7
--- /dev/null
+++ b/archive/ES_0.5673676947884623
@@ -0,0 +1,22 @@
+archive/ES_0.5673676947884623---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T21:27:03.229
+Launch V∞: [6.0984008100361065, -7.730697915215539, -0.16778185618009223] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007396647857785672, -0.0034564297113678587, 0.008790123419383938] km/s
+ V∞_out: [-0.007480865216669544, -0.0037225142989664537, -0.008600515960512855] km/s
+ time of flight: 1.6989607705069962e8 seconds
+ arrival date: 2028-09-13T06:48:20.229
+ thrust profile: [0.24091990606898905 -0.0924477574424297 -0.0946388906526217; 0.121780740195403 0.017601896270054294 -0.13413125488609054; 0.05875334187495483 0.022324304729476555 -0.10814060653655944; 0.10310809732721025 0.05483927013087366 -0.2451925609392618; 0.03981805851286227 0.02617093651137724 -0.12639444057117313; 0.038076968360283785 0.02884735322715325 -0.1439659680468842; 0.01729357135798764 0.015090244127529058 -0.08043458732910427; 0.009042012149654404 0.008217861347432132 -0.04644704811592952; 0.0176808672395855 0.017441824648433416 -0.09941217898278398; 0.002978315239706522 0.0028890096370609904 -0.018531581285391424; -5.380065476056966e-5 -1.5309281956865162e-5 0.00028917135845672563; 0.00040194787285228735 0.0003882536261182797 -0.003290521413620137; -0.00040950808794110464 -0.0006190790733851476 0.003358725907955218; 0.0001231891391035025 0.00016498592605987574 0.0018492080352694668; -0.0005501247845536214 0.0011775450609185594 -0.002011729686024827; 8.482313498091525e-5 0.0007355995836300432 0.0010050937725250243; 0.0026097627618611283 -0.004081084164698419 1.217700637421576e-5; 0.0003454791168501593 -0.0002750202355881359 0.0006107540603094014; -0.00025397285072256465 -0.001577780167923427 0.006269074127775041; 0.002924712015317437 0.0018474910280182632 -0.0018200105075038683] %
+
+Mass Used: 96.19869880986334 kg
+Launch C3: 96.98233344743016 km²/s²
+||V∞_in||: 0.011996815227789158 km/s
diff --git a/archive/ES_0.5673731890501471 b/archive/ES_0.5673731890501471
new file mode 100644
index 0000000..a9f7c27
--- /dev/null
+++ b/archive/ES_0.5673731890501471
@@ -0,0 +1,22 @@
+archive/ES_0.5673731890501471---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T09:24:38.458
+Launch V∞: [7.465324624637224, -6.691091079213584, -0.45615903932009544] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00021632111653749935, 0.014569429578493677, -5.4807929498814755e-5] km/s
+ V∞_out: [0.014047705042517906, -0.002309161840245524, 0.0031030712871613023] km/s
+ time of flight: 1.6243080094534135e8 seconds
+ arrival date: 2029-07-06T09:04:38.458
+ thrust profile: [0.06631275540781674 -0.016059488780413248 -0.03147088920765596; 0.03178495021685928 0.00586508038083818 -0.0444458787190442; 0.12752755087268947 0.0443756596327669 -0.2888026810148484; 0.05241385520339761 0.02246340504299668 -0.17197755126623693; 0.04495682383084412 0.021110563514019368 -0.18573615073459823; 0.028578387940976516 0.013996654288231611 -0.14188068309712398; 0.008482415852486587 0.0041876680480955 -0.04916545955197752; 0.0033576867941438803 0.0017060951697949849 -0.023031835199614957; 0.004359208278533395 0.002133786391900023 -0.03140098172694475; 0.00809917916034753 0.0039148654270878885 -0.06058736412381338; -0.00032175248794912616 -0.00011929336223655097 -3.9606255238425095e-5; 0.0001086209108870145 0.00019578977998128012 -0.0013478968220509537; -6.606359511671366e-5 -2.7714533596203616e-5 -0.00010221439067824105; 0.0022712583842048563 -0.001111052159343204 2.7216706684102775e-5; 0.001115586562335145 0.0004839646746418479 0.00024166720539208587; 0.000718585295338563 0.0009379596291300238 -0.0042340856125589145; -0.00018986552936316414 -0.00012290634255381343 0.0018888459325285423; -0.0013782566554272832 -0.0007547083377789788 -0.0008878965187948311; 0.0003507009126667908 0.0018073387282519118 0.0012808768294226866; -0.0004470922840726205 -0.0009077103894383105 -0.0004714237346641559] %
+
+Mass Used: 74.46124676275531 kg
+Launch C3: 100.70985265069994 km²/s²
+||V∞_in||: 0.014571138492831726 km/s
diff --git a/archive/ES_0.5673825142663635 b/archive/ES_0.5673825142663635
new file mode 100644
index 0000000..adf8606
--- /dev/null
+++ b/archive/ES_0.5673825142663635
@@ -0,0 +1,22 @@
+archive/ES_0.5673825142663635---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T19:24:42.682
+Launch V∞: [6.322037570048165, -7.29062884387013, 0.2970305326866288] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.18986311501147e-8, 6.015745743048215e-8, 3.405995115716117e-8] km/s
+ V∞_out: [-2.014292650179142e-8, 3.188435157427074e-8, -6.677454816893477e-8] km/s
+ time of flight: 1.822051596705384e8 seconds
+ arrival date: 2029-02-02T15:57:21.682
+ thrust profile: [0.6323594806722427 -0.16984457509535766 -0.1798218921111293; 0.07187965928535565 0.02202695788877414 -0.06859683031061628; 0.040266357246889095 0.02397819726413458 -0.06404220130576692; 0.032663606255623895 0.026508525177696005 -0.07291590341844666; 0.03444529617620531 0.034583969491571796 -0.09749911937793859; 0.030303565604535697 0.03647820869118532 -0.10689101101760316; 0.01746279150859931 0.023912377228445667 -0.07202104247308515; 0.04410284665622936 0.0677892019524385 -0.18992903263559494; 0.01863400104773878 0.030780930601451924 -0.09765948292128451; 0.003903540206563818 0.006287539086171132 -0.029526952717513967; 0.00033516291061634726 0.002001863900492243 -0.0020862091123996715; 0.0014809779383763138 0.0007954780520485205 -0.007605684112278399; 0.0002836512161052548 4.36773525080663e-5 -0.001201111107901097; -0.00010228932158433835 -0.00034413681565298644 0.0013240320404416155; 0.0013306915073856927 -0.0013176685805718952 -0.0015794343390019248; -2.810975796387169e-5 2.6794063649824358e-5 -0.0012068365296409138; 0.0008646024674534625 -8.03685790118332e-5 -0.0012059855142601702; 0.006409210790507623 -0.0017682648961966983 0.00184901059878163; -0.00833368272704476 -0.0006145702701136585 0.0016266310732539356; -0.005074489104340564 0.0004827669937069209 0.0040451883812614425] %
+
+Mass Used: 118.22327848189252 kg
+Launch C3: 93.20965511351972 km²/s²
+||V∞_in||: 7.613489756070828e-8 km/s
diff --git a/archive/ES_0.5673904625338075 b/archive/ES_0.5673904625338075
new file mode 100644
index 0000000..8d5ab6d
--- /dev/null
+++ b/archive/ES_0.5673904625338075
@@ -0,0 +1,22 @@
+archive/ES_0.5673904625338075---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T13:52:58.764
+Launch V∞: [6.1205114366263675, -7.547101842347774, -0.13472712906307935] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.556912964930178e-6, -2.965281938027109e-5, 1.8410866063541567e-6] km/s
+ V∞_out: [-7.743685978772734e-6, 2.7273321047885862e-5, -9.960588260652861e-6] km/s
+ time of flight: 1.816171105052844e8 seconds
+ arrival date: 2029-01-29T15:04:48.764
+ thrust profile: [0.4377766340978168 -0.11501539891718209 -0.13925696887268876; 0.11308294345105933 0.03207535537214902 -0.10849034473196661; 0.09053825674547673 0.05114675246580514 -0.14343763010159177; 0.042708715827337144 0.03334879952351094 -0.09619317898521096; 0.05130837012791939 0.04864482744108521 -0.14611768366321762; 0.03839867227143067 0.04190691474780994 -0.13297186362464575; 0.021392732966505658 0.02684432573904214 -0.08717599890384824; 0.008308766078842332 0.014808334344187752 -0.04901844199607145; 0.0070987482622923955 0.010366475445081931 -0.04166992096240681; 0.002554559776416015 0.004549997045279339 -0.01649576081016532; 0.0019431035613703333 0.003793803634272658 -0.013839042934450973; -0.0007219780851425819 0.0019453077524512578 -0.001667696899177385; -0.00036061890547985824 -0.0016252348844904172 -0.0053534894351000605; 0.004754681597336849 -0.002014707673421677 -0.0029340051588379384; 0.002627550625681465 0.0011756425032806782 0.0009451639741419101; -0.00016267172575163086 -0.01025760224936275 -0.023821440650659477; 0.0005994760344663712 0.0005844016669033253 -0.004344523606961826; -0.0004820190480030802 0.01582488557998915 0.004555283593487478; 9.064661626480665e-5 0.0007420794081582551 -0.00031521158418849893; -0.00257555121393161 -0.010165124152911039 0.019404907763402146] %
+
+Mass Used: 111.06978541640683 kg
+Launch C3: 94.43755786394891 km²/s²
+||V∞_in||: 3.0057357715890895e-5 km/s
diff --git a/archive/ES_0.5673905791837486 b/archive/ES_0.5673905791837486
new file mode 100644
index 0000000..e0dc75f
--- /dev/null
+++ b/archive/ES_0.5673905791837486
@@ -0,0 +1,22 @@
+archive/ES_0.5673905791837486---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T00:28:56.386
+Launch V∞: [7.577131813375037, -6.307826842462885, -0.20554727260622932] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.20564618693145e-6, 3.1904561230259226e-6, -1.562404569751679e-6] km/s
+ V∞_out: [-1.967765980647866e-6, -3.459811445430792e-6, 2.3461519894952334e-6] km/s
+ time of flight: 1.6556050136270338e8 seconds
+ arrival date: 2029-08-08T05:30:37.386
+ thrust profile: [0.28319743538731906 -0.049255493638756094 -0.10864173090408089; 0.056981529072739685 0.018975575244179813 -0.06824675635713474; 0.07376159416672444 0.04311650206587768 -0.14795019954926422; 0.06585663469441254 0.0499698658783447 -0.18583787801344168; 0.047470247397837194 0.042521760497730064 -0.1733170295749519; 0.01874828165277533 0.01903720590094039 -0.08601994464714754; 0.024698564928301033 0.02724126766577378 -0.13007832818988374; 0.017173486790246946 0.020455734705070353 -0.1040568761517027; 0.00180470937819913 0.0029446212476095875 -0.010524017693713998; 0.007190606326413047 0.009549562769592538 -0.05357050927381531; 0.0038131669548121068 0.004268972112147641 4.51635484148543e-5; -0.0013738270260209428 -0.006567851453401724 -0.0022033288567986893; -0.0013051841232873094 -0.004916201899987543 0.001876589564400157; -0.004599567884121469 -0.008140864142225085 0.00334912429366965; 0.006469668568966188 0.002418594699188977 0.00468091014514265; -0.00238443176525557 -0.006540357049349859 0.009732158612563546; -0.0028956221069858616 0.012569394170495123 0.0030020162327521224; -0.0003400600701050395 0.0004185321597184994 -0.002223769031415209; -0.0022160703684223986 0.0002502001260641862 -0.0017902709273918457; -0.006693597811506431 0.005651791424260572 -0.010779531254945473] %
+
+Mass Used: 94.69985095502443 kg
+Launch C3: 97.24385567303123 km²/s²
+||V∞_in||: 6.302290895860685e-6 km/s
diff --git a/archive/ES_0.5674160957517533 b/archive/ES_0.5674160957517533
new file mode 100644
index 0000000..bd5cbb3
--- /dev/null
+++ b/archive/ES_0.5674160957517533
@@ -0,0 +1,22 @@
+archive/ES_0.5674160957517533---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T21:49:10.139
+Launch V∞: [7.997623177186549, -5.6236470631175886, 0.16186815744010274] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.262859581678858e-10, -9.489199035588334e-10, -1.2413495182864356e-9] km/s
+ V∞_out: [9.696694875637058e-10, -1.1820045581137e-9, 3.663492604210146e-10] km/s
+ time of flight: 1.874957778761464e8 seconds
+ arrival date: 2030-04-21T23:58:47.139
+ thrust profile: [0.35415758774199013 0.005112846556138309 -0.10459665168151788; 0.11280187131204929 0.06892468694984553 -0.11643364127119003; 0.06502667712570487 0.06454067793970418 -0.12312540329624261; 0.05486720029247665 0.07310876449977619 -0.15521247688082723; 0.014992800815729899 0.023728676344447322 -0.06193258402940058; 0.019865678379270075 0.03911518514580996 -0.10259147091509126; 0.014011045000284975 0.03228637777130578 -0.09111445954410374; 0.008298000678260507 0.010429441961205333 -0.01665644818767096; 0.01264805537988951 0.0066421080516818635 0.005706222842799959; 0.00022595612267793636 0.0011637333851443488 -0.004114976475296484; -0.0002570975786817352 0.011560172089000363 -0.00759286043604424; -0.001058055105942347 -0.0029162266877633836 0.00044930989914600955; 0.001381467377914148 0.001353955433515615 0.00364216880650383; 0.009764358729557786 -0.010633455530101343 -0.007274642985800191; -0.0009533430573942909 0.004977000563733729 0.0002944149343992713; -0.0014685287440791652 -0.003861500902374336 -0.021131708132231954; 0.005160036176740585 0.028464817928115227 -0.022690775973107733; -0.02180875974493911 -0.026823900974665405 -0.04974560067633749; 0.011838001855654375 -0.009730402613217655 0.015384372829081448; 0.01169764131059673 0.0011992477683234039 -0.010791941864451222] %
+
+Mass Used: 104.23953793852115 kg
+Launch C3: 95.61358407517561 km²/s²
+||V∞_in||: 1.6833394521956462e-9 km/s
diff --git a/archive/ES_0.5674207858082121 b/archive/ES_0.5674207858082121
new file mode 100644
index 0000000..b5968b2
--- /dev/null
+++ b/archive/ES_0.5674207858082121
@@ -0,0 +1,22 @@
+archive/ES_0.5674207858082121---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T05:31:50.309
+Launch V∞: [6.20444168408737, -7.131857481046801, 0.3154999186726595] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002819690472638212, -0.0019090676224577266, 0.002683808809742642] km/s
+ V∞_out: [-0.0026827766949534403, -0.0009733006202303865, -0.0017403218413604927] km/s
+ time of flight: 1.8582437712151423e8 seconds
+ arrival date: 2029-03-15T23:24:47.309
+ thrust profile: [0.9163902520012152 -0.24327428597261738 -0.21732877012918334; 0.08834559405560086 0.02949754621286678 -0.08148501058072545; 0.06548810193870316 0.041371284225883445 -0.10005519870762924; 0.06591736830993832 0.057830430983465506 -0.1424583634915215; 0.04142866716469535 0.04406941168553553 -0.1152958461374502; 0.02094675097369235 0.02656497533936905 -0.07330783663206025; 0.02636912097345773 0.03869970262617201 -0.11015908473874282; 0.01101809227155861 0.019366061637875336 -0.05693679752289988; 0.00806666607015758 0.015157217782342115 -0.047113676322841753; 0.00011865828069431024 0.001260752972167229 -0.006768674518144529; 0.0010237410243789545 0.002074582383130163 -0.007641934561843128; 0.0003991990151228043 0.0013137157595524453 -0.003726355468807655; 0.0005195841344882311 0.0003779104574597052 -0.0018348858422424304; 9.838775061593127e-5 9.973382746714284e-5 -0.0047185837079233035; -0.001187865661324786 -0.000572460452680838 0.0017275666176882083; 0.00014979282521894628 0.0003537912312547093 -0.0017170018365855182; 0.007254111642119809 -0.0045172597926441994 0.0013787809812928656; 0.003299763297081303 0.0029762393692586092 -0.0036560691290803728; 0.003832735490350086 -0.004331412080110061 0.006500692277616972; 0.001776428739799401 0.004317101138339521 -0.008103241039209202] %
+
+Mass Used: 140.1524204602424 kg
+Launch C3: 89.45802793988659 km²/s²
+||V∞_in||: 0.003305582468791768 km/s
diff --git a/archive/ES_0.5674210681830266 b/archive/ES_0.5674210681830266
new file mode 100644
index 0000000..127a4fa
--- /dev/null
+++ b/archive/ES_0.5674210681830266
@@ -0,0 +1,22 @@
+archive/ES_0.5674210681830266---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T00:08:19.267
+Launch V∞: [6.177658850487563, -7.691748936710406, -0.012684715261072189] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.826532278173076e-7, -2.0536436428027683e-7, -3.4587983684083697e-7] km/s
+ V∞_out: [2.380096148250397e-7, -3.4688002455698586e-7, 3.6242691767952274e-7] km/s
+ time of flight: 1.715554423718456e8 seconds
+ arrival date: 2028-10-03T14:25:41.267
+ thrust profile: [0.26887534504531285 -0.10166043529588437 -0.10595967421089819; 0.06543508386013354 0.005442730250510034 -0.07768753135502418; 0.06792249476648327 0.020115445419369302 -0.13565092975799542; 0.05309742651646169 0.022255755113982787 -0.14703558883502355; 0.04086509752709453 0.02080853014998437 -0.1437508791073373; 0.03062381790517573 0.017672242288419602 -0.1289246480909631; 0.019508310221965048 0.012717704539466624 -0.09630085971944778; 0.017219862712206224 0.012032144694847566 -0.09394919018134533; 0.008776029589451083 0.0064800976212056926 -0.05307459385872321; 0.005293126143316628 0.003974408823191037 -0.03514874028245491; 0.004806053543716352 0.003437879950514797 -0.03217543405578916; 0.003070146530073425 0.0023079660456618543 -0.0224144449405468; 0.0004303696480633727 0.0008577853390567861 -0.005852879253494182; -0.0025943594569444233 -0.0004190124198272657 -0.0031422164899725944; 0.001253019892182885 -0.0014953138697481466 -0.003540609453721752; -0.001789072838735575 -0.0031501012111925498 -0.003930274651118478; 0.003051293060271025 -0.0004780671690793098 -0.004749704498450867; -0.00045626756780864385 0.0016922939173225613 -0.002877520681154904; -0.0006037805460022104 0.0008517466304651413 -0.000619212253031326; -0.0018393566870415073 -0.005391168346684802 -0.0006694558232522641] %
+
+Mass Used: 94.25256257789806 kg
+Launch C3: 97.32663148039423 km²/s²
+||V∞_in||: 5.551854432604394e-7 km/s
diff --git a/archive/ES_0.567423205222656 b/archive/ES_0.567423205222656
new file mode 100644
index 0000000..fb115f3
--- /dev/null
+++ b/archive/ES_0.567423205222656
@@ -0,0 +1,22 @@
+archive/ES_0.567423205222656---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T19:15:22.602
+Launch V∞: [5.93804713164651, -7.79127075591343, -0.04611215000332257] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.983489754360436e-7, -2.204136262417855e-7, -3.773349841815389e-7] km/s
+ V∞_out: [2.56562523688093e-7, -3.389465884629813e-7, 4.111137205034916e-7] km/s
+ time of flight: 1.6996349252239493e8 seconds
+ arrival date: 2028-09-14T23:20:14.602
+ thrust profile: [0.2914734429922201 -0.11360585527116453 -0.11475453299976965; 0.17590864123535144 0.02195679661810004 -0.18962993650510274; 0.08871676305062463 0.030231866118617532 -0.16024348218787987; 0.06962367978148162 0.03364480158008624 -0.17275103427666777; 0.041382745178800126 0.024389406200390425 -0.1316058690163566; 0.04284974896162259 0.02891110432741801 -0.16031306896801498; 0.007474593330762022 0.005504076929350925 -0.034028279240700454; 0.010603117404063327 0.00850271822816617 -0.05367643701096739; 0.009629356002995642 0.008190061888467487 -0.05379470457541066; 0.001359395670452737 0.0006920105957213687 -0.008515559493261422; 0.006991597072560988 0.006388741686053573 -0.04668746035621687; -0.0026821577399027867 0.0003018206248503049 -0.0024913954558529916; -0.0007817563869900513 -0.0010582236033152663 0.0013292099671310359; -0.00167723746730082 0.0032509914097842135 0.0007279915541786395; 0.0004208001721996333 -0.0005692498128525949 0.0019056521673551335; -0.0021398621939821127 -0.0014967743748070588 -0.00215593790756614; 0.0007712899420773136 0.00047761819436239095 -0.002104542608391795; -0.0015503641634376573 -0.0003750363481412667 0.005081057989833807; 0.0017496918133736552 5.1681988493337784e-5 -0.00484628062296822; 0.0012792360358102055 0.001330841523469753 -0.0035908852758637353] %
+
+Mass Used: 102.18956407651876 kg
+Launch C3: 95.96643005998511 km²/s²
+||V∞_in||: 5.913085177394973e-7 km/s
diff --git a/archive/ES_0.5674289207064941 b/archive/ES_0.5674289207064941
new file mode 100644
index 0000000..670bd1d
--- /dev/null
+++ b/archive/ES_0.5674289207064941
@@ -0,0 +1,22 @@
+archive/ES_0.5674289207064941---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T14:06:19.084
+Launch V∞: [7.7040618514154495, -6.423293445028864, -0.23748891018668214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.461488056427101e-10, -3.261475073249285e-9, 1.2891399824545329e-8] km/s
+ V∞_out: [2.9876768409854237e-9, -9.861347473665099e-9, 1.5960819829797207e-9] km/s
+ time of flight: 1.6984816738248798e8 seconds
+ arrival date: 2029-10-01T10:09:06.084
+ thrust profile: [0.08064973729780146 -0.015403410035419453 -0.03730643845832022; 0.04941226298746567 0.011784808341366583 -0.07273333248038141; 0.0279913387239271 0.010953329761490119 -0.06927524663792116; 0.02658607986926509 0.012059286706683808 -0.09476694011160139; 0.02303373283757955 0.012523816109062195 -0.10455054144136593; 0.0180590283042882 0.009491976992648251 -0.09305538744869295; 0.011398266730883951 0.0060261501732376006 -0.06756938773717165; 0.0286871520982486 0.018421274573416337 -0.17443793125730325; 0.0227016998173966 0.015451819109114664 -0.15659021535204107; 0.003772990649264272 0.002145292456251401 -0.02820653536595179; -0.0008530624002686601 0.002184970024140492 -0.006729312627708335; 0.007726458464939077 0.004139240570207631 -0.06299129416780025; 1.0145087634279342e-5 0.0009612232184946462 -0.004260729720789041; -0.00038791538366066266 -0.0009340351917441739 6.451435481553557e-5; 0.0028261787116285308 0.0018198099579835483 -0.008349377097451713; 0.0007540416707662175 0.0016385733224479034 -0.008994918012804998; 0.0008615917440354477 -0.0003756507510171141 -0.0016824286788093296; 0.006516598671218581 0.0012346786826375076 -0.0036761005520229923; 0.00038007033634132083 4.276152363780818e-5 -0.0026570888533783282; -0.007354537287325019 0.00010798922141430398 -0.004107893065005251] %
+
+Mass Used: 74.77234022680068 kg
+Launch C3: 100.66766867384726 km²/s²
+||V∞_in||: 1.3308782348795802e-8 km/s
diff --git a/archive/ES_0.5674291022936987 b/archive/ES_0.5674291022936987
new file mode 100644
index 0000000..89cba80
--- /dev/null
+++ b/archive/ES_0.5674291022936987
@@ -0,0 +1,22 @@
+archive/ES_0.5674291022936987---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T07:02:11.421
+Launch V∞: [6.1930069623892745, -7.491381218087936, -0.12126477634096337] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.359783694988999e-8, 7.362338150002133e-9, -1.0707102386858293e-8] km/s
+ V∞_out: [3.425504580885971e-8, -3.310750496041355e-9, 4.338358251694199e-9] km/s
+ time of flight: 1.8412727379925248e8 seconds
+ arrival date: 2029-02-28T09:30:04.421
+ thrust profile: [0.4516675703221076 -0.1107065504389448 -0.14273061870079823; 0.09717036282670252 0.02908814763506939 -0.09470033097649966; 0.07648480105304256 0.04403753352112269 -0.12380275556947462; 0.05356736893108025 0.04313153464949863 -0.12374639945052539; 0.02953828172666081 0.027845310569112075 -0.08840907350078683; 0.03871289979437501 0.04387309798614647 -0.14039547678523626; 0.03512877455727105 0.04699941237783377 -0.15083906964407587; 0.0060557994279979875 0.00852767309423288 -0.03299742686252805; 0.00435378879912203 0.0074404318670805505 -0.028089813801964417; 0.0026246345407935972 0.004480296336893839 -0.02086997349439515; 0.001767406513557707 0.0027023381986200122 -0.015419194402377828; -0.0020886310543764856 0.0005691958771760082 0.002563442156160301; 0.007531467337761734 0.0014344492842480862 -0.0036056195602881883; 0.001462273431511423 1.8905556992875592e-5 0.001670864385323531; -0.0011631457017479245 -0.0005601856051840573 0.006566321301934732; -0.0028852768757647914 0.004765548297345155 -0.0016701078474796868; 0.0038430276166382623 0.00044996151544460196 0.005053802355666154; 0.011048692360815286 -0.001355413775847051 -0.016665862397604207; -0.0064701411001437115 -0.017085818900964164 -0.0007648625624793275; 0.0020388257824780352 0.002440322957011282 -0.008287346047719614] %
+
+Mass Used: 110.81576054404331 kg
+Launch C3: 94.48883293690375 km²/s²
+||V∞_in||: 3.602305806381569e-8 km/s
diff --git a/archive/ES_0.5674516581713827 b/archive/ES_0.5674516581713827
new file mode 100644
index 0000000..a6fa578
--- /dev/null
+++ b/archive/ES_0.5674516581713827
@@ -0,0 +1,22 @@
+archive/ES_0.5674516581713827---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T13:52:51.771
+Launch V∞: [6.63651511234221, -7.411757998154956, 0.16794491749541263] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.600269623236405e-7, -3.405748245232093e-7, -4.005973004650344e-7] km/s
+ V∞_out: [-5.167547600015091e-7, -3.1064646883101867e-7, -9.498686057984501e-9] km/s
+ time of flight: 1.8749577787471753e8 seconds
+ arrival date: 2029-04-10T16:02:28.771
+ thrust profile: [0.16443526663303384 -0.04300985325677338 -0.06373133172551369; 0.022149230402439064 0.005144720513601866 -0.022152811982333133; 0.045848751454602175 0.021665156557054532 -0.09109044419236217; 0.04630589799843643 0.029824017565015647 -0.12846972791929445; 0.048981330669423485 0.03690565394741575 -0.17387963970836237; 0.04191402722166129 0.034852259204891455 -0.17826452149590605; 0.010774215842308235 0.009981413228998974 -0.059212188300755184; 0.011644129737341014 0.009182174873016941 -0.0501104069277831; 0.012475303083749424 0.000927515156295881 -0.050717197094707026; -0.0007172180444077136 0.0006042005115948477 -0.00859261522438617; 0.004228558335815281 0.0008988100391302781 -0.017096010849607362; -0.005055434549449866 -0.0010826441447762596 0.005410100656348212; -0.0032893966476105667 0.010595476206741585 -0.018940515817862255; -0.006574055228514127 0.010908223262711285 0.0009493741662257153; -0.0035930970845927802 0.004717053182704411 0.006596974047920898; 0.0011004709630278789 -0.002804592659570458 -0.0015095424062064671; -0.006538277228227252 -0.007261353565214913 -0.006381571212558587; -0.00873510430455629 0.001966591115642455 0.003867789618249351; 0.010684598543229767 -0.030328431452260787 -0.0010379904666724033; 0.001998968396780912 -0.0026757155543232717 -0.0018400072961115657] %
+
+Mass Used: 84.49371396318702 kg
+Launch C3: 99.00569495487304 km²/s²
+||V∞_in||: 6.372509881034912e-7 km/s
diff --git a/archive/ES_0.5674548585571284 b/archive/ES_0.5674548585571284
new file mode 100644
index 0000000..ee2078e
--- /dev/null
+++ b/archive/ES_0.5674548585571284
@@ -0,0 +1,22 @@
+archive/ES_0.5674548585571284---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T15:52:09.587
+Launch V∞: [6.43409967194782, -7.483650769770818, 0.07716798736688077] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2654681412523531e-7, -1.347716329122187e-6, 7.667801741576962e-8] km/s
+ V∞_out: [-5.416520128494262e-7, 1.1438219425590019e-6, -6.733366500283043e-7] km/s
+ time of flight: 1.856754798321445e8 seconds
+ arrival date: 2029-03-19T16:23:28.587
+ thrust profile: [0.2589728065756205 -0.06127757752189158 -0.0919419764053656; 0.0471708873413316 0.013884970789391536 -0.05383851519787736; 0.046022704903998325 0.026667278145886503 -0.0870819904545315; 0.0731535500613414 0.05772991622184319 -0.18354255473999626; 0.03677181202629734 0.034069665561559624 -0.1191240610995224; 0.03719811272971953 0.04058878524012483 -0.15301851714955117; 0.020964986032674954 0.029020489970344975 -0.11137770798135228; 0.004092724633060535 0.006482937212022213 -0.025784898283256048; 0.0006787014556202953 0.0009377282670131335 -0.013463051223685168; 0.0037648939705797347 0.004953556948549375 -0.018054714274326505; 0.004395577004457661 0.0076191844158943365 -0.03571523270287224; 0.006191111238901294 -0.000989209930164495 -0.0037265609015414624; -0.0006626927825146792 -0.002452123119375952 0.0010229861583117162; -0.0026374485954130163 -0.00027779695769601263 0.007154301891334043; -0.00031083634241869636 -9.819178566504737e-5 -0.0011714396107677947; -0.00236042503066304 0.005599387193297382 -0.009874653084905458; -0.00015654961751135213 0.002203958239176443 -0.00356533204332477; -0.016890654662190897 -0.013675277000551265 -0.014421354766197323; 0.002995576498997923 -0.0008755213461431118 0.0008749640854061028; 0.0035423706414760585 0.0006438028965458367 0.03721105108563793] %
+
+Mass Used: 93.81370472075605 kg
+Launch C3: 97.40862233072464 km²/s²
+||V∞_in||: 1.368774006594109e-6 km/s
diff --git a/archive/ES_0.5674570606429018 b/archive/ES_0.5674570606429018
new file mode 100644
index 0000000..4480c44
--- /dev/null
+++ b/archive/ES_0.5674570606429018
@@ -0,0 +1,22 @@
+archive/ES_0.5674570606429018---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T15:23:55.355
+Launch V∞: [6.568772608583947, -7.556219877013771, -0.768022077142018] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.017742306127319713, 0.00874471487922254, -0.020298783201372912] km/s
+ V∞_out: [0.017454068972545485, 0.0070873858799983015, 0.021194211312656235] km/s
+ time of flight: 1.8749577781264883e8 seconds
+ arrival date: 2029-04-13T17:33:32.355
+ thrust profile: [0.11393011377540735 -0.04069716516140387 -0.0546266753522735; 0.027150169833335167 0.001573759769448917 -0.03958241527870522; 0.036013139614192675 0.006043390474764103 -0.09135469093513832; 0.03720613403240656 0.007302763441074659 -0.13332873670505835; 0.032527833604160276 0.006299884734208109 -0.14796019336453706; 0.02464055423153446 0.004474719247326322 -0.1335247157495062; 0.01716966982203565 0.0028271054494033773 -0.10627571262726185; 0.010571114244599585 0.0015409806318255675 -0.07252181128977263; 0.0037362956648551845 0.0004522532239386527 -0.02754629413479856; 0.002365337880341405 0.002928132456294176 -0.0091157507813052; 0.0019340718022027377 0.00019791333233578484 -0.016220049200602316; -0.001229422732568161 0.000997315871342567 -0.004219323677940209; 0.0003572423526344016 0.0004064262951946671 -0.0034018994269038104; 0.0008769744243375847 -0.0011828430778369578 -0.002920003576970944; -0.000429491537591609 0.0005189434575299074 -0.0025352379526689265; 0.0004045805889830348 -0.005013928961445048 0.0005332218677358428; -0.0017939936966312592 0.0031706884944784734 -0.017260519039077493; 0.002826789726400396 0.0012719783800994135 -0.0021743031179001174; -0.0017098126168668768 -0.006062278883442007 -0.0016361460167070394; 0.0005380042672446389 -0.0007509865655809948 -0.0015449069127733226] %
+
+Mass Used: 73.82854385982864 kg
+Launch C3: 100.8350903240383 km²/s²
+||V∞_in||: 0.028342548659052554 km/s
diff --git a/archive/ES_0.5674585863499164 b/archive/ES_0.5674585863499164
new file mode 100644
index 0000000..f7f6efc
--- /dev/null
+++ b/archive/ES_0.5674585863499164
@@ -0,0 +1,22 @@
+archive/ES_0.5674585863499164---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T13:22:01.327
+Launch V∞: [6.157968743951819, -7.454662813292781, -0.05953205750760802] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.7138298198548577e-9, 5.6797817648142184e-9, 1.9887937730558055e-9] km/s
+ V∞_out: [-2.803473406417777e-9, 4.457053956303746e-9, -7.090698590849978e-9] km/s
+ time of flight: 1.8749577779548365e8 seconds
+ arrival date: 2029-04-08T15:31:38.327
+ thrust profile: [0.495241664901041 -0.10970789095985847 -0.1291717317483275; 0.09691637973888448 0.03596309658904661 -0.08453403511883385; 0.1077679580918508 0.0733762738151768 -0.15102259385642483; 0.07489172972871432 0.06716788955997267 -0.1460517935040199; 0.04345671387329062 0.05304733112025444 -0.1189392194765668; 0.027577754445322063 0.04052692338872483 -0.09909298715047807; 0.019545998204778717 0.028023522118189956 -0.0731312842776141; 0.007534102850428957 0.01049696529026044 -0.033994392455630726; 0.008319007859758313 0.01876558409088281 -0.05154030976496059; -0.00022387249977295041 0.007294723370766123 -0.015710539942577723; 0.003262988474043345 0.003993577554800045 -0.012874228952819141; -0.003182666114765183 0.004253580848664567 0.0012491285402733013; 0.0010020381314551421 -0.0002878189703065283 -0.0029504106709655783; 1.0445355050440531e-5 -0.0007624371415436947 0.0027395118787142993; 0.003834648094234338 0.0054471124051307575 -0.004048149886092714; 0.0009417693305957202 0.0012894454835764772 -0.006140540886135105; -0.018127452351373568 0.002265158330215662 0.0061620998640829865; -0.0007356555022514544 0.0006317003166381504 -0.002496329261184779; 0.01729723415548525 -0.005270036107446656 -0.011192728532787986; -0.005966682844232349 0.002406298861097025 -0.004899230254262388] %
+
+Mass Used: 116.64097954095087 kg
+Launch C3: 93.49612077724886 km²/s²
+||V∞_in||: 7.071616045749715e-9 km/s
diff --git a/archive/ES_0.5674670833909383 b/archive/ES_0.5674670833909383
new file mode 100644
index 0000000..3e1715a
--- /dev/null
+++ b/archive/ES_0.5674670833909383
@@ -0,0 +1,22 @@
+archive/ES_0.5674670833909383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T22:44:40.072
+Launch V∞: [6.227631351912511, -7.570516602380383, 0.11028704341988872] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.03451284438290049, -0.015969548841266872, 0.03898589493168398] km/s
+ V∞_out: [-0.035436409135152315, -0.014170323457148717, -0.038849645827280704] km/s
+ time of flight: 1.7664281827373067e8 seconds
+ arrival date: 2028-12-01T10:11:38.072
+ thrust profile: [0.3442796516462767 -0.10562525415931082 -0.11977892298959956; 0.07034624785541149 0.015648063986247178 -0.07474195024032824; 0.06612741995368747 0.031769044707711046 -0.11386449280616272; 0.06652360544088673 0.04274068595097572 -0.15548374154377412; 0.037052533947667936 0.029662819564813963 -0.11232026958397794; 0.038031859226866555 0.034851113538286786 -0.13506086206771606; 0.032924493089445624 0.03402210534010454 -0.13736652590197693; 0.019075745237053632 0.020552441746531654 -0.08845993847225708; 0.010358621699649444 0.012615171812594621 -0.057220541190336476; 0.002714741702825121 0.002270766527088264 -0.014613083439338651; -0.001213803822127981 -0.00011241888710098618 -0.0014539242423296183; -0.0035641859084405425 0.007634726802876589 -0.005362746138902418; 0.0015133202342082247 0.0017895289004854094 -0.002778284669111003; -0.001269012426190941 0.0016119341186964181 0.002487802323966184; -0.005782482354783425 -0.007389204514458022 -0.0011820768768656949; -0.0017383791748318443 -0.001081524426931233 0.0006629325980238229; -0.008137865207470518 -0.005768955021407441 -0.0008572151546006389; -0.011019318524556496 0.004471635182745222 -0.002622628974019646; 0.0022588039224567245 -0.004527113787986047 -0.0009739237589999885; 0.007324907802281791 0.006007809319393174 0.006933221165815039] %
+
+Mass Used: 101.41331412333739 kg
+Launch C3: 96.10827711418698 km²/s²
+||V∞_in||: 0.05446157288599198 km/s
diff --git a/archive/ES_0.567476899396054 b/archive/ES_0.567476899396054
new file mode 100644
index 0000000..3216c17
--- /dev/null
+++ b/archive/ES_0.567476899396054
@@ -0,0 +1,22 @@
+archive/ES_0.567476899396054---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T23:18:03.913
+Launch V∞: [6.4739620127011746, -7.515351126812004, 0.09446554870913952] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2609218522325933e-8, -5.581344392629657e-9, 1.4275049192372688e-8] km/s
+ V∞_out: [5.2797610968618644e-9, -1.1840810479047703e-8, -1.638009347036564e-8] km/s
+ time of flight: 1.8449033416764948e8 seconds
+ arrival date: 2029-03-06T06:36:57.913
+ thrust profile: [0.19710714401701057 -0.05342744818832129 -0.072311227999086; 0.031251056579068535 0.00783333297886612 -0.035156923921240986; 0.051227779598844364 0.024374030388416918 -0.09250109834043335; 0.051420656667691814 0.03256227376074059 -0.12957288109280937; 0.035990493200411075 0.02832364328015415 -0.1185435421852101; 0.03538975331760153 0.031219341848723575 -0.139334226653385; 0.026929800573271222 0.025496121818102874 -0.12365011187444087; 0.013568662963189808 0.0114902601557249 -0.07010826591410467; 0.006727893503197537 0.008357778977520613 -0.03747441187721076; 0.004035290848210447 0.008370701941993521 -0.03569535627143649; -0.0004190300076601578 -0.0036422495460806926 -0.006744587427817558; 0.003985316054628077 0.0027845872998234237 -0.015083083407672416; 0.0019811095016722363 0.0021164022375309626 -0.015184478389601299; 0.0010791296282122442 0.0004930630070538275 -0.0033127205652224998; -0.0010216907048485682 -0.003184570399833469 0.004410088824456684; 0.006086927269366148 0.004783462739999729 -0.004517363243362517; 0.003924331666909495 -0.006682640149779659 -0.013296624566512306; 0.0064488445399458185 0.004783503272004948 -0.009254503852381454; 0.0041482275858163685 0.005290773998609303 -0.018844823312812384; 0.0067740958470202655 0.004265282992487178 -0.02516543079494665] %
+
+Mass Used: 88.04698838918239 kg
+Launch C3: 98.40161044106523 km²/s²
+||V∞_in||: 1.9847438787349014e-8 km/s
diff --git a/archive/ES_0.5674778815060701 b/archive/ES_0.5674778815060701
new file mode 100644
index 0000000..fba78e5
--- /dev/null
+++ b/archive/ES_0.5674778815060701
@@ -0,0 +1,22 @@
+archive/ES_0.5674778815060701---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T04:45:58.547
+Launch V∞: [5.883798518866333, -7.7313373788657715, 0.31903834075911564] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010295090340322608, -0.007297985235412568, -0.008180266442126155] km/s
+ V∞_out: [0.006603821648847356, 0.01111878604888747, -0.008026778569692057] km/s
+ time of flight: 1.7292727423743185e8 seconds
+ arrival date: 2028-10-18T16:07:12.547
+ thrust profile: [0.3546599501675584 -0.11672163241549192 -0.1130364800727522; 0.2133755425503421 0.04391785269730512 -0.1864608504870692; 0.1054692939603945 0.04749984810432861 -0.1504760784972886; 0.10001082117581991 0.06652502911738585 -0.2011667965341805; 0.05622943611290242 0.04580791297866163 -0.14587568389339106; 0.028186344401743054 0.025829561423511477 -0.08689674098826926; 0.011494356692368582 0.013983238683034247 -0.04683406839406264; 0.012964927047322158 0.016338643552411755 -0.05632712445229448; 0.010227744124515126 0.014845145146451839 -0.048879211247162074; 0.005535623152056281 0.00809403578623471 -0.03063160621263309; 0.0009307281369083292 0.0019504889358230846 -0.010797904031889089; 0.0003950588179229178 -0.00016171660089890118 0.0013492065425206794; 0.0017417335152215903 0.0015343535964372774 -0.00885769180257285; -0.002544436112396601 -0.0011198960754057663 -0.00021490759812628274; 0.001346105737537762 0.0006878817528058695 -0.00010182865651110133; -0.00017352964187661491 0.000936373230703783 -0.0005941667559611673; -0.006640421737764962 -0.0009641825209296955 -0.0024320846452411046; 0.0037366553137563787 0.005254232851375806 -0.005497304654508758; -0.0031453414936458103 0.004587918079994126 0.0012572486855222703; -0.004429115786425859 -0.006695773581669928 -0.0001125444013352914] %
+
+Mass Used: 110.83991427762749 kg
+Launch C3: 94.49444813933503 km²/s²
+||V∞_in||: 0.015038824178634414 km/s
diff --git a/archive/ES_0.5674848194074166 b/archive/ES_0.5674848194074166
new file mode 100644
index 0000000..2b7e97e
--- /dev/null
+++ b/archive/ES_0.5674848194074166
@@ -0,0 +1,22 @@
+archive/ES_0.5674848194074166---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T06:10:39.468
+Launch V∞: [5.985204135664965, -7.772322254270178, 0.04756077434401297] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012340810264566862, 0.00907050479098574, 0.010086273136172589] km/s
+ V∞_out: [-0.007983406367733216, -0.013966026377031157, 0.00880367187800557] km/s
+ time of flight: 1.6667960710197902e8 seconds
+ arrival date: 2028-08-06T10:04:06.468
+ thrust profile: [0.331541512414377 -0.1402414456534737 -0.13074414767847337; 0.06154156914698156 0.006162651452461638 -0.06707357403281866; 0.08755010711904414 0.02780148151502618 -0.15236846552017963; 0.09678540162721402 0.04409153553993947 -0.22776333937132268; 0.07134154392375397 0.03980452739524131 -0.21052405009326453; 0.04219765993567298 0.026996948665892334 -0.14969626727109855; 0.019576015070326882 0.013916406344666265 -0.08154356914599083; 0.008268172199461788 0.005952006509784572 -0.039836114942372734; 0.009212078344375117 0.006954378120969737 -0.04751057575010488; 0.0034230330803516375 0.002656356159978996 -0.017367097852251705; 0.001303234799825159 0.0012764459709641864 -0.008068770745467113; 0.0009122455344434484 0.0009086929851924517 -0.006515549631691684; 0.0006716644431101581 -0.0003243668064226936 -0.0034587763486404067; 0.0010577481689324402 0.0016725865904363606 9.110591634243635e-5; -0.0026304622316790835 -0.0006216115977659258 -9.913133865642617e-5; -0.00013437832121309556 0.0004389029668794206 0.0010694026857386981; -0.0008681679091305856 -0.0006477072085896873 0.003931999807879784; 0.0013068416767375662 0.0015868768589550185 -0.0003202012399539779; -0.0002781249232478063 9.157397525988344e-5 0.00047882135483838344; 0.0031140856771828627 -0.00512141529003809 0.0012971198261075615] %
+
+Mass Used: 100.70106715913198 kg
+Launch C3: 96.23392379706068 km²/s²
+||V∞_in||: 0.018338553948629946 km/s
diff --git a/archive/ES_0.5674997313724894 b/archive/ES_0.5674997313724894
new file mode 100644
index 0000000..30d1239
--- /dev/null
+++ b/archive/ES_0.5674997313724894
@@ -0,0 +1,22 @@
+archive/ES_0.5674997313724894---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T20:28:17.358
+Launch V∞: [6.247768667697634, -7.580926109977707, 0.0066644908863775845] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.884639733571952e-8, -8.218185963280622e-8, -3.599962553628911e-8] km/s
+ V∞_out: [3.225439344442466e-8, -4.939907792871335e-8, 7.470017426574924e-8] km/s
+ time of flight: 1.8427573644492316e8 seconds
+ arrival date: 2029-03-04T16:10:33.358
+ thrust profile: [0.35690262652892984 -0.10513369226704718 -0.1357904777716488; 0.07281496915268458 0.014240040262442522 -0.08474077039095596; 0.04578277185067154 0.01856618676686867 -0.08965620554180768; 0.047779651206308935 0.025571088130892518 -0.12937385102580715; 0.025497307219527404 0.01659333722377726 -0.09017139621639554; 0.037746231125654756 0.02772131820802291 -0.15543770622016292; 0.024761359264129135 0.020012995553052786 -0.12495673573528886; 0.004082974742842435 0.004060854776688608 -0.02300595901139624; 0.0056225235591989605 0.005653398756029047 -0.03772297622297405; 0.005320204155835881 0.005302324945384483 -0.03812750984010295; 0.006160144964548811 0.006039384985291368 -0.04303714784246198; -0.0007151932808499405 -0.0022221346474577477 -0.0010991625520178055; 0.00192559308232646 -2.1582081707520982e-5 -0.002902469209836147; 0.009942688475986495 0.00450101142821414 0.0005049684781449487; -0.007630954119273784 -0.0013893602666879392 -0.004233948335854808; -0.0013846045198131992 -0.011185217568051041 0.0030818968180748928; -0.003549706645230359 0.005897100531730049 0.007821751265948286; 0.0009663863181228068 -0.002481167032040661 -2.729796447229621e-5; 0.0030267863179918256 0.001640114782643678 -0.004126502705335338; 0.00510683093397628 -0.000978868918810897 0.011126870608446412] %
+
+Mass Used: 99.13661245280991 kg
+Launch C3: 96.50509842544477 km²/s²
+||V∞_in||: 9.776949257014634e-8 km/s
diff --git a/archive/ES_0.5675045655614281 b/archive/ES_0.5675045655614281
new file mode 100644
index 0000000..38235d5
--- /dev/null
+++ b/archive/ES_0.5675045655614281
@@ -0,0 +1,22 @@
+archive/ES_0.5675045655614281---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T17:10:08.443
+Launch V∞: [6.376942654839619, -7.246525105590236, 0.18366846695949227] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.920045146796994e-5, -3.029730982797755e-6, 5.1440375110353795e-8] km/s
+ V∞_out: [4.175658872727677e-6, -9.530597414628993e-8, -1.8983181396734145e-5] km/s
+ time of flight: 1.8577165351573846e8 seconds
+ arrival date: 2029-03-16T20:24:21.443
+ thrust profile: [0.5543353496233976 -0.13684813819252933 -0.16427511984483872; 0.1575682158870734 0.05216688188487188 -0.1460977423298106; 0.0662222350425905 0.041216455176435005 -0.10659229700493553; 0.03280222793844702 0.027241626226442286 -0.07609965006576194; 0.03034282983524803 0.03111632201903766 -0.0903299399270232; 0.023770725190046655 0.028705366121232877 -0.08755222897277107; 0.013410184485201131 0.019154095291220002 -0.06102340115849028; 0.028993501652237623 0.04635024713224271 -0.14390339447233524; 0.01454966442672425 0.024447193228256784 -0.08291512537952465; -0.0003719007774037799 0.0017715669137855364 -0.0041532482037172904; 0.0018540619778843789 0.0014249891248236763 -0.006412144958641487; 0.0016293910582810848 0.0037957868494217185 0.00020158204240507994; 0.000988080272117838 0.001474224585739403 0.0010504575767685612; 0.0012035081533541088 -0.005019268166718581 0.002267712077029954; 0.0050523738548139945 -5.009255980373717e-5 -0.00041695172198667144; -0.0028234138078515186 0.0010499683419845736 0.0013218238879693506; 0.003572387167213747 0.001395739994193247 0.0003870390017971406; -0.00036912247132567016 0.010095150217925918 0.0038115970786972804; -0.0036972980487691262 0.005145930100914154 -0.0035418525910515977; -0.0027221636951791023 0.0026481651133081845 0.00884272318308816] %
+
+Mass Used: 118.35632245189572 kg
+Launch C3: 93.2112578348178 km²/s²
+||V∞_in||: 1.9438087676368403e-5 km/s
diff --git a/archive/ES_0.5675107186539925 b/archive/ES_0.5675107186539925
new file mode 100644
index 0000000..2098549
--- /dev/null
+++ b/archive/ES_0.5675107186539925
@@ -0,0 +1,22 @@
+archive/ES_0.5675107186539925---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T05:58:15.567
+Launch V∞: [7.5478632033204045, -6.026433333935926, -0.5362579665262812] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.8124292506490245e-6, -4.250932263017314e-6, 3.071008959689e-6] km/s
+ V∞_out: [-9.038468428255535e-8, -7.11420661625654e-6, 3.044064725485844e-8] km/s
+ time of flight: 1.874957778243795e8 seconds
+ arrival date: 2030-04-21T08:07:52.567
+ thrust profile: [0.36764083682119836 0.04223216053286085 -0.07597570780257609; 0.15651422948720872 0.127061805437749 -0.10772140892572468; 0.10597061069656188 0.14737303528462875 -0.13374862267551535; 0.07060809222031565 0.14167637077726075 -0.1400418968077168; 0.04341174970369393 0.11796851380912765 -0.12693858063140512; 0.02350840462891219 0.08268330821939268 -0.09860405953030338; 0.012412711659537378 0.05645783099980052 -0.07326294652439697; 0.004671542499464234 0.027114350348024778 -0.03844838647678548; 0.0010367406371818808 0.006659173113593833 -0.010568769232514739; 0.00023637425864675798 0.004556430302752947 -0.0035610381360792337; -0.0014483292565497098 0.0033951344022919725 0.0005530785742470902; -0.0015111803424775752 0.0025606698199590423 -0.0010740478927586772; -0.0007137845596500967 0.0030721880958841496 -0.0014386981642714757; -0.0005612631297412924 0.005740798548631713 -0.0043593395950046465; -1.5017724625852512e-5 0.0007170591881706092 -0.0033513874436577632; 0.007222693999792784 0.00018776002747249214 -0.00013173165957392667; -0.000296931143864752 0.0018525359630022502 0.0007826619300151064; 0.00023262010097280944 -0.00022444235199967343 -0.010058221084044167; -0.0005809711382032386 0.0023153214531463737 0.0004690614482231793; -0.000319595403576554 0.0022873852441901103 0.001157218561572619] %
+
+Mass Used: 116.23752851505287 kg
+Launch C3: 93.57571027107514 km²/s²
+||V∞_in||: 7.11765385697801e-6 km/s
diff --git a/archive/ES_0.5675249511347568 b/archive/ES_0.5675249511347568
new file mode 100644
index 0000000..27fc5e5
--- /dev/null
+++ b/archive/ES_0.5675249511347568
@@ -0,0 +1,22 @@
+archive/ES_0.5675249511347568---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T17:44:23.978
+Launch V∞: [7.475360913869517, -5.832487118398432, 0.1701881741443182] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3825577335526654e-6, 0.0001521800916382476, 2.82203274328154e-6] km/s
+ V∞_out: [0.0001468745806273273, -2.2144845435416634e-5, 3.299335634895344e-5] km/s
+ time of flight: 1.7598347664036378e8 seconds
+ arrival date: 2029-12-03T14:02:19.978
+ thrust profile: [0.8438239929268588 -0.054450651473704176 -0.19844324021456447; 0.23803570456673623 0.13279618574640945 -0.20034758815614845; 0.0432150262368654 0.04241479030072005 -0.07414872880021849; 0.02517278147873445 0.03279967349872453 -0.06289611597910486; 0.03675309550640272 0.061337304389868806 -0.12123673667486032; 0.033829152043420414 0.06430914827392727 -0.13736243379602422; 0.013040939796270476 0.02913113744208955 -0.0690357773919417; 0.009982644881543096 0.02780569307905815 -0.06772985977247632; 0.0057731227956069045 0.01786984266508618 -0.04408939355407071; 0.0019356031857296007 0.006123261633129315 -0.016549915966985553; 0.002014659644029082 0.0037140900270442277 -0.008292006743194396; 0.0005214411640175952 0.0028315134623756585 -0.008410479119527935; 0.0002740226344375099 -0.0026762679668164762 -0.0026553447251631466; -0.006901225872495377 -0.000162536170373417 -4.911923664810327e-5; 0.00600773243269867 0.0014411164849727654 -0.0034595375095300917; -0.004850783719671556 0.003744258333161111 -0.006260720217668285; -0.007344610646132482 -0.002574607024771836 -0.001662732971180885; 0.001996731630822274 -0.002533332316729991 0.012174309349477743; -0.0010595137631962148 0.0007527841071285047 0.00305562734202448; 0.0028530141362618534 0.0005584575129011486 -0.0033713060143346404] %
+
+Mass Used: 137.53308002840595 kg
+Launch C3: 89.92789079351033 km²/s²
+||V∞_in||: 0.00015222490184323752 km/s
diff --git a/archive/ES_0.5675290513923071 b/archive/ES_0.5675290513923071
new file mode 100644
index 0000000..28056e1
--- /dev/null
+++ b/archive/ES_0.5675290513923071
@@ -0,0 +1,22 @@
+archive/ES_0.5675290513923071---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T00:53:14.241
+Launch V∞: [7.815562033587855, -5.851904080524597, 0.09781484000494045] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9822161239484913e-7, 2.2207968553886836e-6, -4.602398005771261e-7] km/s
+ V∞_out: [3.225599582237458e-7, -1.2789939986370473e-6, -1.8134376302403852e-6] km/s
+ time of flight: 1.807665678973716e8 seconds
+ arrival date: 2030-02-02T05:49:21.241
+ thrust profile: [0.4044870615366595 -0.01760208347719467 -0.13168062842688005; 0.08948876048470386 0.04426284330714635 -0.0975152718207606; 0.069508958374716 0.05683180972274424 -0.13549700132307632; 0.0493540920220789 0.052767365963559125 -0.1408368427050901; 0.03351793237409978 0.04312411404082416 -0.12733994401302406; 0.020476237175757122 0.030432497212839832 -0.09776719430999964; 0.010288909238189505 0.019301382597560982 -0.06679092832259383; 0.0065292435718471865 0.013466150745566013 -0.05305133082616782; 0.003672852574009952 0.006023788809188824 -0.024426527339682612; 0.002182078410443257 0.004499890861520939 -0.01493294536355869; -0.0015074395116128694 0.001316596906909892 -0.0021084958111972146; 0.00624806995155022 0.009042761207399993 -0.009787494503423005; 0.004816815924169636 0.005153238020017067 -0.00953107510324763; 0.0004770519642879269 0.007147646205581586 -0.01186348163757727; -0.015259880358516494 -0.017122540577244598 0.00137799714820111; -0.01895972897064525 -0.02450424614967934 0.010387465105737285; -0.0008897996117558137 -0.011496539718203004 0.01778339227933335; -0.01811063976923333 0.02182138410928826 0.035121263206589634; 0.00010602357099443153 -0.001874083060081755 0.003205065577386833; -0.005751919061237469 0.0028271019361434894 -0.004195413304217094] %
+
+Mass Used: 105.98263239092603 kg
+Launch C3: 95.33735901144554 km²/s²
+||V∞_in||: 2.2766315368455985e-6 km/s
diff --git a/archive/ES_0.5675706682714478 b/archive/ES_0.5675706682714478
new file mode 100644
index 0000000..56414e8
--- /dev/null
+++ b/archive/ES_0.5675706682714478
@@ -0,0 +1,22 @@
+archive/ES_0.5675706682714478---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T21:25:43.523
+Launch V∞: [6.016906631080548, -7.809375912721078, -0.10054310801029977] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.052204151873072e-6, -3.6130112699808215e-6, 2.7947808666503423e-6] km/s
+ V∞_out: [-4.106064279603663e-6, 5.3875229331328475e-6, -3.6300794201364253e-6] km/s
+ time of flight: 1.6738810185821316e8 seconds
+ arrival date: 2028-08-15T06:07:24.523
+ thrust profile: [0.23199869616676633 -0.09390422038106856 -0.09344404556916354; 0.10818182378515342 0.013149249776252382 -0.11862915419521904; 0.08228158596671242 0.028556526989833044 -0.1461627927080989; 0.06757521798899747 0.03344263720141936 -0.16365217458092182; 0.0541284962847362 0.032806938775127525 -0.16458267876892418; 0.03262242810128162 0.022337022549399475 -0.11955369415466946; 0.029813384289299142 0.022740103142222315 -0.1256721735105016; 0.020816211503739367 0.017364006203277417 -0.10042330268898376; 0.005356461379986727 0.004787263757403763 -0.029268422606269294; 0.0007063713844807234 0.0005784122674806151 -0.0018665135153348041; 0.009890433115197024 0.009346833162260247 -0.06016694206160796; -0.0003232285906647548 0.0004136244915830155 -0.003463053946241223; -4.6125757686363523e-5 0.0005029805803538731 0.00042965311656846414; -0.0002521934663182452 -0.000930952886888515 -0.00026165686231048504; -0.0005042358270025131 -0.0002865560662637319 -0.0017773148653902541; 0.0001249586087686616 -5.0432973812723704e-5 -0.0004343046021925219; 0.0028126412392175653 -0.001127609809948803 -0.004143974244432672; 0.0005564910159576608 -0.0006784381030007921 -0.0013335826905214814; 0.0002489076651960564 0.0004481712935222199 -0.00037227963718228425; 0.0005482132803906505 8.81376070000178e-6 -0.003026421113134646] %
+
+Mass Used: 95.16795857561965 kg
+Launch C3: 97.19962646989761 km²/s²
+||V∞_in||: 7.582468306927033e-6 km/s
diff --git a/archive/ES_0.5675768032379397 b/archive/ES_0.5675768032379397
new file mode 100644
index 0000000..11edc73
--- /dev/null
+++ b/archive/ES_0.5675768032379397
@@ -0,0 +1,22 @@
+archive/ES_0.5675768032379397---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T04:16:23.726
+Launch V∞: [5.961945154849711, -7.702263006972149, -0.051822255164423466] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.282039034540345e-7, -6.031634514023101e-6, 3.855777698714626e-7] km/s
+ V∞_out: [-2.412033541523629e-6, 4.695258366808154e-6, -3.047661644572277e-6] km/s
+ time of flight: 1.683361240065508e8 seconds
+ arrival date: 2028-08-24T12:18:27.726
+ thrust profile: [0.41017399978406477 -0.14761407791462275 -0.13892824849434704; 0.13899709272256555 0.027615443454750047 -0.1318658161987946; 0.07613877256928385 0.0343379997981136 -0.11990077991103772; 0.0648530210865158 0.04195704746539582 -0.1394718236381322; 0.0473480197082485 0.03681510913492692 -0.12697873402120358; 0.03407069809653505 0.030026257259315143 -0.10899101017404696; 0.05787618685025075 0.059896668270870604 -0.20230324535434874; 0.021659937919657663 0.02523877628179787 -0.09546348996172992; 0.009093353371343305 0.01071983241541119 -0.04361293021039447; 0.0045890601150537095 0.005788640996940584 -0.02469222501596318; 0.002230043475413697 0.0022676376703918404 -0.01023650202335839; 0.00016267896444840363 0.0002261515733087271 -0.0010071648885346123; 0.0001860425047428644 -0.00017077639897912083 -0.00016678220272339875; 0.00017688284205391708 -0.00019844279228723116 -0.00015250118390984453; -6.128357416800126e-5 0.00029796530004412894 -0.0003931922352726666; 0.00019003760273504148 0.0004725714175557514 0.00023825603660003735; 0.0001923211603974337 0.00022838077759582324 -0.0010136880415376364; 0.00017271023858329767 7.176865254597865e-5 -0.0007176394203696889; 0.0002212697647184555 7.266421476842625e-5 1.627868155925849e-5; -0.0002968350280177712 -5.039432854103445e-5 0.00013381634877263445] %
+
+Mass Used: 108.7510062534584 kg
+Launch C3: 94.87233100413792 km²/s²
+||V∞_in||: 6.10042677466669e-6 km/s
diff --git a/archive/ES_0.5675866076851295 b/archive/ES_0.5675866076851295
new file mode 100644
index 0000000..399e42f
--- /dev/null
+++ b/archive/ES_0.5675866076851295
@@ -0,0 +1,22 @@
+archive/ES_0.5675866076851295---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T13:42:51.173
+Launch V∞: [7.326260270900561, -6.466342927506887, -0.20472655783160454] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009616164070978786, -0.00351730403694882, -0.005258878703552286] km/s
+ V∞_out: [-0.0055492656722673055, -0.0006071681798615315, 0.0030700968744448547] km/s
+ time of flight: 1.56967361165515e8 seconds
+ arrival date: 2029-04-28T07:45:32.173
+ thrust profile: [0.47289536232335705 -0.10195667227381791 -0.17478423585167485; 0.08950059445860459 0.025231652301599093 -0.10066906354736968; 0.060279973694849616 0.0312771629354101 -0.1128396360635542; 0.06437405409150174 0.04435811443860748 -0.16549839094660715; 0.06284679225541435 0.05270507576730096 -0.2055621658495175; 0.0474213014393559 0.04523663741579223 -0.1916352953390104; 0.030516774591661768 0.03195090374257111 -0.14529155664826693; 0.012631956473852688 0.014039288531480742 -0.06941128665326045; 0.004440284451877731 0.005329141466155319 -0.027724431616535594; 0.002861032113494235 0.0035802639672323495 -0.019567580431096698; 0.0008908385742472376 0.0010089919280762997 -0.006492810653877854; -0.0002057435393572275 8.827452498448124e-6 -0.0002548990052338115; 0.00014731386130984527 0.0012661137346026369 -0.0006449042495475597; -0.0004399567446605031 0.00015395385115686333 0.0002981456754933714; 0.0006056710639579554 0.00013888075986146243 -0.0001931477303186164; -0.0002646732644924669 -0.00033387904689015027 0.0007480066300689276; -0.0002745787183545481 -0.0007167755482943915 -2.5140568553774366e-5; -0.0004771300260702673 4.098864209750133e-5 0.002066448880021588; 6.497228245816135e-5 -0.00038385190893216363 0.0012531099815133928; 0.0006833887756159183 -0.00014511413259277365 -0.0014956672686030075] %
+
+Mass Used: 104.9284142692918 kg
+Launch C3: 95.52959337657587 km²/s²
+||V∞_in||: 0.006399370205060187 km/s
diff --git a/archive/ES_0.5675872770426034 b/archive/ES_0.5675872770426034
new file mode 100644
index 0000000..7ce12dd
--- /dev/null
+++ b/archive/ES_0.5675872770426034
@@ -0,0 +1,22 @@
+archive/ES_0.5675872770426034---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T09:30:30.388
+Launch V∞: [7.423840754763571, -5.993486665511341, -0.3805250385681088] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8575731844542856e-10, 2.651831628723303e-9, -2.0731797999487318e-9] km/s
+ V∞_out: [1.4411491528421186e-9, 2.975622768429407e-9, 7.66097793706461e-11] km/s
+ time of flight: 1.819774341160874e8 seconds
+ arrival date: 2030-02-12T14:47:44.388
+ thrust profile: [0.4919297650391586 0.01668617690597681 -0.10123177133865217; 0.2855293083654524 0.20523684476309176 -0.18654523127872458; 0.13862321831822033 0.17345551414052524 -0.17294110844439087; 0.06398287405382841 0.11056335390464357 -0.12558827166237493; 0.04362948887020997 0.10111323904006324 -0.12355611139788192; 0.02101016232834756 0.06127240466552729 -0.08168872483023888; 0.014391016312139977 0.05073332936775758 -0.07192658282512956; 0.005918492485722643 0.02746460390463617 -0.04163292750550281; 0.0002844704612067493 0.0029692129226568183 -0.006492799445297629; 0.0004776332918575937 0.0015407898453700655 -0.002232158510909608; 0.0008472656311632805 0.0022629556482613713 -0.003787092414417667; 0.0006598846449721023 -0.000276919946998791 0.00029106325619180143; -0.0003653239110435859 0.00023328725788551634 -0.0007979279521709751; 4.132927390874865e-5 -9.396254501798447e-5 0.00032477604860064774; 0.0019614450625192906 -0.001296330442514372 0.000666683506263239; -0.0010122908423282383 -0.00134674621523986 0.00128733918124626; -8.372254255323351e-5 -0.0001775617355963229 0.0003861155383553276; 0.0003836389362796312 -0.0015656680955269465 0.0028286848901242995; -0.0013191437674364107 0.001664309787850797 0.0007976406722698304; -0.0007212691900268222 -0.0005821740476965626 0.00017438514444238437] %
+
+Mass Used: 130.30127916045694 kg
+Launch C3: 91.18009326672805 km²/s²
+||V∞_in||: 3.3781567037450867e-9 km/s
diff --git a/archive/ES_0.5675919068241342 b/archive/ES_0.5675919068241342
new file mode 100644
index 0000000..aa8924f
--- /dev/null
+++ b/archive/ES_0.5675919068241342
@@ -0,0 +1,22 @@
+archive/ES_0.5675919068241342---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T15:15:50.789
+Launch V∞: [6.452330822690634, -7.486034319085202, 0.13775092773794684] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009906050472564495, -0.006066888090260744, 0.008300299446063706] km/s
+ V∞_out: [-0.007061313745239016, -0.005938888890961205, -0.004640056695512196] km/s
+ time of flight: 1.874957778740211e8 seconds
+ arrival date: 2029-04-11T17:25:27.789
+ thrust profile: [0.28530454288108203 -0.07582553535854601 -0.10795697599230357; 0.03328760978310607 0.007902406953674692 -0.03887826868992523; 0.043559478685131346 0.019451730066968785 -0.08645180682919834; 0.049632258847906265 0.029156405872158325 -0.13735688063338722; 0.040154850527170494 0.02787924011049994 -0.1418128746968089; 0.021395182130907485 0.016828178611210134 -0.0918157479714854; 0.00906663342442922 0.008458288665776715 -0.04529191045952263; 0.014053101649565795 0.01309185466987085 -0.0801089892537037; 0.0062120214951186725 0.0065482410420168585 -0.03930148988460122; 0.014360931420791263 0.013187500522374931 -0.08941593238543098; 0.004911030725106759 -0.005907899826531489 -0.0066419033602517375; -0.0004485881397044551 -0.0007591863208320106 -0.0006504489513734424; -0.00011821730430803504 -0.001177364961152815 0.0014059671175541146; -0.004472778220394286 -0.0048377769037076055 -0.019820908553683514; 0.007051432052375926 0.008364244125687814 -0.009905438208414418; -0.0015641587219053774 0.004023455060913245 -0.0023376434827805897; 0.0021556836950014533 -0.012057888749726358 -0.02585364720900945; 0.001073299236907664 0.0022724016600856 -0.014316333711248045; -0.004830850711670291 0.001731226847370758 0.002129319625843949; -0.00267796102311517 -0.0062509917077260245 -0.01161884252637813] %
+
+Mass Used: 92.31905185281994 kg
+Launch C3: 97.6922581900577 km²/s²
+||V∞_in||: 0.01032876567425765 km/s
diff --git a/archive/ES_0.567596180651539 b/archive/ES_0.567596180651539
new file mode 100644
index 0000000..6b6b2a6
--- /dev/null
+++ b/archive/ES_0.567596180651539
@@ -0,0 +1,22 @@
+archive/ES_0.567596180651539---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T11:30:30.101
+Launch V∞: [6.280071264728376, -7.425918393437197, 0.005858964357559796] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.357908570154768e-6, 5.214424618121801e-6, 5.911862508843401e-6] km/s
+ V∞_out: [7.978560286072688e-6, 5.216106840653921e-6, 1.6516373456612135e-7] km/s
+ time of flight: 1.8749577784948906e8 seconds
+ arrival date: 2029-04-07T13:40:07.101
+ thrust profile: [0.32738622623538705 -0.05857468734029096 -0.08907448360421223; 0.24037970859354077 0.09746725138630122 -0.1806520169634577; 0.07523638620414684 0.056656534980760606 -0.10478532263127832; 0.05567112078164726 0.05734714852682759 -0.11352894477473296; 0.03597595001881629 0.04608326937493575 -0.09595229974640418; 0.029579964947119505 0.04369787823287737 -0.09661522889133671; 0.01870792167776183 0.035084300086341016 -0.08040982872983385; 0.007886049647370707 0.01344833567147644 -0.03318820936005404; 0.01891410764412929 0.041287611362657003 -0.09511137537511666; 0.002219611344363286 0.0027142028444460905 -0.005172185921275914; -0.0002179362653665477 -0.0006552082104734781 -0.008788468517951993; 7.708239954557969e-5 0.0007196985248590182 -0.0023969999005418476; 0.005034211602743476 -0.0037898570061355484 -0.0057275287055392424; -0.0032706189818180738 0.0019345401891976517 -0.00624823856810364; 1.4099974170197148e-5 -0.002344211639285691 0.0005803894273008008; -0.0016684942261549294 0.008095955470190368 -0.0005848947972556728; -0.0005764730477703353 0.0014130605953289609 -0.011033560385371486; 0.0028191171579654284 0.003114907362828094 -0.008647465439119446; 0.007843496256190881 -0.0022235413365710244 0.007338613930462489; -0.0028059667638017797 -0.001714316225786697 -0.008728912018054223] %
+
+Mass Used: 110.45791590626641 kg
+Launch C3: 94.58359340351927 km²/s²
+||V∞_in||: 9.531396889631697e-6 km/s
diff --git a/archive/ES_0.5676079391659079 b/archive/ES_0.5676079391659079
new file mode 100644
index 0000000..1d717c2
--- /dev/null
+++ b/archive/ES_0.5676079391659079
@@ -0,0 +1,22 @@
+archive/ES_0.5676079391659079---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T15:39:25.247
+Launch V∞: [6.600101829536633, -7.195319702151153, 0.2717871689145128] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.6589768252778307e-7, 3.4647179289786257e-6, -2.0784576064583112e-7] km/s
+ V∞_out: [1.2313589321917563e-6, -2.883875326015516e-6, 1.5568779734182432e-6] km/s
+ time of flight: 1.8749577787482688e8 seconds
+ arrival date: 2029-04-05T17:49:02.247
+ thrust profile: [0.4125679869072943 -0.08741579270395276 -0.11244303763407512; 0.0952302086345811 0.036841273787434424 -0.08910108937584453; 0.07618502149057436 0.05424037939534027 -0.11858875481670676; 0.05368874272365745 0.05106127735695232 -0.11697362069061226; 0.04386760156050365 0.05179012860329333 -0.12372045444899657; 0.023784621898527168 0.038465696965109424 -0.09890541182685558; 0.02015035999964329 0.0335927042717378 -0.0904063886620225; 0.015917934521613733 0.02964063718793981 -0.08315543196403759; 0.008371158477250444 0.017306611096627372 -0.05019783150494134; 0.0003274995766517722 0.002256815374777425 -0.0061433577091312315; 0.001310941578640008 0.002964022550830642 -0.011076855089442113; -0.00133257429282017 -9.675591235949933e-5 0.003441505262141888; -0.0010880342706854128 -0.002487170550297965 0.0033655782220942047; 0.006247729877349369 -0.002624746203600965 0.0006652979968573323; -0.001858268249652393 -0.001186727784590878 0.002167398025590571; 0.0023454391360900745 -0.0010739465492923144 -0.0005900903973029615; -0.0027136394655288883 -0.003985344207565471 0.0042064242855620665; -0.0002545850058567773 0.0020322340212548524 0.0003394437751474135; 0.007206040440091078 0.003575508243113146 0.002554157127773223; -0.004569607300226155 -0.0033155416011986434 -0.0029787737369740006] %
+
+Mass Used: 105.66354045086973 kg
+Launch C3: 95.40783804160392 km²/s²
+||V∞_in||: 3.5020752188080055e-6 km/s
diff --git a/archive/ES_0.5676089978355191 b/archive/ES_0.5676089978355191
new file mode 100644
index 0000000..6f9d0a4
--- /dev/null
+++ b/archive/ES_0.5676089978355191
@@ -0,0 +1,22 @@
+archive/ES_0.5676089978355191---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:38:25.989
+Launch V∞: [7.493091161547829, -6.3259524063638475, -0.8977489227042521] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4996360773760224e-9, -4.689075521370569e-9, -1.0805257091807342e-9] km/s
+ V∞_out: [-8.583544126471261e-10, -1.7711949812353564e-9, -4.533022652512972e-11] km/s
+ time of flight: 1.8030457525432977e8 seconds
+ arrival date: 2030-01-30T02:14:40.989
+ thrust profile: [0.24574084197442445 0.009890597818554885 -0.07263397652235981; 0.1196887704147773 0.08220496992322011 -0.10280762638326908; 0.07977446558415208 0.09200170964823765 -0.1220215634004046; 0.06148345870830952 0.09817396361154386 -0.1433769519439349; 0.04469513946663905 0.09267813334524147 -0.1437791171007068; 0.025956244694372577 0.06865161921832076 -0.11294887213877569; 0.014806225727745542 0.04912164681385546 -0.08716146748213484; 0.006043349960790529 0.023971430387789254 -0.04750359422447977; 0.0025977664465622143 0.01201821874697543 -0.024999176112459484; 0.00044524499277148955 0.0021317485829662713 -0.003073766199572745; -3.5526708338889576e-5 0.0004529622522722262 -0.0006068117306987728; -3.994727319322599e-5 5.846841782259531e-5 -0.001375577438162621; 0.002094712510925214 0.006103634421203447 -0.005140872111763256; -0.0018408634823962626 -0.0006403116628463911 -0.002649400338574411; 0.0012009797541437709 0.0014656065456290987 -0.0003806683176198302; 0.0009761825983462623 -0.00206029505363236 0.005930119289970769; -0.0021436139338973687 -0.007974429868615202 -0.0013184348199590966; -0.0008289978229002999 -0.0021036464010520902 -0.0020548429652993867; -0.00589601743915792 0.0005660917437423609 -0.0026513174142531694; -0.00591209366008235 -0.01166236489293937 0.009331287649297637] %
+
+Mass Used: 96.55191837690245 kg
+Launch C3: 96.9700421310634 km²/s²
+||V∞_in||: 5.4224667424187114e-9 km/s
diff --git a/archive/ES_0.5676164609000713 b/archive/ES_0.5676164609000713
new file mode 100644
index 0000000..8a3849c
--- /dev/null
+++ b/archive/ES_0.5676164609000713
@@ -0,0 +1,22 @@
+archive/ES_0.5676164609000713---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T20:06:42.121
+Launch V∞: [5.936935453452307, -7.817887055977923, -0.034850492698269196] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007050883225254639, -0.004518622922803556, -0.007634331900267188] km/s
+ V∞_out: [0.004621836984547714, 0.008504331044381717, -0.005891958763879377] km/s
+ time of flight: 1.6967786486995304e8 seconds
+ arrival date: 2028-09-11T16:51:06.121
+ thrust profile: [0.2628363362131232 -0.09794982387057227 -0.09806669625117823; 0.13889866956194 0.016959781652695686 -0.1469818450858183; 0.11748336638502431 0.04169712557040442 -0.19966780989248417; 0.06516534249829925 0.0315932788896019 -0.15519278971217945; 0.052864521508666475 0.03148747136208829 -0.15775263997953437; 0.03874037126281153 0.02647747540621143 -0.13833930198458594; 0.025254134674732615 0.019043497102991174 -0.10419232688586196; 0.013097859282042504 0.010668797095065883 -0.06084129464093527; 0.001402672628662911 0.0008360124885069463 -0.007772957631634814; 0.00038499715271339655 -0.00011715362004522528 -0.0009440421336163424; 0.0012557779475213975 0.0016111961947652843 -0.009084784136874484; 0.00455869373513312 0.003092685051587698 -0.017444278100985467; -0.005654312628043714 0.002666279248266746 -0.006369306483883883; 0.0007413455394821244 -0.002694473328461831 -0.0010453449827740532; 0.0005456722621954779 -0.0007198547691136771 -0.0038334873532863334; 0.004575394336262794 0.0036448632072910415 -0.003803893215922811; -0.001013720314200511 0.00039036740128184117 -0.004332616556086797; -0.003071862623045431 0.002472546169056601 -0.0006424522923557897; -0.005439704888123107 0.0025810044093803877 0.005703411007034149; -0.003198964950549285 0.0004026044521980099 0.01035440741677637] %
+
+Mass Used: 100.07384931067327 kg
+Launch C3: 96.36777515532742 km²/s²
+||V∞_in||: 0.011332075314702962 km/s
diff --git a/archive/ES_0.5676186135738343 b/archive/ES_0.5676186135738343
new file mode 100644
index 0000000..6e4f4b3
--- /dev/null
+++ b/archive/ES_0.5676186135738343
@@ -0,0 +1,22 @@
+archive/ES_0.5676186135738343---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T20:19:15.133
+Launch V∞: [7.348904104625731, -6.601635105908244, -0.2674515079024494] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0406780074685765e-8, -2.1919015628613184e-8, 8.130948853411379e-8] km/s
+ V∞_out: [4.238668877475336e-8, -1.7098043356520586e-7, 2.5562603755060794e-8] km/s
+ time of flight: 1.578882495674716e8 seconds
+ arrival date: 2029-05-11T06:10:04.133
+ thrust profile: [0.2615349759078814 -0.06158634850206469 -0.10809715680286515; 0.09768279957040998 0.023601952169886826 -0.1169600216674701; 0.08080925412609721 0.03675858640603596 -0.16244543810133028; 0.06870459777317281 0.040385412361043135 -0.19206272660224724; 0.05202722325150083 0.03537548830302693 -0.1832772032545947; 0.03816374798950582 0.028332567863948322 -0.1616798533200795; 0.024662827480697053 0.020115267542692043 -0.12212440307557518; 0.012089207193841682 0.010685739330772158 -0.06853054468868018; 0.0038564961205189412 0.003972228592605046 -0.027704416842783502; 0.0017880871542702405 0.0018496890721665404 -0.013419719854856942; 0.003190397895291391 8.486146108875234e-5 -0.004269202473004418; -0.00016510887440019978 5.778273033804886e-6 -0.0025920353159831467; 0.0007288172862352637 -0.0002556721178939663 0.0005534782571065609; -5.8924306761466835e-5 0.0016739565270498568 -0.006063896186114575; 0.004381882924086575 -0.0011704155149987153 0.00013970156324813032; -0.00020647812850743973 -0.00042424208040714716 0.0030579551902881587; 0.0004431080766873225 -0.0031120387126741264 0.0015051088455459427; 0.0009758349324483756 0.0014194073998285732 0.0008380877202954855; -0.0003765591189478065 0.000829003015731862 0.004339488654169656; 0.00031601660146170733 -0.0008954057560120814 0.0013077862568125626] %
+
+Mass Used: 92.54125297166456 kg
+Launch C3: 97.65950791962436 km²/s²
+||V∞_in||: 8.485267964731253e-8 km/s
diff --git a/archive/ES_0.5676207898766928 b/archive/ES_0.5676207898766928
new file mode 100644
index 0000000..ca8ba75
--- /dev/null
+++ b/archive/ES_0.5676207898766928
@@ -0,0 +1,22 @@
+archive/ES_0.5676207898766928---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T01:31:05.972
+Launch V∞: [6.30162508233435, -7.700735128804735, 0.02798137678331721] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5485788893773978e-11, -1.5295715312907693e-9, -1.3667029061968731e-9] km/s
+ V∞_out: [-4.299624509273237e-11, 2.248063764408139e-10, -3.192747213489492e-10] km/s
+ time of flight: 1.7530965701393e8 seconds
+ arrival date: 2028-11-18T02:38:42.972
+ thrust profile: [0.12391583226273205 -0.04759736110866589 -0.056023552196102784; 0.07749959347961582 0.008163528202476374 -0.10146094912090484; 0.05729668551535216 0.01538191950213404 -0.12162318080715318; 0.051881754961199456 0.01893327874477537 -0.15278048941419936; 0.043413801659296085 0.018633237448977356 -0.1617988966754474; 0.030541005151660063 0.01437572013453387 -0.13615075956005104; 0.015333973903780747 0.0074350049671255075 -0.07936568808032245; 0.016791303991665996 0.007927062531315466 -0.09499426676184797; 0.009067519419981709 0.0034593806573763224 -0.05220808207794896; 0.0050461208198716405 0.0018366319924630202 -0.03271204251674718; -0.0005731886314047153 0.00241358640832198 -0.002527576802895245; 0.0018285875606419764 0.001809122248197041 -0.01967431261751963; 0.0015666966772141554 0.0015375032754380636 -0.0010820416393178618; -0.0028027640883103973 0.0009949592758197179 -0.002000269781112198; -0.00048350779536197056 0.0013347570067090888 0.004345543101812728; 0.001084187244229027 -0.001269361836540121 0.0046712333267568806; 0.002369229747043381 0.0006112566446280047 0.0066844195380378005; -0.0030343244835770843 0.0022026512436889778 0.006053266750342446; 0.0005038395540531493 -0.0011564673174498407 -0.003072710961215112; -0.0030561204188978806 -0.012202598756572057 0.004321520332016533] %
+
+Mass Used: 84.65085309087863 kg
+Launch C3: 99.01258315975937 km²/s²
+||V∞_in||: 2.0512692930963087e-9 km/s
diff --git a/archive/ES_0.5676290180290016 b/archive/ES_0.5676290180290016
new file mode 100644
index 0000000..8fd21e9
--- /dev/null
+++ b/archive/ES_0.5676290180290016
@@ -0,0 +1,22 @@
+archive/ES_0.5676290180290016---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:31:22.108
+Launch V∞: [7.315106909734832, -6.346710061133388, -0.11943255288906036] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00038535418128563025, 0.00026777809439125136, -0.00016067479586461938] km/s
+ V∞_out: [-0.0002001170841114135, -0.000367610645472002, 0.00026586280474963044] km/s
+ time of flight: 1.6294766179805845e8 seconds
+ arrival date: 2029-07-07T04:45:43.108
+ thrust profile: [0.5426097654836399 -0.09077052532001113 -0.1891252683809757; 0.13356130421183346 0.04542843319514069 -0.14235392513444617; 0.11305989453774175 0.06946743113729655 -0.204686604036549; 0.049391302829368246 0.040076631628532 -0.1288230674584165; 0.03859017763836641 0.037416450194830614 -0.1305177362947439; 0.0424212968232234 0.04691516246174193 -0.17334171503019571; 0.02305956952338795 0.028209436192469593 -0.10994203212367104; 0.00417067672474043 0.00619869981870552 -0.0231206821645887; 0.006307929798505944 0.00723791582211574 -0.03572019494444887; 0.001724040753084045 0.002197546219127281 -0.012081668019445827; 0.0037992890802284697 -0.0005178246937138416 -0.004820713049843214; -0.0016137927566386924 0.0016056599914419365 -0.0058843049239504785; 0.002637913817803184 0.0001697727371078724 -0.0027468913927646338; 0.002508043077093779 0.003795860080977912 0.004453238920710477; 0.0033076510568014143 0.001892587256954933 -0.0030681981500426414; 0.0018898943967383868 0.0034024563922041883 0.007962523373321206; 0.009128387159511316 -0.001778073283909002 -0.013028677790992843; 0.007771703042774749 0.0021173662013347005 -0.009540369825917187; 0.0005653533341078139 -0.0019928199476143575 -0.00889563873057273; 0.005127850996986287 0.00494692461857954 -0.011956425487359017] %
+
+Mass Used: 115.03346032598392 kg
+Launch C3: 93.80578183563165 km²/s²
+||V∞_in||: 0.0004960033698436589 km/s
diff --git a/archive/ES_0.5676298657024716 b/archive/ES_0.5676298657024716
new file mode 100644
index 0000000..3bcb963
--- /dev/null
+++ b/archive/ES_0.5676298657024716
@@ -0,0 +1,22 @@
+archive/ES_0.5676298657024716---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T04:34:39.058
+Launch V∞: [6.566699468947386, -7.5772091453886965, -0.12292776136550793] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9856277523539348e-7, -1.3774150203393718e-6, 8.481467365617886e-8] km/s
+ V∞_out: [-5.07393664575016e-7, 1.144096819468581e-6, -6.135298058229275e-7] km/s
+ time of flight: 1.874957778431965e8 seconds
+ arrival date: 2029-04-13T06:44:16.058
+ thrust profile: [0.07393886316518579 -0.022035749718564816 -0.033380100001812026; 0.03369914016609935 0.005010747474929471 -0.045395313425126115; 0.05855842398219275 0.01916314147784533 -0.1375311554285392; 0.03198787664433987 0.013414078729089604 -0.1034456567091646; 0.03234702411243199 0.016148799160496077 -0.13372516190103634; 0.02737287416217525 0.014191458457838316 -0.13368745921393146; 0.023334371187072364 0.013062572629123446 -0.1283642040804309; 0.007978728444640298 0.0044718553641367505 -0.05179141117179485; 0.0022074374571423106 0.001431764801665161 -0.018861590921670314; 0.004600115687774357 0.0007956649277083374 -0.039823246140845696; 0.00012269385154361264 0.0010809170272321682 -0.020019664851837468; 0.0014279767327863887 -0.0003361298124886858 -0.005125896386243317; 0.000800691409375395 5.5775789865446636e-5 0.001341388391128428; -0.001406740823979321 0.0012269069548226934 -4.451356309725018e-5; 0.0017879104544183014 0.0021650626359244257 0.007191602034526904; -0.006692372661834923 0.0025374369093234595 -0.0023353785687748635; 0.008086466054739963 -0.0016635919455065527 0.004755006210279282; 0.0045845902029521875 0.003354168154665267 0.00025887472376126606; 0.00023689665437300013 -0.000799573352966752 0.0012578709043947534; 0.00015772524415410394 0.004410278397447575 -0.03351322929600352] %
+
+Mass Used: 75.68879241900686 kg
+Launch C3: 100.55075158295031 km²/s²
+||V∞_in||: 1.394235576519656e-6 km/s
diff --git a/archive/ES_0.5676392716100257 b/archive/ES_0.5676392716100257
new file mode 100644
index 0000000..e48e962
--- /dev/null
+++ b/archive/ES_0.5676392716100257
@@ -0,0 +1,22 @@
+archive/ES_0.5676392716100257---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T12:38:56.315
+Launch V∞: [7.690291385136466, -5.764285408856825, -0.0026068192022296274] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0038953999310364054, -0.0026411269502903596, -0.00017331189758958203] km/s
+ V∞_out: [0.003393331197596718, 0.0015775211266641819, -0.0028533598580132023] km/s
+ time of flight: 1.8371497673348433e8 seconds
+ arrival date: 2030-03-06T20:35:12.315
+ thrust profile: [0.5252124019470089 -0.007442896891931412 -0.13725796469708645; 0.2550686704252913 0.14952615197130278 -0.21792241944230042; 0.057614598238030466 0.055957497116567154 -0.09257113154826611; 0.05216561912613853 0.0706183481204832 -0.12634337105587548; 0.03141396617025079 0.053457820302571166 -0.10257000533722022; 0.02288324555598253 0.044164100307069694 -0.09453809590872281; 0.005305367016291776 0.012109513393112276 -0.025030342927347654; 0.0017572297031369687 0.010096055097585478 -0.021666399439631123; 0.009329930825512714 -0.003984008792540144 -0.014943049014214024; -0.006814149933240548 -0.002688031000373522 -0.01676841201417807; -0.0006077224852683235 0.0015252037900905552 -0.004691033999338534; -3.75747210444224e-5 4.5549381829528425e-5 -0.0029749243210639596; 0.0005044913988591135 0.019012562467792093 -0.020527986015289754; 0.0004691755214083793 0.003667930852947777 -0.003079766307671988; -7.759924777541013e-5 0.0036312509792956653 -0.008843268184105434; 0.007496750568541369 0.004639920157936323 -0.007223512989935434; 0.0022414550745975224 0.027012900641310882 -0.0223597457627917; 0.01799270438541637 -0.0038414232240194693 -0.03853229892690448; -0.0011245691605951368 -0.018405085601629175 -0.03168085520966989; -0.0018469817332368 0.007976279707951296 0.004240377831994538] %
+
+Mass Used: 123.4349647033705 kg
+Launch C3: 92.36757465857019 km²/s²
+||V∞_in||: 0.004709535986072788 km/s
diff --git a/archive/ES_0.5676581490860245 b/archive/ES_0.5676581490860245
new file mode 100644
index 0000000..327a3b9
--- /dev/null
+++ b/archive/ES_0.5676581490860245
@@ -0,0 +1,22 @@
+archive/ES_0.5676581490860245---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T12:05:45.858
+Launch V∞: [6.46371820852843, -7.574717210499725, -0.003556521795211986] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008941709592186226, 0.00014309647510905204, -0.006119026598946966] km/s
+ V∞_out: [0.010365065275509348, -0.00010773867403927972, -0.0031342491870767993] km/s
+ time of flight: 1.8749577787459025e8 seconds
+ arrival date: 2029-04-13T14:15:22.858
+ thrust profile: [0.21588450177535437 -0.06956152090022572 -0.09387313315193356; 0.025956886442425685 0.0025771940258772588 -0.0387457731968012; 0.04736299349074401 0.011855382258269383 -0.11666651761934267; 0.023446579605239617 0.006749977264507479 -0.07942950999703502; 0.03538357569642052 0.012366322290736042 -0.15083165119396552; 0.02547404048562905 0.009005675357767647 -0.13307192745847457; 0.015091433837097335 0.004724471464946491 -0.09113314928793707; 0.01121493869778006 0.003711250103050404 -0.07286034131842531; 0.007435098428792046 0.002579317460206696 -0.05334187804513825; 0.004915444898521266 0.0019398778901266087 -0.042190562303035535; -0.0016497738339062778 0.003567192509382717 -0.0024608172130200067; 0.0008950706953086494 -0.0005922402622775484 0.001332092436931315; 0.004602763421183428 -0.0006877056443353772 -0.01341179857066728; -0.0005812913405527585 -0.001206753112064408 -0.0019612353473214684; 0.007735431559802754 0.0014380385487770017 -0.003061879005782097; 0.007364654794395719 0.005075553570427263 0.003219498026635341; -0.0026455400955570987 0.003113819043793901 0.006792252917751497; -0.002901893061101165 -0.0008672355873207582 0.011084255076908764; -0.0006468008592390934 -0.0032840851530912723 0.0009167810672393261; 0.0027486778044093583 -0.0024767434772954566 -0.0006556286788056042] %
+
+Mass Used: 83.8578024086537 kg
+Launch C3: 99.15600654714999 km²/s²
+||V∞_in||: 0.010835918675903963 km/s
diff --git a/archive/ES_0.5676720542130493 b/archive/ES_0.5676720542130493
new file mode 100644
index 0000000..94260d5
--- /dev/null
+++ b/archive/ES_0.5676720542130493
@@ -0,0 +1,22 @@
+archive/ES_0.5676720542130493---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T01:28:31.470
+Launch V∞: [7.449450060350027, -6.322886311905356, -1.1436574268622577] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4370082793055098e-8, -8.62486392361735e-9, 8.177335475193322e-9] km/s
+ V∞_out: [-6.975104450366239e-9, -1.307101886316875e-8, -4.168783563891617e-10] km/s
+ time of flight: 1.7692140768566716e8 seconds
+ arrival date: 2029-12-20T18:18:38.470
+ thrust profile: [0.27956222101672784 -0.0023620065571792735 -0.08748976811307302; 0.13582967413428226 0.08114241141120863 -0.12424748334528288; 0.09692204726473024 0.09854890493456021 -0.15593746010795764; 0.06793515246430586 0.09502129594095032 -0.1632248026032372; 0.04290654309286294 0.07620115500100014 -0.14321495137421528; 0.02158242505726353 0.04636784562853922 -0.09690797612490995; 0.01504131170871304 0.03906333028992102 -0.0864041240877409; 0.0013339992859232707 0.005042190815388386 -0.012039649965653203; 0.003553389681301228 0.011449469887058588 -0.03384596436121246; -0.00019348869571250645 0.00108175986430884 -0.0009824858507680747; 0.001067581369848733 0.005634921582563889 -0.015277920791652735; -4.5363975856068e-5 0.0011226484769232192 6.65375180200988e-5; -0.00040170238641006615 0.0007041283676386223 -0.003563353981401977; 0.00014732774495751022 0.0028818064573175707 -0.0068916869357422; -0.0018091136026791939 -0.002520804322761183 0.0050506483489565325; 0.001889385469705414 0.0014687384340355927 0.0025705231928850915; -0.00018567700746003962 -0.002492817113285896 -0.00034793957584841736; -0.0003870370792477879 -0.0035951749683315317 0.0012890104012486317; 0.00033284413923647413 0.006761669880609929 -0.007472720280837391; -0.0029807622798676387 0.004240898540147448 -0.0022712253753427083] %
+
+Mass Used: 97.72735593637071 kg
+Launch C3: 96.78114982494633 km²/s²
+||V∞_in||: 1.8648227064630823e-8 km/s
diff --git a/archive/ES_0.5676740467666315 b/archive/ES_0.5676740467666315
new file mode 100644
index 0000000..ceefcea
--- /dev/null
+++ b/archive/ES_0.5676740467666315
@@ -0,0 +1,22 @@
+archive/ES_0.5676740467666315---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T22:51:44.364
+Launch V∞: [6.646126702885148, -7.3651855443795515, 0.12627302820120698] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.361187880075961e-8, -1.474642944240077e-8, 1.775457639681213e-8] km/s
+ V∞_out: [-7.333042536376528e-8, 1.801760665471941e-8, -9.061911184633989e-9] km/s
+ time of flight: 1.874957778745322e8 seconds
+ arrival date: 2029-04-10T01:01:21.364
+ thrust profile: [0.2005219894795107 -0.05231482767178425 -0.07715381877380584; 0.028472663666054006 0.00743442381701529 -0.034162427380805514; 0.05135217209257554 0.024786762879301222 -0.10238947234321259; 0.06460209419240379 0.04150669502734371 -0.17774840300273728; 0.044041588270846456 0.03378012099656066 -0.15614794986167924; 0.023666461545942253 0.02049324543292212 -0.10302575601679566; 0.015112347263453991 0.014182910044201002 -0.0759783470199671; 0.005306841291013147 0.006279314670131187 -0.033714816305097636; 0.008249693913798473 0.009284535563518074 -0.05479915511546473; 0.0032948305195724826 0.004574380347480587 -0.026416350804539947; 0.0030673270279407408 -0.0032447190421319586 -0.008890076065803026; 0.0025862978111493005 0.003725091871320632 -0.02292352236059007; 0.008726833644761785 -0.0035862492494171984 -0.0039180477855311575; -0.009100061938070749 0.002058833530388603 0.0047557025093923; -0.00597106584649475 -0.00044816892349118184 0.0025738864581722077; 0.015068263589237636 -0.012836918934182883 -0.00363398580690644; -0.00988433917195319 0.004504460746056646 0.0009041938441045365; -0.0024206354186105143 -0.0007735400330967953 0.0010431244818859147; 0.007369798294536007 -0.000862707443760429 0.009309044735810332; -0.02021238025322148 0.013784026017434703 -0.010598522172298475] %
+
+Mass Used: 88.09445296011882 kg
+Launch C3: 98.43290313159163 km²/s²
+||V∞_in||: 6.766944132244977e-8 km/s
diff --git a/archive/ES_0.5676872857661472 b/archive/ES_0.5676872857661472
new file mode 100644
index 0000000..eec90d2
--- /dev/null
+++ b/archive/ES_0.5676872857661472
@@ -0,0 +1,22 @@
+archive/ES_0.5676872857661472---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T09:11:04.589
+Launch V∞: [6.671306386628002, -7.370098577768718, 0.07611387899275472] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.80094754337804e-9, 2.5711125548995395e-9, -1.2881464821258293e-8] km/s
+ V∞_out: [-3.896308838496368e-9, 8.947457530994071e-9, 1.1998758964867933e-8] km/s
+ time of flight: 1.8749577787493524e8 seconds
+ arrival date: 2029-04-09T11:20:41.589
+ thrust profile: [0.13471835831375947 -0.031597632239798376 -0.04817521739791376; 0.08454667710715374 0.025570494504527502 -0.09375158631078963; 0.05534952064336281 0.03110361149763706 -0.1041203481359556; 0.03617790068723189 0.02534429518753933 -0.08851789038204286; 0.021074630657068407 0.01733282834746035 -0.0676856832133129; 0.033773346708648205 0.03670020604488983 -0.12652412616723369; 0.010654873928279601 0.013380117209990456 -0.05603188266362302; 0.018843667758889144 0.023941714547020248 -0.09513804263642027; 0.013834888794921129 0.02010985272862948 -0.08765617260106674; 0.0010739195030416402 0.003042001985783958 -0.008156853999104652; 0.013207337464301463 0.02047998537279258 -0.09197767833382126; 0.0007475216685139485 0.00020926560103115598 -0.0074151194380084546; 0.0009154927059550587 0.0008404247831211285 -0.006359385468752211; -0.00013879913445234964 0.0014911418912442942 -0.002839550454966514; 0.0009301568263319215 0.0031320199704160823 -0.0075189411807047996; 0.00041413186445588197 -0.0018474883422219795 0.0036900499807816824; -0.021082377542664295 0.004146063352493612 -0.005457374956089646; -0.00014235919346349164 0.0006916865679908665 0.00011062906365379068; 0.0010651728960431393 0.007730939842509055 -0.006409626789356368; 0.012605109321369918 0.005771683960926979 -0.024379793292498377] %
+
+Mass Used: 85.79072763544536 kg
+Launch C3: 98.83047527286737 km²/s²
+||V∞_in||: 1.5811370382499076e-8 km/s
diff --git a/archive/ES_0.567724857822523 b/archive/ES_0.567724857822523
new file mode 100644
index 0000000..accc193
--- /dev/null
+++ b/archive/ES_0.567724857822523
@@ -0,0 +1,22 @@
+archive/ES_0.567724857822523---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T14:11:54.212
+Launch V∞: [7.427776257929321, -6.035415981165043, 0.14793810962804455] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5525995710226555e-9, -1.2330996986388455e-9, -1.3413106161969448e-9] km/s
+ V∞_out: [2.2611374168922192e-10, -2.0579366162882323e-10, -1.6629693088986527e-10] km/s
+ time of flight: 1.665816486586214e8 seconds
+ arrival date: 2029-08-15T14:52:42.212
+ thrust profile: [0.8339686446292096 -0.11908572419122437 -0.22301278450396436; 0.073702585840878 0.03223961634071108 -0.06881852529512744; 0.04995412111051812 0.0381601077938995 -0.08019826855634825; 0.034414071210555654 0.03516027716290782 -0.07937932735480234; 0.10885199382974324 0.11786953991540619 -0.26419581391149966; 0.03271919814091252 0.048107496230744694 -0.12066111125297632; 0.021468775487294704 0.03553320528731806 -0.09606115234190425; 0.01770974935144904 0.032967714188035784 -0.09230192590892612; 0.0027227772797418764 0.0056946023087653275 -0.017185964793430524; 0.008710754790179116 0.01956433907905691 -0.05963420019193478; 0.0006899485578210453 0.00011009196284395093 -0.001970539575684668; 0.0009709766914757092 0.0017481623398858167 -0.008636097053097033; 0.0001524631406139934 0.0006624366246433854 -0.002455814918749662; 0.0011839859465584887 0.0008040904065869631 -0.003211055521843355; 3.5942303942727285e-5 0.00014568985374079183 -0.0006397655551600519; -0.0003899266599978185 -0.0008222251193256162 -0.00037326060015386675; 0.00017621529752819454 -0.0004606433484859614 0.002131882840286119; -0.00037880663472412637 0.0036304678758756945 0.0005932123849870675; -0.0002181038018221808 -0.00018464242052726183 -0.0003911807915392481; 0.0001429086710340667 0.00016664972776257703 -0.0015169216346502014] %
+
+Mass Used: 127.89571478053631 kg
+Launch C3: 91.61999188784124 km²/s²
+||V∞_in||: 2.393786637076407e-9 km/s
diff --git a/archive/ES_0.567753415838923 b/archive/ES_0.567753415838923
new file mode 100644
index 0000000..57c2c90
--- /dev/null
+++ b/archive/ES_0.567753415838923
@@ -0,0 +1,22 @@
+archive/ES_0.567753415838923---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T19:18:26.327
+Launch V∞: [7.665485503505424, -5.732716319061813, 0.41729385738094177] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7985378397184205e-6, 4.253456856791627e-5, 8.022708151405327e-7] km/s
+ V∞_out: [4.107152588579365e-5, -6.293002729162347e-6, 8.988153464650048e-6] km/s
+ time of flight: 1.7737676627393967e8 seconds
+ arrival date: 2029-12-19T18:37:52.327
+ thrust profile: [0.7855824133841153 -0.044371238564806445 -0.16730434413352255; 0.08675602384061351 0.05130828716933945 -0.0758503792621308; 0.05923358351638601 0.059068594281827744 -0.09194094233901166; 0.03956270181417239 0.05349801665599216 -0.09543624117065048; 0.030529239555683693 0.051759194358282815 -0.09806147237017349; 0.057708006409537244 0.10943575832967498 -0.20099614762181844; 0.022272119718483675 0.05300399786095766 -0.10582941909290784; 0.004664762666228081 0.013424785286608978 -0.03098864292161471; 0.003123642165001237 0.012739650058269339 -0.023782749043954582; 0.003177694753149582 0.008393826224133124 -0.02021499046609549; -0.00042070691562374617 0.0013048156265954977 -0.002708582956230726; 0.0032425793803779294 -0.00284936426285422 -0.0010540505996656617; -9.559707651952379e-5 -0.0010044000741318139 -0.002298865192714888; 0.0009140434929912086 -0.001977149326131292 -0.003388788923960541; 0.0008802009701980731 0.004399199719988292 -0.00716739501911662; 0.0005866698183456904 0.0044102650357468725 -0.001819523229591928; -0.00587530217200157 -0.0014802044777351654 -0.003975063992646721; -0.0027956432574588533 -0.0018174060085409233 -0.004853013756154075; -0.012044526548257729 0.00702292413970587 0.0022803816835184204; 0.003544471117742781 0.005033335726596269 0.014746968740280971] %
+
+Mass Used: 126.8915935296759 kg
+Launch C3: 91.79783856269731 km²/s²
+||V∞_in||: 4.258013504065594e-5 km/s
diff --git a/archive/ES_0.5677583776864666 b/archive/ES_0.5677583776864666
new file mode 100644
index 0000000..e70d953
--- /dev/null
+++ b/archive/ES_0.5677583776864666
@@ -0,0 +1,22 @@
+archive/ES_0.5677583776864666---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T02:17:15.102
+Launch V∞: [8.060201612486674, -5.340699366648273, 0.31385793639533544] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004101934182169158, 0.018921525466393342, 0.027191787362439] km/s
+ V∞_out: [-0.005738874429482497, 0.0050687296601388855, -0.03248741418229664] km/s
+ time of flight: 1.8749577785444352e8 seconds
+ arrival date: 2030-04-16T04:26:52.102
+ thrust profile: [0.5987066985885979 0.011864571581601603 -0.13313895485587135; 0.17555436136975172 0.12120667195088466 -0.14198942569786843; 0.06934557414967644 0.08403531167359633 -0.10783746619227666; 0.050105229966534895 0.0814318166777476 -0.11363775362501476; 0.04759927114421736 0.10430651449763485 -0.1605933985323142; 0.007586191826217003 0.021136899451477738 -0.03699683752321272; 0.00808799121725997 0.02482718896890503 -0.046844167350503896; 0.0016577530861585294 0.00832259098262539 -0.015892168880337672; 0.003193079168052507 0.01835782086148549 -0.03607895041575319; 0.000530707684930354 0.006270712447253657 -0.013394301600405271; 0.00017919773398912233 0.002173462342834441 -0.004901983933128522; -4.551686868702206e-6 0.0014255697919810712 -0.003285383456268821; 6.985323046919452e-5 -0.00019685391965886922 -0.0016109212228695832; -0.00019201610084873207 0.0009318668839226456 -0.0011196162840130357; 0.0010177257319341137 0.0015717905369651108 -0.0016636098657872773; 0.0010124284251444005 -0.0005210868758202506 2.0974254415052603e-5; 0.0005943072666373486 0.0010667087408334692 0.00010821979308559253; 9.893518322320202e-5 0.0003295851457116457 -0.0012852010136833768; -0.000510962524785073 0.0009990847075978305 -0.0013709998336914513; 4.2724713551060584e-5 0.00017389208448393583 0.0005798781255156539] %
+
+Mass Used: 116.45228568286211 kg
+Launch C3: 93.58842656308839 km²/s²
+||V∞_in||: 0.033380282952280634 km/s
diff --git a/archive/ES_0.5677653347350511 b/archive/ES_0.5677653347350511
new file mode 100644
index 0000000..b5a5d39
--- /dev/null
+++ b/archive/ES_0.5677653347350511
@@ -0,0 +1,22 @@
+archive/ES_0.5677653347350511---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T09:38:48.052
+Launch V∞: [6.094572811319612, -7.737687121144293, -0.09455402119875038] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.868208495706236e-9, -9.597573140215125e-10, 1.5084650434228387e-9] km/s
+ V∞_out: [-1.941270192261348e-9, -1.874553338720251e-9, -1.4618011277834994e-9] km/s
+ time of flight: 1.742612875989531e8 seconds
+ arrival date: 2028-11-05T07:33:35.052
+ thrust profile: [0.2550533091100862 -0.09375120737430193 -0.10255758962397805; 0.07363056792383253 0.009943104989117081 -0.08381717138000744; 0.09134120185856726 0.03183489855789114 -0.16942105554802467; 0.07676812757619705 0.03742897794152316 -0.1962175772741425; 0.0571327374069232 0.033479780440552206 -0.18488968433654948; 0.04044281068292081 0.027079072414481938 -0.15882328977793114; 0.009400666554943942 0.00701805751253274 -0.04483287893728764; 0.00824051330023685 0.006938522548355398 -0.04456323643412134; 0.0025993266348141785 0.0012256643967592457 -0.013829422152105518; 0.002433892552037288 -0.002850458343486899 -0.008982852570853815; 0.0018343399741606232 0.001536703748630602 -0.012246236318244445; 0.0012460699820458954 0.0014668139409992524 -0.009840252076702544; 0.002321167573305836 -0.00018774761576511277 8.362812182951054e-5; 0.00013499986749125896 0.0004945165237100102 -0.0038318599397936743; 0.001601406474374071 0.0010816218577484019 -0.0033812959402491427; 0.00534987757077458 0.004837862897197238 0.00406869546686379; -0.01177125478402804 -0.00021833657781229139 0.001566756963819946; -0.0013112389242786976 -0.0007417744732670277 -0.003099430658313253; 0.0014948278802266455 0.008628116955518874 -0.01052066138956385; 0.004706743637593069 0.00021648196522610938 -0.02913787730707071] %
+
+Mass Used: 96.41628935684002 kg
+Launch C3: 97.02456020012336 km²/s²
+||V∞_in||: 2.585885510318547e-9 km/s
diff --git a/archive/ES_0.5677709654726598 b/archive/ES_0.5677709654726598
new file mode 100644
index 0000000..0d2f2c5
--- /dev/null
+++ b/archive/ES_0.5677709654726598
@@ -0,0 +1,22 @@
+archive/ES_0.5677709654726598---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T14:13:31.576
+Launch V∞: [7.259024422719747, -6.303144857123804, -0.05693774525308276] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005400382466668833, -0.0016122703518110656, -0.0028897416490019467] km/s
+ V∞_out: [-0.0030241096174430286, -0.00032881715841851254, 0.00140332203716459] km/s
+ time of flight: 1.6429080586977932e8 seconds
+ arrival date: 2029-07-22T02:33:36.576
+ thrust profile: [0.643663126947355 -0.09514981881479269 -0.19302504628545158; 0.17976176793085727 0.0711914560252021 -0.16640377674322046; 0.06851336506213693 0.04827842117295629 -0.11308430580710979; 0.06620781917016928 0.06186548996533365 -0.15241138318313555; 0.04234606750286894 0.04830153823028655 -0.1289518480907039; 0.024341850899189405 0.03418142245280109 -0.09846067380214062; 0.011602837288321581 0.017534874242234544 -0.052120648983435; 0.02394506635960059 0.03943192063017792 -0.12229241399001815; 0.012823839858699788 0.023708703567496117 -0.07925885618256388; 0.0008766741772487773 0.007319602935864843 -0.0174205551822737; -0.0028665233870828716 0.007234121223437891 -0.01060242353362811; 0.0016444318730350221 0.0034531001774527536 -0.014963377212366335; 0.0035035684244447435 0.006210019904299693 -0.006514794915798676; 0.005014457545538884 0.0016540358902878251 -0.008970004185602957; -0.0018233436523928835 0.0029384920638513973 -0.006122142761928911; 0.002238226354057023 -0.0038031395941820817 -0.004249936175645584; -0.0015742702118800344 -0.003169755910165558 0.0010949080817050155; 0.00020984007342161233 -0.0006940891578798253 0.0015926153399540895; -0.0021247222708475283 -0.0011092014875930909 -0.015194729598691163; -7.02074657023117e-6 7.296417306567292e-6 -0.008801936419864636] %
+
+Mass Used: 123.24596974765518 kg
+Launch C3: 92.42631256636251 km²/s²
+||V∞_in||: 0.003352859047614216 km/s
diff --git a/archive/ES_0.5677759677318918 b/archive/ES_0.5677759677318918
new file mode 100644
index 0000000..8e05d80
--- /dev/null
+++ b/archive/ES_0.5677759677318918
@@ -0,0 +1,22 @@
+archive/ES_0.5677759677318918---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T22:30:35.588
+Launch V∞: [7.492325317290481, -6.420271382300467, -0.18296516358744883] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00022503730964692272, 0.014677978022372818, -5.593103023473342e-5] km/s
+ V∞_out: [0.014172336731023529, -0.002329653896765598, 0.0030331586739711777] km/s
+ time of flight: 1.6144566512144083e8 seconds
+ arrival date: 2029-06-20T12:31:40.588
+ thrust profile: [0.23048640667878004 -0.044981933960186814 -0.08567164416995751; 0.10559379277955629 0.033275526318316546 -0.11581923824782832; 0.09576609723706056 0.054460636378987834 -0.17585854715404134; 0.08176735298419745 0.06081515084538595 -0.2098841526743569; 0.05226726414452915 0.04640980047697939 -0.17400237043408026; 0.023796943329296955 0.02435545374279775 -0.09961395737508309; 0.013325449325206866 0.016708361194887687 -0.07491637461786911; 0.0168757195037242 0.015706557325112114 -0.07506960256460024; 0.013711849126439685 0.005803399303380337 -0.053539195620703535; 0.0028268221098984923 0.004997468996680807 -0.022502386230115377; 0.0029702133105283524 0.0007670206620530276 -0.01975852207034887; 0.0012359784796333274 0.002907075417702001 -0.010332381585420262; -0.008413161484301594 -0.0047312017595381875 -0.0018028294117199278; 0.00100094507455061 -0.0023983481291006284 -0.002566120196298106; 0.0006119339830405869 -0.0029965514018694458 1.2246491946025628e-6; 0.0011651190850978108 0.001284550606174559 -0.003034615379398708; 0.0025987047873964565 0.003686379195256116 -0.0034221196989255302; 0.004238073057032769 0.008117088787872317 -0.0019057632495062884; -0.0013108744365906175 0.00856429384956001 0.0036206040303062743; 0.00241580966141986 -0.011987005722001648 0.003461801110625778] %
+
+Mass Used: 94.30688174129546 kg
+Launch C3: 97.38829953358484 km²/s²
+||V∞_in||: 0.01467980956607189 km/s
diff --git a/archive/ES_0.5677827375004456 b/archive/ES_0.5677827375004456
new file mode 100644
index 0000000..603b3c3
--- /dev/null
+++ b/archive/ES_0.5677827375004456
@@ -0,0 +1,22 @@
+archive/ES_0.5677827375004456---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T14:37:18.426
+Launch V∞: [6.574564643351258, -7.487539091369941, 0.023849554506057517] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011913212285046115, -0.00036807333607113594, 0.008384900936992592] km/s
+ V∞_out: [-0.01402103342032745, 0.0001354501634688615, 0.0039659234894599505] km/s
+ time of flight: 1.8588780616831312e8 seconds
+ arrival date: 2029-03-23T02:07:24.426
+ thrust profile: [0.12002479394409171 -0.033372785714271325 -0.048287055669375065; 0.049694532651873034 0.010519402748142713 -0.06132615798154397; 0.06223504035843259 0.02781286743018792 -0.12460783365887307; 0.044730613672794496 0.026538699039678853 -0.1257283100165995; 0.03559987114324896 0.024648922987911676 -0.12765215386502252; 0.027312809837312286 0.02186648304129741 -0.12075524001703668; 0.02469882450435618 0.02056473551650964 -0.12264664335119184; 0.005551428845578802 0.005372207299019594 -0.03324382513817718; 0.008218935279756073 0.009207754945627025 -0.0582201200905541; 0.002259782435779648 0.004797750275751896 -0.029701291283015296; 0.002696256487252737 0.003081986045125678 -0.019532597100720184; 0.0010458929638925564 0.0009794942354661314 -0.008534299680409118; 0.00032895737792372134 -0.0017444720169388429 -0.0042344736868260065; 0.0012443951626166742 -0.0012479871773575018 0.0016968224541797652; -0.0012754646220446545 -0.003959324851514562 -0.0010902928522274046; -0.0011508165962463793 0.0028757319694998986 -0.001446719278482467; -0.008159527867785907 -0.0048824876040051805 0.0023801685276108034; 0.00031472058415908086 0.004432676433670577 -0.002848213196672412; 0.002620614754559733 -0.0032188203606430873 0.009053387448491528; -0.002499900146273726 -0.005431052525279882 0.05323252712577248] %
+
+Mass Used: 83.22904802590892 kg
+Launch C3: 99.2887106956476 km²/s²
+||V∞_in||: 0.014572805792038795 km/s
diff --git a/archive/ES_0.5677838407799115 b/archive/ES_0.5677838407799115
new file mode 100644
index 0000000..3032bd3
--- /dev/null
+++ b/archive/ES_0.5677838407799115
@@ -0,0 +1,22 @@
+archive/ES_0.5677838407799115---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-07T07:00:03.717
+Launch V∞: [6.496151880950448, -7.71493620821046, -0.20204870770651456] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.53445479990217e-7, -3.5128256904952562e-6, 1.8320950531748625e-7] km/s
+ V∞_out: [-1.296464102613566e-6, 2.8743510539146797e-6, -1.6086327578810643e-6] km/s
+ time of flight: 1.8749577784192434e8 seconds
+ arrival date: 2029-04-15T09:09:40.717
+ thrust profile: [0.05757174195281942 -0.017702040144737936 -0.028003543502175154; 0.021939635078594255 -0.0018265756167581534 -0.03246170293631848; 0.027767629091259412 0.005327149421170483 -0.07214907149805302; 0.04259109942865065 0.009201205373204407 -0.14301675788086524; 0.036939510982971005 0.008188409092718146 -0.15657713339216212; 0.022713613690956286 0.004807054572798935 -0.11451654584740414; 0.013145451340796066 0.0025999428451354794 -0.07156854491907497; 0.017552660292046444 0.0026965440742428987 -0.1136110947268397; 0.0054132257038857125 0.003948996359603735 -0.05263601938532758; 0.003934988836084271 9.559156050338829e-5 -0.02918460454357703; 0.0009921275314043122 -0.00011311435000712813 -0.010519943844527733; 0.0010158143544906002 -0.0009303795733971991 -0.005771610654400814; 0.0005464598228140692 0.0010306722472422376 -0.001251699761361486; -0.0010435402376930193 7.728904530973516e-5 -0.0025606474213294766; -5.1121355988639284e-5 -0.0006094920371223671 0.0001356110420428205; 0.0012097090908847062 0.003363493296765866 -0.003747206970075881; -0.0015120369022140067 -0.001472944090408185 0.0030977546799011157; 0.000101927660881155 1.4153656238322856e-5 -0.0002502530686196517; 0.003546274933178815 0.00399834937647779 0.0005729445910770434; 0.0018817253729332749 -0.004148868983646758 -0.00034754323318828765] %
+
+Mass Used: 68.80833469162098 kg
+Launch C3: 101.7610536374187 km²/s²
+||V∞_in||: 3.5467059164759784e-6 km/s
diff --git a/archive/ES_0.5677845493752545 b/archive/ES_0.5677845493752545
new file mode 100644
index 0000000..0e63142
--- /dev/null
+++ b/archive/ES_0.5677845493752545
@@ -0,0 +1,22 @@
+archive/ES_0.5677845493752545---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:37:31.856
+Launch V∞: [7.5870485480161465, -5.552004169384681, 0.15658035747649293] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.63712432782853e-5, 0.000890109539057718, 1.7887488272046998e-5] km/s
+ V∞_out: [0.0008614060117585369, -0.0001252008228240578, 0.00019203264926250053] km/s
+ time of flight: 1.8749577787339693e8 seconds
+ arrival date: 2030-04-17T00:47:08.856
+ thrust profile: [0.8748695540246103 0.023680052734306963 -0.1730677700191265; 0.27691791461760984 0.19352640372190416 -0.20213590662510925; 0.0709890407459918 0.08709467007587379 -0.1066288641614993; 0.040953067233091556 0.07135492848201329 -0.0973457345337761; 0.023467431796912408 0.054158762140178014 -0.08064866140859384; 0.008343172757643399 0.024712848168866434 -0.03957003515344767; 0.006339198778627141 0.02494358117358123 -0.04205999915594589; 0.01114727607922554 0.05534131630802637 -0.09586202846425174; 0.002218153490063514 0.010349370803228883 -0.021117550155272106; 0.002095361037826703 0.0030230207806405188 -0.0041672013665881484; -0.00044844685271618685 0.0012643353980911873 -0.002179428950246484; -0.0014445187551816283 -0.003642827322598983 -0.002612734516789261; 0.002318910159765755 -0.0015644467667167501 -0.0016602840443237221; 0.0009085780791376463 -0.0005996738338693345 -0.0019346693487947398; -0.004621534707825116 -0.0027003665018988862 0.0012368173946377412; -0.0033235859425451144 -0.0024544456612848875 0.0012955748072217158; 0.0006450968271053996 0.0018001450269694854 -0.007946134620189844; -0.001284796435344542 0.009297568199758842 -0.0016271792702685674; 0.0019047443440889575 -0.006544403784647207 -0.013993283606944741; -0.003103842933503939 -0.0008375621891685182 0.0014093051128232833] %
+
+Mass Used: 146.67529624932695 kg
+Launch C3: 88.41257337516626 km²/s²
+||V∞_in||: 0.0008910318855662989 km/s
diff --git a/archive/ES_0.5677853780561469 b/archive/ES_0.5677853780561469
new file mode 100644
index 0000000..42b27fb
--- /dev/null
+++ b/archive/ES_0.5677853780561469
@@ -0,0 +1,22 @@
+archive/ES_0.5677853780561469---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T01:32:11.709
+Launch V∞: [7.566614513480463, -6.374810950799066, 0.04642903436011118] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0001008531692313752, 7.851361923492293e-5, 6.481719480484715e-5] km/s
+ V∞_out: [2.545462422452501e-6, -0.0001417662615137303, 2.1832424408842634e-5] km/s
+ time of flight: 1.8749577781384724e8 seconds
+ arrival date: 2030-04-29T03:41:48.709
+ thrust profile: [0.38754823722635856 0.032896843983985055 -0.13255035345734426; 0.06513135652603012 0.03844589499197729 -0.07535959716006674; 0.06366427077960635 0.06304927871996881 -0.12871531590754784; 0.0544666972863701 0.07557765304195758 -0.1658100212172376; 0.03785968583214431 0.06096228730597079 -0.14973730467870658; 0.018776670913632484 0.0302444755436726 -0.08781555927423196; 0.00781555957886378 0.014174766231000151 -0.04719910001530658; 0.0013244568597500378 0.0024553998507653944 -0.007782534910908154; 0.0009450371412865557 0.000968244883465935 -0.0022905319950628274; -2.2150656047688013e-5 0.0012386515419195814 -0.002449168178683191; -0.0005062219432911603 0.001819198541371333 -0.0020818465702858815; 0.0007647037436868102 0.0007396922743740902 -0.0024179782267768233; 0.00041819789748383696 1.6425646155756213e-5 -0.002066343131261239; -0.000701952576994547 0.00032431640494307224 -0.0037297236676667664; -0.0024605379025115434 0.001789357933094335 -0.0013454585654929195; -0.000947075682779352 0.0013346901519642842 -0.0011788632203359906; 0.002203817722154532 0.00027980289060528305 -0.0006242498133304597; 0.003994879120647134 0.003653087379722337 -0.002206857402337354; -0.00022771195442377196 -0.0031503365684231446 0.0024135692243671056; 0.0023801235170620673 -0.003823571119549727 -0.003798776504752443] %
+
+Mass Used: 91.36779226141516 kg
+Launch C3: 97.8940255092725 km²/s²
+||V∞_in||: 0.0001433074279015166 km/s
diff --git a/archive/ES_0.567797245174017 b/archive/ES_0.567797245174017
new file mode 100644
index 0000000..cffc2fe
--- /dev/null
+++ b/archive/ES_0.567797245174017
@@ -0,0 +1,22 @@
+archive/ES_0.567797245174017---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:03:56.240
+Launch V∞: [7.533285132078942, -5.551985837300402, 0.4402369744495285] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.12790179605950838, -0.7528299727119222, -1.0911756051234183] km/s
+ V∞_out: [0.5935915991170224, 0.2664755065529041, 1.160355649916011] km/s
+ time of flight: 1.8749577787483972e8 seconds
+ arrival date: 2030-04-17T00:13:33.240
+ thrust profile: [0.9582014917216203 0.02888031786564003 -0.18513349358118542; 0.2417265944664786 0.16750906470581128 -0.17360359056465757; 0.1040310110473779 0.12254816013013761 -0.1424236675151115; 0.03822110089947698 0.06574294050577648 -0.0864679261826013; 0.010414714104471834 0.023866000886770333 -0.036566635140490154; 0.01871529875247953 0.047935246801179936 -0.07795691127303839; 0.0021018301412356662 0.00815917409389223 -0.014578404759071763; 0.0031919450444188313 0.019322151766182266 -0.04123746374710114; 0.005564240396465116 0.037643994626009473 -0.06849033436662814; 0.0013683998356295091 0.00877975057681555 -0.017542043684729423; 0.003501096835016732 0.003483331358237208 -0.010323553739882935; -0.0002944503979315998 0.0012720992125900517 0.0009253591191006342; -0.004283930533580451 0.0037594192980190343 -0.004555291616592152; 0.001136357212596858 -0.0014230192945954125 -0.0035963180607770655; -0.0042266231674107264 -0.0011927958794833793 0.003009566583217255; -0.007861639075931022 -0.0006911732934303215 -0.00011083722528083904; 0.0015103104817288519 -0.0037749267146626065 -0.002141985158339242; -0.0003866587182337673 0.006877060215817871 0.0024170915852545867; -0.012767308699497496 -0.002454510924641491 0.003505379353989688; 0.0025314598818125793 -0.002253786013653651 -0.004422453529088183] %
+
+Mass Used: 150.44580146367935 kg
+Launch C3: 87.76874021245835 km²/s²
+||V∞_in||: 1.3318318356553651 km/s
diff --git a/archive/ES_0.5678175720381111 b/archive/ES_0.5678175720381111
new file mode 100644
index 0000000..55eb264
--- /dev/null
+++ b/archive/ES_0.5678175720381111
@@ -0,0 +1,22 @@
+archive/ES_0.5678175720381111---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T05:09:58.506
+Launch V∞: [6.340769891809116, -7.706389727835739, 0.0777981860562272] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0896353631001241e-6, 0.0003222450643722291, -0.00023398769055155207] km/s
+ V∞_out: [-0.00017752335975666452, -0.00034902268329826903, 7.2472811063281e-5] km/s
+ time of flight: 1.7666424207409805e8 seconds
+ arrival date: 2028-12-04T22:34:00.506
+ thrust profile: [0.11944834413345085 -0.0464042500533586 -0.056243026370198596; 0.025521323912104543 0.0013620461073862913 -0.03738491778719472; 0.054017921091778845 0.01366741402630705 -0.13006321191951056; 0.05797214155042098 0.023818251184679857 -0.21932437225495668; 0.0406270228491106 0.015972010741811364 -0.16965939341939917; 0.02776288785625379 0.010837090352306933 -0.13571646113143848; 0.014678920781208521 0.004771771468574107 -0.08385381692345611; 0.0065512686078412164 0.0031892016312346193 -0.0447245038915759; 0.0052392945009996856 0.001497016208981653 -0.0334479254367612; 0.005261729464014457 0.0008223353662962303 -0.017474459900249845; 0.001988403535535668 0.0010430586835444506 -0.017903707062799517; 0.008763627078890864 0.0033041985538991405 -0.008545923854256527; 0.0034118200706676734 -0.003118606268183956 -0.007028406187481793; 0.0015902823462089267 -0.0017895963841531898 -0.0066306589084760715; -3.447957059167679e-5 7.103164850291298e-5 -0.005792686271077371; 0.0008629791153431089 -0.0040825650166393095 0.0017240624478504782; 0.00546312476927693 -0.004814061472377137 -0.014525033086255065; -0.0093374850705573 -0.0031291108492675925 0.002300751947644911; 0.00788489148036759 -0.005673549138786444 -0.015158590444024022; -0.00304051042366521 0.0028173031184756314 0.0033922426084776547] %
+
+Mass Used: 81.4546622849366 kg
+Launch C3: 99.59985801591881 km²/s²
+||V∞_in||: 0.00039823775329209495 km/s
diff --git a/archive/ES_0.5678327390873191 b/archive/ES_0.5678327390873191
new file mode 100644
index 0000000..5a7c222
--- /dev/null
+++ b/archive/ES_0.5678327390873191
@@ -0,0 +1,22 @@
+archive/ES_0.5678327390873191---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T08:30:30.530
+Launch V∞: [6.327150994338717, -7.300589894310879, 0.1349969732233181] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.356963672153061e-9, 8.519391680572174e-9, 2.756522736454775e-9] km/s
+ V∞_out: [-2.7605357053685307e-9, 4.469816814188087e-9, -6.9184194107496786e-9] km/s
+ time of flight: 1.851136296860527e8 seconds
+ arrival date: 2029-03-09T20:57:39.530
+ thrust profile: [0.5842645873733785 -0.14298802908340347 -0.15911614535027202; 0.08135011868655016 0.0272209064697964 -0.0778257077141919; 0.06023705046320711 0.03806543644247864 -0.09587235479552071; 0.03834302031778837 0.030047492315034733 -0.08108794167853117; 0.02664277856897945 0.02959832240653114 -0.07975968836330995; 0.017969431181270076 0.024980345706766893 -0.07338653888852348; 0.018905860747908714 0.025768143342170494 -0.07468654392410705; 0.037840933799297094 0.06409006806797049 -0.1801161418204626; 0.015823220564943542 0.028557174250911498 -0.0910121660429822; 0.008394544128336805 0.010001815152447724 -0.037287300330011076; 0.0022930863005117103 0.00476700920484078 -0.01686224321779413; -0.0004026354816722061 0.00013723563087095924 -0.0007465321509084306; -0.001318939639928466 -0.0047133961203547235 0.0004888291244048358; -0.002522279532554207 -0.0014317800567816442 0.0016785009312348313; -0.0019644678916117568 0.00029424034684230474 0.0033234106484132404; -6.934921818377835e-5 0.0012865789341098984 -0.0008889034557697935; -0.008513510536810171 -0.0012625724018052863 0.0019622189939669885; -0.006368786644833011 0.00034138384127925986 0.006133599915421041; -0.005835498092317143 -0.007609692882557026 0.009876458550401637; -0.0018039315803502565 -0.0023334332579252113 0.001047886174545057] %
+
+Mass Used: 117.93174822688479 kg
+Launch C3: 93.34967669285501 km²/s²
+||V∞_in||: 1.0434342911192928e-8 km/s
diff --git a/archive/ES_0.567833647951001 b/archive/ES_0.567833647951001
new file mode 100644
index 0000000..af35e05
--- /dev/null
+++ b/archive/ES_0.567833647951001
@@ -0,0 +1,22 @@
+archive/ES_0.567833647951001---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-06T02:25:17.475
+Launch V∞: [6.360553868883498, -7.7382022904729775, -0.7839358054501548] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.823273638106202e-9, -2.183684369083182e-9, 4.980008865051804e-9] km/s
+ V∞_out: [1.7812969786348185e-9, -4.3450936277471585e-9, -6.4846285867772215e-9] km/s
+ time of flight: 1.8573771863745135e8 seconds
+ arrival date: 2029-03-24T20:13:55.475
+ thrust profile: [0.13316985643198542 -0.040061107018844924 -0.06216520158403339; 0.017308997774939147 0.0027128398254985964 -0.02426533205632789; 0.02942437007546502 0.010103263846853078 -0.06943854325406028; 0.05276125290051506 0.02435250395668011 -0.17156105878291408; 0.031645753053954284 0.01686949602662674 -0.13347504052764703; 0.03010618286154444 0.017774404198956654 -0.15262305934876916; 0.013388428482253478 0.00837642824833505 -0.08011901980707221; 0.009269982732447907 0.0057850332843406545 -0.06430929773088127; 0.003271315121664944 0.002413417855250405 -0.02459122775168462; 0.0047796912048032 0.0033162598011984494 -0.040540430553434356; 0.0032623599869729372 0.0018991611237349042 -0.028024592773430206; 0.0008644022128305669 0.0005232365627181912 -0.0076643638794364295; 0.00024134255984795602 -5.315698912019103e-5 -0.0016841772590956304; 0.0002444628434871033 3.636327540118344e-5 -0.0025972717571064717; 0.0007079052927678294 0.0008405987257860404 0.00010061834394704876; -0.0001552767664383945 -0.0007122132640364222 -0.0015309774735084805; -0.0004405930699998938 -4.3912465431646995e-5 -0.0008065882376547258; -0.00021672959112486702 0.0012416424536153335 0.0004121088919716708; 0.0006001020995985018 2.5520207511274887e-5 0.0006137826841000999; -0.00059847901798403 -6.010797281447177e-5 -0.0016687911318402397] %
+
+Mass Used: 73.59189854265287 kg
+Launch C3: 100.95097555431686 km²/s²
+||V∞_in||: 7.967401181315988e-9 km/s
diff --git a/archive/ES_0.5678377967123315 b/archive/ES_0.5678377967123315
new file mode 100644
index 0000000..25367b6
--- /dev/null
+++ b/archive/ES_0.5678377967123315
@@ -0,0 +1,22 @@
+archive/ES_0.5678377967123315---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:59:22.953
+Launch V∞: [7.369351703483594, -6.308482901208502, 0.012857896939299774] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.322052265280703e-7, -6.042191000758378e-6, 1.1567348244570679e-6] km/s
+ V∞_out: [-8.689952281398026e-7, 3.946957681349627e-6, 4.69551434129927e-6] km/s
+ time of flight: 1.6506613167778164e8 seconds
+ arrival date: 2029-08-01T04:41:33.953
+ thrust profile: [0.4718278697182551 -0.0791121863067971 -0.16309125734805896; 0.1644688025795601 0.05767307393805667 -0.17392908934211504; 0.13743550782003558 0.0850283363461681 -0.24683654362351826; 0.053803807039009346 0.04352642695958247 -0.1404753875346044; 0.038018408808524015 0.03670001174928372 -0.13013703335795349; 0.023672636112467862 0.02680361812226329 -0.10033821613928859; 0.009581460555530314 0.012265730037016833 -0.050292139662162824; 0.008213898505686027 0.011119436634717053 -0.04782211990102151; 0.006610813486753422 0.006956545586830998 -0.033096675194408974; 0.0028095440591607004 0.0067019285346669 -0.03063214744450906; 0.00020681140590558193 0.0022835021377696886 -0.006357055377006137; -4.637534003189064e-5 0.0016150556754620875 -0.003132214399744906; 0.0019528684229172396 -0.0024460937188053654 -0.0025543465150871; -0.003585678494904384 0.002388156373028261 -0.0021529694972802953; 0.0003151563369872004 -0.0029129097788604965 -0.010484958365814156; -0.010479566466007534 0.005662718596284437 0.0016244961657169437; 0.004404826192783931 -0.0029048456004653247 -0.0016291483896159792; 0.01360052370156227 -0.0017071293834028049 -0.00038455266360609783; 0.001712218050815085 -0.01757906825276659 -0.02331052623128946; -0.011770621373364144 -0.00719674259941268 -0.011816159841138856] %
+
+Mass Used: 113.53470900611 kg
+Launch C3: 94.10446636999029 km²/s²
+||V∞_in||: 6.195339541745252e-6 km/s
diff --git a/archive/ES_0.5678380604189023 b/archive/ES_0.5678380604189023
new file mode 100644
index 0000000..a126bce
--- /dev/null
+++ b/archive/ES_0.5678380604189023
@@ -0,0 +1,22 @@
+archive/ES_0.5678380604189023---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T20:54:13.652
+Launch V∞: [7.447474689730845, -6.3841841075933115, -0.2841620728003198] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4914339239056026e-7, 3.491546067771258e-7, -1.7376542459354107e-6] km/s
+ V∞_out: [-4.3870514115924976e-7, 1.7199944960813594e-6, -2.6364132901842323e-7] km/s
+ time of flight: 1.6156805593889597e8 seconds
+ arrival date: 2029-06-21T20:55:08.652
+ thrust profile: [0.37296349594158656 -0.07355268065779008 -0.14409128718888542; 0.09646816653276843 0.02914415224897495 -0.11388301868638323; 0.07868875614394413 0.04333572897695322 -0.15751510409915373; 0.054853819564012876 0.03935105917661323 -0.15515383006515016; 0.03495220321356568 0.029368421025494914 -0.1273932211126498; 0.030549892777152147 0.02917646759307495 -0.13484417477145627; 0.014453066693133206 0.014483407101997097 -0.07416035453098399; 0.01606786554288817 0.017644551304302113 -0.09401893966667468; 0.013225848639752005 0.015216285365189767 -0.08657056827877878; 0.005511982492485891 0.006281822302447914 -0.03817892481280454; 0.0020040412424147383 0.002066796212098956 -0.013369535171369728; 0.00035873048174784716 0.0009390755842486357 -0.003434245907533909; 0.00026052965135905514 0.0016236134889767743 -0.002646434820465388; -0.0019706741119344755 0.006198237216860405 -0.005068701740811681; -0.009510634638895074 0.00745681839149005 -0.01147784271809853; 0.0011667222453723512 0.0010207702513445735 -0.0009361155138061933; 0.0034457994629876585 -0.004228793579764007 0.0009544890454913713; 0.0019310702510576378 0.0014740680915537032 0.0011813758489223692; 0.00174153012967607 0.0022076835201700114 -0.015460884439551924; -0.006369646823363741 -0.00017905328794529953 0.0018733476517389545] %
+
+Mass Used: 100.70770515361346 kg
+Launch C3: 96.30343405744672 km²/s²
+||V∞_in||: 1.7898110648397856e-6 km/s
diff --git a/archive/ES_0.5678424261441046 b/archive/ES_0.5678424261441046
new file mode 100644
index 0000000..e3d0305
--- /dev/null
+++ b/archive/ES_0.5678424261441046
@@ -0,0 +1,22 @@
+archive/ES_0.5678424261441046---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T07:49:16.579
+Launch V∞: [5.69286029321763, -7.80793706348919, -0.11214793442381721] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.398256636643358e-9, -1.7496860814080073e-9, 9.964142088650842e-10] km/s
+ V∞_out: [7.778577044272259e-10, -1.7738456370886248e-9, -2.5657663916683672e-9] km/s
+ time of flight: 1.643403350880775e8 seconds
+ arrival date: 2028-07-09T09:54:51.579
+ thrust profile: [0.5076923735685248 -0.2140172308869211 -0.18685825157845978; 0.13850636316469414 0.01574973440924452 -0.1384797471322491; 0.17815776080671258 0.061666509430226536 -0.2806456908876134; 0.06035492609655083 0.030612560440203107 -0.13364343116301627; 0.08079847377649811 0.04986674974122942 -0.22072620116827474; 0.015346899926393777 0.011016759195275842 -0.05292593403468669; 0.0077092708310304075 0.00604396920674463 -0.031037501745296427; 0.022911740816658147 0.021767407193664885 -0.10614882206151809; 0.0034916792468177695 0.002987055527657828 -0.017168322963684115; 0.006290937269259747 0.006651238188555122 -0.03144365812091147; 0.005024047995662537 0.004437254714019852 -0.030256858797545142; 0.0007771422622455602 0.001092554210369397 -0.00727000745085959; 0.0002241325840271382 -7.856086612003472e-6 -0.000994119740210198; 3.0286171577781416e-5 0.0002795786037642153 -0.0003699908991241746; 0.0001388412660899938 0.0006439869997562245 -0.00037052903211442893; -1.0097223937344506e-5 4.560769445618486e-5 -0.0002173665988063542; 3.703676271995355e-5 0.00021441918602347948 -0.00015553164576614345; 0.00012082330991254783 -0.00020344167285607517 -0.0005608655896697404; -1.854247230925662e-5 -0.0001551333559341971 -0.0004216785507257086; 5.3223537672113296e-5 0.0004770742841392005 0.00026157784240847374] %
+
+Mass Used: 117.7363166240525 kg
+Launch C3: 93.38511666469765 km²/s²
+||V∞_in||: 2.4514004734066473e-9 km/s
diff --git a/archive/ES_0.567850330783661 b/archive/ES_0.567850330783661
new file mode 100644
index 0000000..ed946fd
--- /dev/null
+++ b/archive/ES_0.567850330783661
@@ -0,0 +1,22 @@
+archive/ES_0.567850330783661---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T04:03:28.297
+Launch V∞: [6.347660233951283, -7.580397403668179, 0.004093794698689483] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.353181226172527e-10, -1.3088978261434531e-9, -2.461416823258656e-9] km/s
+ V∞_out: [3.183510067804079e-11, 3.9518603396101955e-11, 2.3452051193292472e-11] km/s
+ time of flight: 1.7947740341305825e8 seconds
+ arrival date: 2029-01-05T10:53:31.297
+ thrust profile: [0.22939058740648607 -0.0737450550867071 -0.08814359900162703; 0.04952799566681765 0.007942177256167278 -0.05430044564626833; 0.06330478760867873 0.02608235048371544 -0.11804983393502756; 0.059086546182294114 0.03314052568687739 -0.15141802080186312; 0.038744778374384725 0.02602066820456048 -0.12690612634258674; 0.020979597655277262 0.015426876376473888 -0.082802827077983; 0.019289563907184237 0.01641705577151635 -0.09123915444223255; 0.019870329305863466 0.017962703730514635 -0.1035616593784958; 0.01592501611885354 0.01488448863369899 -0.09187466640665143; 0.005228414040471829 0.006171974866467815 -0.04015307646522174; 0.0018191902661237947 0.002120185710751483 -0.011241061503772565; -0.000859668928208851 0.0011281191829501068 -0.004349983315200767; -0.0038345691262908627 0.004352950871052303 -0.009927692946373325; -0.0012486748959559773 0.0026325648818961473 -0.0013370989542300588; 0.0028417849882227822 -0.003638386888702801 0.0001565454706729504; -0.0009036244787936397 0.00023033721112851403 -0.0028859960144324006; -0.0024713471852538978 -0.004917647828031514 0.001204772055924121; 0.016389929265758288 0.00960235805978171 -0.016444093553541782; -0.0024482128850152243 -0.002715089843983347 0.013324042493681857; -0.0007782530131184156 -0.005841938216878126 0.014735282700175094] %
+
+Mass Used: 92.25319923371671 kg
+Launch C3: 97.75523200238077 km²/s²
+||V∞_in||: 2.910247869697116e-9 km/s
diff --git a/archive/ES_0.5678672226313797 b/archive/ES_0.5678672226313797
new file mode 100644
index 0000000..756f30c
--- /dev/null
+++ b/archive/ES_0.5678672226313797
@@ -0,0 +1,22 @@
+archive/ES_0.5678672226313797---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T14:37:30.503
+Launch V∞: [6.429344967803953, -7.473807305282587, 0.10710426993327304] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.133625224148724e-6, 4.044722794356637e-6, 4.445587538262537e-6] km/s
+ V∞_out: [6.154583220529396e-6, 3.914771573747615e-6, 1.2731542714105543e-7] km/s
+ time of flight: 1.816574197455463e8 seconds
+ arrival date: 2029-01-30T03:01:09.503
+ thrust profile: [0.25887695964854496 -0.07516895475988246 -0.09342567775929572; 0.0798010056234114 0.018495365022832288 -0.08716714596024253; 0.05936564187431593 0.02828152145537104 -0.10806355323864549; 0.05411595280939814 0.03524821882003849 -0.13679940461639542; 0.03521380542957351 0.02739390948229015 -0.11347688874311668; 0.03144773150936549 0.028224119887304507 -0.12296436082259161; 0.01760783595341373 0.018038083798037695 -0.08406630905638254; 0.008963519641656663 0.009244789876310548 -0.047806569836803085; 0.005497174101460221 0.005993330486728922 -0.02823527040888945; 0.010259503179939008 0.011650291326975367 -0.06412692045662027; 0.00851344527714332 0.010889691847062054 -0.0581222349065098; -0.0004976423948047644 0.0014758385609880392 -0.006123167057929689; -0.004548620887929769 0.002615404493234504 -0.0030967985647412342; -0.006707404786343593 -0.0001558845884924862 -0.00923053978535325; 0.007928841578349008 0.008939641684501308 -0.004568168330129193; 0.0006915777485686364 -0.0041873836307207285 -0.00060735860339719; 0.014620454706177073 0.005087450179281205 -0.006458998275310566; 0.00459625551887723 -0.001991438214326016 -0.016764666412726417; -0.00715245612314274 -0.003913391688815779 0.004266993811849536; -0.0017791999062974455 0.0025846896025808258 0.007958805527483076] %
+
+Mass Used: 95.47825495901361 kg
+Launch C3: 97.2057436761593 km²/s²
+||V∞_in||: 7.2945108497596955e-6 km/s
diff --git a/archive/ES_0.5678715614517589 b/archive/ES_0.5678715614517589
new file mode 100644
index 0000000..bce7a8b
--- /dev/null
+++ b/archive/ES_0.5678715614517589
@@ -0,0 +1,22 @@
+archive/ES_0.5678715614517589---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T13:21:26.165
+Launch V∞: [5.988159282014351, -7.569380240415951, 0.02162040500992213] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9212396808034432e-6, 0.0006151800354577331, -0.0002509682813179236] km/s
+ V∞_out: [-0.0005624331765286695, -0.0002724700516386389, 0.00022524684280803416] km/s
+ time of flight: 1.7435867193091536e8 seconds
+ arrival date: 2028-11-03T14:19:17.165
+ thrust profile: [0.5779582968456047 -0.18245031905580658 -0.18408499156186633; 0.09951002454246748 0.02243894639616844 -0.09553465969061202; 0.05947394422696235 0.02943890980589889 -0.09393172802550073; 0.05396630176222698 0.03670736821944001 -0.11736541528810321; 0.04884600802818419 0.04021345228413863 -0.13189270860502164; 0.04688297420998583 0.044232487311180395 -0.15045487572465654; 0.0477706947220911 0.05090283651625029 -0.17425053518246494; 0.012459698147449854 0.015396402531080702 -0.06081105346836336; 0.0066838882822385206 0.00861557694249781 -0.033600140614551625; 0.0028472952906119803 0.004249769215222996 -0.01735430279084041; -0.001422352540646244 0.0004749712656565187 -0.0029004607832429355; 0.0009773936787711751 0.0013496033184090092 -0.012573571288728668; 0.0011741508880565039 0.0021396703728876693 -0.00882849545444575; -0.0001995916120700323 0.004548171947058839 -0.0013690492490317206; -0.0025428070926748537 0.00403230811271416 -0.00012761558603919913; 0.0039113633506289635 -0.002995407061701819 -0.004874452768401161; 0.008744131032412934 -0.0014298096227383533 -0.012562360404947492; 0.001068559428649174 -0.00039497280160769504 0.005153833801850291; 0.0005146245025731274 -0.007515110185668927 0.00040426527528529977; 0.000790959737048783 -0.005005754353311258 -0.0067385025736306225] %
+
+Mass Used: 119.11827688637868 kg
+Launch C3: 93.15403625268685 km²/s²
+||V∞_in||: 0.0006644059342114287 km/s
diff --git a/archive/ES_0.5678803402111968 b/archive/ES_0.5678803402111968
new file mode 100644
index 0000000..e266842
--- /dev/null
+++ b/archive/ES_0.5678803402111968
@@ -0,0 +1,22 @@
+archive/ES_0.5678803402111968---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T02:01:38.810
+Launch V∞: [7.384036612549028, -6.588768469241414, -0.2450092421128188] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009867215399355169, 0.0049517212675390014, 0.00037497914250691545] km/s
+ V∞_out: [-0.008285073250333088, -0.004601373285798476, 0.005675082817163252] km/s
+ time of flight: 1.5729500586986607e8 seconds
+ arrival date: 2029-05-03T15:05:03.810
+ thrust profile: [0.22991984637866628 -0.047212319428707225 -0.09141684660665012; 0.07627247100169199 0.022013782532326318 -0.08633361999487658; 0.077277317916162 0.04107463332911927 -0.14612838940784065; 0.05747248478806942 0.04289928354514213 -0.15560947434281622; 0.07245544422930436 0.06241586173392049 -0.23264418409620122; 0.041543275067789015 0.041548379370299544 -0.17423775662675628; 0.015165815809294275 0.01609233693768759 -0.07473093516874334; 0.02336903148312419 0.02796099351939709 -0.12682461880240226; 0.005948567875590818 0.007024357203318063 -0.03549190601076236; 0.005364356894045026 0.006554609883301367 -0.03442766125358477; -6.706726220848884e-5 -5.41122440152848e-5 -0.00040708753684481945; 0.0005176676150549263 -0.0011209047656536865 -0.003822314751971816; -0.00023364780434022834 0.00023041648126727896 -0.0017318902217658338; 0.0001667391000773209 0.00021687391866780868 -0.0018593434830659287; 0.0005173993980891062 -0.0016865321545447127 0.0012992262704817309; -0.0004243363382316383 -0.0017048303058129516 0.0020097076771309636; 0.0010244679652404976 -0.0017091933647462186 0.0011964891220126814; -0.001076203520018845 -0.002480837629454311 0.0026683412391175594; -0.0008063106475087562 -0.0007034179514560879 -0.00014790667247338931; 0.0009443029655297116 -0.0008077235942627814 -0.002336224229189174] %
+
+Mass Used: 90.88433594790831 kg
+Launch C3: 97.99589616545508 km²/s²
+||V∞_in||: 0.011046361057198206 km/s
diff --git a/archive/ES_0.567880374378348 b/archive/ES_0.567880374378348
new file mode 100644
index 0000000..db745b0
--- /dev/null
+++ b/archive/ES_0.567880374378348
@@ -0,0 +1,22 @@
+archive/ES_0.567880374378348---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T15:22:28.051
+Launch V∞: [6.258501477929988, -7.347835212413451, -0.00829225710963506] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.173043493958193e-7, 2.6775449977475257e-7, -2.7251728085500735e-9] km/s
+ V∞_out: [-1.8369896349788941e-7, 4.699518701856625e-9, 9.409820167396086e-7] km/s
+ time of flight: 1.8112709800484627e8 seconds
+ arrival date: 2029-01-21T00:27:26.051
+ thrust profile: [0.5731890205287018 -0.1582254099086123 -0.17507127926776975; 0.12580760966303361 0.038000538708370515 -0.11896475519107383; 0.05728303242769524 0.03425686381959345 -0.09301734160705495; 0.06977578241737224 0.05730610908742459 -0.15313215287068882; 0.03300534311019067 0.0333961161418305 -0.0965147004255302; 0.013845423694425908 0.01620714244491337 -0.05067189767434314; 0.019594657427615708 0.025901489713935 -0.08267532387093453; 0.011455627184552583 0.015637682448419024 -0.05668524604851248; 0.027839847685840705 0.04578645770930437 -0.14829844389805844; 0.00798542665439116 0.014452473809806047 -0.05118834920078692; -0.00012615921654632106 0.0003135313402060601 -0.0007291522836138837; -0.00025380919128890867 0.0004238828625588481 -0.0013139474682943137; 2.3362581757821954e-5 0.0010059446869504869 -0.0009663451873426817; 0.0005687456532134387 -0.0002166786351837295 -0.002464593274145568; -2.81522208902007e-5 0.0017505658573362518 -0.0051073764098298734; -0.002439103491857626 -0.001745256572643399 0.0002947233307730177; -0.001148940176056773 0.0018547866773298855 0.002733670814481972; 0.0005507876606740125 0.005078815555671846 -0.0016382984402797006; -0.0033451863717142245 -0.0017897794619603348 0.009459162062655091; -0.0008054965967051808 -0.004968475937817449 0.0028574372585164435] %
+
+Mass Used: 119.09615116062287 kg
+Launch C3: 93.15959181956283 km²/s²
+||V∞_in||: 9.55587341971916e-7 km/s
diff --git a/archive/ES_0.5678924488230581 b/archive/ES_0.5678924488230581
new file mode 100644
index 0000000..2a96769
--- /dev/null
+++ b/archive/ES_0.5678924488230581
@@ -0,0 +1,22 @@
+archive/ES_0.5678924488230581---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T09:35:59.623
+Launch V∞: [7.471133990067734, -6.302785354910629, -0.030287440571558695] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.036582738514095e-7, -1.3272706578060007e-6, -1.3316591498766868e-7] km/s
+ V∞_out: [1.1121502572888565e-7, -5.847897528558817e-7, -1.4968998505396785e-6] km/s
+ time of flight: 1.6311611068325883e8 seconds
+ arrival date: 2029-07-09T07:37:49.623
+ thrust profile: [0.4193850962144025 -0.07649080291428668 -0.152786243906278; 0.07877394892113353 0.024846750799779146 -0.0910314525123617; 0.10876501859085777 0.062082849981827025 -0.2098961232489285; 0.059559277520507235 0.04416730796709765 -0.1641139223937636; 0.07015599172399767 0.062342706430943515 -0.2479563170356856; 0.02341371066899971 0.02324330623944953 -0.10262207535341107; 0.012519367672967146 0.01333357059101852 -0.0644669872104568; 0.008111662305662464 0.009446046662636222 -0.04819076602474542; 0.006002839881947959 0.007153321088215768 -0.03867127669673834; 0.003298606815217476 -0.0028903574929469754 -0.003436205910646896; -0.005326497302194505 0.0012124948844311353 -0.002384467772474241; 0.001149297506372755 0.0015515526233027053 -0.0010418199622110283; 0.0012293818469422471 0.0020171003931987296 0.0031393162412626063; -0.0005952791620344748 -0.0006643745145134024 0.004837916259821604; -0.00034475680823843196 0.004139836767910665 -0.005919139830929202; 0.004099325828906165 -0.00593087732020125 -0.016583427425747626; 0.0026330973644090204 0.0012473127176101228 0.0054640692912518805; -0.013689043080226566 0.0016318768184983901 0.012354698724621815; 0.0019461223953055327 0.001999958498877111 0.004733065922323244; 0.0019792630778624736 -0.011112365327276334 -0.0036071811531007145] %
+
+Mass Used: 105.20198562961468 kg
+Launch C3: 95.54386365667769 km²/s²
+||V∞_in||: 1.6112041571096402e-6 km/s
diff --git a/archive/ES_0.567896658498721 b/archive/ES_0.567896658498721
new file mode 100644
index 0000000..d5c2bab
--- /dev/null
+++ b/archive/ES_0.567896658498721
@@ -0,0 +1,22 @@
+archive/ES_0.567896658498721---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T07:10:28.623
+Launch V∞: [6.399021886689359, -7.218682702084143, 0.22275299293150266] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.824901402860958e-7, -6.405075133153177e-6, 3.823200019475805e-7] km/s
+ V∞_out: [-2.298240483143785e-6, 5.22423045120834e-6, -2.9384794114772843e-6] km/s
+ time of flight: 1.8749577793027842e8 seconds
+ arrival date: 2029-04-05T09:20:05.623
+ thrust profile: [0.5542250483521689 -0.12503866734357008 -0.12385715713348379; 0.13246018387908828 0.05346967056781545 -0.10903392322467037; 0.0794316090156964 0.05793719520760637 -0.11187288569575785; 0.045887488918381215 0.04580829004130468 -0.09425698886377865; 0.0507370399831817 0.06395781180390268 -0.13058199851080546; 0.02899353751702614 0.04405284716346491 -0.09861131839835516; 0.01905967140611512 0.033005516596448334 -0.07678524585134075; 0.01521750490008171 0.03289167491135 -0.07329750657946553; 0.0057735191216770065 0.013374703717587894 -0.03371884272819366; 0.008202818500201247 0.02149816538212267 -0.055345344574972685; 0.001002142539106079 -0.0028537925892402273 -0.0044565382037196665; 0.0001403111855828147 -0.001157761835860091 -0.00031655718899664003; -0.0004479185098680313 0.0005614793558750921 -0.001582424133808661; -5.5862565280096876e-5 -0.00019319457356292528 0.00143407955275917; -0.0006506765843055048 0.0015447570311429458 0.0006461287297840181; 0.0022012792551581307 -0.004084507471483978 0.0023408285086260177; -0.0017562373817925768 0.0007256004317501766 -0.0020716510348726693; -0.007539876210226656 0.0061135972305304265 0.006582070058689358; 0.00035837867643920447 -0.003453008440527542 0.0030833681192230004; 0.006248414699510206 0.006458334145481668 0.0015366821405980412] %
+
+Mass Used: 119.4249685077516 kg
+Launch C3: 93.1064799555582 km²/s²
+||V∞_in||: 6.476877711747271e-6 km/s
diff --git a/archive/ES_0.5679253997852971 b/archive/ES_0.5679253997852971
new file mode 100644
index 0000000..faa8538
--- /dev/null
+++ b/archive/ES_0.5679253997852971
@@ -0,0 +1,22 @@
+archive/ES_0.5679253997852971---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T03:20:03.286
+Launch V∞: [7.223082702904259, -6.677912707243088, -0.12699270774571222] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.304780594104292e-9, 2.782428348749877e-9, -4.475544323094613e-9] km/s
+ V∞_out: [3.79603192259901e-9, 7.341874364235187e-9, 2.432883502826689e-10] km/s
+ time of flight: 1.6011989077175787e8 seconds
+ arrival date: 2029-06-07T09:04:53.286
+ thrust profile: [0.37946897478598374 -0.07108838236990259 -0.14085875441814386; 0.05597869155297375 0.01617739900025319 -0.0642314335921447; 0.04260290294761724 0.02263387322127159 -0.08187229642747797; 0.09477088469206699 0.06967995902222521 -0.24279381761566374; 0.05607423638805063 0.04848004581102742 -0.18875693442742458; 0.04484721693376751 0.04133618061315382 -0.17507181647402797; 0.019194389610260442 0.019246290900972247 -0.09203538485424914; 0.009692997091169013 0.010120445861454705 -0.053385232108135255; 0.011310050750434831 0.012792877212752482 -0.06933273770997177; 0.0022715308397258114 0.0029803099903547817 -0.017454084324252883; 0.0009203705745971198 0.0008163332930267523 -0.0036930612962355744; -0.000918291417637667 0.0004406552916898332 -0.002287443418979276; 0.00025756046467609144 0.0035554221229109695 -0.008198543916672327; -0.00011067859753745556 -0.00043414661762543913 0.0005161704239868767; -0.0013314719956286731 -0.00030674914250233246 -0.004956346886803098; -0.0017382163512962828 0.00019947988629544954 0.0011628328447955561; -0.0015274359020288376 0.005604519022767261 -0.009294283367107777; -0.001422017266647306 0.0013424914076778155 0.0004075210453903409; 0.0012883268117074307 0.0004614347220025601 0.003724072142804101; -0.004027286789723978 -0.0008873872597713414 0.004227040561524827] %
+
+Mass Used: 98.00881387899835 kg
+Launch C3: 96.783569006374 km²/s²
+||V∞_in||: 7.477506379502252e-9 km/s
diff --git a/archive/ES_0.5679445522578283 b/archive/ES_0.5679445522578283
new file mode 100644
index 0000000..9891fae
--- /dev/null
+++ b/archive/ES_0.5679445522578283
@@ -0,0 +1,22 @@
+archive/ES_0.5679445522578283---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T17:08:49.209
+Launch V∞: [6.643211489933035, -7.308946830378907, 0.22896872061296145] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.488453578167797e-6, 4.134299889582439e-6, 4.980669826154465e-6] km/s
+ V∞_out: [6.149531142855121e-6, 4.921180863729681e-6, 1.225119774100497e-7] km/s
+ time of flight: 1.8749577787493396e8 seconds
+ arrival date: 2029-04-08T19:18:26.209
+ thrust profile: [0.24703914732531002 -0.06174758082312928 -0.0890595677522873; 0.0621144471540866 0.017418677667973996 -0.06905087446815643; 0.059353398223820866 0.0315556679075616 -0.11347704987216364; 0.05314325625673383 0.03845136756668988 -0.13619977839453914; 0.03970053472558947 0.03461994403668115 -0.1314008984153541; 0.03152816800819218 0.03274622055736475 -0.12857977580285954; 0.016478401188233283 0.01815470192096426 -0.08084195128305982; 0.007975696327877788 0.00958679974965095 -0.04504621015220752; 0.0032119636276287567 0.004639368202880275 -0.020343246978584802; 0.0026808951033668953 0.00729247399187827 -0.03370957310399805; 0.005202430548486432 0.006616229580111357 -0.04066229213268832; 0.0007718401783338199 -0.000989549453088635 -0.00011470590095708508; -0.0011556600922969368 0.006634902893467062 0.003458402284862349; -0.0007871943053500241 -0.001475647617419937 0.008202802607150726; -0.00303820058413202 -0.0045985721297942105 0.006163078171092442; -0.0009880447092826489 -0.011061221175251344 -0.005959307254297818; 0.0025209672931695 0.00013313166129675275 -0.00520203379353909; -0.016772296414752405 -0.004525278282849298 -0.0037511034941465496; -0.002711106328544985 0.002369777708326037 -0.007256577700914183; -0.016688132989200983 0.016039280168067726 0.010442036129019594] %
+
+Mass Used: 93.2372064590304 kg
+Launch C3: 97.60538934430329 km²/s²
+||V∞_in||: 7.876910753432096e-6 km/s
diff --git a/archive/ES_0.5679536153854066 b/archive/ES_0.5679536153854066
new file mode 100644
index 0000000..44d0572
--- /dev/null
+++ b/archive/ES_0.5679536153854066
@@ -0,0 +1,22 @@
+archive/ES_0.5679536153854066---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-06T11:22:40.358
+Launch V∞: [6.474888482520053, -7.67471634567726, -0.2164521094465014] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.915356506726321e-8, -7.601698996450882e-8, -4.19741493708526e-8] km/s
+ V∞_out: [2.179287423046336e-8, -4.3881926264740206e-8, 7.061802336424818e-8] km/s
+ time of flight: 1.874957778230821e8 seconds
+ arrival date: 2029-04-14T13:32:17.358
+ thrust profile: [0.1040703743735506 -0.03128417478592601 -0.048649870501632726; 0.02353418637527676 0.0039570163210309595 -0.03308228416324909; 0.03544469337995114 0.009409895625326733 -0.08464647622603423; 0.03139943718430399 0.011152983195177048 -0.10360296030799507; 0.025282552923897177 0.011774189590683834 -0.10296071240035191; 0.032488327565415 0.01577946375159143 -0.16112109964455268; 0.01815223746784173 0.008697384479124487 -0.11450261562329753; 0.014632962849141113 0.006079106432830896 -0.09348164188083927; 0.0045741658096146685 0.0024451342937698477 -0.03305998845511048; 0.006472549254618779 0.005413527161045931 -0.05603038868307216; 0.0024639697394930942 0.0013239224950650917 -0.02157998903723; 0.0001329143291252773 -0.00107460211270115 -0.0035893504508344156; -0.002038064446127119 0.0016816406737024654 0.0027630712801583347; -0.0018497011581418456 0.002727117671811 0.004088130608970487; -0.0005042533712114126 0.001221665857242115 0.0018367475715054013; 0.004851782551699579 -0.0018187810104711671 -0.0023028230504402647; 0.0004729430065438392 0.003824643307364559 0.002196180452370711; 0.0011802842885634238 0.002169722392976663 -0.0011081098086461187; -0.0006126200805889951 -0.0003394807887311123 0.0037693762388469635; -0.0015769915870307762 -0.003967019311871066 0.004646384306613887] %
+
+Mass Used: 74.19078166337204 kg
+Launch C3: 100.8723033633604 km²/s²
+||V∞_in||: 9.525446780150154e-8 km/s
diff --git a/archive/ES_0.5679582448614515 b/archive/ES_0.5679582448614515
new file mode 100644
index 0000000..d03160d
--- /dev/null
+++ b/archive/ES_0.5679582448614515
@@ -0,0 +1,22 @@
+archive/ES_0.5679582448614515---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T06:16:58.590
+Launch V∞: [7.362635945887031, -6.550274987712969, -0.24533906100773004] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008095097752748423, 0.001561488425755101, 0.0005660681181416936] km/s
+ V∞_out: [0.0005519399640447437, -0.0013256584774193878, 0.001162443431334668] km/s
+ time of flight: 1.6031061449011678e8 seconds
+ arrival date: 2029-06-08T17:00:32.590
+ thrust profile: [0.29486245529384514 -0.06441884345457827 -0.1168342699619448; 0.10335277409610263 0.026715225482392906 -0.11867557557365484; 0.06136719976794824 0.029135331986169025 -0.1194876348858784; 0.053690490918014304 0.032939553178055296 -0.1471098911178024; 0.07113540182146254 0.05164536205707102 -0.2447082614702126; 0.04631803924327386 0.03706928451656532 -0.19212428744488452; 0.0224583265105112 0.01914913172880814 -0.10914536965739546; 0.0029126717572318674 0.0030055579619608632 -0.008356509096069975; 0.005368897548443472 0.0038706785954781484 -0.014420030166094389; 0.006597356145789831 0.004955772348176351 -0.034495038397006884; -0.0018285160507699597 -0.0034971043037919473 -0.014966696470260027; 0.007944553550700452 0.002650887793788461 -0.007080557557207741; -0.0006215922910032484 0.0012890192431182896 -0.002761281671214277; -3.3039106035119494e-5 -0.000961503695617494 -0.002006236270486553; 0.009328667610656285 -0.00027307296025268804 -0.0018124422753805262; 0.00016608939880676833 0.00036343303729044485 -0.0037488694705324786; 0.00035979131784348 -0.0012405208627601565 -0.0004839120148099937; 0.01337912658528914 0.004463079664235902 -0.014356584361328058; 0.0003508247246916175 0.0010609018630783598 0.0036002204361633965; -0.004124065503235416 -0.0028062844970288083 0.013413154234576372] %
+
+Mass Used: 95.7655255147979 kg
+Launch C3: 97.17470174118209 km²/s²
+||V∞_in||: 0.0018476972951241629 km/s
diff --git a/archive/ES_0.5679679953923968 b/archive/ES_0.5679679953923968
new file mode 100644
index 0000000..e4fa2d8
--- /dev/null
+++ b/archive/ES_0.5679679953923968
@@ -0,0 +1,22 @@
+archive/ES_0.5679679953923968---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T03:06:53.834
+Launch V∞: [6.088836018382324, -7.646127051812704, 0.2553659580603303] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.020397384788993878, -0.008907751028693144, 0.021389615533945968] km/s
+ V∞_out: [-0.019419708446002992, -0.00795172239532914, -0.022627926561406685] km/s
+ time of flight: 1.6997104657231855e8 seconds
+ arrival date: 2028-09-12T09:17:39.834
+ thrust profile: [0.30983503847130484 -0.1142815644376495 -0.10901233680283791; 0.19321015379644435 0.032950500249626 -0.1867288219961248; 0.11905825248088406 0.0495049212187534 -0.1886137083047879; 0.05996245083072398 0.03467773386687683 -0.13176334332723705; 0.055283346190582124 0.03931244530423426 -0.1524261238473383; 0.03694136671235847 0.030249697138235703 -0.12270286702312955; 0.026599682914824844 0.024304709787160754 -0.10269532330333928; 0.007786432149937045 0.007810733127695739 -0.03476320932406507; 0.004845964197041804 0.005157592856241784 -0.02384623097620517; 0.011172045157540887 0.012718572077019973 -0.05955052791307179; 0.00021467310904335645 0.0006756175089024622 -0.003762653599041157; -0.00040103693677175805 -9.239291372332037e-5 -0.002637307448275324; -0.0005650726616552262 0.0009241985009984876 -0.0010994401280664473; 0.0004128634284124616 -0.001066201226070186 -0.0010097317126073419; -0.00029192122433394747 0.0014465908713430843 0.00034193144911096865; 0.0016501943630114362 -0.0010763201538738856 -0.0010145706544280862; -0.0018378024352150937 -0.0017333137860261728 -7.329712048768271e-5; 0.0005049007556781024 -6.527998574907737e-5 0.0007873802185066655; -0.0011985668747864465 0.00013514937084670655 0.003713852742806024; -0.0025683312865013262 -0.00039098585162250125 0.0024460354036771738] %
+
+Mass Used: 104.94869206926614 kg
+Launch C3: 95.60239472374802 km²/s²
+||V∞_in||: 0.0308693535291798 km/s
diff --git a/archive/ES_0.5679824297765074 b/archive/ES_0.5679824297765074
new file mode 100644
index 0000000..d1fbc82
--- /dev/null
+++ b/archive/ES_0.5679824297765074
@@ -0,0 +1,22 @@
+archive/ES_0.5679824297765074---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T01:50:34.026
+Launch V∞: [6.469226702613253, -7.5466324626817745, 0.1454342520157757] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7788984610368534e-6, -1.8737154970997772e-6, -1.9977469619678113e-6] km/s
+ V∞_out: [-2.7277989667944972e-6, -1.8391929285967888e-6, -5.641692269815919e-8] km/s
+ time of flight: 1.8364140576309985e8 seconds
+ arrival date: 2029-02-24T13:20:39.026
+ thrust profile: [0.13027729089325374 -0.03948417739911813 -0.05211477308193402; 0.07651912083133972 0.013924765218527311 -0.0899615346198411; 0.0784141698959168 0.029760657557251394 -0.15263541308076717; 0.051722278616970145 0.026467765708133122 -0.1412534466617531; 0.042024139814012186 0.025342431917759953 -0.14569466644809356; 0.03424651579632367 0.023061841987453185 -0.1427098988958445; 0.013704225041895009 0.010563279121185641 -0.06404690643239115; 0.0068293471508314866 0.006644973665823839 -0.038968930428656554; 0.004745551820440259 0.004686788306480747 -0.028160659019267266; 0.0025572123265172175 0.003294568778407094 -0.016707533926693507; -0.0011648769489840587 -0.004230764343728954 -0.005126293033718564; -0.000247802016961643 -0.005337107888244653 -0.0111890972817995; -0.003115957886786518 0.0018245054613008395 -0.0035937120613849472; 0.008580173478482184 0.008539234899079463 -0.004425853382983597; 0.0020097964504546123 -0.0035532226108928823 -0.0008698278628408301; 0.00029313557231057266 -0.00021450588283169892 0.00019066591252978396; -0.0003366711463885886 0.004318027867454449 -0.029567785915108086; 0.021368732751631397 -0.012996008194646903 -0.005476222094059414; -0.01733415029883208 -0.017725357235175418 -0.006375958110084694; -0.004939430029094705 -0.006058496913538962 -0.004785382145125836] %
+
+Mass Used: 86.17454519937291 kg
+Launch C3: 98.82370677826611 km²/s²
+||V∞_in||: 3.265927498093424e-6 km/s
diff --git a/archive/ES_0.5679890564896607 b/archive/ES_0.5679890564896607
new file mode 100644
index 0000000..0092de9
--- /dev/null
+++ b/archive/ES_0.5679890564896607
@@ -0,0 +1,22 @@
+archive/ES_0.5679890564896607---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T11:36:37.414
+Launch V∞: [5.877201381420866, -7.665588240652853, 0.04972453824121304] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.167410186312773e-8, -1.3056938300649327e-7, -5.454395737525723e-8] km/s
+ V∞_out: [4.8498983783518024e-8, -7.871430943655628e-8, 1.2473900073663537e-7] km/s
+ time of flight: 1.693385834988934e8 seconds
+ arrival date: 2028-09-04T10:06:20.414
+ thrust profile: [0.5226856287146591 -0.18211617261805604 -0.14995850321291013; 0.07518840737668511 0.016476860947747148 -0.06631954860785833; 0.10785210496368523 0.0524055994006614 -0.1500212234311728; 0.1850665991227024 0.1282729985839053 -0.31370362481236586; 0.05657304522100026 0.04650611499248393 -0.13560541307759066; 0.02307828639851744 0.02283758818159383 -0.07147301361185827; 0.029026519979274103 0.031927502839175004 -0.1007321527114348; 0.022018598663554493 0.026395092252584854 -0.0860162027245825; 0.002208003606544941 0.003410967810995795 -0.01108644445432197; 0.0062211677395676394 0.009583387115107027 -0.032517451928462365; 0.0006069163700871722 0.001146367604973672 -0.003716420363535306; 4.452453948716457e-6 -0.0005142871010458325 -0.0014369727523248586; -0.0003688167480918126 -0.0012547253276155629 -0.0006974791355097192; 0.0006818833068434435 5.4532161486407294e-5 0.000895531960992259; -0.0023151859510688816 0.0007005160348452896 0.000684837413876494; -0.0036482621648465095 0.0006393120936185338 0.0003124567525588462; -0.0009310225764256796 -0.0045537993272486855 0.0009604402029349216; 0.00016352773493037254 8.8186585330633e-5 0.000829717920481695; -6.672371940567558e-5 0.00029116041495987267 -0.00019602324869177207; 0.00013111934830642858 0.0005499818916358722 0.0006947147570534612] %
+
+Mass Used: 118.37349775543953 kg
+Launch C3: 93.30521168271393 km²/s²
+||V∞_in||: 1.543602989938594e-7 km/s
diff --git a/archive/ES_0.5680126504697722 b/archive/ES_0.5680126504697722
new file mode 100644
index 0000000..bdfc0c3
--- /dev/null
+++ b/archive/ES_0.5680126504697722
@@ -0,0 +1,22 @@
+archive/ES_0.5680126504697722---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T02:58:36.724
+Launch V∞: [6.184091994276149, -7.76835714573143, 0.023366745018386453] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007239947433220507, -0.0036251924736641966, 0.010818148978799723] km/s
+ V∞_out: [-0.008797010091003914, -0.0035743366885942415, -0.009603647173932802] km/s
+ time of flight: 1.7424989189180583e8 seconds
+ arrival date: 2028-11-05T21:43:27.724
+ thrust profile: [0.16708987537356823 -0.0602632534697893 -0.06974065809926762; 0.055052441506073475 0.0070799700411166774 -0.06595263129050957; 0.0572306622746534 0.020203740818648824 -0.11245952617102582; 0.05490604132124914 0.02586954442949256 -0.14568024534325197; 0.04310464122131718 0.02486565522067283 -0.1437337887770678; 0.02935217170113258 0.018551932900132125 -0.11679002449783547; 0.02667454682841551 0.018933888675227648 -0.12528507920073942; 0.01962171365827135 0.014911033793664517 -0.10344260759630249; 0.010924112599119688 0.008604048860623856 -0.0646954537931868; 0.004357626545129643 0.003451390523639503 -0.0176771331426612; 0.0036289540241825225 0.003533133470959474 -0.025321484996797858; -2.052124043982204e-5 -0.000951881534298627 -0.006366622910664095; 0.0008524966334000734 0.0007811751226851368 -0.005139247199873921; 0.001334856919079251 -0.0004026752418384537 -0.012571014612782368; 0.004214555930801455 0.0024306400305991412 -0.007400783733868608; 0.008204368937249459 -0.007242629743656703 -0.004475960866523973; -0.00014110614321736554 -0.010765421260586763 -0.006673383370160731; 0.0016531344915124628 -0.0018702424915413053 -0.007530619043284867; 0.0011713440852407259 0.0032984981921130125 -0.011367609954073911; 0.0007860899107434718 0.0004465810412353779 0.0013206774006812006] %
+
+Mass Used: 87.56776905260267 kg
+Launch C3: 98.59091254207969 km²/s²
+||V∞_in||: 0.013512631373437715 km/s
diff --git a/archive/ES_0.568024814888977 b/archive/ES_0.568024814888977
new file mode 100644
index 0000000..43b7f7e
--- /dev/null
+++ b/archive/ES_0.568024814888977
@@ -0,0 +1,22 @@
+archive/ES_0.568024814888977---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T07:01:51.257
+Launch V∞: [6.185481630012444, -7.740087720691177, -0.2339769055509531] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.489157772090966e-10, -3.1096836668171144e-9, -1.1488801282278622e-8] km/s
+ V∞_out: [4.3343237092554636e-9, 6.401595382714103e-9, 3.1829539943899656e-9] km/s
+ time of flight: 1.7085954480857703e8 seconds
+ arrival date: 2028-09-24T20:00:55.257
+ thrust profile: [0.14818003397720417 -0.053340282892016304 -0.06002272178772338; 0.09180188071881745 0.015833041641872634 -0.10090721503100078; 0.0857013604534781 0.03662891173926897 -0.1523131190352082; 0.06116521689186257 0.036408280352682 -0.1496535289591122; 0.06086845483366943 0.0451683936633537 -0.18703703911202416; 0.030209695749468163 0.02469533933576114 -0.11268878889274722; 0.022531701040350245 0.02110371441224648 -0.09889215227801972; 0.017330442496399784 0.01704159136537845 -0.08614412631834817; 0.00808115874219444 0.007757077830642226 -0.04254142598635966; 0.003950301415531363 0.004181561116130273 -0.02330265596802913; 0.0033230194926645485 0.002301178029389621 -0.013714999851816779; 0.003064983883491624 0.005054465606604948 -0.024978054892825303; 0.0005593101176883653 -0.00020998018681137411 -0.015621319807507996; 0.00040209868109664353 -0.0007439430274970415 0.0008856253174941075; 0.00030092482380503086 0.00014543023249462535 0.0005704760423039905; 0.0002904428548436079 -0.001356045399183289 -0.002258042343549823; -0.0005840146825846964 0.003385965223334594 -0.004740744598164497; 0.0001981677549523866 0.00041723121666294334 -0.0017303189080529816; 0.0011475935487870776 0.0032994882768191936 -0.009675931247925686; -0.0024875343697917654 -0.0022105907899022856 0.007705509292289442] %
+
+Mass Used: 89.72294838644939 kg
+Launch C3: 98.22388611154695 km²/s²
+||V∞_in||: 1.190481610422856e-8 km/s
diff --git a/archive/ES_0.5680308048323167 b/archive/ES_0.5680308048323167
new file mode 100644
index 0000000..3eafd08
--- /dev/null
+++ b/archive/ES_0.5680308048323167
@@ -0,0 +1,22 @@
+archive/ES_0.5680308048323167---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T21:38:35.630
+Launch V∞: [6.274702102809324, -7.493081154964863, 0.09302514644703873] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004278130327015918, 0.0029106384741968356, 0.004434545419261035] km/s
+ V∞_out: [-0.004648349132593874, -0.002468235861257082, 0.004329312763356626] km/s
+ time of flight: 1.7984106128897417e8 seconds
+ arrival date: 2029-01-08T09:29:36.630
+ thrust profile: [0.37144381217633643 -0.12083707193105103 -0.11976161626369349; 0.08879786790363779 0.018238793859080848 -0.09641239560019135; 0.09686316918963213 0.0417149045568708 -0.1693090123881001; 0.06343672020617633 0.03807742043853318 -0.15936247564535644; 0.030022223633221438 0.022364331182733746 -0.0945012019681837; 0.028875286379259416 0.02463858590672588 -0.11674580693292642; 0.01834650243031236 0.017490575128647844 -0.09240010904355178; 0.016565050089880833 0.01661032721716595 -0.0755993803926762; 0.011252143793082075 0.010310525646008163 -0.053196433606664255; 0.00406261087337772 0.005606006894628228 -0.02215910167275913; 0.0012779898248028135 0.0006216497464068406 -0.0015792763568612611; -0.002922866322681907 6.114727751732369e-5 0.000927998173220753; 0.0038859379677009145 -0.007375283211874642 0.0005223407013752353; -0.005871646256112511 -0.004600186152618013 0.0031419346575409348; -0.006543917085274657 -0.009438079971935466 0.006840577414055304; 0.003874988169335953 -0.002421635754827268 0.000256466625789297; 0.005367340970170633 -0.0019349705083747978 0.009843920088898245; 0.0023091113392772313 0.005099545979055641 0.002302279677544553; -0.004552547058056544 0.0016928545596170972 -0.0027217375420384984; 0.01135772644728879 -0.0114649532396786 -0.0004248238857468428] %
+
+Mass Used: 105.46290775243142 kg
+Launch C3: 95.52680535176081 km²/s²
+||V∞_in||: 0.006814646615775262 km/s
diff --git a/archive/ES_0.5680325978028574 b/archive/ES_0.5680325978028574
new file mode 100644
index 0000000..1d8a1b5
--- /dev/null
+++ b/archive/ES_0.5680325978028574
@@ -0,0 +1,22 @@
+archive/ES_0.5680325978028574---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T11:30:40.217
+Launch V∞: [6.57994155430359, -7.4538005035882975, -0.830215320072136] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1336415048434013e-6, -0.0003825423183752991, 0.00025241818841799564] km/s
+ V∞_out: [0.00023648059008964095, 0.00038441863556994165, -8.045005326112543e-5] km/s
+ time of flight: 1.8749577779260203e8 seconds
+ arrival date: 2029-04-11T13:40:17.217
+ thrust profile: [0.1553911180145717 -0.04687274424703322 -0.06792544141561781; 0.050141915817792655 0.009390839797823517 -0.06644702218942557; 0.05218348791184176 0.020420787459958494 -0.11858911926711015; 0.048484904954123643 0.0250615853067161 -0.15556571278392217; 0.03619774147036607 0.022223711551548377 -0.15053209761349765; 0.02639535129731962 0.018173674755378184 -0.13386710484325345; 0.015954643297378168 0.012009473207689783 -0.09521456894454143; 0.00700921769514849 0.005671940555586409 -0.04804825080332315; 0.0014309963912351685 0.0011573525187227045 -0.012606814056209965; 0.0009742011435663019 0.0010408333091314417 -0.010554318176644258; 0.0008315000911905475 0.0021365758303344474 0.00026447954484736316; 0.0056545807987292305 -0.0014556044530112952 -0.0069970071969544245; -0.005652392353642975 0.004828660917554907 -0.0071221484066773; 0.003053574497765581 -0.0044162241074480755 -0.0004883684982050439; -0.009460475139170527 0.0031080352212471203 -0.003345244740450918; -0.007263757235174039 -0.005215130626641572 -0.002870868009917196; -0.001862730469608447 0.002704845487726592 -0.008538931831705183; 0.005971404685390136 -0.0031159232585183634 0.001809177027014994; -0.00718877888534728 0.00331541365526773 0.004618226596361429; 0.005306193870569851 -0.0036940900781150367 0.002900480860632629] %
+
+Mass Used: 82.03118745234406 kg
+Launch C3: 99.54403028302679 km²/s²
+||V∞_in||: 0.0004583174143922888 km/s
diff --git a/archive/ES_0.5680425309641314 b/archive/ES_0.5680425309641314
new file mode 100644
index 0000000..63f729d
--- /dev/null
+++ b/archive/ES_0.5680425309641314
@@ -0,0 +1,22 @@
+archive/ES_0.5680425309641314---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T20:21:50.867
+Launch V∞: [6.126515009920965, -7.614041342549877, -0.05275777286739958] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1495398529008508e-7, 6.405158820740295e-8, 9.892612886011267e-8] km/s
+ V∞_out: [-5.029433294159973e-8, 8.343976521113959e-8, -1.3354978072186546e-7] km/s
+ time of flight: 1.7398618471361947e8 seconds
+ arrival date: 2028-10-31T13:51:34.867
+ thrust profile: [0.38051393044109333 -0.14078689738943456 -0.14515019746257157; 0.13025103097465815 0.01826449646572672 -0.14640637214822913; 0.052320597338038344 0.018838441634074995 -0.09895085653974368; 0.051148610823150864 0.025810315380115356 -0.13102168620761195; 0.028216093679014377 0.017426455227592473 -0.09242693958239018; 0.035419025647539557 0.024879399104522356 -0.13883398008093195; 0.01591268641760383 0.013037917138219068 -0.07462798407977256; 0.027669480840766703 0.021694909288717302 -0.1438864325876612; 0.0008669965850222472 0.000995981936011462 -0.007430415763693502; 0.01408777424774416 0.015062587965354863 -0.09984372454187065; 0.0007038061593875818 0.001360898285554573 -0.00535149946125993; 0.0010853924354218944 0.0013231554945198054 -0.00038510096023639147; 0.0008360040714487859 -0.00025459817348061483 -0.0030422842167338975; 0.0026047085833159943 -0.00041104715697201817 -0.005526713261221394; 0.002672541577309424 0.0013132352096877468 -0.003510111470229507; -0.006946038287796674 0.0033311317042231106 0.0003025623353878422; -0.002210946463017965 -0.0016157097345902136 -0.0031239876997298972; 0.0015554177077159962 -0.00010353967157332908 0.005071905721149084; 0.00046593609285259206 -0.005777714476229434 0.0050570371899202205; 0.0026580719044230743 -0.0006466126690665508 -0.014639323617921779] %
+
+Mass Used: 105.57114795139933 kg
+Launch C3: 95.51059511544354 km²/s²
+||V∞_in||: 1.6463111387951984e-7 km/s
diff --git a/archive/ES_0.568060420223396 b/archive/ES_0.568060420223396
new file mode 100644
index 0000000..57ce171
--- /dev/null
+++ b/archive/ES_0.568060420223396
@@ -0,0 +1,22 @@
+archive/ES_0.568060420223396---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T09:45:05.635
+Launch V∞: [5.97838659416437, -7.579284721526901, 0.08604385389592477] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.796346512925572e-6, 1.8082427000722799e-6, -1.3275429944054318e-6] km/s
+ V∞_out: [1.2007415589190597e-6, -2.9142796985029072e-6, 1.7086740923981994e-6] km/s
+ time of flight: 1.7475834796937466e8 seconds
+ arrival date: 2028-11-08T01:44:12.635
+ thrust profile: [0.5069604270332213 -0.16283104087515254 -0.1474294997946359; 0.17780373484519107 0.03637978935528534 -0.1576666654136647; 0.0637693036901411 0.03143062307021469 -0.09874605223310322; 0.07324553668748686 0.05026801259056352 -0.15495876388618388; 0.08149050881699986 0.06856725563133839 -0.21022953495157812; 0.027491571619503347 0.026508912034151788 -0.0886607594656159; 0.02876947698944812 0.03171900991423245 -0.10689578813552514; 0.016348232468814644 0.01951655619998238 -0.07164637612745343; 0.0031344877498494066 0.004472516468643649 -0.017037481931193345; 0.0003348154118132002 0.0005423571076244065 -0.003398247742438779; -0.001300549072285495 0.0035629054274955996 -0.005896413186543859; 0.0006460896670552399 -0.002044989330277887 -0.002455067766239289; -0.001979014506240209 0.00019556371990656508 -0.0025264595183514755; -0.0007353500422820149 0.001471602399758488 -0.004859688550719792; 0.0010079546684839645 0.0023289031212826356 -0.003420103593945144; -0.003419040165111676 -0.007563953415142086 0.000745338319814306; -0.003929935799219382 0.00384077647701515 0.005160075179806476; 0.014412636841320943 -0.0025806023336713718 -0.0003815203396286097; -0.0026003230074897023 -0.0013784821156851061 0.009338104732238778; -0.005225583545785181 -0.0020716846580485543 0.00882825360157644] %
+
+Mass Used: 119.10510115367833 kg
+Launch C3: 93.19406670404862 km²/s²
+||V∞_in||: 3.5849220193346794e-6 km/s
diff --git a/archive/ES_0.5680763731272853 b/archive/ES_0.5680763731272853
new file mode 100644
index 0000000..e854989
--- /dev/null
+++ b/archive/ES_0.5680763731272853
@@ -0,0 +1,22 @@
+archive/ES_0.5680763731272853---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T06:20:47.690
+Launch V∞: [6.481851372223643, -7.33874946677687, 0.1829693220008691] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6607703112414863e-7, -3.6381835472986445e-8, 4.542610233315562e-8] km/s
+ V∞_out: [-1.7453274376809417e-7, 1.7627831605555864e-8, -2.0108565890575958e-8] km/s
+ time of flight: 1.8749577787492234e8 seconds
+ arrival date: 2029-04-09T08:30:24.690
+ thrust profile: [0.4011573628308408 -0.10295782708933511 -0.13304958759547997; 0.053515729807447204 0.01465019249744698 -0.0630629462912292; 0.04685627870720964 0.02491793529908073 -0.09272621797620216; 0.04035078122212251 0.02905612261474013 -0.11201871187504435; 0.03338664468347286 0.029404480988634272 -0.12053961336662723; 0.02965998388640133 0.031041751416331413 -0.13380971887875687; 0.021855726617160592 0.02541092673408911 -0.11637797537054106; 0.01270068852004253 0.01540607494665298 -0.076415359747328; 0.005779004555283058 0.006564914093753816 -0.03782587274461431; 0.003798271608091142 0.004740819197160154 -0.028170918502926433; 0.0006916232099052822 0.00024452719241846584 -0.0022782621310413827; 0.0012557643648417156 -0.0009016635127391237 0.0026306401431776217; -0.0010049330556226646 -9.497383219052343e-5 -0.0017718993081659255; -0.001274258982046415 0.0024226161763015544 0.00682438862344373; -0.008406986042431043 -0.0004071658290713574 0.006397810523329734; -0.010747099587822356 0.004134315865794204 0.012114065398702075; 0.008854564369812044 -0.010720934074032752 -0.004243723084720813; -0.007872144239486841 0.00890613706841967 0.008324990304077129; -0.01601802774121424 -0.006302924572720991 0.0014795864168319634; -0.001347656592617511 0.008471803120975886 0.005424088505346815] %
+
+Mass Used: 103.30924277886515 kg
+Launch C3: 95.90511872050877 km²/s²
+||V∞_in||: 1.759793993414491e-7 km/s
diff --git a/archive/ES_0.5680876336378602 b/archive/ES_0.5680876336378602
new file mode 100644
index 0000000..4a15c46
--- /dev/null
+++ b/archive/ES_0.5680876336378602
@@ -0,0 +1,22 @@
+archive/ES_0.5680876336378602---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T04:39:35.211
+Launch V∞: [7.269784191325434, -6.034411314582767, 0.22004222752497724] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7823233471474997e-9, 1.547219906015437e-9, -3.259492032744859e-9] km/s
+ V∞_out: [2.553966031582303e-9, 4.863540660676852e-9, 1.5984539333567653e-10] km/s
+ time of flight: 1.6939920310592338e8 seconds
+ arrival date: 2029-09-16T19:59:38.211
+ thrust profile: [0.8481636080049151 -0.09741454959914819 -0.2091891118149942; 0.3199440312569588 0.15226085085292096 -0.2550295933396138; 0.08566860296486684 0.0715182449667792 -0.1261894765477567; 0.041425219758167944 0.04627924324457467 -0.08826869272766591; 0.03449078392758199 0.0479236108149764 -0.09735696642414012; 0.033355321671861865 0.054048582925067104 -0.11645689283974457; 0.017559695310984152 0.03285345719865211 -0.0753142670037185; 0.019750212699697473 0.04265335408413094 -0.10075479339031866; 0.00243916476265026 0.00604118542506306 -0.013811112474655949; 0.0024414766459414554 0.005866111704495598 -0.014192936406633275; 0.0008109759337137259 0.0021434989380200607 -0.005606104211599531; 0.0006711157492778003 0.0025053615342965343 -0.006290306930009168; 9.298253538298718e-5 0.0020688105528175473 -0.0020311899812187786; 0.0017431422089088996 0.00160869149688359 -0.003440227537905236; 0.0011563407382964843 -0.0007726067227806048 -0.0020335569451364398; 0.0012915924592648816 -0.00035376380866024727 -0.004266703690780369; -0.002398832628759692 0.0007541174157296658 -0.0008011484612007926; 0.00039440161357856595 -0.00012469977059379432 0.00015120478546951782; -0.0007712544538846366 -0.003248460370024617 -0.0010731814139319593; 0.003044483376534994 -0.0016664852159019529 -0.0019171670280380398] %
+
+Mass Used: 141.78048525473105 kg
+Launch C3: 89.31230068390387 km²/s²
+||V∞_in||: 4.556259535757341e-9 km/s
diff --git a/archive/ES_0.5680889364559316 b/archive/ES_0.5680889364559316
new file mode 100644
index 0000000..2960f2c
--- /dev/null
+++ b/archive/ES_0.5680889364559316
@@ -0,0 +1,22 @@
+archive/ES_0.5680889364559316---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T20:14:08.682
+Launch V∞: [6.207779496429777, -7.730759033726229, -0.21330333102893884] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3724449372982624e-6, -9.300091228457691e-6, 6.385297613208192e-7] km/s
+ V∞_out: [-3.365956616397336e-6, 7.680504695763452e-6, -4.338873564454968e-6] km/s
+ time of flight: 1.700081226259984e8 seconds
+ arrival date: 2028-09-14T12:42:50.682
+ thrust profile: [0.14680938730575704 -0.05715052927234102 -0.0592646245660378; 0.06009689046390077 0.007789908467259739 -0.06669211831479724; 0.0869307776821472 0.03164924249939675 -0.154109183048221; 0.09766635818633543 0.050406939303683757 -0.23400619720384788; 0.07719787957445583 0.04874558173658648 -0.2332557299092666; 0.04223896549320712 0.030458413928854056 -0.1555110758465824; 0.01326196037238594 0.010319932216059773 -0.058525307252027044; 0.007017045179446626 0.00551104347019968 -0.03473124051758683; 0.006593856914984325 0.0058140695708495515 -0.03902969561036855; -0.0024169796416633246 0.0025528789283362245 -0.010705426121005425; -0.0014908157446641055 0.0029371323457177273 -0.006279287208452157; 0.0004166377942239735 0.0019088761419545999 -0.0046715054591015895; 6.469534213204375e-5 0.0004777669035581052 -0.0020413963796268933; -0.000625737864044699 1.8184144750654687e-5 -0.00046314378249715134; -0.002071644698970075 -0.0003782311245901648 0.004013339013326057; -0.0029330422986279347 0.003424917479952479 0.0072873885149915794; -0.002807415206739848 0.004629772972036356 0.0045792379658995234; 0.0028625530790242592 0.0005750047720733458 -0.007064656686612212; -0.008129125918218596 -0.004636018768642152 0.0005703332439156404; 0.0012697020093315628 0.001999832000078748 0.0037686339085173945] %
+
+Mass Used: 89.0815768868938 kg
+Launch C3: 98.34665982486166 km²/s²
+||V∞_in||: 9.42247431514906e-6 km/s
diff --git a/archive/ES_0.5680942385052924 b/archive/ES_0.5680942385052924
new file mode 100644
index 0000000..032d271
--- /dev/null
+++ b/archive/ES_0.5680942385052924
@@ -0,0 +1,22 @@
+archive/ES_0.5680942385052924---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T09:28:38.564
+Launch V∞: [6.600817592725682, -7.25081054382165, 0.2673429829128698] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.994415636979789e-9, -2.5829643188928217e-10, -4.984542240791341e-9] km/s
+ V∞_out: [-1.8236424095888396e-9, 3.949101150877025e-9, 5.421857910327372e-9] km/s
+ time of flight: 1.8749577787484014e8 seconds
+ arrival date: 2029-04-05T11:38:15.564
+ thrust profile: [0.29067442029186674 -0.047851539905093166 -0.09161266355426013; 0.14528946385178704 0.04794501613116404 -0.13014977704592168; 0.083782834823823 0.06428968754692986 -0.1120137794396939; 0.07813838488929797 0.08300113076862281 -0.15587117939384262; 0.02305466382697741 0.030179705309651614 -0.06102325267827697; 0.043100802435835174 0.06854616066531992 -0.141966894259273; 0.027946448626501794 0.0643231105512617 -0.12927072143574253; 0.006263771644079388 0.011540142104312057 -0.027192222653861297; 0.006270640428770893 0.014453132050110746 -0.0339856568242739; -0.0014415954337883188 0.0017425650176113847 -0.0010357466742604822; 0.0002999363733916887 0.001557709325288719 -0.0029442995647632475; -0.0004433359851764172 0.0015160827264478443 0.00047505484409081735; -0.00039425600255418505 -2.8185556051779832e-5 0.0010675895826377578; -0.0012385229195566853 -0.001159974975347612 0.0014569314627040305; -0.0008898623974156373 -0.004379700691970755 0.0015628533104937996; -0.001348264127119811 -0.006604711555049944 -0.006346277609894603; 0.0006985017943707068 0.0023336451892757588 -0.004237502750937168; 0.0007493702960972863 -0.0032613257261391686 0.0024492734273617997; 0.004224032930224254 -0.007246240606509812 0.002044268069340372; -0.0013841634255206405 -0.004445102771280779 0.00965507874260371] %
+
+Mass Used: 101.51358580832948 kg
+Launch C3: 96.21651870534485 km²/s²
+||V∞_in||: 7.0609182088357405e-9 km/s
diff --git a/archive/ES_0.5681051095115723 b/archive/ES_0.5681051095115723
new file mode 100644
index 0000000..9f860da
--- /dev/null
+++ b/archive/ES_0.5681051095115723
@@ -0,0 +1,22 @@
+archive/ES_0.5681051095115723---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T06:18:23.504
+Launch V∞: [7.231349864485257, -6.387074402731894, -0.002397717752424655] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.1350036785635894e-8, 2.8633747352317467e-8, -6.349564998666233e-8] km/s
+ V∞_out: [4.598899924782839e-8, 8.769856524090784e-8, 2.986939851583246e-9] km/s
+ time of flight: 1.595030964871186e8 seconds
+ arrival date: 2029-05-27T08:43:19.504
+ thrust profile: [0.6442028841912326 -0.12365708647053889 -0.22361213290428206; 0.14042294407221514 0.04361591206557144 -0.15552974588530447; 0.07827050881953174 0.044852187950443025 -0.14858513949331772; 0.06367797985555293 0.04853261484377745 -0.17031868911227985; 0.07705062746199326 0.06988499792176428 -0.255869700080795; 0.037740676452669965 0.038298546103523574 -0.16056044988760493; 0.016837593778687085 0.0187760627425273 -0.08338246506645446; 0.005581052206780898 0.006719399307265381 -0.033457303009394854; 0.0011715535972081144 0.0003030450754018597 -0.0014930591100563015; 0.0008528830301058207 -0.0003583364546188954 -0.00020640811855417857; 0.0017994946975778132 0.0035174650579402906 0.003912496047009316; 0.0004958409297947528 0.0029240647324760938 0.0015576323721511478; -0.001325714634366954 -0.0026920923234032335 0.0026614280661291455; -0.00017533744791697897 -0.002901205083916554 -0.00010429246202732999; -0.0017082585672991057 -0.0025473825296800654 0.005129167056739256; 0.001347236491756602 0.00045164941558803874 -0.0020428893497440146; 0.0010627140142055928 0.0004518179492826397 0.0005552474521960185; 0.0007176615564443218 -0.008239760006699152 0.005075675370086101; 0.0012511114148177648 0.0010086853772492944 -0.0041766132634458416; 0.006359029036504026 -0.0014611743348785277 0.002541654907822043] %
+
+Mass Used: 119.780942543734 kg
+Launch C3: 93.08714603767436 km²/s²
+||V∞_in||: 7.638333496991215e-8 km/s
diff --git a/archive/ES_0.5681246063619044 b/archive/ES_0.5681246063619044
new file mode 100644
index 0000000..809f5a3
--- /dev/null
+++ b/archive/ES_0.5681246063619044
@@ -0,0 +1,22 @@
+archive/ES_0.5681246063619044---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T19:11:45.603
+Launch V∞: [6.160366879619166, -7.511581166138071, 0.16903574614407518] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3354741337223422e-8, -5.24661687049026e-9, 1.7799408802147792e-8] km/s
+ V∞_out: [5.998918283812502e-9, -1.3922081170940566e-8, -1.8369064472567792e-8] km/s
+ time of flight: 1.7406584903131172e8 seconds
+ arrival date: 2028-10-30T10:49:14.603
+ thrust profile: [0.48464032955866726 -0.16343069583300968 -0.16531431830019683; 0.0919006171012298 0.018654728567136264 -0.0937716461791297; 0.09494747905888867 0.043253903695232465 -0.15541613378150437; 0.0595968920144554 0.0376775895843192 -0.13574150888486042; 0.039988578409917215 0.031193647839397015 -0.11730615150410303; 0.042371845226704494 0.03738455801459885 -0.1459289992198482; 0.022965716121955724 0.023147769661767084 -0.09527802142629044; 0.014602562824578943 0.01605876439814439 -0.06651210069449229; 0.008635418924749822 0.010669640281216163 -0.04827175158515965; 0.0050982489546522345 0.0062365244028692035 -0.02903504609344109; 0.0053956784890159025 0.006389782691826988 -0.02751504647836021; -2.9780382061692873e-5 -0.0012891268754453452 0.0012022466203130897; 0.0013713335122088634 -0.002502775395753034 -0.004661473314347057; 0.0004825482155875791 0.0028251065913414376 0.00018758367720483242; -0.006214787300828017 -0.002074932276737408 -0.004413716850822363; 0.00869753415864031 -0.0006340905712431224 -0.001271339706272018; -0.0018237946668598253 0.002810090362377119 -0.0022368759838539073; -0.0052239596242597925 0.0018856815048834369 0.0027119449291953006; 0.004732637852291291 0.00028084624601494476 0.0024828643581211894; 0.00036424009788377405 0.00019277292718532766 -0.001020768006618523] %
+
+Mass Used: 112.13052947785172 kg
+Launch C3: 94.40254479046344 km²/s²
+||V∞_in||: 2.2862525199020193e-8 km/s
diff --git a/archive/ES_0.5681266851193401 b/archive/ES_0.5681266851193401
new file mode 100644
index 0000000..868c2d2
--- /dev/null
+++ b/archive/ES_0.5681266851193401
@@ -0,0 +1,22 @@
+archive/ES_0.5681266851193401---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T04:08:08.518
+Launch V∞: [5.897907635291804, -7.6395801124006315, 0.08151378628158949] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.924568210827299e-7, 5.55152504343701e-7, -3.9045877055902735e-7] km/s
+ V∞_out: [3.5730387140972986e-7, -9.369660116246533e-7, 4.994857689633005e-7] km/s
+ time of flight: 1.737145165285222e8 seconds
+ arrival date: 2028-10-27T18:10:04.518
+ thrust profile: [0.5486694785915271 -0.1899935685034701 -0.1752381019970461; 0.09972415216727447 0.02169278600169451 -0.10186568430184313; 0.08166703732639337 0.03947918690774102 -0.13612296265826002; 0.12615892852337407 0.08555530620496503 -0.2584400357328541; 0.026042799813236137 0.02069743095967631 -0.07643900810513606; 0.02781757735255629 0.025559663347550228 -0.09771766198307504; 0.01730370346962114 0.01792118319143872 -0.0737008315503931; 0.013228285989473444 0.015242582641404167 -0.06524936846186037; 0.01338727312350569 0.01650892326797067 -0.07084485947607733; 0.004853458733934533 0.0064177217212504625 -0.029701232571989755; 0.0005294925322560747 0.0006593501971048405 0.00015554252131042652; 0.0034106058197031002 0.001514581018118541 -0.012540185268922255; 8.572005830546583e-5 -0.00040343881792471146 0.0014030737230490671; 0.00180096644377498 0.0032190177374379655 -0.004977403894504113; 0.0010274877053871884 0.0007166900214824088 0.0018741420266726065; -0.009026561069802779 0.00363842481256173 -0.0036464196746370217; 0.006271865944096209 -0.004295287718210693 0.0007090556368250255; -0.0028009892782466825 -0.010120737858850978 -0.00019389696606877515; 0.009889935098908037 0.0010463513902640206 0.007594552297941561; -0.007642357188291356 0.0019114779534010356 0.0018882827741150336] %
+
+Mass Used: 119.4094635900451 kg
+Launch C3: 93.15514326557457 km²/s²
+||V∞_in||: 1.121218770839412e-6 km/s
diff --git a/archive/ES_0.5681360835650969 b/archive/ES_0.5681360835650969
new file mode 100644
index 0000000..20eb605
--- /dev/null
+++ b/archive/ES_0.5681360835650969
@@ -0,0 +1,22 @@
+archive/ES_0.5681360835650969---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T21:45:55.818
+Launch V∞: [5.952862714802932, -7.88658438164237, -0.13143384217432139] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.920467602759668e-5, 4.3113667689776446e-5, 5.637877576628972e-5] km/s
+ V∞_out: [6.918763779049364e-5, 4.2435406309161015e-5, 1.9370595464470895e-6] km/s
+ time of flight: 1.646230195337962e8 seconds
+ arrival date: 2028-07-14T06:22:54.818
+ thrust profile: [0.22006156858334214 -0.09610473776426372 -0.09318261896264338; 0.05927969804962113 0.00449004436689744 -0.06773845440316754; 0.10040562319890872 0.028781347953053607 -0.18284966491438776; 0.08276409720335225 0.034675303285280505 -0.20524762041013808; 0.06351755827682067 0.030775877675288683 -0.1915948549011061; 0.03062510030359131 0.01745503760016373 -0.11476413502870332; 0.035498256341085443 0.021821697515863457 -0.14836479050894438; 0.017435450747542495 0.012396481684537566 -0.08258821474477006; 0.005243116610351342 0.0031226489470878426 -0.027837109641198836; 0.002101638201498581 0.0019419989673563035 -0.012266122760337677; -0.0006508143784369506 -5.508650977636498e-5 -0.0025448655937762707; 0.0012345175677566204 0.0011600150879224505 -0.007814180719374068; 0.000472402483985779 -4.0505643359862705e-6 -0.003664395926332217; -0.001162587028119479 0.0003322769409013505 -0.0009671758453535945; -8.344449977677271e-6 3.32231517860782e-5 0.00040264831006037193; -0.0035046439255716675 0.0009045110333761276 -0.0016536734289860835; -0.0003149072782637956 0.0005094911822641514 -0.001959045281505163; -0.004255067361092874 0.004030200609880694 0.0009542660659335985; 0.000980786313307379 0.0003875442195958544 -0.00475471966412557; -0.00010857552935890661 0.0003583184183138835 0.001414233541039856] %
+
+Mass Used: 93.18839919721722 kg
+Launch C3: 97.652062564925 km²/s²
+||V∞_in||: 8.108243534205706e-5 km/s
diff --git a/archive/ES_0.5681435821996209 b/archive/ES_0.5681435821996209
new file mode 100644
index 0000000..c169938
--- /dev/null
+++ b/archive/ES_0.5681435821996209
@@ -0,0 +1,22 @@
+archive/ES_0.5681435821996209---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:30:38.980
+Launch V∞: [7.369142124483341, -6.455223110566013, -0.15603783468875398] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000265092731060284, 0.0007113664650282279, 0.0016971967304948538] km/s
+ V∞_out: [0.0016952408176868872, 0.0002031638303517595, -0.0007288952881639747] km/s
+ time of flight: 1.6006712289128962e8 seconds
+ arrival date: 2029-06-04T02:36:00.980
+ thrust profile: [0.38227124763951326 -0.07365520768448439 -0.13424979470101503; 0.10867389225238876 0.03494004863963505 -0.11701862156097585; 0.04504131668819158 0.02640177656524934 -0.08494345198056462; 0.10610453642557763 0.08141790911428536 -0.25645255260375227; 0.047177837687138506 0.04548495637745722 -0.15738173389673418; 0.01841822761849826 0.019372510707087738 -0.0767056982032408; 0.028725315069960376 0.0340863733162355 -0.1370232795186229; 0.017148489147783115 0.021941008563230564 -0.09591748823160784; 0.009066012654737924 0.012282282463987746 -0.05707385303831624; 0.004044874017400549 0.005257551882446934 -0.027520329062022817; 0.00133994170004944 0.0008953680109607233 -0.008749513133353396; -0.0017551639023746079 0.0031816451423481874 -0.006705235681545704; -0.0010812274895082908 0.004080145567020115 -0.0025713149856392394; 0.001241583270037849 -0.001854026845294862 -0.003876294299588313; -0.0017653573793254326 -0.0008832940960249537 -0.00342319976060958; -0.002282068858179107 0.00535733757573009 0.0011922794955440616; 0.004529270072142838 -0.0012751335263390894 0.005218964197074611; -0.006951295013835977 0.007949273528143482 -0.005510012570309843; -0.003755918114488996 -0.002114607319289772 0.00047844249739792703; -0.00045342359598491214 0.002459458819528244 0.006703469554510676] %
+
+Mass Used: 102.84287752695491 kg
+Launch C3: 95.99850886387476 km²/s²
+||V∞_in||: 0.0018592453161512007 km/s
diff --git a/archive/ES_0.5681475937762817 b/archive/ES_0.5681475937762817
new file mode 100644
index 0000000..83327d6
--- /dev/null
+++ b/archive/ES_0.5681475937762817
@@ -0,0 +1,22 @@
+archive/ES_0.5681475937762817---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T16:11:51.779
+Launch V∞: [6.516062301451393, -7.379144789200586, -0.03698589794522666] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.560411027356325e-6, -6.872936005453564e-7, 1.2746389184802008e-8] km/s
+ V∞_out: [8.588951798789117e-7, -1.994179714052037e-8, -4.482194112942093e-6] km/s
+ time of flight: 1.8655921669565138e8 seconds
+ arrival date: 2029-03-28T22:12:07.779
+ thrust profile: [0.2865236455198605 -0.07067320891486599 -0.09523366879454132; 0.06048807427001536 0.018510422326098643 -0.0640178746147443; 0.0729548836703674 0.04070787785019269 -0.12214856791610365; 0.040178630886774286 0.033301997542205065 -0.1030083874200339; 0.04633592028853767 0.04258850123028433 -0.1437753900181285; 0.02719034287681786 0.02667460930499286 -0.10366947625016072; 0.022139104206341742 0.025903470458689508 -0.10068562996334508; 0.004773970965711891 0.005917623078854076 -0.024691874312740263; 0.011153302551804445 0.01434691081267014 -0.06991899025004814; 0.0031713217696782508 0.008579432977949376 -0.035765423908453685; -0.00032045445918483595 0.003351675053588158 -0.010053265153133269; -0.005743413182194524 0.0009779150698847165 -0.011514345678308035; 0.0010383353325618923 0.0015486564310371268 -0.011949706608147306; 0.0003981103954681137 0.0051450565069291595 -0.004413970095798154; 0.003588104555129038 0.0014021295326946434 -0.0005759948479184575; -0.014893826479394244 0.005585307845064138 -0.013557787366400216; 0.01588339767749353 0.02151900981108662 -0.003547856734471014; 0.001842915425891183 0.00040499665533360284 -0.007051574184487631; -0.014274694253346255 0.01046960435307228 -0.014518512549015145; 0.015266435152271409 -0.0007184038591808316 -0.005162777256434147] %
+
+Mass Used: 97.51761286299279 kg
+Launch C3: 96.912213693029 km²/s²
+||V∞_in||: 4.611928414689567e-6 km/s
diff --git a/archive/ES_0.5681691621626597 b/archive/ES_0.5681691621626597
new file mode 100644
index 0000000..8a12f7b
--- /dev/null
+++ b/archive/ES_0.5681691621626597
@@ -0,0 +1,22 @@
+archive/ES_0.5681691621626597---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T22:19:59.013
+Launch V∞: [6.304770203070629, -7.677810616233178, -0.05524675049829887] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.247841705735233e-9, -3.3160205056803304e-9, 7.207036578957902e-9] km/s
+ V∞_out: [8.290936275518523e-10, -1.967473879123252e-9, -8.076053005051606e-9] km/s
+ time of flight: 1.753357087893887e8 seconds
+ arrival date: 2028-11-17T06:41:47.013
+ thrust profile: [0.10405946472689266 -0.03675147988394596 -0.03926164524755106; 0.0928494979897201 0.014939840170398556 -0.09815213432600124; 0.06384214298020224 0.024541585515699297 -0.11111181870685624; 0.0815729778207743 0.043778285635781684 -0.19712972700012504; 0.05974748790339887 0.03856761214333249 -0.1816344556748262; 0.028819756710652625 0.020898563231472284 -0.10439579729688543; 0.02104044012676511 0.016656375316205233 -0.08813869774365836; 0.014181905169430145 0.012240170422373844 -0.06759451655617198; 0.0027061207374700575 0.0022598455334790295 -0.014597297364214794; 0.0038594222447201005 0.0030736173362973245 -0.040924035738446274; 0.002507403356417334 0.0030018192793464637 -0.017293238279267382; 0.0017435045350291901 0.001809773000372993 -0.011773220415637267; 0.0031166697801864093 0.002052394833290404 -0.006650745187629497; 0.005275020235387704 -0.0003558545914114611 -0.017361045327102493; 0.010345881316430336 -0.0006973245925577911 -0.0036485906351951623; 0.0018449290029708648 -0.00030233802871927054 -0.00335423323713389; 0.005981081611500244 -0.005454770900569204 -0.00631024339589701; 0.0029022127871348516 0.0011014610664774845 -0.0068736329627723; -0.020067074793802115 -0.0001703907587121451 -0.005740490649325414; 0.0053701220063477155 0.011906302928664757 -0.0026500745368208626] %
+
+Mass Used: 87.1026161647901 kg
+Launch C3: 98.70195537571078 km²/s²
+||V∞_in||: 8.998973686010715e-9 km/s
diff --git a/archive/ES_0.568173953376528 b/archive/ES_0.568173953376528
new file mode 100644
index 0000000..aa76fde
--- /dev/null
+++ b/archive/ES_0.568173953376528
@@ -0,0 +1,22 @@
+archive/ES_0.568173953376528---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T22:16:55.925
+Launch V∞: [6.481613468728088, -7.399907948859346, 0.17421409251401604] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.226314033762785e-8, 5.179316300162053e-8, 1.8220754203561085e-8] km/s
+ V∞_out: [-9.904739202728776e-9, 3.6675888370624693e-8, -5.164482191504405e-8] km/s
+ time of flight: 1.824495951179671e8 seconds
+ arrival date: 2029-02-07T14:43:30.925
+ thrust profile: [0.3187416602508587 -0.0878939191975884 -0.10853594070603943; 0.05401543366838243 0.014646043110580593 -0.0572666369289925; 0.048852779064804626 0.026272593826924165 -0.08568538664597147; 0.051113231471524724 0.03752157435390958 -0.12302188044026752; 0.0337402242294912 0.030132912537169373 -0.10497008912832718; 0.03436023659869388 0.035553737640382006 -0.1283305104838746; 0.014543216489317827 0.016541111583937795 -0.065307947310093; 0.014591934339784517 0.01908328136589903 -0.07521562225945023; 0.011249412954656295 0.01638472444579729 -0.0671830847494598; 0.007100285910324727 0.009544270397599558 -0.04782023839190327; 0.0027341243600493116 0.005590419408185253 -0.03070976538910001; 0.007187018327487972 0.009889329363958055 -0.05242598388282921; 0.0018492421685285493 0.004874704965093701 -0.009015987072691816; -0.0029632446792641344 0.004368839780253167 -0.0007821208083381788; 0.002403797973843951 0.006721746909646415 -0.0035652107006760793; 0.0097614939390189 0.0005012723832725302 -0.015803397060954415; 0.002545106577810389 0.0004543686580263496 -0.002090827273967818; 0.00807387697157996 -0.0061688979986905465 -0.009173799309268132; 0.0010330281735564033 0.000878776950552572 -0.0046050107913434436; 0.008317979550327603 -6.859695421464348e-7 0.012268236523789942] %
+
+Mass Used: 98.20118767483518 kg
+Launch C3: 96.80030135961957 km²/s²
+||V∞_in||: 6.368231969632145e-8 km/s
diff --git a/archive/ES_0.5681766610695796 b/archive/ES_0.5681766610695796
new file mode 100644
index 0000000..4813d51
--- /dev/null
+++ b/archive/ES_0.5681766610695796
@@ -0,0 +1,22 @@
+archive/ES_0.5681766610695796---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:58:09.355
+Launch V∞: [6.667004341591415, -7.335112297604253, 0.11461713209610444] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.910730833218704e-6, 7.511979339193638e-7, -1.919102942452159e-8] km/s
+ V∞_out: [-1.357519860358579e-6, 2.9540776448974463e-8, 6.8178399038497e-6] km/s
+ time of flight: 1.874957778749278e8 seconds
+ arrival date: 2029-04-09T05:07:46.355
+ thrust profile: [0.17536921747929196 -0.04568535447358376 -0.06051987003038495; 0.08602770904342345 0.02196349981130064 -0.09044750557752607; 0.05900036830732696 0.029518773841386216 -0.10795553942018818; 0.04897484682876306 0.03131312024745316 -0.1223677550437423; 0.03677708660863716 0.028130348296365834 -0.11774795785202258; 0.027281975564507708 0.021309025831262565 -0.09872931860370301; 0.017095946099742187 0.016967816505173865 -0.07412671080126003; 0.01713782882308886 0.018140919929293283 -0.08205767445871445; -0.0027547920977659063 0.005521845472523507 -0.025961535013880044; 0.005482017411591558 0.010106998769739872 -0.03241748237412069; -0.0020669919127090574 0.010990785328135586 -0.028281475181634548; 0.007806089229201531 -0.001525303006868218 -0.019209123164696338; 0.0041985228305208445 -0.0030147058690078855 0.0028627498392002028; -0.0026902584324227877 0.0064443314280187135 -0.010822811479493044; -0.0008538091094766713 -0.0026164027655947823 -0.011225617287369337; 0.014905263676227694 -0.001756347859757975 -0.014462962021544214; -0.0002763687714256583 -0.0016607145500623813 0.007641591413018568; 0.0033932831567412853 -0.0007848920406543381 -0.009232236939392836; 0.0027715056893757328 0.009985632921962084 -0.03552829551057103; 0.00011574136002614338 0.0033257654072882063 -0.007305000070849929] %
+
+Mass Used: 89.65469226981213 kg
+Launch C3: 98.26595639623385 km²/s²
+||V∞_in||: 6.951465117565848e-6 km/s
diff --git a/archive/ES_0.5681947209540541 b/archive/ES_0.5681947209540541
new file mode 100644
index 0000000..a88aaef
--- /dev/null
+++ b/archive/ES_0.5681947209540541
@@ -0,0 +1,22 @@
+archive/ES_0.5681947209540541---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T13:14:19.716
+Launch V∞: [6.2843410316608885, -7.269510899302277, 0.25297311379467863] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.954578282159343e-7, -3.055096288224034e-7, -2.1649926188521662e-7] km/s
+ V∞_out: [9.369354995899155e-8, -2.2679401431934935e-7, 3.1736283901004793e-7] km/s
+ time of flight: 1.8749577796228412e8 seconds
+ arrival date: 2029-04-04T15:23:56.716
+ thrust profile: [0.49338593105817546 -0.09133397594857054 -0.11595060771789652; 0.29026063007753 0.11524469647852267 -0.2014887806107844; 0.07214671131682002 0.053476071857323386 -0.09389091502009114; 0.06693118110769335 0.0683336471962752 -0.12029157946688665; 0.07025471000529804 0.0898719923398763 -0.16224001349844858; 0.01842819321601765 0.028650351322779283 -0.05686462055501356; 0.02246518493100764 0.03932274303797064 -0.07723142229549171; 0.011520914222958348 0.02340800051756728 -0.05221915186765486; 0.002919334769686517 0.006947511261790257 -0.015095763492306053; 0.0021104426817548268 0.005432231577068782 -0.012358903323155845; -0.0020906445592871535 9.349286568717009e-5 -0.005071943407150257; -0.00024962737572315977 0.0001641255399315749 -0.0006208804903144573; -0.0015267545613473128 0.0034815533949102066 -0.0038604015053651857; 0.0033910222762126027 0.00023804498704526212 -0.002315663671080546; -0.0016450369062962437 0.0014733134210781016 -0.00039563529888818295; 0.0022701521836348336 -0.0025414952484155034 -0.002089588251585014; 0.0015648661705533623 0.002744024577124554 -0.003458737546983236; 0.002744491557081827 -0.004908934465849436 0.0014422988906038605; -0.001915044164213508 0.007821100774562013 -0.0007762744680109223; 0.004640021351459846 0.0023704666568873994 0.0014316275853855065] %
+
+Mass Used: 123.8779376170969 kg
+Launch C3: 92.4027263135942 km²/s²
+||V∞_in||: 4.223882412081757e-7 km/s
diff --git a/archive/ES_0.5681980608269791 b/archive/ES_0.5681980608269791
new file mode 100644
index 0000000..295a901
--- /dev/null
+++ b/archive/ES_0.5681980608269791
@@ -0,0 +1,22 @@
+archive/ES_0.5681980608269791---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T09:19:07.940
+Launch V∞: [6.405387860785678, -7.321798895683742, 0.10180323670848689] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.849216404722567e-5, 2.9718334185716227e-6, -4.1415928709722906e-8] km/s
+ V∞_out: [-3.3209609230671924e-6, 7.155759302444761e-8, 1.84241114316457e-5] km/s
+ time of flight: 1.8474282478763044e8 seconds
+ arrival date: 2029-03-05T14:46:11.940
+ thrust profile: [0.4288897595944264 -0.11230551560250554 -0.13765751511260538; 0.11737746950295201 0.033721963066072315 -0.11344510671789712; 0.08727263645405593 0.04872819317980974 -0.14158994754909224; 0.05296101733299312 0.03934564061749807 -0.12071791862551919; 0.05403499460481881 0.049130261689550626 -0.15645874493327563; 0.025812740986848826 0.027090991554107532 -0.09099168423774358; 0.025659594495485064 0.030654670920434824 -0.1091887847753635; 0.003510289665957463 0.00694083936612475 -0.01758985302615813; -0.0001812895273004796 0.002554324405587863 -0.01913948478525346; -0.001576762742437822 0.0017546303200310868 -0.02230804489606237; 0.0003192366818584001 0.0005743732309055072 -0.004252036582180686; 0.002463598925675938 -0.0026084864370861573 -0.0019222676608701451; 0.00025468919776132045 0.0035284068253396044 -0.00881864132300729; 0.00253366516637716 0.01352425949334827 -0.007110154540835579; 0.009406767201316408 0.012718178698911465 0.003234369347174278; -0.0024792402967973304 0.0016293677942500922 -0.0004572046970424113; 0.01227504915540339 -0.0011735280894635044 -0.016872116810245294; 0.003117618453185768 -0.0019193551626967699 0.010455305233728526; 0.005444289444964256 0.0030016844533766853 -0.027428378317868853; 0.001569229279505265 0.0008344111683745084 -0.0027325397865242103] %
+
+Mass Used: 110.78384071098935 kg
+Launch C3: 94.6480966149405 km²/s²
+||V∞_in||: 1.8729485852430536e-5 km/s
diff --git a/archive/ES_0.5682188348408466 b/archive/ES_0.5682188348408466
new file mode 100644
index 0000000..bf4b3c7
--- /dev/null
+++ b/archive/ES_0.5682188348408466
@@ -0,0 +1,22 @@
+archive/ES_0.5682188348408466---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T00:18:19.170
+Launch V∞: [6.303804249118622, -7.224319079375126, 0.2284451862084059] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0086569429013066, -0.00025273430660503163, 0.005721177416750999] km/s
+ V∞_out: [-0.00993708015360349, 0.00010235170102209608, 0.0029865168089792385] km/s
+ time of flight: 1.8749577785380045e8 seconds
+ arrival date: 2029-04-05T02:27:56.170
+ thrust profile: [0.5635485942170899 -0.12348212982333802 -0.14786835735035014; 0.24569181289525688 0.08895084153840963 -0.19549388717763622; 0.11925284149822934 0.08097103695816851 -0.16240243073922483; 0.035348397785000686 0.03338542816887378 -0.07410587988319421; 0.04658131620892151 0.05466332183847645 -0.12187280383885545; 0.025748376266604277 0.03594114053659076 -0.08603529273327862; 0.007756415493949948 0.010519930382456693 -0.02736190148941757; 0.01568125897804668 0.025862180046872178 -0.07178902484976947; 0.003620131478766852 0.006857210179468 -0.02505490885329794; 0.004831146054654257 0.010183247712152971 -0.03172244943541284; 0.00187990433627605 0.0020916803944315324 -0.007063188355176603; -0.0029296194173144955 0.002663610367463663 -0.002400585452050619; 0.0016612733709077893 -0.0006161202808720599 0.001665444649038633; -0.00030959587076350803 -0.0014872259589546345 0.0025934186907080395; -0.001747158769364994 0.0013723308826442062 -0.0015440624427770708; -0.0064752465909617115 -0.004222057241306331 0.002751291751122598; -0.001386428394870735 0.0018227141848448484 0.0010912939328123642; 9.698713001825532e-5 -0.00036927337118987684 0.0024234630798903585; 0.011379644293152698 -0.004497296424940872 -0.007264564838444248; 0.0083228495905639 0.006457667135776892 -0.002356026897163389] %
+
+Mass Used: 126.36659929388861 kg
+Launch C3: 91.98092137493126 km²/s²
+||V∞_in||: 0.010379711270558516 km/s
diff --git a/archive/ES_0.5682239253215048 b/archive/ES_0.5682239253215048
new file mode 100644
index 0000000..a064901
--- /dev/null
+++ b/archive/ES_0.5682239253215048
@@ -0,0 +1,22 @@
+archive/ES_0.5682239253215048---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T13:48:00.304
+Launch V∞: [5.9703511438874495, -7.68363067769967, 0.13205358833891045] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.014803838922210183, 0.011106770353824427, 0.011777351138441399] km/s
+ V∞_out: [-0.009639554580990752, -0.01652110458620164, 0.010739991790417881] km/s
+ time of flight: 1.6884134236198246e8 seconds
+ arrival date: 2028-08-30T18:10:22.304
+ thrust profile: [0.43121522327591444 -0.1605533895701006 -0.14844806035943547; 0.144601758452867 0.025068833174722742 -0.14324373636684373; 0.08101264702984708 0.03390745464974535 -0.1324773274440365; 0.0579526437037444 0.03402368199262318 -0.12981731057679566; 0.039325827638524054 0.028264248706867827 -0.11184335614845375; 0.028229497304127927 0.023726839852740083 -0.09877532147754649; 0.037835548263620636 0.03683259784903283 -0.15399213841320433; 0.024567080781204367 0.024724818781147302 -0.10606146010000653; 0.009270983143259762 0.009691301242460688 -0.045821378852760115; 0.010279716182444231 0.011870970214463279 -0.05581080517668005; 0.0009685818627508435 0.0006027863340904465 -0.0016789560103832601; 0.00436341626830792 0.004473782330799364 -0.02392807059424146; -0.0002326835851698822 0.0007545184838733663 -0.002369403710737935; 0.00042601700579031256 0.0004425839906337446 -0.0022523571854690828; 0.00013769106958348926 0.00013633637689348927 -0.0005838043626590456; 0.0009495439985733618 0.0009980361469132738 -0.001437706797334028; -0.0005610550796006112 0.0018352837116333454 0.0008962158637334594; -0.0009106216767784192 -0.0012127310928286453 -0.00048170621996361366; 0.0006406804692118007 0.00128167704042873 -0.001152776648805876; -0.0008077993181729868 0.0008925982797597419 0.0025112735249828034] %
+
+Mass Used: 110.50709682542902 kg
+Launch C3: 94.70071132279884 km²/s²
+||V∞_in||: 0.021936727065938647 km/s
diff --git a/archive/ES_0.5682452211361938 b/archive/ES_0.5682452211361938
new file mode 100644
index 0000000..2253a51
--- /dev/null
+++ b/archive/ES_0.5682452211361938
@@ -0,0 +1,22 @@
+archive/ES_0.5682452211361938---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T20:08:23.612
+Launch V∞: [6.206462087063948, -7.314814192841574, 0.0735754968307732] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00011646385978969818, 0.0001414789667806811, 0.00012399722673704587] km/s
+ V∞_out: [-0.00013914593131420089, -7.154414626549702e-5, 0.00015635733956989738] km/s
+ time of flight: 1.8464324632757208e8 seconds
+ arrival date: 2029-03-01T21:55:49.612
+ thrust profile: [0.5483141537056525 -0.13989601641287158 -0.11078534951911291; 0.19191799882370503 0.07153946704885665 -0.13945838221758172; 0.1414785754713842 0.10045676203698363 -0.16657071661928222; 0.07714679663464999 0.07589243291894332 -0.132862354819557; 0.029843461491522214 0.03690472933598236 -0.07095538198325216; 0.02464964696429314 0.03767688913935909 -0.07415995602924982; 0.03632298926632795 0.06205038675834969 -0.12165888635601378; 0.014774665029585472 0.029396106056484017 -0.0627985505598006; 0.004791978294388203 0.010676422710667342 -0.024065396173676354; 0.004488149634584825 0.009507500434210185 -0.022671605272015276; 0.0034793420227646555 0.008482085915653474 -0.019688658221707914; 0.0014041769709634102 0.0020987135997352978 -0.0050504846496878895; 0.0013401496441802156 0.0009261140296886051 -0.001108942307826793; 0.003007558714066317 0.0023298521794735587 -0.002005395381190521; 0.0010142100570677977 0.0009483927614701817 -0.00012498039200097661; 0.0004614029247235297 0.00014354118144282952 0.0009040470416703888; 0.0016461165659528165 0.0009283020653002949 -0.0006727931685090237; 0.00039523115879465604 0.0010464783026433513 -0.0015951961547832102; -0.0002660539644449969 -0.0006350263284283126 0.0007739858188822455; 0.0014405383163381873 0.0005901486772924317 -0.0005826525823193194] %
+
+Mass Used: 126.0988899306858 kg
+Launch C3: 92.03209166769261 km²/s²
+||V∞_in||: 0.00022125876461040342 km/s
diff --git a/archive/ES_0.5682619598530758 b/archive/ES_0.5682619598530758
new file mode 100644
index 0000000..0475f0d
--- /dev/null
+++ b/archive/ES_0.5682619598530758
@@ -0,0 +1,22 @@
+archive/ES_0.5682619598530758---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T18:48:15.653
+Launch V∞: [7.340602921612862, -5.74202143914186, 0.4105092581597476] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8671008904931163e-6, -2.7930484151807265e-6, -2.548782936015524e-7] km/s
+ V∞_out: [2.4155074407590573e-7, -1.1854365796950464e-6, -3.139780764960387e-6] km/s
+ time of flight: 1.8456873408154154e8 seconds
+ arrival date: 2030-03-12T23:53:49.653
+ thrust profile: [0.950800566108284 0.0001619525704873658 -0.11409625044982145; 0.2567926364843201 0.18353857369591556 -0.15858766450100942; 0.12815599243335576 0.15488667654521726 -0.15636806877401613; 0.03360023008002366 0.060016327507311805 -0.06756349282230176; 0.0637825302848404 0.1262030742726989 -0.14095101432204019; 0.01239513740166397 0.03666426971029943 -0.04795398196680295; 0.0070930073806699185 0.03362952921278936 -0.046907950417854456; 0.005243503187894076 0.03284575977412965 -0.04824047085524905; 0.0051444280226969836 0.03369549359733826 -0.0492178217429074; 0.00014012077203447336 0.0006539033420510822 -0.001722029731691786; 2.46767766597149e-6 5.1323043383217066e-5 0.0003525528079442843; -8.798974131737859e-5 -0.00033384590560600093 0.00019500199265599038; 8.575082091540456e-6 -0.0003052665256293162 0.000540055793793849; 0.0011465131286756054 -0.00272683159796674 0.0005654152177459676; 0.00021996133054541132 6.198114845236196e-6 0.0003019925721582051; -0.001113197344222638 0.00010433714437020213 -0.0005752064481885711; -0.0011658767549358533 -0.0008684904324034438 -0.0003054087707882739; 2.925662154841861e-5 0.0006798297039316639 -0.0002341401797474156; 0.001781299334082857 -0.0006906282572920319 -0.0004807621943812004; 0.0012174627449899338 0.0003574430964405349 -0.001086545874114595] %
+
+Mass Used: 155.3335738454748 kg
+Launch C3: 87.02377931139091 km²/s²
+||V∞_in||: 3.3692949009211104e-6 km/s
diff --git a/archive/ES_0.5682847201308769 b/archive/ES_0.5682847201308769
new file mode 100644
index 0000000..da00d54
--- /dev/null
+++ b/archive/ES_0.5682847201308769
@@ -0,0 +1,22 @@
+archive/ES_0.5682847201308769---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T19:45:31.141
+Launch V∞: [6.449281771561744, -7.31742973317731, 0.5525027143607836] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00045445628739818305, -0.0028490174882331715, 0.003986649408307132] km/s
+ V∞_out: [-0.0033106869425711975, -0.0028777413572391468, -0.0022259989745501687] km/s
+ time of flight: 1.8142634424805427e8 seconds
+ arrival date: 2029-01-23T15:57:55.141
+ thrust profile: [0.39561691842483476 -0.10337405978328805 -0.10720350021887597; 0.14197924676719503 0.045756744482563595 -0.12721039696594824; 0.09482555834998749 0.05977965608592975 -0.14433483179966505; 0.058167063165918374 0.04934641377494276 -0.1237361452226954; 0.04554752241388637 0.04887281798614506 -0.12707377477288698; 0.028542713642409866 0.03661075426255007 -0.10015281908692632; 0.021263920722031735 0.027755198263049438 -0.07838244403795251; 0.013123251059889292 0.021625779563111586 -0.06300855749922586; 0.006719644713612131 0.01004372045660452 -0.03181296993084531; 0.0028933948725386074 0.004834582965666013 -0.0144889801671417; 0.004915337738742561 0.005418315577083092 -0.02005103002010775; 0.0004895784463795782 0.0030545670898918143 -0.00864324198048265; -2.7505761771438614e-5 0.0029721429034287473 -0.002899920152676917; 0.0006837539604790305 -3.461476467390935e-5 -0.0013395048747476693; -0.001629582453382471 0.0009824944214919923 0.003038088432908332; -0.0006891536832772766 -0.001427992445206765 -0.007665833373724346; -0.0019054530261297848 -0.001117098084111779 -0.0007904960598278899; 0.0015513433942953346 0.0019238962408052434 -0.004290406300255914; 0.002761487053998887 -0.0005547545862793648 -0.0032140541161254955; -0.006323713394641136 0.0034882641490371173 0.0016199937950568516] %
+
+Mass Used: 106.24641712891162 kg
+Launch C3: 95.44327251836198 km²/s²
+||V∞_in||: 0.0049210572715799395 km/s
diff --git a/archive/ES_0.5682946598738513 b/archive/ES_0.5682946598738513
new file mode 100644
index 0000000..8daabae
--- /dev/null
+++ b/archive/ES_0.5682946598738513
@@ -0,0 +1,22 @@
+archive/ES_0.5682946598738513---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T22:47:40.344
+Launch V∞: [6.232608472712914, -7.221728840531365, 0.2805583019956382] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000889418950314275, 0.0008346630335920475, 0.0007756823780456589] km/s
+ V∞_out: [-0.0009685543344286868, -0.00046793925817846906, 0.0009642497635309713] km/s
+ time of flight: 1.8388462047642335e8 seconds
+ arrival date: 2029-02-21T05:51:20.344
+ thrust profile: [0.7063493231859531 -0.1869976451713787 -0.2045665644857186; 0.1773997905688999 0.0525667545548453 -0.1591925838675762; 0.10989655138472726 0.06428076350455483 -0.16625942668264385; 0.05523905312391381 0.04429616920899156 -0.11895262769605518; 0.05865285461995991 0.05745259358883221 -0.1611919076125898; 0.022404169671869336 0.02625430810029736 -0.0775390077093; 0.014913429804921696 0.020060155939252946 -0.06068847141658711; 0.0014894974093365505 0.0020343800679185546 -0.007611380262548454; 0.00303252552700177 0.004008561048807953 -0.01264208858891278; 0.004436279851840573 0.0076650792682538705 -0.02870285710963535; -0.0002694197265750676 0.00013238967408700313 -0.0007348619553568326; -5.974470265694579e-5 0.0018896150590350163 -0.002939159625322277; 0.001575722528600164 -0.0012103534096845503 -0.00035236079893477545; -0.0038304796868204962 0.0003024071673185264 -0.0028614805958865775; -0.006847196461666056 -0.0030607509202926083 -3.20513404229051e-5; -0.0015267562792602536 0.002053642867792603 -0.0007717001613866915; 0.0028689253257724073 -0.00020952499959848097 -0.00030418839723783133; -0.00014728536054541995 0.0009811210546560145 -0.0022241550284951856; -0.012655135975135888 -0.01982019925547514 -0.005678573996439728; -0.0044392503116835865 -0.012265685026943873 0.006211007747201021] %
+
+Mass Used: 131.72508529632842 kg
+Launch C3: 91.07748878111397 km²/s²
+||V∞_in||: 0.0014454797129097989 km/s
diff --git a/archive/ES_0.568317876690575 b/archive/ES_0.568317876690575
new file mode 100644
index 0000000..b6a1e70
--- /dev/null
+++ b/archive/ES_0.568317876690575
@@ -0,0 +1,22 @@
+archive/ES_0.568317876690575---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T14:56:00.712
+Launch V∞: [5.9131349717017105, -7.637360416911568, -0.0026186715874819836] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.014263772839717373, 0.010965428879444772, 0.01048306927742349] km/s
+ V∞_out: [-0.009385378217938802, -0.015584008239993927, 0.010129257950042235] km/s
+ time of flight: 1.705376008937903e8 seconds
+ arrival date: 2028-09-19T10:29:20.712
+ thrust profile: [0.5385969861345603 -0.19624173298129477 -0.17976885333305734; 0.1421323880640811 0.02602668069629738 -0.13524778541341975; 0.06395736304181115 0.027712931141889458 -0.10066219359667249; 0.07126364464846711 0.043422508740063766 -0.15154650629125302; 0.052024118445738274 0.03892122320655339 -0.1401864322879246; 0.03822706997055079 0.033366569370117234 -0.12451862461378141; 0.061213141918859765 0.05997342583374238 -0.22249401618103934; 0.006334380514319949 0.00671586875722252 -0.03396748993983431; 0.0051299147044037135 0.0054950069839032264 -0.025974651694617094; 0.0008995723204653966 0.00047127544182015246 -0.006692444492192414; 0.002408347499498916 0.002993028996987717 -0.009435458020358395; 0.00011454493223361849 -0.0015068152573152632 -0.004290628238243747; 0.0010890996820252308 0.0010253954155689748 -0.004484431482203712; -0.0030951350228609403 0.005073307604437692 0.0014210672912567234; 0.0003493919213195468 -6.685925247346353e-5 -0.00026453073975041307; -0.006007897056747162 0.001969959659713224 0.005160259538532103; 0.003715863690718329 0.007519836366796351 0.002568066950551325; -0.00040253721190939803 -0.0044220035708280245 -0.0011326883931901564; 0.0011988164451818724 -0.00010955161138047044 -0.0007310495235584389; -0.0004629037973127209 -0.005295559534166274 -0.008807994330624888] %
+
+Mass Used: 118.8199200376107 kg
+Launch C3: 93.29444618881031 km²/s²
+||V∞_in||: 0.020822838125684997 km/s
diff --git a/archive/ES_0.5683187131183755 b/archive/ES_0.5683187131183755
new file mode 100644
index 0000000..8345815
--- /dev/null
+++ b/archive/ES_0.5683187131183755
@@ -0,0 +1,22 @@
+archive/ES_0.5683187131183755---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T16:27:14.283
+Launch V∞: [8.038478837990782, -5.704141864738036, 0.043092548137285525] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.7099915953798755e-6, 4.075011457594111e-6, -2.9216125693649398e-6] km/s
+ V∞_out: [9.162215592110164e-7, 6.80828463558558e-6, -3.32818464740811e-7] km/s
+ time of flight: 1.8749577787459508e8 seconds
+ arrival date: 2030-04-23T18:36:51.283
+ thrust profile: [0.27133224208222256 -0.0003566622909377333 -0.08921832575646048; 0.08044727256425124 0.04551282597785067 -0.09640015798948619; 0.05856502719186089 0.05334491205249083 -0.12614909142484426; 0.04028221886122452 0.048036455345244235 -0.1302511950575153; 0.020125467913081355 0.02890494604761309 -0.09419830827926343; 0.008682934242767879 0.01698219003605006 -0.061328709779480954; 0.013022169003539292 0.018658831674706222 -0.09031954172336708; 0.010090836188272693 0.029360140309355753 -0.0885994947847664; -0.0015080571844475407 0.0047759470217742465 -0.014174780502241885; 0.0003382415244466995 0.006629599630124918 -0.00857664769735456; -0.003339259627173118 0.00475441299563177 -0.005598642945554807; 0.0012541236967154549 0.0019705725458198705 -0.01722990134067705; -0.012060374436739766 0.00488137344452184 -0.006431846045863618; -0.0016001832992877355 -0.0034872179932776094 0.008852572421590306; -0.0019834344119811884 -0.002042509068409513 0.005194798300649357; -0.003577949328661001 0.007587941274221816 0.002987233322467744; -0.04296363637088417 -0.004806363351743563 0.019004463540530366; -0.005380339389088827 0.0005004028418739851 0.007725548413581006; 0.01663153284873864 -0.0055851132662605345 0.0500655062982355; 0.0024906531082840386 -0.018348011256774408 0.017160670780310413] %
+
+Mass Used: 96.29380374884295 kg
+Launch C3: 97.15623340958773 km²/s²
+||V∞_in||: 6.879357470981105e-6 km/s
diff --git a/archive/ES_0.5683215587298596 b/archive/ES_0.5683215587298596
new file mode 100644
index 0000000..a6af306
--- /dev/null
+++ b/archive/ES_0.5683215587298596
@@ -0,0 +1,22 @@
+archive/ES_0.5683215587298596---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T13:36:05.201
+Launch V∞: [7.354601744794448, -6.523217229490511, -0.15576525235548386] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00034522329505784266, 0.00023956752011125812, -0.00011430326553720238] km/s
+ V∞_out: [-0.00019445524783221393, -0.0003306436226571776, 0.00020583992417366805] km/s
+ time of flight: 1.6082378499321592e8 seconds
+ arrival date: 2029-06-13T22:52:29.201
+ thrust profile: [0.2538268807834722 -0.05133257732166937 -0.09855196257625774; 0.2021024979656654 0.06045433709991752 -0.22429051161518387; 0.07900205980546314 0.04204686055678553 -0.1510360148526541; 0.06490140181279212 0.04503796742532501 -0.1736227960767378; 0.05436816698824399 0.04453810469070485 -0.18650748015618085; 0.03565619451465826 0.03259466453189575 -0.14835972786653245; 0.022655895956541824 0.022511922626896892 -0.11089400294247863; 0.004541576331952961 0.004987080586361997 -0.027346342011647262; 0.0011071455339348015 0.0007224198173411801 -0.004775502711042356; -0.0023016859997986414 -0.00522273528835494 -0.01826242602215391; 0.0005987719489957814 0.0024552863716565676 -0.005634978068224146; -0.001608275517402695 0.0015385881898149917 0.003842113643899192; -0.0031657837004523634 -0.001207770537022568 -0.0015717710168692; -0.0009066709524021409 0.0018715988535115172 -0.004482516343455644; 0.0016798666410587748 0.00020292626220777684 0.0031460258901763235; -0.0023518415213102167 -7.683912138338033e-5 -0.00187311212002009; -0.002693221809706363 5.789196755095287e-5 -0.003589590051902528; 0.0035897532918561566 0.01735884445130899 0.009320828874712014; 0.011146154003707467 -0.002140635307488936 0.01936501050511363; 0.0008181619961110526 0.0006786778306775203 -0.0005440466195695487] %
+
+Mass Used: 99.15219465943846 kg
+Launch C3: 96.66679266149676 km²/s²
+||V∞_in||: 0.0004354732559587564 km/s
diff --git a/archive/ES_0.5683333777767325 b/archive/ES_0.5683333777767325
new file mode 100644
index 0000000..6d36699
--- /dev/null
+++ b/archive/ES_0.5683333777767325
@@ -0,0 +1,22 @@
+archive/ES_0.5683333777767325---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T16:07:28.472
+Launch V∞: [6.297614191167729, -7.525117595161667, 0.11021983246072692] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.6599461257159465e-6, 6.868556304321978e-7, -1.685771482377342e-8] km/s
+ V∞_out: [-8.915805617205604e-7, 2.055142915025234e-8, 4.626038602983612e-6] km/s
+ time of flight: 1.8040842144735357e8 seconds
+ arrival date: 2029-01-15T17:34:29.472
+ thrust profile: [0.34071442699221277 -0.10411464319377901 -0.11872860272913996; 0.06285449345415009 0.014391989050088335 -0.07174157637254987; 0.06015777218320073 0.028493426427213663 -0.11260648388213004; 0.058485128106128215 0.036738793136512696 -0.14582372643544564; 0.034190441052133126 0.026742851054937514 -0.11385033381809391; 0.021195831526318976 0.020249621843349625 -0.0907112083134509; 0.01917401358693834 0.021556442973237083 -0.0900734271178755; 0.01885924909632839 0.022557833744862893 -0.10553649312089004; 0.011238906794691535 0.01394837872990348 -0.07924117539866814; 0.005009836383350276 0.005492720604671372 -0.03308733857545883; 0.0030525818007525567 0.002328198712753379 -0.003366412604339252; 0.0022327619151884487 0.002894233608672861 -0.016666183487326493; 0.0047018383778006075 0.001043541999301823 -0.008119755337826131; 0.00995043189782481 0.0043708699754371905 3.499616562928527e-5; -0.0030677371492253197 0.008630341025279075 0.00035084515652296713; -0.0008949297878571097 0.0026993786817670353 -0.0026767165661260323; -0.0013089557048657097 -0.01587710581570762 0.0015209807943262696; 0.01791310522034614 0.005441290158890412 0.00573734392413178; 0.0015272178781802776 -0.0028361014179297105 0.011097763382540541; -0.0067147963880418065 -0.0003969075486868966 0.001756455068983363] %
+
+Mass Used: 101.30859562874139 kg
+Launch C3: 96.29948773327655 km²/s²
+||V∞_in||: 4.7103240582979585e-6 km/s
diff --git a/archive/ES_0.5683437029839276 b/archive/ES_0.5683437029839276
new file mode 100644
index 0000000..45cce9a
--- /dev/null
+++ b/archive/ES_0.5683437029839276
@@ -0,0 +1,22 @@
+archive/ES_0.5683437029839276---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T05:21:58.733
+Launch V∞: [6.551623643136607, -7.320770040378381, 0.253030841877942] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.628821955127288e-7, 0.0002213197245632164, -0.00012220593184850264] km/s
+ V∞_out: [-0.00012820092050345005, -0.00021317982013470302, 4.450313488171139e-5] km/s
+ time of flight: 1.808180027242032e8 seconds
+ arrival date: 2029-01-17T00:35:20.733
+ thrust profile: [0.3341032450105635 -0.09569153062639668 -0.10595707949936288; 0.07891246086947709 0.021404715510024052 -0.07712919550385951; 0.07299193078956362 0.03993989668961516 -0.11741523808499449; 0.08832670681231623 0.06616600160444262 -0.19308834995618762; 0.04297276090856244 0.039385515156265705 -0.12330229345350789; 0.0233011375818148 0.024823126355562112 -0.08283176018264225; 0.03134853877326429 0.03833538557118116 -0.13012034515071966; 0.00744550167753329 0.010029756921459724 -0.03771766463520847; 0.009571569444244345 0.014077815506691141 -0.053593781053732935; 0.0034317815728994324 0.005565333905544462 -0.023406738119882836; 0.0039602816369080415 0.007058620125775126 -0.022141843521606763; -0.0028965981187826437 0.0010043453382644087 0.0008852945393351586; 6.367095558059967e-5 0.000879790925225676 -0.00082643687353508; -0.005104238329889783 -0.0021751868404387706 0.0024134170150232016; -0.00068008442584111 0.0007409569025175246 0.0030012438526228146; 0.000185290055520503 -0.0024806379779248114 0.0028091782451698773; -0.00227531434877526 -0.0029883643090733453 0.0012486188348034303; -0.0041951152853092295 -0.00239757362450936 0.004535076754470363; 0.00021684779569321026 -0.0017163264901650281 0.004306723142699193; 0.0006527083189685846 0.00032086099487797055 0.00013129900282658888] %
+
+Mass Used: 99.67573959254196 kg
+Launch C3: 96.58147095234973 km²/s²
+||V∞_in||: 0.00025281841244755883 km/s
diff --git a/archive/ES_0.5683466675267036 b/archive/ES_0.5683466675267036
new file mode 100644
index 0000000..3ca34ec
--- /dev/null
+++ b/archive/ES_0.5683466675267036
@@ -0,0 +1,22 @@
+archive/ES_0.5683466675267036---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T01:21:40.624
+Launch V∞: [5.9754546044296335, -7.241836639974111, 0.25458454226522614] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01803061662179582, 0.00029844697329320304, -0.015275612096688302] km/s
+ V∞_out: [0.023131960665448384, -0.00018198748799232574, -0.004906556340469408] km/s
+ time of flight: 1.8483924682692012e8 seconds
+ arrival date: 2029-03-03T09:35:46.624
+ thrust profile: [0.8341908258072941 -0.2002065329899016 -0.19207528386364825; 0.3382538734507374 0.12262266400100585 -0.2399114503250459; 0.07669824252257032 0.054464325931664656 -0.10187459168552947; 0.06434291723544268 0.06270827725698544 -0.11924678356168379; 0.02682275739099628 0.032726082782737156 -0.06743478899100504; 0.03328439789261629 0.04722691326648402 -0.0992370048121439; 0.01941431885109006 0.03325990830370922 -0.07705219912454497; 0.015352133501965345 0.025260689488066077 -0.061804218023087436; 0.007327928835236574 0.016425501751587496 -0.03892562155570264; 0.0012490760623421434 0.001067806333104313 -0.002303209495925787; 0.00037129368282611355 0.0010322514035333932 -0.001364722617703139; 0.0020146652997881896 0.00031227415122060307 -0.0002701326439832956; -0.001014799640477716 0.0006988468462337831 -0.0004996049641876896; -0.00045385837265082086 -0.0007208751488436242 0.0006559795454929698; -0.001009581040766414 -0.0013744536960847375 -0.0015039828308622658; 0.0004562659929699687 0.0024859658183435107 -0.00014013087645202383; 0.0016969675294665459 -0.001223328899622554 -0.002132721020728279; 0.0021357231464322864 0.0006665197420646363 -0.0022218695360560164; 0.00033526350689357267 -0.0027930821527431928 -0.0014863025985138124; -4.5272265648774675e-5 -0.0021528737886432523 0.0016716364082425854] %
+
+Mass Used: 148.4832099713053 kg
+Launch C3: 88.21506893883124 km²/s²
+||V∞_in||: 0.023633377483688985 km/s
diff --git a/archive/ES_0.5683529377467695 b/archive/ES_0.5683529377467695
new file mode 100644
index 0000000..9a0cc51
--- /dev/null
+++ b/archive/ES_0.5683529377467695
@@ -0,0 +1,22 @@
+archive/ES_0.5683529377467695---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T22:57:36.336
+Launch V∞: [7.938998558754267, -6.223077409877822, -0.1355308208492254] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4941290856720713e-9, -2.036445167186257e-9, -5.479822802770969e-9] km/s
+ V∞_out: [-5.752221217404784e-10, 1.992140423680985e-9, -2.9948217891741763e-10] km/s
+ time of flight: 1.8749577778627205e8 seconds
+ arrival date: 2030-05-01T01:07:13.336
+ thrust profile: [0.18119902212927455 -0.012342616055067526 -0.07961945454149796; 0.02402736946969952 0.007349584056738114 -0.03784108245134327; 0.020991648867162226 0.009087163182063712 -0.05707295836801263; 0.019511714941195878 0.00936437831847948 -0.07381653444038964; 0.016747713879516304 0.008216572423571529 -0.07941054049876099; 0.02006971041983906 0.009368652832491347 -0.11304837381391479; 0.022551994279494683 0.0134976294218203 -0.15852884294536085; 0.007321720690216808 0.002811013557430216 -0.051702627692150435; 0.007737598048799822 0.004427353938312158 -0.05730291448998908; 0.003858054356319117 0.002331324350074476 -0.041132673441330425; 0.0009209329334033629 0.0005463626454009185 -0.00879980694679669; 0.0007388420493041367 0.00011948573932932547 -0.006741426881651037; 0.0006885358842578472 0.00022178095723725488 -0.006045088136569424; 1.2809433203546567e-5 -0.00037675462526476735 -0.0016398439418283143; 0.002576348333677499 0.00072363375489734 0.0016759582022668799; -0.0019799710011973366 -0.0004258908289247558 -0.0006760094237108986; 0.001159248485482952 0.0007578512629660349 0.0008694234518505232; 0.0003469290065369242 0.0003365455751179388 -0.0023076627945924563; 0.0001188674381735612 0.00023670235373201274 0.0005893872720158012; -0.001544574544574846 -0.004746004145711425 0.00023502395755208103] %
+
+Mass Used: 69.40399888753245 kg
+Launch C3: 101.77275916863405 km²/s²
+||V∞_in||: 6.355804179230221e-9 km/s
diff --git a/archive/ES_0.5683724213882718 b/archive/ES_0.5683724213882718
new file mode 100644
index 0000000..656c5d7
--- /dev/null
+++ b/archive/ES_0.5683724213882718
@@ -0,0 +1,22 @@
+archive/ES_0.5683724213882718---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T18:39:13.102
+Launch V∞: [6.012175020432102, -7.367269145872943, 0.3353278279775801] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7073776548440676e-9, -1.2475861282965133e-9, -2.5662117488531287e-9] km/s
+ V∞_out: [-3.066128726864657e-10, 6.708079837564419e-10, 9.181475300542479e-10] km/s
+ time of flight: 1.7761462851492402e8 seconds
+ arrival date: 2028-12-08T12:03:01.102
+ thrust profile: [0.6713995800824495 -0.20125383097434155 -0.18119271118175534; 0.32887662834647985 0.0903227626188918 -0.2618740658197661; 0.09607935713127778 0.055469955832069325 -0.13454033534042265; 0.07630093201710642 0.0602816365237758 -0.14644747000347677; 0.03700156475856768 0.03665006284846172 -0.09519750810016905; 0.026850360552501725 0.030809397955514028 -0.08398512607318288; 0.027265906803905005 0.03611550670333064 -0.099456884409361; 0.006986877747404781 0.010387624785875703 -0.030950270305339984; 0.001988698483324613 0.0037850160610688687 -0.011284387471838039; 0.0024352233472475227 0.004542918313715233 -0.015969359471678945; 0.0004883146446527238 0.0008799987158027555 -0.0028339157403818446; 0.0019665800362444765 0.003989796974920014 -0.013635032180682672; 0.00027510011720959177 0.000274788086506337 -0.0015725117878459078; 0.000930386710571715 -0.0004830853600212236 -0.00031649867799478804; 0.0018013889965706627 0.00107041208530634 -0.0006708998620625677; 0.00040561748690732993 0.00021994916904716845 -2.9528266214830148e-5; 0.001715593395057747 -0.00038045426707664396 -0.0012736134918346783; 0.0009411668139783526 -0.0008329742998024511 0.001110491054396697; 0.0002692092874597748 0.00014181896256355403 -0.00048707441555611056; -0.0005082226421667873 -0.0009574346755592066 -0.0036640108560412584] %
+
+Mass Used: 134.97829555816088 kg
+Launch C3: 90.53534789625536 km²/s²
+||V∞_in||: 3.933421875850426e-9 km/s
diff --git a/archive/ES_0.5683758195710448 b/archive/ES_0.5683758195710448
new file mode 100644
index 0000000..7894aac
--- /dev/null
+++ b/archive/ES_0.5683758195710448
@@ -0,0 +1,22 @@
+archive/ES_0.5683758195710448---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T04:03:18.157
+Launch V∞: [7.36939547780404, -6.479407292667179, -0.07149257105040234] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00042889643437381785, 0.0002817038449666138, -0.00013073059554978122] km/s
+ V∞_out: [-0.00021910101974124927, -0.0004042162866220164, 0.00026246312513550563] km/s
+ time of flight: 1.6021033641698942e8 seconds
+ arrival date: 2029-06-06T10:55:34.157
+ thrust profile: [0.37332072160165763 -0.07518599884860183 -0.13656517556864653; 0.09271437538935544 0.02553923127075371 -0.10223928674867003; 0.07271532776480612 0.041819745244542586 -0.14175652269884184; 0.05691978254787327 0.0426773814156226 -0.15137569495560876; 0.03944749239582012 0.033556735040007564 -0.13089894669941068; 0.029701314569650684 0.026544219853789023 -0.12054694850944497; 0.01649012098517185 0.020858232219097283 -0.09910878574337947; 0.03166779197539185 0.03677877443406216 -0.16949103982791172; 0.012198164876753117 0.012539342186236067 -0.06652128489090399; 0.0028385501019104606 0.0034836540749448794 -0.021151399515078915; 0.004878462270825209 0.00556492450756598 -0.028547629049306095; 0.002733089942006558 0.0006057469377096032 0.000871845325563093; -0.0007883939498342127 -0.00019812839605547585 -0.0031404975836996562; 0.0015609570030984611 1.3403489036753198e-5 -0.001639714969269821; 0.004703430262364394 0.004688562726827372 -0.0024466124854065226; 0.0035122341014057223 0.0019766534402863765 0.0017782923644330622; -0.0017798571726691725 0.0030705990199474463 0.005769867616750156; -0.00495360528643463 -0.0010757721943589463 -0.0028829231229252207; -0.0010010793771960465 0.006618542560504832 0.00048339850562458876; 0.005241445890160799 -0.0023286721142294904 -0.0030174076677659404] %
+
+Mass Used: 101.37950756468672 kg
+Launch C3: 96.29581976026266 km²/s²
+||V∞_in||: 0.0005295278050304338 km/s
diff --git a/archive/ES_0.5683800919173589 b/archive/ES_0.5683800919173589
new file mode 100644
index 0000000..68ed309
--- /dev/null
+++ b/archive/ES_0.5683800919173589
@@ -0,0 +1,22 @@
+archive/ES_0.5683800919173589---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T11:06:20.567
+Launch V∞: [5.8796980765685385, -7.699513759979515, 0.023779731897833185] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8088982555167846e-6, 1.7932945155102162e-6, -1.2586487339165936e-6] km/s
+ V∞_out: [1.3736198361721747e-6, -2.847117718248814e-6, 1.6424158630393483e-6] km/s
+ time of flight: 1.7434908765969184e8 seconds
+ arrival date: 2028-11-03T09:24:27.567
+ thrust profile: [0.3437458772368016 -0.10052004608098333 -0.10256240161605201; 0.24561821767922581 0.06558217612712652 -0.19448485350281394; 0.1550782936085921 0.08610744684725716 -0.2027488003268019; 0.07297400265868532 0.05474394563438301 -0.13561173854176412; 0.0719396932222589 0.06744193429814727 -0.16808831016628592; 0.04753416682578699 0.051523608332406046 -0.1347393130495134; 0.019015592900381465 0.023044659568349498 -0.06444953384095302; 0.0061709765317855296 0.007839334369986248 -0.023398194689906875; 0.005071532813379796 0.001461738608706894 -0.011810214537064174; 0.00017237724148050002 0.0044006944408646175 -0.0033727731109086147; -0.0038424499983745453 0.002548113904661188 -0.005470469847870419; 0.003496468617774022 0.0026751949194425634 -0.012635290948949537; 0.002463043093126343 -0.001257930629711739 -0.0036231062379418126; -0.006463412282096785 0.002960007201126599 -0.0018933111937174565; -0.005491272727321873 -0.004801111971791273 0.0006521405855196688; 0.0014020454897180233 0.0008396388883575162 -0.007695522309112361; 0.0009521823951774992 0.0019426373605433529 0.0008053154011275427; 0.006320111421370169 -0.0018759837501903498 0.005487619617679176; -0.0012890380989360527 -0.003956173942469587 -0.008033517087961978; 0.003474930820786623 0.0014587177575956431 -0.010118261967396227] %
+
+Mass Used: 115.62886589394566 kg
+Launch C3: 93.85392708736681 km²/s²
+||V∞_in||: 3.5623042071942847e-6 km/s
diff --git a/archive/ES_0.5683852065856351 b/archive/ES_0.5683852065856351
new file mode 100644
index 0000000..4588367
--- /dev/null
+++ b/archive/ES_0.5683852065856351
@@ -0,0 +1,22 @@
+archive/ES_0.5683852065856351---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:19:11.312
+Launch V∞: [7.580041823970782, -5.668269666100624, 0.0016510020421794435] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9069855885720004e-6, 6.5478596789698045e-6, 1.4800359816878574e-5] km/s
+ V∞_out: [1.4688562252167788e-5, 1.5906442787187409e-6, -6.862129195012596e-6] km/s
+ time of flight: 1.8749577788375852e8 seconds
+ arrival date: 2030-04-16T10:28:48.312
+ thrust profile: [0.674443870195772 0.037067532089765744 -0.11784739161463811; 0.2864183227686345 0.22111796604745182 -0.1839266649082731; 0.14279717026137345 0.18464204168040685 -0.16892463306991562; 0.039698052362635704 0.07530646058865742 -0.08327905292640769; 0.0340221111448337 0.08767733845849038 -0.10256973988804881; 0.019309814856138443 0.06619909100388886 -0.08364913584319779; 0.006647583815609781 0.030264892467677707 -0.04173386481209482; 0.004139188976624178 0.025751984275914134 -0.03748696945111652; 0.00151185557995842 0.014841987570727532 -0.023247310094088557; 7.43540072778028e-5 0.0016247268644211574 -0.0027512224508704176; -0.00024425577592432704 0.0021594984318569583 -0.0030335993584915373; -0.00034561031991342615 1.7166345562057062e-5 -0.00013121869853330566; 0.0001219345960320791 -0.00010417373493070206 -0.000506209955962541; -0.00041724003126728296 0.0003895191816033073 -0.0003335471487665559; 4.365368523594063e-5 -0.00016351075159332448 0.00027645637798523524; 0.0003441075999541359 0.0003326519133466912 0.0005153323000402795; -9.128197545030977e-5 0.00013318240829639244 -0.0001593456448112921; 7.265121517862946e-5 2.498928711076607e-5 0.00042802191240851506; -1.5017679644250149e-5 -3.038633571063101e-5 -8.716701424856873e-6; -0.00014822476546764508 0.0003138412982231341 -0.00026786459602123793] %
+
+Mass Used: 140.52922059479624 kg
+Launch C3: 89.58631778659051 km²/s²
+||V∞_in||: 1.629606428311983e-5 km/s
diff --git a/archive/ES_0.5683886026111945 b/archive/ES_0.5683886026111945
new file mode 100644
index 0000000..bfd0b23
--- /dev/null
+++ b/archive/ES_0.5683886026111945
@@ -0,0 +1,22 @@
+archive/ES_0.5683886026111945---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T06:11:08.663
+Launch V∞: [6.245482227003379, -7.776848341080372, -0.2618678559873348] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2008385424957196e-7, 1.0694512821782496e-7, 1.2220069224813324e-7] km/s
+ V∞_out: [-1.3779450244200746e-7, -6.340730930740439e-8, 1.2962323631226347e-7] km/s
+ time of flight: 1.8133817492891526e8 seconds
+ arrival date: 2029-01-31T01:54:02.663
+ thrust profile: [0.17952032961994766 -0.06161049600120224 -0.08015693772319982; 0.02566933085605615 0.0039239297991979435 -0.03339536244427082; 0.034115811577295055 0.009776802151022952 -0.07886917324866033; 0.04880413100465573 0.0184488160053242 -0.15041402708205973; 0.04043095074368231 0.017671915983904832 -0.15757083877142763; 0.04540616843433284 0.0214471248108331 -0.2086000066434578; 0.009774911709889226 0.005425553644497162 -0.05670620076841242; 0.01430988201132909 0.0074634954479668204 -0.08979688549241788; 0.0034217138112437504 0.00046871040656097825 -0.04006563663646896; 0.00311236463936243 -0.00023212767024873926 -0.019223617255461223; 0.0006806821519983885 -0.001011047575052033 -0.0038627992131058672; -0.0002032281177271932 -0.0006051279184505914 -0.0030790565740065044; 0.000393198744812513 0.009837394383806396 -0.0004656837055253501; 0.00021745688367172584 -0.0011313159278891816 -0.0028329691910545527; -0.00090102747547812 -0.0009077500440292621 0.004201214714718808; 0.0008899089136916423 -0.002472664014097256 -0.0065610903312830204; -0.005782908960143446 -0.00027703232668243574 0.016544935980101556; 0.0027065726281191582 -0.0007690078506273563 0.0004728032424124451; -0.00019148953779800164 0.001183549471928265 -0.005921183939618567; 0.0016156401189939351 0.0010376348634946056 0.0007684779797217287] %
+
+Mass Used: 82.38840971818263 kg
+Launch C3: 99.55399314197902 km²/s²
+||V∞_in||: 2.0196633800433782e-7 km/s
diff --git a/archive/ES_0.5683938454768334 b/archive/ES_0.5683938454768334
new file mode 100644
index 0000000..66b219d
--- /dev/null
+++ b/archive/ES_0.5683938454768334
@@ -0,0 +1,22 @@
+archive/ES_0.5683938454768334---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T01:32:00.132
+Launch V∞: [6.154115692627612, -7.593380434883656, 0.18167146392446815] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.267758255926894e-6, 8.273209330206437e-7, -1.7614363444998974e-8] km/s
+ V∞_out: [-1.244191089801905e-6, 2.8046286014122845e-8, 6.198044442631232e-6] km/s
+ time of flight: 1.7887371525529522e8 seconds
+ arrival date: 2028-12-27T08:40:35.132
+ thrust profile: [0.3460161233828134 -0.08794532797730775 -0.09610122966875151; 0.08577528361233053 0.027399439125205868 -0.07305507830637976; 0.04116986510577578 0.024825912346781862 -0.05875071029550253; 0.09742309462068567 0.08359745964956626 -0.18252008822053964; 0.06508205923336352 0.06937792715385223 -0.1566912401542105; 0.038072912444102984 0.04388274222161195 -0.11176853085194104; 0.026361743238046898 0.034940955574853716 -0.09017988580461452; 0.03160379396681775 0.04872951512514885 -0.12847185823647297; 0.0032598678088387165 0.004884359985055664 -0.013211697992275562; 0.010815325687152133 0.019820838523938483 -0.058726792809856536; -0.0036483825350574475 0.0006297191926783684 4.843101775628498e-5; 0.0006577346996468744 0.0011091422028810414 -0.00485355883349893; 0.00041933068462016594 -0.0013124490392658126 -0.0013773742454367844; 0.000633666642375883 -0.0016214225687030733 3.67240733421619e-7; -0.004964550049482342 -0.005835284018611911 -0.008245149738841771; 0.000693373128807258 0.0008755041813637828 -0.0024032402710054226; -0.005990618344029177 0.004685786461787814 0.004918713253887087; 0.0056326017402268174 -0.006528355860722272 0.011391044825906728; 0.0033783023107786248 0.004660173796871328 0.007476126445915126; -0.004329975457884406 -0.003303090586443782 0.010400711554516698] %
+
+Mass Used: 105.66032276008355 kg
+Launch C3: 95.56557090792379 km²/s²
+||V∞_in||: 6.322148665347365e-6 km/s
diff --git a/archive/ES_0.5684101991076171 b/archive/ES_0.5684101991076171
new file mode 100644
index 0000000..1ad121a
--- /dev/null
+++ b/archive/ES_0.5684101991076171
@@ -0,0 +1,22 @@
+archive/ES_0.5684101991076171---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T16:15:57.418
+Launch V∞: [8.16998217102016, -5.880946888183414, -0.26368287857865486] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.045286572417431e-6, -2.4621728030110603e-5, -4.793595016232642e-7] km/s
+ V∞_out: [-2.3544412342328448e-5, 4.179875343075191e-6, -6.19479668552582e-6] km/s
+ time of flight: 1.874957778755006e8 seconds
+ arrival date: 2030-04-27T18:25:34.418
+ thrust profile: [0.04202186258525911 -0.00197568737384465 -0.018234699506615177; 0.021956451177793847 0.008410857738519236 -0.031998723658939784; 0.029470267727784844 0.018548341538820637 -0.07532746913221362; 0.03248037423742059 0.02450141524213732 -0.11779645495331857; 0.02860839685423074 0.023968366443935758 -0.13480460057639368; 0.022736069329456866 0.020424318860782775 -0.12917895181318292; 0.008339598979702151 0.007909022560207628 -0.05774221404657654; 0.004907537460482163 0.004843620864099521 -0.03784117613356993; 0.005229681011171165 0.005495389306726299 -0.04577646062767342; 0.007120976208820196 0.006894721641901804 -0.06560905990443847; 0.0037249024387533587 -0.006811902659940842 -0.00116505006540918; 0.0005830088512573312 0.0005949163257201487 -0.010033377325494431; -0.011552261589062758 0.00915138260780549 -0.008855878575509013; 0.005933666622666067 9.833080623433037e-5 0.00525071191364147; 0.002163198767321356 1.4475537739866402e-5 -0.006001226293558618; 0.015664987207035835 -0.029421495921283215 -0.0035014368266351563; -0.01675382483024132 0.019763278192448393 0.00547272430890848; 0.019190914736231503 0.022653161667804733 -0.010613006274891224; 0.006748524837195469 -0.01137826578892523 -0.0366045015041789; -0.002504335778860241 0.0015499130219679101 -0.002067491015903016] %
+
+Mass Used: 71.62380274377074 kg
+Launch C3: 101.40367363687702 km²/s²
+||V∞_in||: 2.4648567924709276e-5 km/s
diff --git a/archive/ES_0.5684126474690383 b/archive/ES_0.5684126474690383
new file mode 100644
index 0000000..a089ea6
--- /dev/null
+++ b/archive/ES_0.5684126474690383
@@ -0,0 +1,22 @@
+archive/ES_0.5684126474690383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T05:16:40.496
+Launch V∞: [5.855118304808203, -7.769643907186122, -0.1770578793578751] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.453687891592906e-7, 0.0003055684052792126, -0.00012311483475075437] km/s
+ V∞_out: [-0.0003400489339580825, -0.000170231668069975, 0.0001420880697276897] km/s
+ time of flight: 1.682995320000276e8 seconds
+ arrival date: 2028-08-26T03:08:52.496
+ thrust profile: [0.47187888213319285 -0.1940107050267346 -0.18899294012911538; 0.054633173738660286 0.006019625442345902 -0.060131624052782634; 0.08388567120148875 0.028089401209326403 -0.14855775696598428; 0.08738380723310606 0.04176130374195715 -0.2110123425812504; 0.06760090873207655 0.03958577133719268 -0.20539351277067538; 0.041489552213537326 0.027837203014281015 -0.15137681880021733; 0.011897038872277159 0.00888131135238228 -0.05127739195264374; 0.006661669699595689 0.005216879399832368 -0.032772886911248744; 0.008850980130068953 0.007575233499363482 -0.047656727071261444; -0.0015419591956476672 -0.0005306194446401688 -0.008760288223367094; 0.0036120504980223507 0.0036330307484515618 -0.023724996267541133; 0.0057443064650704225 -0.0009953025480798406 -0.007269192394078818; 0.0015580635701816397 0.0016643566068335624 -0.01110108755284029; 0.0009510769332346232 0.0024132576634594907 -0.007105096506039188; 0.0002754206675869851 0.0006096461961874735 -0.0021989309239781245; 0.002430365228548588 -0.003316409551550591 0.005491935778500142; 0.0009003186198656779 0.0009372710371277973 -0.007122091824421981; 0.0018788247829650568 0.005094359048053609 -0.013378293212615406; -0.0011637980409412354 0.0020065115943146443 -0.006338342978691932; -0.00288941968810175 -0.0071845349979303445 -0.004249508504241523] %
+
+Mass Used: 110.84151862811086 kg
+Launch C3: 94.68112630041722 km²/s²
+||V∞_in||: 0.0003294392304549265 km/s
diff --git a/archive/ES_0.5684321908532398 b/archive/ES_0.5684321908532398
new file mode 100644
index 0000000..e74d221
--- /dev/null
+++ b/archive/ES_0.5684321908532398
@@ -0,0 +1,22 @@
+archive/ES_0.5684321908532398---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T11:21:15.641
+Launch V∞: [7.48083147044057, -6.660569311887499, -0.2879048128142729] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.647722794576816e-7, 8.095719982183963e-7, -1.4007064614003112e-6] km/s
+ V∞_out: [-8.366007128556008e-7, -1.6240553708593193e-6, -5.560026768391724e-8] km/s
+ time of flight: 1.626728169975969e8 seconds
+ arrival date: 2029-07-09T06:14:51.641
+ thrust profile: [0.10229763031722658 -0.02526187194377009 -0.05010972884305284; 0.07273438315473048 0.012456093054235028 -0.10548803053953115; 0.03619091878457732 0.011360777358006028 -0.08823006714471948; 0.06490292603461335 0.02396145994023591 -0.21297921070600034; 0.03965161021014112 0.016861081951484867 -0.17167357674637782; 0.022913225821552325 0.009517838293089397 -0.11380807577412572; 0.01592393286843984 0.0066239631667246055 -0.09172567841548566; 0.005779552493214055 0.0023678537696888 -0.03649352991210947; 0.018291868722343615 0.007395458653351582 -0.1242786410753021; 0.004840412378145584 0.0009159914644398437 -0.029640215094850708; 0.002105884609725772 0.0008623647553687222 -0.021472758454575625; 0.002271841747523183 0.0015737784765138374 -0.013813487956058388; 0.0023209033513009836 0.0012628910239768953 -0.0019473234153848202; 0.0007061947681149784 -0.0013980477723553745 0.00016258430804809714; -0.0011639045482580482 -0.000982423418315895 -0.0032692787822768635; 0.0003081993420045049 -0.0006486438418710581 -0.0014083906566199678; 0.0010463487196896441 -0.0013578449591207203 0.0005980414313350333; 0.00011115152082627868 0.0002650360294674265 0.0004625210975087333; -0.00040828033535507836 -0.0016023117515443334 -0.0016444109653585013; -8.768683440914943e-5 -9.413480657091168e-5 0.0001419505729072419] %
+
+Mass Used: 77.45223466058633 kg
+Launch C3: 100.40891222883316 km²/s²
+||V∞_in||: 1.8344526449669785e-6 km/s
diff --git a/archive/ES_0.5684383541581144 b/archive/ES_0.5684383541581144
new file mode 100644
index 0000000..9f014b0
--- /dev/null
+++ b/archive/ES_0.5684383541581144
@@ -0,0 +1,22 @@
+archive/ES_0.5684383541581144---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T09:37:51.355
+Launch V∞: [7.533769003516054, -5.8371552195640755, 0.20496739150987578] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2937703577125695e-7, -8.481406826968325e-6, 1.4528354116339198e-6] km/s
+ V∞_out: [-1.4185266041191614e-6, 4.975394208133625e-6, 6.880624572013994e-6] km/s
+ time of flight: 1.8749577787516433e8 seconds
+ arrival date: 2030-04-18T11:47:28.355
+ thrust profile: [0.5392052342667074 0.04113125263236993 -0.09098127591022055; 0.2277342614500463 0.18161488091972214 -0.14039911115773313; 0.14381133564792103 0.19978212448639093 -0.16614913787022179; 0.057582688799372846 0.11305675291299197 -0.10873054335569314; 0.029462446037979314 0.07263812423274431 -0.07939924956448943; 0.02020205098845273 0.06775047527071117 -0.07767143785243984; 0.01506757075036445 0.06757782144395094 -0.08239685228508258; 0.0009128154730580715 0.006335241137865313 -0.00867725269923058; 2.343146713185715e-5 0.011761277378986166 -0.012817903537656763; 0.0026302636003332283 0.011928767995209333 -0.019777784125901875; 0.0023014821758451116 0.005924789704155655 -0.007616908171131943; 0.0017325943155943827 0.0033936562444753064 -0.004769414635491291; -0.0008741685090045271 0.003983986235563231 -0.0030436100042957564; -0.0011769890976733896 -0.0008627439946575898 -0.0036573403476068784; -0.003570268006901977 0.0052481386289854465 -0.003582347072679222; 0.0007961020694850843 0.002384821169230427 -0.0019883919831834335; 0.004151883832262428 -0.002892546052587699 -0.00021445599094979326; 0.0002480849793083039 -0.0013070637391933272 -0.002992745245510164; 0.012955753657089623 0.0049098537025834745 0.00394329686982907; -0.006348381427406679 -0.008474124569213924 -0.007374263083619902] %
+
+Mass Used: 133.0910160090998 kg
+Launch C3: 90.87206808720578 km²/s²
+||V∞_in||: 8.607996649765938e-6 km/s
diff --git a/archive/ES_0.5684403959807384 b/archive/ES_0.5684403959807384
new file mode 100644
index 0000000..82efcb0
--- /dev/null
+++ b/archive/ES_0.5684403959807384
@@ -0,0 +1,22 @@
+archive/ES_0.5684403959807384---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T18:35:36.821
+Launch V∞: [6.455629577307908, -7.59718321084052, -0.05905833598090847] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00018829434524340495, -0.00012923692091023419, -0.0001946846961422671] km/s
+ V∞_out: [0.00021010645816662603, 0.0001154292325684235, -0.00018131502196323934] km/s
+ time of flight: 1.8226261554782546e8 seconds
+ arrival date: 2029-02-08T07:05:51.821
+ thrust profile: [0.10076341769551189 -0.02820997436444347 -0.039781773837619716; 0.08023305053266692 0.018600374292039135 -0.08879365810678717; 0.03368845989400205 0.015840296097462337 -0.06498981070640465; 0.03064364310173835 0.018335071034784586 -0.08331089038198955; 0.028933439388365723 0.021736663861611227 -0.09736025659047189; 0.02301959715701934 0.019918536127217296 -0.09215431166456324; 0.0373900900935367 0.03378297941191788 -0.1643958022363477; 0.018310143716940248 0.018725355530524977 -0.09513237625602712; 0.024076251970770797 0.02769842973294351 -0.14048575353590143; 0.0041873426637708015 0.0046975172306992895 -0.029295953800165586; 0.0021241704673125904 0.0020697289988151762 -0.01727362671657691; -0.0012524418929093298 0.001152113374064769 -0.01305301647708772; -0.003064481960952003 -0.002896566932099484 0.0003375067284459325; 0.00030557131465483965 0.002593181664736568 -0.005992068020130259; 0.007148089279466667 -0.0011541764871758524 0.0063461982022694876; -0.0009627657957944043 0.0004761083032897393 -0.001401806633598716; -0.016225965392276262 0.001357347892357291 -0.003385659604630503; -0.0010616418334757995 -0.010730125440765036 0.008101741515085564; 0.0020175957336838195 0.011282684520191134 0.010673172900637764; 0.003019912271741466 0.003140831669818656 -0.0020913801385515594] %
+
+Mass Used: 83.37143109521958 kg
+Launch C3: 99.39583386553859 km²/s²
+||V∞_in||: 0.0003000984389979521 km/s
diff --git a/archive/ES_0.5684418027150691 b/archive/ES_0.5684418027150691
new file mode 100644
index 0000000..d10e820
--- /dev/null
+++ b/archive/ES_0.5684418027150691
@@ -0,0 +1,22 @@
+archive/ES_0.5684418027150691---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T19:58:03.045
+Launch V∞: [7.433268788541548, -5.771580274077768, 0.21516250729897615] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3162378569950064e-7, 1.1867832974243143e-6, -2.5115486692618484e-5] km/s
+ V∞_out: [-1.0124353411218385e-6, 2.5100295028028456e-5, -3.1980771508531705e-7] km/s
+ time of flight: 1.7619585208283824e8 seconds
+ arrival date: 2029-12-05T03:15:35.045
+ thrust profile: [0.9960466417683971 -0.07295879807449494 -0.22737472742228176; 0.21201786647908002 0.11369509098898563 -0.17421877665327984; 0.0325622100313733 0.030386273737794244 -0.05700785055414116; 0.07280308494059898 0.09883066366700145 -0.17429070525393206; 0.0377597586570863 0.0619885289790009 -0.12479747910230728; 0.01107462373522808 0.02104745086954861 -0.048898138253228765; 0.023016841891398847 0.05364068247289126 -0.12124758182585554; 0.006508971886201046 0.01883108872477981 -0.04492619384171941; 0.0031622006429233634 0.007547658718017957 -0.024217291620852562; 0.001851309690676014 0.004501351715868587 -0.011814596629786296; 0.00040290606997747593 -0.001207906134708748 -0.0032586696210487086; 0.0006091140066844616 0.0008006481055738626 -0.002683975570064966; 0.0019428792695516193 0.0027408494841430616 -0.0014168705534063593; -0.003537239892945213 0.0035298359001948976 0.0012586663224857927; -0.0021183077807819034 0.0051493622715304155 0.0003972825696553163; 0.0010729446666915541 -0.0030122653650287924 0.002811473017346344; -0.000762843756956091 0.010486877832951684 0.0001004576773294128; 0.0008383610573602419 0.0032170979176788647 0.004570603436890644; 0.0014288732176430605 -0.0005501969725811099 -0.005671065959875217; -0.003344716260572933 0.009803507188487225 0.0002971743141909944] %
+
+Mass Used: 146.28507772454986 kg
+Launch C3: 88.6109186473767 km²/s²
+||V∞_in||: 2.5143855138444925e-5 km/s
diff --git a/archive/ES_0.5684420626994732 b/archive/ES_0.5684420626994732
new file mode 100644
index 0000000..1284ce3
--- /dev/null
+++ b/archive/ES_0.5684420626994732
@@ -0,0 +1,22 @@
+archive/ES_0.5684420626994732---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:32:34.289
+Launch V∞: [6.630203515070426, -7.399316670318679, 0.17957548330371492] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.473493141646567e-7, -7.447769275549095e-5, 5.0244459648620397e-5] km/s
+ V∞_out: [4.5107908108061805e-5, 7.739731727561454e-5, -1.6152906612583777e-5] km/s
+ time of flight: 1.8749577787473008e8 seconds
+ arrival date: 2029-04-10T12:42:11.289
+ thrust profile: [0.16618274147916912 -0.045683704214677996 -0.061567544123539; 0.0631832807200223 0.013462839387130027 -0.06884327163372383; 0.04699308134232307 0.01958235360323648 -0.08460185051572784; 0.035692090522803935 0.019392798152238207 -0.0894400966923777; 0.032023456363214894 0.02115766837904723 -0.10454138178635075; 0.036798192019534895 0.02792582347335659 -0.14907361603423336; 0.01917495634942885 0.01560889767066546 -0.08825250841171162; 0.01670599444231988 0.014684921600181075 -0.08921584761410895; 0.006539663592463993 0.0034650549932079095 -0.03854077994894275; 0.005183550744766477 0.011068138191881951 -0.0318534403712621; -0.0030528851226494357 0.00014728027617383647 -0.014800871592911602; 0.002302136584924586 0.005323486529712385 -0.03477367202385223; 0.003011501192852267 -0.0016798340853571708 -0.014741001842618513; -0.002376406915172522 0.0011241276168832586 0.0016300859310953025; 0.009641746133109308 0.005776888711438787 -0.010944342055439685; 0.013606012673118572 -0.0047523205602656785 0.0021711067732395235; 0.006196981993037337 0.014879962257400445 -0.00586258181149912; -0.011208348527932187 -0.002589466863199519 -0.006364283638507813; -0.0019521355569913535 -0.0046085118190027224 -0.01856309096094025; -0.005616052614322642 0.015879483927093038 0.01196028482012711] %
+
+Mass Used: 87.18896285623259 kg
+Launch C3: 98.7417331931119 km²/s²
+||V∞_in||: 8.984149166864033e-5 km/s
diff --git a/archive/ES_0.5684448361249995 b/archive/ES_0.5684448361249995
new file mode 100644
index 0000000..decba6d
--- /dev/null
+++ b/archive/ES_0.5684448361249995
@@ -0,0 +1,22 @@
+archive/ES_0.5684448361249995---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T20:23:50.754
+Launch V∞: [5.981468509620019, -7.5497698934180395, -0.03287826576231068] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8326839161419329e-9, -7.2781095166859444e-9, -3.281031338745693e-8] km/s
+ V∞_out: [1.4835068904811037e-8, 2.2259536054659595e-8, 1.0901150346095794e-8] km/s
+ time of flight: 1.7587187796626943e8 seconds
+ arrival date: 2028-11-20T09:41:47.754
+ thrust profile: [0.49683665602258326 -0.1544009670635717 -0.14347763951024678; 0.19735977701065532 0.048203065683313374 -0.15852505489292074; 0.11970736389291278 0.06166918109923079 -0.1590309776076617; 0.08196287257324597 0.05929230334592969 -0.15075029730276093; 0.06990895719662286 0.06157304184465802 -0.1635320334872246; 0.02390237552672575 0.025786485039520492 -0.07258170942003786; 0.014020519543761396 0.018077317000103885 -0.053201829278742827; 0.012208250034995854 0.019771174627471442 -0.06013346138297794; 0.00797345526512146 0.01515827656900753 -0.046377180903788465; 0.007261707066465596 0.010991097703299925 -0.03544901887368948; 0.0003627860312004358 0.0018065289047587076 -0.008101705803837997; 0.003414615894628409 0.007000487467306264 -0.023879233690166674; -0.00023080612643166815 0.0006309537360903502 -0.0006222430836318607; 0.0009643066014893794 0.0043708294372145524 -0.0006377636682033346; 0.0013053948329480019 -0.00346561756046004 -0.007712356614154517; -0.0004206701973189825 0.00030760302716284136 -0.0002740966348282524; 0.0028807116987100093 -0.0064206273715200065 0.001160643233210866; 0.0007038106253907884 -5.0926405511202274e-5 0.005132053042786544; 0.010001381938835707 0.0016392558546733085 0.002371543615769003; -0.002788845092592142 -0.0044819190754606785 1.0536170985339828e-5] %
+
+Mass Used: 121.98022240543423 kg
+Launch C3: 92.7780719554969 km²/s²
+||V∞_in||: 3.365778176078297e-8 km/s
diff --git a/archive/ES_0.5684462022587581 b/archive/ES_0.5684462022587581
new file mode 100644
index 0000000..ffbba3e
--- /dev/null
+++ b/archive/ES_0.5684462022587581
@@ -0,0 +1,22 @@
+archive/ES_0.5684462022587581---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T11:03:11.322
+Launch V∞: [6.621492572357158, -7.347871285053948, 0.1414963209306528] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010064790621289476, -0.006192161715878879, 0.008745752442420401] km/s
+ V∞_out: [-0.007284255951529797, -0.006171800989822868, -0.004969105821416156] km/s
+ time of flight: 1.8749577787493458e8 seconds
+ arrival date: 2029-04-09T13:12:48.322
+ thrust profile: [0.23274363949957416 -0.05812150111712568 -0.0843170639844538; 0.0525722982406649 0.01348521910050078 -0.06092856341786418; 0.05474963079613124 0.027681647079669337 -0.10706959708817042; 0.058565000820713704 0.040407252380281124 -0.15881348305747514; 0.03958725506698744 0.032476755717607025 -0.13914392115429416; 0.017451114248818424 0.015503501156683853 -0.07379062044361509; 0.011874110397718915 0.012384180667868686 -0.05740438252007416; 0.014922352603625033 0.01590636960344317 -0.08502775863364946; 0.010838141629218144 0.012548681953365904 -0.06728471273761504; 0.0012337285283684346 0.002141508747114204 -0.017629067750294786; 0.0011296125965570033 0.0010061623998747211 -0.005754173679717308; -0.0013438354215598383 -0.0017582232102224008 0.0018066377413453218; 0.0020402910025604628 0.0024159584761909397 -0.023717816804306284; -0.010979266685154039 0.011238381894608853 -0.004170395886356003; 0.00805061587667424 -0.0033659084606691607 -0.004126557961841278; 0.0028210960133412703 -0.0026864354786829397 -0.0032241897866193466; -0.0030412695525211197 0.0033423945730954893 -0.0013561148888699822; 0.015142007839805677 -0.0022030959524744565 -0.013133948446983536; 0.021298416284133617 -0.004228037641421935 0.010062810153623557; -0.021901891497831387 0.02082605514529048 0.00632620258641865] %
+
+Mass Used: 92.36408378991109 kg
+Launch C3: 97.85539751633829 km²/s²
+||V∞_in||: 0.010763087503230774 km/s
diff --git a/archive/ES_0.5684671593250529 b/archive/ES_0.5684671593250529
new file mode 100644
index 0000000..dd3f808
--- /dev/null
+++ b/archive/ES_0.5684671593250529
@@ -0,0 +1,22 @@
+archive/ES_0.5684671593250529---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T23:43:09.178
+Launch V∞: [6.4781259616786535, -7.59639010086578, -0.09776690174496298] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.97883782099125e-7, 4.552913254912183e-7, 4.2277771191725916e-7] km/s
+ V∞_out: [-1.7969796875008835e-7, 3.288307188233092e-7, -5.266858054146418e-7] km/s
+ time of flight: 1.8356524795672798e8 seconds
+ arrival date: 2029-02-24T14:03:56.178
+ thrust profile: [0.09621633089765023 -0.030414355167787583 -0.04088900642703537; 0.06052588680924914 0.00947072355011541 -0.0741509566017002; 0.044186245911314856 0.015517608903210939 -0.09279089252781068; 0.05264568349757785 0.025318904521936678 -0.15566829823291495; 0.03433337409853363 0.01894797317318366 -0.1281934522046646; 0.03205060704011424 0.019647274078197597 -0.14299199445670482; 0.016784237456453237 0.011228486508026403 -0.08944451657654984; 0.008588888570280418 0.006980059191506262 -0.05393970087507408; 0.007080047647908599 0.004002625540199757 -0.04489425276427138; 0.008491842383550318 0.005824003785783428 -0.058451356454514984; 0.006302436973847778 0.0028063052088744614 -0.008844396147010037; 0.00012846462898960547 -0.00011076025061854621 -0.0037170667106835587; 0.0015763679508808825 0.000501604859187096 -0.008210595422738557; -0.00011260002665112664 -0.0002952089388329381 0.0008088756174745447; -0.0001821897655012528 0.00017740605004743664 -0.0007779776263697586; 0.007077770720457524 -0.007562490624595391 -0.0053919917694614985; 0.0028001689022371613 -0.0013602783861279548 -0.004105648722701303; 0.00035208000615669235 0.01662617982955908 0.007527105728577051; 0.009688065956522753 -0.01569635324501393 0.013292199607525338; 0.01599275837191294 -0.01317318468549961 0.016609759227457416] %
+
+Mass Used: 81.74025392182511 kg
+Launch C3: 99.68081690698341 km²/s²
+||V∞_in||: 6.520653157310221e-7 km/s
diff --git a/archive/ES_0.5684779329410806 b/archive/ES_0.5684779329410806
new file mode 100644
index 0000000..02608c7
--- /dev/null
+++ b/archive/ES_0.5684779329410806
@@ -0,0 +1,22 @@
+archive/ES_0.5684779329410806---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T21:28:05.969
+Launch V∞: [8.126459969466676, -6.007289854566493, 0.3129117803335614] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002776179816303452, 0.00020957242606491194, 0.013451330453895379] km/s
+ V∞_out: [-0.012410183698925607, -0.004677383687731811, 0.0022431395732833083] km/s
+ time of flight: 1.8749577795091578e8 seconds
+ arrival date: 2030-04-29T23:37:42.969
+ thrust profile: [0.07431769279688288 -0.01116128816462901 -0.035579042393548956; 0.019062625900933543 0.002430423948081039 -0.03324731682786297; 0.03389490498703228 0.007155567840211379 -0.09257521670518452; 0.02937951376081096 0.0017972695817359897 -0.12556388071240654; 0.014768910458457123 0.0007701919205888016 -0.06848428599758764; 0.0237479711141968 -0.0013817145328864908 -0.12356041814479024; 0.011080175609549507 -0.0010012873535311512 -0.06492896040430457; 0.014280256372316644 -0.0029565817003688478 -0.09437610702398957; 0.007563324903446523 -0.0006084820896554751 -0.05084082926943222; 0.0038867551485049947 -0.001556608575045426 -0.026488005771387765; 0.0038147502147917066 0.00014954708090364347 -0.040264747251726456; 0.0010642912933463017 0.002002920261493738 -0.0008402334973129297; 0.00133090523150893 -0.0005229081057861905 -0.002825516574876875; -0.004880988895729075 -0.002305607873860539 -0.0024165395017306723; -2.756042170619894e-5 0.004381703190819994 0.0032474855136625227; -5.1722058207977315e-5 0.0027117333516771063 0.0013713007307335787; 0.015771583930862636 -0.002526086843783323 -0.0034561966135177296; -0.003152412801948429 0.012177017843831643 0.0035204402394097977; -0.006292797758870835 -0.01013639158974411 -0.005971021838308263; -0.0061272130146823485 0.004627188139991195 0.0029255288427535767] %
+
+Mass Used: 66.91294034729935 kg
+Launch C3: 102.22479681439337 km²/s²
+||V∞_in||: 0.013455827114131055 km/s
diff --git a/archive/ES_0.5684814666414428 b/archive/ES_0.5684814666414428
new file mode 100644
index 0000000..26fd8a8
--- /dev/null
+++ b/archive/ES_0.5684814666414428
@@ -0,0 +1,22 @@
+archive/ES_0.5684814666414428---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T17:30:22.232
+Launch V∞: [6.381326419104954, -7.185634858160285, 0.21916518989665068] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2100654169020767e-7, -4.429690358210956e-8, 5.8543968450887094e-8] km/s
+ V∞_out: [-2.30575123140358e-7, 2.0245048620494722e-8, -2.6071879357317975e-8] km/s
+ time of flight: 1.858921223914879e8 seconds
+ arrival date: 2029-03-17T06:12:24.232
+ thrust profile: [0.6521207566703439 -0.1622793044736499 -0.17231907901222854; 0.08254896226848688 0.02690983112467497 -0.0771219970620062; 0.11001396458391675 0.06984594717737343 -0.1659938559336778; 0.05653042491889318 0.04863183073030677 -0.12387321702036963; 0.03986697535072321 0.04213807894230107 -0.11369963945860967; 0.025835150868804856 0.03178014928934539 -0.0912944256090278; 0.0253645925421293 0.03545910680824936 -0.1084837207165274; 0.014424643796248117 0.022543859244347868 -0.07143610036856189; 0.00043144866876054853 0.0017391419114575557 -0.006585883888695859; 0.0015828200400698255 0.004717654649830238 -0.016849376368008113; 0.002202475734364517 0.0018331999314259114 0.0003805300849647848; -0.00027237765984816946 0.0007457713498582238 0.0010631596948992793; 0.0016414397825708217 0.002183998510950255 -0.0005466969989700249; -0.00046851335830741764 -0.00044468222779617733 0.0036279637401353797; -0.0005426191581192305 -0.00033010291959535026 0.0024242891352702304; 0.0031223181673738706 -0.0007017913344260655 -0.001481448033309473; -0.00091230655208843 0.005354331260371249 0.00022981284488536114; -0.0005953664892217852 0.004142592653997322 0.006226581852611656; -0.004864452330837779 0.0068369727048325475 -0.015703964020151635; 0.0035425957356508926 0.015450928099367373 -0.011893530410720757] %
+
+Mass Used: 124.21257780079804 kg
+Launch C3: 92.40270856243747 km²/s²
+||V∞_in||: 2.3288087808750352e-7 km/s
diff --git a/archive/ES_0.5684927660428626 b/archive/ES_0.5684927660428626
new file mode 100644
index 0000000..658cecd
--- /dev/null
+++ b/archive/ES_0.5684927660428626
@@ -0,0 +1,22 @@
+archive/ES_0.5684927660428626---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T07:38:53.308
+Launch V∞: [6.129298792810844, -7.616663025996803, 0.1919150175848033] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009462423165942518, -0.0058185172449469955, -0.00773158084719371] km/s
+ V∞_out: [0.006025543066197578, 0.009754916806336984, -0.007189870732624719] km/s
+ time of flight: 1.7471269430681017e8 seconds
+ arrival date: 2028-11-08T10:57:07.308
+ thrust profile: [0.3356710427374218 -0.11071474276877945 -0.10953086025118099; 0.15225927245109172 0.03115655236909186 -0.14534434700969504; 0.06213718330130322 0.0279559362241394 -0.09948563333828918; 0.04959987402689677 0.03144246125868772 -0.1106096679946024; 0.059395277349462317 0.04862495688582587 -0.17450597130364034; 0.034329735752711144 0.031251822935578495 -0.11992136480882024; 0.03144452155756629 0.030456803482777694 -0.12028057278098987; 0.015755707145118696 0.017159464965782655 -0.07177151047446151; 0.010292749844944554 0.012470533113007418 -0.05422266524529516; 0.0012133748102631724 0.0013137143715279951 -0.006615495216517551; -0.0013245620731614982 0.0036408668656142274 -0.015293599448525713; 0.0071471695944402515 -0.0012786103371964712 -0.007939242460199336; 0.005722472816447619 0.0006368785653248543 -0.0036230881188393177; -0.006680877783482779 0.0005702482635133932 -0.00887268723076339; 0.0006331071377251416 -0.0022362592430149476 -0.00576047093223908; -0.0010726217116086424 0.0024858771384364403 -0.0035483196059957825; -0.001757921125809826 0.004574887937570876 0.0006604734883570336; 0.0002408165013012952 0.000992589399930816 -0.004030219859012954; -0.00923266072574866 0.010484648734099399 0.00048511350398943755; -0.01137243414642064 -0.01924342522702976 0.0054334556046903015] %
+
+Mass Used: 105.46586453350892 kg
+Launch C3: 95.61869071711384 km²/s²
+||V∞_in||: 0.013534028871618524 km/s
diff --git a/archive/ES_0.5684991541478273 b/archive/ES_0.5684991541478273
new file mode 100644
index 0000000..84e01f3
--- /dev/null
+++ b/archive/ES_0.5684991541478273
@@ -0,0 +1,22 @@
+archive/ES_0.5684991541478273---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T04:22:05.081
+Launch V∞: [7.240101626074293, -6.537599219490187, -0.316530127257711] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0577985099883122e-7, 2.8973859295152645e-7, -1.482456367032819e-6] km/s
+ V∞_out: [-3.7032042135766113e-7, 1.4635776055483882e-6, -2.1159823609642265e-7] km/s
+ time of flight: 1.5648003029844818e8 seconds
+ arrival date: 2029-04-23T07:02:35.081
+ thrust profile: [0.4712574676600181 -0.11531612485379299 -0.18566110551792656; 0.12226511854478112 0.030255587621554537 -0.13732707076654793; 0.0707740623459308 0.03381949112126101 -0.13333503706592387; 0.07893429859005811 0.04938871890529864 -0.2067838451283633; 0.08837510983583573 0.06557277685886852 -0.29477623151706295; 0.037315247232181395 0.030894537104079158 -0.15068990946611271; 0.01243318389474651 0.011070445017256042 -0.059216641127096833; 0.003856689880379832 0.002446517017951759 -0.02207914971364615; -0.001671200771076923 0.003598873376962334 -0.014295513164817699; 0.0012440794736576645 -9.18205916177994e-5 -0.0019896174438356166; 5.673641121794158e-5 0.0004362592591680026 -0.00017062659792773348; 0.0018293227988635122 0.0005039584549506322 -0.004456650016651856; 0.0009570123665195085 0.00335957282147872 -0.009050300155776382; 0.0015929349137953257 -8.363719339583549e-5 -0.004857497759640103; -0.000624594429729649 0.004205434711590118 -0.007772215278628561; 0.0004173898100118095 -0.003262012357064333 -0.005942080203932836; -0.0021770307341346705 0.004761776854168448 -0.003877916945015502; 0.00046611770187191155 0.0008004586575824043 -0.0025150645462751857; -0.00477576191628596 0.006820486496975597 -0.01040654469489195; -0.006325479800722506 -0.0013402033324423715 0.0013751606955584392] %
+
+Mass Used: 107.5687923189912 kg
+Launch C3: 95.2594664320241 km²/s²
+||V∞_in||: 1.5244575033364411e-6 km/s
diff --git a/archive/ES_0.5685233549327371 b/archive/ES_0.5685233549327371
new file mode 100644
index 0000000..474e6d8
--- /dev/null
+++ b/archive/ES_0.5685233549327371
@@ -0,0 +1,22 @@
+archive/ES_0.5685233549327371---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T04:25:17.053
+Launch V∞: [5.791938277929079, -7.482001315836454, 0.08191383942386297] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005989763431580152, -0.016935661582807855, 0.006132361969799631] km/s
+ V∞_out: [-0.012985486709756648, -0.007125824337699638, 0.011868176880019074] km/s
+ time of flight: 1.8031819687921527e8 seconds
+ arrival date: 2029-01-10T04:48:33.053
+ thrust profile: [0.6515354282770539 -0.1631060758214563 -0.14768176188791224; 0.3112980488905422 0.10992527080125251 -0.2083379554552672; 0.18469357325977304 0.1254327049482054 -0.21183170444287247; 0.06156190986221753 0.05700738427743667 -0.10413568602859384; 0.055907352658925345 0.06606322243312254 -0.12299664715965317; 0.031099287111639885 0.042479545094187915 -0.08412189044006783; 0.014143675436289999 0.022473519405203736 -0.04690823609054619; 0.012744130347789652 0.022804474295468023 -0.04896031753205016; 0.0037970802773706278 0.007670195381991483 -0.01725332719172758; 0.007448116483397928 0.01648811040982759 -0.037207532029119104; 0.0004931007499283117 0.00080806669610657 -0.0020437465017057446; 0.0008077711115401451 0.0022238988180307336 -0.006344885303566551; 0.0005837640984082132 0.0005779811291911082 -0.0005405540424732454; 0.0007707409824102156 -0.0005295388709556353 -0.0011803365184549254; 0.0010402042009069166 -0.0016497325732019587 0.00013567061633000874; -0.0029479826492172095 0.0005148032466478166 -0.0007982498668618297; -0.000906623802874573 0.0015222064712083622 -0.0003925458796296406; 0.0002856282801680493 0.00018682310715526494 0.0017871692378007545; -0.0003909776183963601 0.0009779923887724242 0.0034507477263115366; 8.948166462535836e-5 -0.000665669699292677 -0.0002189072939660819] %
+
+Mass Used: 140.99789902298198 kg
+Launch C3: 89.53360258260766 km²/s²
+||V∞_in||: 0.01898156375387269 km/s
diff --git a/archive/ES_0.5685506412067531 b/archive/ES_0.5685506412067531
new file mode 100644
index 0000000..962a6e2
--- /dev/null
+++ b/archive/ES_0.5685506412067531
@@ -0,0 +1,22 @@
+archive/ES_0.5685506412067531---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T13:11:57.386
+Launch V∞: [7.381453364219408, -6.654531738063755, -0.46286510871976894] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3112005984535316e-6, -2.0466043946319083e-6, 1.0403072583628681e-5] km/s
+ V∞_out: [5.100051688234483e-6, -8.980837092625462e-6, 2.709398420254208e-6] km/s
+ time of flight: 1.592432769760309e8 seconds
+ arrival date: 2029-05-28T15:26:33.386
+ thrust profile: [0.22818578396295544 -0.0532473225439495 -0.10120664128830677; 0.05446120304320862 0.011814659877362351 -0.07127546870861164; 0.04648467547219136 0.019355560856305135 -0.10246578052164994; 0.047445024101279966 0.02541278992433331 -0.14476251574028995; 0.03472850638810574 0.021287638229880935 -0.13494079933942266; 0.02757387296225927 0.018656621011357944 -0.12983690303014597; 0.03198898223860819 0.023028446353185412 -0.1701125836615098; 0.025912248591388878 0.019332308433841483 -0.1531645330836221; 0.007951751396468414 0.005856478652830708 -0.05321873196693021; 0.004137761989651145 0.003019431914724756 -0.02966886505698528; 0.0007717572897974732 0.0006001508999383863 -0.005806818935823755; 0.003182512513236866 0.002445818927662629 -0.02689253367028908; 0.000727791339475616 -0.0001808652719807881 -0.0023255684311606567; -0.000267281969675648 -9.735223978431381e-5 -0.0015700940253074625; -0.0004111881599932919 0.00022826553078857288 5.190966395744842e-5; -0.0016754896917650572 -1.866719844135905e-5 0.001766608338899217; 0.00020417615224573894 -0.0003106257428822471 -0.0022665139306066004; -0.002716041615750469 0.001997458027012381 -0.0004451241110922002; 0.0002462788514908129 0.00034405905308266583 -0.002242872038851848; 0.00126587223062261 0.0008485200165710364 -0.001464710243294745] %
+
+Mass Used: 85.90888665004695 kg
+Launch C3: 98.982890529914 km²/s²
+||V∞_in||: 1.0683246498034118e-5 km/s
diff --git a/archive/ES_0.5686045356120264 b/archive/ES_0.5686045356120264
new file mode 100644
index 0000000..57fe23b
--- /dev/null
+++ b/archive/ES_0.5686045356120264
@@ -0,0 +1,22 @@
+archive/ES_0.5686045356120264---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T05:32:54.678
+Launch V∞: [7.914743360204995, -5.8913115691667235, 0.15268612798525433] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.705444009509282e-7, -5.633288723164655e-6, 1.0528029205925943e-6] km/s
+ V∞_out: [-8.740372166414178e-7, 3.4080984451680346e-6, 4.57337475367956e-6] km/s
+ time of flight: 1.8749577787490034e8 seconds
+ arrival date: 2030-04-25T07:42:31.678
+ thrust profile: [0.22758891676133677 0.0030631260778678435 -0.07410987681973415; 0.13929192384630204 0.08134912101028977 -0.15712616093217813; 0.06467369123437935 0.05947604750663977 -0.13591653139762663; 0.036243046649358256 0.04021327501892783 -0.10742527956278039; 0.02269640856672446 0.02917030311474558 -0.08369657272808748; 0.00979295316290483 0.02620388796816296 -0.07730890175718994; 0.00545937541274825 0.023451582812705027 -0.06606466387209492; 0.0069927025646025365 0.008820604863529605 -0.029966982490853177; 0.002672192327628961 0.010256850288071032 -0.043823821547983435; -0.01041202293424574 0.004266915704014497 -0.011309127184008219; -0.016020617818081097 -0.000998803176781091 -0.011732356956913529; 0.00278241534565307 -0.005796787606484453 0.0015373193724254; 0.01004243160641796 0.0030351259906004845 -0.009754076846115374; -0.00047270953011010986 -0.006127318156435912 -0.0004573317988354964; -0.006218390680125768 0.003156408908006441 -0.005285627267724647; -0.016473139777951916 -0.007927797801073472 0.000333837929513265; -0.035859030946671096 0.02294065790575856 0.017238795672365373; -0.003304994095122826 -0.015120328316367346 -0.013370578118507219; 0.008656899214420689 -0.04611192424008777 0.005782994015345062; 0.0007116858084778002 -0.0039884073566081035 0.004136503677900865] %
+
+Mass Used: 95.35679770061324 kg
+Launch C3: 97.37402751658587 km²/s²
+||V∞_in||: 5.769919030782755e-6 km/s
diff --git a/archive/ES_0.5686168394301518 b/archive/ES_0.5686168394301518
new file mode 100644
index 0000000..8c4b3df
--- /dev/null
+++ b/archive/ES_0.5686168394301518
@@ -0,0 +1,22 @@
+archive/ES_0.5686168394301518---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T06:59:00.658
+Launch V∞: [7.363586336005949, -6.54153083040382, -0.29494938269459714] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.9370511267168304e-9, -3.1832379166791495e-9, -9.871370411152258e-10] km/s
+ V∞_out: [-6.717163291673584e-9, 4.959470192337287e-9, -2.3797968612866224e-9] km/s
+ time of flight: 1.5989478138157716e8 seconds
+ arrival date: 2029-06-03T22:12:01.658
+ thrust profile: [0.3476551863388683 -0.08316402644295892 -0.14379733865954758; 0.05066518641455516 0.011547010654025136 -0.062347744172953815; 0.07210488327117918 0.038542068325239986 -0.15802498330773515; 0.06299510705743035 0.034232923378257334 -0.18658716419718566; 0.03725613584463334 0.024036220856704392 -0.1401202010961193; 0.047196530371489714 0.036322440189288936 -0.20405859425243716; 0.023750402854485313 0.018346202382282944 -0.12146250989701904; 0.008890855225079326 0.00927363409088119 -0.06212962581346866; 0.0031167294724169146 0.004073027436223563 -0.02622418918378298; 0.0011756434462276725 0.0020803820089519364 -0.013279501535516153; -0.0057507509104714975 0.0013903823955706304 -0.010256510680985934; 0.0003080598643019892 0.0018268437842023952 -0.004816248020099164; 0.0054401255398194275 0.001298105598522879 -0.010361753538810633; 0.0007074073199123336 0.003744076604178985 -0.0073748568170811666; 0.007057978828056229 0.001895314801904901 -0.0024119600784974493; 0.012117542142365333 0.0031212734397298935 0.0021162322732943273; 0.005436773413679675 -0.0010301925187114896 -0.004718908203718995; -0.0025444616616058704 0.0042551882313733806 -0.0023776412654843582; -0.0028549776305279682 -0.0022260736556966518 0.013132517502517104; 0.002194908959473254 0.005075894240083865 0.0034120698142455453] %
+
+Mass Used: 96.96366991932382 kg
+Launch C3: 97.10102447128914 km²/s²
+||V∞_in||: 7.696110803958632e-9 km/s
diff --git a/archive/ES_0.5686216648698952 b/archive/ES_0.5686216648698952
new file mode 100644
index 0000000..ad91358
--- /dev/null
+++ b/archive/ES_0.5686216648698952
@@ -0,0 +1,22 @@
+archive/ES_0.5686216648698952---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T02:53:10.131
+Launch V∞: [7.468251508530169, -6.505848296052578, -0.23865648264307912] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008771977767412405, 0.00435653299368061, 0.000340033147047484] km/s
+ V∞_out: [-0.007358153760097763, -0.004081685202753836, 0.005023718213268004] km/s
+ time of flight: 1.603309399517069e8 seconds
+ arrival date: 2029-06-08T19:15:29.131
+ thrust profile: [0.23265557210689652 -0.05296471481061235 -0.0962624435159241; 0.0697789223501195 0.018255424522174653 -0.08589164258446985; 0.06931102892053957 0.03284198233296574 -0.14205083109516808; 0.05428574291125369 0.03330748341846491 -0.15534916657432668; 0.04196249432407757 0.03024375062313353 -0.1526389907231153; 0.01739778298681646 0.014077186400819931 -0.07974260861848999; 0.039685652766969316 0.03645017529544069 -0.2022852930405738; 0.0062217025466576835 0.005879466294119057 -0.04537816974274199; 0.008568260844266375 0.008202187713784661 -0.05758234134401738; 0.0104149706577385 0.009892653074421515 -0.06709053622985998; 0.003852436965855231 0.0044690531340414695 -0.022085385378010147; 0.0023736654034094487 0.0029241648073869567 -0.025603600047141347; 0.0007454074012111717 0.0015860363813029368 -0.003890565613141378; -0.0019746971877571563 0.00019109052526762027 -0.0037000075799960134; -0.0022019286692566958 -0.0008041738046918299 0.0029219073258601614; 0.00038426342960569827 -0.003379655657864668 -0.008493318481665388; 0.0008271807042198708 0.005237435388262899 0.0017812069872636801; -0.00549382100478732 -0.0075132410318661524 -0.002617733093202536; -0.00042631632705037847 -3.2753039226417365e-5 -0.007642589146885367; 0.000982872230912915 -0.0034594625325895735 0.0004032433031154405] %
+
+Mass Used: 90.80477823292222 kg
+Launch C3: 98.15779956262095 km²/s²
+||V∞_in||: 0.009800132459211778 km/s
diff --git a/archive/ES_0.568630396197192 b/archive/ES_0.568630396197192
new file mode 100644
index 0000000..54b692e
--- /dev/null
+++ b/archive/ES_0.568630396197192
@@ -0,0 +1,22 @@
+archive/ES_0.568630396197192---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T15:06:57.022
+Launch V∞: [6.087128367775351, -7.667495585075736, -0.004736455536391366] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0087811865643943, -0.005780714768212093, -0.008877850710243182] km/s
+ V∞_out: [0.00587100233219698, 0.01028629521083748, -0.0070044858439196715] km/s
+ time of flight: 1.7288307740431142e8 seconds
+ arrival date: 2028-10-18T14:11:34.022
+ thrust profile: [0.3492922551657511 -0.132906280269169 -0.11409008876405179; 0.10083884270194529 0.016309423038745732 -0.10017825055791035; 0.06410337700898844 0.02676677279225291 -0.10948245430836331; 0.06656785953102436 0.037179195897371814 -0.14810820392358962; 0.04245405278694126 0.029968941498251998 -0.1253828416551381; 0.02859519522215217 0.022961701975825824 -0.10223654702992954; 0.010447440266505756 0.008339862222523035 -0.04449081486104393; 0.021215645065953147 0.020415044573506087 -0.09689401764502366; 0.015104311907741459 0.015193406673732856 -0.07843042658736774; 0.011523245977394563 0.011965371921728904 -0.0654212597912767; 0.006443449529848689 0.007901119381306665 -0.054299963669211665; 0.00586064175811996 0.005432799152389824 -0.03591300109775442; 0.002450397615464164 0.003868889802928676 -0.010222685863528024; -0.0019265366875505785 0.003025572439468917 -0.008984380002165922; -0.0007701089407976737 -0.0006227385689955795 -0.002988923412518253; 0.0061355949006521955 0.008885634067549414 -0.008218510417716068; 0.002389985375568807 -0.0004104122973876765 0.0005704356791436885; 0.0006991022403868836 0.003183388003354794 -0.0065348538304180245; -0.0008992144551517663 -0.0013119901434853615 -0.001048839086902943; 0.00292444855100394 0.00039178416556261933 0.0007222554778935295] %
+
+Mass Used: 104.31421287289368 kg
+Launch C3: 95.84364274694235 km²/s²
+||V∞_in||: 0.013760164749867267 km/s
diff --git a/archive/ES_0.5686371502519515 b/archive/ES_0.5686371502519515
new file mode 100644
index 0000000..2feb0d6
--- /dev/null
+++ b/archive/ES_0.5686371502519515
@@ -0,0 +1,22 @@
+archive/ES_0.5686371502519515---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T05:14:30.324
+Launch V∞: [6.127493285662109, -7.387091750613617, 0.09077390723780045] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.184587848051722e-7, 0.00030686584606102004, -0.00021511925785707955] km/s
+ V∞_out: [-0.00019290946824963558, -0.00031408697146773377, 6.754305059868393e-5] km/s
+ time of flight: 1.8521571641067976e8 seconds
+ arrival date: 2029-03-12T22:03:06.324
+ thrust profile: [0.6985844392311289 -0.18461588646675764 -0.20728086876861462; 0.048774811410804274 0.013629696173547704 -0.05144827136693851; 0.052517194404155136 0.028557340751177048 -0.09011719809802572; 0.06373271598305741 0.046017555760162185 -0.15050695678324252; 0.03624375998769377 0.03271680114793313 -0.11281867740931857; 0.044488753505855856 0.04482015521328884 -0.16315693555236807; 0.007670593197012814 0.010225624484519023 -0.04058875939804804; 0.008739876080255882 0.012211493332529515 -0.04907506098498326; 0.012359928289473484 0.013627786312252282 -0.06142907373966133; -0.0008289116266952806 0.0017876294206932563 -0.007953544509955675; 0.0035283481501568554 0.005075755108930028 -0.027296702215879036; -0.004029682984327432 0.005846122199960469 -0.0036127833685219417; -0.001037565408029949 0.0011381791333136618 -0.0017165964228873518; -0.00867709515424971 0.0078035962179882614 -0.00802633928316247; 0.011472632033146121 -0.010940745129639756 -0.006795086533573592; 0.011086739108712091 -0.0024327351312858165 0.007773856345290115; 0.00792854660604116 -0.008382746124991937 -0.012887627860732564; -0.00011304270171660875 -0.008429690907207299 0.0048691019433627376; -0.004600199605137925 -0.0041306153300019015 0.004270191322221533; -0.006140282131329205 0.012539389592110376 -0.020564991128075423] %
+
+Mass Used: 126.02270129363296 kg
+Launch C3: 92.12353840005322 km²/s²
+||V∞_in||: 0.0003747583036388463 km/s
diff --git a/archive/ES_0.5686414347843554 b/archive/ES_0.5686414347843554
new file mode 100644
index 0000000..5ddaa4a
--- /dev/null
+++ b/archive/ES_0.5686414347843554
@@ -0,0 +1,22 @@
+archive/ES_0.5686414347843554---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-08T05:35:20.868
+Launch V∞: [6.465042878493497, -7.768409308705006, -0.24926575416265837] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3728318150048073e-5, 2.191931617461726e-6, -3.816433279153716e-8] km/s
+ V∞_out: [-2.6787886331110827e-6, 5.960954668662581e-8, 1.3638073111166552e-5] km/s
+ time of flight: 1.874957778355881e8 seconds
+ arrival date: 2029-04-16T07:44:57.868
+ thrust profile: [0.07255202319513829 -0.02590675509352027 -0.03654826785649529; 0.020566252517891875 0.00019790823976107534 -0.03284780769689108; 0.015801665327741046 0.0007897252387786286 -0.041594305539973696; 0.01715315404118338 0.0013358978047782201 -0.06341784279931584; 0.031839427924176655 0.0022721255028570315 -0.143897287626002; 0.03110970518189639 0.00155314431076621 -0.16843502372714125; 0.030024422579749542 -0.0014857481446540403 -0.18181588407886154; 0.009655014428303247 -0.0006429819971277583 -0.0658615319215127; 0.00719814799214126 -0.0007258328743337078 -0.05226022340825184; 0.001796825674656577 -0.0002475244286463838 -0.018989777500698947; 0.001766874980538847 -0.00039901747073745633 -0.02112941617993985; 9.191228667847956e-5 3.1802970048354134e-5 -0.0006055527221668709; 0.00013545376265426077 1.9164447784611682e-5 -0.0006878520149036189; -2.6359214891667933e-5 3.6427549051387697e-6 -0.00021376493886630547; 0.00011154279721098588 -7.272017951207705e-5 -0.000588290787362942; 1.0654110412729859e-5 -7.510098013694853e-5 -0.00017672288632473114; 2.031094798779628e-5 -0.00013026278847403077 -0.00010461360857217912; -0.00015035361079197726 0.00021452483643065196 -5.778622548411775e-5; -2.32185478481218e-5 3.5487290347842504e-5 0.00014398854485600174; -1.4244978088317527e-5 9.433390970870106e-5 -0.00044570818099829996] %
+
+Mass Used: 67.20694710530915 kg
+Launch C3: 102.20709602453235 km²/s²
+||V∞_in||: 1.390225664994231e-5 km/s
diff --git a/archive/ES_0.5686437933884556 b/archive/ES_0.5686437933884556
new file mode 100644
index 0000000..dbb8f2c
--- /dev/null
+++ b/archive/ES_0.5686437933884556
@@ -0,0 +1,22 @@
+archive/ES_0.5686437933884556---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T17:55:19.419
+Launch V∞: [6.619281375110357, -7.359107420653558, -1.070009079806732] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.507865174822757e-8, -2.185330644285695e-8, 2.700471214445054e-8] km/s
+ V∞_out: [-8.06488996021738e-8, 3.6140352570512845e-8, -1.0225822550673139e-8] km/s
+ time of flight: 1.874957778578082e8 seconds
+ arrival date: 2029-04-09T20:04:56.419
+ thrust profile: [0.18059590313853757 -0.053720159227702104 -0.06327015627062028; 0.0773429373316229 0.018020809659703974 -0.08679241659183115; 0.05441893851041398 0.025953548810752188 -0.1047657175645085; 0.049162872053211584 0.030392265699315933 -0.12945110058476847; 0.03164929442326153 0.025226996532742987 -0.1135674836176093; 0.022873722520930444 0.021801426098500894 -0.1041878187675622; 0.016943239182462603 0.01860962539625124 -0.09422483470935285; 0.011877651710345766 0.015040126024548866 -0.08000635691608128; 0.007952176730712239 0.01157488220311638 -0.06411466863174578; 0.0038652867845822875 0.006816940167384368 -0.03902947253496626; 0.00173126185550367 0.003185797660724851 -0.018820163682085726; -0.0005367321130671802 0.0004222970529220515 -0.001849898376731977; 0.002013139926133528 0.0006130355467257205 -0.0022848773200418687; 0.001805558389150206 0.0001444692167902448 -0.0013538712645790115; 0.00031230888383957734 0.0006157556272405766 -0.004602400965227619; 0.00048620936401486174 0.000639744691190627 -0.003986938973411904; 0.0010668608560164047 0.0006125777905507821 -0.0034634368550040193; 0.0014327749161931352 1.8998215533000407e-5 0.00019054988170348348; 0.0010275315373940736 0.0005278062244549673 -0.003945954266559172; 0.0017412546858874061 0.0014736806789496203 -0.0027037251231039373] %
+
+Mass Used: 85.23953255545666 kg
+Launch C3: 99.11626738246999 km²/s²
+||V∞_in||: 9.189776092912293e-8 km/s
diff --git a/archive/ES_0.5686464023533101 b/archive/ES_0.5686464023533101
new file mode 100644
index 0000000..57a7cde
--- /dev/null
+++ b/archive/ES_0.5686464023533101
@@ -0,0 +1,22 @@
+archive/ES_0.5686464023533101---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T19:25:24.325
+Launch V∞: [6.494461166834957, -7.3109007687585805, 0.2661906851818441] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.0595360543410334e-8, 4.68415076256319e-8, 3.5498878497982296e-8] km/s
+ V∞_out: [-1.690230620437544e-8, 3.2856134822060215e-8, -5.5671232390801074e-8] km/s
+ time of flight: 1.8143107876189685e8 seconds
+ arrival date: 2029-01-23T16:56:42.325
+ thrust profile: [0.3898499006553742 -0.10116610345537629 -0.11116856989574485; 0.10657799254583858 0.03502986660254312 -0.09619911328022174; 0.09057132545711316 0.05648377327515202 -0.13175708889491056; 0.05245151361457256 0.04554658310624503 -0.1104206899074663; 0.024959413656095438 0.026460448557859884 -0.0706147061561758; 0.041304463326092604 0.05382492302511731 -0.14349877097165242; 0.014428159931734469 0.01762444236636362 -0.05391203209433209; 0.036357089920240386 0.057352316875099035 -0.1415494984395325; 0.016855119482159668 0.020260552332017852 -0.07564618353368097; 0.0039021432304781906 0.00627178466170275 -0.020124977427633157; 0.0014520301634626729 0.0011839631780912912 -0.007321164953038725; 0.001548060679428127 0.0014386744916694704 -0.0039168514502498815; -0.00011556657741135739 -0.000994247719706626 -0.0016039557514704404; 0.001398050732580329 -0.0004365154718042109 0.0015303586663290335; -0.00018667479888292122 0.0015216491149673867 -0.0011718212539344737; -0.0006822660015638974 -0.0008509387949243476 0.003296646334143674; -0.00206002614094308 -0.0001931339032145792 0.0007896026792215305; -0.0002875900630494167 -0.0020364474535931832 0.003027483579017741; -0.0002481326364357886 0.00028711997116342015 0.0013737662498868961; 0.0013752366709114425 0.005884319105928545 -0.0019264200899613143] %
+
+Mass Used: 105.18157470113056 kg
+Launch C3: 95.69815337903964 km²/s²
+||V∞_in||: 6.625989207686586e-8 km/s
diff --git a/archive/ES_0.5686748914926125 b/archive/ES_0.5686748914926125
new file mode 100644
index 0000000..2e9ce7d
--- /dev/null
+++ b/archive/ES_0.5686748914926125
@@ -0,0 +1,22 @@
+archive/ES_0.5686748914926125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T16:02:14.711
+Launch V∞: [6.2626235742302345, -7.404948947733505, 0.2072166415824975] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.455568408704534e-8, 2.5321886190435784e-8, -2.9024273622153836e-8] km/s
+ V∞_out: [9.897596258698074e-8, -2.581837220843799e-8, 1.213197325253688e-8] km/s
+ time of flight: 1.795747781022944e8 seconds
+ arrival date: 2029-01-03T01:55:12.711
+ thrust profile: [0.4960226427958592 -0.14361894713029968 -0.15273335559223838; 0.08843361997584134 0.023881717723326486 -0.08604038697917633; 0.09054516716186936 0.04752854378048022 -0.14619244434315226; 0.06341969300844558 0.04726994972538212 -0.14057968392735518; 0.06392029383066049 0.05932526158145688 -0.17615397644565903; 0.040519772355769035 0.04943240602985196 -0.1516397403257055; 0.014130287729787068 0.016088582528869515 -0.05836190769462537; 0.004108519862844403 0.0050306226932728395 -0.02071317620201168; 0.004897258078607494 0.006569310173285243 -0.018198750828964393; 0.004466032163561986 0.006691423813265754 -0.028237894812627357; 0.0028648576725588885 0.004698415075818214 -0.0037782164020217146; 0.002622796274762392 0.0017901043699687304 -0.0009803735667727504; 0.0007039032052621007 0.0019156087901111174 -0.00876636887878949; -0.00030843040369046067 -0.0014511721743613623 0.00668988665213752; 0.00359535786584529 -0.0028222779571649317 -0.016744591902376343; -0.0013384113133664318 -0.00187194455448103 0.0015632195410031154; -0.003137701591384149 0.005149818683788803 -0.006604406906878802; -0.014107531194099162 -0.005311518608970942 -0.0074721890929842555; 0.0046051688330223045 0.008427120870725852 -0.029028984416484667; -0.0007115306439918656 0.0013604025923839387 9.256551965061916e-5] %
+
+Mass Used: 114.55684689709142 kg
+Launch C3: 94.09666168759256 km²/s²
+||V∞_in||: 1.0209987156066435e-7 km/s
diff --git a/archive/ES_0.568722977749476 b/archive/ES_0.568722977749476
new file mode 100644
index 0000000..e94c09a
--- /dev/null
+++ b/archive/ES_0.568722977749476
@@ -0,0 +1,22 @@
+archive/ES_0.568722977749476---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T14:57:38.879
+Launch V∞: [7.362621721202637, -6.110875158382791, 0.05831012753007413] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0016911097691288126, 0.0012926386790198248, -0.0010658931057440208] km/s
+ V∞_out: [0.00033865974963001686, 0.0023575828192714024, -9.853470052001656e-5] km/s
+ time of flight: 1.7215585457443598e8 seconds
+ arrival date: 2029-10-19T04:01:52.879
+ thrust profile: [0.5275788730826859 -0.026676197901841194 -0.10946274244981095; 0.3270621911938919 0.1868128681532032 -0.21092499962457517; 0.09922275929110558 0.09801338956709126 -0.1232965484404646; 0.0660698342933843 0.09021185789635691 -0.12140806506866562; 0.08917763619220188 0.15406119340627614 -0.20909199948254198; 0.02514450738421839 0.05494117035668862 -0.08636120289340217; 0.0116060333189845 0.02786245980825748 -0.0492678426494576; 0.011869700792658698 0.03879282157144933 -0.06812036500121492; 0.00322278770897544 0.011061979588985084 -0.020800530280663924; 0.001012585900454478 0.0034756745105622745 -0.00669509169281298; -0.0006670317627657173 0.001442442742388211 -0.0012987347162779223; 5.082605480695478e-5 0.0006177167355127821 -0.0010967158459829983; -0.0014733096885040317 -0.001394395425679189 -0.0007087212678115276; 0.0006674956059112829 0.0016460003533913547 0.0005729071824972498; -0.0006871329281357195 -0.00037770938044366035 -0.00023422368797637334; 0.0008495095354080356 0.00045565923283976285 -0.0020886264060858946; 0.0009774735091604581 -0.000687342206514952 -0.0007131052312894015; 0.0017994576838859446 0.0006332599350400202 -0.00013856408064716135; -0.0014252040884578754 0.00016271820530125122 9.736471992886106e-5; 0.0003430864562954479 0.0019191228263490251 0.0011295694559854501] %
+
+Mass Used: 129.4428430636708 kg
+Launch C3: 91.55439388183736 km²/s²
+||V∞_in||: 0.0023805241268707316 km/s
diff --git a/archive/ES_0.5687447591929974 b/archive/ES_0.5687447591929974
new file mode 100644
index 0000000..27d174f
--- /dev/null
+++ b/archive/ES_0.5687447591929974
@@ -0,0 +1,22 @@
+archive/ES_0.5687447591929974---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T01:04:29.791
+Launch V∞: [5.998449080609152, -7.580379057328371, 0.06690013442608186] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5229811637357787e-9, 1.1448929621805053e-9, 9.366873012885995e-9] km/s
+ V∞_out: [-5.338536911116604e-9, -7.673958360233818e-9, -3.6555535805397123e-9] km/s
+ time of flight: 1.745376600657427e8 seconds
+ arrival date: 2028-11-06T03:45:29.791
+ thrust profile: [0.5142810149301136 -0.1748239940477382 -0.15480247957402138; 0.17336282823094282 0.0341756523617914 -0.17091041578956875; 0.07370743059981666 0.03217390277988502 -0.12468926969812939; 0.04253412681994676 0.025957013084381624 -0.09916558986530702; 0.029969109668595294 0.021626345328933882 -0.08654212018316762; 0.021028129544420772 0.018177060405621684 -0.07729265770967436; 0.03691919773485877 0.03764209941902368 -0.15136729366576612; 0.020207614601304217 0.022189504316438496 -0.09614104058845181; 0.01192608703571273 0.01398099567039318 -0.06404960933261204; 0.004605399211851499 0.0056354610270950315 -0.02782081964484099; 0.0014488297158329654 0.001067871216799955 -0.006985404281177837; 0.0051756041756216824 0.004501183473815797 -0.0224606452731385; 0.0009512271020517167 0.0019129058794132086 -0.01044751168442173; -0.0028634449964246088 -0.0021687922058662747 -0.007059394955325592; 0.005444013283003752 0.0017885804784347175 -0.001827873443985344; 0.005231005802277394 -0.0046580604451726 0.0027461330775655603; 0.0019669900301387995 0.0017726389851220284 -0.01590757787941805; -0.0009778269765250622 -0.002825304806545514 0.001089829219624141; 0.0016241744297331535 0.0041709467614853045 -0.0023404458904691576; 0.001389821983815247 0.00894167862271036 0.010836361609439592] %
+
+Mass Used: 118.4221394134911 kg
+Launch C3: 93.44801365342957 km²/s²
+||V∞_in||: 9.558690368427904e-9 km/s
diff --git a/archive/ES_0.5687452696476555 b/archive/ES_0.5687452696476555
new file mode 100644
index 0000000..7a2d32e
--- /dev/null
+++ b/archive/ES_0.5687452696476555
@@ -0,0 +1,22 @@
+archive/ES_0.5687452696476555---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T09:09:18.036
+Launch V∞: [8.209938918977159, -5.645359194330318, 0.08242475228857242] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.492092782899867e-6, 1.364070938685308e-5, 2.957261932785278e-5] km/s
+ V∞_out: [3.000283898018709e-5, 3.3669424957071404e-6, -1.3807460492409807e-5] km/s
+ time of flight: 1.8749577787451226e8 seconds
+ arrival date: 2030-04-24T11:18:55.036
+ thrust profile: [0.144846710159948 -0.0027404722556068086 -0.05419811292781265; 0.03931512641380595 0.020584900608532297 -0.05238581594180855; 0.031305292771792705 0.025600401959111993 -0.07436709522542663; 0.03576923479182798 0.03761933563345879 -0.12176869862806669; 0.027927484340038184 0.0348151347409726 -0.1265238771476668; 0.022114416963475936 0.03154743955136128 -0.12607962011506368; 0.009127111087909975 0.014737926778151795 -0.06530726792171097; 0.013378042557995804 0.022941367833094216 -0.1074105926246393; 0.0020678630184894626 0.0004903337753180649 -0.03053161300359517; 0.006350130214508815 -0.005839801879563889 -0.00832990252798218; 0.002673111098928855 0.001192201342585547 -0.010706705627691823; -0.0024255968106640193 0.001454874855678477 -0.00910823601119425; -0.012863869037098971 0.0015581796566904633 0.012042345138257818; -0.002392149677762293 0.0016902928739144021 -0.0019920047124937137; -0.0017859908700345374 -0.0027982834471026504 0.024193302181019623; -0.003084019291858437 0.015684940493313496 0.027185300413091196; 0.028964883632715273 -0.007623360295144651 0.004413651182521971; -0.001085841713280055 0.016827776714211578 -0.021594133798006312; 0.013097038629327297 -0.00558678529964996 0.0017875520332962095; -0.008898428857396976 0.008675006617111625 -0.031102568811208577] %
+
+Mass Used: 84.40298185314077 kg
+Launch C3: 99.27997132613554 km²/s²
+||V∞_in||: 3.320777070488855e-5 km/s
diff --git a/archive/ES_0.5687505639855515 b/archive/ES_0.5687505639855515
new file mode 100644
index 0000000..6966adb
--- /dev/null
+++ b/archive/ES_0.5687505639855515
@@ -0,0 +1,22 @@
+archive/ES_0.5687505639855515---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T11:56:00.584
+Launch V∞: [5.890841111007284, -7.38191002338245, 0.08724087939252136] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2115129389443605e-6, 0.000688959827946161, -0.00047699002274859836] km/s
+ V∞_out: [-0.0003826961371837728, -0.0007294983034677037, 0.00015328607678919762] km/s
+ time of flight: 1.8507824458955842e8 seconds
+ arrival date: 2029-03-06T14:33:24.584
+ thrust profile: [0.6641469252277354 -0.14348741660640654 -0.13634192754779728; 0.32012327775165483 0.1306001658557275 -0.2026787479989306; 0.15163613820883845 0.11597007090068998 -0.16804683050279726; 0.0663879895254812 0.06939563450532549 -0.10870092703699694; 0.08480253302766334 0.11097218265289076 -0.17175227527428846; 0.02606953692784461 0.03938444182338708 -0.06797179327661286; 0.018029288118137102 0.03618868281021147 -0.06439219770493275; 0.005140118009107844 0.010377217482688507 -0.01983003408761341; 0.004979996554268364 0.011129467870383629 -0.02193237281865231; 0.0001356055564667169 0.0011780500450299825 -0.0018616560553127415; -0.0002847916405731635 0.00039594623081981573 -0.0018717532595211447; 9.171706152812456e-5 0.0006091763016706092 -0.0030783100931450987; -5.132562541246646e-5 0.0002290657681053537 -0.0018297419742157252; -0.00014435476545915458 0.0005207713029995514 -0.0016341460098678443; 0.00012763614680386278 0.00041310773823192656 -0.00022513322849311308; 0.0023046235839817106 -0.0010679006964765788 -0.0010001884600057056; -0.0007914538318513509 0.0008035280492830262 -0.0004355583815123065; 0.0014949462777240122 0.001485867681981914 0.0008861631005801472; -0.0012536205714234446 -0.0008902712711709216 0.001918727768268495; -0.00044142942605723205 0.001293521069930883 -0.0009176319241388676] %
+
+Mass Used: 143.19606721948094 kg
+Launch C3: 89.202215559485 km²/s²
+||V∞_in||: 0.0008379677900222605 km/s
diff --git a/archive/ES_0.5687515926178707 b/archive/ES_0.5687515926178707
new file mode 100644
index 0000000..ba028d3
--- /dev/null
+++ b/archive/ES_0.5687515926178707
@@ -0,0 +1,22 @@
+archive/ES_0.5687515926178707---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T18:48:19.688
+Launch V∞: [7.502353520934823, -6.4004055017678825, 0.04618833225545791] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005655900727453392, 0.0004646896221964291, -0.00034075835478123654] km/s
+ V∞_out: [9.86017369232836e-5, 0.0008003274985997328, -3.469961679077146e-5] km/s
+ time of flight: 1.6482222137751028e8 seconds
+ arrival date: 2029-07-31T10:45:20.688
+ thrust profile: [0.29161014358626763 -0.05331478295842646 -0.11317090946307463; 0.06281269105278357 0.019028561900189037 -0.07418491835957837; 0.05991346828736341 0.031900706007478095 -0.11971195814194799; 0.06324047962655692 0.04322414639903082 -0.17696861877155765; 0.041225854253086995 0.03278751669086285 -0.14796139197552904; 0.05437167079088923 0.04843357055167876 -0.2336987105246054; 0.01970037507114817 0.019070994376406972 -0.10122633861413158; 0.009411496052705566 0.009927627402427211 -0.05390656439214013; 0.003860773694840971 0.005064367909291067 -0.025835047506979146; 0.0026531216181725093 0.002914393656722975 -0.00646476618098064; -0.00015694590359628766 0.0012936218656113489 -0.005965769750876468; -0.0031552082496018497 -0.012680708235068243 -0.005609626989403968; 0.00020716888098381257 0.00013625054687849266 -0.013830211961343219; -0.006946349934538264 0.005982340277751515 -0.0033243675672115997; 5.282823641261907e-5 -0.0023340106342880106 0.001728968448556861; -0.004632847735629307 0.005230536416291445 0.007304832038166625; -0.0050695208272228355 -0.0054867336156964935 0.005705433833693663; 0.026309589485319834 -0.002721851949655362 0.0007657708074108233; -0.004219658402345661 5.2598395176145876e-5 0.013089776876778578; 0.0020765740524188894 0.011674288079652512 -0.011438731383242355] %
+
+Mass Used: 96.23650295813104 kg
+Launch C3: 97.25263230218025 km²/s²
+||V∞_in||: 0.0008074310074045666 km/s
diff --git a/archive/ES_0.5687663512952146 b/archive/ES_0.5687663512952146
new file mode 100644
index 0000000..432da1b
--- /dev/null
+++ b/archive/ES_0.5687663512952146
@@ -0,0 +1,22 @@
+archive/ES_0.5687663512952146---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T03:24:54.145
+Launch V∞: [5.932584579959424, -7.932359395103733, -0.21005237542983685] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.654871187936675e-6, 2.8277939034363197e-6, -2.1034964454130264e-6] km/s
+ V∞_out: [2.550822937760178e-6, -3.298796555927407e-6, 2.1892727356141284e-6] km/s
+ time of flight: 1.6546964227548566e8 seconds
+ arrival date: 2028-07-25T07:12:16.145
+ thrust profile: [0.18832032655320602 -0.08299227714634812 -0.08415563228433405; 0.0856650718032271 0.0049542975012441615 -0.10258228851424198; 0.07230517644591795 0.01790194252114881 -0.14051097606068622; 0.07032725465875624 0.025984752178083166 -0.18656395417318256; 0.05664003872094918 0.025516142521701802 -0.1881518203598038; 0.02874902055830503 0.014584434410502634 -0.11571607179147479; 0.022914677270052464 0.012657985842152568 -0.1052636518986535; 0.013965047563863495 0.00834742456546545 -0.07292995733555659; 0.015003996713484813 0.009365325736577038 -0.08476530926283145; 0.002384551382093607 0.001462603627505349 -0.014590693265585642; 0.0029926944334015405 0.002518984209864184 -0.02246341684100258; 0.0013325433602648356 0.0002564958718843744 -0.012011347856513971; 0.0026735527648401773 -0.0004710802370283356 -0.00344850302895517; -5.146762323368832e-5 0.0003690484681914542 -0.0005218958625076756; 0.0008227891484079279 0.0015529231594122288 -0.001293637429637434; 1.5667984130861463e-5 0.0003884849892100544 -0.002092254167112326; 0.0003772410145509782 0.00021981143221589186 -0.0021938744037541032; 0.001542963856748506 -0.0010036148080735446 -0.005830064165123048; -0.0008810311084277908 0.002069793447421284 -0.004861687077667863; 0.0010330653427539195 -0.0013854884336092846 -0.0028458780320221875] %
+
+Mass Used: 90.94903350841241 kg
+Launch C3: 98.1620073718865 km²/s²
+||V∞_in||: 5.838573578577206e-6 km/s
diff --git a/archive/ES_0.5687802329288792 b/archive/ES_0.5687802329288792
new file mode 100644
index 0000000..299bf32
--- /dev/null
+++ b/archive/ES_0.5687802329288792
@@ -0,0 +1,22 @@
+archive/ES_0.5687802329288792---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T22:31:52.414
+Launch V∞: [6.41396436530386, -7.329444417271345, 0.17172571681968918] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002340119183145002, -0.005306685520964426, 0.007214044753444673] km/s
+ V∞_out: [-0.006754308488740784, -0.005161032793974126, -0.0028181204461188176] km/s
+ time of flight: 1.8749577787487122e8 seconds
+ arrival date: 2029-04-09T00:41:29.414
+ thrust profile: [0.4851793245901717 -0.11740712531973152 -0.14970445720512005; 0.07750487496235416 0.024666150947059477 -0.08182884291017598; 0.030377398820882022 0.01695345958335398 -0.053035851745740624; 0.02508012208955471 0.02089986698887048 -0.06595569930290321; 0.014157698783665369 0.012757700453649186 -0.044797876241679815; 0.016634700263106036 0.018101342162299146 -0.063597055651678; 0.019318015037648593 0.024585783663744774 -0.09054569574806103; 0.008775908669900061 0.010952813300956099 -0.04493446626465403; 0.03651713513651432 0.052791916047458386 -0.1923650409522375; 0.019683923884791104 0.03509023920401999 -0.13443533694361698; 0.002986250202273932 0.004319605284380653 -0.01743205816958066; -0.001178705259608141 0.00016823629615057037 -0.002115338493150239; -0.00023734182498227994 -2.301167240604557e-5 -0.0004936754490620552; -0.00028407937809750373 -0.002643845900904868 -0.0008735203358383023; 0.007056063549711503 -0.007534551415014927 0.0035866429674904984; -0.00496819398592868 -0.0033970987129974396 -0.00979204423104145; 0.0028809547525418307 0.0018485165270416969 -0.0012880632454861601; -0.0015038579383192877 0.006587044589873735 -0.005403931087008677; -0.011673408938793803 0.0006652487069991463 -0.01890274022721687; -0.0151391353785264 -0.0034926456972497666 0.006363108971507835] %
+
+Mass Used: 110.05669802575449 kg
+Launch C3: 94.88918406707508 km²/s²
+||V∞_in||: 0.008958689329418078 km/s
diff --git a/archive/ES_0.5687811272545243 b/archive/ES_0.5687811272545243
new file mode 100644
index 0000000..9fab46f
--- /dev/null
+++ b/archive/ES_0.5687811272545243
@@ -0,0 +1,22 @@
+archive/ES_0.5687811272545243---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T10:07:04.796
+Launch V∞: [7.364619253431945, -6.656778072422238, -0.2890653048819257] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006947353299561557, -0.0025405153588404644, -0.003908989654999675] km/s
+ V∞_out: [-0.004125702551311261, -0.0004286551134846863, 0.002237087757133388] km/s
+ time of flight: 1.5569111886959416e8 seconds
+ arrival date: 2029-04-15T09:39:02.796
+ thrust profile: [0.19406150257303956 -0.045442406013990015 -0.08156155785810774; 0.06320421635885193 0.01614409202850227 -0.07708740142002868; 0.08404234963504083 0.04151924984591174 -0.16643945331659563; 0.06442092966470814 0.04131132050838541 -0.17709971302154112; 0.07030495873791069 0.05749898332169215 -0.2483897277532163; 0.04654744353353737 0.04000008269734239 -0.1950050924018889; 0.014356126506392876 0.010996461770030067 -0.06993584564710839; 0.01651312143267512 0.012709851858281348 -0.07782676650177955; 0.005350567221432938 0.00471494916203049 -0.031589232321450215; 0.004122310961966471 0.0032240275228059014 -0.028615426253367368; 0.0017894213315838479 0.0017976208598248957 -0.013761295180957474; 0.001128943997795446 0.0013148294930072505 -0.005778984322034505; 0.0003907458024952667 -0.0005299774673043599 -0.0019438949036745742; -0.00016533203236755202 0.00012207538213700045 -0.00029493623898264616; -6.37555043151957e-5 0.000282810000342893 -2.091391969715091e-5; 0.004338716747648668 -0.00014057447812701088 0.0010384971635396664; -0.000787535850410608 -0.0011604534140693737 0.001970707013276977; 0.000268178596780658 0.0034957570474434974 0.0019325378406084134; -0.000335416989918299 -0.0006935109818199014 -0.0004032262410742023; 0.00016691667534154798 -0.004386663122274396 0.0023197865610577665] %
+
+Mass Used: 88.2137412736788 kg
+Launch C3: 98.6338698039885 km²/s²
+||V∞_in||: 0.0047134992935279054 km/s
diff --git a/archive/ES_0.5687969366932395 b/archive/ES_0.5687969366932395
new file mode 100644
index 0000000..d8335e6
--- /dev/null
+++ b/archive/ES_0.5687969366932395
@@ -0,0 +1,22 @@
+archive/ES_0.5687969366932395---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T14:56:59.228
+Launch V∞: [7.493077580577847, -5.587774798167059, 0.13219006567394928] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.015217559853593122, -0.01008663438159384, -0.0006454574656446152] km/s
+ V∞_out: [0.013524154910571256, 0.006302001504598842, -0.010585961176820077] km/s
+ time of flight: 1.8588996638776022e8 seconds
+ arrival date: 2030-03-28T03:03:05.228
+ thrust profile: [0.9859541899529035 0.011879411197934677 -0.16995861546272895; 0.24613827177386874 0.16889664986030078 -0.16448165044791305; 0.07893592386994464 0.09191876482489025 -0.10383100244269809; 0.05497363972709222 0.0973349983672548 -0.11790106341110546; 0.025204899958315544 0.058327551975100506 -0.07916869563356185; 0.016683026427553902 0.05041242937449139 -0.07328677176051678; 0.02458586067714928 0.08013052887472728 -0.11756954482097826; 0.002058902634914436 0.00987259546591348 -0.01734080277813107; 0.0013195190945667627 0.010529800618043594 -0.01890423718598771; 0.000537407829350299 0.00681176767754929 -0.01270864913683505; -6.624081342411966e-5 -0.00023284638665348504 0.0010634940955973507; -7.300174245030997e-5 -0.0014518325908151573 -0.0003755473380805778; 0.0006455053585198085 -0.0016067696891514701 0.0008700187378662405; -0.00019614420511223003 0.0007373177914512506 -0.0018355177206816867; 0.0002968766469714641 0.00044232438112829105 -7.807175977270773e-5; -0.004343387985980884 -0.00020428915686576937 -0.0004074110167593774; 0.0036230084719582885 -0.00022667958638199117 0.00039773193461971204; 0.0021906422780122474 -0.004657035310670462 0.001589256599942477; -9.523956907452062e-5 0.0002937494260138373 0.0002433417190049656; -0.0008840258307443583 -0.0009850885311923894 0.0007083543862710801] %
+
+Mass Used: 153.83943342597513 kg
+Launch C3: 87.38691303705217 km²/s²
+||V∞_in||: 0.01826830414640605 km/s
diff --git a/archive/ES_0.5688022621618092 b/archive/ES_0.5688022621618092
new file mode 100644
index 0000000..a72ae14
--- /dev/null
+++ b/archive/ES_0.5688022621618092
@@ -0,0 +1,22 @@
+archive/ES_0.5688022621618092---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T15:26:15.234
+Launch V∞: [7.558484086043648, -5.62158278730936, 0.5637372768355201] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.365290838976269e-5, -0.0002639594280149839, -0.0005988289113513186] km/s
+ V∞_out: [-0.0006143446352801808, -6.92070852257355e-5, 0.0002497883748710184] km/s
+ time of flight: 1.8216020128849155e8 seconds
+ arrival date: 2030-02-11T23:29:36.234
+ thrust profile: [0.9138491120803722 -0.004292591064352976 -0.16398430282845822; 0.22618437563756916 0.1496398132934383 -0.16524599552484928; 0.11253731604678592 0.1253887407087245 -0.15252811815900713; 0.051840228513401435 0.07955695260379599 -0.10909981970169813; 0.04163942463575118 0.0826951777618916 -0.12136728677502567; 0.012460327484815768 0.03255883574021763 -0.05300181332165023; 0.015600530965506464 0.04715564189590435 -0.07931178655133425; 0.0008517244276081004 0.004341194431955195 -0.00795604262406108; 0.001109503098863325 0.006160791800469106 -0.01272900024582568; -0.0004585495064552183 0.0012009134903130851 -0.0022278038407653055; 0.00041354431472812286 0.0018290525186870853 -0.004442692226299365; 0.0003582403744750408 0.0033168301933345834 -0.005108379971173496; -0.00048325688628428223 -0.0009096920172175353 0.0005352508279306458; -0.001436352015693975 4.858498572438553e-5 0.00195375166454357; -0.0016550626989624776 -0.0013060214824618277 -0.003622398273072946; 0.0011523614030265806 -0.0017100337309190938 0.0006766344259092493; -0.001256749900816887 0.0014370240290934384 7.468169660082276e-5; -0.0025992030407273954 -0.00030750127649998736 0.000394828403684476; 0.0011323742508840134 -0.0031788309913233035 -0.001713750561053044; -0.00328964932877953 0.00026589647449876277 -0.003074296025417118] %
+
+Mass Used: 144.14037167553306 kg
+Launch C3: 89.05067443084188 km²/s²
+||V∞_in||: 0.0006610911525334945 km/s
diff --git a/archive/ES_0.5688077111499742 b/archive/ES_0.5688077111499742
new file mode 100644
index 0000000..f958579
--- /dev/null
+++ b/archive/ES_0.5688077111499742
@@ -0,0 +1,22 @@
+archive/ES_0.5688077111499742---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T21:15:30.735
+Launch V∞: [6.259047198288048, -7.600714999423568, 0.22955782888118254] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.731699029889883e-8, -8.749554954050011e-6, 5.942485249014054e-6] km/s
+ V∞_out: [5.334093608361025e-6, 8.934645011780786e-6, -1.859992307494762e-6] km/s
+ time of flight: 1.8396888519872248e8 seconds
+ arrival date: 2029-03-01T03:43:35.735
+ thrust profile: [0.3073475000563275 -0.09128958982726365 -0.11587291196450647; 0.08274369110651142 0.015420371082338269 -0.09914325456059292; 0.07300386610301485 0.02856929579278345 -0.14549509515904366; 0.03632451343331813 0.01895557334403139 -0.10268712498185777; 0.02241264620258836 0.013805738516538695 -0.08097891538091409; 0.039607042196907416 0.02829101246712169 -0.1701266379691867; 0.022154572434540193 0.016638951416486934 -0.11074887113539195; 0.008393671894590773 0.006898095584293896 -0.04932423272726073; 0.0029810842019761434 0.0021174400315047905 -0.018507664800200968; 0.00550615543133957 0.004901187416336213 -0.039855757307281484; -0.0008407433753019925 0.002841470026470572 -0.006431096847596934; 0.0012671647936265268 3.769429317877185e-5 -0.014560686596817857; 0.0044645562542360365 0.0010967819528838688 0.0009433781634230801; -0.0020449317921286585 -0.0013617517568059903 0.0009221592500141171; 0.005531917651578186 -0.003203006941737678 0.003330676543924764; -0.015603843830702038 0.002723179834578929 0.002926899140892136; 0.003740942022551374 -0.0020512779389154153 0.003300110357845061; -0.005258378410868386 0.006575312595086716 0.011957829267443204; 0.00017298273707088514 -0.00715133628252034 -0.007840792635955133; -0.0021745606718579884 -0.0029582300597912146 0.018507859502882137] %
+
+Mass Used: 97.78011308528357 kg
+Launch C3: 96.99923712966051 km²/s²
+||V∞_in||: 1.0576794838071205e-5 km/s
diff --git a/archive/ES_0.568808065694471 b/archive/ES_0.568808065694471
new file mode 100644
index 0000000..747a2bc
--- /dev/null
+++ b/archive/ES_0.568808065694471
@@ -0,0 +1,22 @@
+archive/ES_0.568808065694471---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T21:29:04.312
+Launch V∞: [5.94024346443424, -7.807833597868925, -0.1274907166849016] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.925241665490379e-5, 2.0605197065661813e-5, 2.629632739637367e-5] km/s
+ V∞_out: [3.212339024483691e-5, 2.077910788927607e-5, -2.0067946447269644e-6] km/s
+ time of flight: 1.680722132118536e8 seconds
+ arrival date: 2028-08-24T04:12:37.312
+ thrust profile: [0.349978391873276 -0.1444981154478198 -0.14754880474804377; 0.08728975272368707 0.0072662525758827095 -0.11010412447869183; 0.06736530915322865 0.019442545911231006 -0.13816140264804253; 0.06735138577343791 0.027981037862944147 -0.18775163318056856; 0.0312946409694478 0.01525198928663111 -0.10753671761668732; 0.021983946340897963 0.012349559127726516 -0.08974808893290528; 0.021202400467969822 0.012320019873248886 -0.09535116311219252; 0.03394963348256718 0.021089612264855572 -0.18277422245997338; 0.0073788680873990995 0.006618035952223065 -0.04906186713665119; 0.004540966080578849 0.003842861392389598 -0.03834544379959695; 0.0010520488091925815 4.83575377646559e-5 -0.006727132412262781; 0.0003825802805093692 0.00169401006293757 0.00048336515394284277; -0.001461875452590204 0.001849475330774591 0.0020564080331709695; -0.002045728799911688 -0.0008445990631832585 0.0016019491892036372; 0.0009261103161642194 -0.003804774247336434 4.276576825745348e-5; 0.0008289770229825262 -0.0013854354685505798 -0.0006753043789490038; 0.002069004994378138 0.006746184113677612 0.0038780277408638686; 0.0006718823983239035 0.00015822493790201522 0.00011711978347809498; -0.006518844487931578 -0.0019149206156635016 0.0026863685765271495; -0.0034043372639642466 -0.00046469506283236116 0.0033165439218590053] %
+
+Mass Used: 102.06350785918494 kg
+Launch C3: 96.26501179160533 km²/s²
+||V∞_in||: 3.855809289508556e-5 km/s
diff --git a/archive/ES_0.5688153503393215 b/archive/ES_0.5688153503393215
new file mode 100644
index 0000000..e351ea1
--- /dev/null
+++ b/archive/ES_0.5688153503393215
@@ -0,0 +1,22 @@
+archive/ES_0.5688153503393215---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T18:40:25.377
+Launch V∞: [6.262968952303489, -7.434785605128445, -0.0218619098820705] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.062999442570514e-5, -3.140293052233909e-6, 7.560385422862741e-8] km/s
+ V∞_out: [4.028372609668173e-6, -9.706947352534989e-8, -2.0506652253828436e-5] km/s
+ time of flight: 1.8556076571680743e8 seconds
+ arrival date: 2029-03-16T11:19:50.377
+ thrust profile: [0.4067203267640162 -0.09008858169244853 -0.12584371287112767; 0.12799873128398498 0.04471899099145285 -0.12241795573272247; 0.11138980405214986 0.07131335079248233 -0.1811754790515582; 0.06545444649258461 0.051790049038671904 -0.14746001853118745; 0.031081247270902886 0.031213670258509824 -0.09323489879349124; 0.033948515394007533 0.044148869877433626 -0.12561584796087555; 0.017487934227871996 0.023009555060065245 -0.07782418152229119; 0.005641044551980928 0.008730639711418433 -0.03061754076910251; 0.0019486718777471184 0.002662486607140459 -0.01324308447472397; 0.0028661749106398344 0.0036389272198560922 -0.01667886238107829; 0.0018375462891355677 -0.0018412542652877385 -4.483846618609467e-5; 0.001942102260289176 0.0007474121937499366 -0.009223133374551027; 0.0019986184510644824 0.0022571245639073905 0.0006491161449963317; -0.007327640801950464 -0.0020955916462760934 -0.0027898122130751313; 0.00030472479464392177 0.004502715559114107 -0.0010799874759304996; -0.015291575915906682 0.01683300016782706 -5.590392711987517e-5; 0.010680255582581056 0.0035991167102490226 0.001818143917579942; 0.014225462141160453 0.006235240754164583 0.004934092161676437; -0.014709398548193411 -0.010579625475178362 -0.02169293677399968; 0.010649564547094665 -0.007874518142601239 0.008278248311579323] %
+
+Mass Used: 112.3603543592717 kg
+Launch C3: 94.5012950348463 km²/s²
+||V∞_in||: 2.0867770039017297e-5 km/s
diff --git a/archive/ES_0.5688416336404964 b/archive/ES_0.5688416336404964
new file mode 100644
index 0000000..3141e38
--- /dev/null
+++ b/archive/ES_0.5688416336404964
@@ -0,0 +1,22 @@
+archive/ES_0.5688416336404964---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T02:09:04.805
+Launch V∞: [6.4723769217038605, -7.426548102596526, 0.02123278454921236] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01311891135600221, -0.0004503735486942265, 0.009339335543727617] km/s
+ V∞_out: [-0.014753918840241798, 0.0001390452680919989, 0.0041998381982127735] km/s
+ time of flight: 1.8749577787482598e8 seconds
+ arrival date: 2029-04-11T04:18:41.805
+ thrust profile: [0.3101861930363548 -0.0939924357198873 -0.1239327579551241; 0.08114181423943188 0.015372817972012275 -0.10300768218236127; 0.050883982487813374 0.018493525427349854 -0.10818667585391809; 0.027979128190999684 0.012445448210903116 -0.0826533300247969; 0.019271336057129124 0.009497186295665101 -0.07123498846760985; 0.016953020143260507 0.008829241686537025 -0.07445459182871599; 0.014861831076631426 0.008578208213404565 -0.07700750966378743; 0.02259198843735061 0.015216671583496164 -0.1349138995623441; 0.010752585921440697 0.00732336453251267 -0.07136980517426933; 0.005643328555283314 0.0018555774933869417 -0.021094207225568543; -0.0030869786394306284 0.004649884598820882 -0.012480573275405511; 0.002255364196757869 0.0016616320635167692 -0.003820493894498313; 0.0014027299932125549 0.002992506537368645 -0.0173530630202505; 0.017068517315818564 0.022537844573919035 -0.023070309858013994; -0.003632633920286501 -0.010571913548500619 -0.01408035145337771; 0.0025380207208188284 -0.0006260886791791117 -0.0071955775374782874; 0.01980168037317307 0.019734942359199273 -0.011670345562473513; -0.0016090414188204144 4.6865161593485005e-5 -0.0008860212406669025; -0.0053248584705629515 0.0010186349867437675 0.0014297172405208138; -0.009137781516265701 -0.01761857202356979 0.0039405780650669416] %
+
+Mass Used: 97.54847760101939 kg
+Launch C3: 97.04573056792452 km²/s²
+||V∞_in||: 0.01610999254805356 km/s
diff --git a/archive/ES_0.5688434133550254 b/archive/ES_0.5688434133550254
new file mode 100644
index 0000000..59ae53b
--- /dev/null
+++ b/archive/ES_0.5688434133550254
@@ -0,0 +1,22 @@
+archive/ES_0.5688434133550254---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T07:43:37.351
+Launch V∞: [5.9026981061137365, -7.8524706876800865, -0.15168659836798057] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.025675443828904677, -0.012988339118007458, 0.028312170870275877] km/s
+ V∞_out: [-0.02624135175718643, -0.010760518145062441, -0.028722588116407637] km/s
+ time of flight: 1.7002969740736416e8 seconds
+ arrival date: 2028-09-17T06:11:54.351
+ thrust profile: [0.31153457216958574 -0.13394546548231062 -0.13531245887425833; 0.10827060265137316 0.007311863900260426 -0.13104758468806252; 0.0820318488157218 0.02103332896904245 -0.1634556177365693; 0.06283630479502358 0.023108748524921067 -0.1721838460450091; 0.045584234199092556 0.020423949379687886 -0.15778951532717567; 0.026253597757331503 0.013433660794312545 -0.10993352468595004; 0.0111800965747476 0.005972505872222395 -0.05357774357901926; 0.013991633734090994 0.007999009981995358 -0.07568676808712188; 0.0035688607365249123 0.0015204804162479827 -0.016676908642293264; 0.007189092799956469 0.0043023395569879285 -0.046218886849482735; 0.006964602906349866 0.004653642461941639 -0.04917908760176704; 0.0002814797449236908 0.0007257701574758243 -0.0017432222844446024; 0.0005860568600275861 0.0007267242677828459 -0.004507872068119468; 0.0008701274757057413 0.0009460565840690466 -0.0024515818797196344; -0.00020442817225593856 -0.0002563337547638469 8.932917922436926e-5; -0.002523989881413443 0.007928799269543088 -0.00646008911112457; 0.0015349805781801622 -0.0005753739871058839 -0.00265016641715771; 0.00030066687648364423 0.001980503052192163 -0.01402344035872453; 0.0019936495505756954 -0.002912059225229602 -0.006925355782370367; 0.00773580433847771 0.001467541545377836 -0.007028182613628673] %
+
+Mass Used: 100.58144258217408 kg
+Launch C3: 96.52614965691811 km²/s²
+||V∞_in||: 0.04036712013809382 km/s
diff --git a/archive/ES_0.5688601790738772 b/archive/ES_0.5688601790738772
new file mode 100644
index 0000000..446f295
--- /dev/null
+++ b/archive/ES_0.5688601790738772
@@ -0,0 +1,22 @@
+archive/ES_0.5688601790738772---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T15:49:15.960
+Launch V∞: [7.710807074137062, -5.92503617129495, -0.7752751672556797] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.083791306261855e-10, -2.5819394767177594e-9, 9.845224679036607e-9] km/s
+ V∞_out: [2.105155808016895e-9, -7.3081349244190136e-9, 1.0646271474022629e-9] km/s
+ time of flight: 1.874957777178933e8 seconds
+ arrival date: 2030-04-21T17:58:52.960
+ thrust profile: [0.37001354527358066 0.039956392035739696 -0.10512578387968098; 0.08693681696627695 0.07821970389118021 -0.07143053781727927; 0.04990392312273785 0.0839669389779467 -0.08247237456718956; 0.043371967645053924 0.09704681277935358 -0.10593163373763388; 0.026320570574082585 0.08589993186426044 -0.09680525640509408; 0.018969928286534557 0.08415683353767073 -0.1012884858418511; 0.011832380638486985 0.0860977450835502 -0.1186359069463274; 0.005812121596075542 0.060012261048742035 -0.08021571990711705; 0.0025129446695096843 0.04241650551267349 -0.05932076134593752; -0.0007690364280868937 0.005484991612074757 -0.004326938030526445; -0.0007918166976968138 0.0013282324362618092 0.001522753752185157; -0.001826675476486397 0.004359239996655492 0.001989492795214866; -0.0005008857028245736 -0.00042366122435895815 0.002873257825303217; 0.005579635508678004 -0.00018266248382804566 -0.007967509996175674; -0.0031860696373859155 0.006427281404975187 -0.001607819213092262; 0.00289905276776455 0.004281996784175933 -0.009112243454084578; 0.0031333301290922804 -0.002878079383344766 -0.007780134906615745; -0.0030819357772708627 0.003969693497651758 -0.0005749262159516598; -0.00238554916822765 0.004073616825933616 -0.0022607047045693405; -0.0007428813033577271 0.0004544480876807616 0.0026286873328981797] %
+
+Mass Used: 108.54891170722931 kg
+Launch C3: 95.16365095067898 km²/s²
+||V∞_in||: 1.0190844409694482e-8 km/s
diff --git a/archive/ES_0.5688929913293753 b/archive/ES_0.5688929913293753
new file mode 100644
index 0000000..233b69f
--- /dev/null
+++ b/archive/ES_0.5688929913293753
@@ -0,0 +1,22 @@
+archive/ES_0.5688929913293753---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T00:08:46.932
+Launch V∞: [6.223380362653011, -7.50920874827629, 0.08681119563067483] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.243660751877114e-10, -7.497363481610951e-10, -3.136269601150524e-10] km/s
+ V∞_out: [-4.782184124420629e-10, 9.979161832352733e-10, 1.4556494396538233e-9] km/s
+ time of flight: 1.8749577787483537e8 seconds
+ arrival date: 2029-04-10T02:18:23.932
+ thrust profile: [0.3015896974714105 -0.07415583777011263 -0.10381069148149388; 0.29997768692317467 0.08578450825758323 -0.2933857315235269; 0.054018699880578516 0.029973425911789406 -0.10022890115928058; 0.03798182727601108 0.028265716895942025 -0.09940971325938538; 0.03482749006378582 0.031016559081005028 -0.11620942460920428; 0.02525711481457459 0.02579457992084293 -0.10329348247065485; 0.008381029640620524 0.00873410716438294 -0.04512816219304279; 0.0029210367977271414 0.003650955766505912 -0.026282294219518876; 0.009324763650783848 0.012979042212029567 -0.03280092839560742; -0.002717814711476287 0.0011212086935565926 -0.008208542379393958; 0.012934290778002611 0.00736107171923215 -0.0130144665295143; 0.0023446493331081572 0.00820684611632048 -0.0022576685398306108; -0.007817859160204041 -0.008515984736982264 -0.006080821713743861; -0.008983927197897468 0.008492543765851096 -0.002778469478344435; -0.0021890813086637997 -0.002040924300698601 -0.0005138087333541172; 0.004187071985789348 0.005409809415754047 0.001711781397727825; 0.0019522921495357289 -0.0012647845713596743 0.004614336295773844; -0.02051773468377245 0.006637397892743219 0.005896394011348205; -0.0110925941039083 -0.012089157065597803 0.0014915532663870449; -0.008211778161391837 0.0009820352983613964 -0.008829109828003496] %
+
+Mass Used: 108.80556702600643 kg
+Launch C3: 95.12621534713111 km²/s²
+||V∞_in||: 8.430934690531538e-10 km/s
diff --git a/archive/ES_0.5689024303340172 b/archive/ES_0.5689024303340172
new file mode 100644
index 0000000..559bbf8
--- /dev/null
+++ b/archive/ES_0.5689024303340172
@@ -0,0 +1,22 @@
+archive/ES_0.5689024303340172---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:03:39.986
+Launch V∞: [7.271559182740606, -6.338801973418237, -0.05956913055535076] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005483211378383371, 0.03496356839379095, -0.00014841269597618508] km/s
+ V∞_out: [0.03372417141261891, -0.005399687734854963, 0.007480129805611045] km/s
+ time of flight: 1.6280166787749892e8 seconds
+ arrival date: 2029-07-05T00:44:46.986
+ thrust profile: [0.6362874221320821 -0.10260379384272497 -0.18739153249993432; 0.10280247787583119 0.039445266827519136 -0.1050759505659751; 0.08609343361069276 0.06076512232634461 -0.15120517292502972; 0.06776140151476294 0.06509126336619583 -0.1713723214422832; 0.03433328710629911 0.04006295266952307 -0.11497093200338507; 0.04322395187778364 0.055553972314504194 -0.16550535871465438; 0.01644738009753438 0.02352518460862277 -0.07719215642931371; 0.0185147272664501 0.028795315586930492 -0.09947378769555507; 0.011394932726099151 0.019681259374958907 -0.07244044590566587; 0.0017662160078475056 0.003409817310538057 -0.01272154469566548; 0.0032948832733289395 0.0016786324613037003 -0.0010589923568876444; -0.0007491527767034965 -3.885355023156641e-5 0.0017391724461116782; 0.0019115540976792438 -0.00601462795115364 0.0005890387665353656; 0.0037543794854602505 0.0045518585546765 -0.006641391737233979; -0.00040439810706284024 -0.007182621680287947 0.0040238602663437385; 0.009537757099254756 0.0010749351677137768 0.0045973141715284944; -0.006077845418864859 -0.011317440160608233 -0.0016176632704470006; -0.009390859793386103 0.0033624019734686175 -0.003547966544183256; 0.0007105204734350163 0.01128486757562087 -0.00023846946235287804; -0.00032989595740940493 -0.0019849260874211542 -0.0029921473775377525] %
+
+Mass Used: 120.87223271187258 kg
+Launch C3: 93.05953188762528 km²/s²
+||V∞_in||: 0.03496818264116431 km/s
diff --git a/archive/ES_0.5689111658512104 b/archive/ES_0.5689111658512104
new file mode 100644
index 0000000..afc1a28
--- /dev/null
+++ b/archive/ES_0.5689111658512104
@@ -0,0 +1,22 @@
+archive/ES_0.5689111658512104---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T03:32:44.745
+Launch V∞: [6.474143496581044, -7.290960965643769, 0.2973027606161238] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.67907279131996e-7, -3.6718784932551786e-8, 4.684448018210609e-8] km/s
+ V∞_out: [-1.7644887440708908e-7, 1.724089704569358e-8, -2.15167549573086e-8] km/s
+ time of flight: 1.8548328181420347e8 seconds
+ arrival date: 2029-03-12T22:40:45.745
+ thrust profile: [0.4065806785884678 -0.0882551297681877 -0.09059335854834827; 0.094695216120833 0.035931027843827054 -0.07790464761200284; 0.08904053564885629 0.06269743260346558 -0.11914167973471812; 0.04321314983213102 0.04135715296280917 -0.08366811499452871; 0.043492720349647976 0.051792198512998155 -0.10755580004548014; 0.047463842169784144 0.06754813178592119 -0.1400775337795605; 0.029504280640372513 0.04760596137487421 -0.10635804248862181; 0.01695258851669234 0.03037574139963664 -0.07203134547490925; 0.009777938405146834 0.01889041966262704 -0.04641890919197219; 0.0067913242535885526 0.015171486697075541 -0.03882224693788409; -0.0037643618792398436 0.003240569754626693 -0.0015427474332686342; -0.001585476465248424 0.003918041923766387 -0.003573652415502802; -0.003608367944726433 -0.0008038369844143723 -0.002896020897757463; -0.0008912196662420105 0.0018667639723258995 -0.00029390413559264757; 0.0010375382442599707 0.00035546559425031395 -0.003320650979137539; 0.0003870375913409785 0.00019147685465288112 -0.0008792552112598059; -0.010640482379800996 0.011704224829819787 -0.004762914448787741; 0.0037995593151012546 -0.005761465140285602 -0.01697743837428602; 0.0021120391312485632 -0.011505886834717715 0.0010596441322560366; 0.0005330474905464192 -3.3518960460593104e-5 -0.0010207876259839055] %
+
+Mass Used: 108.6236574611321 kg
+Launch C3: 95.1610347483337 km²/s²
+||V∞_in||: 1.781446852307549e-7 km/s
diff --git a/archive/ES_0.5689113232981524 b/archive/ES_0.5689113232981524
new file mode 100644
index 0000000..24a478d
--- /dev/null
+++ b/archive/ES_0.5689113232981524
@@ -0,0 +1,22 @@
+archive/ES_0.5689113232981524---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T04:32:49.410
+Launch V∞: [7.883447244624852, -5.511546518706388, -0.13969232740688214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00023107522348967804, 0.00017004187599516777, -0.00013010339050125152] km/s
+ V∞_out: [-0.0002233400366359051, 0.00029754979788459903, 4.105055303515514e-5] km/s
+ time of flight: 1.8749577773042315e8 seconds
+ arrival date: 2030-04-18T06:42:26.410
+ thrust profile: [0.5573635865406248 0.013672361911816174 -0.14026178656834498; 0.21998698296291475 0.15219335142585727 -0.1926050643325942; 0.07275717501049563 0.084371249527235 -0.12432219979501764; 0.0524178970859838 0.08371498412460567 -0.1357864998065707; 0.024218286393344824 0.05016441439727604 -0.09143343821663272; 0.011713325341405283 0.029514339234888814 -0.060118898080154234; 0.009541438220803177 0.029559653269283965 -0.06354876397194892; 0.0009150485916393333 0.005008308307756679 -0.01918824576106586; 0.0032578625094674876 0.014819996125103405 -0.03700729937338705; -0.002235080063011584 0.0032727923503031854 0.0025348718386902303; 0.0035261386281656053 0.00837617524695193 -0.007957080883488057; 8.590881043429716e-5 0.0050601167912398826 -0.014129065749684285; 0.0034874153442485626 0.000943366866911127 -0.0014791261066152356; -0.00771481681748131 -0.004603310047302759 0.0022924102531902556; -0.010013605820952658 0.002266439698309101 0.006283561789848938; 0.002929694647209222 0.008050359359098348 0.007908587466230032; 0.010611534237776481 0.003742001107410353 0.00731844719325492; 0.0012370303313779985 0.0008550269359683857 -0.006170022459702267; -0.001208888125369622 -0.009362797121313072 -0.0009422929125063508; 0.015041058842045141 0.0031546091948189752 0.005603535180458369] %
+
+Mass Used: 123.8817138221043 kg
+Launch C3: 92.54539943298403 km²/s²
+||V∞_in||: 0.00031501887359757 km/s
diff --git a/archive/ES_0.5689232415181253 b/archive/ES_0.5689232415181253
new file mode 100644
index 0000000..994e9a2
--- /dev/null
+++ b/archive/ES_0.5689232415181253
@@ -0,0 +1,22 @@
+archive/ES_0.5689232415181253---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T19:47:43.509
+Launch V∞: [6.139989752845699, -7.756470595755766, 0.8982460180992401] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.839046311624002e-10, -4.004111745419425e-9, -1.6511254905613418e-8] km/s
+ V∞_out: [5.871088435998627e-9, 8.309734468775895e-9, 4.0695306357692264e-9] km/s
+ time of flight: 1.7440448725943795e8 seconds
+ arrival date: 2028-11-07T09:29:10.509
+ thrust profile: [0.17271841045040728 -0.062150073866923186 -0.06606555014177165; 0.07926504717891047 0.010529385766815818 -0.08954263249497144; 0.06566977161712605 0.021215316633998626 -0.12207041605231997; 0.11353524707562175 0.051635501833263216 -0.2726876288929356; 0.04282929212396326 0.022185035496092374 -0.1363027387667022; 0.028795619296629795 0.017022530375422958 -0.10688121598791794; 0.020133842223588324 0.013240361217990418 -0.08931067084235549; 0.012135967501174244 0.008200632909761566 -0.05961114494254005; 0.007694249915701059 0.006113930474513418 -0.04389236822097041; -9.630549279050752e-5 0.0009276229513686864 -0.0031654850016100645; 0.0018714199836659278 0.0014961393647442598 -0.01116665955263791; -0.0004325910426692515 -8.925671686933951e-6 -0.00047057509304716273; -0.0023810250366923485 4.7854144692627406e-5 -0.002947892305270475; 0.0009519287836862896 0.001203003899662275 -0.006627483499534031; -0.0003379695576999979 0.0021397984754595867 -0.007889381374706862; 0.0018526182750906236 -0.0008398838594298359 -0.007098153471190913; 0.000982511656564293 0.00042728194833736724 -0.005108134717144937; 0.0011399004330542454 -0.00281128138769559 9.854296576216389e-6; 0.0023863161615499343 -0.0015367264302646917 -0.00818092195722848; -0.00019037693883326167 -0.0002503941653926727 0.00047563381079359594] %
+
+Mass Used: 88.17370407253293 kg
+Launch C3: 98.66915617690513 km²/s²
+||V∞_in||: 1.6990829006888156e-8 km/s
diff --git a/archive/ES_0.5689287949281379 b/archive/ES_0.5689287949281379
new file mode 100644
index 0000000..5e19ec7
--- /dev/null
+++ b/archive/ES_0.5689287949281379
@@ -0,0 +1,22 @@
+archive/ES_0.5689287949281379---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T05:32:30.342
+Launch V∞: [6.597764289254704, -7.428996184226874, -0.8531657000628299] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9320636419706683e-8, 1.1604332098490902e-8, -3.9182274356486714e-8] km/s
+ V∞_out: [-1.1901636709462946e-8, 2.7252633398941647e-8, 3.492674116391883e-8] km/s
+ time of flight: 1.8373980262655464e8 seconds
+ arrival date: 2029-02-24T20:22:32.342
+ thrust profile: [0.1518407920885105 -0.05302505734263 -0.06705060818911665; 0.0633519138559195 0.008958882765948313 -0.08556086488024885; 0.049231991975796995 0.016490821800760974 -0.113721962239095; 0.043221897896716155 0.01932294065859188 -0.14003078686294343; 0.03302878261193427 0.017674909909231838 -0.13816129962895; 0.027003299319755945 0.015839806920774593 -0.13665471457044573; 0.017864074959920134 0.011494781338555677 -0.10665644761328066; 0.013149018829863112 0.008048065484569954 -0.08001600480430279; 0.005861271645935425 0.0041299664590153055 -0.044965692784785724; 0.0015351049786154149 0.000816340850928569 -0.014034999653810777; -3.0308555004106958e-6 -0.0007763349569947255 -0.0017881372422006675; -0.00299758452983876 0.0005702322184138213 -0.0017588306479466645; 0.001815455070310826 0.0037942931154165494 0.0002214282113737363; -0.002191726313952453 -0.0016118521215129245 0.0029938650412929054; -0.0024335583588557487 0.0010427974469861421 0.0011133921565300731; -0.002609341204811144 0.0007540504323982882 0.0035461025988238228; -0.003775946515416642 0.00788738058125212 0.0026888972455046643; -0.0008001702872482465 -0.005083149081249314 -0.00253295976994264; -0.006290705526786121 0.005680424364476753 0.00606749992020791; 0.004332639694908898 0.0021551591527618702 0.00825317580659132] %
+
+Mass Used: 83.63477122024369 kg
+Launch C3: 99.4483696335858 km²/s²
+||V∞_in||: 5.029523702355614e-8 km/s
diff --git a/archive/ES_0.5689560569516849 b/archive/ES_0.5689560569516849
new file mode 100644
index 0000000..aebcfb0
--- /dev/null
+++ b/archive/ES_0.5689560569516849
@@ -0,0 +1,22 @@
+archive/ES_0.5689560569516849---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T22:45:00.573
+Launch V∞: [6.519136555467251, -7.563727224157491, 0.10708900328478926] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.9444950808667295e-9, -3.251470265697956e-9, 6.996607017070572e-9] km/s
+ V∞_out: [2.1368859496945247e-9, -5.048062219384749e-9, -6.33857279125631e-9] km/s
+ time of flight: 1.8251654669061634e8 seconds
+ arrival date: 2029-02-11T09:47:26.573
+ thrust profile: [0.11893363358208299 -0.03536626589209923 -0.044343074378430096; 0.029055125213289963 0.005471529211482607 -0.03260572436017174; 0.023466458914271075 0.010632849497868186 -0.04516595888513558; 0.033073714870871566 0.01950995591643123 -0.0850964852756114; 0.02563585409675598 0.018067384865716123 -0.08394980579291193; 0.013492771736758304 0.011085762806440382 -0.05516871316862589; 0.014462830650303486 0.011231126396680157 -0.0628420114374479; 0.008862521210907357 0.010252020646169641 -0.05872550646893535; 0.01729871074919841 0.017824550134623342 -0.0919349600583463; 0.051332655984620335 0.05550950876228554 -0.29006224588851803; 0.0009165085214541006 0.001033577403307281 -0.0023925949644656662; 0.01684609221060907 0.010488254442811122 -0.10124922505587987; -0.0019436884193089028 0.00040912658323861945 -0.004089027974445651; 0.0017679546263979107 0.0007543222639535621 -0.006813567666718412; 0.003972758107914651 -0.0006943509010277479 -0.0036603650951764996; 0.0005298572531569918 -0.0002895530820635579 -0.0019165913390300536; 0.0017673204558914133 -0.00043171295344117595 0.00039870219701613747; 0.0017771775216374533 -0.00067741601176319 0.0011700691142217425; -0.0016117349594769966 0.0021875058551147518 -0.005483221479205326; -0.0008712741303046673 -0.0006629167603281786 -0.004681605675465781] %
+
+Mass Used: 82.07868891496082 kg
+Launch C3: 99.72057900491514 km²/s²
+||V∞_in||: 8.665079923637226e-9 km/s
diff --git a/archive/ES_0.5689616373303492 b/archive/ES_0.5689616373303492
new file mode 100644
index 0000000..06f3250
--- /dev/null
+++ b/archive/ES_0.5689616373303492
@@ -0,0 +1,22 @@
+archive/ES_0.5689616373303492---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T18:40:29.654
+Launch V∞: [5.91432990522212, -7.770151805720462, -0.016068202884253646] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5699536296512479e-6, -8.556274444436644e-7, -1.4842281124308423e-6] km/s
+ V∞_out: [1.077634296039271e-6, -1.3849228002693236e-6, 1.5139435398139712e-6] km/s
+ time of flight: 1.6772829017437425e8 seconds
+ arrival date: 2028-08-19T01:51:59.654
+ thrust profile: [0.41076791871818036 -0.16610731645514884 -0.15773372315319212; 0.06835337069727512 0.008480013663474145 -0.07559882540401992; 0.07314619203853856 0.025974789266445433 -0.1292959930064224; 0.09006947839248536 0.04490343330578728 -0.21246531336457658; 0.06323272358443364 0.03905821096221938 -0.1884492637129352; 0.029123943677013615 0.02053721195565552 -0.10671311510275139; 0.011250684313890539 0.008345194993023443 -0.04850297859438684; 0.01524744674939264 0.012291612170899868 -0.07156617761528207; 0.02330300505720941 0.021180547058704136 -0.12043685347677674; 0.0022303305243793216 0.0020706426775807213 -0.011677275711359346; 0.0008224624958057498 0.0009886792452372107 -0.006878850626722388; 0.0021583912286080083 0.0029689202990388474 -0.011138356844031097; 0.004479456848962643 -0.0009455623414254898 -0.007462950800942306; -0.005737212899892878 -0.0028080755263095655 -0.00520143616576702; 0.004337308738599899 0.004347889252638121 -0.001757755893856479; -7.689305153050141e-5 0.0036442808913396993 -0.00679884764453941; -0.0010975661643305421 0.004891971893669984 0.0029730498812548566; 0.004730554329235746 -0.006610626701615822 -0.007952550791453225; 0.0015821993279750608 -0.0065204869554346505 0.0034637834454940017; 7.497140917915693e-5 0.000940698431024534 -0.00022687788294421113] %
+
+Mass Used: 107.5521531418849 kg
+Launch C3: 95.35481549888958 km²/s²
+||V∞_in||: 2.323743921491855e-6 km/s
diff --git a/archive/ES_0.5689891475646064 b/archive/ES_0.5689891475646064
new file mode 100644
index 0000000..7e92ed0
--- /dev/null
+++ b/archive/ES_0.5689891475646064
@@ -0,0 +1,22 @@
+archive/ES_0.5689891475646064---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T00:50:20.225
+Launch V∞: [6.279791506388169, -7.3059885990833395, -0.14690498732652862] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.6326646855708707e-8, -5.4894185143970367e-8, -3.710432516450652e-8] km/s
+ V∞_out: [1.7376694962791348e-8, -3.8676441582324696e-8, 5.80616496166433e-8] km/s
+ time of flight: 1.8749577781931672e8 seconds
+ arrival date: 2029-04-05T02:59:57.225
+ thrust profile: [0.4618313703182554 -0.09526347840680839 -0.11201703383403304; 0.19616915767295554 0.07862783822772422 -0.14074827704815987; 0.16739359867813483 0.1247019327807553 -0.19841294864811074; 0.06976722827963461 0.0734713715064445 -0.12732242878861338; 0.025877556777401108 0.035978040986728764 -0.07065646320647474; 0.021806596115972812 0.034476050889826575 -0.06920654428952981; 0.02225547982179026 0.04308386142773933 -0.0873408951181753; 0.012082446809996919 0.02512751122980977 -0.05151643162529636; 0.006177047130339015 0.016955100470101077 -0.03741058312875951; 0.006925581839741727 0.016809159400334076 -0.037749178954966434; 0.0029593248630093018 0.005391829983928791 -0.012537388633688083; 0.0009737728095915208 0.00258687144643483 -0.0011432529622115368; 0.0013604250403179137 -0.0008833933990099077 0.002386909141528293; 0.0008769103398717155 -0.0011761936561914127 0.002426228515048376; -0.00021552913219436256 0.002720544817462438 0.00031357779774610496; -0.00466420188544915 0.0005716526593970782 -0.0017894174971912356; -0.0017257484711059013 -0.0030009732105743215 -0.001882960374344983; 0.0024408731843227147 0.004377340530780942 -0.0004930926518580867; -0.0007443684289714981 -0.001394118084341927 0.0020200886134176363; 0.0002730229676638121 -1.8292989010565332e-5 -0.0009132863531567971] %
+
+Mass Used: 122.28415303987822 kg
+Launch C3: 92.83483184894214 km²/s²
+||V∞_in||: 7.556274068820757e-8 km/s
diff --git a/archive/ES_0.5689899100436812 b/archive/ES_0.5689899100436812
new file mode 100644
index 0000000..8ec1d9b
--- /dev/null
+++ b/archive/ES_0.5689899100436812
@@ -0,0 +1,22 @@
+archive/ES_0.5689899100436812---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T08:15:23.536
+Launch V∞: [6.233142792956231, -7.133491400747147, 0.40425615733868187] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.838229243664475e-7, -1.1828082363761214e-7, 1.5006310873468203e-7] km/s
+ V∞_out: [-7.96616796639096e-7, 7.181066373284951e-8, -8.410158822430628e-8] km/s
+ time of flight: 1.8749577787496114e8 seconds
+ arrival date: 2029-04-03T10:25:00.536
+ thrust profile: [0.7852433542042174 -0.16787916530840502 -0.18009998122121762; 0.21400875855744406 0.08087748233915253 -0.16115312178358893; 0.09263117554565868 0.06604910601139909 -0.12322073285250285; 0.09565118964921053 0.0921890986820352 -0.17382508920895712; 0.03719806667191489 0.045157586761380576 -0.0939075410236399; 0.01706063173581573 0.024389394773108287 -0.054624806272619356; 0.015087475412929973 0.02521661995486736 -0.058704602139458294; 0.006819157787332971 0.012815574785697524 -0.03128531154067952; 0.00948021884280246 0.020359539012279645 -0.051053509654981996; 0.0025071792742359603 0.0031821545614898507 -0.005114382582048007; 0.00021842822666226426 0.0007338467254935149 -0.0017084455667127781; 0.00030873342762061313 -0.0006034324268733811 -0.000349010497613946; 0.001210753420492105 0.004070983749098491 -0.0034279427705748667; -0.0026920110572660133 -0.0007872615734159471 -0.0023083881258596757; 0.002658646486255362 0.001195304816591414 0.0005418133675524892; -0.0018050804387781689 0.0011961078173494428 -0.0012192621649919954; 0.0024362109901419383 0.0050002453830115395 -0.002139009227419182; -0.0012235989037486122 -0.005139267891956827 -0.0017799515445401678; 9.2657912180403e-5 0.0004962853096092158 -0.0013858559648775863; 0.0026509629819115098 -0.0015766241697490783 -0.011921048267340747] %
+
+Mass Used: 139.3921102354334 kg
+Launch C3: 89.90219168266194 km²/s²
+||V∞_in||: 8.067760944685201e-7 km/s
diff --git a/archive/ES_0.5689992346177978 b/archive/ES_0.5689992346177978
new file mode 100644
index 0000000..a8813ff
--- /dev/null
+++ b/archive/ES_0.5689992346177978
@@ -0,0 +1,22 @@
+archive/ES_0.5689992346177978---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T22:52:33.878
+Launch V∞: [6.330191952609234, -7.458027728222551, 0.07476109975721659] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6875915149021276e-9, -1.3810587398723474e-9, 1.2630219283433741e-9] km/s
+ V∞_out: [6.870622722280913e-10, -1.5661128382815529e-9, -2.2917924237588824e-9] km/s
+ time of flight: 1.8569885728411016e8 seconds
+ arrival date: 2029-03-19T05:53:30.878
+ thrust profile: [0.33539934346461847 -0.08412837440033737 -0.11083706232653855; 0.14167087651929652 0.04117644039094412 -0.14400633631635876; 0.06873481563164782 0.03723874568606415 -0.1178527633548157; 0.04268437131048891 0.030127973110607165 -0.10795028279369866; 0.036159320370052705 0.037165507322455806 -0.12054955199263119; 0.02977400307697456 0.031568456149779815 -0.11537665756000173; 0.02863048485281059 0.034436373460682144 -0.12812905496336263; 0.01204993946676889 0.011492253834661955 -0.05171170800370318; 0.00393925636097173 0.0055623394692018635 -0.0152361156912661; 0.00034539674150826547 0.0015563884339760761 -0.003076675804994301; -0.0057662263087573246 0.009147155593083756 -0.007721011598428362; 0.00032538544592916016 0.0016783994812723181 -0.0004573829909997589; 0.009801447031905202 0.00637261178538969 0.0026614418005737397; 0.0012848614952385158 -0.003180236135687859 -0.002143787795776045; -0.0016404963111003976 0.00024947018317102165 -0.007396986701571611; -0.009567181813075865 -0.027828195120428213 -0.006369337687760973; 0.0023999524809451235 -0.0009161542986417994 0.005064879954940308; 0.0004776233660708719 -0.010773158260348041 0.005420836487639297; -0.033034788401952314 0.00027692919704723755 -0.02095009046854689; 0.0009487497399019156 -0.002512444283568379 0.0064190811977684874] %
+
+Mass Used: 105.58770803996049 kg
+Launch C3: 95.69909697385204 km²/s²
+||V∞_in||: 2.520022372048246e-9 km/s
diff --git a/archive/ES_0.5690723561325931 b/archive/ES_0.5690723561325931
new file mode 100644
index 0000000..e6c2d48
--- /dev/null
+++ b/archive/ES_0.5690723561325931
@@ -0,0 +1,22 @@
+archive/ES_0.5690723561325931---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T12:00:41.324
+Launch V∞: [6.546766864784345, -7.436845522839625, 0.018844932103833485] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006179578415198571, -0.0038638823376992743, 0.005426110783475571] km/s
+ V∞_out: [-0.0046096484819543, -0.0037649444255111373, -0.003047733412971212] km/s
+ time of flight: 1.874957778747981e8 seconds
+ arrival date: 2029-04-10T14:10:18.324
+ thrust profile: [0.20815958073799953 -0.05334871470502362 -0.0748422977247563; 0.04231508753203338 0.011061120395525738 -0.0456720954859353; 0.0765692257859871 0.038017704529970886 -0.13755054421841564; 0.03636811081868193 0.024877858016965883 -0.09202116200702765; 0.033981695095460014 0.028225087013112077 -0.1115330708358219; 0.0354294637205901 0.033186525627301566 -0.14137732544526352; 0.009068562760073009 0.009370052503407342 -0.042725399480350534; 0.004962404033475903 0.005621765860057406 -0.02766628064092326; 0.005229111863801521 0.006675288559430428 -0.03123787349377481; 0.014875988030444771 0.019296685332257233 -0.10165753163453042; 0.005155504276904354 0.006593890856936303 -0.031788559313738855; 0.00016305115549299554 -0.000523715260045819 -0.0008414579752410999; 0.0018506295972975538 -0.005110132469725345 -0.008943294604957021; -8.832496011880182e-6 -0.0017216992482630207 -0.010372004638729518; 0.008215211989223646 0.014882107981946413 -0.04324140938137759; 0.0011256275106929338 -0.0021119241464125616 -0.010397173183885581; -0.02069921749781929 0.012791414728597489 -0.02091951768627706; -0.007707892065228532 0.00754735242048873 -0.00981994678598283; 0.0010933370999008638 -0.0024017986914110293 0.003484417095344641; 0.009635181270013018 0.0034136749376343454 -0.02291187773114987] %
+
+Mass Used: 91.27584889870195 kg
+Launch C3: 98.167182843884 km²/s²
+||V∞_in||: 0.0066898532755233255 km/s
diff --git a/archive/ES_0.5691138437207974 b/archive/ES_0.5691138437207974
new file mode 100644
index 0000000..fc0b03d
--- /dev/null
+++ b/archive/ES_0.5691138437207974
@@ -0,0 +1,22 @@
+archive/ES_0.5691138437207974---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T12:07:07.407
+Launch V∞: [5.830319879467176, -7.688838012455938, 0.057315199610637683] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.47350873415839e-6, 0.0005054775227450788, -0.00022086763315845492] km/s
+ V∞_out: [-0.0004454978202007234, -0.000253774611472599, 0.00020331816183176] km/s
+ time of flight: 1.704047782715015e8 seconds
+ arrival date: 2028-09-18T18:46:45.407
+ thrust profile: [0.5454001091751112 -0.20346007688826703 -0.18109891269210765; 0.13486615605660518 0.02233968454087501 -0.1357525800517044; 0.10815848508847876 0.045405746606289085 -0.17716859684359312; 0.060489029125372205 0.035108054526191666 -0.1392222201400893; 0.051500095573973066 0.03677565413102311 -0.14964961758876344; 0.03490713973515141 0.02888759689668386 -0.12270247659525409; 0.0306130554064843 0.028165549406493972 -0.12481926789508273; 0.011853005196035191 0.012138881475341302 -0.055845656415175526; 0.007444682876097403 0.008407290021050161 -0.039696794473273955; 0.00033002266887658467 0.0008841750738198844 -0.005050178059387766; 0.0029186736280634997 0.003047340806466854 -0.018111797805480986; -0.002011559885596417 -0.0004266918694903097 -0.003493985454291319; 0.0032528632760700587 -0.005007669633190055 0.0004915284438832455; -0.001440568088257124 -0.0019376531807611518 0.007661588755606922; -0.005378824257783216 0.004389314161438548 0.0012717021768081649; 0.0019244403020638786 0.003479767625550745 0.0009651576632034893; -0.0010452059416256499 -0.0028566388075629036 0.005785155344164788; 0.0033236974766494985 0.004146953386384875 0.0014056429694442227; 0.004963535291413884 -0.011886735961127992 0.0067263739939463375; -0.0014170119055501454 0.003943542563221577 -0.003914305519697967] %
+
+Mass Used: 120.80030569457404 kg
+Launch C3: 93.11414491080393 km²/s²
+||V∞_in||: 0.0005516268744409659 km/s
diff --git a/archive/ES_0.5691178405287219 b/archive/ES_0.5691178405287219
new file mode 100644
index 0000000..e13dc1b
--- /dev/null
+++ b/archive/ES_0.5691178405287219
@@ -0,0 +1,22 @@
+archive/ES_0.5691178405287219---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T07:01:59.178
+Launch V∞: [7.872953883190636, -5.797179067919158, -0.011544465733657217] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5331284929392287e-7, -5.0465413329402e-7, -1.4725009705141363e-6] km/s
+ V∞_out: [-1.4163367511662236e-6, -1.6691568377202214e-7, 6.400081068150122e-7] km/s
+ time of flight: 1.8449497210310137e8 seconds
+ arrival date: 2030-03-17T15:38:11.178
+ thrust profile: [0.35187514816920806 0.003408652937997734 -0.08928710479588584; 0.08461976210224494 0.0538300589761766 -0.07716549943456684; 0.06533931085157318 0.06869047574592956 -0.10604664781467388; 0.056288917484704416 0.07934232855844674 -0.13409178005245576; 0.024361984214101576 0.04705173993339269 -0.08984702993724715; 0.018145482442098078 0.037937614709282044 -0.07786255402665908; 0.013048153883584386 0.033808520781284324 -0.0720809566105572; 0.010378684033298027 0.032366230161160706 -0.0747860256552136; 0.004855843181701529 0.010159949466653195 -0.030426009620302733; -0.0017008098709659408 0.007117473667830384 -0.018748127913671808; 0.0004848687405949547 0.00014264971255266383 -0.0010418074867983135; 0.002614983312101994 0.002138576382654519 -0.004851958748886066; 0.006065035585144775 0.01899276013511988 -0.01844358935580173; -0.004838292092969578 0.008581925308531097 -0.004794398240383498; -0.014034931492036839 0.0024675784104055383 0.001338280973615808; -0.018362779162438784 0.010877591447354552 -0.040237284187651844; 0.014508352049113368 0.018976339646796132 -0.02942165384967719; 0.0011983994058805238 0.004619764357683884 -0.024255560361670522; 0.0076416908711631135 0.00626600242277872 -0.02917992872788811; -0.0034116658597251083 0.009562200745894494 -0.04239156546713871] %
+
+Mass Used: 106.35768989235112 kg
+Launch C3: 95.59082126705563 km²/s²
+||V∞_in||: 1.5641098849423697e-6 km/s
diff --git a/archive/ES_0.5691216795841247 b/archive/ES_0.5691216795841247
new file mode 100644
index 0000000..3ee406a
--- /dev/null
+++ b/archive/ES_0.5691216795841247
@@ -0,0 +1,22 @@
+archive/ES_0.5691216795841247---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T01:34:01.685
+Launch V∞: [7.586121681757784, -5.673708693466104, 0.2495578052853371] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.989332933236371e-9, -1.2345672827582336e-8, -6.405870300150816e-10] km/s
+ V∞_out: [-3.1231935272071856e-9, -6.307273657035748e-9, -1.611350379354982e-10] km/s
+ time of flight: 1.8749577787419757e8 seconds
+ arrival date: 2030-04-17T03:43:38.685
+ thrust profile: [0.6109819521302504 0.025534071892235912 -0.11465758661021362; 0.3740312738138105 0.26617078801551064 -0.2471428125409568; 0.13497147164440457 0.167751727679526 -0.17115325936460615; 0.039724283808557935 0.06881034980799278 -0.08216573705405675; 0.02421835711044513 0.056224293846734275 -0.07311834540123165; 0.010207646518237712 0.03112827086931695 -0.042758586747509014; 0.0026418703855827634 0.012150798196064558 -0.02001766381670984; -0.000361329024850938 0.00457980609481017 -0.009193860823889273; 0.005124981548565721 0.03390772172386823 -0.053405799296012725; 0.0022643297665100627 0.009516575714512468 -0.015552584365754797; -5.3411854874520735e-6 0.0042823126986987654 -0.010700708481960414; -0.00570744073440731 0.0070066068838113066 -0.0029774460572453095; -0.0015263537974226696 -0.0016727388431582424 -0.0022650729227874904; 0.0005562696852096482 0.002942258314942247 -0.005480436010758773; -0.005942827931283114 0.001900019848941302 -0.0035974323979312134; -9.310761431028346e-5 -0.00032951836826180733 -0.00024786801471351864; 0.008562616428276031 0.00268130910256552 -0.003864636801484159; 9.6335034967766e-6 0.0015752765636466437 -0.000856578428756586; -0.0011503109068617397 -0.006592720758139198 0.003908879917310979; -0.013269175701290577 0.006754463801227994 -0.015748448495099293] %
+
+Mass Used: 140.12742514107003 kg
+Launch C3: 89.80249160692722 km²/s²
+||V∞_in||: 1.2990025656669532e-8 km/s
diff --git a/archive/ES_0.5691286456593836 b/archive/ES_0.5691286456593836
new file mode 100644
index 0000000..2466ea8
--- /dev/null
+++ b/archive/ES_0.5691286456593836
@@ -0,0 +1,22 @@
+archive/ES_0.5691286456593836---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T02:22:31.591
+Launch V∞: [7.283557388348158, -6.72433785804046, -0.5832111402121587] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00011235353668070706, -0.007349628598103895, 2.8901919708498016e-5] km/s
+ V∞_out: [-0.007122639786698971, 0.0011379689501310195, -0.0015011591758155656] km/s
+ time of flight: 1.544672447147006e8 seconds
+ arrival date: 2029-04-01T21:56:35.591
+ thrust profile: [0.25272089486120836 -0.06774727533564147 -0.11540936367495201; 0.07325822763989764 0.014218665486474998 -0.09583316456264099; 0.06916902094042503 0.02733048815319528 -0.15041759876882538; 0.07707178835123243 0.03988086906721321 -0.2296939431965247; 0.05562093064420631 0.033356974517732674 -0.21050323742389743; 0.029965001892957054 0.019518528573608987 -0.13776013627790357; 0.021065862321139196 0.014562899456879838 -0.11199883381897241; 0.008522084305273533 0.006070872758606323 -0.051676337581407314; 0.00981161769038692 0.007287723974547547 -0.06507431576918493; 0.000628802347786141 0.00038111444499233215 -0.004146981869518859; 0.0010133834546241383 0.0007861071695692894 -0.007556442910972252; 0.000369185899499294 0.00029447684389114447 -0.0028157192832474883; 2.5073190641419394e-5 0.0006475408327779324 -0.003541830171901964; -0.0010060403019095435 -0.00046195934538819413 -0.0014835134148480603; -0.00017639700009933727 0.0001551888731157587 -0.001214693136801961; -1.78651937608066e-5 -0.0001568979219024446 -0.0005324820819597004; -9.719196318111608e-6 0.0003017382906567923 -8.55066704147342e-5; 0.00026807845127946783 0.0002940334219324642 -0.0006621119510777909; -0.00018302969065898364 -0.00022928260832666273 0.0022423994287971935; 4.354681196610329e-6 -0.0003858887871059217 0.0007226103009695115] %
+
+Mass Used: 88.77555189633631 kg
+Launch C3: 98.60706309250477 km²/s²
+||V∞_in||: 0.007350544140962227 km/s
diff --git a/archive/ES_0.5691295707467039 b/archive/ES_0.5691295707467039
new file mode 100644
index 0000000..a4b18d3
--- /dev/null
+++ b/archive/ES_0.5691295707467039
@@ -0,0 +1,22 @@
+archive/ES_0.5691295707467039---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T17:24:33.736
+Launch V∞: [6.3944978140925235, -7.198076723011526, 0.2297214806160309] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.4590602229958415e-6, 4.309167694785161e-6, 4.797988215088781e-6] km/s
+ V∞_out: [6.605844039009152e-6, 4.222616208821333e-6, 1.274840149350375e-7] km/s
+ time of flight: 1.8749577787457055e8 seconds
+ arrival date: 2029-04-05T19:34:10.736
+ thrust profile: [0.593783162413884 -0.13123800687145798 -0.1630327073552332; 0.1502663015952485 0.05291789453751384 -0.13236143636558134; 0.06919561113973711 0.04583845642332943 -0.10621088190847777; 0.04506895092533251 0.04082791482794793 -0.09902753811165141; 0.04052413984463033 0.04530247739684379 -0.11433322873919163; 0.014841746093434457 0.01983797481668888 -0.05470857278368566; 0.023850280346709295 0.03615797896216458 -0.09903144435783219; 0.013700501372903294 0.023432921868846147 -0.06909449288868133; 0.0048810008618882985 0.009767927874542646 -0.025847210934640888; 0.0032156326364928683 0.010828852119423691 -0.0361834176491029; 0.00477871411839063 0.010321751561354819 -0.032773121363341706; 0.0002887245651962923 0.0021918212301770034 -0.013971821956762647; -0.0032962854813012024 0.003155205961910339 0.0011944143109680321; 0.0015439087462717448 -0.004576612277295737 0.0011435301544760901; 0.00704927134171463 0.0007919077952052092 0.0004815973780429982; -0.00642273545661668 -0.011213988990909715 -0.007718539019086484; 0.008841726230898862 0.007809918201215733 0.002811696549765498; 0.0007169531379334282 -0.00010059202275539266 -0.003204521561311862; 0.0031443139007960304 0.005453598594297639 -0.006379426362556097; -0.0054152077508031644 -0.005847018701761651 0.013589410548809043] %
+
+Mass Used: 122.91551641769138 kg
+Launch C3: 92.75468276345083 km²/s²
+||V∞_in||: 7.840461415389696e-6 km/s
diff --git a/archive/ES_0.5691316134738685 b/archive/ES_0.5691316134738685
new file mode 100644
index 0000000..e0cb7e7
--- /dev/null
+++ b/archive/ES_0.5691316134738685
@@ -0,0 +1,22 @@
+archive/ES_0.5691316134738685---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T15:36:46.395
+Launch V∞: [7.469972996014116, -5.6696115499956985, 0.26088521400810866] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.732059400132482e-10, 2.0879475065344882e-9, -1.7688104324235723e-9] km/s
+ V∞_out: [1.3220160578542618e-9, 2.749820393290372e-9, 7.269961291225039e-11] km/s
+ time of flight: 1.8589192482512552e8 seconds
+ arrival date: 2030-03-28T04:15:30.395
+ thrust profile: [0.872204299276797 -0.008207962851976534 -0.11879393278662184; 0.2516979175548021 0.18837865821632208 -0.14957840192784255; 0.09981290896697591 0.12956393925182783 -0.12060118698855309; 0.05776309658469121 0.10340726744242228 -0.10529209612105182; 0.040860655625884534 0.10162692479181673 -0.1166813745242487; 0.019099944782643527 0.05361648692439728 -0.06406243586692992; 0.007929853680101203 0.02784044109998003 -0.037035491545132; 0.005202087173842463 0.031000536291671606 -0.041334099098319275; 0.00645582142291799 0.05054590997263296 -0.06921951676754463; 2.5800860479372424e-5 0.0013646395026069413 -0.0018168593034506918; 0.0003349167554623437 0.0013966824143738514 -0.002396475377686039; -0.00012887230113656028 0.0009768485072389494 -0.001845197867246508; -4.939903052249544e-6 0.000429684038685793 -0.0007407631909681987; 0.00014410779910819117 0.0003500051096837183 -0.0006484634585540207; 0.00036969548601010127 3.459322019974242e-5 -0.001012380498647872; -0.0002265694614539777 0.0006102696985407531 -0.0011810473671327371; -0.00017687140529796272 -0.00027306032887008567 -0.0006344728864839254; 6.79296897729221e-5 0.00016926465143210398 -0.0002948424467580416; 0.00018461504781358597 -0.00021020570303426317 0.00032809413996665775; -0.0001619176487103894 -0.00037997713132573076 0.0007134003984820324] %
+
+Mass Used: 150.57740781335542 kg
+Launch C3: 88.01305278391278 km²/s²
+||V∞_in||: 2.818052762735853e-9 km/s
diff --git a/archive/ES_0.5691634930656995 b/archive/ES_0.5691634930656995
new file mode 100644
index 0000000..5527078
--- /dev/null
+++ b/archive/ES_0.5691634930656995
@@ -0,0 +1,22 @@
+archive/ES_0.5691634930656995---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T22:09:47.233
+Launch V∞: [7.258176623512393, -6.707522017129237, -0.33739590199862163] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.177482604156834e-6, 6.814486547129813e-6, 3.4844656560954634e-6] km/s
+ V∞_out: [5.389228469950306e-6, -5.016361298441931e-6, -3.0170107586759246e-6] km/s
+ time of flight: 1.5419716701601714e8 seconds
+ arrival date: 2029-03-29T14:42:34.233
+ thrust profile: [0.32646672448336284 -0.09193289670320408 -0.14690469473055603; 0.051909429176406695 0.008921076164389362 -0.06708341490561522; 0.09474005087150209 0.03436408583546494 -0.200215596597357; 0.055116725673533276 0.025718274953350054 -0.1622237085383326; 0.05507635618618761 0.029551888628533016 -0.2034598852148481; 0.0361414954191697 0.020950940683137707 -0.1596130369422236; 0.025800549764934434 0.01570187375549111 -0.13117449750239485; 0.016424672873717322 0.01016892113021867 -0.09404624408264078; 0.007426868319811046 0.004599655569299987 -0.048507661101073615; 0.0007172059205739071 0.0005650121662733799 -0.005044157872881189; 0.0005132728080993004 0.00027623279724658495 -0.0035530527845568233; -5.2252414321295616e-5 -1.892002937517974e-5 -9.757881389125736e-5; 3.148380701912521e-5 4.7358770244629e-5 -0.0002608927346116742; -0.00021164223215124555 0.000613199468690146 -0.0003978284663663759; -5.191795801383478e-5 -0.0006732477410523749 -0.000834835952518109; 0.00019345687696705293 -2.4859400662562278e-5 -0.0006110925924232293; 0.00026483203751054545 0.00028722009261764395 -0.00038540548052798515; 0.0002530947345479563 -0.0007244877519597352 8.582570332965069e-5; -0.0001974884063600511 -0.00014215702899206777 -0.0011237643967613384; -0.0002325342980819575 -0.0001437771593008028 -0.0003592926058369828] %
+
+Mass Used: 93.60681814212876 kg
+Launch C3: 97.78581550306068 km²/s²
+||V∞_in||: 7.957396452416306e-6 km/s
diff --git a/archive/ES_0.5691844366611248 b/archive/ES_0.5691844366611248
new file mode 100644
index 0000000..75e54d4
--- /dev/null
+++ b/archive/ES_0.5691844366611248
@@ -0,0 +1,22 @@
+archive/ES_0.5691844366611248---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:50:28.018
+Launch V∞: [6.411993404405433, -7.47913015845817, 0.11883974317895875] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.6875743794187734e-7, 2.6453074125796912e-6, -1.6131565080593566e-7] km/s
+ V∞_out: [1.0372617867526719e-6, -2.0701054009588794e-6, 1.3433488500551555e-6] km/s
+ time of flight: 1.8489817666661072e8 seconds
+ arrival date: 2029-03-10T15:26:44.018
+ thrust profile: [0.3046201662253757 -0.08752523477047035 -0.10779214317720932; 0.048129936263923145 0.01175143252871179 -0.05405289544819039; 0.03665720586944591 0.018853568085453257 -0.07137799592913836; 0.0420744893838567 0.02823367814607561 -0.11099235540377887; 0.042007960325646486 0.03461255877837916 -0.13722623122700303; 0.03394063582188981 0.03169806334014535 -0.13357887354460482; 0.020024735771369498 0.021730387273670743 -0.09794715128870515; 0.015404133956854242 0.016027099717147077 -0.08152400433298264; 0.009142371208176256 0.012948684052290377 -0.05680530490912398; 0.007714519263517643 0.0003347759078908591 -0.02455387055081979; 0.003946025391346817 0.004835905997438236 -0.03264134799844068; -0.007696829347529368 0.0029474422753697003 -0.011010554546941104; 0.0007606371438034988 -0.0008223638399740968 0.002184356851131636; 0.006289471882877906 -0.010405252229620413 0.004579001863191563; 0.0022632502569862292 0.0160249953817033 0.0029163093566804644; -0.005967407901013338 0.00915259917254559 0.00304606509494331; -0.0009270908988022932 0.0018803037718024289 -0.0049561628226876785; -0.017047862024098092 0.004056574372436323 -0.024558417265444457; -0.019469064634695513 0.01386684668201837 -0.011945935347802488; -0.00240242025684416 0.0013250887548874842 0.0017152907476504445] %
+
+Mass Used: 97.83501643048476 kg
+Launch C3: 97.06517022985615 km²/s²
+||V∞_in||: 2.6757533694796053e-6 km/s
diff --git a/archive/ES_0.5691974152252376 b/archive/ES_0.5691974152252376
new file mode 100644
index 0000000..4c586ff
--- /dev/null
+++ b/archive/ES_0.5691974152252376
@@ -0,0 +1,22 @@
+archive/ES_0.5691974152252376---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T11:50:50.672
+Launch V∞: [6.48595834379541, -7.162659714242978, 0.2817561589720335] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.085865445852534e-6, 9.070146203401848e-7, -1.9179682710623544e-8] km/s
+ V∞_out: [-1.1481589392832077e-6, 2.4469483231829428e-8, 7.046652184253618e-6] km/s
+ time of flight: 1.8749577787484106e8 seconds
+ arrival date: 2029-04-03T14:00:27.672
+ thrust profile: [0.4753142741942069 -0.10392810646283035 -0.11910573064649027; 0.19767864627357712 0.07163699021962587 -0.14906743354052746; 0.12220581820941477 0.08293375144982629 -0.15483854550779688; 0.12708311097623975 0.12047942953743933 -0.22789467695992774; 0.050317873430506366 0.0573956479185269 -0.11665220988382427; 0.02067176878566197 0.027835018483173893 -0.05932573483453519; 0.002602708707543901 0.005081316573012023 -0.008873746777646442; 0.0023253262518194906 0.004748623408197036 -0.01062554264068657; 0.0029532899945611452 0.006553929098261729 -0.016220088670651268; 0.005116770330014968 0.01027220690080213 -0.02631217692832446; 0.0018394424056426876 0.005491681651934749 -0.014060563088887921; 0.0005845891382727033 0.0038030435857277713 -0.00730713648684453; 0.0027059267057845462 0.0036019600886145735 -0.006719800325500809; 0.00014135924771974958 -0.0017085454928502213 0.00017892312479038603; -0.0012596405673185244 -0.002295824787899814 0.00036957909962462884; -0.0018084272647176406 0.0032518516559000427 -0.004418893382606451; 0.0043054207290094924 -0.002017133808858527 -0.002131824514024306; 0.00020555101296078533 -0.0007219237074641369 -0.001971909656171925; -0.00036650160985918234 -0.0013973986697103597 0.0038987331881679427; 0.0008223540703545284 0.0008227505633805296 -0.0025833121751082273] %
+
+Mass Used: 118.93435570590145 kg
+Launch C3: 93.45073635260728 km²/s²
+||V∞_in||: 7.143705795906398e-6 km/s
diff --git a/archive/ES_0.5692165857713638 b/archive/ES_0.5692165857713638
new file mode 100644
index 0000000..e4a6ba3
--- /dev/null
+++ b/archive/ES_0.5692165857713638
@@ -0,0 +1,22 @@
+archive/ES_0.5692165857713638---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T11:50:01.005
+Launch V∞: [7.263808670007072, -5.973454731017526, 0.4484831952465809] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.310492760203633e-9, 3.959969962267182e-8, -9.77248840903544e-7] km/s
+ V∞_out: [-4.0202967688074455e-8, 9.61708844891315e-7, -7.507937010090007e-9] km/s
+ time of flight: 1.7453043377939332e8 seconds
+ arrival date: 2029-11-15T12:30:34.005
+ thrust profile: [0.8961857789017783 -0.03026644547054147 -0.15986294513067598; 0.24186894950044338 0.14458077398875702 -0.1639841230192362; 0.1180129487431644 0.12039691987341353 -0.14920983233214524; 0.058008630864315944 0.08078882312928276 -0.11255082490994711; 0.04096807646832311 0.07325892453712708 -0.10886192806903267; 0.026062624825890793 0.055696239697415856 -0.08911800424279472; 0.0177449437627046 0.04542761628557425 -0.07664739600520962; 0.009676122410082234 0.02823729712992192 -0.05003608353305512; 0.006516701064747174 0.02318130519622163 -0.04127963988691634; 0.00036923322527717697 0.004604711725688104 -0.012038419157452896; 0.0005128353270180454 0.005233414245690803 -0.0116678596493428; 0.00013381117025946366 0.0017771047166889923 -0.005921046955698188; -0.00043138148003111446 0.0038777375388152954 -0.0015992311536537434; -0.0003786537406120045 -0.00027039006573769547 0.00282234892851118; 0.0023887288340771447 0.0016405894404924906 -0.0031234646923067426; 0.005053796773556612 0.0010752704247682999 -0.00017485851035871965; 0.0005307702407361028 0.0015886532182561525 -0.002640895228512138; 0.00033541660449936224 0.0019505289233724228 0.0012394466231255927; 0.0010552413142514352 -0.004566734343840237 -0.001219518837604861; 2.8502177841564445e-5 0.001091311027294109 -0.0009522981434651074] %
+
+Mass Used: 146.9830959325668 kg
+Launch C3: 88.64621499440416 km²/s²
+||V∞_in||: 9.780711914663486e-7 km/s
diff --git a/archive/ES_0.5692245955522779 b/archive/ES_0.5692245955522779
new file mode 100644
index 0000000..506f257
--- /dev/null
+++ b/archive/ES_0.5692245955522779
@@ -0,0 +1,22 @@
+archive/ES_0.5692245955522779---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T22:42:59.002
+Launch V∞: [6.302660819186842, -7.323785275318161, 0.10100575885748073] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4220880780898174e-9, -1.8783800245140354e-9, 1.977176088141924e-9] km/s
+ V∞_out: [1.0379305126586378e-9, -2.4764543082394987e-9, -3.3663852669345743e-9] km/s
+ time of flight: 1.8498573042843005e8 seconds
+ arrival date: 2029-03-05T23:38:29.002
+ thrust profile: [0.43916184743362 -0.09256517758512112 -0.10179457500371286; 0.20371651182608402 0.07874652203891497 -0.14595711092477912; 0.13900944904520163 0.09949949844807449 -0.16688454762778313; 0.056102109135445284 0.05731347483121057 -0.0989998163450096; 0.05501152720035579 0.0686054943635022 -0.1252851254830365; 0.04008081761862027 0.05981566856247244 -0.11661121548151437; 0.028456496608770088 0.05121151112638905 -0.10369104317887502; 0.006314996837656692 0.011110147153315493 -0.026331092203026003; 0.004145857747963793 0.008346687255357317 -0.017729459860397413; 0.0047877883520989675 0.010889211445958589 -0.02418275580570678; 0.0006548539145143323 0.0020970205425244323 -0.005270175690621779; -0.0008401170832323469 0.0005728802587261995 -0.003167123572042921; -0.002873440269972392 -0.002828083717646756 -0.002224623775788341; 0.0037258198664175666 0.0006961373109348294 -0.0013595009944662615; -0.0005993465978974388 0.0012282402328139938 -0.0002542228960205487; -0.0010652913981403856 0.0012531961664738228 -0.0023897564238719096; -0.0015404182250266416 0.005550951275154422 0.003324258916228764; -0.0013241580539837272 0.002726970793606556 -0.0010798272463270766; -0.0004340997203792769 -0.0013081125582015125 0.003521003296213258; -0.0012918510709004443 -0.001695036167681696 0.010861107335593374] %
+
+Mass Used: 119.42789125431 kg
+Launch C3: 93.37156632400244 km²/s²
+||V∞_in||: 3.647471378645537e-9 km/s
diff --git a/archive/ES_0.5692256656303389 b/archive/ES_0.5692256656303389
new file mode 100644
index 0000000..c089101
--- /dev/null
+++ b/archive/ES_0.5692256656303389
@@ -0,0 +1,22 @@
+archive/ES_0.5692256656303389---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T06:05:31.538
+Launch V∞: [6.680546812979104, -7.162772243463131, 0.2722836753500178] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.1328030579687496e-8, 4.9381663746382484e-8, 3.381411341193035e-8] km/s
+ V∞_out: [-2.158642822879228e-8, 4.506919525528456e-8, -4.6178746713735245e-8] km/s
+ time of flight: 1.8749577787484002e8 seconds
+ arrival date: 2029-04-05T08:15:08.538
+ thrust profile: [0.37517992056932625 -0.08421216066461282 -0.10325319088047422; 0.09421285260372156 0.03419449644726642 -0.08424041713423121; 0.09506457464917197 0.06371943839051811 -0.13989870300870969; 0.05430407675086123 0.05000310005760578 -0.11489738468636863; 0.026913668361163504 0.03088120925581708 -0.07601681676229424; 0.01788055897638759 0.024560353798129465 -0.06217456025379633; 0.024766846119865 0.0392082735146498 -0.10464408756779874; 0.02302478232902358 0.04028396407313864 -0.11022154400784634; 0.008773828566916175 0.017532342436077847 -0.049241392060404454; 0.0030431291160792845 0.006711117508839154 -0.019233441638897102; 0.0027054652535506486 0.007105091217335423 -0.024648592024531964; -0.0045885089913853695 -0.0019651076579180254 -0.008755090956050017; 6.087126627338159e-5 0.0008043251216070836 -0.003902531602262507; 0.00013375559968083802 -0.005519996861994213 -0.0033388444713886413; -2.4034748322698492e-5 0.0028769914255011757 0.006184837885815074; -0.003635598394741804 0.0041556029070532125 -0.002090717600090453; 0.002999758886226193 -0.0012639344204877188 0.004440351576483375; 0.0019466458775941622 0.0002448477309785155 -0.0008748274528346351; -0.0009896409326141037 -0.002962058572823561 0.008999999577279953; 0.0010989447114594455 0.005893297371961873 -0.004970364300509774] %
+
+Mass Used: 104.04323296543498 kg
+Launch C3: 96.00915033199323 km²/s²
+||V∞_in||: 6.755285693586548e-8 km/s
diff --git a/archive/ES_0.569227238659475 b/archive/ES_0.569227238659475
new file mode 100644
index 0000000..c4a024e
--- /dev/null
+++ b/archive/ES_0.569227238659475
@@ -0,0 +1,22 @@
+archive/ES_0.569227238659475---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T04:58:14.904
+Launch V∞: [5.8492053863515165, -7.88189005357563, -0.23736664169842148] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.773900597999023e-9, 1.256363498064346e-9, 1.0756380205540839e-8] km/s
+ V∞_out: [-5.976511205961534e-9, -8.486454196870748e-9, -4.304654665329195e-9] km/s
+ time of flight: 1.7005681693787822e8 seconds
+ arrival date: 2028-09-17T10:58:30.904
+ thrust profile: [0.33580701238644883 -0.12629290178049943 -0.13270034465031502; 0.09044915908036912 0.012434452443224922 -0.10069151973901742; 0.04682461898789654 0.017717839848566144 -0.08779289476699893; 0.07838301959165377 0.039704580211721 -0.19292619010674789; 0.041808578736975854 0.02686545317536358 -0.13306046058983315; 0.042322716438675634 0.03043166784774171 -0.15873477824179846; 0.03328705557797094 0.029657138137885494 -0.14101227031110145; 0.012663833387959381 0.01139831465814034 -0.06552489548898632; 0.012707269447138427 0.00874362483192584 -0.06523644470235625; 0.0013795231760544559 0.0016176379914235534 -0.009253857493147295; 0.0018447544813402447 -0.0007547104206831988 -0.014171384531006113; 0.0018619127082182033 0.001417086758313066 -0.0003298234427502357; -0.001305549319958085 -0.0006073716503445882 0.002929897679576799; 0.005807306918135122 0.0001893748094854803 0.0020984094328408524; 0.0012590507600025993 0.00020497355897760553 -0.004891512251130779; 0.0046434126945883725 -0.009157191952301977 0.004645917200241793; -0.0069412134508655896 0.016751243804783628 0.0020750687115370326; 0.0008015504627743946 0.0006074308310341401 -0.0024376919207680188; 0.0017273250195114149 0.0031994000251186856 0.0008147127307752593; -0.0016699761523934886 -0.0005956655588648114 -0.0031177059457668027] %
+
+Mass Used: 101.80164365540031 kg
+Launch C3: 96.39373739096924 km²/s²
+||V∞_in||: 1.0973827395079648e-8 km/s
diff --git a/archive/ES_0.5692274294701987 b/archive/ES_0.5692274294701987
new file mode 100644
index 0000000..a9669dd
--- /dev/null
+++ b/archive/ES_0.5692274294701987
@@ -0,0 +1,22 @@
+archive/ES_0.5692274294701987---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T18:00:30.226
+Launch V∞: [5.879216372570344, -7.943916255826492, -0.3233479025883626] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.164383279547538e-6, 4.626546333284006e-6, -3.80672889088562e-6] km/s
+ V∞_out: [5.002907988595841e-6, -6.908519736974336e-6, 5.4599442495314496e-6] km/s
+ time of flight: 1.6253591314860234e8 seconds
+ arrival date: 2028-06-19T22:52:23.226
+ thrust profile: [0.20606054122408018 -0.09325762839597644 -0.09017997338055174; 0.10751246783394311 0.0071457224782836325 -0.12347038509877471; 0.07705334328280297 0.01997589246809753 -0.13906207286395647; 0.07382581906874523 0.02830110849241976 -0.17868731615579683; 0.057613556986202887 0.02722759553843117 -0.17287890432522604; 0.02887997430949405 0.0165445935569473 -0.10786280062642532; 0.04106501482996961 0.028506864656494678 -0.17143679420149743; 0.031766778866714404 0.02113196900132422 -0.15381777356751078; 0.0014847249674738345 0.0017329609021494122 -0.009515408771609352; 0.0024039502427092717 0.0007904328545514494 -0.012148174665018163; 0.0006625676134345461 0.0002928534979637201 -0.004209338163359366; 0.00016720711394106882 -0.0001975348691009229 -0.0012413931260675673; 0.0020963765459810673 -0.00037915048051657615 -0.004885769175058897; 0.0002949672637743959 -0.00033750504465040906 -0.0009451213412568608; -9.068281570328078e-5 0.0013788255615222258 -0.0008064921510724625; -0.0011037446945433974 -0.00029841116427341984 -0.0005278978529528728; -0.005016949414454361 0.0018478268722201213 -0.0026802615945655537; 0.001156237778311854 0.003956669248562429 -0.0014849845371758307; 6.342231663145207e-5 0.0025261404031496205 0.0002894318534765163; 0.0002960035126064049 -0.0012624513267019879 -0.00035949459940685545] %
+
+Mass Used: 93.74132479161244 kg
+Launch C3: 97.77554450119189 km²/s²
+||V∞_in||: 1.0126858849519053e-5 km/s
diff --git a/archive/ES_0.5692513711755627 b/archive/ES_0.5692513711755627
new file mode 100644
index 0000000..3bd90e0
--- /dev/null
+++ b/archive/ES_0.5692513711755627
@@ -0,0 +1,22 @@
+archive/ES_0.5692513711755627---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T16:49:01.855
+Launch V∞: [5.937451918127766, -7.570162563705861, -0.7677535141172369] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.341080822636657e-8, -5.3503828128996896e-8, -7.987099667318609e-8] km/s
+ V∞_out: [4.032513907950651e-8, -6.36681376257002e-8, 1.0672589468473879e-7] km/s
+ time of flight: 1.781187793968394e8 seconds
+ arrival date: 2028-12-18T06:15:20.855
+ thrust profile: [0.5407646071145349 -0.16659957240102788 -0.15633106575088795; 0.16354459202205995 0.050093389605903926 -0.14934250634923155; 0.06400787277165769 0.038183988741546965 -0.10014057225879563; 0.07423990332112383 0.06189475046906031 -0.1553725071089696; 0.052476235522137295 0.05442088787775859 -0.1424061711616853; 0.025922385493736044 0.03026471110144073 -0.08800332250415613; 0.018389193485294233 0.024698245351059255 -0.07371731672633365; 0.016791551979922804 0.026867521907569084 -0.07983429552259322; 0.0070355159984163956 0.01236768799244874 -0.03757836953731133; 0.00971798483517548 0.015567106966100095 -0.051678414238588516; 0.0037517559770404154 0.007910144071976138 -0.02701308637456469; 0.0012738286568488044 -0.0008785835795091608 -0.0014200101832062733; -0.0014112480835707548 -0.0008075547869730759 -0.002714734064712453; -0.0012231443722408547 0.00042119471917661925 -0.0042182037792661276; 4.1013864156516644e-5 0.0012882873536301806 -0.0024736628330529493; 0.0004570974545297999 0.0055499298010370755 -0.005379728829538609; -0.00044004771408898786 -0.0008311383437379014 -0.0029829428767628695; 0.0009392566972902298 0.0007911519995829732 -0.0017541127499784313; 0.001161537888261734 -0.002008622866058931 -0.002472931575534771; 0.001564880740397125 -0.00025727964360625533 -0.004400148318148649] %
+
+Mass Used: 120.75077149135222 kg
+Launch C3: 93.15014197945216 km²/s²
+||V∞_in||: 1.3404333190251717e-7 km/s
diff --git a/archive/ES_0.5692519552559967 b/archive/ES_0.5692519552559967
new file mode 100644
index 0000000..58f1573
--- /dev/null
+++ b/archive/ES_0.5692519552559967
@@ -0,0 +1,22 @@
+archive/ES_0.5692519552559967---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T17:36:32.328
+Launch V∞: [7.151834272015178, -6.681624278561725, -0.4484731301072506] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4993127184651414e-9, 1.2859472024028176e-9, -2.8402393549231762e-9] km/s
+ V∞_out: [2.474440545411362e-9, 4.44108905003185e-9, 1.24287785457315e-10] km/s
+ time of flight: 1.5534074240807408e8 seconds
+ arrival date: 2029-04-11T15:48:54.328
+ thrust profile: [0.4637339894301333 -0.12127569112739307 -0.19070156127717838; 0.10721418190209159 0.022642127083886236 -0.12775116615933307; 0.08201943294133955 0.03409713443799627 -0.1649296295396168; 0.06132285536367563 0.03293720931964406 -0.17179785429656794; 0.041005019185901014 0.0255217606605511 -0.14626826205149424; 0.032663924167136586 0.02261014982136245 -0.14194429263877198; 0.022127632681063103 0.01639668924557172 -0.11290537095859664; 0.018926278445860187 0.015321049608207063 -0.10839037447574035; 0.0046390224488673075 0.0035768248158970783 -0.029914997363699753; 0.002646454101272736 0.002537511358256349 -0.01822351053957056; 0.0027638456980933687 0.002415764004161503 -0.020448233542367994; 0.001384721132925018 0.00035212510481455076 -0.004154853615086205; 0.001219961104681538 0.0011693938879837732 -0.0038539287751155303; 0.0009982796362689862 0.001380267765693636 -0.005550186624491863; 7.505450481462908e-5 -0.000375561127123167 -0.003057851219012062; -0.0008941573216876425 0.0035928429945422634 -0.0037017156636200994; 0.0006787512159461032 0.0012201606756518215 -0.002231805503600863; 0.0018931508008163105 -0.0003153815966962368 -0.00023952477170361355; -3.082667731442218e-5 0.0007568505298299801 -0.00041615098621406365; 0.00016225560984154059 0.000143453716096226 0.00028047956564552666] %
+
+Mass Used: 104.16248761645284 kg
+Launch C3: 95.99396460266458 km²/s²
+||V∞_in||: 3.995895877685462e-9 km/s
diff --git a/archive/ES_0.5692544301934819 b/archive/ES_0.5692544301934819
new file mode 100644
index 0000000..cd181bd
--- /dev/null
+++ b/archive/ES_0.5692544301934819
@@ -0,0 +1,22 @@
+archive/ES_0.5692544301934819---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T09:16:53.595
+Launch V∞: [7.2687620463669145, -6.460549038902435, -0.1660743489339287] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004743757025055902, 0.003815207627386293, -0.0018889428917981284] km/s
+ V∞_out: [-0.0018216171654578809, -0.003240459864966986, 0.002129345536821318] km/s
+ time of flight: 1.5884133512735757e8 seconds
+ arrival date: 2029-05-19T19:52:28.595
+ thrust profile: [0.4693641782302739 -0.08655613629394479 -0.15485354539066876; 0.18698121962263967 0.06552895242027668 -0.18563477680426385; 0.07422164353860193 0.0472175604788133 -0.13056274994760492; 0.048594405861701974 0.041343568694559116 -0.12153387173715328; 0.04993213989084017 0.05154532312737177 -0.15744367896774406; 0.04630326267010417 0.05521415306996305 -0.17263986963463537; 0.020112489172249955 0.027328022200123085 -0.0940316641966419; 0.013260032549366226 0.018763934599799716 -0.06460083113068954; 0.018685159014252634 0.02921772862611878 -0.10960083631299178; 0.0018943776235619324 0.0029571108848961353 -0.013970521349618953; 0.0033284082149399406 0.0017562242218494219 -0.015690995561647703; 0.0009280192962049 -0.0009799264148474573 0.003741645750919973; -7.633721800140325e-5 0.00025750562103074153 0.0005253962104904641; -0.001811830666275491 0.00011663454893914637 0.0020181846252672574; -0.006036629090190698 0.0001321915149034005 0.001415274208364826; -0.0010512952248882866 0.0021148843568597493 0.00030591533667524235; -0.00017070200569963082 0.00019620628526532036 -0.00042298533400987213; -0.0009374926343230028 -0.008665382509729268 0.0029748276573267614; 0.002715782994877534 0.0010275950915333131 0.005711213758528055; -0.001235775660076494 -0.0001684632028510306 0.00025980448097767] %
+
+Mass Used: 112.2899737082389 kg
+Launch C3: 94.60117626014114 km²/s²
+||V∞_in||: 0.00428356706445328 km/s
diff --git a/archive/ES_0.5692558476406293 b/archive/ES_0.5692558476406293
new file mode 100644
index 0000000..9e05b95
--- /dev/null
+++ b/archive/ES_0.5692558476406293
@@ -0,0 +1,22 @@
+archive/ES_0.5692558476406293---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T08:40:51.010
+Launch V∞: [5.633880156197649, -7.943926261526477, -0.11600269365720511] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2995677307169376e-6, -8.157365883102641e-7, 5.764260702239638e-7] km/s
+ V∞_out: [-9.56064507763442e-7, 1.220587386407116e-6, -7.56669605194758e-7] km/s
+ time of flight: 1.6555753755333397e8 seconds
+ arrival date: 2028-07-25T12:53:08.010
+ thrust profile: [0.38921145485989106 -0.15305645666008857 -0.135207523519246; 0.19989917212463118 0.028590212924660408 -0.18237140179921796; 0.07837939862403902 0.03228370837362097 -0.1258044982323413; 0.04444515990458556 0.02447686009000981 -0.09546128443052955; 0.04719658147207371 0.03464374519341371 -0.12975426787233194; 0.055611138153688386 0.045363748712064715 -0.17567689173666604; 0.020113046803293632 0.0181118521926771 -0.07581786898214816; 0.028188510084376315 0.02788900178911409 -0.12048244553063914; 0.018409873787584453 0.019923979291242965 -0.08660620941978485; 0.007441027851266033 0.008652225032496939 -0.04052526438724142; 0.002898096852217737 0.0030869193391091553 -0.016104469894403298; 0.0002838077620933684 0.0008415953603163615 -0.002233193332960731; 0.0008743202075487699 -0.0006186041520622092 -0.0017445039672553662; 0.0009009714742107674 9.170191418389007e-5 -0.0017084471041705256; 0.0006966118643361155 -0.00029412383390447247 -0.001051451765731255; 0.00012154202668845134 -0.0014053742365943284 -0.0013544628042317535; 0.00019648779740484822 -0.0002556657359921381 0.0002820846263533118; -0.0016541342828193845 0.004863221865434555 -0.0010895765706620663; 2.431500047553976e-5 -0.00010021412422921735 0.0015776215009499993; 0.0008443727432217432 0.0009302631277165287 -0.002888100581427665] %
+
+Mass Used: 110.7816665679643 kg
+Launch C3: 94.86002668790341 km²/s²
+||V∞_in||: 1.6390758013779235e-6 km/s
diff --git a/archive/ES_0.5692798862477824 b/archive/ES_0.5692798862477824
new file mode 100644
index 0000000..b56b51f
--- /dev/null
+++ b/archive/ES_0.5692798862477824
@@ -0,0 +1,22 @@
+archive/ES_0.5692798862477824---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T15:00:48.362
+Launch V∞: [7.999157335294519, -6.273667512864161, -0.23606475229990875] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3942540344163095e-9, -2.129045150534563e-9, -1.871515218574677e-9] km/s
+ V∞_out: [-6.475095817799409e-10, 5.840271665825614e-10, -2.2386120891608336e-10] km/s
+ time of flight: 1.8459805110519025e8 seconds
+ arrival date: 2030-03-28T04:14:59.362
+ thrust profile: [0.04713317803363781 -0.007121328958933444 -0.023317566623719164; 0.008858118152598855 0.0013035089437502853 -0.013607894021767306; 0.023239012932488562 0.0045531401875176045 -0.06559630777407775; 0.028321778062653475 0.005143352930897805 -0.10581305898860363; 0.02828539322016406 0.0035645869195338976 -0.12873470597703873; 0.028694948438567684 0.000344372561072935 -0.14796289454618447; 0.013374067171763801 -0.0003945117060165857 -0.0798273898492477; 0.013400070846222738 -0.001007938209152042 -0.08452955176782716; 0.0032276361384247876 -0.0017124682246258155 -0.036005222833430585; 0.0019827480786783953 -0.00027765342253271855 -0.012329238086439301; 0.0060165027979181065 -0.001616150427916928 -0.05701288393087693; -0.000714193845352207 -0.0004731284592466541 -0.004885859328044601; 0.00022399932238985579 0.0010705550962721872 -0.0002171273361720009; -0.0015924407154771308 0.0011207310584294351 -0.001140615742806994; -0.0010195733303559366 -0.00032172197921386805 -0.0013550316480824072; 0.00036311066121110837 0.0005013307975942681 0.00213233423891692; -0.002723839297164428 0.0010273810634500889 0.00319027302366539; -0.0006351101649932152 -4.573646947268924e-5 0.004087951911830276; -0.00044611602155473536 0.003473333166817029 -0.0017107874694503528; 9.632504935694598e-5 -0.0006926237353173995 -0.0009320531638550931] %
+
+Mass Used: 60.98649984883605 kg
+Launch C3: 103.4011487040417 km²/s²
+||V∞_in||: 3.710506009655575e-9 km/s
diff --git a/archive/ES_0.5692844339734241 b/archive/ES_0.5692844339734241
new file mode 100644
index 0000000..5be632e
--- /dev/null
+++ b/archive/ES_0.5692844339734241
@@ -0,0 +1,22 @@
+archive/ES_0.5692844339734241---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T10:31:30.508
+Launch V∞: [6.569336550999466, -7.173473989416709, 0.26958431314184733] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5226140484538383e-7, 2.0565859963198285e-7, 8.540749948756938e-8] km/s
+ V∞_out: [-8.650257590059311e-8, 1.3600146803067538e-7, -2.1679159333211294e-7] km/s
+ time of flight: 1.8506228217930326e8 seconds
+ arrival date: 2029-03-06T08:42:52.508
+ thrust profile: [0.4700968789978931 -0.10658994050031527 -0.1233580539696657; 0.15795070214925874 0.05707723944994678 -0.1364368003526473; 0.08864361084395181 0.060110840838723055 -0.130384564321684; 0.04893842024288777 0.044770468722711884 -0.1014159434235342; 0.03623095012720004 0.03899972222783477 -0.09344084477143368; 0.02133728601373493 0.03059849938302235 -0.07924740526753259; 0.030064243749627316 0.047359789548331345 -0.11804545714459982; 0.015438218512567246 0.024163413391261636 -0.06606482645883237; 0.007353319579307232 0.013541334577944033 -0.04094553452188819; 0.005585501993493984 0.01325642762966496 -0.04087954320456914; 0.00041120267794021986 0.0009000315149212964 -0.0032898117425321483; -0.0005548436283300972 2.543600348212872e-5 -0.0018777117096238837; 0.00016666315485643136 -0.00014647563731220504 -0.0015676541959438956; -4.115243199755122e-5 0.0022068565860632813 0.00038142994819761745; -0.00018527684627388878 0.0028080345050952578 -0.001064924641100972; -0.00021278810503871129 0.0010344083952031975 -0.0006755584318708094; -0.0012507874021652826 0.0024123537593588543 -0.0050716646445804914; -0.0002959438185503177 -0.0011294318524333994 -0.0007572106707421436; -0.0014103190210654295 0.00020575994989763241 -0.005187986474737444; -1.4855490593501949e-5 0.0010136206252649548 0.00245368442108002] %
+
+Mass Used: 111.82091255799924 kg
+Launch C3: 94.68758749902781 km²/s²
+||V∞_in||: 2.697655203631429e-7 km/s
diff --git a/archive/ES_0.5693019244424644 b/archive/ES_0.5693019244424644
new file mode 100644
index 0000000..8ceb943
--- /dev/null
+++ b/archive/ES_0.5693019244424644
@@ -0,0 +1,22 @@
+archive/ES_0.5693019244424644---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T13:52:22.268
+Launch V∞: [8.068090395429595, -6.059899573233582, -0.21465961149086893] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.8313600158432746e-5, -4.400147922916728e-5, -0.002910392599702389] km/s
+ V∞_out: [0.00259562117238793, 0.0008830498206094312, -0.00098215482739846] km/s
+ time of flight: 1.8749577779246897e8 seconds
+ arrival date: 2030-04-29T16:01:59.268
+ thrust profile: [0.08929589321559692 -0.006857511916825329 -0.0391419245395299; 0.007668088736054437 0.002187302736143763 -0.01226586789037879; 0.025102115858846467 0.012200941880452584 -0.06642332345932525; 0.036793956322754916 0.01806996133060276 -0.1260077720210407; 0.029780580432756047 0.016192618378293864 -0.12866575805376648; 0.023192161407342086 0.012229532780603049 -0.13438736453968322; 0.01143330660376675 0.008830808907493094 -0.07540189065999982; 0.008246423041872397 0.0026567367464909245 -0.06108448144605288; 0.0030726917121781504 0.0018297759710352588 -0.025367819726768773; 0.0012254475965561723 -0.00011752577693569573 -0.01307335298479411; 0.00335387408411756 0.012362642422723934 -0.03582368020070938; 0.0016090978069001238 0.001133225903207585 -0.01798983075957696; 0.0008806205092961065 -0.0028266565379890893 -0.01108298900513115; 0.0011336457524620952 0.0006398411240552374 0.003951377747589756; 0.004378126195254711 -0.0030537840649979054 -0.005246853586549991; -0.011891226704129131 0.005180890103941163 0.005415544393823201; -0.005182058399906987 0.006610164145888976 -0.001416170395380634; 0.012190138106413076 -0.006759241860664909 -0.008725810052848382; 0.010086992643209197 0.0009222066049186122 -7.55672819038513e-5; -0.010455612937720331 -0.033011120965361795 0.02857994427767864] %
+
+Mass Used: 69.98740392692798 kg
+Launch C3: 101.86254421530523 km²/s²
+||V∞_in||: 0.0029113092742854064 km/s
diff --git a/archive/ES_0.5693091285080429 b/archive/ES_0.5693091285080429
new file mode 100644
index 0000000..c753c4b
--- /dev/null
+++ b/archive/ES_0.5693091285080429
@@ -0,0 +1,22 @@
+archive/ES_0.5693091285080429---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T07:48:56.065
+Launch V∞: [6.499932120154428, -7.430631248028121, 0.1956793693919105] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5424664034563622e-8, -6.711737885541797e-9, 2.1068007397614685e-8] km/s
+ V∞_out: [6.973531595435699e-9, -1.5931553673495646e-8, -2.1620578871572504e-8] km/s
+ time of flight: 1.840758310902199e8 seconds
+ arrival date: 2029-02-27T19:59:27.065
+ thrust profile: [0.25406449417261323 -0.07095739553013027 -0.0895976907159962; 0.03457424369319458 0.006949584966167835 -0.03587549828975413; 0.04098534459743446 0.018812704053876115 -0.07283670382747083; 0.09807250512218565 0.06410228905523449 -0.2393459109077335; 0.059954106703219066 0.04687309449888184 -0.18872290454355786; 0.01677160949137931 0.01295326601870366 -0.0627230475419793; 0.019059316417481192 0.016333121127811167 -0.08788450898935922; 0.011821628729413305 0.010129195738461444 -0.05484017755291614; 0.005633869489732383 0.006082631711305417 -0.03251510618102568; -2.0148942307042614e-5 0.007042168381558009 -0.020496491118590733; 0.0018759100367895314 0.0010460610396813732 -0.01195657271441406; -0.0013298553141632334 -0.0006749966467988412 -0.010682852980073088; -0.0026591696626520997 0.01739913696142572 -0.005673706959596056; 0.003484092187628746 -0.0009805576101081692 -0.0009711716844913768; 0.008933195660505718 0.0032904012782287656 0.004710317708399788; 0.0013944300500315224 -0.00025513090960320055 0.0004313515168991442; -0.03803014091487109 0.007625734644128513 -0.006133988102422009; -0.007778404810939184 -0.0037473542958154945 0.014685208249381838; -0.023286008578032064 -0.004100527128396301 0.01531203874385771; -0.0010794337972090551 0.00032079063247219587 -0.005778816543853696] %
+
+Mass Used: 95.43413235542539 kg
+Launch C3: 97.5016887263928 km²/s²
+||V∞_in||: 2.6959759303994623e-8 km/s
diff --git a/archive/ES_0.5693147570974684 b/archive/ES_0.5693147570974684
new file mode 100644
index 0000000..d37b525
--- /dev/null
+++ b/archive/ES_0.5693147570974684
@@ -0,0 +1,22 @@
+archive/ES_0.5693147570974684---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T23:20:04.264
+Launch V∞: [8.00104742969509, -6.244922068107017, -0.09855391553656054] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.1816261892151135e-6, 0.00022826490822589992, 3.941963205478401e-6] km/s
+ V∞_out: [0.00022011106551224073, -3.382937494773239e-5, 5.031203547238282e-5] km/s
+ time of flight: 1.8510262965926573e8 seconds
+ arrival date: 2030-04-03T08:43:53.264
+ thrust profile: [0.09514496707457044 -0.018272688338765816 -0.04651909452600143; 0.011025470442141718 0.0008539449835563445 -0.019052462859547224; 0.023714680626237977 0.0011797114823701405 -0.06772811780931337; 0.023376259355465803 -0.0011362743618627041 -0.09045669197248732; 0.023100343052549044 -0.003226678123510305 -0.10623083683732017; 0.014269924376196022 -0.0032538627433991913 -0.07475537434057422; 0.013862670357845388 -0.003977746841557975 -0.07938153471128605; 0.033396015036150424 -0.009338229988390564 -0.17770957247323516; 0.010558048124559339 -0.003971615235907231 -0.06845924536031721; 0.005234492926673196 -0.0024712628387951545 -0.0340128173763447; 0.0006670644887355337 -0.0002417785891548374 -0.004186374742158688; 0.00042223390225381836 -0.00022675454426327737 -0.0025481856489844527; 0.00017097822941186962 -2.3394774490204872e-5 -0.000966448078991133; 5.770414211102477e-5 -0.00013426824137246184 -0.0008880073314603659; -6.914689920254182e-5 0.0001842155509381277 -0.0007350131316104362; 4.930126891728472e-5 -0.00014531111709738644 -0.0004921519843647092; 0.0001903650584163133 1.6630042683608934e-7 -0.00025357070315028057; 1.364698737488316e-5 -0.00025278913327923835 -0.00020624024307083457; 0.0002866306536859994 -0.00048653373457473246 -0.00024268006239275047; 0.0002442316241328226 -0.0011235275521180824 -0.0002770692305037179] %
+
+Mass Used: 63.21832379488296 kg
+Launch C3: 103.02552448322801 km²/s²
+||V∞_in||: 0.00022832111191587115 km/s
diff --git a/archive/ES_0.569321346270821 b/archive/ES_0.569321346270821
new file mode 100644
index 0000000..eb12a2f
--- /dev/null
+++ b/archive/ES_0.569321346270821
@@ -0,0 +1,22 @@
+archive/ES_0.569321346270821---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T03:09:54.937
+Launch V∞: [6.599154454282105, -7.471395766062452, -0.14423522825368468] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.996698506317745e-9, 1.2637174491635363e-8, 6.889151694279256e-8] km/s
+ V∞_out: [-4.495824722701244e-8, -4.287400426427407e-8, -2.01439583848134e-8] km/s
+ time of flight: 1.852461196202649e8 seconds
+ arrival date: 2029-03-15T04:25:13.937
+ thrust profile: [0.13132626276280576 -0.03681845931537833 -0.051796658901335495; 0.02659732120376635 0.005823492457668448 -0.03301444996239265; 0.03987215473947817 0.01819355797685719 -0.07948817101092723; 0.04161374287234986 0.02520899813877822 -0.11417567937692075; 0.033574159835105706 0.024451602062501264 -0.11800652612680078; 0.029107470992995356 0.024085740716642014 -0.12393552496244808; 0.04547343866096497 0.041864212084784115 -0.21959514313689843; 0.01084924975469383 0.010796880152616161 -0.06358296619051068; 0.003054956074360237 0.005113586934805225 -0.02636619039328539; -2.384191785062984e-5 0.006002177083978116 -0.012977331108958056; 0.0015583918709103192 -0.003252258818965694 -0.01396073312935784; 0.002661882009652772 0.001989490003289779 -0.016141042867166416; -0.0004378824209637427 -0.0016162294598493796 -0.0012283255201371553; 0.009495104142903906 0.0006515895378120268 0.008149634202092696; 0.00017605750236488035 -0.003751720417960208 -0.0014678296092309065; -0.0106339650863485 0.005618472268390096 0.002637977410119014; -0.006003625439772071 -0.0001631710585156816 -0.007923246437551372; 0.023354542660256057 -0.013879016109170758 -0.018799197058961572; 0.0008704501556767046 0.01691621912558649 0.00016786248481735376; -0.006109324358338916 -0.005388780278519745 -0.02853897458670069] %
+
+Mass Used: 84.42508228284396 kg
+Launch C3: 99.39139800567666 km²/s²
+||V∞_in||: 7.06164277617092e-8 km/s
diff --git a/archive/ES_0.5693319977342736 b/archive/ES_0.5693319977342736
new file mode 100644
index 0000000..12bc243
--- /dev/null
+++ b/archive/ES_0.5693319977342736
@@ -0,0 +1,22 @@
+archive/ES_0.5693319977342736---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T22:15:55.684
+Launch V∞: [6.1668436314929, -7.341861252937188, 0.07402661902459616] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.585779402464827e-8, 2.4146107809124386e-8, 1.675743444453128e-8] km/s
+ V∞_out: [-4.974094332237191e-9, 1.1317415609283269e-8, -3.23408721282508e-8] km/s
+ time of flight: 1.8328128743396193e8 seconds
+ arrival date: 2029-02-14T05:44:02.684
+ thrust profile: [0.5627519254637057 -0.13373451189052846 -0.14277472506727304; 0.22885370354093018 0.08171752204324918 -0.1734443017235275; 0.10232668319461577 0.06953978727001041 -0.13424027726844817; 0.08069612489527918 0.07379104586651053 -0.14675552567292244; 0.033970043032375864 0.03816177715537257 -0.08171187932273544; 0.02986882379612032 0.03894660913301698 -0.08844843803208163; 0.032072323795311906 0.04891543269558788 -0.11093967863387655; 0.006689962199355479 0.012834680854971579 -0.03183963768337358; 0.0023002117310468324 0.004900801497051487 -0.014560151949015193; -0.0003170712605092001 0.0034705748592575 -0.00636788335849829; 0.004215927844568845 0.0109256964196856 -0.031170446449004487; 0.0006511584676787889 0.009469272578233835 -0.02259546502767612; 0.0012976044950468169 0.004611253266524706 -0.013303208728385202; 0.001468714784181594 -0.004838797241585083 -0.0018840189862432046; -0.002924665777178319 0.006399357721519789 -9.878120466821905e-5; 0.00022521364868583903 0.0028266988233281313 -0.003989973138002021; 0.00021431180638304835 0.003949532045405926 -0.0007648233100278398; 0.0006520180336148675 -0.0037758511614801784 0.00018370589511271154; -0.003216220878406584 0.0011536988201443963 0.005530962185911668; -0.0015617986126232712 0.0038204834489748863 -0.0073651451663274085] %
+
+Mass Used: 127.91352334754902 kg
+Launch C3: 91.93836697298916 km²/s²
+||V∞_in||: 3.3396343554658664e-8 km/s
diff --git a/archive/ES_0.5693390709236326 b/archive/ES_0.5693390709236326
new file mode 100644
index 0000000..7da9fda
--- /dev/null
+++ b/archive/ES_0.5693390709236326
@@ -0,0 +1,22 @@
+archive/ES_0.5693390709236326---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:05:01.636
+Launch V∞: [7.6013205790079805, -5.8168366005351055, 0.5987514193666185] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011770681399797433, 0.06819639528263703, 0.07543394783479816] km/s
+ V∞_out: [-0.019349232160722006, 0.016241522754597122, -0.09913363629958831] km/s
+ time of flight: 1.8749577787474135e8 seconds
+ arrival date: 2030-04-18T01:14:38.636
+ thrust profile: [0.3861264673376207 0.028489525527303355 -0.07177622505422743; 0.3454270309778265 0.26081814390674213 -0.1785326543034711; 0.12305700355187552 0.1608501160589965 -0.1372528917066938; 0.07197280312335946 0.13212873182988158 -0.12471393263664969; 0.04366707452687322 0.10833276131746025 -0.1108611504358128; 0.0245739588549305 0.07885385050531053 -0.08666531634011934; 0.005533022079067905 0.02307057562214107 -0.02656216409753982; -0.0004160764414972864 0.0013501715131566945 -0.0026838242027173585; 0.00020610045526752753 0.0029932786639513213 -0.00614599145094469; -0.0003867319734455435 0.009313108524907856 -0.0044562685376774895; 0.0009281594620850382 -0.0031166353519633313 -0.004940953370445157; 0.004370652301991445 -0.001262180113940957 0.0012402080779339937; -0.0007982362907838661 0.001919723249712018 -0.004169682381025348; 4.048911639498852e-5 -0.0003172770125188976 -0.00615366783278062; 0.00017193858780306139 -0.0006241027929888164 0.00011120150891071674; 0.0007916645824694127 0.0004311459493716103 -0.0006020977821831592; 0.008039201338410908 0.007040944609614216 -0.020530990636564106; -0.007896484460714235 0.006984297219241091 -0.006688855847879936; -0.0007373331554132974 0.01095468166657221 -0.004805254041186402; 0.0007906359389682331 0.00016922504745535877 -0.0008487813039644869] %
+
+Mass Used: 127.71294865208802 kg
+Launch C3: 91.97416584436856 km²/s²
+||V∞_in||: 0.10236980881150588 km/s
diff --git a/archive/ES_0.5693431257617476 b/archive/ES_0.5693431257617476
new file mode 100644
index 0000000..9cbe650
--- /dev/null
+++ b/archive/ES_0.5693431257617476
@@ -0,0 +1,22 @@
+archive/ES_0.5693431257617476---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T21:41:36.257
+Launch V∞: [7.6830027121819695, -5.447462967484936, 0.22569971912117645] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.59482728116542e-8, -8.028846931919575e-7, 1.3594948583162193e-7] km/s
+ V∞_out: [-1.2168599497864284e-7, 4.5799218426419584e-7, 6.709904872714833e-7] km/s
+ time of flight: 1.8639334564215687e8 seconds
+ arrival date: 2030-04-03T05:37:21.257
+ thrust profile: [0.990539861319736 0.018505985486713478 -0.1962612333435428; 0.15695705401638974 0.10846118636656847 -0.12681953370782614; 0.07648918002890642 0.08957160854436083 -0.11601156315358298; 0.04231024823129714 0.06925181416068021 -0.09967913599243723; 0.02494816779855677 0.0530195136992744 -0.08319270377649818; 0.015663585109027007 0.0431866086233404 -0.0724328825862518; 0.00991137714546019 0.033595895331299676 -0.056963068385110886; 0.009232773924452984 0.03146472440509035 -0.06104901132412217; 0.00022764008475629577 0.00435849366526357 -0.007416296867493934; 0.002743656410217571 0.010767758865252715 -0.014926001815731144; 0.004033494893039331 0.0025510956475266406 -0.011239975391825547; -0.0008208436755441786 0.0064815559893368815 -0.009266678856009264; 0.0013953742769377956 0.0019807119547184974 -0.006101136771836813; 0.003452552496407869 0.001268687836645675 -0.01344479515700894; 0.0052434303522287794 0.004100979715226518 -0.006481201653959453; 0.005704111454268429 0.001764981094324952 -0.004097430887269968; 0.004653974774902203 0.00030527967659625937 -0.005583432950651769; -0.006227587144071239 0.00036764121410073273 -0.004575760430565798; -0.0034914724462988093 0.0018500750016390158 -0.0028106421914751317; 0.003152932866070205 -0.0018910669591568254 -0.008850407772115898] %
+
+Mass Used: 146.50009110113342 kg
+Launch C3: 88.75432382072667 km²/s²
+||V∞_in||: 8.188364909181397e-7 km/s
diff --git a/archive/ES_0.5693472749630989 b/archive/ES_0.5693472749630989
new file mode 100644
index 0000000..6bb754d
--- /dev/null
+++ b/archive/ES_0.5693472749630989
@@ -0,0 +1,22 @@
+archive/ES_0.5693472749630989---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T15:55:44.882
+Launch V∞: [6.389940379693726, -7.373556738926379, 0.1597808032989353] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.357120772015794e-6, 1.3031643258723492e-6, -2.179549500980579e-8] km/s
+ V∞_out: [2.3236298955091845e-7, 3.6599173377350486e-8, 8.481890396039018e-6] km/s
+ time of flight: 1.874957778648954e8 seconds
+ arrival date: 2029-04-08T18:05:21.882
+ thrust profile: [0.395217312422226 -0.09091260854746078 -0.11937739004223367; 0.09131274093096378 0.029751215022203265 -0.08746680253299048; 0.08660993874970178 0.054486644109603216 -0.13772338953204039; 0.03225756016364837 0.026260041284885415 -0.07534657033651065; 0.028325933804962903 0.02697788613749232 -0.08169724606649058; 0.028250676543065747 0.03398095075363794 -0.10393597895080761; 0.05658108193867056 0.06262976377379575 -0.19539167632048532; 0.011895531875442162 0.014439059307676432 -0.054320905701962435; 0.0016527802079770507 -0.0012449486677489803 -0.019378617077544652; 0.003081215514056785 0.011287512195653125 -0.023830716692359172; 0.0023550728704539365 0.004616428623126684 -0.013600914121525864; 0.0007571648063531088 0.0018947094302740998 -0.0037407335156237832; -0.0008760555128419143 -0.0022582944046171294 0.0018648149034035137; 0.010168555909456506 0.0004632318766799527 -0.003695696344473959; -0.0015277402054760913 0.004379385147248798 0.01222304569802029; 0.0017412403818248279 0.007072784289484065 0.008355089358478144; 0.008768700995033823 -0.02411676226692825 0.0011206260551210917; -0.018307827530721577 0.006852929563788854 -0.009083481223012564; 0.002067878531007128 -0.009146987162354514 0.016140710858192905; -7.158370493841532e-5 0.0033327255671152557 -0.0017176594812116934] %
+
+Mass Used: 108.75228028764104 kg
+Launch C3: 95.22620694330989 km²/s²
+||V∞_in||: 8.458142816356729e-6 km/s
diff --git a/archive/ES_0.5693579568879895 b/archive/ES_0.5693579568879895
new file mode 100644
index 0000000..7cbbd94
--- /dev/null
+++ b/archive/ES_0.5693579568879895
@@ -0,0 +1,22 @@
+archive/ES_0.5693579568879895---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T04:32:36.817
+Launch V∞: [5.9532805396593345, -7.71459800349151, 0.10669204791462228] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0035538865001210683, 0.0024434953693659657, 0.002647730086212209] km/s
+ V∞_out: [-0.00220807088121218, -0.00378635788581924, 0.0025201795776784107] km/s
+ time of flight: 1.702086778869585e8 seconds
+ arrival date: 2028-09-17T04:43:53.817
+ thrust profile: [0.45024560986132073 -0.1732252412877874 -0.16754299294643793; 0.05756573911731482 0.00839089177237634 -0.061590623713965245; 0.0707020709549965 0.02693335277471019 -0.12120515532654541; 0.07055274785229373 0.03783415647704271 -0.16389305477819244; 0.07631938719657272 0.049819401952584726 -0.22012532723804892; 0.021257311164048567 0.01579600225669424 -0.076035089538916; 0.017862817976187384 0.014722654846022606 -0.07460018008622465; 0.011728394472316427 0.010819305997385153 -0.05676728677365745; 0.005578454502048709 0.004462024290507078 -0.0258885667530169; 0.02616293531908617 0.02822690505847863 -0.14339226332525326; 0.0007257754615086296 0.00024234619227322474 -0.013863781859458444; 0.0005332257862324607 0.0017262605152053685 -0.004352425860367638; 0.0008451333837547002 0.0019736043211648242 -0.004612121518056014; 0.0003279582332486737 0.0010678697056587408 -0.003554903000979353; 9.934630912338026e-5 -0.00427679530140047 -0.005922059087104135; -0.004016534893358793 0.00013781800016185523 0.0054896527877144555; -0.0007992308815762393 0.003387117145000759 0.0003754779677686529; -0.0027104972011201267 -0.0022373452469567176 -0.0010261495652937897; -0.002438979738989713 -0.01453408170114877 0.003973416145097759; -0.00152612420845068 0.0005845710553315714 0.01109250852691078] %
+
+Mass Used: 110.271213763363 kg
+Launch C3: 94.96795473244995 km²/s²
+||V∞_in||: 0.005060756216741625 km/s
diff --git a/archive/ES_0.5693728280987795 b/archive/ES_0.5693728280987795
new file mode 100644
index 0000000..b8f69d5
--- /dev/null
+++ b/archive/ES_0.5693728280987795
@@ -0,0 +1,22 @@
+archive/ES_0.5693728280987795---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T19:07:03.885
+Launch V∞: [5.854266780963518, -7.894585717228044, -0.1893383030070496] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7362686272885217e-9, -2.088697239126097e-9, 3.038984359578463e-9] km/s
+ V∞_out: [1.3323217768147984e-9, -3.3214514956814584e-9, -4.2337073978833576e-9] km/s
+ time of flight: 1.6495882896455115e8 seconds
+ arrival date: 2028-07-18T01:00:51.885
+ thrust profile: [0.29799360272658393 -0.12010689710941719 -0.11488561084853918; 0.065388521061173 0.007882583998779363 -0.06651109685377345; 0.06812056953665599 0.02393674124686108 -0.11087019635109328; 0.09761493776857756 0.05009705347021771 -0.21408634449781364; 0.07372861541943393 0.04657086774586594 -0.202578169158265; 0.04777235341924232 0.034824089477067485 -0.15666947879547496; 0.03615014614138172 0.02844181671174909 -0.13210682302450166; 0.01715680517794821 0.015251087294646987 -0.07608366326899434; 0.004260044763560102 0.006663262273817657 -0.025135934951908852; 0.000550622331681763 -0.0015896446421835974 -0.00840508540116585; 0.004469325113698977 3.2165497899068994e-5 -0.014935068633704468; 0.004373677766146744 0.0030919124716068053 -0.007581823127773177; 0.0008130370473895411 0.004262392247364752 -0.0018576201389095088; 1.0685044517067628e-5 -0.006736337636479429 -0.0072613126140271145; 0.0019261725535411195 -0.0003313242486499312 -0.0014993510976756587; 0.002153494039653202 -0.001230315880853285 -0.008055185244414773; 0.01299934347838584 0.0026197765065288287 -0.007243913013370442; -0.00018635733845582614 -0.004223595011429364 -0.010299601611466262; 0.0005541233839206244 0.0005625376549013099 -0.003867301714142849; 0.00010048772556747209 6.751808995530137e-5 -0.0006421359253705157] %
+
+Mass Used: 100.57712838492853 kg
+Launch C3: 96.63277218233958 km²/s²
+||V∞_in||: 4.0758693355653436e-9 km/s
diff --git a/archive/ES_0.5693750689191094 b/archive/ES_0.5693750689191094
new file mode 100644
index 0000000..9250316
--- /dev/null
+++ b/archive/ES_0.5693750689191094
@@ -0,0 +1,22 @@
+archive/ES_0.5693750689191094---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T18:45:36.764
+Launch V∞: [7.439279589496639, -6.663615114202099, -0.28534800528728693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00020393143367837923, 0.0005533767828577451, 0.0013837494397972543] km/s
+ V∞_out: [0.0013177262996591072, 0.0001599679439429706, -0.000708260074524546] km/s
+ time of flight: 1.6386507667957655e8 seconds
+ arrival date: 2029-07-23T08:50:12.764
+ thrust profile: [0.171430971278838 -0.0367805539212928 -0.07882710006884691; 0.048574802513489765 0.01075871491763614 -0.0658700856278685; 0.046706447073524435 0.018451933878014883 -0.10794357453381415; 0.055354581150501424 0.027725498153637274 -0.17777125790374448; 0.03419178377533217 0.01869101172073417 -0.1392195459812568; 0.025214509775027923 0.015157583855700178 -0.12231310296846669; 0.014714080397566828 0.00941080660654356 -0.08305334971179876; 0.007893498885395183 0.005325766113188613 -0.05074468225335237; 0.0158985000397994 0.010191299892470465 -0.10871522290182437; 0.004302438958999797 0.0028749499952637494 -0.03097695338807381; 0.0118251647603163 0.007169159978939813 -0.09410433519128235; 0.0008223937615824597 0.0007107896297163447 -0.007969808689322296; -0.000785294089201713 -9.539433767187777e-5 -0.0008798165854382771; -0.0008139628141985776 -0.0010736874503620582 -0.00200895550072699; -0.0016209530637827296 -0.00010430494909712389 0.0018486627990352477; -0.00032548304552026995 -0.0022557519608445613 -0.0005510042557534422; 0.0017140923006256218 -0.0008847192279025292 -0.0028373803296283936; -2.8491933652569166e-5 0.0001108168197058966 -0.0014540161616159453; -0.0009143603977404062 0.00367721906224753 -0.004538041685674325; 0.002668931647599353 -0.0005394945060111753 0.00021315046925920317] %
+
+Mass Used: 81.94050140952959 kg
+Launch C3: 99.82807068504538 km²/s²
+||V∞_in||: 0.0015041862935113199 km/s
diff --git a/archive/ES_0.5693773718334278 b/archive/ES_0.5693773718334278
new file mode 100644
index 0000000..94cf874
--- /dev/null
+++ b/archive/ES_0.5693773718334278
@@ -0,0 +1,22 @@
+archive/ES_0.5693773718334278---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T13:58:53.960
+Launch V∞: [6.251691721631475, -7.5803989626330885, 0.061503916414715004] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5245948631014289e-6, 1.1085533382021332e-5, -6.468176070450165e-7] km/s
+ V∞_out: [4.693540990039561e-6, -9.187406278261598e-6, 4.3727986260315306e-6] km/s
+ time of flight: 1.7306950573459026e8 seconds
+ arrival date: 2028-10-18T16:50:38.960
+ thrust profile: [0.2613480580867463 -0.08905909481055894 -0.08872462773721075; 0.1377758564871044 0.028239613444074278 -0.12915575340945407; 0.08668595209696214 0.039860801218095876 -0.13314945380311435; 0.07106570763903661 0.045428224357923916 -0.14947995502798792; 0.07720532031342131 0.06134529558440033 -0.20398806709680545; 0.03345433493751111 0.030686707891298525 -0.10837371995460279; 0.017966973951232052 0.018290241589259872 -0.06915682523349051; 0.022619419832561063 0.02532667930448151 -0.09647906892201229; 0.0044641733840196 0.005706627142172457 -0.023980264253927547; 0.005132880899967413 0.006348380507412138 -0.026500773376718308; 0.0016707213722696739 0.0028526027556415186 -0.012329016909109489; -0.0016560273485576454 0.0011905637432877189 -0.002217535730468746; 0.001493668867791108 0.0028809920982226607 -0.012309474186232662; -0.0016126932887135961 0.0007673263159589812 -0.003379222694416005; -0.002528216911306362 0.0004704150814364702 -0.0006189559735490305; -0.0017130419484018985 -0.001966577155852559 0.0003783997632662269; -0.0068955775731742155 0.0007914514026123882 -0.0027050283961783292; 0.002941785792708251 0.0004366904739210592 0.0021290983015085693; -0.014314331731494928 -0.012365441584539246 -0.0017605364285037802; -0.008315432201913421 -0.0020986351661893415 -0.004174829006280239] %
+
+Mass Used: 101.06596394969029 kg
+Launch C3: 96.54988054673866 km²/s²
+||V∞_in||: 1.1208559803885957e-5 km/s
diff --git a/archive/ES_0.5693964606773354 b/archive/ES_0.5693964606773354
new file mode 100644
index 0000000..8354900
--- /dev/null
+++ b/archive/ES_0.5693964606773354
@@ -0,0 +1,22 @@
+archive/ES_0.5693964606773354---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T13:59:16.828
+Launch V∞: [7.767155445037966, -5.60489735693278, 0.19733434646049566] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00530091231061471, 0.0029630636691719684, 0.0002329002616613481] km/s
+ V∞_out: [-0.004301480049478281, -0.0025200018226594714, 0.0034685048408689733] km/s
+ time of flight: 1.874957778746886e8 seconds
+ arrival date: 2030-04-17T16:08:53.828
+ thrust profile: [0.5470858515322691 0.026581796206265388 -0.10806540558542996; 0.24342229190806158 0.17719649855257436 -0.16720838918737377; 0.11912280607961495 0.14737164315916898 -0.16159334762322217; 0.05404821526769929 0.09489986736439152 -0.11833653018118073; 0.02781550591185135 0.06499123087486638 -0.09012142224699679; 0.007402181285461781 0.021947469100322897 -0.03187949675113029; 0.0030024604179651436 0.010204332777638504 -0.017017392458103964; 0.008283060572684936 0.0331709730156755 -0.053596434756807296; 0.0053655679256767895 0.03333489367040437 -0.0567509712397815; -0.0006882390199011634 0.002508487031416102 -0.004534080214337914; 0.0074508789221419715 0.0022694981603872096 -0.006566985085888418; 0.0010134057250921708 0.007497782061310206 -0.006180974598908512; 0.003701545318424066 0.008311073883283653 0.0011423230362812; 0.0054391339578892875 -0.0007471314372020238 0.00032406337869325436; 0.004205255108045886 -0.0019771889969822263 0.0007768216695129685; -0.0004491747303836395 0.002060967600967494 -0.0096400443704407; 0.009947502741379559 0.008030865968661677 -0.01738154228497609; -0.014295102208760938 0.0026268108001121352 0.006752539589055643; 0.005167969261446816 -0.0005426935548805104 -0.003013736500075429; 0.002493917125559593 0.011759622025462558 -0.0009594047449211513] %
+
+Mass Used: 128.89784367856146 kg
+Launch C3: 91.78251893342798 km²/s²
+||V∞_in||: 0.006077306982889325 km/s
diff --git a/archive/ES_0.5694180056275862 b/archive/ES_0.5694180056275862
new file mode 100644
index 0000000..47f7599
--- /dev/null
+++ b/archive/ES_0.5694180056275862
@@ -0,0 +1,22 @@
+archive/ES_0.5694180056275862---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T01:31:02.095
+Launch V∞: [5.761363748453039, -7.762590906821619, 0.06687023215601749] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00037025552134305965, 0.0004392261464295672, 0.0003746978382022829] km/s
+ V∞_out: [-0.0004255530142193547, -0.00021835318264427944, 0.0004915994605471407] km/s
+ time of flight: 1.6717490986279127e8 seconds
+ arrival date: 2028-08-10T22:59:31.095
+ thrust profile: [0.5006769128027236 -0.18770155201008307 -0.1351156727103484; 0.11447341486752213 0.023093085844091827 -0.10048098353830504; 0.09675777530633994 0.04554230921753993 -0.13477560979182743; 0.13512064845683314 0.08212746980620884 -0.22849503342583716; 0.05781296361621453 0.04825518253602673 -0.1400875144544532; 0.049179942035017 0.04733216761146248 -0.1427540244251702; 0.017436361229277345 0.017931659455118012 -0.05758674910029655; 0.01434328279994346 0.01653126928637197 -0.054757085453153664; 0.0020220004249377256 0.0025197269593179544 -0.009003470687643688; 0.005270330082127115 0.008559223207796111 -0.030548013400535843; 0.028761468442767432 0.03937903969071627 -0.12832889465290495; 0.0021002862215627376 0.0024486929189714724 -0.007489554137379973; 0.00032504872072896477 0.0007992117897307585 -0.0011878001047214246; 0.0002954511791509359 -0.00019818048534187498 0.0007933384302115133; 8.040752533927866e-5 -0.00018531043553267194 0.0005342585489925156; -0.0009374528474182581 -0.0011700346601470056 6.298169513343797e-5; 0.0005251536434584057 0.0010944851595285807 0.0011312453954201295; 0.0008525447025842526 0.00022234806134931086 -0.00017063595862513233; 0.00017421358601175507 -9.650899925589945e-5 0.0004077565157639487; 0.00043628344135088226 0.0007893738498026368 -0.0004571614530477747] %
+
+Mass Used: 119.16333140197548 kg
+Launch C3: 93.45560145660714 km²/s²
+||V∞_in||: 0.0006858623978217881 km/s
diff --git a/archive/ES_0.5694425215727621 b/archive/ES_0.5694425215727621
new file mode 100644
index 0000000..2a5184b
--- /dev/null
+++ b/archive/ES_0.5694425215727621
@@ -0,0 +1,22 @@
+archive/ES_0.5694425215727621---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T03:05:14.225
+Launch V∞: [7.198479144642883, -6.469849777382663, -0.027191189778475285] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006276114534813897, 0.003162022610850601, 0.0002393272131138741] km/s
+ V∞_out: [-0.005303574883368634, -0.002908519460115134, 0.003576774597081473] km/s
+ time of flight: 1.5518973578142917e8 seconds
+ arrival date: 2029-04-06T07:20:49.225
+ thrust profile: [0.6154737987246689 -0.1442806825756298 -0.20954446320050105; 0.1077281642011727 0.03325959138478004 -0.11086305156005719; 0.12793188870086247 0.0724459132264142 -0.21187547000758472; 0.08419141953584569 0.06439587193471145 -0.19690386206481686; 0.05221539713451057 0.04879758264650301 -0.15922531512447358; 0.01963351174567122 0.02067150465100136 -0.07513622576927802; 0.03681549300665754 0.045930946211598864 -0.15975643155994812; 0.020576649404673766 0.026719347083637313 -0.10327872761049085; 0.0064472289783091335 0.008880107964915354 -0.03794659936432389; 0.0022702334398584613 0.0030879828224703305 -0.014235280134598018; 0.001237809013119632 0.0021700688393636427 -0.010227661291512102; 0.00029965500073802245 0.00012287183366742712 -0.0007796392202677465; 1.3459669377223844e-5 6.718022737197813e-5 -4.86217727809328e-5; 0.00016345112007376701 -2.3824813728394326e-5 -0.0002660301978267687; 0.00013001716069284037 0.00022956910572932351 -0.0003590670314942581; -0.0003806806694947497 0.0005422647829259545 -4.897886151507456e-5; 0.0001406943633742946 6.703471303449494e-6 -0.00010025423352104158; -0.00025461831646750706 9.350316882640879e-6 -5.406770678338237e-5; -2.0187628179968575e-5 0.0005362571555735424 0.0004799960429959291; 0.00010710324344150556 -1.366252315089277e-5 -0.0001277873452080714] %
+
+Mass Used: 117.89578975996392 kg
+Launch C3: 93.6777974985586 km²/s²
+||V∞_in||: 0.007031733652561762 km/s
diff --git a/archive/ES_0.569468935612536 b/archive/ES_0.569468935612536
new file mode 100644
index 0000000..6a9718d
--- /dev/null
+++ b/archive/ES_0.569468935612536
@@ -0,0 +1,22 @@
+archive/ES_0.569468935612536---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T08:15:23.508
+Launch V∞: [6.022707641400405, -7.593068666431151, -0.13036545931567384] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.165876168227315e-9, -3.78916733064754e-9, 6.0792300213817394e-9] km/s
+ V∞_out: [2.6169355366601456e-9, -5.462238491594833e-9, -7.159922235085749e-9] km/s
+ time of flight: 1.75433486799143e8 seconds
+ arrival date: 2028-11-14T19:46:49.508
+ thrust profile: [0.3494647195677321 -0.09906286369128674 -0.09990733492524355; 0.29681798124828607 0.08741441801755498 -0.2189046961124362; 0.08353075542476142 0.05032448325199443 -0.11464979320041946; 0.06474917753521031 0.052361185029666336 -0.12074041395676388; 0.052300431537012776 0.05296888111710698 -0.12625535968494558; 0.05784108479409869 0.07034038278556559 -0.16705469951695762; 0.02629027810048975 0.038158422337385665 -0.09568260661372158; 0.015208398988957535 0.023064860865298974 -0.06453764138205677; 0.007292974621534018 0.012026878753196532 -0.034038895870828666; 0.002567065962607945 0.001178912351057113 -0.0037478919809848816; 0.0017643283855811637 -0.00020763337007680648 -0.003745398853086915; 0.001816040624468519 0.002605613978196488 -0.002051808852822722; 0.002092883843854863 0.0026091379202003826 9.478202419776517e-6; 0.003157520907195282 0.002877982726849587 -0.004576151832156518; -0.0031894573664779193 -2.2739042866189033e-5 -0.0047089681203236235; 0.001740611256992419 0.004190831206222382 -0.0036179383370430478; 0.005150101385296283 0.0003172689174244741 -0.008186057175489755; -0.0009370366031402406 -0.00013353359464638912 0.00988262021552173; -0.00014329145558088024 -0.000401782659490587 0.0017406044255403623; -0.0009709419712202391 0.004369067954369219 -0.006176800899017296] %
+
+Mass Used: 116.36970836518549 kg
+Launch C3: 93.94469425990397 km²/s²
+||V∞_in||: 8.286697228783005e-9 km/s
diff --git a/archive/ES_0.5694695009257529 b/archive/ES_0.5694695009257529
new file mode 100644
index 0000000..92e7b6e
--- /dev/null
+++ b/archive/ES_0.5694695009257529
@@ -0,0 +1,22 @@
+archive/ES_0.5694695009257529---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T20:24:22.274
+Launch V∞: [7.55222868279127, -5.640231407135601, 0.11456901586464827] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.4096878552523157e-6, 4.844684791324877e-6, 5.144197842031374e-7] km/s
+ V∞_out: [-4.227070740649452e-7, 2.060903297974221e-6, 5.557172376573839e-6] km/s
+ time of flight: 1.8749577787127608e8 seconds
+ arrival date: 2030-04-15T22:33:59.274
+ thrust profile: [0.726396184432544 0.03458228892426168 -0.12968676899835346; 0.3107627500233791 0.23273108479687835 -0.20093520278848928; 0.1383168142321915 0.17748758688658026 -0.17294403770208983; 0.08200047117613958 0.15059994847847452 -0.16300311406609708; 0.028526483530167457 0.07059293696424888 -0.08862911512717472; 0.010292564215720756 0.034035470054432714 -0.0477390730793587; 0.0026665181469656403 0.012152507673104069 -0.018388580628479253; 0.0009434684985881247 0.0073369907475430455 -0.011573488113283365; -0.00021217930610880037 0.00279859893072418 -0.0023014095583952622; 0.0008327893690876948 0.007742423112113325 -0.013261754469505763; 0.00032562874303103384 0.0028228667361373163 -0.005622833289580601; 0.0015045696316577702 -0.001313012558777673 -0.00165464418284607; 7.187247910007098e-5 -0.0004255596739200697 0.00019196759712261906; 0.0017993995031938582 -0.0011611659906745975 0.00018366577583232672; 0.0012431465973770667 0.002023768181838235 0.0009973266558661038; -0.003117597271488119 -0.001826168006326209 0.001305479503098071; -0.0008188370174501806 0.001504881278616991 -0.0017647196811257071; 0.00018639441984156138 -0.002802624554747508 0.0013585458987572005; 0.0003787838640698857 -0.0033593277656225316 -9.386375967923057e-5; 0.0004691011730220652 -0.0008645561637659759 0.0009963937849623386] %
+
+Mass Used: 146.02236671481887 kg
+Launch C3: 88.86149446261021 km²/s²
+||V∞_in||: 5.946559485276281e-6 km/s
diff --git a/archive/ES_0.5694710418571147 b/archive/ES_0.5694710418571147
new file mode 100644
index 0000000..3f59991
--- /dev/null
+++ b/archive/ES_0.5694710418571147
@@ -0,0 +1,22 @@
+archive/ES_0.5694710418571147---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T13:11:25.939
+Launch V∞: [6.418300454584098, -7.458725299304338, 0.1431444706868295] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.157159274239342e-8, 1.8242095422520211e-7, 8.125721637274177e-8] km/s
+ V∞_out: [-6.559574901575249e-8, 1.0770852999882283e-7, -1.8050244748024287e-7] km/s
+ time of flight: 1.8537865834639773e8 seconds
+ arrival date: 2029-03-16T03:15:43.939
+ thrust profile: [0.28464574918073815 -0.08020482099833161 -0.09823117136724718; 0.08469524787678193 0.019864054845663733 -0.08740868322991002; 0.06460468503206761 0.02900269856858785 -0.109909417539021; 0.04518048555894326 0.02625888309647089 -0.10707845151674177; 0.0436427587514556 0.031314452008987054 -0.13183210544736926; 0.044180168134336034 0.035916624880695136 -0.160668018973913; 0.022387666579536697 0.01949578177016247 -0.08976691177429744; 0.005566143248402642 0.0044816135490143546 -0.025955590297378362; 0.006342176048552967 0.0004010408948648741 -0.03969290782844826; 0.0062411377414122796 -0.0001500470950555905 -0.020098152055238655; 0.0028584994407821075 0.003435219809033234 -0.02283838296262137; 0.0004462204492025829 0.00386724395163773 -0.011423390420192699; -0.002348108204140527 -0.002066360569356997 0.004829129991525839; -0.01249293508116975 -0.0006934042787620192 -0.013971633534743134; -0.0030459863315010155 -0.0030102516527796223 -0.0125012963171218; -0.001356637903159927 0.007220931586963349 0.008374249264484476; 0.0007347294296865779 0.0018949834920355506 -0.018549843171795644; 0.0032849944575703127 0.0009501641583802775 -0.0011991511202216112; 0.01878709579412121 -0.003520266647749866 0.013271500377537535; 0.012957326484402926 0.012842651673096837 0.03217500485334959] %
+
+Mass Used: 99.43823292746993 kg
+Launch C3: 96.84765415528524 km²/s²
+||V∞_in||: 2.196940972135087e-7 km/s
diff --git a/archive/ES_0.5694869723998814 b/archive/ES_0.5694869723998814
new file mode 100644
index 0000000..359172d
--- /dev/null
+++ b/archive/ES_0.5694869723998814
@@ -0,0 +1,22 @@
+archive/ES_0.5694869723998814---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T13:04:25.932
+Launch V∞: [5.955076187843052, -7.9000544888986175, -0.1677015287520649] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0648722077601355e-5, 1.7764905717977215e-5, 2.7817577929338336e-5] km/s
+ V∞_out: [3.407821367412544e-5, 1.880316798748413e-5, 9.01227372926597e-7] km/s
+ time of flight: 1.6439031790818876e8 seconds
+ arrival date: 2028-07-11T05:03:02.932
+ thrust profile: [0.19531191125041697 -0.07733034608561651 -0.07945724289050633; 0.07910121235307631 0.009974535069440621 -0.08608145448264595; 0.07467806171404504 0.02733526758881841 -0.12818969115500833; 0.06667543724629924 0.0348634518101029 -0.15320306724909274; 0.053413790564324784 0.03465607673444257 -0.15400013633334836; 0.051309679207382934 0.03762958346075344 -0.17478620889425026; 0.03499841621157202 0.029624020873971937 -0.14222319573498074; 0.027867994406527565 0.02511701846694012 -0.12800593249664907; 0.012099094330952942 0.010673605418885967 -0.059824326212762; 0.003962427982560743 0.004119266659539377 -0.02148526866130591; 0.002902690527746765 0.002032690153309661 -0.017703408012142034; 0.00019336408967452715 0.00013216683100843293 -0.002289177452441396; -0.0007115228151128522 0.0009065526416927522 0.002247860559986557; -0.0014059111732559082 -0.00010948116358347557 0.0012539947392846888; 6.729363657361322e-5 -0.0027112781863952475 -0.00045900551461896394; -0.0015033747504621473 0.0011283758413683734 0.0028271261529998135; -0.0011626922616534098 -0.0006344121688252832 -0.0008295037601734724; -0.0002086795709949214 0.0005391532864070605 0.0002974308559007317; -0.002176490709310073 0.001340013656109028 0.0035349653455580745; -0.0007123269837185084 0.003581363187743711 0.0031469625851251993] %
+
+Mass Used: 93.30695118877975 kg
+Launch C3: 97.90191713332833 km²/s²
+||V∞_in||: 3.89330096506994e-5 km/s
diff --git a/archive/ES_0.5694872581091869 b/archive/ES_0.5694872581091869
new file mode 100644
index 0000000..fed20be
--- /dev/null
+++ b/archive/ES_0.5694872581091869
@@ -0,0 +1,22 @@
+archive/ES_0.5694872581091869---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T07:19:33.991
+Launch V∞: [6.506627629953801, -7.507902455840154, 0.10352103501472963] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010708013022545982, -0.007123394037541796, 0.00944782652021045] km/s
+ V∞_out: [-0.00833015032993573, -0.006814772666235664, -0.005030187499060636] km/s
+ time of flight: 1.8434627160541588e8 seconds
+ arrival date: 2029-03-03T22:37:24.991
+ thrust profile: [0.12773919009029688 -0.03337734123893038 -0.043226443803246174; 0.10347595166820032 0.02567140639706321 -0.09719778046774132; 0.03204361603498895 0.018659161884024354 -0.0555697625262013; 0.06585205203443999 0.04125539586261309 -0.13968184848797283; 0.015303950725071576 0.012190168127281537 -0.045625243245385326; 0.025021395907888988 0.023794795183670538 -0.09585768156009793; 0.014484326758002155 0.014394130880217085 -0.0588732521551153; 0.009959384200406731 0.009431392988202194 -0.05537212919989733; 0.021915392987399127 0.03064313656705588 -0.12890385592717607; 0.027379926645908142 0.040610331004906644 -0.16090519280278953; 0.002865260767343998 0.005347155952123714 -0.026124512596239668; 0.00396323944737883 0.006511823092641086 -0.008355490457380526; -0.0007151261147549475 0.00044211208583286017 0.000711891501602448; -0.0020922611587230896 -0.0039029359494354566 -0.012126778917758312; 0.0006728780915797906 -0.0018801025463341956 -0.0008927908528955091; 0.00020388332243593058 0.0003723934313354196 -0.0037679244412499634; 0.005126526752539725 0.003966692027434172 0.004064419409294517; 0.0002673874510968708 0.0026713968738755027 0.007920307585162528; -0.013853957869620171 0.026538875999994462 -0.013058044183060558; -0.00621980281537729 -0.0053870388463865635 -0.014252846495743774] %
+
+Mass Used: 88.56127359250513 kg
+Launch C3: 98.71551900597935 km²/s²
+||V∞_in||: 0.011880689542235671 km/s
diff --git a/archive/ES_0.5695163087085553 b/archive/ES_0.5695163087085553
new file mode 100644
index 0000000..1c9aa9c
--- /dev/null
+++ b/archive/ES_0.5695163087085553
@@ -0,0 +1,22 @@
+archive/ES_0.5695163087085553---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T13:50:50.405
+Launch V∞: [7.6696703277439, -5.640488105204916, -0.04266218738272986] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.185774021355913e-6, 2.0814529172853903e-5, 5.645029682534015e-5] km/s
+ V∞_out: [5.385813840603118e-5, 6.3933523152458475e-6, -2.6236198505771673e-5] km/s
+ time of flight: 1.8749577787113753e8 seconds
+ arrival date: 2030-04-17T16:00:27.405
+ thrust profile: [0.6363668941287413 0.026822458653717973 -0.1254674767403942; 0.24960930744685406 0.18218835172621656 -0.17270460261058376; 0.09840451742362948 0.12318742669297923 -0.13301165413631263; 0.04527049937665334 0.0832722370767064 -0.10094292644018246; 0.037809829705260416 0.09208261790946919 -0.11908764225685575; 0.016473948765633496 0.05578229473878144 -0.07843236037373667; 0.006896842156054797 0.037952195426408444 -0.05710181492079954; 0.0014411908051582423 0.012094146167306787 -0.022937483063406802; 0.0011333070437789998 0.007117534972777771 -0.015955739462170177; 0.0008961607496021588 0.005587893890503404 -0.009247067972146153; -0.007093844906540667 0.00887722485558708 -0.005393552101517202; 0.0007337457688509104 0.000185904508445092 0.00011480551371160401; -0.0022123111461722564 0.00618835599258253 -0.00736446841982567; -0.005521732678406761 -0.0038906860485404884 0.0031867216265573876; 0.00321920657264773 -0.005077975220967784 -0.006895470610716018; 0.011150243973941876 -0.009237160027508583 -0.008582638961276498; 0.0014584792215094958 0.0024082938618712364 -0.005740419515849379; 0.009423049292701744 0.006558802039787965 0.00883386550136795; -0.009209245901247345 0.0038144448468945408 0.005749406813874312; -0.00015802651411188248 0.003138231478439726 -0.0032216382122000255] %
+
+Mass Used: 135.69787395643152 kg
+Launch C3: 90.64076906346564 km²/s²
+||V∞_in||: 6.048259614632854e-5 km/s
diff --git a/archive/ES_0.5695248391577905 b/archive/ES_0.5695248391577905
new file mode 100644
index 0000000..645a77d
--- /dev/null
+++ b/archive/ES_0.5695248391577905
@@ -0,0 +1,22 @@
+archive/ES_0.5695248391577905---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T09:41:57.203
+Launch V∞: [6.302197933820298, -7.173015532372668, 0.6155094589919572] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.184422267040803e-5, -7.179054262643424e-6, 1.181661012302833e-7] km/s
+ V∞_out: [7.862553664920192e-6, -1.9267029300054697e-7, -4.172485545155659e-5] km/s
+ time of flight: 1.874957778762917e8 seconds
+ arrival date: 2029-04-03T11:51:34.203
+ thrust profile: [0.6894635577672992 -0.13933905861099144 -0.1325687151937445; 0.18414004757939054 0.07689194084541269 -0.12216143988359528; 0.06357376184125672 0.04891920440560158 -0.07470668070872707; 0.029587562560812648 0.0312226713914324 -0.05012278148898488; 0.06015182565055785 0.08079826501126464 -0.1278162871317265; 0.06076921381022548 0.09457765757049175 -0.1495534569294195; 0.027604230587052168 0.050727564070651876 -0.08868139046425283; 0.009581913070501475 0.019466599372239473 -0.03659452686218689; 0.014206189708425849 0.03350676241561783 -0.0629817173311474; 0.005731252258789594 0.014986694260121327 -0.02997286962187991; 0.0003050943135839413 0.0008885312224741124 -0.0008058617561010306; 0.0005497350440226549 0.0018268381538594175 -0.0035463537832452164; 8.503448987114395e-5 -0.000424194677764224 -0.00024405674079558783; 0.00020407490301239408 0.00032800238531894513 -0.0007580201971591819; 0.00012096671481265912 -0.0002236731259517542 0.00026168728127929286; 0.0007256188086475057 0.0010143999490163588 -0.0006641350360783169; 0.00024010604011184063 0.0009173351170022201 -0.0008440535827699031; -0.0014105916480459256 0.0002526649860030773 -0.0017027526782215164; -9.839284346606589e-5 -0.0001868252186504665 0.00330426882366681; 0.0011320623139648661 -0.0003707863759775489 0.00012935145433303353] %
+
+Mass Used: 130.41154765765668 kg
+Launch C3: 91.54870251881695 km²/s²
+||V∞_in||: 4.245576232061024e-5 km/s
diff --git a/archive/ES_0.5695299316252888 b/archive/ES_0.5695299316252888
new file mode 100644
index 0000000..03fcc65
--- /dev/null
+++ b/archive/ES_0.5695299316252888
@@ -0,0 +1,22 @@
+archive/ES_0.5695299316252888---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T08:36:18.852
+Launch V∞: [5.650172920643197, -7.697116144694492, 0.19955185489307992] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.708052763210698e-7, 2.7436430477200215e-6, -1.7172316930254004e-7] km/s
+ V∞_out: [1.0307209589937195e-6, -2.353184500992678e-6, 1.0405246499645496e-6] km/s
+ time of flight: 1.6796648339322293e8 seconds
+ arrival date: 2028-08-18T09:57:41.852
+ thrust profile: [0.6004706727983797 -0.21035176977397316 -0.14928406791438228; 0.2532820482205982 0.05887432664251181 -0.18108574488723087; 0.1177556153461288 0.06401961644365013 -0.1473222006816927; 0.12585257159755348 0.09306767563208652 -0.19651575987296507; 0.049942580714158157 0.047062795676205846 -0.11142191790286732; 0.04457335821119883 0.04834678542090993 -0.11285839119001835; 0.04932464285506397 0.06109604843415033 -0.1398026990721148; 0.01922116960917864 0.02356605832921516 -0.06466565663678182; 0.010971869672474563 0.016014429728769958 -0.044901888529299515; -0.00024040067361042196 5.550416862651591e-5 -0.00026232284988787037; 0.001608290813990595 0.0026682843670946775 -0.007280849960898011; 0.00038963716103940883 0.0007127025937193049 -0.0007670043499241549; 0.0002055984582438304 0.0002917468026675732 -0.0015757229815101428; -0.0002159643159699275 -0.00020445958927886135 -0.0001684093883208153; -0.00027665606349243496 0.00032731131895752483 -0.0005532431018769103; 9.641030759328223e-5 0.00021629757364372584 -0.0006703047340427861; 0.000592936539955942 0.0007157486269273113 -0.0009785226346877528; 0.0008568330503014355 0.0005216160890956013 -0.0008707845931508639; -2.174851539500335e-5 8.963593953759618e-5 -0.0005463470380785232; 0.00011868355819086258 -0.00033483544725535256 -0.000338968261022311] %
+
+Mass Used: 132.39400069105113 kg
+Launch C3: 91.20987192087755 km²/s²
+||V∞_in||: 2.7739074557607833e-6 km/s
diff --git a/archive/ES_0.5695304283277063 b/archive/ES_0.5695304283277063
new file mode 100644
index 0000000..459577a
--- /dev/null
+++ b/archive/ES_0.5695304283277063
@@ -0,0 +1,22 @@
+archive/ES_0.5695304283277063---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T00:35:28.923
+Launch V∞: [6.123865142384784, -7.300155906717871, 0.14387330636497653] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.011549239114153788, 0.0003563140250015881, -0.007687180285673984] km/s
+ V∞_out: [0.01324480684789688, -0.00012176621931912502, -0.00388915537759602] km/s
+ time of flight: 1.8749577803493127e8 seconds
+ arrival date: 2029-04-05T02:45:06.923
+ thrust profile: [0.6791247669850924 -0.12851222303706653 -0.13552836322176776; 0.15507004140736572 0.0662187480852002 -0.11286275263269903; 0.08060156725450249 0.061451548959357206 -0.09906386084270671; 0.06899979794620459 0.07362101692509727 -0.12040187530098323; 0.08769041642333282 0.12075326773069565 -0.192439704319071; 0.03463455412231251 0.05474077827729887 -0.09907074569592082; 0.024810937432124622 0.04457198742897382 -0.08499722751713046; 0.0076244382780710765 0.0156949925022341 -0.031520604099763545; 0.003380980981697441 0.007813444195844899 -0.01600588965992084; 0.0012591347996280928 0.003224512877257716 -0.006018820997860696; -0.0017325779608590589 -0.0007557702659195136 -0.0056904863521374345; -0.000815550911295742 0.0013175591803001013 -0.0014913454088894803; 0.00010940412394341154 0.002250529931379583 -0.0021382663252737964; -2.7009372610398413e-6 -0.00030048536206046285 -0.001931187216751058; -0.005656717754391509 -0.0012341139909917767 -0.0001610999076882124; 0.0011912459658930926 0.0001144699597065888 -0.001166642009245387; 0.014849788609823887 0.003951943559390557 -0.0026995842423071436; -0.00019030675835829663 -0.001591450609732158 0.0012021141662204645; -0.007313089596758622 -0.00496436596104451 -0.015172116967447089; 0.006628286437471491 0.014225357822706444 -0.012684776612626162] %
+
+Mass Used: 134.69974929106274 kg
+Launch C3: 90.81470007278763 km²/s²
+||V∞_in||: 0.013878206820218791 km/s
diff --git a/archive/ES_0.5695459376546546 b/archive/ES_0.5695459376546546
new file mode 100644
index 0000000..48aff9c
--- /dev/null
+++ b/archive/ES_0.5695459376546546
@@ -0,0 +1,22 @@
+archive/ES_0.5695459376546546---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T16:16:49.275
+Launch V∞: [6.250312286726474, -7.585191662568228, 0.20049636109190158] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013414049246569021, 0.009842253658890066, 0.010647996755814213] km/s
+ V∞_out: [-0.008629570630857127, -0.014968399026867533, 0.00957625970680235] km/s
+ time of flight: 1.719062141321999e8 seconds
+ arrival date: 2028-10-05T08:00:23.275
+ thrust profile: [0.30189717111480957 -0.10821370543979537 -0.10134124551910359; 0.0922826662952106 0.016836540349314387 -0.09184676691811633; 0.08159235545852223 0.034808365557492026 -0.13145430255248586; 0.0665317120369241 0.03957539837096607 -0.14673752608880772; 0.048612196723911164 0.035347283904447885 -0.13551807832139762; 0.03411351649519375 0.02742930324430448 -0.1126170590921325; 0.0298719265240524 0.02679553176535292 -0.1152594303414638; 0.015768156542349605 0.01419789972304111 -0.06821013181289372; 0.01637563937123024 0.01822135219545823 -0.07943867043979927; 0.010235408024227 0.0123602322820646 -0.05487163939289796; 0.003246523185255439 0.003958358271582345 -0.01924931997160553; -0.0007177687190231452 0.001967041275467045 -0.003227054464722494; 0.002824333097662353 0.0007338390615186637 -0.0051946709991502965; 0.0007663533011020803 -0.004072413485894084 -0.00613380245478781; -0.0003972638149238383 0.0017947066816593935 -0.0065432094384946324; -0.0007078046905441412 0.002160011586549726 -0.002444197280694334; 0.0004009602106447869 0.00019017188025377617 -0.0015296138782108296; -0.0035042318712915953 -0.006639473733610832 -0.005650501947398972; 0.0047805416563448805 0.0012236900861980005 -0.010858501248236159; -0.0022919218286817683 0.004610733603465387 -0.0037446926232149167] %
+
+Mass Used: 100.72680625362455 kg
+Launch C3: 96.64173503030956 km²/s²
+||V∞_in||: 0.019753139223605547 km/s
diff --git a/archive/ES_0.5695534238651296 b/archive/ES_0.5695534238651296
new file mode 100644
index 0000000..1042cdf
--- /dev/null
+++ b/archive/ES_0.5695534238651296
@@ -0,0 +1,22 @@
+archive/ES_0.5695534238651296---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T23:42:28.301
+Launch V∞: [7.987677181008222, -5.725086800330832, 0.141136346594325] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001162082631815779, -0.0008320326322232701, -0.0007122146992544425] km/s
+ V∞_out: [-0.00014467667708422598, 0.0009864338357096936, -0.0012462022121727005] km/s
+ time of flight: 1.8749577787886652e8 seconds
+ arrival date: 2030-04-23T01:52:05.301
+ thrust profile: [0.30082534306898917 0.012525549009744515 -0.07512422797458919; 0.06119245720681744 0.036560385239699164 -0.05671747662746627; 0.06826105909519747 0.08304611376890962 -0.11345672084760425; 0.02381549221033933 0.02984788586212482 -0.059734570270250455; 0.01375107909856075 0.02750874317993083 -0.06554845039028329; 0.03433082425818908 0.07359122976821299 -0.13038944527754706; 0.015019815075010282 0.03487257706155826 -0.06096290849675362; 0.014233571802560536 0.0371365877536523 -0.09079272566868951; 0.00033070717912142035 0.007312873604155233 -0.023735698370262244; 0.0012679490522091374 0.006033598367133366 -0.015960862731949653; 0.0017005711153067413 0.006612774646803078 -0.02509531660933241; 0.01530402874355412 0.022397374070945514 -0.06404568915158104; 0.0022548962533048243 0.006492542027269264 -0.0077725230493454825; -0.006343537399094448 -0.01586016684706194 -0.018108229158100862; 0.008750385246540836 -0.010283476143597495 0.0029274219117998842; -0.0075026069726530035 0.009651032910152514 0.0003661653096196523; 0.003962966815854554 0.005900797916622677 -0.007984349823387332; 0.01394766457369947 -0.0015040659661317744 -0.006223366334975063; 0.0043327682784845035 -0.009832226029334904 0.041005114760966896; -0.012929439359685237 0.03511228815642635 -0.04659868417463412] %
+
+Mass Used: 100.98176483134921 kg
+Launch C3: 96.59952508765177 km²/s²
+||V∞_in||: 0.0015968607084171015 km/s
diff --git a/archive/ES_0.5695580729245312 b/archive/ES_0.5695580729245312
new file mode 100644
index 0000000..8e8bf76
--- /dev/null
+++ b/archive/ES_0.5695580729245312
@@ -0,0 +1,22 @@
+archive/ES_0.5695580729245312---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T15:18:58.499
+Launch V∞: [6.395220521087042, -7.74264789931541, -0.06954118155823044] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.018946167084283174, 0.0002842442295292343, -0.012825541466538285] km/s
+ V∞_out: [0.021862356910130696, -0.0002308598559432855, -0.006743307593114282] km/s
+ time of flight: 1.7606990240451327e8 seconds
+ arrival date: 2028-11-29T11:37:20.499
+ thrust profile: [0.06785705047568998 -0.03590821487068308 -0.03801738592906897; 0.035485107605351396 -0.00677932229157074 -0.06274530629395314; 0.03557720641906281 -0.007075702748564908 -0.1076569642927982; 0.03175590950468646 -0.00870253899673967 -0.13474297028438662; 0.027184669926841647 -0.010673955320258326 -0.14135721149071825; 0.022664500853694463 -0.011039486179984704 -0.13699754019003113; 0.018180788154719088 -0.01044875443778418 -0.12290978019906101; 0.01382127887923189 -0.008889030144372001 -0.10185957340619388; 0.00953967657706601 -0.006561701771495297 -0.07493990008699819; 0.005508190511570106 -0.0038593722286065497 -0.046028384827137475; 0.0011235043882754261 -0.0007114755807196157 -0.011726414891678201; 0.0010349569420105825 0.0018838535553484122 0.0008737724790520776; 0.00046863883662781895 9.805600602260539e-5 0.002614325259404811; -0.0004307422459683592 0.002162349862799516 0.00035523590419203306; 0.0009215741780629538 0.001281986167830625 0.0016291717085345579; -0.00023094520173519168 -0.000881668684068519 0.0031020214158475477; -0.00025897934433343167 -0.001307300988280382 0.0006483757915147268; -0.001812985509545049 -0.004099055529881547 0.0005493938147893701; -0.0004891176718586528 0.0004600124569746998 0.0066411254721125005; -0.0019960394499236706 0.0006731240773642054 0.0047102935732962255] %
+
+Mass Used: 76.17946351672754 kg
+Launch C3: 100.85227798203866 km²/s²
+||V∞_in||: 0.02288083381080088 km/s
diff --git a/archive/ES_0.569604642050682 b/archive/ES_0.569604642050682
new file mode 100644
index 0000000..ff96041
--- /dev/null
+++ b/archive/ES_0.569604642050682
@@ -0,0 +1,22 @@
+archive/ES_0.569604642050682---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T06:09:12.720
+Launch V∞: [6.3029003630215, -7.502049514771543, -0.18963461896549955] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.0124538502883906e-8, -6.182638073455863e-8, -4.151448930976489e-8] km/s
+ V∞_out: [1.8642749613797333e-8, -4.236912994233257e-8, 5.5707247042331543e-8] km/s
+ time of flight: 1.8749577788825664e8 seconds
+ arrival date: 2029-04-10T08:18:49.720
+ thrust profile: [0.30870545862547893 -0.07159481248643533 -0.10657399368405882; 0.12602081245984456 0.03772447133309293 -0.12934900615255795; 0.08442044751371788 0.04781838827846268 -0.14715045900633966; 0.06721821577574684 0.050990095603290285 -0.1654329905534458; 0.049683747340636596 0.04594146671698557 -0.15941859815930795; 0.022190941223699908 0.023407621122289394 -0.08547079066726912; 0.007615151125282672 0.009856868115574556 -0.037343000683668214; 0.0076215986498526424 0.009249330578321589 -0.03976662666373971; 0.0039338436729012 0.006904389780085318 -0.028210686553364832; -0.0013945782402018862 -0.0024183293368038564 -0.0012909652890467724; 0.0012400125722940062 0.002614951582509822 -0.010469776970411206; -0.0003449216935900234 0.0017070172601556157 -0.0014370734838899707; -0.0007406925018768684 0.01072296878809475 0.004074308356411829; 0.0013464694255377835 0.007707954200536659 -0.005461755239687177; -0.0035523940611305576 -0.00273060883517713 -0.007714926758635962; -0.02018833586383688 -0.006657166550754021 -0.001717379880885631; 0.027205743283532077 -0.004805270335326319 0.005093931195163104; 0.005035180028177366 -0.00438566534465262 0.012542663959631717; -0.015094193008705166 0.007500437447117098 -0.014579014195725295; -0.001516934695520095 -0.006923686942818232 -0.005910949912529951] %
+
+Mass Used: 104.28639207679998 kg
+Launch C3: 96.04326119697069 km²/s²
+||V∞_in||: 8.459274654161903e-8 km/s
diff --git a/archive/ES_0.5696083005598692 b/archive/ES_0.5696083005598692
new file mode 100644
index 0000000..924f386
--- /dev/null
+++ b/archive/ES_0.5696083005598692
@@ -0,0 +1,22 @@
+archive/ES_0.5696083005598692---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T03:15:05.103
+Launch V∞: [8.01740707449307, -6.303047874756516, -0.15572995402176038] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8194800632484428e-9, 1.4129626630296184e-9, 3.8583552780652637e-10] km/s
+ V∞_out: [1.5781596687067987e-9, -1.494652593152167e-9, -1.1992643249115742e-9] km/s
+ time of flight: 1.841652421617063e8 seconds
+ arrival date: 2030-03-23T16:15:47.103
+ thrust profile: [0.02027766752017226 -0.003999162984623554 -0.010013780264447212; 0.0128418294851398 0.0005757295433099851 -0.021483960620698364; 0.028624463499180044 -0.0004885626686763157 -0.08463047313113956; 0.03089586210854412 -0.004391941285489862 -0.12412267480988716; 0.029129357480122426 -0.00760488349704443 -0.1404233340974485; 0.024750443361397926 -0.008689385299199975 -0.1330947148116056; 0.01905674095247671 -0.007869280378778043 -0.10972267428642454; 0.012298617246856217 -0.005592817101113829 -0.07394483049786724; 0.005339754513937735 -0.002606887129020726 -0.03296456150859766; 0.0010544499893823838 -0.0005306154701004653 -0.006919295665795242; 0.0009934793919303454 -0.0007255994854377289 -0.0055690386524405696; 0.0004081794087119953 -0.00031975174082445187 -0.0032123421787536664; 2.8846263913229582e-5 -9.655340249712601e-5 -0.0005902414627719237; 0.0003815431540369665 -6.55605461831311e-6 -0.0004077952559075409; 0.0007628335887544212 0.0003002038960883165 -0.0005182447224332888; -2.9972398471690882e-5 6.478382904085778e-5 -0.0005876712258588784; 0.0003274456207450683 -0.00029906441502297967 -0.0003678745001429247; -5.777125655739981e-5 2.2350353437047005e-5 -0.0008262911994544636; 0.0004637008463999622 -0.000392263380356396 -0.0006947598672035612; 0.0001060846264430024 -1.2089448235997648e-5 -0.0007867855058205544] %
+
+Mass Used: 57.69271423877535 kg
+Launch C3: 104.03148052818378 km²/s²
+||V∞_in||: 2.3357740135107352e-9 km/s
diff --git a/archive/ES_0.5696266882976199 b/archive/ES_0.5696266882976199
new file mode 100644
index 0000000..4b20bba
--- /dev/null
+++ b/archive/ES_0.5696266882976199
@@ -0,0 +1,22 @@
+archive/ES_0.5696266882976199---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T02:01:49.184
+Launch V∞: [6.385832546119905, -7.62277146799273, 0.14607660603492062] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5358118910224625e-9, 6.274208285493839e-10, 8.27323653114475e-9] km/s
+ V∞_out: [-4.8214175735589175e-9, -6.786008093035222e-9, -3.2525207695170553e-9] km/s
+ time of flight: 1.8003285654035684e8 seconds
+ arrival date: 2029-01-12T19:09:25.184
+ thrust profile: [0.14785480131126705 -0.0469910475987766 -0.056743046691708945; 0.039432878633170305 0.006846247024103574 -0.04467182156197908; 0.044895799333932715 0.01805348281815863 -0.08390766772582521; 0.04311233330294716 0.023387987484159576 -0.1138728828864587; 0.055482162658283186 0.03534634439017456 -0.17834038640418834; 0.052078490328964354 0.037655713614211495 -0.2001758060899896; 0.02150519201563991 0.016873110825741867 -0.0970575512073594; 0.017648498149492257 0.014625370182664531 -0.08841702836674593; 0.0029397313812786667 0.004739331990301312 -0.01977085335017667; 0.006890672650714957 0.005845828781427733 -0.03760184461530572; 0.008885935051951812 0.002030222728968969 -0.004205238523348357; 0.0028479960289231657 0.0027670706790856262 0.0022729943375514707; 0.001023254727938178 -0.00576003472217504 -0.007014552297481296; -0.004853733745339385 -0.0004645353943581764 0.0037513440626752836; 0.0037126756105359503 -0.005081992029735055 -0.0025915719755773927; -0.004400093463959101 0.002450612519010059 0.006616021929891773; 0.0008451524120731888 -0.004195195084659101 -0.012122981257155309; -0.007728615759409797 -0.006332289318228597 0.007704230149950666; -0.008366995880783908 0.01217864136016515 -0.023402921413588712; -0.0015407256117456413 -0.0033794088408689894 0.02591334034762993] %
+
+Mass Used: 87.60789989212935 kg
+Launch C3: 98.90684053515893 km²/s²
+||V∞_in||: 8.437939189219818e-9 km/s
diff --git a/archive/ES_0.5696398415515007 b/archive/ES_0.5696398415515007
new file mode 100644
index 0000000..f08d914
--- /dev/null
+++ b/archive/ES_0.5696398415515007
@@ -0,0 +1,22 @@
+archive/ES_0.5696398415515007---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T22:29:54.988
+Launch V∞: [6.081582669727113, -7.969789511462437, -0.10453833548730386] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.736772449135564e-7, 0.00024699922662855487, -0.0001592333545509671] km/s
+ V∞_out: [-0.00014522970627191907, -0.0002500920489259687, 5.214888876548676e-5] km/s
+ time of flight: 1.6991532020003414e8 seconds
+ arrival date: 2028-09-17T13:11:54.988
+ thrust profile: [0.04953136323785668 -0.02192706961384991 -0.023394922330742866; 0.02821551847280672 0.0005735754439303399 -0.038149305621040415; 0.05867864122824633 0.0100668036697503 -0.12152504263982776; 0.06231772902662159 0.01595177097697335 -0.17417411632551455; 0.05426117943142773 0.0163964813920439 -0.18920595260047499; 0.03989267722546427 0.012936622948545976 -0.16581262964833796; 0.024393582811213423 0.007908614572854938 -0.11812671980258867; 0.009031890056459381 0.0030752991333825876 -0.05200793335232204; 0.009481312748544753 0.0038272301514221023 -0.05533677295001079; 0.005669528834288603 0.0016327742105277472 -0.046041889616956364; 0.0029421252463416826 0.005969004215439548 -0.038916583416275005; 0.0005815397732325386 3.376049258858189e-5 -0.004362905792766868; -0.00041909398055031916 0.0008442163771635691 0.0009381472717162891; -0.0019829449990598205 0.004238895886634978 -0.006686321754841249; 1.6780218974525583e-5 0.004617172699624998 0.0004358049296588791; 0.005123371206055799 0.0008955883022886883 -0.002153502836437602; 0.004158453319657786 -0.0030540561892699104 -0.0024347282949446656; 0.0013113810358820694 0.005065321611346924 0.0012105674177559297; 0.0009652907805180313 -0.004154463463329266 -0.0030238265636004483; -0.0004740518469248629 -0.0009443954076937986 0.0039692080173671235] %
+
+Mass Used: 78.2474432890026 kg
+Launch C3: 100.51412088932828 km²/s²
+||V∞_in||: 0.00029387809206827333 km/s
diff --git a/archive/ES_0.5696699681842783 b/archive/ES_0.5696699681842783
new file mode 100644
index 0000000..cb6d7bd
--- /dev/null
+++ b/archive/ES_0.5696699681842783
@@ -0,0 +1,22 @@
+archive/ES_0.5696699681842783---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T02:22:18.831
+Launch V∞: [7.458160009670592, -5.773267087205727, -0.5121477903828789] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3093786551735795e-6, 2.332671704245062e-5, -0.00045150519920282464] km/s
+ V∞_out: [-1.8930062760453904e-5, 0.00045249555676124683, -4.854555394363561e-6] km/s
+ time of flight: 1.815031821594033e8 seconds
+ arrival date: 2030-02-05T19:55:20.831
+ thrust profile: [0.7687271939859782 -0.01870773194972288 -0.1773694461744846; 0.3161378497769775 0.1986596928124878 -0.2360587567218027; 0.1260087567534983 0.13867542355682833 -0.18087607109565929; 0.0234237956464292 0.03682746257343391 -0.05928365122233981; 0.02128592416779429 0.04376215668272925 -0.07468782784794781; 0.020600271515052643 0.05078564819609578 -0.09206091769148897; 0.01357300550802619 0.045409283260505084 -0.08561118700424956; 0.0011192417796989916 0.010425243861678623 -0.020686527907026752; 0.0007093565156696245 0.002871126232388356 -0.009215148457185168; 0.0038015845189509566 0.03137915198641237 -0.06757710038310509; -3.9126675089101053e-5 0.0005402031259571511 -0.0016813277449456774; 0.000690516428042157 0.00018373664362874567 0.0016135729643282186; 0.0002349851598580907 0.00036452000519434074 -0.0027498269446664114; -0.0028545706394788213 0.000796311731855955 -0.002175180813627303; 0.0027955716307904157 -0.0032022279878911085 -0.00036677262033965607; 0.0025326585583373045 0.0023955632057973504 0.0007599489153483751; -0.0033174738840312454 0.0028817663116878904 -0.0004930143020850759; 0.0011294375529773285 -0.00040839313981149957 -0.0016005311564528998; -0.0009580057753038112 -0.0014775494807219305 -0.0026197403744932274; -0.00020837098146317477 0.0008767554917773631 0.0004753442059071627] %
+
+Mass Used: 144.18211901099448 kg
+Launch C3: 89.2170589492566 km²/s²
+||V∞_in||: 0.0004521132754796456 km/s
diff --git a/archive/ES_0.5697189864128147 b/archive/ES_0.5697189864128147
new file mode 100644
index 0000000..27fb671
--- /dev/null
+++ b/archive/ES_0.5697189864128147
@@ -0,0 +1,22 @@
+archive/ES_0.5697189864128147---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T22:56:33.537
+Launch V∞: [5.741042971688384, -8.026186798611192, -0.2885114378294348] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00022036606093882153, -0.00013378555190765327, 9.987095444959576e-5] km/s
+ V∞_out: [-0.00014519521049420153, 0.00020184247052267956, -0.00012754085438027705] km/s
+ time of flight: 1.5968286738966006e8 seconds
+ arrival date: 2028-05-18T03:17:40.537
+ thrust profile: [0.26911991010681574 -0.129960729416309 -0.12051383964879828; 0.05022729117296297 0.0005565548542840671 -0.0604823645247168; 0.09498482656144323 0.020237515335331538 -0.1770189004732971; 0.10419789076503685 0.034803354783626304 -0.2607777187288274; 0.07625833345287072 0.031364431333721285 -0.23840341655839167; 0.034015361496404425 0.015448123143518344 -0.12838246624732588; 0.012490458459969003 0.006124870473399766 -0.05675694908040058; 0.020886517685455724 0.010939293037462895 -0.10109017180644084; 0.005814305128058543 0.0034330308792046545 -0.03252534237060835; 0.0038758957872229802 0.0025071206508205804 -0.023276678534099125; 0.0007802753422892459 -9.287203575677875e-5 -0.003644638030245683; 0.0002621357009596431 -0.0005006531216573602 -0.004038696953857494; -9.325134800420952e-5 0.00025544144003557343 -0.0007021879102288855; 1.2682272840279529e-5 0.0005297963978865104 -0.00016169564194561158; 0.0018312456400736725 -0.0003942988117296342 -0.000705204423931938; -0.0016358186076506427 0.0006737685485726848 -0.00046178791658379624; -0.0006277983663737031 0.002327933298768789 -0.0013593519151979862; 0.0003606149058828624 -0.000779463660703599 -0.0021030311866251754; -0.00021120802039615086 0.0021299336082466497 -0.0006030573513858718; 0.00017617901791623734 -0.0005636315464758765 0.0007039674253678601] %
+
+Mass Used: 96.14097210568298 kg
+Launch C3: 97.46248777873157 km²/s²
+||V∞_in||: 0.0002764669641306191 km/s
diff --git a/archive/ES_0.5697313954826122 b/archive/ES_0.5697313954826122
new file mode 100644
index 0000000..7bb2dfe
--- /dev/null
+++ b/archive/ES_0.5697313954826122
@@ -0,0 +1,22 @@
+archive/ES_0.5697313954826122---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:50:25.570
+Launch V∞: [7.268954064185742, -6.551998719229103, -0.2723565116500164] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.024622752020822116, 0.012612455754736665, 0.000944961060836446] km/s
+ V∞_out: [-0.021951385140471222, -0.010437095923180031, 0.013248558030420852] km/s
+ time of flight: 1.5600726115365773e8 seconds
+ arrival date: 2029-04-17T11:11:26.570
+ thrust profile: [0.37593630589065186 -0.08904530177277206 -0.14604289247874547; 0.16267409798554747 0.04219236989636151 -0.17922132656508705; 0.09992836395684196 0.04958873105861786 -0.18509286599413755; 0.06673520949411266 0.043531859551379094 -0.1732288500860705; 0.09213789045057062 0.07309629732348427 -0.3023045084215743; 0.029652081053830926 0.025361745012776066 -0.11883025758373394; 0.014116484344265231 0.012853341149559284 -0.06588796961946931; 0.004151500948081803 0.004251055264023694 -0.02335446311977403; 0.0004557211903570971 0.00174292178529649 -0.010118770938655076; 0.0017286276802503677 0.004815367067704263 -0.008619962427006515; 0.0014625802601756996 0.002198574442850382 -0.012576956238187591; 0.00038366914415967953 0.0035991040183607124 -0.006253868277120837; -0.001202815464121047 -0.002354497148249834 -0.001981573276591631; -0.00635028443597278 0.0005524209788932587 -0.0004436312561018991; -0.0017826526229135272 0.0022914002865881784 -0.004333569818512445; 0.002702012083949327 -0.0006205370909755691 -0.0023801069321659945; 0.0019977400633849817 -0.0033228360263746312 0.0033658207969078533; -0.0043802018278520545 0.0035233363606942416 0.0017750285992084464; 0.004923155574701758 0.007174994001142333 0.01747811998619484; -0.0009385763529199642 0.0027572746666506102 -0.0009023638353997461] %
+
+Mass Used: 105.61670363452868 kg
+Launch C3: 95.84055847346038 km²/s²
+||V∞_in||: 0.02768116523289052 km/s
diff --git a/archive/ES_0.5697577296621928 b/archive/ES_0.5697577296621928
new file mode 100644
index 0000000..3f3f9fd
--- /dev/null
+++ b/archive/ES_0.5697577296621928
@@ -0,0 +1,22 @@
+archive/ES_0.5697577296621928---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T03:52:37.495
+Launch V∞: [6.607267682861476, -7.174086889306231, 0.29284153260198476] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7354597706193096e-8, -8.375747215563669e-11, -6.870784607565356e-9] km/s
+ V∞_out: [-7.045052906497372e-9, 1.650974341579872e-8, 2.245554523153685e-8] km/s
+ time of flight: 1.874957778748312e8 seconds
+ arrival date: 2029-04-05T06:02:14.495
+ thrust profile: [0.4095802634792076 -0.08651434266463533 -0.11625329047623285; 0.12284990040924595 0.044237590867040315 -0.10962590352761298; 0.09125737503765406 0.061861107732114694 -0.1383143853344602; 0.05889932518852136 0.05353738557658377 -0.12586775758939472; 0.058383000194349464 0.06724025604944307 -0.16250264738088993; 0.02763515556932188 0.036485711066639226 -0.09600768191112644; 0.02085791061467023 0.03225581454139075 -0.08749249433692115; 0.0034471733535753153 0.00395741973469323 -0.0126689010144753; 0.0033109504791382846 0.007966587276315018 -0.021357366045037563; 0.0011664545717229061 0.0008736527262457731 -0.006798081084558176; 0.0004876335834594781 0.004324467424442003 -0.00791944438494497; -0.006956506531481195 0.0010318333070804364 -0.00507063869223913; -0.000407055593544251 -0.0006344914991275876 -0.001533125460835163; -0.0013744539410962154 -0.0009454809290230847 -0.003422549590527942; 0.0036408301270619454 -0.008535064750860428 -0.001198055164458551; 0.0008323494214479518 -0.0019924760550990447 -0.0006609082771348736; 0.008147673386289364 0.005119697412205909 -0.007756357442854063; 0.00020843044227585603 -0.0012980931412284885 0.0060042120526356095; 0.011272870750867253 0.0001623473113281562 -0.019522024606037962; 0.013576380592323006 0.0158733694596152 0.016852593564204047] %
+
+Mass Used: 109.32997157203727 kg
+Launch C3: 95.2092650915179 km²/s²
+||V∞_in||: 2.820440944436461e-8 km/s
diff --git a/archive/ES_0.5697666562143175 b/archive/ES_0.5697666562143175
new file mode 100644
index 0000000..1638136
--- /dev/null
+++ b/archive/ES_0.5697666562143175
@@ -0,0 +1,22 @@
+archive/ES_0.5697666562143175---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T22:45:16.870
+Launch V∞: [5.802086712049595, -7.881331783294456, -0.23162774624625906] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.319081556492524e-6, -9.544523853756837e-6, -1.558004534532458e-5] km/s
+ V∞_out: [-1.6303600821233002e-5, -1.1819607304232719e-5, -6.406989233388961e-7] km/s
+ time of flight: 1.6331460532400095e8 seconds
+ arrival date: 2028-06-28T03:55:21.870
+ thrust profile: [0.34199531684901385 -0.14772642993020987 -0.13222760141734; 0.13766850014870044 0.014766713574624342 -0.14105956227451244; 0.06329754503882234 0.021140382367970546 -0.10453841367146845; 0.0709106055437597 0.03485580506896962 -0.1585995891365604; 0.07919614189760399 0.049080716716043825 -0.21966798587392602; 0.04433164884451935 0.0308089631154848 -0.14710891971738604; 0.03697263859638531 0.028679511959863645 -0.14126316899943836; 0.0102255335493554 0.008338994009995455 -0.043440920745666495; 0.009429001792080371 0.008265066617983069 -0.044472335019735354; 0.005816369290550164 0.005358112097848144 -0.029792092610578635; 0.0017680302113701062 0.0017764278252879893 -0.00841836012434145; 0.001741873110177261 0.001074504026072602 -0.008660581400102351; 0.00046266600063771864 0.0008654732290082094 -0.006052323539628469; 7.16036634655498e-5 0.0012362642941440066 -0.007249891249981509; -0.0013930052202957579 0.00022537623956570398 -0.000531909298578405; 0.0007033508799011485 0.004758847462027593 -0.007781785197014186; -0.0034082785536129504 -0.0007277706530372105 -0.008296849536761547; -0.0009667627120181284 -0.0014369000958238327 -0.005550201294959566; -0.0019031158628638094 -0.00231096343721211 -0.003941993213166797; 0.0017029770616486242 -0.002530388495519757 0.00041880392608487993] %
+
+Mass Used: 105.70046046888137 kg
+Launch C3: 95.83325230534098 km²/s²
+||V∞_in||: 2.0075927537747228e-5 km/s
diff --git a/archive/ES_0.5697876152603203 b/archive/ES_0.5697876152603203
new file mode 100644
index 0000000..ad645ed
--- /dev/null
+++ b/archive/ES_0.5697876152603203
@@ -0,0 +1,22 @@
+archive/ES_0.5697876152603203---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T10:37:20.228
+Launch V∞: [6.23182988425798, -7.255598062336475, 0.13835389615350635] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.971911086213897e-6, 0.0003145948179778425, -0.00021696669781330158] km/s
+ V∞_out: [-0.00017674070110327515, -0.00033171166152582104, 6.870004086798679e-5] km/s
+ time of flight: 1.8749577787098873e8 seconds
+ arrival date: 2029-04-05T12:46:57.228
+ thrust profile: [0.6412162768501952 -0.13488221676029413 -0.1562065677917684; 0.15951266720940455 0.06001358979966095 -0.12518035809733685; 0.10541345528690177 0.07358382173695796 -0.1397093413714527; 0.06905186742240138 0.06684370643762241 -0.13126726157994045; 0.019020592740901475 0.023965516254415335 -0.05143395917282389; 0.029021722376781505 0.04398071176082624 -0.08955788785451713; 0.01911056011229531 0.03189503662286928 -0.08091654722213242; 0.02345871880092912 0.04443714407459322 -0.10145748778786284; 0.01123602719034423 0.018841397194663236 -0.048174845457891316; 0.0004643813476650663 0.0029984537341508207 -0.0039039394481999593; 0.001139888624358279 0.003421789896259961 -0.011385990239754363; 0.00045037790043905016 -0.001091854754352672 -0.0011210995065174508; 0.004436777547830111 -0.00014973539977660734 -0.00239706330798461; 0.0008288268263644164 0.0006164035617442522 -0.0007010676678180642; 0.015481783200656327 0.005593665498601959 0.002444868759659187; -0.0076133938530385005 0.0006877255899617044 0.004339339099137593; -0.0003974648752863276 0.004048946793979906 0.0032451253698004903; 0.01004395447757549 0.00015870519893314912 -0.017239788523471782; 0.002015344658447116 -4.94009359288986e-5 0.006035973865061978; 0.011392376112233904 -0.008680881259869377 -0.008084184580720343] %
+
+Mass Used: 131.01068343400084 kg
+Launch C3: 91.49854874909249 km²/s²
+||V∞_in||: 0.00038216917682359566 km/s
diff --git a/archive/ES_0.5698080488765028 b/archive/ES_0.5698080488765028
new file mode 100644
index 0000000..dd83801
--- /dev/null
+++ b/archive/ES_0.5698080488765028
@@ -0,0 +1,22 @@
+archive/ES_0.5698080488765028---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T07:34:38.516
+Launch V∞: [7.419528467116166, -6.488599366763568, -0.2193146210393606] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.2952344761103705e-9, 8.194704558692334e-9, -3.262535020202853e-8] km/s
+ V∞_out: [-9.610033473291056e-9, 3.277535045517657e-8, -5.1943545328590274e-9] km/s
+ time of flight: 1.5988400760909495e8 seconds
+ arrival date: 2029-06-02T19:48:05.516
+ thrust profile: [0.31309540412951015 -0.06680022118683687 -0.11644029050356407; 0.0379060582394537 0.011469363353044555 -0.04466660010430419; 0.10111833292821999 0.053077118687316016 -0.18518499889012657; 0.060174372342504244 0.042723670367423944 -0.15701351333995345; 0.044884985417115435 0.038197314814447464 -0.15077145622354113; 0.031998510451417904 0.031475107214193714 -0.13071010795908433; 0.009657016723804118 0.009249974667024326 -0.05023101752834743; 0.02276615051263867 0.01882812792439725 -0.10549488879122641; 0.011711294209848552 0.010626078639226225 -0.06361584780420035; 0.009618070379895014 0.013076594457407914 -0.05879275381007635; 0.005835925637159241 0.002656883680703194 -0.025242104348522303; 0.009534389917206431 0.011531105876877966 -0.06472610568304511; 0.002052183876395836 0.0033324524102637688 -0.018919573018180622; -0.004549397696606987 0.006094704561641557 0.0019491659392291572; 0.005468994042580529 -0.00028511302013838817 0.0003231514686547743; 0.003522171400384833 0.003834453635988432 -0.004017251871899547; 0.00042801666642421337 0.0011478641044846282 -0.005035373326384345; 0.000256942061984054 0.0005733286579196069 -0.0021118939072177862; -0.0005554370403840605 0.0031168486066749336 0.007190478831305044; 0.000527761129688633 -0.0016610024082900833 -0.009165523678418453] %
+
+Mass Used: 97.77942099092525 kg
+Launch C3: 97.19942331971338 km²/s²
+||V∞_in||: 3.3911881366477194e-8 km/s
diff --git a/archive/ES_0.5698124909159262 b/archive/ES_0.5698124909159262
new file mode 100644
index 0000000..e286c67
--- /dev/null
+++ b/archive/ES_0.5698124909159262
@@ -0,0 +1,22 @@
+archive/ES_0.5698124909159262---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T17:10:39.972
+Launch V∞: [7.646443909306588, -6.25622545664153, 0.0472854490350575] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7213044128113003e-8, -1.1325219355256735e-8, 9.605913171415926e-9] km/s
+ V∞_out: [-8.218525287682612e-9, -1.67674681888162e-8, -4.980299140909802e-10] km/s
+ time of flight: 1.6852952514131117e8 seconds
+ arrival date: 2029-09-12T06:56:04.972
+ thrust profile: [0.2262367891103743 -0.03330674208137784 -0.08144086967452246; 0.045122614633381075 0.016635039241748487 -0.05324510328263275; 0.13424841726497944 0.07735507475305349 -0.23827569920077346; 0.02979397955778011 0.024672599834097107 -0.0829737407009872; 0.040460233097041574 0.04150526382638932 -0.1465931236409045; 0.024873854518284205 0.03127393610224366 -0.11421843190428958; 0.02083572749728981 0.025545300499103408 -0.09725858949177725; 0.01695814683381509 0.016652310296864523 -0.08081477414977112; 0.012215379065520742 0.017312390298580033 -0.08294288341822775; 0.0028821052299522385 0.0032379390495184345 -0.013209772957700677; -0.0002708379043632285 0.0017950164369153142 -0.0017136900629116693; -0.006379723414674774 -0.0023036359837258265 -0.00872334394651266; 0.00017179755538729855 -0.0014742953325294196 -0.008262090881780497; 7.037997295652586e-5 0.00012405443803844727 -0.008600448922802793; -0.0014119048605973762 0.0005895775628935404 0.00790016292070055; 0.008279066936031455 -0.003305070105460681 0.01052722539092164; -0.002233044946373249 0.001346833441537063 -0.020913789446211063; -0.022699485543571866 -0.02297455222876947 -0.029121012116821204; -0.021046546537639023 -0.010816034493743448 0.012592422184946116; -0.009430494527739818 -0.01618529560805556 0.01209824179156331] %
+
+Mass Used: 95.38550494079527 kg
+Launch C3: 97.61069733619178 km²/s²
+||V∞_in||: 2.273374253082473e-8 km/s
diff --git a/archive/ES_0.5698192220056314 b/archive/ES_0.5698192220056314
new file mode 100644
index 0000000..3e18dd5
--- /dev/null
+++ b/archive/ES_0.5698192220056314
@@ -0,0 +1,22 @@
+archive/ES_0.5698192220056314---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T02:26:09.575
+Launch V∞: [7.903081661490054, -6.224214646638824, -0.11373027352988842] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008230644344250923, 0.00416637009886815, 0.00030275570582208756] km/s
+ V∞_out: [-0.00583692958734029, -0.003336991164369138, 0.006323091324544844] km/s
+ time of flight: 1.8749577786936948e8 seconds
+ arrival date: 2030-04-30T04:35:46.575
+ thrust profile: [0.1558328382420952 -0.0006863795153885049 -0.0628050619780735; 0.06417648305351342 0.031025526719879876 -0.08677094609868904; 0.020401212154336597 0.014685537857519786 -0.05104449543532627; 0.01610397592079764 0.01447736145462221 -0.05823499675972425; 0.015950227672063094 0.01649806329178643 -0.07444828823275196; 0.017864588732396814 0.019376755473692917 -0.0984607822552028; 0.021771833535033064 0.028829819459684887 -0.14776178305297902; 0.010441880586289474 0.013994052063723953 -0.09084646897356148; 0.0062792789525638075 0.00863827391185933 -0.055535246223853564; 0.0027078109514683335 0.003505335574442602 -0.025206631375282926; 0.001963569866116637 0.003107006058660413 -0.02499557180421679; -0.0007287759940937256 0.0005261376887130784 -0.00021646771311147148; 0.0006542447127750638 -0.0005036237752344933 -0.0030721426503590448; 0.001552265371222104 0.0005263501973010456 -0.00216409044334547; 0.0005008547370580917 -0.0007328804164842246 0.004017532853813864; -0.0003058483550675889 9.055421391808872e-6 0.008711020917083104; 0.005147355008198134 -0.010234315321061935 -0.007664845727475102; 0.000905699752393287 -0.0016437908243699486 0.011724561042528673; 0.005001754135184241 0.0028451300939553534 -0.004437794384578658; -0.0037281354270525873 -0.001918940015572866 0.011798687606106998] %
+
+Mass Used: 74.38294564397347 kg
+Launch C3: 101.21248229073083 km²/s²
+||V∞_in||: 0.009230049140698013 km/s
diff --git a/archive/ES_0.5698261051026632 b/archive/ES_0.5698261051026632
new file mode 100644
index 0000000..272a3a3
--- /dev/null
+++ b/archive/ES_0.5698261051026632
@@ -0,0 +1,22 @@
+archive/ES_0.5698261051026632---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T06:41:31.165
+Launch V∞: [5.788627515361349, -7.355162172988974, -0.04109642920034422] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.411215236192522e-8, -1.2104391931927014e-8, 1.695382288628158e-8] km/s
+ V∞_out: [-5.27327101938303e-8, 1.3868267974285554e-8, -6.740090428318713e-9] km/s
+ time of flight: 1.8334551166145658e8 seconds
+ arrival date: 2029-02-14T08:00:02.165
+ thrust profile: [0.8393686648259115 -0.1976975101626804 -0.1971901626602714; 0.3058758552600402 0.10854351774117099 -0.21843860031082674; 0.10830897011562442 0.07303637126845602 -0.13535209012584903; 0.13441396889671126 0.12595310123562642 -0.2282627568605587; 0.04241429234365944 0.048922568935074816 -0.09755436903545046; 0.02557714564064296 0.03554545898575769 -0.07434791678876453; 0.017817615463504063 0.028554573028556154 -0.0622759950713029; 0.0011954760272696314 0.0024051207020588353 -0.008169416424012269; -0.0009683041212691771 0.0022047275478982204 -0.005580495627281473; 0.001275324995385725 0.0022829211974653963 -0.007396900845111727; 0.000730497764548186 0.0010955311403512496 -0.0038313225224826607; -0.002490160985078598 0.001875926081587587 -0.002578526817268268; -0.0005098418235182877 0.00011085290212253351 0.0005199415900168916; -0.0026258145624709363 0.0011374600269378036 -0.0003115571713609522; 4.341244514786941e-5 -0.0006977426719790783 0.004295128289059875; 0.004849473845143914 5.000913485080668e-6 -0.0006829286270236584; 0.0006541658037458013 0.0007489227794560397 -0.0016682075495466206; 0.0003528539358997681 -0.0011293631434248334 0.0032026763647692255; -0.0027583265434080436 0.0005444718524899351 -0.00371762228600257; -0.00027695841048851417 0.010043770991167624 0.018495681585188727] %
+
+Mass Used: 153.7486591752604 kg
+Launch C3: 87.60830801905941 km²/s²
+||V∞_in||: 5.7983389412324924e-8 km/s
diff --git a/archive/ES_0.5698623679465354 b/archive/ES_0.5698623679465354
new file mode 100644
index 0000000..8d68abb
--- /dev/null
+++ b/archive/ES_0.5698623679465354
@@ -0,0 +1,22 @@
+archive/ES_0.5698623679465354---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T11:00:35.346
+Launch V∞: [7.02015397140948, -6.420793179812477, 0.0415025502495389] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005279269462223794, 0.0003561090534904898, -0.00018026728355313235] km/s
+ V∞_out: [-0.0002701041531647996, -0.0005062340187918127, 0.00032982809631227267] km/s
+ time of flight: 1.594560913039872e8 seconds
+ arrival date: 2029-05-25T00:22:06.346
+ thrust profile: [0.6636723773895029 -0.11698437304093566 -0.18894575647481657; 0.4587857943377432 0.17576906915300242 -0.3727362796791737; 0.09781984450512123 0.06580156547899363 -0.15222345418034153; 0.06857261410404497 0.06249940416354104 -0.15240776834771233; 0.04057677296962862 0.04495463899872611 -0.11905634584424406; 0.015716787094504994 0.019959461730696505 -0.058924319514747116; 0.022389944533077754 0.0296556241604557 -0.09399167030565822; 0.010745573437833894 0.01710774285857777 -0.05591821911769295; 0.006559305665768731 0.012821452078280096 -0.0415726989222872; 0.0060302877409064105 0.010589573605253694 -0.037489908736332976; -9.849389951939374e-5 -0.00020268642768372707 0.0004995968582108525; -0.0004569502780967316 -0.0010619064663003309 -0.0014089813295018257; -0.0014638754880164902 -0.0012578513528674522 -0.00020965319993469333; -0.0023223404558523437 0.002541528096281717 -0.0020119113007718275; 0.00010379131101260228 0.0006293598431361029 -0.0007091238197857688; -0.0009789897360541451 -0.00041543008580859596 0.0004275471278545814; -0.00044820618547782926 0.0034071497144176127 -0.0033418793560592696; -0.001210992675372976 0.00213853551889829 -0.0008115561031489657; 0.0022790183607704012 0.003507688534715699 -0.0010747901271216263; 0.0008013670909377639 0.003365192532235407 0.0022705736929994843] %
+
+Mass Used: 136.85935834320844 kg
+Launch C3: 90.51086930189993 km²/s²
+||V∞_in||: 0.0006618283856448022 km/s
diff --git a/archive/ES_0.5698799506517693 b/archive/ES_0.5698799506517693
new file mode 100644
index 0000000..123be60
--- /dev/null
+++ b/archive/ES_0.5698799506517693
@@ -0,0 +1,22 @@
+archive/ES_0.5698799506517693---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T22:35:44.929
+Launch V∞: [7.210109049008092, -6.568042324883352, 0.4313850305458192] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005246487017492496, 0.008555107108166014, -0.00012838448642125605] km/s
+ V∞_out: [0.00827717646170208, -0.001351611546525424, 0.0017552480871939914] km/s
+ time of flight: 1.577994441360721e8 seconds
+ arrival date: 2029-05-09T07:46:28.929
+ thrust profile: [0.4835180231476179 -0.10121702195933273 -0.1712436833362843; 0.08085924447272164 0.021766147371047775 -0.09071659330173788; 0.11936556305297806 0.06187238963873864 -0.21666380669417631; 0.07262998857145718 0.04885908988309195 -0.18696930303723872; 0.04479650243285796 0.034671619212066476 -0.147457146868397; 0.029929372897370115 0.02524335767087925 -0.11868905517816312; 0.01563993213921112 0.013910815353405076 -0.0713750656485927; 0.020973496044965494 0.0203584568102213 -0.10618343000489633; 0.017630191431573457 0.018190765227395697 -0.09778831391689907; 0.00485083247568 0.004330247061802739 -0.029455588842532222; -0.0019678011114540135 0.00020924379804210973 -0.0022171121001499147; 0.0008789751527913291 0.0003429296604650681 -0.0010933651649397856; 0.0002829485941361843 0.002669236476335137 -0.0019983050937544735; 0.0005546224411777214 -0.0006836187305265825 -0.004155824716936949; 0.0009229927406828032 0.001188164974447422 -0.0005320535663282512; 0.0020517212309832866 -0.0004691547647993755 0.00015486850651857888; -0.00023394668647311345 -0.00033631396312217487 0.0012854763308229665; 0.0007771709148433461 0.0013402333854535065 0.0014464001087328322; -0.0007124558311604988 0.00103401084211888 -0.0014207467573151406; -0.0014118838379463764 0.004836369337724271 0.0018132130395951294] %
+
+Mass Used: 108.87942686674296 kg
+Launch C3: 95.31094552462649 km²/s²
+||V∞_in||: 0.008572140716810095 km/s
diff --git a/archive/ES_0.5698855876412106 b/archive/ES_0.5698855876412106
new file mode 100644
index 0000000..c7208f9
--- /dev/null
+++ b/archive/ES_0.5698855876412106
@@ -0,0 +1,22 @@
+archive/ES_0.5698855876412106---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T12:01:47.463
+Launch V∞: [6.154963939559629, -7.647294749025836, 0.15406118016973472] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.813024257847367e-6, -7.776668080604127e-6, -1.2073511421237415e-5] km/s
+ V∞_out: [-1.4150694700522905e-5, -9.13770064615576e-6, -3.901036670060392e-7] km/s
+ time of flight: 1.7134187372066528e8 seconds
+ arrival date: 2028-09-29T14:59:40.463
+ thrust profile: [0.32260581808090594 -0.11678528555690239 -0.11847648375828292; 0.08104416381975614 0.01343331795688712 -0.08413982775546239; 0.06443982398427248 0.025831305992307093 -0.10829192002848849; 0.08316316283966727 0.0472813169507752 -0.1890890701476135; 0.050678287319213464 0.03494124130469602 -0.14630054527878167; 0.022651949156847692 0.018245438268965214 -0.08112597652504128; 0.02796079098352275 0.025078814315364725 -0.11225411250510495; 0.008216145748808886 0.008207211691971958 -0.03978968345668052; 0.010215749851167272 0.010698343120945848 -0.053301834008142715; 0.024376213517181753 0.026771283974024444 -0.1328546470950029; 0.002757936469525896 0.0015086760417655143 -0.017344088887482047; 0.0024016505620999967 -0.0011106951628024682 -0.0030875558158079994; 0.004862744464484052 0.0032811370094094575 -0.018244241360148315; -0.0018756577144330181 0.0015116655918034968 -0.005086581762008251; -0.004081784339692252 0.003294952399001982 0.001732267204214447; 5.2076551188950135e-5 -0.002220363575029078 0.00709894025274865; 0.0025530760992930864 -0.00013896620803890416 -0.0018689155644998068; -0.004934059765543652 -0.003736837520245959 -0.0054261952232572755; -0.0021655745703256296 0.00037014691290395156 0.010035612407128084; 0.003754456428362889 -4.5522475965528155e-5 0.0008245918079233731] %
+
+Mass Used: 102.60066019728765 kg
+Launch C3: 96.38843292299279 km²/s²
+||V∞_in||: 1.6849796468920433e-5 km/s
diff --git a/archive/ES_0.5698865158967972 b/archive/ES_0.5698865158967972
new file mode 100644
index 0000000..980540a
--- /dev/null
+++ b/archive/ES_0.5698865158967972
@@ -0,0 +1,22 @@
+archive/ES_0.5698865158967972---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:02:26.698
+Launch V∞: [6.3215070072467805, -7.353664298422573, 0.2159481725469835] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.749189898952577e-6, 7.4791368983173256e-6, 8.340001249728683e-6] km/s
+ V∞_out: [1.1496994966701107e-5, 7.298279110897246e-6, 2.3240300250917808e-7] km/s
+ time of flight: 1.8749577787959114e8 seconds
+ arrival date: 2029-04-09T06:12:03.698
+ thrust profile: [0.5207995391291658 -0.12921317648130715 -0.17138086198486666; 0.09212268678868725 0.025175047948511664 -0.09796885540001646; 0.05005043363920134 0.025592276879063985 -0.09255544263303049; 0.03347853617558854 0.023882477495187116 -0.08452292843360172; 0.046422572656719015 0.04123978733585015 -0.14904725342708175; 0.0370482985012593 0.03286591865113336 -0.13766153361399971; 0.01404902662252142 0.01818520298932609 -0.0703763844548666; 0.011874013225371217 0.014554242479385382 -0.07231010461811581; 0.0056572112755808625 0.006480668177859764 -0.030603415610903417; 0.003260113575444255 -0.0007254328704362463 -0.006476838650088634; 0.0013122050429426914 0.0021327928233496555 -0.009113561349802264; 0.0017122643516650983 0.00047884439937735364 -0.012784701170645672; -0.0009339102137396913 -0.005703725150068447 -0.00807372905276586; -0.003701512857193272 0.0006784802072299055 -0.008025336068278321; 0.021439538105728486 -0.0042511874893907346 -0.00122063795083472; 0.006967672827752929 -0.00993764046618292 -0.00044057340884591165; 0.0009164025807173134 0.018687280878568857 0.019958150242024526; -0.0005062210360959616 0.010346337950167433 -0.00038438816727307673; 0.02329577221274958 0.0035553888913667374 0.0326632326166178; -0.0009392332357630625 0.002803712429011185 0.0010013383053516858] %
+
+Mass Used: 116.04156730581417 kg
+Launch C3: 94.08446306979128 km²/s²
+||V∞_in||: 1.3621418930466693e-5 km/s
diff --git a/archive/ES_0.5698875693162002 b/archive/ES_0.5698875693162002
new file mode 100644
index 0000000..3f4aeba
--- /dev/null
+++ b/archive/ES_0.5698875693162002
@@ -0,0 +1,22 @@
+archive/ES_0.5698875693162002---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:27:29.995
+Launch V∞: [6.377819099751107, -7.495587538841766, 0.12623095765500308] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.119081567566936e-7, -2.5325146240998427e-6, 1.464063454564106e-7] km/s
+ V∞_out: [-9.165268429560143e-7, 2.081108600464648e-6, -1.1926123439988911e-6] km/s
+ time of flight: 1.8367095954921642e8 seconds
+ arrival date: 2029-02-23T15:10:08.995
+ thrust profile: [0.28685266291300365 -0.07397889126483473 -0.09882558132267086; 0.08395945659702296 0.023037410836314522 -0.09199137563342126; 0.04809678152962336 0.02462734804673597 -0.0892091264789075; 0.058540025723618626 0.041075569504478965 -0.14636754257228096; 0.02536159798235968 0.021056882773642347 -0.08199647269594884; 0.027159750646498886 0.02578224418998293 -0.1063344364769244; 0.025883726494347285 0.029482149811667274 -0.12138088283084479; 0.015318475851835855 0.01877355515402741 -0.0819740506029393; 0.011374412297314946 0.01450596167248371 -0.06809608468731174; 0.00777190059102827 0.010728755882114223 -0.053072797834256134; -0.0021360363281450407 0.004534049186642419 0.0034060546378255467; -0.0034435291576857792 -0.004263079657657212 -0.00027749535245414443; -0.001686288220089803 -0.004100877360641851 0.014672791978182232; 0.0012805643451090816 -0.0010988931197434167 0.0025146873909094427; -0.0013030701582386406 0.00133562067161442 -0.004766363896371665; 0.0039618024891738745 0.014201696486620834 -0.003646390903031498; -0.003360200905133833 0.0011910130953551126 -0.0007906544134783709; 0.021745800013870605 -0.008767106975148316 -0.031216403182269883; -0.0015094529292925022 0.0006649479035468515 -0.005977193071888438; 0.00020819741454685173 -0.0057034963653956735 0.01847443142284759] %
+
+Mass Used: 99.7568284240474 kg
+Launch C3: 96.87634327626049 km²/s²
+||V∞_in||: 2.569967600743668e-6 km/s
diff --git a/archive/ES_0.5699143378524071 b/archive/ES_0.5699143378524071
new file mode 100644
index 0000000..e31e1a2
--- /dev/null
+++ b/archive/ES_0.5699143378524071
@@ -0,0 +1,22 @@
+archive/ES_0.5699143378524071---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T14:23:10.422
+Launch V∞: [6.530215432202332, -7.5365041937298525, 0.006867214416325724] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011776181183744228, -0.00035949850308734216, 0.008375128370585478] km/s
+ V∞_out: [-0.013865482617126702, 0.00013594522902736714, 0.004079549581168154] km/s
+ time of flight: 1.8462992494047046e8 seconds
+ arrival date: 2029-03-08T12:28:34.422
+ thrust profile: [0.11982318847274943 -0.034894582503583856 -0.04699818227748276; 0.030685550258392688 0.006218033558704997 -0.03309703934020341; 0.04020450948496507 0.01634953485984035 -0.075847914997108; 0.05358261966073662 0.03274718557418018 -0.1495591375570047; 0.047791044203080675 0.031061400204490983 -0.168196980576039; 0.03478768985674056 0.028145354726984786 -0.1395026732446492; 0.01850043877218814 0.014360337687890972 -0.08414025832871572; 0.013953450200463256 0.01335610225486173 -0.07899777858079665; 0.0033306534286376916 0.0055561055779314895 -0.018398753020672756; 0.006185688269932699 0.006144284145275493 -0.038546337795832136; -0.0023991853444023763 -0.0005737115264207337 -0.00963427685155943; 0.002776916545391543 0.0013552347802512994 -0.012591710854803664; 0.0033538996637995483 -0.0073301323011244635 -0.01734411806826812; 0.000798886830314993 0.00197746406562419 -0.005071586602220157; 0.005618829400233477 0.012823645238795166 0.00017425162516486632; 0.01928719354358299 -0.015541808958964815 -0.006939254511178049; 0.003756684696607419 0.0015209501358445809 -0.006358157433998994; 0.00012635376266087418 -0.0011342937842949766 -0.0044668247703137515; 0.010038852838036587 0.013216562807954232 -0.0004293544591359706; -0.016044077387057855 -0.015554697516202143 -0.05286097324128673] %
+
+Mass Used: 84.81789959280422 kg
+Launch C3: 99.44265621171498 km²/s²
+||V∞_in||: 0.014455118735931553 km/s
diff --git a/archive/ES_0.5699636173622582 b/archive/ES_0.5699636173622582
new file mode 100644
index 0000000..69abeaa
--- /dev/null
+++ b/archive/ES_0.5699636173622582
@@ -0,0 +1,22 @@
+archive/ES_0.5699636173622582---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T10:46:26.501
+Launch V∞: [7.7291745996184265, -6.3355950820998, 0.08966193619351534] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.708858799971501e-7, -5.590106298228279e-6, 1.0785956853926132e-6] km/s
+ V∞_out: [-1.0748841896297538e-6, 3.530651326445433e-6, 4.421460040826732e-6] km/s
+ time of flight: 1.8749577787482724e8 seconds
+ arrival date: 2030-04-30T12:56:03.501
+ thrust profile: [0.28152258621644205 -0.010501352142652522 -0.09863404520069571; 0.08539470745643896 0.03799285214525278 -0.10922509197803128; 0.05093392709770548 0.03423249518105 -0.11650048648706038; 0.035961431275166926 0.029414943260152322 -0.11836774286865401; 0.025997293572265778 0.02387997193323756 -0.11085224506106461; 0.017992438258127384 0.01772410623190248 -0.09315532139352409; 0.011311093298754992 0.01162503129114527 -0.06786299211580224; 0.005435776408838082 0.005943140222567151 -0.03563874405608734; -0.0006255651869191631 0.0015958931078795678 -0.013443361615673837; 0.0009409178850898269 0.0013029441637331383 -0.01067456006070113; 0.002431994894930954 -0.0007132011752755299 -0.003225864980259133; 5.686906415922143e-5 0.0010281390695229793 -0.0011619042962497967; 0.0001437227672631701 0.0025717368552862618 -0.018401521659342224; 0.0005679492933464751 0.00520183310825256 -0.006595036158504763; 0.0011652123874560175 0.001168601452571325 -0.000944064476742845; 0.00012813123474333596 -0.0016627980378633887 -0.004514133469944422; -0.0001654623768302854 -0.00023583615167806335 -0.0013677486224507266; 0.0003435166960481649 -0.00022484959139205257 -0.004068517279416862; 0.0020589384870004883 0.00250086235203688 -0.00437708030199746; -0.0003016345261818861 -0.0008529899966414116 0.007098947037629451] %
+
+Mass Used: 82.27787851462563 kg
+Launch C3: 99.88794429851582 km²/s²
+||V∞_in||: 5.759435674961345e-6 km/s
diff --git a/archive/ES_0.5699656931956888 b/archive/ES_0.5699656931956888
new file mode 100644
index 0000000..3bc159d
--- /dev/null
+++ b/archive/ES_0.5699656931956888
@@ -0,0 +1,22 @@
+archive/ES_0.5699656931956888---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T10:04:55.060
+Launch V∞: [6.562957902012872, -7.4914408879759895, -0.935701243750285] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.010616712242992831, 0.00016521006972421474, -0.008307713752333074] km/s
+ V∞_out: [0.013214415560683807, -8.286009749869189e-5, -0.002709898034716542] km/s
+ time of flight: 1.823723607015188e8 seconds
+ arrival date: 2029-02-09T05:04:15.060
+ thrust profile: [0.1226501617728119 -0.04331436639651164 -0.058074935086210894; 0.04739822965285082 0.007317115268154732 -0.0671280443629736; 0.04647129513638971 0.016055920414548064 -0.11154652556473034; 0.04079719934188572 0.018941844254236263 -0.1389580293197993; 0.032919498655184946 0.018076453835102296 -0.14440473868159417; 0.02492000917224244 0.015325180706039497 -0.1325273912910489; 0.01740298182380808 0.011770668251111923 -0.10830904195532558; 0.00987554380309788 0.0077879565083564355 -0.07357294412584739; 0.003571712173724957 0.003410074798358895 -0.03240165423381182; 0.004499522184746584 0.003695962905160967 -0.04302699563284311; 0.006417936970012889 -0.005167171189675807 -0.010781844174809848; -0.0007267041888668097 0.0013816146527123965 -0.009207871959657731; 0.001326562231660265 2.1421491482481812e-5 0.0017250952633420047; 0.0014554186710367379 -0.0005540861656035271 0.0012586303945947425; -0.005815587483737601 0.0026206484195651918 -0.0073344396111657585; 0.0009279353234721626 0.003746321210923926 0.003475847523387264; -0.0031023667578727737 0.0004066515266657783 0.0074463631583525985; 0.011681224196515218 -0.006680374091871831 -0.004351410222292257; 0.0070317971010452045 -0.0021868964580948596 -0.011160871523475096; -0.0010693491745138437 9.368502778477885e-5 0.001513529385926813] %
+
+Mass Used: 81.22040978304312 kg
+Launch C3: 100.06963981918751 km²/s²
+||V∞_in||: 0.013481838932740452 km/s
diff --git a/archive/ES_0.5699665099762419 b/archive/ES_0.5699665099762419
new file mode 100644
index 0000000..7ba69b4
--- /dev/null
+++ b/archive/ES_0.5699665099762419
@@ -0,0 +1,22 @@
+archive/ES_0.5699665099762419---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T22:17:25.185
+Launch V∞: [7.630464843112167, -6.179781125429389, -0.200434273482433] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.938119670494699e-7, -2.2940612637468577e-6, 5.797843076800532e-5] km/s
+ V∞_out: [2.5078757405110834e-6, -5.8002312982468865e-5, 4.242890497056564e-7] km/s
+ time of flight: 1.8749577779263452e8 seconds
+ arrival date: 2030-04-30T00:27:02.185
+ thrust profile: [0.6452782176046463 -0.07065278943845275 -0.23597640228942085; 0.004651710511386926 0.0009847966714247236 -0.007331054870965632; 0.019593754430768308 0.007596243795548255 -0.05326423031722489; 0.02904934096114447 0.011928085845367826 -0.10655353467463624; 0.026659418806667286 0.010852011756909287 -0.12161007133056054; 0.016380276659755735 0.0060441052259729115 -0.08967274697960172; 0.00947139544398502 0.003120714109735722 -0.060005555499261704; 0.008298774007152567 0.002416612023994441 -0.05787417172337612; 0.0072210592815383536 0.002399673166627906 -0.05695979813427333; 0.0030964116669532625 0.0004398672820806631 -0.029109047726809924; 0.0029078462500606033 0.00044091821285657156 -0.030929517390580627; 0.0012441876028058154 9.236116031391395e-6 -0.01063300989277643; -4.889613545017835e-5 -0.0001505575071029556 0.0008368847954286317; 0.00017047117023151573 -8.441251298663358e-5 0.00043138886955742704; 0.00028137985886079813 -0.0005117229433097704 -0.0014876088062574066; 0.0003901572070872852 0.0016054420042741788 0.0008806801983840277; 0.004935068599170672 0.0038321203127771814 -0.008195792047785639; 0.0007777362406714043 0.005972672294810288 0.0017041031393990745; 0.005690398160301235 0.006596868976234836 0.0035631921230476755; 0.004782130220415877 -0.005985751347821317 0.0003663012257736846] %
+
+Mass Used: 102.31339776628738 kg
+Launch C3: 96.45386237817054 km²/s²
+||V∞_in||: 5.8025134547604463e-5 km/s
diff --git a/archive/ES_0.5699672785669578 b/archive/ES_0.5699672785669578
new file mode 100644
index 0000000..a9e3c9c
--- /dev/null
+++ b/archive/ES_0.5699672785669578
@@ -0,0 +1,22 @@
+archive/ES_0.5699672785669578---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T03:56:16.810
+Launch V∞: [6.607585295683914, -7.34660384923168, -1.0869052517508533] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.867067076631264e-9, -1.6634438967751909e-9, 1.957663631588248e-9] km/s
+ V∞_out: [9.270438061209936e-10, -2.1737117533192285e-9, -3.0511000138591117e-9] km/s
+ time of flight: 1.8521993912980357e8 seconds
+ arrival date: 2029-03-12T21:55:15.810
+ thrust profile: [0.19778276895555005 -0.059512424299094875 -0.06465598807926035; 0.07575125861225232 0.01472864873759801 -0.07817840549336023; 0.05628076169520858 0.02216313805293449 -0.0965176520118484; 0.06174608678668755 0.03740660603515332 -0.1449986007561956; 0.034750898149332195 0.023141760135479115 -0.1027506136629936; 0.03923258418764648 0.030206492152532842 -0.14079241569818673; 0.02516951479555478 0.02152889389559195 -0.10485829412254787; 0.014099265203666137 0.013073887036390503 -0.06925570949353425; 0.012073025322889498 0.011649682125666042 -0.06614758714454133; 0.0056921772538619944 0.006698146697396146 -0.03860579333547916; 0.0015371668407598987 0.003348883046309463 -0.019020782476058855; 0.0001594450492723163 0.0018626815298368243 -0.010103969269487643; -0.0003489938148337634 0.00076987384930816 -0.00377666942555124; -0.0004853988822073911 -0.0003297807662497301 0.002172552323533399; -0.00031080142365036005 0.00040776447076608174 -0.002370222795160675; -0.0013347714193266392 -2.7751872182865114e-5 0.002058802368110127; -0.0020121089823795578 0.000394409918222858 -0.0002729110511742582; -0.0011467510769704497 -0.000318121309535268 0.003428397277999602; 0.00022465275161779425 0.0001973315228223158 -0.0015841948055036218; -0.00037726849232689414 -4.519788289401493e-5 0.0005034944531968014] %
+
+Mass Used: 88.54603992397324 kg
+Launch C3: 98.8141345835676 km²/s²
+||V∞_in||: 3.8496189569962455e-9 km/s
diff --git a/archive/ES_0.5699847394786715 b/archive/ES_0.5699847394786715
new file mode 100644
index 0000000..760f1b4
--- /dev/null
+++ b/archive/ES_0.5699847394786715
@@ -0,0 +1,22 @@
+archive/ES_0.5699847394786715---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T05:41:41.203
+Launch V∞: [7.291712056672383, -6.561659450988906, -0.4236190736402045] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000719988425450627, -0.002634011085526185, -0.003984822571875509] km/s
+ V∞_out: [-0.0042214031412372574, -0.00047200254239785055, 0.002300790453889636] km/s
+ time of flight: 1.540710470592116e8 seconds
+ arrival date: 2029-03-25T11:12:28.203
+ thrust profile: [0.37826620345438056 -0.09018074970550077 -0.14849969468609553; 0.11179443247332786 0.030578091261484114 -0.12503174426175187; 0.101698835639847 0.05351762643499593 -0.18795076171895447; 0.08529846065964233 0.05984309903352712 -0.2189537087913185; 0.06014584490752168 0.050603179620831704 -0.19808508625975574; 0.03697858919331607 0.03533945337592071 -0.14887627414157764; 0.01718280765336273 0.018020466748847646 -0.08196650303925701; 0.010533568191941177 0.011015423354981544 -0.05398017880087527; 0.008748679043097571 0.01054995494018707 -0.05214054547341182; 0.004153719209418489 0.004934715874156071 -0.026849519621429528; 0.0007275331459679468 0.0012378678398102072 -0.006724346121881422; 0.00043706221797644825 -0.0005518187216706639 -0.0006408769225946568; -0.00047409620976313153 -0.001434074413803204 0.00045336910944253654; -0.001877149546347769 0.0005149655545647193 0.0011797851085825466; 0.003775213070762221 -0.0005550521286070841 -0.0007733921877210038; -0.001373767867448626 0.0007760668911218253 -0.004616792595528414; 0.0030227495254236503 0.00033789344742634004 -0.0009262110414090593; -0.000409389927280487 -0.002818968234416611 0.000527428166049979; -0.0004167934447011773 -0.0006020903081589125 -0.0004668538688500281; -0.00046075466925690495 0.001288312901102841 -0.0015573278856329277] %
+
+Mass Used: 102.62615596338628 kg
+Launch C3: 96.40389258772521 km²/s²
+||V∞_in||: 0.004830653026329489 km/s
diff --git a/archive/ES_0.5699963140945987 b/archive/ES_0.5699963140945987
new file mode 100644
index 0000000..f598b45
--- /dev/null
+++ b/archive/ES_0.5699963140945987
@@ -0,0 +1,22 @@
+archive/ES_0.5699963140945987---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T05:48:12.708
+Launch V∞: [5.748018719707337, -7.749427724950826, 0.005862958541469324] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005564522786953079, 0.003921709418064864, 0.005126298820229349] km/s
+ V∞_out: [-0.0034820990427067927, -0.006418272092112782, 0.004392071107691094] km/s
+ time of flight: 1.6379021918185678e8 seconds
+ arrival date: 2028-07-01T23:05:11.708
+ thrust profile: [0.5961006512061596 -0.23944925677285384 -0.18709685558988376; 0.11002361347538403 0.01603148309379614 -0.1041868817727516; 0.0654627070438002 0.025409003446025896 -0.09963060089400562; 0.09640374760825593 0.050924214656385525 -0.19852181908872019; 0.03054045724573403 0.020725900780016196 -0.07918258213042728; 0.059904807880308414 0.05079214263716602 -0.18106737533478945; 0.06315503704643485 0.05529408708208521 -0.21098799977879726; 0.028383579782533298 0.02903737297156905 -0.11223228702417913; 0.005305578907113766 0.004946254377502117 -0.02499562122588717; 0.001209846160243968 0.0017582241929747586 -0.008811621112038643; 0.0016029706759823582 0.000604390059253199 -0.004665532266291271; 0.0012874762001999626 0.000848767517413284 -0.006688839671163223; 0.000506399926385441 0.0012963168727666255 -0.0011703172320935498; 0.0010674468655646127 0.00228858005681664 0.0006767364136172607; -0.00014565875716142458 0.0020555256460020317 0.002920255355513076; -0.0017298479413208312 -0.004602201613766885 0.0004929843829086643; -0.001135959003590516 -0.0009469733173403069 -0.0013113090787884012; 8.463903525886046e-5 0.0009813171312303523 0.002275699211606534; -0.0012292836719697904 -0.0012081825895919555 -0.0006045352096159755; 0.0015657149560794133 0.002138832277837391 -0.0004933336447011081] %
+
+Mass Used: 121.95096187338368 kg
+Launch C3: 93.09338364062539 km²/s²
+||V∞_in||: 0.008521892876617468 km/s
diff --git a/archive/ES_0.5699971273170893 b/archive/ES_0.5699971273170893
new file mode 100644
index 0000000..7788ac9
--- /dev/null
+++ b/archive/ES_0.5699971273170893
@@ -0,0 +1,22 @@
+archive/ES_0.5699971273170893---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T10:52:33.859
+Launch V∞: [6.215720084493216, -7.285982053377673, 0.23736489939360406] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.59183246701151e-7, 4.21652735750328e-8, -5.365415802474178e-8] km/s
+ V∞_out: [1.7064412604825325e-7, -3.010322846888676e-8, 1.3795945154113958e-8] km/s
+ time of flight: 1.8488031514242095e8 seconds
+ arrival date: 2029-03-04T06:31:08.859
+ thrust profile: [0.591560903739356 -0.12498595258028142 -0.12508392064472332; 0.24084853214132906 0.09797697016770712 -0.1686525928269433; 0.09585290501227715 0.07136532138624901 -0.11677264945724272; 0.03656917282512784 0.03805088191952957 -0.0653524552328722; 0.03826084747530233 0.04722658017203444 -0.08505850332467166; 0.04775041689260092 0.07424753669156323 -0.13307905892490624; 0.02060336994337085 0.03654552874609922 -0.0724471997083072; 0.02135222504451435 0.043241704338912695 -0.0859631380064461; 0.010905407872008992 0.02238786195095898 -0.049390130090409386; 0.0065549496150504654 0.016049734324568708 -0.03573870709519842; 0.00047797797732867164 0.0014940883698503257 -0.003741610112887385; 0.00015186978689573372 0.00043927686268153726 -0.0008424350951316624; -0.0010577688943987872 0.0006120883422490387 -0.003874692001972085; 0.001505602904928468 0.00263183939567638 -0.007266346846793276; -0.0008970476959113279 2.4182554042958125e-5 0.0003180368125854324; 0.0015965194075533238 -0.0025017631996486676 -0.0054578713233552475; 0.0004084106858745261 0.0014950250622424235 -0.003264654903172251; -0.0026022349293038176 -0.0027040741954285816 0.005512295808238207; -0.0008341709088586752 0.0011009583465543325 0.004019926764543289; -0.0002408609258924625 0.0003255429427431863 0.0021858231385490433] %
+
+Mass Used: 129.6305075160658 kg
+Launch C3: 91.777052746378 km²/s²
+||V∞_in||: 1.731934900604547e-7 km/s
diff --git a/archive/ES_0.5700048556044037 b/archive/ES_0.5700048556044037
new file mode 100644
index 0000000..e0ef7b3
--- /dev/null
+++ b/archive/ES_0.5700048556044037
@@ -0,0 +1,22 @@
+archive/ES_0.5700048556044037---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T16:48:51.029
+Launch V∞: [6.157210996313146, -7.787700765048301, -0.40943174392521847] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6204737252951682e-6, -1.5027277287046959e-6, -1.7855748225381548e-6] km/s
+ V∞_out: [-2.3753835139149446e-6, -1.5347537728213949e-6, -4.941652042426721e-8] km/s
+ time of flight: 1.80700020321922e8 seconds
+ arrival date: 2029-01-23T03:15:51.029
+ thrust profile: [0.23989087621508687 -0.0724033575557699 -0.10014904534118232; 0.05091433362294459 0.008576215018029427 -0.06429297043496793; 0.044060626205955945 0.01685690575765659 -0.0905479930155155; 0.03001117318454867 0.0156751475520118 -0.08733861929130543; 0.02019373567763169 0.01247782815500458 -0.07599117374182444; 0.020140188583667028 0.013122061552580487 -0.0844409086833156; 0.01562203960529119 0.012253586453229532 -0.08200853751943203; 0.016886859366847265 0.014587765542038606 -0.09778210411951231; 0.02628847769764512 0.02326046726497924 -0.1759106107701299; 0.007216429204620287 0.008352433588534224 -0.054523303449496734; 0.000992053221606686 0.0006051523629589698 -0.004681357284874344; 0.007993528622815995 0.005018632811226548 -0.056442076361614114; 0.0028798115207548085 -0.0014286608583289782 -0.0026945552113453995; -0.0009893549010001335 0.0027338015259782507 -0.007074910267309225; 0.00017413062546151308 -0.0014804958233909874 -0.0028421117571467472; 0.0006253147638542827 -0.0004372233019942365 -0.002431018092309113; -0.0006327209664145784 -0.00039859054539551856 -0.004191663115089787; -0.0023708307036777168 0.006743767561912957 0.002105956718567557; -0.0027848648079067495 0.005886954733185958 0.005389628120807089; 0.0012554713110279683 0.00015960149661981698 0.003029666527169018] %
+
+Mass Used: 89.09720346854647 kg
+Launch C3: 98.72716481198705 km²/s²
+||V∞_in||: 2.8411974883615774e-6 km/s
diff --git a/archive/ES_0.5700139909835318 b/archive/ES_0.5700139909835318
new file mode 100644
index 0000000..7ace881
--- /dev/null
+++ b/archive/ES_0.5700139909835318
@@ -0,0 +1,22 @@
+archive/ES_0.5700139909835318---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T02:42:56.895
+Launch V∞: [6.410863336528749, -7.275146191329931, 0.28527498165632853] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013550789521450553, -0.006525589922549437, 0.015414868667751123] km/s
+ V∞_out: [-0.013619798110662587, -0.005733936082131475, -0.015647481006955108] km/s
+ time of flight: 1.8450858907994145e8 seconds
+ arrival date: 2029-02-27T15:06:05.895
+ thrust profile: [0.4286963124250187 -0.09739864480465707 -0.09558772498472361; 0.16462953385490559 0.06336774861644853 -0.12275257621173762; 0.12941434264426682 0.09445461147280938 -0.16003082414354355; 0.09507677116342561 0.09693508483584728 -0.16335751292383274; 0.049535627092231735 0.060911536121949626 -0.11381312019213244; 0.028403039921264188 0.04130328562462275 -0.08002666686599284; 0.030730837519169836 0.0536453230020861 -0.10586776719438158; 0.011921701467364364 0.022303920465015264 -0.0462892225884302; 0.002489126485687207 0.004985242199083744 -0.01039314321980688; 0.001529055525899581 0.004055969339208023 -0.007527916582807039; 0.002345511591551528 0.001995194150340293 8.441741242604757e-5; 0.00024642246145075786 0.0013914017385617732 -0.002913124800359096; 0.0021817671977640398 -0.0028048130549970353 -0.003612518687262134; 0.004423736464908472 -0.00023396844293979647 -0.005318281489942424; 0.0007706098320848865 -0.0009422553956711635 -0.0026086954294347003; -0.003221573494757622 0.005819067201627806 -0.0036942266338240394; 0.0004881853172318196 0.0014783912258083058 -0.000579636954453818; -0.0010517265059696048 -0.0008829707470561455 -7.98660193335333e-5; 0.0005416048142549345 -0.0060545052714561145 -0.002963512938036103; 0.0025789002824619716 0.0026208221218073434 -0.007990387018131847] %
+
+Mass Used: 116.05122408061243 kg
+Launch C3: 94.10830264002995 km²/s²
+||V∞_in||: 0.021536605966027893 km/s
diff --git a/archive/ES_0.5700369696503689 b/archive/ES_0.5700369696503689
new file mode 100644
index 0000000..b1a7ee7
--- /dev/null
+++ b/archive/ES_0.5700369696503689
@@ -0,0 +1,22 @@
+archive/ES_0.5700369696503689---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T21:50:50.160
+Launch V∞: [5.7387385457203335, -7.977148611657775, -0.18526920699192523] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.243207143536394e-7, -2.3047227736836682e-7, -3.8114527173007987e-7] km/s
+ V∞_out: [2.469146623599275e-7, -3.3764441453908726e-7, 3.9252472569264103e-7] km/s
+ time of flight: 1.5816723582968336e8 seconds
+ arrival date: 2028-04-28T13:11:25.160
+ thrust profile: [0.23955298656471077 -0.11263078915734206 -0.10079134836444666; 0.18955287551312863 0.00990161003350914 -0.20255516410832938; 0.12046907261469278 0.03172458350804427 -0.2046797448302239; 0.10086445311803645 0.04044914500638417 -0.23051830406596957; 0.07523531867613548 0.037109589031594746 -0.213285031282738; 0.04966554383366102 0.028114671320916888 -0.1678843465424884; 0.026577974663880757 0.01646180874540755 -0.1043986784293056; 0.0020502035021657673 0.001377485554415486 -0.010062026410446106; 0.0014719548041814269 0.0012790572149188467 -0.004431575331016826; -1.1397330884311174e-5 5.792869361592463e-5 -0.003575826055259917; 0.0004157700977504105 0.00044968086910612435 -0.004006737509690856; 0.0007477289746143404 0.000559711408373506 -0.005245123213278776; -0.0014538464538713578 0.001160436877271064 -0.0005619613449498404; 0.0008180887010996962 2.5378922743078588e-5 -0.0010512947039414758; -0.000891248076206983 -0.0002309839162332324 -0.0008117467090705977; 0.002442557426893941 -0.0010747993463788243 -0.00012954258436552284; 3.513239377438211e-5 0.00013593267020901715 0.0004433044800795261; 9.122112290524723e-5 -0.0002234990026918752 -0.0007183988474220087; -0.002082838950588209 0.0011143911906391767 -0.0007468220902121727; 6.67449623753601e-5 -0.0015636254683455398 -0.0016139058775744611] %
+
+Mass Used: 101.52945356402597 kg
+Launch C3: 96.6023447476693 km²/s²
+||V∞_in||: 6.151725428098532e-7 km/s
diff --git a/archive/ES_0.5701035923775374 b/archive/ES_0.5701035923775374
new file mode 100644
index 0000000..2deaf83
--- /dev/null
+++ b/archive/ES_0.5701035923775374
@@ -0,0 +1,22 @@
+archive/ES_0.5701035923775374---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:55:51.873
+Launch V∞: [7.372113307064192, -6.611832685919842, -0.44036838308823134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.08853816066245e-7, -2.1521505728746875e-6, -1.1389092893885316e-6] km/s
+ V∞_out: [-1.7548371958686757e-6, 1.5548001396177542e-6, 9.685461870606546e-7] km/s
+ time of flight: 1.556660944801554e8 seconds
+ arrival date: 2029-04-14T16:30:45.873
+ thrust profile: [0.22773324645080997 -0.056412252366196146 -0.09596561029102128; 0.07012224819824613 0.016625988481472242 -0.08524947824166351; 0.09309441072451041 0.04303365843446828 -0.1852805438442958; 0.08623247889700882 0.05219097515725985 -0.23710094290998757; 0.0599661386294412 0.04275324728599292 -0.21103304321083355; 0.032723905435337174 0.025864127531860827 -0.14061374977601784; 0.018216937107333655 0.015175710061658885 -0.09262357691216065; 0.012137950998412677 0.011116209796640316 -0.06888363792161048; 0.0027800938099264046 0.0025014859586245464 -0.017175562536052836; 0.0017108363337998405 0.0010458186995629755 -0.005664839783456261; 0.0034196014763110206 0.0030963879543257676 -0.02307195140918936; 0.0018262572042472068 0.0008966333758165107 -0.00763951900630952; 0.0001276525929491271 0.0007307684532897883 -0.0032664070166162104; 0.0012671959741918856 0.0024046774312445974 -0.006755505372142237; -0.006881418982780001 -0.001010652815488294 -0.009131137554361625; -0.0010272739519733064 0.0031242993829510408 0.0057000234601682674; -0.0035192822062490624 -0.0010591953800676182 0.003623636377957422; -0.003867354647255334 -0.008061276660711604 -0.001414679221359438; -0.0017196741156086106 0.011911616735903203 -0.002311708120321988; -0.00028321362731476593 -0.00023043449853653265 -0.0020342162693406753] %
+
+Mass Used: 91.94738048937461 kg
+Launch C3: 98.25831039161469 km²/s²
+||V∞_in||: 2.536008712589926e-6 km/s
diff --git a/archive/ES_0.5701302003149444 b/archive/ES_0.5701302003149444
new file mode 100644
index 0000000..bed4e8f
--- /dev/null
+++ b/archive/ES_0.5701302003149444
@@ -0,0 +1,22 @@
+archive/ES_0.5701302003149444---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T18:10:39.722
+Launch V∞: [7.521062977666012, -5.469101231519245, 0.3608045644359459] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00042005498109760355, 0.0025900121462541672, 0.0031515332773739265] km/s
+ V∞_out: [-0.0014277988730993945, 0.0012143284573646429, -0.0036458613867303316] km/s
+ time of flight: 1.8749577787336463e8 seconds
+ arrival date: 2030-04-14T20:20:16.722
+ thrust profile: [1.0 0.009328366434935589 -0.2145534051693982; 0.3609187007273937 0.2436352900273366 -0.26480143128612466; 0.15869217063608723 0.18197067407261372 -0.22041223423785164; 0.03829591716219964 0.06165656658769647 -0.08604500093737867; 0.010363987546646277 0.022176427287658052 -0.03632334103061475; 0.003399698707641402 0.008926516260412043 -0.016561586631157817; 0.004213306036915499 0.01431096705836324 -0.026778280110861342; 0.0015543396243992889 0.007563379924324729 -0.0162570914241487; 0.0004486633521697214 0.0024021981305425094 -0.005309579231307329; -0.0003696416341007541 0.004360849063871465 -0.009804278530060035; 0.0005119938204589058 0.004995259783286999 -0.012315127718651099; -0.0008659775939126617 -6.039209556330492e-5 -0.001050249720615347; -0.0007946008216078676 0.000935008392495085 -1.1643221210253223e-5; -0.00021965876640491112 -0.0006279827787490026 -0.002067041710469554; 0.0009971025908772635 0.0004616145559535385 -0.0013755536772578744; 0.00475179201477 0.003327379546564462 0.002202533765718288; -0.003032943352148109 -0.0007550847146290051 0.0013664793953570972; -0.0004601820582979227 0.000373930976837687 -0.0023291807783267786; -0.0007362462513186445 -0.0007756735251651629 -0.0007421245639308325; -0.004585185414577144 0.006843580117465709 0.0037389325044388253] %
+
+Mass Used: 159.94068728544335 kg
+Launch C3: 86.60763652834146 km²/s²
+||V∞_in||: 0.004100825661166818 km/s
diff --git a/archive/ES_0.570134257210723 b/archive/ES_0.570134257210723
new file mode 100644
index 0000000..c1efb69
--- /dev/null
+++ b/archive/ES_0.570134257210723
@@ -0,0 +1,22 @@
+archive/ES_0.570134257210723---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T14:53:55.149
+Launch V∞: [5.558880054013274, -7.90363793472465, -0.16002579547665724] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00012235805116362855, -0.00015368771464510593, 2.7501131295381825e-6] km/s
+ V∞_out: [3.65403506845321e-5, -9.076264817488664e-7, -0.0002010296717542077] km/s
+ time of flight: 1.5917168946298203e8 seconds
+ arrival date: 2028-05-08T21:15:24.149
+ thrust profile: [0.461429976880497 -0.19488002599470583 -0.16078897890537663; 0.23027183127974313 0.029151180399685724 -0.20787292307425564; 0.15329205130253218 0.05789367382192552 -0.22126547857347514; 0.1274800091775638 0.06981738371540236 -0.2464559947035617; 0.07187249265132865 0.04836176387710728 -0.17630865794229128; 0.03833868620282948 0.029429449125632227 -0.11245236874605011; 0.01980305140307105 0.017124456952589025 -0.06772196181628469; 0.018467983823847043 0.017435537854695995 -0.0705262948360782; 0.003037886883374716 0.002322134656290977 -0.012291814809873064; 0.0006196130430001052 0.00032211227628674863 -0.0018553060020706411; 0.0018723601291674465 0.0019465197869917308 -0.00930861783303942; -0.0002904099299121854 -0.0006490568894643333 -0.0007716535895840745; 0.0005990200292871562 0.0004900194177078108 0.00011916547091011544; -0.00027811614243815607 0.00016328429063714562 -7.793375777829885e-6; 0.0009222234850326266 0.0011391862425719863 -0.0004461398323742002; 0.0001407913433322297 0.0006850547945876569 -0.0017129256443265467; 0.0002015722315513256 0.0005894505177163583 0.0004421332660845059; -3.8036713466460356e-5 -0.0005624284455244791 0.00041463921955485895; -0.0011047613003559436 -0.0010830519066228365 0.00025350149646614613; -0.00011355334020514299 -0.00016836637064683766 0.00024323409626093037] %
+
+Mass Used: 120.3568515846755 kg
+Launch C3: 93.39424831334308 km²/s²
+||V∞_in||: 0.00019646620431927194 km/s
diff --git a/archive/ES_0.5701600565778453 b/archive/ES_0.5701600565778453
new file mode 100644
index 0000000..605a489
--- /dev/null
+++ b/archive/ES_0.5701600565778453
@@ -0,0 +1,22 @@
+archive/ES_0.5701600565778453---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T09:42:12.941
+Launch V∞: [5.728642375026923, -7.878564059077867, -0.014610681834821018] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.9980202029649214e-5, -5.943138575720955e-5, 1.0607129833771076e-6] km/s
+ V∞_out: [1.3779554902894223e-5, -4.150591335204931e-9, -7.644872684813928e-5] km/s
+ time of flight: 1.6315531490973282e8 seconds
+ arrival date: 2028-06-24T18:37:26.941
+ thrust profile: [0.360817630914472 -0.13255050273306807 -0.11582174422843945; 0.10877827336568394 0.02031944567611725 -0.09444046458483547; 0.1909487370174086 0.08909929087211002 -0.23969504840846384; 0.09881849665469895 0.06362141676013013 -0.17857810232931148; 0.06903529028319035 0.05303327057338366 -0.15281793451851614; 0.04498813026626094 0.04153096111655673 -0.12431560453264057; 0.026273085977924878 0.024903251404938726 -0.09220580580337731; 0.021131284981840963 0.026198431510948274 -0.07769057063322293; 0.018698501392331614 0.022469246136963217 -0.07759436130571655; 0.007786187980712767 0.008065977040677479 -0.03301062956117193; 0.001724372345436494 0.0010951598116105922 -0.006928411816665092; 3.904676112253104e-5 0.0013434936678725835 -0.001023739803434023; -0.0011832014248683818 5.805511624136256e-5 -0.0013860689088459606; 0.0006450805498423417 0.0004712590589617139 -0.00034035059191748194; -0.0009510184802582847 -0.0005807731505452874 0.0004581406061022065; 0.00034874890876670584 -7.451770112082743e-5 -0.001207587058599549; -0.001786729694438222 -0.0009424299818323229 -0.0002199795404471203; -0.0010989162283455245 0.00045004000247734707 -0.0016232397343248315; 0.0019698308473302764 0.0001392766498616343 -0.0009181392738411879; -0.00015902206376461076 0.002108149364435347 0.0016635754996220595] %
+
+Mass Used: 111.66564937265366 kg
+Launch C3: 94.8893285659713 km²/s²
+||V∞_in||: 7.766102832167435e-5 km/s
diff --git a/archive/ES_0.5702063530156851 b/archive/ES_0.5702063530156851
new file mode 100644
index 0000000..274ca92
--- /dev/null
+++ b/archive/ES_0.5702063530156851
@@ -0,0 +1,22 @@
+archive/ES_0.5702063530156851---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T00:06:30.651
+Launch V∞: [6.6415623401799735, -7.356800707865314, -0.7488811434500653] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.364674779959069e-7, -0.00018640428011356625, 0.00011962620131801255] km/s
+ V∞_out: [0.00011388053973372043, 0.00018613525385151187, -3.838583397534784e-5] km/s
+ time of flight: 1.852372586599866e8 seconds
+ arrival date: 2029-03-12T22:54:08.651
+ thrust profile: [0.2008695325620269 -0.04917172575043547 -0.07454921546431896; 0.05012987904581522 0.01502829619404095 -0.058490411341780464; 0.038654839631344376 0.022660742983745655 -0.07547589447871367; 0.03085265288854819 0.02465663665876604 -0.08469730124259797; 0.021918613651117795 0.021577653766497864 -0.07686593000102138; 0.033578650644018555 0.0431857193775635 -0.14388763717920325; 0.021148886313600075 0.03235049467077006 -0.11359208769143544; 0.032320274823761125 0.04636091686951334 -0.17652931743581593; 0.01085486711321746 0.01568011081098496 -0.066798920509184; 0.0023171086471583326 0.005365644601912153 -0.02152403665862797; 0.005455795649711153 0.009224274476319606 -0.04078052050320709; -0.0023107433256286366 0.0011508026673434086 0.000637533024155187; -0.006033947463420565 0.0007452222913616569 0.0011923832208149522; -0.001907527368926359 -0.004868188919297145 0.0012299049623145423; -0.00017593419820756667 -0.0005454487854247528 -0.0008266132134791219; 0.00714735173132633 -0.0021595600638509437 0.0037550843676757194; 0.0007975216255626286 0.0002872641291277189 -0.0006743795549139097; 0.003404278229395143 -0.0037439439627269112 0.0015966554910264096; -0.006891376791479675 -0.0019114019229128107 0.006279465442488899; 0.00994243291172909 -0.0025810630973213218 0.0034064074222497688] %
+
+Mass Used: 88.9442205305354 kg
+Launch C3: 98.79368994075953 km²/s²
+||V∞_in||: 0.00022148876152931437 km/s
diff --git a/archive/ES_0.5702330420293562 b/archive/ES_0.5702330420293562
new file mode 100644
index 0000000..ce58d0a
--- /dev/null
+++ b/archive/ES_0.5702330420293562
@@ -0,0 +1,22 @@
+archive/ES_0.5702330420293562---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T19:57:20.139
+Launch V∞: [6.377192396335489, -7.275209033995388, 0.4472411280948402] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.7675855068501175e-6, 1.7630057021235137e-6, -1.2798150987040937e-6] km/s
+ V∞_out: [1.932614225309842e-6, -1.4994225293897682e-6, 2.5344489737602103e-6] km/s
+ time of flight: 1.8749577787478516e8 seconds
+ arrival date: 2029-04-06T22:06:57.139
+ thrust profile: [0.5234898893448994 -0.11435659752849023 -0.13713926054091388; 0.09943326709124342 0.034287165787877515 -0.08426451693226988; 0.06925034295227464 0.04460313573703881 -0.0982850685864673; 0.05468809164623496 0.047739395354706116 -0.109482724963153; 0.05026819601804948 0.05398670861040828 -0.1295376816838391; 0.024000825264051808 0.030322264141417206 -0.07821025129547837; 0.02489512592285282 0.0360044483595304 -0.09424657678358012; 0.009186129432082128 0.015396995344074028 -0.04308893031279358; 0.010352000003971306 0.012735422820502466 -0.03791815479318723; 0.003916088930262163 0.00751405931113526 -0.0197297384267224; 0.005973267180460443 0.012875222672417388 -0.03923253622623163; 0.00012631231708931656 0.0013148192252441194 -0.013122873876589098; -0.003172292039758506 0.006491830930126487 -0.0002497299607090789; -0.001534669450037389 0.001341058463180766 -0.018362808579575632; 0.002988809440659188 0.0013689934275401905 -0.01355036363610624; 0.01461790356101906 0.0013519184816758343 -0.00667158706993253; -0.008021835364671548 0.007673872600535032 -0.004175991810184527; 0.006184797037470474 -0.0006406637820333414 -0.009303144132823543; -0.01432600192198362 0.013228138319303293 0.006380234919166821; 0.029318473778099617 0.009011983036740136 -0.0016797083715307426] %
+
+Mass Used: 118.12111751419252 kg
+Launch C3: 93.79727397486681 km²/s²
+||V∞_in||: 3.5221648641592307e-6 km/s
diff --git a/archive/ES_0.5702399412666245 b/archive/ES_0.5702399412666245
new file mode 100644
index 0000000..91c143b
--- /dev/null
+++ b/archive/ES_0.5702399412666245
@@ -0,0 +1,22 @@
+archive/ES_0.5702399412666245---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T04:42:27.064
+Launch V∞: [7.264824265484357, -6.556152698939382, 0.008080944282574743] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0444264963319031e-9, -1.6292672569495644e-9, -1.4495996964463787e-9] km/s
+ V∞_out: [-1.772119919724784e-11, 1.8078764541833798e-11, 1.0620014046427953e-11] km/s
+ time of flight: 1.548295301463242e8 seconds
+ arrival date: 2029-04-03T04:54:37.064
+ thrust profile: [0.3293744246531352 -0.07384214682566773 -0.12242923111358198; 0.31292903625678237 0.0801333465139527 -0.35590804338774534; 0.06339684719110598 0.027994594832632322 -0.11603431820570477; 0.05333072173734909 0.030927216019144933 -0.132299654894736; 0.04235261817059229 0.03410033756194402 -0.1448746626383005; 0.029223614302997924 0.03178415252331094 -0.13631820481479295; 0.024630861518704097 0.03390694804792782 -0.13259378483374024; 0.010822914559121535 0.016706365944119582 -0.07577188817264549; 0.0077439557760663625 0.007223858811833319 -0.0421010391273749; 0.003790314971718482 0.004256324148700649 -0.02511217122164066; 0.0007386725705820416 0.00020666245033777817 -0.0038857244279797533; 0.0015874575489502726 0.0007191956975522747 -0.004623495812030183; -0.0002913402732874058 -0.0005616506184605771 -0.0016832986115977234; 0.0010596189198762485 -0.0015677068848210483 4.071053042181336e-5; -0.0012718432924124664 0.0014455172648864894 -0.0005114466870747574; 0.0006270668042427071 0.0002216861432877253 -0.0011203250692314172; -0.0011625611509611105 -0.0027781501904995593 0.0005710078080314357; 0.00040999605155596884 -1.4775678891603924e-6 -0.0023031334937777216; 0.00032960435249472525 0.0016779723663549648 -0.0005573070018343505; 0.0013957144474618446 0.0010124283706070426 -0.001144281755695193] %
+
+Mass Used: 106.67482660032283 kg
+Launch C3: 95.76087512184097 km²/s²
+||V∞_in||: 2.4179904426497483e-9 km/s
diff --git a/archive/ES_0.5702422446707771 b/archive/ES_0.5702422446707771
new file mode 100644
index 0000000..56d53f5
--- /dev/null
+++ b/archive/ES_0.5702422446707771
@@ -0,0 +1,22 @@
+archive/ES_0.5702422446707771---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T04:39:17.369
+Launch V∞: [7.126901283361206, -6.040448633157692, 0.08447076548951858] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1305557671971645e-9, 9.393619656751472e-10, -5.840531925505368e-9] km/s
+ V∞_out: [-2.214038482053e-9, 6.964244850534206e-9, -1.1319939594205852e-9] km/s
+ time of flight: 1.7017552861492905e8 seconds
+ arrival date: 2029-09-24T19:38:05.369
+ thrust profile: [1.0 -0.10560322691331692 -0.21442256088330142; 0.27989102998946885 0.14065339260179754 -0.199727013102597; 0.1694220496456766 0.14961463863251953 -0.21234416541618323; 0.05189904096512879 0.06470803171380361 -0.10225878336661297; 0.026312591047672827 0.041482465332689594 -0.07127821675032732; 0.05451313832226585 0.10505612270303837 -0.16889334735011696; 0.00596474146766674 0.014132476028278948 -0.027516611545298084; 0.014761607012629173 0.03821454764473485 -0.07465174167839393; 0.003949875771904847 0.011698102268971574 -0.023947129199615287; 0.0005119492301119106 0.0033606209937322986 -0.0066238652379025775; -0.00018155404225116522 -7.039035921184477e-5 -7.118332985101678e-5; -0.000599784382011206 -0.00035190902699791375 0.00013233698078219378; 0.00012797199772711528 -0.0022089962204846496 -0.0012762734607485665; 0.001689989801505806 -0.0008826992186289479 0.0001480113945488904; -0.0001799378806632317 -0.0006839262766349381 -0.0007241174143525482; -0.0003917686034991861 -0.0010060749248870246 -0.0007162609187141178; 0.002899876792367138 0.0005945475252175821 -0.0036067013111876454; 0.000778885458580186 -0.00015792107799450663 0.00023992346795561042; 0.0005757299712437795 0.0004888197729047453 -6.822827562876367e-5; -0.0006905910172995046 0.004461161401234759 0.00014484468997916867] %
+
+Mass Used: 156.10917018282134 kg
+Launch C3: 87.28687690281463 km²/s²
+||V∞_in||: 6.022654764980912e-9 km/s
diff --git a/archive/ES_0.5702840569192517 b/archive/ES_0.5702840569192517
new file mode 100644
index 0000000..ecfa88e
--- /dev/null
+++ b/archive/ES_0.5702840569192517
@@ -0,0 +1,22 @@
+archive/ES_0.5702840569192517---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:33:25.506
+Launch V∞: [8.154096810644115, -5.608261662691666, 0.12749081054694417] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.615697437314238e-5, 6.153768176144339e-5, 0.0038918604353536954] km/s
+ V∞_out: [-0.003641232396270767, -0.0012165785385116826, 0.0006650034932278856] km/s
+ time of flight: 1.8749577787453333e8 seconds
+ arrival date: 2030-04-23T19:43:02.506
+ thrust profile: [0.26170813486647565 -0.008474086649210075 -0.09195564313077913; 0.03980403587412091 0.019229462364645136 -0.049653122691931395; 0.04224196015355616 0.033491160260871476 -0.09758963975295253; 0.025881560379010994 0.02837412367673335 -0.09150177076069098; 0.02968022836538694 0.03684336624198013 -0.127363028144689; 0.01677283707246812 0.02211250947417756 -0.08647389689210248; 0.011245014282618161 0.014608613370200777 -0.06567919350823098; 0.0062909397004525264 0.007867677192583338 -0.059727681915161736; 0.009180674471443289 0.014913066485568963 -0.08458378254015177; 0.0025541474826478216 -0.008952549321361056 -0.012679646119508598; 0.005472127535448508 0.011406161262865554 -4.534252167537334e-5; -0.00039667792473343155 0.0016921775946363157 -0.008810305711740287; -0.02583663210377388 0.012137408204606851 0.0001720514115772804; 0.00017430287535866464 0.001120284854644024 0.0015330614915214438; 0.003131344630983103 -0.0006316819688816431 0.005221164610449622; -0.0013645014845781837 0.0012601407071394007 0.011904870964010569; -0.04151748631702779 -0.033693101063411106 -0.0072568511698401774; -0.03541750067269756 0.011992928710594103 -0.043800238717474564; -0.004590788221795722 0.008920683401898352 -0.05258565242142542; -0.0028188474210996683 0.005143182665272766 0.0083339262188286] %
+
+Mass Used: 93.90887218126636 kg
+Launch C3: 97.95814758134752 km²/s²
+||V∞_in||: 0.003893300342740226 km/s
diff --git a/archive/ES_0.5702990871192952 b/archive/ES_0.5702990871192952
new file mode 100644
index 0000000..1dd4574
--- /dev/null
+++ b/archive/ES_0.5702990871192952
@@ -0,0 +1,22 @@
+archive/ES_0.5702990871192952---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T00:46:22.231
+Launch V∞: [7.23851066622458, -6.511546890821862, -0.1757507653025118] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7809806268605333e-10, -1.4867047466080945e-9, 2.976948363345354e-9] km/s
+ V∞_out: [1.214120480647775e-9, -4.799682662426959e-9, 6.810638422198151e-10] km/s
+ time of flight: 1.549292281586422e8 seconds
+ arrival date: 2029-04-04T04:40:10.231
+ thrust profile: [0.549047699210638 -0.1286614765032928 -0.1965653073744962; 0.05845450232180562 0.016624420629982754 -0.06321303859083889; 0.08941556133461431 0.047504256997658464 -0.15554305606795388; 0.10157679885296868 0.07112116158164776 -0.24364001030149246; 0.057001837634893325 0.04848494522575229 -0.17397601546922634; 0.03459092236874096 0.03388578045111399 -0.13053216331658052; 0.031804615987009774 0.025146951594198604 -0.12640748052799705; 0.013625435070185921 0.015966997232087995 -0.06916979847087998; 0.005498828423033766 0.00749248459978948 -0.03492682800712239; 0.011243866152702179 0.014463777350142778 -0.06802778484664394; 0.0022401686679656583 0.0006446440521075101 -0.004312687567084654; -0.0008590215219725071 -0.0012474473710074488 -0.0012428766497406454; 0.0033973000002556213 -7.758993055655009e-5 -0.0008463542087659573; 0.000572861267888595 0.000717164917126879 0.00020644332045570033; -0.001896027283828079 -0.00021032036443607025 0.002200259590958873; 0.0015434635833036737 -0.0003770337047050013 -0.00020526075073680722; -9.722356443172799e-5 0.001777104802573083 -0.003715589403227114; -0.0007325455546872003 -0.0023813684935082547 0.003497994621912404; 0.0014132927319405325 0.000982534681387932 -0.004271769375313449; 0.0013736985109036237 0.005461785433607677 -0.00022950693606432586] %
+
+Mass Used: 112.19045550962528 kg
+Launch C3: 94.82716790792328 km²/s²
+||V∞_in||: 3.3323012291124204e-9 km/s
diff --git a/archive/ES_0.5703132046235956 b/archive/ES_0.5703132046235956
new file mode 100644
index 0000000..0926b2c
--- /dev/null
+++ b/archive/ES_0.5703132046235956
@@ -0,0 +1,22 @@
+archive/ES_0.5703132046235956---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T00:31:12.499
+Launch V∞: [7.632891562243214, -6.3587379897769605, -0.4907149289635127] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.400052104954068e-6, 1.3571172099114974e-5, -0.00028792271829696095] km/s
+ V∞_out: [-1.0981317960401423e-5, 0.00028803271329351114, -2.962682408339438e-6] km/s
+ time of flight: 1.8396905014532265e8 seconds
+ arrival date: 2030-03-19T07:02:02.499
+ thrust profile: [0.40196109988971174 -0.0167841008520575 -0.15147111106237035; 0.009393393805758871 0.0036856586471369496 -0.012124616164404621; 0.03341225691073915 0.019836691457086875 -0.07592185549975662; 0.03814495841977194 0.02824182549129583 -0.11211096296744041; 0.027344640580849386 0.024840900879760902 -0.10866343736127097; 0.02516919158774692 0.03277552533860767 -0.1576655216761373; 0.01230754687242585 0.013204311774608613 -0.07132903964685279; 0.010105509412850518 0.010544750782192188 -0.07157352364338865; 0.003616650612990323 0.004341649005787056 -0.031545086452193324; 0.002209052064510447 0.0026338050292034243 -0.020892589697148377; 0.00045640404039148545 0.0001322335943068876 -0.005987698276004086; -0.001672726610554344 0.0001399675781026551 -0.0027248779340606015; 0.0017681880476234162 0.00029503889169056396 -0.003151641598922582; -0.0024559667197416126 -0.0005564969170558613 -0.0007855414571588549; -0.002695969306946192 0.0003653906300952294 -0.0023776524486924713; -0.0056173161395296056 -0.011719280695314057 -0.0007460011830611852; -0.0056232991307863895 0.00036420456208448407 -0.0007711419362943931; -0.0008468851328500707 0.003378985506243396 -0.01138508209983178; -0.013196436982614539 -0.007850182072137163 -0.004765309832209956; -0.003459523812349133 0.0034406480829181846 -0.006992657575490131] %
+
+Mass Used: 88.2423345977545 kg
+Launch C3: 98.93538356510405 km²/s²
+||V∞_in||: 0.0002882457780602372 km/s
diff --git a/archive/ES_0.5703282436181368 b/archive/ES_0.5703282436181368
new file mode 100644
index 0000000..a990a8d
--- /dev/null
+++ b/archive/ES_0.5703282436181368
@@ -0,0 +1,22 @@
+archive/ES_0.5703282436181368---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T08:11:40.918
+Launch V∞: [6.663893149606229, -7.1366226434854, 0.24124338625348712] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.366111741847026e-8, -2.2621064428181572e-8, 2.3228034489739166e-8] km/s
+ V∞_out: [-8.822461749593871e-8, 1.315238781517379e-8, -1.7962138133364507e-8] km/s
+ time of flight: 1.8480388568195328e8 seconds
+ arrival date: 2029-03-02T06:36:25.918
+ thrust profile: [0.41802091169726713 -0.10370175991383797 -0.11726189227096914; 0.15062140665909318 0.050235638076062156 -0.1287968104998408; 0.12573756836631594 0.08091338955044552 -0.17907503355785842; 0.08758904258064325 0.07697583427831238 -0.17549592079354676; 0.05935101933244871 0.06410163673477799 -0.15391001296163326; 0.03104975225208281 0.038964964014509454 -0.09949133915071708; 0.009010386807861367 0.013250254003548288 -0.03608565345361472; 0.002327290016581783 0.0035726711009889302 -0.011063323484200863; 0.002291771790596762 0.0037060488265831006 -0.012900849382177587; 0.0032127422118186917 0.004516521112147149 -0.015173506458824964; 0.00033432025457640356 0.0007255267544861946 -0.0026884466938106376; 0.00027447557164151417 0.0007349444410951597 -0.002726451827468289; -0.0003218465750129327 0.00024221703624900177 -0.0009517183151738404; 0.0005263017493662148 0.001009874374084818 0.0008891848565197378; 7.405368390370559e-5 5.585194631939339e-5 0.00030183119745892726; -0.00109458309889696 -0.00031447961918951026 0.0009736726169568468; -8.496128148834652e-5 -0.00025077353546236534 0.0008163332627292945; -0.0005262911991967609 0.00019838305738787142 0.0013313478788427658; -0.00048675897549379425 0.0010346146046037686 -0.0011456834954266934; 0.0008926216736506174 -0.0007218250880629009 -0.0014588341665330848] %
+
+Mass Used: 108.90014150947718 kg
+Launch C3: 95.39705303628841 km²/s²
+||V∞_in||: 8.972422588034695e-8 km/s
diff --git a/archive/ES_0.5703469673380229 b/archive/ES_0.5703469673380229
new file mode 100644
index 0000000..dbdf369
--- /dev/null
+++ b/archive/ES_0.5703469673380229
@@ -0,0 +1,22 @@
+archive/ES_0.5703469673380229---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T14:12:22.252
+Launch V∞: [8.118649720882592, -6.171168896357644, -0.13270028334153472] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0066001319179461344, 0.004582776949217463, 0.00027390172014080463] km/s
+ V∞_out: [-0.005712206263589038, -0.0033982509513600704, 0.0045224787505942] km/s
+ time of flight: 1.874957778748606e8 seconds
+ arrival date: 2030-05-01T16:21:59.252
+ thrust profile: [0.005001321525999911 -0.0004954057096477003 -0.0017369932977883147; 0.007431957291331861 0.0011438300222300518 -0.012837417447106023; 0.025459024718255892 0.004046677432475428 -0.0718739643610582; 0.030417031067552933 0.002505534740583141 -0.11438552107739638; 0.029519993652689962 -0.00015569949327703448 -0.13392245903752759; 0.023767297176885225 -0.0018318947797292843 -0.12303650308129412; 0.015634189090317357 -0.002025074372148205 -0.09002489325272699; 0.007845410850753437 -0.0014723630022050644 -0.050427305044235975; 0.011072038563536593 -0.002563382707918234 -0.07222885200271015; 0.007530339055947837 -0.0019449525771731754 -0.03800172629012936; -0.002172485470906443 0.00029128641971247265 -0.004817640275839148; 0.0005618398775875449 -0.00010773923943572356 -0.004669636651487124; -4.1139897382633196e-5 0.00023198913363281035 -0.004112446013902842; 0.004977990003070434 -0.00025320458541749766 0.001208951692688387; -0.0003770581593011844 0.0006206509361362353 0.005705178362617264; -0.002826016039338784 -0.0063369042413946985 0.004808881843868264; 0.0012918153438539305 -0.0024799035502258426 -0.002616623258481214; -0.0024710905228220717 0.0012469149736414572 0.004450037643285151; 0.0033421004988367755 -0.003542209911762032 -0.000261164559443323; -0.0039730588557547785 0.0016093091961319728 0.004965522179367577] %
+
+Mass Used: 58.659914043772005 kg
+Launch C3: 104.01340820295795 km²/s²
+||V∞_in||: 0.008039813931482887 km/s
diff --git a/archive/ES_0.5703580261106075 b/archive/ES_0.5703580261106075
new file mode 100644
index 0000000..e035080
--- /dev/null
+++ b/archive/ES_0.5703580261106075
@@ -0,0 +1,22 @@
+archive/ES_0.5703580261106075---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:11:04.515
+Launch V∞: [7.281260089749604, -6.678660090362964, -0.4563697839393219] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003550297011519047, -0.0012389920247857895, -0.0020325199550392426] km/s
+ V∞_out: [-0.002099511291795987, -0.00022171080684323373, 0.001156454221956342] km/s
+ time of flight: 1.537662563174805e8 seconds
+ arrival date: 2029-03-23T12:02:00.515
+ thrust profile: [0.26169411461633363 -0.06579586269849252 -0.10912709880773619; 0.11024478364618016 0.026495560000091695 -0.1293209747273893; 0.0995111898161959 0.0465565679211473 -0.1922032348365015; 0.08284592553199899 0.05122878775823056 -0.22150493405788796; 0.03803597666921793 0.027618914679777094 -0.13124974186616362; 0.027437416096212038 0.021716402513169215 -0.11419728906864748; 0.02577652104622584 0.021178984621218058 -0.1258943399535568; 0.012055635955887278 0.010634705036880476 -0.06400437806614268; 0.014061026353232151 0.013628393606647204 -0.08383596971216416; 0.008867693292541149 0.009242134241657486 -0.05810047517762339; 0.00023830536699367497 -2.733512373012392e-5 -0.00039532612326177426; 0.0007328496313033957 0.000933705359785967 -0.003524747327383529; 0.0003163089987100657 -6.774547128387003e-5 -0.0008380983365274743; -0.001934080459094541 0.00043998364326494393 0.0010497087433400361; 0.0002658635706778652 -0.0009298617172912787 0.0008076718481249147; -5.5140067679951166e-5 0.00018947112050234888 0.0035034937052379027; 1.2105595691061779e-5 -0.003313027461373119 -0.0006043708231749558; 0.0007988012706911859 0.0011389198909838845 -0.0003250119633745731; -0.00019017922983334892 0.0002351905089248772 -0.002730957001452628; -4.397106480944098e-5 3.5576208746682374e-5 -0.0006828112134372394] %
+
+Mass Used: 94.74548268057379 kg
+Launch C3: 97.82952247688027 km²/s²
+||V∞_in||: 0.0024067165794533275 km/s
diff --git a/archive/ES_0.5703683727036064 b/archive/ES_0.5703683727036064
new file mode 100644
index 0000000..f867121
--- /dev/null
+++ b/archive/ES_0.5703683727036064
@@ -0,0 +1,22 @@
+archive/ES_0.5703683727036064---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T04:43:38.535
+Launch V∞: [7.273340904325141, -6.633517185093405, -0.45235947142280036] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.56610271099356e-9, -2.2600119018022364e-9, -1.011561192697739e-9] km/s
+ V∞_out: [-3.927601319416009e-9, 2.875018081844309e-9, -1.3783232865055977e-9] km/s
+ time of flight: 1.531242556448618e8 seconds
+ arrival date: 2029-03-15T11:14:33.535
+ thrust profile: [0.33700858832668457 -0.09018750706794762 -0.14372602892263941; 0.12412596067011364 0.02680981178895659 -0.1470037239545466; 0.07577965650344604 0.03309422858433104 -0.15041069570162313; 0.08452652869198068 0.048601280964802394 -0.2317830047089161; 0.04998928076956466 0.03382626020977371 -0.1744235626083739; 0.029917318422315924 0.022874165831452156 -0.1265008228467422; 0.028717436613209274 0.023777918059145697 -0.13960282470374957; 0.005222971594537583 0.004251663715568041 -0.02828629745029901; 0.005201645388283136 0.0029975299776886215 -0.02926574930509391; 0.013269829617559773 0.012716240126445013 -0.08675056371127204; 7.411861618447676e-5 -0.00011324461330824883 -0.0015317489606648453; 0.00038412865643492873 0.001084104222593432 -0.0028154087116968054; 5.942953047953145e-5 8.137022903547027e-7 -0.0006691040162730027; -0.000393271632096889 -6.518045806671311e-5 -0.0008367529996462507; 0.0017599576384974426 -0.000840640758600553 0.00041132271021737047; 0.00029318160786695225 0.00042993734995270134 -0.00022002138781735764; 0.0005324005541788833 0.00040900643152089086 0.0013375823725673723; 0.0015430461566490051 -0.0006573955786361488 -0.003096273397563546; 0.0012219724272158417 -0.0007728673001126804 0.0014482952603637996; -0.0011796683079774747 -0.002649732442440852 0.002478020735432386] %
+
+Mass Used: 98.95670921428018 kg
+Launch C3: 97.1096672468447 km²/s²
+||V∞_in||: 5.194247184164667e-9 km/s
diff --git a/archive/ES_0.5703694549990099 b/archive/ES_0.5703694549990099
new file mode 100644
index 0000000..dff3767
--- /dev/null
+++ b/archive/ES_0.5703694549990099
@@ -0,0 +1,22 @@
+archive/ES_0.5703694549990099---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T14:02:14.919
+Launch V∞: [6.1166155949380405, -7.315321527792755, 0.20793209568344762] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012430525176253126, 0.00823376542181322, 0.011580327313696789] km/s
+ V∞_out: [-0.007259633851066392, -0.014851468111799788, 0.009115071640597714] km/s
+ time of flight: 1.8157162038292024e8 seconds
+ arrival date: 2029-01-23T02:35:54.919
+ thrust profile: [0.6122279953661793 -0.1539804920110955 -0.14122156327600638; 0.2658723906780348 0.09040659590256292 -0.18431528410241646; 0.14216353614757912 0.09502684319006474 -0.16894894839753208; 0.12645676079865636 0.12338381249287729 -0.22059378329857038; 0.07175746686954694 0.08416600482445527 -0.16460546133030274; 0.01690367594920541 0.022966980857736418 -0.0491065639409785; 0.008994271120033915 0.014110807199389994 -0.031844730881536845; 0.005057988405018691 0.009151361824391425 -0.0215454780750977; 0.002040695742571948 0.0043509807297530045 -0.010735432203408456; 0.000479354100298186 0.002862464779058193 -0.007223442952187135; -0.00034936169042392654 -0.0007121679536801801 8.607165085225735e-5; -0.00015543863754361218 -0.00018791695922640506 0.0006428915296434446; -0.0012965573563069877 0.00024220465041162466 0.0018642378629045516; 0.0003662965229829752 0.0004495552114900695 -0.0006610740363018994; -4.7567415694846106e-5 -0.0007791992552161819 0.0013867380620930984; 0.0017181773664036626 -0.0015529482720149925 0.0019201071911759625; -0.0001969024359466157 -0.0010166836003119343 0.0025938481048173668; 0.002293776437002239 0.0026624497312643085 -0.0024911461951811677; 0.0014216459278634111 0.002624397904780252 0.0007937276647742851; -0.00020232810224748868 -0.00023345234012342952 0.004231343001064133] %
+
+Mass Used: 134.7718158042626 kg
+Launch C3: 90.97015114764268 km²/s²
+||V∞_in||: 0.01887900500215151 km/s
diff --git a/archive/ES_0.5703706134615194 b/archive/ES_0.5703706134615194
new file mode 100644
index 0000000..dbc9614
--- /dev/null
+++ b/archive/ES_0.5703706134615194
@@ -0,0 +1,22 @@
+archive/ES_0.5703706134615194---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T00:45:56.264
+Launch V∞: [5.849157276141522, -8.02527349714152, -0.3039091826967806] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.056991056286332e-7, -3.068647037518254e-7, -5.109189160353802e-7] km/s
+ V∞_out: [3.844213053829647e-7, -5.135584687064807e-7, 5.896067226773398e-7] km/s
+ time of flight: 1.6067183682589614e8 seconds
+ arrival date: 2028-05-29T15:49:52.264
+ thrust profile: [0.14941877392022132 -0.069627142916297 -0.06804715244820134; 0.07063712873794163 0.0033242536550654395 -0.08429077165245384; 0.08484989141908662 0.021259761696760547 -0.1591149631251591; 0.08505343796915807 0.03178222516108295 -0.2141534076374796; 0.0643468253693024 0.029863372757315838 -0.20268542617635632; 0.04659594870137817 0.025058284450630356 -0.1749457050137643; 0.036478691180524915 0.02172460671588878 -0.15639143624596477; 0.005921741173690564 0.003176723886339991 -0.030319787861230955; 0.006304788007735102 0.004250948185305635 -0.03500571402354697; 0.0033203398519336155 0.002027377665003811 -0.019296391370694735; 0.0007544569648853244 0.0013684440157541206 -0.0017560162687421067; 0.0018342458953901038 0.0011974065927832988 -0.015029385803599228; 0.0006052435900239478 0.0033073240778886273 -0.001563873810685961; 0.0017181756841944647 0.001448525505256849 -0.004080167134442702; -0.00016873653229557812 0.000661383154423641 -0.0015181742792927343; -0.005282533466447274 0.0024531471054754497 -0.0030604603531270767; 0.002056146663989975 -0.003485443436884052 -0.005499476423464796; -0.00171197009659543 -0.002106890984314291 -0.0031154653803924944; 0.0008626261195901671 -0.0009800096919811915 -0.004976868076523958; -1.2103530046081153e-5 0.0006705214424215424 -0.0018108122433856712] %
+
+Mass Used: 89.62395374342123 kg
+Launch C3: 98.71001633628882 km²/s²
+||V∞_in||: 8.497502525629455e-7 km/s
diff --git a/archive/ES_0.5704378745675773 b/archive/ES_0.5704378745675773
new file mode 100644
index 0000000..129a4a3
--- /dev/null
+++ b/archive/ES_0.5704378745675773
@@ -0,0 +1,22 @@
+archive/ES_0.5704378745675773---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T13:03:31.935
+Launch V∞: [5.978149274260823, -7.731604700746686, -0.011975933363545833] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.052150228619838e-6, 1.0290427987018365e-6, -2.2393416467544165e-8] km/s
+ V∞_out: [-1.5768137924597976e-6, 1.511646092053253e-8, 7.962918497271822e-6] km/s
+ time of flight: 1.6712562904836372e8 seconds
+ arrival date: 2028-08-10T20:50:40.935
+ thrust profile: [0.3922446884096485 -0.1618290941550662 -0.13309099291582538; 0.07220450057140662 0.011614266097478836 -0.07386667831014718; 0.08414080946161755 0.03660354251572528 -0.13671212127221655; 0.06942689689435338 0.039468371922743786 -0.1498518809974385; 0.05002761835862553 0.0363481633095744 -0.13849431444795043; 0.042547483036075896 0.03918136481806486 -0.1463288958046299; 0.051330722888915395 0.036966742117463834 -0.1907872175870216; 0.012984168011600539 0.012497251726713647 -0.057663474132654484; 0.012514303849261443 0.012955402705267648 -0.06065468684406509; 0.0055010087110972 0.005969366693874726 -0.030971884516125862; 0.004662770999926455 0.004463707788520118 -0.02038475038936191; 0.0014863162231407035 0.0011255853770158419 -0.004580381414556297; -0.0011224329720852856 0.0029929185620992662 0.0003583621692031624; -0.0005567594896935108 -0.0021018314303515124 0.0014801543458261126; -0.004184486074538682 0.0021179012782974885 0.00571435692602602; -0.001594360663911773 0.004373214673313735 -0.0021049969166479316; -0.0066816030464578735 -0.00041530502536647377 -0.0047443684140759295; -0.00016121105303855952 0.0016866044275730874 -0.003245403831990219; 0.0022572045534984316 -0.008670494767817135 -0.008412313916375076; 0.007398705959455464 0.0006794315164984086 -0.007059249378775199] %
+
+Mass Used: 108.33346706339535 kg
+Launch C3: 95.5161234169334 km²/s²
+||V∞_in||: 8.117669237590535e-6 km/s
diff --git a/archive/ES_0.5704546088045824 b/archive/ES_0.5704546088045824
new file mode 100644
index 0000000..d050fda
--- /dev/null
+++ b/archive/ES_0.5704546088045824
@@ -0,0 +1,22 @@
+archive/ES_0.5704546088045824---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T21:24:12.085
+Launch V∞: [6.009136571390384, -7.355671839090415, 0.27323592702586635] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4488885863136577e-8, -5.224918503265775e-8, -3.6891665422830793e-8] km/s
+ V∞_out: [1.4712874370183177e-8, -3.0514226034832487e-8, 4.871007445553508e-8] km/s
+ time of flight: 1.8749577798388803e8 seconds
+ arrival date: 2029-04-03T23:33:49.085
+ thrust profile: [0.5829130430062758 -0.11013450033007502 -0.11262730182691874; 0.21523845553648463 0.09135344690046084 -0.13114604106156838; 0.25420010581159685 0.19658876880592915 -0.2439644450699833; 0.09717425530984884 0.10516444726629674 -0.14253607900757606; 0.04557782480394603 0.06274714457960479 -0.09041720084964916; 0.0396155811977901 0.06216145886866162 -0.09637748134691468; 0.0035602273364322367 0.00733659471976466 -0.01324173694070191; 0.010834056709170002 0.024527493544066723 -0.04158475165141669; 0.0019259733293372282 0.005340458306265977 -0.010338242398928341; 0.0041509948528581685 0.01123536985056992 -0.01994715946946217; 0.000608179943313532 0.0012698741527742896 -0.003704433203727346; -0.0017462967883588355 0.004472208446234754 -0.008595156515764901; -0.001830842807305068 0.0008562947358597312 0.0023193627103069592; 0.0013385995843494603 0.0013896694843367665 0.00044211179308666624; 0.0019086364292826524 -0.0018893033524098948 -0.0028041849544060147; -0.0035624101040388607 -0.0018345744190287603 0.0028003799935398203; 0.00138546616171304 0.0029235836361568212 0.00028586723985920637; 0.0028890830428626307 0.000670811824707442 -0.005511803803353665; 0.0009693996563967615 -0.0007015289056540937 0.0032485852215087888; 0.00036474067332084576 -0.0008563122422187964 -0.00047906559411053516] %
+
+Mass Used: 138.83702788135633 kg
+Launch C3: 90.29028840982683 km²/s²
+||V∞_in||: 6.558124829402071e-8 km/s
diff --git a/archive/ES_0.5704632175582904 b/archive/ES_0.5704632175582904
new file mode 100644
index 0000000..b7ac5d6
--- /dev/null
+++ b/archive/ES_0.5704632175582904
@@ -0,0 +1,22 @@
+archive/ES_0.5704632175582904---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:26:11.991
+Launch V∞: [7.735313239364827, -5.600309137949263, 0.46437702569622824] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.08597677883338024, 0.5068950436531952, 0.529061054800624] km/s
+ V∞_out: [-0.11783068009636516, 0.3085218470573809, -0.6601766038472847] km/s
+ time of flight: 1.8749577785172868e8 seconds
+ arrival date: 2030-04-16T17:35:48.991
+ thrust profile: [0.6320063624063489 0.023515976730993173 -0.0962309923665802; 0.17651597793531695 0.13842128202702395 -0.11296073764126441; 0.1049940294439277 0.13939799082771967 -0.12399910102868793; 0.0686932354775112 0.12949509295337205 -0.12744812646063106; 0.04496056982513891 0.11793238861103125 -0.12630872674947946; 0.014939533818145945 0.051274551151779306 -0.06267360644237645; 0.010489031989245142 0.04751293124387731 -0.06082660958437701; 0.002341594011198254 0.012148633650707326 -0.022409649442665613; 0.0026735568575973617 0.022199257469343637 -0.032483699970449434; -0.0002196893733823871 0.0052479476781573334 -0.007279292560085093; -0.00290325086583987 -0.002625578157603113 0.002980142811722005; -0.00011891880355276391 0.00414796570759949 -0.0019109925384903398; -0.001253524242496153 0.0003289138955900312 -0.003582224168975388; -0.0002036316682068015 -0.00024062441148867196 -0.0017851182615960795; -0.0029859658244444265 0.006277217106831129 0.0002478028675135472; 0.005653108303482637 -0.001831009531488018 0.0008590238045297037; 0.0017627058858813794 -0.0011578873617294032 0.0019850782183933684; 0.009272627976437386 -0.004409152562864463 0.0019598091715003737; 0.00039503624271861054 -0.005245496238452616 0.0077658846511859635; -0.005064029088901786 -0.002838236879587613 0.007043954124250176] %
+
+Mass Used: 132.2910408048415 kg
+Launch C3: 91.41417937368527 km²/s²
+||V∞_in||: 0.7377263662669835 km/s
diff --git a/archive/ES_0.5704667173431435 b/archive/ES_0.5704667173431435
new file mode 100644
index 0000000..3c1cece
--- /dev/null
+++ b/archive/ES_0.5704667173431435
@@ -0,0 +1,22 @@
+archive/ES_0.5704667173431435---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T17:54:33.870
+Launch V∞: [7.327094343350108, -6.432199538063929, 0.5186959991828489] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004700530281542027, -0.0016608019327198115, -0.002558685145189385] km/s
+ V∞_out: [-0.0027189827836475375, -0.0002825550718327016, 0.0014286021614009438] km/s
+ time of flight: 1.5766791325377712e8 seconds
+ arrival date: 2029-05-05T14:33:06.870
+ thrust profile: [0.4849924301334507 -0.1133845631418522 -0.16745783662129257; 0.0833956944092953 0.027583712085210065 -0.08058910664142019; 0.08539658724541185 0.05518961500706413 -0.14476634429244806; 0.04599037777927601 0.03769035909099247 -0.10826557607013489; 0.0639018009661451 0.0677725668430851 -0.18080367343842008; 0.05852019408154185 0.05972976718038775 -0.18358731364806183; 0.020000583574617602 0.024375347409289254 -0.0800777154737686; 0.034882164215970575 0.07976856501915247 -0.22593647938610512; 0.006416240420224139 0.008901306203966007 -0.033421361349118064; 0.002647117716301091 0.004022646210626403 -0.015656578880349617; 0.0010725010965472795 0.0010949451779893433 -0.00614482903634478; -2.585788090995227e-6 -2.9407910373567585e-5 -0.00012565720128556536; -0.00015995051088566273 -0.0003432056805188291 -0.00019976894372299755; 0.0001310679699042708 -0.00022995477276365535 0.00036312794869962893; -9.369567847695423e-5 -0.0002874455470125171 0.00048456964511662474; 0.0005615070658464765 0.0010605579993151035 -0.0009456017995297087; 0.0001222435317548919 -3.0121166660675994e-5 -0.000287873053867286; 6.742974561861606e-5 -0.0007348941161791039 -0.00031746831009131336; -5.223942784100583e-5 -4.040789370588551e-5 -0.0016136465702441753; 7.967869374974921e-5 0.0009811204483413333 -0.0009610372244845864] %
+
+Mass Used: 109.46130717221831 kg
+Launch C3: 95.32854795339126 km²/s²
+||V∞_in||: 0.003086435254661212 km/s
diff --git a/archive/ES_0.5704755954315884 b/archive/ES_0.5704755954315884
new file mode 100644
index 0000000..59811a1
--- /dev/null
+++ b/archive/ES_0.5704755954315884
@@ -0,0 +1,22 @@
+archive/ES_0.5704755954315884---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-08T01:24:05.985
+Launch V∞: [6.32832838075743, -7.769786198737075, -0.003412202960865522] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008246714870841389, 0.0010016933632729776, 0.0009403282472485263] km/s
+ V∞_out: [-0.0011741376296693798, -0.00044348131096066793, 0.0009960338499727733] km/s
+ time of flight: 1.874957778748754e8 seconds
+ arrival date: 2029-04-16T03:33:42.985
+ thrust profile: [0.2019521142662136 -0.07439613565771265 -0.09206894596253452; 0.04524325101357582 0.0009383021306357623 -0.06632280239788399; 0.022123985627925977 0.0022306305447257454 -0.05508783079033683; 0.03237750002470778 0.0033085841106627796 -0.1117355139639346; 0.03135934479964988 0.0025008664719839164 -0.13494424609401154; 0.026096852997057496 0.0010926197397425985 -0.1321642625961445; 0.022906562462519636 -6.214218292213843e-5 -0.13151694429785735; 0.011789121055522786 -0.0005467623987724776 -0.07578106627684245; 0.001969787292935541 -0.00010465697466780702 -0.014122289797271538; 0.00729816336513329 -0.0009750905456187849 -0.050490622255983164; 9.995749605325494e-5 -0.0002152060044945839 -0.002773825934933599; 0.00012458057127721613 -9.637052744841277e-5 -0.0016726964733757294; 0.00024318660879103386 0.000853666959734467 -0.00569066774844248; 0.0023078160929489904 0.0001199322277608152 -0.003269161675363663; -6.437557477957038e-5 -0.0010709102092245236 -0.004829687802992685; 0.0010753999551787975 0.0001380477253175226 0.0001337373536722218; -0.00030866972998474184 -0.0018397585535344383 -0.0004156234461944498; -2.6340565240368178e-5 -0.0003178678094833396 0.0025304500576288362; 0.0008722584745276434 -0.001733456752579101 -0.000303428746090376; 1.4032856608799995e-5 -0.0002353905835671372 0.0030642468001965944] %
+
+Mass Used: 79.78710701735417 kg
+Launch C3: 100.41732931191412 km²/s²
+||V∞_in||: 0.0016024012818917051 km/s
diff --git a/archive/ES_0.5704811161301212 b/archive/ES_0.5704811161301212
new file mode 100644
index 0000000..265bbf7
--- /dev/null
+++ b/archive/ES_0.5704811161301212
@@ -0,0 +1,22 @@
+archive/ES_0.5704811161301212---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T09:10:04.456
+Launch V∞: [7.32333735260727, -6.4527382249441745, -0.1759586088492076] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.765074530043722e-6, 0.00022631510419636195, 2.8507360365253247e-6] km/s
+ V∞_out: [0.00021535428744602685, -3.167469088881879e-5, 6.206616176833785e-5] km/s
+ time of flight: 1.6146094647378168e8 seconds
+ arrival date: 2029-06-20T03:25:50.456
+ thrust profile: [0.40729508398323533 -0.06593720398345142 -0.13225697117200946; 0.10333741123681943 0.0382390839398084 -0.10218904387607462; 0.10086483440379597 0.06730657249272808 -0.16507331236030948; 0.05510576210588362 0.04941278622972039 -0.13208578357357423; 0.07965378468926053 0.08460005389458568 -0.22763953317038801; 0.03921816161441595 0.048068919225994974 -0.14414543911078803; 0.019649999196606135 0.026925135295192564 -0.09227840215488434; 0.010818541855712072 0.014903396397480988 -0.050323194841536675; 0.003258664177531498 0.010900307279081424 -0.03586585030132855; 0.003516674779033905 0.005086999707179213 -0.01849720372318087; 0.0022984359633689225 7.578423272416384e-5 -0.005218388686664169; 0.004340607032744668 0.000660191820792848 -0.004013432633422304; 0.0002857019059567681 0.0033037769265042336 -0.013243209573579497; -0.0004468707335065744 -0.0013094126376438672 -0.0023841791225783413; 0.022928161115067024 0.003094270545962954 -0.015294218736147804; 0.001853954048943338 0.004922777578968038 -0.005312713579904073; -0.01183331622231199 0.019318583995050907 -0.01180736770124885; 0.01304287534423202 -0.006498850436911249 -0.0005778741920142413; -0.00922799841590348 0.0034106699840496272 -0.02546040913365545; 0.0032434608957292435 -0.0002857744414330515 -0.013181570902629107] %
+
+Mass Used: 109.64427374977731 kg
+Launch C3: 95.3000620117767 km²/s²
+||V∞_in||: 0.00022634994747186668 km/s
diff --git a/archive/ES_0.570526778220384 b/archive/ES_0.570526778220384
new file mode 100644
index 0000000..b1e1fe4
--- /dev/null
+++ b/archive/ES_0.570526778220384
@@ -0,0 +1,22 @@
+archive/ES_0.570526778220384---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T20:31:42.036
+Launch V∞: [7.261618154471929, -6.570291621301676, -0.21554832558816964] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.589229183959567e-9, 2.5527603820514156e-9, -1.3541045136977671e-9] km/s
+ V∞_out: [2.6442043613066708e-9, 5.161260104855979e-9, 1.6517499020162732e-10] km/s
+ time of flight: 1.563601926064948e8 seconds
+ arrival date: 2029-04-22T13:54:54.036
+ thrust profile: [0.434249618742277 -0.10676771746746196 -0.16394919680675432; 0.11116310158582188 0.025587465481722485 -0.13103491390245645; 0.06308056900284531 0.0289619424204246 -0.12637737059220203; 0.07193260824943229 0.043166152292968045 -0.1981307128910269; 0.031072892552174436 0.021754028449184483 -0.11156847827419043; 0.050766520222482334 0.03761346022109009 -0.2055738330134607; 0.02291482503650015 0.019251703052937177 -0.1114312671757442; 0.007809037466517107 0.006719246318604812 -0.05502951700373099; 0.016467045975998185 0.015595588733570578 -0.10421242285419044; 0.0022478155059820074 0.0008236224048005878 -0.017666490446864077; 0.0009590712969171132 0.0005130464185582139 -0.006333030047842146; -0.00017230008891173302 -0.001175317698597049 -0.0032118015372747622; 0.00045956851591127625 0.00022854977138335973 0.0007062816755849621; -0.0015796957124229079 0.000823520941486006 -0.002386323341711726; 0.005483007249198559 0.0007471385870016698 0.006053632543747812; 0.0029351086469061316 0.0011306710703547038 -0.0016504173635833136; 0.0021033665885481717 -0.0010749893854973497 -0.0028093373926541994; 0.006113475063199432 0.009917862728600062 -0.004550975629747032; -0.00015063317235134278 0.0034133544931270027 0.014454273542105442; 0.006620278451839019 0.0012862444772004285 -0.00025044489508387296] %
+
+Mass Used: 105.9278753931394 kg
+Launch C3: 95.94629129096718 km²/s²
+||V∞_in||: 4.607900903575837e-9 km/s
diff --git a/archive/ES_0.5705418725155025 b/archive/ES_0.5705418725155025
new file mode 100644
index 0000000..a711bdb
--- /dev/null
+++ b/archive/ES_0.5705418725155025
@@ -0,0 +1,22 @@
+archive/ES_0.5705418725155025---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T09:13:17.715
+Launch V∞: [7.222568819016708, -6.709798116624502, -0.40659172617342976] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.867074101958038e-6, 1.0706162762267287e-5, 5.4339365005164974e-6] km/s
+ V∞_out: [8.631544687134237e-6, -7.82006037348318e-6, -4.8428296473869095e-6] km/s
+ time of flight: 1.5183253161300537e8 seconds
+ arrival date: 2029-02-28T16:55:28.715
+ thrust profile: [0.33874909245307894 -0.08486776647994551 -0.13919288885787115; 0.09389080669744461 0.022138861501189707 -0.11255922086248099; 0.09525074493188174 0.044588511235513696 -0.18429103552891127; 0.06411520927424953 0.04015445695398257 -0.1757111216996553; 0.04683286801045586 0.035996341449610315 -0.15980233907151192; 0.03747861830830017 0.031230215664376098 -0.15706259756253135; 0.030543092227518085 0.02800644049422719 -0.14758324568083175; 0.01629723832290882 0.015648055177170595 -0.09229826417174505; 0.01329814691581197 0.01189686989324966 -0.07817676630246796; 0.0019030151967065296 0.0018701857341181264 -0.012879795698363204; 0.0014272593511682721 0.0015475232795488705 -0.010493721697634267; -1.686400448433511e-5 3.873383809800809e-5 -0.00019631317852761483; -9.189437470170804e-6 1.8139921347240272e-5 -6.79540451451842e-5; -3.603437974871891e-6 2.5315895688174953e-5 -0.0002564178251713968; -9.316686311563172e-5 -6.611980993648662e-5 -0.0002194872896831197; -5.3439917226698525e-5 2.4617582508925215e-5 -0.00020161021111570577; -2.427675793244202e-5 0.0001647288026235439 -4.821599887020027e-5; -5.256219564526697e-5 -0.00023470980545454978 0.00015767654453347415; 0.00014141815680520408 2.4570826845705596e-5 -0.00010909845788978844; -0.00014607461654514734 -0.0001703269932072313 6.252368156475034e-5] %
+
+Mass Used: 97.74430493343652 kg
+Launch C3: 97.35220794308282 km²/s²
+||V∞_in||: 1.2613637425177512e-5 km/s
diff --git a/archive/ES_0.57055237248586 b/archive/ES_0.57055237248586
new file mode 100644
index 0000000..d41db37
--- /dev/null
+++ b/archive/ES_0.57055237248586
@@ -0,0 +1,22 @@
+archive/ES_0.57055237248586---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T21:46:51.134
+Launch V∞: [7.718614736757986, -6.091785717747016, -0.08641901606014711] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.202524802271934e-6, -0.00016937460998746472, -2.9861060159948423e-6] km/s
+ V∞_out: [-0.00016406674398549307, 2.4843313390660657e-5, -3.614114730841999e-5] km/s
+ time of flight: 1.8749577777004185e8 seconds
+ arrival date: 2030-04-28T23:56:28.134
+ thrust profile: [0.544478815268061 -0.04532723146410489 -0.20143523563190494; 0.014034265912908862 0.005464434839582726 -0.020733781940348767; 0.017127597288203747 0.009363169633800246 -0.0402120210224618; 0.046463978010761714 0.027620627070616043 -0.16294407140766687; 0.027547468239981176 0.013372762932041551 -0.10490712026152511; 0.014616647493460871 0.009121009932420852 -0.09238787119411704; 0.005123751839313735 0.0023809293212866175 -0.02937908555895657; 0.009691595875542948 0.001093449810143652 -0.04552503023727082; 0.004783499824961146 -0.0004054716116814825 -0.027245261722795733; 0.004382214289911035 0.009803144384452563 -0.05156344207426219; 0.004507602111102323 0.0056604251069627175 -0.04402478460363589; -0.0024243624866856386 0.0008187733300554164 -0.008346193396099866; 0.0033068123438269076 0.0008514889264117461 -0.015794307392479348; 0.0006173446323238722 0.0023029431982928778 -0.0050203312746160715; -0.010055669794750765 0.0035286646856902844 -0.010348209004578222; 0.019542790459779434 -0.014015696953573025 0.0022590872876343832; 0.002060041344901324 0.0012476465883743749 -0.01316101063929355; -0.013344291229837851 -2.6757152826562035e-5 0.006271188543861304; 0.014447133916812006 0.022236094267517784 -0.007825043766822845; 0.0015156201948589689 0.0019250647435401936 0.006065529389595034] %
+
+Mass Used: 101.5941474647816 kg
+Launch C3: 96.69433493178087 km²/s²
+||V∞_in||: 0.00016955397872380314 km/s
diff --git a/archive/ES_0.5705838247664983 b/archive/ES_0.5705838247664983
new file mode 100644
index 0000000..f3acd09
--- /dev/null
+++ b/archive/ES_0.5705838247664983
@@ -0,0 +1,22 @@
+archive/ES_0.5705838247664983---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-07T17:53:38.652
+Launch V∞: [6.395073980999523, -7.8308870454425215, -0.583529025876716] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0010860614143763457, 0.0062986436744865626, -0.008586116174918116] km/s
+ V∞_out: [0.007244846100125107, 0.0060471266533162525, 0.005058363307275799] km/s
+ time of flight: 1.8599748845228255e8 seconds
+ arrival date: 2029-03-29T11:51:46.652
+ thrust profile: [0.02217599358178399 -0.007905743465591744 -0.011412004538807181; 0.057590306784003745 0.0004650418526826357 -0.08885070818482702; 0.04415034867569703 0.006743949689591947 -0.12072355934619272; 0.02955115054139491 0.005410949063519835 -0.11424407805020212; 0.033909296624299784 0.007057788231039337 -0.1623703994318454; 0.009848238978265228 0.0011084955157600878 -0.05492077357011484; 0.011475404483045315 0.0009744365129834413 -0.07338906853657305; 0.007269127629432862 0.0004608818285618193 -0.04988898698593559; 0.008610620461724207 0.0004693097433750511 -0.06640876134338428; 0.008201365038850189 0.0006473409331991222 -0.057144661885668836; 0.005307234550841315 0.00017253693907351894 -0.050800913828124454; 0.00021659246445779182 -5.488743568869762e-5 -0.0013698223801904144; -0.0005600738896949021 -0.00011625261862939173 -0.0003890932106980543; 7.634617091936273e-5 5.672531042811386e-5 -0.0008998191634951817; 0.00013198500821985626 -4.774166153857643e-5 -0.0003953950759092048; 0.00046831733216908813 -0.00019136910464271609 -0.0006766672350387486; -0.0003045977635948187 -0.0014482126144760505 -0.0014582991715554037; -7.042766789938637e-6 -0.0019942190871296154 -0.0004676990319675145; 3.5258027769163305e-5 3.462487134280523e-5 4.422158671932172e-5; 5.9986502866672475e-5 0.00039836742997170137 -0.0003979459445808801] %
+
+Mass Used: 67.41289151521414 kg
+Launch C3: 102.56026926497722 km²/s²
+||V∞_in||: 0.010703916689844762 km/s
diff --git a/archive/ES_0.5705920986647848 b/archive/ES_0.5705920986647848
new file mode 100644
index 0000000..8e009c7
--- /dev/null
+++ b/archive/ES_0.5705920986647848
@@ -0,0 +1,22 @@
+archive/ES_0.5705920986647848---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T06:07:26.236
+Launch V∞: [6.205920426867448, -7.497751886805073, 0.21794856350231473] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012713129078956796, -0.005800779466793214, -0.023322899244192386] km/s
+ V∞_out: [-0.017547722821063934, -0.007092674468463115, -0.019514412045323785] km/s
+ time of flight: 1.7543604802624956e8 seconds
+ arrival date: 2028-11-15T18:21:34.236
+ thrust profile: [0.465008777248815 -0.15262547427330364 -0.14982819006061637; 0.0897941084480717 0.020428091489167757 -0.08695677583052107; 0.07200610407402801 0.03530098965504445 -0.11350007461572169; 0.04529763884636333 0.03097516714962656 -0.10014737871448595; 0.04286393427800179 0.035984354371593225 -0.11997419799970566; 0.028042286665227057 0.027198832491339968 -0.0945638704389363; 0.01665513881360081 0.018029368964683462 -0.06721827224273673; 0.010882114792445153 0.010085081457056074 -0.04499708539272305; 0.01893705136553847 0.024061553519271032 -0.0921808404217276; 0.004321837791540568 0.0030102319989837294 -0.011689645624868206; 0.0384942034064209 0.054326645218200666 -0.1984905847224473; 0.0023564543284462953 0.0030168648991066274 -0.002905683245776133; 0.0003083522657681125 0.0002856879044120247 -0.0015181192241436638; 0.0005217042924718271 -0.0018391723510071479 -0.0011242305821296998; -0.00457417224368792 0.003503599635222651 -0.002665270580350402; -0.00027993832242277 -0.003748070744325001 -0.011285028540675587; 0.0005368674726334433 -0.000757144192950599 -0.0007531470299920857; 0.00126275589430904 0.00319831094478831 -0.0014077852508261064; 0.0011302999300106843 -0.0005317492394572021 -0.00619226573577126; -0.011582314780974618 0.003227777941598933 0.00294361022094665] %
+
+Mass Used: 112.82358765955996 kg
+Launch C3: 94.7772332770324 km²/s²
+||V∞_in||: 0.027188790384188415 km/s
diff --git a/archive/ES_0.5706337391225589 b/archive/ES_0.5706337391225589
new file mode 100644
index 0000000..0497977
--- /dev/null
+++ b/archive/ES_0.5706337391225589
@@ -0,0 +1,22 @@
+archive/ES_0.5706337391225589---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T09:31:22.044
+Launch V∞: [6.874039508989821, -7.175829076670336, -1.2018565574953077] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.665246779596888e-6, -3.7132271072069094e-7, 8.617913430841464e-9] km/s
+ V∞_out: [4.947648433797449e-7, -1.1226114556554035e-8, -2.6430157553332215e-6] km/s
+ time of flight: 1.8749577783064124e8 seconds
+ arrival date: 2029-04-08T11:40:59.044
+ thrust profile: [0.18189350442724667 -0.060423981993330274 -0.08134958832098506; 0.01917091132069342 0.0031977793738358707 -0.02673992373212045; 0.053967768184674345 0.01843364314564972 -0.12806124356248313; 0.05840749202303326 0.025102223490263222 -0.19955813812159615; 0.03538315777854394 0.01871399775644151 -0.15367367431894038; 0.028674912822086188 0.016748293591184914 -0.15167011872870126; 0.015170337089245879 0.01006766455794032 -0.09402418538870076; 0.006419145562875245 0.0046972771588450445 -0.04632097617357742; 0.001937405555726761 0.0014936060501634307 -0.01598543188283403; 0.00011707213487165884 0.00041616340046829784 -0.0044677859191771235; -0.0001962167816349454 0.0005792806747615426 -0.0036436961983074565; -0.0005577690373122848 0.0008850726311312675 -0.001618106075359398; -0.0008358789060860323 -3.0451503115586434e-5 -0.0010505677461082716; -0.0001326111521541833 0.0012206237333053913 -0.0006472247868812288; 0.001508884119511729 0.000503005288282927 -0.0028119346375022544; -0.00069309366196143 -0.0010348842722750409 -0.001022481591086548; 0.0014412929927568002 0.0004175168975900952 0.0007280031948025674; -0.0015842069761535422 -0.0006821756900857934 0.00143982394044257; -0.00213747511682334 -0.0008804351464083339 -0.0007617659235127211; -0.0005877441805700016 -0.0005106624317601432 -0.0006747944809324548] %
+
+Mass Used: 81.30118809736496 kg
+Launch C3: 100.18940129353493 km²/s²
+||V∞_in||: 2.6910026421541183e-6 km/s
diff --git a/archive/ES_0.5706812262388509 b/archive/ES_0.5706812262388509
new file mode 100644
index 0000000..285e13f
--- /dev/null
+++ b/archive/ES_0.5706812262388509
@@ -0,0 +1,22 @@
+archive/ES_0.5706812262388509---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:49:54.532
+Launch V∞: [7.227937950738403, -6.689748284853356, -0.5400930734552932] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00010060464118334974, 0.0016256429062963902, -2.2249122705880453e-5] km/s
+ V∞_out: [0.0015180860984099478, -0.00024868197085689943, 0.0003200909736414455] km/s
+ time of flight: 1.5376329249887002e8 seconds
+ arrival date: 2029-03-23T15:51:26.532
+ thrust profile: [0.32846097213310727 -0.08059381234481891 -0.13621844355808901; 0.12405553729342936 0.028569702592342438 -0.14985247452911354; 0.09471940048075722 0.04328665745643816 -0.18737712417251925; 0.05281874162708362 0.031049529300684997 -0.14726435844515798; 0.039252358808992666 0.02722339307315745 -0.1377231473697821; 0.033776713412053516 0.026427481516263594 -0.14440348786568255; 0.029961820440039567 0.02581401683040474 -0.15449885601384408; 0.023456037097504025 0.02062860066714922 -0.12685239555655775; 0.004295676375218761 0.0034408210946982277 -0.025273001458786623; 0.0014623801080341377 0.0027623166139242195 -0.008895850443642255; 0.0018126530204319756 0.00044056803959666873 -0.004731774388049242; 0.0011386893605010854 0.0009875729785929746 -0.008091256540661897; -0.0006489560933140492 -0.0004859459206814705 -0.0036067676910550035; 0.00015117709088239593 0.0014173514030706323 -0.0018414098924268716; -0.0017190773005850563 0.001318458741204306 -0.0025099302084998472; 0.0035746046892948147 0.0017537461947267218 -0.0034791322605919953; 0.0015789708094516362 0.0026908708560748804 -0.0018099060649055879; -0.0021808193164245242 -0.002283722439363909 -0.002331382992344249; 0.0019582405196274548 0.001330915215829386 0.005859542914863584; 0.005062044661771625 0.0040949884918163315 -9.460462752921618e-5] %
+
+Mass Used: 98.2842325812253 kg
+Launch C3: 97.28751966241727 km²/s²
+||V∞_in||: 0.0016289049008707003 km/s
diff --git a/archive/ES_0.5706864393892398 b/archive/ES_0.5706864393892398
new file mode 100644
index 0000000..47e00af
--- /dev/null
+++ b/archive/ES_0.5706864393892398
@@ -0,0 +1,22 @@
+archive/ES_0.5706864393892398---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T07:43:35.833
+Launch V∞: [5.7534584720168835, -7.673612376971402, 0.07907731438053407] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4641499207774514e-6, -1.5662219251623203e-6, 1.179339420161605e-6] km/s
+ V∞_out: [-1.6891057489372574e-6, 2.2033271759173694e-6, -1.4888207878803232e-6] km/s
+ time of flight: 1.636193759047149e8 seconds
+ arrival date: 2028-06-29T01:33:10.833
+ thrust profile: [0.6722179106774056 -0.28207266549487436 -0.23678197503967163; 0.14667251979646329 0.01808678298695633 -0.14645068425895535; 0.12537824408571777 0.04611468844441102 -0.19980126139350174; 0.08149801802469048 0.04277766356816069 -0.17814654798908644; 0.05120320422508897 0.03280527313828946 -0.14121210485072763; 0.03428867770319489 0.02546642959804087 -0.11327162549134598; 0.02703908137523086 0.022318624647279572 -0.10247553107956263; 0.019353333395660435 0.017405766815568345 -0.08324698820851936; 0.006302824618056568 0.006165322076614921 -0.03059040566438984; 0.005362282378066466 0.005343770347265264 -0.028207027114569183; -0.00011007784197670915 0.0031644230059001545 -0.004559430068767923; -0.000864872215532195 0.0022084514551747383 -0.0024236221769767677; 0.0009913287227601543 -0.0012081944769350953 -0.0011099285341761253; 0.004051302410717355 -2.3680786739906773e-5 0.0015197217562277097; -0.0015332579014578236 -0.0005455169700140951 0.0009529494670050492; -0.000735922784345389 -0.0008739722719336414 -0.0028920398278887644; -0.00019194731358886477 -0.00101410143612448 -0.0006909904209766585; -0.0055659411425769394 -0.0028546463918405715 -0.0007262582681769477; 0.0005989588653197953 -0.004331123202290038 -0.002061683795921638; 0.0007668370594052433 0.001079683872516024 -0.003075108952330729] %
+
+Mass Used: 129.1758029039729 kg
+Launch C3: 91.99286452288118 km²/s²
+||V∞_in||: 3.1489565603345177e-6 km/s
diff --git a/archive/ES_0.5707169409216226 b/archive/ES_0.5707169409216226
new file mode 100644
index 0000000..15aa428
--- /dev/null
+++ b/archive/ES_0.5707169409216226
@@ -0,0 +1,22 @@
+archive/ES_0.5707169409216226---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T13:51:43.360
+Launch V∞: [6.172899507756495, -7.723089194518419, 0.012388827612957216] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008471098011588579, -0.005425145785834893, -0.008497742982826951] km/s
+ V∞_out: [0.005464620507806921, 0.00986600700720801, -0.006795317817928243] km/s
+ time of flight: 1.7316607332828298e8 seconds
+ arrival date: 2028-10-22T19:32:56.360
+ thrust profile: [0.1947385409683376 -0.07185843454448536 -0.0767254627916082; 0.06598406708796405 0.009065598848701166 -0.07292717363068849; 0.09215354239782465 0.03327543597871379 -0.16572912959770975; 0.08025498872810692 0.04043082395405865 -0.1977770547134523; 0.0406904318364295 0.024565617962966683 -0.12766241201727127; 0.03534010013775763 0.024424241954448877 -0.13326720309802997; 0.012695405865659894 0.009375539396141875 -0.05956327615420628; 0.019675976970252695 0.013303506343683904 -0.08201140871360414; 0.014498305562061355 0.00823135745049466 -0.06573070047937153; 0.006161051609702178 -0.0006470108400931348 -0.01896144943234461; 0.011328182610799153 0.004312993250299575 -0.028140705038268522; 0.00022605122667474832 0.0008154632609040241 -0.0059800059520557355; -0.0020706107355316413 0.00012621789601433443 0.006534190329079615; 0.0017218282850085611 0.0007181873648622965 -0.010699584999898717; 0.0028819343455565322 -0.0008538164659663262 -0.007432216239690754; -0.0026926641327286852 0.014172478390191402 -0.004942889382925759; 0.004130371547869025 0.005148896759455584 0.0037527845070928776; 0.0008584555455648964 0.004075695412851786 0.0004948181921916647; 0.0019686870542517574 0.0035259933301691826 -0.011330133733036221; -0.04118617300279925 0.012993321854947913 0.010605178761610459] %
+
+Mass Used: 95.62256469457634 kg
+Launch C3: 97.75094852239717 km²/s²
+||V∞_in||: 0.013168270354214586 km/s
diff --git a/archive/ES_0.5707215023017138 b/archive/ES_0.5707215023017138
new file mode 100644
index 0000000..9e03bbd
--- /dev/null
+++ b/archive/ES_0.5707215023017138
@@ -0,0 +1,22 @@
+archive/ES_0.5707215023017138---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T13:56:03.170
+Launch V∞: [6.012122594610497, -7.458478878872989, 0.120946058273188] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.118999546516455e-6, 2.0265753079196843e-6, -1.4079634533712522e-6] km/s
+ V∞_out: [1.319687951902707e-6, -3.241303072782815e-6, 1.8895437336454944e-6] km/s
+ time of flight: 1.752091474537187e8 seconds
+ arrival date: 2028-11-10T11:08:30.170
+ thrust profile: [0.48423375590113393 -0.15766969390933286 -0.13512197769678796; 0.45475885372167707 0.10907505817583094 -0.3405213050206547; 0.08512294919449874 0.044513938648311165 -0.1195515971692241; 0.0656852706429679 0.048833132698536376 -0.13020543455088734; 0.04479866007284768 0.04031828309396881 -0.11282521166714438; 0.02857499513016798 0.030006910218452504 -0.0881941550017092; 0.027370226137419386 0.03448924658697804 -0.12319499270779727; 0.0072174329866067834 0.008325645855265693 -0.02369400933427756; 0.003655689867166332 0.0037665528299894537 -0.013367914997824032; 0.0003284818378487121 0.0023647263795993165 -0.006572089729436025; 0.002869637282334263 0.002773711076271595 -0.004384315633669642; -0.0014868030466820665 0.0009371751001963284 -0.0017720303642427392; -0.00043526599434062264 -0.002212166964611925 0.0007033629311001908; 0.0016685501667245684 0.0015202118430583415 -0.002588056248481995; 0.0002532118775581565 -0.002372911464698099 0.004954945143475732; -0.001197584688007658 0.0032443526550170847 -0.00932820446293575; -0.009222099386314589 -0.008522540644249423 -0.0027105773678520488; -0.0005310196114080347 -0.000678053779740102 -0.0031677440218407698; 0.0036687961775221773 -0.002882854550610517 -0.004271015650004491; 0.0006226110957557895 0.000416432564267792 -0.0003760699632392629] %
+
+Mass Used: 130.4050255206439 kg
+Launch C3: 91.78915322823237 km²/s²
+||V∞_in||: 3.977125436275391e-6 km/s
diff --git a/archive/ES_0.5707245829851213 b/archive/ES_0.5707245829851213
new file mode 100644
index 0000000..6755b8a
--- /dev/null
+++ b/archive/ES_0.5707245829851213
@@ -0,0 +1,22 @@
+archive/ES_0.5707245829851213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-08T03:24:09.192
+Launch V∞: [6.2163243367672925, -7.860947843213834, -0.19127000913937214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.266346408370801e-9, -1.6078016529731705e-9, 2.5044340387807374e-9] km/s
+ V∞_out: [9.210074296401742e-10, -2.0492597015591167e-9, -2.7352822972870656e-9] km/s
+ time of flight: 1.874957778381516e8 seconds
+ arrival date: 2029-04-16T05:33:46.192
+ thrust profile: [0.21613292842813034 -0.057271235588954715 -0.09120690460488157; 0.03082986663903099 0.005570151392284965 -0.041641623017900156; 0.028378870986546918 0.009820166291859351 -0.06357246883866831; 0.04787764151249461 0.020825893729289613 -0.14849561345665896; 0.03121141127654728 0.015001700311128085 -0.11957104386765316; 0.033313169259872606 0.016933203026744288 -0.15910558289018942; 0.01143019878153833 0.007232358322369202 -0.061812420556562116; 0.010396872249034407 0.006521333304748144 -0.06239742532228194; 0.006944494336426984 0.005373673569799129 -0.06002383177439193; 0.0051289555524844915 0.0028231448441747267 -0.04294350079802217; 0.0017527316567245432 0.0011529941699942865 -0.015431053984717379; 0.00036066352616555345 0.0005331090284239887 -0.00041837634907934793; -0.00011844139643185581 -0.0008402761568206922 -0.001578167519051406; 0.0013673390785575307 -0.0006220541126172481 -0.0021781314964958646; -0.000122793917801813 0.0005399857952518898 -0.0008604124354545314; 0.00033540328273599224 0.0006069307056125984 -0.0018335331478670685; -0.000533287906064891 0.0009538322019685675 -0.0009227141213077835; -0.0003398780587375019 0.00029621145208222474 -0.0011088097041335155; 6.306045825419195e-5 -8.970508008305589e-5 -0.0002743786016611025; 6.377948872851602e-5 -0.0006574663133980632 0.0012182917792108797] %
+
+Mass Used: 79.74833490758465 kg
+Launch C3: 100.47377347000973 km²/s²
+||V∞_in||: 3.740794307716222e-9 km/s
diff --git a/archive/ES_0.5707681656074521 b/archive/ES_0.5707681656074521
new file mode 100644
index 0000000..3e2a0ba
--- /dev/null
+++ b/archive/ES_0.5707681656074521
@@ -0,0 +1,22 @@
+archive/ES_0.5707681656074521---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T20:15:48.970
+Launch V∞: [6.016080426591399, -7.5341739120445546, 0.03639585214554741] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.021539992656677318, 0.015825066021186298, 0.01712821372474223] km/s
+ V∞_out: [-0.0150378162376851, -0.02284239134781176, 0.016121617781898044] km/s
+ time of flight: 1.7010987383468345e8 seconds
+ arrival date: 2028-09-12T17:00:21.970
+ thrust profile: [0.6147677854558843 -0.21936017285697637 -0.19480809478111186; 0.11984057589782217 0.024148700838447994 -0.11207775989897478; 0.09249603517057453 0.04315369398571665 -0.13957302944662484; 0.045886477696811444 0.03047023845809737 -0.09652830699465491; 0.03921045786681176 0.03140770321079646 -0.10192559726956944; 0.03454681436203794 0.03278786699756957 -0.10948517362878499; 0.033327031774530516 0.03564533790774748 -0.12623436027838567; 0.04695294811381847 0.05474514354750403 -0.18964692353351775; 0.011725827288189767 0.01379474622930677 -0.05295222931729721; 0.0009930313827655204 0.0013453957612144303 -0.005859482535283156; 0.0053397815146557365 0.008636998109842874 -0.03259379673324245; 0.0005381473727112104 -0.000212544352966972 -0.0015168443398030737; -0.00047809720173047995 0.00032714582361809927 0.0010687046065040806; -0.0007819707953932665 -0.0020357900425749223 -0.0006643395538985847; 0.0002101736541348972 0.00010343812397260775 0.0008823435147961203; 0.0011340369954209208 -0.001122982849668885 -4.9689176088525276e-5; -0.001973079805181143 0.001270415377724298 0.004490744128507958; -0.0001736634610518283 0.0006682550877200556 5.220487858320725e-6; -0.005039822013587363 0.0017087800649394618 0.00026387283051595664; -0.0003131905901806551 -0.0038350705351660437 0.007071318180795342] %
+
+Mass Used: 123.639297992514 kg
+Launch C3: 92.9583248942023 km²/s²
+||V∞_in||: 0.031745546201397544 km/s
diff --git a/archive/ES_0.5707925638659523 b/archive/ES_0.5707925638659523
new file mode 100644
index 0000000..ca76166
--- /dev/null
+++ b/archive/ES_0.5707925638659523
@@ -0,0 +1,22 @@
+archive/ES_0.5707925638659523---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T10:09:26.454
+Launch V∞: [6.548661300603439, -7.400537469909829, 0.09260847353442782] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4588285234642255e-7, 3.836685322036807e-8, -4.64297008580165e-8] km/s
+ V∞_out: [1.5239453488776032e-7, -3.830377501968548e-8, 1.9313698662854358e-8] km/s
+ time of flight: 1.8749577787501624e8 seconds
+ arrival date: 2029-04-10T12:19:03.454
+ thrust profile: [0.24308555979238078 -0.06459064250720145 -0.09158370921185152; 0.08102810623408074 0.01858120762944112 -0.09248871818322578; 0.05205810298471298 0.023378341369599855 -0.1004998783932954; 0.044947527930280735 0.026694547827073735 -0.12232353763180845; 0.034662017055018 0.02446765258115549 -0.12029593542728982; 0.021822929390099152 0.017412984713837783 -0.0918393226318277; 0.010426053940244873 0.009666685595462911 -0.052068954820155104; 0.01536513166993755 0.013325434183463965 -0.08203371726419342; 0.01084781321005725 0.009981988897718883 -0.06350856103609896; 0.0010821016399105473 -0.001170236501193217 -0.0058904940524045725; -7.26417225998012e-5 0.0026139256797095283 -0.009124586147062722; 0.0029833191843386085 0.0006458080280929961 -0.00956499522111949; 0.010221133285641715 -0.007315175470872204 -0.004716264764396018; 0.006668418961322087 0.004349589013728375 -0.005335298246012093; -0.02381154329541314 -0.013431482910161191 -0.03504417724985891; 0.005763274713223595 0.0009024665311313555 -0.037306729956447494; 0.010487493145567671 0.001498451450470671 -0.02606027636121134; -0.018043156008846692 0.014992443772702533 -0.00770324855211882; -0.007113776421061331 0.0025109583437856187 -0.02163448699776455; 0.011502168478763806 -0.008256054987271316 -0.003161958433269189] %
+
+Mass Used: 96.2325978265144 kg
+Launch C3: 97.66149600293087 km²/s²
+||V∞_in||: 1.5782756146036818e-7 km/s
diff --git a/archive/ES_0.5707980265338999 b/archive/ES_0.5707980265338999
new file mode 100644
index 0000000..44e9de2
--- /dev/null
+++ b/archive/ES_0.5707980265338999
@@ -0,0 +1,22 @@
+archive/ES_0.5707980265338999---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T20:49:56.122
+Launch V∞: [6.66740916392803, -7.343569462101642, -1.1341060368618336] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.637485729595372e-6, -3.474317860205479e-6, -3.91229077834366e-6] km/s
+ V∞_out: [-5.3083500074630995e-6, -3.5184704977813797e-6, -1.4380011409387996e-7] km/s
+ time of flight: 1.859158476430046e8 seconds
+ arrival date: 2029-03-21T16:07:23.122
+ thrust profile: [0.15474679322564452 -0.04753243979377883 -0.06164713317408067; 0.07193979524369275 0.016095838940910417 -0.08798219856956839; 0.057480070087175636 0.026403950549740984 -0.11897440234701163; 0.03981868304073765 0.025438871247372735 -0.11909789509098326; 0.03185626939216908 0.024639725782250342 -0.12341271265026645; 0.023779185797706083 0.02147130917805505 -0.11449956630184868; 0.016692165697005542 0.017279080076140495 -0.09717960979987403; 0.011899931234407449 0.013698737288757283 -0.08093783692047442; 0.007547829864855809 0.009565162960079652 -0.05883987794800929; 0.004214544231406188 0.005724740852587331 -0.036402157801826575; 0.001316593311518111 0.0017799405093652093 -0.011169912685732008; 0.0003832532222509415 0.000569067336049756 -0.003335381771077787; 0.002479345114336153 -0.0015949445090721426 -0.0029357341686609357; -7.680641655310479e-5 -0.00021465238279979055 -0.00027624844848239466; -0.004126487286229181 0.0022462348394366137 -0.009102756456584008; -0.0026711891721222375 0.0010323520301569696 -0.002746651979416012; 0.006608330718023003 -0.0002241347485945869 -0.008783900165948287; 0.005942794796758515 -0.0005296376105170689 -0.0032366285868420247; 0.0056069965278204015 0.00014800202672031546 -0.006435242866188426; 0.0013651370991456784 -0.0006153240500104842 0.0015894607598675374] %
+
+Mass Used: 84.53113316660983 kg
+Launch C3: 99.66855390678973 km²/s²
+||V∞_in||: 6.37245683869774e-6 km/s
diff --git a/archive/ES_0.570825020361168 b/archive/ES_0.570825020361168
new file mode 100644
index 0000000..52fee1c
--- /dev/null
+++ b/archive/ES_0.570825020361168
@@ -0,0 +1,22 @@
+archive/ES_0.570825020361168---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T13:44:38.664
+Launch V∞: [6.508932115555804, -7.48619730783656, 0.0061980729821473814] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008763832992210419, 0.0002823231672753773, -0.005872374691810846] km/s
+ V∞_out: [0.0101467042834473, -9.743523243678577e-5, -0.0029028489310217484] km/s
+ time of flight: 1.8567970835029045e8 seconds
+ arrival date: 2029-03-20T15:26:26.664
+ thrust profile: [0.19185642946662662 -0.053805967939154584 -0.07381524851554154; 0.07334460717600345 0.01652572549256588 -0.08679349372683469; 0.04231277661630691 0.019043311791730577 -0.08245349042916546; 0.0382978325430314 0.024398610374742846 -0.10668615231977897; 0.02387169533067076 0.018408456675752517 -0.08565414372084271; 0.022592174211587365 0.018915479220131932 -0.09630464724251929; 0.014240900397352162 0.014090501987512065 -0.07287710077859134; 0.027198579414425775 0.025880945814302343 -0.15097409355041783; 0.014277912785089669 0.015171950233311977 -0.09152073358230112; 0.0026249972357832935 -0.0015155031150816132 -0.012758994519111052; 0.0032201824233906275 0.005917974297025379 -0.01634576157613818; 0.0008190606029770833 0.0012137209261606694 -0.006435583402085826; 0.002308243658472155 0.0006656209887833432 -0.0024008402510020312; -0.0057846212407290445 -0.006025694891976173 0.0013199717460042788; -0.0042619245289773336 -0.013888901264503381 0.0006667728760590928; 0.022099678806086903 -0.010354043052929755 -0.006354532307383292; 0.01937803668099223 0.0036300616523455022 -0.027476245431851877; 0.0014608278285861448 -0.010046548657506168 -0.03238757535639089; 0.002832498642164427 0.0112185480559837 -0.022748085802400328; 0.005494430209194207 -0.0002973621202338606 -0.0032136379977272277] %
+
+Mass Used: 91.90777306288555 kg
+Launch C3: 98.4093858328818 km²/s²
+||V∞_in||: 0.010553163488127943 km/s
diff --git a/archive/ES_0.5708370868781211 b/archive/ES_0.5708370868781211
new file mode 100644
index 0000000..6491ebb
--- /dev/null
+++ b/archive/ES_0.5708370868781211
@@ -0,0 +1,22 @@
+archive/ES_0.5708370868781211---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T01:37:29.451
+Launch V∞: [6.647335792422472, -7.419313040222501, 0.03823837937837881] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2915496803790866e-8, -3.545961576405112e-8, -2.0334260122774698e-8] km/s
+ V∞_out: [-1.4140551036377954e-8, -2.3303807796722032e-8, 3.446800885221986e-8] km/s
+ time of flight: 1.8749577787466508e8 seconds
+ arrival date: 2029-04-11T03:47:06.451
+ thrust profile: [0.13770446105535095 -0.038549439319591594 -0.05757003625755346; 0.08395839931907986 0.01635856098760957 -0.103214864320961; 0.03216263362670559 0.012832471067648893 -0.06852628709934053; 0.027810610221284525 0.014921790325074413 -0.08441349742705881; 0.023126074734645993 0.014516393062248655 -0.0895320039021103; 0.017297627171958877 0.011869204282229782 -0.08057405052658373; 0.008593815335283927 0.008178348532593789 -0.056394317859031165; 0.02092659482854486 0.013248445829477363 -0.1232600412047311; 0.014717602060996371 0.01678910524242827 -0.12375215396831923; 0.006432851497351703 0.006051604775780887 -0.05901825507943755; 0.0019436638925175685 0.0013341847010355744 -0.010720399839950243; 0.0050617321097043205 0.004370007925540854 -0.0438993570572876; -0.004781562607422291 0.007392691123702209 0.0045472634081789014; 0.0017818955871160582 -0.0025391150506553686 0.004100168085333113; 0.0005246526043301705 0.0033687242160537136 -0.0033186912985010584; 0.0007802415034901458 -0.008819695466990077 0.013081929906472424; -0.005907581096993508 0.00047594046287596694 0.002879753219838729; 0.0022151378760589045 -0.0030549269215859928 -0.0016025640115213246; 0.0055931735734070466 -0.0037820092599416626 -0.04586237318837576; 0.00028983305594857376 -0.0035495184364244987 0.01759982515774619] %
+
+Mass Used: 87.10727710959281 kg
+Launch C3: 99.23474129969402 km²/s²
+||V∞_in||: 4.686135378581542e-8 km/s
diff --git a/archive/ES_0.5708441139062098 b/archive/ES_0.5708441139062098
new file mode 100644
index 0000000..e88bc7d
--- /dev/null
+++ b/archive/ES_0.5708441139062098
@@ -0,0 +1,22 @@
+archive/ES_0.5708441139062098---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:51:36.045
+Launch V∞: [5.676608439818659, -7.854651754480129, -0.3350209386502166] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.640778175952375e-6, 1.5241682162770887e-6, -1.0721733918668616e-6] km/s
+ V∞_out: [1.109749463535313e-6, -2.620154027403566e-6, 1.533553554646382e-6] km/s
+ time of flight: 1.5807973574567172e8 seconds
+ arrival date: 2028-04-26T06:53:51.045
+ thrust profile: [0.5275713440318048 -0.24920373274654134 -0.20887469586539467; 0.11558340772967175 0.007541809890779937 -0.11865663245714535; 0.0838824886582178 0.02466074180792187 -0.1369892070635763; 0.14136398950296572 0.06270429428633499 -0.30675594493961905; 0.06499466280281219 0.03583937595566934 -0.1779623649118113; 0.04721570198401685 0.030415053058036115 -0.15384472457662376; 0.025233424718163262 0.018139603556977725 -0.0956043791703585; 0.014123180721749172 0.011099700957690794 -0.06085288821905578; 0.003742438931633055 0.00298216800362699 -0.01832993669143044; 0.002707174244421949 0.0024604812378895948 -0.01430238427328603; 0.0012825405197078336 0.0006454520264091234 -0.005856675691110721; 0.0006784352982134724 -0.00021261310901050012 -0.001076231335176334; -0.00018639942413695534 -6.539880634999138e-5 -0.0005264184852909319; -0.0005686636753634631 0.0008131586045424448 0.0004226833975109688; 0.0008281506748677934 -0.0004518760193543579 -0.0012889962005403583; 0.00034012837735722715 0.00014134706345637698 -0.001055425419185996; -0.0007277183392140612 0.00013027203104060467 -0.0011075433947422982; 0.0006884258192547312 0.002195544381228575 -0.0014288461947482012; 0.0011445542883779703 0.0009534114666934133 -0.0010330776855648316; 0.002028334969646049 0.0010235487624300228 -0.001554715366408056] %
+
+Mass Used: 117.4666861009232 kg
+Launch C3: 94.03167659251227 km²/s²
+||V∞_in||: 3.2320819773518936e-6 km/s
diff --git a/archive/ES_0.5708644127218805 b/archive/ES_0.5708644127218805
new file mode 100644
index 0000000..c7ca782
--- /dev/null
+++ b/archive/ES_0.5708644127218805
@@ -0,0 +1,22 @@
+archive/ES_0.5708644127218805---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-06T11:44:16.342
+Launch V∞: [6.182852125474715, -7.956647591804593, -0.31888820354389447] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.021329803020194323, -0.009392351153761925, 0.023403340318924912] km/s
+ V∞_out: [-0.021044251507420904, -0.008648254914365648, -0.023941698649888887] km/s
+ time of flight: 1.801523554254443e8 seconds
+ arrival date: 2029-01-19T14:03:31.342
+ thrust profile: [0.0946718397092322 -0.04109481669074475 -0.05109926220955143; 0.04884690512063872 -0.0037680131563762706 -0.08020021132977175; 0.03848010628202163 -0.00034416668170526843 -0.10044835363333143; 0.03771215752619888 -0.0015848159291726746 -0.14405387572755401; 0.033124565887150556 -0.003090764680163807 -0.15888043318890352; 0.02432918411076583 -0.0035985407854494636 -0.1347088245101737; 0.01691235033798882 -0.0036921655796585537 -0.10099120258192504; 0.01139583950417862 -0.0029294668006274835 -0.08032496038152101; 0.00627076288365393 -0.0017781672086211715 -0.0500274883797369; 0.0009845212604397118 -0.0003605134932869223 -0.007960247776038118; 0.0001823697430687553 -6.35932637555496e-5 -0.0018388580560668509; 0.0004277817809332406 -0.0001914673374788681 -0.004175377539067359; 0.0009948304945480483 -1.5300455047520043e-5 -0.003011644304726459; 7.961308565647245e-5 -8.193520033603161e-5 -0.00015599743052026617; 7.77502991153775e-5 -5.921541704035335e-5 -0.00090227993557244; 8.229933580888296e-5 -0.00019224627283495783 -0.00012140198578340503; 2.7655519033349413e-6 -5.887918186825176e-6 -0.0003496049549284121; 3.3311445673714195e-6 -6.549505205878692e-5 -0.0004029142600971969; 0.0002887251481425158 -0.00029883133658784695 -0.00012884661713851142; -0.00020817706738987437 -0.00010740709466424347 -0.0005191872579292775] %
+
+Mass Used: 73.12253405543106 kg
+Launch C3: 101.63759099201648 km²/s²
+||V∞_in||: 0.03302867080521528 km/s
diff --git a/archive/ES_0.5708918824220744 b/archive/ES_0.5708918824220744
new file mode 100644
index 0000000..5acf953
--- /dev/null
+++ b/archive/ES_0.5708918824220744
@@ -0,0 +1,22 @@
+archive/ES_0.5708918824220744---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T06:25:58.142
+Launch V∞: [7.511683073849457, -6.263460674314784, 0.028082284799217674] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.729106539269154e-9, 1.0012046325358867e-8, -3.8426217396096795e-8] km/s
+ V∞_out: [-1.1806876528473808e-8, 3.812182341101456e-8, -6.411302669781946e-9] km/s
+ time of flight: 1.621955969021197e8 seconds
+ arrival date: 2029-06-27T12:45:54.142
+ thrust profile: [0.3905318701400257 -0.07180265160387449 -0.13068448741419858; 0.13042479160364165 0.040703649758432395 -0.1381141509684239; 0.0901039370029645 0.05055747827982668 -0.1631874020418272; 0.09416200252894359 0.06934823354536326 -0.23925470000666366; 0.048391673421760706 0.04109137843800298 -0.16069485862908992; 0.029153251482011266 0.029980688175536306 -0.12485385813017436; 0.009572379976169158 0.010333795373334507 -0.04989601556447355; 0.0065079282486027994 0.010976382747120662 -0.04202289107874685; 0.011738285322037433 0.01219767852295752 -0.053260049515534; -0.00017237571098887498 0.009634116323033085 -0.014834168118837816; 0.006620322217767631 0.0011413514673657495 -0.01689241318875522; 0.003424279281124822 0.0011999098456833067 -0.00799261018425725; 0.0006223838902031724 0.0018058043241402835 -0.0027732467149521947; 0.007374223052998735 -0.001697362313075598 -0.001537182655200667; 6.559440318344842e-5 0.0033850074857694184 0.004278786716693477; -0.0072251643209298895 -0.018951317797023186 0.006058583373993665; 0.0030675821592616994 -0.0027042354071087358 -0.009283010830948363; -0.009854407742687716 0.016609419416193545 -0.009365381028904742; 0.021509960443470703 0.0039058819675108864 0.0030308392179511723; -0.0009837268661204899 -0.002844613889430158 -0.008437258962541971] %
+
+Mass Used: 108.04071628613156 kg
+Launch C3: 95.65711083536377 km²/s²
+||V∞_in||: 4.0120293078833815e-8 km/s
diff --git a/archive/ES_0.5709781035201839 b/archive/ES_0.5709781035201839
new file mode 100644
index 0000000..09ca233
--- /dev/null
+++ b/archive/ES_0.5709781035201839
@@ -0,0 +1,22 @@
+archive/ES_0.5709781035201839---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T06:43:13.520
+Launch V∞: [6.01606567625349, -7.736755666944507, -0.4102259163002004] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008043865287187573, -0.0005311098254653383, -0.0007900480418863645] km/s
+ V∞_out: [0.0005143347225631617, 0.0009227698731211609, -0.0006607167717246641] km/s
+ time of flight: 1.7298583641545263e8 seconds
+ arrival date: 2028-10-19T10:20:29.520
+ thrust profile: [0.2530139429056433 -0.07843623435136193 -0.0872965776690852; 0.12938677555301845 0.03124568564102886 -0.11741065422004796; 0.11250400158362306 0.058335429480585455 -0.16678888093345967; 0.09726538444862744 0.06795533835333728 -0.19946302094736454; 0.06311740208945069 0.05612037280100721 -0.1623761347078902; 0.03617171968398687 0.03802521461562689 -0.1153103533254347; 0.020984009262653678 0.024196491531115232 -0.07883845877278214; 0.006906694072632861 0.008696448908440513 -0.028594103997718168; 0.006140779140778823 0.008434529751291737 -0.028222983275896067; 0.004455852407790357 0.006408180895346318 -0.02273510916358966; -0.0035478823664401226 0.0018961650810159474 -0.0005591494438181106; 0.00027980611515400895 0.0029954562004334325 -0.005452595986718443; 0.0009255974502875852 9.603099272785087e-5 -0.004613514176050883; 0.012326842172724234 2.2336836327014123e-5 -0.021418764769830415; -0.0008628949250841711 0.011049576050010283 -0.02273710976443924; -0.0014079357491528725 -0.012385115553214298 -0.01622147060962649; 0.00488121770172322 0.001933183451496231 -0.025141801323137095; -0.002416633403110902 -0.0026739831814332113 -0.00133542729769275; -0.0033953179448137872 -0.00189178358891839 -0.013103178458752068; 0.014819960979207299 -0.0052101054733783 -0.0038600495128320953] %
+
+Mass Used: 104.86525542872823 kg
+Launch C3: 96.21871977339765 km²/s²
+||V∞_in||: 0.0012463110537817247 km/s
diff --git a/archive/ES_0.5709814194490026 b/archive/ES_0.5709814194490026
new file mode 100644
index 0000000..b6f63e7
--- /dev/null
+++ b/archive/ES_0.5709814194490026
@@ -0,0 +1,22 @@
+archive/ES_0.5709814194490026---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T06:54:29.444
+Launch V∞: [6.164333165555618, -7.268628349786463, 0.26238594244351754] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.745446679660421e-8, -2.463568139816639e-8, 3.038034810753356e-8] km/s
+ V∞_out: [-9.571442254574689e-8, 8.830913746072594e-9, -1.1332213532642554e-8] km/s
+ time of flight: 1.8310956873423627e8 seconds
+ arrival date: 2029-02-10T14:40:37.444
+ thrust profile: [0.6435692420744809 -0.17415554963135657 -0.13818144525744627; 0.2732606313734508 0.09014405719924844 -0.17098362686609378; 0.09444669849093965 0.06556900036557554 -0.11705579414446218; 0.07253222026945393 0.06969273508950706 -0.12464873166469581; 0.050751412202285774 0.06115093566437913 -0.11671516821324938; 0.041333850364111115 0.05861926825822377 -0.11366919761310958; 0.02759228796850461 0.04568207952247186 -0.09154991322149028; 0.010968616260345425 0.01958389049680184 -0.04319800195037922; 0.006566285826006291 0.014357405753046008 -0.031957310902704254; 0.0022123815717596577 0.002706524673545648 -0.012006919025094463; -0.0001377243457730353 0.002023410376760556 -0.0020067759019226235; -0.00010537997647521564 0.0027683193866012805 -0.002169206868135139; -0.0001760737925163569 0.0017851104675163636 -0.008410926347722938; 0.002644301938523095 -0.0006051269716074181 -0.001332040030422214; 0.0005354778957565446 0.0015990026973380983 -0.0013847828672739516; 0.00012653674857236304 -0.003906722987747104 0.002485357487563458; 0.0021836898827707644 -0.0005919324163737552 0.006080946919405854; -0.001959925668792865 -0.0032391115274913564 -0.0007361333145004295; 0.005139586611257891 -0.0023911220840923467 -0.00020876899830551444; -0.0029641685357523727 0.00012059763670233437 0.003594222600032387] %
+
+Mass Used: 135.89027692170066 kg
+Launch C3: 90.90080784608041 km²/s²
+||V∞_in||: 9.58027458466887e-8 km/s
diff --git a/archive/ES_0.5709924887984703 b/archive/ES_0.5709924887984703
new file mode 100644
index 0000000..f4f685d
--- /dev/null
+++ b/archive/ES_0.5709924887984703
@@ -0,0 +1,22 @@
+archive/ES_0.5709924887984703---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T23:51:47.783
+Launch V∞: [7.411497593100596, -5.749982267937662, 0.04221710556198132] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006477661824594547, -0.005319491070539194, -0.00034244859373493386] km/s
+ V∞_out: [0.006074428349881278, 0.002817136343175049, -0.005047720494188248] km/s
+ time of flight: 1.8749577778587013e8 seconds
+ arrival date: 2030-04-17T02:01:24.783
+ thrust profile: [0.7667872121390866 0.030386668591684575 -0.13889829736399473; 0.34025938404927575 0.2628462091536122 -0.21846322784672215; 0.11156787790493473 0.1542552111828055 -0.1417865721649281; 0.04834301742357799 0.09280959259333997 -0.09419946669883329; 0.018768643011347425 0.048673390515201385 -0.056344171665592385; 0.011079773923470362 0.05243338567625831 -0.06151753043268632; 0.01003055929493188 0.049573331450190466 -0.06486556315315094; 0.0016987217876616178 0.021921545307338895 -0.030974120485174766; 0.001751834662728478 0.016939495545926546 -0.022894152977729152; 0.0002130366652412424 0.014830561850781528 -0.023507767905811088; 0.000882769873810908 0.0017556780542458818 -0.006979297581180614; -0.0012998110120947099 0.0004050906866489599 -0.004791584732352526; -0.007105811331646605 -0.0009298295413634793 -0.0019265362155516251; 0.0005430117765346416 -0.0007197768812637418 -0.006416102769930738; -0.0023589086925844445 0.0025412206246177853 0.002998581795825785; -0.003418863084401551 -0.015481050855411238 -0.002747803546776763; 0.0005861583950330996 -0.00011792341536880123 0.00016578006813023445; 0.006855152098011678 0.00982279323897194 -0.0033972289845089574; 0.00048589024756211474 0.0010174497135569036 -0.004456309387327211; 0.00024318034133819584 0.0076578637773780526 -0.0006087120854239127] %
+
+Mass Used: 152.85738312575813 kg
+Launch C3: 87.99437493813551 km²/s²
+||V∞_in||: 0.008388942662976474 km/s
diff --git a/archive/ES_0.5710112603129831 b/archive/ES_0.5710112603129831
new file mode 100644
index 0000000..00cdda0
--- /dev/null
+++ b/archive/ES_0.5710112603129831
@@ -0,0 +1,22 @@
+archive/ES_0.5710112603129831---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T12:07:12.158
+Launch V∞: [6.493706546212006, -7.616034563070193, 0.047105433921311474] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000481504709753254, -0.0005449318997265837, -0.0005048096097115507] km/s
+ V∞_out: [0.0005852149535014154, 0.00029052610370897217, -0.000600862120721192] km/s
+ time of flight: 1.873745000367293e8 seconds
+ arrival date: 2029-04-12T04:35:32.158
+ thrust profile: [0.11402366863740711 -0.033628885782065514 -0.04764536102985566; 0.03262772043569539 0.0053244758511092095 -0.04035439635989651; 0.041203184871194516 0.013734143112440764 -0.0871413175823205; 0.05100981402991549 0.02190337155567224 -0.15084075778248066; 0.02940606492551327 0.014474606150697181 -0.11006127443887517; 0.026111169169269886 0.013980569693337736 -0.11739075177709286; 0.014317830209844997 0.007934487113201555 -0.07447296814922513; 0.025872768801134347 0.015252933295616193 -0.1501468138889553; 0.00011424884671498507 2.9190163770911803e-5 -0.00750456758292404; 0.0027189473223533187 0.002105663560736981 -0.019970771482404833; 0.0010722848765833605 0.0011762058963071878 -0.008258297863466638; 0.0022042978432008685 0.0019677387589310275 -0.016574906953172364; 0.003635944647038253 0.0034232796867601544 -0.01458000304557784; 0.00033104039529613236 0.00037109043489810025 -0.002065347930242279; 0.0018703225758606602 -0.0006105273718303392 -0.005322073343842537; 0.0042490830451773105 -0.002635425919469898 -0.0007291491115481261; 0.0013465760482190294 0.009926906832017196 -0.004993121663667288; 0.034167157396204025 -0.006655706982050154 -0.02012963885651511; 0.042249615034795754 0.004684849487724027 -0.028160838647972763; -0.004215599037423814 -0.006704709000994531 -0.005167063414116142] %
+
+Mass Used: 81.8289848045556 kg
+Launch C3: 100.17442609610136 km²/s²
+||V∞_in||: 0.000885228955079598 km/s
diff --git a/archive/ES_0.5710234787255706 b/archive/ES_0.5710234787255706
new file mode 100644
index 0000000..1d6d1fc
--- /dev/null
+++ b/archive/ES_0.5710234787255706
@@ -0,0 +1,22 @@
+archive/ES_0.5710234787255706---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T01:55:06.244
+Launch V∞: [7.28386340583972, -6.721525787224747, -0.4598072109157768] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0006400772317452781, 0.010237814434136327, 0.001174976265475921] km/s
+ V∞_out: [0.00998652476297591, -0.0015848296756653146, 0.0020703127915509883] km/s
+ time of flight: 1.5244961714708245e8 seconds
+ arrival date: 2029-03-08T13:02:03.244
+ thrust profile: [0.24606159753088333 -0.06760067928128859 -0.10665818151297264; 0.07948375495655907 0.015426275467027947 -0.0967437113958255; 0.08682072940401309 0.03491951612124663 -0.17401157142435603; 0.07768313018166621 0.04121725810927889 -0.21478546369880824; 0.056735215218289836 0.03501738262370993 -0.19877699528455223; 0.03154118141578694 0.02135847013520586 -0.13360629785139466; 0.01626289173593387 0.01224688956367752 -0.08286662499445703; 0.029146396412578292 0.021504394825802856 -0.1443925737626237; 0.009392798541125721 0.007829145023651464 -0.059049501468197034; 0.0016915675096743482 0.0008240232292766616 -0.01234890615382592; 0.0008317754273935339 0.0009913443533350408 -0.0031850196566732677; -0.00025363535884212745 -0.0007111169276330031 0.001065036702783016; 0.00011152305532010394 0.0015869433368563726 -0.002405639964776436; 0.00010191301127795543 0.00017949861380270581 -0.0009898456932466747; -0.0024875666956604486 -0.001205819921389835 -0.0009257886136567874; 0.0014553063007110118 0.002304175495578241 -0.0034605655829268835; 0.0016349911578628468 0.002283253904436559 1.1571382752227199e-5; -0.003460042840948702 -0.0030277539717424393 0.003840717843002561; -5.2927766917826936e-5 0.0003500771831391746 -0.00011025862304172033; -0.0006963978229580074 0.000595226886100519 -0.0009460610617086683] %
+
+Mass Used: 91.93157196209995 kg
+Launch C3: 98.44499769446841 km²/s²
+||V∞_in||: 0.010324878327362534 km/s
diff --git a/archive/ES_0.5710552232370011 b/archive/ES_0.5710552232370011
new file mode 100644
index 0000000..361b106
--- /dev/null
+++ b/archive/ES_0.5710552232370011
@@ -0,0 +1,22 @@
+archive/ES_0.5710552232370011---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:49:24.215
+Launch V∞: [7.123332977231349, -6.6414100976410895, -0.1803578538436538] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000565552854777872, 0.001126242725613477, 0.00041067368191130495] km/s
+ V∞_out: [0.00047930819853828646, -0.0006733172184343042, 0.00103549490575643] km/s
+ time of flight: 1.533889710431947e8 seconds
+ arrival date: 2029-03-18T03:52:15.215
+ thrust profile: [0.529121252807096 -0.12227414399602976 -0.19136195532634206; 0.11567065876757875 0.0303484817730044 -0.1298130499619174; 0.0943875036203211 0.047324753693961163 -0.17673112157574847; 0.08215256276675212 0.055590636970266685 -0.20529863823757477; 0.06519846507829583 0.0513576756902187 -0.2123221340191513; 0.0349416866928074 0.031614367325181296 -0.14296699136037247; 0.017608964895131578 0.017563667100512485 -0.08556656129504202; 0.012072437848479655 0.012645584206044586 -0.06189480944928556; 0.008114437778197838 0.00958643563750883 -0.05282654635331071; 0.004513091149412876 0.005151264496981173 -0.02961446539506798; -0.00029779725023110746 -0.00026065232658867765 -0.0024278637884321335; -0.0033346636307000606 0.0011305595500676674 -0.004822808496064242; 0.00437365443094801 0.0006925326761062185 -0.004176516784342725; -0.0012044494121569431 -0.0027733610630947094 -0.001676198708189058; 0.0011870899471062664 0.002868024790266538 -0.0001372358631994441; -0.0004955058922846238 0.000343059685978548 0.0017235605148998656; -0.0032582867027528247 -0.0004399033760983866 0.0022193649656868414; -0.0004768122432448548 -0.0010578446937985655 0.0075091249210050524; -0.0019545337391639267 0.00047613210954762936 0.007475680050739142; 0.00045132906689826816 -0.0004215574787925394 -0.0007466812790379483] %
+
+Mass Used: 112.74850359731272 kg
+Launch C3: 94.88272974500374 km²/s²
+||V∞_in||: 0.0013254906946332222 km/s
diff --git a/archive/ES_0.5710628467226965 b/archive/ES_0.5710628467226965
new file mode 100644
index 0000000..4067158
--- /dev/null
+++ b/archive/ES_0.5710628467226965
@@ -0,0 +1,22 @@
+archive/ES_0.5710628467226965---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T00:43:59.354
+Launch V∞: [5.837502767342806, -7.881371545030049, -0.2155957093574607] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3309622220755001e-7, 7.712135647831076e-5, -5.4572484147973304e-5] km/s
+ V∞_out: [-4.721992050664322e-5, -8.037488194034793e-5, 1.5373885307169167e-5] km/s
+ time of flight: 1.630105233252941e8 seconds
+ arrival date: 2028-06-24T17:26:02.354
+ thrust profile: [0.30696054039339365 -0.1349443631164512 -0.12794093438841042; 0.12919894061664386 0.010003465030683192 -0.14050236970669766; 0.10386879067840055 0.03032826698325348 -0.1818549181059778; 0.06908425642918141 0.029375994860768008 -0.16475548261932157; 0.05764464101623955 0.03027968137393869 -0.17189516492075024; 0.05785953218247433 0.03450376423944403 -0.20389948013844084; 0.01684222953390356 0.01111529810868047 -0.06887466313144235; 0.017730730672925743 0.01229489566209986 -0.07820075418709287; 0.00437695153101165 0.0022572931060568253 -0.01022186966593544; -0.001992886199924951 3.724345523988676e-5 -0.016264482454389273; 0.0032435971298694416 -0.0008079221269086355 -0.008401929231614303; 0.0030802212632817924 0.00217722792336134 -0.008104811233413754; 0.0006749211789962221 0.004558442926991412 -0.007167070020422821; 0.0006618069548583004 0.00047496848180986033 -0.005605399167912445; -0.0003390238917444924 0.00015378069651038177 -0.004730317459528292; -0.006322850214350093 0.004164077638847297 -0.005386027369152577; 0.006097068881612021 -0.014159994812682992 -0.014211356801371866; 0.00015615181470167525 0.0017909441101378511 0.0032976747085043424; 0.001293374065226087 0.0117592695530771 -0.00512601539424877; 0.009116134072980089 -0.00036785839677880056 -0.0029221931783691216] %
+
+Mass Used: 104.84618576309322 kg
+Launch C3: 96.2389374994376 km²/s²
+||V∞_in||: 9.447705533612004e-5 km/s
diff --git a/archive/ES_0.5710723277287377 b/archive/ES_0.5710723277287377
new file mode 100644
index 0000000..6d18c7d
--- /dev/null
+++ b/archive/ES_0.5710723277287377
@@ -0,0 +1,22 @@
+archive/ES_0.5710723277287377---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T12:55:45.947
+Launch V∞: [5.881488496826273, -7.9582917314580675, -0.5754746401738096] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8408182789905005e-6, 0.0006646768914330236, -0.000297065522421872] km/s
+ V∞_out: [-0.000592385022159327, -0.0003298668536745306, 0.0002658359086153373] km/s
+ time of flight: 1.6834808927593067e8 seconds
+ arrival date: 2028-08-29T00:17:14.947
+ thrust profile: [0.18703098200775503 -0.07641020610983973 -0.08131837594164594; 0.1161759104254547 0.010814866445457724 -0.13421942904272904; 0.06449725745595271 0.019584751959715138 -0.1230104269415918; 0.0577139433810026 0.024941449544137736 -0.1497613278201088; 0.05195605416555871 0.027721975523225816 -0.16992327810213823; 0.040212126131957834 0.024414414654163573 -0.1579291449154859; 0.02443922559158576 0.01650761613330549 -0.11162128530419638; 0.017396355808617533 0.011864075312053265 -0.08706846221895678; 0.007668033937714499 0.0038763573972115163 -0.025643210883700678; 0.000148577171818276 -0.000862842656628758 -0.003699973484268693; 0.001246878062340888 -0.00028834796318900273 -0.003054098642202485; 0.002567522496853896 0.003372639859042795 -0.011001510112280925; -0.0007640583409021184 0.0010077730926932342 -0.0009895225941841039; 0.004748766033776077 -0.0018377737264577121 -0.00671389693370012; 0.006067495617509634 0.008206729811018106 -0.007387662749478525; 0.0018184519658080067 -0.007656244215661344 -0.023548801162748184; -0.0009938420906923256 0.00204696829088943 -0.007135375904560652; 0.013622871784566124 -0.005052170645504583 -0.016519308849244786; 0.0005830413951351152 0.0015539744733977223 -0.009988510057877167; 0.0060771158383950245 0.004496215273932199 0.000380372444540974] %
+
+Mass Used: 93.08238486732944 kg
+Launch C3: 98.25748528277678 km²/s²
+||V∞_in||: 0.0007280430503952246 km/s
diff --git a/archive/ES_0.571076688355779 b/archive/ES_0.571076688355779
new file mode 100644
index 0000000..cf2860b
--- /dev/null
+++ b/archive/ES_0.571076688355779
@@ -0,0 +1,22 @@
+archive/ES_0.571076688355779---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T20:37:36.368
+Launch V∞: [5.673559503804839, -8.038915944612057, -0.2651614429374779] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.893217103557307e-5, -0.00012683314163272155, 2.171608064209921e-6] km/s
+ V∞_out: [3.271560368402114e-5, -7.690206710675827e-7, -0.00016490280794931558] km/s
+ time of flight: 1.5752961259759948e8 seconds
+ arrival date: 2028-04-22T02:51:08.368
+ thrust profile: [0.2715886080167703 -0.13111684316262331 -0.11575025232213727; 0.1393400413394519 0.004285441769110802 -0.14889351345888624; 0.08257244033433375 0.021031075137552705 -0.14297131466788648; 0.0959704449767654 0.03622279094567604 -0.22109254702888814; 0.05627506896637013 0.02705522544989773 -0.1628046593983357; 0.0796301313105025 0.042677979682752144 -0.2666764675213297; 0.019153615039933618 0.011982514197969025 -0.07785800602185917; 0.012466665205324235 0.008641488668840493 -0.05668904858066114; 0.003663684456139857 0.0023051285475642943 -0.017774680712167354; 0.0024644743291406773 0.0015942869855420246 -0.01192267630909027; 0.005638351736105067 0.0037120076912269357 -0.027605888813959572; -0.00023765659991176294 -0.00029887030600957723 -0.002549403924019489; 0.0001495754758945453 0.00017104472742313613 -0.0015840929033657408; -6.4481043638522125e-6 -0.00040499139974891425 -0.00029906924287873926; 0.00026654358723618194 -6.651285980014684e-5 -0.0014680748344123632; -0.00040567122592859904 -0.0014374897020798677 0.00022822716296675132; 0.0009835619138291154 -0.0001506435806196388 -0.0005085964563491508; -0.0024989897564533297 -0.003145165980956699 0.00020062155044801757; -0.0008102529019610092 -0.002138990065887482 0.00028581341324519793; 0.0014289023264205038 0.0018858392005319958 -0.004161843450709612] %
+
+Mass Used: 101.10088375673377 kg
+Launch C3: 96.88375759857286 km²/s²
+||V∞_in||: 0.000160869313928488 km/s
diff --git a/archive/ES_0.5710779769426625 b/archive/ES_0.5710779769426625
new file mode 100644
index 0000000..7fd585c
--- /dev/null
+++ b/archive/ES_0.5710779769426625
@@ -0,0 +1,22 @@
+archive/ES_0.5710779769426625---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T14:56:25.152
+Launch V∞: [6.4140428864670636, -7.198359250824884, 0.2284158937595576] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.616668470875735e-10, -1.794287819489729e-9, 5.392893190621778e-10] km/s
+ V∞_out: [6.753285195163776e-10, -1.5288029051996995e-9, -2.0775648096300188e-9] km/s
+ time of flight: 1.874957778745677e8 seconds
+ arrival date: 2029-04-06T17:06:02.152
+ thrust profile: [0.612955018779611 -0.14867248106295097 -0.18797998157722795; 0.09066434198308423 0.027091360239355086 -0.08622693318866285; 0.05726869218607019 0.03303414510218907 -0.09190700438137944; 0.050505154298637014 0.03924053419980826 -0.1142597686399813; 0.045919516605704876 0.04349388946380785 -0.13449151699435247; 0.03088334741105059 0.03404647586496185 -0.1106171276902637; 0.023956462116051257 0.02919936070919649 -0.10070249581398567; 0.003257942943306437 0.004670739053533814 -0.0188058131015469; 0.001922249834585444 0.0011965801697009608 -0.017045242599893987; 0.007300701983888757 0.014057815297008312 -0.04340568121495623; 0.0005434368344154363 4.827004446446596e-5 -0.0192652380852465; -0.0019035772908054648 -0.001907234891147414 -0.01122337358431154; 0.009684023503332256 0.005737957232827093 -0.004256653633654447; -0.015358399550828657 0.006582853861016513 0.0034915801415962375; -0.009123438615058465 -0.005740567447733077 -0.0007009915691568998; 0.00026949788214394844 -0.009706037660293569 -0.005532152257624703; 0.0006311638669348759 0.013033533260296428 -0.03202687047407793; 0.001963434284468075 -0.005488527741349062 0.009674074604985181; -0.0022288981119243747 -0.002971324998967704 0.013778077130449134; -0.014030897921223414 0.016901728851724775 0.013136654470148753] %
+
+Mass Used: 123.70808050204096 kg
+Launch C3: 93.0084958738969 km²/s²
+||V∞_in||: 2.022483160566752e-9 km/s
diff --git a/archive/ES_0.5710899872215148 b/archive/ES_0.5710899872215148
new file mode 100644
index 0000000..cc93e29
--- /dev/null
+++ b/archive/ES_0.5710899872215148
@@ -0,0 +1,22 @@
+archive/ES_0.5710899872215148---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T15:23:22.813
+Launch V∞: [5.644512623928371, -8.023424360320277, -0.07526015609399973] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.263240006093247e-6, 5.141488864321861e-6, -3.9338007557662936e-6] km/s
+ V∞_out: [5.3093063978644026e-6, -7.5673550826197885e-6, 4.9764710432315795e-6] km/s
+ time of flight: 1.572890265292409e8 seconds
+ arrival date: 2028-04-19T02:47:08.813
+ thrust profile: [0.31972324696965665 -0.14452644961022032 -0.12689319255751952; 0.14586080536934493 0.002712323201338301 -0.16231416888902542; 0.1113704748498021 0.025479485729107864 -0.19959596580145939; 0.09357139161912933 0.03287258732191663 -0.2255236070566962; 0.0729484577733703 0.032337375961546316 -0.21863688308755236; 0.04226057631268884 0.02143756021361127 -0.15127933784262512; 0.023662672700248494 0.01317789200689775 -0.09745805346557543; 0.010104914862655023 0.005870391656066413 -0.04592279229765144; 0.004808382563344775 0.0028609005040635006 -0.023917300587804613; 0.002684825886769584 0.0017016467786224814 -0.014344194047817348; 0.0005881935562095709 0.00028404496979152286 -0.003284453323733271; -0.0006328990705106478 -0.00039204920468511976 -0.003334549581235984; 0.0003652726993729953 0.001456923072482982 -0.0036948631241379825; 0.0006042369172153494 0.0005242002449289665 -0.0011066327024352469; -9.764997768762617e-5 -0.000206393251724263 -0.0009440212757270395; -0.0001528730223921441 -0.0014726529348698452 -0.0001192634588309011; -0.00024453671386313777 0.0009587208316156615 -0.0015060958068435948; 0.00013515275550950688 -9.352068865088213e-5 -0.0002655532057989681; -0.00038878379860257553 -0.00382533423325366 0.0025553591774475064; 0.003963669216460563 -0.0010444706893934779 0.004682345327161794] %
+
+Mass Used: 104.86275406681716 kg
+Launch C3: 96.24152531856288 km²/s²
+||V∞_in||: 1.0497182075505458e-5 km/s
diff --git a/archive/ES_0.5711329794002833 b/archive/ES_0.5711329794002833
new file mode 100644
index 0000000..f78bc56
--- /dev/null
+++ b/archive/ES_0.5711329794002833
@@ -0,0 +1,22 @@
+archive/ES_0.5711329794002833---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T03:12:00.538
+Launch V∞: [6.548526789649284, -7.369564405080929, 0.14620097298726023] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006374736060710092, -0.004110756705036626, 0.005833796025493886] km/s
+ V∞_out: [-0.004907191717993164, -0.004161766505171737, -0.003152443155153598] km/s
+ time of flight: 1.8749577787494358e8 seconds
+ arrival date: 2029-04-09T05:21:37.538
+ thrust profile: [0.2501910057563335 -0.05907827395150579 -0.08515639327456676; 0.09547213944209967 0.027498265423450966 -0.10000772510025431; 0.060664401122785476 0.03231874737049847 -0.10545889051371488; 0.03959878001601402 0.02959118157511386 -0.09919003453939873; 0.033280479324929 0.02856413227357681 -0.10671620842295627; 0.02591501695781471 0.02579958284504769 -0.09773797254905846; 0.022129976144911617 0.02560544466323381 -0.1007200254396902; 0.021325269683735215 0.02392359045238127 -0.10746503635231688; 0.010445706481026265 0.013814340151435811 -0.06380086417763928; 0.0029917539916368635 0.0063932839057891395 -0.018381668142027283; -0.005550505731521128 0.004654621032289078 -0.011342816789323099; -6.677023782818663e-5 0.0006422475476939957 -0.0007276431324503229; 0.0006900465003729486 0.0006150295540882965 -0.0013961920854159452; -0.0018524734229368855 0.0007517958520624333 -0.005104565865216875; 0.0017227446791669228 0.006445802619793232 -0.0048227699755746655; 0.0042513422861275105 0.007223876651752455 0.0075595058262033395; 0.0029543813366187943 -0.005210651273168699 0.0239299824947314; -0.0003921840663663405 -0.0012014350065525426 0.0015396504806872047; 0.021448358438796358 0.037964513285474046 0.01563645309248861; 0.016236172761529045 -0.03725169938831621 -0.012970276776525362] %
+
+Mass Used: 99.23397470095688 kg
+Launch C3: 97.21505735989261 km²/s²
+||V∞_in||: 0.007165044965211943 km/s
diff --git a/archive/ES_0.5711414680756352 b/archive/ES_0.5711414680756352
new file mode 100644
index 0000000..c8d7b66
--- /dev/null
+++ b/archive/ES_0.5711414680756352
@@ -0,0 +1,22 @@
+archive/ES_0.5711414680756352---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T03:08:15.511
+Launch V∞: [7.844941533415223, -6.081456364759762, -0.13406206404555215] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.2474275575058275e-10, -1.069954429083178e-9, -1.4822638612651976e-9] km/s
+ V∞_out: [8.680858609868333e-10, -6.972833335507314e-10, 3.397248604529219e-10] km/s
+ time of flight: 1.7788530459452853e8 seconds
+ arrival date: 2030-01-01T23:43:19.511
+ thrust profile: [0.18939387506394442 -0.019653694691167935 -0.059822694370153105; 0.05054794465578735 0.023314915250518133 -0.05901829176418734; 0.03539092271532029 0.0257422083994999 -0.0693464047275441; 0.04314083029038519 0.04128416836426589 -0.1291052225994077; 0.02476723617663003 0.027302670197548805 -0.09441520513652465; 0.022584577266392226 0.02807082389572821 -0.10086460304534663; 0.016318552784511598 0.024886611084450255 -0.09923509881233486; 0.018161157675293103 0.028509929022219025 -0.103820977175321; 0.0066427206571130475 0.011075909513860664 -0.04752892725398988; 0.004038457236883703 0.0020231614318898103 -0.019114426367189734; 0.003520660282795336 0.0009488504504770404 -0.009985158712423163; 0.0007977021962940313 0.006378570237193345 0.003752929289191879; 0.014385327939682153 0.015225425759742017 -0.014008772495335857; 0.0012939097279827776 0.003248384916309733 -0.015758825735775094; 0.008327818257658246 -0.008452401407814197 -0.07440316351665513; 0.00013830430190862365 -0.01554924734864653 -0.046900975010069186; -0.014503671471511733 0.004987771331998903 -0.006029959438082214; 0.01040599751326854 -0.015723667032153447 -0.01260041875831998; -0.026549295510444 -0.030224633524779658 -0.04074993168270451; -0.01230936181264754 0.009934751208829373 -0.0013444792607585163] %
+
+Mass Used: 91.48476049376222 kg
+Launch C3: 98.54519181619636 km²/s²
+||V∞_in||: 1.876783163631356e-9 km/s
diff --git a/archive/ES_0.5711449382477101 b/archive/ES_0.5711449382477101
new file mode 100644
index 0000000..2adf91e
--- /dev/null
+++ b/archive/ES_0.5711449382477101
@@ -0,0 +1,22 @@
+archive/ES_0.5711449382477101---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T07:09:00.174
+Launch V∞: [6.245878254355896, -7.578661381749757, 0.15468626347840647] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9411746806336346e-6, 1.3233359207570551e-6, -9.73181989473164e-7] km/s
+ V∞_out: [9.140929938096759e-7, -2.118352020367623e-6, 1.0714006277003966e-6] km/s
+ time of flight: 1.7882039303880608e8 seconds
+ arrival date: 2028-12-27T23:28:53.174
+ thrust profile: [0.2975361715867048 -0.09064519556901642 -0.10494098659630512; 0.099833042386267 0.021111263926716254 -0.1045185248154938; 0.05814610227739718 0.027154734011730245 -0.1005707978041293; 0.053103713026477956 0.03199716542349551 -0.12397286264138058; 0.051316291569465204 0.03833772144543547 -0.15312112889067075; 0.03615694374480949 0.031212756721163904 -0.13177678935681283; 0.028764698853666348 0.025501284249249905 -0.11485802267873602; 0.015633194334735135 0.020051929871182806 -0.08314331176529324; 0.005819119323790275 0.008320635223384009 -0.03354408390161755; -0.0012125330451143584 -0.0015721969014873619 -0.008109773755451138; 0.0025687289623043813 0.0028580974984649104 -0.007526237001218315; 0.0033099014285281093 0.001096690333701977 -0.01548723234753126; -0.004852128767636948 -0.0013999905136572253 -0.008976089870802301; -0.0012690427470765423 -0.003358002550243698 -0.005684005232313213; -0.0017349033759256815 -0.0007721609537962399 -0.0014342632229202845; -0.0003476107724071628 0.0008912693084263692 0.007655479821929281; 0.004592333395146217 0.006140962815607429 -0.0002921294996704269; 0.01074117549515094 0.007892803870371109 0.01075960789681275; 0.023055219816958458 -0.01648231447136636 -0.04070051007395662; -0.0005042972760181923 0.0012507444524310532 0.039076599586087356] %
+
+Mass Used: 103.58807842817077 kg
+Launch C3: 96.47103134756989 km²/s²
+||V∞_in||: 2.5429235703288372e-6 km/s
diff --git a/archive/ES_0.571168787222789 b/archive/ES_0.571168787222789
new file mode 100644
index 0000000..3d73cd6
--- /dev/null
+++ b/archive/ES_0.571168787222789
@@ -0,0 +1,22 @@
+archive/ES_0.571168787222789---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T18:57:08.810
+Launch V∞: [7.276815542889449, -6.672942119830421, -0.37951472250127194] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0007195553042440841, -0.005184019014676469, 0.002744310969008276] km/s
+ V∞_out: [0.0023065295969549138, 0.004550879070992985, -0.0029801097139681557] km/s
+ time of flight: 1.528278807894798e8 seconds
+ arrival date: 2029-03-12T15:08:28.810
+ thrust profile: [0.30964162811221296 -0.08649979050597073 -0.1348167284092878; 0.09430044699148817 0.017616166203806297 -0.11770332170421852; 0.1010062164196487 0.03946363093343925 -0.20708146736033287; 0.06444490846903865 0.03289397147720778 -0.18598133106632284; 0.045752082043699266 0.026932785805580926 -0.1678303550191648; 0.0353936222071433 0.0226286107016678 -0.1552724323315005; 0.027008631299424053 0.018752763081823654 -0.13618387743327798; 0.014673004802876408 0.010650092770124926 -0.08401672248640206; 0.0015759515160052703 0.001387119136725601 -0.017997598235813646; 0.0013291498233445778 0.0033769456532697834 -0.015958492347673176; 0.005318290792440847 0.0036553425798058797 -0.03098559622726704; -0.00030878291393317357 0.0013050220532991245 -0.0017487341991892112; 0.00010238076347777222 -0.0006672331160025871 -0.0010604027607496102; 0.0015104242251165758 -0.0030853645311215688 -0.002108705087265549; -3.448781655302619e-5 -0.0015211250066588754 0.0006733232208249377; 0.00012551057363953015 -0.00267191826846255 0.000557810212529767; -0.00029851304666056184 -0.000782368373580318 0.0024058189154567834; 0.000300416307946985 0.00044905031892164267 -0.0015576312935169404; -0.0015021333592311543 0.0015314971897860512 0.00220003237096959; -0.001360207490357064 0.002897404026739626 0.009613047404956176] %
+
+Mass Used: 96.8888960673562 kg
+Launch C3: 97.6242324044396 km²/s²
+||V∞_in||: 0.005909573222747318 km/s
diff --git a/archive/ES_0.5711764652483291 b/archive/ES_0.5711764652483291
new file mode 100644
index 0000000..70bb758
--- /dev/null
+++ b/archive/ES_0.5711764652483291
@@ -0,0 +1,22 @@
+archive/ES_0.5711764652483291---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T19:00:01.838
+Launch V∞: [6.1867422850259075, -7.3685897642457565, 0.23038805070708404] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.984663401887806e-7, 0.0002495854653067472, -0.00017636217258107774] km/s
+ V∞_out: [-0.0001538722205381252, -0.00025797384493851997, 5.552971580071388e-5] km/s
+ time of flight: 1.7878374728935295e8 seconds
+ arrival date: 2028-12-22T01:09:08.838
+ thrust profile: [0.4989842125724028 -0.1353209936375569 -0.13512441690779223; 0.3033568746370596 0.09385799485308415 -0.2349929538126135; 0.12871952029929468 0.07698699914567286 -0.16894328171396497; 0.051967780539324 0.04186248302632376 -0.09722447702618646; 0.05141375884576831 0.05088515968383782 -0.11945323615123672; 0.038044679140492005 0.045490322375013846 -0.10842078486765562; 0.025375195873369144 0.03374468568830989 -0.08417074382474281; 0.004645684570212378 0.007001958519831587 -0.020047887011752568; 0.006781747138151814 0.011171435266458175 -0.03207335371645553; 0.0013788796044572422 0.0015255937880662629 -0.008897416842256898; 0.0036417617169144387 0.006544190858500338 -0.021078970921027083; -0.0002473004728864687 0.002296787634353358 -0.004532973427661331; 0.002928869254018754 0.0014076469422225084 -0.0017450891749877287; 0.0010221320295223293 0.0036442853911623847 0.0017743398965037603; 0.0017427660048744723 0.0018364176702196896 -0.0036056906405644395; 0.0023890728020381194 0.0034842634278371074 -0.0015474660392648424; -0.000545918713642673 0.0035763576093938527 -0.005105230823711161; 0.003357551407603461 0.008130646855357445 -0.009192188074175437; -0.00296776751409821 0.00621912222719322 0.0020540011502700444; 0.000172065858119854 0.0025740866884049127 -0.003321794483441766] %
+
+Mass Used: 126.06019522064662 kg
+Launch C3: 92.62497386898355 km²/s²
+||V∞_in||: 0.0003056094860412546 km/s
diff --git a/archive/ES_0.5711969087790897 b/archive/ES_0.5711969087790897
new file mode 100644
index 0000000..bf9f5cf
--- /dev/null
+++ b/archive/ES_0.5711969087790897
@@ -0,0 +1,22 @@
+archive/ES_0.5711969087790897---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T02:50:57.123
+Launch V∞: [8.077389005244237, -5.237614840238461, -0.34422151853611105] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.16885560874138053, -0.8450914153424232, -1.5068794960958038] km/s
+ V∞_out: [0.7654980549278215, 0.33716096139723356, 1.5209952247778376] km/s
+ time of flight: 1.874957778749377e8 seconds
+ arrival date: 2030-04-16T05:00:34.123
+ thrust profile: [0.7231453530922856 -0.04826371969892532 -0.1652345281603104; 0.1593937013910467 0.10162938567756134 -0.15196658094360266; 0.0638438209979277 0.06907269622479788 -0.1197498114447451; 0.04169592746685674 0.06206591852953929 -0.12072746738285006; 0.027791839160225602 0.0533122283958476 -0.11407318650757216; 0.017668821936945172 0.04234212669721192 -0.0984432471822871; 0.007550849672792451 0.022026910705566793 -0.05716181945222438; 0.0026248131476298915 0.00999060488664337 -0.026030706490612544; 0.002679999380418042 0.01118313222740697 -0.032135973709549355; 0.00013495899423453123 0.00092950068963319 -0.0021723207504326623; -0.00014306911018078313 0.0004583997652666536 -0.0009689109302652042; 0.00023031110756679122 0.0011116470828959487 -0.002632858905254139; -0.0011759506801024095 0.0018490324513153887 -0.001443935039194255; -0.0010291197823506775 8.979968965328218e-5 -0.0012809068214006615; 0.0005435989378843517 0.0008238569136590074 -0.0007865260017827778; -0.00011652089761365607 -0.0003351056315319405 -0.0014726261663720271; 0.0013117004679265834 -0.0033817043508834977 -0.005964967702902554; 0.0029809594022388508 -0.004131147110474137 -0.003821940928791995; 0.0034731793857025756 0.001997044275540135 -0.0043325059998353755; 0.00017945000772457383 -0.0012580582834755523 0.0001736929121500608] %
+
+Mass Used: 125.09041384739658 kg
+Launch C3: 92.79531081054995 km²/s²
+||V∞_in||: 1.7359082731074318 km/s
diff --git a/archive/ES_0.5712063887468053 b/archive/ES_0.5712063887468053
new file mode 100644
index 0000000..346e3c9
--- /dev/null
+++ b/archive/ES_0.5712063887468053
@@ -0,0 +1,22 @@
+archive/ES_0.5712063887468053---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T00:39:25.699
+Launch V∞: [6.098582573273634, -7.304338214871621, 0.2568344270124542] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.404658893837517e-9, -2.28606396692598e-9, 5.071709545614603e-9] km/s
+ V∞_out: [1.644543083889585e-9, -3.4950047312735676e-9, -6.68648393033655e-9] km/s
+ time of flight: 1.7905708364314988e8 seconds
+ arrival date: 2028-12-24T10:44:08.699
+ thrust profile: [0.7159474997387778 -0.19244658597957906 -0.17241041879033892; 0.26117821036021155 0.0840003959657061 -0.19437008838535785; 0.10823585884303699 0.06763582608246552 -0.13847150291785237; 0.0765839788689288 0.06605790397728356 -0.13701766754782663; 0.05012807901291119 0.0534924531973827 -0.115901197944548; 0.021823217184418556 0.02725695707495307 -0.06275623520537958; 0.03024296707785042 0.04404131962258185 -0.10256037534187853; 0.020775311940069954 0.03291310920434172 -0.08045455068524733; 0.004103460673443651 0.007917575967080292 -0.019432560463851063; 0.0018075692745761875 0.004815963436798598 -0.012270396931423051; 0.00018928040504049008 0.0006324595113732989 -0.0013141181779062275; -0.0001404123043191573 0.000244540515823031 -0.0023402620701760608; 0.0009304469079499496 -0.0007812242565921549 -0.0021909837994123996; 0.00014365738705246592 0.002221322871760762 -0.001751857589134633; -0.0013399976120750468 -0.0018006393171680402 -0.0012327706198267795; -0.0020657974275613508 -0.0009139695064376567 -0.0009207181525984331; -0.004886054853849581 0.0005330425068088859 5.5678837693507556e-5; -0.001263262907381709 0.0008480208419258998 -0.001407922783846669; -0.0018724783311692562 0.001988923433380298 0.003501576197237939; -0.0003090926557934707 0.0007181510196437804 -0.00288113967835407] %
+
+Mass Used: 137.8372780527834 kg
+Launch C3: 90.61203008316963 km²/s²
+||V∞_in||: 6.5222717176872145e-9 km/s
diff --git a/archive/ES_0.5712415184491458 b/archive/ES_0.5712415184491458
new file mode 100644
index 0000000..f0e6bc1
--- /dev/null
+++ b/archive/ES_0.5712415184491458
@@ -0,0 +1,22 @@
+archive/ES_0.5712415184491458---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T00:41:41.736
+Launch V∞: [7.211511165790797, -6.496655946384052, -0.3772343933829754] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0094547095186274e-8, 1.444609384219096e-8, -1.7002045023246584e-8] km/s
+ V∞_out: [1.1830011216867539e-8, 2.4930785913295595e-8, 8.35812159614436e-10] km/s
+ time of flight: 1.55938175276894e8 seconds
+ arrival date: 2029-04-15T20:51:16.736
+ thrust profile: [0.5710059236716275 -0.123038638831717 -0.19643951173577634; 0.13282228449585148 0.04094510361721495 -0.13670901646400235; 0.0712726666567218 0.041088699381261466 -0.12343890975955021; 0.04965598354928917 0.038022643295783164 -0.12049254566344256; 0.038923537502608574 0.035570569274574394 -0.12028901237939837; 0.03673908289277928 0.040114917749983256 -0.14767773245147334; 0.026145860133705495 0.03154730724524893 -0.1220960948886777; 0.04431627706547707 0.053315113928287326 -0.20015208247416508; 0.00882246225355315 0.012613914361032251 -0.050454934615906916; 0.002054677805394111 0.0027867451532323445 -0.01513716994781934; 0.0029647614816667037 0.0017527859226468875 -0.0045206028394325064; 0.000904063187775045 0.004657740733260926 -0.015293143824650194; 0.006846642710067052 0.0063566479758145585 -0.010238762531133098; 0.00019336495789934222 0.000790860064706318 -0.00022283898428915896; 0.0013829102621650143 -0.002064236524868595 -0.0027760618409835274; 0.005761655122185792 0.0039041029499994094 -0.007287715489985057; -0.000877585963627265 0.005574612837285232 -0.007218037883090892; -0.00017294911691381976 -0.0012621315591436117 0.001489703078965832; 0.005309320034283307 0.0013636771014536864 -0.010332898926003465; -0.0004291719821085493 0.0011170252691521864 -0.002711166121464364] %
+
+Mass Used: 116.04580237988239 kg
+Launch C3: 94.35473756756362 km²/s²
+||V∞_in||: 3.002582197426993e-8 km/s
diff --git a/archive/ES_0.5712441125198925 b/archive/ES_0.5712441125198925
new file mode 100644
index 0000000..0ffb8e4
--- /dev/null
+++ b/archive/ES_0.5712441125198925
@@ -0,0 +1,22 @@
+archive/ES_0.5712441125198925---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-06T19:56:12.987
+Launch V∞: [6.371474606943042, -7.812091237981627, -0.5657592475641161] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.008352637183661e-7, -2.0703317252224082e-7, -9.133802883980788e-8] km/s
+ V∞_out: [1.130832580901706e-7, -1.851288786523106e-7, 1.0268542556279357e-7] km/s
+ time of flight: 1.848634481273522e8 seconds
+ arrival date: 2029-03-15T10:53:40.987
+ thrust profile: [0.05983891099229063 -0.02034353147836445 -0.0295768944827196; 0.023576484654874764 0.0019459567584319544 -0.03493453788820435; 0.03615961276358994 0.007697976135933074 -0.09049864106682413; 0.04387522148178861 0.011728495471136123 -0.15432605819840364; 0.03816636409446677 0.011139617270058464 -0.16992302314680757; 0.022805537862133234 0.006781884078820993 -0.12080955541688991; 0.012915316274541332 0.004168769293188362 -0.07837155578276378; 0.007682022404162045 0.0023197607609219107 -0.05315504813156694; 0.008128976487507895 0.0013197735225288988 -0.048483316210160304; 0.006268893350167736 -0.002125085943509654 -0.03116286418702038; 0.002752811301828557 0.000572368437205058 -0.023515952567485232; 0.0009668618705168362 7.214627369045258e-5 -0.010114821803688187; -0.0005836721556004397 -0.0015693292658301068 -0.006849209509612297; 0.00034447886143247576 -0.00017006045690725344 0.000888151050712462; 0.00026232052094280877 0.0023291021638661563 -0.0028276149395746806; -0.006168734807680943 0.0039228430768106165 0.004232476253171835; 0.0022334446435819644 -0.0034543340321119814 -0.008033905328624077; -0.00045103533267517356 0.00040677165323300425 -0.006548705043596591; 0.00255639126949808 0.0009000525693159487 -0.0013232444198965929; 0.009174946644909105 0.017240605570351654 -0.003732727841643561] %
+
+Mass Used: 71.77497133511179 kg
+Launch C3: 101.94454170367362 km²/s²
+||V∞_in||: 2.4773598940428086e-7 km/s
diff --git a/archive/ES_0.5712560404467 b/archive/ES_0.5712560404467
new file mode 100644
index 0000000..4454288
--- /dev/null
+++ b/archive/ES_0.5712560404467
@@ -0,0 +1,22 @@
+archive/ES_0.5712560404467---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T04:03:19.145
+Launch V∞: [7.308243698100029, -6.5903057193359365, -0.35398816453262627] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000214251664386404, -0.00035835474939675355, -3.085302652168031e-5] km/s
+ V∞_out: [2.1688303708633332e-5, -0.00010502498642247162, -0.00040469235739400535] km/s
+ time of flight: 1.5637820222841692e8 seconds
+ arrival date: 2029-04-23T02:26:41.145
+ thrust profile: [0.36703102965648265 -0.0892045798423403 -0.14774649001083423; 0.05328885367759151 0.013315019554936088 -0.061249101014637035; 0.07811176094606598 0.037132933571049756 -0.15116590528590404; 0.06639226684395394 0.041294937695755124 -0.1788002607028937; 0.052614606990437934 0.03846106670419607 -0.1800198722505465; 0.04296490370164977 0.03506367120785632 -0.17659726622233562; 0.022490879789511867 0.020067676151649293 -0.10738329535945572; 0.004157824785797926 0.004515406766903578 -0.02151992117438762; 0.02320637169676131 0.022341884193609367 -0.13384223575716644; 0.00851461667783938 -0.0036976783487200357 -0.013011865674511727; -0.002208958833618754 -0.0023744983252429273 -0.012685809770440329; 0.0004218881400109015 0.0024254431754114217 -0.015027004362221374; 0.005578763700566302 0.0007199218237815485 -0.005899078253764263; 0.008401200249110143 -0.0019044451286550895 -0.005969258053571102; 0.0008696903291629532 0.002790711248719757 -0.0013528787234818951; 0.009822915225867968 0.004904265489884098 -0.002103902681639633; -0.001497649158606508 -0.008166253250198003 -0.0002025792067530544; 0.0004618177457698042 0.0010302151288590043 -0.0001927969022126547; -0.010922589494253026 -0.009747652860318128 0.015405497446680873; -0.0003945658802283192 -0.0008112551070359586 0.005712583010239295] %
+
+Mass Used: 100.81951275421716 kg
+Launch C3: 96.96786304575991 km²/s²
+||V∞_in||: 0.00041865715251635416 km/s
diff --git a/archive/ES_0.571314711482567 b/archive/ES_0.571314711482567
new file mode 100644
index 0000000..7c1fd7d
--- /dev/null
+++ b/archive/ES_0.571314711482567
@@ -0,0 +1,22 @@
+archive/ES_0.571314711482567---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T20:36:25.257
+Launch V∞: [5.67578296614906, -7.966323181859477, -0.1928084237581] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.798814045496967e-5, -0.00011071076706511546, 1.9591205343241745e-6] km/s
+ V∞_out: [2.546919984525381e-5, -6.329110593144426e-7, -0.00013911222601517778] km/s
+ time of flight: 1.5777451437374592e8 seconds
+ arrival date: 2028-04-23T22:51:39.257
+ thrust profile: [0.3634462441373331 -0.1691497560280191 -0.14510660710721418; 0.14113302246815887 0.009869515445679924 -0.14811141767481453; 0.10806894062474659 0.03234705536152154 -0.180531258211841; 0.0765537980396274 0.034936563995639096 -0.1756401337568256; 0.07058891108297301 0.03635222487796267 -0.18712202892893254; 0.0381366953521245 0.023504143359508303 -0.12419132517712106; 0.01715610405329166 0.012414906263925036 -0.06655064472119392; 0.036176619045787034 0.02643889744500833 -0.1429683210133605; 0.013729550202418369 0.011554311272442469 -0.06806370381081996; 0.0072631590619071235 0.006038287490780303 -0.037147093609208634; 0.0027293490920076648 0.00208006657862128 -0.014595655402940739; 9.617009529781735e-6 -6.37747245315569e-5 -0.00023646272591322328; 0.0002791529089983878 -0.0001451904349603823 0.0009237429252843916; -7.198151849655778e-5 -2.7319288894952408e-5 0.00021958732147873427; 3.948866457285833e-6 0.0002913597661807266 0.0004495963088513605; 0.0002631011048937061 -0.0005813975643245572 0.0006485923429416416; 0.00015935213418770302 0.0003332823925242384 -3.006534324840899e-5; 0.0008214045432873832 4.4810131461410794e-5 0.00041937952777848357; -9.989324306365085e-5 0.0003843381188438445 0.0002326568225164956; -2.297639528149198e-5 0.00015208412943511842 -9.355139839670149e-5] %
+
+Mass Used: 108.20220770089372 kg
+Launch C3: 95.7139924049316 km²/s²
+||V∞_in||: 0.00014143063656131135 km/s
diff --git a/archive/ES_0.5713624944616625 b/archive/ES_0.5713624944616625
new file mode 100644
index 0000000..4af26c7
--- /dev/null
+++ b/archive/ES_0.5713624944616625
@@ -0,0 +1,22 @@
+archive/ES_0.5713624944616625---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T09:07:27.803
+Launch V∞: [6.362505216552561, -7.15304456399771, 0.510266413658592] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.726940162686802e-5, 6.877694695486669e-5, 5.8715935651550415e-5] km/s
+ V∞_out: [-6.312524371661272e-5, -3.523483501269326e-5, 7.918042266182253e-5] km/s
+ time of flight: 1.8749577786247486e8 seconds
+ arrival date: 2029-04-02T11:17:04.803
+ thrust profile: [0.6092220977274926 -0.12069424374052627 -0.11757598742301033; 0.24018044250026252 0.1005689285141834 -0.15470035792000347; 0.1270176537790211 0.09821506601461387 -0.143667583463241; 0.055537227216355275 0.058810054539515266 -0.09400718889994186; 0.05422697598664395 0.0727938287314332 -0.1180176654080565; 0.036756468561157225 0.05952163000006938 -0.10187801593970754; 0.017856945590531262 0.03404974700824262 -0.06176859170480594; 0.009114108415538613 0.018945744670231798 -0.037534937152939506; 0.009994218273888269 0.02463360049763297 -0.04903148257285517; 0.0002888306425701144 0.004044149794324732 -0.007032791840759631; -0.00044602280028358465 0.00017963945112165164 -0.001856063333652502; 0.000786967719605359 0.001095454630497647 2.71046658482689e-5; 0.00034144044292454593 0.001627229949296734 -0.0030151546982207945; -0.0016470383720234448 0.000354049222645523 -0.0005607122475265879; -0.0007920390159359498 -0.0006248149271627795 -0.001173854387813784; 0.0006148676231799493 0.002735260769010939 0.0016444608210781538; -0.00040381490733577954 -0.0011725268412756753 0.002021204721333051; 0.00042935887194773485 0.00016007874881552396 0.0005107734953520549; 0.0001692251176802289 -0.0008705537213688293 0.0012783729148972865; 0.0017939428114507794 0.0007814602752790183 0.0021860548712329658] %
+
+Mass Used: 130.46021283300115 kg
+Launch C3: 91.90789097810375 km²/s²
+||V∞_in||: 0.00010704024427554838 km/s
diff --git a/archive/ES_0.5713724018634772 b/archive/ES_0.5713724018634772
new file mode 100644
index 0000000..10db147
--- /dev/null
+++ b/archive/ES_0.5713724018634772
@@ -0,0 +1,22 @@
+archive/ES_0.5713724018634772---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T16:38:09.902
+Launch V∞: [6.549722155555147, -7.331680105280519, 0.1378110259854445] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.947368192154487e-7, 0.0002941195842975399, -0.00020430172565074906] km/s
+ V∞_out: [-0.0001836265988204039, -0.0003006073739835026, 6.457426710086028e-5] km/s
+ time of flight: 1.8749577787493432e8 seconds
+ arrival date: 2029-04-08T18:47:46.902
+ thrust profile: [0.31832195868217616 -0.07595696452984566 -0.1031374026580858; 0.060071077559655586 0.01906626497992706 -0.06195528833073255; 0.06307233147316099 0.036791545575198106 -0.10594314061502193; 0.046223911125534055 0.036752457408614436 -0.11240735920005457; 0.02372528967453544 0.022990753922063716 -0.07522916321023716; 0.03248482788526757 0.036834762451803185 -0.13527273848084076; 0.014693369141894584 0.020595115623151503 -0.07884162471288486; 0.013189751578981163 0.018903705455083627 -0.07128166791427218; 0.004107651645514183 0.007370817218443943 -0.02714542443522889; 0.015416231241510158 0.022716916494075045 -0.09521284126321324; 0.00616587860253392 0.0046485838268971545 -0.005626959803864947; 0.0018583496609529781 0.004216767558577554 -0.026155471715074312; -0.00394497220768333 0.0012175031840077465 -0.00047288588798213805; 0.00667821059914564 0.005250773772974497 -0.006761260443429981; 0.0015733180992280496 0.0009326390614117085 0.0037779768199812736; 0.013127404477559654 0.008551978604018578 -0.002080601020352414; -0.011679954051451395 -0.013640707750784437 0.0043855368872559135; -0.01728117193716493 -0.018851131315402222 -0.01625298659431074; -0.01306040678082152 0.018222914889672065 -0.01230621490028672; -0.010302896461137363 0.006256514413832631 0.029028498727444254] %
+
+Mass Used: 102.68472090727755 kg
+Launch C3: 96.67138536001929 km²/s²
+||V∞_in||: 0.00035811496132555993 km/s
diff --git a/archive/ES_0.5713767835482633 b/archive/ES_0.5713767835482633
new file mode 100644
index 0000000..7b3d98b
--- /dev/null
+++ b/archive/ES_0.5713767835482633
@@ -0,0 +1,22 @@
+archive/ES_0.5713767835482633---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T19:38:33.648
+Launch V∞: [6.07637473561046, -7.2913646648477, -0.06386460247073471] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0867871217657022, 0.0014721823925868205, -0.06632913941543414] km/s
+ V∞_out: [0.10706501760430816, -0.0008440931632161555, -0.021878334534243364] km/s
+ time of flight: 1.7883188012704027e8 seconds
+ arrival date: 2028-12-21T15:09:53.648
+ thrust profile: [0.7392076663452354 -0.21784266542275446 -0.1997642439395015; 0.25195598491750265 0.07335727778850636 -0.19848497976278578; 0.13939194986629583 0.08362329863099698 -0.18370560576743086; 0.09079881046332212 0.07606195217570448 -0.1683240912650652; 0.0647309239602031 0.06774815013366355 -0.15527184704858485; 0.02103025188042389 0.025855444943375584 -0.06362498828209726; 0.01958104019224188 0.02773264502100181 -0.0701929358363642; 0.005186474409768398 0.008486513848167876 -0.022679019896747213; 0.001413523024145776 0.002395417314241895 -0.005047951295575855; 0.0021028736570429317 0.0010753316242887872 -0.007844206075589602; 0.0009999706216101414 0.002301192966490142 -0.005603506538769191; 0.0010659039507423525 0.0001785525152916234 -0.001695378794637539; 0.0006614438137226258 -0.00020907588322243223 -0.0002156492578365564; -7.188267778958238e-5 0.0015015140449667847 -0.0028113886015130388; -0.0002910274695348005 0.0005616656189063737 -0.0007502022133149301; -0.003994657026070067 -0.0007891301101156231 -0.006159433051907268; -0.00014017621304412333 -0.000950396994908461 -0.0015187763923163926; -0.0010086709375087839 0.0027449779738550756 -0.004168316336037796; -0.0004666004829798274 -0.0002901031410694366 0.0018692384712259043; 0.000956716041655922 0.0006109982625340663 -0.0056832765989756565] %
+
+Mass Used: 141.0788716099537 kg
+Launch C3: 90.09040729080344 km²/s²
+||V∞_in||: 0.10924159720987221 km/s
diff --git a/archive/ES_0.5713934340568044 b/archive/ES_0.5713934340568044
new file mode 100644
index 0000000..473d2b5
--- /dev/null
+++ b/archive/ES_0.5713934340568044
@@ -0,0 +1,22 @@
+archive/ES_0.5713934340568044---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T01:18:13.677
+Launch V∞: [7.242185113048421, -6.736933748091412, -0.49251182615631645] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00032699913747269503, -0.0011961641229542425, -0.0018787426112688058] km/s
+ V∞_out: [-0.0019589047168120377, -0.00020747447388773344, 0.0010906169277572423] km/s
+ time of flight: 1.5294213196706134e8 seconds
+ arrival date: 2029-03-14T05:13:44.677
+ thrust profile: [0.2312223801429665 -0.060490074635886903 -0.09849488992483191; 0.1247286338076729 0.02703088515120812 -0.14631991678297432; 0.11313665950406895 0.049607241260791565 -0.2195293012293423; 0.08925365625744743 0.0516808090410444 -0.24079385952780685; 0.05148753781660725 0.034676784743696204 -0.1775721725477549; 0.03145183484755055 0.023473292053819657 -0.13110841100043463; 0.01456713737504143 0.011517322484073408 -0.07138059762240626; 0.01633447112196159 0.013509406151278274 -0.08900088834806276; 0.003975752696415449 0.003488397235890337 -0.025516243330944786; 0.0004994291529797981 0.00040140859401124104 -0.00543844140399407; 0.002903500472692813 0.002999130358409199 -0.025065868106056627; -0.0010296357576953848 0.002821610550852903 -0.0026051386639916233; -0.00029391921335394314 -0.0008360776495210706 0.00271304785000283; 0.0009123131977589303 0.001478856032640218 0.0033174671162510333; -0.000705025048322365 -0.0037249117722711624 0.0005658645384159491; -0.0009026514234041149 -6.0504905443552236e-5 0.004283299146636777; -0.00012588657359669626 -0.0022726232317199562 -0.0056917839825924126; 7.677027133742932e-5 -2.1982599350913552e-5 -0.00226710105197138; -0.000686280810345567 0.0007682321145070167 0.002567386713066817; -0.0034680644000847864 0.0029648957365351826 0.006758350101578039] %
+
+Mass Used: 94.50348468530592 kg
+Launch C3: 98.07808943673702 km²/s²
+||V∞_in||: 0.0022510910342204977 km/s
diff --git a/archive/ES_0.5713972423281799 b/archive/ES_0.5713972423281799
new file mode 100644
index 0000000..8e644e0
--- /dev/null
+++ b/archive/ES_0.5713972423281799
@@ -0,0 +1,22 @@
+archive/ES_0.5713972423281799---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T12:21:42.504
+Launch V∞: [7.303741221715132, -5.883563162582316, 0.018426293562060353] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.2117974093536864e-6, 3.270459571767894e-5, -0.0006450662959831771] km/s
+ V∞_out: [-2.5503562207125004e-5, 0.0006471320837737553, -6.947312071658188e-6] km/s
+ time of flight: 1.76666210499708e8 seconds
+ arrival date: 2029-12-11T06:18:32.504
+ thrust profile: [0.8887058310712048 -0.06166800151908839 -0.21903181873496466; 0.2912802774114677 0.1550473557749976 -0.23882332667743417; 0.1941911954534252 0.1790257081406452 -0.28330192409837585; 0.029811949229119023 0.03837633902699801 -0.06847693134357859; 0.012764840185024356 0.022603728093657224 -0.0450344168393186; 0.005213734798167089 0.014001947102295707 -0.0306424750922705; 0.005965415159757454 0.024011661413145903 -0.052193510888124135; 0.0074810383991809875 0.01622993832951074 -0.03419109729761745; 0.0006747773725858048 0.002389924362279086 -0.006223914183421952; 0.010208342066455624 0.009952739825164876 -0.038436527440270506; 0.001200627867842303 0.01166981340048577 -0.02000156872500038; -0.0007622262744466646 0.0034405059446892127 -0.008233728023541761; 0.002461249649083629 -0.004720780858825157 -0.0058403820367821475; 0.0009142210373731561 0.01433280202210987 -0.007985765900806484; -0.005707766020297524 -0.017181180781915686 -0.011113920538336337; 0.0008920217390853715 0.019164542799417535 0.006802191649714277; 0.02632505759990172 -0.011005033181060279 -0.021580192051084655; 0.0015633865208593853 0.0046086636644412475 -0.004168782074094933; -0.002901027980591087 0.0036794062895769333 0.0021353873639511772; -0.00662975273423916 0.004231067983303432 -0.007470192482692005] %
+
+Mass Used: 153.52258609021283 kg
+Launch C3: 87.96129085017091 km²/s²
+||V∞_in||: 0.0006459028041718904 km/s
diff --git a/archive/ES_0.5714083029707634 b/archive/ES_0.5714083029707634
new file mode 100644
index 0000000..2758b56
--- /dev/null
+++ b/archive/ES_0.5714083029707634
@@ -0,0 +1,22 @@
+archive/ES_0.5714083029707634---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T21:57:06.450
+Launch V∞: [5.801899999473712, -8.005582334782918, -0.2748433140011001] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.993048448369309e-5, -9.588227487851901e-5, -0.00012626756764063784] km/s
+ V∞_out: [-0.0001669862847472314, -0.00010273791694423601, -4.816710033766497e-6] km/s
+ time of flight: 1.5864999882832655e8 seconds
+ arrival date: 2028-05-05T03:23:44.450
+ thrust profile: [0.21803472411512562 -0.10396500356244333 -0.09536888736107028; 0.07145268133900078 0.002778239964386984 -0.07943958952232025; 0.10434363448519526 0.026044718118288315 -0.18511908577787678; 0.10007953037663947 0.038009265551759035 -0.23856255493725118; 0.07006593957118126 0.03295252004617314 -0.20877102565064967; 0.03222904064765002 0.01736393661486862 -0.113690161425269; 0.03474821834184841 0.020814030501573773 -0.14191722020574324; 0.007833215183543287 0.005224456339507363 -0.03519877940784005; 0.003959498393090999 0.0031337852577041966 -0.020256345104682445; 0.01544614474706436 0.010595992431533568 -0.08469882060777964; 0.0019466545889432335 0.0015110818435430128 -0.010058657357451943; -0.00042923532938640946 0.000767028310575377 -0.004517097395524543; -0.00010052429024873726 -0.00028954506409441 -0.005182270003224352; 0.0004406679255022887 0.0009979902857412924 -0.0021445882670878; -0.0005106436377749703 -0.0010039865989846376 -0.004649702891485361; -0.0022687445701518516 -0.0012389794241868418 -0.003477129343913501; 0.0009524508018270113 -0.001961515753589394 -0.0009603388719654224; 0.0009745990880508812 -7.220641117967907e-6 0.004332794596293649; -0.000657295711947906 -9.071817294063972e-5 0.0026917232450217317; 8.743752931723251e-5 0.0015347329457443253 -0.001636774425173355] %
+
+Mass Used: 95.9859228067844 kg
+Launch C3: 97.8269309701325 km²/s²
+||V∞_in||: 0.0001822756190861375 km/s
diff --git a/archive/ES_0.5714250456128694 b/archive/ES_0.5714250456128694
new file mode 100644
index 0000000..249addb
--- /dev/null
+++ b/archive/ES_0.5714250456128694
@@ -0,0 +1,22 @@
+archive/ES_0.5714250456128694---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T07:15:18.642
+Launch V∞: [5.94855467519646, -7.675177266606916, -0.11153593713519969] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.024009974006774e-5, 8.864279386681293e-6, 1.4331602807163112e-5] km/s
+ V∞_out: [1.6958690970807954e-5, 1.0050814851023857e-5, 4.6169038545564895e-7] km/s
+ time of flight: 1.697591584760703e8 seconds
+ arrival date: 2028-09-11T02:34:36.642
+ thrust profile: [0.4971611343674251 -0.18451775952488078 -0.17280194426010145; 0.09598958214344933 0.016516143013702207 -0.10187034722429557; 0.07545540989391479 0.03104786075011861 -0.12761399683046695; 0.06025893998900052 0.03494608060197446 -0.13916831786259937; 0.03149422729422229 0.022607814989726176 -0.1013439476213395; 0.02246463170889663 0.019862972861963445 -0.08525720096474544; 0.029586371510090508 0.029202041428580267 -0.12143146559969771; 0.01328869183991338 0.015098191591601778 -0.07187549306310041; 0.016270836219799186 0.018338116548520453 -0.08573066278625148; 0.017021504174913313 0.0184014952573715 -0.08831192563757535; 0.011617533071318699 0.01544434027035849 -0.06696931658185086; -0.0015806136430361354 -0.0011039201129234722 -0.00018071806348040394; 0.0010604916466843933 -0.0017840453509050474 0.0025327903163894737; -0.0020415481987940227 -1.5617694341713896e-5 -0.0032245876070311247; 0.00331068176337383 0.0014315279416285593 -0.004150275480702868; 0.011170775881559911 0.0013912849282469173 0.006595262507989523; -0.002978934347566726 -0.006711728848199964 -0.015515318411106208; -0.0021099789566323473 -0.0017177694380463458 0.002887062194056913; -0.0008707777388068498 -0.0005904948199763722 0.006953843474835906; 0.0014791450148149488 -0.008665501339637501 0.004870856484122476] %
+
+Mass Used: 116.5437003480165 kg
+Launch C3: 94.30608906291391 km²/s²
+||V∞_in||: 1.971877102544588e-5 km/s
diff --git a/archive/ES_0.5714336528071506 b/archive/ES_0.5714336528071506
new file mode 100644
index 0000000..d4dfb06
--- /dev/null
+++ b/archive/ES_0.5714336528071506
@@ -0,0 +1,22 @@
+archive/ES_0.5714336528071506---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T06:54:57.307
+Launch V∞: [7.369130756713634, -5.991399858548754, 0.14090965059808291] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1176269954829448e-6, -5.893993259050059e-6, -2.813075963968194e-6] km/s
+ V∞_out: [-4.640200971331252e-6, 4.306275090062509e-6, 2.6566620026530666e-6] km/s
+ time of flight: 1.679311459580466e8 seconds
+ arrival date: 2029-08-29T22:27:22.307
+ thrust profile: [0.9000555296328648 -0.09979053980691097 -0.20841575076583763; 0.20227262197645715 0.10076528272119019 -0.16658999191484206; 0.05495823949727415 0.047012438894623094 -0.08554526839719086; 0.056612273889487356 0.0651863192970469 -0.1207227040390636; 0.033306203719234324 0.04808187189697377 -0.0996327847192992; 0.023769599597893397 0.03933168395935272 -0.08751328478044758; 0.0557892017396807 0.11513429213146671 -0.2337847275255352; 0.006567850548500869 0.01473335642330092 -0.03721940582883217; 0.0062101633959649035 0.015623725334731381 -0.03994138801400711; 0.0009732262139306008 0.0024643677319959034 -0.007150964139171026; 0.0027616286079463126 0.009700515901875633 -0.02395274230438383; -0.0013591169155313504 -0.0008586896432216221 -0.000766567408947313; 0.0007967982632395706 0.000978548681755072 -0.0017518890557028394; 5.043129324219534e-5 -0.001975895361045977 0.0012357122851639982; 0.002158783755716175 -7.29076189607507e-5 -0.0016050092597013658; -0.0007987767666557354 0.0031105091598358317 0.001083899035108422; 0.000611791572465508 0.004432772426693201 0.0031624540039261887; 0.0014918753192926669 0.002431918379114709 -0.00435419754505368; -0.0038569540133048846 0.004068260163441178 -0.0035458888512252358; -0.0005453807077352453 -0.0004952417290203827 -0.0005300851189126861] %
+
+Mass Used: 140.38450216721913 kg
+Launch C3: 90.22081590419256 km²/s²
+||V∞_in||: 6.86563158120076e-6 km/s
diff --git a/archive/ES_0.571436117296873 b/archive/ES_0.571436117296873
new file mode 100644
index 0000000..d166aa9
--- /dev/null
+++ b/archive/ES_0.571436117296873
@@ -0,0 +1,22 @@
+archive/ES_0.571436117296873---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T22:06:13.798
+Launch V∞: [7.3934798216723365, -6.467159521407149, -0.23454148173619244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.577380917096859e-9, 4.97286391814735e-9, -6.894028354237938e-9] km/s
+ V∞_out: [5.422036036971849e-9, 1.106176811938508e-8, 3.623913353764806e-10] km/s
+ time of flight: 1.5931314037023714e8 seconds
+ arrival date: 2029-05-26T19:45:13.798
+ thrust profile: [0.39051878702683823 -0.0807309281152355 -0.1489090929571213; 0.05086640385052154 0.014623773143598754 -0.05893193114418065; 0.07596126754275094 0.0410180847429421 -0.1489097361505607; 0.057894613203862445 0.040949310838049584 -0.15888009609488266; 0.04215068155468214 0.035124646221745624 -0.1486316397599528; 0.022643922603080593 0.020667094105057012 -0.0952624595271101; 0.010968114636099603 0.012770155002281913 -0.06633146832086147; 0.032061072944499926 0.036302169358201075 -0.171933819785498; 0.016559835778096294 0.016894611284098242 -0.09631668070676631; 0.002701993077899404 0.0018935440550338486 -0.013872717767920439; 0.009786938114293292 0.013252282468938587 -0.06995782887214558; 0.0018716907339598082 -0.0007321812594904202 -0.013416046383255869; 0.005542963287946789 0.0030933895163664286 -0.001556473270261454; -0.00060527532685016 -0.001832041280246062 -0.001245234081015809; -0.007307590961154921 0.0027326077862898585 0.0038093737849163637; -0.001205597847825242 0.0014027423590350237 0.0022570851965423447; 0.0029607462126943263 0.0007534494556952442 0.00592329617074786; 0.008929088592428002 0.00013005067052686612 -0.015780657650305053; 0.0032954482811038805 -0.00439416987196936 0.0080928626572636; 0.003393718182328501 0.00701701494663818 0.019762949030881057] %
+
+Mass Used: 103.50968602284593 kg
+Launch C3: 96.54270585545817 km²/s²
+||V∞_in||: 1.207594575569242e-8 km/s
diff --git a/archive/ES_0.5714379256153916 b/archive/ES_0.5714379256153916
new file mode 100644
index 0000000..66c5829
--- /dev/null
+++ b/archive/ES_0.5714379256153916
@@ -0,0 +1,22 @@
+archive/ES_0.5714379256153916---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T20:00:07.940
+Launch V∞: [7.986134973370233, -6.326069791241371, -0.001666236536034087] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004428481517221555, 0.012016701534568823, 0.02813038685525145] km/s
+ V∞_out: [0.028084771473056463, 0.0034219097333238117, -0.012113776902176727] km/s
+ time of flight: 1.827004916593888e8 seconds
+ arrival date: 2030-03-06T10:08:18.940
+ thrust profile: [0.046381000203171235 -0.01117831323540178 -0.024152756951299315; 0.0074851715394346225 -0.0004919451371709224 -0.01348430974988251; 0.018101313300153726 -0.0027489152431465743 -0.05552933060298267; 0.03550559584615238 -0.01086067292003222 -0.13868741852300845; 0.035842811025431534 -0.015504315072352342 -0.16387418590246505; 0.02797344280714805 -0.014841807034621016 -0.14216093705443716; 0.01805362810116272 -0.010926777359526666 -0.09948573350419818; 0.008709672234941481 -0.005830110085403276 -0.05324766215432002; 0.005775168688290004 -0.0039362657212275425 -0.03540151632511078; 0.0018364530957073596 -0.0012354390781735521 -0.012485941791361381; 0.0018989582837167006 -0.0009666500975538537 -0.011358530037404321; 0.0009961701970811958 -0.0009712001303826036 -0.006666596677287609; 0.004113333331149953 -0.0034786529856988967 -0.026559311887193172; 0.00014863527163494592 -7.520995397106907e-5 -0.001432596298543655; 0.00018361662499499407 3.659837791331077e-5 -0.0006280245506365353; -0.0004606911155143342 0.0005270355632611839 -0.0012314818211076463; -0.0001592095213201895 -0.0002228928882572793 -8.253601690318108e-5; 2.5296926547447568e-5 -5.470650139321293e-5 -0.00015401669784750622; -0.0006107890624756256 -0.00014402619946535768 0.00017953421831955972; -0.000858468821909295 -0.0007634334964207404 -0.000514529561387252] %
+
+Mass Used: 61.19208392611017 kg
+Launch C3: 103.79751359288801 km²/s²
+||V∞_in||: 0.030908432974600723 km/s
diff --git a/archive/ES_0.5714516056780469 b/archive/ES_0.5714516056780469
new file mode 100644
index 0000000..d35c066
--- /dev/null
+++ b/archive/ES_0.5714516056780469
@@ -0,0 +1,22 @@
+archive/ES_0.5714516056780469---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T15:14:05.361
+Launch V∞: [7.6193937044698625, -5.7858357361566775, -0.07969054351828855] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.916624229487002e-6, 2.829541091081281e-5, -0.000563003047705953] km/s
+ V∞_out: [-2.2528176936196897e-5, 0.0005599308780573457, -5.709092020848331e-6] km/s
+ time of flight: 1.8064808535900193e8 seconds
+ arrival date: 2030-01-26T11:15:30.361
+ thrust profile: [0.597221636909122 -0.001211377954753917 -0.12005882892968993; 0.2597039800640321 0.17435108010638334 -0.1773114780553728; 0.08535840230532868 0.09951367639065534 -0.11894180410263565; 0.068956630479695 0.11404832800590688 -0.14382584394446749; 0.02559393118491985 0.054493471076546306 -0.07782496553015408; 0.023277839929018964 0.06303800362862665 -0.09560794126340132; 0.01777105746957529 0.06073606173943167 -0.0964482914528325; 0.00649049426244743 0.024521734542308726 -0.042875673726417436; 0.0011271138587246638 0.025565940224201392 -0.0380115750659072; -0.0019676302882595045 -0.0007216439547492095 -0.0068489979958455; -0.0010969534083617434 5.228995305369506e-6 0.00033600728324286854; 0.0002821110538902303 0.0006333070308953067 -0.0009340994819947895; -0.0001475637118329765 -0.0004365725635329309 -0.001027275010421583; -0.00756505501369727 0.01110867342643341 0.002219453887225592; 0.005217742403795482 -0.01097549973060976 -0.007591702393162377; 0.011085536394831447 -0.0013031078354904025 -0.001061112752442557; -0.002175264056372783 -0.002871108805848646 0.0018632513788285603; -0.01289596493160303 0.01010987674744211 -0.0008602457759194382; 0.0005915480317855239 -0.002174621303040605 0.001439662593787049; -0.00014056933386333062 -0.0019255644193446747 -0.0036796010065399884] %
+
+Mass Used: 132.7253372863861 kg
+Launch C3: 91.5374061722289 km²/s²
+||V∞_in||: 0.0005637211799300248 km/s
diff --git a/archive/ES_0.5714720332383227 b/archive/ES_0.5714720332383227
new file mode 100644
index 0000000..c852727
--- /dev/null
+++ b/archive/ES_0.5714720332383227
@@ -0,0 +1,22 @@
+archive/ES_0.5714720332383227---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-23T00:08:48.199
+Launch V∞: [8.022422430080818, -6.343467455119923, -0.1228051136004346] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.106536685347406e-7, 7.972589047465384e-7, 2.161390264506476e-6] km/s
+ V∞_out: [2.071787112482341e-6, 2.444560465981093e-7, -1.0032924242926967e-6] km/s
+ time of flight: 1.8539238720351958e8 seconds
+ arrival date: 2030-04-07T18:01:55.199
+ thrust profile: [0.009750151514058303 -0.0016918588799306085 -0.004991884037067994; 0.009659406220149032 0.0007787639147808585 -0.01662838358358368; 0.032364143748465427 0.0014559325360365826 -0.09467788437041735; 0.03237321962081594 -0.0009384662903693546 -0.1263348511477777; 0.027376889242380423 -0.003320345218215699 -0.12829370066831658; 0.01948138151235636 -0.004203409058461484 -0.10356299316415267; 0.01940482143815872 -0.005916201669607517 -0.11155860021286403; 0.01271210285591663 -0.004010926252729063 -0.07705824560056405; 0.00860789035247183 -0.003251692093099895 -0.05400686184892776; 0.0013364408076164626 -0.0005908831068226558 -0.010723524959602257; 0.00011848348135017067 -0.00014615511572906405 -0.0011677595562350695; 0.0006757848039278527 -0.0003570516998136419 -0.004643788696811756; -3.431375313114123e-5 -0.00014208072204028064 -0.0004180382442350999; 7.08109312570941e-5 -7.013914039233411e-5 -0.00047304708984883994; -0.0002141372993486717 -0.00018823926698436673 -0.000771147227961132; -4.258056685458702e-5 -0.00031293185532423154 -0.0009368781847502147; -6.482937563023864e-6 7.521245147936774e-5 -0.00011069183707517632; -0.00011164528546055592 0.0009263498981100186 -0.0003028714843557967; -5.983258998017052e-5 -0.00019509578809814192 0.00020512828659342516; -0.00016978280441769006 -5.670442606750694e-5 -0.00011490618087706345] %
+
+Mass Used: 56.469493213633996 kg
+Launch C3: 104.61392209675586 km²/s²
+||V∞_in||: 2.3133535408078396e-6 km/s
diff --git a/archive/ES_0.5715589775336628 b/archive/ES_0.5715589775336628
new file mode 100644
index 0000000..ba8a2eb
--- /dev/null
+++ b/archive/ES_0.5715589775336628
@@ -0,0 +1,22 @@
+archive/ES_0.5715589775336628---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:25:09.144
+Launch V∞: [7.358266291152504, -6.81947831010473, -0.047614515421452556] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004939128596801335, 0.007799934082605475, -0.00012048638478004084] km/s
+ V∞_out: [0.007519612308062783, -0.001227337129389554, 0.0017431611746358553] km/s
+ time of flight: 1.6044107195570946e8 seconds
+ arrival date: 2029-06-14T04:23:00.144
+ thrust profile: [0.14832786941377377 -0.04153944198214134 -0.06996518986291352; 0.03339683559611238 0.0035769219906359355 -0.04776817061235825; 0.058298092772759415 0.012515403085482563 -0.1376215349474859; 0.06411566096624029 0.015560251243597405 -0.20644290647489355; 0.05432182119025888 0.01302278845709355 -0.21712720388731535; 0.03962658938288091 0.008873353245493978 -0.1859927407259263; 0.023198843131584088 0.004713770859856469 -0.12415596169103317; 0.006797088750863416 0.0011296224218039289 -0.03969664341322199; 0.0052419015754379145 0.00050441352640499 -0.031813470292594376; 0.0019986981742062277 0.00026046134177951536 -0.014177508071205712; 0.0007794786548085971 -0.0009162857748494348 -0.006761134796549548; 0.0012394247198343655 -9.068717220827693e-5 -0.0032621215420729427; 0.000373432524152429 -0.00024016634719705604 -0.0023107300415292974; -0.00028348323033889613 0.0013898825802234113 -0.0029210548192604244; 0.0011132091650668907 7.610441378936938e-5 -0.001796433587099009; -0.000849965610147589 -0.0003274476085790281 0.00041815014461362245; 0.00024028499432133328 -8.045540379277548e-5 -0.001483366431814184; -0.00020614171777542543 -0.0011690693343744424 -0.0019872305855014863; 3.952004976340179e-5 0.00010034284890253595 -0.0012459213795926755; -3.365034782715779e-5 -0.0009255064426045624 0.0004550163225615499] %
+
+Mass Used: 79.68427326506298 kg
+Launch C3: 100.65163437557892 km²/s²
+||V∞_in||: 0.007816485052430234 km/s
diff --git a/archive/ES_0.5715628944235059 b/archive/ES_0.5715628944235059
new file mode 100644
index 0000000..2bec307
--- /dev/null
+++ b/archive/ES_0.5715628944235059
@@ -0,0 +1,22 @@
+archive/ES_0.5715628944235059---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:23:35.607
+Launch V∞: [7.348449490746021, -6.623128849825633, -0.3177359650588448] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008106278006489132, -0.005953840658410021, 0.0033082758595610186] km/s
+ V∞_out: [0.002759964947159731, 0.0052229553401241715, -0.0034861952105497227] km/s
+ time of flight: 1.5406390629040152e8 seconds
+ arrival date: 2029-03-26T19:55:21.607
+ thrust profile: [0.28240883741323136 -0.07295984796065541 -0.11568201739069343; 0.08679142676345647 0.01995621073350334 -0.10028269939277958; 0.06293307225005838 0.028031183086395187 -0.12194552844706949; 0.0524576933942778 0.030703914182730534 -0.14095746532754888; 0.039342890937052594 0.026611087412168364 -0.1336586431743335; 0.027853298029332615 0.020709164724940617 -0.11317191191052206; 0.03076568484729096 0.025520015581752875 -0.14597415820837586; 0.029726334983313483 0.027268224597308814 -0.15824373288978322; 0.013121209077049308 0.009749087564480527 -0.06967205940600715; 0.019267459659083032 0.019112234410169363 -0.1273500543285046; 0.0010174620237888032 0.0011481168927642248 -0.007505947134057571; 0.00017104770610164972 0.0006537421347091105 -0.0034440502047424905; 0.00046429722989596833 0.0005873581764465281 -0.003357072733974692; 0.00029564679804596167 2.6193687117191146e-5 -0.0012754508491682184; 0.004506714691988111 0.0005788537392063869 -0.005844396646148877; 0.0006773844924260494 -0.0007255311976247366 -0.0014184584875850522; -0.0008859578417315386 -0.0004560659082828969 -0.0005964736398174071; 0.0018223127986336436 -0.00038716345897975236 -0.006252188606450066; 0.0008203311034901289 0.0006922148303038814 0.001442154611806001; -0.00033091470270086155 -0.001614608164448545 -0.00020687782687382237] %
+
+Mass Used: 95.35211619366555 kg
+Launch C3: 97.96650182292994 km²/s²
+||V∞_in||: 0.006859302091311868 km/s
diff --git a/archive/ES_0.5715639839872315 b/archive/ES_0.5715639839872315
new file mode 100644
index 0000000..7418c33
--- /dev/null
+++ b/archive/ES_0.5715639839872315
@@ -0,0 +1,22 @@
+archive/ES_0.5715639839872315---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T23:13:22.676
+Launch V∞: [5.8111001513348, -8.04039474490868, -0.229332407596371] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008968532998423196, -0.006153814435692593, -0.008935269829074506] km/s
+ V∞_out: [0.005617149150707797, 0.009742509354013386, -0.00846457586209779] km/s
+ time of flight: 1.6323992036467135e8 seconds
+ arrival date: 2028-06-30T07:38:42.676
+ thrust profile: [0.21708188235187592 -0.10338710293022563 -0.10196526292586694; 0.06108777788042557 0.0004513814751110984 -0.07961404553902279; 0.0579374566451417 0.010700610604318513 -0.12421064206066275; 0.05490791591882812 0.015873707507757018 -0.15566315338605563; 0.050370545018587315 0.01575154418201915 -0.17894798435657844; 0.03864225803910639 0.013071153166595604 -0.1591685230178991; 0.02340061690057823 0.009598600728803995 -0.11197562302854787; 0.022878108754766674 0.012335069999860348 -0.1299992299966989; 0.014414348442473544 0.007191392410980553 -0.0842850954997553; 0.0037779484052036525 0.0010266008594499256 -0.025935556531673756; 0.0015261227581682007 0.0007579862754793371 -0.010755132378056354; 1.3402449873008452e-5 -7.501017005792896e-5 3.4039025104249006e-5; 0.0013750049502790841 0.0014666940414846267 -0.005276722599276324; -0.0001362319662031367 -3.2114627989958766e-5 0.0004817463222766582; -0.0014200280918954314 -0.00031202839948414347 0.00228022419741806; 0.0006701336721087087 -0.0002560474403854627 0.0033821611995850593; -0.0013216350772725293 -0.0015357355381121268 0.0032714237731270293; 0.004877399891356305 0.003485953488440144 0.006557954082138721; 0.004026066707511481 0.0008594343210612642 0.005136314740643903; 0.0034630900600878005 -0.000985775874031723 -0.0019959707166075165] %
+
+Mass Used: 92.41966312526438 kg
+Launch C3: 98.4694259759724 km²/s²
+||V∞_in||: 0.014076329889964694 km/s
diff --git a/archive/ES_0.5715763233700528 b/archive/ES_0.5715763233700528
new file mode 100644
index 0000000..54eb2d2
--- /dev/null
+++ b/archive/ES_0.5715763233700528
@@ -0,0 +1,22 @@
+archive/ES_0.5715763233700528---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T02:17:44.096
+Launch V∞: [5.87097300406663, -7.486587942077518, 0.22274675806151553] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008776681794325588, -0.004314743275135917, 0.00979165134265899] km/s
+ V∞_out: [-0.008905784356858385, -0.00390886454942647, -0.009832652691400096] km/s
+ time of flight: 1.7217938998572013e8 seconds
+ arrival date: 2028-10-05T21:54:13.096
+ thrust profile: [0.780481802995736 -0.25255711246668927 -0.18850340642218164; 0.13439597321727256 0.03762378709668868 -0.10972413619616049; 0.12395123550276196 0.07455533571172646 -0.1595731640702397; 0.06308926454838029 0.05157147691123699 -0.11705946538930358; 0.04138498124675716 0.04124768560811939 -0.09892768293186871; 0.04913355930414783 0.058881952571071504 -0.13506821758728818; 0.02976996560048211 0.03742335026825502 -0.09348001740557745; 0.026097946997884414 0.036027949229867545 -0.09664884844715463; 0.019814381655903976 0.03540721459080909 -0.1002305746291742; 0.0005619932573941071 0.0009395963643450977 -0.006936420819270695; 0.001991459270856751 0.0038638428966848307 -0.012438584581100729; -0.002040521066490292 0.0012642998092870445 -0.0003717574676512007; -0.0016555082659184702 -0.0018113016543890308 -0.0019479567727261778; -0.0019777068308538164 -0.001213716595441132 0.0027614585824536518; 0.0024229813585347646 0.0026050850831122133 -0.0015714133413032626; -0.0025795665038944194 -0.0006366070099024625 0.0017929597482088068; -0.004499097857397742 -0.00177200826395642 4.6051337148576496e-5; 0.0019917211859596814 0.0027168378102447946 -0.0035365952483305024; 0.0037694804006971113 -0.0016059288016796658 0.00041605883897468917; 0.0018596998836416549 0.0004180681430054295 -0.002696317384163427] %
+
+Mass Used: 138.53189890658996 kg
+Launch C3: 90.56693914716656 km²/s²
+||V∞_in||: 0.013839204777203509 km/s
diff --git a/archive/ES_0.5715874378437125 b/archive/ES_0.5715874378437125
new file mode 100644
index 0000000..021dfe9
--- /dev/null
+++ b/archive/ES_0.5715874378437125
@@ -0,0 +1,22 @@
+archive/ES_0.5715874378437125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:32:31.904
+Launch V∞: [6.622625996182994, -7.32019536958593, 0.15933319649395747] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1745675223369004e-5, -3.487971952536803e-6, 5.9310681497222404e-8] km/s
+ V∞_out: [4.319098934441139e-6, -9.797579543825266e-8, -2.1596225911758252e-5] km/s
+ time of flight: 1.8749577787493235e8 seconds
+ arrival date: 2029-04-08T21:42:08.904
+ thrust profile: [0.25669162683974095 -0.06165807668552353 -0.07919750234712757; 0.07160361172643433 0.0220795192939135 -0.08010573735152252; 0.041769722271591814 0.02362829023323821 -0.07832723812504913; 0.04134069469578355 0.031508631774286235 -0.10527420922301109; 0.029919701726509283 0.026262058171070933 -0.09455099195920831; 0.02699241550867908 0.029433782630955956 -0.10777758993266057; 0.030964596244124534 0.03041565079281922 -0.14598734149134737; 0.01482868796436291 0.017766864709896947 -0.07513975640573534; 0.014074913061045139 0.015607599263458366 -0.05848074981614099; 0.0035846462506198325 0.007185310167163389 -0.029542992939182264; 0.0006582359835347732 0.002152464205464239 -0.004343784297150087; 0.0008870217851930553 0.0045818250898505206 -0.0010599398819596062; 0.006921017034656424 0.0010898745774404108 -0.008636934884709829; -0.00482688941927431 0.0026842876687095253 0.007732729614321005; 0.010448857962150535 0.005779832425131246 -0.001699807446668896; 0.0058808515015595295 0.0006512264577827725 -0.01143394303284274; 0.025453157597205962 -0.002735449433785415 -0.008268447288807785; -0.0075911403262658265 -0.011934141413379113 -0.03455976283443564; 0.014552311067551792 0.004751368124736868 -0.0029647049805939466; 0.04515472153021659 0.005579054296732652 -0.00036599954641102677] %
+
+Mass Used: 98.27804680756662 kg
+Launch C3: 97.46982240173107 km²/s²
+||V∞_in||: 2.2023711245357077e-5 km/s
diff --git a/archive/ES_0.5715896197229404 b/archive/ES_0.5715896197229404
new file mode 100644
index 0000000..af0a55e
--- /dev/null
+++ b/archive/ES_0.5715896197229404
@@ -0,0 +1,22 @@
+archive/ES_0.5715896197229404---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T04:35:30.079
+Launch V∞: [6.2069023040046165, -7.3258448530970535, 0.1840714776023781] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0649846426408077e-7, -2.0978211087234086e-7, -9.447704463673304e-8] km/s
+ V∞_out: [6.893302757604285e-8, -1.280008456245722e-7, 2.0804266997092806e-7] km/s
+ time of flight: 1.874957778719183e8 seconds
+ arrival date: 2029-04-06T06:45:07.079
+ thrust profile: [0.5646506259285061 -0.11240518284982248 -0.12848270449343357; 0.15653913736540345 0.060257266544670285 -0.11961487283538898; 0.10310395832245615 0.07195750550271428 -0.1333613128546111; 0.06980578751455173 0.06593857135581413 -0.12361151147561489; 0.04456350373118139 0.05386578162710656 -0.10546796706017109; 0.03129262526570932 0.04456524730082787 -0.09726635309602029; 0.027355281772457832 0.04068702393675946 -0.08944567139455897; 0.009236127058761761 0.016858946744792734 -0.03710491326690352; 0.007133697488397126 0.01911611044980021 -0.035036597123162705; 0.001150553915689423 -0.004475242101772458 -0.011050296531215278; 0.005172296164758785 0.010693482162958826 -0.023782647412755886; 0.0041286616675672815 0.00921194321615716 -0.019160255128599632; 0.0031703185460929015 0.0023150630883302056 -0.0061701441955133544; 0.003626982239360731 -0.0018805749454599173 -0.0017294893519058663; -3.919743102788801e-5 -0.0006958402045836565 0.0019405472572309795; -0.004973740979233567 0.003203928716624588 0.002402631998247736; -0.0049073142552063555 0.002337796704302725 0.0023496151528918253; -0.00022099273511054984 0.0006587389049091254 -0.00013265305283472915; 0.03047690219942854 0.004244262485781248 0.01190899187260868; -0.04251079497799444 0.010018655358433924 0.019633699066573394] %
+
+Mass Used: 128.8606819069205 kg
+Launch C3: 92.22752133197314 km²/s²
+||V∞_in||: 2.535278463915829e-7 km/s
diff --git a/archive/ES_0.5716264668640015 b/archive/ES_0.5716264668640015
new file mode 100644
index 0000000..e7bbd2b
--- /dev/null
+++ b/archive/ES_0.5716264668640015
@@ -0,0 +1,22 @@
+archive/ES_0.5716264668640015---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T15:53:12.803
+Launch V∞: [6.648327505258319, -7.419582326550219, -0.015116722065680885] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012536125281898373, -0.000380729209254913, 0.00860004315642201] km/s
+ V∞_out: [-0.01454241311461345, 0.00022471208644452202, 0.004438862984164014] km/s
+ time of flight: 1.8749577787493965e8 seconds
+ arrival date: 2029-04-10T18:02:49.803
+ thrust profile: [0.12415806169988956 -0.0337427028667184 -0.04581947816153468; 0.038677456444926026 0.009200844593903659 -0.04029318033907571; 0.055625188517264224 0.02470263314972283 -0.10226775034767357; 0.05318815862649065 0.031006696650934033 -0.1375503219906325; 0.04491928271559525 0.030758138483191887 -0.14789153308158864; 0.030280768514693888 0.02350419892212929 -0.1197459117245274; 0.01688044469227248 0.014631810131347813 -0.07598062791738475; 0.009796874368514593 0.009617486371032663 -0.05104527591745476; 0.004225440468341725 -0.002089751562162465 -0.02336793112529605; 0.006507064520598536 0.0063305301590669775 -0.03288163799938839; 0.008235407409056482 0.006696370295515363 -0.03415481050729789; 0.0042758324229164495 0.003290447485363582 -0.02903231333024258; 0.003364460687711157 -0.0028878489881954 -0.008789386294606478; 0.01873107034087814 -0.00409474198881379 -0.0033802692419677254; 0.015930515823123655 0.013285326516955985 -0.0034348595699632747; 0.01370826074345038 6.472865573856467e-5 -0.008513211412777558; -0.04547919000673082 0.007099992258711078 -0.021929725637702124; 0.0043624205400588124 -0.01614793934354547 -0.00365534881476766; -0.01230287022347959 0.005768077380351313 -0.019306468308309534; -0.009655305665248089 -0.004976809146173492 0.014493811460150566] %
+
+Mass Used: 87.93519198265449 kg
+Launch C3: 99.25068903291667 km²/s²
+||V∞_in||: 0.015207239529465974 km/s
diff --git a/archive/ES_0.5716361857436635 b/archive/ES_0.5716361857436635
new file mode 100644
index 0000000..a90232e
--- /dev/null
+++ b/archive/ES_0.5716361857436635
@@ -0,0 +1,22 @@
+archive/ES_0.5716361857436635---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T20:40:48.638
+Launch V∞: [7.1639527709161595, -6.687032830078609, -0.02991356113422716] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6365710257923893e-6, 7.444594298682093e-6, 3.870356650931418e-6] km/s
+ V∞_out: [6.100722687292767e-6, -5.391743897724208e-6, -3.324852540417119e-6] km/s
+ time of flight: 1.5391959218797576e8 seconds
+ arrival date: 2029-03-25T08:07:20.638
+ thrust profile: [0.4224296348307106 -0.1101324118265469 -0.1640102494661681; 0.12162712267153829 0.027457490839295683 -0.1374308201416089; 0.08428902806695317 0.038482261037670454 -0.16140031743219696; 0.06693333413031549 0.04044876150102301 -0.17662384012276466; 0.0557003235553309 0.04023901830405913 -0.18488771439304935; 0.03987939161498526 0.031201818835002212 -0.1603256570796319; 0.034001670578248974 0.028836568095750505 -0.15844947009054755; 0.010095736224133735 0.008529835204369193 -0.05433074589889198; 0.004048705072463498 0.0038403046571822154 -0.025784816554952815; 0.004005785306490932 0.0030302756675774827 -0.02407766864545459; 0.003381001459004218 0.004772485225216325 -0.02816455883988213; 0.0010243977623010333 0.0012970529783745618 -0.005667691463889754; 0.0028740452138276765 -0.0003392320335857956 0.00046964260607860455; -0.0006065087689474548 0.0034274202850536374 0.0012012181681909607; -0.002788815811478347 0.0009575008602561435 0.0006690878391292846; -0.0025846521833491516 -0.0047928814259993475 -0.0007417319477569525; 0.0014421247134733834 -0.000621763268938807 -0.001973664066051976; -0.004611527303058007 0.005029232985950593 -0.0023817276573449638; 0.0007801966020217562 0.0015173380379696463 -0.0008164333244275181; -0.0044556785460830185 -0.003908130304647782 0.009359272522012983] %
+
+Mass Used: 106.67833722657133 kg
+Launch C3: 96.03952219560618 km²/s²
+||V∞_in||: 8.795064050444825e-6 km/s
diff --git a/archive/ES_0.5716404413547432 b/archive/ES_0.5716404413547432
new file mode 100644
index 0000000..33b5628
--- /dev/null
+++ b/archive/ES_0.5716404413547432
@@ -0,0 +1,22 @@
+archive/ES_0.5716404413547432---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T12:26:21.115
+Launch V∞: [8.015520222356848, -5.776453610085274, 0.2908822503611646] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0017710300360833022, -0.001270369792989461, -0.07360438410015038] km/s
+ V∞_out: [0.06723490462219832, 0.02702001492420955, -0.012931476525891212] km/s
+ time of flight: 1.8597020235700542e8 seconds
+ arrival date: 2030-04-05T22:49:43.115
+ thrust profile: [0.22911912782561694 0.007039591129243534 -0.07531254203932998; 0.07324151138770686 0.04574573432350438 -0.08469002426124869; 0.04463692883828496 0.04293288494169944 -0.08826778065496885; 0.03760357003129519 0.04828065074901427 -0.10923944426782915; 0.024334353881031008 0.03734750973665555 -0.0955309000571947; 0.01716706746557838 0.033022387550695934 -0.0881860793639275; 0.017532944103199014 0.034315631661433664 -0.09844335217500172; 0.010657849248741847 0.02719798162625148 -0.08347851223527593; 0.006427596015803732 0.014163314725438778 -0.05190114663226015; 0.004483628874380457 0.013133678570415622 -0.042662128086205724; 0.002108259299094169 -0.0012408626097142397 -0.01745972629769736; 0.0019642184761351697 -0.0031246533360872134 0.006070385429690565; 0.009594609377216337 0.004867053479177486 0.008508929757203881; 0.001163286853542346 -0.00778865016304746 0.013237122187629484; -0.0021528285353762974 0.0003119594440615277 -0.0023287708083630588; -0.00261683933181738 -0.021441688260635354 0.01814620448223794; -0.019705842372150725 0.024077505522865982 0.001966916575550529; -0.012569261773958201 -0.02996578336497396 0.0251040261242611; -0.019775145806511355 -0.01046539372570496 0.021166178724283276; 0.01616187022670451 -0.0006721461116432276 0.027503974822608006] %
+
+Mass Used: 96.99372108355237 kg
+Launch C3: 97.70059322805395 km²/s²
+||V∞_in||: 0.07363664675663958 km/s
diff --git a/archive/ES_0.5716424391156902 b/archive/ES_0.5716424391156902
new file mode 100644
index 0000000..c08d9b9
--- /dev/null
+++ b/archive/ES_0.5716424391156902
@@ -0,0 +1,22 @@
+archive/ES_0.5716424391156902---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:04:35.448
+Launch V∞: [7.254908334364902, -6.6401158383029975, -0.5195099238329839] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001008723319402708, 0.015813808295754378, 0.0018963228622783381] km/s
+ V∞_out: [0.015262602473094801, -0.002867425794748682, 0.0037104877104697075] km/s
+ time of flight: 1.5123731538264236e8 seconds
+ arrival date: 2029-02-21T05:26:30.448
+ thrust profile: [0.4203557518111806 -0.10746637069684645 -0.16098114373967926; 0.058891122532002724 0.011921969598796468 -0.069699966664135; 0.07585746918030727 0.03261645539441506 -0.14580095844627483; 0.06433041737311307 0.0370877895382755 -0.1703008127905594; 0.04960691667231538 0.03382016297363239 -0.16740931526230254; 0.022391187373407225 0.01631566281144748 -0.09241591613466649; 0.06901738962619058 0.03127231799688964 -0.22826316877143052; 0.03475738286401403 0.024652469453648268 -0.18910260003503165; 0.0015313394861815714 0.0014920548274777094 -0.011483614704854914; 0.0025987757866605585 0.002505449560821505 -0.01597180305788426; 0.002337041675551156 0.0026989610004227757 -0.022801396117908376; 0.00012163728990802178 0.0004585508647365691 -0.0022863364709136613; 0.0005246607648160097 0.0006722750140867188 -0.0018554569019364133; 0.0003622416741993882 0.0003075801053886887 -0.0008341192427340301; 0.000508930398431218 -1.0487505452673094e-5 -0.0013724624324039359; 0.00021392398704461762 0.0005783415746570761 -0.0008692992785260428; 2.9052480369962997e-5 -0.0008329931648605884 -0.0005506845304243677; -4.217778703618407e-5 8.460851831515353e-5 -0.00015425010386161406; 0.0008759147383640645 -0.0009288637212439346 0.0006832676035095454; -0.0004800677433423905 0.0003082831808378686 -7.225207210451623e-5] %
+
+Mass Used: 101.11362319366845 kg
+Launch C3: 96.99472384708059 km²/s²
+||V∞_in||: 0.015959013000432586 km/s
diff --git a/archive/ES_0.5716910814024115 b/archive/ES_0.5716910814024115
new file mode 100644
index 0000000..a9b6f83
--- /dev/null
+++ b/archive/ES_0.5716910814024115
@@ -0,0 +1,22 @@
+archive/ES_0.5716910814024115---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:46:40.297
+Launch V∞: [6.340419807569118, -7.414760986266031, 0.22382923934612609] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.024030921770962825, -0.0003903872875998755, 0.02056097449582832] km/s
+ V∞_out: [-0.031016408947115486, 0.00023014951681816484, 0.006150941134414483] km/s
+ time of flight: 1.874957778728931e8 seconds
+ arrival date: 2029-04-09T02:56:17.297
+ thrust profile: [0.36854535738034194 -0.08317664873658107 -0.11792807319111911; 0.1369098339529802 0.0431321531983949 -0.1348553112482777; 0.09403939637560474 0.05549341482170255 -0.15685845403978985; 0.03741520957173225 0.02999665127322615 -0.09414320341171732; 0.044730457405323186 0.04383740769386602 -0.14060126366229758; 0.02374304804683809 0.028765629080636783 -0.09815209286251955; 0.010453338353606512 0.013330947161333456 -0.05044206201805312; 0.01237443557940563 0.01713157572716763 -0.06130065330818299; 0.008978436232238676 0.014444780999589563 -0.05568962026772533; 0.004125759083326639 0.0026020573983937915 -0.012424983273398645; -0.0018749177358854444 0.006650176526520822 -0.00380147233935048; -0.0015320027962743752 -0.0020531167289194207 0.0003010049936392118; 0.002092216211540164 0.0024536631547604796 0.004039680742412759; 0.0001727504270750756 0.0011505842554918513 -0.0033679529384890773; 0.003918102324080887 -0.012628375193681561 0.004195606510771098; -0.014520611479282481 0.014128228282054841 0.010978380702749282; -0.008399349742260013 0.004391205240183396 0.009788088510659567; -0.003409446507569495 -0.0016718508583082054 0.015930923186052298; -0.00039372819429403516 0.013657735901152723 -0.02973535679156292; 0.010099161532359457 -0.03388795981589754 0.007251891180277546] %
+
+Mass Used: 111.46632543916576 kg
+Launch C3: 95.22970334805389 km²/s²
+||V∞_in||: 0.0316289626073091 km/s
diff --git a/archive/ES_0.5717130638174542 b/archive/ES_0.5717130638174542
new file mode 100644
index 0000000..f7a84f4
--- /dev/null
+++ b/archive/ES_0.5717130638174542
@@ -0,0 +1,22 @@
+archive/ES_0.5717130638174542---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T17:01:02.057
+Launch V∞: [7.575996748624382, -6.196984837078249, -0.027531609884514287] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005388447378125162, 0.0006830555011383533, -0.0005532543730137505] km/s
+ V∞_out: [0.00012427989635098945, 0.0010225644178028502, -4.3391551478677264e-5] km/s
+ time of flight: 1.699452506179909e8 seconds
+ arrival date: 2029-09-28T16:01:52.057
+ thrust profile: [0.4175203436809585 -0.05335187051461133 -0.14364454897421305; 0.056329101660784996 0.020815163554076015 -0.06266784537461945; 0.06437247405329966 0.04193071564706014 -0.1270705562016943; 0.0427775045252634 0.03576394540656794 -0.1197437701067069; 0.034276795456696145 0.03400612933137307 -0.12466352666708978; 0.02421176719883837 0.026784592804733463 -0.10674659881027763; 0.027088893861933742 0.036085864206476505 -0.15196615229456617; 0.007822756531310862 0.009916843315324523 -0.039342975714260583; 0.007704062720393978 0.009389003243075105 -0.04755339932280504; 0.004540563500660852 0.007104344821862373 -0.028080236500744114; -0.00830129678393465 0.005792836956040141 -0.00981894831488392; 0.0004425817095557276 0.0012728292479340891 -0.01982485462173328; -0.00287140001323267 0.005054929830559326 -0.01967711999565109; -0.0018327043149238614 -0.002764001046577033 -0.015992558618302292; 0.0021162800435178333 0.0005404395996781284 -0.02211090876552617; -0.0013829070331916682 0.00199693841149263 -0.004820658037757698; 0.010432452876834374 0.011554257985225518 -0.022313289204174608; 0.0032950844599001143 -0.003508413612433801 0.016018930326546176; -0.04492328580443032 0.018565106046359175 -0.090673284295882; -0.0016191062057522739 -0.003131969563316987 0.01610704335834396] %
+
+Mass Used: 108.17045731218468 kg
+Launch C3: 95.79910579568777 km²/s²
+||V∞_in||: 0.0010310232152393292 km/s
diff --git a/archive/ES_0.5717200689016012 b/archive/ES_0.5717200689016012
new file mode 100644
index 0000000..464acc6
--- /dev/null
+++ b/archive/ES_0.5717200689016012
@@ -0,0 +1,22 @@
+archive/ES_0.5717200689016012---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T16:00:54.210
+Launch V∞: [6.492984088179707, -7.171895895544389, 0.19765603707749194] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.6545989959946564e-6, 4.41174728326896e-6, 5.1133045203033455e-6] km/s
+ V∞_out: [6.467114285404544e-6, 4.132060688935844e-6, 1.1987845111094478e-7] km/s
+ time of flight: 1.874957778715429e8 seconds
+ arrival date: 2029-04-06T18:10:31.210
+ thrust profile: [0.5877191334025367 -0.14297379119874137 -0.17468806137974252; 0.08816103511344019 0.023496558323694475 -0.0876080593555472; 0.03912284340521156 0.02176000546830965 -0.06666207547484272; 0.039919808441712216 0.031180555973702416 -0.096848928623824; 0.031651412436884165 0.030425809289428292 -0.1001743269401917; 0.01977254155053444 0.02166851722417693 -0.0765328191895269; 0.025739963605352068 0.030002495052187245 -0.1015509138031223; 0.015477141304454274 0.02103496197584587 -0.08272774021668808; 0.010892505576565235 0.017194860686419327 -0.06333733859305944; 0.007199955588112528 0.014021685456900048 -0.05741401144700678; -0.0043161314824492 0.0006168620571526644 -0.010828438440593625; 0.0017360122504379736 0.001985896134455077 -0.018763478011916142; 1.4376686349115968e-5 -1.4295605670060219e-5 -0.009470782814193045; 0.008381438548057094 -0.0036337141611785173 0.002460936367287973; 0.0014314651753401983 -0.0014445951839059808 -0.008891660570310864; 0.008111859158890263 -0.003784214594937792 0.0064475337554394585; -0.0033893938462308463 0.011209453286132556 0.008707120615722534; -0.014896308435309638 -0.007842105294216787 -0.015788990300442424; -0.019842587183282252 -0.01797463818714596 0.0005236184779653751; -0.01650672147907272 -0.0013203724131935033 -0.01897741332002873] %
+
+Mass Used: 120.80840779843356 kg
+Launch C3: 93.63400101487449 km²/s²
+||V∞_in||: 7.678899076710855e-6 km/s
diff --git a/archive/ES_0.5717769032710559 b/archive/ES_0.5717769032710559
new file mode 100644
index 0000000..fc50522
--- /dev/null
+++ b/archive/ES_0.5717769032710559
@@ -0,0 +1,22 @@
+archive/ES_0.5717769032710559---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T03:57:55.665
+Launch V∞: [7.596799110610423, -6.219104727020684, -0.7030859077673948] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.719152243879913e-7, 2.496276356938102e-7, -7.454641164358249e-7] km/s
+ V∞_out: [-4.5407796127873474e-7, -7.997906711418798e-7, -2.7256097126058018e-8] km/s
+ time of flight: 1.6398836640587628e8 seconds
+ arrival date: 2029-07-17T04:17:21.665
+ thrust profile: [0.27195557374331025 -0.03726643663285344 -0.08617515606411612; 0.12088752166153449 0.055746561006117884 -0.11490538276236596; 0.12885298356969171 0.09402679034876191 -0.19247947033214752; 0.0974261837312086 0.09719739814306544 -0.20521792946097514; 0.05920432428099848 0.07657662397491072 -0.17015300104145775; 0.027642436148769062 0.04816125887722355 -0.1135502034413595; 0.01020676514876706 0.022241296568434304 -0.05948424620678996; 0.009473671337974146 0.017033118744340117 -0.048932128149593516; 0.010232508453144475 0.022917560617882398 -0.06608897450278334; 0.0007764200084027768 0.007688267497125859 -0.026961988298739862; 0.0011884905101890188 0.004816824418530505 -0.017714458330313893; -0.0030332309525891816 -0.0017785284189821833 -0.0032162228161248143; -0.0041064420404548635 -0.0016216888331047764 -0.00015727844380389149; 0.0011431029746552352 -0.0004692750022030226 0.002301657990635529; 0.00389490085551685 0.0015745965124091207 -0.0006898565673737565; 0.00031353537228170675 0.0014605216298835479 -0.00476520110453986; -0.001644760732319102 -0.004065094775416814 0.007500126430899898; 0.0007794638482584481 0.000226610211889314 -0.0025809381441071226; -0.0020908178804766517 -0.004859151781349397 0.0035167693023026624; 0.0010898131609012862 -0.0003335028397592209 -0.005022554944321534] %
+
+Mass Used: 101.92251141267843 kg
+Launch C3: 96.88295012632344 km²/s²
+||V∞_in||: 9.169158545933726e-7 km/s
diff --git a/archive/ES_0.5717843829482296 b/archive/ES_0.5717843829482296
new file mode 100644
index 0000000..0cfe95a
--- /dev/null
+++ b/archive/ES_0.5717843829482296
@@ -0,0 +1,22 @@
+archive/ES_0.5717843829482296---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T19:20:08.438
+Launch V∞: [7.798608786634322, -5.493209012723315, 0.35799316247459856] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005962804241769728, 0.0017025709899539455, 0.0037285676546972295] km/s
+ V∞_out: [0.0039002722981321767, 0.00044615856422866443, -0.001311184424976501] km/s
+ time of flight: 1.8397854549206677e8 seconds
+ arrival date: 2030-03-05T04:29:13.438
+ thrust profile: [0.7987822588809577 -0.019102414395849476 -0.13536704321962498; 0.16115358445689798 0.11139071892727853 -0.11932955956410866; 0.07296009601527806 0.08719932561770947 -0.10218363278652062; 0.09305831708417578 0.13887404439021436 -0.17097801855688052; 0.024856829075575456 0.05442916870065186 -0.07623603032550073; 0.013091623191891184 0.03748914913833479 -0.056406030426371434; 0.00838896256784972 0.031676617008973805 -0.053590035219696804; 0.007459662934676867 0.041707893857470854 -0.07437689437593245; 0.0026564283905780002 0.011963848092793253 -0.02371294947823365; 0.0016901480211748583 0.016653062804961385 -0.030834508175836814; -0.002482579760326117 0.0019253705527039566 -0.0026389030273252737; 0.002618512028753088 -0.0001135970253011763 0.000597184150574623; -0.0030559380610988545 -0.0018446426122864673 -0.0005747287901725683; -0.00024637628030723866 -0.0036769999755678156 0.002390275518447024; -0.00015283276803820255 -0.0010313249647339526 0.0021159165650782357; 0.0017821393653124598 0.0006515954713058929 -0.0034427431007388667; 0.005100295874488728 0.0005733397903143014 -0.0011855302240021156; -0.00041106547647472215 -0.0003622749834255711 -0.0021301701848173912; 0.0016825526589805523 0.002274459810699166 -0.003080469916662801; -0.00485843561130057 0.001042324925380516 -0.008138143710779464] %
+
+Mass Used: 135.5379271215238 kg
+Launch C3: 91.12180336881327 km²/s²
+||V∞_in||: 0.0041420423797619245 km/s
diff --git a/archive/ES_0.5717911696706255 b/archive/ES_0.5717911696706255
new file mode 100644
index 0000000..ef383a8
--- /dev/null
+++ b/archive/ES_0.5717911696706255
@@ -0,0 +1,22 @@
+archive/ES_0.5717911696706255---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:00:42.352
+Launch V∞: [7.359988613631909, -6.646461772571278, -0.5358795437152257] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005187621820523291, 0.008209319505234937, 0.0010176298758354171] km/s
+ V∞_out: [0.007916118077098388, -0.0015984156055390748, 0.0018652942884252717] km/s
+ time of flight: 1.5342884750714546e8 seconds
+ arrival date: 2029-03-19T11:08:09.352
+ thrust profile: [0.24467174355994745 -0.06000480178351071 -0.10287905787409957; 0.057794935144688996 0.012937289537865257 -0.06784805788833868; 0.07192480183296941 0.03391740238126816 -0.13533963591049114; 0.07219169251211037 0.034710292314548384 -0.19168173248511783; 0.028765094776949877 0.019588981588948617 -0.09819615308640936; 0.02592769610644897 0.019846701842150503 -0.10652987324869725; 0.05237491649852183 0.04606009617840882 -0.22982750736519353; 0.03175708906679864 0.03009829749029163 -0.16371696553385626; 0.006163238449310716 0.005699816161302515 -0.043088669686166266; 0.0041813917107606565 0.005533827826211575 -0.03240365547279683; 0.004179742337187819 0.005536053187736568 -0.02907881506842668; 0.004879627870904807 0.0006322991113593955 -0.003744053719778967; -0.002641056597033125 0.0008447152821008546 -0.011611046120630887; -8.372081923411242e-5 9.049981767528378e-5 -0.000604955118861719; 0.000854310048097021 -0.0008911681108310435 -0.003699430405216697; 0.00033596168708401974 -0.0008228261772450125 7.694492086342567e-5; -0.000107798128991517 -0.00020441561939485734 0.00010015292502383189; -0.0067740766699813035 0.00043818433587076847 -0.00755353602617565; 0.001788480980639458 0.0006054372048268689 -0.001805619918683987; -0.004268022979020689 0.003115797809392304 -0.0027013049034828856] %
+
+Mass Used: 91.73605327664154 kg
+Launch C3: 98.63205337241513 km²/s²
+||V∞_in||: 0.00828840222870194 km/s
diff --git a/archive/ES_0.5717962693444983 b/archive/ES_0.5717962693444983
new file mode 100644
index 0000000..1e8d1c1
--- /dev/null
+++ b/archive/ES_0.5717962693444983
@@ -0,0 +1,22 @@
+archive/ES_0.5717962693444983---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T02:01:19.609
+Launch V∞: [7.217621981494347, -6.758969859771191, -0.6130091670589652] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005609109904096301, 0.008200504194518664, 0.000924192221106396] km/s
+ V∞_out: [0.007942264204522672, -0.0014042426175933447, 0.0018341695555309046] km/s
+ time of flight: 1.5103311707009524e8 seconds
+ arrival date: 2029-02-20T03:39:56.609
+ thrust profile: [0.3226731229064832 -0.09253108793320457 -0.14366304332513608; 0.054412492271295 0.009672962106181938 -0.07112163258903605; 0.0886369657702904 0.03442838792805317 -0.18253389749598073; 0.07511441607357955 0.03860165538631547 -0.21321987832172062; 0.057234509198050246 0.03438166125143638 -0.20549792223595761; 0.03424908586202975 0.022725700167703356 -0.15015852294512624; 0.022106359656092322 0.015935072048468942 -0.11421027090117312; 0.01362918760955468 0.011563401744463707 -0.08132145801100625; 0.006835454451451496 0.004964514842582503 -0.04552921683930401; 0.00522011213808703 0.004503886294420096 -0.03469846044102577; 0.0011620799761527915 0.0005159530938949143 -0.009032124717897706; 0.0005219836227403743 0.00028683672144063103 -0.0030208375015101326; 2.8923502959334182e-5 0.0007252615306424292 0.0011402072238447733; 0.0005642885780672991 0.0018104531461734861 6.377838148088552e-5; -0.0011144409366071386 -0.0007984177468360038 0.0004713824900295808; 0.003202772571839909 0.0003663577955059118 -0.00047698164118340343; 0.0006231483391166356 0.0011384392007266109 0.001027533850844046; 0.000995530834691818 -7.006291677582287e-5 0.0007176485579114365; 4.4231652173000714e-5 0.00015392193545807196 -0.0004039835979020881; -0.0011991185598106114 -0.001877651443013161 0.0032563289572484348] %
+
+Mass Used: 94.53344248224084 kg
+Launch C3: 98.1535208719441 km²/s²
+||V∞_in||: 0.008271458241751215 km/s
diff --git a/archive/ES_0.5718409557896349 b/archive/ES_0.5718409557896349
new file mode 100644
index 0000000..2313de1
--- /dev/null
+++ b/archive/ES_0.5718409557896349
@@ -0,0 +1,22 @@
+archive/ES_0.5718409557896349---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T07:21:56.193
+Launch V∞: [7.435816629974283, -5.79267339838994, 0.0011984836760086757] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004076536863218443, -0.00032580544828378214, -0.00026214489203088526] km/s
+ V∞_out: [-5.342004207510438e-5, 0.00037058861209174126, -0.00044665055167672306] km/s
+ time of flight: 1.8749577787061194e8 seconds
+ arrival date: 2030-04-16T09:31:33.193
+ thrust profile: [0.6843626168983197 0.03958614700531103 -0.10414866306230014; 0.2662886657977923 0.20706450294723708 -0.14474108898270183; 0.16239568820641262 0.2275006099082793 -0.1699384287122316; 0.05233429956795594 0.10511225020855197 -0.09571185154845968; 0.04098893427798517 0.11433487283560811 -0.1089328491283928; 0.019200640185354268 0.06882361568277812 -0.0728517496284314; 0.006986402147871146 0.034195932735185515 -0.04026503586667389; 0.006009788904431868 0.04291131486085503 -0.05065089784489313; 0.0003934076797187982 0.0034988780060796216 -0.004270893361700056; 0.003560820966124698 0.03272282405238961 -0.03975212312359403; -0.00021537413212458889 -0.0007694781795039524 0.0007275200936690824; -5.1027174186472305e-5 -0.000815809846853853 0.0001399653150578054; -0.0009218918658660499 -4.928908244784954e-5 -0.00039793435684107884; -2.7633963264080857e-5 0.0004850721009236268 -0.0008691627649469517; -0.0011342723049894304 -0.0005048984060576215 -0.00048733677349791795; 6.349509671393455e-5 4.7994432310831544e-5 -0.0009093092629562887; -0.0005279208649277239 0.0017541382789762732 -0.0008852182062264295; -0.0012790183314062775 -4.1450966153496675e-5 -0.0004970361936130209; -4.0777109369353613e-5 -0.0009967471897851768 -0.0001127734486226619; 0.0016074773222735906 0.0005785178780263903 0.0013758044717791106] %
+
+Mass Used: 148.8769080548591 kg
+Launch C3: 88.8464354913797 km²/s²
+||V∞_in||: 0.0005839954302227624 km/s
diff --git a/archive/ES_0.5718548526512005 b/archive/ES_0.5718548526512005
new file mode 100644
index 0000000..ba60362
--- /dev/null
+++ b/archive/ES_0.5718548526512005
@@ -0,0 +1,22 @@
+archive/ES_0.5718548526512005---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T23:20:07.715
+Launch V∞: [6.370082729754531, -7.632283021554807, -0.42491559146609603] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009680454007002532, 0.005818228374755986, -0.008269555619351084] km/s
+ V∞_out: [0.007102303002894247, 0.005646958002977331, 0.00457534723554265] km/s
+ time of flight: 1.8749577781897807e8 seconds
+ arrival date: 2029-04-14T01:29:44.715
+ thrust profile: [0.26560320789822656 -0.07955256612738804 -0.11820527585854541; 0.019193890034137434 0.003988896037241503 -0.03067233587365715; 0.020244510807793107 0.006803329689751107 -0.050007298245507745; 0.04813162301253438 0.018627443463886346 -0.151830144314164; 0.03284110521324854 0.015096068531846212 -0.13647033466278002; 0.01168512670750576 0.0064464887843587405 -0.062226468334811616; 0.016037924883564886 0.008454805497921707 -0.09440314748390496; 0.031293433572147665 0.01567864297769995 -0.1807495102818963; 0.0025420776255597756 0.0010851777924797527 -0.014027367663581255; 0.000325281859469867 -0.000749009753493097 -0.02443342846376303; 0.00491945913704071 0.001536480627737306 -0.026125932599186517; -0.003842872932356826 -0.0012271632654671993 -0.0016260598319641157; -0.009557378108435136 0.003758029350912879 -0.0035457822572292014; -0.0003838523994869206 -0.010662997191053647 -0.001655868445897297; -0.0008305283235094268 -0.004300945485734622 0.009884048519642127; -0.002743104137359717 0.014034583421077215 -0.004394329647393734; -0.0061408875623675165 -0.000990344964730988 -0.0022385010514382564; 0.004930837364064772 0.0032760384434894468 0.0039017742385580216; 0.007409832471950165 0.006127689744637635 0.009121225928240138; 0.0012667909600039 0.006376125231008923 0.017284793051920475] %
+
+Mass Used: 89.60419513114084 kg
+Launch C3: 99.01025136490168 km²/s²
+||V∞_in||: 0.010157482141760018 km/s
diff --git a/archive/ES_0.5718685759539658 b/archive/ES_0.5718685759539658
new file mode 100644
index 0000000..79fa8c3
--- /dev/null
+++ b/archive/ES_0.5718685759539658
@@ -0,0 +1,22 @@
+archive/ES_0.5718685759539658---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T11:41:23.860
+Launch V∞: [7.955371619014209, -6.268096316799476, -0.07095255751690287] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.636786594358863e-7, -1.4714359473809641e-6, -1.449072342668261e-7] km/s
+ V∞_out: [1.2596856756645596e-7, -6.253792319605932e-7, -1.6460415003826655e-6] km/s
+ time of flight: 1.8464432398503575e8 seconds
+ arrival date: 2030-03-28T13:46:46.860
+ thrust profile: [0.10166871172450725 -0.01600260882595473 -0.05154318679520735; 0.03248386367745523 0.004465410125880248 -0.055289012019537086; 0.025095537039628146 0.0033704545560912314 -0.0707618796433486; 0.02655077623548583 0.0031082120327858773 -0.10364312020089855; 0.02535422848736275 0.001652571760049211 -0.12196712566939315; 0.01647314988407832 -0.00032958682434071476 -0.08812118651273333; 0.02117157941316156 -0.0028286206992277963 -0.12744694555701097; 0.008383205392373938 -0.0017409538152340048 -0.054851504942715665; 0.007131221411446313 -0.0026696337994950724 -0.04295099918189498; 0.0012355520530340047 0.000953284448384123 -0.019065561576455378; 0.0012567231635239801 -0.0006400974247245438 -0.01515553420926731; 0.0022199331455084953 0.0015397538451804393 -0.018026142249514186; 0.00011346961050448003 -0.00024626798682238313 0.0006076674026614173; 0.004694225154728494 -0.0009277566877602945 -0.037506578441731254; -0.0018941987584652374 0.0005730092531914673 -0.010662427298949263; -0.002916503704345934 0.004716162251636978 0.01523323940632515; -0.0011138276424285671 0.0013101111161521223 0.0023774612293267694; -0.0009903025588127328 -0.00020431437888018835 -0.0009562853985905406; -0.0018043797902975592 0.0035465445794826576 -0.0019832863918607746; -0.0013193672921835457 0.0028547868347746004 0.00321294080402253] %
+
+Mass Used: 68.78498603715116 kg
+Launch C3: 102.5820032987101 km²/s²
+||V∞_in||: 1.7648791495283532e-6 km/s
diff --git a/archive/ES_0.5719111226463951 b/archive/ES_0.5719111226463951
new file mode 100644
index 0000000..40a2953
--- /dev/null
+++ b/archive/ES_0.5719111226463951
@@ -0,0 +1,22 @@
+archive/ES_0.5719111226463951---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T07:54:31.954
+Launch V∞: [7.545286092534377, -6.612001597904061, 0.20105133204658965] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.577485365737779e-9, -1.568941651164289e-9, -1.5624982024399797e-9] km/s
+ V∞_out: [8.375287512329257e-11, -7.703761344192468e-11, 2.8120836782610095e-11] km/s
+ time of flight: 1.6945954874874362e8 seconds
+ arrival date: 2029-09-28T16:00:19.954
+ thrust profile: [0.16487664709225772 -0.03424842192334482 -0.07427972404203875; 0.02025744266945422 0.003892506053940822 -0.02455562609427453; 0.0509107203555477 0.014558097201715452 -0.12313290148367534; 0.04076114685311087 0.012282499126832463 -0.1300972127293613; 0.029359679115753108 0.008580841856889305 -0.11271694843989977; 0.026869653369128377 0.007026929433691332 -0.12619843895993788; 0.02950805451344378 0.008826431271686717 -0.15939573655964995; 0.008736482186751184 0.0030515641575425785 -0.059336623431731524; 0.016983330040150492 0.00534562748094422 -0.11303039058510937; 0.005258264595427286 0.002523216078641479 -0.023382920687129216; 0.010722065899140137 -0.0019791244957861427 -0.028443927382112707; 0.001126751310443092 0.0012689646452932676 -0.006533029614616104; -0.006237808943606298 -0.0006423912805299363 -0.005555408535741008; 0.001084905677846393 0.002100806207608435 -0.004759074948566306; -0.00032264526018478505 -2.45375628575217e-5 -0.008357720601202368; -0.0037296908987922246 -0.0059379227557912004 0.0005664055824645188; 0.0020919962986199097 0.0032284823209863724 -0.01563839079165569; 0.0003386801855103634 0.0020463785591661055 -0.004032426135118301; -2.9778574443249748e-5 0.00035412116201729557 -0.0002672412057151492; -0.0004498480861781923 0.0020866082208078895 -0.0008236536302746206] %
+
+Mass Used: 79.86939066331615 kg
+Launch C3: 100.69032898699625 km²/s²
+||V∞_in||: 2.718720032754963e-9 km/s
diff --git a/archive/ES_0.5719513863962368 b/archive/ES_0.5719513863962368
new file mode 100644
index 0000000..4d8d531
--- /dev/null
+++ b/archive/ES_0.5719513863962368
@@ -0,0 +1,22 @@
+archive/ES_0.5719513863962368---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T08:55:33.647
+Launch V∞: [5.610219701052052, -7.812304340685158, 0.13663970208588422] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005481238243470484, -0.0015677951465406007, 0.004623381937758062] km/s
+ V∞_out: [-0.0034186649890266168, -0.0027933133065959114, -0.0021510302850192833] km/s
+ time of flight: 1.646402510692054e8 seconds
+ arrival date: 2028-07-11T22:19:44.647
+ thrust profile: [0.4930997302323832 -0.1838040059964717 -0.15092880203068842; 0.2825264146589713 0.049235892892084125 -0.23055081736878477; 0.16460405401342076 0.07093539841436011 -0.21942274236551187; 0.05523397698820136 0.03297614341537366 -0.10462173820505746; 0.051368746497268004 0.038099595989088575 -0.12131367552456468; 0.041787445987548154 0.03617892797600679 -0.11783195423831662; 0.026962570533578627 0.02426775177544308 -0.08443774539459997; 0.027744837362673386 0.029733199700027555 -0.10272276609485381; 0.013039063270686326 0.015112714987592016 -0.053396487031557915; 0.0012773372423958902 -0.0005221075148892036 -0.005867593994771882; 0.002990292786276419 0.0028810086669195855 -0.019398446891958476; 0.0012608979118062624 0.0002537464643058312 -0.004301708348513172; 0.0013916788601531721 0.003408947085756884 -0.005730362749342884; -0.006143732168826148 0.0035820215183273484 -0.00549000349328634; 0.007906426200721482 0.0002102364383688686 -0.01021466763461417; -0.005191806349654574 0.001899510657932751 -0.0006799466344641876; -0.0004948225057197315 0.006313747831271468 -0.004259692424877376; 0.00433925486903452 -0.0034533929551211267 -0.003349441170255969; 0.0018338685723563808 -0.004155268859303249 0.009568829958750793; 0.0017823211090774254 0.0025408478033024555 -0.0073141106776720005] %
+
+Mass Used: 127.54549888208612 kg
+Launch C3: 92.52533461374686 km²/s²
+||V∞_in||: 0.004912645101238292 km/s
diff --git a/archive/ES_0.5719720394319138 b/archive/ES_0.5719720394319138
new file mode 100644
index 0000000..7c9b54a
--- /dev/null
+++ b/archive/ES_0.5719720394319138
@@ -0,0 +1,22 @@
+archive/ES_0.5719720394319138---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T13:21:48.344
+Launch V∞: [5.741580137075954, -7.496697337329526, 0.20135244385747333] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006087368390878098, 0.004055086368359456, 0.005960953511445709] km/s
+ V∞_out: [-0.0040455658456253095, -0.007003694060417115, 0.0048575336875744226] km/s
+ time of flight: 1.7321147802771682e8 seconds
+ arrival date: 2028-10-19T07:39:46.344
+ thrust profile: [0.796189623759994 -0.2767675735471171 -0.2454042202827125; 0.26079681113737696 0.053074153471302496 -0.23382648943602233; 0.1325658323372308 0.06183816245474841 -0.19894148821457203; 0.07443162203119377 0.04870435193649996 -0.15686138875394684; 0.045741634392286096 0.03710106675487966 -0.12417379065763282; 0.016225101997858253 0.015022537132252161 -0.05124996187552497; 0.014881356832264651 0.015274924625073266 -0.056531719839024795; 0.014150082048817061 0.017053090687927246 -0.06373930711558055; 0.007072871329205694 0.0034071912696756325 -0.016973723893576275; 0.0007272879003721016 0.0012897353940421875 -0.006012017805082794; -0.0028484491961260723 0.0007505174388371295 -0.0027776592455247295; 0.0017010311117214127 0.0009188427522647399 -0.0057451513556849975; 0.0023458198017513327 0.005684278917997605 0.0021158058806884095; -0.0005953105746017094 -2.2244279724059927e-6 0.00012205088963863171; 0.008312518648718821 -0.012275021338482517 -0.008532447299011769; -0.0011813846085749152 -0.0019517896115120433 0.0014635771632859939; 0.01064090409456659 0.02175150896604152 -0.010774715413333195; -0.00019305769935416736 -0.013310376488400902 -0.012507291023605045; -0.004800652543342953 0.004533901047898303 -0.025192680816051555; -0.01257529735326525 -0.006714232508974375 0.009150098254973246] %
+
+Mass Used: 146.92796791018873 kg
+Launch C3: 89.20675624463613 km²/s²
+||V∞_in||: 0.009435716514750399 km/s
diff --git a/archive/ES_0.5719735862530898 b/archive/ES_0.5719735862530898
new file mode 100644
index 0000000..6d407cc
--- /dev/null
+++ b/archive/ES_0.5719735862530898
@@ -0,0 +1,22 @@
+archive/ES_0.5719735862530898---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T14:04:46.208
+Launch V∞: [7.731998000682213, -6.276788345092118, -0.06976830801095361] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0249624822505934e-5, -2.6288534435739583e-5, -7.84711670334987e-5] km/s
+ V∞_out: [-7.633157277751861e-5, -9.57395620485602e-6, 3.239551908232681e-5] km/s
+ time of flight: 1.874957778382454e8 seconds
+ arrival date: 2030-05-01T16:14:23.208
+ thrust profile: [0.47924466430888524 -0.07373672446802078 -0.1705868943998767; 0.017002104179322502 0.0023847532657508587 -0.028535446429999292; 0.031690486461979375 0.0050685072003106586 -0.09041715327576678; 0.025430487598636805 0.0024785644172975155 -0.09938021740724771; 0.02886502821938008 0.000645137045506361 -0.13356885505260757; 0.010277503375170492 -0.0005054806566715809 -0.05473860709591187; 0.014782506452346534 -0.0016871936816196386 -0.08538803473226886; 0.011162115518040791 -0.002192092530092172 -0.0745807490562611; 0.00583570453802806 -0.0017344605761247438 -0.03961164491392596; 0.0055316826637993805 -0.0014318083526092592 -0.0374341461159252; 0.000817877968025533 -0.0002737286002090715 -0.005361191800981361; 0.00010348305732642819 -5.1856734981119355e-5 -0.0005964039178113866; 0.0001567704511143718 -0.00018390275143325847 -0.0002931547440491571; -0.00029920102023330616 0.00012113678128180207 -0.0003424350430361449; -0.0003045919124951551 0.00022682167579174888 -0.00032178123285087697; 0.00017512893172931125 8.782172174634539e-5 -0.00011354442110392214; -0.0005486204326795897 0.00030075804094095796 -0.0006511559710270638; 0.0002545997003922979 1.8437350712000483e-5 0.0002662783754564887; 6.813440719028172e-5 -0.0003839474545196102 0.00033731043910635887; 0.00041669982217978116 7.587602671146936e-5 -0.00036207339131432] %
+
+Mass Used: 88.7132436293673 kg
+Launch C3: 99.18673262844071 km²/s²
+||V∞_in||: 8.338984295092808e-5 km/s
diff --git a/archive/ES_0.5719810476020389 b/archive/ES_0.5719810476020389
new file mode 100644
index 0000000..ba31808
--- /dev/null
+++ b/archive/ES_0.5719810476020389
@@ -0,0 +1,22 @@
+archive/ES_0.5719810476020389---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T20:13:03.863
+Launch V∞: [6.525065140986905, -7.136767804071208, 0.7360020021566075] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.8508189989970265e-6, 0.002104142460051388, -0.0028216000666841023] km/s
+ V∞_out: [0.0026129991517098447, 0.0020821918160860604, 0.0016749903210723375] km/s
+ time of flight: 1.8749577790129983e8 seconds
+ arrival date: 2029-04-04T22:22:40.863
+ thrust profile: [0.5343714338593754 -0.11966475498716471 -0.13272747314170352; 0.16472068911093282 0.05849258305036049 -0.13586295610667098; 0.07116506235475915 0.047753776735825516 -0.10346406361767366; 0.04761857521160555 0.0429118758685913 -0.09967948865601234; 0.027006780435240647 0.031142455507984702 -0.07475436941436424; 0.015507632310101369 0.02081547844133602 -0.05382834823281712; 0.01989412816060831 0.030055978711315004 -0.07908551872739102; 0.03378375489893207 0.04993405408225321 -0.13431968267092556; 0.005520924589824427 0.011343649081804007 -0.03179477811880094; 0.006826949296941922 0.012241564755198851 -0.03981006862777421; 0.0027880744287647028 0.004162225343311677 -0.010973653884690415; 0.0013982496431274214 -0.0008034673499769307 -0.0004944043443766396; -0.0013878566190463528 -0.002805696290276379 -0.0026365737213774852; 0.0007238061686696463 -0.003435309519554167 0.004694776198214177; 0.007465437454533933 -0.006945323431209405 0.0031334296936531246; -0.0045022784042233754 0.0012176396884920073 -0.0057313928181087995; -0.008096539743898163 0.009951499171063645 0.007219819567015668; -0.006379291791411295 -0.004484149568872262 0.0038932647610422947; -0.005209752936178066 -0.009578532475791605 0.0073829794995688815; -0.005543531225523501 0.011278862754595036 0.012641568286554196] %
+
+Mass Used: 118.6767212742966 kg
+Launch C3: 94.05162873052836 km²/s²
+||V∞_in||: 0.00351978085359157 km/s
diff --git a/archive/ES_0.5720300781001788 b/archive/ES_0.5720300781001788
new file mode 100644
index 0000000..8c69e2d
--- /dev/null
+++ b/archive/ES_0.5720300781001788
@@ -0,0 +1,22 @@
+archive/ES_0.5720300781001788---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T22:06:53.456
+Launch V∞: [6.62032954407892, -7.373907102298319, -1.2715439916226858] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006450798576202026, 0.00018546511302698068, -0.004294848836291094] km/s
+ V∞_out: [0.007424909270110604, -7.710505992782547e-5, -0.0022308991282459067] km/s
+ time of flight: 1.8749577781255722e8 seconds
+ arrival date: 2029-04-11T00:16:30.456
+ thrust profile: [0.17531938280712486 -0.06478156363411794 -0.06429874607753755; 0.05936430778934579 0.007823548621226034 -0.0751392561772999; 0.05892514743601479 0.015980686771553836 -0.11956562920301086; 0.04596743987341518 0.016593086167461434 -0.13114174501467912; 0.03997921832557722 0.016390594404909746 -0.1443032029034275; 0.027442505726161064 0.012943277658149052 -0.12513138147407352; 0.015815247621129784 0.009315941218405007 -0.09365488300778237; 0.007468365607301865 0.006282261479372568 -0.05844121341292592; 0.005050945983346682 0.004649403326272138 -0.044468910595337134; 0.002598664752477548 0.0021442377205577964 -0.019974005296094454; 0.0017454485320594574 0.000386405186798879 -0.0031534520264739968; -0.0015225788774537795 2.881106018153158e-5 -0.0013952815544065417; 0.0026029176356155035 -0.002300961280562846 0.000884614654969173; 5.872407254632183e-5 -0.00028070854040945656 0.0024881149251833367; 6.100327393850731e-5 -0.0014778792252927656 -0.0036002680877000276; 0.0019824289234592627 -0.0006973119374910499 -0.00536519614433025; 0.0040793729787115774 -0.0017823962946943157 -0.016739553378556066; -0.002613578457856258 -0.0002035054285688044 -0.003429264824587402; 0.003992267168265775 -0.0014199842801307003 -0.016211783555171385; 0.003668975548275273 -0.0031376158748211294 -0.011578234344262122] %
+
+Mass Used: 85.08454658593291 kg
+Launch C3: 99.82009334816155 km²/s²
+||V∞_in||: 0.007751962726011469 km/s
diff --git a/archive/ES_0.572044968442898 b/archive/ES_0.572044968442898
new file mode 100644
index 0000000..75c5d59
--- /dev/null
+++ b/archive/ES_0.572044968442898
@@ -0,0 +1,22 @@
+archive/ES_0.572044968442898---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T00:33:46.366
+Launch V∞: [6.3853103793595425, -7.849634493080871, -0.16843292670685006] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009506132375437683, 0.0044838704646692935, -0.010831523403370236] km/s
+ V∞_out: [0.010257401556863858, 0.0037269732160131585, 0.010472074527116773] km/s
+ time of flight: 1.874957778421932e8 seconds
+ arrival date: 2029-04-17T02:43:23.366
+ thrust profile: [0.09183540349430014 -0.03270530598672317 -0.044970099261909965; 0.0056462372312271235 0.00018795069229984835 -0.007642075546249784; 0.031372589461856656 0.0021511079662804838 -0.08077522377291772; 0.039663690575460556 0.002473293143561313 -0.1409516067333796; 0.03618498017091683 0.0010785829261640571 -0.16011767348432654; 0.029894363479826803 -0.0004572601879770045 -0.1555409007802868; 0.021442700783465513 -0.0014159048421726584 -0.12647218460553236; 0.007414169328573036 -0.0006351482421681226 -0.047336660905781695; 0.002303122725693952 -0.0022049814908590678 -0.0191150452518033; 0.0008030522480720356 -0.002587705684784832 -0.014950128177694023; -0.0007729247422439606 9.164962337429907e-5 -0.011140481594142968; 0.0007467162839448404 0.0001189314975969605 -0.005960414408819861; -0.004311242136891016 0.003069138601387792 -0.009293056062144051; -0.0008011911717887196 -0.0015312101111326021 -0.003925979962594091; -0.0012527027340112034 -0.0014302071915934015 -0.0012857898529554804; 9.58398132378408e-5 -7.895275076182344e-5 0.00013562006502215103; 0.0016800482822719735 0.0037198014003323445 -0.00655911522878443; 0.0006406181759287142 -0.0018664575291697872 -0.0014161193739770492; 0.0012035056087227295 -0.006124336340525735 -0.002766608879489042; 0.00031865557657544574 -0.0016302306897073952 0.0011376034684747443] %
+
+Mass Used: 69.95143004534339 kg
+Launch C3: 102.41731996652072 km²/s²
+||V∞_in||: 0.015092830957810242 km/s
diff --git a/archive/ES_0.5720858596669577 b/archive/ES_0.5720858596669577
new file mode 100644
index 0000000..a1d1b35
--- /dev/null
+++ b/archive/ES_0.5720858596669577
@@ -0,0 +1,22 @@
+archive/ES_0.5720858596669577---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T21:16:59.251
+Launch V∞: [7.29311179636219, -6.635144365342501, -0.16881904181644772] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00036344301935142993, 0.005583432761672691, -8.43664232979987e-5] km/s
+ V∞_out: [0.005372642428754099, -0.001055511548531081, 0.001153434222118419] km/s
+ time of flight: 1.5441393752051774e8 seconds
+ arrival date: 2029-03-31T02:02:36.251
+ thrust profile: [0.32340184516223675 -0.09069050460718706 -0.1311884982043474; 0.0975432943782753 0.02224301505510153 -0.12006169450276992; 0.0932863200672556 0.03999994417455742 -0.18652248652793563; 0.060616458324135813 0.03469136505446433 -0.17192188325156119; 0.04257196524966482 0.02809862293513941 -0.15245102885444073; 0.02243606639960037 0.016105399989551114 -0.09601145860418737; 0.035144844852236776 0.02896752840917168 -0.17613635848939113; 0.01834689467373966 0.015465893050600952 -0.09636196203640626; 0.008826863560166726 0.006759725787973837 -0.05314760560062884; 0.0028447360733448845 0.0010749634281665855 -0.024096245382003875; 0.004981622334169291 0.004621571277981089 -0.03782328455328263; 0.0023462990501854405 -0.00037402734436898914 -0.008759406384347194; -0.0013703903882286636 -0.0011046648073391794 0.001109469724279068; -0.002650600460122 0.0021948152207737137 0.0020232786358609462; -0.0006151661875753097 -0.005243983416716896 -0.00396515998696133; 0.003105204181059842 0.005966619987655518 0.0026896414195549446; 0.0020166831355841303 -0.0005436141269426826 -0.004844211884327971; 0.0016180788380718248 -0.001164263418254669 0.006936185977897829; -0.0020585274741887383 0.0015624772441335693 -0.0038656556706722824; 0.0015577485349641917 -0.00900579147721613 0.002603546187480432] %
+
+Mass Used: 100.1819679078053 kg
+Launch C3: 97.24312029205349 km²/s²
+||V∞_in||: 0.005595885088689305 km/s
diff --git a/archive/ES_0.5721350444677508 b/archive/ES_0.5721350444677508
new file mode 100644
index 0000000..2173850
--- /dev/null
+++ b/archive/ES_0.5721350444677508
@@ -0,0 +1,22 @@
+archive/ES_0.5721350444677508---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T18:31:19.496
+Launch V∞: [5.629313070447991, -8.03007324219238, -0.1752463623600154] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0015209889517615353, 0.0009545860600164682, -0.0008128363614396478] km/s
+ V∞_out: [0.0010200940726786173, -0.0014229593483856265, 0.0009016880785275188] km/s
+ time of flight: 1.5657468971802688e8 seconds
+ arrival date: 2028-04-10T23:29:28.496
+ thrust profile: [0.36053940131371365 -0.18165772880690606 -0.1580973866235837; 0.09373810078334208 0.0008197044448022569 -0.10613809943130212; 0.10807898219670559 0.022470719977488944 -0.19341277717775016; 0.08743818239835108 0.028503863838256017 -0.21110304502585256; 0.06629407798646454 0.027063999511331455 -0.19897323587036875; 0.05041773126082119 0.023670176973324887 -0.1788989076207397; 0.03864611879392151 0.01974290251749322 -0.15545040282496142; 0.006823322167708407 0.003753520719620662 -0.03188014538696641; 0.004234103130680795 0.0030602743094110766 -0.022931678069149558; 0.0015361162130299304 0.0007299665161334976 -0.009904443022287284; 0.0025922224245572964 0.0024294831393793367 -0.01793820332637712; -0.0037802282365285086 0.0006609709894536854 -0.00022577908390251575; 0.0016358725931995754 0.0007770442070804309 -0.0007259430857673361; 0.0011232417640419652 -0.000717565616169159 0.0006174792866871976; -0.0002250249323632293 0.001952141811187093 -0.0002119849466908736; 0.00045635606143219396 -0.00019376279925970388 0.00011727521086529519; -0.0004972641063761172 0.0002805543345303409 -0.0041777094816329375; -0.001259943745629166 -0.0021777542378099337 -0.002954222059718429; 0.00033461446907459764 0.004488065292089532 -0.0019567333709619153; -0.0007580618499118169 -0.0033998681285686894 0.008723063700504921] %
+
+Mass Used: 106.31282483464474 kg
+Launch C3: 96.20195320761104 km²/s²
+||V∞_in||: 0.0019711278212832532 km/s
diff --git a/archive/ES_0.5721390295842772 b/archive/ES_0.5721390295842772
new file mode 100644
index 0000000..c4125c3
--- /dev/null
+++ b/archive/ES_0.5721390295842772
@@ -0,0 +1,22 @@
+archive/ES_0.5721390295842772---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T12:02:22.323
+Launch V∞: [5.712761269279577, -8.045696310891504, -0.2912427700290003] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.0727843357864863e-6, 1.5657926810817841e-6, 2.5705336646538496e-6] km/s
+ V∞_out: [-1.8957707789465672e-6, 2.535099204498107e-6, -2.9106437222643096e-6] km/s
+ time of flight: 1.5794571582816222e8 seconds
+ arrival date: 2028-04-27T13:50:57.323
+ thrust profile: [0.278785070589999 -0.1327968719825548 -0.12155135202948479; 0.09932666067879059 0.003971592472226658 -0.12071484482489198; 0.06851177554212605 0.016831723918619316 -0.13314767967594676; 0.059251972254323576 0.022417101686602103 -0.1579836519514733; 0.05050600819799459 0.02348337542397075 -0.1634601103465849; 0.03873688672649283 0.021429613542799857 -0.15353139945340472; 0.03541196841637396 0.021167157647409927 -0.15636274170298117; 0.011675707665003013 0.00669848647388086 -0.05583682709648298; 0.025373279841644315 0.015801605785722997 -0.12526273099842664; 0.009195608031674967 0.006309811232044714 -0.05458794350216626; 0.0009670168315456574 -2.5961318000846153e-5 -0.009301076626165935; 0.00036683008967945273 0.0002648646062807453 -0.003773520592542113; 0.0011451390607921975 0.0007546997192774789 -0.0003430678697443899; 0.0003490229900199002 0.0011806888965702148 -0.001042054887357714; 0.0007476708048907686 0.0018934786986508786 -0.001900696192588098; -0.0004519720916528556 -0.00039656064552657383 -0.0009369226003519417; -0.000545114399579148 0.002131779930601399 -0.00023892788679878924; -0.0015124898938399314 -0.0010436401319026682 -0.00015345944175849122; 0.0003294830886463639 -0.0002555866272111523 -0.00035874413690102636; 0.0018770296495686286 0.003958591990602888 0.0006323333745356212] %
+
+Mass Used: 99.01565986017613 kg
+Launch C3: 97.45369279796812 km²/s²
+||V∞_in||: 4.3013199852490435e-6 km/s
diff --git a/archive/ES_0.572176693414322 b/archive/ES_0.572176693414322
new file mode 100644
index 0000000..1208cb8
--- /dev/null
+++ b/archive/ES_0.572176693414322
@@ -0,0 +1,22 @@
+archive/ES_0.572176693414322---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T13:13:26.480
+Launch V∞: [5.871695738759417, -7.3363781432633655, 0.17289265302576137] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.233025742552207e-7, 3.861887604721031e-6, -2.3618844263228605e-7] km/s
+ V∞_out: [1.3648621549931872e-6, -3.167492548179799e-6, 1.8336865102495292e-6] km/s
+ time of flight: 1.812870394267488e8 seconds
+ arrival date: 2029-01-20T18:44:05.480
+ thrust profile: [0.8001156334604013 -0.20777269692518094 -0.20047259397095613; 0.3538643402297126 0.11549035621614115 -0.26845593933920153; 0.09892925604703254 0.06457628593747454 -0.130545437156775; 0.08291554556791458 0.07390477841232457 -0.15166800789246465; 0.04023653793154724 0.046219267287429776 -0.09574489858970801; 0.0270078802169207 0.035909266408049825 -0.07827168746456022; 0.011911855540964087 0.02035389590394085 -0.0433366065023178; 0.01025263809335804 0.017615569983054954 -0.041375288453168846; 0.001600286212807116 0.003253429718400532 -0.018075056474825577; 0.003716807193330066 0.007923511025324766 -0.01951342253126807; 0.0015051626336152991 0.0027063036104760753 -0.005813063773075307; -0.00150029685699927 0.0022195071880768053 -0.0011531479612417444; -0.007915508821011018 -0.005675849192157498 -0.006270240658500297; -0.0019044148621014832 -0.0011897604013711266 -0.002050162165116994; 0.001694977258255308 0.004703360193259956 0.0006919999271260237; 0.005463292358469985 -0.009654551348996893 -0.0053453955065073805; -0.006718418787491943 0.00779480591443266 0.01073244211721558; 0.012433324795403511 -0.006666519752025074 -0.020800609305418737; 0.0005514225291487075 -0.006027441258808294 -0.0017955506505018504; 0.006502052133248334 0.0062039017048698165 -6.697104382475506e-5] %
+
+Mass Used: 152.28611827261102 kg
+Launch C3: 88.32914697898822 km²/s²
+||V∞_in||: 3.90433175282956e-6 km/s
diff --git a/archive/ES_0.5721831216201186 b/archive/ES_0.5721831216201186
new file mode 100644
index 0000000..ea18bcf
--- /dev/null
+++ b/archive/ES_0.5721831216201186
@@ -0,0 +1,22 @@
+archive/ES_0.5721831216201186---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T03:41:30.682
+Launch V∞: [5.765337358028782, -7.940301724821788, 0.06858179939774878] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.568866489419777e-5, 1.9420164549205747e-5, 1.9310615284363108e-5] km/s
+ V∞_out: [2.6939017809933206e-5, 1.640108413396326e-5, 7.746270401501375e-7] km/s
+ time of flight: 1.5927700873336244e8 seconds
+ arrival date: 2028-05-11T15:18:18.682
+ thrust profile: [0.3024179580877918 -0.14144017371814713 -0.12385945941795143; 0.1378169437456686 0.006728861428143894 -0.14464005836222682; 0.10842042076263703 0.028383109717489904 -0.18178366275749944; 0.09527061184359926 0.03752148999401427 -0.21539256132426707; 0.058257035296336745 0.028264806016112195 -0.16400215788878816; 0.033909246297672745 0.018169424265296195 -0.11095143853330436; 0.046501040683982524 0.029090605967911184 -0.17787527680504286; 0.016621757316087206 0.011237132385002352 -0.06996005559085795; 0.0027935114023102054 0.0016068416566839875 -0.013704048514939268; 0.004144556330469948 0.00286796643835021 -0.02184034781218429; -0.00037529376268705984 0.0023737436908889903 -0.014435335545648346; 0.0026733006219508424 0.0015170395555070795 -0.011050850821561495; 2.191183519139147e-5 -0.0035625818596719296 0.00030176758628128967; 0.0005173157843175362 -0.0011511948937729883 -0.0052190893733872; 0.001537298079951669 0.0017924427984565494 -0.002002314240481683; 0.0006130655081910357 0.006785084048940939 -0.0032373160268570197; 0.0023588305188366864 0.0024450685793092663 -0.0030596749597095445; 0.0014688903357388298 -0.002749263165590961 -0.0006191852649105868; -0.0005010289099300042 0.011572958282687538 -0.010270431285474693; -0.0019628395755044844 0.0018606443435228255 0.000265313120926711] %
+
+Mass Used: 105.84241807839544 kg
+Launch C3: 96.29220979629879 km²/s²
+||V∞_in||: 3.1562269562585944e-5 km/s
diff --git a/archive/ES_0.5721850063128554 b/archive/ES_0.5721850063128554
new file mode 100644
index 0000000..c731fcc
--- /dev/null
+++ b/archive/ES_0.5721850063128554
@@ -0,0 +1,22 @@
+archive/ES_0.5721850063128554---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T17:28:48.187
+Launch V∞: [6.432723692655415, -7.575053915643403, 0.15517086969052568] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0048726804903771554, 0.003127920696546224, 0.004798592548994214] km/s
+ V∞_out: [-0.00321260140376163, -0.005475796444898757, 0.004030350199637351] km/s
+ time of flight: 1.775770177850376e8 seconds
+ arrival date: 2028-12-14T00:25:45.187
+ thrust profile: [0.15123252701888984 -0.059954275571247335 -0.0630845889348739; 0.06517062901547976 0.005801561894094337 -0.07551938564370568; 0.056823174779953044 0.015098065199276992 -0.11191401163519711; 0.048020395593135604 0.0173985570791309 -0.1312339416196121; 0.0402706953867235 0.01703953409555199 -0.13878945248293223; 0.03148765271318866 0.014481776384443975 -0.12939268609779117; 0.024789519889463797 0.011983473825779942 -0.1168414405269985; 0.01798855620448682 0.008886368592291824 -0.09478243713635366; 0.011998659486698968 0.005932419248010111 -0.0686110305713436; 0.006764406541760421 0.0032208180949122706 -0.040466552210593705; 0.0026186537528680286 0.00028449742927478053 -0.009340127336982466; -0.005358833083276163 0.001304442565390643 -0.00513753553973869; 0.003966918118919961 -0.0005523597147066011 -0.0015553517534841257; 0.005081552227606272 0.00030903321094887383 -0.0033037266114709124; -0.002421603226838702 0.0010441753635267066 0.00022202208562321652; -0.004492980517952088 -0.0006972565133792289 0.010673757600921636; -0.0024195578358872146 0.0026373309300109036 0.019278891802902702; -0.029970945387626687 0.0025629155139128496 0.010260715728895576; 0.004878517895698285 -0.02042715507195807 -0.01590776456072851; -0.01972748150921028 -0.008453700786684762 -0.006807538002153767] %
+
+Mass Used: 91.30069277475877 kg
+Launch C3: 98.78545392975529 km²/s²
+||V∞_in||: 0.007520199033034109 km/s
diff --git a/archive/ES_0.5722260918659717 b/archive/ES_0.5722260918659717
new file mode 100644
index 0000000..5822ead
--- /dev/null
+++ b/archive/ES_0.5722260918659717
@@ -0,0 +1,22 @@
+archive/ES_0.5722260918659717---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T20:53:49.783
+Launch V∞: [6.483742208735468, -7.376382357154615, 0.026633501853375607] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.065887763291213e-7, 0.000169120559523567, -0.00010246369206712065] km/s
+ V∞_out: [-9.421581735675477e-5, -0.0001697173562827695, 3.411995329293851e-5] km/s
+ time of flight: 1.8476879838133124e8 seconds
+ arrival date: 2029-03-07T09:33:47.783
+ thrust profile: [0.3317757882867481 -0.08742278607389777 -0.11266512459967307; 0.05396952729416926 0.015353722192758303 -0.05823319370415226; 0.06725055317818836 0.03686028195017193 -0.11835540284736024; 0.04380560449503716 0.0327723927681535 -0.10916640285463189; 0.05509164929272785 0.04985784721890868 -0.17077147558055858; 0.030842844063408474 0.03250057538457453 -0.1199928099094051; 0.007129938581510352 0.011040284332360472 -0.04612298765062194; 0.004418709279614309 0.00710927757568007 -0.03445154247819217; 0.01778395402922857 0.024515496399804704 -0.10570243676036294; 0.008119468259820165 0.009205005023882976 -0.04228870876206575; 0.0009455067433678495 0.0011049578806048045 -0.0065262988831272; -0.00485499764232693 -0.002708757946068235 -0.0037930046586778384; 0.01847557721673204 0.001573793714157608 0.007853259716063028; 0.0005027977275157662 0.001728157021416917 -0.007263507970825747; -0.002202247834841863 -0.0003554501229188175 0.0027323392658324007; 0.006163724839356371 0.0104075911347386 -0.00665952729554513; -0.012128735872144797 -0.02423547512028097 0.008476289476932818; -0.01146823849484239 -0.010453389206265398 -0.003568584773260006; -0.002355864224989661 -0.00523220427678208 -0.0177286886615009; -0.0013555372009282484 0.02135180662304421 -0.04357343106011266] %
+
+Mass Used: 104.9683793753793 kg
+Launch C3: 96.45063905170075 km²/s²
+||V∞_in||: 0.0001977392942178625 km/s
diff --git a/archive/ES_0.572243753532643 b/archive/ES_0.572243753532643
new file mode 100644
index 0000000..dec2d7c
--- /dev/null
+++ b/archive/ES_0.572243753532643
@@ -0,0 +1,22 @@
+archive/ES_0.572243753532643---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T22:52:25.777
+Launch V∞: [5.957564802857694, -7.865132282469438, -0.2384185645721689] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.592872465185433e-5, -8.057551006481584e-5, 1.6967144234914687e-6] km/s
+ V∞_out: [2.158258222623392e-5, -5.224582340306055e-7, -0.00010860196207020338] km/s
+ time of flight: 1.6387131325133145e8 seconds
+ arrival date: 2028-07-04T14:40:58.777
+ thrust profile: [0.19622007557764018 -0.08600195076497523 -0.08287306290037962; 0.13493590788087614 0.011681977576520057 -0.14912827184266642; 0.11109476787814081 0.03391941865022873 -0.19731620880153578; 0.06706272203757811 0.02948026053232805 -0.16335874653193588; 0.06667198699395337 0.03640100922738379 -0.20222559303022702; 0.03989135896778924 0.024882161048442954 -0.14542190137170874; 0.030863078098813154 0.021284694728827592 -0.1296409367354645; 0.006949702321936564 0.004399106104535355 -0.03224175238493248; 0.005448519225932253 0.004358918953909762 -0.030249430397504436; 0.001125103312688633 -1.1074830241716328e-5 -0.007395870973736935; -0.005234650321019758 -0.0035349420122142102 -0.007919111307947327; 0.008034689460974728 -0.0022518517588439074 -0.007116866198431493; 0.0080267669899542 0.0010454935269095839 -0.005590406513288284; 0.0022565511959329577 0.002407238862894085 -0.004060142776160997; -0.00030718653236561056 0.0002534393375023716 0.0011009791837805838; 0.009174611650816206 0.010171689450518231 0.007149276993684786; -0.010150037104850266 0.007390661944002944 -0.020276098415018533; 0.0007491379157404427 0.0010527144156110338 0.0016733299347358784; -0.0035561511278727584 0.003306465923091855 0.011117638250731856; -0.003523189809181867 -0.0017324263613121074 -0.01714010184832046] %
+
+Mass Used: 99.39430137935778 kg
+Launch C3: 97.4097276129244 km²/s²
+||V∞_in||: 0.00011072697453329625 km/s
diff --git a/archive/ES_0.5722700475592617 b/archive/ES_0.5722700475592617
new file mode 100644
index 0000000..8fa9f62
--- /dev/null
+++ b/archive/ES_0.5722700475592617
@@ -0,0 +1,22 @@
+archive/ES_0.5722700475592617---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T05:59:31.254
+Launch V∞: [5.630757838062387, -8.100653469908263, -0.16072036474676415] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.153377933849641e-6, -0.0011738979448635495, 0.0005246833801602472] km/s
+ V∞_out: [0.0010454753371057475, 0.0005770055271068504, -0.0004798248829050926] km/s
+ time of flight: 1.54840530581462e8 seconds
+ arrival date: 2028-03-21T09:15:01.254
+ thrust profile: [0.20110201873344924 -0.0981927535956691 -0.08760816486058202; 0.16830438742756235 0.006156072207056421 -0.17846168170014653; 0.14467785650899978 0.036846441477511926 -0.24066562730804783; 0.08955382304101543 0.034353289797929 -0.2022756790466489; 0.05657413429601029 0.02685638439290578 -0.15892372802711957; 0.056894303470089135 0.031400047176761564 -0.1882760306310468; 0.03644325545066179 0.022335796782528897 -0.13766390185181188; 0.018560895088447604 0.011790288182827565 -0.07756515011518628; 0.0013671318973465269 0.0011368258416697813 -0.007032779316125845; 0.0005310845592123674 0.00038659502004900433 -0.0026531499698405304; 0.0006376911529984267 -0.00023995730714474915 -0.0007332511070356407; 0.00010668870427031727 6.677118450973169e-5 -0.0006107236886075422; 0.0006264311090744665 -0.000621845858005778 -0.00013882436225078575; -7.86948364003468e-5 -0.0024722143671563218 -0.0030640354717017242; 0.0024093945249636832 -0.00016920470598726035 -0.003027444062019131; -0.0018932257404992569 0.0012959239222692532 -0.0021414341034286834; 0.002345838262808329 -0.0011715966258025814 -0.0012305836317705533; 0.0008313053104732421 0.0012430681827545985 -0.0007975594775182944; 0.000497333480913817 0.0007101148049972787 -0.00213710735840144; -0.00011661477046388311 -5.8770321031453606e-5 -6.362782899897745e-5] %
+
+Mass Used: 99.76258836699299 kg
+Launch C3: 97.35185150608211 km²/s²
+||V∞_in||: 0.0012858222964949866 km/s
diff --git a/archive/ES_0.5722890297868093 b/archive/ES_0.5722890297868093
new file mode 100644
index 0000000..4aeef10
--- /dev/null
+++ b/archive/ES_0.5722890297868093
@@ -0,0 +1,22 @@
+archive/ES_0.5722890297868093---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T19:28:09.264
+Launch V∞: [6.124664780898585, -7.64873345947042, 0.02653108575929564] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5083496890261104e-9, 1.0606057261952863e-9, 7.342066017289385e-9] km/s
+ V∞_out: [-3.069344722471453e-9, -6.645594876138725e-9, -3.4144024650973722e-9] km/s
+ time of flight: 1.7036932101602757e8 seconds
+ arrival date: 2028-09-17T16:16:50.264
+ thrust profile: [0.34453745917498285 -0.12311372549335331 -0.1249784020962181; 0.08813154327202773 0.015448144435655852 -0.09105513442925449; 0.08753283233269811 0.03712126611820054 -0.1450313850758141; 0.06786607862692125 0.04019586578034436 -0.15253092644694408; 0.04235024335755713 0.031021102657822822 -0.12312564991012118; 0.04354477909713937 0.035372059898209324 -0.1471905871505642; 0.02642454024500363 0.025190491701316025 -0.10593357001453667; 0.01848347355126091 0.01878772095163183 -0.0859061031906245; 0.015536393451312306 0.015132053198117728 -0.07189350208510457; 0.0033521394069331934 0.0039037309914964533 -0.01910735569985214; -0.0014865606573033793 -0.0010189296449188657 -0.005676444895920514; 0.005712927572087447 0.007883786696756712 -0.04292595496678932; 0.0033010702602444047 0.00848920687858771 -0.0019847758426941855; 0.009265323791947671 -0.0010397081904593365 -0.0018553224598175226; 0.0007922736063004503 -0.002456241782576902 9.946024367731162e-5; -0.0011183808062462002 -0.003332344268438615 0.0022487865455108843; 0.006158547689188342 0.006420422325271484 0.005000596850555951; 0.003312230196495792 0.0010467322165760374 -0.0008973036871577872; -0.023895457144144355 -0.00713346495786569 0.0060506468542165116; 0.0006505448174596732 0.016642724407722298 0.01618499858016212] %
+
+Mass Used: 107.5810157709493 kg
+Launch C3: 96.01534611091341 km²/s²
+||V∞_in||: 7.570068473472284e-9 km/s
diff --git a/archive/ES_0.5723277491634279 b/archive/ES_0.5723277491634279
new file mode 100644
index 0000000..cb970b7
--- /dev/null
+++ b/archive/ES_0.5723277491634279
@@ -0,0 +1,22 @@
+archive/ES_0.5723277491634279---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T04:24:14.450
+Launch V∞: [6.472175068701023, -7.833207618055872, -0.7751767467077167] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.03676184205641259, 0.0004718921118603517, -0.024922486404999646] km/s
+ V∞_out: [0.04356189352537024, -0.0003343529079786507, -0.008734977779217407] km/s
+ time of flight: 1.8749577779944777e8 seconds
+ arrival date: 2029-04-17T06:33:51.450
+ thrust profile: [0.016885780171350066 -0.0067129599681482206 -0.009571219736330162; 0.006523850833435025 -0.00040286158107170124 -0.011198529925583393; 0.018682825982261335 -0.00020710952630447694 -0.05388843311528177; 0.02746283350796213 -0.0011856923657137589 -0.10958765626226766; 0.03181683399361591 -0.0030883749959696822 -0.1575263226590446; 0.02513852355805022 -0.004160395423749811 -0.14654899768888174; 0.011019436038962011 -0.002640525213381627 -0.07326087518515943; 0.005753395204826766 -0.0016525636454364362 -0.04266377784056436; 0.015378056819274732 -0.0055386456530071414 -0.12039032524438373; 0.007993684635036089 -0.0033805629142291335 -0.06621874784478683; 0.0003691251027550114 -0.0001392388646616985 -0.003729293354922644; 4.261639506652819e-5 0.00024461553283484336 -0.0007447860950587787; 0.0001404732309678306 -0.0001771891694831754 -0.0008356481351236054; 0.00021423876073031794 -0.0002713109985060446 -0.0013807020133320398; -5.830749099258037e-5 -0.00024179724182852682 -0.000449834948152073; -0.00037783642336311257 -3.625629627561431e-5 -0.0004142106077625321; -0.0008434739785645361 0.00023043177892007508 0.0001520760022581815; -0.00011977873829396911 -2.0302000743887302e-5 -9.764171860534427e-6; -0.0007472557383783697 -0.00029209260845992365 0.0008305544951702629; -0.0003941998510674784 0.00043333940355022555 0.0007228189922758369] %
+
+Mass Used: 61.92934496329917 kg
+Launch C3: 103.84909069612 km²/s²
+||V∞_in||: 0.04441605613011193 km/s
diff --git a/archive/ES_0.5723366151073054 b/archive/ES_0.5723366151073054
new file mode 100644
index 0000000..cd938f9
--- /dev/null
+++ b/archive/ES_0.5723366151073054
@@ -0,0 +1,22 @@
+archive/ES_0.5723366151073054---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T20:26:07.915
+Launch V∞: [5.9096967429538285, -8.161940061174912, -0.48599353831016917] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4670774161462352e-5, -1.966032748692803e-5, -3.2233145570304896e-5] km/s
+ V∞_out: [-3.8692926917530356e-5, -2.3141662506784652e-5, -1.0271755771428181e-6] km/s
+ time of flight: 1.7066027245321402e8 seconds
+ arrival date: 2028-09-29T02:03:59.915
+ thrust profile: [0.06300746723067177 -0.028410165093739028 -0.03243985795196615; 0.04356573503075619 -0.0012309760102896105 -0.062139273235591215; 0.043541281356945016 0.0037420031023188134 -0.10124994503884926; 0.04942957612671189 0.007777425950496436 -0.15953732807658838; 0.03295523474896524 0.00514353966530402 -0.13349479104374878; 0.02420291141830802 0.003269258791376758 -0.11314854255846164; 0.028088225904721122 0.005222622717551752 -0.1564115430180364; 0.030868756760686827 0.005431652164139768 -0.18441229872547235; 0.006496987209478984 0.0007633748998489893 -0.04336484252253107; 0.0009693246162404387 9.511547673091322e-5 -0.007178225508589087; 0.0002029894718061879 1.346775868467626e-5 -0.0018179698731309304; 0.0002495137844821672 3.728344209196377e-5 -0.0011813499683923996; 0.0006094403895596609 -0.00033409713184617894 -0.0012001666877313548; -8.01304630498447e-7 6.490147196412035e-5 -0.00012818458169167914; 0.0002862286680427327 0.00018567435796301365 -0.00034568518313966867; -0.00024444905123428037 -0.00011880084037353499 -0.00017197132536671852; -7.155913215652808e-5 -0.00021917629475078266 0.00028654982723917916; 0.00020375993263604676 -0.00010628545274712285 0.0006571364546368952; 0.0009450893046735992 -0.0012317281369566054 0.00031058923951939613; 0.0005989171822820124 -0.0007397849186200387 0.0003150151171609402] %
+
+Mass Used: 74.02122085336305 kg
+Launch C3: 101.77797087517025 km²/s²
+||V∞_in||: 4.510156591489482e-5 km/s
diff --git a/archive/ES_0.5723440680990837 b/archive/ES_0.5723440680990837
new file mode 100644
index 0000000..43a2e78
--- /dev/null
+++ b/archive/ES_0.5723440680990837
@@ -0,0 +1,22 @@
+archive/ES_0.5723440680990837---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T22:16:58.943
+Launch V∞: [7.3037121366684365, -5.9369013031619415, 0.1916613032854126] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003657597920505884, -0.0036634988953925403, -0.00021329675211282956] km/s
+ V∞_out: [0.0037017102040037856, 0.001734588324588142, -0.0031761189500672587] km/s
+ time of flight: 1.7163387984571588e8 seconds
+ arrival date: 2029-10-11T10:21:37.943
+ thrust profile: [0.9924258615207355 -0.06837165351180623 -0.19253142592358125; 0.1854173925927752 0.1051432612031945 -0.1414963059871853; 0.09060671311322006 0.08576429782425792 -0.12003062622843823; 0.07781246717182072 0.10206799179711244 -0.15220082073742117; 0.07365194578507141 0.12577662625757213 -0.19314124022926932; 0.029110379209866692 0.05923116722201741 -0.10324930585801406; 0.021791556880870873 0.05432213046691929 -0.09667425387924453; 0.000615169878767931 0.0027710193963137813 -0.005990757627888258; 0.0044178307137627175 0.013516144547951995 -0.0269195764650987; 0.0006359003792970254 0.0015889841953957518 -0.003013765425925767; 0.00038273089661294997 0.00012223587375700186 0.0002657572043034764; -0.0010671740416297315 0.0006969888128242525 0.0012455111202682085; 0.001796971589259933 -0.0007097833510434598 -0.0010879147660047463; -0.00023550154867549942 0.0021111264267079 -0.0025520259629292514; 0.004905444232678594 -0.0022449215046221774 0.0006713634510161832; 0.0032059254556995763 -0.004262464656420258 -0.0024640365765256937; 0.001968010250063647 0.008294179529220172 0.0014673556559308184; -0.00018968738711381725 -0.0007314651438128058 0.0034570669395985036; 0.006331126712558647 0.005829146180315026 -0.009464408556220447; -0.0003935129908261336 0.0013370813188659356 -0.0016775388865115076] %
+
+Mass Used: 150.73958378404268 kg
+Launch C3: 88.62774211398084 km²/s²
+||V∞_in||: 0.005181191195959981 km/s
diff --git a/archive/ES_0.5723503576939876 b/archive/ES_0.5723503576939876
new file mode 100644
index 0000000..f6b7e1e
--- /dev/null
+++ b/archive/ES_0.5723503576939876
@@ -0,0 +1,22 @@
+archive/ES_0.5723503576939876---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T15:44:18.322
+Launch V∞: [5.643040841337317, -8.031103306825504, -0.2556441776099774] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.898841969853168e-8, 4.1870419402312256e-8, 3.1027601587899205e-8] km/s
+ V∞_out: [-8.862847839799164e-9, 3.3861868563892485e-8, -4.919604860720584e-8] km/s
+ time of flight: 1.5724927523591447e8 seconds
+ arrival date: 2028-04-18T16:05:33.322
+ thrust profile: [0.36021278303161214 -0.16757185915685124 -0.14639343157489487; 0.07593450948614767 0.005837349520651487 -0.0806890202870424; 0.07623865793501933 0.023440790611835176 -0.12619527566912545; 0.07432965590942964 0.03418309240048105 -0.16334155317990828; 0.056887729981679236 0.032261119679922734 -0.1553811178927535; 0.04358683483459343 0.028293107051684713 -0.14090517824566565; 0.046712219358913 0.034452888345170025 -0.17001393734768938; 0.039896808510990325 0.031315068844489674 -0.16407658988435145; 0.013565514186912772 0.011842320652241386 -0.06453680597557178; 0.009804299225543534 0.008628291172987178 -0.04950540408280016; 0.001240480988726205 0.000874475872846778 -0.001831149597827653; 0.00025552807562679024 0.00010079349215834344 -0.0010606501418948403; 0.0013148887427002162 0.000962184349356431 -0.0074667168892750295; 7.131101274747257e-5 -0.000862584740988047 -0.0024952796993688905; 0.002469272469108643 -0.0004394787636290394 -0.0001113009990314853; 0.0003150047449729899 -0.0003268724388529477 -0.003234061263748757; 0.0011811072735770723 0.0004728672958164269 -0.0025406947227155515; -0.0005701070719454286 -0.0005940253177783308 -0.002016906384918779; 0.0013201166462891403 0.001442279048018263 -0.0007494284478235423; -0.00028174695174960646 0.0012961613703335484 -0.00037701563174753045] %
+
+Mass Used: 105.36275943285818 kg
+Launch C3: 96.4078842074504 km²/s²
+||V∞_in||: 5.96336528970107e-8 km/s
diff --git a/archive/ES_0.5724065547043291 b/archive/ES_0.5724065547043291
new file mode 100644
index 0000000..537788a
--- /dev/null
+++ b/archive/ES_0.5724065547043291
@@ -0,0 +1,22 @@
+archive/ES_0.5724065547043291---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T06:21:10.234
+Launch V∞: [5.7810029971329975, -7.774356145850278, -0.16513892193940113] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007406961889711927, -0.00512015355903117, -0.00559371093807186] km/s
+ V∞_out: [0.00455430848440495, 0.008031343801119603, -0.005209943168005417] km/s
+ time of flight: 1.669314652483067e8 seconds
+ arrival date: 2028-08-08T08:12:15.234
+ thrust profile: [0.38660759995659566 -0.15977799717750826 -0.12280868996695336; 0.29425285050191496 0.040771969530665204 -0.2519456262519602; 0.11612544067362685 0.05620774525359037 -0.1831994040883844; 0.03986334799297075 0.026809003970237538 -0.08787449496363535; 0.02704517929212503 0.019035988153660942 -0.07145783261147312; 0.023952408081414762 0.022094252368741945 -0.07779735743108175; 0.03064545246072973 0.033358682836632535 -0.12173555966869432; 0.05129239911336877 0.05638295386991685 -0.20482469349819935; 0.004776419421351256 0.005862812298595919 -0.023448614106131322; 0.006148471906542253 0.0070304666919080135 -0.0251439127013986; 0.0016669791344940243 0.005404362546724238 -0.03303831090346515; 0.0020608035610223305 -0.002327315041281511 0.0019534869856454528; 0.0008837812369689672 -0.0046911222472510485 0.006689464382458225; 0.0007954844735517796 0.0028418185759065684 0.00362991897489245; 0.0027794753891226026 0.0019218980259437554 -0.0057041374053131266; -0.0032247553290735784 -0.0012963935381312595 0.0018816661179925794; 0.0037361052618242654 0.002640867532321578 0.005530818324068326; -0.007982078059950944 -0.0027505761948841074 0.005443766628134471; 0.000964659564678864 -0.001625356124651523 -0.0027283167610615594; 0.010477494001406271 0.00035962149885648473 0.008239720026372781] %
+
+Mass Used: 120.12834716135058 kg
+Launch C3: 93.88787999892 km²/s²
+||V∞_in||: 0.010600408433754295 km/s
diff --git a/archive/ES_0.5724683069072967 b/archive/ES_0.5724683069072967
new file mode 100644
index 0000000..9827a46
--- /dev/null
+++ b/archive/ES_0.5724683069072967
@@ -0,0 +1,22 @@
+archive/ES_0.5724683069072967---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:42:55.828
+Launch V∞: [7.306406211739927, -6.561118850758313, -0.35779744089379406] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.381754624224662e-6, 9.679884954310475e-6, 4.868683769345281e-6] km/s
+ V∞_out: [7.5130619779294574e-6, -7.465034329516852e-6, -4.079034514290414e-6] km/s
+ time of flight: 1.5532785552856082e8 seconds
+ arrival date: 2029-04-10T06:20:30.828
+ thrust profile: [0.4182355088766311 -0.09977139474472323 -0.1700902431598026; 0.06503893563506083 0.016398441325221558 -0.08139003333430901; 0.0713588183412268 0.03302942665924265 -0.14384349743382574; 0.06741296072902268 0.04259370938426561 -0.19751673645646006; 0.042478987704003074 0.030334587970708964 -0.15558183109091453; 0.034508742827909646 0.028492261508344923 -0.15216263910450809; 0.02050408727751801 0.0171945546135689 -0.10496571930830305; 0.011228252360996607 0.009835292883303596 -0.0626470909864658; 0.01253068643781853 0.011994741468325035 -0.08494286949793665; 0.013881568079306478 0.012562099873656824 -0.08281476325166749; 0.001005004047640207 0.0006503663766164082 -0.005555916416513615; 0.0030097667272722195 -0.0004896633625526817 0.0010260748765625442; 0.0009495437406969493 -3.822112237825094e-5 -0.0019637257406239076; -0.002937324265002149 -0.0024335677460840307 0.003593280873360173; -0.000831212834213953 -0.01322174935379328 -0.003137610896302106; 0.001112661070946921 0.006214754247202118 -0.0060932710201136095; 0.011671602845707969 0.00036812403330804285 0.004585093612478341; -0.0023318702236214896 0.013902895369036024 -0.002233417719139821; 0.002067683631139405 -0.0010267455513389328 0.0008631263438723866; 0.009136342354751147 -0.0066871874031842774 -0.0024332886670555124] %
+
+Mass Used: 104.61377539679097 kg
+Launch C3: 96.55987131343802 km²/s²
+||V∞_in||: 1.1350793748149834e-5 km/s
diff --git a/archive/ES_0.5724768524245776 b/archive/ES_0.5724768524245776
new file mode 100644
index 0000000..8a956dd
--- /dev/null
+++ b/archive/ES_0.5724768524245776
@@ -0,0 +1,22 @@
+archive/ES_0.5724768524245776---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T06:51:01.744
+Launch V∞: [7.728131147821267, -5.603158797705687, 0.19340165271137966] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3451204250549145e-6, 9.039260495448704e-5, 1.6050241293326765e-6] km/s
+ V∞_out: [8.691903160214073e-5, -1.314183224951473e-5, 2.085507016984904e-5] km/s
+ time of flight: 1.8749577787473494e8 seconds
+ arrival date: 2030-04-20T09:00:38.744
+ thrust profile: [0.739712573950165 0.023989736765727934 -0.18226693376394718; 0.09824041647436657 0.060269611968506824 -0.10428578530569652; 0.08118444353165143 0.08425103277119118 -0.1573988061277074; 0.047758551065531805 0.06656605351731218 -0.13953991896918877; 0.03821949416473511 0.071867091352737 -0.15334865326170746; 0.006049813623477628 0.012139312443253277 -0.026813274679782385; 0.00890848466338458 0.014363924925904815 -0.03659019959756723; 0.006118543601184932 0.020693279232423818 -0.04369652541207767; -0.0027086135374088122 0.0019112367697069399 -0.008834092252100866; 0.0040619181001668786 0.011930472036642326 -0.01403614613295279; 0.0022047185456966025 0.0013700411259417694 -0.004873206998914784; 0.0041118629913231355 -0.002590981401478982 -0.008421855698190747; -0.0021128632608687667 -0.0024914084734591986 0.0059764234275682185; 0.00619844932667725 -0.0032119975296896744 0.00557252367673507; 0.029770277530980792 0.014930051812132037 0.015358810700600772; -0.0025279411164045302 0.004850140141795169 -0.018722530301081976; 0.008872607019334126 0.0072083654868624735 0.007698765842344636; -0.0003131624804559555 0.019869267489434118 0.03818338329351146; -0.020678061838006606 -0.04755517460863035 0.03886385464467076; 0.000800434837803541 -0.011997486264923512 0.013569722453450807] %
+
+Mass Used: 136.1416392899041 kg
+Launch C3: 91.15680374950338 km²/s²
+||V∞_in||: 9.041685950015956e-5 km/s
diff --git a/archive/ES_0.5725071751028319 b/archive/ES_0.5725071751028319
new file mode 100644
index 0000000..c5ab23f
--- /dev/null
+++ b/archive/ES_0.5725071751028319
@@ -0,0 +1,22 @@
+archive/ES_0.5725071751028319---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T04:47:48.944
+Launch V∞: [5.600486980105735, -8.038165193707115, -0.4074985581061789] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004365136746315002, 0.0005936616582417328, -9.191457666128162e-6] km/s
+ V∞_out: [-0.00015142161495579164, 3.291156270182935e-6, 0.0007209325797840055] km/s
+ time of flight: 1.5514038125008258e8 seconds
+ arrival date: 2028-03-24T19:20:49.944
+ thrust profile: [0.37895242630250753 -0.18410562507814013 -0.16311821694373804; 0.129712664844912 0.0042461306878691955 -0.14215807406771164; 0.07497125089101492 0.018332919005103043 -0.1308028981474699; 0.08025050820418585 0.030651465438829687 -0.1873547005775549; 0.06712831587311836 0.03217329840593474 -0.19398684195761542; 0.03120741594062721 0.016740476498133323 -0.10639274309806518; 0.04221464883637919 0.025952041762930485 -0.16457059443816818; 0.01244111918436176 0.008136969648306111 -0.0573424038530587; 0.027496910873764133 0.01998379118058552 -0.13107013325584002; 0.005500431494769055 0.003949860687076178 -0.029470950997664457; 0.0012854489525372763 0.0008530693571364618 -0.006839204075524118; 0.000701122846145044 0.0005467836969457919 -0.0044003465179266; -1.4031871740606474e-5 -4.936980948552999e-5 -0.0002961294727474832; 3.6498902957079376e-5 0.0003005314754286737 -0.0001852553075710298; -0.00012857978692118124 -0.00016447946093562564 -0.000464984611836223; 0.00030553808656117365 0.0002628511065631971 -0.00032558390648580857; 0.00010766054908302697 0.0002654564010161996 -9.935485045473025e-5; 0.00016639886906219905 -0.00031669625196732666 -0.00043827569673685887; 2.7913779393758966e-5 0.00013105428389184636 -0.00044476570415172344; 4.3112097282947556e-5 -1.991105878346969e-5 2.6909834898055187e-5] %
+
+Mass Used: 107.08731745862133 kg
+Launch C3: 96.14360917051702 km²/s²
+||V∞_in||: 0.0007369279717181642 km/s
diff --git a/archive/ES_0.5725752064644716 b/archive/ES_0.5725752064644716
new file mode 100644
index 0000000..cb7cf27
--- /dev/null
+++ b/archive/ES_0.5725752064644716
@@ -0,0 +1,22 @@
+archive/ES_0.5725752064644716---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T01:37:27.130
+Launch V∞: [7.21016138659377, -6.739207878386822, -0.4132148077772864] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.6307938664414334e-6, 1.0493325280368786e-5, 5.2826144015041575e-6] km/s
+ V∞_out: [8.401781273684976e-6, -7.715223309816395e-6, -4.591955918148248e-6] km/s
+ time of flight: 1.4939615217203516e8 seconds
+ arrival date: 2029-01-31T04:33:19.130
+ thrust profile: [0.3559917266944864 -0.10064871780800178 -0.14880498447524904; 0.06793166968167791 0.01202001881606009 -0.0823540190793134; 0.08071116390863893 0.032794642707291065 -0.16473136481501585; 0.11302092511411718 0.061223560004843504 -0.29966803760020816; 0.04694592428983255 0.03012072653823523 -0.1705671963505819; 0.03606576199330476 0.02607157494234191 -0.15891348766694074; 0.02640515225258571 0.02037918113379819 -0.13672270216954582; 0.013617333976583759 0.010013717665355295 -0.07026685529240433; 0.005872651371371744 0.004737404164523949 -0.03350518591834113; 0.0013755901852070627 8.890606124485351e-5 -0.003564101072304628; 0.0037968801096807505 0.0033532080408496014 -0.02653998083228119; 0.0023771443592332593 -0.001565570555246816 -0.0011182204365018636; 0.00025205168171826007 0.0001427688926054888 -7.162514216423619e-5; 0.0007101077612670211 -0.0017879428277355193 -0.001755861667402528; 0.0009258083482397948 0.0003138390959606681 -0.0019344065951982488; -0.0012856168384560041 0.0004765619612919691 0.0007615797430625895; 0.0005934424050257096 0.000815442697246831 -0.0019145588420901175; -0.00012931231191526816 -0.0005077602502923245 -0.0022061815885976513; 0.0019064442133539796 -0.0021542807960530245 -0.0022162132729183024; 0.0006538654277541489 0.0002297227999990669 -0.0020585260871934163] %
+
+Mass Used: 98.82217780568635 kg
+Launch C3: 97.57409652620522 km²/s²
+||V∞_in||: 1.2296282139540982e-5 km/s
diff --git a/archive/ES_0.5725921530697726 b/archive/ES_0.5725921530697726
new file mode 100644
index 0000000..ef48625
--- /dev/null
+++ b/archive/ES_0.5725921530697726
@@ -0,0 +1,22 @@
+archive/ES_0.5725921530697726---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T03:15:45.706
+Launch V∞: [5.664909718687796, -7.799025872252095, -0.024233640163681885] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005754219569828617, 0.000564559629934407, 0.0006362328619953005] km/s
+ V∞_out: [-0.0007041223092990669, -0.000352616372561302, 0.0006587216424981643] km/s
+ time of flight: 1.6168311587658656e8 seconds
+ arrival date: 2028-06-06T11:14:20.706
+ thrust profile: [0.4926568505426078 -0.2039419524848098 -0.16150486639843384; 0.2645890664129069 0.036242272181223605 -0.2320758528704639; 0.09617432831995372 0.03659813550800787 -0.13757904230919413; 0.1459781884252507 0.08136187833041303 -0.2753394331034017; 0.07939108951204563 0.054716551208907026 -0.1898030932660155; 0.04313112255455739 0.034317302556024464 -0.12392035974719104; 0.020351974996097855 0.01820650886868994 -0.06740720924546618; 0.0028103179391965553 0.0030044038807032062 -0.01154508591824142; 0.007213207797855902 0.007998417467299375 -0.031477288302668716; 0.004590906079345445 0.0052573550653736145 -0.021453416321635478; 0.001846245157160845 0.0013244346390409198 -0.004258782242097741; -0.0009500221586997214 3.0508759326924417e-5 -0.004577179134773715; 0.002242796410841346 -0.003514940799754512 -0.002014710909649659; -0.005122230798347569 -0.000606254491597631 0.0013154207825018783; -0.0004830210409419285 -0.002538841815675967 0.004307012523813674; 0.0004945048198262854 -0.0008554353392036139 -0.0026343935161763175; -0.006747892596917559 0.002309043121141702 0.006253506693321904; -0.008890879110899565 0.003129686998120056 -0.0006877826658584999; -0.011904612097164462 0.006125597300396928 -0.008338976850093827; 0.0009184249764190907 -0.0003762946307500992 -0.0005175978463602196] %
+
+Mass Used: 126.01071389490471 kg
+Launch C3: 92.91659394625658 km²/s²
+||V∞_in||: 0.0010269519263394913 km/s
diff --git a/archive/ES_0.5725953854633378 b/archive/ES_0.5725953854633378
new file mode 100644
index 0000000..f8dda20
--- /dev/null
+++ b/archive/ES_0.5725953854633378
@@ -0,0 +1,22 @@
+archive/ES_0.5725953854633378---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:22:18.835
+Launch V∞: [7.819232676592754, -5.629783322780001, 0.6023498861775896] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3114946801792233e-9, -1.3301122932092682e-9, -1.3485888948268388e-9] km/s
+ V∞_out: [-2.818958091561574e-10, -1.776759140950842e-10, -1.2497224095768408e-10] km/s
+ time of flight: 1.84127363973969e8 seconds
+ arrival date: 2030-03-11T17:51:41.835
+ thrust profile: [0.6028303496953613 -0.009494257407948835 -0.1645698653485035; 0.11570221618424419 0.06594642576245126 -0.11271252180867394; 0.07957563396144061 0.07427698353028836 -0.1393144047890946; 0.045857463740912735 0.0567868091321074 -0.1189582984083101; 0.036053664629135576 0.05512610008895786 -0.12750910067755877; 0.017672761575285367 0.030327936039693883 -0.07530455693854833; 0.007571415054531427 0.015980356533397123 -0.04117218555907861; 0.002907250387209834 0.006398287758773015 -0.017432930524759062; 0.005506862974064544 -0.006868156220083639 -0.002922203502037615; 0.0004043731741389268 0.006272851571600061 -0.020087298635564202; 9.987701804236443e-5 0.003497733630217874 -0.008969133100398343; -0.0030334701484858208 0.00826733166434911 -0.01646447044403332; -0.005997681820280088 0.006015663011782621 -0.008270406980849916; 0.002478363655351091 -0.0042547273726553075 0.004859847496457261; -0.006433115319347121 0.00011437913444315318 -0.0011045759180837375; -0.0014988728010934737 -0.0595955897328925 -0.039387642296466976; -0.009386318739266816 0.005870217653100883 0.0038350733471716227; -0.0027941755972850533 0.020399483386062997 0.018961433403810513; 0.008218380114060411 -0.014538884445175346 -0.00906200732542329; -0.03901234051476946 0.06540917468902743 0.004463954437228124] %
+
+Mass Used: 124.37478547165983 kg
+Launch C3: 93.19768529752587 km²/s²
+||V∞_in||: 2.3038899747893986e-9 km/s
diff --git a/archive/ES_0.5726198197887307 b/archive/ES_0.5726198197887307
new file mode 100644
index 0000000..cd9f9a4
--- /dev/null
+++ b/archive/ES_0.5726198197887307
@@ -0,0 +1,22 @@
+archive/ES_0.5726198197887307---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T16:08:16.102
+Launch V∞: [7.15861784701814, -6.586093143192868, -0.24868374915061994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005255204937664064, -0.001997058445899868, -0.0029408931740323944] km/s
+ V∞_out: [-0.002285059543777423, -0.0005195526578862552, 0.0027206557601441076] km/s
+ time of flight: 1.513123529223611e8 seconds
+ arrival date: 2029-02-20T23:20:48.102
+ thrust profile: [0.5997145258636847 -0.1562674952594329 -0.22761584559655884; 0.09038739803224571 0.02143889984846946 -0.10159755118554309; 0.07468440566808211 0.03548979762230199 -0.13916507485623347; 0.07531309525700723 0.04767816537436568 -0.19178217929197514; 0.07189336752682644 0.054172187677626625 -0.22926795672732633; 0.05340031602413821 0.04478640809399617 -0.2056388790765548; 0.021500975734666364 0.019387961935458914 -0.0957537628549838; 0.00964192250294828 0.01246818141279035 -0.060182534404883865; 0.0034230693344836937 0.003202759249289658 -0.01798453701177323; 0.009290928818061477 0.010561664807917126 -0.05943029263233235; 0.0012436674770496061 0.0011006926435703 -0.006032616722542025; 0.0021752017596334116 0.002251507276500566 -0.007001569076965355; 0.0012380275253676813 0.0005562097743610341 -0.0019398664181234937; -0.002771343427818997 -0.0029847043675199428 0.00020956118422191077; 0.0020263367776756558 7.687483627265984e-6 -1.2957280217524604e-5; 0.0022031507962079733 0.0008843702023452205 -0.0008616067506532149; -0.0035746379701578446 0.00237267479039739 0.0017727078787671954; -0.0007779950393593824 -0.0012059114864931525 0.005668778183931605; 0.001433990008918504 -0.0001386733262789063 0.004358184542632874; 0.0015669057856687717 -0.0008771526966996073 -0.0038305282479417714] %
+
+Mass Used: 115.7315132178087 kg
+Launch C3: 94.68427597755034 km²/s²
+||V∞_in||: 0.0035935034279625804 km/s
diff --git a/archive/ES_0.5726838399345766 b/archive/ES_0.5726838399345766
new file mode 100644
index 0000000..eb6d5ad
--- /dev/null
+++ b/archive/ES_0.5726838399345766
@@ -0,0 +1,22 @@
+archive/ES_0.5726838399345766---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T10:58:18.080
+Launch V∞: [8.055360048936862, -5.9038145177484616, 0.0038630576511327194] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012854385591909482, -0.00762425418860071, -0.008209146872279227] km/s
+ V∞_out: [0.0019398587597698985, -0.0017740590552383286, 0.010949693190602745] km/s
+ time of flight: 1.8574512462640536e8 seconds
+ arrival date: 2030-04-06T06:50:22.080
+ thrust profile: [0.16463003826117928 -0.010531924008766251 -0.06167100179378388; 0.025451593624899682 0.008655379929312255 -0.03525935624056541; 0.024235167657964164 0.011159268662609224 -0.05406112212533293; 0.016373166846009847 0.0148635659980676 -0.08421532816422311; 0.024552806891950045 0.0266948986377444 -0.13729024702050951; 0.023264936635534125 0.016155438661579244 -0.09823358978638025; 0.013183562645865963 0.015558067694280945 -0.09558408313125084; 0.0054556597106362025 0.004925149412168414 -0.048717719791509795; 0.013100257548940668 0.007026257155184138 -0.06858129507271596; 0.0022704066067488586 0.0043112193559940275 -0.010344984995180431; 0.01274246332501201 -0.0013749641279587697 -0.03983523865697242; 0.003401923144081514 -0.000404838085992462 -0.014346659819998444; 0.0015821604456808048 0.007680415050683674 -0.02644282496360099; -0.021887518531309835 0.03300910430589126 -0.02700122181863277; 0.00024011051572445414 -0.001833309565195498 0.0022044818167371565; -0.011791067501796676 -0.00798613655216413 0.008270320788059251; 0.03999292454714877 0.043008313282726765 -0.015400386906071038; 0.007836735452870655 0.017418378462089542 0.002176301436904277; 0.032206192846098505 0.03588915487661273 -0.0467590299102867; 0.02678121121810231 -0.003052020670109047 -0.005346282142359887] %
+
+Mass Used: 86.29192650000596 kg
+Launch C3: 99.74386630120001 km²/s²
+||V∞_in||: 0.011277042901066849 km/s
diff --git a/archive/ES_0.5726993980034054 b/archive/ES_0.5726993980034054
new file mode 100644
index 0000000..9e05c3d
--- /dev/null
+++ b/archive/ES_0.5726993980034054
@@ -0,0 +1,22 @@
+archive/ES_0.5726993980034054---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T14:56:25.357
+Launch V∞: [6.154595416204258, -7.707020172101383, -0.1185938949351082] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.17814737586029e-8, -1.076350008559362e-5, 4.41572304336292e-6] km/s
+ V∞_out: [8.649781060854053e-6, 6.034557921486456e-6, -4.703524241324928e-6] km/s
+ time of flight: 1.7571899013789153e8 seconds
+ arrival date: 2028-11-22T09:46:15.357
+ thrust profile: [0.2530237446122134 -0.08512803301397538 -0.09797306705192359; 0.08136751650856792 0.015108445136202391 -0.08931412221325383; 0.04983671126052952 0.020349879020792994 -0.08985729306180458; 0.06477746750316346 0.03734557482556252 -0.15969353753669513; 0.037681012362626186 0.026036394551387825 -0.11879906796939237; 0.02970433221504446 0.023071344807321113 -0.11298242224520552; 0.024616288848412795 0.021429050504751593 -0.11014905099674997; 0.009787574094725401 0.008862021613943099 -0.04905192291573891; 0.006760382501842044 0.009000282072347687 -0.04419810785727354; 0.01243486940227944 0.012707636426969128 -0.07490690915268282; 0.0019026637860841532 0.0018164731306755154 -0.014803797714519552; -1.647193933295636e-5 0.002433769924460305 -0.005478674598596715; 0.00019409483008267153 0.002602058023126653 -0.000511757981123219; -0.004649676335565808 0.012805409812889443 -0.021569420816233517; -0.0018012110436761986 -0.002936264249292191 -0.04926459065209268; -0.002618148756845787 -0.0009443465403495856 -0.00642334710637814; 0.004698613432333539 0.008443232063331564 -0.03783326504686761; -0.004486209783378649 0.009141058948575713 -0.03360712269209677; 0.009396273365949715 0.01827574676762868 -0.005901293205532111; 0.009502582509280042 0.00748024632263895 0.008852546524507343] %
+
+Mass Used: 100.61689410747977 kg
+Launch C3: 97.29126918225597 km²/s²
+||V∞_in||: 1.1634111661417663e-5 km/s
diff --git a/archive/ES_0.5727115891022849 b/archive/ES_0.5727115891022849
new file mode 100644
index 0000000..dbf331d
--- /dev/null
+++ b/archive/ES_0.5727115891022849
@@ -0,0 +1,22 @@
+archive/ES_0.5727115891022849---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T20:17:48.719
+Launch V∞: [6.736071134308554, -7.244915229830256, -1.307420490173289] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5051575420330346e-9, -1.8858706037447277e-9, 9.177539625066991e-10] km/s
+ V∞_out: [7.959496738448779e-10, -9.598702024790698e-10, -1.2593206799332447e-9] km/s
+ time of flight: 1.8689032843148336e8 seconds
+ arrival date: 2029-04-01T22:16:36.719
+ thrust profile: [0.17305871017087138 -0.0706583732777679 -0.053108981703242554; 0.08851030796594876 -0.0014294347563413954 -0.08834425560040444; 0.08433130528458015 0.02047489767172755 -0.14180201830521022; 0.04251489807373138 0.011540234578555771 -0.10504810005218419; 0.037579941013950666 0.015151061597729368 -0.12153546477443698; 0.031073137317395316 0.013526960742138217 -0.11615793286594993; 0.022804715805447084 0.010947244924627772 -0.10465862556666407; 0.01596708645010695 0.007445309727968011 -0.09145923605996044; 0.005640567391545992 0.0024507535729493338 -0.04094535605157107; 0.00650072147250217 0.003171321264643492 -0.05085638474971718; 0.0011111785791114862 0.002046828556504199 -0.00841308404319638; 0.0006969157872656069 0.0013953407124263498 -0.00415727668537065; -0.0001834879316817962 -0.00020768779702976773 0.0014362162815789003; 0.0013670448182796432 0.003763989800988382 -0.0005053506463439635; 0.00017658955871488295 0.00024805640639942596 -5.245359781390357e-5; -0.0010358623843402946 -0.0011028675947905818 -0.0003599716605957757; 0.0002614943179498636 0.00037280652222537676 0.0003929154375783208; -1.714902006094259e-5 0.0006025264617061355 0.002548716352818106; 0.00047085490798699835 0.0012044159026697596 0.00506019897621374; -9.608803872874626e-5 -0.0009504484448198205 -0.0019567716130876904] %
+
+Mass Used: 87.32219106590401 kg
+Launch C3: 99.57279935201629 km²/s²
+||V∞_in||: 2.5815265824903256e-9 km/s
diff --git a/archive/ES_0.5727228422935038 b/archive/ES_0.5727228422935038
new file mode 100644
index 0000000..8677f76
--- /dev/null
+++ b/archive/ES_0.5727228422935038
@@ -0,0 +1,22 @@
+archive/ES_0.5727228422935038---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T21:20:13.618
+Launch V∞: [5.950404303722007, -7.8608696338117365, -0.15168047285746933] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003159700411035869, 0.0024990810616933126, 0.002529456297974331] km/s
+ V∞_out: [-0.0019508000185669311, -0.0036237232716884037, 0.0023875815947314223] km/s
+ time of flight: 1.6699116280948356e8 seconds
+ arrival date: 2028-08-11T15:46:15.618
+ thrust profile: [0.2356064236938346 -0.09892946940944444 -0.09814548535969539; 0.1328052577893011 0.010872386427928225 -0.15058217979480737; 0.06271762077721062 0.017365108159702797 -0.11915670006692916; 0.07963971608082568 0.03097891157754459 -0.19975938230359047; 0.038229183211303815 0.018681657425914006 -0.12355560404340583; 0.025755087495272666 0.013275054443928862 -0.09364727736592007; 0.023995795260598037 0.010031498805505763 -0.09740773108812283; 0.024530926301382303 0.016149972238149506 -0.14165805454873387; 0.004891599036926293 0.0032867246238460638 -0.029358950478282242; 0.0049005594780973955 0.004077689703685975 -0.02613144193776839; 0.0008845550475353164 0.0030830090978358118 -0.008754243398314515; 0.001307833478748386 -0.0016138049682410706 -0.012848877564493858; 0.00014997111843568839 0.0029060176306006324 -0.007533036599592454; 0.01939987802235514 -0.020437522479127366 -0.049610509556350185; 0.020352257076243267 0.005694606155625529 -0.0052051725472163435; -0.0058443576890792204 0.0017207430548727481 -0.0038098487521945872; -0.003398197604006262 -0.010792764260730295 -0.003173345766883477; 0.002282388861527683 0.0021142648667046076 0.003508311761915673; 0.017377748630349937 0.007963111750842572 -0.006351517107282264; -0.0025280094561849825 -0.0024505034827702653 0.006765571933789679] %
+
+Mass Used: 101.03904250601954 kg
+Launch C3: 97.22358974338312 km²/s²
+||V∞_in||: 0.004756812168225315 km/s
diff --git a/archive/ES_0.572733518590475 b/archive/ES_0.572733518590475
new file mode 100644
index 0000000..de476aa
--- /dev/null
+++ b/archive/ES_0.572733518590475
@@ -0,0 +1,22 @@
+archive/ES_0.572733518590475---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T20:50:43.163
+Launch V∞: [5.7815237136794275, -8.06192795421824, -0.3564345109741713] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.387337156083002e-6, -1.9717269935682224e-6, 1.5319144888010297e-6] km/s
+ V∞_out: [-2.0389021079546605e-6, 2.770931975855472e-6, -2.42549497785609e-6] km/s
+ time of flight: 1.5855153678704208e8 seconds
+ arrival date: 2028-05-04T22:56:19.163
+ thrust profile: [0.17477147194512224 -0.0857514214609799 -0.08088117806500236; 0.09375285921551656 0.0013137302356774027 -0.11209518729737575; 0.08081394599472705 0.017124816160982593 -0.15409843237669205; 0.07560828592842006 0.024799767354588987 -0.19364742835494964; 0.05751981521930133 0.023614908822170797 -0.18401476135319172; 0.0401858674924415 0.018617789871936248 -0.1533546959145132; 0.02265326343974065 0.011183805700162626 -0.10057219157174992; 0.008993140114232653 0.004221176509983064 -0.04587222708686848; 0.014042803725678813 0.007302342581340495 -0.0750811512001871; 0.020265485638376546 0.01242324840412048 -0.11524379208613841; -0.00037164753534041817 0.0008622454459504155 -0.0031412885061544178; 5.7051921920178646e-5 -0.0009341100901621712 -0.002325862917639819; 0.0011072665598903185 -1.5356825284986082e-5 -0.0014725887373249948; 0.0004975251125965761 0.003539068514008369 -0.002932375035812053; 0.00042348792566399024 -0.0013017623446333173 0.00023039533808263523; -0.0003070536639683055 0.0010863312307294324 -0.003118379442135917; 0.004117306250940957 0.0006638675088945153 -0.0002415972791948379; 0.006063108157307342 0.0026155367287376014 0.0031375263442934504; -0.0006576707764183216 -0.0016101589519206684 0.0027077791903842375; 0.00032689283696198324 0.006138268326098121 0.0022429924998656615] %
+
+Mass Used: 93.32726297205818 kg
+Launch C3: 98.54774435145646 km²/s²
+||V∞_in||: 4.208149515778233e-6 km/s
diff --git a/archive/ES_0.5727493707422555 b/archive/ES_0.5727493707422555
new file mode 100644
index 0000000..38e245a
--- /dev/null
+++ b/archive/ES_0.5727493707422555
@@ -0,0 +1,22 @@
+archive/ES_0.5727493707422555---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-08T03:01:42.320
+Launch V∞: [6.362926762379152, -7.900479104389279, -0.406191429767051] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3984567921594084e-5, 2.2252832026472085e-6, -3.996366281824316e-8] km/s
+ V∞_out: [-2.748910255958729e-6, 6.162919461135924e-8, 1.3892254492648277e-5] km/s
+ time of flight: 1.843850288064867e8 seconds
+ arrival date: 2029-03-11T05:05:30.320
+ thrust profile: [0.022623939903517576 -0.009122284443925443 -0.011890906293370663; 0.02488420537660605 -0.0014917889748505776 -0.039913592422175216; 0.020238200599369798 -0.00034711299611401376 -0.055524478497851595; 0.05189154369508296 -0.0012569063663666472 -0.19522827558210853; 0.02609077659518927 -0.002970891339413883 -0.12441674565281884; 0.023783844382577843 -0.004304004116380831 -0.13288520932268713; 0.014833798555779583 -0.0035083228206992654 -0.09309561404597955; 0.01262279374525628 -0.0037395836279735545 -0.08698587204757456; 0.007001257199064952 -0.0023909875277671393 -0.05170585772017292; 0.005356497619649709 -0.002078954664652985 -0.04181245575107284; -0.0004634925847913289 -3.0996450527196156e-5 -0.0019739176994643852; 0.00027550695033318716 -0.00024462561012650953 -0.0021999626297879104; 0.0016422165899625811 0.0018161049394528654 -0.00016062121862991138; 0.0007227393543785782 -0.003361655773110908 0.0012598733816417459; -0.002826189403539618 -0.0011789394924313665 -0.002824301769529151; 0.0005280509437560084 -0.0002603236782415297 -0.00302320790226057; 0.0012716948696588131 3.0302159426662853e-6 0.0009722338674072583; 0.0031072052487289086 0.005766884067198953 -0.004953828482222279; -0.000818691979962712 -0.004160762346508096 -0.0033932308020334424; 0.0043674632313548765 0.002410500696395361 0.00021196282706525748] %
+
+Mass Used: 66.96944104983095 kg
+Launch C3: 103.06939853990866 km²/s²
+||V∞_in||: 1.4160565750703887e-5 km/s
diff --git a/archive/ES_0.5727583566594261 b/archive/ES_0.5727583566594261
new file mode 100644
index 0000000..9f6b9fa
--- /dev/null
+++ b/archive/ES_0.5727583566594261
@@ -0,0 +1,22 @@
+archive/ES_0.5727583566594261---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T21:12:22.016
+Launch V∞: [5.714080443544866, -8.04820445841845, -0.5969635289080243] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0016714113632302786, -0.0010439665958522565, 0.000998895197921293] km/s
+ V∞_out: [-0.001124652764437815, 0.0016029612809335095, -0.0010232510303793808] km/s
+ time of flight: 1.5508047897460005e8 seconds
+ arrival date: 2028-03-23T19:07:00.016
+ thrust profile: [0.23441179975544987 -0.11433518500251758 -0.10697200755313917; 0.11018256096612365 0.005358752860988872 -0.12340783533720891; 0.10957631068138805 0.03006755526522727 -0.19241277675180293; 0.08699992564158113 0.036360057718515575 -0.20413493867063917; 0.07094400705071717 0.037331959778763586 -0.20808042213023156; 0.051425250794188485 0.03154636976779992 -0.17922833386302994; 0.03189857877973786 0.02151294340407732 -0.12697299326901812; 0.01041300994393644 0.0072065274788763525 -0.04629282121595087; 0.007693219037861494 0.005581179202618535 -0.037392164442486456; 0.005218391806214505 0.003986267284926654 -0.027598379836557243; 0.0008799868297059951 0.0008160124854391128 -0.005433194182156574; 0.0013402253859289455 -0.0001464736741552551 -0.0034536666397320566; 0.0005972086084746377 0.0008041659497209983 -0.0045187228093249605; 0.0007534118034372812 -0.0011409544649684557 -0.0009160117836341107; 0.0002140692675947924 0.0018257329460975857 -0.0016094652652395942; 0.001599967971581831 6.382053537543112e-5 -0.0019758798371695458; -4.116538060728865e-5 0.0006613800493774878 0.0003039854109340573; 0.00023877260266442045 0.0013931819082328525 -6.979812599066195e-5; -0.0017029593587491963 0.002245704789043554 6.0861309984067493e-5; 0.0009281666939142486 -0.002742936872401048 0.0016102866106275716] %
+
+Mass Used: 97.83080741717731 kg
+Launch C3: 97.78067577465484 km²/s²
+||V∞_in||: 0.0022093604990632166 km/s
diff --git a/archive/ES_0.5727617937270508 b/archive/ES_0.5727617937270508
new file mode 100644
index 0000000..f4d4806
--- /dev/null
+++ b/archive/ES_0.5727617937270508
@@ -0,0 +1,22 @@
+archive/ES_0.5727617937270508---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T22:38:13.768
+Launch V∞: [5.9575884773675005, -7.875366972567868, -0.04769773988375867] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.344451586539265e-6, -2.040152104901715e-6, 1.5219236502804456e-6] km/s
+ V∞_out: [-2.305192500114426e-6, 2.9445319132100324e-6, -2.0300654611272762e-6] km/s
+ time of flight: 1.652312924540238e8 seconds
+ arrival date: 2028-07-21T08:13:05.768
+ thrust profile: [0.2380093389802217 -0.09822749347075695 -0.09539542592225796; 0.0751392930400405 0.007488898123737205 -0.08195191275882274; 0.07455543637721017 0.023969464778152753 -0.13010696453103063; 0.05799333697809567 0.026749222069766636 -0.13781672557631405; 0.041347274432649385 0.023252796924510443 -0.12319766751484806; 0.05043197454939679 0.033191217962681235 -0.17631786244930592; 0.018843930702392524 0.014862662149858288 -0.08220268656710264; 0.012190261815456765 0.00934657178040131 -0.0577017310483151; 0.04156027934272642 0.03687560277480519 -0.20812707846343248; 0.008005010905846563 0.006753274479745394 -0.04454324795771054; 0.002695314537180549 0.002168823005948813 -0.010750314608369187; -4.312278597142634e-5 0.0036097743305383736 -0.0072269650049686125; 0.0018892919928321641 0.0007121641387107504 0.005240445384209717; 0.0014491762205102031 -0.005543479115581248 0.002517233561227812; 0.0030184641497368256 0.0023965384540889376 -0.0025001961113017804; 0.006173608840179999 0.011240447418366974 -0.010535380854587885; 1.1451810724103935e-5 0.0007146093618296055 -0.0018187879995898435; -0.00042971321636478587 -0.00018435240411392563 -0.0003406416359767147; -0.0023636731332240795 -0.013735964943586889 -0.012285040630974242; 0.01583205484706534 -0.010971528151501939 -0.011013519242365316] %
+
+Mass Used: 99.37560647434793 kg
+Launch C3: 97.5165404926648 km²/s²
+||V∞_in||: 4.2028357835065195e-6 km/s
diff --git a/archive/ES_0.5727724139065546 b/archive/ES_0.5727724139065546
new file mode 100644
index 0000000..02793ce
--- /dev/null
+++ b/archive/ES_0.5727724139065546
@@ -0,0 +1,22 @@
+archive/ES_0.5727724139065546---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T19:52:10.648
+Launch V∞: [5.728527403187237, -8.138608331149676, -0.3489855791331802] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.671928380561865e-8, 3.0320120155357914e-8, 5.2131038033973404e-8] km/s
+ V∞_out: [-3.492098392460245e-8, 4.6247083581916645e-8, -5.546356589436199e-8] km/s
+ time of flight: 1.5999053651757675e8 seconds
+ arrival date: 2028-05-23T13:41:06.648
+ thrust profile: [0.16919839001846862 -0.08636128307530151 -0.0819204617007119; 0.06603724119230643 -0.0019735762464899434 -0.08325782982196032; 0.07594003212740458 0.009440542554134738 -0.15244311178410577; 0.05979412208058979 0.012614774533608205 -0.16387805642582742; 0.048049890093125235 0.012153795419595461 -0.1628213573273256; 0.038105044924752404 0.010467066145041164 -0.15374480925597186; 0.03539457510025978 0.011466917083237481 -0.156706038600294; 0.02582609198983531 0.009628186790212549 -0.1329552335299961; 0.005832833692430322 0.001906318612936706 -0.037104195104963975; 0.0032896439331997545 -0.0007741091858372558 -0.01677126431704659; 0.0039149537548989035 0.0017168871502257453 -0.03205762739710853; -0.00023630050451029267 -0.00024421100945103884 -0.005790188161174171; 0.0006158250287064 -0.0002492562468763194 -0.0058516757620133975; -0.002757790116923408 0.0007794557390271666 -0.0019884553720874616; -0.0009244478186178324 0.004302868828872286 -0.0013889565322280346; 0.0007734221011277453 0.00221803870787473 0.0001838102784714763; -0.0009030867719588242 0.0036434166458055948 0.00028387918392873727; 0.00028884232796963104 -0.0006022852751186858 0.0001652931286490304; 0.004763711312724533 0.005295544686063497 0.0011372581720139933; -0.0005931244731254563 0.00035308564594672086 0.002877625963347176] %
+
+Mass Used: 89.71503374132817 kg
+Launch C3: 99.17476271136896 km²/s²
+||V∞_in||: 8.27890812133897e-8 km/s
diff --git a/archive/ES_0.5727895791564782 b/archive/ES_0.5727895791564782
new file mode 100644
index 0000000..5bc0f2c
--- /dev/null
+++ b/archive/ES_0.5727895791564782
@@ -0,0 +1,22 @@
+archive/ES_0.5727895791564782---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:44:09.476
+Launch V∞: [7.229159222937927, -6.70671381726863, -0.40020011824693713] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.291055646039621e-6, 1.4303486235962972e-5, 7.548955758115113e-6] km/s
+ V∞_out: [1.1514412123240558e-5, -1.0756605336333825e-5, -6.419863802823845e-6] km/s
+ time of flight: 1.504794237954207e8 seconds
+ arrival date: 2029-02-12T14:34:32.476
+ thrust profile: [0.3293536428938134 -0.09222736072972149 -0.14041127564818376; 0.10215126592785018 0.020103316140315557 -0.1209001290611527; 0.10402804754311769 0.04355955441390767 -0.20326462956473662; 0.08522123833448486 0.04705830023546483 -0.22941134503686758; 0.054337724248739734 0.035220011656006835 -0.18589098832515646; 0.04693063676299524 0.034379100582282995 -0.19238338965604082; 0.022273734161053823 0.017649388509493817 -0.10523974189033763; 0.008997399667732584 0.005534570771010108 -0.046746658002431545; 0.006440412075196534 0.005278437677451233 -0.041269392256310614; 0.001272133752726732 0.0011925741166845909 -0.007843957471118495; 0.00021609154217664545 0.001243740605132279 -0.007612745530141891; 0.0045934556763167315 0.0013464844770784022 -0.0031863416195798814; 0.0020867924692537006 0.001379781888627031 -0.0039020961574995957; -0.0025379097256465286 -0.0013586387221262855 -4.3206757847046246e-5; -0.0026142396461749334 -0.0021136369679821583 0.0034231601698462904; 0.002340452436636139 -0.0026994087235915677 -0.005786593910522136; -0.0001962238760062132 -5.589436610090243e-5 0.0011114435210839114; -0.0025555139454990737 -0.005039558418520756 -0.008826917996562331; -0.006886212329660196 -0.0002618611604068479 0.0030329566136681253; -0.0013513017649467117 0.002337706439359434 -0.00031997062321075843] %
+
+Mass Used: 100.08251399603523 kg
+Launch C3: 97.40091343197533 km²/s²
+||V∞_in||: 1.701680702687344e-5 km/s
diff --git a/archive/ES_0.5728595353568129 b/archive/ES_0.5728595353568129
new file mode 100644
index 0000000..4b94fb7
--- /dev/null
+++ b/archive/ES_0.5728595353568129
@@ -0,0 +1,22 @@
+archive/ES_0.5728595353568129---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T19:42:20.148
+Launch V∞: [7.862459485362803, -6.351012645681632, -0.13040978865516878] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0749139517632915e-5, -2.6765627428126007e-5, -7.864694999868961e-5] km/s
+ V∞_out: [-7.672355676786044e-5, -9.559532452965329e-6, 3.2551922964656045e-5] km/s
+ time of flight: 1.8749577783336142e8 seconds
+ arrival date: 2030-05-01T21:51:57.148
+ thrust profile: [0.18636264435664548 -0.011935885339719081 -0.08280640230149122; 0.055841519230758675 0.01807361836228662 -0.08242823833860809; 0.02956305582829989 0.013683498362790765 -0.07631065807410092; 0.01673802361231133 0.007985236898377109 -0.05992438004894751; 0.028132574357542146 0.014652407069613554 -0.12833215747680296; 0.01554641922623377 0.007759216884222944 -0.08479435239767612; 0.019814253641240204 0.009971717678713505 -0.12233912499289014; 0.01206616399280068 0.005600980445589267 -0.08285181220412428; 0.003059835930850376 0.0013156911411989526 -0.023486478417454288; 0.0019163668577686676 0.0011827515096364206 -0.015309824509885654; 0.0034274099075268464 0.0012798897102371883 -0.0062548266314429455; 0.000511996491649339 0.0005799842746057435 -0.005084418116363898; 0.0027025954601008796 0.000336091715941058 -0.0010885220526942819; -0.0014148677716010897 0.0020184916949923934 -0.005562010936275784; 0.0014731401793410372 -0.00621741207330684 -0.00026400412661242104; 0.0003298136651730579 0.0011482399217724723 0.0005025002110337633; 0.00042793950543919593 -1.1360959837391832e-5 -0.003399502620492236; -0.007718745425293342 -0.00491383250188856 -0.0033475025672220302; 0.0042746379510432645 -0.0028888545791173406 -0.0015453061865521884; -0.001522216278140162 0.0007156228233053233 0.0035531882204538233] %
+
+Mass Used: 72.34073918053491 kg
+Launch C3: 102.1706374975566 km²/s²
+||V∞_in||: 8.376923991589736e-5 km/s
diff --git a/archive/ES_0.5729675675437077 b/archive/ES_0.5729675675437077
new file mode 100644
index 0000000..f54d7e6
--- /dev/null
+++ b/archive/ES_0.5729675675437077
@@ -0,0 +1,22 @@
+archive/ES_0.5729675675437077---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T03:03:05.411
+Launch V∞: [5.889255216584354, -7.846560107477342, 0.06493378099457442] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.2804693105656335e-9, 3.978437405604892e-11, -4.350892962986026e-9] km/s
+ V∞_out: [-1.3567160716118747e-9, 2.993737658731835e-9, 4.088923267677042e-9] km/s
+ time of flight: 1.5837034018335032e8 seconds
+ arrival date: 2028-04-29T02:48:45.411
+ thrust profile: [0.3331678000357432 -0.156856742245241 -0.12788315868246894; 0.1181250532927427 0.008163635192374967 -0.11824437931815614; 0.10344224357844138 0.0305054839833045 -0.16378047803269466; 0.09888535192822634 0.04345047632269647 -0.20933788792162702; 0.08415322062649454 0.04584028879128956 -0.22093222450307415; 0.07109760461963856 0.04478308533412897 -0.22192565659348443; 0.025621352636133903 0.01795795603213283 -0.09486337041640004; 0.006298933988910807 0.0045475661747249345 -0.025326448118758386; 0.0057643489869643755 0.004659404414782693 -0.021406353929705548; 0.00806663935384113 0.008391693350775867 -0.027247464515022947; 0.0045509267131177075 0.005277075269564942 -0.026869614762643525; 0.000265924501782985 0.00033711863128678757 -0.002033304595735238; -0.0006891659365465243 -4.523756896882025e-5 0.0025307114612656985; -0.0016930275300149355 -0.0014627388329668137 -0.0010425436188620245; 0.0009195329963656397 -0.000623554217570024 -0.0037963194442885715; -0.0006822861349277411 0.0010762940970677139 -0.0015750743546363705; 7.790015868268049e-5 -0.0004823480166805203 0.00026959954509304376; 0.0022364012762227407 -0.0003774552498349618 0.0013629104799550602; -0.0013844234090410487 0.0004476440433823298 -0.0012311827976688363; -0.0014003493817427235 -0.00046396659419250326 0.004393995506585484] %
+
+Mass Used: 106.96854342128745 kg
+Launch C3: 96.25604892223512 km²/s²
+||V∞_in||: 5.4491587671257404e-9 km/s
diff --git a/archive/ES_0.5729901766489669 b/archive/ES_0.5729901766489669
new file mode 100644
index 0000000..491bc76
--- /dev/null
+++ b/archive/ES_0.5729901766489669
@@ -0,0 +1,22 @@
+archive/ES_0.5729901766489669---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T02:16:44.834
+Launch V∞: [5.771034348384091, -7.889120788084391, -0.17019093502246863] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0013522334691655998, 0.001495480296344937, -2.3501702401238654e-5] km/s
+ V∞_out: [-0.0004006450913007021, 9.021390936378112e-6, 0.001973984802450153] km/s
+ time of flight: 1.5652845916903573e8 seconds
+ arrival date: 2028-04-07T18:24:23.834
+ thrust profile: [0.3983723995680747 -0.18823071039556666 -0.15702624375921226; 0.09992284914073819 0.00676889134196647 -0.10604820221244757; 0.15580645037878957 0.0484403875131138 -0.24846923056765155; 0.08561892264293765 0.03995704640712699 -0.19064018874268066; 0.08370466423481006 0.048439621800374554 -0.22645340155171773; 0.04014926565942023 0.02658132017525034 -0.13347250297324326; 0.023382039329743014 0.016972738322035916 -0.08937180322258932; 0.022445849205754455 0.017654602877955183 -0.10248105336612115; 0.008336566099263604 0.006569243208623204 -0.035602265924211195; 0.00010308095700954162 0.0009874849488728107 -0.0014831195613876436; 0.0013675502292696674 -0.0005641611433834411 -0.004104067042879617; 0.0006171887619687972 -0.00018056648179763538 -0.0016646862049187923; -0.000316702646617437 0.0012683186733553568 -0.004649016696486303; -0.0007398006770216064 0.0010847218337809257 -0.0011115215725865245; 0.0022115350107435364 0.0006429976986753628 -0.0007689101519411379; 7.56229250322548e-5 -0.000823779148514793 0.0008608482260560647; -0.002464541486951192 0.002131780201567699 0.00026282515222221135; -5.560158607049586e-5 1.987554415945592e-5 9.2004303274914e-5; 0.0007383021056670626 0.000549630445513828 0.004726192773542385; -0.00021712585979827612 -0.0022647366950055868 -0.004597235553300536] %
+
+Mass Used: 110.9850356779225 kg
+Launch C3: 95.5720292135781 km²/s²
+||V∞_in||: 0.0020163206594942507 km/s
diff --git a/archive/ES_0.5730197245034802 b/archive/ES_0.5730197245034802
new file mode 100644
index 0000000..9c28b57
--- /dev/null
+++ b/archive/ES_0.5730197245034802
@@ -0,0 +1,22 @@
+archive/ES_0.5730197245034802---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T21:44:27.104
+Launch V∞: [7.29437962711671, -6.532644641638466, -0.22064595269951814] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.96616169716093e-5, 0.0005915479985883728, -0.00030382946262251374] km/s
+ V∞_out: [-0.00025864598991261634, -0.0005220029555166596, 0.0003300313072799829] km/s
+ time of flight: 1.5796325151786402e8 seconds
+ arrival date: 2029-05-11T04:25:18.104
+ thrust profile: [0.41866343200142087 -0.09460597153008184 -0.1643224909479305; 0.0882272882633526 0.021686482708278342 -0.09815770725761339; 0.08708593836925442 0.04140650959705177 -0.16315728837021348; 0.0661066838598078 0.041279414289240805 -0.1731806579206627; 0.04771501368141889 0.03470199820422353 -0.15898974790814355; 0.043713403471214454 0.036195139413122586 -0.17733334152111246; 0.023225870838878043 0.02021215605387473 -0.10579832327737936; 0.015835179898742505 0.014146563860955863 -0.08025415175059829; 0.002668689536992716 0.003691322692153507 -0.00507732586123184; 0.005243827537942989 0.01571531311149712 -0.031112921566340934; -0.001301198056568809 -0.0018876673418177284 -0.02220473977623168; 0.0026608755969351103 0.0014705904329388143 -0.029035061963397436; 0.0013271558493548334 0.0005114229275329414 -0.0021188495644270874; 0.0014673507067047898 -0.0016718977191949032 -0.002151375481428046; -0.000305234080092896 0.00028307584034210475 -6.209764272185078e-5; 0.008209496292975524 0.002218701808121154 -0.013860117643936362; 0.01626252823597003 0.002836967526601266 0.0071248417252384715; -0.0011904978850369062 0.0016402425696683594 -0.0004420799944352686; 0.004463966447409082 -0.006634372447235926 0.024873391288986777; 0.045102990736727674 0.008178513577032333 0.013474223695835796] %
+
+Mass Used: 108.91906728401 kg
+Launch C3: 95.93210479486575 km²/s²
+||V∞_in||: 0.0006697666386211889 km/s
diff --git a/archive/ES_0.5730312948801355 b/archive/ES_0.5730312948801355
new file mode 100644
index 0000000..972fee5
--- /dev/null
+++ b/archive/ES_0.5730312948801355
@@ -0,0 +1,22 @@
+archive/ES_0.5730312948801355---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T14:00:14.279
+Launch V∞: [6.116484451519423, -7.41709954382731, 0.5418144451323965] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.65260516149038e-6, -8.928619413023519e-5, 1.5358427949344071e-6] km/s
+ V∞_out: [1.6095019672884633e-5, -4.237974567970799e-7, -8.826247568647291e-5] km/s
+ time of flight: 1.7787761965206623e8 seconds
+ arrival date: 2028-12-10T08:27:13.279
+ thrust profile: [0.4370463042552863 -0.12036768242819823 -0.10317442108445277; 0.42094142240124516 0.13373740928586034 -0.25607925968805834; 0.09018959238764807 0.057646893455837143 -0.10055169509132737; 0.06775401753546088 0.06003722969250559 -0.10323783858847162; 0.035126891253705016 0.038102669340529145 -0.06884388460319714; 0.030260330071344013 0.03895329549291349 -0.07228415413067349; 0.08677548290206599 0.13500396963587102 -0.22953378978812308; 0.012244661135255479 0.020294163643597662 -0.04132369190809315; 0.002646742508652903 0.004750631890030511 -0.010662996404721651; 0.003490482102676911 0.0062747795436756066 -0.013891139214887742; -6.62257625453762e-5 0.00015700940187069975 -0.00097986394150136; 0.0003637245414081674 0.0009810952271581894 -0.002780249005586871; 9.162095829881932e-5 0.00032337533688738836 -0.0009436905949334676; -0.0002768206260494072 0.0001652151239246144 -0.001101922358173405; 0.0004155658976081074 0.001197300881688691 0.0005151978068883216; -0.0004758859169954998 0.0001916296332171854 -0.00041690019055732333; 0.0008288659776918454 0.0025702520382953962 -0.002043321878412246; -4.0693424493724525e-6 3.387334971840551e-5 -0.00013506520955015438; -0.00019236608262478648 -0.0001316213183798938 0.001545394812046278; -0.0004064227057660832 -0.0004732842395896047 -0.0004812190802604428] %
+
+Mass Used: 127.67969896704653 kg
+Launch C3: 92.71831058167628 km²/s²
+||V∞_in||: 8.971761728575635e-5 km/s
diff --git a/archive/ES_0.5730322262209405 b/archive/ES_0.5730322262209405
new file mode 100644
index 0000000..f38481e
--- /dev/null
+++ b/archive/ES_0.5730322262209405
@@ -0,0 +1,22 @@
+archive/ES_0.5730322262209405---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:55:55.472
+Launch V∞: [7.164107422957488, -6.754427153312845, -0.4829690417223112] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.003691431586443e-6, 7.417653986733996e-6, 3.84801493344474e-6] km/s
+ V∞_out: [7.241162639791382e-6, -6.134819878573212e-6, -3.970339603396125e-6] km/s
+ time of flight: 1.494508314962419e8 seconds
+ arrival date: 2029-01-31T14:03:06.472
+ thrust profile: [0.3631862470834388 -0.09335866678670318 -0.15156466987611358; 0.1277575868442259 0.02891162819023103 -0.1477371312833844; 0.08159420715662213 0.039361817699527686 -0.15494081131029896; 0.0554715322779233 0.03656357424971283 -0.15768079221098696; 0.07573298093101162 0.05667147446955125 -0.2446164697159737; 0.04397969493838224 0.036681671991607906 -0.17239234206218465; 0.027419583732283346 0.024555559637069648 -0.12259032047040089; 0.008240274515933389 0.009299951210347239 -0.05084163405682386; 0.0028909811881359156 0.0029185042308467785 -0.016405663211869766; 0.009785619605425143 0.009142134081702903 -0.06026852035561027; 0.0058557183776818894 0.0048020785318093505 -0.03918469847365193; -0.0009708615582867344 -6.662840386148288e-5 -9.11219693391157e-5; 2.8001421289745865e-5 0.00035854546128772887 -0.0005969444673171628; -0.0006749855474209494 -0.00017463387377266858 1.7056401363124154e-5; -0.0006430905883964628 -0.00010536152246422256 0.001277373730064398; 0.0016054882641768353 -0.002927663101512866 0.00047751335537182566; 0.00013704555034636223 -0.00015640157805424252 -0.0007660239036895268; -0.0005130627703300383 -0.0017449032506359657 -0.00022965161627603225; -0.00021602028464306095 0.0006341912023923975 0.00018250088543852132; 0.0020395360748394304 0.000789802231031593 0.0009306038637880633] %
+
+Mass Used: 101.65437806907539 kg
+Launch C3: 97.17998043234661 km²/s²
+||V∞_in||: 1.0289466477938929e-5 km/s
diff --git a/archive/ES_0.5730587792318337 b/archive/ES_0.5730587792318337
new file mode 100644
index 0000000..af30fab
--- /dev/null
+++ b/archive/ES_0.5730587792318337
@@ -0,0 +1,22 @@
+archive/ES_0.5730587792318337---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T10:35:51.417
+Launch V∞: [5.54534718904652, -7.601293683916711, -0.2315396418739115] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.864404671593589e-5, 2.9385691837791973e-6, -5.2880960922706284e-8] km/s
+ V∞_out: [-3.7086947982731695e-6, 8.35029447241767e-8, 1.8506168627560417e-5] km/s
+ time of flight: 1.6752393226861495e8 seconds
+ arrival date: 2028-08-11T09:01:23.417
+ thrust profile: [0.76478800002265 -0.27923806884259755 -0.20238716223946074; 0.3109179582779884 0.06942353018349823 -0.22905748303654994; 0.27731949001802914 0.14235639909874595 -0.31920711113953093; 0.10359095195062286 0.0762667142976486 -0.1762285860170364; 0.04374557936786879 0.04012841335589011 -0.10123046659119089; 0.03836530148517072 0.04006472211144922 -0.10564804938500667; 0.020799486466331972 0.024287040066665377 -0.06692834017485237; 0.001677999582636658 0.002141017880466629 -0.006919208333071421; 0.003020917706090326 0.0044145406858486355 -0.013559025449983646; 0.003380269730110401 0.005451759829475722 -0.017045769115157504; -0.0007282345681032464 0.0005554262488459213 -0.000907133786366486; -0.00019519919119362111 -0.000658498307895879 -0.0011972731239084707; -0.00023308821030688573 0.0027724447752054955 0.00041942215144428335; -0.0020596707774201924 0.0021503819137387273 0.0012909910622482073; -0.0008513431997838819 0.0019538500703983335 -0.002172918094390386; 0.0005582611579613056 0.0019196431884830854 0.0002690925682530571; -0.0016292729167203767 -0.0019421922687512978 0.0021686767901633176; -0.0029534717987487876 0.0012598132523703614 -0.0021339470316958996; 0.0002247601523112792 0.0017841858067549517 0.0008353711629974152; 0.0009426381417320044 0.006211501346860228 -0.0008817884579053346] %
+
+Mass Used: 151.82769072560495 kg
+Launch C3: 88.58415172197732 km²/s²
+||V∞_in||: 1.8874280468136653e-5 km/s
diff --git a/archive/ES_0.5730711856739756 b/archive/ES_0.5730711856739756
new file mode 100644
index 0000000..ac7d5c2
--- /dev/null
+++ b/archive/ES_0.5730711856739756
@@ -0,0 +1,22 @@
+archive/ES_0.5730711856739756---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T05:25:28.912
+Launch V∞: [7.638919139995747, -5.903447244142187, 0.43964934184477594] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.984022489366828e-9, 2.468310120620382e-9, -7.30166218808993e-11] km/s
+ V∞_out: [5.127455324575504e-9, -4.602061066794827e-9, 1.6602821843199331e-9] km/s
+ time of flight: 1.831690114444359e8 seconds
+ arrival date: 2030-03-04T05:42:19.912
+ thrust profile: [0.6424378354227062 -0.029304296312442187 -0.20794733168512866; 0.07218859495679676 0.03648691029254158 -0.09126146708420928; 0.043165932821891545 0.031897535989616484 -0.09753879524912354; 0.03196127459563235 0.030326281315740687 -0.10504528525517959; 0.02587794981824172 0.025568502821911285 -0.10401416969709128; 0.02255970456037566 0.026493823036636104 -0.11765257512861906; 0.011790140387784148 0.019689541038081126 -0.08541250408739988; 0.00507393020418832 0.008279233883202867 -0.025754469061425655; 0.00036340585514402484 0.010585571293293254 -0.014555315396101887; 0.0035067513835128914 0.007850311517064053 -0.03409470250241302; 0.00193398026176498 0.000481140869522859 -0.013517786843080876; 0.012374739992318681 0.00653972971127622 -0.012293066240405444; 0.0034396952338320227 0.0004863741299526821 -0.007175156243376285; 0.007409692582527611 -0.008586726066083246 0.026426855116965388; 0.02520319163999587 0.008373097700435744 -0.010446516414697158; 0.000900006651617922 -7.042567626361449e-5 -0.0035965308666604514; -0.00364233195290833 -0.02462525167030712 0.020506596568342313; 0.0044486958180180525 0.04259556261713999 -0.043061326255884755; -0.009127444450909673 0.012765949686961752 0.004231267120503253; 0.05835138018468834 0.018751664708288297 -0.0019332579629013516] %
+
+Mass Used: 123.76682849560893 kg
+Launch C3: 93.39706653554788 km²/s²
+||V∞_in||: 5.562226753121651e-9 km/s
diff --git a/archive/ES_0.5731047156123771 b/archive/ES_0.5731047156123771
new file mode 100644
index 0000000..41384e2
--- /dev/null
+++ b/archive/ES_0.5731047156123771
@@ -0,0 +1,22 @@
+archive/ES_0.5731047156123771---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T07:15:36.516
+Launch V∞: [7.220251585758332, -6.76066593676215, -0.5707405767601573] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00048593520636451, -0.0037053254910517086, 0.001951117474662459] km/s
+ V∞_out: [0.0016523699300707315, 0.0032105778599003628, -0.0021762809481074086] km/s
+ time of flight: 1.4948052295444238e8 seconds
+ arrival date: 2029-02-01T09:37:38.516
+ thrust profile: [0.2920465319128534 -0.08586224132520726 -0.12721686908282528; 0.09002891085048233 0.015857577154928405 -0.1040102983955276; 0.0941470920930585 0.036278195202286055 -0.18205321414040473; 0.08251957697783802 0.04230937845040917 -0.22054841557187396; 0.05522963800233987 0.0328426628658598 -0.18394751272255033; 0.03537010104396309 0.02204670284009901 -0.1300190946556412; 0.0385024348691268 0.028114842003089658 -0.16342164673849832; 0.01568145462439716 0.011405914080697301 -0.0766446701284382; 0.010314386404181423 0.008792314586134966 -0.05937942590104183; 0.001096251942542638 0.0010808555450845644 -0.009789509646704598; 0.001881251056632133 0.0017382738578383687 -0.012580727489986853; 0.001146163422831137 0.002258436735989034 -0.0065772465963735375; -0.00042942912309276954 -0.00019945417863408968 -0.00415308191811517; 0.0006700130979972224 0.00028459077315203527 -0.003059432700062012; 0.000975508705766023 -0.0019052956453803759 -0.0011021956328122909; -0.001626977659583973 -0.0023576435616608103 -0.0006753982588531882; 0.000956841211229166 0.0027390865314521028 0.0018763464742744189; -0.00015156063539590496 6.530176330191476e-5 -0.00238749043067043; -0.0007939148138943622 0.00014391258567983834 0.002717959921352293; -0.0006060860810917374 -0.0014545003316705487 -0.003971368315211673] %
+
+Mass Used: 95.99660843717675 kg
+Launch C3: 98.16438167610227 km²/s²
+||V∞_in||: 0.004215735928560435 km/s
diff --git a/archive/ES_0.5731150104318515 b/archive/ES_0.5731150104318515
new file mode 100644
index 0000000..74cabc4
--- /dev/null
+++ b/archive/ES_0.5731150104318515
@@ -0,0 +1,22 @@
+archive/ES_0.5731150104318515---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T17:37:37.445
+Launch V∞: [7.972489636036596, -5.61193758960078, 0.022567170763368036] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.214671679271733e-6, 1.796776363870845e-5, 5.211086588787744e-5] km/s
+ V∞_out: [6.270278112848683e-5, 7.170250898848844e-6, -3.0585144882769396e-5] km/s
+ time of flight: 1.8749577792874435e8 seconds
+ arrival date: 2030-04-21T19:47:14.445
+ thrust profile: [0.4336910296113376 0.004361511805246919 -0.11645295260731697; 0.09299118616409749 0.05844147022885303 -0.0905312663575806; 0.048952766322868 0.051066755207919284 -0.08774995161239596; 0.03714653463914156 0.051895695487991694 -0.0998220498784413; 0.021112195005483024 0.03737256935249459 -0.07879936030292468; 0.02288812575950264 0.04807683207124193 -0.10959442370528188; 0.01327160991081089 0.03291438638348172 -0.0791716826669664; 0.005887142260276359 0.006054657755777308 -0.023020070333698767; 0.0056433967866893996 0.004099682893183944 -0.007245479281661356; -0.002554600935112567 -0.01096100982326245 -0.012099181529422664; 0.005422444711875889 0.013466066113401143 -0.0166507813019829; 0.0007338178985089813 0.006569321448699959 -0.015968567138072806; -0.003136542142771942 0.010155869478966422 -0.017300793981494318; -0.0011011109121417293 -0.00012980067096383734 -0.00048275990410788006; 0.0004235895094584605 0.003148129028830002 -0.008958920145506893; -0.04910236995625754 -0.012588907599768705 -0.048158185760136925; 0.04199027499927661 0.035448172109264466 -0.09062488681451807; -0.04791273078343572 0.011727716419575028 -0.047272718677865505; -0.0018249275672727492 0.006005840853791425 -0.010446037194004018; 0.002119881482108707 0.011972106282158501 -0.027495363672693368] %
+
+Mass Used: 114.14700676685197 kg
+Launch C3: 95.0549437834814 km²/s²
+||V∞_in||: 5.536764104134689e-5 km/s
diff --git a/archive/ES_0.5731257657062625 b/archive/ES_0.5731257657062625
new file mode 100644
index 0000000..6657cd6
--- /dev/null
+++ b/archive/ES_0.5731257657062625
@@ -0,0 +1,22 @@
+archive/ES_0.5731257657062625---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T11:09:01.475
+Launch V∞: [7.565620914456208, -5.683132511154015, 0.6128928426837514] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5991970816993442e-5, -0.0012925168771185508, -1.669129996181203e-5] km/s
+ V∞_out: [-0.001253390241205229, 0.00015304753331444747, -0.0002711330787499879] km/s
+ time of flight: 1.805180024489074e8 seconds
+ arrival date: 2030-01-22T19:02:23.475
+ thrust profile: [0.8034102871260342 -0.002632713552023468 -0.13851680898313737; 0.2872053034203572 0.19004495084404463 -0.18773293212979655; 0.13023062303465754 0.14618328583282586 -0.16031089709417762; 0.059738468983588366 0.09220251909802536 -0.11398440484977336; 0.04984634843328802 0.10007129265519879 -0.13142379334859905; 0.022683395121114076 0.056159909661660866 -0.08029405099920943; 0.0037653717324976107 0.011599858889881732 -0.017830594546212764; 0.0036474723262759643 0.003145115680651426 -0.0060712089621790645; 0.001694910168564903 0.0027839743973885247 -0.006328118207651547; 0.001012205782758429 0.014664302008264895 -0.020607951072176337; 0.0007502680254935278 0.0013451613255482276 -0.0027167543077108013; -0.00028993243791162224 0.0017070199003251778 -0.0034336166995128864; -9.348362326648725e-5 0.0031119572751978734 -0.008202445349637356; 0.00036858357276083384 0.0006024896241245499 0.0006708990632363003; -0.002509474137282664 -0.0010070848353909182 -0.00555510827883045; 0.0036219204513632647 -0.0008533925424158285 -0.004502226820289788; -0.003628431441646745 0.00018535837021846347 -0.0021349328455015693; -0.005636962369767419 0.009618622669770958 -0.005689090101395109; -0.00041417668218657463 0.0007676399636227973 -0.001708191531091323; 0.0007744510608916229 0.0008735901779708686 0.004231465658525075] %
+
+Mass Used: 144.15858650693872 kg
+Launch C3: 89.91225259720588 km²/s²
+||V∞_in||: 0.0012927235668391435 km/s
diff --git a/archive/ES_0.5731445290373638 b/archive/ES_0.5731445290373638
new file mode 100644
index 0000000..841ebe1
--- /dev/null
+++ b/archive/ES_0.5731445290373638
@@ -0,0 +1,22 @@
+archive/ES_0.5731445290373638---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T13:57:13.949
+Launch V∞: [6.504204868027722, -7.252440759087243, -1.0175434276255169] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.596768190440077e-10, -1.6311164103307058e-9, -3.0713052202547413e-12] km/s
+ V∞_out: [5.085595264601227e-10, -1.1589965994336048e-9, -1.5591903120463462e-9] km/s
+ time of flight: 1.8481156448340115e8 seconds
+ arrival date: 2029-03-04T14:29:57.949
+ thrust profile: [0.36674583415746353 -0.09159963850588403 -0.12384756948672355; 0.15951036054288206 0.0534374028706149 -0.15203788629942125; 0.07419222611455538 0.04778195546509682 -0.11944313136576513; 0.09455054822804598 0.08578300564951132 -0.2128880188790302; 0.03688301431902925 0.04160362298389785 -0.11089456397008479; 0.0336607310704963 0.04525088644850131 -0.1264406167797817; 0.021766246688770946 0.0335910931319078 -0.09877165169583722; 0.010276731975986714 0.017858656153281624 -0.0553152483154992; 0.000177095937434796 0.0010098925469452474 -0.0024971832655224942; 0.00041185853215349973 0.0003954413070389243 -0.003757174403138207; -0.0007215065348260253 0.001214698771359951 -0.00644923077249403; 0.0003537264045970802 -6.716606889296459e-5 -0.0011965886875685526; 0.0002519747052231459 0.0006306470433823821 -0.0031049017718768365; -1.3485383942210636e-5 -0.00020803151538205744 0.0014332648195740268; -7.578424116204342e-7 0.0007696150073258287 0.0004504963320329106; 0.0003883660733181169 0.0017226063723555036 0.0014250261464247133; 0.00115670655809488 -0.0005696923298348611 0.0023643931955195895; -0.0004555306438450901 0.00016775800485149958 -0.00039076723475939257; -0.0006210266018301282 0.000500822555384369 -0.0008078552209553401; -0.000537913414615605 -0.00039447596294229636 -0.005585191406213926] %
+
+Mass Used: 109.03044396430323 kg
+Launch C3: 95.93797255644935 km²/s²
+||V∞_in||: 1.638916368673489e-9 km/s
diff --git a/archive/ES_0.5731695342789618 b/archive/ES_0.5731695342789618
new file mode 100644
index 0000000..4bf43ee
--- /dev/null
+++ b/archive/ES_0.5731695342789618
@@ -0,0 +1,22 @@
+archive/ES_0.5731695342789618---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T17:56:12.864
+Launch V∞: [7.600297166323754, -6.278939818713831, -1.6186284915858666] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7427224231058413e-9, -1.8198924056537116e-10, -1.1770318031697093e-9] km/s
+ V∞_out: [1.7385085105801773e-9, -1.2617442140900772e-9, 6.36823290878994e-10] km/s
+ time of flight: 1.63231726542504e8 seconds
+ arrival date: 2029-07-11T00:04:58.864
+ thrust profile: [0.24575836222519626 -0.045492497109413124 -0.10587131428941048; 0.05418515895077898 0.02059666367554942 -0.06885585171789106; 0.06988375600978271 0.04831104149718952 -0.15616672724891625; 0.0541069149347133 0.04959244007365248 -0.17575279956185888; 0.014495498814764517 0.015713436701027095 -0.06435497803525549; 0.036221337158450904 0.050633114547302085 -0.1881959029885975; 0.020238785992697666 0.032493141784483655 -0.13046483145143603; 0.011516781050373941 0.02017285639056371 -0.08559115081848909; 0.006529579568300342 0.011074692408550416 -0.05188078268091874; 0.003533571667803038 0.006046655771452154 -0.030863319746043203; 0.0015481572069535974 0.002777815848321739 -0.014957219931383672; 0.00013816312634486029 0.0001970619645455767 -0.0010016754839567564; 5.6648029484525055e-5 0.00022752118685726326 -0.0014725427484485172; 0.0003110426443808799 9.151815072880472e-5 -0.000827728442920425; -0.0001897948077235936 0.00012182224016368272 -0.00023432430718804673; -0.00023170834787117345 0.0005534476422853611 -0.0008090432398606751; -0.00034079289767042326 -0.00022208812454130623 -0.0010207978621033474; -9.21093064432831e-5 6.79023994756006e-5 0.00022864838404304424; -0.000942650368111819 0.00012444249712083652 0.001371475611298422; -2.83915666004679e-5 -0.00022932985159974793 0.0019014726526243707] %
+
+Mass Used: 86.47535399159915 kg
+Launch C3: 99.80956045723251 km²/s²
+||V∞_in||: 2.1108304984887803e-9 km/s
diff --git a/archive/ES_0.5732348572632244 b/archive/ES_0.5732348572632244
new file mode 100644
index 0000000..62d690a
--- /dev/null
+++ b/archive/ES_0.5732348572632244
@@ -0,0 +1,22 @@
+archive/ES_0.5732348572632244---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T00:15:57.605
+Launch V∞: [7.200891949093761, -6.827386089603173, -0.2473667377911997] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.212936420491373e-8, 1.2430982054522838e-6, 6.550476401549458e-7] km/s
+ V∞_out: [9.71543944151611e-7, -8.788678310121838e-7, -5.15077565478258e-7] km/s
+ time of flight: 1.50257954528508e8 seconds
+ arrival date: 2029-02-11T02:35:11.605
+ thrust profile: [0.17696139970568253 -0.05048132085266959 -0.07713963780957867; 0.18515579141509936 0.03374903373078155 -0.21598758910737983; 0.10291388099932208 0.03986216317903803 -0.19987141912696246; 0.06330251734545471 0.03239990818552994 -0.17046766881066958; 0.05349189636697719 0.031809116400769465 -0.1806539568904921; 0.039265101479888716 0.02574668514297373 -0.15835935098628032; 0.03314992219139186 0.023394523113812724 -0.15334757175538447; 0.020457995354854264 0.015566798263845133 -0.10686163416747664; 0.0018322176621802125 0.0013055218787726111 -0.013266906592041957; 0.0016123729851112141 0.0011951584328604209 -0.010912011642655733; -9.33059179937547e-5 -0.0001276403107883569 -0.000830143018464602; -0.00017860857816115824 -2.0986428189870502e-5 0.000609746710086453; -0.0004923917125787397 -0.0004357365299976239 0.0019702774009734657; -0.00047728483835651726 0.00021318357038016883 0.0020218955421051127; -0.0016190118391205305 -0.0001277820880861575 0.002272509258621397; -0.0005136899239769478 0.00032718365098077193 -6.950147408532061e-5; -9.576686435026018e-5 4.018725540940208e-5 0.0025870314539873504; -0.0011099698263871607 -0.0020712193844213077 0.0046765064708154894; 0.00232154064522768 0.0013660578932491278 0.00011990151168482098; 6.744659308497304e-5 -0.0012351639186729475 -0.003455028299078414] %
+
+Mass Used: 94.03179024545352 kg
+Launch C3: 98.52723598199572 km²/s²
+||V∞_in||: 1.4064994195404982e-6 km/s
diff --git a/archive/ES_0.5732358841440162 b/archive/ES_0.5732358841440162
new file mode 100644
index 0000000..1264bd2
--- /dev/null
+++ b/archive/ES_0.5732358841440162
@@ -0,0 +1,22 @@
+archive/ES_0.5732358841440162---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T20:37:32.431
+Launch V∞: [7.762271157904532, -6.334179851805588, -0.6781707190400755] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.276166797571474e-5, 5.295306532613354e-5, 3.9193941836880244e-5] km/s
+ V∞_out: [8.286775916053859e-6, -5.780185651431445e-5, 6.988284766549179e-5] km/s
+ time of flight: 1.8749577782590047e8 seconds
+ arrival date: 2030-05-01T22:47:09.431
+ thrust profile: [0.359222589463848 -0.04826721413012898 -0.1358457065963867; 0.04756703631811296 0.010598980804580877 -0.07907108215540998; 0.03391709276463777 0.01042615198163447 -0.09946247257837125; 0.01875637718472166 0.005462565157961036 -0.07712564260688035; 0.017232571497484386 0.004153681282846881 -0.09032416184614593; 0.012758599023897753 0.0020464811666112046 -0.07913172221986205; 0.009217879678228416 0.0011005068156023157 -0.06393720497477082; 0.00887362534859843 0.0006791587809846397 -0.06441324154699722; 0.008327590832264647 0.000564346629523961 -0.06598066714754246; 0.002321475337729552 -0.0002456390499597041 -0.018732631126628905; 0.0019841966023874877 -0.00019467955287905527 -0.017524416125835315; 0.00022400184994973758 -3.7295707938174785e-5 -0.0016057235950027525; 0.0006610443605191483 -0.0004528521794549261 -0.0037741213107822316; -0.00013047729560838122 -0.00010981555791814997 -0.0009987464448260968; -5.257021799289169e-5 0.00011932800198500539 -0.0005741452298378099; 0.00013978058453045574 9.52225196751541e-6 -0.00023215706376094995; -0.0002450396201266926 -0.00018211957527205987 0.00018765746602503712; 0.0004965468347127549 -0.0003457421145018865 -3.441718107632073e-5; -0.0003061919642992235 -0.00044660065491257606 7.918570562622884e-5; 0.00029969970521870153 6.858896073483572e-5 -0.00017357674704152276] %
+
+Mass Used: 80.57334472123694 kg
+Launch C3: 100.83460344801975 km²/s²
+||V∞_in||: 9.09902147004851e-5 km/s
diff --git a/archive/ES_0.5732793653167936 b/archive/ES_0.5732793653167936
new file mode 100644
index 0000000..810cf9f
--- /dev/null
+++ b/archive/ES_0.5732793653167936
@@ -0,0 +1,22 @@
+archive/ES_0.5732793653167936---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T02:17:26.190
+Launch V∞: [7.468262605993037, -6.733566702561323, -0.716082501308801] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002141133378575923, 0.009097643648386158, -0.0128384355306923] km/s
+ V∞_out: [-3.305229680733287e-8, 1.1044321358990856e-6, -1.2419428104992415e-8] km/s
+ time of flight: 1.721841918753685e8 seconds
+ arrival date: 2029-10-31T23:13:57.190
+ thrust profile: [0.15992503858174373 -0.024142579975236774 -0.07503573780257755; 0.06937665077982447 0.019178085258927714 -0.0991392491168198; 0.049885700161826196 0.022668673395689766 -0.12356157082472223; 0.03825069891876721 0.021200850458479244 -0.13432328397315377; 0.023608148660609035 0.013841380801789606 -0.10536395087968235; 0.01851109123630593 0.011428415353351597 -0.09949926835810141; 0.019605465179056956 0.012841849542531161 -0.12193407447359815; 0.01518351778809413 0.01001649101404186 -0.10578892649605481; 0.002632517784501226 0.001509833421183133 -0.020689082483571562; 0.0021482583627370805 0.0011676129155676256 -0.017845879465980152; -0.0003000342651506699 -0.00045160902729563185 -0.004050374324757005; 0.0008120615926063743 0.00048556047161088376 -0.005193173603234712; 0.0006760581177140076 0.0005195486959531669 -0.0012701917203018632; 0.0009878070880482562 -0.002754626221383883 -0.003054484439578067; 0.002284744333304143 0.000774824221035795 -0.0026943347363857953; 0.001676209004503932 0.0033521473532130766 0.0006614046521593499; 0.00626536199650066 0.008254320659654035 0.0018194829498662723; -0.0001971652034866928 -0.0010525338429914401 0.004246725463099812; -0.0009494343209640326 -0.000514663715711689 0.005697086854168431; -0.0010575450392130508 0.0012024181846806451 0.006551310657403546] %
+
+Mass Used: 75.99218681110915 kg
+Launch C3: 101.62864103859714 km²/s²
+||V∞_in||: 0.01588008183145211 km/s
diff --git a/archive/ES_0.5733167082321495 b/archive/ES_0.5733167082321495
new file mode 100644
index 0000000..168385a
--- /dev/null
+++ b/archive/ES_0.5733167082321495
@@ -0,0 +1,22 @@
+archive/ES_0.5733167082321495---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T17:31:03.221
+Launch V∞: [7.324694971549301, -6.222791969771397, 0.06267681074428494] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.650891462590507e-7, -2.4605757136238195e-6, -7.1572840791918365e-6] km/s
+ V∞_out: [-6.878337918303908e-6, -8.375273653455699e-7, 3.1379320458195177e-6] km/s
+ time of flight: 1.6456403404563966e8 seconds
+ arrival date: 2029-07-23T09:44:57.221
+ thrust profile: [0.5884123897631671 -0.0747587612521641 -0.164466172916983; 0.26201522567086055 0.11405735330401594 -0.22472647386888908; 0.10561577960563669 0.08116977461660882 -0.16159647203164268; 0.04378377654001462 0.044138281484060994 -0.09493965853544174; 0.05095332706747861 0.06425271181602832 -0.15137949667445197; 0.056428758360411634 0.08602803895003981 -0.2014326895589684; 0.018241342905634728 0.0330010981280415 -0.08336467501328367; 0.003222895569565707 0.007211278228357939 -0.021690860160821463; 0.0064320141943261504 0.003805987585291569 -0.015980740275826327; 0.006170570651133598 0.006726771321265392 -0.016458653955666327; 0.00021283828788675211 0.0011661890465109984 -0.0027218909076475936; 0.003948165209279337 0.0032936163048313837 -0.003038049275760902; 0.0001531169204199538 -0.0006321532131890783 -0.0017941586049224352; -0.0013701234320274151 -0.0007188519100084221 -0.0007989510845897957; 0.00044229537298897076 -0.0028689353614776377 0.005498266747969011; -0.02119191422067364 0.012638291750560141 0.006193016363603059; 0.004646832930885185 -0.004227221831364732 0.004073301912182702; -0.0175168442925248 0.008001052566078429 -0.0357869473287479; -0.005768756865646296 -0.0053011999922625225 0.005834658063404108; -0.004552728782921378 0.018005751768739163 -0.023981176477930626] %
+
+Mass Used: 129.9965154747806 kg
+Launch C3: 92.37822470789608 km²/s²
+||V∞_in||: 7.607003985436823e-6 km/s
diff --git a/archive/ES_0.5733355225261525 b/archive/ES_0.5733355225261525
new file mode 100644
index 0000000..991d4e0
--- /dev/null
+++ b/archive/ES_0.5733355225261525
@@ -0,0 +1,22 @@
+archive/ES_0.5733355225261525---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T01:05:13.239
+Launch V∞: [5.729036958563012, -7.953630219819011, -0.21564895654287436] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.796383539978394e-5, -7.461321256773643e-5, -9.536394092697746e-5] km/s
+ V∞_out: [-0.00011394650808032842, -7.923232372454769e-5, -3.7486589391648445e-6] km/s
+ time of flight: 1.5623405131047067e8 seconds
+ arrival date: 2028-04-05T07:26:04.239
+ thrust profile: [0.3559726760536102 -0.17186047089081216 -0.14066979413020694; 0.10182035587929109 0.0052335281255740974 -0.104828075546936; 0.07822439373946462 0.02150712322449798 -0.1275847291434453; 0.14666239124539532 0.060962726838846584 -0.30522843299694036; 0.05819520379246352 0.03162492631472643 -0.15924837686426763; 0.05462041233937651 0.0341019114031393 -0.17475871130180273; 0.01740829700443273 0.012059088485735883 -0.06765865408690577; 0.020841648530392845 0.015152048929082843 -0.08782820843316909; 0.014228850542256076 0.011316418567132648 -0.0650402199199401; 0.009153765988083273 0.007478972012943104 -0.0437342066930461; 0.0019802441604195187 0.0016645170937644258 -0.008308627119094551; 0.003058451737435811 0.00315859735187555 -0.01041645850823733; -0.0002445037210075671 0.0004033447362399794 0.0001342436078755221; -0.00036429792028504313 0.00020276857865715676 0.0024561202669214775; -0.0003145271457330219 -0.0014038087786764377 0.003314560068292129; -0.0005296676580870166 -0.005325052539859631 -0.0014026501956851023; 0.0004094957721419604 -0.0006953520960300097 -0.000658862885855288; -0.002882952314640359 0.0015409238039848982 -0.001375515546859301; 0.0013109601909793744 -0.0005273499397570402 -0.0017886134659470376; -0.0002993852139632738 0.003329520643863253 -0.002609324696779304] %
+
+Mass Used: 108.14126100501107 kg
+Launch C3: 96.12860261865717 km²/s²
+||V∞_in||: 0.00013885422442637887 km/s
diff --git a/archive/ES_0.5733496731121001 b/archive/ES_0.5733496731121001
new file mode 100644
index 0000000..cf5dfa2
--- /dev/null
+++ b/archive/ES_0.5733496731121001
@@ -0,0 +1,22 @@
+archive/ES_0.5733496731121001---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T20:04:01.663
+Launch V∞: [6.518871623695912, -7.297538426105179, 0.4206634507208305] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5315209921067645e-5, -2.0778170971044242e-6, 4.0378829255357467e-8] km/s
+ V∞_out: [2.9549507321495785e-6, -6.826372918563134e-8, -1.516174715040302e-5] km/s
+ time of flight: 1.874957778747709e8 seconds
+ arrival date: 2029-04-04T22:13:38.663
+ thrust profile: [0.21770932459907788 -0.03966948586746782 -0.057801470265494155; 0.24968759123978412 0.09911182335674912 -0.16172150036755975; 0.0890868323859141 0.06711895469552319 -0.10983418128030403; 0.07090243845960324 0.07345482166295084 -0.12375431694903027; 0.07631868113560698 0.09822246375115891 -0.17008243314830823; 0.06009873849397608 0.09254970845921427 -0.16689991746446192; 0.01010654283044992 0.01629631164864054 -0.03626813747988249; 0.005860121822888073 0.010298362854045832 -0.024330348914330432; 0.0022383145606437813 0.004724351010608288 -0.011926167220656862; 0.0010937306901108767 0.0007783716586453617 -0.004072188839840507; -0.0003006805659635332 0.0002435202533149815 -0.001808031138441636; 0.00020927069356251808 0.0006578733452620917 0.0035349837888092803; 0.0021111136348016357 -0.009553586403676408 -0.0012825749976278626; -0.001097989991235955 -0.0023068042168821043 0.006107353978036381; -0.00764376661452053 0.011685270415534433 0.0081744946040062; -0.00236251803267216 -0.013562381864509629 -0.0007447802566283521; -0.0008108354757441428 0.0065221202031200045 -0.003613865248984871; -0.013749435403906881 0.0018130898783420683 0.00783381862608809; 0.0003894212331867308 0.0017466162815205689 -0.003702627358955807; -0.009323206480901309 0.023673986328167217 0.015073379692837402] %
+
+Mass Used: 109.33546491547304 kg
+Launch C3: 95.92671206548178 km²/s²
+||V∞_in||: 1.5455568875497283e-5 km/s
diff --git a/archive/ES_0.5733607874965504 b/archive/ES_0.5733607874965504
new file mode 100644
index 0000000..d9d4e9b
--- /dev/null
+++ b/archive/ES_0.5733607874965504
@@ -0,0 +1,22 @@
+archive/ES_0.5733607874965504---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T08:48:46.329
+Launch V∞: [7.184617932226176, -6.730415476083287, -0.31274569686175385] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0003946577466907974, -0.002842629947617559, 0.0015934710924918238] km/s
+ V∞_out: [0.001252027034535511, 0.002575365445985943, -0.0016024828007927192] km/s
+ time of flight: 1.5114777574080798e8 seconds
+ arrival date: 2029-02-20T18:18:21.329
+ thrust profile: [0.3672196183636577 -0.0997894742921729 -0.14606243701307808; 0.09759431728741895 0.021353087241934014 -0.11114676136253873; 0.09087363247983815 0.040172032947391384 -0.16851521716157813; 0.0673288304637959 0.039478025547008855 -0.17326676679623942; 0.06231835429705774 0.043013134345329065 -0.20216362206267524; 0.040631254644148726 0.031427730496362834 -0.15958399314144367; 0.02533922664291529 0.02123784949554057 -0.11109110451165904; 0.021599015983660506 0.01816083689226996 -0.10527708253179041; 0.013878767090280474 0.013031145900700328 -0.0800915745135611; 0.003085428650112804 0.0030451882296394475 -0.019347730143742792; 0.0009100241514366373 0.0006205693135466543 -0.005297587321677212; 0.0024319637366994767 0.0009280251374306592 -0.00284079630293752; 0.0002883930332870178 -0.000181316745844195 0.0012298955187162533; -0.0015311390656915069 -0.002844573633506324 -0.0024949788087362014; 0.003956286250893197 -0.0003475941801465058 0.002867234603230427; -0.004775643816882468 -0.0013105506636642357 -0.007194645308618237; 0.0010661199055282855 -0.002268870753610781 -0.002281696597905083; 0.006251920314078781 0.0012105762051163 -0.007279480391592076; 0.004746045093212264 -0.006445543482535372 -0.006480034464596883; 0.005984343425052848 -0.0013700435151686823 0.002030716996979506] %
+
+Mass Used: 102.99986850788355 kg
+Launch C3: 97.0150371836729 km²/s²
+||V∞_in||: 0.0032825980379453026 km/s
diff --git a/archive/ES_0.5733639266801209 b/archive/ES_0.5733639266801209
new file mode 100644
index 0000000..e1c613d
--- /dev/null
+++ b/archive/ES_0.5733639266801209
@@ -0,0 +1,22 @@
+archive/ES_0.5733639266801209---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T20:16:24.059
+Launch V∞: [7.7861246722568875, -5.9851665749501874, -0.16274206586439932] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0998944309733087e-7, 1.573477715682375e-6, -3.0300092341397398e-5] km/s
+ V∞_out: [-1.133642412022107e-6, 3.0314750360260714e-5, -3.184930835073519e-7] km/s
+ time of flight: 1.7209363935790464e8 seconds
+ arrival date: 2029-10-21T16:03:43.059
+ thrust profile: [0.2974244530026626 -0.032147140939277175 -0.10102895800758359; 0.1235626774165784 0.05088977900183412 -0.13231011452711816; 0.0881180987917274 0.061631460158011464 -0.1622577014278513; 0.06381094092320487 0.05812695175908429 -0.1666896058047834; 0.0396737977893646 0.04338658771528316 -0.12790934011525784; 0.018854660606478425 0.033351019888310754 -0.10242491928657023; 0.008888663776134863 0.016782485106478333 -0.052399183875558974; 0.0073815553990677525 0.015164973647989391 -0.05054273103251194; 0.004116171202987798 0.009072668546722347 -0.033098688792593756; 0.0022913009614704415 0.0070900161980947535 -0.024366223242340515; 0.004235377924219666 0.007042569399588649 -0.03312879429701594; 0.005354744874531785 0.00751926115551318 -0.02155848089019881; -0.002607143637305552 -0.012947192245267398 -0.007986103645124518; 0.002823498390585588 0.004182335957593068 0.0006897656685501755; -0.007679561288360905 0.009424935262151638 0.006761224203572204; -0.0006463185397408488 -0.022598253984119698 0.0015501391854624812; 0.0145087289626411 0.01658462809279852 -0.0041358748601469965; -0.02624637085470442 -0.02402196392912331 0.010734866144165783; -0.023032038000095085 -0.007736604742559541 0.005920439698040782; -0.003968780264060768 0.011658276668182657 -0.04294463627453698] %
+
+Mass Used: 106.1686734161317 kg
+Launch C3: 96.47244132183019 km²/s²
+||V∞_in||: 3.0341646685458103e-5 km/s
diff --git a/archive/ES_0.5733656912971795 b/archive/ES_0.5733656912971795
new file mode 100644
index 0000000..a407138
--- /dev/null
+++ b/archive/ES_0.5733656912971795
@@ -0,0 +1,22 @@
+archive/ES_0.5733656912971795---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T12:00:55.077
+Launch V∞: [6.119292894174716, -7.556354780991922, 0.03268199467946321] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6229323292568978e-8, -7.157146406377139e-9, 2.1973332123199596e-8] km/s
+ V∞_out: [5.889880883738686e-9, -1.713176723452525e-8, -2.2500918825923025e-8] km/s
+ time of flight: 1.7449638357682037e8 seconds
+ arrival date: 2028-11-05T03:13:58.077
+ thrust profile: [0.45167121845356956 -0.15038332355508285 -0.15189699601096707; 0.1128397865384114 0.019542486487418777 -0.1076719783570275; 0.06951855487397093 0.027655032256785922 -0.11079105727192542; 0.05951866764308615 0.038232340794287265 -0.12370677986779365; 0.05405127074377153 0.04490285375419779 -0.14269969664182344; 0.03299122390629217 0.026556229198334752 -0.10513534689195131; 0.02020602886256304 0.019476462838887605 -0.07775578027180476; 0.026936663472234067 0.027565643597651974 -0.09062756887260554; 0.005624752318035175 0.013098311559766004 -0.03980555641610498; 0.003954592825572662 0.012257959874749884 -0.05239913829908054; 0.004515506848058218 0.009108674009986502 -0.05083430720947282; 0.001649007142410286 0.004035599538058282 -0.024982732052805656; -0.0025637579142502006 -0.002595340295308961 -0.0003257178320720186; 0.005411321781347478 0.002660687031811372 -0.004890230223795323; -0.006095392567697188 0.008865621375199103 -0.019643609601542503; -0.0005717189792785698 -0.0007750150716532489 -0.00013657647066165485; 0.0010756627298949542 0.020583843503484647 0.009150690387164062; 0.012827739577420052 -0.027695509283656276 -0.012819601101442922; 0.007823885091924384 0.00330948574628508 0.0074639372277536115; -0.011409358691276631 -0.020158133861531605 -0.0156801357762813] %
+
+Mass Used: 117.412324433501 kg
+Launch C3: 94.54531121369287 km²/s²
+||V∞_in||: 2.8239033337093437e-8 km/s
diff --git a/archive/ES_0.5733892823103109 b/archive/ES_0.5733892823103109
new file mode 100644
index 0000000..b5c49a7
--- /dev/null
+++ b/archive/ES_0.5733892823103109
@@ -0,0 +1,22 @@
+archive/ES_0.5733892823103109---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T11:05:22.888
+Launch V∞: [5.551993581455543, -8.067269491891068, -0.3782277780792332] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001961114047176399, 0.0012352548798448691, -0.0010889627799012657] km/s
+ V∞_out: [0.0013068542521200081, -0.0018767239992327157, 0.0011519540161339572] km/s
+ time of flight: 1.530300016460045e8 seconds
+ arrival date: 2028-02-28T15:25:23.888
+ thrust profile: [0.3440669746430718 -0.17961985033130917 -0.13729636168666298; 0.17450692558310088 0.003161696300768734 -0.17627875873622345; 0.11229146591444175 0.02687626002911253 -0.1815576736785305; 0.08511187890097804 0.03212703713944664 -0.18528832696033493; 0.07472840729474958 0.036332779213219986 -0.20060416378598095; 0.05865063099491953 0.033147502144275275 -0.190835064527698; 0.021054526135056584 0.013073031736809477 -0.0788398897656556; 0.02317293099506069 0.01549872354413622 -0.09567590917045093; 0.0119704489582501 0.008608345967567202 -0.05488877274279948; 0.0036145164714092375 0.002296248851368612 -0.016345950850634988; 0.002475249634206976 0.0021843827663585147 -0.013299008010206803; 0.000336707662315595 0.00026005528720401093 -0.002007141364788332; 0.00026718642976217624 0.00021892968256128075 -0.0016647342570829265; -1.0641046302151026e-5 -0.00010076119147516224 -0.0009229342335646506; 0.0002645429932430962 0.00029487907597503394 -0.002458755164272473; -0.00022857851133582563 0.0010515134582565738 -0.0011849182231785777; 3.855931664989903e-6 -0.0002182437478232526 -5.2742405679571036e-5; 0.0008967247331398285 0.0004279884875360661 -0.0007359012636634331; -0.0003352580349746619 -0.00032865798094273356 0.001304147023627274; 0.00017335278930054882 0.0005085571497037023 -0.0010560551642345693] %
+
+Mass Used: 108.6710941553506 kg
+Launch C3: 96.04852603543065 km²/s²
+||V∞_in||: 0.002560793404440009 km/s
diff --git a/archive/ES_0.5734029969163971 b/archive/ES_0.5734029969163971
new file mode 100644
index 0000000..2a8ee59
--- /dev/null
+++ b/archive/ES_0.5734029969163971
@@ -0,0 +1,22 @@
+archive/ES_0.5734029969163971---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T12:11:40.269
+Launch V∞: [6.5625630317524495, -7.435840952141529, 0.13380651798577384] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001247692079425386, 0.0011267287187515238, 0.0013083576587883058] km/s
+ V∞_out: [-0.0014927073451659464, -0.0007313170055936421, 0.0013322617807531377] km/s
+ time of flight: 1.8533129153158152e8 seconds
+ arrival date: 2029-03-15T13:06:31.269
+ thrust profile: [0.19699047149732013 -0.054479408273562575 -0.06609109303160571; 0.04002976855348574 0.009003042240035983 -0.04051781538257141; 0.03909002161226534 0.018323741231608962 -0.06873949028097671; 0.0668070589317688 0.04038255225286018 -0.1589262979850632; 0.046336245787969625 0.03460083838094722 -0.13884640217170502; 0.023356532031602446 0.020016175230897045 -0.08924660617020665; 0.005778006446247926 0.006770305345513093 -0.02902238024156489; 0.003919622385497616 0.012144431140860194 -0.0420254818188692; 0.008190866370311987 0.005687120065185735 -0.03929086600717722; 7.788538572108005e-5 0.0009042152222984152 -0.014095618552718955; 0.03540929384981631 0.03674566460593737 -0.2137402725478517; 0.003439483216847984 -0.006927714308693253 -0.007922780890863238; -0.007279213488853784 0.0022604111496029944 -5.9038395065031876e-5; 0.00016113240651155947 0.0002510366806027897 -0.017723756952804922; -0.007439013489892023 -0.005900677243948823 0.0038731523149391654; 0.01443921208790614 0.015805026797786947 0.011950389015760978; 0.0056920826770781325 -0.011309047895161132 -0.00654839670151778; 0.0023368376575356184 -0.0003548041788160672 -0.010954562805506026; 0.009182217858170885 0.006671781126168828 -0.024998050181252382; -0.00633594214300803 -0.018779899202622352 -0.035240016359723854] %
+
+Mass Used: 95.10509742857084 kg
+Launch C3: 98.37686839552441 km²/s²
+||V∞_in||: 0.0021302706152107323 km/s
diff --git a/archive/ES_0.5734495891002759 b/archive/ES_0.5734495891002759
new file mode 100644
index 0000000..0184cbb
--- /dev/null
+++ b/archive/ES_0.5734495891002759
@@ -0,0 +1,22 @@
+archive/ES_0.5734495891002759---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T16:25:15.450
+Launch V∞: [5.699994879629667, -7.969468070321092, 0.05256073005760959] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.004784152822456e-10, 4.791419520213202e-10, 2.6875017183921852e-8] km/s
+ V∞_out: [-1.4903744473605592e-8, -2.135988315775467e-8, -1.0766843112986925e-8] km/s
+ time of flight: 1.576432993167883e8 seconds
+ arrival date: 2028-04-22T06:13:34.450
+ thrust profile: [0.32611930065638467 -0.1528003533206751 -0.12568321976075342; 0.15381655193529492 0.009946008591219227 -0.15004547201890608; 0.09311099856740827 0.026598548306756762 -0.14683396211665636; 0.0887387587596783 0.03605083694777926 -0.18161153617739345; 0.07895292134706372 0.04173590770644538 -0.20318773541786167; 0.042122783115859465 0.026163081113785 -0.13296432001865185; 0.027007470810882395 0.019385116974140186 -0.09862243560880796; 0.025224125881626914 0.017346563575913503 -0.09716676931691724; 0.003673835503416004 0.0030214841283288133 -0.01772900149932569; 0.030890702005124178 0.023372510490300445 -0.13505501637378547; 0.0002163001405471291 0.00019205666906649084 -0.0013140913435996944; 0.0008718714507396715 0.0005199130211514602 -0.002498164801293504; 0.0006609394162162951 0.002843800749027599 0.000915107607965745; -0.00263026308900796 -0.0009567482724550714 9.985913658401677e-5; -0.00029617121744739496 -0.001390033104447969 0.0014505265187759516; -0.003962095508977807 -0.0039559157404281675 -0.0003169019485735372; -0.00016544444945315834 0.00019266250950566958 -0.00020812022701198994; -0.002959042259179697 0.004103720764323093 0.002798675572252547; -0.0012423402851305559 0.0013943055039169956 0.00027488911304838034; 0.0035550622929601448 -0.0024628561106842836 0.0007500053086787835] %
+
+Mass Used: 108.99462138856188 kg
+Launch C3: 96.005125582016 km²/s²
+||V∞_in||: 2.688841378096815e-8 km/s
diff --git a/archive/ES_0.5734840121557289 b/archive/ES_0.5734840121557289
new file mode 100644
index 0000000..d49a685
--- /dev/null
+++ b/archive/ES_0.5734840121557289
@@ -0,0 +1,22 @@
+archive/ES_0.5734840121557289---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-08T17:57:13.304
+Launch V∞: [6.4666739203029975, -7.825135545726853, -0.13345518340720502] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.051072669779868e-6, -6.693188626817506e-7, 1.4546175527709258e-8] km/s
+ V∞_out: [1.3239816776882755e-6, -2.254224995146353e-8, -4.920611986536491e-6] km/s
+ time of flight: 1.874957778196056e8 seconds
+ arrival date: 2029-04-16T20:06:50.304
+ thrust profile: [0.013747110721571518 -0.005080396911059695 -0.006582744789117045; 0.010947890392420275 -9.687446430191204e-5 -0.016048249563159343; 0.03108268549471951 0.002520950033522098 -0.07833107365844885; 0.03592141928828848 0.00296254863403084 -0.12488717430785969; 0.034464484211205515 0.001963886389720741 -0.14918549864777123; 0.025814176377659977 0.0003581514233226953 -0.1317035732689324; 0.0225699870663893 -0.000634741370350808 -0.12892958648336925; 0.015199414850985835 -0.0011451464119870323 -0.09645376103950297; 0.005130481419055353 -0.0011500957099272542 -0.03929541070185519; 0.0022414752619779738 -0.0009239268883080784 -0.016353096916943907; 0.0008577985631449184 0.002935512273268174 -0.0072312241308862485; -0.00035121814399974657 -0.003710364193452455 -0.005294161461364157; -0.001827784821527994 -0.0015822148961134495 -0.005232357240934887; 0.0003760189676764109 0.0038441400175135585 -0.004572640273090738; 0.0005569535732534048 -0.00030621307620898536 -0.0008365364947558922; 0.008488296631428995 0.0028233288244781194 -0.0014490363754066083; -0.00951666528832609 0.002639511875513978 -0.005296143597614095; -0.012765296286070451 -0.008910925389118175 -0.006492797220791934; 0.002501279190533424 0.0031644334047894905 0.003783504980823426; 0.0018312649843542077 0.01029078079337805 -0.013307477906401043] %
+
+Mass Used: 67.83218309374888 kg
+Launch C3: 103.0684281865031 km²/s²
+||V∞_in||: 5.095246259658232e-6 km/s
diff --git a/archive/ES_0.5735353728814503 b/archive/ES_0.5735353728814503
new file mode 100644
index 0000000..4a12e65
--- /dev/null
+++ b/archive/ES_0.5735353728814503
@@ -0,0 +1,22 @@
+archive/ES_0.5735353728814503---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T14:11:07.475
+Launch V∞: [7.323876628472513, -6.087073022021358, 0.28352921802442504] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.818566713236675e-9, 4.118816334357792e-9, -5.8598188211064565e-9] km/s
+ V∞_out: [4.946670946462392e-9, 9.00592859765059e-9, 2.539687892167158e-10] km/s
+ time of flight: 1.6177063092351073e8 seconds
+ arrival date: 2029-06-17T22:28:17.475
+ thrust profile: [0.8356238112646868 -0.15126224846040692 -0.23419670811320628; 0.2657712199508048 0.10141537422469903 -0.23117316290170736; 0.16119740914846042 0.11183021920352042 -0.24006888012654837; 0.09552971302814188 0.08938310147418903 -0.2042278759582654; 0.03874588648053897 0.04462008093763128 -0.11029962078289647; 0.028134287986934046 0.03763847751687746 -0.1005384292665074; 0.012068014597720255 0.018926361571664465 -0.05285618971109416; 0.004614031250072114 0.007281231806446677 -0.02092566091916678; 0.0028313499639841177 0.003244314229749557 -0.013809151229348376; 0.0011973955879204523 0.005240390852045214 -0.012148839371484062; -0.0003115215820230549 0.00181805334656194 -0.004575786474131166; 0.0013482221376443673 1.9565791061113783e-5 -0.0048301677786437725; 0.0023781371695403347 0.000837016700359726 -0.003248521307345189; -0.0004778746605375735 -8.332514205859295e-5 -0.00019430379215387619; -0.0014795849691194652 -0.0006746326120686189 0.0004736374157549609; -7.16774370610462e-5 -0.000824901765112089 0.0006013566306339785; 7.5789417793902e-5 0.0006124762209052084 -0.0003598105131609737; 9.627981767438358e-5 0.0006448704644763431 0.0003148817935157527; 0.0003721399442427644 -0.00210446750518181 -0.0010285757821635766; -0.0003089656125030961 -0.0012694947257109943 0.002068027722254298] %
+
+Mass Used: 139.6211770001437 kg
+Launch C3: 90.7720156619797 km²/s²
+||V∞_in||: 9.889134271270929e-9 km/s
diff --git a/archive/ES_0.5735361402496031 b/archive/ES_0.5735361402496031
new file mode 100644
index 0000000..386acbb
--- /dev/null
+++ b/archive/ES_0.5735361402496031
@@ -0,0 +1,22 @@
+archive/ES_0.5735361402496031---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T06:56:02.978
+Launch V∞: [5.638150007630752, -7.80663059279948, -0.25780964624269603] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0032991441223456444, 0.0033526360816389838, 0.004636506058284587] km/s
+ V∞_out: [0.0058154375199294525, 0.0031484885422269466, 0.0001567648254219475] km/s
+ time of flight: 1.6023324835579723e8 seconds
+ arrival date: 2028-05-20T20:10:10.978
+ thrust profile: [0.605009610627649 -0.2599434923140337 -0.2020222183509575; 0.18184660006589443 0.024966252061303814 -0.15846775133250632; 0.07762901096546558 0.031414338138904985 -0.11224030389043335; 0.0565473077399419 0.03280899079074769 -0.110809161941173; 0.05464709611811435 0.039247898893698834 -0.13154130117696217; 0.017910223782506323 0.014755735723389337 -0.05425063783207957; 0.06321377709658885 0.05521145948187376 -0.20266771098451616; 0.026365217138905817 0.02733854380969175 -0.09747106262544361; 0.04741263367275167 0.0548634599990357 -0.18477346978254705; 0.007878182666321015 0.00984896220994698 -0.03697370435766778; 0.00035078656226231414 0.0007591917944212586 -0.002687543606488987; 0.0026364969195129787 0.002418702028081263 -0.011681885710416383; 4.3514975843011056e-5 0.002568573252629515 -0.0018433221800935506; -0.0027290672488157128 0.0016725160137863368 -0.002135451588796836; -0.0008317378520191469 -0.001801051201560075 0.0008017778920090415; 0.00013192156121199226 -9.518676152501569e-5 -0.0004088255183742714; 0.0005712766985128205 0.0006377164568349615 -0.00010857540596965424; 0.0011624725558587613 0.00116649101612479 0.001566545119796384; 0.0011888346906547237 0.0007588489615015649 0.000510873031616168; 0.00012074368636334659 0.0039132625568754405 -0.0038842394705739676] %
+
+Mass Used: 127.79984883893167 kg
+Launch C3: 92.7986825346752 km²/s²
+||V∞_in||: 0.0066046732746158675 km/s
diff --git a/archive/ES_0.5735605109390886 b/archive/ES_0.5735605109390886
new file mode 100644
index 0000000..b490dfa
--- /dev/null
+++ b/archive/ES_0.5735605109390886
@@ -0,0 +1,22 @@
+archive/ES_0.5735605109390886---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T06:54:06.098
+Launch V∞: [7.350325452662261, -6.544123509749408, -0.18094306143473574] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.059349771686623e-6, -1.481356231366395e-6, 2.4858757919898526e-6] km/s
+ V∞_out: [1.4124781395948344e-6, 2.7378557212227056e-6, 9.064791362438129e-8] km/s
+ time of flight: 1.5490547487602264e8 seconds
+ arrival date: 2029-04-04T04:12:00.098
+ thrust profile: [0.26528308243900184 -0.06680920441329044 -0.10240126067479641; 0.16651695613274986 0.04046682767004672 -0.18033821512806136; 0.12222841518504479 0.057832648381219307 -0.22093620605770306; 0.09016683088317676 0.05603181998704854 -0.2267206253059107; 0.06705697866613076 0.049180460636821355 -0.21478367866407297; 0.0345436144976602 0.02774199541104339 -0.13378560894417932; 0.010733795707409104 0.009077977762374671 -0.048982440427763; 0.010568074807315508 0.010398390002833777 -0.056552007196934415; 0.0045023038645405035 0.004526069690777629 -0.026840879486280153; 0.0014402676623452007 -0.002805310225997089 -0.010487522865913021; 0.006871127095282195 0.007834646831565789 -0.007560181163375654; 0.0006123882299591057 -0.0007396187785565782 0.0005936410288616576; 0.003965070886030383 0.00805345130869146 -0.004542383561943614; 0.007836789259990698 -0.001107924036296943 0.0021221129710093656; 0.0015808789383571138 -0.0006002601773129421 -0.007278259126122644; 0.0028892752229821637 0.009815546472684261 0.0008816241512091929; -0.0005674623654835427 0.00046093716059568716 0.0029995045638019965; -0.006934148421129792 0.0013707468827715704 0.007135630017778973; -0.01195902428749317 -0.003812909526835567 -0.017920420780272506; -0.003086869232231293 -0.020460277842696013 0.023619036912619188] %
+
+Mass Used: 103.98806264832274 kg
+Launch C3: 96.88557716239096 km²/s²
+||V∞_in||: 3.081593204201639e-6 km/s
diff --git a/archive/ES_0.5735710513308498 b/archive/ES_0.5735710513308498
new file mode 100644
index 0000000..1c4bb73
--- /dev/null
+++ b/archive/ES_0.5735710513308498
@@ -0,0 +1,22 @@
+archive/ES_0.5735710513308498---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T16:49:16.857
+Launch V∞: [7.260080180293811, -6.148557075968389, 0.3503364999498026] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0037806110091268158, 0.02316017943603464, 0.029248438541354067] km/s
+ V∞_out: [-0.0156662570884299, 0.012906284351529731, -0.03146526582133399] km/s
+ time of flight: 1.6407493081961334e8 seconds
+ arrival date: 2029-07-15T17:11:26.857
+ thrust profile: [0.7759691326300413 -0.10969134294500378 -0.18049462387516219; 0.2778553905276457 0.12063604814372839 -0.20525910656074942; 0.15265411226326128 0.11975200935226912 -0.19942452916462353; 0.0567940338004492 0.06424722400885677 -0.11809564018798427; 0.033687206359614544 0.04822577627072811 -0.09476572235001915; 0.028450955366090613 0.050558719603261144 -0.10407798056723112; 0.024793115560887556 0.04911376322345875 -0.10090574527002157; 0.008943798076504559 0.016877072038947727 -0.04048330715570317; 0.006579146821727028 0.013474480707751578 -0.037060888829998494; 0.012973027004466524 0.0331513537048437 -0.0790845939385431; 0.00035362630399334835 0.0012910268267546214 -0.001951595548286009; 0.0011897740005955833 0.0005619469101031662 -0.0031795626499794834; -0.0022280470218269443 -6.60627130465892e-5 0.0031824922243332858; -0.0006133041199190778 -0.0008894036441928896 0.0005857465888132207; 0.0003884918868679492 0.000575861700802961 -0.002861995001239003; 0.0010712182451344282 0.0008372888212427995 -0.004040795132817664; 0.0017591010401665054 0.00414533580146196 -0.0017865124731788846; 0.00014623491306794566 -0.0008726209036907136 0.00977298933575707; -0.0009365041125385346 0.0018219904069738174 0.0014229884612673538; 0.0018004870007307216 0.0022078187607415976 -0.0013734902852603503] %
+
+Mass Used: 140.45474486304875 kg
+Launch C3: 90.63625400393305 km²/s²
+||V∞_in||: 0.037498774489561904 km/s
diff --git a/archive/ES_0.5735795055271431 b/archive/ES_0.5735795055271431
new file mode 100644
index 0000000..7359c4f
--- /dev/null
+++ b/archive/ES_0.5735795055271431
@@ -0,0 +1,22 @@
+archive/ES_0.5735795055271431---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T17:10:39.664
+Launch V∞: [6.4007862422650375, -7.897496991599107, -0.2154232144520485] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.094635011056471e-7, -0.00019373485974900047, 0.00013880230431534895] km/s
+ V∞_out: [0.00010861837706455129, 0.00020806973124911125, -4.321208395255599e-5] km/s
+ time of flight: 1.8749577782605654e8 seconds
+ arrival date: 2029-04-17T19:20:16.664
+ thrust profile: [0.03340326827054884 -0.012921742207981769 -0.01773658420897333; 0.030210783882318282 -0.0015693346496637945 -0.0502477582147636; 0.03606052590887629 -0.0009932682013527297 -0.10094228843432657; 0.03479173806462052 -0.004059600248241824 -0.1338147071841083; 0.026278010223143824 -0.004224903259042832 -0.12482089626959057; 0.024862723492498767 -0.006666088431357835 -0.13950457943067845; 0.012279693432260817 -0.003946738035101338 -0.0770901263937256; 0.008858418286727102 -0.003352706594137929 -0.06090930595421336; 0.008267156234127916 -0.0035195804556987266 -0.06114762523963172; 0.0060479758108768975 -0.0025888632020802304 -0.04714671506642598; -0.0001502306597712255 -0.0007057585248728735 -0.0019743128876700605; 0.0006980397486496197 0.0008128518263446006 -0.001139071650485914; 0.0011133244336510948 -0.0008249880682722062 -0.010698134149679255; 0.0007573136391542134 0.00014990486265957303 -0.0008760536002491397; -0.00025422877116532995 0.0006446457052981967 -0.0008576366011045404; 0.0006783094052613499 0.000545448578029828 -0.0012707948356637157; 0.0002822062078013134 -0.0002839675603161652 -0.0016511711047456465; -0.0001224082176107422 0.000533865975478725 -0.0008802227254520586; 1.006932656752812e-5 -0.00011091137221391615 -0.00017401067862886463; 0.00028492708668832723 0.0008369039654003607 -0.0006980448589933045] %
+
+Mass Used: 66.08566237360174 kg
+Launch C3: 103.38693041281118 km²/s²
+||V∞_in||: 0.00023832676520058505 km/s
diff --git a/archive/ES_0.5736312171058123 b/archive/ES_0.5736312171058123
new file mode 100644
index 0000000..f1bfc0e
--- /dev/null
+++ b/archive/ES_0.5736312171058123
@@ -0,0 +1,22 @@
+archive/ES_0.5736312171058123---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T07:37:16.610
+Launch V∞: [7.291025716003237, -6.782755487029236, -0.4096022507240029] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006709493193550441, -0.0022702692935353975, -0.003678545123919016] km/s
+ V∞_out: [-0.0038492325802404878, -0.0004006841096280321, 0.002039163303952287] km/s
+ time of flight: 1.510493583806075e8 seconds
+ arrival date: 2029-02-20T13:46:34.610
+ thrust profile: [0.1703459827282152 -0.04983719566660125 -0.07587363632088796; 0.07922727732707893 0.013511899137042186 -0.09665291039171409; 0.09140551434676622 0.03312977973945321 -0.1834303947323738; 0.07622596578196686 0.03620782339967661 -0.21056986886368292; 0.06867095923839185 0.037758110412321653 -0.23786835206292378; 0.04226796704532865 0.025490153094001846 -0.17504459348841594; 0.02129233322810159 0.013781167358544053 -0.10117993923932679; 0.01075285185511303 0.007329366349943703 -0.0555208029367575; 0.008830449159364215 0.004308845861164311 -0.04604748035538325; 0.004784440714358157 0.0021611105741794418 -0.02771705965440575; 0.00018809908358925114 -0.0005572523244215186 -0.008658524162979986; 0.00031076462391744976 -0.0028160245346997566 -0.004434493966870826; -0.0016441070521183059 -0.0008214114400273984 -0.002143069121242595; 0.007486243737474138 0.002088202686598515 -0.0060369835720397854; 0.0017519099482407043 -0.0014002379712857308 -0.002423646697524865; 0.006005565912606553 0.0005650925151608188 -0.0019361384729067108; -0.009289627628162603 -0.004600044777619442 -0.004169371674590666; -0.0004653229284935882 0.0008700688226675635 -0.002144918291827551; 0.001328132033134464 0.0017085368370646555 -0.0020656192060514436; -0.005716021066825537 -0.009814952197892716 0.014047712555721969] %
+
+Mass Used: 89.79624166985832 kg
+Launch C3: 99.33260199204389 km²/s²
+||V∞_in||: 0.00437447024027151 km/s
diff --git a/archive/ES_0.5736996240745401 b/archive/ES_0.5736996240745401
new file mode 100644
index 0000000..e677d1b
--- /dev/null
+++ b/archive/ES_0.5736996240745401
@@ -0,0 +1,22 @@
+archive/ES_0.5736996240745401---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-08T22:32:31.557
+Launch V∞: [6.277932038578323, -7.927727167630044, -0.6855324364200989] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5180107538440303e-5, 2.3432322666481634e-6, -4.180769739543667e-8] km/s
+ V∞_out: [-5.695129621259343e-6, 7.159852523934713e-8, 1.4262612309759602e-5] km/s
+ time of flight: 1.857455910086508e8 seconds
+ arrival date: 2029-03-27T18:32:22.557
+ thrust profile: [0.11510190459189754 -0.04284029838956475 -0.05864901119207654; 0.00998710601788786 -0.00015722041734198453 -0.01675963196684572; 0.02237560433498763 0.0019945995556439897 -0.06069905955996888; 0.03331882767614581 0.0019209517140607116 -0.12352975414115233; 0.039165668167857055 0.000616923522344984 -0.1810904025300167; 0.030479557656514326 -0.000918513753235208 -0.166641731634102; 0.017684376818420267 -0.001110191824421941 -0.11112511619163772; 0.008109965227726463 -0.00040084512797393065 -0.05812008844682472; 0.0020991362244791984 -0.0006694794476353287 -0.017006528715313118; 0.001138748386381125 -0.0004156441801481549 -0.009095596701147797; 0.0027516320562534593 0.00011246375990720892 -0.02646849617075736; -0.00019272478437252528 -0.0006297497095742849 0.0007795514611102807; -0.00028035186561478225 0.00012137246749676283 -0.0035052156043805212; 0.0005529193897181817 -0.0007022965267146713 -0.001967029229123193; 0.0009129653737134846 -0.0005488172113417853 -0.0012195817305922555; 0.00048245882429453704 0.00151995124490096 -0.0008464165876440649; 0.0008086683848642547 0.0025509800825069323 0.0016005157844257727; -0.00017300496618203237 0.0007022718828640475 -0.00021474069915008857; -0.0002618661054469212 0.000542402829442687 0.0023650229182220327; -0.0012489916541874222 0.003014728680767297 -0.00139294701011498] %
+
+Mass Used: 70.05064131412837 kg
+Launch C3: 102.73124344677173 km²/s²
+||V∞_in||: 1.535995280649113e-5 km/s
diff --git a/archive/ES_0.5737025327582089 b/archive/ES_0.5737025327582089
new file mode 100644
index 0000000..1b92aeb
--- /dev/null
+++ b/archive/ES_0.5737025327582089
@@ -0,0 +1,22 @@
+archive/ES_0.5737025327582089---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T12:18:00.188
+Launch V∞: [5.590723890882658, -7.975794209110892, -0.20320260599229567] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.19000809277269e-5, -0.00011257889539942558, 1.2778544252375197e-6] km/s
+ V∞_out: [2.721125804947824e-5, -6.372244748885183e-7, -0.00014275176816948385] km/s
+ time of flight: 1.5580519439109308e8 seconds
+ arrival date: 2028-03-31T19:31:14.188
+ thrust profile: [0.48229470473714164 -0.23271068556538044 -0.18745226448228877; 0.07804525278224467 0.004419267384509755 -0.0814965576582977; 0.09502051085208887 0.025627481531320235 -0.15216156382986304; 0.06979983032637617 0.030704757598427015 -0.15609455109947065; 0.10581338724626367 0.05266037974317249 -0.266567676272269; 0.06241673086390436 0.03574571538801343 -0.1921922686283234; 0.030342112734096496 0.024227725986694558 -0.12127336442830858; 0.022157482094150735 0.013910763247207856 -0.07981056673947858; 0.00471059769294774 0.004337532224075514 -0.024848840949694875; 0.0026581394733219605 0.001879845321011096 -0.012621118953921397; 0.0003777322393926513 0.0011307809541593427 -0.005043295292327396; 0.006603564269395674 0.007182834779098802 -0.038855308889241824; -0.0007204249481182845 -0.0007377424411070694 0.002082560029054453; -0.0002981328607467099 -0.001505029926773364 0.0028794814895095034; -5.841130332214713e-5 -0.0005649335192948032 0.0027082548620928114; 0.002529878187912618 0.0024626871515699288 -0.005063764652632514; 0.00175515537559759 0.0003759093392878783 -0.002340837218817582; 0.0005488478975173294 0.0015717028066010775 -0.00625602154596545; -0.0055506407068158965 -0.007179648570801202 0.00459731023499221; -0.00011960461588793534 -0.0026073024482495205 0.0016130987531496653] %
+
+Mass Used: 115.67341544725605 kg
+Launch C3: 94.91077818925503 km²/s²
+||V∞_in||: 0.00014533157081587488 km/s
diff --git a/archive/ES_0.573727362062327 b/archive/ES_0.573727362062327
new file mode 100644
index 0000000..d143605
--- /dev/null
+++ b/archive/ES_0.573727362062327
@@ -0,0 +1,22 @@
+archive/ES_0.573727362062327---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T10:57:07.414
+Launch V∞: [7.621834086891873, -5.665958144324058, 0.3118494153838667] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.098333524014999e-10, 3.660755588277795e-10, 1.8692665910360156e-9] km/s
+ V∞_out: [-5.329279827095817e-9, 4.617928184483864e-9, -1.7727888819872766e-9] km/s
+ time of flight: 1.8630852546953776e8 seconds
+ arrival date: 2030-04-01T19:19:12.414
+ thrust profile: [0.6074019107289688 0.016684797645156985 -0.08849673595611196; 0.3677464338390595 0.2575977245103598 -0.19036202812384118; 0.09281985953150304 0.12149128891630408 -0.10896984979490348; 0.056069526591227964 0.10887545208466881 -0.10645717240614723; 0.03491324600056436 0.08944328320427512 -0.09683103598830883; 0.014998422043751234 0.04887711722760007 -0.05684867012373245; 0.0061351616969456515 0.02398505641106147 -0.02964988915189364; 0.009816094589795429 0.04773158669132712 -0.0625849836487587; 0.003139072211377725 0.02171269236581269 -0.029968464539949936; 0.0014759815254358848 0.01551497926803354 -0.02160224936531709; 0.00026294669698794285 0.006092432284537219 -0.007692289079602834; -0.00016401230398583602 0.003483771624913993 -0.003914997690098777; 0.005591247107748614 0.0015459725284144058 -0.0005329669964776971; 0.000760659083437841 0.0018613171330380555 -0.0022140725348927743; 0.002931087757841625 0.013497183745091419 -0.008414596862750786; 0.002867399085323473 -0.0003943388839537427 -0.007922389574390627; 0.007505287645317746 0.005756072121648345 -0.015875164215261445; 0.00010498570088708941 0.00024177793005063483 0.0005391318789535122; -0.0013385298524157632 -0.0007428766676553413 0.0056861510812256984; -0.00245267129037899 0.00173997069595525 -3.6716119030538524e-5] %
+
+Mass Used: 142.64125057729825 kg
+Launch C3: 90.29268659921426 km²/s²
+||V∞_in||: 1.9718262982208725e-9 km/s
diff --git a/archive/ES_0.5737385364942549 b/archive/ES_0.5737385364942549
new file mode 100644
index 0000000..a9ea7c9
--- /dev/null
+++ b/archive/ES_0.5737385364942549
@@ -0,0 +1,22 @@
+archive/ES_0.5737385364942549---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T18:45:05.946
+Launch V∞: [6.3615736082990635, -7.533873816901356, 0.005695865436434697] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002395999113079766, -0.015938923830166353, 0.01971057940733297] km/s
+ V∞_out: [-0.01674872931056347, -0.01581691753925648, -0.010838501227833159] km/s
+ time of flight: 1.8513220681012738e8 seconds
+ arrival date: 2029-03-14T12:21:51.946
+ thrust profile: [0.30363834270543144 -0.08846980335215442 -0.12122188975071448; 0.029892810539943814 0.0038930372706610324 -0.037219844758261955; 0.06000777844142863 0.022410887673855212 -0.12330662486867576; 0.05387716407643405 0.025780570437119794 -0.15408726113122168; 0.05674518098852036 0.03464019156480116 -0.20566764603955978; 0.025018215494680387 0.01628987751074679 -0.1101677663872491; 0.01961104662924663 0.012902770906211052 -0.0990918646968728; 0.008698903138709326 0.004610948472840331 -0.052454651997872685; 0.003029894976432055 -0.0005830844653958406 -0.01688418676443973; -0.00011321146427001934 -0.002104756419701593 -0.0037354318839817446; 0.002173047684970435 0.004529086851622073 0.0038282233793716057; 2.2375223185821212e-5 0.0014283584314769083 0.0032316716726453866; -0.0009746842728635019 0.002281919884763138 -0.002677383827135594; 0.004117042672853276 0.007164788592307798 -0.011074392622712242; -0.0036696731228538075 0.024417531159317486 -0.01099647164588631; -0.014478692115701668 0.002383982813935103 0.01005157726787508; 0.001087151369015874 0.006044562288084887 0.016224900048677018; 0.010552696233548608 0.004203326513688094 0.050453418079374444; 0.01909981396848128 -0.012293353336467389 0.005157688772433196; -0.012291854248729068 -0.015517441390592857 -0.013619867625564651] %
+
+Mass Used: 102.19300812681877 kg
+Launch C3: 97.22890590568205 km²/s²
+||V∞_in||: 0.025461677972720146 km/s
diff --git a/archive/ES_0.5737409856186735 b/archive/ES_0.5737409856186735
new file mode 100644
index 0000000..041b21a
--- /dev/null
+++ b/archive/ES_0.5737409856186735
@@ -0,0 +1,22 @@
+archive/ES_0.5737409856186735---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T22:04:11.785
+Launch V∞: [7.226818012777741, -6.8030740044698135, -0.14162340093703268] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005062781484764624, 0.00804097374403241, -0.00012143514797260421] km/s
+ V∞_out: [0.007752464747900151, -0.0013480115898816946, 0.0017330587587759605] km/s
+ time of flight: 1.5016037790429366e8 seconds
+ arrival date: 2029-02-09T21:17:08.785
+ thrust profile: [0.20479314925420192 -0.0605802498635679 -0.08853022312461743; 0.1088297245623357 0.01774628316221294 -0.12933340160159304; 0.1112975279239246 0.039475501276827946 -0.21809284921905206; 0.09910478231414342 0.046137740242051604 -0.26661195521399284; 0.07458132010932689 0.04016497117286473 -0.2519104356453647; 0.045904249300880204 0.027075581190310265 -0.18486495924988924; 0.017548272559962778 0.011140107766895162 -0.08149766875507475; 0.005427271293242541 0.004067857157997964 -0.029595041484219035; 0.0031025821329715023 -0.0003853416736090761 -0.0055224093183504405; 0.0007165856421197587 0.0006178320981224184 -0.005148274635641656; 0.0011496255497481312 0.0013044708748195996 -0.011177203746325661; 0.0008708838272438644 0.0008914140757630431 -0.007766301558710574; 0.00016751541960020465 -0.00022029372169429925 -0.00421819052396678; -0.00020635782291472812 -0.005442620729530118 0.0031258820735085334; 0.0009817691238234057 0.00010612404416332147 0.001796651806631133; 0.005640269939882134 0.0007415431612899518 -0.0011729833576640798; -0.0003704006368298339 0.0024022488500674718 0.003657905463185003; -0.00020729973919293135 0.004456459153357365 0.005258732361317729; 0.004160000021905939 -0.006438961541330706 0.006901530831951178; -0.00022631061846838183 -0.00015962896586174885 0.0016669719851532265] %
+
+Mass Used: 94.61331504298323 kg
+Launch C3: 98.52877168779473 km²/s²
+||V∞_in||: 0.00805781129159814 km/s
diff --git a/archive/ES_0.5737565544334876 b/archive/ES_0.5737565544334876
new file mode 100644
index 0000000..5cffaf9
--- /dev/null
+++ b/archive/ES_0.5737565544334876
@@ -0,0 +1,22 @@
+archive/ES_0.5737565544334876---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T02:45:07.091
+Launch V∞: [7.3547710997328, -6.5657333144223875, -0.23138416669734493] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005151612464691962, -0.0017173105867570896, -0.0027458325926209217] km/s
+ V∞_out: [-0.0028099365777038646, -0.00031935066857221716, 0.0016604894929553992] km/s
+ time of flight: 1.5747882685323632e8 seconds
+ arrival date: 2029-05-05T18:52:13.091
+ thrust profile: [0.30956961267164335 -0.06717064776016099 -0.12224842155355559; 0.0814009305839016 0.02241483219260309 -0.09409911711871885; 0.08006802561382698 0.04168865012115938 -0.1546496032843487; 0.06607712006725404 0.04528396512987848 -0.177837243682663; 0.047515547157942595 0.0384085824379436 -0.16384197750192042; 0.019505571037922505 0.01742010207777214 -0.08081548368820218; 0.024309212169053584 0.02388600099054128 -0.11715185542028787; 0.011363647067036787 0.012024393861760262 -0.062800012686813; 0.021573415199761838 0.02472150970935815 -0.13119362267917836; 0.007125473892431545 0.008164431342931754 -0.04718995879867291; 0.0031146002456552205 0.004014549580848294 -0.019289182943669658; -0.002168385705680096 -0.008324647931694473 -0.012575335050444413; 0.004616726815994685 0.002549712854937665 -0.009007668496921922; -0.0001672123787703692 -0.0005216189575287312 -0.004919096894767456; -0.009825046874394568 -0.003220199077859554 -0.013624793293607024; -0.001204123325916651 0.0037927594623785718 -0.0006858410089777239; -0.0028385846728986998 -0.003058819450963827 0.0097016451100894; 0.004103153982821657 0.007092337403779277 -0.0011738920450608207; -0.0004494796477386194 0.02855134860313315 -0.01310140201748165; 0.008090773817478794 -0.007580109922228994 -0.03335116690446875] %
+
+Mass Used: 102.06151881635788 kg
+Launch C3: 97.25505051817903 km²/s²
+||V∞_in||: 0.0032793510620168446 km/s
diff --git a/archive/ES_0.5737862431455832 b/archive/ES_0.5737862431455832
new file mode 100644
index 0000000..1b0edab
--- /dev/null
+++ b/archive/ES_0.5737862431455832
@@ -0,0 +1,22 @@
+archive/ES_0.5737862431455832---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T12:08:09.180
+Launch V∞: [6.404703866402049, -7.860793868539052, -0.3617973189878615] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.044554598853769e-7, -3.6569810289312417e-6, 2.1679248684953438e-7] km/s
+ V∞_out: [-1.4179952650792612e-6, 3.0044806846206312e-6, -1.6201738545594932e-6] km/s
+ time of flight: 1.8749577777657655e8 seconds
+ arrival date: 2029-04-17T14:17:46.180
+ thrust profile: [0.07235917799262949 -0.028883660985557957 -0.0381574781033561; 0.01567466240747896 -0.0013777265791151893 -0.027290436221177695; 0.03629848344570306 -0.0023503847078383683 -0.09911474749791514; 0.03824704495564382 -0.00662517246470324 -0.14233885289596443; 0.029641399904066376 -0.007760831213264347 -0.13689338439438892; 0.016769540045931206 -0.005274731166880686 -0.09652123573349841; 0.008075115883406358 -0.003071646096494417 -0.053035619821765544; 0.011528759385609684 -0.005342016842069267 -0.08199281072349361; 0.00577254294319661 -0.003160319137991676 -0.04471222261422672; 0.004650843444523559 -0.0026302169793595257 -0.037116571581161925; 0.006841288606197763 -0.0026804324651195795 -0.04632980288568066; 0.005153020842757147 -0.003183042896644842 -0.04197594157596094; 0.00012545399054424432 -0.00016070473284812389 -0.0007977410414034074; 0.0003187743071504409 -2.051661795095254e-5 -0.0006368496368698344; 2.381629994655947e-5 -5.840052793428384e-5 -0.0003855398012835688; 0.0008480936578157684 -0.00037310250666690065 -0.0003650238772056248; -0.0001786309203060572 0.000260959285860488 0.00022838967339722054; -0.00012896194143952416 4.286611996998218e-5 -0.0002519759377244828; 5.7733940506326354e-5 0.00040153900409879007 -0.0005765899569052982; -2.060799234814985e-6 0.00020266019168198904 0.0001981339717559052] %
+
+Mass Used: 68.91523023655282 kg
+Launch C3: 102.94320915999332 km²/s²
+||V∞_in||: 3.6979703269936575e-6 km/s
diff --git a/archive/ES_0.5738352480681743 b/archive/ES_0.5738352480681743
new file mode 100644
index 0000000..328ba93
--- /dev/null
+++ b/archive/ES_0.5738352480681743
@@ -0,0 +1,22 @@
+archive/ES_0.5738352480681743---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-06T13:26:41.047
+Launch V∞: [6.162123002155432, -8.044839603677016, 0.03312394770390745] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4582122138146522e-6, -9.441149438576471e-7, 6.802547357282218e-7] km/s
+ V∞_out: [-6.613351362235047e-7, 1.507294533444505e-6, -8.752882406660822e-7] km/s
+ time of flight: 1.7838196339677826e8 seconds
+ arrival date: 2028-12-30T03:59:24.047
+ thrust profile: [0.025405753554054448 -0.011120880725215 -0.013424649985626081; 0.03335124840143885 -0.0026028879883836895 -0.05228697370639651; 0.040516389075515566 -0.0006656307436745965 -0.1071579444194098; 0.03637795275315607 -0.001055261931093999 -0.1326225039486021; 0.029235377378109453 -0.002066550764195054 -0.13300086349395185; 0.026476001388775938 -0.003416551022786668 -0.14271436069305224; 0.018681088792121377 -0.003346505437674559 -0.10917470036648397; 0.02646738092190846 -0.005109326664279124 -0.1644578559976652; 0.007716289187291519 -0.002164610620741659 -0.05464844876276685; 0.001211511741537206 -8.154680742220553e-5 -0.008756260194873416; 0.00020190831004919182 -0.00043276047128142304 -0.006336458118986914; 0.00047272113924457865 -0.00023821538872796042 -0.002448869235095349; -5.429440433751362e-5 0.0006457861410778165 0.0005280779849076941; -0.0008221405185491932 -0.000210721587089194 0.0020266189097408846; -0.00011370440371197208 -0.0003241546130872975 -0.0020415296706468846; -4.034050225424783e-5 9.716034308519057e-5 -2.8113887905121247e-5; -0.0005956506140010016 -0.001356966110224368 -0.0016997266954682996; 3.3388981602895104e-5 0.0007790719110577068 -0.0004264463834558009; -0.000409532142502604 0.0005253083829082757 0.003734134282451157; -0.00036005648539186286 -0.0026998690117503387 -0.00026366952686985613] %
+
+Mass Used: 70.43603160498424 kg
+Launch C3: 102.69230133849472 km²/s²
+||V∞_in||: 1.8656051010903218e-6 km/s
diff --git a/archive/ES_0.5738491666244824 b/archive/ES_0.5738491666244824
new file mode 100644
index 0000000..a9e95d7
--- /dev/null
+++ b/archive/ES_0.5738491666244824
@@ -0,0 +1,22 @@
+archive/ES_0.5738491666244824---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T07:40:01.917
+Launch V∞: [6.049389657291794, -7.56519998744419, 0.05025983090900961] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1837254815965926e-9, -1.0858319733029966e-9, -2.089857467837553e-9] km/s
+ V∞_out: [-1.3982283898455106e-10, 3.113008006070185e-10, 4.632732875476911e-10] km/s
+ time of flight: 1.7653074355678296e8 seconds
+ arrival date: 2028-11-28T11:59:04.917
+ thrust profile: [0.4224720327358798 -0.12602012344453972 -0.1255108812015001; 0.1722726931107149 0.04593856754291956 -0.14825003552553281; 0.09569870241463208 0.053158702985695895 -0.13883300369081797; 0.0883448722980455 0.06712343564225047 -0.17480344835360134; 0.09654321388982924 0.0911035569390141 -0.23542176458107666; 0.02299957500030527 0.024079445563963617 -0.07158962247910244; 0.015374866409448506 0.017804165098320224 -0.055567618170413086; 0.0062990714506595885 0.007592209264583453 -0.026455349853228765; 0.008188015782812513 0.011709542557788576 -0.0390927170387226; -0.0009987240519446741 0.0014107203993296961 -0.002786223643688609; -0.002760886967736325 0.004162704365345075 -0.011418066979577375; 0.002268068090593852 -0.002087708663821937 -0.0018344758126696333; 0.002787104658187265 0.0070098647872872495 -0.01706901886393112; 0.0038165598506133937 0.02644799555493433 -0.003940610086716934; -0.000834240976790961 -0.005585948611180653 0.0008450337377859962; -0.0025961659113166186 0.009495373609770992 0.00834038197653412; -0.007123033536078308 -0.011783394579689703 0.011255765406862198; -0.0005575813405328716 0.00018005077835745245 0.000663237345144524; 0.024192515987003414 -0.02703571338339188 -0.023782002182134953; -0.01074220434618114 -0.008715156149556185 0.03596870974037226] %
+
+Mass Used: 122.14965699136064 kg
+Launch C3: 93.8298921263775 km²/s²
+||V∞_in||: 3.2117273061543904e-9 km/s
diff --git a/archive/ES_0.5739201225140069 b/archive/ES_0.5739201225140069
new file mode 100644
index 0000000..743d82c
--- /dev/null
+++ b/archive/ES_0.5739201225140069
@@ -0,0 +1,22 @@
+archive/ES_0.5739201225140069---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T09:16:53.152
+Launch V∞: [6.017047856512564, -7.206954135382583, 0.1912081822396558] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0178723792908808e-10, -2.9597876398918672e-9, -1.1228182939686685e-8] km/s
+ V∞_out: [1.8512674134405682e-9, 2.741742912775777e-9, 1.3867728489308637e-9] km/s
+ time of flight: 1.8298417598188734e8 seconds
+ arrival date: 2029-02-09T06:13:08.152
+ thrust profile: [0.9650588757674833 -0.2537691422645333 -0.22527824954331016; 0.15563720958091842 0.054072379490782266 -0.1206940530543917; 0.07926698504655315 0.05129578532658809 -0.09890042154268634; 0.09187107051668611 0.08139067390261452 -0.15954887763084477; 0.0494131655853298 0.055349632695598554 -0.11220031245006121; 0.0062457976203963445 0.009880378310238027 -0.01766999934994436; 0.03507392593171077 0.0570049171416474 -0.12200649411881848; 0.009328911754802813 0.009211750645952643 -0.023696183234140543; 0.011293673494794173 0.025470266443971115 -0.0417102407641893; 0.00512330679559268 0.017448646375321706 -0.051048232723889954; -0.0029568369963387086 0.009695481739273882 -0.016389265193174712; -0.0019253699514817204 0.0070437330325035675 -0.030344934327428963; -0.004443785269153759 -0.0014092284650601035 -0.005021513580656802; -0.0010743464356505069 -0.0017257571140826327 0.0047172455775110235; 0.0021506505240764 0.0035608005563425396 -0.00527268786699233; -0.011116819264671188 0.0005740638227862927 -0.011527876199994555; -0.0026265230647852748 -0.009824348650849331 0.004127023387033246; 0.011308292815804923 0.0021078799084771225 -0.03201180931155985; 0.003657297147155761 0.002655612007161067 -0.0012548990810489994; 0.0007305569635230336 0.0007147886523483134 -0.0031780029530291158] %
+
+Mass Used: 155.18073151452336 kg
+Launch C3: 88.18161338602594 km²/s²
+||V∞_in||: 1.1613490133879601e-8 km/s
diff --git a/archive/ES_0.5739352349270787 b/archive/ES_0.5739352349270787
new file mode 100644
index 0000000..425ebb2
--- /dev/null
+++ b/archive/ES_0.5739352349270787
@@ -0,0 +1,22 @@
+archive/ES_0.5739352349270787---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T19:58:08
+Launch V∞: [6.098739489547694, -7.487458267565201, 0.16349630661685557] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003685238738194763, 0.002536477061708339, 0.00330026973713796] km/s
+ V∞_out: [-0.0039041690745556332, -0.002033963385842223, 0.0033939059293391525] km/s
+ time of flight: 1.7222205767549765e8 seconds
+ arrival date: 2028-10-07T03:25:45
+ thrust profile: [0.5697407629673338 -0.19521774550802326 -0.14565868515279176; 0.14363041093865223 0.03656973330529738 -0.1347472866750839; 0.09979933984798275 0.05172910662186079 -0.15240249310956772; 0.052889978511218204 0.03817383463913437 -0.11205855228560024; 0.03921034469151889 0.03289341370423538 -0.10360183958269013; 0.049958558732661605 0.05014631114136632 -0.15745690895893424; 0.023182714920955288 0.024676389057790158 -0.08219495961770933; 0.007935824063627788 0.010367433199378384 -0.034064019618886415; 0.009521364683288987 0.0128138320903218 -0.042985119049755625; 0.025624927758035165 0.03927805628045813 -0.1236302744275055; -0.0012547919502234376 0.0050702127223788765 -0.003257919388365424; -0.00020094390381143658 -0.002003724410312777 -0.0056508520007553424; 0.00033851714757249306 0.0009473470884211261 -0.0001384713808674279; 0.0029804448862547567 0.0017705647036261592 -0.011739647965492048; -0.010007327987836458 0.010085582825058979 -0.0051172085850862414; 0.0025191769354001156 -0.01689434459015176 -0.009352425015678017; 0.001720562399024859 -0.0013590922960670163 -0.0054241936758885455; -0.001562941619838738 -0.004033648114332258 0.005780597495698707; -0.005139657619623221 0.004683467611165772 -0.00032394139861604697; -0.010042991901798996 -0.008496424850605606 0.013038268313979464] %
+
+Mass Used: 125.43802409389673 kg
+Launch C3: 93.2833857121763 km²/s²
+||V∞_in||: 0.005559359745504203 km/s
diff --git a/archive/ES_0.5739673156113866 b/archive/ES_0.5739673156113866
new file mode 100644
index 0000000..408351f
--- /dev/null
+++ b/archive/ES_0.5739673156113866
@@ -0,0 +1,22 @@
+archive/ES_0.5739673156113866---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T13:09:33.178
+Launch V∞: [6.985235892070404, -6.662780760103648, -0.061718528916536904] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.0279742241054536e-6, 1.3059437578184114e-5, 7.422906852467775e-6] km/s
+ V∞_out: [1.0391321723279476e-5, -1.0385025085778601e-5, -5.9236706575432695e-6] km/s
+ time of flight: 1.4827807598364684e8 seconds
+ arrival date: 2029-01-15T17:30:48.178
+ thrust profile: [0.6255686680839367 -0.17365084242708145 -0.22415354977519514; 0.2737101753410574 0.061387521483944565 -0.27864615700154227; 0.12617046643551286 0.05722956929658409 -0.21375474401497632; 0.10144024622126033 0.06216832777568507 -0.2372623878485552; 0.0679120103389068 0.04901294904063505 -0.1996830674265718; 0.051419953478767155 0.04207490799899834 -0.1815279765740047; 0.01396311594103069 0.012702577020228268 -0.056886742771631325; 0.0008459404113423588 0.0007859314511593537 -0.005762708584997028; 0.003326008867474567 0.003259197437469708 -0.017245246034290736; 0.0006602701354683507 0.0011629742198445041 -0.00662098628827756; 0.00050693477230108 0.0016742609440329134 -0.004418874310823077; -0.000843544500060427 0.00010819387481298597 -0.004041352962617838; -0.00038382844509596476 -0.00047431264959184923 0.0003524806012393288; -1.6806418376957442e-5 0.0012739144034929649 -0.0013005490344650606; 0.00019706909630397184 0.0007347868690894808 0.00040624878964000063; 0.0001447421091746536 -0.00033345382145326776 -0.0027753882074830053; -0.0011745946292821246 0.0022202382962527253 -0.00449923079188915; -0.001767631610043052 -0.0018037197948674766 -0.006902010975102734; -0.0008271694607594913 0.0003540676832667981 0.00038978480234188413; -0.0013193146113481204 0.0009932567934147968 0.002738595694492662] %
+
+Mass Used: 126.02033511894024 kg
+Launch C3: 93.18997710188756 km²/s²
+||V∞_in||: 1.5840738013021024e-5 km/s
diff --git a/archive/ES_0.5740016376759522 b/archive/ES_0.5740016376759522
new file mode 100644
index 0000000..d480cf1
--- /dev/null
+++ b/archive/ES_0.5740016376759522
@@ -0,0 +1,22 @@
+archive/ES_0.5740016376759522---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T13:23:56.360
+Launch V∞: [5.7700727388977, -7.8500814912571695, -0.6745161013641631] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.397106948033601e-5, 6.509107357732493e-5, -1.0585785918117016e-6] km/s
+ V∞_out: [-1.4350252342150152e-5, 3.303670481094207e-7, 6.792214176502522e-5] km/s
+ time of flight: 1.5884873818083578e8 seconds
+ arrival date: 2028-05-05T02:02:54.360
+ thrust profile: [0.41543660276712124 -0.1906562654008348 -0.16916434514781106; 0.1395939511950462 0.011908551585863975 -0.14321154250768356; 0.10019974837421004 0.032433514985023365 -0.16363578966571157; 0.08594259487894304 0.04150325480717735 -0.18946372725705019; 0.08536562975762149 0.051725214370456296 -0.23385875209977403; 0.06880449870651703 0.048669714751629393 -0.22468361219257335; 0.02208794626098412 0.018078581405324447 -0.08313051534187524; 0.007942584402501446 0.007922321830278991 -0.03618913458130122; 0.0020234771392410806 0.0020037077796847226 -0.009675545063698108; 0.0021936728676237166 -0.0005891987654870322 -0.007789216512022247; 0.0025542692228179924 0.00024424536430537355 -0.0019558271116400716; -5.7269884773702095e-5 0.0027490253298613487 8.404653560111506e-5; 0.0026872112041308512 0.0018356704018463823 0.0019024170531393436; 0.0006152300067224 -0.00039858419029476736 -0.0036885265664419395; -0.0008381486738266301 0.0010926757184731967 -0.0030000659515007516; 0.0012590729563574956 -0.00023928349580635807 -0.0012445048047846354; 0.005933659431629655 -0.0024086138192001287 -0.001159215623212025; -0.006786391251378619 -0.004634426546998232 0.0027763656322204074; 0.010771568714222916 -0.004195538182870698 -0.004157288935595399; -0.0019884904307728283 -0.010815515096802616 0.006820749648049836] %
+
+Mass Used: 113.32904760707925 kg
+Launch C3: 95.3724908025483 km²/s²
+||V∞_in||: 6.937276569457835e-5 km/s
diff --git a/archive/ES_0.5740424796588457 b/archive/ES_0.5740424796588457
new file mode 100644
index 0000000..6608a56
--- /dev/null
+++ b/archive/ES_0.5740424796588457
@@ -0,0 +1,22 @@
+archive/ES_0.5740424796588457---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T21:19:53.292
+Launch V∞: [7.144465897536386, -6.708660192587249, -0.19423161910877138] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00036968494016357477, -0.0013560326668488132, -0.002189699788352174] km/s
+ V∞_out: [-0.0021704788013361138, -0.0002637097449602551, 0.0014072805584047022] km/s
+ time of flight: 1.4875105412451053e8 seconds
+ arrival date: 2029-01-22T13:04:07.292
+ thrust profile: [0.4209377818494039 -0.12100609128437871 -0.165602318147328; 0.14969861878653162 0.030255792188347903 -0.16183511160061; 0.10692084304399901 0.04547533043360791 -0.1902442450939367; 0.10088784284469353 0.056876079969700045 -0.24703328092798058; 0.06466675997960071 0.04328941239285709 -0.19929570517283896; 0.05626369884693601 0.04259931405540695 -0.20753862209977775; 0.008293309007906329 0.007255550755662316 -0.03522104604075241; 0.015582930088755729 0.013587683793512599 -0.07891261070424366; 0.004160478382385242 0.003789828779249471 -0.026145544398558103; 0.002436769652335852 0.0023951118015365738 -0.01517838425521974; 0.0015248364922156002 0.0015741425327367635 -0.005683512942541474; 0.0029755883107317324 0.0034582347900562966 -0.021370905803768953; -0.00025884494883789437 0.002027661819291478 -0.0036829901551395684; -0.0012211656328573015 0.002123137277565194 -0.004349552081766541; -6.720143715850045e-5 0.000545911328626824 -0.002200010481035508; 0.004198294646348438 -0.002265212500157339 -0.0038537991569926678; 0.00038889298777499326 0.004038966117604091 -0.0007206635480524436; 0.002600227354224297 0.0040060339206816785 -1.0212043556811698e-6; 0.00455040908843001 0.003029327795018886 -0.0031970602529816376; 0.00017819984923172144 -0.0013595837552374795 -0.0020932364951571636] %
+
+Mass Used: 109.20732357058023 kg
+Launch C3: 96.08724046252681 km²/s²
+||V∞_in||: 0.002601975540172199 km/s
diff --git a/archive/ES_0.5740634130117191 b/archive/ES_0.5740634130117191
new file mode 100644
index 0000000..f8ef2a5
--- /dev/null
+++ b/archive/ES_0.5740634130117191
@@ -0,0 +1,22 @@
+archive/ES_0.5740634130117191---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T23:18:15.183
+Launch V∞: [5.5081874676321325, -8.007015215538, -0.19249060034709564] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8131727072586232e-7, -9.679248150357037e-8, -1.736588045911142e-7] km/s
+ V∞_out: [1.2739026178205115e-7, -1.6921863925515718e-7, 1.674763053197469e-7] km/s
+ time of flight: 1.5442676225069323e8 seconds
+ arrival date: 2028-03-15T07:37:37.183
+ thrust profile: [0.44780496850517254 -0.21362606199381076 -0.17512217226596613; 0.19148256626256527 0.010360909056949606 -0.189553520464823; 0.08588586500735845 0.02384895870478691 -0.13947567628284874; 0.16498435645371548 0.07204783565303173 -0.3354965121056758; 0.0636977242929796 0.03299035915705503 -0.16842978751484572; 0.04950464556537303 0.028505843101497237 -0.15254250998243085; 0.01986615640100719 0.012996863420150733 -0.07324102356483768; 0.013289370603116281 0.00974080414218679 -0.05485065434666568; 0.006226738228172204 0.006240316472529486 -0.0303476868583033; 0.001691198432885279 0.0012336117918087738 -0.009078706714515695; 0.00284326813355414 0.0017668595070897452 -0.014077035297296658; 0.002527846025429539 0.0011727046512073143 -0.006362008768970735; -0.0017490667827253078 0.005169389232602674 -0.0015416669682073291; -0.0026265601894621443 0.00032444821575796615 -0.0010818887259518434; -0.0014802367817380857 -0.003647515451980958 0.002170437901523533; -0.001406055640779111 0.001802769551215655 0.005080799759141828; 0.00014597487952824222 -0.00043269209786515536 -0.00020551049363697472; 0.005182432903622212 -0.0012621064443980984 -0.0072070317627091094; 0.0029688244250227844 0.0013340332596674183 -0.00433523718669002; 0.0002435961376734458 0.005267218092198203 0.008320153040218402] %
+
+Mass Used: 118.5520474289965 kg
+Launch C3: 94.48947447165872 km²/s²
+||V∞_in||: 2.690764158210627e-7 km/s
diff --git a/archive/ES_0.5740830110171711 b/archive/ES_0.5740830110171711
new file mode 100644
index 0000000..13bdd2f
--- /dev/null
+++ b/archive/ES_0.5740830110171711
@@ -0,0 +1,22 @@
+archive/ES_0.5740830110171711---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T20:51:44.919
+Launch V∞: [6.771057939131758, -7.197516481549884, -1.101793173556501] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.251925701921683e-7, -0.0001750120126115258, 0.000116798357947611] km/s
+ V∞_out: [0.00010546582837741191, 0.0001777931914658994, -3.9862500436963034e-5] km/s
+ time of flight: 1.874957778519641e8 seconds
+ arrival date: 2029-04-05T23:01:21.919
+ thrust profile: [0.1881371367587189 -0.049748719508679436 -0.061155063304228666; 0.09421432628901287 0.03734000901450162 -0.08795239540109413; 0.08190108989115491 0.049793481841240696 -0.12659363248813996; 0.06751110588935594 0.055906181463687796 -0.14562596515219642; 0.04971578622737371 0.05131613730987332 -0.13953249241845764; 0.03645037927201871 0.04539104427342627 -0.1266736403674537; 0.021763488726763713 0.03357656780955128 -0.09547171037868275; 0.008726492774275492 0.018253332460436453 -0.05591184803150711; 0.005787649853931374 0.014494880496634662 -0.0465951582839074; 0.0026797524522933487 0.008955019002180938 -0.031404333916177654; 0.001133602940492421 0.005333226713896926 -0.020098550239239923; 0.0001603014932575848 0.0019366541317597601 -0.008307196467327825; -0.0003948027881379441 -0.0008228419271708619 0.0021295628374004404; 0.0002998794281253677 0.0004585964419066759 0.0016169425019464377; -0.00010930557631080135 -0.00015640255252737881 -0.00014912928811631294; -0.00027869063271491687 0.0004647109972249529 -0.00028470434423063075; 8.809762942093457e-5 -0.00031454364353013155 0.0012275991183438425; 0.0005165196539492747 3.6138274491460417e-5 0.0005554528852382192; -0.0005553001142346334 9.32815324382082e-5 -0.0010715141493742627; 0.000305815494207951 2.174225443720848e-5 0.0007948255839176162] %
+
+Mass Used: 93.04857851844963 kg
+Launch C3: 98.86541731455713 km²/s²
+||V∞_in||: 0.00021040754930570083 km/s
diff --git a/archive/ES_0.5741942178771333 b/archive/ES_0.5741942178771333
new file mode 100644
index 0000000..3c5019e
--- /dev/null
+++ b/archive/ES_0.5741942178771333
@@ -0,0 +1,22 @@
+archive/ES_0.5741942178771333---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T21:07:42.189
+Launch V∞: [5.956582509120386, -7.655523000378889, -0.08374859171065395] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01092763321222626, -0.008220676488892006, -0.008615789391719251] km/s
+ V∞_out: [0.007398206952698345, 0.012447456995515799, -0.007213234842201681] km/s
+ time of flight: 1.6748884129291728e8 seconds
+ arrival date: 2028-08-13T09:48:23.189
+ thrust profile: [0.49729463769369175 -0.18038375156191525 -0.15045462849914873; 0.1018732724900669 0.021362724796972165 -0.09533247029308874; 0.11352292388444069 0.05202590508305671 -0.16161159198800246; 0.07948743854506117 0.05128086490116503 -0.15373576129205901; 0.04253458250122028 0.03429013372903998 -0.10909585913291292; 0.037325609693337126 0.0369577680709895 -0.11844922334819749; 0.03556154593478686 0.039616869117341955 -0.12486246697004266; 0.024061069376580115 0.028162274606576304 -0.09842441196855273; 0.012944850819117311 0.01603824519057051 -0.058250327257734665; 0.013039070811139914 0.018178259932396416 -0.06692878003135605; 0.0026221689479118612 0.0018423236349134353 -0.004385523011056882; 0.0041882085892626765 0.008528218413403671 -0.02858741164991835; 0.007166690014210815 0.0055135849740692786 0.001641795130098106; 0.0010707411669602681 -0.0002528448371067123 -0.0038970625242766123; 0.0001778377858250673 -5.511036910962864e-5 -0.0030757318586874917; 0.004727818594168944 -0.0058495074603855685 0.0010721025072977061; 0.006381053397802194 0.01713971252538414 0.0007799644569343148; -0.0161667971530365 0.005100832494119014 0.0010876551074888803; -0.015617884414621665 -0.001593862540224119 -0.00319370999646137; 0.000332140232701285 -0.0014740656200027404 0.0024607096107559867] %
+
+Mass Used: 121.00621255055694 kg
+Launch C3: 94.09492142390262 km²/s²
+||V∞_in||: 0.0161624415358087 km/s
diff --git a/archive/ES_0.5741978409019508 b/archive/ES_0.5741978409019508
new file mode 100644
index 0000000..0927b76
--- /dev/null
+++ b/archive/ES_0.5741978409019508
@@ -0,0 +1,22 @@
+archive/ES_0.5741978409019508---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T15:59:59.200
+Launch V∞: [5.704742474911252, -8.11064194221146, -0.5291256773787539] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.5586095638630574e-5, 5.897845749177851e-5, -1.0156441670007495e-6] km/s
+ V∞_out: [-1.444082184046861e-5, 3.3786190610875746e-7, 7.248724944485657e-5] km/s
+ time of flight: 1.561283890696582e8 seconds
+ arrival date: 2028-04-06T16:59:48.200
+ thrust profile: [0.21027640042262435 -0.10438465404295408 -0.09764131064063242; 0.07175988702694565 0.00012309179498566682 -0.0880337496783775; 0.07173666450217533 0.014642765696242626 -0.1398988633125552; 0.09001484161800023 0.029929591284681416 -0.2282202475794589; 0.05459586008867208 0.022637917452698934 -0.17926285878528436; 0.054164352183938995 0.02592189089496688 -0.2058457457137553; 0.010340635222780071 0.005057004429416444 -0.051432833437900644; 0.011692989479236868 0.005960881363722024 -0.05637778413744205; 0.00597602146896352 0.0034492608142713457 -0.029033014653123954; 0.020976580196627223 0.010629846438739552 -0.1079610936932339; 0.009785131750710243 0.007274761139428146 -0.07179446778117042; -0.001825496722584018 -0.0021921251671296075 -0.0006272487866021677; -0.0023085029960030166 0.001237832333937115 -0.0005729244829842593; -4.024373137932497e-5 -0.000609164652109241 0.0002588224382052847; -0.0004890482474825771 -0.0007435573143041175 0.0027503882767588427; 0.0004863084031304283 -0.00043199871201584196 -0.00152705390633675; -0.0013432292211288995 -0.0004761614220714362 0.0018225634384636525; 0.001417499148198342 0.0008388416757849637 0.0019055452690593371; -2.152762495676193e-5 0.0005766248991613224 0.0035951930001722897; -0.0005649623301259391 -0.00046401813977452677 0.003985389579508952] %
+
+Mass Used: 94.69246953898892 kg
+Launch C3: 98.60657340227777 km²/s²
+||V∞_in||: 7.454919246214448e-5 km/s
diff --git a/archive/ES_0.5742899710224181 b/archive/ES_0.5742899710224181
new file mode 100644
index 0000000..6a102ee
--- /dev/null
+++ b/archive/ES_0.5742899710224181
@@ -0,0 +1,22 @@
+archive/ES_0.5742899710224181---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T00:25:09.792
+Launch V∞: [5.712715322478515, -8.175924430077549, -0.2019702912968251] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.821911147468741e-5, 4.316313023457995e-5, -7.8973182831182e-7] km/s
+ V∞_out: [-9.797984240116966e-6, 2.475854185247594e-7, 5.68889227372809e-5] km/s
+ time of flight: 1.5783791532726634e8 seconds
+ arrival date: 2028-04-27T20:17:04.792
+ thrust profile: [0.12370186973269091 -0.060117730875868684 -0.058069676455615546; 0.06648427248328813 0.00044913807595685286 -0.07938994342680021; 0.07520111519202219 0.014962540545564102 -0.14467750796652834; 0.07704173171483805 0.02372425008374379 -0.2000061118290323; 0.057627172614999354 0.022206918820994615 -0.18505912487577164; 0.035931501292908695 0.016047701646383104 -0.13586278687476536; 0.026929223234955394 0.013372989034513593 -0.11459481439350862; 0.025127869712800645 0.013204384102134181 -0.11801461622754286; 0.021467241052785854 0.011836671216833334 -0.11821167591115367; 0.0034698913343679215 0.0016276467886718903 -0.019762249305952214; 0.005952993557191305 0.002664819881559978 -0.03546102914034032; -0.001058981891789375 0.0008022736054947634 -0.0009658378699139955; 7.926029171306912e-5 -0.00023035678217848043 -0.004289898541268772; 0.0011087601967882889 0.00020554910183989567 0.000847141826360984; -0.0024417457714553904 -0.0021429540573715197 -0.0015853620431082688; -0.0032130421373036348 0.0021926889766038142 -0.003841719209629645; -0.00029990301280943127 -0.0002023768574585918 0.002713289699344827; 0.0002679542404316708 -0.004224889031306691 0.0015438939309774867; -5.230596974201884e-5 0.0007325400027484838 -0.008484326045796383; -0.0018659799413430868 -0.005347950438145656 -0.0007031547550396703] %
+
+Mass Used: 89.46201578940145 kg
+Launch C3: 99.52164864058622 km²/s²
+||V∞_in||: 5.765743638007626e-5 km/s
diff --git a/archive/ES_0.5742964457323037 b/archive/ES_0.5742964457323037
new file mode 100644
index 0000000..1af6252
--- /dev/null
+++ b/archive/ES_0.5742964457323037
@@ -0,0 +1,22 @@
+archive/ES_0.5742964457323037---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T14:15:50.751
+Launch V∞: [5.960592411446979, -7.266553932154116, 0.36396278604329213] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.050183012346372e-5, 1.3880791592823495e-6, -3.002789136459026e-8] km/s
+ V∞_out: [-2.039993121980795e-6, 4.618302683219305e-8, 1.037642160161701e-5] km/s
+ time of flight: 1.8749577781327704e8 seconds
+ arrival date: 2029-04-01T16:25:27.751
+ thrust profile: [0.691456304129194 -0.1331029643016909 -0.122009954095548; 0.3367106045913413 0.14389221812548178 -0.18626084100200882; 0.2512158341679879 0.19871948704826536 -0.23083209470642077; 0.11365320946376167 0.1240684491666532 -0.15533822812771586; 0.03772187089496706 0.052703034652985176 -0.07221215972147733; 0.02040876730684446 0.03444087895454653 -0.049785897474004887; 0.015794460960125663 0.0313077086281291 -0.04681297152238783; 0.005003372141459984 0.011340598375152108 -0.01776052412217103; 0.0032674163221808835 0.008436944080684938 -0.013564983066589136; 0.0023071621259113427 0.006666907289537807 -0.01086004483522534; 0.00031256802678579303 0.0014477279314497817 -0.0023063213998659763; 0.0008872991746859018 0.0032728871848055575 -0.006741084099005084; 0.0004371361028266614 0.002951539638833283 -0.003189780374030456; -0.0009412746969782657 -0.0007924673100419559 -0.0034031946459565712; 0.0015086125739537438 0.0026044422541306525 -0.0021424549065203204; 9.799321698006477e-5 0.0006676779717259921 -0.0011602713003959985; 0.0021267038527210983 -0.0018289865214723344 -0.004040918721668358; -0.0036662502605280603 0.0028579946732050325 -0.004308828889341275; 0.0006792164740473315 -0.0005768678132890277 0.003059340626553237; -0.0016097328682130037 -0.004560490653664597 0.0012407324488116966] %
+
+Mass Used: 153.9728883731068 kg
+Launch C3: 88.46393685392815 km²/s²
+||V∞_in||: 1.0593210154093224e-5 km/s
diff --git a/archive/ES_0.5743095725291952 b/archive/ES_0.5743095725291952
new file mode 100644
index 0000000..b7ed3b0
--- /dev/null
+++ b/archive/ES_0.5743095725291952
@@ -0,0 +1,22 @@
+archive/ES_0.5743095725291952---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T08:59:18.527
+Launch V∞: [7.405420717884969, -6.631409131634249, -1.5340829668955065] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.479667968816117e-9, -1.0958536911672176e-8, 4.0367845114461105e-8] km/s
+ V∞_out: [1.0357738025317912e-8, -3.671332545393934e-8, 5.701574148999673e-9] km/s
+ time of flight: 1.5878455721441358e8 seconds
+ arrival date: 2029-05-23T03:48:35.527
+ thrust profile: [0.17194416883213273 -0.04188606590930932 -0.08538651566270895; 0.04696200768249071 0.009903449291183886 -0.06640878396524995; 0.06289692449214168 0.028197922758587544 -0.1530174337106979; 0.04650332760041599 0.027480121787908523 -0.16193902489926765; 0.03323193244044198 0.022679296053411832 -0.14840080766329508; 0.01977605121801274 0.014668096830842687 -0.1057995306464118; 0.011883256661193407 0.008734501480005154 -0.07208458339448987; 0.006338990401724548 0.005408877420152629 -0.04600234064377301; 0.022001563349423645 0.020561758740556577 -0.17151199749529633; 0.0014756058526130395 0.0017276938821073652 -0.01344150798892655; 0.0023621901384609026 0.0022207514420914155 -0.02232124657443377; -0.0007096590271082051 -0.001754772963139025 -0.0008367059819156105; 0.0009267418541751572 0.003908228164905945 -0.002219420032052596; 0.0031994359384564593 0.0005932644314929658 -0.004321039688244342; 0.0007011714773095884 0.003204497466389679 -0.008230217657306749; -0.0009333514031234296 -0.003932601832119736 -0.0009110295629571; 0.010402288258341157 -0.001172983705047721 -0.0009523040691044134; 0.0006677972557559937 0.0002972669994002301 -0.008014672106211321; -0.000715569229174521 -0.0006847245274779905 0.0004953800474595242; -0.004901318424451498 0.006900605003975834 -0.0012437947674485664] %
+
+Mass Used: 79.87385511302227 kg
+Launch C3: 101.16925362932095 km²/s²
+||V∞_in||: 4.2186244339572024e-8 km/s
diff --git a/archive/ES_0.5743124468239842 b/archive/ES_0.5743124468239842
new file mode 100644
index 0000000..8df1c4d
--- /dev/null
+++ b/archive/ES_0.5743124468239842
@@ -0,0 +1,22 @@
+archive/ES_0.5743124468239842---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T12:26:18.438
+Launch V∞: [5.751949355303375, -8.006076596271939, -0.33013608943935835] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6191093221765818e-6, 2.887935931266512e-7, -3.684235516001384e-7] km/s
+ V∞_out: [1.6179541974524354e-6, -4.2218047526569e-7, 1.9862793820678804e-7] km/s
+ time of flight: 1.5971889685270458e8 seconds
+ arrival date: 2028-05-18T02:47:54.438
+ thrust profile: [0.27330126862805065 -0.12679411190691794 -0.11923745410786094; 0.09745845171438706 0.003062964299655487 -0.10536824730819071; 0.0661806655797181 0.015211979113674362 -0.12487635861344584; 0.08450602317592754 0.03300791664984515 -0.20706307189479684; 0.048265575167836965 0.022055258043218263 -0.15368424293437302; 0.028307400501745725 0.016658971633410204 -0.11302315977730215; 0.045517538850310915 0.03274784285003467 -0.17829192400207117; 0.031010956300605973 0.022081930977139112 -0.12730332474173395; 0.006233622458260863 0.002258023782894738 -0.044489853343431675; 0.002487521388150655 0.001809860469988842 -0.01558532859395011; 0.0028281340948474866 0.001980736520921795 -0.017669435005498824; -0.0003511005230343164 0.0008983133016804032 -0.010945713508062735; 0.0034658072575142152 0.0008796842542139895 -0.00827507190001062; -0.0009295547229226319 0.002038237233861368 -0.006389994923579024; -0.006949641437876414 0.004440805238542325 -0.001399399076255756; 0.004311369742913193 0.006820005917156953 0.003976872688019523; 0.005288211956262874 0.0029937705851787563 -0.011623921355973824; -0.002645977295091777 -0.007648185987673302 0.012610559396223823; -0.0017022765076344995 -0.0006471945921622888 0.016347455277135735; -0.001276356890719563 0.004453184130811765 0.0068291936041792525] %
+
+Mass Used: 102.49934144274039 kg
+Launch C3: 97.2911736888985 km²/s²
+||V∞_in||: 1.6854235817632824e-6 km/s
diff --git a/archive/ES_0.5743628083526926 b/archive/ES_0.5743628083526926
new file mode 100644
index 0000000..8b253d3
--- /dev/null
+++ b/archive/ES_0.5743628083526926
@@ -0,0 +1,22 @@
+archive/ES_0.5743628083526926---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T11:16:37.731
+Launch V∞: [6.680482248047088, -7.202390791640962, -0.294918901790186] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008603970535684943, 0.0002601769420038268, -0.005679162995703207] km/s
+ V∞_out: [0.009915866171137638, -9.466846525877798e-5, -0.0028524687023784483] km/s
+ time of flight: 1.8317305916674334e8 seconds
+ arrival date: 2029-02-11T12:40:56.731
+ thrust profile: [0.334173091391399 -0.08725702788760523 -0.10158801788877195; 0.10724803260341342 0.03457840104366045 -0.09523949008695518; 0.11427646597061282 0.0723132892224976 -0.16801514625268812; 0.08744674237940073 0.07622562244954113 -0.18017323679739172; 0.08676173078936995 0.09403428878719146 -0.22872474327056283; 0.02667867178806935 0.03420445770757721 -0.0892919561271494; 0.010962946301727427 0.016224451126186697 -0.04415659565643538; 0.009496197877874302 0.015716108308150244 -0.044335133390343236; 0.000507685338977726 0.0008064668182127043 -0.0023013832706618976; 0.004572897937858525 0.0019431078447666693 -0.006758982282624492; -0.0015171264496991012 0.0003729455065784705 -0.002071932633688482; 0.0005307021785535226 0.0019522977397558366 -0.0008108904654040925; 0.0024869526450312634 0.0014957415254883946 0.002193500454057087; -0.0031015374473625556 -0.00010804878853987361 -0.003127123079379398; -0.00011790280475747986 -0.0006839762369139435 -0.0008784028506555286; 0.0001732553420867916 -0.002264481857677212 -0.001255343509954879; 0.0011164222566963614 0.0018478207011073979 -0.005147472639296331; -0.00802500209655123 -0.014288795768831583 0.005110680821002848; 0.001686819169973561 -0.0005462693471409809 -0.0051009654350463104; 0.010983422417108575 -0.0030198201502911613 0.001094776406878621] %
+
+Mass Used: 106.64679859119178 kg
+Launch C3: 96.59025334061992 km²/s²
+||V∞_in||: 0.010312559980521312 km/s
diff --git a/archive/ES_0.5743872713869254 b/archive/ES_0.5743872713869254
new file mode 100644
index 0000000..51075b0
--- /dev/null
+++ b/archive/ES_0.5743872713869254
@@ -0,0 +1,22 @@
+archive/ES_0.5743872713869254---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T09:51:34.293
+Launch V∞: [6.928385293263555, -6.688817026478578, -0.31505502929721024] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00042239802162810777, -0.0006221610180018867, -5.918124173841962e-5] km/s
+ V∞_out: [4.133127103152474e-5, -0.00019523120987799072, -0.0007268182558378923] km/s
+ time of flight: 1.5070958318472555e8 seconds
+ arrival date: 2029-02-12T17:37:57.293
+ thrust profile: [0.5356072526855872 -0.11417872706551123 -0.1720406967468807; 0.40695384663004 0.1316271082779908 -0.33903470599426766; 0.10181307060994839 0.06035385734483166 -0.15760328001489646; 0.09972693882349061 0.0780537779421513 -0.2075325625348871; 0.08815756407949266 0.08702845339755465 -0.2346058107674123; 0.014866696823624008 0.01746585315291744 -0.055745391466503806; 0.021342150814550088 0.02620636529612061 -0.08673522037298138; 0.016990301913112783 0.023778927445176037 -0.08050168670432409; 0.0013829123574850791 0.004732074828095087 -0.010848074236847418; 0.002981329940042951 0.0004417163191016019 -0.012036273359653108; 0.0006397913254975868 0.002896501099686138 -0.012971637226447806; -0.0011553930120162884 -4.7895558854277364e-5 -0.0010486402020594087; -0.0008385741003602261 -0.001426252473786819 0.00030866772114113063; -0.002670407986029709 -0.002346513321603467 0.0050138694931841105; 0.0023339257956270327 -0.0006750037742279465 -0.01038886078442381; -7.915669884663316e-5 -0.0009524600675373778 -0.002571127029053203; -0.0016442671897627333 0.0009209678772714358 0.005822689300523659; -0.0005894036102290876 -0.002014360536430695 -0.0028565828317992587; -0.0036078523579517207 0.0038134055202268522 0.00370448248298475; 0.00010400931386845733 0.00038257796523257404 -0.0009887162678797936] %
+
+Mass Used: 128.5398252849618 kg
+Launch C3: 92.8420556571059 km²/s²
+||V∞_in||: 0.000754325420737088 km/s
diff --git a/archive/ES_0.574395516558468 b/archive/ES_0.574395516558468
new file mode 100644
index 0000000..0cfd1e0
--- /dev/null
+++ b/archive/ES_0.574395516558468
@@ -0,0 +1,22 @@
+archive/ES_0.574395516558468---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T18:33:53.539
+Launch V∞: [5.367404654032926, -8.047401298745678, -0.2935436577943446] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.170475833938632e-5, 0.016564040611286433, -0.005476385950653532] km/s
+ V∞_out: [-0.014164174909026361, -0.007792787795557143, 0.006543806968421597] km/s
+ time of flight: 1.5201792206633824e8 seconds
+ arrival date: 2028-02-17T05:45:55.539
+ thrust profile: [0.619287602904116 -0.32676843454404 -0.2534945550357975; 0.1190555762035688 0.00012655004750466403 -0.13030740295476043; 0.09429891415457531 0.01952355691508994 -0.1615691253162337; 0.10593768640551438 0.03180573161711817 -0.23257528780193537; 0.05603516267755269 0.02391035012153251 -0.1615504410272946; 0.038193994286627904 0.02068210262434782 -0.13564104943729505; 0.0380743184639275 0.01962079105304921 -0.14944813866104822; 0.002929363574276597 0.0036475987069064545 -0.019710721937955037; 0.02514655838915871 0.014190051692669313 -0.12616242943333095; 0.003191696289768157 0.0019731477758474277 -0.0175642843023923; 0.003009061541306664 0.0013700540024464865 -0.01925806514760904; 0.0011178649645521383 0.0017776570683694555 -0.007441504773914846; 0.0003701202776515255 -0.00018764676188615106 -0.00041516280015050527; 0.000385351647784362 -0.00017578615788521831 -0.001266045522129282; -0.00012572993847924244 0.000605099091359754 -0.001283965407614426; 0.0003694606139805658 -9.631343819655776e-5 -0.0015407231550873186; -0.0001063160727981657 0.001009716264958086 0.00028809555721367986; 0.001496749702766827 0.0012479322373838415 -0.0011381882954518007; 0.0005928334697507937 0.000362157832195907 -0.0006488857230238261; -0.0018189888960842733 -0.0022350240146347365 -0.0024073261627335675] %
+
+Mass Used: 123.8022044552672 kg
+Launch C3: 93.65586826221922 km²/s²
+||V∞_in||: 0.017445894922432696 km/s
diff --git a/archive/ES_0.5743956317149539 b/archive/ES_0.5743956317149539
new file mode 100644
index 0000000..101c1bf
--- /dev/null
+++ b/archive/ES_0.5743956317149539
@@ -0,0 +1,22 @@
+archive/ES_0.5743956317149539---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T14:56:46.131
+Launch V∞: [6.802649344955996, -7.125774100871023, -0.10083137735018498] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.421746894388335e-9, -3.3221489073532405e-9, 7.486839892392244e-9] km/s
+ V∞_out: [2.208637204047605e-9, -4.768542854034313e-9, -6.497171361760646e-9] km/s
+ time of flight: 1.8405216870471796e8 seconds
+ arrival date: 2029-02-20T20:32:54.131
+ thrust profile: [0.32801051856196967 -0.08755356794538854 -0.09606773115600332; 0.13591199072342033 0.04376946020760862 -0.11781474165243486; 0.10830340993474953 0.06818566384053301 -0.15675858327819087; 0.11245372916584745 0.0975026488247323 -0.2273003156294621; 0.058979407490218815 0.0636268959781501 -0.1560363779873259; 0.03215267631021546 0.041321314762158945 -0.10657732660411526; 0.011616378297709659 0.01759645831277021 -0.04892230755069827; 0.0027977994374392186 0.004937362742264725 -0.01347764671726684; 0.0016573004803935691 0.003194409080850283 -0.007951077813144991; 0.001995344036941391 0.0042763063061741526 -0.016452381419258616; 0.0015227000926776786 0.0011927276653512858 -0.0021034506597534795; 1.6773470902179646e-5 -0.000145538097327937 0.0002588372213611929; -0.00046523457080746165 -0.0006392989589920557 -0.00025696984131058555; 0.00020654894740293136 -1.203798430499521e-5 0.0010758597026974174; -0.00042238958007994926 -0.0003885274677129316 0.0014264555843669022; 7.222250432712524e-5 0.00041463557288511674 -0.0008824439657503076; -0.0018320340601609146 0.0006705583855815013 -0.0005671982267425535; 0.001085660665088009 -0.0012457602761645624 -0.0018087751214692985; -0.0006746926233091558 -0.00028025822946019854 -0.00017367996536293633; 0.00019364310926014598 0.0010830097912675352 -0.001943398991608916] %
+
+Mass Used: 103.92821092067152 kg
+Launch C3: 97.0628616137328 km²/s²
+||V∞_in||: 9.30813034583085e-9 km/s
diff --git a/archive/ES_0.5744162587529422 b/archive/ES_0.5744162587529422
new file mode 100644
index 0000000..837e6a8
--- /dev/null
+++ b/archive/ES_0.5744162587529422
@@ -0,0 +1,22 @@
+archive/ES_0.5744162587529422---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T22:28:14.684
+Launch V∞: [7.26592218345945, -6.753081076235253, -0.21529556629801583] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005025542239282903, 0.008235544225020118, -0.0001229695660815061] km/s
+ V∞_out: [0.007987447342814797, -0.0012714082745065016, 0.0016333989655466026] km/s
+ time of flight: 1.5159517290569288e8 seconds
+ arrival date: 2029-02-26T12:14:26.684
+ thrust profile: [0.2295883715439873 -0.06283003092969039 -0.09728469734753073; 0.08145903468642135 0.01581540862298228 -0.09615771977283886; 0.09383497831619358 0.03805650030128938 -0.18182208612557804; 0.08713135571437731 0.04660397159116298 -0.23140114235248233; 0.06046876497375905 0.03763641395226061 -0.20350814333585288; 0.027748757114425544 0.01868484024035271 -0.11257858618219811; 0.028469457984993087 0.020771534740274256 -0.13248854690672476; 0.013799504016527665 0.010398719393442099 -0.07082795332536744; 0.009401415623639112 0.007546339158588131 -0.0555015824756225; 0.00585509277791709 0.004732073682332378 -0.042244701908194564; 0.003520116696513443 0.0010004672014734082 -0.014564077364859042; 0.0032883664150614774 0.004230527097517645 -0.00704942163810751; 0.013402015096577694 0.004887603050109343 -0.007303202565061475; 0.0012735118215268727 4.5378765364084716e-5 -0.0008110887671058777; -0.0003046265669059377 0.0011015365057437023 -0.010088438979163266; 0.005191593904994969 -0.0018435223500298534 -0.005210395159545571; -0.008354235948856401 0.008115942266359897 -0.0041592445684139855; -0.005130956701855084 0.0012785619918184896 -0.0009883363752961473; 0.01099212530369514 0.0009704855374609524 -0.019935791234490286; 0.0002964730978739651 -0.0018687490254904243 0.0012967196857923864] %
+
+Mass Used: 95.8951604999852 kg
+Launch C3: 98.44408137916241 km²/s²
+||V∞_in||: 0.008251779865243175 km/s
diff --git a/archive/ES_0.5744193871561453 b/archive/ES_0.5744193871561453
new file mode 100644
index 0000000..2daa3b9
--- /dev/null
+++ b/archive/ES_0.5744193871561453
@@ -0,0 +1,22 @@
+archive/ES_0.5744193871561453---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T12:47:05.903
+Launch V∞: [7.33237686619863, -6.078709069477498, 0.22159627192591588] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.81341014837359e-10, 2.0220364083828872e-9, -1.7636552561244343e-9] km/s
+ V∞_out: [1.539324738820847e-9, 2.5810084190677653e-9, 6.668253860035488e-11] km/s
+ time of flight: 1.6587097965695837e8 seconds
+ arrival date: 2029-08-04T08:03:24.903
+ thrust profile: [0.7282779955955166 -0.08595262818070842 -0.15565402748392862; 0.3455744010520038 0.16265112633678983 -0.23638176582924494; 0.1514570080119518 0.12733120564081518 -0.1870333378284255; 0.05095594820295341 0.06041199113181463 -0.0973386317634473; 0.0510507058750954 0.07436350125155262 -0.12542124734259283; 0.04635496554323442 0.08028829790370905 -0.1409700818186271; 0.027297664051866073 0.05356706420917507 -0.09778497117260522; 0.009909766974332785 0.025203394395604727 -0.05036081969342113; 0.001955164519575757 0.005449956732301597 -0.011915224750937873; 0.001855868513083727 0.0055510617186649265 -0.012378226590050605; 0.0006635163868639118 0.0022274056287228433 -0.005128478882559093; 7.394433534418578e-5 0.00013664857645960917 -0.0003546221714608729; 5.7932518387811694e-5 0.00022616948480316373 -0.000397786360823753; -3.8404130731005957e-5 0.0007205734929082357 0.00014371561113970708; 9.049003527397014e-5 0.000650175364378613 -0.0007863152375010106; 0.0005426578655439754 0.00016278220701940315 -0.0007081177755251803; 0.00045527503162826825 8.117878783816884e-5 -0.0005446478297930367; -4.813022495668381e-5 7.953812481594088e-6 -0.00037465751895554637; -2.4540043647020655e-5 0.0005869452388654602 0.0002344574895956149; 4.335057298061781e-5 0.0006593705326005618 -0.00044850986374890935] %
+
+Mass Used: 140.70185537441102 kg
+Launch C3: 90.7635593670443 km²/s²
+||V∞_in||: 2.7682732303334714e-9 km/s
diff --git a/archive/ES_0.5744723248293575 b/archive/ES_0.5744723248293575
new file mode 100644
index 0000000..3f7ccdf
--- /dev/null
+++ b/archive/ES_0.5744723248293575
@@ -0,0 +1,22 @@
+archive/ES_0.5744723248293575---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T14:59:59
+Launch V∞: [5.741868578343162, -7.664072905978784, 0.41787591955692255] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.468402971455486e-9, 2.691593869071894e-9, 1.710025281499405e-8] km/s
+ V∞_out: [-9.080844925657304e-9, -1.2463205141569943e-8, -6.521321933662256e-9] km/s
+ time of flight: 1.670290958955799e8 seconds
+ arrival date: 2028-08-05T19:58:14
+ thrust profile: [0.5142537131232586 -0.17306023866424416 -0.12269921587327814; 0.3356168807863016 0.08057804638264562 -0.22972642463735576; 0.16523141691807833 0.08871177646874322 -0.19261246391413508; 0.09589172800503863 0.0695948925648316 -0.15422569383862908; 0.09450715896960693 0.08889869163810922 -0.18473061147419914; 0.06939570191883185 0.0691422450472252 -0.16360950138379382; 0.016791948009985576 0.018804051899589412 -0.046514887683894425; 0.011667896150457551 0.014465890469841609 -0.0366473946920136; 0.0031017957062270656 0.004002211357184874 -0.005565894910412778; 0.0032759085780309652 0.0030123834529291725 -0.007897593290300684; -0.0008836190112589573 -3.4981563051424396e-5 -0.003036735310799371; 0.0011075031635151115 -0.0008284980122521958 -0.0003629790294905715; -0.0066913638851100205 0.0011050561038250131 -0.00758499190673252; -0.0010508911327043644 0.0013138510235345007 -0.0011359678984275904; 0.003457968847830362 0.002838534979764947 0.0020503695613930473; 0.0052445394107241295 0.008064028726034995 -0.0014885526335595527; 8.686955655875779e-5 -0.00012101994712070845 -0.0015304149177074197; -0.002647963281199822 0.004671416030825224 0.0018592028550716237; -0.00021903784124921162 -0.008762006359668385 0.0013685356848705545; 0.00029896679765456275 0.009539351926951226 -0.0008774377639749847] %
+
+Mass Used: 134.2411956818528 kg
+Launch C3: 91.88168856326816 km²/s²
+||V∞_in||: 1.7485889657727674e-8 km/s
diff --git a/archive/ES_0.5744933819344222 b/archive/ES_0.5744933819344222
new file mode 100644
index 0000000..6cace0b
--- /dev/null
+++ b/archive/ES_0.5744933819344222
@@ -0,0 +1,22 @@
+archive/ES_0.5744933819344222---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T18:10:01.996
+Launch V∞: [6.559589486409153, -7.329035001557215, -1.3748726610399256] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8688783986054539e-6, -2.16849818292708e-6, -2.5931105995004633e-6] km/s
+ V∞_out: [-3.830982518670762e-6, -4.754164906984016e-7, -7.884970693026882e-8] km/s
+ time of flight: 1.874957778649008e8 seconds
+ arrival date: 2029-04-06T20:19:38.996
+ thrust profile: [0.1282068149146869 -0.051862007233424046 -0.06242180744782415; 0.13290532314603634 0.04557047712172772 -0.10715973699080651; 0.15067804565967463 0.09553808028191993 -0.2132930033286993; 0.06955712449829529 0.0705898761982037 -0.1352473139794934; 0.06285179762269646 0.07046187536016965 -0.16000258848234475; 0.040431289635762376 0.05588503371342994 -0.12875636612938413; 0.012212889445265752 0.023376661182888777 -0.0590730484734703; 0.008596698999753207 0.019322650572440626 -0.05178781528711633; 0.0016030964490948893 0.004060952775169433 -0.018595292366900575; 0.0007917130617359852 0.00171523879219043 -0.00720231929159661; 1.0924063761919836e-5 0.0006404460682180287 -0.002689203984435137; -0.0007320439020670556 -0.0011946385689158294 -0.0017418717516573718; -0.0001606851890402607 2.850586447553441e-5 -0.002337076905752188; -0.0001878801581620843 -0.0008386153454197469 -0.0008951902431331924; -0.0017345037978944626 -0.0006376124174368987 -0.001962031837638788; 0.0001905082050789541 0.0030017973174467317 -0.00017785812821141065; 0.0001969294859423761 -1.8394118736710433e-5 0.0010794346498356829; -0.0005511997623944562 -0.0007654760550716397 -0.0004665486532048841; -2.9129471131002526e-5 -0.00028943834926099105 0.000540153491819071; -0.00031735550487091966 -0.0001106393793826337 0.0004947008024930198] %
+
+Mass Used: 94.88169406653697 kg
+Launch C3: 98.63324311833526 km²/s²
+||V∞_in||: 3.862552707649928e-6 km/s
diff --git a/archive/ES_0.5745124956561825 b/archive/ES_0.5745124956561825
new file mode 100644
index 0000000..3e7f1bd
--- /dev/null
+++ b/archive/ES_0.5745124956561825
@@ -0,0 +1,22 @@
+archive/ES_0.5745124956561825---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T12:35:00.823
+Launch V∞: [6.412509649985214, -7.871026719654803, -0.6031485697348018] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.6178202044996527e-9, -3.239522721792389e-9, 6.023281668491974e-9] km/s
+ V∞_out: [1.8625579802645563e-9, -4.553418199432251e-9, -5.7480869858224155e-9] km/s
+ time of flight: 1.874957778307353e8 seconds
+ arrival date: 2029-04-17T14:44:37.823
+ thrust profile: [0.0486346743381039 -0.01867812814365371 -0.0252297589419257; 0.02464248711295292 -0.0016124522434274432 -0.04047149954894883; 0.022556414936935026 -0.0006207646335808686 -0.06320693426827642; 0.028349236570988888 -0.0016922591553774344 -0.1096215525956999; 0.023297318831802714 -0.0028557992239410636 -0.11233935482805504; 0.015703081411347422 -0.0031027792740703102 -0.08879289639786556; 0.011860611154589657 -0.003960362218572591 -0.07724560913847882; 0.021172669926475603 -0.006784116641983855 -0.14616172422480964; 0.007149528099172436 -0.003548975243799609 -0.04942929640356204; 0.009355144407572404 -0.004345494577779154 -0.07284610264242962; 0.003124869373518244 -0.0017167158297330114 -0.025144816168099635; 0.0006943155529481412 -0.0004893592363513172 -0.006677342818153164; -0.00013711110576317001 0.0014088945851066141 -0.007485650912153456; -0.00040908667288826694 0.0002865375869865834 -0.0012938391400055297; -0.0012988674981585322 0.001977651373057836 -0.003373881409253328; 0.0011457968715965557 -0.000970270127388155 -2.7243603277390428e-5; -0.0003483336540173826 0.0007503942463466164 -0.001132177540490273; -4.5532349046500074e-6 0.0020029448083572574 -0.0010199158090747331; 0.0025023892891375076 -0.00031574375269245307 -0.00025421133306775335; 0.0013870606187441274 -0.0020852610882328175 9.052306311019913e-5] %
+
+Mass Used: 66.88132092477508 kg
+Launch C3: 103.43712982984647 km²/s²
+||V∞_in||: 7.737121722907463e-9 km/s
diff --git a/archive/ES_0.5745311681034032 b/archive/ES_0.5745311681034032
new file mode 100644
index 0000000..fcc400a
--- /dev/null
+++ b/archive/ES_0.5745311681034032
@@ -0,0 +1,22 @@
+archive/ES_0.5745311681034032---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-08T12:59:42.829
+Launch V∞: [6.270217393404503, -7.9894448019979585, -0.29867141395940844] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005613731416615637, -0.0006886635806302653, -0.00048591375272129413] km/s
+ V∞_out: [0.0006436568366258338, 0.0003300082368812008, -0.0007096631717292137] km/s
+ time of flight: 1.8258565492782792e8 seconds
+ arrival date: 2029-02-18T19:13:56.829
+ thrust profile: [0.05223715808918762 -0.024213458795433362 -0.03064041848231526; 0.027493288591585265 -0.0050814956335679135 -0.05081310904948665; 0.03255438911837143 -0.0073821248305197505 -0.10481677356294863; 0.02129498084376045 -0.006327954079911044 -0.09104052546034827; 0.021725582345513958 -0.00981522438741727 -0.11605480952780871; 0.019402493201203543 -0.009826107325762536 -0.12003970793100076; 0.02801070630966359 -0.017064156059297755 -0.18739423471555228; 0.010562949328595599 -0.007239178481146251 -0.07829203222029357; 0.009353986541694037 -0.006699004366789015 -0.06897100115995976; 0.003056674424510935 -0.0025622505483294472 -0.024912943515431347; -8.047676333273448e-5 7.42902079880698e-5 -0.000357129227253539; 0.00010421899268484242 -0.00010924444844327287 -0.0005749144834754988; 8.604232371307337e-5 -4.94462353612797e-5 -0.0006035321147980146; -0.0002536489439317495 3.1418445709595713e-6 -5.2013660637616936e-5; -4.4843049508017834e-5 -3.820944402367643e-6 -0.0003230267002217782; 0.0004213948660476552 -0.0002192027648581499 -0.00045431732774087863; 8.306658671670705e-5 0.00015689341935088167 -0.00024048003176977691; -8.059411665585069e-5 -4.297218733023396e-6 -0.0005652351329492341; -2.4069332965858515e-5 -4.432778025089624e-5 0.00022526659376832076; 0.0002508038407907023 -0.00013689129314809324 3.2166346047107124e-5] %
+
+Mass Used: 68.07601851423078 kg
+Launch C3: 103.23605901824108 km²/s²
+||V∞_in||: 0.0010126744326530432 km/s
diff --git a/archive/ES_0.5745856914948658 b/archive/ES_0.5745856914948658
new file mode 100644
index 0000000..2298464
--- /dev/null
+++ b/archive/ES_0.5745856914948658
@@ -0,0 +1,22 @@
+archive/ES_0.5745856914948658---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T04:23:39.382
+Launch V∞: [7.644974153703848, -6.461508697263512, -0.12531665341199355] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00010374619158209846, 8.471577020401579e-5, 6.826356018229899e-5] km/s
+ V∞_out: [1.3272912140504788e-5, -9.657530766723772e-5, 0.00011460112470802052] km/s
+ time of flight: 1.8749577779953855e8 seconds
+ arrival date: 2030-05-01T06:33:16.382
+ thrust profile: [0.3337210247260808 0.015725239636325404 -0.13599008083663286; 0.05004728589566083 0.023595251821796538 -0.06843715235924201; 0.053550252087670835 0.04115520842109381 -0.12897812299704664; 0.04590622818618035 0.045883500938216915 -0.16014417883388293; 0.03380997378156108 0.03850428071332059 -0.15426132913523036; 0.016234814248731612 0.0179678848662789 -0.09046742288880612; 0.006763643858574238 0.007878619529211258 -0.04568697393419634; 0.0016914817526042538 0.002239541347982432 -0.009761798830986969; 0.0015740424341551757 0.001236879054561119 -0.00518106936100491; 0.00029737243856688887 0.00012880932618728423 -0.0014307754408757881; -0.00039893709366357313 -4.901568826580263e-5 0.001951925422507432; -8.53335504208982e-5 -0.0008233565489513127 -0.003777793399520857; 0.006146806213969137 -0.004403911981102458 -0.0022776506717773633; -0.0007695721999676945 -4.886384623473727e-5 0.0004863723672743356; -0.0015219246121424331 0.00604628005671785 0.004358345928239404; 0.004466048796312362 0.0010807213312535877 -0.003968575403621167; 0.0033114323878724056 0.003381400805087304 -0.0038953747540509797; -0.0018033169141989714 0.0008940186047241755 0.00799289991926692; -0.0008601634384369372 0.001177278613812597 -0.006190054384405596; -3.2207280382121083e-5 -0.007711325111588502 0.009848407462611163] %
+
+Mass Used: 85.77747254847691 kg
+Launch C3: 100.21242871923425 km²/s²
+||V∞_in||: 0.00015033278962957961 km/s
diff --git a/archive/ES_0.5746128528938002 b/archive/ES_0.5746128528938002
new file mode 100644
index 0000000..b753005
--- /dev/null
+++ b/archive/ES_0.5746128528938002
@@ -0,0 +1,22 @@
+archive/ES_0.5746128528938002---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T02:17:59.998
+Launch V∞: [7.116476207502739, -6.614686183078417, -0.4433243337543846] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3024409326172732e-8, -8.486398449767864e-9, 6.929069566538978e-9] km/s
+ V∞_out: [-5.983779221600116e-9, -1.139470699306042e-8, -3.7492665160703123e-10] km/s
+ time of flight: 1.502549398196025e8 seconds
+ arrival date: 2029-02-08T03:46:58.998
+ thrust profile: [0.5961995518255412 -0.1492390205752341 -0.20882383242272937; 0.1271186371443471 0.03422531770692585 -0.13310472826922531; 0.0998567529606582 0.0522922211226219 -0.1695054300198962; 0.06669416796841587 0.048735613864870325 -0.16007767999210343; 0.04740988409381709 0.04197488867158904 -0.14754174059622113; 0.04171463511517462 0.04225724317382311 -0.15537549815980867; 0.011790500855549474 0.012567054309717317 -0.05143720002270058; 0.049246396968812216 0.05997246538514711 -0.22458736325591458; 0.007424355433295871 0.009033566435444472 -0.039112175271640154; 0.010212264543311306 0.013008472468566411 -0.0589645494356823; 0.0008835089951066451 3.93396475890013e-5 -0.005445781142088199; -0.0028934181113190074 2.8386746662629222e-5 -0.003381309410737748; -0.000670680292531215 -0.0005547597215124927 -0.0014587530685895669; 0.0026012793955107836 -0.0007397742450684765 0.00044105559713185664; 0.0011622504501989156 0.005589812868169513 -0.0012583604863933488; -0.0010305424167004196 -0.0016794051088184297 0.0025752026233511966; -0.0013089571111058972 0.00011561330199363743 -0.0007497915573693386; -0.0003333905788261162 -0.0024777571796342113 -0.002935131092139531; 0.0034225212198047833 -0.004121974637699265 0.001702761917529248; 0.0014769941181765334 0.00012927183107580326 -0.006439994195988086] %
+
+Mass Used: 118.57840867425102 kg
+Launch C3: 94.59484337745985 km²/s²
+||V∞_in||: 1.7019582897411273e-8 km/s
diff --git a/archive/ES_0.5746405519939582 b/archive/ES_0.5746405519939582
new file mode 100644
index 0000000..a364d71
--- /dev/null
+++ b/archive/ES_0.5746405519939582
@@ -0,0 +1,22 @@
+archive/ES_0.5746405519939582---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T23:39:21.462
+Launch V∞: [5.527605631237921, -8.011498382599774, -0.43146380972951753] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.06858079909591e-8, -2.8933453594806772e-8, 6.139422158325882e-8] km/s
+ V∞_out: [2.6146192375416824e-8, -5.810590086747456e-8, -7.529958315694954e-8] km/s
+ time of flight: 1.5021046205123603e8 seconds
+ arrival date: 2028-01-25T12:47:03.462
+ thrust profile: [0.48754630663701193 -0.25649158618413975 -0.21829858775368768; 0.1374897388708944 0.00014879205970727338 -0.14768739305875614; 0.14048825314437688 0.031151393003042243 -0.23604241875778567; 0.11589178761931068 0.04148202714476008 -0.2607792061865285; 0.07929411380451165 0.03588316481793693 -0.22066175854097944; 0.04990056659948182 0.026165750862246987 -0.16385429612495125; 0.02934856243494251 0.017243515316137253 -0.11066319693971671; 0.004957381820826211 0.002894832452423072 -0.021517281260396225; 0.0034831161753698784 0.002334752065719272 -0.016442196121729657; 0.000975730265294618 0.0006352239874038418 -0.005077000639284237; 0.0007691150937331667 0.0004770206974637723 -0.0031591534554801935; 0.0009545833341377659 -0.00013692913617504004 -0.0034510493564464256; 0.0009558599260037768 -0.0002313278057727295 -0.0020627836565252347; 0.00033703637312897816 4.4247560068193074e-5 -0.002058942307266142; 0.0004154831454779651 -0.0013221100589267338 -0.0021338892203298285; 0.001342767530058942 0.0010676607783659052 -0.001161878009799423; 0.0010654131044822292 0.00019628910895876306 -0.001112825897986908; 0.0007634879202462917 0.00041447696109622674 -0.001683792990960589; -0.0004374500670036091 -0.000250556325534139 1.618893221983788e-5; 0.0001423389036999135 0.00014494167721298317 -0.0011730107049400746] %
+
+Mass Used: 116.6866110129613 kg
+Launch C3: 94.92469136799828 km²/s²
+||V∞_in||: 9.799427856804629e-8 km/s
diff --git a/archive/ES_0.5747326674185123 b/archive/ES_0.5747326674185123
new file mode 100644
index 0000000..03cf681
--- /dev/null
+++ b/archive/ES_0.5747326674185123
@@ -0,0 +1,22 @@
+archive/ES_0.5747326674185123---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T00:01:13.804
+Launch V∞: [7.1518451425851755, -6.625397995817593, -0.38867862160910455] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0024881094950463508, 0.03769950507379175, 0.004571720822774835] km/s
+ V∞_out: [0.03648138026847228, -0.006705357357019816, 0.008436892631900313] km/s
+ time of flight: 1.5000220979253432e8 seconds
+ arrival date: 2029-02-05T03:18:02.804
+ thrust profile: [0.47899409865550735 -0.1263568049034128 -0.1816784871578228; 0.19843817689766902 0.04942467162408709 -0.2055834332125781; 0.10354681549537954 0.05227754690753136 -0.18050744851412795; 0.09356733714077373 0.06337559113929254 -0.2245856734098498; 0.05834485037841577 0.047742617550388354 -0.18073962149517706; 0.04577137949590398 0.042663695683392386 -0.1704253222458832; 0.012435116135308424 0.01199791853659917 -0.05454002453107444; 0.004896209007294114 0.0053389698333902915 -0.024379302699552515; 0.012045121392365259 0.013691960323329727 -0.0656805901483432; 0.0022799145546838957 0.0018144197028636005 -0.016207254693469578; 0.0067295381139998054 0.00872996751852977 -0.043693523187243365; -0.0025349587035150916 -0.00010173979911510958 -0.006310940054488182; -0.0028429893328069467 0.0012286511960396126 -0.0019334178624973485; -0.004844275892954259 0.004195663421364189 -0.005990212036898304; -0.006764670583876727 -0.0003884869415207129 -0.0035974723177752046; 0.002098761794042327 0.0015462410057089074 -0.004101970214127097; -0.0020367850819440294 -0.0008704430233627343 0.0003249740506876724; 0.005568629923340828 -0.002787141256358442 -0.0013473994815340574; 0.008787734079386099 0.004354930900683313 0.0017213537953539226; -0.004065754854419205 0.0027095189744873044 0.0019416879664026282] %
+
+Mass Used: 115.21227005343735 kg
+Launch C3: 95.19585861739891 km²/s²
+||V∞_in||: 0.03805711501085681 km/s
diff --git a/archive/ES_0.5747406675491469 b/archive/ES_0.5747406675491469
new file mode 100644
index 0000000..2b3e37a
--- /dev/null
+++ b/archive/ES_0.5747406675491469
@@ -0,0 +1,22 @@
+archive/ES_0.5747406675491469---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T19:47:46.169
+Launch V∞: [5.694487737167067, -7.9378185305170605, -0.1531492552190633] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.119149037362895e-5, -0.00012134654085031186, 2.163563296951094e-6] km/s
+ V∞_out: [2.653880970091779e-5, -6.518975888374154e-7, -0.0001494731907850131] km/s
+ time of flight: 1.5758158633545247e8 seconds
+ arrival date: 2028-04-20T16:27:32.169
+ thrust profile: [0.36450844843637215 -0.16623167078351533 -0.13096600557146293; 0.12088714552164029 0.011513977158994389 -0.11595436763776758; 0.1126474453911718 0.03697859137590781 -0.16809805184512885; 0.17107868132410584 0.0821657729415789 -0.32291753088566905; 0.05393462541577929 0.03432924221840385 -0.14024709980030528; 0.033370003556434706 0.02487425718993078 -0.10344080020059673; 0.027373757839903333 0.02150391281675356 -0.09442724657851942; 0.03390063869647174 0.02930495340140443 -0.12921245874036738; 0.009815565453009273 0.00928493297494257 -0.04187490827231189; 0.006223856202055213 0.0026283999996853675 -0.008918834571483463; 0.0030752856456769313 -0.0009941796199843663 -0.0014653944377049605; 0.0044147690245492175 -0.003969059854336826 -0.0026946722901425016; -0.0014427101281778805 0.0004542837019830509 -0.0008010342998881485; -0.0011041813383178745 -0.0005817122802879365 -0.003307836901379084; -0.0023471823513260197 -0.0016085436811692235 0.0007298097798064344; 0.006023850794937625 0.0031734266530845257 -0.009105516607617976; -0.013745516517869882 -0.0023438180516463444 -0.014560074302649079; -0.0013564136340714471 0.0005430548347672586 -0.0012410879130855762; 0.004848008134515774 0.0047762155300223805 -0.0036297141821227145; 0.008564929421622253 0.02284489266820393 0.0018093250866237582] %
+
+Mass Used: 113.68306368585309 kg
+Launch C3: 95.45960830654028 km²/s²
+||V∞_in||: 0.00015180761475973455 km/s
diff --git a/archive/ES_0.5747849648335056 b/archive/ES_0.5747849648335056
new file mode 100644
index 0000000..c17f378
--- /dev/null
+++ b/archive/ES_0.5747849648335056
@@ -0,0 +1,22 @@
+archive/ES_0.5747849648335056---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T23:23:12.951
+Launch V∞: [6.285648078591361, -7.69796912139325, 0.0319387374453925] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.019015549625054144, 0.008730086628023099, -0.02116716105938805] km/s
+ V∞_out: [0.0188094652585137, 0.007461963264123278, 0.021803711529438205] km/s
+ time of flight: 1.79823278854803e8 seconds
+ arrival date: 2029-01-11T06:17:50.951
+ thrust profile: [0.16598202997745407 -0.05644854103147593 -0.06664072451226309; 0.05501762569830522 0.006740058599012298 -0.06560125614695743; 0.05385423797153818 0.016522478385950563 -0.10640203787581164; 0.048296226206059584 0.021728391295643364 -0.13182177868169279; 0.03592004095434385 0.018367781991140038 -0.12430488964982087; 0.026134495742443503 0.014118107291065824 -0.10590033910606193; 0.023503143451658437 0.016525865473360556 -0.12041698959362687; 0.022181163125242244 0.0145548667524977 -0.11847172361905889; 0.0048394143992123865 0.005041900850334857 -0.022179606943364738; 0.0031029091333490996 0.0041623064852347996 -0.020781099014905643; 0.00032093934702648 -0.0018255003583333117 -0.0072276007962827115; 0.0010695302084479295 0.0018194218581069348 -0.0096021650243894; 0.007349330748672302 0.003388342267756248 -0.029180052163632987; 0.005191841429353158 0.005201555499321581 -0.0052970082861202175; 0.01007672069509856 0.02462339047066742 -0.017548013723621286; -0.002038876500398516 0.0002291990179332131 -0.0017915742443070164; -0.0030301866969837297 0.0319438117612605 -0.02480022275811506; -0.010310583112998511 0.02800217184122703 -0.055605995788537046; -0.011541043886736574 0.008318532633108812 -0.0025936991512182693; -0.004106630925627751 -0.013665990737940477 0.04053449667304856] %
+
+Mass Used: 94.42925637791495 kg
+Launch C3: 98.76912044477284 km²/s²
+||V∞_in||: 0.029763303704222057 km/s
diff --git a/archive/ES_0.5747974566123688 b/archive/ES_0.5747974566123688
new file mode 100644
index 0000000..d3e5670
--- /dev/null
+++ b/archive/ES_0.5747974566123688
@@ -0,0 +1,22 @@
+archive/ES_0.5747974566123688---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T13:20:18.137
+Launch V∞: [6.726065704697215, -7.2806613974106495, 0.24678751859547646] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.155711012637257e-8, 7.868317691182023e-8, 4.399828373352752e-8] km/s
+ V∞_out: [-2.53047084965871e-8, 5.1885842955658075e-8, -8.098027926524746e-8] km/s
+ time of flight: 1.8384908389744487e8 seconds
+ arrival date: 2029-02-22T10:31:41.137
+ thrust profile: [0.17544515367293706 -0.05068485680290517 -0.058092977662581154; 0.07235071064265487 0.01752148593874962 -0.07168459288052483; 0.12302479687825986 0.06198933069054483 -0.2023337400547829; 0.05602553914258306 0.03795576570302335 -0.13030187230820595; 0.06663728151799063 0.05417295223785613 -0.194238109782815; 0.023381079051557705 0.022464200776354772 -0.08604109056838537; 0.018368396357870825 0.019021542852586865 -0.07891884541512352; 0.005942343202044479 0.005612364963450975 -0.024841530637805004; 0.0009929338842170257 0.0008321136161707765 -0.005128461007263279; -0.006009552525847613 0.004725157967082579 -0.0002699150022949788; 0.007297666296752773 -0.0012154037012878788 -0.01049875979232836; 0.003942039205271818 -0.001654490058638498 -0.011987967492943025; -0.0015604202006814366 0.005185627817737612 -0.004217307053425043; 0.0015240502239413506 3.425246227315923e-6 -0.004135846883117827; -0.04014203805599443 0.018836541795359908 -0.02857464980402404; 0.00655191772157444 0.0038763520639076288 0.00017098219932930466; 0.04664581064472817 0.01408295570215195 -0.017172343323352605; 0.010344803160428413 -0.003939215211099715 -0.006166196550976834; 0.007725216689610167 -0.004097023795363857 0.025995125519770235; -0.008554449452701701 0.0035220698696255427 -0.02275366788694135] %
+
+Mass Used: 97.12848247368947 kg
+Launch C3: 98.30889432698415 km²/s²
+||V∞_in||: 9.926673512556083e-8 km/s
diff --git a/archive/ES_0.5748018806272901 b/archive/ES_0.5748018806272901
new file mode 100644
index 0000000..31aa68e
--- /dev/null
+++ b/archive/ES_0.5748018806272901
@@ -0,0 +1,22 @@
+archive/ES_0.5748018806272901---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T22:48:00.397
+Launch V∞: [5.690295602157443, -8.028129850510018, -0.2746988058898055] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0146106506744848e-5, 1.7558115948667043e-6, -2.2241126033280026e-6] km/s
+ V∞_out: [1.010421112967156e-5, -2.6909560847240138e-6, 1.2757429066566696e-6] km/s
+ time of flight: 1.5717113473766643e8 seconds
+ arrival date: 2028-04-18T01:26:54.397
+ thrust profile: [0.3286157043724979 -0.16363192729207018 -0.1397327171238639; 0.05359672650737234 0.002244042066349031 -0.062376885129673834; 0.08997156583785815 0.02115142364153054 -0.15583403549345887; 0.09871886556523067 0.03082526773238776 -0.22911772146283219; 0.0524606343777429 0.02444641054762247 -0.1547056424311052; 0.038970807128310574 0.02141878561639082 -0.13665365997262646; 0.019972178249941495 0.012895662714984409 -0.0925837894413179; 0.025946661069173243 0.017130692101013114 -0.12811913386029802; 0.023386985715413207 0.017234232181803383 -0.09872447954654723; 0.003188594729249413 0.0009253319956908789 -0.01663254150502546; 0.006677903321431761 0.005264517708572393 -0.031061389002192623; 0.0017682279892148123 0.0007798057863745188 -0.011916079416790393; 0.0016488586742226645 0.004046683557787185 -0.0029957206237353003; 0.0026060561999888612 0.0015038178641798997 -0.008803390383251621; 0.0034939512293341666 0.003440311573258369 0.001667853672855978; 0.004763278033254229 -0.0027612985913645057 -0.011324107802362626; 0.0011402103195972259 0.0011074681010677366 -0.00843065247538423; -0.0040483763807155695 -0.002135165714437434 -0.003298597629985205; -0.0016550282622888144 -0.010384461950943271 0.0030947607307833455; 0.0012275029351004158 0.0009128086293591403 -0.017125983351908042] %
+
+Mass Used: 105.31840523702385 kg
+Launch C3: 96.90579237053964 km²/s²
+||V∞_in||: 1.0534373663163888e-5 km/s
diff --git a/archive/ES_0.5748125532853552 b/archive/ES_0.5748125532853552
new file mode 100644
index 0000000..3136827
--- /dev/null
+++ b/archive/ES_0.5748125532853552
@@ -0,0 +1,22 @@
+archive/ES_0.5748125532853552---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T09:38:49.963
+Launch V∞: [5.64217338437802, -7.99545737158784, -0.18550924584892395] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.570977974073115e-7, 2.3333386323302276e-7, 1.2220518803526504e-6] km/s
+ V∞_out: [-8.829247913615367e-7, -7.995306331176186e-7, -3.8336952838112185e-7] km/s
+ time of flight: 1.5255498858127305e8 seconds
+ arrival date: 2028-02-22T02:01:57.963
+ thrust profile: [0.39684227611119044 -0.20152433134631098 -0.16872883633568472; 0.1152381405067494 0.0021039063987776997 -0.12754064025090625; 0.15149323666974737 0.037918000925917995 -0.2582731858848025; 0.11645228714567388 0.04570395663972826 -0.26609695820303586; 0.046410362140571745 0.021830279268737374 -0.13307157412690382; 0.033507001650118724 0.018224847324493275 -0.11426686949557378; 0.026392832640311538 0.016164544409450612 -0.10331779740732377; 0.02105596919484424 0.01496998539913853 -0.09447604342711646; 0.00673974015876716 0.004445967871384201 -0.03183859921022258; 0.014642435301262333 0.008879510538147973 -0.06535125928683204; 0.0007946266911066954 0.000496676795264352 -0.0042620095045286304; 0.0004257080741312078 0.00029786105986407183 -0.00250478292320558; 5.4432206133870915e-5 0.0006296956313339175 -0.0016663687173002492; -2.6828866051106922e-5 -0.00039222894436327584 -0.000383647480028581; -0.0017993881177243531 0.002761817705708652 -0.008338048045224162; -0.0013803846951630607 0.001040066915314972 -0.003077401968707223; 0.0008574195078363091 0.0001717716785805774 -0.0007095488102779848; -0.00036874225645291194 0.0008451567925050572 -0.00025673407138746365; 0.0002343575109652391 -0.0009351202388873079 0.0022424076580763435; 0.00015337854426500461 0.0006375196039711713 -0.0010537485840059445] %
+
+Mass Used: 111.80538772966247 kg
+Launch C3: 95.79587276055747 km²/s²
+||V∞_in||: 1.254007658650825e-6 km/s
diff --git a/archive/ES_0.5749051414709718 b/archive/ES_0.5749051414709718
new file mode 100644
index 0000000..c78cf73
--- /dev/null
+++ b/archive/ES_0.5749051414709718
@@ -0,0 +1,22 @@
+archive/ES_0.5749051414709718---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T21:58:05.138
+Launch V∞: [6.375517518316555, -7.887578403044686, 0.12346237971754738] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.335054664972428e-7, 0.00029946108478200726, -0.00019725911950082965] km/s
+ V∞_out: [-0.00016286457076921323, -0.0003126455986170411, 6.556728111666893e-5] km/s
+ time of flight: 1.8749577787482917e8 seconds
+ arrival date: 2029-04-18T00:07:42.138
+ thrust profile: [0.0982028491109077 -0.04009014837146752 -0.05027423814614759; 0.009574262662075471 -0.000991126807187436 -0.01711381832721187; 0.036868814540425524 -0.005149507476513944 -0.10265072059283543; 0.03075149259985205 -0.006832631429025095 -0.11644858404134903; 0.03043954058561008 -0.009534487799368763 -0.14032193223460604; 0.026219380697557866 -0.010576756092700968 -0.13935089026297887; 0.01958492029131017 -0.009563523248733274 -0.1160377362577025; 0.015512612763672096 -0.008669559567355233 -0.09917612984283512; 0.004965127566836701 -0.0029199760354236166 -0.03527580847215122; 0.00206698892475886 -0.0024647847209167476 -0.017026888387383175; 0.0015039130267242159 -0.0009836933398653786 -0.011168607642974495; -8.851930693336475e-5 -0.0001245330261735087 -0.0002768938044018967; -9.24744995206984e-7 0.00013161262630103125 0.00044576251886659535; -0.00026423772480041886 0.0002436532688909268 0.0002654025989467189; 0.00014575957224746412 -0.00011548829153155214 0.0009498935322562011; 0.00017689461922216216 7.245824518885821e-6 -0.0009687019142762384; 2.9576128907687655e-5 -1.907635412563396e-5 -0.000158184494554514; -0.0016118952457104337 0.00047987026234048096 -0.001209179327397359; 0.000571602810448801 -0.0008879574651431329 -0.001650433744800023; 5.30377745172562e-5 -0.001110688634204195 0.001966442590807826] %
+
+Mass Used: 70.61056709262857 kg
+Launch C3: 102.87635964974376 km²/s²
+||V∞_in||: 0.00035859304644333956 km/s
diff --git a/archive/ES_0.5750160306690814 b/archive/ES_0.5750160306690814
new file mode 100644
index 0000000..60ac6d1
--- /dev/null
+++ b/archive/ES_0.5750160306690814
@@ -0,0 +1,22 @@
+archive/ES_0.5750160306690814---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T22:04:09.154
+Launch V∞: [7.129964571165351, -6.748355105603919, -0.31178786803294356] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.4745561907078346e-6, 6.704733816105358e-6, 3.3256324165524762e-6] km/s
+ V∞_out: [5.617670572245845e-6, -4.6845326819169065e-6, -2.927909598452205e-6] km/s
+ time of flight: 1.5342973067963418e8 seconds
+ arrival date: 2029-03-20T17:26:19.154
+ thrust profile: [0.46005180469598556 -0.1307146870608469 -0.19657056423446356; 0.06635629570705809 0.011517683360613176 -0.08517270753126377; 0.08085814271847555 0.029648240793042784 -0.16765014109386023; 0.08019718787512295 0.038272128585929925 -0.22711936370911223; 0.050505884916109973 0.027697469394708057 -0.18303309099981888; 0.031023543987508333 0.018542107589228043 -0.13774717962483188; 0.014666755578221852 0.008787572720363878 -0.07532241939044777; 0.0117836954083668 0.007088623635860614 -0.06764827064192373; 0.016976963981238536 0.010920580640837958 -0.10432977021176008; 0.004640073561213238 0.0009745938251604676 -0.022224921496157807; -0.0031973062579330686 -0.00018623535105023818 -0.004751693389101949; -0.0060615979208520345 0.0012108051944196832 -0.004287557038759557; -0.010066024168392296 0.004578572459379557 -0.0013630722955486722; -0.0042355005063664675 0.002806192898938471 0.002805260339380728; 0.0015176200776085436 0.0006534863533856934 -0.0018141123155438693; 0.008708425054330608 0.003732412750105942 -0.005857694320071073; 0.0069705767925096526 6.057108318400015e-5 0.0021452133103424848; -0.009045486783579656 -0.011479353522552528 0.0049616877323685775; 0.002819751141729535 0.002817135268884838 0.015367934389247731; -0.009890021897861931 -0.01159065418441475 -0.011712594716055746] %
+
+Mass Used: 108.08760107693433 kg
+Launch C3: 96.4739030920561 km²/s²
+||V∞_in||: 7.88268449551432e-6 km/s
diff --git a/archive/ES_0.5750234213372578 b/archive/ES_0.5750234213372578
new file mode 100644
index 0000000..8d1e163
--- /dev/null
+++ b/archive/ES_0.5750234213372578
@@ -0,0 +1,22 @@
+archive/ES_0.5750234213372578---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T17:57:35.282
+Launch V∞: [6.26503015137804, -7.080899325124621, 0.13822531193694554] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008564878430175379, -0.005894530814304192, 0.0078501904306228] km/s
+ V∞_out: [-0.006777760122049037, -0.0056662400675964635, -0.0043496416114214] km/s
+ time of flight: 1.874957778748581e8 seconds
+ arrival date: 2029-03-31T20:07:12.282
+ thrust profile: [0.8516714486604773 -0.24628632538129017 -0.1409315208065055; 0.1051117889518573 0.04483048393731375 -0.0678997276479419; 0.07230450092027084 0.057149159955598605 -0.07887443687664682; 0.18696925364503403 0.17889761069269006 -0.22299049663553694; 0.09340673260290408 0.1240817227441972 -0.16863503648247954; 0.04067227327690353 0.06683077512945958 -0.09958363358265308; 0.022625776910323494 0.043359585979491355 -0.06733909528881406; 0.007100974169252233 0.01585127648072054 -0.02744132776805638; 0.0038835228778606396 0.0111431634856559 -0.019205841707395137; 0.0017950089711765498 0.004166235339914848 -0.007498316221742615; -0.00025828845959963224 3.279294571824408e-5 -0.00010553008460196882; 0.00021213050219387344 -0.00011700440190626243 2.8111455492526572e-5; -0.00031999550798912586 -0.00015236037902296195 0.00014448501963005802; -0.0004419093119511482 0.00011669217933128675 -0.0002471779318786399; -0.00010953669194195361 -0.00024712997307524664 0.0001249617551008957; -0.00024818327582369924 0.00026645012602407914 -1.2705568925847549e-5; 0.00017629489553273896 0.000412680920604894 3.5495172542788947e-6; 3.967927693375178e-5 9.810855971210459e-5 -0.00022399555360153077; 0.0003341604603509478 0.00017092780964049722 -0.0003587357194718263; -2.589155463525672e-5 4.1247106047368146e-5 -0.00013932278263844444] %
+
+Mass Used: 149.3090665521304 kg
+Launch C3: 89.40884428708634 km²/s²
+||V∞_in||: 0.0098541643350951 km/s
diff --git a/archive/ES_0.575053396856545 b/archive/ES_0.575053396856545
new file mode 100644
index 0000000..b9db06c
--- /dev/null
+++ b/archive/ES_0.575053396856545
@@ -0,0 +1,22 @@
+archive/ES_0.575053396856545---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T21:20:40.816
+Launch V∞: [5.835621085301403, -7.984012670734305, -0.23489909999261324] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.933627761695745e-5, -9.983340066960207e-5, 2.049517016969981e-6] km/s
+ V∞_out: [2.1222133006751193e-5, -5.176250755127242e-7, -0.0001257679682530597] km/s
+ time of flight: 1.555086919798775e8 seconds
+ arrival date: 2028-03-27T18:12:11.816
+ thrust profile: [0.19261729176299483 -0.09459715249433953 -0.08192415799994342; 0.13184648819527967 0.006297478653232698 -0.14007105843371362; 0.1146408932135237 0.03115063515138118 -0.1917554488353693; 0.09222115495036058 0.03782537978979189 -0.2081415068606982; 0.07381256580164698 0.038182379460452005 -0.20571480503798156; 0.05231838194761278 0.03099092574584328 -0.17225938158845044; 0.03633655342039071 0.02375425716483745 -0.13714527854546793; 0.019986827049124942 0.014273867425214838 -0.08509798184129914; 0.005495933262350842 0.004693003731784002 -0.027591337529267696; 0.003223429672934183 0.0019477520294453301 -0.009104494932329803; 0.0019773680607697713 0.0019087757380345533 -0.014217863981949427; -0.00011522276944623625 -0.001736976915548258 0.004343780986784455; 0.000831025705765177 -0.00010773971980061097 0.0002578977532520718; 0.004183296759642966 -0.0005274574032478967 0.0005063535583554359; -0.004058821726316576 0.0037579163195897583 -0.0011360112666035805; 0.003928610443597257 -0.001615951663720324 -0.0018711148075447608; 0.00085281338540442 -0.006654766747009105 0.0037603543610510463; 0.0028911578896772044 -0.011186408127134971 0.0006116408935789787; 0.0035365856553074984 0.0020556488904455036 -0.0005484319863564357; -0.0014257700251329246 -0.003908010952432405 -0.0014503301255332018] %
+
+Mass Used: 100.07999170441644 kg
+Launch C3: 97.85410936483761 km²/s²
+||V∞_in||: 0.00012753491033977752 km/s
diff --git a/archive/ES_0.5750782899471119 b/archive/ES_0.5750782899471119
new file mode 100644
index 0000000..779063e
--- /dev/null
+++ b/archive/ES_0.5750782899471119
@@ -0,0 +1,22 @@
+archive/ES_0.5750782899471119---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T05:06:59.227
+Launch V∞: [7.896647320013671, -5.80982421471794, 0.07636853936831597] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9634585067778925e-8, -2.851438850110954e-7, 4.75014456211544e-8] km/s
+ V∞_out: [-4.385722073516104e-8, 1.6901295531027886e-7, 2.3282356759227e-7] km/s
+ time of flight: 1.8166143638258004e8 seconds
+ arrival date: 2030-02-12T18:37:35.227
+ thrust profile: [0.34852435074755833 -0.007398245569614951 -0.1120106022319188; 0.098799330290049 0.055102438505709485 -0.11096338904303192; 0.04293062571761016 0.03992722039081983 -0.08909396280363781; 0.030385930253594633 0.03766877090019772 -0.09379926407663279; 0.026050032784164796 0.039307343458040774 -0.106231720284235; 0.02036018321106558 0.03627543086418118 -0.10399646186922526; 0.023609488253762315 0.05016171352941503 -0.15359462413066005; 0.0058324718170537325 0.015750588693384707 -0.05456217007517488; 0.008383153622640608 0.021491455066713967 -0.07404592525389408; 0.0010906277824052337 -0.0004454590769454323 -0.005745932033730177; 0.0002989638937209209 -0.008874438578762902 -0.005669585183994031; -0.008508301600873774 0.003544864954817361 0.0027852535916433577; 0.0029553667093857737 -0.011266440225439982 0.006989203843757818; -0.005324317835681935 -0.014401645178627279 0.016462547820210234; 0.02334704476446995 0.0163077579400831 0.03597424696596237; -0.006837319664585734 -0.00620009014416092 -0.00200040234970943; -0.009620834672729756 -0.0010482614150407715 -0.0016206782342492597; 0.005076737434846611 0.011861810211742423 0.011340994403034434; -0.05419506906939138 -0.04064528802099114 -0.006899783117095585; -0.009540455479000514 -0.04036010926737608 0.025158144533556415] %
+
+Mass Used: 110.2425889425881 kg
+Launch C3: 96.11692845640727 km²/s²
+||V∞_in||: 2.905884222185387e-7 km/s
diff --git a/archive/ES_0.5751340844048769 b/archive/ES_0.5751340844048769
new file mode 100644
index 0000000..8685894
--- /dev/null
+++ b/archive/ES_0.5751340844048769
@@ -0,0 +1,22 @@
+archive/ES_0.5751340844048769---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:39:45.833
+Launch V∞: [5.422539121145044, -7.903001535247494, 0.018814053881435477] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3900419763459898e-7, -2.6906443833917953e-7, -1.5191637182458103e-7] km/s
+ V∞_out: [8.646282975137143e-8, -1.719599833411905e-7, 2.687540952198477e-7] km/s
+ time of flight: 1.83222696301613e8 seconds
+ arrival date: 2029-02-19T05:51:21.833
+ thrust profile: [0.505938535574731 -0.09830074810424044 -0.12664162652462468; 0.33554467181560355 0.12497186019901024 -0.230455869964617; 0.195916884853576 0.13569523122650043 -0.23214380716713237; 0.10468660900769405 0.09889545316990095 -0.17691926225393942; 0.03496674639915369 0.04129935983375433 -0.08506242362434112; 0.017131114340060167 0.02281858845523952 -0.050717472540479286; 0.010929087546538981 0.015415191055542617 -0.03571372221909369; 0.006627695117264447 0.009401637520409305 -0.024023569497469366; 0.004226652894386773 0.008672765410179886 -0.023934979013185767; -0.001278937895794626 0.0018899776865034506 -0.0028235348910376616; 0.0005205588604474309 0.0002705521630353301 -0.0035917473585554828; 0.0005174352008131971 5.2908370382881e-5 -0.002125313636526407; 0.001965821609154711 0.0014031292951045544 -0.005493415353891463; -0.0005593120013107418 0.006730929900240627 -0.006734777392671741; 0.003023539831554943 -0.001438820973042086 -0.004665828375721413; -8.784352067913205e-5 0.006799736880377871 0.0074690725646143425; 0.00011313319942578016 0.0008579923381619795 0.0013272059948403435; 0.004360894560955944 -0.004092585971232179 0.01156815594164464; -0.0071099457065589905 -0.01134214271297718 -0.0035852550903175805; 0.003939225013329245 0.0007737336379845492 0.013038083911149065] %
+
+Mass Used: 135.12974490096212 kg
+Launch C3: 91.86171775509617 km²/s²
+||V∞_in||: 3.388162082415202e-7 km/s
diff --git a/archive/ES_0.5751530944873893 b/archive/ES_0.5751530944873893
new file mode 100644
index 0000000..6acf75d
--- /dev/null
+++ b/archive/ES_0.5751530944873893
@@ -0,0 +1,22 @@
+archive/ES_0.5751530944873893---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T14:29:32.807
+Launch V∞: [5.759669582369468, -7.471731741366125, 0.22527908885613804] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.427837996777404e-8, 3.4548746163725935e-8, 4.644318806302349e-8] km/s
+ V∞_out: [-3.617483256581687e-8, 4.137900167392568e-8, -5.416824532354477e-8] km/s
+ time of flight: 1.6579986611791927e8 seconds
+ arrival date: 2028-07-21T14:00:38.807
+ thrust profile: [0.9303174269823307 -0.3752511059396886 -0.2747400060714442; 0.23733696478592659 0.0405836183375866 -0.19895133503287288; 0.11184705334160451 0.04992117643731998 -0.15528815278082264; 0.06922500212367072 0.04449878473828075 -0.13318603923727187; 0.072327455638039 0.05720916803546247 -0.17151488398127443; 0.0272817614074327 0.025842242004978953 -0.08327686937062016; 0.025436804304727053 0.02676291342776173 -0.08657970659609214; 0.02181466604503596 0.0254384598076273 -0.08438624248537323; 0.00929373634462522 0.013542092386985933 -0.04220837264213243; 0.0021461588478471267 0.0023451358972685827 -0.009330083554463988; -0.0017560789341614104 0.0018552079545662709 -0.003546461212919711; 0.002816122954535892 0.0038630198994095673 -0.015174846220513027; 0.0008204362073031325 0.0020075411990481346 -0.004964031848003765; 0.00273940952326064 3.996897111178911e-5 -0.005741895937738908; 0.0016567979071292964 -0.0010504328309785585 -0.0031023902027019785; 0.0011892905366442186 -0.0004974370940104831 -0.005459339591770054; 0.0023648396322256808 -0.002198525085248879 -0.004363328020722413; 0.0016111325683817296 0.000501883448907358 -0.00016652340852433807; 8.678383832861399e-5 0.004957072066872362 -0.00566396180773928; -0.0008814454945148167 -0.004059654419732144 0.005038520733336179] %
+
+Mass Used: 151.54591268011927 kg
+Launch C3: 89.05131958088599 km²/s²
+||V∞_in||: 7.935192569099372e-8 km/s
diff --git a/archive/ES_0.5751844522094671 b/archive/ES_0.5751844522094671
new file mode 100644
index 0000000..24e1e68
--- /dev/null
+++ b/archive/ES_0.5751844522094671
@@ -0,0 +1,22 @@
+archive/ES_0.5751844522094671---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T04:31:17.421
+Launch V∞: [5.970006573003863, -7.165105671898391, 0.1132005893776465] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002286739275103845, -0.0010778079453204455, 0.002674125543317564] km/s
+ V∞_out: [-0.0023963599754841507, -0.0009549269746683066, -0.0026198588882764516] km/s
+ time of flight: 1.8749577787362733e8 seconds
+ arrival date: 2029-04-02T06:40:54.421
+ thrust profile: [0.9154639745182893 -0.20056948599788477 -0.1881236877905048; 0.31445180313585824 0.1251729246776085 -0.20014739221783226; 0.1483601847802855 0.1103653431571205 -0.162442463855743; 0.05564095947691311 0.058379906895951586 -0.09366286169350962; 0.03943837461250544 0.05262916146934099 -0.08801698286528058; 0.026650629116087694 0.04281627520459762 -0.0766333873239804; 0.011787426549198957 0.023942572658807306 -0.043453968361923286; 0.007478023425610433 0.016640363199077895 -0.03265699716828959; 0.008129844684949275 0.02302099116800135 -0.04818001168121185; 0.0027277565927424836 0.007000703628980189 -0.014827354068201628; 0.0026750564274358028 0.014285705085773528 -0.021503768449968246; -0.001813350776219551 0.002865381743249096 -0.006580049269790662; 2.9310603337300532e-6 -0.0009062672258659693 0.0019713230793419415; -0.002736432905698254 0.006302904575370808 -0.004620430114356047; 0.003937268993367268 0.003985976358072825 -0.007382249333873014; 0.002286964583677149 0.0014915522730111538 -0.0082910448907927; 0.008037796078184976 0.0048451191583502775 -0.01725494901238811; -0.0015695472333188752 0.007265668124787299 0.004990096332906653; -0.003612093115190144 0.006376311910065807 0.0013509493632928543; 0.003003656825321364 -0.011317830285412533 0.007465155207085069] %
+
+Mass Used: 163.59209006745596 kg
+Launch C3: 86.99253214461527 km²/s²
+||V∞_in||: 0.003679917648633159 km/s
diff --git a/archive/ES_0.5752042686167727 b/archive/ES_0.5752042686167727
new file mode 100644
index 0000000..d3df7b5
--- /dev/null
+++ b/archive/ES_0.5752042686167727
@@ -0,0 +1,22 @@
+archive/ES_0.5752042686167727---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T20:12:17.005
+Launch V∞: [6.623883178111613, -6.9707134888215965, 0.425806770558584] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006877840066095343, -0.003245288420981816, 0.00814361144151899] km/s
+ V∞_out: [-0.00719112798547988, -0.0028055355103164654, -0.008026936550664318] km/s
+ time of flight: 1.874957778747514e8 seconds
+ arrival date: 2029-03-31T22:21:54.005
+ thrust profile: [0.7013447543884876 -0.16606005024326578 -0.1673472589928924; 0.1899225832739002 0.07076923399568229 -0.14479508082940623; 0.11813925796057304 0.08368051201053026 -0.15386858095682188; 0.07236183030679841 0.07133662893277798 -0.13649289292971067; 0.045075466090944385 0.05609673469166569 -0.11407147732521589; 0.017232355714547554 0.02641876006877499 -0.060826602108074126; 0.011939416819814976 0.02218117106218021 -0.05049841882452981; 0.007955612869042599 0.01597374243457951 -0.03840740057160272; 0.007124916065116028 0.013980650868647962 -0.035932746118486625; 0.00035733663920756246 0.0011211377981279534 -0.002961059776098372; 0.001356771508072294 0.0036158657493423115 -0.009159374724187638; 0.00150498323974994 0.0045119766048875715 -0.012387004098362693; -0.0001920089881650816 -0.00020478803871079197 -0.0005882096576721113; 0.0001690622588280001 0.0006271932519299286 -0.001788575893447401; -0.0010470666931908647 -0.00034512121050687494 0.0003707117504263509; -0.0007535127125012015 0.0007450422237326182 0.00031442853523737813; -0.0013549846463368816 0.00019987016326720758 0.0006166042318949171; -4.2869806479339134e-5 -6.468236203512798e-5 -4.098205181397169e-6; 0.0006642752269613976 -0.001276579760235391 0.002404291698490199; -0.0017941228370437357 0.0012842690738746486 2.024908213112299e-5] %
+
+Mass Used: 130.62505993245122 kg
+Launch C3: 92.6479863063629 km²/s²
+||V∞_in||: 0.011142485728982741 km/s
diff --git a/archive/ES_0.5752430899606068 b/archive/ES_0.5752430899606068
new file mode 100644
index 0000000..91ccfdc
--- /dev/null
+++ b/archive/ES_0.5752430899606068
@@ -0,0 +1,22 @@
+archive/ES_0.5752430899606068---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T23:28:36.129
+Launch V∞: [6.015956747368796, -7.74304427623976, 0.07769933624539312] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.196055543834818e-5, 0.00010307648297708873, -1.7655628715530333e-6] km/s
+ V∞_out: [-2.4683226726294644e-5, 5.806211375813554e-7, 0.00012941959671484678] km/s
+ time of flight: 1.6112986873431975e8 seconds
+ arrival date: 2028-05-31T21:46:24.129
+ thrust profile: [0.4092750162500229 -0.20350143818645358 -0.1642657488936693; 0.06731348739245824 0.002962276377806193 -0.0801396299254869; 0.06667290302828398 0.01520427185195207 -0.13263640903740803; 0.06309660268975928 0.023126125926591145 -0.17423563966736125; 0.0658040004013002 0.03154531399100115 -0.2096016164790691; 0.0356683076126365 0.018517261757036184 -0.14019628460289857; 0.02637502426643133 0.01687182662480257 -0.11115382085045855; 0.01892271803692925 0.013219322089764843 -0.08806536686336044; 0.014305675060264578 0.011293040277054694 -0.07307760657300355; 0.009633163913637813 0.008415891431049797 -0.053162235180107764; 0.003322938711165507 0.002735757062078809 -0.017762508598583297; 0.002724940807236233 -0.002986743508667246 -0.0007512207266913342; -0.0007809157749127521 -0.004416708981156297 0.0031231801541010684; -0.0045342002855764596 -0.0029110173680432596 0.006394862785729165; 0.0004587470025138107 0.0015333880075548588 -0.003763937127720383; -0.0014811602220970832 -0.0008453721639593117 0.0007650918332191897; -0.010909657547562221 -0.004108190758082112 0.0019194303947913608; 0.0004395031218456225 0.002709549914939098 -0.014820277487577105; 0.00021026349014508926 -2.288653476618615e-5 -0.0012880995249484628; -0.0009493900659816152 0.015522021462244327 -0.006759311260656752] %
+
+Mass Used: 110.22731157227372 kg
+Launch C3: 96.15250743687443 km²/s²
+||V∞_in||: 0.00013170197873586416 km/s
diff --git a/archive/ES_0.575325970478781 b/archive/ES_0.575325970478781
new file mode 100644
index 0000000..421b24c
--- /dev/null
+++ b/archive/ES_0.575325970478781
@@ -0,0 +1,22 @@
+archive/ES_0.575325970478781---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T19:29:04.302
+Launch V∞: [6.233569774926571, -7.730101569676359, -0.06350102712694894] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.023765723930705064, -0.010773879488309318, 0.026216696600652574] km/s
+ V∞_out: [-0.025097673890855397, -0.010601045658224648, -0.025015342613186796] km/s
+ time of flight: 1.743016224158989e8 seconds
+ arrival date: 2028-11-06T04:36:06.302
+ thrust profile: [0.1508727165113715 -0.05906085779153766 -0.06345780737537454; 0.07030668799947701 0.005898731057097639 -0.08137939516364409; 0.06917247905594506 0.018709813015793476 -0.13571279469735195; 0.06530184964305896 0.024869706436137704 -0.1783035309839268; 0.04936253871024886 0.022140028473183523 -0.16918962202768514; 0.03153697220936531 0.015473226931116081 -0.1270898182790034; 0.01696680291035752 0.008882769761386489 -0.07536684590197829; 0.008431736067192334 0.004547480386613719 -0.03965251548321464; 0.004924765217656806 0.002777245347310123 -0.02482876488302766; 0.002966742657211257 0.0018670692329544117 -0.01814493592736071; 0.0032319013393996613 0.0007577076535241634 -0.01825973223954839; 0.009480452080619413 0.0016223376353221499 -0.02466033105194161; -0.0005522824571385391 -0.0017342864169697242 -0.008176417110361794; -0.0030484327705379392 0.0065110746002440475 -0.029254623398504237; -0.023703560001809107 0.013224090402360028 -0.015471277799070707; -0.013836594820608552 0.00441240864345863 -0.038530994312776914; 0.004899490580835665 -0.024748381110692615 -0.021322647108900198; 0.0008801856861394937 0.00031479398788812835 -0.0064103316094657765; 0.003360326434777877 0.0010620176473305873 -0.04571182422763911; -0.03832030160355387 -0.004616535378604194 -0.017890729097079245] %
+
+Mass Used: 95.9542459103609 kg
+Launch C3: 98.61589479683718 km²/s²
+||V∞_in||: 0.03698920509864693 km/s
diff --git a/archive/ES_0.5753319880541651 b/archive/ES_0.5753319880541651
new file mode 100644
index 0000000..d71cbae
--- /dev/null
+++ b/archive/ES_0.5753319880541651
@@ -0,0 +1,22 @@
+archive/ES_0.5753319880541651---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T22:25:21.028
+Launch V∞: [6.582132433570003, -7.314840858990533, -0.44020138609910664] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.204208457127033e-10, -2.1538720145525144e-9, 1.0463798040714123e-9] km/s
+ V∞_out: [9.271048874379761e-10, -2.1016342775152706e-9, -2.9720384891807584e-9] km/s
+ time of flight: 1.786030995586954e8 seconds
+ arrival date: 2028-12-20T02:23:40.028
+ thrust profile: [0.3027138470593493 -0.09155915350001108 -0.09835576575666984; 0.12968222431898796 0.03602345951072719 -0.12024521327322797; 0.09869099728018124 0.05664840274262599 -0.1508684948832736; 0.07958076433433832 0.0632200356146017 -0.16613566863859425; 0.04318337115685187 0.04261731505599357 -0.11907011172397919; 0.04586537690286007 0.05374155305485526 -0.15422542121349483; 0.03012563053146944 0.03992610131062505 -0.11766888756177886; 0.011324267523578077 0.01665755076457186 -0.05232588402573479; 0.005983795644942825 0.009944292339356887 -0.03332642069888772; 0.0014964741663222516 -0.0007385687975369177 -0.0026336200352154553; 0.0014908102169003507 0.0027290758747633673 -0.010205544324914693; 0.0004754777447581411 0.0007801593680889826 -0.0030438081702508363; 0.0005913053177243592 -0.0005941163078284503 -0.0020737735733393587; 0.0002933842859578286 -0.001011439289609979 0.002533249697987486; 0.005482296974174055 0.0026281270005955267 -0.0012511050983479376; 0.0018592952183667936 0.0007736069646551869 0.005181643171430265; 0.006440504312055994 0.005573387076154001 0.0013915615610802046; 0.003999741403985065 0.0072388666857334805 0.0029215897341298815; -0.004239263921242205 -0.006396372895498273 -0.0074003753776278845; 6.445562001748277e-5 3.357802932588979e-5 0.00010227381935072415] %
+
+Mass Used: 105.24066107973795 kg
+Launch C3: 97.02514142573509 km²/s²
+||V∞_in||: 2.500616232927084e-9 km/s
diff --git a/archive/ES_0.5753334105176193 b/archive/ES_0.5753334105176193
new file mode 100644
index 0000000..59f1c56
--- /dev/null
+++ b/archive/ES_0.5753334105176193
@@ -0,0 +1,22 @@
+archive/ES_0.5753334105176193---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T03:03:28.114
+Launch V∞: [5.488146115766073, -7.955492068642709, -0.1249685212692913] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002800097715962548, 0.0021093501935148073, 0.00229704066082998] km/s
+ V∞_out: [-0.00182259773490711, -0.003207351370357251, 0.0019844241727240727] km/s
+ time of flight: 1.5709589605593362e8 seconds
+ arrival date: 2028-04-15T08:48:24.114
+ thrust profile: [0.5115140316270539 -0.2326502933472832 -0.17996554858400649; 0.21356095129511918 0.020880880800692107 -0.1977454178039754; 0.11333576885830272 0.037035779416297196 -0.16546417418009396; 0.11334227866935011 0.055235515685690795 -0.22043040958045915; 0.03780832075441673 0.02197088100286939 -0.09260622904116966; 0.02924162319186644 0.02025239049352596 -0.08580861192363172; 0.04218938876044574 0.032858889117594894 -0.14033075443148108; 0.03580002416005779 0.030056507506677117 -0.13178164423780653; 0.004560705601874862 0.007039540095817228 -0.03073053140881269; 0.006634705984338582 0.004323622815730104 -0.02713247822260091; 0.02115378861004385 0.011014157356222944 -0.0362029761415467; 0.00014714445951889048 0.0012492260593929287 -0.00635160645363147; 0.0005649231337182506 0.005708638933257125 -0.010803554352752213; -0.0001372029995135738 -0.005080095453910863 -0.009128437202005547; -0.00014241887368966234 0.003000861323860039 -0.008917902005716887; -0.006965299461436416 0.0082828935840794 -0.008658826445287645; 0.002336163614207247 -0.005634008175174475 -0.009493131905125615; -0.0009484719818023965 0.00106219634286002 -0.001778738033619237; -0.0002474930439985701 0.006884947480006204 -0.0009705242146943044; -0.009550318055298265 -0.012317121995469693 0.005890070661440885] %
+
+Mass Used: 126.2418682582188 kg
+Launch C3: 93.42521897354351 km²/s²
+||V∞_in||: 0.004191217156784634 km/s
diff --git a/archive/ES_0.5753426594162286 b/archive/ES_0.5753426594162286
new file mode 100644
index 0000000..7ad5963
--- /dev/null
+++ b/archive/ES_0.5753426594162286
@@ -0,0 +1,22 @@
+archive/ES_0.5753426594162286---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T09:17:32.677
+Launch V∞: [7.529001137648108, -6.422624624532729, -0.2319188610515271] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.940203920617252e-6, 0.00040015718593821404, -1.4945220520186953e-6] km/s
+ V∞_out: [0.0004557060131655991, -7.257066529354697e-5, 8.653023552569934e-5] km/s
+ time of flight: 1.613739112476372e8 seconds
+ arrival date: 2029-06-20T03:22:43.677
+ thrust profile: [0.2318411227427538 -0.04797453034414613 -0.09293365077671925; 0.05194314326966607 0.012433604204092806 -0.06356664780559498; 0.06697235122926169 0.034009066835248396 -0.13447068813710622; 0.05917156676785962 0.03909582301249712 -0.16671880284175833; 0.047519893743958846 0.0356967508462257 -0.1660955371859162; 0.057727395758417184 0.0504170723736108 -0.23131806803457972; 0.0253318964813347 0.020921749140419933 -0.11363051542017294; 0.006516123319210725 0.010327998823235526 -0.0510942133809666; 0.005348709200033718 0.004055792135799632 -0.026378567538868036; 0.002516986379874451 -0.006559406586336669 -0.029915567198575306; 0.006245456273188147 0.02006509353570747 -0.02200841418379345; 0.0029781291039270743 0.013557979379544437 -0.011117409603850773; 0.007885987381948996 0.005962987582695176 0.0013037931119146205; 0.01089133748144665 -0.0018936129793184647 -0.016945669166769966; 0.0019247307659031629 -0.0012655787196424865 -0.001990302241338894; -0.00014411247940605615 -0.0005019558908256907 0.0013145375772627272; 0.0047401679845498245 0.004177013853054518 -0.000954505249782614; -0.0008559122277131658 0.008455179745259582 -0.0010930240187879314; 0.031043890968269015 0.04898387373762733 0.10473363643090192; -0.007974058806373325 0.008152616332657743 -0.0008544074094576725] %
+
+Mass Used: 99.62621857284603 kg
+Launch C3: 97.98975155647213 km²/s²
+||V∞_in||: 0.00040020406429317146 km/s
diff --git a/archive/ES_0.5753955043319445 b/archive/ES_0.5753955043319445
new file mode 100644
index 0000000..6a87ff1
--- /dev/null
+++ b/archive/ES_0.5753955043319445
@@ -0,0 +1,22 @@
+archive/ES_0.5753955043319445---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T14:44:13.801
+Launch V∞: [5.5497560993196435, -8.005890507814351, -0.23477580659900787] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004705801267314652, 0.005183277839672494, -8.143831504918219e-5] km/s
+ V∞_out: [-0.0015369711244696746, 3.2741167375430705e-5, 0.0068329885342770375] km/s
+ time of flight: 1.524255417039857e8 seconds
+ arrival date: 2028-02-20T19:09:54.801
+ thrust profile: [0.48166737198442033 -0.24328289404778322 -0.1996252492329819; 0.09961320940845951 0.0033714140946240205 -0.10632147056509143; 0.1435009330045012 0.03697828450261965 -0.23414158602856663; 0.10610230516441689 0.04226566062096977 -0.23263855243601922; 0.06073189430254869 0.030421374513516394 -0.16675775052610645; 0.023643811058749853 0.013802709642974111 -0.07913822282268874; 0.03972727195308516 0.027037943022339896 -0.14737595901781517; 0.027514349996634047 0.02049952526791246 -0.11369638572673796; 0.01891876296690165 0.013972483144214442 -0.08618546946836324; 0.0013236658422903736 0.0008500079634413409 -0.007844977418970533; 0.0006278634644688549 0.0012461979819652247 -0.008615121306850557; 0.0003562452980078434 -0.0009682967191165688 0.00028806218479390105; 0.0007584131051677637 0.0001714154866444796 -0.0025127021687205565; 8.038453326201264e-5 1.96818445715812e-5 -0.0009502490780333983; 0.00041428955660592994 0.003216674696341375 -0.00016248281924096162; -0.0018429074674104074 -0.003974399049986418 0.0033446945883726727; -0.004356648917758558 0.0045691569317173695 -0.0011614297892670454; 0.003899025889787938 0.00048077860519193103 0.0005525184676532886; -0.0034789137114729423 0.00020787952501253747 -0.0051096744068304355; -0.0009723103516772564 -0.0035676056476907003 0.0002140195280628984] %
+
+Mass Used: 117.42444934486684 kg
+Launch C3: 94.94919526441173 km²/s²
+||V∞_in||: 0.007001254668261838 km/s
diff --git a/archive/ES_0.5754640924969509 b/archive/ES_0.5754640924969509
new file mode 100644
index 0000000..abb7eac
--- /dev/null
+++ b/archive/ES_0.5754640924969509
@@ -0,0 +1,22 @@
+archive/ES_0.5754640924969509---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-21T09:20:38.275
+Launch V∞: [7.654344001132721, -6.514148589356465, -0.5575783359964025] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.015904352242340294, 0.10055947621689451, 0.1293818132809185] km/s
+ V∞_out: [-0.06625448578375032, 0.057482781386862546, -0.13954735370110063] km/s
+ time of flight: 1.8030112085368806e8 seconds
+ arrival date: 2030-02-06T04:59:18.275
+ thrust profile: [0.332325713522976 -0.06781117562922089 -0.15819681514518238; 0.00855165549959695 0.0006740002780898665 -0.014146101385739494; 0.017380613978450928 0.001079456999061276 -0.04951480167209265; 0.028744206494844358 -0.0019323520431573133 -0.10858286021729206; 0.02447866935109148 -0.00320116032974166 -0.11814674374051101; 0.016661039765587436 -0.0029166767835653693 -0.0924973697851492; 0.02535492506079703 -0.007353815774309788 -0.15167351011758384; 0.0092904979289701 -0.0035979307470001 -0.05884161968660771; 0.006270330576084987 -0.003420320284347272 -0.046717392080528816; 0.003659203601946646 -0.0009945378705541398 -0.025343036329874235; 0.0035201225262490613 -0.0016927131622608105 -0.024176400416023824; 0.0014311440880690443 -0.001280826952819103 -0.008398863353848547; 0.0005513077460554385 -0.00036782721732090464 -0.004023975201900506; 0.00320025284872848 0.001477167773805557 -0.0034753351519711323; 0.0027901013622777136 0.002886287085012919 -0.0008128334671159681; 0.0003264552367561798 -0.0025904678359827127 0.002230171252001096; -0.0014506607564353877 0.0009357701075422995 -0.0024299474563202433; 0.004516486856963774 -0.0004121925877167125 -0.0019890224221312345; 0.000735051505815933 0.00024122473874925963 -0.0008618718106678212; 0.00046365774555305974 -0.0007625017499557122 -0.0021061998991808864] %
+
+Mass Used: 80.2597306392372 kg
+Launch C3: 101.3340075326638 km²/s²
+||V∞_in||: 0.16463538588384657 km/s
diff --git a/archive/ES_0.5755048228318185 b/archive/ES_0.5755048228318185
new file mode 100644
index 0000000..1876e8f
--- /dev/null
+++ b/archive/ES_0.5755048228318185
@@ -0,0 +1,22 @@
+archive/ES_0.5755048228318185---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T13:50:03.997
+Launch V∞: [5.558243791489472, -7.945962671558762, -0.1548977773430438] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.438201745512909e-6, 1.986862873776827e-6, -2.553494493039952e-6] km/s
+ V∞_out: [8.664544930165254e-6, -2.3328756540484284e-6, 1.048994106116797e-6] km/s
+ time of flight: 1.5233309051463127e8 seconds
+ arrival date: 2028-02-18T16:34:53.997
+ thrust profile: [0.5363401529412 -0.27187316511668863 -0.2125262142215338; 0.13804281026445547 0.0052506586394999956 -0.13901247848267792; 0.1305384111792172 0.03465201028074519 -0.2038689159701624; 0.10793458942370099 0.04411288913817546 -0.22469170740911937; 0.09662852053241325 0.04875451629905137 -0.24657797055056374; 0.06555665810804619 0.039312022957973015 -0.19715120028569494; 0.01818822397165489 0.012293931124526314 -0.06559525139890085; 0.01259937463459927 0.010081644250637048 -0.05053883860663867; 0.0048973873300070985 0.003659750992301062 -0.02133251650583937; 0.0021986573864678375 0.0033078021598018778 -0.012699102702402437; 0.0014961620194094034 0.0018954906871736365 -0.011560736672207304; 0.0007586500895626539 0.0006911766424277039 -0.003625124250158631; -0.0004708516734796593 -0.000903740896015223 0.001448884498091503; -0.0004345412106084737 -0.0003086921503441106 0.002645732075125736; 0.001269781219425272 -0.0007473120335267853 -0.0036934391808195726; -0.007804813277630172 0.0017604567348608862 -0.007276456107212953; -0.003592683559121331 -0.0024579734751883006 -0.0026534706172003236; 0.00028832808911200756 -0.0009585004270873001 -0.003019882767115836; 4.196050215971568e-5 0.001563202650738626 -0.0017981355525310376; 0.0018894428418435379 -0.0044109284603371084 -0.006922912541738985] %
+
+Mass Used: 122.76001745875783 kg
+Launch C3: 94.05639014486235 km²/s²
+||V∞_in||: 9.03721234137802e-6 km/s
diff --git a/archive/ES_0.5755064745441583 b/archive/ES_0.5755064745441583
new file mode 100644
index 0000000..64a4dd7
--- /dev/null
+++ b/archive/ES_0.5755064745441583
@@ -0,0 +1,22 @@
+archive/ES_0.5755064745441583---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T17:44:00.034
+Launch V∞: [7.632789889383906, -6.469594063924877, -0.41814865261009626] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1983230978685446e-9, -7.747299608050722e-9, -5.025125633825494e-9] km/s
+ V∞_out: [-3.87821762142259e-9, 3.2093361149681488e-9, 2.014314658303085e-9] km/s
+ time of flight: 1.874957777799855e8 seconds
+ arrival date: 2030-05-01T19:53:37.034
+ thrust profile: [0.4129737980071394 0.012856265999300556 -0.16573031709954397; 0.035210645269817105 0.01521469322009352 -0.049102843972277696; 0.02483052894162927 0.01641640389819381 -0.060673709434411034; 0.022719612415422103 0.01820037495741089 -0.08044891125479026; 0.029935334658666605 0.03024599478995793 -0.14403328787416667; 0.017144932497854107 0.017006624324834668 -0.09768680498984497; 0.010533950370820562 0.010530743832777677 -0.06645651520184517; 0.011286193750988813 0.011608264742410994 -0.0812836516591285; 0.00557550214390478 0.006032760690785981 -0.03795679043365469; 0.00064617540820556 0.0008477409924186842 -0.0052978399286904825; -0.00010847233754369447 0.0001594729922737158 -0.0022143308196076053; 0.0006820162997259386 -0.00014959850458481395 -0.0039649565474668014; 3.664662112385763e-8 0.0019113021574521153 -0.003661865560711952; 0.00017957171894073757 -0.0001512784190217224 -0.001420299379233176; -0.0005290991749705048 0.0002955372997864057 -0.00182279411681399; 0.004928066631963563 -0.003945486044002183 -0.0025484597419682484; -0.0010973682684754006 -0.00010027000754273506 -0.012265798534779318; -0.0035527769347811246 -0.0025605360968915507 -0.0018115018034840528; 0.003954864036044642 -0.002921611170328418 -0.006979236185149979; 7.530644861997399e-5 -0.0012598292070940746 -0.004271166360658132] %
+
+Mass Used: 86.39935363324321 kg
+Launch C3: 100.28997714313282 km²/s²
+||V∞_in||: 9.31174082003565e-9 km/s
diff --git a/archive/ES_0.5755872872319862 b/archive/ES_0.5755872872319862
new file mode 100644
index 0000000..99a9126
--- /dev/null
+++ b/archive/ES_0.5755872872319862
@@ -0,0 +1,22 @@
+archive/ES_0.5755872872319862---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T03:34:15.623
+Launch V∞: [5.506128472113563, -8.133222386225663, -0.441002038144791] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.139058596175405e-6, 1.4975830265876165e-6, -1.905248820241718e-6] km/s
+ V∞_out: [6.360129944892594e-6, -1.7482399244960668e-6, 2.3075884858319175e-7] km/s
+ time of flight: 1.503893110144466e8 seconds
+ arrival date: 2028-01-29T18:22:46.623
+ thrust profile: [0.3921013836791071 -0.21444619722092162 -0.18705149887703285; 0.10714228063104339 -0.002877822247326067 -0.1268383970462565; 0.07191590173141453 0.011815709879836586 -0.138441551185559; 0.07874528402261573 0.02284329605543462 -0.20238100515828875; 0.0959851153416262 0.03643044965934374 -0.29121992145121445; 0.0423369937888211 0.017459878810023526 -0.1647604483020304; 0.022055457506467355 0.009904344095686904 -0.09569917723990055; 0.016241954882029938 0.00788414651966298 -0.07862080142980929; 0.007407871398745105 0.003348404584496434 -0.03686032422568078; 0.005766640002310377 0.0029617990786914372 -0.03326355650869607; 0.003157323428335475 0.001582837528940175 -0.021622420435188392; 1.6217995871203438e-5 -0.00015646011692793985 0.000711489695558271; -3.3737342983996116e-5 -4.995017980357456e-5 -0.001048717334102777; -0.0004188491259341306 0.0013431489952160278 0.0015488978501805662; -0.00012966445816706024 0.0004823278975924236 -0.0006578918161299528; 0.0011220899466928926 -0.0004225164987255558 0.0013673659170285117; 0.0008428590476183878 0.0003741523928633715 -0.0013972493351058466; 0.0013072263123918317 -7.261815496583009e-6 0.0035073897309229976; -0.001036828117280134 0.003248256913886632 -0.003847357114503072; -0.0001115914628041348 -0.001013427320501931 0.002507394221636508] %
+
+Mass Used: 107.66126882891012 kg
+Launch C3: 96.66123993286978 km²/s²
+||V∞_in||: 6.600058214578938e-6 km/s
diff --git a/archive/ES_0.5755894810957699 b/archive/ES_0.5755894810957699
new file mode 100644
index 0000000..c41dc3b
--- /dev/null
+++ b/archive/ES_0.5755894810957699
@@ -0,0 +1,22 @@
+archive/ES_0.5755894810957699---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:01:22.556
+Launch V∞: [6.58758443858855, -7.186005192402637, 0.020695771472013912] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.97912433537216e-9, 8.02205805061684e-11, -5.966380071366559e-9] km/s
+ V∞_out: [-1.2100560149574014e-9, 2.896429091095793e-9, 3.92298537468907e-9] km/s
+ time of flight: 1.8513681030425268e8 seconds
+ arrival date: 2029-03-05T09:54:52.556
+ thrust profile: [0.3585178823716534 -0.08345508607730538 -0.08029889935538469; 0.2841577444977475 0.10286411087126157 -0.18761464939444514; 0.07270133400877282 0.052801478322174036 -0.09060245428655848; 0.11527581010152925 0.11165053434881177 -0.18601097270504927; 0.03308017743510464 0.04247830426945907 -0.0811229471857425; 0.03238973188223228 0.04841956677694196 -0.09246601733541168; 0.01904540693241984 0.029101750061433312 -0.06693866250261515; 0.024192977939689848 0.044926582080181014 -0.09269610407513275; 0.007604020745842925 0.019231214403481155 -0.0408796628576445; 0.002718382236317883 0.006559503447075841 -0.016345244136758336; 0.0015995921097812526 0.003188816805274949 -0.0071218231262681325; 0.0005060155423436321 0.00010769585767152678 0.0006877491445025834; -0.0008637808985038591 -0.00010183728241999317 0.0015087483112833223; -0.003188716808182503 -0.002685067193631853 2.541229825148004e-5; -0.002358651831686147 -0.0015489848808036182 0.0008891414901399102; -0.0004265229118343494 0.0038260696687432956 0.0023659837090820356; -0.0002269404563172179 -0.0012771120209476832 0.002786459694628194; -0.0010187645419452785 0.0010235444666985007 -0.00040356127078213975; -6.171622159426292e-5 0.0037811997344702284 -0.00019633205728649376; 0.0010860111433909749 -0.0006361949507919051 1.5072931503040698e-5] %
+
+Mass Used: 117.14808316998187 kg
+Launch C3: 95.03536767572851 km²/s²
+||V∞_in||: 9.182173108045865e-9 km/s
diff --git a/archive/ES_0.5756620490256166 b/archive/ES_0.5756620490256166
new file mode 100644
index 0000000..1d534b9
--- /dev/null
+++ b/archive/ES_0.5756620490256166
@@ -0,0 +1,22 @@
+archive/ES_0.5756620490256166---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T21:15:53.318
+Launch V∞: [7.4061688486053665, -6.5637226781950195, -0.15972038533296484] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8338241578699213e-5, 5.5854115253405795e-5, 0.000176017041034018] km/s
+ V∞_out: [0.00017024085145471402, 1.980522433402316e-5, -7.335802029655991e-5] km/s
+ time of flight: 1.5903987800182837e8 seconds
+ arrival date: 2029-05-24T15:00:31.318
+ thrust profile: [0.23785121406274132 -0.05115401097595145 -0.09682095198814013; 0.08746324487655198 0.0259926678942967 -0.10577589796611156; 0.06731723706304607 0.03602029107782385 -0.137571312746728; 0.053657860355549494 0.037688586305365965 -0.1548501451328025; 0.0401848360351083 0.033419950465232495 -0.14872415069821313; 0.030072161346148353 0.0279489155989017 -0.13556811924773102; 0.029733719898575317 0.026777922618803393 -0.14795088396166; 0.02051292821596288 0.019344735018549195 -0.12327030199365373; 0.006429816167749584 0.013309199991816546 -0.06320510807406524; 0.0006522049317013727 -0.000546597551226909 -0.0189576996320658; -0.008428868994993878 0.0010432191502030715 -0.006702807314693948; 0.014356494802508618 0.01108444940345965 -0.016118263327304358; 0.007268958470106661 0.002597495631154852 -0.022021601578140797; -0.009083035817570605 0.002182039090294659 0.007020756546457796; 0.010995600584241604 -0.007767336249811888 0.008700322305763997; -0.0022941071103955725 -0.003158411226241958 -0.01331388805351232; 0.02465363984484938 0.007185241435830671 0.018959217967928314; 0.018545930669252017 -0.017209523236747536 0.015794189175588863; 0.00031663000905395294 -7.422791551092321e-5 0.021191575189146748; -0.0057701700083086895 0.003116885256963545 -0.0061331816733224045] %
+
+Mass Used: 100.17645629441495 kg
+Launch C3: 97.95930301179504 km²/s²
+||V∞_in||: 0.00018682809441003415 km/s
diff --git a/archive/ES_0.5757872065067349 b/archive/ES_0.5757872065067349
new file mode 100644
index 0000000..a1306a3
--- /dev/null
+++ b/archive/ES_0.5757872065067349
@@ -0,0 +1,22 @@
+archive/ES_0.5757872065067349---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T14:34:59.862
+Launch V∞: [6.298001336681112, -8.001116350145644, -0.7853263859160845] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008195631255484571, 0.00492712216663243, -0.0065924536709776145] km/s
+ V∞_out: [0.0058378384769389715, 0.004678314591494063, 0.0035292759333820593] km/s
+ time of flight: 1.8516372529304942e8 seconds
+ arrival date: 2029-03-21T16:57:04.862
+ thrust profile: [0.022632381224647304 -0.009282520733528966 -0.012690585843321828; 0.026999583784162805 -0.0022386839042306678 -0.046577953592192994; 0.029660305517448502 -0.0015711418208802788 -0.09116666277823353; 0.03333227532899335 -0.003050860058434689 -0.1356005409737444; 0.028250139106126615 -0.005768475664631294 -0.13532106806011213; 0.028039506261877248 -0.006523055053423837 -0.16421020261091474; 0.012678662171140442 -0.0044429826546834895 -0.08692023471514941; 0.009013646207996035 -0.0038724188375093304 -0.06774183838948347; 0.003315729415510149 -0.0014326076888534253 -0.026865659754432444; 0.0044843332902427735 -0.002594196705245254 -0.03852138409453227; 0.0002988624055102862 -0.0002231205624905954 -0.0027448840244347827; 0.0002511054246222306 -0.0002785878063631086 -0.0013652453934980106; -0.00011104083108367548 -0.00022234376025151372 -0.0006550105847893001; -0.0003423581214628797 -5.0433379795735277e-5 -0.0006133689635159764; 0.0012025745113812564 0.00035265590500713456 9.328945307263603e-5; 8.980349234929063e-5 -0.00020957739795687285 -0.0021932824282337162; -0.0007719880321733953 0.001138126570146071 -0.001077888764048674; -0.0006043714653836472 0.00010167255527723326 1.9339862644498856e-5; 0.0004587569018624513 -0.0012462151924581182 -0.0004657923305140299; 0.0008449313848167606 -0.00047776115180875973 -0.00150201599381321] %
+
+Mass Used: 63.338450487234695 kg
+Launch C3: 104.29942121782103 km²/s²
+||V∞_in||: 0.008270952905540306 km/s
diff --git a/archive/ES_0.5758286641047434 b/archive/ES_0.5758286641047434
new file mode 100644
index 0000000..5a4c610
--- /dev/null
+++ b/archive/ES_0.5758286641047434
@@ -0,0 +1,22 @@
+archive/ES_0.5758286641047434---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T23:53:47.457
+Launch V∞: [5.533666536382321, -8.167260954878582, -0.33542652286745583] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0481294395598645e-5, -0.005029290608506781, 0.0017589423978479582] km/s
+ V∞_out: [0.004273959011324088, 0.0023631463021085044, -0.0021152904659427776] km/s
+ time of flight: 1.4992716659809908e8 seconds
+ arrival date: 2028-01-24T06:19:53.457
+ thrust profile: [0.27535092698890334 -0.15449354342717136 -0.1279010404826271; 0.11711405991164643 -0.005730823174596178 -0.13081277560969667; 0.1268344470266452 0.018544717142359234 -0.22355785852812005; 0.10629260402680743 0.027261060224062515 -0.2511058111207723; 0.09895676079248177 0.032817848225638394 -0.2883791701269195; 0.046321830847979285 0.017318218493624745 -0.15878172362115178; 0.023947431822451678 0.009696397124030042 -0.09378773754719555; 0.002131848574196477 0.004809439857596602 -0.016762364130070817; 0.0020112617898380186 0.009243801055518011 -0.021411387310330765; 0.008432407325523071 -0.005941230184451967 -0.02038539160015195; 7.955546383576735e-5 0.0005666472629514293 -0.0019427895374249371; 0.0005609839684161194 0.0005226248662549996 -0.007213920204302643; 0.0068166572977785694 0.0027001447925281267 -0.006810191348536867; 0.0016776945024546993 0.00021595018063957395 -0.006032808172103994; -0.0012066292973077263 -0.001800522623806383 0.00024121636004481172; 0.0004543627943733334 0.0008369017351976351 -0.007837825449178944; 0.001673704671686742 0.001547307416831003 -0.0008461497446772635; 0.0007216556021988028 -0.0004578052887219035 -0.0012467012971936241; 0.0004889855821658845 -0.003362676096330902 -0.008067481578218719; -0.0005921238298278969 -0.0016197391529490582 -0.00028961709335069115] %
+
+Mass Used: 103.41102932850663 kg
+Launch C3: 97.43812779320469 km²/s²
+||V∞_in||: 0.005328015788386315 km/s
diff --git a/archive/ES_0.5758358871095217 b/archive/ES_0.5758358871095217
new file mode 100644
index 0000000..4c98a5f
--- /dev/null
+++ b/archive/ES_0.5758358871095217
@@ -0,0 +1,22 @@
+archive/ES_0.5758358871095217---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T14:10:03.693
+Launch V∞: [5.46612823233304, -7.981110372881952, -0.09098892048777868] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.492185846003091e-5, 0.028266865806430647, -0.008863665805564157] km/s
+ V∞_out: [-0.023980288487928984, -0.013556317712520916, 0.011045841048908472] km/s
+ time of flight: 1.5344143522944516e8 seconds
+ arrival date: 2028-03-03T12:47:18.693
+ thrust profile: [0.5350336563334037 -0.2609606767122825 -0.2053960202852614; 0.2111956771124156 0.010657188303613143 -0.21734497148591325; 0.15099398354461938 0.042236453204959445 -0.2463347129663499; 0.08440460898184923 0.03647103031641717 -0.19140473251453544; 0.04799516251175285 0.025132580514490358 -0.136222878085366; 0.029319073201803113 0.016800480633613345 -0.09838618591105769; 0.024639624440540304 0.015409701097466758 -0.09449105089270318; 0.023517178828507533 0.0167931445958313 -0.10307145463274404; 0.00918029509498291 0.007013572799025699 -0.04463181401455357; 0.008443475562670364 0.005564562627718221 -0.039239043571630036; 0.006032339580004094 0.0067054426894304 -0.039395804980709145; 0.0002756367301138875 0.0008814337830050665 -0.001171501903459598; -0.0006479699305449863 -0.0004197350084124924 0.0016945880090839982; 0.0014796037343241621 -0.0001140211700549332 0.0018281484267693758; 0.0005677618930432166 0.0004812848420849468 -0.0035773190891916886; -0.0007872963894299703 0.00018643856572125365 0.004699189086097507; -0.00440145281891364 -0.004752047649773184 -0.00035357803294784346; 0.0008901460181273955 -0.0009542018479634167 0.007847163727512417; 0.0019400575247521578 -0.0006994384139581888 -0.002702600750903247; -0.002571849360586846 0.00487935103522048 0.005342351822105442] %
+
+Mass Used: 125.89627051062007 kg
+Launch C3: 93.58495962008377 km²/s²
+||V∞_in||: 0.029624032312330847 km/s
diff --git a/archive/ES_0.5758694299179308 b/archive/ES_0.5758694299179308
new file mode 100644
index 0000000..ccf2312
--- /dev/null
+++ b/archive/ES_0.5758694299179308
@@ -0,0 +1,22 @@
+archive/ES_0.5758694299179308---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T14:10:22.100
+Launch V∞: [5.57898723432496, -7.810216499194361, -0.19747220596287288] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002067101558130116, -0.001328717928719719, 0.001084328748594036] km/s
+ V∞_out: [-0.0013694101250303727, 0.001967254887631644, -0.0012052635829284946] km/s
+ time of flight: 1.5448436275476485e8 seconds
+ arrival date: 2028-03-12T14:29:44.100
+ thrust profile: [0.6386126021756436 -0.29957127076057194 -0.21675649760479376; 0.2719421654611398 0.027734468382890995 -0.23622460230487277; 0.137127750116451 0.048400364489684836 -0.19223689386042958; 0.11739887614691899 0.0615824000485375 -0.2194014215452772; 0.058661398286017075 0.03770216717408461 -0.13886738515461483; 0.054167740437864785 0.041192128910274746 -0.1521154871224492; 0.03584600348782758 0.03030372158498465 -0.11515435539627275; 0.01404460870305773 0.012860079278052354 -0.05145870065159662; 0.017034968297430782 0.01666874963864887 -0.0684951781786186; 0.0005290046522694134 0.000579792678721008 -0.002514003250013792; 0.0012127537301148766 0.001483616176747799 -0.005610810550203893; 0.00015141502659667315 -8.387729576160224e-5 -0.00032382582922865495; 5.8147779467530815e-5 7.46132836557153e-5 -0.0003016486438262374; -8.22674160027686e-6 -9.216303727871568e-5 -0.0004389759648893323; -6.38566304453311e-5 0.00013366933830837976 -0.00038279227148523405; 2.4709429072759937e-5 0.0003084441275706377 -0.0004051042172152988; 7.803454578048975e-5 -8.986909349161822e-5 -0.00023149196479379207; -1.1514572898358431e-5 2.565421853124427e-6 -2.704082902679479e-5; 4.097439879848272e-5 -0.0003585856902241051 -0.0005593621641372286; 3.7238604111801096e-5 5.56052730382427e-5 -5.749635384141522e-5] %
+
+Mass Used: 134.22681058738954 kg
+Launch C3: 92.16357559717653 km²/s²
+||V∞_in||: 0.0026859205164622207 km/s
diff --git a/archive/ES_0.5758901659654818 b/archive/ES_0.5758901659654818
new file mode 100644
index 0000000..936b32d
--- /dev/null
+++ b/archive/ES_0.5758901659654818
@@ -0,0 +1,22 @@
+archive/ES_0.5758901659654818---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T10:14:54.133
+Launch V∞: [6.232799139801482, -7.039924078001757, 0.40047359898414825] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.82942044553789e-7, -8.72656558203147e-8, 4.7795879513538207e-8] km/s
+ V∞_out: [-2.0604075220159417e-7, 1.9216881851600726e-8, -2.628760616324063e-8] km/s
+ time of flight: 1.8432370302254736e8 seconds
+ arrival date: 2029-02-21T19:16:37.133
+ thrust profile: [0.974522643079056 -0.2478444387823751 -0.2091072931965991; 0.2576008908906476 0.09201664596780118 -0.17883666128726114; 0.11745711862550086 0.08127991406732196 -0.14211790496948407; 0.05437762042642033 0.05228928437027827 -0.09454255876697756; 0.053077896117162536 0.06331508346798766 -0.11857120286337358; 0.033178201647841916 0.04634620725450858 -0.09097682443526221; 0.025805437359312493 0.04147434779170199 -0.08634004765804264; 0.011372691671553126 0.021174232042052415 -0.04677608036070762; 0.0016536816084119833 0.002009876891706156 -0.007686974118513099; 0.0017519068169528954 0.0021138558601613757 -0.0057714709163646915; -0.00015328099003610306 0.00020772670913893647 0.00019738430529726955; 0.001302167767784711 0.0026446288048827234 -0.00604422932929418; 0.00020980630191649765 0.0010868796486358991 -0.001973693902464947; -2.5259352548853687e-5 -0.0006308548805074976 0.0006894412840208916; -0.002060846050978774 -0.000991288573931019 8.22935412069459e-5; 0.0005237968639117913 -1.4832794494346665e-5 -0.0008491457035051241; 1.4830386016567298e-5 0.0005678390336413066 -0.0005301582990606004; -0.000624178549010637 0.0016850823431556253 0.0030450068843580784; -0.00012940858223939018 -0.0003434408512583688 -0.00026532255034900825; -0.0009865769734919102 0.0010203239945900785 0.001488278868589302] %
+
+Mass Used: 155.22113803276534 kg
+Launch C3: 88.5686952446223 km²/s²
+||V∞_in||: 2.0824872736644227e-7 km/s
diff --git a/archive/ES_0.5759047319107596 b/archive/ES_0.5759047319107596
new file mode 100644
index 0000000..9081ce8
--- /dev/null
+++ b/archive/ES_0.5759047319107596
@@ -0,0 +1,22 @@
+archive/ES_0.5759047319107596---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T05:47:48.791
+Launch V∞: [6.720472210476635, -7.229183672225476, -1.1518974179902584] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.601252561439375e-8, -1.3879613304695228e-7, -5.6472396787448664e-8] km/s
+ V∞_out: [5.498637435121226e-8, -7.609409276796132e-8, 1.352934518070403e-7] km/s
+ time of flight: 1.8749577786239022e8 seconds
+ arrival date: 2029-04-06T07:57:25.791
+ thrust profile: [0.19684388088101892 -0.043933861083873836 -0.06407826299888597; 0.10522574891426507 0.036376169874497745 -0.09889183420358107; 0.06899041171362295 0.045726350439430755 -0.1083252800015999; 0.05459859031660195 0.049343776708167586 -0.12319137439832384; 0.03891419421836974 0.04447924699591419 -0.11298298834724146; 0.032264663156279114 0.04380688155442781 -0.11639083433690427; 0.032572733307362975 0.05035274967021794 -0.14004727308466935; 0.01654501896821645 0.0307172734101273 -0.08565200027109766; 0.0071112255434205495 0.014463615706806853 -0.043328542744931725; 0.0033376903074766795 0.006130126258006691 -0.01575453198032888; 0.002917308549846235 0.005585561165715964 -0.015842397074839105; -0.0010023786737326226 -0.0008503788608702858 0.00034505453215565073; -0.00015380008264866346 0.0009236545742651698 -0.0038368622707844703; 0.0054893480057191454 0.009831066651569227 -0.007575763208877753; -0.0008609719545968355 0.002644362953145518 -0.010747052072582175; -0.0088502411564154 -0.00434652599416645 -0.01338299460190695; 2.0280680368950742e-5 -0.0008452560005194985 0.0016970578316862087; -0.0008142459357422518 -0.0033783963313586234 0.005204561339178297; -0.0032366568588371543 -0.002280080081716326 -0.0035064088366809536; -0.0013930361038713528 0.0002262785425424997 -0.0011981737540748489] %
+
+Mass Used: 95.83137329511192 kg
+Launch C3: 98.75271096013275 km²/s²
+||V∞_in||: 1.680220289068823e-7 km/s
diff --git a/archive/ES_0.5759402581589124 b/archive/ES_0.5759402581589124
new file mode 100644
index 0000000..266b772
--- /dev/null
+++ b/archive/ES_0.5759402581589124
@@ -0,0 +1,22 @@
+archive/ES_0.5759402581589124---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T05:46:34.525
+Launch V∞: [5.678970907744105, -7.907774414803186, -0.2912661302955788] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8763825491845026e-6, 1.3931940133185694e-6, 2.179155694546611e-6] km/s
+ V∞_out: [-1.7735151866547777e-6, 2.2098279258289145e-6, -2.633513706899362e-6] km/s
+ time of flight: 1.5573858696247247e8 seconds
+ arrival date: 2028-03-29T18:29:40.525
+ thrust profile: [0.4389337286541167 -0.21554034397579364 -0.1815190869996676; 0.143146567035882 0.007198272765770065 -0.14930427918159092; 0.12249286466108311 0.03403420113100629 -0.20187857380046528; 0.12148451292734726 0.05100032532574609 -0.26591136728924664; 0.07779783564988517 0.04112640052084304 -0.2138617334307858; 0.052612709977703814 0.03240384521390354 -0.17244109094576607; 0.02793850169140986 0.0193197904542504 -0.10666879007656899; -4.817462726299394e-7 -0.0013456751242836968 -0.007726478993331124; 0.004231712188350074 0.0031065156382850435 -0.018112079574034132; 0.008166055575568336 0.003562958276560691 -0.01028628271813739; 0.0037625563927887306 -0.003173613080528085 -0.0006526823032865872; -8.636564492221842e-5 -0.000770025795019171 0.002376387459470381; 0.002041814139540691 -0.0010636166307696725 0.0009905869202116965; 0.00016440279499622265 -0.00309268293786384 0.0037970316718922963; -0.0023102768613605775 0.0006280563088820689 -0.005105891866893515; -0.00028355235538042264 -0.0006529645573654977 0.00809110592543693; -0.003733880536308665 0.010172728899367468 0.007573529954388604; -0.00011785738859963237 -0.00046433371741808527 -0.0024601133457270636; -0.011204908888411375 0.006081742171887374 0.0006568834216629338; -0.0037892937357631665 -0.014518316391370247 -0.018277283529716134] %
+
+Mass Used: 118.5310519557811 kg
+Launch C3: 94.86844272507714 km²/s²
+||V∞_in||: 3.868240642601589e-6 km/s
diff --git a/archive/ES_0.5759769133567348 b/archive/ES_0.5759769133567348
new file mode 100644
index 0000000..e1646d1
--- /dev/null
+++ b/archive/ES_0.5759769133567348
@@ -0,0 +1,22 @@
+archive/ES_0.5759769133567348---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T07:49:42.349
+Launch V∞: [7.318934921952971, -6.927896826446889, -1.4358642974704046] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.67268762498826e-9, -1.2550681334183188e-8, 4.675488557283731e-8] km/s
+ V∞_out: [1.2501609661313902e-8, -4.236153398964434e-8, 6.765381254650276e-9] km/s
+ time of flight: 1.6033130880072653e8 seconds
+ arrival date: 2029-06-14T00:18:10.349
+ thrust profile: [0.0932993946636538 -0.025724083744018 -0.049835100675584686; 0.02152244086360045 0.0028099161003951522 -0.03345750863675998; 0.054299851793830414 0.014408632370136053 -0.142050460381995; 0.05006739218879402 0.016154710923909403 -0.18276771134611586; 0.03729289913697426 0.01271651878808634 -0.17319593557484586; 0.02976108309283081 0.010006274288615218 -0.16401377994040622; 0.012316503181679896 0.0041811339755969045 -0.08228035629762653; 0.0033757026271919004 0.0011669439454160253 -0.024323786207988328; 0.00655093403252884 0.0018065142353478427 -0.05302344743902264; 0.003038668138841006 0.0009167365652076301 -0.026847114036885847; -0.0011387219796049044 -0.002039822848672451 -0.002560660296362375; 0.0005773995908988208 0.00012883355309585012 -0.006237840382571942; 0.001290648125721616 -0.0017372878101697675 -0.002070478029031379; 0.0010084048298694076 0.0004847319382757325 -0.0035279068327676282; 0.0013647152495630402 0.00019691511538201715 -0.004076563600580962; -0.0003676535002105966 -0.0011175798413200523 -0.001442359958273754; -0.0012130780311683839 0.0011558259902159545 4.8477899967405724e-5; 0.0005397929029711203 0.002188624534868116 -0.00024093695789364784; -9.514764746979107e-5 0.0006650962727036513 -0.0016196312911152724; -0.0038403334937192213 -0.0018461057929102175 0.0005541767701926748] %
+
+Mass Used: 67.49816243870691 kg
+Launch C3: 103.6242691104258 km²/s²
+||V∞_in||: 4.874134089017268e-8 km/s
diff --git a/archive/ES_0.5759811976951041 b/archive/ES_0.5759811976951041
new file mode 100644
index 0000000..f52fe71
--- /dev/null
+++ b/archive/ES_0.5759811976951041
@@ -0,0 +1,22 @@
+archive/ES_0.5759811976951041---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T03:22:08.935
+Launch V∞: [7.281305352347205, -5.669656937228578, 0.651146029432309] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8144082665737452e-9, 1.3100870150541078e-9, 3.566557931195864e-10] km/s
+ V∞_out: [1.5640951080964024e-9, -1.4327680218399688e-9, -1.2040625893106209e-9] km/s
+ time of flight: 1.8571420458577853e8 seconds
+ arrival date: 2030-03-23T14:38:52.935
+ thrust profile: [0.999999972954426 0.0083887902431605 -0.12278897062580661; 0.44619782683759573 0.3145764409735176 -0.21164280531804439; 0.13340022404531088 0.16392084271774998 -0.13763511739786075; 0.061043807510275064 0.10828991598849314 -0.10263841273621689; 0.0371724922607515 0.0899635850858565 -0.09198063590392302; 0.016415526851795585 0.05231708271291638 -0.058485264729959706; 0.005843883788734285 0.024487019041548732 -0.029733803732709993; 0.003836977272532631 0.020972908280198852 -0.02707047400194581; 0.0015168950152778912 0.012034034955902528 -0.01653071667749158; 0.0005126900221916826 0.0022911883822415444 -0.001882795769230505; 0.0012218787264714768 0.0004637707950976947 -0.0009903307575769948; -2.1419797069248446e-5 0.0007036893677066676 -0.0007595475554741166; -0.0010225916174297176 0.0004555624550349653 -0.0004617246901912884; -0.0020144870569198006 0.00016964684458069062 -0.000983821183405697; -0.0003086092399232806 -0.0007815298584802384 -0.0018691338471416097; 2.8589323854376835e-5 0.0007566077693655276 -0.0008758008260953147; 0.002919983286166899 0.0002571501151864056 -0.0013281835368362473; -2.7357038647113412e-5 0.0007264201174066193 9.379126537454224e-5; 0.0014205535020786937 -0.0018446864365619636 -0.0015614408132531288; 0.0005685871345772497 0.001826591058318955 0.0008360434891899356] %
+
+Mass Used: 172.72401397644853 kg
+Launch C3: 85.58640857162966 km²/s²
+||V∞_in||: 2.2661881430257034e-9 km/s
diff --git a/archive/ES_0.5760284564174429 b/archive/ES_0.5760284564174429
new file mode 100644
index 0000000..0caeb75
--- /dev/null
+++ b/archive/ES_0.5760284564174429
@@ -0,0 +1,22 @@
+archive/ES_0.5760284564174429---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T09:43:14.612
+Launch V∞: [7.584624330799794, -6.6875296878704535, -0.7645529349058754] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.893022916709127e-5, -1.3064508313901666e-5, -1.2544122117994974e-6] km/s
+ V∞_out: [2.5363018162623003e-6, -4.723022106486971e-6, -2.2413783601071834e-5] km/s
+ time of flight: 1.7363311341322902e8 seconds
+ arrival date: 2029-11-19T01:08:27.612
+ thrust profile: [0.14772279636536761 -0.03271337566610452 -0.07628085835047778; 0.03749211306422067 0.004146284504872692 -0.06135464336120264; 0.02547699417264028 0.0048947888429908175 -0.07247113318167206; 0.025284971426888705 0.003709722076969272 -0.09990561882751849; 0.02299733135750426 0.0022080778495371127 -0.11276591289051158; 0.021828705812700754 -0.0001621517561251843 -0.12619684060851252; 0.012517281661415554 -0.0007416034346799295 -0.07882166483317682; 0.019693510945380084 -0.001615427915411762 -0.13198240868396532; 0.010583325429236378 -0.0006514415664328792 -0.07937082494323919; -0.0002928208744864384 -0.0001981487300823767 -0.0009088989788379276; 0.003108776175540469 -0.0004846229185324965 -0.0036762886655858852; 0.003913032516345513 -0.001049745109162761 -0.029526827252380608; 0.00021284601687626649 -6.775218483756162e-5 -0.0018746671117859045; 0.0008421279600763266 -0.00033496101730300565 -0.007861569190290685; 0.0033598585134657077 0.0018726812928197185 -0.009104979576575732; 0.0012729023798679982 0.0016124284972924704 -0.0007140075549560236; -0.004727027312775322 -0.00028886114390297267 -0.007769917979862919; -0.001224963379018678 -0.0009510585776806072 -0.0011873648722825476; -0.002616179605646345 0.006870957701240564 0.0033253012018306222; -0.0010158939945796497 0.008583888643378492 -0.0029019149956530012] %
+
+Mass Used: 72.16749474495464 kg
+Launch C3: 102.83412075578208 km²/s²
+||V∞_in||: 2.3034940933280262e-5 km/s
diff --git a/archive/ES_0.576030195665179 b/archive/ES_0.576030195665179
new file mode 100644
index 0000000..2157b58
--- /dev/null
+++ b/archive/ES_0.576030195665179
@@ -0,0 +1,22 @@
+archive/ES_0.576030195665179---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T10:50:25.594
+Launch V∞: [7.147827886762248, -6.872662114777323, -0.34441479201641306] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005086461749166772, 0.007748338717076767, 0.0009648157551845139] km/s
+ V∞_out: [0.007224069735931808, -0.0014730925358079287, 0.0015480623452544262] km/s
+ time of flight: 1.4707265260475007e8 seconds
+ arrival date: 2029-01-04T16:21:17.594
+ thrust profile: [0.27759113027773746 -0.07588915906977056 -0.11695890917620594; 0.10190076621532553 0.01951648375140862 -0.12095993470124769; 0.10079216914978817 0.04155328792662224 -0.1888058598772031; 0.07867679068348166 0.04033998884569813 -0.19352887305762997; 0.03994720402490996 0.024722991611080797 -0.13106476075852844; 0.03242422008276779 0.022427919323058886 -0.12686315597216682; 0.024150667109132617 0.018509512920160807 -0.11097041628257785; 0.038065300563325584 0.030666860506156923 -0.17822971790568537; 0.013999713971129696 0.01589992409245086 -0.08745734421881754; 0.006855242082362632 0.005372983164466241 -0.04980072245659334; 0.008381347357709117 0.0070116856469606675 -0.04861342794285232; 0.00011166025556682375 7.93566182213107e-5 -0.0005999101076009294; 0.000310864041544514 -0.0001561539992017691 -0.0003591970785938956; -1.2691650457143664e-5 0.00015276611111014998 -0.0005400341991399244; -0.000511260998179054 -0.00011586257591946744 -0.00043257413563420213; -0.0004163850693674866 6.794758828519926e-5 -0.0005682702835836752; -0.00015817291249467687 -0.0002839084130466256 0.00016143834012365192; -0.00022639390329309427 9.693994675941513e-5 -0.00011285264169818796; -0.0014143442526328622 0.0004782500906783738 -0.0010707801656787256; 0.0008591587335618028 0.0002866515379287959 0.0004836545589840868] %
+
+Mass Used: 97.7811889915265 kg
+Launch C3: 98.44354959163127 km²/s²
+||V∞_in||: 0.007824726400792584 km/s
diff --git a/archive/ES_0.5760895151114493 b/archive/ES_0.5760895151114493
new file mode 100644
index 0000000..e49b07d
--- /dev/null
+++ b/archive/ES_0.5760895151114493
@@ -0,0 +1,22 @@
+archive/ES_0.5760895151114493---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T09:11:00.629
+Launch V∞: [7.0763832170043806, -6.858918291966013, -0.5776815358105769] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.532377357777999e-6, 2.13192186431293e-6, -1.1100225358991665e-5] km/s
+ V∞_out: [-5.303152616453192e-6, 9.533805383472975e-6, -3.3150096669496808e-6] km/s
+ time of flight: 1.455382045016762e8 seconds
+ arrival date: 2028-12-16T20:27:44.629
+ thrust profile: [0.38150763343158955 -0.107897699916729 -0.1498450777133032; 0.10742208868150842 0.02286424860353408 -0.11592741069671086; 0.11099567495064694 0.052522470357769385 -0.19304519276161786; 0.08518783503711905 0.05342459617778371 -0.2077686166647318; 0.046674508009432084 0.035549518288639996 -0.14235270306874456; 0.027910092503935478 0.023725827266772016 -0.10191983010165814; 0.043929747200256226 0.04516715035215789 -0.18843509494004201; 0.030070329626564078 0.030788330498604275 -0.1475658901615472; 0.015236210001710151 0.016325624603498973 -0.0812159761821199; 0.004220687162070056 0.003791311583597156 -0.023996867600573776; 0.00161348569391148 0.00195672758075593 -0.01120184766544453; 0.0005536417075360642 0.0003478066208514502 -0.0010020606823947574; -0.0005317334756315047 -0.00034615450446565517 -0.00021576659400892456; -0.00014778882275159061 0.0007821240808864786 -0.0008860171972797811; -0.0002037026898575288 0.0006109997928811345 -0.00046372568509165843; 0.000640150869376812 0.0006576327232297237 -0.001319423292295592; -0.000215232706125261 -0.00019807229196515077 -1.9491433473878543e-5; -0.0001234860149621711 -0.0005906778455535997 0.0008492009495337524; 0.001380921444575477 -0.0008578499226923376 -0.0007810333085989465; -0.0006957770372798541 -0.0007894602342688377 -0.0007943885248869492] %
+
+Mass Used: 103.62466039161927 kg
+Launch C3: 97.45367552658371 km²/s²
+||V∞_in||: 1.1406501401506417e-5 km/s
diff --git a/archive/ES_0.5761068830800884 b/archive/ES_0.5761068830800884
new file mode 100644
index 0000000..3cf0cac
--- /dev/null
+++ b/archive/ES_0.5761068830800884
@@ -0,0 +1,22 @@
+archive/ES_0.5761068830800884---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T06:25:03.237
+Launch V∞: [7.470102373619844, -5.584623252367012, 0.3981566750188151] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6518459907404593e-7, 1.979332722819372e-6, -4.141458053626796e-5] km/s
+ V∞_out: [-1.7326337748855313e-6, 4.136319137511463e-5, -2.3764234879055922e-7] km/s
+ time of flight: 1.8749577787455168e8 seconds
+ arrival date: 2030-04-13T08:34:40.237
+ thrust profile: [0.9291310256252875 0.029174251303764456 -0.11986624039130502; 0.30041111105330587 0.22756822030745177 -0.15975358059676414; 0.16826864679428938 0.2213594729394115 -0.16993103841176949; 0.08984321796120193 0.17198166001554022 -0.15185698161764155; 0.025149985349803373 0.0642928324393023 -0.06721078096811565; 0.016430838525648833 0.05913832775581697 -0.06764980924088225; 0.005891522715931204 0.026075872852401046 -0.03278467621784234; 0.0020261165111345957 0.01070373026144638 -0.013637405009023471; 0.0011382361594621173 0.014467172017730763 -0.019192888666359827; -1.9396266641629067e-5 -0.00011706647196226658 -5.9914482283679365e-5; -3.6231331617822665e-5 9.579952240879997e-5 -0.00018769835201514905; -0.00010019368203374534 0.00024710950311361405 4.7475660832994556e-5; 3.410137255528036e-5 -8.931817076818162e-5 4.564254132130867e-5; -9.122405439083907e-5 -2.6378546366188102e-5 0.00023982645505131616; 9.351331892391488e-5 9.768308632023765e-5 0.00011975632983712571; 8.376161055755255e-7 0.0002703769675575201 0.00010494971369283282; 0.00031337367997321834 -0.0004560094494729409 -5.6925986030323155e-5; 4.884210971598057e-5 -0.000174707839071069 -6.288227189892064e-5; 4.990915703135932e-5 0.0001260748581205204 -0.00045699118545625866; -1.044994692836281e-5 -2.95998861061017e-5 0.0003040254640174256] %
+
+Mass Used: 163.7556756203462 kg
+Launch C3: 87.14897508110118 km²/s²
+||V∞_in||: 4.1462700851418666e-5 km/s
diff --git a/archive/ES_0.5761185086332831 b/archive/ES_0.5761185086332831
new file mode 100644
index 0000000..3f6ca9a
--- /dev/null
+++ b/archive/ES_0.5761185086332831
@@ -0,0 +1,22 @@
+archive/ES_0.5761185086332831---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-08T21:57:49.100
+Launch V∞: [6.1792652634028125, -8.02178921561716, -0.5710823043326353] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01017530548060398, 0.00030673526343012676, -0.006934789709717585] km/s
+ V∞_out: [0.011798849967935116, -0.0001219881695894506, -0.0035582509787091374] km/s
+ time of flight: 1.829442836385605e8 seconds
+ arrival date: 2029-02-23T07:49:12.100
+ thrust profile: [0.12048387408726759 -0.053460989642710864 -0.06460502617178872; 0.03637434374634568 -0.005025727301218836 -0.06094580368569291; 0.015106632542803247 -0.001931143848871072 -0.04360442874356746; 0.027302890278938022 -0.005980458647887983 -0.10966847980697975; 0.043189797053768755 -0.014233310330318235 -0.2137401084234932; 0.021353894030553343 -0.008522614315706833 -0.12252384661370706; 0.020222276382439352 -0.010074839670536169 -0.13139045304413727; 0.009168292987555183 -0.005061046320928647 -0.06397633527574735; 0.005449470407053516 -0.003338698916345668 -0.04186470714239713; 0.0009866007980844985 -0.0011554700162984743 -0.006940029723943158; 0.00021097938664482548 -0.0008125905590105368 -0.0017139721538413594; 0.0009529341137936083 -0.0004425433943538178 -0.004704810273849478; 0.0001602716209849579 -2.9196694682198914e-5 -0.001703237880474811; -0.0006602115683769791 0.0003509976131236746 -0.0007037505250919313; 0.00026204089790110064 -0.0001222549376349441 -0.001716280622172146; -0.0002806925874599866 -0.0004380438996346456 -0.002501051749492005; -0.00010683262993557669 -0.00020324071925053168 -0.0010111119872455204; -0.0016387363017210813 0.0014167943793693852 0.0016926944284417766; -0.0005774604286502376 0.0006267566093186977 -0.0009110697940533237; -0.0029896424363424993 -0.0003111480955882141 0.0012903788983015692] %
+
+Mass Used: 72.13001432610372 kg
+Launch C3: 102.85855641361026 km²/s²
+||V∞_in||: 0.01231755805602092 km/s
diff --git a/archive/ES_0.5761197329853877 b/archive/ES_0.5761197329853877
new file mode 100644
index 0000000..68fef0a
--- /dev/null
+++ b/archive/ES_0.5761197329853877
@@ -0,0 +1,22 @@
+archive/ES_0.5761197329853877---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T03:22:21.060
+Launch V∞: [5.655230662337187, -7.6533619817085965, 0.13221413763680376] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.548170938448217e-7, -1.3943253717867031e-7, -2.2313393239626272e-7] km/s
+ V∞_out: [1.641099428311768e-7, -2.051795519739333e-7, 2.5607080808907336e-7] km/s
+ time of flight: 1.6009190825771326e8 seconds
+ arrival date: 2028-05-16T01:20:49.060
+ thrust profile: [0.7422991246350484 -0.31961460243385664 -0.21869297431894594; 0.29361012334036457 0.04212632745929096 -0.23619741546690834; 0.17374318116908097 0.07356633448562053 -0.23373997234592309; 0.07812151006811996 0.0453617820950592 -0.1441276768040975; 0.0805406008163588 0.05882219556801189 -0.18722499006200802; 0.03524117488515089 0.02901548492432446 -0.09645976383541172; 0.022268100633220638 0.021248624687731903 -0.07247649768577302; 0.03094316678075086 0.03598664506920584 -0.11728399053627608; 0.0025698920683547635 0.002321373781799878 -0.01097398710867815; 0.002096775782638314 0.0023369887199895787 -0.005433686061548988; -0.0004409698551776642 0.0001858649222501637 -0.00020051284959541889; 0.0008921861104299883 0.0004703453233459266 0.0010277534049521722; 0.0017447572829469116 0.0004682836564562022 0.000986991469868539; -0.0025297904599613005 0.0036243099019944006 -0.0021516464105463366; -0.0026072346878693677 -0.00269495448565933 -0.00245390749162873; 0.0002667751078024122 0.0018149268837550428 0.0033257377765428544; 3.402789877188456e-5 -0.0005669552876721891 0.0002785445098399637; 0.0010793348897733107 -0.0016837934544901663 0.0013971251098436359; -0.0009670155109979199 -0.0015407182018659358 0.004836558666338938; 0.0011140834231463809 0.00021944003151270824 -0.0009542526790976939] %
+
+Mass Used: 143.7968148842474 kg
+Launch C3: 90.57306404549227 km²/s²
+||V∞_in||: 3.662812246433359e-7 km/s
diff --git a/archive/ES_0.5761291832359887 b/archive/ES_0.5761291832359887
new file mode 100644
index 0000000..ad3d97c
--- /dev/null
+++ b/archive/ES_0.5761291832359887
@@ -0,0 +1,22 @@
+archive/ES_0.5761291832359887---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T19:06:57.981
+Launch V∞: [7.491677613274576, -6.123323548733428, 0.3682467507881154] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.330452120825017e-9, 4.511932413601286e-9, -6.007558638560589e-9] km/s
+ V∞_out: [5.095297617646358e-9, 9.58123281853125e-9, 3.0829872249158236e-10] km/s
+ time of flight: 1.660841761646285e8 seconds
+ arrival date: 2029-08-08T01:36:33.981
+ thrust profile: [0.44864647284936676 -0.04864225425421055 -0.10653900119570206; 0.27757287278330306 0.13538107185449494 -0.19684625492007374; 0.1652816499021855 0.14198237183174986 -0.204201941737808; 0.09468630085529325 0.11106413076535757 -0.17308221670630936; 0.05079769674316434 0.07478049931602823 -0.12920058996127676; 0.021664782747635884 0.04006284286815608 -0.07716667105188495; 0.013897288495717633 0.03209744062269221 -0.06888326197102182; 0.005224929192911876 0.014021165198785525 -0.03220203939913789; 0.008940603654784312 0.01980595707769687 -0.03481768722789209; 0.0021867470608687607 0.0091242049999126 -0.020610447455933004; 0.007393311629490587 0.007187949491868707 -0.03434939085505083; -0.002063102250504453 0.0025864372902728266 -0.007668233597188077; 0.0015685822331835053 -0.006952242267222289 -0.006012493962651627; -0.001075329176508757 -0.0019838835138111703 -0.006024553290434701; 0.0032534225235058005 0.015716258613268273 0.005342348687230094; -0.00197222411363742 0.015764377293264353 0.0037864095781033574; -0.000452221578047378 -0.002810609626762675 0.007435215686793886; 0.0004572506653947513 0.0009417927761427034 -0.0030496501460000203; 3.6697443670038375e-5 -0.0012932679843115197 -0.0015322291467851014; -0.005219749369455308 0.00654917438643584 -0.002286213602775128] %
+
+Mass Used: 125.24111969844398 kg
+Launch C3: 93.75593041317879 km²/s²
+||V∞_in||: 1.0496848250611128e-8 km/s
diff --git a/archive/ES_0.576171665336409 b/archive/ES_0.576171665336409
new file mode 100644
index 0000000..5a7146d
--- /dev/null
+++ b/archive/ES_0.576171665336409
@@ -0,0 +1,22 @@
+archive/ES_0.576171665336409---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T12:01:01.255
+Launch V∞: [7.380722537053755, -6.59684902174425, -0.3052122686285821] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006398195520402464, -0.0022340577809726024, -0.003610895371149509] km/s
+ V∞_out: [-0.0037537699291116796, -0.00044488528515389307, 0.002036808682067206] km/s
+ time of flight: 1.576898632883e8 seconds
+ arrival date: 2029-05-08T14:45:24.255
+ thrust profile: [0.15330096601851342 -0.03708228068165335 -0.06298466103012759; 0.22461026252861557 0.05418466384833929 -0.2639240319326475; 0.07210721556992537 0.0325651137724465 -0.1419244427301298; 0.04279650683951862 0.025346791922423492 -0.11809199402088003; 0.03639610676895039 0.02509192296818613 -0.1274038041984178; 0.03402679813797642 0.02576342804845647 -0.14249077671238447; 0.02170263515637589 0.017968893020216408 -0.10583384527032076; 0.005377802624615454 0.007081588965508105 -0.04231611935231495; 0.010268156700895915 0.009523880555568283 -0.060945434023993314; 0.006042377035911807 0.006112026929747593 -0.040778549216861394; -0.0006422450199695142 0.000724851053148221 0.00016279424774187943; 0.016800949545200936 0.006189182865385593 -0.025572795270860683; -0.0047213068000905535 -0.009226211639558817 -0.0006281927470567969; -0.00034502366769548855 0.006715748680424419 -0.012848984747538412; 0.011725168810064449 0.012154705452965138 -0.011164544139131835; 0.008497055626062993 0.007265765305875782 -0.057803547853575686; -0.008201209007459041 -0.005289760401013802 -0.02645672970903623; 0.00092449184215318 -6.892984282039134e-5 -0.03301843218993476; 0.006939132481266933 0.0023868765815630946 -0.02329510660199721; 0.013181937291936287 -0.0027961310893156815 -0.013929621952809553] %
+
+Mass Used: 100.02822872991146 kg
+Launch C3: 98.08663671358268 km²/s²
+||V∞_in||: 0.004294059688603101 km/s
diff --git a/archive/ES_0.5761732358060855 b/archive/ES_0.5761732358060855
new file mode 100644
index 0000000..bc6d4ac
--- /dev/null
+++ b/archive/ES_0.5761732358060855
@@ -0,0 +1,22 @@
+archive/ES_0.5761732358060855---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:05:28.050
+Launch V∞: [5.803093703243931, -8.055177847935024, -0.5246872348949412] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.929699608357838e-8, -1.623360473022105e-8, 3.3293510776525484e-8] km/s
+ V∞_out: [1.440024430019956e-8, -3.192732370610619e-8, -4.2315674338672494e-8] km/s
+ time of flight: 1.5176038990525076e8 seconds
+ arrival date: 2028-02-13T02:45:17.050
+ thrust profile: [0.1599838172572671 -0.08418913300015102 -0.07412718505216417; 0.12074494538040446 0.0011087559295548024 -0.13461684811184804; 0.1129002812512761 0.025228612399089908 -0.19668283395651484; 0.09688314015771096 0.03437722975247055 -0.22563616295944117; 0.07331527412209693 0.03305770807147277 -0.21168025313977626; 0.04969936995223636 0.026028724243452598 -0.16953043600359616; 0.028644719202821464 0.016218188992484166 -0.11086460864855913; 0.01815951248440504 0.010784594762094488 -0.07775169744209778; 0.014294310402954456 0.009096741213926172 -0.0669516139501065; 0.005921229682022447 0.0038269188423034088 -0.029891525780227936; 0.002174137016365209 -0.0006129810657329023 -0.001289178099392272; 0.0017009418435102379 -0.001193241372038029 -0.004397724973561744; -0.000713758465448009 -0.0005975539505899674 0.0008277191351488775; -0.0009032341370898301 0.002298232017650053 -0.0013482014379936065; 0.0032886902532447554 0.0013393485508126598 -0.003186158078555059; -0.0005450999677339088 -0.0023919038421303766 -0.0009700104608913636; 4.474614186516029e-5 -0.00018356093766743603 -0.0013591489699032301; -0.001134680775088561 -0.0011139269558125809 0.002687602952629475; 0.0007379862984556334 0.0034096689947637824 0.002750574129100533; -0.0007752890403605834 0.0007819682610969623 0.001210536957244842] %
+
+Mass Used: 95.65245536153361 kg
+Launch C3: 98.8370833849542 km²/s²
+||V∞_in||: 5.4002237764341285e-8 km/s
diff --git a/archive/ES_0.5762147587312444 b/archive/ES_0.5762147587312444
new file mode 100644
index 0000000..83cd969
--- /dev/null
+++ b/archive/ES_0.5762147587312444
@@ -0,0 +1,22 @@
+archive/ES_0.5762147587312444---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T04:17:48.317
+Launch V∞: [7.096081526164937, -6.781244318914915, -0.3933565676614262] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.652012140508305e-6, 9.677618238623894e-6, 5.015399202721821e-6] km/s
+ V∞_out: [7.72543239589889e-6, -7.1512573634567135e-6, -4.618521805486659e-6] km/s
+ time of flight: 1.482820899628903e8 seconds
+ arrival date: 2029-01-18T09:45:57.317
+ thrust profile: [0.466277373559367 -0.13723378425404004 -0.19707958705560807; 0.11903486752530362 0.022497749337238446 -0.14935466686125154; 0.0878871218233778 0.03466563675216113 -0.1822127151364163; 0.057182745116483975 0.028038207437200237 -0.1610328125195479; 0.03961226647073453 0.024751902455072104 -0.14273555327916485; 0.03693956376499859 0.023738644160766906 -0.14652547366916555; 0.0195073007912086 0.014079527770333986 -0.09453440400350047; 0.01899416772751325 0.01331238737068198 -0.09590390783470916; 0.027156069006915085 0.021657262777360242 -0.15099788876216566; 0.00664911960797533 0.006621825549620921 -0.04644005562089008; 0.0014006446994651654 0.0013375890892409494 -0.00893090209853356; -0.0029273830957575906 -3.712291214076711e-5 -0.0017571582373320915; 0.002093168470347093 -0.0039071788827075675 -1.9295804987232157e-6; 0.002772531894319059 -0.002619300849476999 -0.003728910567683364; 0.0039032772423082196 0.0011378533524059537 0.002588787174891411; -0.0016195784123086646 0.0018661563509656388 0.004773488365157407; 0.0018734252363145905 -0.0043112391228927 -0.0011079731678160895; 0.00041186918483809083 0.005571695192860278 -0.0023898942820824386; -0.0017585619463760453 0.0007893745092542475 -0.00824590134242595; -0.0001261617707885915 -0.002271780947528548 -0.002642220959870787] %
+
+Mass Used: 109.3666864390998 kg
+Launch C3: 96.49437692811749 km²/s²
+||V∞_in||: 1.1495552035880162e-5 km/s
diff --git a/archive/ES_0.5762857553198342 b/archive/ES_0.5762857553198342
new file mode 100644
index 0000000..11ab273
--- /dev/null
+++ b/archive/ES_0.5762857553198342
@@ -0,0 +1,22 @@
+archive/ES_0.5762857553198342---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T00:57:04.510
+Launch V∞: [6.244521737446748, -7.198881507475573, 0.20046252050004207] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.392575988533704e-6, 4.015900904601565e-6, 4.823826936506799e-6] km/s
+ V∞_out: [6.546810719359053e-6, 3.971456475341485e-6, 1.2708020509622959e-7] km/s
+ time of flight: 1.8464503629020575e8 seconds
+ arrival date: 2029-02-28T03:14:20.510
+ thrust profile: [0.701327207135344 -0.15646522602477106 -0.15172737934525635; 0.21897110777943582 0.08320461890888871 -0.15876169075818258; 0.11112871127560608 0.07856099572898535 -0.13941470970134984; 0.08025177042370647 0.07984408968288556 -0.14393837628854644; 0.05006786520265877 0.06065774227108262 -0.11249518771884363; 0.03422896001493611 0.051147801930062596 -0.10167514202086428; 0.017028471548855274 0.028328510927531136 -0.05831876346257912; 0.012437237318622629 0.021391870195381683 -0.049322559023265794; 0.002498569992531595 0.008339421832512088 -0.01494578364000029; 0.0009200483622159624 0.006853573603335202 -0.012003793754320898; 0.0014919767317153664 0.0031270157244676624 -0.0077897362420822095; -0.00016385661584653358 0.0020093750588376655 0.0018028323766750773; -0.0006761360563257678 0.003030376333532313 -0.009324380812628225; -0.007240405533931769 0.005342283334370439 -0.0059357174169474515; -0.0009909376671329503 0.0024269265871452498 0.0038783386164155773; -0.003149843810371177 0.0007346545152038715 -0.002603951077232244; -0.00374482845832269 -0.020426694149238638 -0.013892729465995207; 0.0016917308174304022 -0.0010972291812353444 -0.004903757861206878; 0.011305385358004806 0.023889395356732252 -0.0036035408085429706; 0.017278993475037585 0.01719527466615046 -0.022754568795376004] %
+
+Mass Used: 142.3276117300502 kg
+Launch C3: 90.85813191024396 km²/s²
+||V∞_in||: 7.661037149367643e-6 km/s
diff --git a/archive/ES_0.5763054372566939 b/archive/ES_0.5763054372566939
new file mode 100644
index 0000000..2a00a4d
--- /dev/null
+++ b/archive/ES_0.5763054372566939
@@ -0,0 +1,22 @@
+archive/ES_0.5763054372566939---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T12:10:13.194
+Launch V∞: [5.637942898602328, -7.823957730946929, -0.21685312723028838] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6885095757689864e-7, 1.5886850660925677e-7, 2.4983019328863534e-7] km/s
+ V∞_out: [-1.6132607573765654e-7, 2.3831252939548353e-7, -2.6538235635761914e-7] km/s
+ time of flight: 1.5547185463285398e8 seconds
+ arrival date: 2028-03-24T22:47:47.194
+ thrust profile: [0.6065077439409327 -0.27559685066521983 -0.20612122309674494; 0.21694963279109736 0.024781332284410092 -0.20401020378376425; 0.10893653296212205 0.041773373231526405 -0.1767341295837803; 0.07816308562058638 0.04736493718356266 -0.1832671707259952; 0.06039639218989166 0.04915667188937187 -0.160909476062798; 0.05042303921778276 0.038887970716854514 -0.14723771249284767; 0.022999748825342087 0.024088166933369647 -0.08613802110319954; 0.02662241926118838 0.029000653566435358 -0.1280003753771738; 0.007620693198988633 0.007101267110465848 -0.032537741345468066; 0.005766145442999816 0.005303374577428041 -0.025504230240921324; 0.00012637478549202305 0.0012910944909479028 -0.002116328846266823; 0.0027509885738909784 0.0036461804145822277 -0.013326411825938658; -0.0003474271152744419 0.0006029567517270401 0.0014286699209952614; 0.005687018588397317 0.0009629547318092315 -0.0039355842253808; -0.00374860951112717 -0.0025001948250182333 -0.001715875011193814; 0.0019440515779091366 0.00277406111994617 -0.01015789424972956; 0.0012376288623576694 -0.00223133959077675 -0.0055257755442289745; 0.0011484086564551668 0.0012593815457093835 -0.0023260533202778943; -0.0012229427848777397 0.0004024735085321374 0.001779038510172035; -0.0007924622768157477 -0.0015700173841972024 0.0013488694365244923] %
+
+Mass Used: 129.57786023586004 kg
+Launch C3: 93.0477399823342 km²/s²
+||V∞_in||: 3.999189483644251e-7 km/s
diff --git a/archive/ES_0.5764266663083246 b/archive/ES_0.5764266663083246
new file mode 100644
index 0000000..abd745b
--- /dev/null
+++ b/archive/ES_0.5764266663083246
@@ -0,0 +1,22 @@
+archive/ES_0.5764266663083246---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-24T06:42:59.595
+Launch V∞: [7.877911353334458, -6.435311597249914, -0.6920146140439208] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.708841510371157e-5, 6.419663725466747e-5, -4.761535170443462e-5] km/s
+ V∞_out: [1.1512883822190624e-5, 0.00011035330301030453, -4.847847280524002e-6] km/s
+ time of flight: 1.874957776121339e8 seconds
+ arrival date: 2030-05-03T08:52:36.595
+ thrust profile: [0.18681035834984036 -0.022975082294332184 -0.09001063921168238; 0.01870015597744924 0.0034378839024710216 -0.03085292594485847; 0.015543931705170632 0.003340936221084172 -0.044525737656911875; 0.044103327157409604 0.008319965774612878 -0.1706030156386039; 0.022981985105182075 0.002487698011355527 -0.10960530104228755; 0.013332897947419644 0.0004101306969886855 -0.07427050046604053; 0.011970879134652113 -0.0003945749535565491 -0.07421399789751637; 0.006466903799616413 -0.0005782776540147186 -0.04334481048111086; 0.0075330802186589045 -0.0011683098419418521 -0.053881467561734356; 0.005092065684714094 -0.0009529313645620138 -0.03744770178504853; 0.001136059899975312 -0.00016217829156998402 -0.006991578176275775; 0.0011555785169080422 -0.0004695289121525259 -0.006362537290818572; 0.00014161728011989621 0.0003315563053203866 -0.0007777237794625255; 0.0003710591347804427 -0.0001053755899675746 -0.0005135490015176963; -0.0002439517160757568 -0.0005896814060292973 -0.0004873983790339304; 0.00030482891157752304 0.0001556285065695761 2.0172601691774363e-5; -0.00016456592141571042 0.0003706529287875465 -0.00046048097705630835; 6.260321493295191e-5 -0.0001927227035712426 -2.2652831120913695e-5; 0.0005953217584228745 -0.00019653071461221886 -0.0007929483213975093; 4.505616698872745e-5 -8.732305203234495e-6 -6.188200577899688e-5] %
+
+Mass Used: 66.10173728036307 kg
+Launch C3: 103.95360687074555 km²/s²
+||V∞_in||: 0.00011104527768413437 km/s
diff --git a/archive/ES_0.5764390243645301 b/archive/ES_0.5764390243645301
new file mode 100644
index 0000000..dc7239c
--- /dev/null
+++ b/archive/ES_0.5764390243645301
@@ -0,0 +1,22 @@
+archive/ES_0.5764390243645301---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T21:56:17.704
+Launch V∞: [5.385901444815833, -8.104883535357397, -0.22222863671079593] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.5735918120227645e-5, 3.4104971920223652e-6, -4.260128490767266e-6] km/s
+ V∞_out: [5.3960458234308454e-5, -1.3430122793223169e-5, 6.648614983784394e-6] km/s
+ time of flight: 1.5383794613081685e8 seconds
+ arrival date: 2028-03-08T10:42:03.704
+ thrust profile: [0.3252078549077737 -0.14417085551910458 -0.11534969978237194; 0.34388518160278403 0.03398038101471383 -0.2739102262002831; 0.11068616493639305 0.04382467466083194 -0.15511348958211144; 0.07147495207309125 0.03919730765269814 -0.13821417897234967; 0.10910262340510833 0.07159531995053381 -0.23807212187387972; 0.043952219274045495 0.03476359284527043 -0.12013859639809774; 0.05651275683559139 0.04949344458707357 -0.170261943305552; 0.01802952922834661 0.015802431948340984 -0.0657337892139076; 0.009122501773294045 0.008693587126594259 -0.03714217921892011; 0.0037117098309224997 0.005009999911842246 -0.02201818750063943; 0.001078568027476483 0.0024940607730232385 -0.0011057568935118915; 0.000633225690816785 0.003766406366831172 -0.0035283884514475962; -0.004420654349049936 -0.005604310861398192 -0.00015112278973822496; 0.00461654105541198 -0.0027272080261689937 -0.0035190252107547776; 0.0006434585991025593 -0.0033290300977992684 0.003391742837557936; -0.0019001679651606913 0.0075157479631339985 -0.0016513233627435554; 0.005195308628602662 0.002511472406208775 -0.003228992830922148; 0.004738591999201353 0.00038389754747626117 0.006476347041895103; 0.0013294920126301294 -0.005077127417512794 0.008333874488443721; -0.0013708398417529508 -0.002727938608967079 -0.002669916452845444] %
+
+Mass Used: 119.82452889723754 kg
+Launch C3: 94.74645706195102 km²/s²
+||V∞_in||: 5.600243525561509e-5 km/s
diff --git a/archive/ES_0.5764393926470632 b/archive/ES_0.5764393926470632
new file mode 100644
index 0000000..10c276b
--- /dev/null
+++ b/archive/ES_0.5764393926470632
@@ -0,0 +1,22 @@
+archive/ES_0.5764393926470632---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T23:50:47.477
+Launch V∞: [7.095045878855064, -6.728651072367762, -0.3752920510343296] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.026652920134926414, 0.012473928029163013, 0.0009926978520555113] km/s
+ V∞_out: [-0.023295189145314397, -0.011542059997337128, 0.013823749213760825] km/s
+ time of flight: 1.460746945856617e8 seconds
+ arrival date: 2028-12-21T16:09:01.477
+ thrust profile: [0.4576560967376659 -0.13714201718262173 -0.18379284803236556; 0.20096509411351976 0.039139516589491045 -0.21603179249762225; 0.11411134477517326 0.048207417147704115 -0.2029256194225928; 0.10913769070756969 0.06192612245850073 -0.26258323485011403; 0.08191876064100627 0.05494879392065346 -0.24634919090623442; 0.039919857144006296 0.030382570546511355 -0.1472041235130197; 0.010464364521028996 0.009265386037475478 -0.04756623785801244; 0.00538236497112908 0.004733976730807253 -0.026192636216467755; 0.002331598196125651 0.0023519499830629807 -0.019413506565286277; 0.008101028532167034 0.008050365782883222 -0.04770364752867997; 0.00220119147748133 0.0027394101560199603 -0.006973073143749111; -0.0016410144600598254 -0.002788612141573921 -0.0036454178504418426; -0.0003826092909969326 0.00024370622916921724 -0.0022098476904019917; -0.00324717403513187 -0.0007034916584522043 -0.003777263584390697; 0.007389544620274063 -0.0003238787003475883 -0.0053650879820737775; -0.0008782808078510344 -0.0012772044553945546 0.0005408664333000687; 0.0016578098956253687 0.00955555136515479 -0.0007695747345103855; 0.001642686715918061 0.0013806309830070738 0.004735664772187934; -0.001255815710886769 -0.007008807015507902 -0.00132754501378311; 0.00014538509483966636 0.0005118895784180106 -0.001194632850172469] %
+
+Mass Used: 113.94024325313603 kg
+Launch C3: 95.75526540030361 km²/s²
+||V∞_in||: 0.029444226619508622 km/s
diff --git a/archive/ES_0.5764606261168779 b/archive/ES_0.5764606261168779
new file mode 100644
index 0000000..64648c8
--- /dev/null
+++ b/archive/ES_0.5764606261168779
@@ -0,0 +1,22 @@
+archive/ES_0.5764606261168779---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T02:41:52.895
+Launch V∞: [7.328558628119167, -6.506313389085799, -2.0094885325310603] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.27303365322252e-8, -8.191303097549035e-9, 7.294225513989017e-9] km/s
+ V∞_out: [-6.000848152714064e-9, -1.1656765012807197e-8, -3.8333358966284995e-10] km/s
+ time of flight: 1.6707926807678527e8 seconds
+ arrival date: 2029-08-26T21:36:20.895
+ thrust profile: [0.20626129240540403 -0.013784895633099169 -0.07622768097055757; 0.1241797047056869 0.06605811164191368 -0.12280303771672876; 0.0841032293787868 0.07844826439155744 -0.14367102665787537; 0.05950809134433884 0.07686006244160758 -0.14967728494661572; 0.041218079795088354 0.0679348437648954 -0.14191051834772417; 0.02703591470881339 0.0544039262209613 -0.12219203654748025; 0.01928605052371363 0.04620193285785522 -0.10894010562202164; 0.009854988376851953 0.026867671777140084 -0.06900271297609337; 0.005030207496345048 0.015373856824884883 -0.041648783928302076; 0.0004922030029775124 0.001965341867344787 -0.005873881815091316; 3.080884159747282e-5 0.0011950368519182196 -0.004728511856035887; -3.453019431982635e-5 0.0001804763324900401 -0.0009357015319782838; 0.0011931084890029879 -5.626643123621733e-5 -0.0008505114620572619; -0.0003937098165115234 0.0014228103428783273 1.2613741291013026e-5; -0.0006930225084673229 0.0005899939417012331 -0.003451741528830116; 0.0013185632058304673 -0.0003991232930001873 0.0016425726667945863; -0.0007340533550702362 -0.0009534769662272323 0.0014785431296006775; -0.0002858470784529995 -0.00037335517762362167 -0.0002404610121093621; 0.00015682215510481396 0.00020447810688457328 -0.0022848061189745315; -3.162482604688089e-5 -0.00020843682055027778 0.0005830520750647861] %
+
+Mass Used: 88.74947420631088 kg
+Launch C3: 100.07792964515085 km²/s²
+||V∞_in||: 1.680370912949139e-8 km/s
diff --git a/archive/ES_0.5764770388883167 b/archive/ES_0.5764770388883167
new file mode 100644
index 0000000..477243e
--- /dev/null
+++ b/archive/ES_0.5764770388883167
@@ -0,0 +1,22 @@
+archive/ES_0.5764770388883167---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T11:47:29.729
+Launch V∞: [7.9502494477026655, -6.257979267130931, 1.1507701970385709] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.659470799399111e-5, -0.000968649891757027, 0.019978917339922356] km/s
+ V∞_out: [7.481773658190039e-7, -1.9141945783601527e-5, 1.6163517055550648e-7] km/s
+ time of flight: 1.8749577787461823e8 seconds
+ arrival date: 2030-05-01T13:57:06.729
+ thrust profile: [0.10999902747498486 -0.009042693151522917 -0.04596582312812353; 0.027293784644751757 0.007334336168577482 -0.03839328247056604; 0.03484469740987517 0.012326686035742955 -0.08384147115544417; 0.03579215962263889 0.01327089150541075 -0.11772407809744168; 0.03241019538850545 0.01152128827759561 -0.13109335999973185; 0.026440139965429793 0.008455085047144945 -0.12329268870725801; 0.02418784552514564 0.0071496097166990425 -0.12624294268068756; 0.01162315360079226 0.002687193445927502 -0.06596872772616744; 0.004646576950417134 0.0007834013516683596 -0.027786160312528525; 0.0006600189278632889 -0.00031951759248485985 -0.00322462283686398; 0.0008915119887410001 0.0006640464835624491 -0.00870321887129613; 0.0003289426042660801 -0.00019267013803509945 -0.0015923823166795435; 0.0005838170807419401 9.36051010942035e-5 -0.0025588186385924064; -0.0009040109564931354 0.002295379078072502 -0.0031480060114674408; 0.0007560631867738151 0.00012810013009927995 7.794369758870622e-5; -0.0014407269467518677 0.0030040431483853835 -0.001889312463884761; -0.00017311422784950558 -0.0004062474675085825 -0.00024334311040087044; -0.002181858770833449 -0.0035780730773205755 -0.002924174078117238; -0.000530037791867405 -0.00263830302898035 -0.0048025920538611365; -0.000659492642090676 -0.0018114244053333284 0.00042901164586896625] %
+
+Mass Used: 67.68046216594848 kg
+Launch C3: 103.69304283492932 km²/s²
+||V∞_in||: 0.020002618609218734 km/s
diff --git a/archive/ES_0.5764904613339936 b/archive/ES_0.5764904613339936
new file mode 100644
index 0000000..ef5df51
--- /dev/null
+++ b/archive/ES_0.5764904613339936
@@ -0,0 +1,22 @@
+archive/ES_0.5764904613339936---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T17:39:30.907
+Launch V∞: [6.299622794007508, -8.015443040424076, -0.2759484169666069] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.061775880964851e-9, 2.5932717496720347e-9, -1.128880977794897e-8] km/s
+ V∞_out: [-5.372795877108664e-10, 1.169194254684158e-9, 1.1616270925943651e-8] km/s
+ time of flight: 1.845848834058358e8 seconds
+ arrival date: 2029-03-15T03:14:13.907
+ thrust profile: [0.03126257028465962 -0.013557596660642036 -0.017477283176014474; 0.017381234096361806 -0.002640606285690318 -0.03106367272209857; 0.03046239344204407 -0.005255132482181589 -0.09121261279835374; 0.03308938081844872 -0.008658035238395607 -0.13648316393291302; 0.029602475014883948 -0.0108095556449576 -0.15042685496438268; 0.023711392979277313 -0.010935856691121246 -0.13537614549169869; 0.019543225824585748 -0.01094500416173635 -0.1090229408339625; 0.014467035919697148 -0.009293033426024633 -0.09791280750436702; 0.0037312023110324826 -0.0029130381359248753 -0.029269683054703798; 0.004063123986144873 -0.0031735370496211875 -0.03300436432810037; 0.0005983048040577728 -0.0002064957317483517 -0.0038933864488127504; -4.132990992716429e-5 -4.943616352885714e-5 -0.000489785133045114; 0.00018377006782663752 -0.0002512484879819213 -0.0020253786677659523; -0.0006062953193666144 0.0003082812759328798 -0.0015922698703334792; 0.0002500451257603342 -0.0007006612242232771 -0.00216196772779252; -0.0014002364950690535 -0.0014180662475317936 -0.00011477817411088332; 0.00033786203337901567 -0.00021498943551020826 -0.0003129775290477858; -0.0033983636093427717 -0.0025301708168147968 -0.0014854933303941184; -0.00025189133413251166 0.0006980998395892197 0.0002568975679037896; -0.00032002934647943357 0.00028672888114100135 0.0012958360013428816] %
+
+Mass Used: 65.85465983197855 kg
+Launch C3: 104.0087220098881 km²/s²
+||V∞_in||: 1.4112211553306232e-8 km/s
diff --git a/archive/ES_0.5765514007287134 b/archive/ES_0.5765514007287134
new file mode 100644
index 0000000..f2cb21d
--- /dev/null
+++ b/archive/ES_0.5765514007287134
@@ -0,0 +1,22 @@
+archive/ES_0.5765514007287134---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T09:04:12.471
+Launch V∞: [5.910459005948936, -7.898269830453135, -0.15369498833256168] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.581584140986212e-5, -0.0001244700650658666, 2.1188069278528938e-6] km/s
+ V∞_out: [2.9295900412241193e-5, -7.117992286545236e-7, -0.00015433702403522755] km/s
+ time of flight: 1.5697635940531245e8 seconds
+ arrival date: 2028-04-13T05:36:51.471
+ thrust profile: [0.280290649806047 -0.12488995188909728 -0.11402432052516676; 0.12171316420157247 0.011436581471482457 -0.12895287605587377; 0.07732414462762324 0.025539849768265618 -0.13014760643886694; 0.06456427687667986 0.031421905703958836 -0.14511762095488373; 0.039228956465371945 0.02433792323780781 -0.11369651734842279; 0.03482875002034865 0.025394606976279495 -0.12264827481931166; 0.04110276341884235 0.035166916687736686 -0.16356701960364758; 0.038083769515053545 0.021949121732705718 -0.12885478919146476; 0.034882603645334354 0.022934214177575487 -0.1260741304128094; 0.01876958599778977 0.014457667881396546 -0.0794177672406127; 0.011392672010989056 0.009142618585964329 -0.05259407368274517; 3.915568725144903e-5 0.00034480232861923405 0.0006949744030253333; 0.0005926925666287001 0.0011739029132759294 0.0005675993515417187; -0.00042482696771877247 -6.66640795729377e-5 0.0023582597583970393; -0.0005262865817308389 -0.0003416381351949329 0.002647870658773955; 3.016719516657282e-5 -0.0010490430162301812 -0.0005193704966844666; -0.0007688704539470818 0.002465456280783526 0.0005845278392658443; -0.004978466049011773 -5.943719111382043e-5 -0.0005657636337043203; -0.0007501885474735961 -0.0011072462302815153 0.004947488389843185; 0.0016531457096457276 -0.003307102320763475 -0.001237945336796103] %
+
+Mass Used: 104.82771845382103 kg
+Launch C3: 97.33981412508763 km²/s²
+||V∞_in||: 0.00015709220828983986 km/s
diff --git a/archive/ES_0.5765836312966115 b/archive/ES_0.5765836312966115
new file mode 100644
index 0000000..9240de6
--- /dev/null
+++ b/archive/ES_0.5765836312966115
@@ -0,0 +1,22 @@
+archive/ES_0.5765836312966115---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T03:49:51.092
+Launch V∞: [5.751134779267264, -8.028294846661213, -1.0900707028612469] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0018074980059926671, -0.0011556140252195458, 0.0009838693500791383] km/s
+ V∞_out: [-0.001210071766492699, 0.001699758998495142, -0.0011043343359615257] km/s
+ time of flight: 1.5439443551658192e8 seconds
+ arrival date: 2028-03-16T03:10:26.092
+ thrust profile: [0.25484914484934185 -0.13746392918005274 -0.12640063517473774; 0.07858672149699701 -0.00028334383456161494 -0.09993086740754477; 0.09383959095496396 0.018544055327075083 -0.19259808632299022; 0.07945605228188134 0.02564722033281681 -0.22210367553466387; 0.05963899693400463 0.024664198569936232 -0.2085507910733451; 0.042852278272896824 0.021128747838858385 -0.17956725768355458; 0.026475047571825082 0.014654814266662033 -0.12579221844658348; 0.009046808386121166 0.005167837660085957 -0.04746910109168075; 0.0029247082145212933 0.0017751136253506656 -0.019130264560634526; 0.0026753089237588606 0.002078703677906764 -0.019515212090619516; 0.0021718347185379376 0.001977732654366197 -0.017550601464488516; -0.0009186848315473907 -0.0013938908541175543 0.002732335938142474; -0.001255330470289598 -0.0002556155177867056 0.0034971856444814143; 0.003205763078244553 0.0012951353263205517 0.004045906473103414; 0.0003072579407529161 -0.006250392379971655 -0.0001265464688340406; 0.00010541864960346694 7.026082807057085e-5 -0.0004754711020429834; -0.0050648521457413885 0.0011321845162737027 0.0032794890625814947; -0.0011639686476810174 -0.003028153330454662 0.006703788667439405; -0.0010647739576719072 0.0058117118862871355 0.003922062410676307; -0.00046764342467400495 0.0004970882868858336 0.00043095918020826635] %
+
+Mass Used: 96.82984924585799 kg
+Launch C3: 98.71732353146092 km²/s²
+||V∞_in||: 0.002360188915103351 km/s
diff --git a/archive/ES_0.5765866860154715 b/archive/ES_0.5765866860154715
new file mode 100644
index 0000000..581a53b
--- /dev/null
+++ b/archive/ES_0.5765866860154715
@@ -0,0 +1,22 @@
+archive/ES_0.5765866860154715---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-07T05:44:16.338
+Launch V∞: [6.251788204724815, -7.952459961293305, 0.12447828333556127] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8756651617763038e-6, -1.1645376725119282e-6, 7.673259415377204e-7] km/s
+ V∞_out: [-8.264871580654765e-7, 1.8780556996738649e-6, -1.1164930532058143e-6] km/s
+ time of flight: 1.8056720048357582e8 seconds
+ arrival date: 2029-01-25T03:17:36.338
+ thrust profile: [0.08364529623247598 -0.03840692562005442 -0.04491750451280783; 0.026730327919489892 -0.0041190678172986755 -0.04514848676152181; 0.021530197479120935 -0.003289006486758767 -0.062176229612947755; 0.016667212026538644 -0.003597917260590619 -0.06423597677806316; 0.01702421025810688 -0.005223207547535032 -0.08087285152444403; 0.011747901478544442 -0.004227676260266376 -0.06508255681444254; 0.017058252720700447 -0.007888190206629666 -0.10327856559219219; 0.014648343592666748 -0.0079134643571973 -0.09411568962894719; 0.024087415186466152 -0.01196112431792353 -0.1518922946256035; 0.0339013932746406 -0.0255689214773916 -0.22682234234377072; 0.003406941284632415 -0.002296454660454965 -0.024379387335030003; 0.00015108784429228677 0.00015452107259769285 -0.0006549470186123287; -3.0269149714549126e-6 0.00030623624480393996 -0.0011686032752905653; 0.00020564323193064758 -5.733851643281113e-5 -0.00039687998160512774; 0.0002579694485170279 0.0005731068505990453 0.0005293325499666453; -0.0006953745318426922 0.0002777493201572389 -0.00023570481164811167; -0.0002458967064193549 0.00014452977296441699 0.000595461296313574; -0.00011570096772836876 -0.0003212608611051738 0.0006305582981858433; -0.00014834889010926507 0.0002118491319052627 0.0004642277022704265; 2.3796912148285154e-5 1.7603435499634714e-6 -7.800225841518376e-5] %
+
+Mass Used: 75.68964180961575 kg
+Launch C3: 102.3419700357316 km²/s²
+||V∞_in||: 2.337318311731968e-6 km/s
diff --git a/archive/ES_0.5766322661729798 b/archive/ES_0.5766322661729798
new file mode 100644
index 0000000..839781e
--- /dev/null
+++ b/archive/ES_0.5766322661729798
@@ -0,0 +1,22 @@
+archive/ES_0.5766322661729798---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T10:25:27.652
+Launch V∞: [7.838813164583021, -6.411238865714715, -0.18852268015515772] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7824842789874839e-9, 1.1994039418254588e-9, 3.0510384764572734e-10] km/s
+ V∞_out: [1.4697593055475836e-9, -1.3533683566130182e-9, -1.130733887736558e-9] km/s
+ time of flight: 1.8427891992107233e8 seconds
+ arrival date: 2030-03-25T07:00:46.652
+ thrust profile: [0.18563617864596507 -0.029065415131129535 -0.08750594194930328; 0.026678911710761238 0.0037917594324174894 -0.044824078039647886; 0.029532039095451795 0.0046218151964333406 -0.08556164814337842; 0.02180174006775716 0.0025512810992776285 -0.08666385915106257; 0.018623262796173184 0.0008759545543265326 -0.09048121620121097; 0.022865740048742117 0.0003990348587723836 -0.1269723107574868; 0.017805656990545295 -0.001971257838934461 -0.11040686061620823; 0.012562714043172789 -0.0019300770457087435 -0.08333457978872752; 0.008125079742760586 -0.001681741464361421 -0.056382591237112395; 0.0038789711123494767 -0.0008748305145519217 -0.026420739943955086; 0.0009798542297003857 0.00012592166501594984 -0.0031421825097508412; 0.0004797696449568462 -0.0008028759212027538 0.0011917542027088132; -0.0005235236505103491 0.0005922130896867977 0.002191011070178695; 0.006713314782796293 0.003268216262666313 -0.0018817935290905926; 0.00018082914926806094 3.493521326039734e-5 -0.004630609586533967; 0.000961711075718014 -0.000966099065993955 -0.0011873745330336469; -0.004975669851709692 -7.224070230624075e-5 0.007257895034717401; 0.0031737686030454708 -0.01255301231480705 -0.0058485752655750515; -0.004340612949544009 0.007546633071293954 0.004721457659784723; 0.01565807526966259 0.0043009490156438665 0.007120201017667754] %
+
+Mass Used: 74.31629806517049 kg
+Launch C3: 102.58651642342386 km²/s²
+||V∞_in||: 2.1700019304950414e-9 km/s
diff --git a/archive/ES_0.5766584452232547 b/archive/ES_0.5766584452232547
new file mode 100644
index 0000000..bff3f5f
--- /dev/null
+++ b/archive/ES_0.5766584452232547
@@ -0,0 +1,22 @@
+archive/ES_0.5766584452232547---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T01:56:19.968
+Launch V∞: [6.424551200684696, -7.83528038234547, -1.2945404002022254] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.22743897352488e-9, -2.317691981666675e-9, 5.5511701145260724e-9] km/s
+ V∞_out: [2.2394873760942992e-9, -4.920078690785877e-9, -6.8876791881917284e-9] km/s
+ time of flight: 1.8749577776778352e8 seconds
+ arrival date: 2029-04-17T04:05:56.968
+ thrust profile: [0.037478600484937695 -0.013983452693735375 -0.020476035608048837; 0.006844711637897849 -3.9216256058135915e-6 -0.012799863679368424; 0.01400115833635656 0.000505253657017574 -0.04089617695125152; 0.04109764308948508 0.0015887729662368236 -0.16653760624398728; 0.03115616531444308 -0.00010446595767747311 -0.16002049161141685; 0.02949816092964603 -0.001733323196325929 -0.1798641625497236; 0.013996415688126259 -0.0016438983048655143 -0.09779762765836754; 0.00399976744210798 -0.0009680046842079922 -0.03455759093168781; 0.005505015851945095 -0.001232949009433653 -0.04632850598926733; 0.0036299112703631784 0.0025066657324508313 -0.006611823063018733; -0.0002921905813248036 0.0015142463080636615 -0.004246466835035428; 0.0014710676636012386 -0.0014895450761513093 0.0002908249936069934; 0.006288765963940194 1.1868502632520676e-5 -0.0019034492620668352; -0.0006503579592178307 0.0017844137578598008 7.572362527172782e-5; 0.00040836187753396605 0.001850978593771911 -0.0024500129033471277; -0.00037435102258493987 -0.007738918083420892 -0.0010297472530692905; 0.0002618421250341189 -0.0010812231871758949 0.001887898238329965; -0.005738333018577778 0.005758009722464654 0.001366806997772153; -0.003435309709578481 -0.0020330823965693514 0.0027682978984491214; -0.0070348240771362595 -0.000540833048019083 0.006466709004327628] %
+
+Mass Used: 64.10470148079821 kg
+Launch C3: 104.34231164794268 km²/s²
+||V∞_in||: 8.658416825913732e-9 km/s
diff --git a/archive/ES_0.5766616071211349 b/archive/ES_0.5766616071211349
new file mode 100644
index 0000000..b6505c5
--- /dev/null
+++ b/archive/ES_0.5766616071211349
@@ -0,0 +1,22 @@
+archive/ES_0.5766616071211349---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T11:10:42.852
+Launch V∞: [7.248908454896426, -6.786768035597242, -0.5042391273881826] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.099806621680696e-8, -1.2729246826967288e-8, -2.2084227596342646e-9] km/s
+ V∞_out: [-2.718249578053695e-8, 1.8313614566879868e-8, -9.696444998610364e-9] km/s
+ time of flight: 1.510156855057173e8 seconds
+ arrival date: 2029-02-20T07:58:47.852
+ thrust profile: [0.2626883654066734 -0.07518426651831761 -0.11544233053422571; 0.05471625469158579 0.010017865760765498 -0.067471557037214; 0.057548981286624126 0.021741373675885304 -0.11565240959473719; 0.07312359441881629 0.03607323953328387 -0.2011548997433796; 0.05212151682611593 0.029875561270225996 -0.18062545509302474; 0.05491930732820224 0.03467157242940736 -0.22569712955466356; 0.018743616703864718 0.012961482211092975 -0.09086499037096761; 0.020390170272158045 0.013948302366650686 -0.10929090317577826; 0.00697400630952634 0.00857428952226974 -0.04118967727964753; 0.003402698008226913 0.0014731301070653581 -0.036126224886880956; 0.010245982767098018 0.006262860016804357 -0.027780247504308003; 0.003446028084981939 0.00281621182285052 -0.03581711381084102; 0.002373431832637456 0.000871062933339667 -0.003045191131432417; -0.012449427105345344 -0.012059028480140876 -0.005748354858332773; 0.0023142299553870847 0.002117620026759534 0.006367489976957175; -0.0027046488849396776 -0.005779816828306585 0.002750655401438703; -0.0006795227077711909 0.00044365738354759437 -0.0032227006007733866; 0.0005691292957381113 0.009382092099776758 -0.007725383495818211; 0.004295393289598482 0.016099669022476157 -0.002690453010467714; 0.009542669786575862 -0.015206858158831256 -0.010529696631340646] %
+
+Mass Used: 96.08182599262591 kg
+Launch C3: 98.86115125406253 km²/s²
+||V∞_in||: 3.3582599140755566e-8 km/s
diff --git a/archive/ES_0.5767145867470249 b/archive/ES_0.5767145867470249
new file mode 100644
index 0000000..188c501
--- /dev/null
+++ b/archive/ES_0.5767145867470249
@@ -0,0 +1,22 @@
+archive/ES_0.5767145867470249---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T03:42:15.543
+Launch V∞: [7.124014684761835, -6.902251308239345, -0.6775453382286893] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.055705404979167e-6, 4.328262628705076e-6, -2.1654383324715553e-5] km/s
+ V∞_out: [-1.0130749056481428e-5, 1.8821304728611747e-5, -6.330393093633221e-6] km/s
+ time of flight: 1.438954606865277e8 seconds
+ arrival date: 2028-11-28T14:39:55.543
+ thrust profile: [0.3464772261242911 -0.11152859444207655 -0.1595874875760051; 0.06212007156522465 0.008946452501078825 -0.07834924699140919; 0.06900452871034124 0.02394390483044 -0.1413833820659685; 0.07591871939680561 0.03618334445148354 -0.21055342450438702; 0.0547286082441508 0.030678288237697946 -0.19063817235192204; 0.04138267657004415 0.025673315832520617 -0.17185991029625208; 0.05618096095368502 0.0384291775353011 -0.2622663194851901; 0.012568148693961683 0.008445376060242047 -0.07110982776014728; 0.009494675590206033 0.00670385508622912 -0.05683516980557068; 0.0001404645989853486 0.000112493112362036 -0.0010710172023178195; 5.9150554643178175e-5 1.0505919137911054e-6 -0.0008198194867456435; 0.0009965870750012172 0.0007300048942830246 -0.0068210375370843955; -0.00015433638405442767 -4.438668979260097e-6 -0.000710102630252795; -0.00027458318134658115 0.0006797313650552801 -0.0008061671714872265; 0.00014092514233475148 0.00011112781296551471 -0.00043876606546616194; -3.9003258753383255e-5 0.00014952703134215738 -0.000596041455432951; -0.00016043760561049118 1.040724064109872e-5 0.0002387444515402717; 4.8511879216128013e-5 0.00023881255576534973 0.0004974792470229361; -0.0007973202683694014 -0.0007132864549811856 -0.00029033326021215807; -7.165519275854383e-5 9.534501262708139e-5 -0.0005345083300059498] %
+
+Mass Used: 96.19861599399064 kg
+Launch C3: 98.85172603614944 km²/s²
+||V∞_in||: 2.2293126969511993e-5 km/s
diff --git a/archive/ES_0.5767303152120551 b/archive/ES_0.5767303152120551
new file mode 100644
index 0000000..1a439ce
--- /dev/null
+++ b/archive/ES_0.5767303152120551
@@ -0,0 +1,22 @@
+archive/ES_0.5767303152120551---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-23T21:26:48.233
+Launch V∞: [8.002700596979142, -6.35572538114411, -0.5640209159246237] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.33618486114005e-5, -6.237003311170594e-5, 4.840443684653385e-5] km/s
+ V∞_out: [-1.3784232424960724e-5, -0.00010676458012008746, 5.0849660517546795e-6] km/s
+ time of flight: 1.8749577787476552e8 seconds
+ arrival date: 2030-05-02T23:36:25.233
+ thrust profile: [0.05209038037976903 -0.006877713496350635 -0.02468233653274839; 0.02300247047677579 0.00348990697492581 -0.0376968268461005; 0.031323969130221355 0.007122142908652726 -0.08478505300280852; 0.020897629015503887 0.003443808909719641 -0.07907354279672728; 0.019413559185173016 0.0024769490183649268 -0.08635773456232677; 0.015072103266487835 0.000686414957836292 -0.0778138934244465; 0.011939784856200314 -0.00010982505694444354 -0.06864561162325479; 0.018009744700785334 -0.0015076435036985448 -0.11057051367734431; 0.006029820511940346 -0.000552266215160258 -0.03992823228329067; 0.00911409967143081 -0.0049176274879296515 -0.052049758810716044; 0.006544288349302619 -0.0025107405127612063 -0.056985675999745904; 0.0025160925376519682 -0.0012165865891074629 -0.0027016736078209164; 0.0028084694398405343 -0.0017424161057214387 -0.0070056374237657155; -0.002774508954365011 0.0015550455166730753 -0.001953704133520805; -0.0008272908806555121 0.006719086895014051 -0.002559846976503951; -0.0008932771256408121 -0.00039059683937832525 -0.00021588198210472503; -0.0005553868620369688 0.0035695120643965167 0.0003804825170363431; -0.00013220136845832234 0.0023906559265658186 -0.003098786397368047; -0.007819776338498471 -0.007064958190562006 -0.004552075111878789; -0.001703387100923326 0.00018773535123994258 0.009329568522799871] %
+
+Mass Used: 61.77197531983802 kg
+Launch C3: 104.75658155901023 km²/s²
+||V∞_in||: 0.00010777277656471241 km/s
diff --git a/archive/ES_0.5767446259035398 b/archive/ES_0.5767446259035398
new file mode 100644
index 0000000..37948fe
--- /dev/null
+++ b/archive/ES_0.5767446259035398
@@ -0,0 +1,22 @@
+archive/ES_0.5767446259035398---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T11:51:41.915
+Launch V∞: [7.125334602147586, -6.869762474522889, -0.39109569723947324] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9632861048728957e-6, 5.055366915356113e-6, 2.5587292451434987e-6] km/s
+ V∞_out: [4.1461592169126785e-6, -3.6736930357089106e-6, -2.295150479462717e-6] km/s
+ time of flight: 1.4484742582631603e8 seconds
+ arrival date: 2028-12-08T23:15:26.915
+ thrust profile: [0.308115446627536 -0.09236961404997086 -0.13015089251758405; 0.12741482109924557 0.023432507616421124 -0.14287083393645256; 0.09992455002923317 0.04061015561654699 -0.18192433519740164; 0.06920943873628539 0.0377954615487795 -0.17444978126529065; 0.057217005934762116 0.037483288455303715 -0.17943217151301197; 0.060501328512777425 0.04387797052674738 -0.2228153577037854; 0.035372329063942665 0.02838524044058824 -0.15055520195435812; 0.024354053428925628 0.02082486887599714 -0.1243595453773856; 0.007606397525907634 0.008225648073919732 -0.04207679646994979; 0.0023427060093914515 0.0032867749583691476 -0.017311458893910496; 0.0014183012742549188 -0.0005659185417798109 -0.0077622853744848865; 0.001267064243358611 0.0020402124167391506 -0.003270909111977578; -0.0002247917847935959 -0.00035478789503518937 0.00010153684293553262; 0.0012430782342785593 0.0009351059086892301 -0.0019639192611195892; -0.0018232462215655707 -0.00019034108193607708 -0.002148063093376152; -0.0005935369412636207 -0.0011979178993481187 0.000879975001185409; 6.029197354152612e-7 -5.830178178232808e-5 0.0007544973314945859; -3.618810984844802e-5 -0.0006653648207703376 -0.00019251347012592653; -0.0012738148962425256 -0.0021176928940366928 0.0021601276821753357; -0.000430518235547128 9.687727593198406e-5 0.0018706924073005908] %
+
+Mass Used: 100.51964817640783 kg
+Launch C3: 98.11698549332377 km²/s²
+||V∞_in||: 5.9965258548943805e-6 km/s
diff --git a/archive/ES_0.576789210552565 b/archive/ES_0.576789210552565
new file mode 100644
index 0000000..ea98f96
--- /dev/null
+++ b/archive/ES_0.576789210552565
@@ -0,0 +1,22 @@
+archive/ES_0.576789210552565---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T22:40:42.570
+Launch V∞: [5.655220493477168, -7.919093239088647, -0.23538764141179888] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.07158577113841531, 0.05067748735863639, 0.07186073567636458] km/s
+ V∞_out: [-0.04809871360450847, -0.08204923497633386, 0.059181977349545015] km/s
+ time of flight: 1.562245286327019e8 seconds
+ arrival date: 2028-04-05T02:22:50.570
+ thrust profile: [0.4692986983861711 -0.2281960678283916 -0.18539357389116815; 0.1559165801894257 0.007979400591372162 -0.16395544573738285; 0.08033071346017437 0.02205838562378543 -0.13734060267469073; 0.11428215011305215 0.04753349957369781 -0.25369819594884646; 0.038429408105217736 0.020023343933467934 -0.11144798693075056; 0.03178526322512659 0.019198629356235085 -0.10876223102043968; 0.017340300137143154 0.011730617411764717 -0.06863846462702188; 0.009609028392328026 0.006773065514638371 -0.04360949874478708; 0.043240864811353766 0.030732865175120767 -0.1916042350955568; 0.004348693188981702 0.0015106541699960335 -0.019622385914368396; 0.010584191504406388 0.008877044989115573 -0.05828878033438822; 0.0005824529098916968 -0.0005051796227617262 -0.003191383453435241; -0.0016225373202359392 0.00039967758124382453 -0.002884050345825881; 0.002985217744817975 0.00423358251172116 -0.003497482045222584; 0.005064982717026835 -0.0017632772506325067 -0.002755859733053376; -0.0030214610051938233 -0.006255565658476241 -0.0023639340504342694; -0.012967388304478605 -0.0046526443601015155 -0.0024405794933268746; -0.004711297665720195 0.020856448371852708 -0.0063422527472941845; -0.009838046942102892 0.007240022703834117 0.007482798972253936; -0.0013557091053072253 -0.0015199042468401623 0.0010645392482758632] %
+
+Mass Used: 120.2184562224329 kg
+Launch C3: 94.74896390095307 km²/s²
+||V∞_in||: 0.11338737004805546 km/s
diff --git a/archive/ES_0.5768482545818697 b/archive/ES_0.5768482545818697
new file mode 100644
index 0000000..81c5535
--- /dev/null
+++ b/archive/ES_0.5768482545818697
@@ -0,0 +1,22 @@
+archive/ES_0.5768482545818697---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T16:51:19.163
+Launch V∞: [5.353629345075889, -8.169670282581006, -0.2123418401368876] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0024564581812723083, -0.0015446678158901458, 0.001314003777975286] km/s
+ V∞_out: [-0.0016288013678334686, 0.0023181419777570647, -0.0014962464641808213] km/s
+ time of flight: 1.5117348755134055e8 seconds
+ arrival date: 2028-02-07T09:29:26.163
+ thrust profile: [0.3175208332953427 -0.16057671442053803 -0.1314543106019404; 0.2927203179845219 0.008448854299621052 -0.30246305490506414; 0.19245383549878006 0.05200957168078672 -0.32259326227454527; 0.07791061176061728 0.032899318744544076 -0.16770636096672686; 0.04938584004938278 0.02505216944501013 -0.13190451105704296; 0.05259612812418258 0.03131171198892253 -0.16749890159106096; 0.027553905613602443 0.016944149648325264 -0.10374942519797324; 0.008875001091772708 0.005482291167483494 -0.03522772232274912; 0.000551496482533194 5.334707205233917e-5 -0.0045553733546818955; -0.0005716226228006896 -0.00037602847069727276 -0.001671607485372401; 0.0012863293388223178 0.0010528016417446408 -0.0033627928144353636; 0.0008694557023950457 0.0007247291081407285 -0.0024534101269397847; 0.0012588660861541248 -0.0055044631276092 -0.003583308039475397; -0.0002900890841067705 0.006259369511610165 -0.0032108812322794848; 0.0036701918618943855 0.003069801869123908 -0.018603137752298507; -0.005877313198339393 0.00946873418525659 -0.01015132997667399; 0.003554751861465767 0.0015567873417582333 0.0020067466051828893; 0.0016292636305296124 -0.0027373329284224738 -0.01721872993525626; 0.007126065313413237 0.0013775948873060826 -0.002510305014615118; 0.0017951796420625464 -0.0012161140280949924 0.00531914453816729] %
+
+Mass Used: 116.1982626510785 kg
+Launch C3: 95.44994874761763 km²/s²
+||V∞_in||: 0.0031854028609141125 km/s
diff --git a/archive/ES_0.5768695801599711 b/archive/ES_0.5768695801599711
new file mode 100644
index 0000000..b1f3f77
--- /dev/null
+++ b/archive/ES_0.5768695801599711
@@ -0,0 +1,22 @@
+archive/ES_0.5768695801599711---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T06:32:08.526
+Launch V∞: [7.093989181603212, -6.872175458149841, -0.8078062975111977] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.20310140356919e-6, 1.3779822700697695e-5, 7.5237529857585255e-6] km/s
+ V∞_out: [1.1469524277704442e-5, -1.0268252407552262e-5, -6.049789891310089e-6] km/s
+ time of flight: 1.4347038884158483e8 seconds
+ arrival date: 2028-11-22T19:25:16.526
+ thrust profile: [0.3549235980903419 -0.1169822839968642 -0.1560936927747519; 0.10851911738713717 0.016779731723403263 -0.1236756449381599; 0.11383858089995015 0.04156502563609204 -0.21018370151833973; 0.10053421619844567 0.049805464095768436 -0.2541065528974765; 0.07974431235169056 0.04695305125879458 -0.2529512387514522; 0.0443132992167911 0.02955913195044927 -0.16870790794235216; 0.01436028389496155 0.010578355571051816 -0.06449002002940725; 0.004273896169170683 0.0034120988689371034 -0.021737871066508846; 0.015842878214022426 0.013269975671091113 -0.08668269640339914; 0.002248535776136882 0.0018620296102921812 -0.012810001603594983; 0.0007317583306160663 0.000929209840657741 -0.006411636454965854; -0.00040736381185051563 0.0009737132144119554 -0.00317536650635474; 0.0006316335827501953 0.0005155397100697337 -0.002845609815150802; -0.00015267104353474257 0.000280742729156201 -0.001331823076001895; 0.00024457269153725154 0.00010660251744824 -0.0020130525568481687; -0.00029841641186629684 -0.00016494903541737298 0.0008947098680828932; -0.00044665704646566816 -0.0003668149641610555 -0.00036932921814967264; -0.0008784586438564147 -0.0010330643244500248 0.0003697892068061175; -0.003912511587303246 0.002036825506593764 -0.0014850766315550614; -7.03865632183993e-6 0.00016093470008243967 0.0006297994705589064] %
+
+Mass Used: 100.15767405813813 kg
+Launch C3: 98.20402905059913 km²/s²
+||V∞_in||: 1.6539729044612476e-5 km/s
diff --git a/archive/ES_0.5768833741605505 b/archive/ES_0.5768833741605505
new file mode 100644
index 0000000..f868395
--- /dev/null
+++ b/archive/ES_0.5768833741605505
@@ -0,0 +1,22 @@
+archive/ES_0.5768833741605505---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T05:31:47.914
+Launch V∞: [7.112738131103636, -6.771463466352285, -0.3970837471260038] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1472896313481752e-6, -1.9785882624090623e-6, 3.261151501075567e-6] km/s
+ V∞_out: [1.8158502925495382e-6, 3.540773895072426e-6, 1.0807162343267527e-7] km/s
+ time of flight: 1.440644760029475e8 seconds
+ arrival date: 2028-11-28T15:26:23.914
+ thrust profile: [0.473258815114833 -0.14726539394743712 -0.20028319113340123; 0.1210517638903837 0.021521573576742937 -0.14102519012635334; 0.09928835722350833 0.03990701332492115 -0.18712635773950265; 0.07345334944081001 0.04005658771603728 -0.19089364013118082; 0.09065884502450576 0.058750946774750804 -0.28708281935843094; 0.05594561855637122 0.04049343044189724 -0.2146423636342483; 0.02348116342490215 0.01818400272072808 -0.1071524830775642; 0.00704476054547139 0.005636541437189884 -0.03601534331728437; 0.00363808012126273 0.003269591703594971 -0.021168433528441718; 0.007024619774040911 0.006397122310182833 -0.0385900723111519; 0.0011961152508829795 0.0006557570832086735 -0.005591766192549915; 0.00013663299878531544 6.296156330572894e-5 -0.0009523858161860187; 0.0009279183106196299 0.0011310854658555542 -0.00033297715880957224; 0.00048717769545463186 0.0002984588961007232 3.7665556230494755e-5; 0.0028385899431853665 0.0010013406228840632 0.00041119587338130336; 0.0017453366125546668 -0.0008146224550687209 -0.0008537755941023094; 0.0010518384055008827 -0.0005042543115473132 0.001197009096955219; 3.116975273465148e-5 0.00016059729380914786 6.991613109661701e-5; -0.0004932736163218114 0.0018286273485402286 -0.0026827581689271044; 0.00045601470416463055 0.0015072557361469644 -0.001912017813970537] %
+
+Mass Used: 109.52222243712822 kg
+Launch C3: 96.60143670003096 km²/s²
+||V∞_in||: 3.983239149650617e-6 km/s
diff --git a/archive/ES_0.5769144493138458 b/archive/ES_0.5769144493138458
new file mode 100644
index 0000000..5fc2e27
--- /dev/null
+++ b/archive/ES_0.5769144493138458
@@ -0,0 +1,22 @@
+archive/ES_0.5769144493138458---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T00:46:25.005
+Launch V∞: [5.4172467517750915, -8.262154173475349, -0.6712278534146192] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002228224816076473, -0.01402033663902155, 0.019112971183283388] km/s
+ V∞_out: [-0.01679228300619001, -0.013271852192861316, -0.010426912171980027] km/s
+ time of flight: 1.4772735965810323e8 seconds
+ arrival date: 2027-12-30T20:09:04.005
+ thrust profile: [0.3298817723621482 -0.19350765619182891 -0.16860373467488507; 0.07342892596016855 -0.005551660091657107 -0.09205811206089805; 0.10223851496123047 0.011217381106578979 -0.1997517954310274; 0.09962239472101252 0.02055603581471682 -0.26019085701169775; 0.0753478543011403 0.019377963025590996 -0.24309360755131548; 0.04985285928388416 0.01604462092368511 -0.18953234969489935; 0.034418467948605286 0.012390011262097126 -0.14962296370455183; 0.002635732154815597 0.0009074778259769176 -0.013862215953498676; 0.003654033491792316 0.0012814433708845858 -0.021476790783429966; 0.0004534756537510036 0.000352994381936587 -0.003586775542370559; 0.0020121496463371617 0.0008538673931655586 -0.013045420006408358; 0.00032869668686712303 0.0008060138502114358 -0.0013610836020559354; -0.0007252526159181973 0.0004552335694579739 0.00019133455765793918; -0.0003277125602148108 -0.00035318496319068084 -9.79580452355874e-5; -0.0038037430711971984 0.0006599403775860869 -0.0012064649019164829; 0.0002881197839373384 0.0013716998867559908 0.0030305190425359988; -0.0007351439924584252 -0.0008718351682623725 0.0011222657170544947; 1.2636081261777722e-5 -0.002091339716387115 -0.00085061366778709; -0.0015366739826907414 0.00030175493282076 -0.0008945385087036125; -0.0020572058737949907 0.00181562358482628 -0.0015833929943209332] %
+
+Mass Used: 101.04843627477476 kg
+Launch C3: 98.0603007870935 km²/s²
+||V∞_in||: 0.023808412226679256 km/s
diff --git a/archive/ES_0.5769745279801655 b/archive/ES_0.5769745279801655
new file mode 100644
index 0000000..31c3261
--- /dev/null
+++ b/archive/ES_0.5769745279801655
@@ -0,0 +1,22 @@
+archive/ES_0.5769745279801655---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T03:10:29.750
+Launch V∞: [7.466280144554578, -6.431440348748527, -0.3742427508818919] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.266419038824257e-5, 0.00012291427830545955, 0.00018762676824881744] km/s
+ V∞_out: [0.00020360068430754565, 2.1405707448215507e-5, -0.00010704548631743701] km/s
+ time of flight: 1.5347736392189083e8 seconds
+ arrival date: 2029-03-16T11:46:32.750
+ thrust profile: [0.30557729676430684 -0.07683434875872568 -0.11271003970162112; 0.12510213401059506 0.032882487401526744 -0.1275576460918545; 0.1234121009696693 0.06416797419184944 -0.20976866219729737; 0.1044079784909987 0.07274680786388257 -0.24720004211317428; 0.06671623448401129 0.05525857619191231 -0.20137097007627397; 0.028108766283757105 0.025123390449514133 -0.10261247566925412; 0.019443893996399227 0.014394324699732137 -0.08303135127925045; 0.010383661722305275 0.012150808899230725 -0.0644312827180298; 0.012830957583110808 0.0050292578675957 -0.02896268006860063; 0.006227149467502818 0.013476030706261114 -0.027936769273088517; 0.003283957952189606 0.009276232809738674 -0.022118594568160194; 0.014267339612611006 -0.0010382299336752542 -0.016768092028639367; 0.0018965707558500728 0.001458774004353191 -0.008329617092501783; -0.008896274917926689 0.007780770505741583 -0.004458963256702569; 0.009294356147390912 0.020238446810502582 0.0034394492015944206; -0.0057901195114746055 0.004046319392115206 -0.026374831069690453; 2.7116952235342866e-5 -0.0008935836118501763 0.00025060085448843153; 0.0011228322473837114 0.0026519624841256913 0.0003699310821022317; -0.004078196024559132 -0.00012763281699920757 -0.006364429065808556; -0.005360014140016898 0.009204776383233873 -0.005825750357516814] %
+
+Mass Used: 105.85215551729561 kg
+Launch C3: 97.24882179306815 km²/s²
+||V∞_in||: 0.00022666864209362257 km/s
diff --git a/archive/ES_0.5769770854858185 b/archive/ES_0.5769770854858185
new file mode 100644
index 0000000..6ff05a1
--- /dev/null
+++ b/archive/ES_0.5769770854858185
@@ -0,0 +1,22 @@
+archive/ES_0.5769770854858185---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T17:14:50.899
+Launch V∞: [6.670989337348345, -7.268914669631953, -1.3715015534449981] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005674618915212902, -0.0006077388649501395, -0.0005950593399689807] km/s
+ V∞_out: [0.0007305237111331013, 0.00014417319423227405, -0.0007015695217904603] km/s
+ time of flight: 1.8407839912485904e8 seconds
+ arrival date: 2029-02-25T06:08:09.899
+ thrust profile: [0.24258272616507587 -0.057845809821759527 -0.08932688022055392; 0.05660444165248956 0.01812157095656834 -0.0646315489023492; 0.06167501852919572 0.04052729739469253 -0.12329113742796366; 0.05845126413566273 0.05224444342472223 -0.15984649173522403; 0.03917371354512721 0.0439597244424287 -0.14009611102915343; 0.02775314548745039 0.03846105159431333 -0.13405406516908433; 0.02690044994174337 0.041468728752898414 -0.14442767684075614; 0.010631457281746626 0.017745194236608426 -0.066292506129259; 0.00432225392936888 0.008434789234811715 -0.03275329567160513; 0.0014819398625368554 0.004469716870477798 -0.015506185902513682; -8.209254790907073e-5 0.0021229699836824985 -0.004467010597295528; -0.001233497578072095 0.0012266243253032316 -0.0030866420892775082; 0.00038907963012704144 0.0011038063172399692 -0.005932721615393998; 0.0006688060660511275 -0.0005725173221269254 -4.859870642227133e-5; -9.77994068938548e-6 -0.0018952514593428226 -0.0029140659755852285; 0.0010232380592400427 -0.002758819689716938 0.0049718711885010205; 0.0034438478851688803 -0.0029878408813620995 0.0022895540690655233; 0.0019185098366269753 -0.0006896164650117467 -0.004936860870239208; 0.0015773843146247842 -0.006715981351073912 0.0017963957346452302; 0.0028916966317654607 -0.001238024130504008 -0.0025329290145687305] %
+
+Mass Used: 94.35522467382498 kg
+Launch C3: 99.22023572450797 km²/s²
+||V∞_in||: 0.0010224750091733898 km/s
diff --git a/archive/ES_0.5770195632344991 b/archive/ES_0.5770195632344991
new file mode 100644
index 0000000..7071e6f
--- /dev/null
+++ b/archive/ES_0.5770195632344991
@@ -0,0 +1,22 @@
+archive/ES_0.5770195632344991---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T07:16:31.508
+Launch V∞: [7.21928111246315, -6.874156103459543, -0.6205161206334633] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0007503494821299436, 0.012750672427418137, 0.0015392329989524641] km/s
+ V∞_out: [0.012263814520292519, -0.0023762593258246666, 0.0030727180617400257] km/s
+ time of flight: 1.4559469352315134e8 seconds
+ arrival date: 2028-12-18T10:14:44.508
+ thrust profile: [0.1896441515614203 -0.060985553307142955 -0.0903421799827972; 0.08687344778015436 0.012043586639397495 -0.1105970010295451; 0.09891822928706794 0.03373879576199671 -0.20500484372363786; 0.08836554645683996 0.040654986876498475 -0.24987709996846635; 0.06413811034309598 0.034195661027737974 -0.22877573253036376; 0.03926830850876006 0.02296596769852449 -0.1648571888339628; 0.02743734288361046 0.01703660487790584 -0.1283038953310707; 0.011407572564874669 0.006902067778553088 -0.06213798651448265; 0.006245102822155078 0.003996711433309749 -0.03722990648094295; 0.002455030626890259 0.0009342476131799282 -0.0058036516572305755; 0.0009347411398052544 0.0006043363832998879 -0.006645508027929314; 0.0005245868272523936 7.727888845075563e-5 -0.0021372171127253805; 4.601038465630635e-5 0.0002655081748087335 -0.0032081322047013945; -1.3627501100210802e-5 0.0006330212876922277 -0.003589915390407647; 0.007578734154347365 -0.0009395310996587289 -0.00011616882123028326; 0.005822775448037651 -0.001390836647677987 -0.002497863536357647; -0.0005507589625909273 0.003287613246064097 -0.0004761109755010663; 0.004743293782500385 0.004192462302904541 -0.018236494551291064; -0.008507882672260629 -0.002357422113900886 -0.007103143495542077; 0.00045982520142713633 -0.0006208699013394 0.0007044698645271505] %
+
+Mass Used: 91.27317777337976 kg
+Launch C3: 99.75708217146328 km²/s²
+||V∞_in||: 0.012865143214193846 km/s
diff --git a/archive/ES_0.5770730264153152 b/archive/ES_0.5770730264153152
new file mode 100644
index 0000000..01a7fc1
--- /dev/null
+++ b/archive/ES_0.5770730264153152
@@ -0,0 +1,22 @@
+archive/ES_0.5770730264153152---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T17:37:03.835
+Launch V∞: [6.515660754439322, -7.459592207050205, 0.10295621354469146] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.849594420615799e-7, 6.928564358691935e-8, -8.774899282477575e-8] km/s
+ V∞_out: [3.835197190359215e-7, -1.0267280030368137e-7, 4.92133791197557e-8] km/s
+ time of flight: 1.8749577787477854e8 seconds
+ arrival date: 2029-04-10T19:46:40.835
+ thrust profile: [0.21321839062568232 -0.052074720678013754 -0.07930876855344829; 0.058421771829746144 0.015468418083125188 -0.065674948138807; 0.051314568307385344 0.026865519653885714 -0.09948644996592453; 0.04566913975201841 0.03464353181144504 -0.13218385579256153; 0.047780822366686175 0.03882541078052401 -0.15458575435005145; 0.019285661698853318 0.02331658560628686 -0.10474810191987005; 0.010847268819098583 0.011848737928889654 -0.053851642752830615; 0.019049105961708505 0.019929703827443423 -0.10552106174149267; 0.009963997297703468 0.008351064380246995 -0.048212694007635074; 0.0026091180876109074 0.009223203741949503 -0.030414711233103034; 0.007837189209641892 0.007703555662243562 -0.005629623548856871; 0.004698510133808146 -0.0018374843182905492 -0.006386807317499979; 0.004135094908827331 0.0010992019232669223 -0.01599052774058085; -0.01257792082591665 -0.002869325264118274 -0.000695643413207693; -0.02197194606687742 -0.04099790036939363 0.0036270350518046376; -0.004785484328990099 -0.001179762507489742 0.004816188740103554; 0.015352182528933507 0.011668108329985872 2.0125694362636143e-5; -0.032831699947375226 0.0119045882048197 0.0391074092429139; -0.01779615397265593 0.04683616600203078 0.041373172908872075; -0.0061057151079989755 0.0009653371046211454 0.004307890041754626] %
+
+Mass Used: 100.94381697592871 kg
+Launch C3: 98.10995094433241 km²/s²
+||V∞_in||: 4.0086675863855194e-7 km/s
diff --git a/archive/ES_0.5771275028505299 b/archive/ES_0.5771275028505299
new file mode 100644
index 0000000..9bc6dd3
--- /dev/null
+++ b/archive/ES_0.5771275028505299
@@ -0,0 +1,22 @@
+archive/ES_0.5771275028505299---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T23:30:03.524
+Launch V∞: [5.722891777449792, -7.373526586942022, 0.07345461631368627] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.5379049419864335e-10, -4.4226095736919745e-9, -1.7364311666652383e-8] km/s
+ V∞_out: [7.597137085036591e-9, 1.0217688380945391e-8, 5.8170007627076866e-9] km/s
+ time of flight: 1.8259104623028976e8 seconds
+ arrival date: 2029-02-02T07:14:09.524
+ thrust profile: [0.7517199015328915 -0.1798060601310041 -0.13037209754832374; 0.3913066800106677 0.15103994781205893 -0.20584346779428075; 0.23638817786432273 0.1744982062769412 -0.20783615997604163; 0.12526785501640988 0.12856227651520388 -0.15973361905786612; 0.08943351278879547 0.11544441845274658 -0.15274994108485748; 0.014655236750632777 0.02263160985657913 -0.032591627492056775; 0.02423974107336843 0.04337286368864461 -0.0629178582536455; 0.006926938213376206 0.014029962897756878 -0.021937793243454518; 0.003279829481431591 0.007096536699478821 -0.011084897586496872; 0.0004197891272954209 0.0007646103935764342 -0.0021544547056840365; 0.001438014265795011 0.002777880273760231 -0.004558199830501244; -0.0001618194569365421 0.0005151377203656484 -0.0026635504039928476; 0.0006265223482160321 0.0020093599972911768 -0.0037133652969117536; -0.002291369991679759 0.0010589504735856877 -0.0009587547067970508; 0.001595128323450379 0.003934611794859521 -0.00189031283034795; 0.001176534864161478 -0.001301029303787735 0.0006782989003586331; 0.008192915198316615 0.0033466286369837625 -0.0032594730193370534; 0.007079458185901551 3.3379639208087875e-5 -0.0072412610506898175; 0.0001035161474744066 0.0007706522468152882 8.912486195304745e-5; 0.00032342036351858247 0.00014310126990238047 -0.0004483165508367033] %
+
+Mass Used: 165.08170212744517 kg
+Launch C3: 87.1257802054011 km²/s²
+||V∞_in||: 1.7922164010290086e-8 km/s
diff --git a/archive/ES_0.5772162306674139 b/archive/ES_0.5772162306674139
new file mode 100644
index 0000000..7ff6ef7
--- /dev/null
+++ b/archive/ES_0.5772162306674139
@@ -0,0 +1,22 @@
+archive/ES_0.5772162306674139---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T16:12:41.204
+Launch V∞: [7.126140224496407, -6.780885147701116, -0.5146094597058994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008778584922200341, 0.004106592559459971, 0.00032024964627310165] km/s
+ V∞_out: [-0.007751358124280316, -0.0038069010267254093, 0.004412975549011068] km/s
+ time of flight: 1.4826081528219748e8 seconds
+ arrival date: 2029-01-17T15:46:16.204
+ thrust profile: [0.36724912298758333 -0.10360937578579404 -0.15251532238104734; 0.12276435054464285 0.025513036766217224 -0.13666933691312194; 0.12261930836645976 0.05367690035251572 -0.22166574533329317; 0.1029604645062957 0.06039552188864228 -0.2555779226838804; 0.05369023030307042 0.036903495711433136 -0.16992068027428675; 0.024836258877571574 0.018905672581083777 -0.09979542826706986; 0.02655876636768434 0.0173897630952521 -0.11325617694424399; 0.02669670940826095 0.017795384208697914 -0.1224919501799886; 0.0042476749515242326 0.0042991038032866805 -0.021543193222624855; 0.008632817830444513 0.0037251029154261083 -0.031123363416962535; 0.0015962766587899993 0.00168496859412004 -0.010770482462478317; -0.000800855358917104 0.001644111325237531 -0.011573705296375521; 0.0032591458211778234 -0.0011671249216230718 0.002431704004095052; -0.001461236409682004 -0.002866032407404865 0.0016795674627904666; 0.002299414047847067 -0.003137458017263942 0.007923949927347932; 0.0010819873646423506 -0.012713497313868742 0.0029891535092272875; 0.006218365083273604 0.00907525480284782 0.005625405985010102; -0.0019562685944875847 -0.0031053585841865853 0.0030663179595712413; -0.003301297957537118 0.0008106315223686733 0.017780548912265208; 0.0006254466421147766 0.0017906494094620034 -0.008607931891837459] %
+
+Mass Used: 107.42751455312737 kg
+Launch C3: 97.02710078151809 km²/s²
+||V∞_in||: 0.009696917836180381 km/s
diff --git a/archive/ES_0.5773241512875309 b/archive/ES_0.5773241512875309
new file mode 100644
index 0000000..63bc26b
--- /dev/null
+++ b/archive/ES_0.5773241512875309
@@ -0,0 +1,22 @@
+archive/ES_0.5773241512875309---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-11T00:20:04.694
+Launch V∞: [6.376827981129698, -7.987684332544186, -0.35949289712342775] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.752434344307249e-8, -1.8972616984779326e-7, -8.707780350420615e-8] km/s
+ V∞_out: [7.399131888398589e-8, -1.1479238127619136e-7, 1.812144168872282e-7] km/s
+ time of flight: 1.8749577783987033e8 seconds
+ arrival date: 2029-04-19T02:29:41.694
+ thrust profile: [0.02434507571799376 -0.01023942890808691 -0.013975213348032279; 0.02153402676456671 -0.005182280117712088 -0.037857074152349776; 0.027639361076082496 -0.006148945972417159 -0.08476761617733067; 0.024423116671258724 -0.007632689536886656 -0.10293773004902701; 0.027548130189124973 -0.012572467616641473 -0.14042465443182084; 0.020483101626178283 -0.011466770230112486 -0.11988968375315054; 0.023161733790986065 -0.015299916976853397 -0.15299288188642302; 0.012045603762740166 -0.008528757887069615 -0.08514817230837217; 0.0064990456829590515 -0.005244601458874763 -0.04918684304588963; 0.0013428406735581924 -0.001215829851450943 -0.010845313061520048; 0.0005359725801413469 -0.0004950741212466127 -0.0038068097343352124; -3.198278681186182e-5 -0.00017554845192083006 -0.0011231358054633598; 0.0001209831819225011 -0.0002494392066183059 -0.0006811478747517851; 0.00014931546767194817 -2.6651561434265112e-5 -0.0008496199200605928; -0.0006372715240922928 -0.0005417936847092221 -0.0011330540137933706; 0.0005622940311139728 0.00039266973027464946 -0.00022905584009579765; 0.000506967554212504 -0.0009430757177605343 0.0003484295814324657; 0.00017357119026626994 0.00019423738201993673 0.00023551117609033317; -3.884931098588644e-6 -0.00012623116267524554 -0.00016031883080514875; -0.0006696021287221645 0.0006071065038458045 0.00035717756668032005] %
+
+Mass Used: 63.399927599945386 kg
+Launch C3: 104.5962712403727 km²/s²
+||V∞_in||: 2.3041172051836508e-7 km/s
diff --git a/archive/ES_0.5773345772413209 b/archive/ES_0.5773345772413209
new file mode 100644
index 0000000..3feba86
--- /dev/null
+++ b/archive/ES_0.5773345772413209
@@ -0,0 +1,22 @@
+archive/ES_0.5773345772413209---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:05:27.747
+Launch V∞: [7.1663622258556785, -6.887538246693052, -0.845962508149472] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.104691339971321e-6, 1.58100196320829e-6, -7.644721195764317e-6] km/s
+ V∞_out: [-3.386964909544034e-6, 6.724339369510388e-6, -2.3431447455356302e-6] km/s
+ time of flight: 1.4304062953214288e8 seconds
+ arrival date: 2028-11-17T21:35:56.747
+ thrust profile: [0.22948270654369343 -0.07660066537106386 -0.1036169183653586; 0.11617530099479674 0.016412711414974145 -0.1343202179729903; 0.11787735717323299 0.041350213850040486 -0.22167224859625898; 0.10049975590892925 0.04810656573394755 -0.2589655493070177; 0.0715632999335433 0.04049068475911515 -0.23146138840693387; 0.04500639932384675 0.02824656123658854 -0.1736639882009897; 0.02608550955947509 0.01759920771544608 -0.11671290799398591; 0.002125909532719348 0.0014398941689065675 -0.011417760281538665; 0.0019707903972038545 0.0018902223925832745 -0.012738563658808546; 0.0011315105802934028 0.0005860221738415377 -0.00715540344356185; 0.011790442488763738 0.008837553124428936 -0.06762215407676689; 0.0005194850894540858 0.0003958818767932153 -0.0030053218628605773; -0.00023345245112824824 0.00022613877361992566 -0.00041969336334630325; 0.0001600173251903969 7.050839167607219e-5 -0.0005969398282774136; -0.0002063563278557273 -2.76227636256774e-5 2.3260604467547567e-5; 2.6566944367861962e-5 2.3383981026535496e-5 -0.0006952514198407217; 0.00010104548390533648 4.315189112533499e-5 -0.0004150876178355998; -1.7101120886312175e-5 -2.6703178485528215e-5 3.1621879549936316e-5; 2.0493907891884768e-5 -5.762557589498112e-5 -0.0003341619577857248; 1.987303677949498e-5 0.0003578182103297853 -0.0009340768896530681] %
+
+Mass Used: 93.0786046822268 kg
+Launch C3: 99.5105832170253 km²/s²
+||V∞_in||: 7.884267393058427e-6 km/s
diff --git a/archive/ES_0.5774314404369079 b/archive/ES_0.5774314404369079
new file mode 100644
index 0000000..aa8dd51
--- /dev/null
+++ b/archive/ES_0.5774314404369079
@@ -0,0 +1,22 @@
+archive/ES_0.5774314404369079---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T01:10:40.104
+Launch V∞: [6.461238074029437, -7.108620132452109, 0.459089374215429] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3630641348643857e-7, -2.9520709241300314e-8, 3.829544065045821e-8] km/s
+ V∞_out: [-1.439462767581288e-7, 1.2596938012866112e-8, -1.6204323853495042e-8] km/s
+ time of flight: 1.8289398047429046e8 seconds
+ arrival date: 2029-02-04T21:03:40.104
+ thrust profile: [0.6605701398887707 -0.16586810151046058 -0.14755979965948; 0.2931556483170609 0.10410940909341045 -0.20336084581808225; 0.10940296450577926 0.07422356576079857 -0.13091243794821456; 0.06686143223161584 0.06296019347497353 -0.11343480416679944; 0.07709498542427089 0.09047650732058896 -0.1661498614197468; 0.04721803102994335 0.0657541095772458 -0.12679200144576303; 0.007399591610186525 0.012064366276913362 -0.025363115108085695; 0.007361302250718535 0.013636737382441904 -0.0293311596175181; 0.00355857212033679 0.007580545198679514 -0.016831544178097707; 0.00023367676151136361 0.00041362431066085253 -0.0010922677799684996; 8.978515587814613e-5 7.794927317624623e-5 -0.0003261283849251933; 9.257007244179513e-5 -1.26419851980466e-6 3.4204235246431086e-5; 5.6919165449196134e-5 -0.00029829338279418983 0.0005619894184157829; -0.00019289484710716787 -0.00011656423418305391 0.00041622911374847646; -0.00023172171828566147 -0.0002616607870168222 0.000582027848642873; 0.00010680420255458728 -0.00015363366825009558 0.00010759058725844564; -3.5658386584221764e-5 -0.0005703890911713593 0.0003622795832749733; -4.1157970476466156e-5 -0.00018717868679693787 0.000706372658407327; -6.800132037630013e-5 -0.00019923710887810887 0.00040048233526130696; 2.2763364551699726e-5 2.8278385327083815e-5 -0.00010911938307971457] %
+
+Mass Used: 134.14010981625916 kg
+Launch C3: 92.49084069030857 km²/s²
+||V∞_in||: 1.4462866730443907e-7 km/s
diff --git a/archive/ES_0.5775341209273406 b/archive/ES_0.5775341209273406
new file mode 100644
index 0000000..00f3944
--- /dev/null
+++ b/archive/ES_0.5775341209273406
@@ -0,0 +1,22 @@
+archive/ES_0.5775341209273406---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T01:16:08.511
+Launch V∞: [7.635262839365482, -5.409611029232033, 0.4046364389642043] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0240455680819866e-9, 2.1648419760310868e-9, -9.170489252121373e-9] km/s
+ V∞_out: [-2.9174877737248057e-9, 9.792134808189685e-9, -1.573985129495546e-9] km/s
+ time of flight: 1.874957778726442e8 seconds
+ arrival date: 2030-04-13T03:25:45.511
+ thrust profile: [1.0 0.0035893022619969614 -0.1651561585006746; 0.374885376037756 0.2633420557277807 -0.21424929521726113; 0.06401177339457152 0.08391924727905005 -0.08115788764166536; 0.033252559700974925 0.063080964447899 -0.06806226979419314; 0.03080952492088643 0.07903234203916688 -0.08931096494843634; 0.01707521088977216 0.06346300685369279 -0.07669903082957807; 0.008051450892909078 0.03656479286296215 -0.048854749960374075; 0.0016624686878718214 0.0190910979659264 -0.02841838337059824; 0.001709279522003028 0.011764341998676008 -0.016622366694089313; 0.002855642693835626 0.030620338711465765 -0.04648398001489753; -0.0001085277752472272 0.0007606705150887304 -0.0023593230156748876; 0.0007995895147305358 0.0002610742685858128 -0.0033842152949059394; -0.0005742950022782997 0.0009495652683215832 -0.00063123019892274; -0.0003694828184845677 -3.683076552888579e-5 7.557973562330694e-5; -0.0010627239446641974 0.0004040838374557191 -3.6652900750553166e-5; 0.0009410652831446545 -0.0010935517429365815 -0.003790325470915645; -0.00016486123565414738 0.0006761248788685795 7.2794181206611505e-6; 0.00099515178392657 -0.0015614912480970578 0.001127471172351186; 0.0017254077567218037 0.002709068691805362 -0.002713343772911438; 0.002723052541224371 3.979377486000075e-5 -0.0023470490464901784] %
+
+Mass Used: 162.06145330635263 kg
+Launch C3: 87.72486076152194 km²/s²
+||V∞_in||: 9.478031611572529e-9 km/s
diff --git a/archive/ES_0.577559872280828 b/archive/ES_0.577559872280828
new file mode 100644
index 0000000..c05b658
--- /dev/null
+++ b/archive/ES_0.577559872280828
@@ -0,0 +1,22 @@
+archive/ES_0.577559872280828---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T11:43:48.700
+Launch V∞: [7.305395002789839, -5.971512533896223, 0.15284791628050745] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6114251500088335e-9, 9.195067343037508e-9, 4.971667558721047e-10] km/s
+ V∞_out: [4.528972288765405e-9, -7.985051609002339e-9, -3.3048090070876487e-9] km/s
+ time of flight: 1.6954321310809904e8 seconds
+ arrival date: 2029-09-16T19:04:01.700
+ thrust profile: [0.9894742497943146 -0.11246628724649498 -0.1961989045704571; 0.15359489115608127 0.08320620752971242 -0.1092830546141439; 0.08155593671204288 0.07756072913692469 -0.10334766226711425; 0.05574406387620158 0.07168576184742918 -0.10166374612410224; 0.08484999935853527 0.1382754010758338 -0.19494962724403103; 0.04904589724037056 0.09632016809400998 -0.14851395686347693; 0.02063691496045599 0.048795280977318896 -0.08091754799174819; 0.015228689898639456 0.045251417124968746 -0.07696869056845136; 0.0013077590564928416 0.004218088826386367 -0.005462237923360098; 0.0064254061846179605 0.006574325745034581 -0.009273674903430769; -0.002052990315608372 0.006368227146119886 -0.011516726096625782; 0.004952233600391159 0.006986179456659721 -0.01799582324807504; 0.003067742261335937 -0.0009854161182724953 -0.006265909654392647; 0.007556073428686822 0.0037379047736767535 -0.0040784430035573855; 0.003536367112693267 -0.0014798194856606825 -0.0021505779393321354; 0.006462534201552958 -0.004389511475656057 0.000491691973575614; 0.010330469528026973 -0.01799868806841637 0.004924212823239282; 0.0008039118425260399 0.007428817578926331 -0.020055432239636274; 0.0015641075384589575 0.0006367068259981292 -0.0012479620318170204; -0.007624171008946997 0.023628632900506926 -0.0004875240303274025] %
+
+Mass Used: 154.35498097476238 kg
+Launch C3: 89.05112057477776 km²/s²
+||V∞_in||: 9.348429239194157e-9 km/s
diff --git a/archive/ES_0.577584359499576 b/archive/ES_0.577584359499576
new file mode 100644
index 0000000..4108f10
--- /dev/null
+++ b/archive/ES_0.577584359499576
@@ -0,0 +1,22 @@
+archive/ES_0.577584359499576---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T00:06:13.179
+Launch V∞: [5.998245304734321, -7.378584706957655, 0.26496074366731676] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.131520471915377e-6, -8.364490947368005e-6, -1.208509280456812e-5] km/s
+ V∞_out: [-1.4607714896005694e-5, -9.266149363715219e-6, -4.0473147959710965e-7] km/s
+ time of flight: 1.7497771143861127e8 seconds
+ arrival date: 2028-11-08T05:01:24.179
+ thrust profile: [0.842345469076848 -0.27321004362138634 -0.23088208960132; 0.10951898328260233 0.028725756140019987 -0.1000382586221823; 0.0627437199802525 0.034845747363970066 -0.09609987857500447; 0.04132035296922746 0.029888607745071186 -0.08751807491330418; 0.04954221061754866 0.04681867246007246 -0.13209266643908713; 0.051725509277994415 0.05619080462450957 -0.15859087507858816; 0.039507678731617674 0.04659049792755727 -0.14584255807556853; 0.021888500425856067 0.030459154181374116 -0.09478343266110777; 0.014618988619101839 0.021450525149495466 -0.07328426163330874; -0.0005172238771156315 -0.0013240248969193155 -0.00382686674116553; -0.001480975144179634 -0.0019010981691327516 0.004215289416996551; 0.0015522473181045927 0.0005815922772062901 -0.0025928358463085423; -0.00892118981133543 -0.019358210269189467 0.006022008407191835; -0.01606592374544557 0.013763578478826085 0.01771669144262029; -0.003923788737031056 -0.004288263877341772 0.01581486653353162; -0.0012446094765851477 0.0022313860272938843 0.008581462508087369; -0.0005902119312186514 0.0014291127457483868 -0.0049230494532581225; 0.0017004024705933479 -0.0007095714200601138 -0.0023422952802353465; 0.003538958816916145 0.0019416548251076735 -0.0007520096015699834; -0.026084654943608752 0.013262277994191633 0.03464531950314486] %
+
+Mass Used: 145.9745506958302 kg
+Launch C3: 90.49266320920145 km²/s²
+||V∞_in||: 1.730314546643572e-5 km/s
diff --git a/archive/ES_0.5777085429628662 b/archive/ES_0.5777085429628662
new file mode 100644
index 0000000..23f15ff
--- /dev/null
+++ b/archive/ES_0.5777085429628662
@@ -0,0 +1,22 @@
+archive/ES_0.5777085429628662---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T09:26:14.074
+Launch V∞: [5.504731602691218, -8.114149744012673, -0.47018869615718206] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0551544115213383e-7, -4.474803983248543e-8, 9.175978456741336e-8] km/s
+ V∞_out: [4.32555848084379e-8, -9.909741988131912e-8, -9.443110125501551e-8] km/s
+ time of flight: 1.4717544837988362e8 seconds
+ arrival date: 2027-12-21T19:30:22.074
+ thrust profile: [0.4089302843122936 -0.2245563023282151 -0.1860818657723212; 0.14174964686774932 -0.002501759732630137 -0.15637747785866046; 0.1013537706973907 0.02022658413713577 -0.1730636392852894; 0.0878074263033057 0.0294960872288172 -0.19793061053872335; 0.08492457000415173 0.03558242636042536 -0.235980341348188; 0.06352573913054264 0.031369211353349344 -0.21009026323618035; 0.045708828905209796 0.02500750417899341 -0.17429417128722616; 0.01136706061250275 0.006528045308029666 -0.04641032959403846; 0.0012129587612066644 0.0007725186365122311 -0.007508373163435617; 0.003334105481757678 0.0019810139705542158 -0.016437331617742676; 0.0007674642787471653 0.00043854178111350697 -0.005925621372322018; 0.001030826263048105 0.00034517251903053506 -0.005314106232430491; 0.0010279542807249535 0.0005475532090292094 -0.0062251062531271; 0.0008448573467994794 0.0006119969004793628 -0.00502266100645468; 0.0008577086513348417 -0.0001089271647403061 -0.001155826780127657; -0.0019042944540519982 -0.0023163665357023968 -0.0034018939692123267; -0.0024548742571310713 -0.0016407183681692427 -0.006405663480274074; 0.0005183446542673406 -0.0016810541011871441 -0.004532277373556258; 0.0017795326185629306 -8.976981266741309e-5 -0.0010556055549669641; 0.001677618003262586 -0.0016700520045241332 0.0019443810924388173] %
+
+Mass Used: 111.87828806379684 kg
+Launch C3: 96.36257349592236 km²/s²
+||V∞_in||: 1.4681877759413892e-7 km/s
diff --git a/archive/ES_0.5777150695242587 b/archive/ES_0.5777150695242587
new file mode 100644
index 0000000..7078dfb
--- /dev/null
+++ b/archive/ES_0.5777150695242587
@@ -0,0 +1,22 @@
+archive/ES_0.5777150695242587---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T04:22:54.820
+Launch V∞: [5.386225692680143, -8.341521721588707, -0.5433986289102647] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6971551378717623e-8, -2.5926665163322908e-8, -1.3249281845626406e-7] km/s
+ V∞_out: [9.332800563623528e-8, 8.553784956134192e-8, 4.3113001723804735e-8] km/s
+ time of flight: 1.5063719180159473e8 seconds
+ arrival date: 2028-02-04T16:02:45.820
+ thrust profile: [0.2970266676658988 -0.1720507212478156 -0.1614497819414192; 0.06143551569695807 -0.006178205696765045 -0.08436320210930696; 0.08195207998309896 0.006138127966386594 -0.17731092220295008; 0.06477222906496784 0.010699357162188849 -0.19074387772436363; 0.06100470098529294 0.014802810942996906 -0.22194934941424352; 0.03645708193211474 0.008374808097076195 -0.15598768968186427; 0.026025499567482555 0.007358831192416985 -0.12144736776441954; 0.023412322733217895 0.006773490193279738 -0.13784929770096274; 0.00471509386221182 0.0012540929416786873 -0.029181281460217208; 0.0028816453609062883 0.0007552079252482437 -0.018908710898262807; 0.00021338293192930326 1.568081827635809e-5 -0.0015955233755793898; 0.002270317216167384 0.0005764500800334825 -0.01789444287880591; -0.0006403201039275113 0.0007920166221317001 -0.0035117705843509405; 0.0003114040589013695 0.0004065792597965378 -0.0018092383645252996; 0.00016060317609176307 0.00013727963691880906 -0.0019023014475582157; 0.0004331112679887758 -0.00012500746531234562 -0.001259863001975568; -0.00014014832502942144 0.0005833736985125567 0.00048092158917138294; -0.000756210856833942 0.002059554991460392 -0.00020505000909028478; 0.0021041950211407832 0.0006252395735509342 -0.00015947256987926847; -0.00015160259020248175 -0.00014185420393770707 0.0008645915416136444] %
+
+Mass Used: 97.15603327923645 kg
+Launch C3: 98.88769391412548 km²/s²
+||V∞_in||: 1.3606826398971975e-7 km/s
diff --git a/archive/ES_0.5777345145141418 b/archive/ES_0.5777345145141418
new file mode 100644
index 0000000..102c414
--- /dev/null
+++ b/archive/ES_0.5777345145141418
@@ -0,0 +1,22 @@
+archive/ES_0.5777345145141418---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T07:38:09.479
+Launch V∞: [5.4625315939040835, -8.075379880568303, -0.2973155089196814] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.487813975775642e-7, 3.553584743902992e-7, 4.14931606010389e-6] km/s
+ V∞_out: [-2.880106598837235e-6, -2.758860059319697e-6, -1.3183230702339268e-6] km/s
+ time of flight: 1.5068414991911852e8 seconds
+ arrival date: 2028-02-01T08:20:38.479
+ thrust profile: [0.4705769850689393 -0.2505299882793712 -0.20736407816911348; 0.16321450429699585 -0.0017819291169695877 -0.18216853141012554; 0.11392384649899748 0.023008982415953765 -0.20191133776218362; 0.07272043812153893 0.024118637016752875 -0.17482781096656966; 0.052409840572605344 0.02198307677131216 -0.15597325782477953; 0.0387810928519708 0.018797262468086794 -0.1361255617272649; 0.03632484982623658 0.019873166942580903 -0.14583943093489735; 0.026980599591690684 0.015354669466988673 -0.11873147264073025; 0.011068174504321024 0.00635948516213665 -0.05508465709153981; 0.005206108078432032 0.003100613695562945 -0.028506045050917504; -0.0011051225221307057 0.0035858734331396386 -0.004080783976479215; 0.002095805177325039 -0.00020831425612053388 -0.009743765898316083; 0.003120067517561522 -0.0011362060266446965 0.0032631939035157194; 0.0029762511989863383 0.002945400495046346 0.001315841431757875; -0.0007557307984619158 0.0007387026999500041 0.003731167215715811; 0.009029776010566941 0.005791639232456061 -0.009682126776693195; 0.0036211786790365935 -0.009164185251914373 -0.0014993568483079923; 0.0058947869915904685 0.0017889851087971274 -0.0025041914474779204; -0.0017752411635328065 -0.0008787761699563244 -0.010932522986271433; -0.0004584826999333596 -0.003105528463490279 0.002703352224258641] %
+
+Mass Used: 119.04371943973001 kg
+Launch C3: 95.13940814173179 km²/s²
+||V∞_in||: 4.20050764006974e-6 km/s
diff --git a/archive/ES_0.5779334114636643 b/archive/ES_0.5779334114636643
new file mode 100644
index 0000000..1c6874b
--- /dev/null
+++ b/archive/ES_0.5779334114636643
@@ -0,0 +1,22 @@
+archive/ES_0.5779334114636643---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T05:24:56.210
+Launch V∞: [5.48226209342548, -8.245788453779376, -0.6730974341084995] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.53583531101056e-7, 1.4945904510256938e-7, -3.076254837315996e-7] km/s
+ V∞_out: [-1.40375315714438e-7, 3.2122204994127096e-7, 3.03974209530912e-7] km/s
+ time of flight: 1.4522984961814234e8 seconds
+ arrival date: 2027-11-30T03:02:25.210
+ thrust profile: [0.22801074617175354 -0.13135453462804478 -0.11124211313321576; 0.14646199733374052 -0.006516761005627313 -0.16594470914496431; 0.1394953694433651 0.022579855240543248 -0.2430242305366371; 0.11587252429619455 0.032929758439011254 -0.2682751833639643; 0.08690715795245113 0.03215699978162917 -0.24865635921335405; 0.053453892084254155 0.023219027372383048 -0.1819210834214092; 0.021983014705035903 0.01010467308013484 -0.08756738828809016; 0.010278522890106449 0.005798405984629936 -0.0470673033520897; 0.00494335922221816 0.0026770945663202057 -0.023647275882340817; 0.0008465433748267004 0.0006595793315299049 -0.0045257662788030575; -5.582026261285829e-5 0.000365005929802561 -0.000387039274238898; 0.0006416929065038687 0.0006463648828537263 -0.003734359141716774; 0.001098691894319395 0.00010867241233714994 -0.0008941147413659165; 5.110146790531227e-5 -7.550565951037526e-5 -0.00036507795539022635; -0.0009263439477809148 -0.00035257757895619263 0.0015913975755723817; 1.0854839094298304e-5 5.437014885418249e-5 -0.0003460060378407281; -0.0012861324291864517 0.0004672867337763997 0.00036484675851673596; 0.0005342959613859625 0.001781912427025356 -0.002076694790938352; 0.0005508167239156364 -0.0011564849119588382 -0.0029742150504830462; 7.020917205870903e-5 -0.0004399766685655571 -0.0003269451979891066] %
+
+Mass Used: 99.66481730005626 kg
+Launch C3: 98.50128504129464 km²/s²
+||V∞_in||: 4.919275941334903e-7 km/s
diff --git a/archive/ES_0.5779580914941217 b/archive/ES_0.5779580914941217
new file mode 100644
index 0000000..cc11855
--- /dev/null
+++ b/archive/ES_0.5779580914941217
@@ -0,0 +1,22 @@
+archive/ES_0.5779580914941217---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T15:21:31.524
+Launch V∞: [7.545969481776026, -6.662737467174882, -0.4247422920146118] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.616863588785436e-10, -4.816932764627425e-9, -4.795416448205371e-9] km/s
+ V∞_out: [-2.408640193771976e-9, 1.97846763981055e-9, 1.5332691683731103e-9] km/s
+ time of flight: 1.833068874763267e8 seconds
+ arrival date: 2030-03-14T05:56:18.524
+ thrust profile: [0.3668258739372811 -0.0063541564971028855 -0.15933218655639853; 0.03940261397673279 0.012724782494532795 -0.05808167140364784; 0.024197866887443513 0.011486216185384526 -0.06271811096715474; 0.028692448321624726 0.01634660470492564 -0.10469513908535337; 0.03651537684861081 0.02631476427455263 -0.1747535312616578; 0.02410721659018088 0.015946450399365347 -0.13486848445660501; 0.007164368802372435 0.003795214524546218 -0.04570318169532869; 0.007364399709076893 0.003841181297272933 -0.05118089524218437; 0.0016390087478267109 0.000983664214656465 -0.014452996769579146; 0.0015416750072032603 0.0005757930565221848 -0.014478455585134437; 0.0005525918862670029 0.0002718977796340697 -0.004639978653042129; -0.0008586065845127952 0.0014042665582918818 -0.004657620957360237; -0.0006056343547888221 -0.0007363684433129504 -0.0020786915003951556; 0.0009572818259306385 0.0006104784723388794 -0.003374250555024763; -0.0007163994110382054 0.0007794888441626815 -0.0032805611352019733; -0.0005256389960742736 0.0008075028752656862 -0.002807353342380308; 0.0018121591973184541 -0.001073031702892305 -0.0014550246542168138; -0.0027218373437141036 -8.992835200372117e-5 -0.0022768470604102864; 0.0007838153370939439 -0.0003738412284365635 0.0006936958185723399; -6.825838618342798e-5 -0.00028529510001221604 0.0007956464273295221] %
+
+Mass Used: 82.1186701288766 kg
+Launch C3: 101.51413199101692 km²/s²
+||V∞_in||: 6.851376763230671e-9 km/s
diff --git a/archive/ES_0.5781190822545484 b/archive/ES_0.5781190822545484
new file mode 100644
index 0000000..8045c1c
--- /dev/null
+++ b/archive/ES_0.5781190822545484
@@ -0,0 +1,22 @@
+archive/ES_0.5781190822545484---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T10:59:20.681
+Launch V∞: [5.4275795077733395, -8.109801231038988, -0.4496270917131541] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.872542709120703e-5, 0.01176185011093262, -0.004986338377967597] km/s
+ V∞_out: [-0.010317775231899199, -0.005859789324009306, 0.00499585803607725] km/s
+ time of flight: 1.480030373962817e8 seconds
+ arrival date: 2027-12-31T10:56:37.681
+ thrust profile: [0.4442539382714023 -0.2424233217283461 -0.19595954047011543; 0.15755591071548272 0.0004058227654861735 -0.16967320186263227; 0.14129171337315147 0.03147534550593458 -0.23453694086782287; 0.12263428297246795 0.04393903201083772 -0.2694647630578907; 0.0991898252963527 0.045123442723593754 -0.26756350524343575; 0.029115240324745544 0.014191258958603886 -0.09096176090968973; 0.02047200035988013 0.011104613064678383 -0.07500291679923542; 0.008313849198961774 0.003958953972141514 -0.03167257271830312; 0.005424539171251966 0.002855879644112415 -0.02349511550459703; 0.014518312092973589 0.009732656439320054 -0.07566434465601662; 0.001518674557131058 0.0007630237547718866 -0.008347520051701671; 0.002391665541397344 0.0011154644622969414 -0.0014470313818269812; 0.00115829871572965 -0.0004510116150790998 6.358582866033708e-5; -0.0031458508688788503 0.002199032348672318 0.00012679935334636728; -0.0016163493469181665 0.0001863936968656401 4.734611280334672e-5; -0.0004063876018352894 -0.0004466870478850403 0.002408967425563047; -0.00014488151591130258 -0.00017457469928453613 0.0027642165983525345; -0.004084277926123926 0.0010565026235668424 0.00014168958230655447; -0.005099355939444067 0.002179960012334628 0.008616440859169659; 0.002566683116567805 -0.0023614246835082058 0.012320845104037232] %
+
+Mass Used: 117.79924688667734 kg
+Launch C3: 95.429659841765 km²/s²
+||V∞_in||: 0.012775191333275591 km/s
diff --git a/archive/ES_0.5781806949142353 b/archive/ES_0.5781806949142353
new file mode 100644
index 0000000..f4c6827
--- /dev/null
+++ b/archive/ES_0.5781806949142353
@@ -0,0 +1,22 @@
+archive/ES_0.5781806949142353---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T10:06:54.206
+Launch V∞: [7.028025324805335, -6.752168250680654, -0.45925056880478815] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.706877336829979e-7, -1.099927853611227e-6, 1.770997234824527e-6] km/s
+ V∞_out: [9.111068795436716e-7, 1.9948643268734546e-6, 6.107984976192114e-8] km/s
+ time of flight: 1.4249851651318744e8 seconds
+ arrival date: 2028-11-09T17:02:10.206
+ thrust profile: [0.5914067514375786 -0.19754034595350353 -0.2517069266459555; 0.1875123964302083 0.029363193082418294 -0.21242393740293777; 0.13461115182682395 0.05041661637191812 -0.24899155750815835; 0.09995424647036057 0.05082443507742586 -0.2532585548137527; 0.06189152736658437 0.03710749314731782 -0.1969649169434874; 0.035661709356976365 0.023767809548419436 -0.13654710897005223; 0.026015049842895398 0.018901384753362026 -0.11406659844030839; 0.0035975341890756266 0.0029103484627192476 -0.018241157666513387; 0.003581176532846795 0.0030046403821405773 -0.019876924496617127; 0.0014665234618667972 0.0012676828039558754 -0.008463520728575723; 0.007138001089252412 0.007288623763225045 -0.04519481011766428; 0.00045856294757783193 0.0005162284704434188 -0.004495083768990868; 0.00032935037888455064 0.00016030499156432425 -0.0012568625208012735; -0.000273870527375124 -0.0002794313852691455 -0.0017963606515901613; 0.000804673891430685 0.0007413438189133 -0.0014723436208299548; -0.0003036353317286035 -5.291107116924443e-5 -0.0009103905815568611; 0.000714752541705641 -0.00031411053430777005 0.00032479784295619545; 8.425681370893816e-5 0.00068768347075758 -0.0009853645490785889; -0.00015389422746846606 -0.00015727167143973503 -0.0002936859094615095; 0.00101711113518382 0.000119111826261778 0.0002797495085059688] %
+
+Mass Used: 119.23515243671818 kg
+Launch C3: 95.19582713655251 km²/s²
+||V∞_in||: 2.1899987500039257e-6 km/s
diff --git a/archive/ES_0.5782006422043046 b/archive/ES_0.5782006422043046
new file mode 100644
index 0000000..fee9f82
--- /dev/null
+++ b/archive/ES_0.5782006422043046
@@ -0,0 +1,22 @@
+archive/ES_0.5782006422043046---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T04:47:59.295
+Launch V∞: [6.569714125145838, -7.201566369267201, -0.538932681439661] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.2773686416667925e-6, 9.652604930652142e-7, 1.1170866101575178e-6] km/s
+ V∞_out: [1.4739741504715293e-6, 1.2802812978482722e-6, 4.060419566007403e-8] km/s
+ time of flight: 1.8749577787467024e8 seconds
+ arrival date: 2029-04-02T06:57:36.295
+ thrust profile: [0.3414460463486829 -0.06418738384914581 -0.07909765446560008; 0.18817741254889603 0.0808466739152009 -0.13045601814257335; 0.14521937914797525 0.11815117634498999 -0.15698771660010694; 0.05342936839707051 0.061364698864450964 -0.0937080438586301; 0.07956361575046073 0.11849780038349025 -0.1732955848438092; 0.04709145853470252 0.08831560191814383 -0.14036143222826342; 0.038399010058290946 0.0736198764550779 -0.1293592580971545; 0.005176549148956872 0.010721901046791035 -0.02037490484872358; -0.0001408542513826735 0.0023544373690171792 -0.004168515981398134; 0.002759298182666676 0.006976322717137795 -0.016182724246197232; 0.00017720186315651064 0.0018367598643809538 -0.000550363658405867; 0.0015374114182791858 -0.0009881386735950512 0.0003461007044233172; 0.00026990675923624407 0.0008669363231772862 -0.0008658275140705739; -0.00042219987868973355 -0.0012839790126976183 0.0021693075050537615; -0.0005586600509432084 -0.0016645520563697497 0.0041216534103559275; -0.0019798461573077575 0.0016946042081134264 -0.00014860382004375217; -0.001980997621868396 -0.0034059693928543103 0.0017188137821266291; -0.0008198605679444819 -0.000643669426288948 -0.00031846933105470995; 0.0014489333578584797 -0.00015572957791999751 0.002391020994139851; 0.00041752724507147104 0.0006981147538369 0.00022743753145018056] %
+
+Mass Used: 118.56820586704362 kg
+Launch C3: 95.31415029222487 km²/s²
+||V∞_in||: 1.9522502300625763e-6 km/s
diff --git a/archive/ES_0.578221046022363 b/archive/ES_0.578221046022363
new file mode 100644
index 0000000..00a4498
--- /dev/null
+++ b/archive/ES_0.578221046022363
@@ -0,0 +1,22 @@
+archive/ES_0.578221046022363---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T01:44:01.590
+Launch V∞: [7.155997785198263, -6.7953850565382545, -0.6080704197460259] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009208586199937014, -0.005070455788627195, -0.004971164211042235] km/s
+ V∞_out: [-0.006255851113566252, -0.0007343316314006356, 0.00340499879420783] km/s
+ time of flight: 1.448862099685215e8 seconds
+ arrival date: 2028-12-08T23:54:10.590
+ thrust profile: [0.35127622769354694 -0.11432154806662272 -0.15845878479645123; 0.17462926295719625 0.02748108872411154 -0.2089029405406111; 0.07899166917117716 0.027594528639413606 -0.15620181982697656; 0.07126241671770843 0.03417179273757728 -0.19519517406509412; 0.06285200229418302 0.036052262260252224 -0.2165883550899483; 0.03548578954103363 0.02323810923096661 -0.14738014399533908; 0.022779984531640447 0.015947847018074137 -0.10721992897465248; 0.015181703401554465 0.011292488314575659 -0.07961940173583718; 0.007216095013112127 0.0051904757008948655 -0.04047784481769983; 0.013812884062069418 0.011044156041461755 -0.0835592196042254; 0.0020775701290771838 -0.0013868524697437526 -0.002227358021261231; -1.0526380028453273e-6 -0.00018504196702781985 -0.0011536413388160591; 0.001336142463877925 -0.0005622586351650184 0.0015667585707681698; -0.0004452554364663004 -9.596648799250961e-5 0.004464789125146914; -0.0007598476630645795 0.0003536648076870356 -0.0025021105529142674; 0.0018390442401433182 -0.007501113620995042 -0.0010922127556043202; -0.005186037948664132 0.0029964618359955056 -0.0019394874603741604; -0.0030184169221822237 -0.004104638759007797 0.003504305552766448; -0.0053172043649481965 -0.00566520639528935 -0.0022450696851694756; 0.0011330458932522463 -0.0016318081681295864 -0.00025284931318898373] %
+
+Mass Used: 104.3519003375136 kg
+Launch C3: 97.75531200375598 km²/s²
+||V∞_in||: 0.007160305588142653 km/s
diff --git a/archive/ES_0.5782421632054731 b/archive/ES_0.5782421632054731
new file mode 100644
index 0000000..a4edce2
--- /dev/null
+++ b/archive/ES_0.5782421632054731
@@ -0,0 +1,22 @@
+archive/ES_0.5782421632054731---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T20:24:47.557
+Launch V∞: [7.4256313960386, -6.29989927133691, -0.14231463372587677] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7514631793578816e-9, 1.385746191620205e-9, 3.465263264426917e-10] km/s
+ V∞_out: [1.5664860403002277e-9, -1.4772303892646236e-9, -1.1226896626325405e-9] km/s
+ time of flight: 1.5730108836459896e8 seconds
+ arrival date: 2029-04-27T11:09:35.557
+ thrust profile: [0.39588415102300806 -0.07262302163822983 -0.1139838827759239; 0.32408670853440297 0.12357799020017902 -0.2582284689888842; 0.17208594954376294 0.12271691041187205 -0.2364927314036656; 0.07056623762672792 0.06930627763213651 -0.14717518613416725; 0.0545980214333759 0.06625474523428106 -0.14928242453376958; 0.01944462937776952 0.030071107239534225 -0.06949276377658953; 0.017851151454115848 0.026172436996189128 -0.0703867945624067; 0.007646846842656334 0.013306167520948134 -0.037288851472575615; 0.021059843330520876 0.04323963199198974 -0.11382657759381837; 0.007578418640691714 0.014083710980526826 -0.04192011817565399; 0.0021907474742595984 0.008835942065185964 -0.02100433126942409; -0.0006228392553700606 0.0010627912420975278 -0.0010880714439426445; 0.0017057164907281755 -0.0021036050845691396 0.003519993331011181; 0.0014148675606478422 -0.004485321178771042 -0.0015004849684451841; 4.8982788470536406e-5 -0.001195878090546827 0.00168115302139148; 0.0003975261109365971 -0.0026788804185773956 -0.0005114449561034559; 0.0016439732700763718 -0.002093292674113907 0.0013535963622812227; 0.0008465868229963142 -0.0010364035709278015 -0.0018446472889304347; -0.002084006899968893 0.0015121973572145813 -0.002417923728405502; 0.006879987737074331 0.0005612388068274422 -0.003980553707452943] %
+
+Mass Used: 121.33010590923004 kg
+Launch C3: 94.84898591379803 km²/s²
+||V∞_in||: 2.260087668908927e-9 km/s
diff --git a/archive/ES_0.5783585941308016 b/archive/ES_0.5783585941308016
new file mode 100644
index 0000000..9f4928c
--- /dev/null
+++ b/archive/ES_0.5783585941308016
@@ -0,0 +1,22 @@
+archive/ES_0.5783585941308016---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T12:34:27.049
+Launch V∞: [5.3839663660879, -8.370985481191598, -0.9801945602070417] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.5115968369533314e-6, 2.211209643517411e-6, 4.32551414540708e-6] km/s
+ V∞_out: [-3.010174399262927e-6, 3.870055597115154e-6, -4.4592989106327e-6] km/s
+ time of flight: 1.5557259013202807e8 seconds
+ arrival date: 2028-04-04T03:10:57.049
+ thrust profile: [0.2727283047842904 -0.15503619434373994 -0.15450093943776957; 0.0902065578437795 -0.010224015401796795 -0.13171979922498747; 0.06314487140324293 0.0013292464408968506 -0.1512324708016447; 0.0494580275113698 0.0037416956280581404 -0.16173610335580874; 0.040120368849187425 0.003761652008222334 -0.16318906618360493; 0.018788743560447622 0.00207541356337418 -0.09474887254151348; 0.028567332671762518 0.0033039265377616555 -0.1590928746948554; 0.021481206219555897 0.002430040355998009 -0.13344176226695229; 0.006150598654876201 0.00041681455553435625 -0.043055566588020865; 0.0014229889229746755 7.808632165640074e-5 -0.009831860361950192; 0.00030852773662916403 0.0001229793683890217 -0.002718458452966068; 0.0003484509852065448 -0.0001570357602184003 -7.98110030671178e-5; 0.00011724583969214368 -9.436344468836472e-5 -0.0015194141020532178; -7.367759071018809e-5 -0.00012022884175761403 -0.001055951443837918; 0.00043793344151847147 6.466269498935842e-5 -0.00047433126489739453; 0.0006138790633049131 -6.117012119826438e-5 -0.0009176006531558837; 0.0005825004826681508 -0.00021483393481763465 -0.0006049515329959851; 1.4868533741596358e-5 -0.0010734123505000616 -0.00027895097026609206; 9.374874560359872e-5 -0.002135310226065472 0.0024030800756186356; 0.0016276311061247206 -0.00038858209314572144 0.0028973981037510896] %
+
+Mass Used: 91.29426654141844 kg
+Launch C3: 100.02127313334573 km²/s²
+||V∞_in||: 6.629783309347934e-6 km/s
diff --git a/archive/ES_0.578379473720214 b/archive/ES_0.578379473720214
new file mode 100644
index 0000000..16db28a
--- /dev/null
+++ b/archive/ES_0.578379473720214
@@ -0,0 +1,22 @@
+archive/ES_0.578379473720214---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T21:44:22.141
+Launch V∞: [5.339348974583127, -8.054865564948551, -0.34802233958593315] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6262490946642034e-6, 6.120081874508703e-7, -8.111194386181046e-7] km/s
+ V∞_out: [2.707907905834035e-6, -7.102754102962131e-7, 3.093877414704251e-7] km/s
+ time of flight: 1.457593050181012e8 seconds
+ arrival date: 2027-12-04T22:26:07.141
+ thrust profile: [0.6765954117704698 -0.3839824482838057 -0.30096504573196764; 0.14066842164348278 -0.0071882948550543455 -0.16519697168845868; 0.1330999888313943 0.02155363036688779 -0.2423619415661789; 0.10957827161603803 0.03153062146450225 -0.2654056241511874; 0.07853718025642348 0.029084827653530466 -0.23813058032743162; 0.036690613544651376 0.015510179191457333 -0.13608589825798395; 0.01544256424011821 0.007144293231105826 -0.06298589001530097; 0.01557109129957547 0.007349404692106002 -0.06882758205295764; 0.008502922550753344 0.005065995856727485 -0.04352206309101387; -0.0014791988768310673 9.633818676296033e-6 -0.0010722904753253982; 0.0005683141163056435 0.000450137467690754 -0.0034968497202699225; 0.0002907006208695605 0.00023912058817337475 -0.002192074012506358; 0.00011878974667816562 -0.0007044813389407253 -0.0002935507095632098; 0.0006565640707265392 -0.0002824372441199341 0.00019040766991345248; -0.003663076967454885 0.0030178252356519893 -0.0010584716316119072; -0.002873136385261211 -0.0005985167762524894 -0.0023586925560191213; 0.00023868513385690024 0.002001632839137489 0.0021250332674557226; 0.0004218594093173832 0.0010425514991652353 -0.001296444924955092; 0.00024141721536052665 -0.006076545639149777 -0.0030580636172471707; -0.005306224103317221 -0.0016227255524202556 -0.002326631587598121] %
+
+Mass Used: 129.29739931159384 kg
+Launch C3: 93.51062629062672 km²/s²
+||V∞_in||: 2.815963968596828e-6 km/s
diff --git a/archive/ES_0.5784995329574804 b/archive/ES_0.5784995329574804
new file mode 100644
index 0000000..bbf1408
--- /dev/null
+++ b/archive/ES_0.5784995329574804
@@ -0,0 +1,22 @@
+archive/ES_0.5784995329574804---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-10T14:11:26.934
+Launch V∞: [6.378382391812387, -7.907678005557272, -0.02584737660811946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.588185477470685e-7, -0.00018123941561663025, 0.000123984353854023] km/s
+ V∞_out: [0.00010904303472129938, 0.00018525738750738233, -4.549334532917709e-5] km/s
+ time of flight: 1.8749577783112383e8 seconds
+ arrival date: 2029-04-18T16:21:03.934
+ thrust profile: [0.10064266786036632 -0.04777985284536189 -0.05404516455645073; 0.02687664003512098 -0.007461778943202834 -0.04872893002394709; 0.030719328584796774 -0.012487644022070204 -0.09668591769564387; 0.03009039713402761 -0.017626336768667768 -0.1284624471638048; 0.025421306296811313 -0.018987437936666865 -0.1316268833670655; 0.021419551212583515 -0.018850657986328623 -0.12578822857053684; 0.016473249697568925 -0.016149721029673266 -0.10551917133189986; 0.011171109953013496 -0.011813242402172026 -0.07554753970993558; 0.0071561899830901625 -0.00808485739974741 -0.0500497185166219; 0.0026482501595058963 -0.0032474830016586843 -0.01892828640091375; 0.00014252296648765988 -0.0004692484522625485 -0.0009542996772658324; 0.0002909158174654253 -6.162339721410125e-5 -0.003553954003457112; 0.0022362918474482293 -0.0010130904008273049 -0.002314813129854431; 0.00043443169303007526 -0.0014406985591672358 -0.003433373773208232; 0.006187904832457371 0.0012525749371603775 -0.0029261253033645305; -2.532741409252677e-5 -0.00022373092413598142 -0.003945597609706478; 1.164550203797566e-5 0.00021991456881326372 -0.0010089262015109063; -0.002699365654460175 0.0034305759721941073 -0.005875049418924319; -0.0022673363899536753 0.003697406693702346 -0.0009088721491968977; 0.00024029229055865452 6.814359420682085e-5 0.004400383248003891] %
+
+Mass Used: 72.82394658502835 kg
+Launch C3: 103.21580146263406 km²/s²
+||V∞_in||: 0.0002195908879070954 km/s
diff --git a/archive/ES_0.5784997865670122 b/archive/ES_0.5784997865670122
new file mode 100644
index 0000000..e79968d
--- /dev/null
+++ b/archive/ES_0.5784997865670122
@@ -0,0 +1,22 @@
+archive/ES_0.5784997865670122---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T17:02:32.538
+Launch V∞: [7.633153162354574, -6.760864121949643, -0.3716036590746802] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004741548054664403, -0.00031434492242468263, -0.01797331567714079] km/s
+ V∞_out: [0.007494199705311586, 0.013819197099246082, -0.00872855566717115] km/s
+ time of flight: 1.7214585016692433e8 seconds
+ arrival date: 2029-11-02T03:20:02.538
+ thrust profile: [0.03944644575101297 -0.00994809681950157 -0.020071578298236546; 0.0207552213992458 0.0009495524864709045 -0.03342686142348216; 0.02532619782307453 0.001191464910232334 -0.07108199845868624; 0.03545062162046011 -0.00019698450937557973 -0.1356165320600331; 0.03473747223934845 -0.0026051536390242253 -0.16153845079401646; 0.02482731688734739 -0.003985322032605065 -0.1327800888720163; 0.017154079647403685 -0.0041995783760813196 -0.10129308319056389; 0.009519250310433453 -0.0027325590893814487 -0.05965690070521221; 0.009336084656402356 -0.0031869113920689174 -0.06208395603106234; 0.008591975309920804 -0.0034245301546154284 -0.05973547856546633; 0.0034821502190290642 -0.0017294321073327442 -0.024718050880874327; -0.00013961322774682424 0.0007855011701931548 -0.004871056071307002; 0.0021331200904522642 -0.0035791059796873676 -0.006318508484571038; -0.0009515221154100339 0.0009683477634275359 -0.005343185773218321; -0.0010165842303809295 0.004663247998614255 -0.009315106178344423; 0.005503383573871416 -0.008318598454854515 -0.007035784171040041; -0.00610729188626098 0.004148594653574085 -0.012507758950395399; 0.004398125149054188 -0.0066230280869902895 -0.0039347638345376135; 0.00010528041174951634 0.002726842604792938 -0.0030741985607767273; -0.0005893066217646102 -0.0019021193218967062 0.005151068464587041] %
+
+Mass Used: 67.59408342478855 kg
+Launch C3: 104.11240015486725 km²/s²
+||V∞_in||: 0.01798231664552585 km/s
diff --git a/archive/ES_0.578502317092705 b/archive/ES_0.578502317092705
new file mode 100644
index 0000000..c21c55c
--- /dev/null
+++ b/archive/ES_0.578502317092705
@@ -0,0 +1,22 @@
+archive/ES_0.578502317092705---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T13:42:27.927
+Launch V∞: [6.607448609982928, -7.490302694554124, 0.06197446268449206] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00021662240242250285, -0.0013860751262798367, 0.0017916452744575428] km/s
+ V∞_out: [-0.001531473392178741, -0.0012450589019855156, -0.0011328455933624928] km/s
+ time of flight: 1.874957778747001e8 seconds
+ arrival date: 2029-04-11T15:52:04.927
+ thrust profile: [0.10028283759723489 -0.025647957126454173 -0.04100640947938378; 0.0318011128165976 0.0020095005535788616 -0.041870044513610115; 0.0391144022367506 0.01679826142609599 -0.08049806733313797; 0.05090412020394007 0.031412793768122914 -0.14301425980801943; 0.059682684674908414 0.043249988958809465 -0.20749592256076058; 0.02276736907694764 0.019767802374120978 -0.10213049641424823; 0.022220216968480113 0.0206487433274307 -0.11563108248917972; 0.011170917128143295 0.011620299583075942 -0.06375309263232602; 0.007126363274091475 0.006460487790136821 -0.019781222026809566; 0.0026490878525082294 -0.000554265170575682 -0.02840562763357657; 0.0036149641041805635 0.005766184993871672 -0.010183128029829968; 0.00919655080121135 -0.006085541814404393 0.008373223979358907; 0.002973790545236262 0.002971968991663838 -0.01075205224080561; 0.00943981043542421 -0.015743445762827192 0.011818840896419679; -0.005491988395224172 0.027627753620401777 0.01153991603653419; -0.04156499638325852 -0.013324211226490348 -0.03406121331357957; 0.028869890465339262 0.011059615870093322 0.0037574346309368067; -0.021232118134153266 -0.022016816489560838 0.025609915840144527; 0.0011177679193464384 -0.002922420508528544 0.04856393347691665; 0.006933038392664913 -9.529440913197937e-6 0.002613674788353346] %
+
+Mass Used: 92.94606413695101 kg
+Launch C3: 99.76685242363513 km²/s²
+||V∞_in||: 0.0022755487932384585 km/s
diff --git a/archive/ES_0.5785500844380799 b/archive/ES_0.5785500844380799
new file mode 100644
index 0000000..468edff
--- /dev/null
+++ b/archive/ES_0.5785500844380799
@@ -0,0 +1,22 @@
+archive/ES_0.5785500844380799---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T14:54:36.920
+Launch V∞: [5.641855921500024, -7.39826178978131, 0.15848819327329594] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.2274103375386445e-9, -4.78625672731516e-10, -3.941785365900909e-9] km/s
+ V∞_out: [-1.292393170958157e-9, 3.306002547001671e-9, 4.179232762899291e-9] km/s
+ time of flight: 1.796536620499579e8 seconds
+ arrival date: 2028-12-29T22:42:18.920
+ thrust profile: [0.7889181459879429 -0.21020953162047296 -0.15074647175641967; 0.4172241691159646 0.14193691324978125 -0.23714101226172776; 0.30553017117302506 0.2047560585153115 -0.2841093699296767; 0.12231665526952806 0.11522174762222952 -0.1705476348915907; 0.033490702156304356 0.04011222946192552 -0.06285938424498368; 0.019266327107515795 0.028197514618949635 -0.045986851377781184; 0.0285564745456336 0.047286304216591815 -0.07926862859392507; 0.0010044727363369525 0.0019552284077757687 -0.004791003832507677; -0.002127463938170697 0.002624876926696586 -0.012142981507780629; 0.0011195939545409288 -0.0023223296046883937 -0.010650494818663389; 0.005184738074041635 0.009156740920897582 0.0016205513210978736; 0.00010320036043510093 -0.0024329524965284377 0.004213873650230634; -4.66469527099525e-5 -0.00038992572018440317 -0.003302025154544309; 0.0015710744110147444 0.008213082976387277 0.0024116216976240628; 9.158459466581499e-5 0.00047248505240607473 -0.0010538424415666907; -0.0002622441757122034 -0.0005198154614602714 0.003667451126793445; -0.003924188909048847 -0.007102377517331023 0.005116742391090489; 0.0013918470299827779 -0.007217048219030003 0.004388542365578028; 0.0049175396087144455 -0.0033889610485918742 -0.010691824685501812; 0.005128446206960396 0.004263154453189262 -0.01044417195266343] %
+
+Mass Used: 169.867148681451 kg
+Launch C3: 86.58993425651008 km²/s²
+||V∞_in||: 5.799806252570585e-9 km/s
diff --git a/archive/ES_0.5785769582601408 b/archive/ES_0.5785769582601408
new file mode 100644
index 0000000..6156413
--- /dev/null
+++ b/archive/ES_0.5785769582601408
@@ -0,0 +1,22 @@
+archive/ES_0.5785769582601408---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T12:19:45.950
+Launch V∞: [5.253420295550398, -7.959786219639131, -0.2704961139944666] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.564702174584996e-9, -6.612746401612903e-10, -1.553956255193401e-9] km/s
+ V∞_out: [1.1471704321455112e-10, -2.630205876549137e-10, -3.2814918414951873e-10] km/s
+ time of flight: 1.487791839413323e8 seconds
+ arrival date: 2028-01-07T11:52:48.950
+ thrust profile: [0.6821915317642493 -0.3701827718512221 -0.2663316107804473; 0.3762569757765791 0.004195696907839537 -0.3478689912888338; 0.20434503568710663 0.049238337902849046 -0.2968146014277055; 0.11658007142337458 0.04526899848203838 -0.2281856201255152; 0.05541253828932764 0.028138628037263885 -0.13679274393093027; 0.017315723433376742 0.010803196803218847 -0.05211741051449032; 0.014855899632632327 0.010154843259806492 -0.05039800507435063; 0.021930644687101007 0.015514111124332989 -0.07868046422889555; 0.004580833015917021 0.00421951855172146 -0.020403398915546843; 0.006806287404872902 0.005976145716604243 -0.030491359859755478; 0.005843474318468541 0.004011576684202437 -0.02238569718748545; -0.0007678209569547622 -0.0005407053355707887 -0.002968454731038063; 0.00011646283333479907 0.0010408604128651646 -0.003436260346520831; 0.002270568750072211 -0.0006316526913198676 -0.002190846129909293; -0.0003257392424750233 -0.002131730169034527 0.001820160990019709; 0.0007207433570082224 0.00047859295740108274 -0.005878566050939346; 0.005178286972403738 -0.0023732221531703396 -0.015308688714309075; -0.00023073134749216942 0.0015922775514649623 0.004828009196228558; 0.0015289142374093115 -0.004518535658233867 -0.00018340846517404764; -0.0006915178613652093 0.008858792622289498 0.0029374611976673397] %
+
+Mass Used: 143.99934523499132 kg
+Launch C3: 91.02978961174394 km²/s²
+||V∞_in||: 2.3022504398796753e-9 km/s
diff --git a/archive/ES_0.5786340629292033 b/archive/ES_0.5786340629292033
new file mode 100644
index 0000000..9ab1b21
--- /dev/null
+++ b/archive/ES_0.5786340629292033
@@ -0,0 +1,22 @@
+archive/ES_0.5786340629292033---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T11:16:03.153
+Launch V∞: [5.662518813877991, -7.379852694499614, 0.5623714876973299] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0765735790428134e-9, -7.126693305093311e-10, 1.07364364186985e-9] km/s
+ V∞_out: [-1.375486776467178e-9, -2.0194548563731234e-9, -1.0431689481290028e-9] km/s
+ time of flight: 1.694731928775389e8 seconds
+ arrival date: 2028-08-30T23:09:15.153
+ thrust profile: [0.972877312288156 -0.36013509372989533 -0.21268519555833285; 0.4986661701369471 0.1132148897919149 -0.3129716235256626; 0.18738292464159054 0.10060804300417843 -0.20161210677309366; 0.05890955603944454 0.044936780346552074 -0.09341242556236024; 0.03535265931919763 0.03327073631437864 -0.07160942150610387; 0.054761535211831844 0.06304296017259421 -0.1303189339728705; 0.02326673129291857 0.02970306762305102 -0.06774880184811831; 0.023367323214964958 0.03301088312541263 -0.0757532405033126; 0.0010805127005605228 0.0016648910701008617 -0.003936833180942076; 0.0014136293457837348 0.0023335018942574216 -0.005705901930699472; 8.921574280396423e-5 0.0008661608904842072 -0.0019718284790757558; 4.470465646447781e-5 0.00014352350511098 -0.0008033085373273905; 0.00036432124836453653 0.0008097557066153892 -0.0020923311280923885; 0.0001352118193161709 0.00036467970413043584 -0.0007991737072959085; 2.951334077061282e-5 2.770554605953054e-5 -0.0003541846528590297; -0.0006884197270300818 0.0001036717138126233 -0.00037239292527020164; -0.000360287977838998 0.0010477860018662465 -0.001388697436396094; -0.00014037329671953615 5.079697579884806e-5 -0.0002558610896367852; 0.0007955735795914009 -3.303113638542074e-5 0.00021757292080277108; -1.2320690652350974e-5 0.0002301971361612668 -0.00032148168134457606] %
+
+Mass Used: 168.49120041617698 kg
+Launch C3: 86.84260680021033 km²/s²
+||V∞_in||: 1.6791720922732209e-9 km/s
diff --git a/archive/ES_0.5786709014547742 b/archive/ES_0.5786709014547742
new file mode 100644
index 0000000..9ba505b
--- /dev/null
+++ b/archive/ES_0.5786709014547742
@@ -0,0 +1,22 @@
+archive/ES_0.5786709014547742---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T00:45:05.031
+Launch V∞: [7.064725731849504, -6.806995058932958, -0.3774930411032103] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.5069917357835494e-7, -1.03126078114987e-6, 1.5776870261695613e-6] km/s
+ V∞_out: [8.745519281940324e-7, 1.7297296256533804e-6, 5.014679424066184e-8] km/s
+ time of flight: 1.4585570818763474e8 seconds
+ arrival date: 2028-12-20T04:13:33.031
+ thrust profile: [0.44214357365994855 -0.12688362562567934 -0.1791990995333212; 0.15495372970424237 0.029935441949852214 -0.16870330281268311; 0.10464434309524473 0.0433729535719005 -0.18558049740637747; 0.07922896844362026 0.04441438540946654 -0.19326022374704244; 0.07307918649484185 0.04865882935894747 -0.22331632633262347; 0.04095753543811733 0.030319655554734315 -0.14942352402829812; 0.033437238832147775 0.026614814500783967 -0.13999483820907865; 0.016494447946127908 0.012922161143374038 -0.07499726119891484; 0.010487292391588052 0.0016709513827952516 -0.03483303339713755; 0.0038278975630405285 0.0016511794448578487 -0.009713789884680132; -1.3325132478553639e-5 -0.00571389866134108 -0.009723817028303943; 0.004915147267757956 0.005700850598731464 -0.008907403829789424; 0.00015083100671762616 -0.0038292156800857746 -0.0035202552090172123; -0.004334231879955826 0.011694452424400203 -0.014137006648834462; -0.004148465655710461 0.003282662758684868 -0.0038558821041988385; 0.0071091509088374236 2.8625703842129115e-5 -0.007691898659604278; 0.0034587833461365135 -0.0039055417952251308 -0.010587977101791414; 0.006854673731716141 0.005366872715835653 -0.01940781785363376; 0.0032176400282083774 0.002995668274389806 0.00011478015904754519; -0.0071723685803836285 -0.005289343853404613 0.014387449838123461] %
+
+Mass Used: 112.8525293949624 kg
+Launch C3: 96.38803239467556 km²/s²
+||V∞_in||: 1.93796927125943e-6 km/s
diff --git a/archive/ES_0.5787447297500612 b/archive/ES_0.5787447297500612
new file mode 100644
index 0000000..37b1870
--- /dev/null
+++ b/archive/ES_0.5787447297500612
@@ -0,0 +1,22 @@
+archive/ES_0.5787447297500612---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T01:48:19.416
+Launch V∞: [5.568199901837439, -8.054561322073836, -0.2532975579567841] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.272945261140116e-7, 2.1814443318637137e-7, -2.7539918668690894e-7] km/s
+ V∞_out: [9.576402349229324e-7, -2.5468140665336815e-7, 7.97876673351659e-8] km/s
+ time of flight: 1.5075155137136677e8 seconds
+ arrival date: 2028-01-31T21:14:10.416
+ thrust profile: [0.3955346785916235 -0.1914159573287419 -0.14707997180845428; 0.13385714786239866 0.008073587852378482 -0.1302201946287743; 0.09941150898585993 0.029366225006968765 -0.1511410353142172; 0.09005652186684153 0.04014192331864637 -0.1779200904809484; 0.10642072442493086 0.061073806773811315 -0.26243933238012085; 0.047250956403442006 0.03065320593907224 -0.138445101212435; 0.017938988061265225 0.012420791729596658 -0.06287587716266133; 0.02946574731588495 0.022908777982029217 -0.11096643735247196; 0.03055665697748431 0.026183269263316884 -0.12264609396175002; 0.006331411801990833 0.005653794642059763 -0.029539240990444925; 0.004719254111102959 0.004304467131256367 -0.02294491444728384; 0.009723217203743592 0.00758327581359383 -0.03739394695834799; 0.0009735331378275995 0.0003086918343957185 -0.002497489772025305; 0.00012177144150642597 0.0032008421467402013 0.0026298488309583487; 0.001952858656905863 0.0022133582231181137 -0.002271806314100406; 0.00021780768438928478 0.0005303144761294744 -0.0014035822806851576; 0.0025329601922432685 4.464344861335661e-5 -0.00047023370462457475; -0.008045825514861283 -4.092397509407642e-5 0.00607628021411588; -0.0037817853153780086 -0.0032927911536192707 -0.0009068455209955939; -0.0035457822167467407 0.001674119440140341 0.011195580938279737] %
+
+Mass Used: 115.5232053457712 kg
+Launch C3: 95.94496789073717 km²/s²
+||V∞_in||: 9.916182954741323e-7 km/s
diff --git a/archive/ES_0.5787504782470383 b/archive/ES_0.5787504782470383
new file mode 100644
index 0000000..475dd2c
--- /dev/null
+++ b/archive/ES_0.5787504782470383
@@ -0,0 +1,22 @@
+archive/ES_0.5787504782470383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T05:48:45.024
+Launch V∞: [7.109616991245436, -6.90435235116034, -0.602676736650264] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0017618283716678382, 0.0014075401576762788, -0.0009660700757904645] km/s
+ V∞_out: [-0.0009927538196076305, 0.00224063752428803, -9.352961883851284e-5] km/s
+ time of flight: 1.4230871419219136e8 seconds
+ arrival date: 2028-11-09T08:00:39.024
+ thrust profile: [0.327818579140705 -0.10649359907238878 -0.14661144262980857; 0.08606101316415493 0.012944590389118809 -0.10210900441572084; 0.10789087444813271 0.039300772782237585 -0.20370447741458583; 0.11538443248057156 0.05769528934266782 -0.294633600616248; 0.0761151212481543 0.045106383755166964 -0.24484686810480222; 0.042045661172622095 0.02738504815372245 -0.16258635743482402; 0.021514553382186486 0.015165196318048345 -0.09683306447060958; 0.013628242237292186 0.010268183186558654 -0.06916844240409403; 0.0036592336750559317 0.00288339914890114 -0.02090890747379688; 0.0024293812978021102 0.0021001829571402056 -0.015524600400167272; 0.003795185475517854 0.0030757660998007724 -0.023012700498875764; 0.001803032998914034 0.002122126081178174 -0.011801381932678595; -0.002196500947989518 0.0021149283589841053 -0.004921046206083194; -0.0014088934213608737 0.0013910462565172082 -0.003103121792166554; -0.001873319171918855 -0.003131351671994918 0.0014903499684743977; -0.0008495622611910856 2.1560846510483784e-5 -0.00041475791736145977; 0.00491459164380029 0.001929201763844463 -0.0018846956988566083; 0.00021879702217627374 -0.0007975811343457486 0.002677909609092851; 0.0009174031615972894 -0.0017631445664394556 0.0008501311256087609; -0.00197096160163007 0.002118190628282298 0.001762116587414159] %
+
+Mass Used: 100.15915728775326 kg
+Launch C3: 98.57995440007853 km²/s²
+||V∞_in||: 0.0024532631122696365 km/s
diff --git a/archive/ES_0.5788204505117103 b/archive/ES_0.5788204505117103
new file mode 100644
index 0000000..2c62b6b
--- /dev/null
+++ b/archive/ES_0.5788204505117103
@@ -0,0 +1,22 @@
+archive/ES_0.5788204505117103---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T14:52:00.391
+Launch V∞: [6.3216740026991465, -7.952230196365598, -0.250048583233994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.11377851561057e-7, -0.00023754966724935943, 0.0001632514752931601] km/s
+ V∞_out: [0.00014511416316257187, 0.00024932857460704743, 3.947898752400316e-6] km/s
+ time of flight: 1.855113972756294e8 seconds
+ arrival date: 2029-03-25T17:48:37.391
+ thrust profile: [0.061647303246232736 -0.027574680526414798 -0.03582927089499675; 0.05570731988512538 -0.010298495906686278 -0.1010129615504179; 0.020145151169439192 -0.004393736124583636 -0.061600040473326595; 0.023523183608163887 -0.008085398657498272 -0.10026980416302068; 0.02258111692067633 -0.010623814187763364 -0.12283695824442534; 0.027204529461009614 -0.015437830261270382 -0.163880705585296; 0.015792168235934052 -0.010316999343316834 -0.10336941609923728; 0.007860428946760702 -0.0064454531908762405 -0.06083704332894308; 0.005207095877365893 -0.003939947085165356 -0.04082106380351402; 0.008237403027443349 -0.007274821633105395 -0.07060385499982226; -0.0004619195874503138 0.00011619360016364123 -0.0037517752118538758; 0.002111431311886257 -0.003271059859080155 -0.0030043852945995015; -0.0007634682064611659 0.0028575235012740954 -0.0007098405408729022; 0.00027373335186210327 0.00027189601896075494 0.002808271178967349; -0.00011005857441683746 0.0004720403523211917 0.000357771111822734; -0.003390346487888221 -0.0011572641027846583 0.004140233605066467; 0.00010289490958429167 -0.00406994891497307 0.0014252324549679015; 0.01035291453882185 0.002169551973173238 0.0022614497488906574; 0.005740043796106145 -0.004537132822714464 0.0007939391949219072; 0.0010856079561770806 0.0059606735290065865 0.01000967165352695] %
+
+Mass Used: 72.91689134317949 kg
+Launch C3: 103.26405158636842 km²/s²
+||V∞_in||: 0.00028823843368663095 km/s
diff --git a/archive/ES_0.5788204930363962 b/archive/ES_0.5788204930363962
new file mode 100644
index 0000000..0f29c4b
--- /dev/null
+++ b/archive/ES_0.5788204930363962
@@ -0,0 +1,22 @@
+archive/ES_0.5788204930363962---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T05:58:32.715
+Launch V∞: [5.516016744141994, -8.209177631459065, -0.552938022546644] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8882624529885282e-5, 0.0077258248015649525, -0.0032087365658410773] km/s
+ V∞_out: [-0.00669426877244342, -0.0038418157632936407, 0.003227220752055197] km/s
+ time of flight: 1.4659530688027465e8 seconds
+ arrival date: 2027-12-15T22:53:38.715
+ thrust profile: [0.261477385315637 -0.1433757620548279 -0.1237539460774114; 0.14635061385027195 -0.0029063208955979443 -0.16218989151114355; 0.11488795433124448 0.0219415805814998 -0.19807927441888334; 0.07975182979962989 0.025183821222690535 -0.18544456643681892; 0.0606398159633052 0.02374928972872679 -0.17302861618279558; 0.04781627322646981 0.02146399514253385 -0.16012367770210756; 0.05073274777153354 0.026829206841111113 -0.1888465749613833; 0.025933160636808065 0.014721818399977176 -0.11085739414796676; 0.011053239093935666 0.006576027015665415 -0.05171697322041341; 0.007694413231131627 0.004671746990373719 -0.03848215481014906; 0.0009432676378296164 0.0005789933990364211 -0.0030141147087841625; 0.0002303448742861601 0.00032077005000949324 -0.001035379830708266; 0.0005054298362155305 0.0005381536315026472 -0.0037448085806543107; -0.00031495672138117693 -0.00016885882874434813 -0.0009795120056320236; -0.0012410807282126613 -0.00042694603582790855 -0.002563551489225725; -0.0006113272032908154 0.002669894300882315 -0.001536882027129312; -0.00031921250346871456 -0.000292819074119413 0.0013423236636634903; -0.001890252529999118 -0.0003841854008470091 0.004810834317682967; 0.0009518385928538259 -0.0007113494597907949 -0.0011335922797586864; 0.005752820891249656 -0.0026586738435968693 -0.00029974986882024164] %
+
+Mass Used: 102.90770025665915 kg
+Launch C3: 98.1227785632805 km²/s²
+||V∞_in||: 0.008365686807844941 km/s
diff --git a/archive/ES_0.578889411206632 b/archive/ES_0.578889411206632
new file mode 100644
index 0000000..a4acf2f
--- /dev/null
+++ b/archive/ES_0.578889411206632
@@ -0,0 +1,22 @@
+archive/ES_0.578889411206632---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T07:15:43.772
+Launch V∞: [7.165649408428178, -6.4887609615366575, -0.18890123197293113] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008196190948863713, -0.001327681629364316, -0.0020812787534807463] km/s
+ V∞_out: [-0.002360261038775876, -0.0002243731866260103, 0.0010664694542498398] km/s
+ time of flight: 1.5207537740700006e8 seconds
+ arrival date: 2029-02-28T10:25:20.772
+ thrust profile: [0.6725949744591201 -0.16790729069199103 -0.240841584479953; 0.1518879767093234 0.042539506695832195 -0.15812229545623757; 0.07574756264454688 0.04148388888126864 -0.1329286725615222; 0.09978701880269826 0.07259760930863585 -0.2380448130340823; 0.058055177508395596 0.05117161516420607 -0.17877487401234665; 0.04072927604341729 0.041439198412554674 -0.1516417448348114; 0.02198522242907875 0.02474317118227589 -0.09742744909692586; 0.012263385571785848 0.0164032178461744 -0.06282403862781968; 0.004539050898572218 0.004648222692257568 -0.01892400487352346; 0.00847914678767951 0.012311220087945385 -0.054221125200392406; 0.0004753609834090315 0.003780972858570337 -0.013484588430963059; -1.1234310911318766e-5 -0.006459824766441664 -0.01022173424759202; 0.0039693237870580406 0.0011166803284131423 -0.001149692909836568; 0.00013911050390667468 0.004368209171978632 -0.002924438294939711; -0.0009924452252897903 0.0030551540473583018 -0.004767944091081201; 0.009909594959399819 -0.01874257437916458 0.004804178533114033; -0.0075252407648549215 0.004233428213821834 -0.006489170797973592; 0.00611213981579421 -0.021732062414844686 -0.018814494974444856; -0.006810839861997761 -0.005355058033930664 0.018460362499472263; 0.01692261810153552 -0.019813877569289966 0.026786386261147696] %
+
+Mass Used: 130.03461511492833 kg
+Launch C3: 93.48623393591011 km²/s²
+||V∞_in||: 0.0026011988042716396 km/s
diff --git a/archive/ES_0.5788997790398432 b/archive/ES_0.5788997790398432
new file mode 100644
index 0000000..58d0b10
--- /dev/null
+++ b/archive/ES_0.5788997790398432
@@ -0,0 +1,22 @@
+archive/ES_0.5788997790398432---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T21:09:06.795
+Launch V∞: [7.045209019569644, -6.5903961968431855, -0.3228974357598303] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.980783158663093e-6, -2.808230866940599e-6, -2.8318795876882347e-7] km/s
+ V∞_out: [2.5087774272384677e-7, -1.1368274906811539e-6, -3.246143095969784e-6] km/s
+ time of flight: 1.4610235788415232e8 seconds
+ arrival date: 2028-12-19T21:08:23.795
+ thrust profile: [0.6946231176232008 -0.19906600655468187 -0.2594582651462159; 0.27434537415977894 0.0632672994384671 -0.27657016706118864; 0.12976723669222784 0.06288701056793851 -0.21954659527446602; 0.09683242280738442 0.0637318950166122 -0.22593780640213326; 0.059108827874443354 0.04687403887466905 -0.1770938911189498; 0.03038433648686874 0.027350417317042953 -0.11022463114476817; 0.02219071629918283 0.02205920650925053 -0.0929468067700382; 0.012672892583775875 0.01357809270661005 -0.0590431607316883; 0.007306086642734161 0.00863914236325902 -0.03849576371716305; 0.003996952513045147 0.005005252321617012 -0.021733829403759158; 0.002668582860508985 0.0003097474870496536 -0.007193625236874055; 0.00074142053283501 0.0010501765047290987 -0.003469275201996566; 0.00039757154740235965 -0.0022068183347559393 -0.0027492477529967706; 0.00039003530146445664 0.0011702395137551842 -0.0023650080362971134; 0.0007376636358239937 -0.002225188567472832 -0.0029736315624848044; -0.006526450807661038 0.0027374715885315477 0.0025188045036979635; -0.00499202689923341 -0.006288487925639397 0.0008476589970760127; 0.005847550576402702 -0.004631102587280375 0.00501401871627826; -0.0018698628705256341 -0.003261143594107663 0.0011204363556127374; 0.004014049369556848 0.002651755063685944 -0.0017597275981284972] %
+
+Mass Used: 131.8765052100871 kg
+Launch C3: 93.17255491481086 km²/s²
+||V∞_in||: 3.44816733115911e-6 km/s
diff --git a/archive/ES_0.5790418624621864 b/archive/ES_0.5790418624621864
new file mode 100644
index 0000000..235db33
--- /dev/null
+++ b/archive/ES_0.5790418624621864
@@ -0,0 +1,22 @@
+archive/ES_0.5790418624621864---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T08:27:51.462
+Launch V∞: [7.197656028329447, -6.834055855909384, -0.632714023105558] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.6420774139486586e-6, 9.542248149052616e-6, 5.4370663145029965e-6] km/s
+ V∞_out: [6.8435717869680485e-6, -8.339518548841245e-6, -4.184625585765354e-6] km/s
+ time of flight: 1.4702905530565333e8 seconds
+ arrival date: 2029-01-04T01:52:06.462
+ thrust profile: [0.25120060598525873 -0.07871644032143187 -0.1148750269392241; 0.10046119229478406 0.01581755653356176 -0.12362221144184006; 0.09638934157760845 0.034542425282933005 -0.19424542870408906; 0.08150703073462404 0.03904263950931791 -0.22576059187674644; 0.05876564239635362 0.033049518804398895 -0.20538594036082983; 0.03842862654082612 0.024054161918200145 -0.16092259622562718; 0.032651764330807916 0.021955438202252098 -0.1564037049167679; 0.00754663036829948 0.005910812687769818 -0.040468209330407914; 0.005228732795399162 0.004271419602052642 -0.030339868467102196; 0.00529364259687373 0.004265626164946457 -0.032927568077020825; 0.006593241948634283 0.002415806519474511 -0.015931370076815846; 0.0015744704870013456 -0.004186243372804396 -0.0009363139377909302; 0.0059211782675016415 -0.008482115354299536 -0.006606319266871139; 0.001192874539478124 0.0008414475171437247 -0.008166616180762414; -0.00409657579887419 0.0037110571005212665 -0.0014996248358637699; 0.004937380778991349 -0.004468204182420183 -0.0017179830599741357; 0.004450756799520159 -0.002909458419379593 0.01124696216175436; -0.010278586227504605 -0.0007376411449393325 0.010872928431292353; 0.00025168662322511034 -0.005127072667562602 0.030886515243890605; 0.0014900941989785393 0.0018379256911949847 -0.008430279260514217] %
+
+Mass Used: 98.5685966624701 kg
+Launch C3: 98.91089877887097 km²/s²
+||V∞_in||: 1.1570692189130096e-5 km/s
diff --git a/archive/ES_0.5790592400608897 b/archive/ES_0.5790592400608897
new file mode 100644
index 0000000..7181144
--- /dev/null
+++ b/archive/ES_0.5790592400608897
@@ -0,0 +1,22 @@
+archive/ES_0.5790592400608897---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T16:37:17.964
+Launch V∞: [6.40595955028791, -7.4886590147392695, 0.10171575718693382] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.412618108725668e-7, 6.004991060620305e-8, -8.976893944329547e-8] km/s
+ V∞_out: [2.541849096910464e-7, -6.681249094826439e-8, 3.0111344292598864e-8] km/s
+ time of flight: 1.8493492155759737e8 seconds
+ arrival date: 2029-03-11T03:25:58.964
+ thrust profile: [0.27680746723904787 -0.07469472180743485 -0.09480334793689686; 0.07665282949589007 0.01918722216942455 -0.08456800710178906; 0.055201075495633814 0.027662882430296777 -0.10243879581653466; 0.04525076208908386 0.03013364479765436 -0.11726322922590332; 0.02016701473541535 0.01602649273221641 -0.07458352538588672; 0.033122490044696154 0.02822779160348905 -0.13327818830015747; 0.02058353739100218 0.013662586824509312 -0.07522798208440488; 0.01809791805594495 0.024634864576316043 -0.11817572107947788; 0.008159048916176217 0.009696686514918899 -0.05826230323635964; 0.012725680513213116 0.015260520292005217 -0.07365879075749314; -0.004906362792032924 0.0030095296992423133 0.003926573523593862; 4.8658966959158313e-5 -0.0001691275335193515 -0.012158208692965149; -0.001287867390947886 0.004903847637295946 0.017630182410354488; 0.0019417703139822172 -0.0006058123497035472 -0.0069409093442756135; 0.0035784271431887347 0.026805880095544358 -0.017378983851609964; 0.006407511731922006 -0.019259553308995765 0.015352777848434522; 0.04238669417897609 -0.014412246294176367 0.014831958011399414; -0.01968882927933352 -0.006975871816458359 0.016793389470701643; -0.002471204607844234 -0.0005449480118869632 -0.012694384235764564; 0.045371494779759394 -0.02110470479455555 0.04617027426968481] %
+
+Mass Used: 108.99682685475045 kg
+Launch C3: 97.12667769422073 km²/s²
+||V∞_in||: 2.643325852748715e-7 km/s
diff --git a/archive/ES_0.5790728543133453 b/archive/ES_0.5790728543133453
new file mode 100644
index 0000000..b1f0619
--- /dev/null
+++ b/archive/ES_0.5790728543133453
@@ -0,0 +1,22 @@
+archive/ES_0.5790728543133453---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T06:57:11.949
+Launch V∞: [6.944971343950737, -6.916365376159559, -0.7336147710201477] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.2177678619119845e-6, 1.639155817700788e-5, 8.953733912082037e-6] km/s
+ V∞_out: [1.3657993168907429e-5, -1.2304216345792614e-5, -7.0421293623474795e-6] km/s
+ time of flight: 1.4194120722621018e8 seconds
+ arrival date: 2028-11-05T03:03:58.949
+ thrust profile: [0.56883122481453 -0.18094710821247462 -0.21439248860514107; 0.10150093176900055 0.018614212793268404 -0.11977395218873647; 0.0895968340267913 0.036251368010214925 -0.16822960223364486; 0.06679986341980276 0.03792604475542507 -0.17352932937741253; 0.07317252728782483 0.04903749157348817 -0.22754393724240368; 0.041698257685239035 0.03082549786109872 -0.16307149926846282; 0.022488549696601624 0.018976747252389733 -0.10654121728983239; 0.023085019915215145 0.018590865237720473 -0.11013574803006834; 0.017832752736416577 0.01694566371364428 -0.09094788032227999; 0.008976849223111967 0.007645313609191746 -0.054450369552188634; 0.0004758865401126004 0.000275668557421234 -0.001501476913426353; 9.09857936814808e-5 0.0009669542528579527 -0.0014082773769298995; 0.0003127674079387605 0.0001632303471550741 -0.0011333606081908218; -0.001741656199284122 0.0008828772934523998 -0.002001196204695286; -0.0006724155931779317 -0.0012710852804178022 -0.0004199016412145864; -0.00017102639486237447 7.467646660795857e-5 -0.00017229173140913528; 0.0003442537139724494 -0.00020155748505411547 0.000384818521570473; 0.001293943879498655 -0.0008767036478516781 -9.546082509770577e-5; -0.0023957326955927664 0.00018162727889725833 -0.0003725310240033649; 0.0011661778391646512 -0.0020326885904766996 0.001932369027347469] %
+
+Mass Used: 112.0445855991843 kg
+Launch C3: 96.60692761709461 km²/s²
+||V∞_in||: 1.9685354140152708e-5 km/s
diff --git a/archive/ES_0.5791081585116498 b/archive/ES_0.5791081585116498
new file mode 100644
index 0000000..e68b828
--- /dev/null
+++ b/archive/ES_0.5791081585116498
@@ -0,0 +1,22 @@
+archive/ES_0.5791081585116498---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T14:45:16.204
+Launch V∞: [5.557970035661612, -8.088565792937084, -0.5253389603123023] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0021057060314914372, 0.001297361704375149, -0.0011845144524752493] km/s
+ V∞_out: [0.0016008842214908503, -0.0018991198934754764, 0.0011632938659713941] km/s
+ time of flight: 1.517492060702377e8 seconds
+ arrival date: 2028-02-13T23:18:42.204
+ thrust profile: [0.33022251598849756 -0.17543334702630667 -0.1537724937322922; 0.18189552914144222 -0.0007464481375612441 -0.20828651802905013; 0.10117095087668683 0.02042041950804747 -0.1867523955072515; 0.08472895482718901 0.02783616870064221 -0.20984873344650407; 0.06696771415500032 0.027909633020793762 -0.2057412508656128; 0.04014072526988054 0.019252717892310683 -0.1468103364645384; 0.02432468261862697 0.012723508333410493 -0.10234296881306917; 0.026339181067063847 0.015083722250667645 -0.12277393132320114; 0.005332247301346501 0.0033004087479005214 -0.029730777669944874; 0.000516949547154746 0.0002300231677643327 -0.0051429395445005905; 0.0053778390099338425 0.0011436769348890609 0.002732513402294592; -0.0004758583844362144 0.002083756882868314 0.005494282570826054; -0.004320226212256108 0.0015609780401724784 0.0029820054830266987; -0.005408142787137524 0.002159302470266678 0.010132238334184853; 0.0024694261433505305 -0.01067057665016335 2.6357516351764804e-5; -0.0028599127383782293 -0.0018697192617889802 0.011924710857014145; 0.01255196287500265 0.004217814740650675 -0.005244249132470208; -0.003579690810564466 -0.005952935997587788 0.0013958610420687439; -0.011263344055136614 0.01351273615890536 0.001986849502969279; 0.00025056411724750564 -0.002054758540859053 -0.0022023029848011527] %
+
+Mass Used: 112.17338518822135 kg
+Launch C3: 96.59190852720629 km²/s²
+||V∞_in||: 0.0027423019110158803 km/s
diff --git a/archive/ES_0.579162190974115 b/archive/ES_0.579162190974115
new file mode 100644
index 0000000..8a0a129
--- /dev/null
+++ b/archive/ES_0.579162190974115
@@ -0,0 +1,22 @@
+archive/ES_0.579162190974115---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:49:47.749
+Launch V∞: [7.1072371101820915, -6.860747367077085, -0.6711232397654779] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.085597599241544e-8, 1.9785900291007113e-8, 2.8067186808574822e-9] km/s
+ V∞_out: [4.67894140715433e-8, -2.8846205893715042e-8, 1.3101843818111591e-8] km/s
+ time of flight: 1.437313039253426e8 seconds
+ arrival date: 2028-11-25T22:11:30.749
+ thrust profile: [0.36652701774886 -0.11795588266952922 -0.1619150275857371; 0.11960519163948108 0.018516981833583523 -0.1392277160639072; 0.09680877093364533 0.0354007320838794 -0.18446004246742023; 0.07564291084801571 0.03743612675591653 -0.19803838094154236; 0.07328683639842933 0.043183000666801696 -0.23844765678465188; 0.04239861449908607 0.02783335310246203 -0.1659209519844089; 0.03200638990577134 0.022334903579490435 -0.14351319307510077; 0.011318689333762285 0.008334616236364207 -0.05624256548295127; 0.006450460840195779 0.006152547709956588 -0.0365078841146921; 0.00233669024952266 0.001956527151247417 -0.02319787041141666; 0.002512750882336952 -0.0014038129383759047 -0.013598710373749039; 0.0017560456836213274 0.0009971660091742183 -0.0013012831974852025; 0.0064675263045596235 0.00034018848143886507 -0.003844386817247825; 0.0004375225544297394 0.002715992757570164 -0.0036417911780583312; 0.005690032592001322 -0.00524859465197732 -0.0068754000857846114; -0.003041991292328756 0.0015667855805239924 -0.012814670548166887; 0.003953294917902025 -0.0064474947163331384 -0.006878149785583222; -0.008384510468042766 -0.0012645848616726013 -0.017359662999351728; 0.0002318536073880298 0.0008563661694559964 -0.00025898335024523945; 0.006506625300138458 -0.005263140516919455 -0.001944669487617283] %
+
+Mass Used: 103.82958843054621 kg
+Launch C3: 98.03308017815795 km²/s²
+||V∞_in||: 5.464146606946308e-8 km/s
diff --git a/archive/ES_0.5792013456498972 b/archive/ES_0.5792013456498972
new file mode 100644
index 0000000..96e9da8
--- /dev/null
+++ b/archive/ES_0.5792013456498972
@@ -0,0 +1,22 @@
+archive/ES_0.5792013456498972---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T18:16:18.768
+Launch V∞: [5.662941280038724, -8.047191006487084, -0.37424478705913894] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8513342277735951e-6, -0.0007082785080716923, 0.0003073635234657049] km/s
+ V∞_out: [0.0006303750130189457, 0.00034716565121199245, -0.0002788612616426583] km/s
+ time of flight: 1.5318815073007658e8 seconds
+ arrival date: 2028-02-29T18:32:08.768
+ thrust profile: [0.25076686320601455 -0.12478562910075094 -0.10511965032686713; 0.16988452511042668 0.006602173398370628 -0.17338724905932365; 0.15058039690574912 0.041079169004268654 -0.23675975513523048; 0.10228648249091568 0.043274452548943465 -0.21690545772724992; 0.05100999124186254 0.02549700603938461 -0.13328846131414115; 0.062272011369271414 0.038876481294269745 -0.19616039296115112; 0.03398911170308209 0.022157208425435 -0.12028401827371056; 0.02251464900253746 0.015321335393231474 -0.08594466196542866; 0.010349131070156219 -0.0018922469693285846 -0.03226976194439503; -0.004094128485183889 0.00559014104507788 -0.010328528971806979; 0.001161507615416265 -5.385429792845295e-5 -0.0014722264772307869; -0.017977621579551132 0.00549784396241533 -0.015677081173414435; 0.0025293037719700045 -0.0019923268704073347 0.0016441288815521448; -0.004039241614619311 0.015255729258772437 -0.0026471699663296712; -7.449621814873482e-5 0.00030671676601177035 0.000258912623204508; -0.01281809758504749 -0.011125561619905515 0.002588149571243244; -0.018923995934941255 -0.004308653283351351 0.0027608013811933887; -0.00032004929686368824 -0.0012638818991291788 0.014520100151800922; 0.0002730579040033538 0.00034872390088561524 0.0016114039449953545; 1.2878276800311602e-5 -0.0007062677693998361 0.018360305004007347] %
+
+Mass Used: 110.09846711083082 kg
+Launch C3: 96.96624619669417 km²/s²
+||V∞_in||: 0.000772097278839874 km/s
diff --git a/archive/ES_0.5792023761395774 b/archive/ES_0.5792023761395774
new file mode 100644
index 0000000..dbc9dab
--- /dev/null
+++ b/archive/ES_0.5792023761395774
@@ -0,0 +1,22 @@
+archive/ES_0.5792023761395774---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-10T17:27:55.109
+Launch V∞: [6.329484332882128, -7.90756498488797, 0.007807523208553989] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.304220721602434e-8, 5.257386494382057e-8, 3.7054097755058e-8] km/s
+ V∞_out: [-1.8165418573962103e-8, 3.877050708558294e-8, -5.8780887313692805e-8] km/s
+ time of flight: 1.8749577787483153e8 seconds
+ arrival date: 2029-04-18T19:37:32.109
+ thrust profile: [0.17789767255945335 -0.08762642146804979 -0.09121585625820114; 0.01011590887945041 -0.003006141857779221 -0.019383605019117418; 0.018458147696658607 -0.008037745387218718 -0.06026972800908613; 0.03222900984862378 -0.01943570735342764 -0.13628997544221244; 0.0228771468165001 -0.017093012091525243 -0.11833024303100724; 0.020059883792895025 -0.017781005424240093 -0.11747380695953187; 0.016176569030122743 -0.016197443699847665 -0.10352194988164806; 0.01073081324498361 -0.012123744747448402 -0.07353338540795741; 0.009812029262000803 -0.011483025880375874 -0.07091767288138069; 0.005113449040862155 -0.006265758165293427 -0.03813716039216211; 0.005830527293608249 -0.0074207645343348045 -0.04453012660430332; 0.0012722931807332939 -0.00013113544092534213 -0.0010306819856141466; -3.0253827697522727e-5 4.1074098387935515e-5 0.00020711845213493795; -0.0001610769882840267 8.248398816431465e-7 -0.0001679415777471327; 0.0009443410032720739 -0.00027389329583095293 0.0006432738656098913; 0.0005192338722050339 0.00033038907674989615 0.0004752482497786004; -0.0001851010647763102 -3.1471253879519496e-5 0.0001912282569105409; 0.0010946390835330365 0.0023183399103437734 -0.0006691462495723308; 0.00033550094216915137 -7.426198095467635e-6 -0.0006864240376425954; 0.00018559771425691665 -0.0011813677669194455 -0.0010363633357026191] %
+
+Mass Used: 77.28267376707618 kg
+Launch C3: 102.59201686784526 km²/s²
+||V∞_in||: 7.231047568146105e-8 km/s
diff --git a/archive/ES_0.5792872470334456 b/archive/ES_0.5792872470334456
new file mode 100644
index 0000000..d8ce86d
--- /dev/null
+++ b/archive/ES_0.5792872470334456
@@ -0,0 +1,22 @@
+archive/ES_0.5792872470334456---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T08:36:49.758
+Launch V∞: [6.471959101906337, -7.263975746831211, 0.1280313278059455] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.068790049882359e-8, 2.3015457552917113e-7, -1.3689315586127151e-8] km/s
+ V∞_out: [4.434963140790985e-8, -1.005649395558136e-7, 5.8166583347223736e-8] km/s
+ time of flight: 1.874957778754351e8 seconds
+ arrival date: 2029-04-07T10:46:26.758
+ thrust profile: [0.4335714288408222 -0.09699895493110154 -0.1314658180269073; 0.11912929680679409 0.04065538178932749 -0.10663043490816923; 0.06192332419187419 0.0393556127583087 -0.09249360392685947; 0.07860491081625437 0.06767952147471448 -0.16735608332477311; 0.031358126205490715 0.03237717510231621 -0.0869198677590934; 0.020090573095209646 0.025097694787456385 -0.06809302985574518; 0.021866758393627554 0.027621859325332957 -0.08689960225980738; 0.0061091391105278356 0.010127356483507363 -0.027157078294171348; 0.008915446332539689 0.016231480024987727 -0.04622238009444309; 0.01005023933233366 -0.002359184963883751 -0.002395250056886425; -0.0015065228565566565 -0.003288665556588464 0.0018878909724491643; 0.0031733746403812928 0.0062613673396244365 -0.026359611354826094; 0.001790420235690179 0.004362561824274549 -0.001156232243339602; 0.035277594202316256 -0.0118523167693802 -0.05037296934907943; 0.004230177795496802 -0.0023207308072389853 -0.017844793400220233; 0.012041895722547977 -0.01712199063634598 -0.04811896798811198; 0.019425964427995233 -0.0037907075142022423 -0.07017357577997095; 0.004797296926159926 -0.009079174857524826 0.00743880654096658; -0.008295244595153397 -0.038319965912916434 -0.008407632084733146; 0.014316548065782801 -0.057892585754120464 -0.005069893866501512] %
+
+Mass Used: 123.60517819118604 kg
+Launch C3: 94.66799028820009 km²/s²
+||V∞_in||: 2.3259465435657637e-7 km/s
diff --git a/archive/ES_0.5793445862408735 b/archive/ES_0.5793445862408735
new file mode 100644
index 0000000..521e54c
--- /dev/null
+++ b/archive/ES_0.5793445862408735
@@ -0,0 +1,22 @@
+archive/ES_0.5793445862408735---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T15:34:48.207
+Launch V∞: [6.748975331488807, -7.158696101766719, 0.06533470448626917] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007376262892924531, -0.00022415827199650414, 0.004905070510805228] km/s
+ V∞_out: [-0.00853484391912394, 8.118084833317685e-5, 0.0023643846950324268] km/s
+ time of flight: 1.802336988034064e8 seconds
+ arrival date: 2029-01-05T16:29:46.207
+ thrust profile: [0.4010755177693476 -0.11523651744275769 -0.11234074467735797; 0.18330583448318352 0.05565104837164823 -0.15093384756585662; 0.10659171208736962 0.06379759174547223 -0.14641945761724415; 0.0604964093334219 0.048769870712356105 -0.11787108864186899; 0.06489228902063725 0.06405825500380814 -0.15495731795259224; 0.03392825703907215 0.04027578763808281 -0.10363383747746649; 0.035407498257016626 0.04706717561115402 -0.1216603939624323; 0.0077911255759990855 0.013411722599760891 -0.03396283089682223; 0.006649612772440014 0.010802073933744626 -0.030643165363210354; 0.0013091810347481696 0.0017398285697923061 -0.005518253912882344; 0.0006388329908331016 0.0025594621315030296 -0.00700084001423612; 0.0001058652895412875 -0.00039117680611188267 -0.002365432209434753; 0.003253848492593731 0.0013278941986323042 -0.009500123096561614; 0.0014024890827724753 0.0009151557983833848 -0.0028255803631883954; -0.00025126504194481007 0.0003707094480417219 -0.0008654578453865592; 0.0004971584438562408 -0.0002968728601895059 0.002041771509741606; -0.0007611169697576202 -0.00027116647203067625 -0.0006975992916080216; -0.0011727029896413438 0.00018801736683470035 -0.00047466082198262174; -0.0005897816003658116 -0.000716231200998812 0.0004463373283675246; -0.00011435653565238483 0.0031800618291998664 0.0008857458713215455] %
+
+Mass Used: 111.2361292120745 kg
+Launch C3: 96.7998665261048 km²/s²
+||V∞_in||: 0.008861107036505703 km/s
diff --git a/archive/ES_0.5793739485692865 b/archive/ES_0.5793739485692865
new file mode 100644
index 0000000..b8333a2
--- /dev/null
+++ b/archive/ES_0.5793739485692865
@@ -0,0 +1,22 @@
+archive/ES_0.5793739485692865---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T05:03:12.485
+Launch V∞: [5.587341499397369, -8.033621058030274, -0.30224368762053194] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009915689933620321, -0.0006398315898787349, 0.0005297335637299179] km/s
+ V∞_out: [-0.0007078375121346166, 0.000893294458059156, -0.0006132066709456367] km/s
+ time of flight: 1.5325888102511403e8 seconds
+ arrival date: 2028-03-02T00:57:53.485
+ thrust profile: [0.4088189974506673 -0.20516524289205554 -0.16245323646101403; 0.09234870313129422 0.003439570380988893 -0.09577835942305461; 0.10719597581803043 0.027884145280491046 -0.17088395668553055; 0.09896966787962323 0.039542696932042924 -0.20912021126938946; 0.05605091742526388 0.02817707842814645 -0.14982495410784147; 0.0523981590402416 0.03057614979799991 -0.16358797731341757; 0.0365619834977912 0.022314561115975164 -0.12331631413426251; 0.010912852938789928 0.007646839646510347 -0.04513169947373457; 0.031242508447371677 0.02343246478001509 -0.13331166123199018; 0.017449574192166795 0.013861076332161047 -0.08265527060618187; 0.003582382280282323 0.000814549317911654 -0.0091134218850367; 0.0004310853642696665 0.00199044020192541 -0.007424911270714325; 0.008467957658776764 -0.003161194334452451 -0.007549469347256044; -0.0018157368014089185 -0.0008758493776998885 0.0001587211966074739; 0.0028591502002953107 0.012857924394448245 -0.002256327904614258; 0.007541216390895113 0.003513940977482372 0.0009423427208454932; -0.0036230813277330727 -0.014987706290332671 0.001133623805891923; -0.004583897338181637 0.006457627058666093 0.005600149325974142; -0.001115189959160187 0.00012070993782934379 0.02152996010173526; -0.0042735191900501665 -0.0002312793602632585 0.018073160800189378] %
+
+Mass Used: 116.81825243803951 kg
+Launch C3: 95.84880358162195 km²/s²
+||V∞_in||: 0.0012935266446988025 km/s
diff --git a/archive/ES_0.5793902779365343 b/archive/ES_0.5793902779365343
new file mode 100644
index 0000000..93826bf
--- /dev/null
+++ b/archive/ES_0.5793902779365343
@@ -0,0 +1,22 @@
+archive/ES_0.5793902779365343---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T12:20:19.270
+Launch V∞: [5.624283961601688, -8.299883240031676, -0.5538477449152696] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.891370707169748e-9, -3.758482621131563e-10, -5.232749751712199e-9] km/s
+ V∞_out: [-1.7044875077483123e-9, 3.959343524919905e-9, 5.512898080413687e-9] km/s
+ time of flight: 1.5867216354273668e8 seconds
+ arrival date: 2028-05-09T23:56:22.270
+ thrust profile: [0.11824065417178442 -0.06293005143204504 -0.062280854946351924; 0.07340769510326729 -0.004904110139919107 -0.10077798800706991; 0.04678496116811283 0.0034378875103632605 -0.10542410993635046; 0.05884696348389599 0.007772310135450124 -0.17778969197481254; 0.04379436574860959 0.00720066734787147 -0.16505465519112147; 0.02360939609201383 0.005008845139809074 -0.10446162073521686; 0.012196874531574118 0.002210135896185881 -0.06000774825993764; 0.02747829427250341 0.005512990221512722 -0.1477038823443006; 0.021415523732756188 0.0021628053098792293 -0.14578569717824763; 0.012128912537936529 0.002699554328635901 -0.08219212013486407; 0.005904850996595382 -0.0012706630462814559 -0.007374443551285696; 0.003019058921517126 -0.0015760266524213347 -0.009407558263210745; 0.000150045460309178 -0.0033381043387184146 -0.0037086009706550622; -0.0007895767862027641 -0.0011185613316234536 -0.006174169346263039; 0.00730621883381722 -0.0022387459314259775 -0.0171647952187028; -0.004881132405342658 -0.0022325393146940273 0.002576389287556141; 0.008807638148840332 -0.0007520958704597908 0.006720412918517698; -0.0036359492344651646 -0.003359810011261579 -0.006892457034831289; -0.0017828376879167652 0.0037569378175222722 -0.00384409581908137; 0.0032021759924210753 -0.012423599518033514 -0.002961710823443264] %
+
+Mass Used: 87.79561223924429 kg
+Launch C3: 100.82737920343641 km²/s²
+||V∞_in||: 7.172756741667448e-9 km/s
diff --git a/archive/ES_0.5793967339909301 b/archive/ES_0.5793967339909301
new file mode 100644
index 0000000..e52742e
--- /dev/null
+++ b/archive/ES_0.5793967339909301
@@ -0,0 +1,22 @@
+archive/ES_0.5793967339909301---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T08:54:17.874
+Launch V∞: [5.531392489970986, -8.270276102570921, -0.8650260486946956] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9170886107208164e-5, 0.012109964478508218, -0.005711700486438333] km/s
+ V∞_out: [-0.010679768168206899, -0.006344577605928621, 0.004997651126572138] km/s
+ time of flight: 1.4431472205863842e8 seconds
+ arrival date: 2027-11-19T16:19:39.874
+ thrust profile: [0.1890986417761532 -0.10907047409914768 -0.09756329892345623; 0.12032719354228198 -0.005765811704912608 -0.14018650283196796; 0.09910607196648481 0.01581171103724933 -0.17817821874140521; 0.09479248543836091 0.02755586974653568 -0.22438265950418357; 0.07191522516897275 0.026761436709134542 -0.20940761294140586; 0.056503894731896 0.024447702359343144 -0.1921423281171369; 0.037566977676371724 0.017495927873042695 -0.14555669263512472; 0.029973814821293857 0.014367279140071939 -0.12411632493650634; 0.009436159590342998 0.004277325330245943 -0.045865749026963595; 0.00022684138822698578 -1.2746136897867367e-5 -0.0016597241967174674; 0.0007100774131799473 0.00042144845427383507 -0.003912064309825176; 0.0002336241438572062 0.00021019888688433792 -0.0014318599605820503; 0.00033997380442104435 0.00013634680317885326 -0.0017252324578367118; -0.00012646020692163456 -3.281377557311162e-5 -0.0009700889001996681; 7.141640674211249e-5 0.00015127361732737547 -0.00039878141798412725; -6.71348235536571e-5 0.0002169036500536134 3.297542100935409e-5; 0.000315973246241769 0.0004000581781446589 0.00030001465259988736; 0.00030476511447085096 -0.00016987821606043418 0.0001215672640255325; 0.0008195487459172713 -0.000748137696421449 -1.086582158789243e-6; 0.0002262891986627338 0.00011389908220801783 -0.00013198099568017125] %
+
+Mass Used: 94.13429108068158 kg
+Launch C3: 99.74203975578345 km²/s²
+||V∞_in||: 0.01338938434201166 km/s
diff --git a/archive/ES_0.5794470854677934 b/archive/ES_0.5794470854677934
new file mode 100644
index 0000000..1b79211
--- /dev/null
+++ b/archive/ES_0.5794470854677934
@@ -0,0 +1,22 @@
+archive/ES_0.5794470854677934---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T21:20:52.944
+Launch V∞: [7.067809676193438, -6.993954213964277, -0.7373350551132598] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.288142941939324e-7, 2.1132101210478696e-7, 2.989307588449277e-8] km/s
+ V∞_out: [4.4306337257296263e-7, -2.7265579646821393e-7, -2.3298292366737287e-7] km/s
+ time of flight: 1.4106632241431877e8 seconds
+ arrival date: 2028-10-26T14:26:14.944
+ thrust profile: [0.24904438383678384 -0.08654844394153631 -0.11732980379318321; 0.15303512242614634 0.017782061318218523 -0.1842676804162164; 0.11423761521652531 0.035704657091672136 -0.2234252963472185; 0.1146969588322168 0.04939631493513425 -0.30235297203057504; 0.053715930991120785 0.0273074351909738 -0.18244880184028436; 0.04695643190504721 0.02633988127455983 -0.18808358971069597; 0.019525152919958013 0.011898074430474359 -0.09338760814425201; 0.00638270672485018 0.004463523013860648 -0.03580695387170394; 0.005387919604458136 0.004466371607870252 -0.031314017439485455; 0.0015522224258393863 0.00023682895609227037 -0.00963353627132407; 0.001766222458646165 0.0018959492375527872 -0.01941601995829201; 0.0015251402836733065 0.0003163411161394523 -0.0024919355666570085; -0.001936156998514453 0.001366737649839753 0.00047548387739359144; -0.0013959443418543518 0.0011736429440482457 -0.0003297449296688409; 0.00023546751619106583 0.0007194992297348073 0.001988040275326808; -0.00019661409428636876 -0.001774058924733402 0.0009411739972644778; -0.000884466749967553 -0.0018317016250718823 -6.547178928538574e-5; -0.0009104965324965228 -0.0012910326508532414 0.0020996708789304272; -0.0007479965150766593 -2.033760814088149e-5 -0.0006527048660243055; -0.0016690700991442702 0.0008220351820256231 0.001931624027948115] %
+
+Mass Used: 96.1124788408024 kg
+Launch C3: 99.41299214942113 km²/s²
+||V∞_in||: 5.702584711222223e-7 km/s
diff --git a/archive/ES_0.5795344756447628 b/archive/ES_0.5795344756447628
new file mode 100644
index 0000000..46fc761
--- /dev/null
+++ b/archive/ES_0.5795344756447628
@@ -0,0 +1,22 @@
+archive/ES_0.5795344756447628---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T13:48:06.631
+Launch V∞: [6.0669406398963055, -7.759657186109128, 0.0640477461009694] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006416607795842778, 0.00430112068947591, 0.00609297711604835] km/s
+ V∞_out: [-0.004061210174741114, -0.007446366773066009, 0.004984352531952256] km/s
+ time of flight: 1.7218566823247668e8 seconds
+ arrival date: 2028-10-11T11:09:14.631
+ thrust profile: [0.21673362390903603 -0.07744110877468914 -0.08313617296912364; 0.15670030393575282 0.023751713038616402 -0.1470201345288849; 0.07247067096692858 0.029616482146280484 -0.12409012801495878; 0.046943994016380365 0.0262547766921268 -0.10604332717380499; 0.0685521512144936 0.05056669865157187 -0.23025462357332904; 0.02403674387516536 0.01852851673556167 -0.07798500579025978; 0.02101219411088619 0.017629918910301922 -0.07842420209951305; 0.009882726358071112 0.008999631333777323 -0.04476088236625567; 0.012119817226886527 0.012551002290036011 -0.05994902223791042; -0.0025031581527064682 0.006064644770066605 -0.01757189888382593; 0.0058558635717178755 0.006698711700772424 -0.03377510473606565; 0.01053938312452212 0.006475236941622482 -0.016835059872113294; 0.005220389402329568 0.004571508269674725 -0.020319925019474085; 0.02916944166224789 -0.021095456046099872 -0.013831217820285551; 0.007733293038814603 -0.030620800439582947 -0.01352660132616211; 0.03469609291607862 -0.023061206993820513 -0.018830286937538805; -0.0022087390817151897 -0.05545376013077872 -0.04287517328254171; -0.0016721947291046656 0.013204797777018443 -0.0011839443398136357; -0.028529500623258614 -0.023714482523192647 -0.031080398284159972; -0.0011052536117194377 -0.002485150067375764 0.011722003811893573] %
+
+Mass Used: 110.14934374040058 kg
+Launch C3: 97.02415048774104 km²/s²
+||V∞_in||: 0.009838539776196309 km/s
diff --git a/archive/ES_0.5795438255441255 b/archive/ES_0.5795438255441255
new file mode 100644
index 0000000..384a2b1
--- /dev/null
+++ b/archive/ES_0.5795438255441255
@@ -0,0 +1,22 @@
+archive/ES_0.5795438255441255---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T10:18:08.312
+Launch V∞: [7.022460401878261, -6.762604197790711, -0.46907017836015946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005355064257843022, -0.0024807496017266277, -0.0030885052643645477] km/s
+ V∞_out: [-0.003492119029296246, -0.00041853958300954033, 0.0018992540124820882] km/s
+ time of flight: 1.427838074300244e8 seconds
+ arrival date: 2028-11-13T00:28:15.312
+ thrust profile: [0.5703912556059838 -0.17930935867203848 -0.23343541774118426; 0.2226335740148865 0.03990532620810227 -0.23983938493052046; 0.10515293213318189 0.042514931381790605 -0.186818718270995; 0.08719557761168857 0.04841328476382737 -0.21236036129932442; 0.061005806104946485 0.04049266652334854 -0.1868539102763339; 0.04331952271869879 0.03193454561933087 -0.15760246586849258; 0.022370991923728267 0.017839088416913805 -0.09263336938220024; 0.020222200725059244 0.01736198598635346 -0.0938049892371446; 0.008790752771622914 0.007668234605789446 -0.04397669792460698; 0.0026970130429723104 0.001059543264236842 -0.022781515186985086; 0.0009227877436286122 0.0006976090952723228 -0.004653260040750366; 0.001662879175588162 -7.747662930916895e-5 -0.009099146954439788; 0.0018774604301854355 0.0006072924693039682 -0.00942302663978032; 0.0008816935762173586 0.001772670667281233 -0.010610434529857386; -0.00022681922878933433 6.562739467011903e-5 -0.005533923018879052; 5.906367830852549e-5 0.0001354210482880933 -0.0027494625770136862; -0.0005432589614058549 0.0011588128469408095 0.0022145268022485867; 0.0018555763220186729 0.002612745155407228 -0.003767484372065268; -0.004101476416673196 0.005181257962599007 -0.004486481193287578; 0.003213207358122914 -0.003173555157873891 0.0011157992262540769] %
+
+Mass Used: 120.40567376059562 kg
+Launch C3: 95.26779246415157 km²/s²
+||V∞_in||: 0.003997468009444306 km/s
diff --git a/archive/ES_0.5796217493115632 b/archive/ES_0.5796217493115632
new file mode 100644
index 0000000..59ed6b3
--- /dev/null
+++ b/archive/ES_0.5796217493115632
@@ -0,0 +1,22 @@
+archive/ES_0.5796217493115632---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T06:14:46.996
+Launch V∞: [7.151995478836141, -6.822584666326157, -0.5382269856196428] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.2307555595598523e-7, -5.621209429955632e-7, 9.278623718780907e-7] km/s
+ V∞_out: [5.098596808992673e-7, 1.0117247891952288e-6, 3.094535483960216e-8] km/s
+ time of flight: 1.4541763630103838e8 seconds
+ arrival date: 2028-12-15T08:02:02.996
+ thrust profile: [0.31653980571266677 -0.09777866490728411 -0.13738607853866994; 0.13476402827899295 0.024180823435143977 -0.15701434034508022; 0.1049192098273638 0.04184180927570391 -0.19924320165581247; 0.08638540342847925 0.04661773370287552 -0.2243559820041236; 0.057128436253669666 0.03663891956519965 -0.18820470622680574; 0.044348072411167394 0.031921752114383146 -0.17461896005008978; 0.03196318317390978 0.025134558152577396 -0.14571489735537124; 0.010079722217646546 0.00796882006721309 -0.06285595569546269; 0.00425153884211499 0.003896757580506945 -0.023538422788946967; 0.0015005145875769872 0.0056105708447957954 -0.029154486991344673; 0.006341041599459814 0.004327812533435508 -0.048247712385134485; 0.0005981902893125144 0.0011360842205824292 0.002614834785255547; -0.0024101871317185634 0.0003348487042370335 0.0049459966267669945; -0.005365722094787007 -0.0021031524391384856 0.00896454050458552; -0.001409157844809627 -0.0018252871683870275 0.0051254652406891536; 0.0013584159320522763 0.004359797325544764 0.014029750617749925; 0.0011377904354169868 0.0010541406997111144 0.0015307837455271942; 0.0007315736224696416 0.0023414274152137103 0.004345776841930445; -0.014569188316070082 -0.007233641199135789 0.006079179217779573; -0.00030823717967524847 0.0005957836882865265 0.00023215939130669105] %
+
+Mass Used: 104.62643750872849 kg
+Launch C3: 97.98838914653061 km²/s²
+||V∞_in||: 1.1319391991435434e-6 km/s
diff --git a/archive/ES_0.5796492309368351 b/archive/ES_0.5796492309368351
new file mode 100644
index 0000000..2552800
--- /dev/null
+++ b/archive/ES_0.5796492309368351
@@ -0,0 +1,22 @@
+archive/ES_0.5796492309368351---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T12:29:21.237
+Launch V∞: [8.005630465698715, -6.334466439141111, -0.24207800042500519] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.04101032572144702, 0.2492734434648319, 0.3260519036631784] km/s
+ V∞_out: [-0.20127227526107408, -0.08551567335219944, -0.34895986880751007] km/s
+ time of flight: 1.8493649724165162e8 seconds
+ arrival date: 2030-04-01T23:44:18.237
+ thrust profile: [0.02119071672453966 -0.00366055795768086 -0.009093239845158111; 0.00973951994000963 0.001102395789645627 -0.012600465784867822; 0.016875351868427587 0.0017331321742317326 -0.04637401839892874; 0.025016408802473095 0.0015452829488248935 -0.0946543951580629; 0.038273268360075954 -9.258761729690943e-5 -0.17477176180892184; 0.02690018111745471 -0.0022200171784733185 -0.14044165904488645; 0.015809851005407542 -0.0028700950252101057 -0.09103436689160778; 0.011386333549873949 -0.0026757983713044265 -0.07135025971614385; 0.011408319530473004 -0.003295842238400197 -0.07266788180387021; 0.0009339215556577012 0.0009600588558692762 -0.007133349055961024; -0.0011774159389388687 0.0008530126626426267 -0.00750038983389252; 0.0038159134057053133 -0.0017209245893219317 -0.012844190293564697; -0.005200780731555963 -0.0017582614509397002 -0.0030352459017582954; 0.0009304640626801127 -0.00166158877598603 -0.0007653565539058778; -0.0038059135976201523 0.005167419573323588 -0.0016931174795542688; -0.008258546660243496 0.00937277004106048 0.003885476279860224; 0.004135172973307259 -0.002520887142959058 -0.004793712904566157; 0.03227149788730153 0.02525200312455396 0.01082182909234241; 0.012404992915077713 -0.008801622907773343 0.038881349880480025; 0.027681654366300865 0.004872801874892966 0.0070811959239107354] %
+
+Mass Used: 67.99135120836763 kg
+Launch C3: 104.27418598021826 km²/s²
+||V∞_in||: 0.4124668960231554 km/s
diff --git a/archive/ES_0.5796506328560878 b/archive/ES_0.5796506328560878
new file mode 100644
index 0000000..3ce2bed
--- /dev/null
+++ b/archive/ES_0.5796506328560878
@@ -0,0 +1,22 @@
+archive/ES_0.5796506328560878---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-10T11:06:29.008
+Launch V∞: [6.250641296007753, -8.052284577617042, -0.6198575815741556] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008025680067331333, -0.0009170187623377231, -0.0008180201768371968] km/s
+ V∞_out: [0.001015315263456814, 0.0004759771542418404, -0.0009483913444920614] km/s
+ time of flight: 1.840327442556374e8 seconds
+ arrival date: 2029-03-09T11:18:53.008
+ thrust profile: [0.08999979212525094 -0.04877150634080354 -0.05410366773106777; 0.00692003416516846 -0.0023425180395646498 -0.013796913675382515; 0.02448786330754831 -0.012361664437457209 -0.08349694215150323; 0.029871569111612137 -0.022496589767914854 -0.13808069376261461; 0.02621805777522408 -0.024049663879918484 -0.14575737163901806; 0.022363192528403412 -0.024070928738140845 -0.14145653939394087; 0.01742132724346234 -0.021081677156589828 -0.12183387628498143; 0.010838880871989169 -0.013832064961389116 -0.08171494786760135; 0.005437656246203927 -0.007371395980056038 -0.04332165096789438; 0.0006990073445156973 -0.0009990458303280056 -0.00578551334141063; 0.0007057034136268135 -0.0009972415373056816 -0.0061199716498891105; 0.00010116402400178695 -0.00018233142208166035 -0.0007957974327467812; 7.509094236890458e-5 -0.00011429907980393727 -0.000501980939315605; 0.00012076845040846556 1.6312851227914804e-5 -0.00029196209466485494; 2.5119353766322024e-5 -2.0397673590704063e-5 -0.0003681317908522543; -1.6611593632762962e-5 -4.0914453162875004e-5 -0.0003660751698094506; 9.65648269626046e-5 -7.226974955808674e-5 5.847570124790767e-5; 0.00024026358551695914 -0.00016845980559824911 -0.00014856982531196857; -1.068466989207044e-5 -1.3416547314875477e-5 -3.8213852486650385e-5; 0.0003503106018489363 7.359850319975687e-5 -0.0008155256324751897] %
+
+Mass Used: 67.87724778039228 kg
+Launch C3: 104.29402695172172 km²/s²
+||V∞_in||: 0.0014677178971531837 km/s
diff --git a/archive/ES_0.5796621974591047 b/archive/ES_0.5796621974591047
new file mode 100644
index 0000000..75e43ee
--- /dev/null
+++ b/archive/ES_0.5796621974591047
@@ -0,0 +1,22 @@
+archive/ES_0.5796621974591047---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T04:33:56.793
+Launch V∞: [6.89378367294568, -6.8227162456369275, -0.4909310916360749] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.316443401112998e-6, 3.378788526128071e-6, -1.6571022211331655e-5] km/s
+ V∞_out: [-7.840770737748893e-6, 1.4526483405443717e-5, -4.348523161543434e-6] km/s
+ time of flight: 1.427468019927147e8 seconds
+ arrival date: 2028-11-13T08:27:17.793
+ thrust profile: [0.6917821134128359 -0.21429438534389575 -0.2734793360967464; 0.20856547500817102 0.03796286172760161 -0.2269909739226687; 0.08408801391038431 0.03482216061003478 -0.15863407626603443; 0.08989735845809549 0.05227723915514856 -0.22065665609746943; 0.055936358021274495 0.04035920119024101 -0.17880475868797854; 0.043101281906464756 0.03166005619028742 -0.17143218062537005; 0.028227329601012978 0.022280963576327424 -0.12219005511312661; 0.014232902189106106 0.012477085935165957 -0.0862630588523348; 0.0062189390142792745 0.008405739952817091 -0.036233085533044815; 0.0005959508097560065 0.0036762042250562225 -0.013438631048217919; 0.0012742530883628252 0.0018807537835611437 -0.006357873365262902; 0.00015296929976533168 0.0014411378200980146 -0.009213272579133933; 0.0009511399984858256 0.0009602656565311474 -0.005029141636686426; 1.1503517748685452e-5 0.0004610376679201485 -0.006452294449980086; -0.0016086895567943619 -0.0011704214268190322 0.008988800255790984; -0.0006488993464818084 -0.0001652127627929592 -0.0050119949303822475; -0.0015538414269096919 0.0007591691202551601 0.005215949296225921; 0.0002864023616959867 -0.0003425000454716585 -0.002056046684126703; -0.004689647600551292 -0.003286091453540376 -0.0024819492949737457; 0.002334909008750609 -0.0026419955878559595 -0.012075586818806525] %
+
+Mass Used: 126.1033425005403 kg
+Launch C3: 94.31472363458548 km²/s²
+||V∞_in||: 1.7069882807544452e-5 km/s
diff --git a/archive/ES_0.579715778374203 b/archive/ES_0.579715778374203
new file mode 100644
index 0000000..0495180
--- /dev/null
+++ b/archive/ES_0.579715778374203
@@ -0,0 +1,22 @@
+archive/ES_0.579715778374203---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T14:12:13.801
+Launch V∞: [6.363023428283962, -7.877308084551952, -1.034921830364077] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.024027214084091e-6, -3.942144709540927e-6, -4.4726478451907645e-6] km/s
+ V∞_out: [-5.9938085684239805e-6, -3.970840713859935e-6, -1.235497050126975e-7] km/s
+ time of flight: 1.8749577781362566e8 seconds
+ arrival date: 2029-04-17T16:21:50.801
+ thrust profile: [0.0781271015066725 -0.030624042392952924 -0.04372978078483796; 0.017391542210242753 -0.001753660501979302 -0.030245413026646996; 0.062212679617929055 -0.003964523150609021 -0.17982072276995087; 0.02100542750747235 -0.002282870394489447 -0.0888889959038112; 0.01592317797487236 -0.0032110394368478875 -0.08326004631405888; 0.013403790993655594 -0.003609188704114566 -0.08304689227908883; 0.017338521875806662 -0.007047399227631979 -0.12720624776338943; 0.01252690006760253 -0.004947352876542577 -0.09396216331997867; 0.006388670875986006 -0.003923037569189383 -0.05199079443456034; 0.00029329592482307923 0.00010256215875314816 -0.002501501848649824; 0.0015753978958598207 0.0021373756823550812 -0.0026709528893844423; 0.0038365348840048667 -0.0005008080892076187 -0.019000540976541934; 0.004209700007538108 -0.00376124471496946 0.00135057308348332; -0.004415751940652786 -0.0009937446625664411 -0.0003685587457708428; -0.00134951136038139 -0.0023415477904718067 -6.777083167637792e-5; 0.013630700226673832 0.0033203417219983835 -0.012126233211479438; 0.003655821324569764 0.01533065425222432 -0.0018650527582333343; -0.00614967423165632 -0.009399900020367698 -0.01628573462614586; -0.0009415498008449505 -0.00315876609476819 -0.00296066278653253; 0.003946004034737669 0.004397443612299929 -0.007923919049525238] %
+
+Mass Used: 71.93691558689034 kg
+Launch C3: 103.61111300280226 km²/s²
+||V∞_in||: 7.1929047454933306e-6 km/s
diff --git a/archive/ES_0.5797414254689287 b/archive/ES_0.5797414254689287
new file mode 100644
index 0000000..81b8d8a
--- /dev/null
+++ b/archive/ES_0.5797414254689287
@@ -0,0 +1,22 @@
+archive/ES_0.5797414254689287---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T00:34:37.331
+Launch V∞: [5.440391296388288, -8.314223608436416, -0.8298418540797984] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0023751972489426103, -0.014959242347813791, 0.020367892791720955] km/s
+ V∞_out: [-0.017485062746047973, -0.014548440945931105, -0.011262509576198105] km/s
+ time of flight: 1.4604280610241172e8 seconds
+ arrival date: 2027-12-11T08:01:23.331
+ thrust profile: [0.2595439724364839 -0.15210717634850804 -0.13308260650866593; 0.05369857838357782 -0.004021059902246337 -0.06770243496452696; 0.09550483628790457 0.010741293256350072 -0.180865690033258; 0.10831386572806365 0.02420581597305628 -0.2709785324707188; 0.058464581622268835 0.016393021643569337 -0.18138685121053333; 0.0394597791339591 0.013180375659554983 -0.1463238799021537; 0.03476997522822265 0.011123399992618997 -0.14240801456104316; 0.025511079778748596 0.008972964411306985 -0.12080905568038935; 0.006439004989190774 0.0027847010326492224 -0.034419842073538466; 0.0028445773257431413 0.0014506738843933858 -0.015133099778728778; 0.0012016791172453818 0.000499049330996162 -0.007630509511892457; 0.008327985445314783 0.004018724215994949 -0.050871143218317844; -0.0005350106094376844 0.001572919086344844 -0.001986539872353676; 0.0006969401931796113 -0.0007935495435006531 0.0007332816739879463; 0.0006910457086260642 -0.0004989334276761896 -0.002550679918657072; 0.0005138854606585156 0.00012269996988205833 -0.003339611878770654; 0.0009577503801856563 0.0018672053768751262 -0.0009000146300096675; -0.0007741850091123828 -0.004559511025218201 0.0016603282352678132; 0.0005581223499820133 -0.00017029821097606652 0.0003421599531824729; 0.0014890041085385336 -0.0012913579585608161 -0.0028979414347973095] %
+
+Mass Used: 96.45694287894139 kg
+Launch C3: 99.4128091716815 km²/s²
+||V∞_in||: 0.02538250480876638 km/s
diff --git a/archive/ES_0.5799012666600933 b/archive/ES_0.5799012666600933
new file mode 100644
index 0000000..21e4e47
--- /dev/null
+++ b/archive/ES_0.5799012666600933
@@ -0,0 +1,22 @@
+archive/ES_0.5799012666600933---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-10T08:35:56.759
+Launch V∞: [6.418246193071689, -7.932634155018398, -0.35622665514621754] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.621262016084342e-7, 3.711516914913256e-8, -4.6274522868367956e-8] km/s
+ V∞_out: [1.6716131569798676e-7, -1.5416662197314184e-8, 2.1234246066835845e-8] km/s
+ time of flight: 1.8749577781528902e8 seconds
+ arrival date: 2029-04-18T10:45:33.759
+ thrust profile: [0.010723314231033372 -0.004937037777902451 -0.006295025502478851; 0.01605157291615773 -0.0009557986757975654 -0.02608026096731824; 0.0145032577757752 -0.0027778029776238822 -0.04227905137119655; 0.03679156888264439 -0.009394048616824555 -0.1458893150490177; 0.04410784456097437 -0.015801533606387724 -0.213995841021135; 0.034393904676827916 -0.01577509787721254 -0.1934149117992598; 0.012599766953189526 -0.007038810597299269 -0.07926713883916346; 0.004120562363923767 -0.0024519170233533627 -0.027841163059672075; 0.001390773541304435 -0.000289873578226824 -0.008286127634705574; 0.004745353537725803 0.0010620480269922844 -0.00152578875409045; 0.0018139107160500775 -0.0015496388569596652 -0.020964050434654793; -0.001296312124520871 -0.0007793320599157761 -0.002230264596629458; 0.0014302437158146182 -0.00032507076257590634 -0.006396432326563742; 0.0023115886813038357 -8.406360285547355e-6 -0.010172890948993606; -0.002808556231814918 0.001507375205262466 0.007422088071476672; 0.0010632290243513878 -0.0009962337772537863 -0.00995336972714647; -0.0032653579146380363 -0.008642792966254293 -0.020296876001358977; 0.012845839144213568 0.010095506284905817 -0.02348174651671977; -0.004089912900780484 0.0023595740348514253 0.005440100430686831; -0.003135159027235466 0.005561456828394398 -0.02069587861261298] %
+
+Mass Used: 68.44125790797352 kg
+Launch C3: 104.24746626208035 km²/s²
+||V∞_in||: 1.7263769141077647e-7 km/s
diff --git a/archive/ES_0.5799292619774761 b/archive/ES_0.5799292619774761
new file mode 100644
index 0000000..4cbbe48
--- /dev/null
+++ b/archive/ES_0.5799292619774761
@@ -0,0 +1,22 @@
+archive/ES_0.5799292619774761---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T13:42:18.941
+Launch V∞: [5.366808483495529, -8.112258423897265, -0.2920817899718737] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.4725449195505305e-6, 8.095627946119192e-7, -1.0157706994371118e-6] km/s
+ V∞_out: [3.261895818650556e-6, -1.393071246179639e-6, 6.218819708013327e-7] km/s
+ time of flight: 1.4456253332622838e8 seconds
+ arrival date: 2027-11-20T17:57:51.941
+ thrust profile: [0.5046249832628936 -0.297105284237052 -0.22596248183315387; 0.19964259613720559 -0.009679231220672916 -0.20881141301878253; 0.17207941932429277 0.027494752223084465 -0.278766169815006; 0.13069097159252877 0.03703164926297258 -0.281500326552457; 0.09490482184895026 0.035121853327172145 -0.2513694044215174; 0.051456137606579445 0.022731404306844886 -0.1613074200077124; 0.007816398480294261 0.004458404542938351 -0.029260400836522146; 0.0076332054597778995 0.0039049804587880273 -0.03381579437511879; 0.0033989955873326753 0.002934016146080676 -0.015409728926748885; 0.005642305779538939 -0.002964452517226595 -0.008579760399451106; 0.0026419597135903298 0.002163430327375766 -0.014555812340976722; 0.000811714071117438 -0.0008731944069847318 -0.0019170897517031722; 0.003139515878208117 0.002307800930688966 -0.014130820138677044; -0.003204037666156068 -0.00686838251762161 0.0019308540635754627; -0.002475565390601556 0.0018003724937232294 -0.0018804680335171792; 0.004025333190329785 0.0015000046780270192 4.662485451225988e-6; 0.0025285354492446907 0.0017318085288072654 -0.002754851367110499; -0.000813492975348807 8.557436358306463e-5 -0.004245193158423631; -0.00018360039507108773 0.006255075681450055 -0.0004658330180714902; -0.000653457522871131 -0.0012551892180267333 -0.0026512059431256707] %
+
+Mass Used: 124.18682843496026 kg
+Launch C3: 94.69668180664489 km²/s²
+||V∞_in||: 3.7075261631647346e-6 km/s
diff --git a/archive/ES_0.5799524146903313 b/archive/ES_0.5799524146903313
new file mode 100644
index 0000000..ffa1084
--- /dev/null
+++ b/archive/ES_0.5799524146903313
@@ -0,0 +1,22 @@
+archive/ES_0.5799524146903313---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T04:07:25.437
+Launch V∞: [7.137270553651459, -6.917509999725683, -0.8006777826640279] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0014582439500406507, 0.0011290981856095493, -0.000775382576098826] km/s
+ V∞_out: [-0.0008038981272724851, 0.0018304902364899814, -7.636890869026077e-5] km/s
+ time of flight: 1.4098499355938056e8 seconds
+ arrival date: 2028-10-24T22:37:18.437
+ thrust profile: [0.2786051627815852 -0.0974110875315996 -0.12820780007131627; 0.09896610989869573 0.011814464860867652 -0.11838221940520156; 0.1152702059077138 0.03647762290055527 -0.22050367317744027; 0.10699646102779713 0.046803558934525015 -0.2779813759812958; 0.07654735028125771 0.03922663450477732 -0.24947892615151088; 0.03670879299703466 0.020997816059876745 -0.14557591968309352; 0.018698396358687256 0.011936704331125213 -0.08635505413061013; 0.01148660304277094 0.007690568548260503 -0.05680764857278006; 0.003177097321969297 0.0029452419363602263 -0.014275265254261992; 0.0008203965393926364 0.0005534868554605947 -0.0028820152000722833; 0.01586538079010287 0.009542162474238801 -0.08720670445184707; 0.000341715546761367 0.0001542205166332585 -0.002308466825637024; -2.5185433138458745e-5 0.0012915482690792513 -0.0030257909693783896; 1.641694790203326e-5 0.0005450243175464053 -0.001544272711797368; 0.002860904385098643 -0.000397818272652788 -0.003234382210092876; -7.03355687747105e-5 -2.1685183317718366e-5 0.0016226374469246853; -0.00021961680508875698 -0.0019073253713812717 -0.0001001563047101902; 0.00012910363145885448 0.00024646817075855607 -0.000992145205101826; -0.00032553654740692987 -0.0007675256210307593 -0.0007108039353492324; -0.00023843299257227197 0.0005131671948210494 -0.0033227946285485956] %
+
+Mass Used: 96.58146443218857 kg
+Launch C3: 99.4336604639768 km²/s²
+||V∞_in||: 0.00200063896540445 km/s
diff --git a/archive/ES_0.5799906946727426 b/archive/ES_0.5799906946727426
new file mode 100644
index 0000000..ca9212f
--- /dev/null
+++ b/archive/ES_0.5799906946727426
@@ -0,0 +1,22 @@
+archive/ES_0.5799906946727426---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T18:18:47.698
+Launch V∞: [5.352142288420842, -8.38904556643382, -0.9474565550465948] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0026088676466228876, -0.01626826624246186, 0.020736566431037454] km/s
+ V∞_out: [-0.018480561864987415, -0.01513764801798445, -0.011467546492717367] km/s
+ time of flight: 1.448721559734599e8 seconds
+ arrival date: 2027-11-28T12:34:42.698
+ thrust profile: [0.24218590552951147 -0.14978266390692002 -0.13445730479687143; 0.10160973197730211 -0.011311616352308623 -0.13252418557575718; 0.10359404883572944 0.006232447929948226 -0.21249748291764098; 0.08520101136257223 0.0128585527623341 -0.2354142547028152; 0.0556319559420563 0.011426170508721602 -0.19045351168483468; 0.051860784301823 0.013604119015603329 -0.21208412349748762; 0.024624337005752932 0.007284667390061691 -0.11290503683450917; 0.00561089638635311 0.0014113691907479135 -0.034287674292815526; 0.003593551961957082 0.0006147254794943537 -0.02083226992145464; 0.005294847162523887 -0.0006704508823842385 -0.03326803892791507; 0.001538964872257161 0.0011156089511665072 -0.015947445465417837; 0.000975961714898577 0.00042573761392187415 -0.007233408920685677; -0.0005137863979312665 -6.331683426725012e-5 -0.0022437750839849587; 0.0003679467083133357 -0.00021840288312481625 -0.0002551090439697982; 4.4461206264341524e-5 -0.00010751497930576214 0.00015813889999950585; 8.780005698293944e-5 0.0006080339115673251 -0.0008531807467248199; -0.000496980035743849 0.00014606064799790527 -0.001238434504870629; 0.0027234571822056554 -0.0004901573322540414 -0.0016150661019663157; 0.0007988528637357844 6.379601959162639e-5 -0.000950439410377596; -0.00012309349130213077 9.480948664767559e-5 0.0003103999693223191] %
+
+Mass Used: 93.79388911457909 kg
+Launch C3: 99.91918651490639 km²/s²
+||V∞_in||: 0.02648523861100838 km/s
diff --git a/archive/ES_0.5800648685448135 b/archive/ES_0.5800648685448135
new file mode 100644
index 0000000..b2da16a
--- /dev/null
+++ b/archive/ES_0.5800648685448135
@@ -0,0 +1,22 @@
+archive/ES_0.5800648685448135---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T09:13:15.574
+Launch V∞: [5.390657861244651, -8.159439972339873, -0.36582332582923016] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.469200750406346e-9, 3.4378369230173425e-10, 4.076226117683742e-9] km/s
+ V∞_out: [1.471958626080491e-9, -3.4112995350368245e-9, -4.753351914576585e-9] km/s
+ time of flight: 1.4525152168595165e8 seconds
+ arrival date: 2027-11-29T12:51:56.574
+ thrust profile: [0.42951997919932966 -0.24759428420941518 -0.1952698227955626; 0.20513845453401736 -0.00868829238547675 -0.21737305930847825; 0.10068015964033003 0.01737928583561897 -0.1660437767304761; 0.12333231119635098 0.035938614377574715 -0.2687564299472987; 0.07606943150032128 0.029131697763135612 -0.2040034097127694; 0.06678564462885496 0.02986378025261624 -0.20940568328043432; 0.025251321331507325 0.012870129440741333 -0.09198866902037313; 0.016632905459760462 0.007819282422148535 -0.06322453673749792; 0.0020966509352056332 0.001943657854148542 -0.01143218443064173; 0.004397744895319112 0.0035792776790749183 -0.02803876232723906; 0.0035327611193740798 0.0023339506843039416 -0.021099365528616815; 0.0009716453074221922 -0.00016104103369052845 -0.00288145270098155; 0.0014029579150131918 0.0023908217513053066 -0.0013440499971406371; 0.0016597864215965469 0.000818193849324684 0.0024500652973332444; 0.001737703912887726 -0.005584785171689529 -0.0009524333408750295; -0.0007995740903066029 -0.004980136542614881 -0.007233935057717206; 0.0022530695914558642 0.00226307117744744 -0.007620455193973266; 0.004451313170488967 -0.0011550252618536129 -0.0015243619569737805; 0.0009060025352368903 0.0009522937793694265 -0.002417955834422974; -0.008336671107449197 0.007691302610916882 -0.0029082070672245583] %
+
+Mass Used: 118.08704929014857 kg
+Launch C3: 95.76947954493723 km²/s²
+||V∞_in||: 6.058676582968622e-9 km/s
diff --git a/archive/ES_0.5800687962528306 b/archive/ES_0.5800687962528306
new file mode 100644
index 0000000..ad60cc2
--- /dev/null
+++ b/archive/ES_0.5800687962528306
@@ -0,0 +1,22 @@
+archive/ES_0.5800687962528306---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-07T03:10:41.708
+Launch V∞: [6.281183429507368, -7.878931124421101, -1.400464575522654] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001061613127127569, -0.0011536200461842142, -0.0010329392340888786] km/s
+ V∞_out: [0.0011986730080542315, 0.0005488630986208615, -0.00133755260134135] km/s
+ time of flight: 1.8298006165226775e8 seconds
+ arrival date: 2029-02-21T22:58:22.708
+ thrust profile: [0.07076120488823719 -0.02906794728248677 -0.03946062455386967; 0.0285759759647629 -0.0013966996332374203 -0.05051762224497929; 0.02434713854056778 0.0008845196127879533 -0.0742186750552345; 0.03837599457439048 0.0016412469114777614 -0.15671888068262907; 0.03239668268478943 0.00029902484995357806 -0.16864116191650436; 0.020896367265778364 -0.0005149397627533664 -0.1330875665558243; 0.012810559517673445 -0.0008018763777694528 -0.09722538789436994; 0.006401569311455197 -0.0008213613324409407 -0.056672087839719915; 0.0032792171938973136 -0.0007423822643061293 -0.032377788112147865; 0.001321958131071138 -0.0010201429965822758 -0.02040973755917266; 0.0010591498716337954 -0.00040408730601081036 -0.004718607244274977; 0.0036458545991137417 -0.0008863177749555938 0.001689108785346752; -0.009828576727167549 -6.405271733142115e-5 0.0014870659894607773; 0.0025971730711952063 0.005525789302874815 -0.003942535526133245; 0.002164739784240171 0.0026202164574680113 0.002744979852578345; 0.0028987045285868256 -0.011302001878641384 0.009416041815914412; 0.0029672535203735784 0.017760462252300248 -0.015427426447325903; -0.0014890131151829736 0.0006877115861184357 -0.00441190611995983; 0.0014699004575112842 0.008494583243471097 -0.002964855207442894; 0.00986517161475774 -0.011080037744964341 -0.015195231680097749] %
+
+Mass Used: 73.0428841612329 kg
+Launch C3: 103.49212196578333 km²/s²
+||V∞_in||: 0.0018774517580933373 km/s
diff --git a/archive/ES_0.5800689299700075 b/archive/ES_0.5800689299700075
new file mode 100644
index 0000000..0075049
--- /dev/null
+++ b/archive/ES_0.5800689299700075
@@ -0,0 +1,22 @@
+archive/ES_0.5800689299700075---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-10T08:43:38.608
+Launch V∞: [6.516851255442644, -7.768626277924343, 0.5462996874630618] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008571305533013674, 0.005320846625293723, -0.007556551688696792] km/s
+ V∞_out: [0.00577136191081862, 0.005366366842853193, 0.004914270238047049] km/s
+ time of flight: 1.8749577781413805e8 seconds
+ arrival date: 2029-04-18T10:53:15.608
+ thrust profile: [0.09784939225356239 -0.06102727772189372 -0.055484779483834075; 0.04013696381913552 -0.0268784067108107 -0.08574823513436163; 0.023361284690516577 -0.02371741128404393 -0.0861354485707763; 0.028763700289821195 -0.04136326923693718 -0.13882129000599708; 0.0244842974695379 -0.04016975722253468 -0.13579186690465098; 0.018822072962608676 -0.03242850527184326 -0.1147288717687876; 0.015659741301544614 -0.027742780337934182 -0.09909571347158709; 0.011726602885025595 -0.021344964202021345 -0.07703283550136508; 0.007777022965218061 -0.014575535473196356 -0.05255345736303811; 0.0036387027175494788 -0.007037640064390109 -0.025154372922089753; 0.0008992781580597526 -0.0017464892320586845 -0.006081540545865193; 0.00033833268084422334 -0.000585997178125846 -0.00231248765094427; 1.4048059391730952e-5 -2.344956034780622e-5 -0.000165510225560116; 1.294057627956112e-5 -1.9051956021501944e-5 -0.0001232916850977887; 7.601313410162961e-5 -0.0002264752508691726 -0.00026276404781561135; -1.835088176483679e-5 8.607562214386292e-5 -4.177461096007142e-5; 8.559359596742609e-5 -1.3776348420616589e-5 -4.8427108073110386e-5; 5.1244546191142566e-5 -0.00018596017508587577 -0.00025494260177678257; 4.546056881122861e-5 -0.00016870456406735136 -0.00011390062008707528; 0.0001117006095468363 -1.7933513718237247e-5 7.420555611819038e-5] %
+
+Mass Used: 75.21755566417323 kg
+Launch C3: 103.11934788014324 km²/s²
+||V∞_in||: 0.009281570719401359 km/s
diff --git a/archive/ES_0.580109069641464 b/archive/ES_0.580109069641464
new file mode 100644
index 0000000..1049c90
--- /dev/null
+++ b/archive/ES_0.580109069641464
@@ -0,0 +1,22 @@
+archive/ES_0.580109069641464---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T07:16:27.318
+Launch V∞: [5.345381797786032, -8.207258352448884, -0.5430201215701621] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.03174486671874e-7, 2.561451046830581e-7, -5.462649007879274e-7] km/s
+ V∞_out: [-1.7834630452151934e-7, 4.0063383385263246e-7, 7.2303078481549e-7] km/s
+ time of flight: 1.4319069083456668e8 seconds
+ arrival date: 2027-11-05T14:27:57.318
+ thrust profile: [0.3953868839918257 -0.23254921556577793 -0.1841108043976837; 0.23395211830252377 -0.012076100026312937 -0.2510420810945401; 0.16124726043393403 0.025241809585661926 -0.2681482207403775; 0.10103050724670999 0.028308425580796742 -0.22497078823498404; 0.08056097577040362 0.02960323809854991 -0.2204544646135232; 0.04503069980889954 0.01956156447155374 -0.14611282053267505; 0.020194224478401253 0.009716826605867675 -0.07504422478437979; 0.005368549164616183 0.0026550015110737286 -0.022038495567514985; 0.01785553070584856 0.009788133636506671 -0.07937677251618132; 0.0018946368660205867 0.0012286743903296331 -0.007506125574614628; 0.0023455065838330815 0.0013349281125765375 -0.01178539917752348; 7.369577844084773e-6 0.001746782676987324 -0.008914609537068512; 0.0005114102480713398 -2.799882020055076e-5 -0.003652057913592996; -0.00011995281819282728 5.3765107235967716e-5 -0.002551125541616459; 0.0006007906745173575 0.0003011559819959749 -0.0028244504487827263; 0.001955395028225537 0.0001898611079912889 -0.002636861125404764; 0.0003321245777203345 -0.0005410126358427548 -0.0010902584044311572; 0.00031405899435910664 0.0008877875411559869 -0.003956004150688757; 0.00035971230897167603 0.0002788842492146052 -0.0020270481354864476; 0.0005037905853568701 -0.001615628118080578 0.002114675823313753] %
+
+Mass Used: 115.46935661285806 kg
+Launch C3: 96.22706708037428 km²/s²
+||V∞_in||: 8.531325324108896e-7 km/s
diff --git a/archive/ES_0.5801211226210808 b/archive/ES_0.5801211226210808
new file mode 100644
index 0000000..070b514
--- /dev/null
+++ b/archive/ES_0.5801211226210808
@@ -0,0 +1,22 @@
+archive/ES_0.5801211226210808---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T13:38:48.670
+Launch V∞: [5.302605149911874, -8.218825679790989, -0.4668379876977658] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011692341116164453, 0.07148060378797041, -0.07731345225969566] km/s
+ V∞_out: [0.07452035677412398, 0.06312683622474786, 0.04104146450976614] km/s
+ time of flight: 1.4292914616112065e8 seconds
+ arrival date: 2027-11-02T20:11:14.670
+ thrust profile: [0.4712044049652023 -0.2694456475761444 -0.21246995278848493; 0.19353072586855471 -0.006844438787866022 -0.20928356699912076; 0.13947729110746457 0.025886347275277544 -0.23474573314322997; 0.07729784320896303 0.02365505820264268 -0.17520445881158137; 0.05739886307897385 0.022337186893060357 -0.15897172312009036; 0.06197909439827382 0.029764638305234386 -0.2017853410168003; 0.036145359534565456 0.01849287305524353 -0.13270369183484745; 0.02353204091285588 0.012504358043306841 -0.09401306954704879; 0.019914353182105236 0.011642426668136117 -0.08793069392955306; 0.0018077864878969462 0.0010701448015197309 -0.008965416133435879; 0.000979266986225727 0.0006581950349713077 -0.005657916995463751; 0.00012096189839219334 7.307642637747722e-5 -0.000553847775454359; 9.348668371712403e-5 -2.9471221439376753e-5 -0.00040570768371493753; 2.7974067422201503e-5 3.4286811510073905e-5 -0.00033351180198376617; 1.7273779809015804e-5 -0.00033160565171592266 -1.842230997421647e-5; 4.6521689253028456e-6 -4.8003306110080014e-5 -0.00011006769398290105; 0.00014385585724956964 -7.996490944519615e-5 0.0002872217276590149; 3.917639439083629e-5 -7.164688406156904e-5 -0.00020307776434588646; -1.685638266457829e-6 -5.937289627912847e-6 -0.0002413583236754984; 7.075519822885595e-5 7.923539388058484e-5 -0.0003068946383750679] %
+
+Mass Used: 117.480824339636 kg
+Launch C3: 95.88465463742143 km²/s²
+||V∞_in||: 0.10594129251138008 km/s
diff --git a/archive/ES_0.580122799518188 b/archive/ES_0.580122799518188
new file mode 100644
index 0000000..795e32d
--- /dev/null
+++ b/archive/ES_0.580122799518188
@@ -0,0 +1,22 @@
+archive/ES_0.580122799518188---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-11T15:44:00.852
+Launch V∞: [6.3732180734128505, -7.9972101476741475, -0.6356298129699887] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.642270316907093e-6, -3.3296060427741097e-6, -3.474717849460343e-6] km/s
+ V∞_out: [-4.644344606067139e-6, -3.855393810490989e-6, -1.183985127605171e-7] km/s
+ time of flight: 1.8749577784347787e8 seconds
+ arrival date: 2029-04-19T17:53:37.852
+ thrust profile: [0.06011787073180791 -0.030174744342088968 -0.0361353375276846; 0.007340234900683652 -0.0025194241641637092 -0.014928753892675187; 0.026227405666282053 -0.014898169940539259 -0.09223709501187703; 0.025200313659731632 -0.020239248527069965 -0.12335374795479838; 0.024128728440454637 -0.02494304048468486 -0.14289107263990047; 0.019680271858743506 -0.023881809939648307 -0.13401081581680419; 0.013705486646440626 -0.018076827411433787 -0.10433291021213191; 0.008845893473387776 -0.01269787500526143 -0.07265307068353691; 0.004143201424752097 -0.005954498864547792 -0.03726087037129868; 0.0036497858620990263 -0.004811132067347433 -0.03184226348683127; 0.0009876269987263882 -0.0012785927034103463 -0.0077019054111610715; 3.871255949279962e-5 -5.4724010979441734e-5 -0.00030687378092633357; 3.5736932024335135e-5 -2.344781942453297e-5 -0.00011981332219323425; 5.352191995382589e-5 -0.00010876916687715366 -0.0001530062415799787; 9.116893011184817e-5 4.055568358051718e-6 -0.0002945051533483553; -4.311886056167807e-5 -0.00011135236854852896 -9.529941983864554e-5; 4.603649678445643e-5 -2.8962548435259824e-5 -0.00012488046543493876; 4.161765779812747e-6 5.1094288851974006e-5 -6.392119435094368e-5; -3.367400209018433e-5 4.403152750239399e-5 -0.00018385337790390632; 1.58589647898886e-5 3.7119079586764704e-6 -2.115904762464854e-5] %
+
+Mass Used: 64.44232600844953 kg
+Launch C3: 104.97730401647482 km²/s²
+||V∞_in||: 6.0354016929164435e-6 km/s
diff --git a/archive/ES_0.5801427012524663 b/archive/ES_0.5801427012524663
new file mode 100644
index 0000000..600a527
--- /dev/null
+++ b/archive/ES_0.5801427012524663
@@ -0,0 +1,22 @@
+archive/ES_0.5801427012524663---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T13:59:25.899
+Launch V∞: [5.8251294137970335, -7.388588856385686, -0.025972745748859244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.7302931963911236e-8, -2.025376012537505e-8, 4.0956582392945056e-8] km/s
+ V∞_out: [1.660505071195145e-8, -3.684687300131678e-8, -5.0868253674735435e-8] km/s
+ time of flight: 1.807816285122986e8 seconds
+ arrival date: 2029-01-15T23:06:33.899
+ thrust profile: [0.8049081702420993 -0.22718943063238817 -0.21205405619042475; 0.2638453541524701 0.07923332415441432 -0.20847938775002225; 0.10571208274587397 0.06273280362996596 -0.14308065334612458; 0.14220516730135083 0.11803794672971007 -0.25989484144831043; 0.024285438646580976 0.02427207969374527 -0.062071168315570656; 0.014418250055883944 0.015990232218146147 -0.044410447232521924; 0.005251363094299736 0.005074963572506256 -0.015333873603839174; 0.00967067805117536 0.014612384020808167 -0.04603076400620507; 0.004290488988694987 0.005588337821049941 -0.01384842776956616; 0.004256958221013346 0.007288111584530542 -0.02281244560921783; 0.009771737244033869 -0.018373516016116295 -0.023824913175444648; -0.001507176233958983 0.00938054865856864 -0.004484938234308335; 0.002149059922221692 0.004785467831188407 -0.0002804662818795572; -0.004570129359916352 0.004393397890249486 0.012490346653741592; -0.0022898327048771357 0.0027010764049981133 -0.00895059976956644; 0.003316348241067254 0.03794380503848627 -0.027893385341724114; -0.00020068348826855596 0.027425601580222878 -0.04172044120127053; 0.0008687360429767323 0.0026006919462561217 -0.00890041208134142; 0.0529099423579866 0.009745480098092299 -0.015825363074238933; 0.022884795715777024 0.011373729703646161 0.04647491221583374] %
+
+Mass Used: 160.44284486289143 kg
+Launch C3: 88.52405255971185 km²/s²
+||V∞_in||: 6.576643378585115e-8 km/s
diff --git a/archive/ES_0.5803161645002375 b/archive/ES_0.5803161645002375
new file mode 100644
index 0000000..c562239
--- /dev/null
+++ b/archive/ES_0.5803161645002375
@@ -0,0 +1,22 @@
+archive/ES_0.5803161645002375---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T08:51:38.040
+Launch V∞: [5.433869192981077, -8.111679586239617, -0.3739273216477779] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00848724689035086, -0.0539644729917105, 0.055767162708439115] km/s
+ V∞_out: [-0.05439053035305224, -0.04779060123565188, -0.030605604683224416] km/s
+ time of flight: 1.442320260390706e8 seconds
+ arrival date: 2027-11-16T17:18:44.040
+ thrust profile: [0.49768058360634554 -0.28391951250881475 -0.21598612158389935; 0.12407211750765482 -0.004199517925208812 -0.13230232104015524; 0.14826015497224726 0.02697170846058123 -0.24559126110155804; 0.16061532463279338 0.05079308440001512 -0.34389884955071026; 0.06467756144414948 0.026824260893456645 -0.17686943956931436; 0.05785465664700446 0.026710659702854918 -0.18862529366048023; 0.040202370349758564 0.019717000362262406 -0.14352579853274317; 0.005368976606692943 0.0027527530502714195 -0.02203335996152515; 0.00097526790649308 0.0005493904092133163 -0.005883500946187111; 0.0011956168509888734 0.0005157545828706565 -0.00593595126490279; 0.0009373229454321852 0.0014984563589594986 -0.008248642795711325; -0.0009154748255084136 0.00024834809070979814 0.0014806883605390838; -0.00023158582086777444 -0.0002505010708999661 -0.00017118690711487262; 0.001309733915412132 -0.00044181578883186856 -0.0017912729280837034; 0.003792786761116975 0.006653010582067312 -0.001811464265938982; 0.001187880992291349 0.0003942886109566217 -0.0007921268720018581; -0.0007081662899897706 0.00043371235462789026 -0.0016512522539854641; 8.54407834570426e-5 0.005763811811001191 -0.011647639677712613; 0.0019261852287296506 0.002474584727701918 -0.004543908607163106; 0.005704092910862985 0.0018738557347930062 -0.008088610678967564] %
+
+Mass Used: 120.1499316612435 kg
+Launch C3: 95.46610175812003 km²/s²
+||V∞_in||: 0.07806519161316613 km/s
diff --git a/archive/ES_0.5804516244468247 b/archive/ES_0.5804516244468247
new file mode 100644
index 0000000..c9aa4d9
--- /dev/null
+++ b/archive/ES_0.5804516244468247
@@ -0,0 +1,22 @@
+archive/ES_0.5804516244468247---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T10:00:13.435
+Launch V∞: [6.9654059839369555, -6.813285373807051, -0.2364279315934523] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.031369094299183914, 0.016799555224414172, 0.002143020207411015] km/s
+ V∞_out: [-0.027829859041698022, -0.014228029298107268, 0.016893917855076053] km/s
+ time of flight: 1.4195443514376628e8 seconds
+ arrival date: 2028-11-03T09:47:28.435
+ thrust profile: [0.5594957784020969 -0.1779218177392156 -0.22000073288769242; 0.24086668058901567 0.041637628839487524 -0.24869483465632686; 0.12356131317731678 0.04882388439071799 -0.20953441273644813; 0.1088973601222775 0.05972267142466917 -0.2518778536137993; 0.08830932444744623 0.05808056726920752 -0.25457369923748935; 0.042092704491788396 0.030157757043166533 -0.14414474992806334; 0.011373516973653006 0.010100786133178554 -0.05056265221936286; 0.024869794337828446 0.02055670444051016 -0.1101755490846212; 0.0016142346758095249 0.0030866736173336606 -0.011415385098030598; 0.003602715668724432 0.003281059169008524 -0.020805098302150434; -0.00016512544186454573 0.0014319141447174922 -0.005679607097199135; -0.00024789599532125156 -0.0002323479646797775 -0.0008495322804723832; -0.002071829736649166 0.0008951671091083697 0.001536591439597351; 0.001425631945286289 -0.001211987515707778 0.0001645363263548423; 0.0011360082263294296 -0.00039685058357112135 0.003883758171903678; 0.0005146512187805507 -0.0026688943109459693 0.00357262521507221; -0.0004674396757435911 -0.001334285244502854 0.0010430768774240345; -0.003143278597743395 0.002077169461496465 0.0024084905501929126; 0.0008423815400406197 0.0014553486397026459 0.00790972517567352; -0.00481580280216598 0.0032660062935905188 -0.006298605234466629] %
+
+Mass Used: 123.06401692975578 kg
+Launch C3: 94.99363627283539 km²/s²
+||V∞_in||: 0.0356488101975172 km/s
diff --git a/archive/ES_0.5805238035096224 b/archive/ES_0.5805238035096224
new file mode 100644
index 0000000..9271a60
--- /dev/null
+++ b/archive/ES_0.5805238035096224
@@ -0,0 +1,22 @@
+archive/ES_0.5805238035096224---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T12:41:10.969
+Launch V∞: [6.993024333991076, -6.728065184604345, -0.39707946107543446] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1523217121539181e-6, 1.5874105444307312e-6, -8.364900121078152e-6] km/s
+ V∞_out: [-3.9602986558682536e-6, 7.183523250818279e-6, -2.5556129587124317e-6] km/s
+ time of flight: 1.43824054529721e8 seconds
+ arrival date: 2028-11-25T03:48:44.969
+ thrust profile: [0.7181972102172647 -0.2161609497346538 -0.26713392233453237; 0.12963811462021727 0.026710601583284192 -0.1421325306899038; 0.09572268985221387 0.04286108647611079 -0.1710203348293686; 0.0636335680815505 0.0388046353265829 -0.157924355985194; 0.06667083256770936 0.04788465165902701 -0.1976342106820614; 0.03560566443768818 0.028184187226975715 -0.1310713496071102; 0.024416860229823874 0.02132281348971745 -0.10129417652458848; 0.013283456127848366 0.012293640356101037 -0.06324124595499904; 0.03775573620045651 0.04284590748038668 -0.1934541669079733; 0.004095640705591417 0.003998965923465391 -0.02072673677545797; 0.009131519140296928 0.00970098482994504 -0.05214180477745938; 0.0011356310914932583 -0.0005548023700710507 -0.004524779606148459; 0.0010400717627475516 -0.0004946681668692142 -0.0073215344953457655; 0.00033255190679992117 -0.0006706083333440217 -0.000795725217881584; 0.0007448946444040674 0.0015162065527108736 -0.006847883812746801; 0.0026757255332365702 0.0018630333176222192 -0.00433155313411038; -0.002558508205506008 -0.00042517834173810517 0.006607110001371763; -0.0006868549129586789 -0.0012582592820955764 0.004286408949934351; -0.004887297677884744 0.0046481487490807865 0.0026021975674179834; 0.001271063425142016 0.004124913997437312 0.0044485954268907515] %
+
+Mass Used: 127.03738914673386 kg
+Launch C3: 94.32692256248438 km²/s²
+||V∞_in||: 8.591814220552287e-6 km/s
diff --git a/archive/ES_0.580546625346555 b/archive/ES_0.580546625346555
new file mode 100644
index 0000000..e1d4e20
--- /dev/null
+++ b/archive/ES_0.580546625346555
@@ -0,0 +1,22 @@
+archive/ES_0.580546625346555---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T22:54:16.137
+Launch V∞: [7.064559503172731, -7.026235741321036, -0.3748541777517473] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0169729169099273e-7, -5.417478485655597e-8, 6.456264520068147e-8] km/s
+ V∞_out: [-2.0542235787397494e-7, 5.8580057637470307e-8, -2.4874481987537468e-8] km/s
+ time of flight: 1.8749577782551518e8 seconds
+ arrival date: 2029-04-03T01:03:53.137
+ thrust profile: [0.23347007782999046 -0.05217040427156269 -0.07690806542843795; 0.0767015023320027 0.027717050693194925 -0.07529947062829066; 0.07783867199722723 0.05688493626258981 -0.1321438613564764; 0.062125936564982914 0.06301203746033983 -0.1509505451003659; 0.04465410572138158 0.05677099964906743 -0.14228094819372003; 0.037729889426576735 0.05842577932814876 -0.15226568991394798; 0.018468371981382223 0.03343274951450873 -0.09202038918189819; 0.008151131295016085 0.01781958671426531 -0.05078454273055944; 0.003142002692809705 0.005929952051951065 -0.01602502224352422; -0.0009412761168958838 0.0015395139169392977 -0.00507189622664166; -0.0014911115462193955 0.0012283967558469819 -0.007458481705446139; 0.005962728964940699 -0.00401510229003293 -0.00805517233093151; -0.005350167204377894 0.0013958222554680767 0.0005480896739232582; 0.0037219547139594783 0.0016224537831788768 -0.005271781995708214; 0.0006336186380026172 0.0015766893406277843 -0.004435710567567846; 0.0027767712517890787 0.002393315413117561 0.001738539716990578; -0.006607117952154882 0.013405697043679752 0.00033560309949973166; -0.0010146146564584124 -0.00686676170711311 0.0014796469884243487; -0.014247223443399838 0.0006036898760275362 0.0031592840261191204; 0.018809514891836167 -0.005381328718238482 0.0129567533487638] %
+
+Mass Used: 97.37478186477847 kg
+Launch C3: 99.41650532106325 km²/s²
+||V∞_in||: 2.1859789556408043e-7 km/s
diff --git a/archive/ES_0.580597275556613 b/archive/ES_0.580597275556613
new file mode 100644
index 0000000..4ce3bae
--- /dev/null
+++ b/archive/ES_0.580597275556613
@@ -0,0 +1,22 @@
+archive/ES_0.580597275556613---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T15:53:25.550
+Launch V∞: [5.371087941018014, -7.968584158382964, -0.3553238017677181] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.660580355865797e-5, 0.006802267764233063, -0.0027942415958270845] km/s
+ V∞_out: [-0.005845209997896807, -0.0034006040841653186, 0.002888694475916613] km/s
+ time of flight: 1.4475413895854515e8 seconds
+ arrival date: 2027-11-21T01:22:23.550
+ thrust profile: [0.7580292195694467 -0.42110297713025635 -0.2985893286850177; 0.19881106749372512 0.00021652969716793373 -0.19047229501852644; 0.11505983933876605 0.026340897626285133 -0.17155065374515982; 0.09491846962773394 0.035235795444243406 -0.1874748719990421; 0.08486997142110606 0.04111435614136311 -0.2028928046349388; 0.10031400954328841 0.056594155422845724 -0.26786454237548685; 0.047692298293518724 0.03268308915144212 -0.1524828385953959; 0.005648513052122771 0.0037062666755462055 -0.022223854466310436; 0.00741345674732951 0.004597481833783151 -0.034464853719382925; 0.006307537077960265 0.005184208896992661 -0.03184601518337772; -0.00022345480159801148 0.0001943413627629186 -0.0005492928040328015; 0.00018344250773899288 0.00029155138361131077 -0.000743454514306922; 0.0003544156334012085 -0.0009831386566244626 0.0010586847249943639; -0.00013312086253609718 -0.000272676737875754 0.0010660390376932161; 0.0002023389634493054 3.1646095529888445e-5 -0.00024663188274620315; 0.0003058589824794687 -0.0001094470071497057 0.0002472624046151678; -0.00017719799316346684 -0.000491112792095088 0.001154544185354203; 0.0005368499236499366 -0.0007400071857924499 0.0007528633656883976; 0.00012804578554180315 0.00045595615716947447 -0.0005631996834500243; -0.0008855614579360907 0.00021348588691310496 -0.0009790677122831289] %
+
+Mass Used: 137.93663886239347 kg
+Launch C3: 92.47317416348372 km²/s²
+||V∞_in||: 0.007353836317520699 km/s
diff --git a/archive/ES_0.580627793557752 b/archive/ES_0.580627793557752
new file mode 100644
index 0000000..cd465ad
--- /dev/null
+++ b/archive/ES_0.580627793557752
@@ -0,0 +1,22 @@
+archive/ES_0.580627793557752---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-11T13:53:18.797
+Launch V∞: [6.27063436070327, -8.093793043517875, -0.2889107289955683] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.914543159469498e-7, -3.6927139975092346e-6, 2.0701499662184912e-7] km/s
+ V∞_out: [-1.3921949675734126e-6, 3.0397065933018855e-6, -1.6527901889910775e-6] km/s
+ time of flight: 1.8749577782394895e8 seconds
+ arrival date: 2029-04-19T16:02:55.797
+ thrust profile: [0.04891008377090195 -0.01817347345925707 -0.02696209559088508; 0.015160883198667008 -0.0009061513554076222 -0.02522160748132437; 0.025318943850302412 -0.0009654188419533175 -0.07396707259774053; 0.03406295020921086 -0.0018508917174888321 -0.13530101586470145; 0.03129883900658448 -0.0034400998784936475 -0.15358490083856202; 0.022815865418045065 -0.0042882207889344175 -0.13178275259136013; 0.013584596721368771 -0.0039570901639871675 -0.08903488809200047; 0.007032917216975079 -0.003533424110491814 -0.05237980445886904; 0.013010277022634268 -0.0035327953650980304 -0.1012378793965746; 0.0007801669246599213 -0.00042790715341023254 -0.006258217696419334; 0.0012892586028516932 -0.0006819768229932468 -0.010434822632428859; 0.00013741563499108922 0.00014187787916517604 -0.001556983431393149; -0.0007306966317124262 -0.00035863103727006983 -0.001995492963226848; 0.0008836076418949571 3.942795048089156e-5 -0.001750992136768918; 4.209387580805975e-5 -0.00011434361100982741 -0.002742816709628733; 9.965226536795229e-5 -0.0009350019744428671 -0.0037744138283646255; 0.0025713496397321376 -6.171913953210563e-6 -0.0018419023029119764; 0.0002866331069020804 -0.0005672853608089247 -0.0008331068030405914; 0.00019843914426996069 -0.00012378142096844993 0.0006067302340818832; -0.0001915461927737964 -7.948748755739527e-5 9.74373329217048e-5] %
+
+Mass Used: 65.4018644141961 kg
+Launch C3: 104.91381052625962 km²/s²
+||V∞_in||: 3.7310212034897175e-6 km/s
diff --git a/archive/ES_0.5806562413044064 b/archive/ES_0.5806562413044064
new file mode 100644
index 0000000..f7c5b08
--- /dev/null
+++ b/archive/ES_0.5806562413044064
@@ -0,0 +1,22 @@
+archive/ES_0.5806562413044064---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T07:29:55.558
+Launch V∞: [7.092357170929488, -7.0177353304381915, -0.7025343558047723] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0010476981680330635, -0.0015435167776550662, -0.00013724922112442355] km/s
+ V∞_out: [0.00010491826031998272, -0.0004839317076663024, -0.0018036612860090101] km/s
+ time of flight: 1.409281524162762e8 seconds
+ arrival date: 2028-10-25T10:12:27.558
+ thrust profile: [0.24616319708527098 -0.08102703766942997 -0.12100928087402452; 0.10536822551807558 0.013163989009602644 -0.13122920628986856; 0.09944885008839878 0.03382025872717212 -0.20350910338577546; 0.058473160141917134 0.02533830890019724 -0.1614615814074809; 0.05946616949240581 0.030310047444090896 -0.1998830666501313; 0.04440977582303558 0.026916915948403175 -0.1846063867743281; 0.03433243112944403 0.02279476354843604 -0.16660155634445023; 0.007794647638439383 0.004658930208415123 -0.042576057181853894; 0.01490255542504055 0.012201844792635948 -0.09625809846368107; 0.015642080620032216 0.008606355363458683 -0.07881882049811405; 0.00020244505747209 3.825900966474958e-5 -0.0008009967748996184; 0.0007550783519238717 3.649487495822139e-5 -0.0004411924591547704; 0.0007648486480407435 0.0008603812953791311 -0.010703133293257523; -0.000296657334697242 -0.0005527975078362209 -0.0010484717352855298; 0.00031513066610081703 -0.0007037754688926396 -4.014143751272624e-5; 0.00045563639231923346 1.1069596225063934e-5 -0.00035790945702984214; -7.052060227544631e-5 9.820731059993927e-5 0.0002356988011989439; 0.0001353798605851725 -9.75425877011947e-5 -0.001169984150669473; -0.0003711169867945379 0.00013768471018892818 0.00035448343707264603; 0.0008091215410499771 0.0009058641861818022 -0.00016760994476903028] %
+
+Mass Used: 93.84406693479923 kg
+Launch C3: 100.0436939292014 km²/s²
+||V∞_in||: 0.0018705488079442827 km/s
diff --git a/archive/ES_0.5806701113977355 b/archive/ES_0.5806701113977355
new file mode 100644
index 0000000..8d0a8c8
--- /dev/null
+++ b/archive/ES_0.5806701113977355
@@ -0,0 +1,22 @@
+archive/ES_0.5806701113977355---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-04T08:30:00.449
+Launch V∞: [5.885840918192739, -8.131016768138304, 0.0037253129285198575] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005950367753234438, -0.004185611104533638, -0.004840996869803064] km/s
+ V∞_out: [0.003859824122717336, 0.006616066536447442, -0.004216241710383602] km/s
+ time of flight: 1.7086194636241272e8 seconds
+ arrival date: 2028-10-01T22:09:06.449
+ thrust profile: [0.15369093250389632 -0.08356241496565565 -0.08054575971859677; 0.05965775960620573 -0.011674002338670468 -0.09550731547424124; 0.048630826307000524 -0.008596568996553868 -0.13173726994382512; 0.04188855109482281 -0.009655821920254094 -0.15581193603821689; 0.03451005902684576 -0.01053737718225619 -0.1593726544816041; 0.027390677873641574 -0.010511252164113529 -0.14810629138711234; 0.019788673427581067 -0.00906463984651204 -0.12092599446280251; 0.014229563967289577 -0.00754231522923099 -0.09563948618193814; 0.006625913897362276 -0.003922754424258912 -0.04910291722595542; 0.0009462234637570886 -0.00043361221702844724 -0.008449666975617054; 0.0005718398085869386 -0.0011350772733767173 -0.004149336541532815; 0.00018005995870030409 0.0002780697935458439 -0.0026712958335684467; 0.001902918787317328 0.002464154433211901 -0.00017147398599559388; 0.007778284324866727 0.006666147656978266 -0.002946779741123301; -0.0016467914691785787 0.000777929589078683 -0.0009381975954269429; -3.9845372964287637e-5 -0.0025728944717714874 0.008764687814959173; -0.0014041617803135815 0.01111635736117421 0.0036812714491014607; 0.003559100373489823 -0.0015163785316397206 -0.018653193843600212; 0.00581058120486745 -0.02137023637951543 -0.013926219494057378; 0.009773635447727495 -0.011937831583769966 -0.024399904339477682] %
+
+Mass Used: 89.7017998541728 kg
+Launch C3: 100.75657087597462 km²/s²
+||V∞_in||: 0.008738504872721112 km/s
diff --git a/archive/ES_0.5806858804953149 b/archive/ES_0.5806858804953149
new file mode 100644
index 0000000..3edc3a5
--- /dev/null
+++ b/archive/ES_0.5806858804953149
@@ -0,0 +1,22 @@
+archive/ES_0.5806858804953149---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T08:58:11.439
+Launch V∞: [5.53086756865834, -8.130440593057426, -0.41840490544719705] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5517346847532922e-8, -7.229121907997683e-9, 1.315697814972357e-8] km/s
+ V∞_out: [5.906552933325535e-9, -1.3137557622859933e-8, -1.7420039362662866e-8] km/s
+ time of flight: 1.5163516666761318e8 seconds
+ arrival date: 2028-02-12T09:50:57.439
+ thrust profile: [0.2970385818794691 -0.1417450984468394 -0.12051763206125761; 0.1432721534138985 0.008499847149275146 -0.14372063895865747; 0.11102406378386168 0.032187913998651195 -0.174034251981472; 0.08965344754381711 0.03950230118119863 -0.18697543352671298; 0.07293112386734418 0.04020477297388168 -0.1847559634303198; 0.05516037362274949 0.034570477797835036 -0.16407162193122746; 0.05495442888135294 0.035250030297224406 -0.173922546728768; 0.023258934972142743 0.01635325655353703 -0.08755735734491994; 0.0188031504297443 0.01625249907637369 -0.06945463944512159; 0.0037127875409874705 -0.0007877666440181015 -0.01078634950610139; 0.004314600740175698 -0.003921635518613149 -0.007802894343559717; 0.0001446733396978714 -0.0008220105659735625 -0.004695063086711427; 0.004567807665913775 -0.001638751884981774 -0.006710712831090211; -0.0038746406704187695 0.0029094100161481977 0.004003143583446626; -3.8636358770376134e-5 0.0032489678810691605 -0.002716895023753746; 0.002509117623450045 0.007025093391113892 -0.013128652738717802; 0.007465812380110597 -0.0031337135677679834 -0.004301298466561702; -0.000547310994983949 0.0018684056262103354 -0.0022864934211250156; -0.0017267898574535876 0.02691287259247928 0.019290655649965297; -0.0017163213549582484 0.051541596373187934 0.005707213708748814] %
+
+Mass Used: 112.39405995351399 kg
+Launch C3: 96.86962296417487 km²/s²
+||V∞_in||: 2.159060746666558e-8 km/s
diff --git a/archive/ES_0.5806985931363179 b/archive/ES_0.5806985931363179
new file mode 100644
index 0000000..735993a
--- /dev/null
+++ b/archive/ES_0.5806985931363179
@@ -0,0 +1,22 @@
+archive/ES_0.5806985931363179---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T18:27:52.031
+Launch V∞: [5.958748254339256, -7.770304538087746, -0.13686525326768006] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.372630906410811e-8, 1.4558606173680658e-5, -1.0320676814566258e-5] km/s
+ V∞_out: [-9.054019626476134e-6, -1.5085115363789582e-5, 3.079293339040234e-6] km/s
+ time of flight: 1.685423468576383e8 seconds
+ arrival date: 2028-08-28T11:46:58.031
+ thrust profile: [0.3675392863967225 -0.13992362370975206 -0.12278777625465905; 0.07780349227996472 0.012593246564754636 -0.08739843652341185; 0.06812736578220481 0.02794074738986028 -0.12159808608393151; 0.07411684039477483 0.04289796564445842 -0.1679037494422297; 0.02667588367632614 0.026990211372237623 -0.06101985798967074; 0.020322110275631446 0.04249410925326531 -0.11118263751141644; 0.047315529883492434 0.04175765038437282 -0.1823036618831932; 0.022135208382782434 0.02190254567654836 -0.11382603084372557; 0.01230918605879536 0.00987233811519763 -0.06322229325665463; 0.0020104232358871005 0.012618436935652986 -0.05108178777865596; 0.005082862025600509 -0.0013698525105062705 -0.001813432019247935; -0.004621368715055354 0.012533285376342376 -0.04761608495369827; 0.0064104644939023386 0.0036493101024758904 0.0007925608924861209; -0.009583926945108318 -0.004694712312415167 -0.0013743511091905522; -0.012074645043062906 -0.0252464248029399 -0.017132297671132838; -0.0034228735584124663 0.00025506503391860627 -0.027701805567773678; 0.010087944746484376 -0.004268294554594444 0.015608582405288618; -0.012115258058415138 -0.006507898411315801 0.019321691843727493; 0.018132564110976104 0.02502070530201267 0.014357945614236457; -0.024175635720617233 0.014913591988990052 0.0601319245478115] %
+
+Mass Used: 118.04726007954469 kg
+Launch C3: 95.9030454707702 km²/s²
+||V∞_in||: 1.7845764080620433e-5 km/s
diff --git a/archive/ES_0.5809039723548683 b/archive/ES_0.5809039723548683
new file mode 100644
index 0000000..6ce963e
--- /dev/null
+++ b/archive/ES_0.5809039723548683
@@ -0,0 +1,22 @@
+archive/ES_0.5809039723548683---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-23T03:41:34.687
+Launch V∞: [7.909238451578536, -6.536820396957248, 0.23401141762581298] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002145964332949543, 0.0021491378908045002, 0.0021310963158293634] km/s
+ V∞_out: [1.1869201509560617e-10, -3.858981596699397e-10, 6.482388151860139e-11] km/s
+ time of flight: 1.8215345104353204e8 seconds
+ arrival date: 2030-03-01T09:52:25.687
+ thrust profile: [0.011223836345057607 -0.002405491450338093 -0.005035848091993523; 0.010192238047969806 -1.815902558530685e-5 -0.01534141662708523; 0.027843945214572667 -0.0015274624207794363 -0.07517215424257974; 0.041120842260989644 -0.006814024190591671 -0.14742916645536588; 0.03538521069239052 -0.009688077852085484 -0.15072147724310106; 0.029817542607801596 -0.010830847436505479 -0.1414987860010657; 0.021178192777742365 -0.009141829613532826 -0.10694770909844549; 0.009730865685205715 -0.004820783828936357 -0.050966963296696324; 0.007623172462812513 -0.004334018176009227 -0.042537971601205204; 0.0012318414237798671 0.0009732745198074371 -0.0073380600411727046; 0.003241986824040332 -0.0022718508044426607 -0.01889615896003673; -0.003469510507351066 -0.0021296196773950026 -0.005767191660868389; -0.002443359801392004 -0.0023157982369630915 -0.006152637627868374; 0.005878497056382689 0.004807752990210958 -0.006074228685341771; 0.0018853109344169558 0.002770283897219178 -0.0026938332268605664; 0.010874673578507929 0.0041606059657862396 -0.014087127072923587; -0.0011947460302190016 -0.0006661098103249367 -0.002447325602800236; -0.007283427175156565 -0.007581128771031615 -0.01388625177354469; 0.0008959184262979086 0.00016214696530379575 -0.0006254102390689763; 0.00470496329600598 0.005321020962407007 -0.003380944911063422] %
+
+Mass Used: 63.23309615810649 kg
+Launch C3: 105.340835129584 km²/s²
+||V∞_in||: 0.003710192461224172 km/s
diff --git a/archive/ES_0.5809434466851848 b/archive/ES_0.5809434466851848
new file mode 100644
index 0000000..5672229
--- /dev/null
+++ b/archive/ES_0.5809434466851848
@@ -0,0 +1,22 @@
+archive/ES_0.5809434466851848---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T18:20:57.870
+Launch V∞: [6.19109425557436, -8.14551372650833, -0.14999841317463988] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.765722436731768e-7, 0.00025055462036021963, -0.00019262963412473673] km/s
+ V∞_out: [-0.0001593924087815079, -0.0002671901394234671, 5.5437924931116165e-5] km/s
+ time of flight: 1.8122738448423502e8 seconds
+ arrival date: 2029-02-04T07:17:21.870
+ thrust profile: [0.019506262543331918 -0.009877209541151826 -0.011144144659408755; 0.014736350048177305 -0.004235340468553265 -0.026743653549460445; 0.030831534871320457 -0.012019946057303823 -0.0953740369806198; 0.03532016877590994 -0.019695527808534546 -0.14920234155623344; 0.03358289778591602 -0.02416817349290026 -0.17311526407323094; 0.026630345508224375 -0.022587588401507673 -0.15681249941286365; 0.018280708795901275 -0.017297190900536413 -0.11812145551526607; 0.012054019359671469 -0.012420718321756796 -0.08359650233809442; 0.004241090219133769 -0.004701093681232851 -0.031228215192855048; 0.0004810389919167762 -0.000568178453518935 -0.0037494854022902427; 0.001309938660074564 -0.0015613286878528498 -0.009900572910036471; 0.0007268532957949037 -0.0009040746193507533 -0.004275670868782994; 0.00026456047778697004 -0.0010216331160190614 4.953720691911129e-6; 0.0001634995895358662 2.855018037701282e-5 -0.0018444743474504478; 0.002669211353431363 0.0007631490327475723 -0.0012318416880910893; -0.0006456089967040953 0.0008240965848612153 -0.00399507466088128; 0.00010260690904538119 -0.000514354035248937 -0.004830992064581341; -0.0013851652006278267 0.0014472322181056023 -0.0048195827919972085; 0.00010445750072073981 -0.00011480485895066025 -0.0012448824649159834; 0.0003284343024672963 -0.0002958150274898919 -0.0011631543480626482] %
+
+Mass Used: 67.00836253382022 kg
+Launch C3: 104.70154147409636 km²/s²
+||V∞_in||: 0.00031604518997412713 km/s
diff --git a/archive/ES_0.5809735818004825 b/archive/ES_0.5809735818004825
new file mode 100644
index 0000000..e7db25a
--- /dev/null
+++ b/archive/ES_0.5809735818004825
@@ -0,0 +1,22 @@
+archive/ES_0.5809735818004825---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T23:16:25.243
+Launch V∞: [7.0370235227979245, -6.997245584639847, -0.9344661373698752] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.2159134883923054, 0.11637160972573853, 0.01513288934517089] km/s
+ V∞_out: [-0.19143050193207853, -0.10040089159638506, 0.1169113149636207] km/s
+ time of flight: 1.4069355792287928e8 seconds
+ arrival date: 2028-10-22T08:49:02.243
+ thrust profile: [0.36177918506811585 -0.1182506415637577 -0.1663040823416119; 0.07904361250750791 0.010696811400892715 -0.09665389093405571; 0.08266601326576976 0.029589959729759346 -0.16126939656307085; 0.0741883663878736 0.03840026981001652 -0.19921867195154125; 0.047046195550754594 0.030464369826494975 -0.16476498085960486; 0.03963029135171363 0.03229146034043426 -0.17377004987856604; 0.06334221777108447 0.04604375094255072 -0.26291483109253083; 0.013884917288377626 0.010209300692240809 -0.06695621578303966; 0.0064882809229947465 0.005777763090245089 -0.039059752092322965; 0.001999470520313654 0.0014321599972923404 -0.012244081034046731; 0.005117816625084751 0.00445879267255748 -0.03381231050468415; -8.891481142785031e-5 -0.00040686855241649027 0.0003775732287853166; -0.0006285023209871934 0.0018868558679436915 -0.0016785996537770809; -0.0015956598201272605 0.00042226969887931804 0.0014809748016843191; 0.0014497732800694049 0.0008866221401007767 -0.005635803368541935; -0.0004455865039431938 0.0007783541890463652 -0.001024262205234036; 0.00011705740695359485 -0.00580331740410458 0.003520127905964609; 0.00040339497344095345 -0.0005554222544049047 0.002752216361444796; 0.0006010924154931115 -0.0011538251356582156 -0.0005309423279785919; -0.0038087492643140482 -0.0006412246485791226 -0.00030528984388773273] %
+
+Mass Used: 98.23533746852218 kg
+Launch C3: 99.35437279406413 km²/s²
+||V∞_in||: 0.2457437493809903 km/s
diff --git a/archive/ES_0.5810655306016442 b/archive/ES_0.5810655306016442
new file mode 100644
index 0000000..5418bb6
--- /dev/null
+++ b/archive/ES_0.5810655306016442
@@ -0,0 +1,22 @@
+archive/ES_0.5810655306016442---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T05:13:16.770
+Launch V∞: [6.98019177258489, -6.948378343684581, -0.696960249049612] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.366970449716911e-6, 2.042714973454229e-5, 1.1711766766137844e-5] km/s
+ V∞_out: [1.8407952804640533e-5, -1.418302319039253e-5, -9.161411404003864e-6] km/s
+ time of flight: 1.3979910779324803e8 seconds
+ arrival date: 2028-10-11T06:18:23.770
+ thrust profile: [0.4886539660032624 -0.17398404695094846 -0.22341340059882234; 0.09941470858314233 0.00949453908397453 -0.117983618527278; 0.11903268664094349 0.03576995925801689 -0.2241378565859658; 0.12313009336966936 0.05230732464369486 -0.3154244694579507; 0.06868108580137622 0.033139818500414135 -0.219373838528407; 0.03692545502641401 0.018392782854720024 -0.15086764397317087; 0.020771069770558273 0.01105906021128839 -0.09143444255245915; 0.007607597646834257 0.004085747510888442 -0.03882906172187619; 0.0013573593905475772 -0.000813656197813525 -0.03252747054341067; 0.002944506828984283 -9.889481217600525e-5 -0.017143732303434155; 0.0023451507410382263 0.005186774444587381 -0.014811553703791652; 0.002218861554371953 0.0027114233175783062 -0.013649388588681494; 0.0013550947923433245 0.002626951993577962 -0.0034916951419631365; 0.001659471875265623 0.0028489459847063046 -0.006367956001823551; 1.9745386330660545e-5 0.0002539139945825241 0.0012827323414114707; -0.0013830298972815677 0.005676964811648106 -0.005087705981434201; 0.002807464619179221 0.0017316373572907068 -0.005217273154551581; 0.0005221745079359691 -0.000826452261502585 0.0017058949085768731; 0.0042919450941576 0.005544855111445998 -0.004683277645609482; -0.0012482530116187812 0.0020849413933187707 -0.002824396558877069] %
+
+Mass Used: 109.22516349807347 kg
+Launch C3: 97.48879237780197 km²/s²
+||V∞_in||: 2.4988799922530455e-5 km/s
diff --git a/archive/ES_0.5811362198740603 b/archive/ES_0.5811362198740603
new file mode 100644
index 0000000..9628d12
--- /dev/null
+++ b/archive/ES_0.5811362198740603
@@ -0,0 +1,22 @@
+archive/ES_0.5811362198740603---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T07:47:59.250
+Launch V∞: [5.5330287791090855, -8.043026173183653, -0.2587675902174697] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.394783276959197e-9, 5.100868592198788e-10, 6.181926506751688e-9] km/s
+ V∞_out: [-3.662404598572483e-9, -5.493309068958566e-9, -2.793910679839192e-9] km/s
+ time of flight: 1.4667879823034856e8 seconds
+ arrival date: 2027-12-13T23:54:37.250
+ thrust profile: [0.43178490560779276 -0.23079848032004938 -0.16794154067278372; 0.1903432570599474 0.0025815891488912457 -0.1769951645947319; 0.15135877663040934 0.03666928650017807 -0.2167655252367327; 0.11691655894084206 0.045176526552262064 -0.22217586292503722; 0.11635378724896936 0.05779757385033107 -0.2686547444530497; 0.09998124853887413 0.05303727729884079 -0.2627271198746732; 0.009863960230044759 0.007347586879197018 -0.03614694763050136; 0.013611990932586098 0.00992159832004575 -0.04855420342971354; 0.008016327022843548 0.0052484433192533575 -0.025720240257606466; 0.006543846208344426 0.0044364906243171374 -0.02353316221389924; -0.0036996177072085045 0.0024330486036587963 -0.004362989984631343; 0.00039422305991638324 0.0008113609689466719 -0.0035511668711696955; -0.0012009590267307788 8.767203844712009e-5 0.0011563074222941945; -0.0069551983875374415 0.0007186182238916508 -0.004411145021663928; -0.0016429520460883814 -0.0018020490761706252 0.0003307236097658214; -5.262648438941411e-5 -0.0015926177506884838 0.005006698673061555; -0.0008645463973819931 -0.0022561910730387025 -0.0021049299868987213; 0.0046427848365294755 0.0025787166656621066 0.004189441018846682; -0.0007057386910485182 0.0032298813074254458 0.011197494553410457; 0.00575482632218679 0.005388368688665288 0.0006876876082886878] %
+
+Mass Used: 121.65770059390752 kg
+Launch C3: 95.37163815871362 km²/s²
+||V∞_in||: 6.3578160030401136e-9 km/s
diff --git a/archive/ES_0.5811762171204626 b/archive/ES_0.5811762171204626
new file mode 100644
index 0000000..d3f1965
--- /dev/null
+++ b/archive/ES_0.5811762171204626
@@ -0,0 +1,22 @@
+archive/ES_0.5811762171204626---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:56:03.354
+Launch V∞: [7.061533757513893, -7.01703412682813, -0.7168458676945596] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.649332356524032e-7, -1.050981324631456e-6, 1.962333596574001e-6] km/s
+ V∞_out: [9.37227194705381e-7, 2.1431028647538188e-6, 6.563243187606466e-8] km/s
+ time of flight: 1.4131495889502636e8 seconds
+ arrival date: 2028-10-30T02:05:21.354
+ thrust profile: [0.28909842616724174 -0.10197478229109026 -0.13725676530295852; 0.08769311049246765 0.009432495060659223 -0.10745576610000149; 0.09278853297388698 0.027266421050608322 -0.18449465842202847; 0.08431106805942674 0.033786914722425516 -0.22840214215531965; 0.08060718097567761 0.037830454849460675 -0.2708673078942945; 0.04929174295177713 0.025435388144799963 -0.19705903716230685; 0.03002807257311803 0.016711846053587973 -0.13746045340487648; 0.007766383071828232 0.005067459958693831 -0.041781266691977605; 0.0010271255681929357 0.0012284639776508097 -0.014723922415382706; 0.005371501410664252 0.003191549814112819 -0.03381875581896339; 0.0015402913599378645 0.001220358591594769 -0.010088314451258247; 0.005333625345342921 0.0019173290452849942 -0.0020621255882227424; -0.00016111709758720883 0.0020722812276279803 -0.003925483851447626; -0.00037316481247264596 0.001575681676554215 0.001907660722858212; 0.004876173080230674 -0.0015401735669682206 -0.0012562997101820442; -0.00779865029212524 0.0018383383996437848 -0.0004912646109244536; -0.005229199113743513 -0.006289277759305548 -0.006601215688879482; -0.00014902129018339125 -0.0008783838025758796 -0.006522289487918699; 0.004530940938233322 0.00093939953670225 -0.004725606879608163; 0.0026900976898634153 -0.0030381913298243553 -0.008992817723542556] %
+
+Mass Used: 96.93453280281665 kg
+Launch C3: 99.61789494360967 km²/s²
+||V∞_in||: 2.3538134471475857e-6 km/s
diff --git a/archive/ES_0.581220610709739 b/archive/ES_0.581220610709739
new file mode 100644
index 0000000..fb6d8b6
--- /dev/null
+++ b/archive/ES_0.581220610709739
@@ -0,0 +1,22 @@
+archive/ES_0.581220610709739---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T06:12:42.208
+Launch V∞: [5.361456301990914, -8.214824590759012, -0.5630863725414519] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007625599864318805, -0.008450073098297654, 0.00013014112069964368] km/s
+ V∞_out: [0.002576403831336756, -5.3514719773982335e-5, -0.011084104909972692] km/s
+ time of flight: 1.4430962104985216e8 seconds
+ arrival date: 2027-11-19T12:13:03.208
+ thrust profile: [0.46990196167817394 -0.26674511820773444 -0.2192712092655073; 0.10934485928599216 -0.005718251336597355 -0.12233369407296103; 0.08670969703167086 0.013187493346604018 -0.15039300315483992; 0.09646185891666324 0.026486152470761658 -0.22041115138299142; 0.05317380748019042 0.01888067218670789 -0.14998398593234; 0.03733929574986887 0.015250951246563244 -0.12277232037533728; 0.06670828384819726 0.031895477747748736 -0.24549183902235164; 0.039981739679102145 0.020244525101529385 -0.1641775297749847; 0.01148702493824217 0.006147344415582164 -0.05204227904354446; 0.002600450651395667 0.0014187810028217277 -0.008804080585016293; 0.0017261470883331844 -0.0004003195916142914 -0.0020117864454693426; 0.001227178203513666 0.0008313796894031512 -0.008883274646516863; 0.0004685479967804297 0.0010171395005979342 -0.0035680961734730005; -0.001378305709144149 -0.0005831464276091001 -0.0012196448641950937; -0.00041167097943319833 -0.0014472878863122072 -0.005626306755561691; 0.0008949254084920542 -0.0013246151838941704 -0.00075586464699349; 0.001711034210227036 -0.0008687972345708806 0.0015178412707702099; -0.0006842283469699883 -0.002932587163282603 0.00034150849241960316; 0.0042824644936011475 -0.009630584382110025 -0.006907367460550168; 0.007657487219742124 0.0019861572885849846 -0.011825447971270572] %
+
+Mass Used: 114.90791167280167 kg
+Launch C3: 96.54562299803894 km²/s²
+||V∞_in||: 0.011382901447722794 km/s
diff --git a/archive/ES_0.5812270998624123 b/archive/ES_0.5812270998624123
new file mode 100644
index 0000000..ec340c6
--- /dev/null
+++ b/archive/ES_0.5812270998624123
@@ -0,0 +1,22 @@
+archive/ES_0.5812270998624123---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T06:21:39.797
+Launch V∞: [7.095748117324197, -6.977401542705304, -0.6222927303560982] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0003056780401001829, 0.005000900977800742, -7.682018623855485e-5] km/s
+ V∞_out: [0.004847229495897946, -0.0007741540016126535, 0.0010016451208825889] km/s
+ time of flight: 1.4460843286524644e8 seconds
+ arrival date: 2028-12-07T23:22:11.797
+ thrust profile: [0.27123784610044377 -0.09077214813213881 -0.1258861614026757; 0.10312055391096013 0.012027412851487807 -0.12714604634890192; 0.08035390062421358 0.023877742245713277 -0.1621018811497772; 0.06079751644686606 0.024189381757688755 -0.1681210991614346; 0.04664983812446071 0.021823066443011612 -0.16154446825405339; 0.05817369507419093 0.029338059342974895 -0.23458163258269293; 0.03399245957062521 0.01804376517970775 -0.15699116751182815; 0.02470473784957687 0.013779562820912987 -0.1278816734029871; 0.0009597253788438025 0.0028445519437177947 -0.013821264899015306; 0.003432052009729889 0.003943552340418742 -0.01888968393253049; 0.006999178348684466 -0.0028876309877616576 -0.010739620558689416; -0.0025029915130029886 -0.007327342296829914 -0.004985215891275863; 0.008266803789796336 -0.0014989938085074558 -0.0026797100224085517; -0.0063697665329781545 0.0033823208897200245 -0.008419297783199066; -0.003317405910116129 0.00028855580345832463 -0.003935769157053899; 0.0009084583681496781 -0.011018478749845365 -0.006624381367545305; 0.0033785779075723218 0.00505247180329034 -0.023326969643818994; -0.0007117890824634523 0.005747476126277089 -0.004179519721452345; -0.0023706179766961807 -0.006101996224924329 -0.015730152691333196; 0.0004941746778727866 0.008536639550644692 -0.014572451625179027] %
+
+Mass Used: 98.14232223583758 kg
+Launch C3: 99.4210218749103 km²/s²
+||V∞_in||: 0.005010823384932025 km/s
diff --git a/archive/ES_0.5813950007409896 b/archive/ES_0.5813950007409896
new file mode 100644
index 0000000..f5e0ece
--- /dev/null
+++ b/archive/ES_0.5813950007409896
@@ -0,0 +1,22 @@
+archive/ES_0.5813950007409896---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T20:28:16.969
+Launch V∞: [7.084525339308547, -6.52270585995374, -0.34517264384704804] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00024244184568384043, -0.00019060810220732782, -0.0006456286471498166] km/s
+ V∞_out: [-0.00011312324317836496, -0.0007057091083782614, 3.250016534079569e-5] km/s
+ time of flight: 1.4657055336429772e8 seconds
+ arrival date: 2028-12-24T06:30:49.969
+ thrust profile: [0.8150512113576136 -0.21089141836714176 -0.2525610963213192; 0.17749735705886463 0.050640319037110346 -0.16544226606244863; 0.09249881225979723 0.05258648241374157 -0.14626336956577143; 0.12594964378326362 0.09471669279864885 -0.24996717313879313; 0.039855096729476264 0.036937240047690806 -0.10882534498734425; 0.03353203363954015 0.03661752362052747 -0.11535938013068764; 0.04601257729070512 0.05159258177323516 -0.16454670846892241; 0.017074851414987536 0.022290688417839533 -0.07540637331367038; 0.01811948172465978 0.025837982820010347 -0.0894428837793797; 0.007014710491267654 0.010406610069678928 -0.03722914089288546; 0.011850767831770935 0.018793479131871436 -0.06676422433001654; -0.00029092159156153107 0.001059620001011809 -0.004437512003893323; -0.00022906994068162237 -0.00031166435192362557 -0.001676522153929022; 0.0015389255116939565 0.0016887517781751789 -0.00036905198911632076; -0.0026825389175823525 -0.001982489950975724 0.00013749326663886207; -0.00011931581335579652 -0.003515493718739963 -0.004733854342813515; -0.0005446705155511648 0.0006296781081973843 -0.001005021423113133; -0.0011439168114599065 -0.000923975717389056 0.0015736498173314303; -0.0037313523803479106 0.0009786812082549724 -0.0021703442808442405; -0.0002727013994780818 0.0008034022585023215 0.001329386482082824] %
+
+Mass Used: 136.63804568958722 kg
+Launch C3: 92.85533517284011 km²/s²
+||V∞_in||: 0.0007155039113702793 km/s
diff --git a/archive/ES_0.5814044076612837 b/archive/ES_0.5814044076612837
new file mode 100644
index 0000000..2faf007
--- /dev/null
+++ b/archive/ES_0.5814044076612837
@@ -0,0 +1,22 @@
+archive/ES_0.5814044076612837---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T20:33:01.709
+Launch V∞: [6.361281046492214, -7.85616195347628, -1.567099187702634] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01681496868172014, 0.009458612796751854, -0.0195772487942827] km/s
+ V∞_out: [0.017368984932426616, 0.00706894451320807, 0.020108828711280065] km/s
+ time of flight: 1.8600304268654e8 seconds
+ arrival date: 2029-03-31T16:03:43.709
+ thrust profile: [0.12734744387607416 -0.06361407153909256 -0.08047790000128137; 0.017323292765232968 -0.01023598152134137 -0.04774456346710704; 0.01605614606588245 -0.017061591638615675 -0.08726408854881444; 0.01854483951536759 -0.0253199459527186 -0.13261182185785425; 0.017298837282795156 -0.028299981701876867 -0.1475457293657764; 0.01202657480338962 -0.024591771874419605 -0.12175751147490937; 0.007936355263035128 -0.01790607651068801 -0.08933532071165412; 0.005848643874472689 -0.012227406277509489 -0.06324184335682094; 0.0028245669707024058 -0.005601685389335526 -0.028699610096967056; 0.00030631910495243855 -0.001337086589451238 -0.0054529255568031; 2.3014515827628926e-5 -5.948360613574881e-5 -0.000286668463914931; 8.759425878660013e-5 -0.00016541171452855012 -0.0010786969700628426; 2.039410546145139e-5 -0.0001995439734975141 -0.0011124213552838895; 0.00031233670948334585 -6.148472017770482e-5 -0.0008394327552017513; 8.701526952328517e-5 -0.0001033186086796383 -0.0004775084359492487; 0.00017812573431710789 -0.00013946985788009317 -0.0005450604814526797; 0.0003922302251869246 -4.887779745125405e-5 -0.00013808335474908406; -2.9332753698517385e-5 -0.00010583445154520336 -0.0007765307898478515; -0.0009646527698970166 0.0005122061429911634 -0.00025227754079404835; 0.00023847040540568028 0.0006542168955709997 -0.0004034500695898315] %
+
+Mass Used: 67.8994427792868 kg
+Launch C3: 104.64097705580758 km²/s²
+||V∞_in||: 0.027485945465989533 km/s
diff --git a/archive/ES_0.5814218583827974 b/archive/ES_0.5814218583827974
new file mode 100644
index 0000000..710807f
--- /dev/null
+++ b/archive/ES_0.5814218583827974
@@ -0,0 +1,22 @@
+archive/ES_0.5814218583827974---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T23:52:49.255
+Launch V∞: [7.087735749444929, -6.921440727925701, -0.8054807914836419] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007668140356568462, -0.004232703241145504, -0.004244118163303003] km/s
+ V∞_out: [-0.005272211748971307, -0.000620581035364357, 0.002887462725419409] km/s
+ time of flight: 1.4108146105820975e8 seconds
+ arrival date: 2028-10-25T21:10:30.255
+ thrust profile: [0.3059459203001824 -0.10629743264119558 -0.134409455836257; 0.15050801604108893 0.020473490932422008 -0.16873448017496434; 0.11565612284931526 0.039897109291942935 -0.21000766019502984; 0.1031269524806311 0.048794261893950794 -0.2546916855426765; 0.07776486540379118 0.04382530030250219 -0.24125851802105164; 0.03559117420742755 0.022763870434087546 -0.13683671321964433; 0.011625048452373887 0.007679566838829853 -0.051711873910537415; 0.013706518287019884 0.0089509198869272 -0.06733970664844997; 0.012300506174902087 0.012320178542599768 -0.0669404961536099; 0.006670106723716603 0.005224142614393575 -0.0373235321009202; 0.0037124246291714612 0.0027684238481556125 -0.025247268483458655; -0.0018019665288723894 0.0008977847577192401 -0.002408765302634287; 0.0004755995389250651 -0.0026286761163868255 -0.003650641888544788; -0.0013144779115315049 0.002333408813513448 -0.0069453910114036736; 0.0001743761946619432 -0.001465645305242819 -0.0017125616934622351; 0.0014852336133620364 -0.0008253994974592078 -0.004770222851466539; -0.0032434333327915894 0.00865027229608822 0.0006120099782467206; -0.0029411494017535685 -0.008543459759487467 -0.000873722612420666; 0.0031551589461265178 0.01060015565170583 -0.002866230829634562; -0.00011250862275207188 -0.00045403787343831437 0.00801318871958408] %
+
+Mass Used: 102.04385664061192 kg
+Launch C3: 98.79113910959744 km²/s²
+||V∞_in||: 0.006042873445386925 km/s
diff --git a/archive/ES_0.5814860762381491 b/archive/ES_0.5814860762381491
new file mode 100644
index 0000000..119a6f5
--- /dev/null
+++ b/archive/ES_0.5814860762381491
@@ -0,0 +1,22 @@
+archive/ES_0.5814860762381491---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T04:34:42.819
+Launch V∞: [7.032415660201451, -6.2896482524239445, -0.05473282342257486] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010144285345142542, 0.06217313443935128, 0.06492541559605287] km/s
+ V∞_out: [-0.016008038047171044, 0.013645517430757122, -0.08787227721758785] km/s
+ time of flight: 1.594617715437577e8 seconds
+ arrival date: 2029-05-19T19:30:53.819
+ thrust profile: [0.6990871591409903 -0.1150011137444405 -0.15996837357768648; 0.6189025581253436 0.26460835488597395 -0.3841387027944023; 0.2290341770726367 0.17789650719801434 -0.25913650982235226; 0.1288145715591669 0.13648068326576074 -0.21098401492392546; 0.05677952307339749 0.07485773451146478 -0.12600041456200958; 0.00829178871487604 0.013186965125179738 -0.025891937892290186; 0.013830264097726966 0.025308127110846713 -0.04896347335978616; 0.002552130743610855 0.005244471013682764 -0.011347587232082823; 0.007045293460087116 0.01643325999053283 -0.036051883572487314; 0.0018316526385780752 0.006103243931604783 -0.013447477805703226; 0.0011986777574033896 0.004756396423233961 -0.006362599968954335; 0.0002301780210058745 -0.00016117216187626912 0.0005045718742033613; 0.000726809547117048 -0.0007601732955825943 -0.00044874560378734744; -0.0019611100293192986 -1.6381910523076198e-5 -0.0008118726861516842; -0.0005850180922132124 0.0003356334150305862 0.00030505450499698056; -0.0004166327642251119 -0.0006076439904410724 -0.0008527710431448412; -0.0007413597368724812 0.0009464980274531943 0.002382148186044605; -0.00121182839161648 -0.00094832130250893 0.0031231051653443434; 0.000369776479040743 0.0002946456385538611 -0.0004942963195201196; 2.1406964536437338e-5 -3.577651911219594e-5 -0.0008755861075018451] %
+
+Mass Used: 159.131434050189 kg
+Launch C3: 89.01754083902598 km²/s²
+||V∞_in||: 0.09046388650449144 km/s
diff --git a/archive/ES_0.5814989700060318 b/archive/ES_0.5814989700060318
new file mode 100644
index 0000000..de2258a
--- /dev/null
+++ b/archive/ES_0.5814989700060318
@@ -0,0 +1,22 @@
+archive/ES_0.5814989700060318---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-11T18:01:56.379
+Launch V∞: [6.222941244329981, -8.097290235740175, -0.37830550874521574] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000759594549750657, -0.0008324359360318916, -0.0007906378159229647] km/s
+ V∞_out: [0.0008987147839283911, 0.0004127783490474374, -0.0009587886522597127] km/s
+ time of flight: 1.8749577783334565e8 seconds
+ arrival date: 2029-04-19T20:11:33.379
+ thrust profile: [0.10450129642334803 -0.04101195588411613 -0.0565846532927551; 0.026817683349757537 -0.003006545681199387 -0.04750204809036376; 0.03194730210404488 -0.0039026901973350184 -0.09620134991059028; 0.03215027678335359 -0.006408107919240902 -0.13187971064794962; 0.027022906429893127 -0.007942159082425217 -0.13755085819284535; 0.021557667835074897 -0.008469558212640506 -0.12832186063873932; 0.015815336507602907 -0.007823497673106364 -0.10644850677013969; 0.009104528572024212 -0.005277392463798262 -0.06765957991813695; 0.004533855892999096 -0.0029552473309875696 -0.035623632552891575; 0.002072172078452334 -0.0014587387514032786 -0.016823500390251513; 0.00013757586211982 -4.421067402598201e-5 -0.00037466873806831354; -8.809225899046244e-5 -0.0001316128316758093 -0.0008905207319915944; 0.00039682418245149894 -0.0005102863459595915 -0.0005107223181859803; 0.00015726458926769692 -0.00024494018775572934 -0.0005175202469987778; 0.00029042451531939226 0.00023293710066856583 -0.000424975654588182; 0.0010761874890582673 0.0006083753241496954 -0.0005103407077641287; -0.000297816661669885 2.109367884439765e-5 -0.0009773460844355233; 5.3108445294797394e-5 4.3356416479562544e-5 -8.191435152672406e-5; -0.0004085824671729002 -0.0005606262957715943 -0.0013433747944269002; -0.0018764152668373326 -0.00037630777815904896 -0.0001819493832476128] %
+
+Mass Used: 69.21583696453445 kg
+Launch C3: 104.43422195014331 km²/s²
+||V∞_in||: 0.0013766051080740733 km/s
diff --git a/archive/ES_0.5815154119817673 b/archive/ES_0.5815154119817673
new file mode 100644
index 0000000..d011889
--- /dev/null
+++ b/archive/ES_0.5815154119817673
@@ -0,0 +1,22 @@
+archive/ES_0.5815154119817673---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T19:29:59.331
+Launch V∞: [6.922087653420882, -6.828106170492235, -0.5303645219703335] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8016782894867874e-7, -7.228683669321788e-8, -1.018507262663203e-8] km/s
+ V∞_out: [-1.4331139014105678e-7, 9.401045950200457e-8, 7.524184658824408e-8] km/s
+ time of flight: 1.3929219543944588e8 seconds
+ arrival date: 2028-10-02T23:46:34.331
+ thrust profile: [0.6265084558530312 -0.20708578595838928 -0.25050626322530806; 0.2999822251243806 0.050455370861313936 -0.3048435052722455; 0.09449149815182344 0.037293669049935384 -0.16397224211310973; 0.09670151506163507 0.05295455190890958 -0.2248116878334892; 0.10844689544887322 0.0719800652887955 -0.3066112701002252; 0.022317133632703837 0.016473378760428002 -0.08094536769518577; 0.015411071951051278 0.012391603395156915 -0.06528894833201461; 0.008164699022911536 0.006536582551602322 -0.03595343412947052; 0.012468760738563638 0.011480292273950917 -0.06387548205480921; 0.015409861937831592 0.014843070267361955 -0.07846656519337394; 0.0003973643169981448 0.00013918088533314122 -0.0011903328031274126; 7.019922109029853e-5 -6.264276155162145e-5 -0.0006216115680541864; 0.0002426193084713019 8.539015016041944e-5 -0.0003129745253685223; 0.0005512004653186591 0.0002464487125782649 -0.0012832689828693403; 2.5738675209314326e-5 0.00023221552921792065 -0.0005811696103997235; 0.00015713175784156012 0.00047041446259845623 -0.0006831055575055279; 0.0007980869529945698 0.00040946719258432674 -0.0005968459271834454; 0.00046325364256481457 6.326022482576297e-5 -0.000811884390872601; 0.0004756858194475183 -1.6607129348512585e-5 -3.690915361101228e-5; -3.744205301506552e-6 0.0002926950951340817 -7.103055252332529e-5] %
+
+Mass Used: 125.32020965935726 kg
+Launch C3: 94.81961788332077 km²/s²
+||V∞_in||: 1.9439539359666442e-7 km/s
diff --git a/archive/ES_0.5815162907993733 b/archive/ES_0.5815162907993733
new file mode 100644
index 0000000..2ee5fb6
--- /dev/null
+++ b/archive/ES_0.5815162907993733
@@ -0,0 +1,22 @@
+archive/ES_0.5815162907993733---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-11T19:11:41.354
+Launch V∞: [6.401972936584716, -8.012194016960516, -0.15195278478941954] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006149943335518283, 0.003959642409385435, 0.006112965027685185] km/s
+ V∞_out: [-0.004025024960022279, -0.007175021435683748, 0.004827350055171069] km/s
+ time of flight: 1.8749577773864797e8 seconds
+ arrival date: 2029-04-19T21:21:18.354
+ thrust profile: [0.0287621018982923 -0.01365474543752751 -0.016535647608219115; 0.002100824182419043 -0.000739432783541426 -0.004086853815052803; 0.01350526373777725 -0.006053295146804425 -0.044090682069967815; 0.01875807854542499 -0.012009818865796081 -0.08279498045938526; 0.017120164797742348 -0.014172471581654087 -0.09146322446541943; 0.05144309315590958 -0.04929652447554509 -0.29599238480090245; 0.01121906285273817 -0.011824124776798938 -0.07316510859524056; 0.007067331554793079 -0.008028234072764762 -0.048818053296789794; 0.010505948959646523 -0.012121208372912216 -0.07318555096318961; 0.0035117811405212225 -0.004456410227421073 -0.02610377290128012; 0.006070103806939819 -0.008208016692645042 -0.046683797599465886; 0.0009040421944010453 -0.0011420633922578217 -0.0034896359975248913; 0.0005134524396387598 -0.000608906739581369 -0.0036161985559204257; -0.002271541358849899 -0.00015393950962246003 -0.0007182709241720032; 0.0007032670999753327 -0.002464352438367445 -0.004983565000960208; 0.0008480646592404327 -0.0005424954575422934 -0.0022592998222789747; 2.2975369163373647e-5 -0.0006006622159426768 -0.0006445946181848114; -0.00010355821515260514 0.0005891097220319607 0.0005874170073056656; 9.189283360912388e-5 0.0006419875677187235 -0.0015012761555645007; 1.725800786378523e-5 0.00022808347846359081 -6.363753759124763e-5] %
+
+Mass Used: 64.7480053785157 kg
+Launch C3: 105.20360009498627 km²/s²
+||V∞_in||: 0.00953251868448164 km/s
diff --git a/archive/ES_0.5815622894000816 b/archive/ES_0.5815622894000816
new file mode 100644
index 0000000..08dcef3
--- /dev/null
+++ b/archive/ES_0.5815622894000816
@@ -0,0 +1,22 @@
+archive/ES_0.5815622894000816---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-11T13:39:05.394
+Launch V∞: [6.271368096073807, -8.065235259465657, -0.8944766328956736] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005330527575955336, -0.035414404217464626, 0.046666361403106725] km/s
+ V∞_out: [2.56209994483781e-5, 2.1101443592696592e-5, 1.6810060108241196e-5] km/s
+ time of flight: 1.8749577785122812e8 seconds
+ arrival date: 2029-04-19T15:48:42.394
+ thrust profile: [0.0664524583482479 -0.027186193986287552 -0.037936853694792994; 0.02146387104229563 -0.0019663121741224174 -0.038946098128753624; 0.018901444149146573 -0.002851036910316737 -0.05922515719647811; 0.040404874411940156 -0.009909307178542283 -0.16942982964347783; 0.036772941615898974 -0.012718676748339377 -0.1903044608879375; 0.018407985212178058 -0.00830540706032806 -0.11405208344965485; 0.01024685829994568 -0.005644092316804389 -0.07267478595018131; 0.0047644987719650716 -0.0031925635049375204 -0.03685617341935393; 0.005544546109952962 -0.003451995763981187 -0.04031011524604786; 0.002006820836815563 -0.001121847367481423 -0.015772414199990422; 0.0005026498651365702 -0.0002890938365263762 -0.0040208854986229225; 0.0002994073229096293 -0.0006036718180226197 -0.0005445723739152454; -0.0006798345661853353 -2.0477782080193373e-5 0.00032253718570158786; 0.000460359730762891 0.0008892643687121216 -0.0014408786040174591; -0.001308390996973692 -0.0004711251595532724 -0.0006525998450219233; -0.0002734704532869908 0.0006140465827719352 -0.0010303878076875033; 0.0007680735720305648 -0.004587815471911552 -0.008139331631993861; 0.00204153493316187 -0.003425752008396161 -0.005512576159429529; -0.00019976899030789294 -7.635300207096024e-5 -0.0008703153824733179; 0.0015908498541683143 0.0010297101970137828 0.0016480028991708983] %
+
+Mass Used: 64.95003576973022 kg
+Launch C3: 105.17816603377686 km²/s²
+||V∞_in||: 0.0588246873083178 km/s
diff --git a/archive/ES_0.5816020105686829 b/archive/ES_0.5816020105686829
new file mode 100644
index 0000000..b13ac2a
--- /dev/null
+++ b/archive/ES_0.5816020105686829
@@ -0,0 +1,22 @@
+archive/ES_0.5816020105686829---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-24T22:18:11.303
+Launch V∞: [7.925015702957565, -6.471348109581751, -0.6211240591766617] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3201526018633373e-6, 1.4594374726845126e-5, -2.1191532485055057e-6] km/s
+ V∞_out: [2.1766998288560785e-6, -9.25245764681783e-6, -1.1363100054994491e-5] km/s
+ time of flight: 1.8749577771285182e8 seconds
+ arrival date: 2030-05-04T00:27:48.303
+ thrust profile: [0.13069182835879942 -0.018965410501387524 -0.06620381839916166; 0.01179242349966534 0.003942163902993892 -0.018556545346073577; 0.014775965784794256 0.001280908765137431 -0.04595328709483029; 0.0405548710055996 0.0016453392482993043 -0.16038999214695457; 0.027867596448703447 -0.0018231171503122637 -0.13561790793523681; 0.01789316007489491 -0.0028723496901642384 -0.10121221157193795; 0.012801309670833783 -0.0031242463484419157 -0.08011800222705136; 0.005679088597712575 -0.0026167584832553674 -0.03592320782024938; 0.004341989780635864 -0.0022580305917980575 -0.027975546012586637; 0.0023345998526854705 0.001273534499375564 -0.015189479105373212; 0.0016748803525490322 0.00228138943891007 -0.008394151779802489; 0.0034499610649380962 -0.0013908381882521254 -0.025129755070016663; 0.0006510013565993503 -0.0018036646439786553 -0.00397789693782426; -0.0032314956046892206 -0.00022025534562322425 -0.0016930979228215607; -0.0007587207893121621 -0.00030039605613159224 -0.0014452255307659677; -0.001955518805580353 -0.003286594569499004 -0.0008632140673434574; 0.0036108896272292143 -0.0038455411247537686 0.0031980860752099717; -0.005653363716184365 -0.00461513425411329 0.006966439847341365; -0.003573387694547449 -0.005983384582686283 -0.013061256977712626; -0.005819822639326032 -0.009494578063271617 0.0076136747015610705] %
+
+Mass Used: 65.62725615446698 kg
+Launch C3: 105.07001534439938 km²/s²
+||V∞_in||: 1.4806396828750529e-5 km/s
diff --git a/archive/ES_0.5816712291680283 b/archive/ES_0.5816712291680283
new file mode 100644
index 0000000..716b6f7
--- /dev/null
+++ b/archive/ES_0.5816712291680283
@@ -0,0 +1,22 @@
+archive/ES_0.5816712291680283---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T20:48:44.108
+Launch V∞: [5.569942513576133, -8.211338574960873, -0.36307864224444325] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.337651972444877e-7, 2.2320636609569288e-7, 1.1655625124661295e-6] km/s
+ V∞_out: [-8.22545042603789e-7, -7.844222672573103e-7, -3.665666129853886e-7] km/s
+ time of flight: 1.4387931304888174e8 seconds
+ arrival date: 2027-11-14T03:17:17.108
+ thrust profile: [0.2704015747293832 -0.16415652859756627 -0.1378823738996129; 0.1149388366506676 -0.010656633244636464 -0.1432968560102556; 0.10551956409244469 0.010350592705038911 -0.20524622465765624; 0.08962082132830392 0.01798735475572531 -0.23266065278841344; 0.06974324517443976 0.01820773050397101 -0.22342522934174555; 0.05138341296108715 0.015782398662198358 -0.19254246770048591; 0.03387191413894418 0.011463321119687354 -0.14425012887544025; 0.017867759803808822 0.006449271027508756 -0.0838943304322737; 0.010762101539972915 0.00407250697969342 -0.05613244879701956; 0.004510639812140308 0.0017777306406648748 -0.023525923088378857; 0.00010227378674157375 -0.0009570019169219115 -0.005077199555236167; 0.000923767657504486 -0.0013668202875940616 -0.0026194892157866845; -0.001070268348982285 -0.0031585841404863056 -0.004405968803949341; -0.0018850777344920815 -0.004510081764325361 -0.0018418197659368278; 0.00045296334057858066 0.0009129385966425826 -0.0019476464415962317; -0.0007760519956662408 0.004985235622246158 0.00165017340848097; 0.00037899289717142556 0.0006473822343383245 -0.0011705358328460808; 0.0011430806563193139 -8.97015635037508e-5 -0.005053210022172187; 0.004295107967638255 0.005045491141988181 -0.0049028326316060775; 0.0007876036221386745 0.0043157816897677415 -0.00326315605593513] %
+
+Mass Used: 103.55379379314854 kg
+Launch C3: 98.58216689763734 km²/s²
+||V∞_in||: 1.1942571667467008e-6 km/s
diff --git a/archive/ES_0.5816881178387447 b/archive/ES_0.5816881178387447
new file mode 100644
index 0000000..3b967db
--- /dev/null
+++ b/archive/ES_0.5816881178387447
@@ -0,0 +1,22 @@
+archive/ES_0.5816881178387447---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T06:18:57.532
+Launch V∞: [5.372143231689432, -8.43722975402838, -0.5919244743210998] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00025451527786503754, -0.0016530558408010803, 0.001939073609405498] km/s
+ V∞_out: [-0.0018312528303871048, -0.0014142229108597346, -0.0010869352988018084] km/s
+ time of flight: 1.4464074594618547e8 seconds
+ arrival date: 2027-11-26T08:18:02.532
+ thrust profile: [0.2078569394292029 -0.1279141033168594 -0.11413930561177961; 0.08772713133871081 -0.010889250832166677 -0.11716786646110061; 0.05688016422043845 0.002212661465934675 -0.12020719824237767; 0.0654481463674205 0.007824348247234329 -0.18342714271091196; 0.05102900715421305 0.008900482461256963 -0.1765433275430701; 0.07068360168409656 0.014483003265541871 -0.2751371200859902; 0.03682655727646009 0.008123108028164006 -0.16698077379138207; 0.023062454782200103 0.005074896156850582 -0.11649663573509714; 0.013754189647055815 0.0024974416414321873 -0.08079423554424425; 0.0012952519593556616 0.00036256505539614185 -0.007840641277307141; 0.001139034692637344 0.0007977336335232558 -0.008125073502789982; 0.0010674437744523134 -0.000360685384001886 -0.007896073900708954; -0.00018866284423360845 0.0002642732128282295 -0.00020654458446561473; 3.075816004073753e-6 -2.163551480685759e-5 -0.0003383315569106692; -9.635804316279849e-5 -0.0004000988158862004 0.0007051230295617519; 0.00017382423944614178 -0.0003198372638902684 -0.0009133755781885728; 4.902572981014054e-5 -0.0005095071065401079 -9.58637179574956e-5; 0.0003154447137030087 -0.0004695777173584815 0.00046348383503503916; 0.0005796088309717273 0.0001666047966351735 0.0008336350799361456; -0.0006722232941949712 0.00048418241790325925 0.00039860920916868597] %
+
+Mass Used: 92.98613426900147 kg
+Launch C3: 100.39714340734868 km²/s²
+||V∞_in||: 0.0025607378042599655 km/s
diff --git a/archive/ES_0.5816985674326716 b/archive/ES_0.5816985674326716
new file mode 100644
index 0000000..b8571f2
--- /dev/null
+++ b/archive/ES_0.5816985674326716
@@ -0,0 +1,22 @@
+archive/ES_0.5816985674326716---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T01:17:50.375
+Launch V∞: [5.513787709989993, -8.246654312946209, -0.6789792602711378] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.899077711263439e-9, 2.951842676827206e-9, -6.822731518186723e-9] km/s
+ V∞_out: [-3.571195245369992e-9, 8.426735305742872e-9, 7.744000857809524e-9] km/s
+ time of flight: 1.47687334526934e8 seconds
+ arrival date: 2027-12-29T09:33:24.375
+ thrust profile: [0.23390222015845116 -0.12481003098926054 -0.11039773787226638; 0.08328406857380835 -0.0004913593801358082 -0.0943112952210756; 0.10233434453888249 0.02182947986246166 -0.17606840568844673; 0.09607119120881212 0.03324387574276705 -0.2178165931310762; 0.06502797174619283 0.028774995574719187 -0.18354998309964554; 0.030644919266598597 0.015473248280808106 -0.10408258467818496; 0.02455485456121683 0.014021325139252689 -0.09394305100384588; 0.059525403933016564 0.03888883980273833 -0.23410061654364925; 0.018129167907268755 0.011453556614274439 -0.09160357991821662; 0.005870686265819531 0.005981853322440377 -0.038602950233135126; -0.0017137701158116553 -0.0013888557182375812 -0.00638394945161064; -0.0002698383359994571 0.0012339408944191596 0.0011209041806511317; -2.9899616311268194e-5 0.001201524104586957 -0.0019320494265961294; 0.0038094208199842055 0.002491063399030753 -0.003990192282247153; -0.0014659618649596883 -0.0012151439470933958 0.004073126490828036; -0.00041800405351108996 0.001503765068667103 0.008546802733296987; 0.00011995071268821311 0.00028287564576075203 -0.002752109281008483; 0.003646106115438184 0.009963380765612229 -0.02094470724095172; 0.001754897296025478 0.009632424552596828 -0.01295745942852159; -0.003974167990612703 -0.008614685330812992 0.01696035647786019] %
+
+Mass Used: 101.90564056507901 kg
+Launch C3: 98.87017510394934 km²/s²
+||V∞_in||: 1.0847048872692321e-8 km/s
diff --git a/archive/ES_0.5817371548168608 b/archive/ES_0.5817371548168608
new file mode 100644
index 0000000..9225ff7
--- /dev/null
+++ b/archive/ES_0.5817371548168608
@@ -0,0 +1,22 @@
+archive/ES_0.5817371548168608---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T01:51:52.322
+Launch V∞: [7.218126251495006, -5.966872025981802, 0.5900478280398307] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0310649454007818e-9, -1.0379692643986353e-10, -1.2449895995836903e-9] km/s
+ V∞_out: [6.276554955307557e-10, 1.2143694029127941e-9, 3.335839369708904e-11] km/s
+ time of flight: 1.668767044086029e8 seconds
+ arrival date: 2029-08-13T12:30:16.322
+ thrust profile: [1.0 -0.1358406599154018 -0.1961933635791376; 0.4773107187980786 0.23498662221743058 -0.29548101814086863; 0.1340682914545545 0.11824171407000203 -0.1548309115171268; 0.05716348865464281 0.06949445808418013 -0.09784620358475163; 0.08601980826811542 0.1299322406327545 -0.18736417335692718; 0.026115472293432213 0.04782599317686174 -0.07647216443205924; 0.015490156713626241 0.032665079566924576 -0.05603720087920111; 0.005319407243345139 0.012817068358681325 -0.023192912416110874; 0.003356670691138686 0.009066391435400284 -0.016392555266491; -0.00030709200168973984 0.0008852899379825169 -0.0021848423572558198; -0.0013762292311914064 0.0006630742775702783 -0.002649836275234748; 0.00039248437994575413 0.0007377583761809744 -0.000728132194334783; -0.0020207596913909566 2.460622132210359e-5 -0.0002356214340184426; -4.9878208741009584e-5 0.0008651643469343392 9.787659428241646e-6; -0.00043246106676119085 -0.00018648070751350258 0.0005717737322579867; -0.002080441740703224 0.00430896381039538 -0.0008624147908191932; 0.002587835971748465 -0.0010319805604368656 0.0011115027553786922; 0.0017860735533600897 -0.0012216022417475489 -0.0005177685397847053; -0.0032193765937360954 0.002655134633092909 -0.0018192781855935216; 0.0015654572019819688 0.00031810609749641553 -0.0021051031800081083] %
+
+Mass Used: 165.0504693076873 kg
+Launch C3: 88.05306479634004 km²/s²
+||V∞_in||: 1.6198357406367588e-9 km/s
diff --git a/archive/ES_0.5817548925478687 b/archive/ES_0.5817548925478687
new file mode 100644
index 0000000..42d8e0f
--- /dev/null
+++ b/archive/ES_0.5817548925478687
@@ -0,0 +1,22 @@
+archive/ES_0.5817548925478687---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T04:38:16.907
+Launch V∞: [7.29768358617055, -6.661693335830505, -2.31342368210534] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0009518581945135535, -0.014945414395598433, -0.0017777851877504012] km/s
+ V∞_out: [0.015041885463753145, 0.0006831250280786865, -0.0008995406534166782] km/s
+ time of flight: 1.6045911538552135e8 seconds
+ arrival date: 2029-06-12T08:36:51.907
+ thrust profile: [0.2180892628786359 -0.04407680591339775 -0.10467327764328593; 0.03818974827075121 0.011701738270251682 -0.054309796725040015; 0.06734896377332908 0.039104393367926885 -0.15631788974109762; 0.047439470591411716 0.037063138077364624 -0.1593730297656215; 0.040570650104714626 0.03855052690563446 -0.1777162877674194; 0.016735551261844003 0.01789653812586093 -0.09504618200535017; 0.011900320852384995 0.014482140043225894 -0.08263541449607484; 0.0036079489186172675 0.006142852607912326 -0.0337763851077728; 0.004413424636954176 0.007506971393034418 -0.046549330570758995; 0.0032713321569999383 0.005516912609806953 -0.0379240484801199; 0.0003726727562845585 0.0032883315038513485 -0.015708274959296407; 0.0014284704155658997 0.0030515237416145263 -0.014143096970018509; 0.0011550950068482575 -0.0014882708720833195 -0.006743354395827607; 0.00022501207760229982 -0.004275792716216577 -0.002585370026192529; -0.00033285680825219583 -0.00309052928347956 -0.002924253859932927; 0.0008292109415598513 0.0006977509641262081 -0.0035618173409249824; 0.0006088190435969348 0.004609822145118158 0.009453474803251613; 0.0003518599659221473 0.00028264439155438774 -0.0036236589258391017; 0.004102689648504397 0.0017032997338287583 0.0007768455910830306; -0.000917663859739906 0.0023075621812111624 0.0017307412869715924] %
+
+Mass Used: 77.96078238746168 kg
+Launch C3: 102.98627295743745 km²/s²
+||V∞_in||: 0.015080847643697227 km/s
diff --git a/archive/ES_0.5817560095838296 b/archive/ES_0.5817560095838296
new file mode 100644
index 0000000..455f584
--- /dev/null
+++ b/archive/ES_0.5817560095838296
@@ -0,0 +1,22 @@
+archive/ES_0.5817560095838296---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T17:33:15.979
+Launch V∞: [6.969941668515925, -6.876983010655905, -0.6438281760853262] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.86643021331841e-7, 7.9728448865957e-7, -1.254606237693743e-6] km/s
+ V∞_out: [-6.691653852293762e-7, -1.4089921849832738e-6, -4.478879727985965e-8] km/s
+ time of flight: 1.4115703570554876e8 seconds
+ arrival date: 2028-10-26T11:50:30.979
+ thrust profile: [0.5510488221874784 -0.18809527338018925 -0.24372101739932386; 0.19556748800365717 0.025656483286148606 -0.22215542213566092; 0.08673694777642099 0.028992245144767975 -0.1607833833044888; 0.06400287234634484 0.029319890288915063 -0.16210258826061963; 0.04763332756700974 0.02588061676487479 -0.15062394954315783; 0.04058066513390707 0.024546036724952168 -0.151803924413147; 0.020349737475571627 0.013236748248630782 -0.08658929798831198; 0.055139229138277374 0.03832783985657294 -0.2585629107775455; 0.002847330210421016 0.00423378987796048 -0.02167675396234667; 0.002104897965922923 -0.00033738346723684526 -0.016121501848912104; 0.00033094891949830927 0.0006844531141944308 -0.007834691729118985; 0.0037424199607267302 0.0024461174428854716 -0.009832083348217922; 0.0009987997120658543 0.0017881591694057408 -0.0059531300818753095; 0.0004552580395424076 0.0004738884995977954 -0.005236030390543846; -0.001872198922662339 0.0016630661889036448 0.0005265720387214836; -0.0005793140848508963 -0.00041197044042265906 -0.00332268744016408; -0.017210143691327007 -0.00037577659183569756 -0.007757246933255206; -0.0029775032082456805 -0.0027718540142497865 0.003270445532527336; -0.001905487451167828 0.007306862805987021 -0.008404065921528241; 0.005674257363002762 0.0016763642885397397 0.000432227462968662] %
+
+Mass Used: 117.03827919630021 kg
+Launch C3: 96.28749691168588 km²/s²
+||V∞_in||: 1.5641357990047357e-6 km/s
diff --git a/archive/ES_0.5818106044984165 b/archive/ES_0.5818106044984165
new file mode 100644
index 0000000..ab043e5
--- /dev/null
+++ b/archive/ES_0.5818106044984165
@@ -0,0 +1,22 @@
+archive/ES_0.5818106044984165---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:08:42.894
+Launch V∞: [7.096792896687844, -6.81738120048287, -0.4246449988265091] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.5078537832174247e-9, 9.322209574383464e-10, 3.7607648624582387e-10] km/s
+ V∞_out: [5.899942458531702e-9, -3.534689805416952e-9, 1.4969976531167528e-9] km/s
+ time of flight: 1.4565558560280862e8 seconds
+ arrival date: 2028-12-18T04:01:47.894
+ thrust profile: [0.3778871631287528 -0.11859679372419618 -0.16425363147143557; 0.1655964622008546 0.02613877643608586 -0.19089638050519764; 0.11939795736507512 0.043515170949929384 -0.2262677895391773; 0.07596901328605149 0.03666708726179352 -0.19916162635434814; 0.060919749709401255 0.03428211929768448 -0.1998516673982483; 0.04454138269034405 0.027823061836642883 -0.17352259294061864; 0.027657476216269298 0.018313003729377976 -0.12245670962307906; 0.011639146577380447 0.007794098851402185 -0.053439934303537315; 0.0027360911881055103 0.0031498410313751135 -0.007978423049054375; 0.00924901056809133 0.007576595641912854 -0.02724607133050178; 0.012238206126963722 0.0012670777612054243 -0.016488328437976922; -0.003914003852176782 0.010491397113665361 -0.011904372814945937; -7.09755080745964e-5 -0.017649252321975766 -0.003458591096927327; 0.007546570041801286 0.0013498240581003573 0.004825380330643494; 0.0008127598032617632 -0.0004759319890592313 -0.0016770691430457027; 0.003643091516754335 0.0012632308921129353 -0.00789397702201318; -0.001290268356836688 0.00838621636754478 -0.00744488250762953; 0.03245339959282216 0.006507496457502175 0.006568722334775127; -0.0018701306653837197 -0.025707261657997818 0.00951356781400273; 0.024515851806455026 -0.0006045721961376302 -0.007072541296494004] %
+
+Mass Used: 112.82040976195867 kg
+Launch C3: 97.02147922620466 km²/s²
+||V∞_in||: 1.812206519290054e-9 km/s
diff --git a/archive/ES_0.5818437504773835 b/archive/ES_0.5818437504773835
new file mode 100644
index 0000000..550ce7a
--- /dev/null
+++ b/archive/ES_0.5818437504773835
@@ -0,0 +1,22 @@
+archive/ES_0.5818437504773835---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T10:55:51.254
+Launch V∞: [5.499337586492773, -8.28804010097217, -0.687451106896945] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0014440933195177922, 0.009083088407207828, -0.011563945471721007] km/s
+ V∞_out: [0.010428245028391157, 0.008481670729227798, 0.006170868789580324] km/s
+ time of flight: 1.461767218827906e8 seconds
+ arrival date: 2027-12-12T07:34:32.254
+ thrust profile: [0.2042335897000046 -0.11749238099553558 -0.10373600458177683; 0.10905895910479647 -0.00725565878036681 -0.1327204394327144; 0.09039423920606147 0.011892651213564033 -0.17206483512461618; 0.11132911672290816 0.027293140325753796 -0.26496866951247866; 0.038790850021682866 0.012432992469893118 -0.12355349816985493; 0.046321432929242366 0.017586706803109208 -0.17263629023679905; 0.029677843493068255 0.012153053944624997 -0.12450764336154385; 0.027823079498242104 0.012544725593808172 -0.12910520539359518; 0.013244241202254906 0.007677979761985294 -0.06552027652201496; 0.010085834364398926 0.004683260114172166 -0.04895581443955012; 0.004492099108414469 0.002256893102894248 -0.029657106802060795; 0.0012614353189218607 0.0007417393889306967 -0.002142886197701592; -0.001388148116643214 0.0012238203530715677 -0.003779115906884128; 0.006176780314643207 -0.00828602153531885 -0.0023725556067634435; -0.001518878418315328 0.0032450770345646925 -0.0029114316099857485; 0.013394353362841303 -0.010876158812784444 -0.002650943315131702; -0.002814061946401103 0.0006854758219154539 0.005609571977023244; -0.003698664076477127 0.00253479552087868 0.00633010791553863; -0.00016137793843477312 -0.001475453042196472 0.003512934096324577; 0.00025508523318675463 0.003771803672663772 -0.010560140592787341] %
+
+Mass Used: 98.94405771581296 kg
+Launch C3: 99.40691162990876 km²/s²
+||V∞_in||: 0.014775409821780442 km/s
diff --git a/archive/ES_0.5818692625496528 b/archive/ES_0.5818692625496528
new file mode 100644
index 0000000..8c89115
--- /dev/null
+++ b/archive/ES_0.5818692625496528
@@ -0,0 +1,22 @@
+archive/ES_0.5818692625496528---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T12:22:04.105
+Launch V∞: [7.057000294675981, -6.8978851690795695, -0.17618879281495056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012057862438280818, -0.007085367503759147, -0.00690103200779126] km/s
+ V∞_out: [-0.008808965885787879, -0.000985969819081774, 0.004539839162463021] km/s
+ time of flight: 1.429794876334909e8 seconds
+ arrival date: 2028-11-17T08:53:31.105
+ thrust profile: [0.4038578438869661 -0.13158400114688948 -0.1638557892367828; 0.1683680736087943 0.024371259143738777 -0.1922961826170965; 0.06832090784248093 0.023089688070983834 -0.13449517827972077; 0.06107724556272759 0.027790857673098638 -0.1654867932397467; 0.06846305712637749 0.037989885022499795 -0.23891780628870837; 0.026220224960218932 0.015274124403815552 -0.1026447199506402; 0.05077506451936275 0.033527521265886345 -0.22119856969814744; 0.029386263229364634 0.019832007023401307 -0.14413051197665294; 0.010399062291866532 0.006780057081763701 -0.054274397747517446; 0.0026511458819696806 0.0007399639902740331 -0.014539243433238945; 0.004798062889925038 0.0033762577608352933 -0.02668328114150224; -0.0019497400139198656 0.0024994427128625252 -0.0018971942259699477; 0.0025090272400329064 -0.0006557061248118752 -0.0013074278364385169; -0.001367639881757303 0.004820276244838658 -0.0029730090407549523; -0.0005933784676638955 -0.0020031140487554496 -0.0006338464511683628; -0.0006177461971679513 -0.001228864387676146 0.0021163582822002203; -0.010432306424121256 -0.0028053217286973277 -0.005585565019074079; -0.0005960930769286633 0.0011765070873924542 -0.014652978698933134; 0.004484380053278493 -0.0013459405390437618 0.006113333711222069; 0.0018578089178546721 -0.008491535747636272 0.010607704460472643] %
+
+Mass Used: 110.6042994837212 kg
+Launch C3: 97.41311545557835 km²/s²
+||V∞_in||: 0.009963964868549599 km/s
diff --git a/archive/ES_0.5818822035304504 b/archive/ES_0.5818822035304504
new file mode 100644
index 0000000..1446b7d
--- /dev/null
+++ b/archive/ES_0.5818822035304504
@@ -0,0 +1,22 @@
+archive/ES_0.5818822035304504---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-10T16:59:51.682
+Launch V∞: [6.2376799908009914, -8.138177563989343, -0.3234678977959405] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6718163173496863e-6, -1.8892497331299687e-6, 1.3805819297604752e-6] km/s
+ V∞_out: [-1.1433510995565816e-6, 2.773591970337502e-6, -1.8977986118583993e-6] km/s
+ time of flight: 1.838012475147855e8 seconds
+ arrival date: 2029-03-07T00:53:58.682
+ thrust profile: [0.012501957073144089 -0.005488525753317347 -0.007135358761664825; 0.013648556481083833 -0.002407021977281197 -0.027017421805103244; 0.0191030876291119 -0.004102067302311465 -0.0560498974108052; 0.02609508910476445 -0.009108213508360725 -0.10382927676644878; 0.02085637706564981 -0.009977346087781365 -0.10191373123753109; 0.04452495457560437 -0.02704056890829667 -0.24606651177636796; 0.016821818852120515 -0.011609433388386334 -0.1108772169659687; 0.010710945045161752 -0.007479331897827936 -0.06866786689546088; 0.004163291777579125 -0.003064066559405469 -0.031017905847532508; 0.002501331589856736 -0.0016901139208779343 -0.022714060325109954; 0.0072860119635165315 -0.007371977470249597 -0.05462172819996347; 0.000828082564314463 -0.0009238322394657134 -0.008210462590071283; 0.0010065042368371815 -0.0010484235509176155 -0.0014679214233430814; -0.0004241871789495215 -0.0006244570119890054 -0.0011577701152827849; -0.00014090067442229254 -9.013645724244053e-5 0.0008951463991649414; -0.0024673510745523717 0.0011358479482811595 -0.0024737293412110187; -0.0010303675372801684 -0.0005793161159329992 0.0012615000564684296; 0.001019509606212022 0.0011562789850486982 -0.0022085335440965408; 0.0011115206274024967 -0.00043309030768825044 0.0018400025202747563; 0.003143819348248163 -0.0001497279755414232 -0.0006218924809831606] %
+
+Mass Used: 64.94380371807392 kg
+Launch C3: 105.2432172115631 km²/s²
+||V∞_in||: 3.5516015334731534e-6 km/s
diff --git a/archive/ES_0.5819729834872093 b/archive/ES_0.5819729834872093
new file mode 100644
index 0000000..d1da8cd
--- /dev/null
+++ b/archive/ES_0.5819729834872093
@@ -0,0 +1,22 @@
+archive/ES_0.5819729834872093---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T21:28:36.712
+Launch V∞: [5.50518831212842, -8.399206457704919, -0.9006788445021299] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0255499115121496e-5, 0.004282422691944757, -0.0017115812743362384] km/s
+ V∞_out: [-0.0004408369827051065, -0.0002779310474823036, 0.004582275758449612] km/s
+ time of flight: 1.4865819958706632e8 seconds
+ arrival date: 2028-01-12T11:25:15.712
+ thrust profile: [0.1029095424652238 -0.06034970202965258 -0.058228347437427566; 0.023341855518925453 -0.0025814769330118 -0.03229291117033767; 0.07872102170311403 0.0059094366802527705 -0.16684871120145525; 0.09132239913212906 0.014041702484631102 -0.2564843033564893; 0.07639834179667294 0.015662126924437282 -0.265565748874339; 0.050722952735742934 0.012585876892106213 -0.20949109372666871; 0.021658839958356546 0.005823921318367413 -0.10557431808488572; 0.00852740756066218 0.0015338414173968172 -0.04688009003647562; 0.007841346863130448 0.0006599426932543659 -0.047671001941750515; 0.0035349454526966855 0.000499212209911398 -0.021356880892525423; 0.0011029671992847795 0.00023866114042561172 -0.009819225855211012; 0.0014817533671621797 -0.0009709181903025392 -0.0014443703853099367; 0.004797340842039529 0.0022739239642185676 -0.0002777360601338857; 0.008484400397900308 0.002671411896476296 0.00681781703183215; -0.013707625134696432 -0.005803321099525118 -0.0017294239289260913; -0.015436430125447773 0.003596271270190912 -0.01189658706655037; -0.000195888633537231 0.001889980818339338 -0.00523720194275348; -0.005395557167183122 0.002353442430452943 -0.01105119621766294; 0.0011481884292752157 0.0010234482583535045 -0.00020687427773656537; 0.015377227809173987 -0.010333858261744367 0.008172007569831264] %
+
+Mass Used: 85.92270659793803 kg
+Launch C3: 101.66498985208106 km²/s²
+||V∞_in||: 0.00461180655995066 km/s
diff --git a/archive/ES_0.5819795377268387 b/archive/ES_0.5819795377268387
new file mode 100644
index 0000000..3270870
--- /dev/null
+++ b/archive/ES_0.5819795377268387
@@ -0,0 +1,22 @@
+archive/ES_0.5819795377268387---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T01:42:24.947
+Launch V∞: [5.488554850527768, -8.292796752124328, -0.5503707964289637] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6133168997692535e-9, -1.2452886022452682e-9, 2.1491915831936894e-9] km/s
+ V∞_out: [1.6348334800556534e-9, -3.696783866705425e-9, -4.704051536719088e-9] km/s
+ time of flight: 1.527181395013158e8 seconds
+ arrival date: 2028-02-28T15:24:43.947
+ thrust profile: [0.22887636178309087 -0.12815435858999202 -0.11868626029725685; 0.04757000147167203 -0.0027231061760393614 -0.06462013377127633; 0.09284103774026414 0.009370076715428523 -0.19313871145010578; 0.10071631610998183 0.01862567809699734 -0.27924298500040756; 0.06806287845626341 0.016374514490678015 -0.23714746147049096; 0.033256341586246525 0.009916583472497483 -0.1397042309547571; 0.013040624120057196 0.004455655945906376 -0.06244890855509761; 0.013010246447473296 0.004403508605325104 -0.06446185698704476; 0.009614004012563156 0.002535391039711708 -0.04637682593513499; -0.0015800316775768618 0.0035424131432363094 -0.004665991219950905; 0.0012049397380325243 -0.004528293012476959 -0.004246514709096847; 0.008548383575992264 0.003611098216866359 -0.058812027530387834; 0.006685854775540273 -0.011129723296478364 -0.0038446634516475214; 0.00320636270629061 0.004125398155910422 -0.009587856781592529; -0.0031292432490627547 -0.0004890555437069928 -0.0014657694094141497; 0.0001873923237234341 0.0007308559398741265 0.0015001858079014651; -0.00875504059010903 0.006261696189728693 -0.009152153582164244; -0.0014982741395036818 -0.012894368867590711 0.011924821774271933; -0.012747355597351455 0.027824014599976 0.006317058842460065; -0.008995536841100549 -0.00048322158937863947 0.035424695129849484] %
+
+Mass Used: 100.32334207297617 kg
+Launch C3: 99.19762033285754 km²/s²
+||V∞_in||: 3.6054394160451724e-9 km/s
diff --git a/archive/ES_0.5820793088461838 b/archive/ES_0.5820793088461838
new file mode 100644
index 0000000..e424d22
--- /dev/null
+++ b/archive/ES_0.5820793088461838
@@ -0,0 +1,22 @@
+archive/ES_0.5820793088461838---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T03:56:21.129
+Launch V∞: [5.358427240968885, -8.150702205467722, -0.5588844867287255] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001135113117047718, 0.005298931870040384, -0.007377355261591984] km/s
+ V∞_out: [0.005625729298096343, 0.005972709645160111, 0.0043120567914480094] km/s
+ time of flight: 1.413828152317262e8 seconds
+ arrival date: 2027-10-14T12:56:36.129
+ thrust profile: [0.5172660482506929 -0.3012666688510042 -0.23397791285700406; 0.21543774084681777 -0.008784527227825766 -0.23094971872204265; 0.1640167266151424 0.029214746708305386 -0.2705603054254012; 0.09478720610438926 0.029235784097216905 -0.21159062419485636; 0.06132008398311004 0.02448013449617456 -0.16980408824380272; 0.034641843271498614 0.015931815661684532 -0.11380643497114619; 0.041360962271922264 0.02171096500952756 -0.1508886512968949; 0.022619285088379057 0.01318259140226415 -0.09400679087038293; 0.011424618714256183 0.006988668134368459 -0.05150121990121923; 0.0030386698881905605 0.0018773699593084038 -0.014761459968463543; 0.0048061162740922776 0.0030837776728456674 -0.024473752197138123; 0.00017610536732211985 -9.91597314160798e-5 -0.00022623893314866595; 0.00013575140121497312 0.00018469074364806847 -0.0007350448252490972; 6.176229277802032e-5 0.00022981668419185008 -4.823524151505881e-5; 0.0003481752514911153 0.0002647304727896487 -0.0003008475680639544; -0.00017033680921959508 0.00042347434505168305 -0.0007544314280571553; 0.00020447366900394075 0.0003037062846083943 -0.0011855199581241927; 0.00024322820970591426 -0.0003323832633147557 -0.0018367344978722166; 0.0026368990555165114 -0.0006478729667199837 -0.0023064938790529647; 9.056996308671824e-6 0.00019492453111123438 -0.0006575139977719569] %
+
+Mass Used: 122.24812227108214 kg
+Launch C3: 95.45904080847983 km²/s²
+||V∞_in||: 0.009153826052944332 km/s
diff --git a/archive/ES_0.5821316456160769 b/archive/ES_0.5821316456160769
new file mode 100644
index 0000000..443a509
--- /dev/null
+++ b/archive/ES_0.5821316456160769
@@ -0,0 +1,22 @@
+archive/ES_0.5821316456160769---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T11:28:02.453
+Launch V∞: [5.295657049070303, -8.214430340747073, -0.8344812293126306] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007153602977229078, 0.05852579437043115, -0.0416214728149236] km/s
+ V∞_out: [0.05091095272086125, 0.042963055807902675, 0.02775662314961503] km/s
+ time of flight: 1.4154694758058572e8 seconds
+ arrival date: 2027-10-17T18:03:49.453
+ thrust profile: [0.4942165598268943 -0.2896486538581842 -0.2494701975274732; 0.20482656302408778 -0.014560519541102114 -0.23650196625205244; 0.15174279961114465 0.02089298878850516 -0.27114755290273024; 0.08021548623597546 0.020314338802672326 -0.19355174480628043; 0.05066351594306676 0.017244790564991067 -0.1531687563233483; 0.038863749357066976 0.01614083325282037 -0.13730457232018484; 0.022096977703236848 0.01044097294734348 -0.08635146546070387; 0.01503521258807112 0.006496517410981529 -0.06515694079697217; 0.007982445463216043 0.00362106982956633 -0.039022461250057365; 0.019261660083305904 0.010387613930544139 -0.09771202261581151; -0.0008853317600536984 0.000534889712284639 -0.002926681584658508; 0.0005203974829364399 0.0012213188107076927 -0.0062003563733383504; 0.002627382282719011 -0.0007886236035637129 -0.0010716294305448213; -0.00012336912083410066 0.00028223040698890223 -0.0026847888711244855; -0.0005381756460231783 0.00033611549022624973 0.00018214471818246984; -0.0005628890533978168 0.00020088779915431398 -0.0005762851130912824; 0.0015684967705703258 0.0006681872763808791 -0.0045430013190138; -0.0004703253612919939 0.0004202605026696253 0.0005332793671857585; 0.0010669768206314548 1.6151317819196865e-5 0.0011833981092635392; -0.0016319437936068077 0.003544108140438774 0.0029159259269945703] %
+
+Mass Used: 117.88653798125279 kg
+Launch C3: 96.21720832642919 km²/s²
+||V∞_in||: 0.0721719449753797 km/s
diff --git a/archive/ES_0.5821824918290721 b/archive/ES_0.5821824918290721
new file mode 100644
index 0000000..f5e23b7
--- /dev/null
+++ b/archive/ES_0.5821824918290721
@@ -0,0 +1,22 @@
+archive/ES_0.5821824918290721---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T23:28:46.908
+Launch V∞: [7.304400515338396, -5.652381733089946, 0.43275071747343946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.996794005286533e-6, 2.5524051438657195e-5, 7.459161488671935e-5] km/s
+ V∞_out: [7.275127272713663e-5, 8.776162524881921e-6, -3.0506278949305744e-5] km/s
+ time of flight: 1.8749577787459177e8 seconds
+ arrival date: 2030-04-12T01:38:23.908
+ thrust profile: [0.9450502037234153 0.022754807280144916 -0.11319658299144751; 0.44127772628285716 0.3257041137850896 -0.20604117136267253; 0.24151140513579838 0.31060861442302035 -0.21828823839909553; 0.07092117752719974 0.13120841081728254 -0.10957894417073454; 0.014328428972912567 0.0368065904216341 -0.036681604702608936; 0.004612329032117966 0.017667616544238762 -0.01915301407907797; 0.016837383343746348 0.07423874442536837 -0.07777801599562773; 0.0008148516334016581 0.003058249569863928 -0.003510266828942236; 0.0018702013472948842 0.019386801773263698 -0.023009922813310265; 0.0002447519398790057 0.0006357892798259483 -0.0015391696005496941; -7.867931986757681e-5 0.00035151188477462844 -0.0012442201197188898; -8.543633541620746e-5 0.0012476783452803556 -2.2460234113254145e-5; 0.00015245377250015758 0.0013840160047107657 -0.001880520032248617; -0.0006785229020414719 0.0002959903865572139 -0.00018702553940323302; -0.00125989481526218 -0.00042036853735002186 -0.000798534384019585; -5.837288169661234e-5 4.942374974123545e-5 0.0011803875756376866; 0.0004800872996002698 0.000588206762014463 -0.00047594207534283996; 0.0021425585570690716 0.0011756530248026326 0.00024359503152116625; -0.0020516516646443203 -0.0006498954344416237 0.0026656879323374116; 0.003369973027009908 -0.0007707688556649825 -0.001939881227176667] %
+
+Mass Used: 180.5156443842261 kg
+Launch C3: 85.49095932851851 km²/s²
+||V∞_in||: 7.946900089743171e-5 km/s
diff --git a/archive/ES_0.5821872792139735 b/archive/ES_0.5821872792139735
new file mode 100644
index 0000000..9af1a01
--- /dev/null
+++ b/archive/ES_0.5821872792139735
@@ -0,0 +1,22 @@
+archive/ES_0.5821872792139735---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T17:18:31.634
+Launch V∞: [5.998009652733452, -7.453824628710263, 0.06458348298707782] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.394603852952177e-6, -5.338189377040855e-6, 0.00022443682336011308] km/s
+ V∞_out: [0.0001801310555233753, 0.00010447785093610402, -8.423412389949936e-5] km/s
+ time of flight: 1.6679236343334547e8 seconds
+ arrival date: 2028-07-31T04:31:14.634
+ thrust profile: [0.6867353477111824 -0.26540721258791905 -0.19091804241456684; 0.3239447468544098 0.06490832579153465 -0.24275621311683931; 0.19314667212174189 0.09299543669487625 -0.23493247746918264; 0.11595875015831272 0.07882917616481491 -0.19554545102690044; 0.05765084334706196 0.04801573688670146 -0.12722346316357674; 0.03744729205538962 0.03625928192889161 -0.10105161815060788; 0.008751103278876236 0.009474709388306994 -0.027687882396709593; 0.0040408393438101115 0.004458043392042758 -0.015077068210063384; 0.004693269951708584 0.006113872201594837 -0.01843145736597668; 0.0010978154690539747 0.005181051951365137 -0.007197266524366546; 0.008842463936789877 0.013269282093202786 -0.049457587363138364; 0.0002712415970911621 0.0009377286743201699 -0.00516108042420119; 0.00111650696305852 0.0007485575157104047 -0.0016317212452240481; -0.0018923071069749048 0.0032165223939753934 -0.005334926945862303; 0.0010690055763303587 0.0067119891908241636 -0.020203358653079595; 0.0008630492813225248 0.0031344238303027024 -0.002864903652556995; 0.003183869216018485 0.0026149048798997697 -0.014852824079773754; 0.0007516685786391055 0.0014343507074941583 -0.010602229879139191; 0.0008017846581689827 0.0011731354288560788 0.0009939688599622813; -4.1511366595531644e-5 -0.0008591330581293544 -0.0007025241175883548] %
+
+Mass Used: 145.23636998890015 kg
+Launch C3: 91.5397924161261 km²/s²
+||V∞_in||: 0.0002245046299427039 km/s
diff --git a/archive/ES_0.5822865353705988 b/archive/ES_0.5822865353705988
new file mode 100644
index 0000000..69c3b69
--- /dev/null
+++ b/archive/ES_0.5822865353705988
@@ -0,0 +1,22 @@
+archive/ES_0.5822865353705988---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T08:31:22.055
+Launch V∞: [5.627494617190996, -8.13995179747382, -0.5065190225166666] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4190684357363463e-6, 5.747031631525235e-7, -7.209906021671539e-7] km/s
+ V∞_out: [2.3604293936762263e-6, -1.0312522630011538e-6, 2.5971413408724974e-7] km/s
+ time of flight: 1.473553008273255e8 seconds
+ arrival date: 2027-12-23T20:33:02.055
+ thrust profile: [0.22675604551461448 -0.12810060274088966 -0.10015395028777667; 0.15507053610298382 -0.0035823034340716833 -0.1644008671640603; 0.12439246755913429 0.023577967250772006 -0.20594537341780228; 0.10217800724032776 0.03243203948590359 -0.22528839665495845; 0.07669127899036353 0.03143079357413286 -0.20965610695057324; 0.05062548544980344 0.024162604906562208 -0.16514867799316746; 0.027279416190535984 0.012884368725276851 -0.10245076673629519; 0.009855941768827413 0.007987351231118989 -0.05022487400830537; 0.01474989453069401 0.009025092868706487 -0.07128515883152989; 0.012463820339455825 0.008430288964508774 -0.06512756885461714; 0.0023666115241282835 0.0012444334338287666 -0.008424568540182701; 0.0019824465691815714 0.0048777909436198185 -0.028914383678508106; 0.0020563167966884603 -0.0028160220558600063 -0.0032136216743749993; -0.006190211228513563 0.004164682318654568 -0.0027886038544182377; 0.0037442058163379695 0.00797221174155998 0.0022756936114120465; 0.00398466640130054 -0.00880335018888178 0.0006346271737230338; -0.003959215487425129 -0.00011290795977019559 0.008831392821652316; -0.009314556195330446 -0.012417696889411235 -0.0075481679124501265; -0.0024417441155896577 -0.003001208970568293 -0.0021094903030836566; 0.017127910187743803 0.0038728697658368914 -0.010857534914917137] %
+
+Mass Used: 106.59386862971951 kg
+Launch C3: 98.18407245188214 km²/s²
+||V∞_in||: 2.5888227577272963e-6 km/s
diff --git a/archive/ES_0.5822875906403592 b/archive/ES_0.5822875906403592
new file mode 100644
index 0000000..41f1284
--- /dev/null
+++ b/archive/ES_0.5822875906403592
@@ -0,0 +1,22 @@
+archive/ES_0.5822875906403592---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T13:18:06.673
+Launch V∞: [5.380254110474038, -8.253019865241232, -0.7649443366105558] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.0189927355260907e-5, -4.498930216504523e-6, 5.307707430019788e-6] km/s
+ V∞_out: [-1.9607986151955513e-5, 7.735777182219557e-6, -3.3433657813763557e-6] km/s
+ time of flight: 1.4291518303916737e8 seconds
+ arrival date: 2027-11-02T15:57:49.673
+ thrust profile: [0.3358822343138075 -0.1932193400758237 -0.15297081839264384; 0.13981946449202146 -0.0038662908246151436 -0.1446876438571429; 0.14113363254201458 0.02660404730096744 -0.2219816915227697; 0.12886022132578065 0.041135843268569165 -0.26682617940112685; 0.09126112157017781 0.03811655439019237 -0.2323670599135476; 0.03647843724515639 0.01894921188116443 -0.10974666224185643; 0.0383681137751019 0.023798960675657746 -0.12864459510007542; 0.029717087320767947 0.01958862882716984 -0.11608937880178762; 0.008969961837151928 0.006789497193767972 -0.03929720884851145; 0.0029101436486158845 0.004340034337489768 -0.016980771438404506; 0.0041830709793116184 0.003394472812304638 -0.021256785793886297; -0.0004003077910318231 0.00024687067434257467 0.0013284032910031388; -0.0009877287007804905 -0.0005507914434709177 0.0020366905639675687; 0.0016468302675137871 -0.004563232631907296 7.51097623854103e-5; -0.0015512977159868576 0.003284562041485888 0.005225411319410922; 0.0017502337164258888 -0.004799614223025498 0.0013337708734060692; -0.0006525160741841851 0.001356994802685535 0.0063898713364878845; 9.674875801352306e-5 -0.00206410085179492 0.001027986201976857; -0.0016721345664330906 -0.0007556307018324732 0.006070626396816572; -0.0011782015151072188 -0.0005995160158357615 -0.0032757079063125633] %
+
+Mass Used: 109.74195808695049 kg
+Launch C3: 97.64461102745175 km²/s²
+||V∞_in||: 2.135521711119738e-5 km/s
diff --git a/archive/ES_0.5823178425100198 b/archive/ES_0.5823178425100198
new file mode 100644
index 0000000..7dfc5f7
--- /dev/null
+++ b/archive/ES_0.5823178425100198
@@ -0,0 +1,22 @@
+archive/ES_0.5823178425100198---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T08:50:16.422
+Launch V∞: [7.669314499407917, -5.617409517195735, 0.06402214940442756] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00020671251440267628, -0.000663665712376491, -0.001131138332593519] km/s
+ V∞_out: [-0.0012101396894300066, -0.00015169900740633546, 0.0005277910124967382] km/s
+ time of flight: 1.7879177005698615e8 seconds
+ arrival date: 2029-12-31T17:13:06.422
+ thrust profile: [0.780784749528202 -0.04407910292788673 -0.16396463519866558; 0.37705959092944813 0.22595398793380134 -0.26446825572683125; 0.16280390407061793 0.17180195202517082 -0.21102354776763954; 0.06663746795544116 0.100155676985404 -0.1352095386532169; 0.020489716894141363 0.03945661414159919 -0.06002483628750823; 0.011783955188613424 0.02942098589066526 -0.04735331426152901; 0.006635091740751366 0.0177564480094073 -0.03261084079021469; 0.006774270737185417 0.02471332064814396 -0.04338362092463352; 0.002451981721635321 0.011877056629786616 -0.020790777058882336; 0.0007208911191165377 0.007773752759638772 -0.012997042067672505; 0.0003305443732872669 0.0003936324443849179 -0.002124155166384419; -0.0013999631944050426 -0.0002969610067183159 -3.929673405739741e-5; 0.0019053552866228056 0.0005562065614490738 -0.0012096334530773405; 0.0002654892925234728 -0.0002451175611918444 0.0010205491285301053; -0.0033346929878972286 -0.01042359107089439 -0.006565462123283874; -0.005849676431512758 -0.00017123839834352664 -0.005577366579845941; -0.000327056581686361 -0.0016557449796239644 0.005411515012947673; 0.006870623168143448 0.004636116630005242 -0.0052731571303062386; 0.011926263907337038 0.005772814140049948 0.0029896680283754322; 0.002064965225718001 -0.003029851970637836 0.010697607200722917] %
+
+Mass Used: 152.16713803479934 kg
+Launch C3: 90.37777341032408 km²/s²
+||V∞_in||: 0.001327650620026714 km/s
diff --git a/archive/ES_0.5824491753109826 b/archive/ES_0.5824491753109826
new file mode 100644
index 0000000..69e3ea3
--- /dev/null
+++ b/archive/ES_0.5824491753109826
@@ -0,0 +1,22 @@
+archive/ES_0.5824491753109826---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T07:59:43.354
+Launch V∞: [6.296630392262508, -7.001101562133677, 0.3908469952374952] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008342086383819032, 0.0008602652825832128, 0.000830072885374889] km/s
+ V∞_out: [-0.0009931245254442783, -0.00048011179736787894, 0.0009516964815324697] km/s
+ time of flight: 1.8342905254307815e8 seconds
+ arrival date: 2029-02-09T08:30:35.354
+ thrust profile: [1.0 -0.2720272576997086 -0.20956276213172806; 0.3079225696743242 0.10876164231031618 -0.2074820726824745; 0.11197214091098107 0.07636546708912124 -0.1303181188911677; 0.10970438893559231 0.10423239909416622 -0.1789065046275604; 0.049673573489934585 0.058479711781270066 -0.10553862877446654; 0.029242521741977185 0.04095278088532676 -0.07700270623047263; 0.022968652273646403 0.03730881964975221 -0.07253252807562104; 0.001141217629712192 0.0019916634378595328 -0.004475076373921088; 0.0013607094962399362 0.0022631673351465225 -0.003721689936720236; 0.0006400653234486019 0.0007147089503937477 -0.0022602522728689877; 1.896257672131857e-5 -0.00021305988965520653 -0.00273948430951771; 0.0006707706523930442 0.001766993271700429 -0.003931823418541799; -0.00014426688996761034 0.0010003862292125732 -0.00015079881327124435; 0.0008185067563160213 0.0012514111227266813 -0.001944324722190182; -0.0002883929088944729 0.0015877211113249855 0.000248123002407886; 0.0009186390346396828 0.0016256918782808576 -0.0006128303826717452; 0.0006549311062644912 0.000841507308742803 -0.0007663177740746775; 0.0022781687771974662 -0.0014434644341626856 -0.003022134097442087; 0.0016598585878428882 -0.00026841264368363416 -0.0020203050742911366; -0.000426485941399655 0.0021052231208842868 0.0004912324400186854] %
+
+Mass Used: 161.4322284658756 kg
+Launch C3: 88.8157387537607 km²/s²
+||V∞_in||: 0.0014577315952546126 km/s
diff --git a/archive/ES_0.5824886879429229 b/archive/ES_0.5824886879429229
new file mode 100644
index 0000000..7a15c4d
--- /dev/null
+++ b/archive/ES_0.5824886879429229
@@ -0,0 +1,22 @@
+archive/ES_0.5824886879429229---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T06:38:21.697
+Launch V∞: [5.372966202576427, -8.292755890494785, -0.534641868372175] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.768408730320267e-5, 0.00742708809651872, -0.0030536024858297296] km/s
+ V∞_out: [-0.006369432080573513, -0.0036822780448553328, 0.003217861488632154] km/s
+ time of flight: 1.426096724102754e8 seconds
+ arrival date: 2027-10-30T20:26:13.697
+ thrust profile: [0.3028767178717254 -0.19048594593866489 -0.13884274143809186; 0.19179807461330006 -0.008435419161448979 -0.209149946371677; 0.0870731592261322 0.015271658601148336 -0.1556568112753127; 0.10702693014073905 0.030816459520968637 -0.24556073111702528; 0.07723445885919983 0.02845455088002081 -0.21807268605418026; 0.04153894014192737 0.01820822877883831 -0.14273945575532318; 0.027453784617980675 0.013761923763589888 -0.10961353376302675; 0.025207580588182274 0.012186304036091881 -0.10050009129839282; 0.017369913118505 0.008763720382661143 -0.07793433212746895; 0.01053110497618124 0.005815940726109952 -0.048994104375682; 0.002486676036353231 0.0010128147655005964 -0.013422014342209456; 0.004637793151217629 0.002233505914385016 -0.018757460998049313; -0.0013508386970913153 0.00022926252476851075 0.0035806613225330877; 0.001549837276161715 -0.00010500718742231602 -0.0018745384284098348; -0.0004484179890909974 -0.0015070225134081149 0.0014150760118808068; 0.002075083008087697 0.00018476805455968308 -0.0005976109104651441; -0.004789672823212587 0.0009789313310554731 -0.003244661691742316; 0.0005655532044960555 0.0007435215895905061 -0.0010173647955247444; 0.002310948432714374 -0.0005969731030674744 -0.003452794461255029; 0.001758363079425883 -0.0022604475660626946 0.0036912599175262205] %
+
+Mass Used: 108.34442259552088 kg
+Launch C3: 97.92440800078099 km²/s²
+||V∞_in||: 0.008030344853233846 km/s
diff --git a/archive/ES_0.5826349812810319 b/archive/ES_0.5826349812810319
new file mode 100644
index 0000000..6307fa9
--- /dev/null
+++ b/archive/ES_0.5826349812810319
@@ -0,0 +1,22 @@
+archive/ES_0.5826349812810319---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T18:27:40.150
+Launch V∞: [5.4228824683232615, -8.292985398257839, -0.86980997927002] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7642989248263207e-6, -6.135594845460509e-7, 7.244052134221403e-7] km/s
+ V∞_out: [-2.7150752912761873e-6, 1.0839978212141093e-6, -4.684326885150916e-7] km/s
+ time of flight: 1.416694785195375e8 seconds
+ arrival date: 2027-10-19T11:05:38.150
+ thrust profile: [0.2542033942178368 -0.14947195896012203 -0.12542270851157683; 0.14559246158392133 -0.007131300060346314 -0.16240611105137576; 0.14332629166886215 0.02335532546531186 -0.2426699855615071; 0.12405604633545367 0.035928770952228836 -0.2767046195188789; 0.08781751628017803 0.03350196118806544 -0.24185756722169321; 0.043671212446324555 0.019607336081076173 -0.14431188865030756; 0.018419589428216417 0.009283588551667585 -0.07049072299832873; 0.011176434073381715 0.005601948346274589 -0.05139091290911898; 0.009144307979370379 0.004373466686660437 -0.039332714916238805; 0.014302434320346915 0.008088219543614954 -0.06940764989429253; 0.00028041749447851416 -0.00026483098164623085 -0.00292389202256556; 0.0004888523816253796 0.0002464619482941237 -0.002577246838615894; 0.00023880290266488097 0.001066887454445263 -0.0015960872971138916; -0.0017378449712693589 0.003372306478086378 -0.0047517914621510145; 0.005226677302710693 0.006390847483806259 -0.0019834890807756264; -0.0007847103795889006 0.0003963206900454111 0.002294820552952807; 0.0004270209604279316 -0.001804688898713571 -0.0009742568653797205; 4.060379057082555e-6 -0.00027923040405909575 -0.0011962773575029846; 0.0007919289713107327 0.000366015928719684 0.0047308093848992885; -0.006244310460344236 0.0006322616401756786 0.007141192675991382] %
+
+Mass Used: 102.60346702201832 kg
+Launch C3: 98.93783048100323 km²/s²
+||V∞_in||: 2.9227669595959147e-6 km/s
diff --git a/archive/ES_0.5826361699973581 b/archive/ES_0.5826361699973581
new file mode 100644
index 0000000..5f5cf12
--- /dev/null
+++ b/archive/ES_0.5826361699973581
@@ -0,0 +1,22 @@
+archive/ES_0.5826361699973581---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T00:02:12.672
+Launch V∞: [6.44609305640883, -6.903383053903391, 0.7607070831878705] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012747443163675926, -0.005762894169105177, 0.015205678378701801] km/s
+ V∞_out: [-0.013127743904503124, -0.00582465536238911, -0.014839191615511152] km/s
+ time of flight: 1.8749577787479886e8 seconds
+ arrival date: 2029-03-29T02:11:49.672
+ thrust profile: [1.0 -0.23759439685349074 -0.14516219382367962; 0.25279096150086255 0.10220981956427366 -0.15037666699668378; 0.09346322669187135 0.07244220481898014 -0.10450064733189499; 0.08071676981048524 0.08801802902368132 -0.13032966291162107; 0.05619258248760819 0.07688403512267325 -0.11932197540427913; 0.046234431503934206 0.07865785765333844 -0.1156080031556485; 0.009120020752835162 0.01735314454913359 -0.030113622664211238; 0.010346874151251457 0.01981566369234821 -0.03692838921136083; 0.0023593155152211664 0.007152083057680791 -0.012396224002779633; 0.0010185379236728066 0.0027457200737959478 -0.005631183405987826; 0.00012197336009117204 0.0006666549381236434 -0.0011024126169497301; 5.1488192269217073e-5 -1.163540400123689e-5 0.00022659838473745332; -0.00032621427488147237 0.00014834532982351613 -0.00046738966825997656; 0.0002553521643373153 1.7332157903336798e-5 -0.0003337297720705001; 0.00029974771370480495 0.00032500183563790685 -0.0005460282069383875; -0.0002333727163445265 3.503219949458814e-5 -0.0004203284560941256; 0.00017286535217015496 -9.235699822854775e-5 1.351593728623663e-5; 0.0002704182638864422 0.00032423770251867453 0.00018561573742097195; -0.00018953230939764136 -0.00010268854284177159 -1.9501281501539742e-5; -0.00016337323160921138 -0.00016433768523096005 0.0007253796938918001] %
+
+Mass Used: 155.98184847149787 kg
+Launch C3: 89.78748854721485 km²/s²
+||V∞_in||: 0.0206620645476674 km/s
diff --git a/archive/ES_0.582673933161944 b/archive/ES_0.582673933161944
new file mode 100644
index 0000000..33ce00b
--- /dev/null
+++ b/archive/ES_0.582673933161944
@@ -0,0 +1,22 @@
+archive/ES_0.582673933161944---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-23T07:46:00.025
+Launch V∞: [7.521776502096289, -6.694752764578151, -0.3437999744703748] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.473405863030035e-6, -0.00036811126126213406, -6.352145644263261e-6] km/s
+ V∞_out: [-0.0003560909361638837, 5.197276732271308e-5, -7.910038075024872e-5] km/s
+ time of flight: 1.87495777809551e8 seconds
+ arrival date: 2030-05-02T09:55:37.025
+ thrust profile: [0.3007522384645069 0.01538459091673179 -0.11131327349380553; 0.10462906943309809 0.05936558513943002 -0.12192367684619146; 0.04883762727291934 0.04194968734000627 -0.10071734456768278; 0.0625276463759093 0.08036307981441099 -0.19579718604034607; 0.025160981451941435 0.032005353163988066 -0.09993203581442411; 0.019703142299311974 0.028777060045858723 -0.09820301977209817; 0.004260927447670723 0.005826439344016362 -0.025059989250901207; 0.0034365142414651178 -0.0006297203077354665 -0.004964275505617658; 0.0022540085785221916 0.0035724439346107423 -0.004044480929815054; -0.005524746142926255 0.002809523645799304 -0.0038359643301211508; -0.000541347593971556 -0.00010606903075146624 -0.0025465081760385924; 0.002706331495536553 0.008217032647852635 -0.0027368588476257864; 0.0008973650128930848 0.0004370531612664909 -0.00611219902562141; 0.003181603673715017 0.004103545933158068 -0.005537514875076723; 0.00018584808398951962 -0.008575096194707562 -0.005651574056551431; 0.001925012936609219 0.0028970395102776267 -0.010625765732168602; 0.0002708462384359184 0.0006423975171832652 -0.007075401356268291; -0.011781773885935298 0.004500983379803739 -0.007827735621928983; 0.005066062809248608 0.009226874288704986 -0.008876237302336668; 0.0002970940320755893 -0.0003046324543979977 0.0008236788280938921] %
+
+Mass Used: 87.61521932116511 kg
+Launch C3: 101.51503474876051 km²/s²
+||V∞_in||: 0.0003682067470783588 km/s
diff --git a/archive/ES_0.5827294198470607 b/archive/ES_0.5827294198470607
new file mode 100644
index 0000000..7838ab3
--- /dev/null
+++ b/archive/ES_0.5827294198470607
@@ -0,0 +1,22 @@
+archive/ES_0.5827294198470607---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T07:57:43.624
+Launch V∞: [6.372243520102794, -7.034995379681757, 0.24689394696186656] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004814747945214396, -0.0001535682596706278, 0.003099748129309419] km/s
+ V∞_out: [-0.005486625410729067, 5.572631588286072e-5, 0.001624642518293906] km/s
+ time of flight: 1.8749577787437618e8 seconds
+ arrival date: 2029-03-29T10:07:20.624
+ thrust profile: [0.7674885913359343 -0.1654971190053245 -0.144092339918097; 0.29475020416663644 0.12181529099482502 -0.17858203222138913; 0.2562212785369642 0.19918478776103252 -0.2574692406290696; 0.0946948718992501 0.10151494560892076 -0.14369263108121663; 0.04579853797371261 0.061913495787934536 -0.09345888603616412; 0.012181307206898088 0.02000759116692865 -0.03237343733538562; 0.01633451266875725 0.03044784250206124 -0.050904260566837084; 0.005301995896420935 0.011943141363120326 -0.02069603059415908; 0.003940940072109913 0.009551104373502874 -0.01695590375136508; -0.0007278734887533502 -7.873920753794037e-5 -0.0013379504113546071; -0.00015281067723264786 -0.0008036976609606539 -0.0018648162776346894; -0.0013653357671922393 0.0010272170558398464 -3.927707505221455e-5; 2.7259170402789363e-5 8.762223700169646e-5 -0.0009037435096328024; -0.0006565141839184848 -2.5739994382034984e-5 0.0014275642920603948; 0.0011600435334846906 0.0007020230005025793 -0.0013641530806107664; -0.0009160856895770109 -0.0003746707513460439 0.0004729724413295698; 0.0011359144939930474 0.0017893419226989685 -0.0001011996374240048; 0.0006233018808955411 -0.0007669041284247774 0.00034370770942632883; 6.743706162963634e-6 0.0007622018085840137 -0.0013477862867242972; 0.0009924567527166527 0.0005203336136474026 -0.0010878987298749106] %
+
+Mass Used: 153.93163261425843 kg
+Launch C3: 90.15760409268213 km²/s²
+||V∞_in||: 0.005728334788704458 km/s
diff --git a/archive/ES_0.5827777649682344 b/archive/ES_0.5827777649682344
new file mode 100644
index 0000000..a02e1eb
--- /dev/null
+++ b/archive/ES_0.5827777649682344
@@ -0,0 +1,22 @@
+archive/ES_0.5827777649682344---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T20:11:35.140
+Launch V∞: [5.493027691163228, -7.663526769414862, 0.080074437670327] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.2764218871548555e-5, -5.596224478322014e-5, -7.537737703841791e-5] km/s
+ V∞_out: [-9.026324298437344e-5, -5.83780271075637e-5, -4.595863743843161e-6] km/s
+ time of flight: 1.5722368172717983e8 seconds
+ arrival date: 2028-04-11T13:26:16.140
+ thrust profile: [0.8371664436254548 -0.3801283397849811 -0.2530159040619064; 0.35968836967774703 0.0434301215229463 -0.2852016547481924; 0.2586309128369823 0.09927423425042907 -0.32374483220119393; 0.13859889681951623 0.07816229965859597 -0.23867786221037243; 0.05423696257470765 0.039119333837643905 -0.12123539240723252; 0.02800388003878429 0.023527463518193424 -0.07645072024219264; 0.019036147342620054 0.01798230657267027 -0.05880237631284338; 0.005630320601555598 0.006183494761227701 -0.021250839173965797; -0.00544427846989135 0.003344791635443983 -0.013621991370556497; 0.003457251355013174 0.0020780055631243726 -0.0039465231121199144; 0.0012520322122143894 -0.0017523658001817725 0.00027193434439169977; 0.0003674285347574618 0.002518710981593313 -0.0007758122614645443; 0.0070892703903798334 -0.007593100333222132 -0.009301579208204954; 0.01911537407674556 -0.0029027882875446876 -0.0027142604293878096; 0.0006005255308646591 -0.00015467003598832084 -0.0010997391778043285; -0.0017995727290407563 0.002275557546343584 0.013962288808764593; 0.010462792799849574 -0.012783486635472859 0.004619594756604221; -0.0009874835423134254 0.0012621277866657105 -0.0024921775447070663; -0.01749201764743323 0.019880600520946694 -0.03262411864995303; 0.001035728423929693 0.0003822261598015386 0.0006453179112355112] %
+
+Mass Used: 161.26918101381762 kg
+Launch C3: 88.90940767699243 km²/s²
+||V∞_in||: 0.00010769208236213813 km/s
diff --git a/archive/ES_0.5828031694915905 b/archive/ES_0.5828031694915905
new file mode 100644
index 0000000..91e8ee7
--- /dev/null
+++ b/archive/ES_0.5828031694915905
@@ -0,0 +1,22 @@
+archive/ES_0.5828031694915905---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T11:07:55.384
+Launch V∞: [7.022482349696949, -6.87019073500815, -0.5342220930169572] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6543440256670063e-6, -1.060050875705526e-6, -1.5378261639089536e-7] km/s
+ V∞_out: [-2.2480014396085175e-6, 1.3474917472081211e-6, 1.1494316153225211e-6] km/s
+ time of flight: 1.3912364052190945e8 seconds
+ arrival date: 2028-10-01T16:35:15.384
+ thrust profile: [0.4805089363862854 -0.16232061982450346 -0.20225735182517335; 0.16590094217380214 0.025567183226823102 -0.17792119185405847; 0.15543804704473327 0.05857116320749333 -0.266483053304408; 0.1151618797570548 0.05978968067442531 -0.2690171470233545; 0.06360665786639615 0.039981202889033236 -0.18830754874749814; 0.05625639912217824 0.040230250023960336 -0.19732649920103568; 0.017265745895688505 0.013639514923128194 -0.07077232859719883; 0.01499329386956663 0.013863711412814138 -0.07238890409626039; 0.00198020810217563 0.0016011565341081616 -0.012196767404449957; 0.0033284547004226 0.001620054536863892 -0.016362420470422315; 0.0024869830219724645 0.0025643257569334726 -0.014718821441930924; 0.0028498026224536206 0.0016847068572836616 -0.01777473318546431; 0.000848196843993709 0.002133561987447965 -0.01406280813782899; -0.003281985651334401 -0.002280856819614037 -0.0031594274343801788; 0.0010234301306187776 0.000202921362972936 -0.004009123029081142; 0.0003639877412841934 -9.518592618086818e-5 -0.001381291697605948; -0.005694427620872647 -0.005334491802282116 -0.006599990012126603; 0.006203823799787259 -0.00043945257904988953 -0.003938385894797892; 0.0009006061808236405 0.005234273319411262 0.0030963618345624397; -0.002095464471406538 -0.0019906549055951316 0.004276778664936209] %
+
+Mass Used: 115.26935913764646 kg
+Launch C3: 96.80017233186443 km²/s²
+||V∞_in||: 2.862324083464731e-6 km/s
diff --git a/archive/ES_0.5828971010481364 b/archive/ES_0.5828971010481364
new file mode 100644
index 0000000..c8311ee
--- /dev/null
+++ b/archive/ES_0.5828971010481364
@@ -0,0 +1,22 @@
+archive/ES_0.5828971010481364---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T06:16:33.527
+Launch V∞: [6.907170674045998, -6.768023460212713, -0.5065792535402813] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.292832628659113e-5, -9.824403539673375e-6, -0.0006883189353936862] km/s
+ V∞_out: [0.0006165404446709748, 0.00021560098489215187, -0.00022918354049848133] km/s
+ time of flight: 1.3863855863516057e8 seconds
+ arrival date: 2028-09-24T20:59:11.527
+ thrust profile: [0.7793455132754924 -0.2647975261941619 -0.32337687859514125; 0.27571257836900215 0.04215928330262197 -0.3050567888255181; 0.10795110912373261 0.039985666053816295 -0.19731867080081797; 0.09651828825778212 0.04959931043739705 -0.24068382563871388; 0.06058379630303291 0.03749831714315086 -0.18819555066194665; 0.04857236478166154 0.03446062581169357 -0.17793732142959645; 0.026755217628462776 0.02072069692867322 -0.11343358191099216; 0.009849091859567373 0.007476954196107294 -0.04535662667335211; 0.0037892951032478107 0.0032639957927795603 -0.0231480896994858; -0.0017242621456122834 -0.0004722097214060853 -0.0039172082879047575; 0.0007243540736957826 0.00038400737394548115 -0.004569080561005979; 0.0008876631815217134 -2.6278184102252345e-5 -4.360591323384656e-5; -0.00039901940739176553 0.001154930641129144 -0.004085024613435998; 0.0017682017786183747 0.0037483166706137674 -0.0003168984384070393; -0.0018316430458668025 0.0004586495469231047 -0.0015187665139060396; 0.00047316648489284855 -0.00015475546510858328 -0.004071636874130277; -0.0028577707606514584 -0.0022283788209768824 -0.0006190048155919157; 0.003652284180480451 0.0014282981631989443 0.002815764355991194; 0.0004424942955161548 -9.888785215050335e-5 -9.595515696257228e-5; -0.0011298882689252962 -0.001236285320822333 0.008013325335300145] %
+
+Mass Used: 133.0446214481949 kg
+Launch C3: 93.77177081850814 km²/s²
+||V∞_in||: 0.0006885104337241234 km/s
diff --git a/archive/ES_0.5829750891655172 b/archive/ES_0.5829750891655172
new file mode 100644
index 0000000..573b8ce
--- /dev/null
+++ b/archive/ES_0.5829750891655172
@@ -0,0 +1,22 @@
+archive/ES_0.5829750891655172---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T08:44:06.441
+Launch V∞: [7.427095371329878, -5.607048531189424, 0.300078479565589] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0002181232439837608, 0.0007397797279471477, 0.001983966545026978] km/s
+ V∞_out: [1.8913128487491042e-8, 2.0571493729974465e-9, -8.25994996956812e-9] km/s
+ time of flight: 1.874957778744494e8 seconds
+ arrival date: 2030-04-12T10:53:43.441
+ thrust profile: [0.9030992301874212 0.026482060219518575 -0.1212263678564198; 0.3930247746749991 0.2901182486924016 -0.1955336160289107; 0.2148144566417178 0.2781899518292696 -0.2044753802788653; 0.04987997270589445 0.09466488371854588 -0.08217093849391081; 0.029623870263061916 0.07641189093186872 -0.07176891905145448; 0.007257070899256164 0.025968013434724647 -0.028064788205632026; 0.005252039593382827 0.02429831471546647 -0.02737677994261665; 0.00974519260897869 0.06359848129864439 -0.06906012119609019; 0.00037491640520167873 0.005982462360446911 -0.0071922142163560725; 0.004286856763226427 0.008550811120031514 -0.007998807750567837; 0.0024959101588758483 0.004146058272717204 -0.005383340999175965; 0.00041616946763510976 2.2012292175607566e-5 -9.888279388167416e-5; 0.000697784416419977 0.0015826990832226767 -0.00213977086884548; -0.0019652460609265923 0.0002592194475583582 -0.004942332059717149; 0.0008283721790057739 0.0032284410208481985 -0.002430259293035892; -0.00659083051429326 0.0031095698694028743 -0.0047212135888409145; -0.006003838832592522 0.0020680123498284823 -0.0049436504395949646; -9.624692774763989e-5 -0.00046190131467836563 -0.00263599052617016; 0.0030172122963962027 0.0049823285681822906 -0.0013778062793152392; 0.010259488883851474 -0.0036266640395740788 8.346907350438126e-5] %
+
+Mass Used: 174.44135247736085 kg
+Launch C3: 86.69078597984156 km²/s²
+||V∞_in||: 0.0021286087116315763 km/s
diff --git a/archive/ES_0.5830580354235602 b/archive/ES_0.5830580354235602
new file mode 100644
index 0000000..85fcaf0
--- /dev/null
+++ b/archive/ES_0.5830580354235602
@@ -0,0 +1,22 @@
+archive/ES_0.5830580354235602---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T20:36:03.561
+Launch V∞: [7.187423898382696, -6.864206347963519, -0.23962533995043186] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1438837036398964e-5, 5.994018483330631e-5, 3.051796547235309e-5] km/s
+ V∞_out: [4.642901211173509e-5, -4.725216525578457e-5, -2.4375312370147435e-5] km/s
+ time of flight: 1.5006658416509515e8 seconds
+ arrival date: 2029-02-09T17:45:47.561
+ thrust profile: [0.2551160615338024 -0.07470006561358888 -0.11148554520987951; 0.0879597002019951 0.01485944122111184 -0.1085133845366636; 0.05610847898790585 0.017660309003225523 -0.11429521993266273; 0.04892925105825746 0.019900923820676902 -0.13368675745136116; 0.0794262740542431 0.04605665284937538 -0.25908157936119347; 0.035934041307139425 0.017194206216883022 -0.13619720102913485; 0.03824172659731987 0.01662026392785013 -0.16799633768750927; 0.03439800006062457 0.021855087629736175 -0.17108751596050142; 0.008181163400883294 0.004957186678050228 -0.04597216659301858; -0.008195343686552649 -0.004535515728395332 -0.010925348178244962; 0.009883360426873444 -0.0023536904703773632 -0.002674173765417511; 0.0015151651195216811 -5.73877876775754e-5 -0.009442243066996316; -0.003943798258740154 0.01417251032667505 -0.016149804114055734; -0.0028184044795458 0.0001248529600150696 0.008197080653095604; -0.007543159737547692 0.00340216424215606 -0.021832856578934592; -0.0026877267666263398 -0.0034340500070743855 -0.0009503999360032723; -0.015457274735372527 0.01814932509008889 0.004802614957276708; 0.004895539814375856 -0.017745211016401422 0.0260413580486934; 0.015660946696153637 0.018237746350408375 0.014084387786392065; -0.000299693334885572 -0.0008482576796281715 -0.04489721392615078] %
+
+Mass Used: 103.70380824241829 kg
+Launch C3: 98.83381138601175 km²/s²
+||V∞_in||: 7.059600348387954e-5 km/s
diff --git a/archive/ES_0.5831059177008584 b/archive/ES_0.5831059177008584
new file mode 100644
index 0000000..3fab71a
--- /dev/null
+++ b/archive/ES_0.5831059177008584
@@ -0,0 +1,22 @@
+archive/ES_0.5831059177008584---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T08:41:37.315
+Launch V∞: [5.40897961049589, -8.24541747098837, -0.3931343398265838] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.2288344528208033e-5, 9.531633631238882e-6, -1.8730156761283894e-5] km/s
+ V∞_out: [-9.106000722317028e-6, 2.124206943948228e-5, 2.012194867928525e-5] km/s
+ time of flight: 1.4346765903847453e8 seconds
+ arrival date: 2027-11-08T20:49:16.315
+ thrust profile: [0.30359421852208296 -0.16679721444999926 -0.13208791501848582; 0.20440429038229824 -0.0006151782490458215 -0.2003109302645462; 0.11975766695809777 0.02599501168309693 -0.1875928096449574; 0.10018940373778519 0.036304897875297226 -0.20647861674634405; 0.06961433056415312 0.031811818061409855 -0.17615573000161708; 0.04982657724327608 0.024819610423459128 -0.14811254702022106; 0.03322413014901805 0.018462544882925397 -0.11340062156242504; 0.023951418770188894 0.015886219834378008 -0.09449853244669043; 0.04181317903773206 0.028875750528957234 -0.15686996224806735; 0.012376128840034247 0.00843273157753383 -0.05521489013682191; 0.0025613108036797016 0.002772883425143652 -0.013259670353365574; -0.00027388147633928455 -0.0003625913384124365 -0.0033933380262264135; 0.0036981543118920048 0.000336364790828953 -0.002530062359524267; -0.003106470607453609 0.001661749128937337 0.0012830498222616846; 0.002828758158530158 -0.003384498454315245 -0.002278596947366679; 0.004462039737927796 0.004160820719709754 -2.7860735473321562e-5; 0.001263512242835867 -0.0029057393340049345 -0.006272157593761728; -0.0009785847148057357 -0.0006077656774652107 0.0014248281465558555; 0.007543293089713309 -0.006012650280886265 -0.0007042350078715252; -0.002351887776872565 -0.0006814123382817981 -0.0027371499153177937] %
+
+Mass Used: 112.132178861385 kg
+Launch C3: 97.3985243067914 km²/s²
+||V∞_in||: 3.063398625367802e-5 km/s
diff --git a/archive/ES_0.583115214793768 b/archive/ES_0.583115214793768
new file mode 100644
index 0000000..8169107
--- /dev/null
+++ b/archive/ES_0.583115214793768
@@ -0,0 +1,22 @@
+archive/ES_0.583115214793768---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T16:57:31.756
+Launch V∞: [5.522913243698057, -8.236931922860036, -0.6011198050263378] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6210988306283663e-5, -3.635609988459656e-6, 4.268457261429923e-6] km/s
+ V∞_out: [-1.5732823706744355e-5, 6.2532984489453e-6, -2.740582662785108e-6] km/s
+ time of flight: 1.4635278146839926e8 seconds
+ arrival date: 2027-12-13T14:30:32.756
+ thrust profile: [0.24254782030788366 -0.13852147778185805 -0.11681483428003425; 0.10925496888919628 -0.0055697610676264326 -0.12669226086199667; 0.10108340574130174 0.015576818964981838 -0.18080565325650305; 0.08698772305165627 0.023744219220223836 -0.2065426863330079; 0.06739585528860634 0.022878511036810847 -0.1917717899830456; 0.039816977832141776 0.018114214927553 -0.13250451294053214; 0.0450676187406398 0.021553594119140308 -0.17220365090364387; 0.03540318091086565 0.017950117730254584 -0.15092515367716178; 0.0075947074901183366 0.00629806561756973 -0.055684700672542733; 0.0033949461817921545 0.0029778613094060993 -0.015921767341424205; 0.005050981381176357 0.005780007302896995 -0.02752251973447471; -0.0004094592050887109 -0.005066479230232972 -0.0012643218697334186; -0.0012037970558407215 -0.0015880941842316895 -0.010540905348056222; 0.0014745800486304086 -0.0028219923804424897 0.009335063680673519; 0.00013947785375246818 0.004337345271310536 -0.005685074766655842; 0.003489604955052148 0.002488805787106203 0.005711979689286682; 0.004141417293151977 0.0025937899631904193 -0.0020615498324913794; 0.005233857830492428 0.009397501147518661 -0.019294787396940977; 0.004718633532121285 0.007103798127863159 -0.008467402609846774; 0.018648650003570917 -0.021276157433961 0.006618107253066097] %
+
+Mass Used: 104.48713181382345 kg
+Launch C3: 98.71096321924102 km²/s²
+||V∞_in||: 1.7153236698865525e-5 km/s
diff --git a/archive/ES_0.5831191059645637 b/archive/ES_0.5831191059645637
new file mode 100644
index 0000000..02009cd
--- /dev/null
+++ b/archive/ES_0.5831191059645637
@@ -0,0 +1,22 @@
+archive/ES_0.5831191059645637---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T13:51:16.401
+Launch V∞: [5.39637458928933, -8.308774981588117, -0.7131628674633393] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.38558800667145e-5, 3.3425154221598165e-5, -6.210159152623458e-5] km/s
+ V∞_out: [-2.9227310962990224e-5, 7.186315903359597e-5, 6.576998719059411e-5] km/s
+ time of flight: 1.4207804952466035e8 seconds
+ arrival date: 2027-10-24T23:58:45.401
+ thrust profile: [0.3171688681059821 -0.188070155243037 -0.15560240753450766; 0.12161816989070266 -0.008501695855610995 -0.14417140610055218; 0.10274205572991095 0.01338199636263054 -0.18742908704789615; 0.07031682900378439 0.018410782232623973 -0.17301132506425826; 0.056873669469841674 0.020457140703920376 -0.1723015101305516; 0.0501450248432151 0.021079753526565725 -0.1736126391134016; 0.0355943975193598 0.017162760536294886 -0.1378825560065587; 0.04298024807909911 0.020334772261015373 -0.17931114321124653; 0.016618933250384337 0.008513987233588202 -0.07901347855928226; 0.009787627210287028 0.005202651723054495 -0.05018408795344643; -0.0006382802203696371 -8.216731376014104e-5 -0.002705998001031747; 0.00010111586827155311 6.651022479303584e-5 -0.007436732357663035; 0.0007561260454304522 0.0002875321399259422 0.0011681717248465322; -0.0016128411082778759 -0.0019133209949918724 0.0005548148767378375; 0.0007138662022820573 -0.0032119813425188506 0.0033272351299409816; 0.0020454445502147735 0.0005820880818012649 0.0041677065608007715; 0.002731158593545682 -0.0020590886024226913 -0.003337448785116403; -0.00020868265593640672 0.002962719315825076 0.00047809851977860356; 0.0006916302418864084 -0.0004748229157379392 0.00027379639400356283; 0.0016114441124495792 0.0008167398836062267 -0.0018228500607162445] %
+
+Mass Used: 104.75861383628671 kg
+Launch C3: 98.66520167812074 km²/s²
+||V∞_in||: 0.0001021202214316921 km/s
diff --git a/archive/ES_0.5831672379591943 b/archive/ES_0.5831672379591943
new file mode 100644
index 0000000..77603cd
--- /dev/null
+++ b/archive/ES_0.5831672379591943
@@ -0,0 +1,22 @@
+archive/ES_0.5831672379591943---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-26T02:51:02.573
+Launch V∞: [7.983583713389477, -6.571875977265756, -0.6482537208478615] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.528114212127661e-7, 6.393470808699354e-6, -1.1387791165582121e-6] km/s
+ V∞_out: [9.73359255044505e-7, -3.602520784388297e-6, -5.36628595370163e-6] km/s
+ time of flight: 1.8749577775491586e8 seconds
+ arrival date: 2030-05-05T05:00:39.573
+ thrust profile: [0.016233966052525604 -0.002845195674406395 -0.008932382886805016; 0.023054020917199207 0.0010106314191262323 -0.04191975812384159; 0.02342954652323074 -0.0006864406271595137 -0.0724832585817648; 0.0377293371894011 -0.004875773903713204 -0.15410967597664424; 0.027399239987087105 -0.006890648487175649 -0.13495945932285577; 0.01495607929513152 -0.005362400524019512 -0.08299404921037819; 0.011370202331758063 -0.005045799563375563 -0.06847564644603445; 0.0072186806422741825 -0.003701841730113585 -0.04625644463152073; 0.004138943411403234 -0.0023896637949806163 -0.027872527914515756; 0.005980843184884249 -0.003634982180909452 -0.040675455373408075; 0.00023078594678530766 -0.00023434139133175883 -0.0015253641488956226; 0.00026676864223530293 -0.00017158661233241266 -0.002508754333776952; 0.0002496244387981631 -0.00016347231151848322 -0.0010775333922429194; 0.0006297388995492377 -0.00035574353727071945 -0.0029529961517031087; 0.0004670859084619436 8.867037615475145e-5 -0.0002620251192563614; -0.0005096996328006471 -0.0001673242735570415 -0.0013323908135985463; 0.0004073386413439116 0.00020950518892332817 0.00010878434096811117; -0.0005011198068176023 0.0007087159831340494 -2.9977621558556863e-5; 0.0003647819090770823 -0.0002911364349618721 -0.0027937592784654294; 0.0006233746684917133 -0.0004991025444487577 -0.0008108392256616688] %
+
+Mass Used: 54.1686362932478 kg
+Launch C3: 107.34739565585353 km²/s²
+||V∞_in||: 6.537584561128694e-6 km/s
diff --git a/archive/ES_0.5832166729908046 b/archive/ES_0.5832166729908046
new file mode 100644
index 0000000..ed2664f
--- /dev/null
+++ b/archive/ES_0.5832166729908046
@@ -0,0 +1,22 @@
+archive/ES_0.5832166729908046---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T03:43:54.788
+Launch V∞: [7.225011071489064, -6.636798330412581, -0.35840054945533284] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007942558445643164, 0.004038726697128936, 0.00029573196821277924] km/s
+ V∞_out: [-0.0067664135918062696, -0.003739789333042449, 0.0044411156737004685] km/s
+ time of flight: 1.5598742506852186e8 seconds
+ arrival date: 2029-04-18T13:34:19.788
+ thrust profile: [0.40811455805410335 -0.09540594166539017 -0.16676705439479592; 0.08290368704855218 0.020727986862336716 -0.0966690071436583; 0.08671390007018466 0.04175687344203704 -0.16970817825005136; 0.06062810470804469 0.03782217312598315 -0.16483035577819424; 0.07597242934287758 0.05998328211950031 -0.26250634416041385; 0.03808141972351324 0.03250202542939349 -0.1604382007386355; 0.01735766223013037 0.015859151670835625 -0.08507744816373208; 0.01716605610957092 0.012044510712542112 -0.07776685884613779; 0.0035779926193222457 0.0016211216226750323 -0.022815296319285416; -0.0013209033157481804 -0.005507262786734518 -0.013827302535680947; -0.007843595227131867 0.003522489766901482 -0.002723049469869717; 0.004148092846055067 -0.0016683873722374348 0.004072407769120633; 0.008698778756219529 0.01096681506052398 -0.007796103166468208; -0.04034108530640882 0.004911102215515208 0.004615114765005151; -0.01792863394731855 0.02523656163449854 0.00961286061126557; 0.004030180078783113 -0.03610283720144402 0.012883864028826202; -0.015955696492020256 0.029317898979764067 -0.012574054718708077; -0.007496591543624503 -0.03297469170879089 0.00969987400066696; -0.05491906038089193 -0.012024785812059527 0.008878453889989174; 0.020003303927831718 -0.011380345827245602 -0.0013691861247598824] %
+
+Mass Used: 118.22420506519165 kg
+Launch C3: 96.37632801555664 km²/s²
+||V∞_in||: 0.008915324188922272 km/s
diff --git a/archive/ES_0.5832209851075401 b/archive/ES_0.5832209851075401
new file mode 100644
index 0000000..1edec99
--- /dev/null
+++ b/archive/ES_0.5832209851075401
@@ -0,0 +1,22 @@
+archive/ES_0.5832209851075401---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T07:15:33.344
+Launch V∞: [5.413478018614436, -8.29850214757497, -0.8002898668919771] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.9674592874608965e-5, 0.01612211034940354, -0.007436930725470698] km/s
+ V∞_out: [-0.013945148908887003, -0.008507129137858777, 0.006838363280930961] km/s
+ time of flight: 1.418009391990476e8 seconds
+ arrival date: 2027-10-21T12:24:32.344
+ thrust profile: [0.3238271906648884 -0.18965820287173654 -0.15448763750006975; 0.11791365609551241 -0.0067151207282916394 -0.13181611597785267; 0.05558965177447099 0.007861280938693755 -0.09614129851380705; 0.09888378129135972 0.02701534490069119 -0.22197248873914555; 0.05700938069667499 0.020496419324370657 -0.1601585046653303; 0.05564122042412771 0.023067297163204922 -0.17962171909815047; 0.030054239108521726 0.014000418364843 -0.11085007055197098; 0.05198927815925783 0.029469553066672698 -0.2101930217581998; 0.021423319399493854 0.010659049736692475 -0.09446822318633542; 0.01727701368176685 0.009684522937561038 -0.08134947339264728; 0.002429403265681701 0.0006010892140001097 -0.005943583343335697; 0.00012535725608394505 0.0011500420964088134 -0.0033834253498710156; -0.000732022595850665 0.0008669465584195872 -0.0018317224857890466; 0.0007923916217676555 -0.0006473380450328297 -0.0029602094543294813; 0.0013842701320402773 0.0008497937304683134 -0.0023778034172026946; -9.736662481047239e-5 -3.30366535289115e-5 9.978046534139112e-5; 0.0015651652739184568 -0.0017098877775192924 -0.0008347744061285295; -0.0018426474407740165 -0.00032967640043290655 -0.00030843357202733294; 0.001690199023179351 -0.0017018400684841355 0.0030201260257238095; 0.0009760894031522174 0.0001821496294117941 0.0003008281836304151] %
+
+Mass Used: 104.02496416159147 kg
+Launch C3: 98.81134602237805 km²/s²
+||V∞_in||: 0.017754772733186833 km/s
diff --git a/archive/ES_0.5832559144878273 b/archive/ES_0.5832559144878273
new file mode 100644
index 0000000..ec2e800
--- /dev/null
+++ b/archive/ES_0.5832559144878273
@@ -0,0 +1,22 @@
+archive/ES_0.5832559144878273---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T00:30:59.334
+Launch V∞: [7.061454366682718, -7.021409962415605, -1.0016187758704873] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012182693574070442, -0.0018643796930549823, -0.00015633355544552473] km/s
+ V∞_out: [0.00011944676090110012, -0.0006259796708783727, -0.00213935326883447] km/s
+ time of flight: 1.3901938170233694e8 seconds
+ arrival date: 2028-10-03T01:00:40.334
+ thrust profile: [0.30321383387971923 -0.11325064275022008 -0.1476111381477561; 0.08239316325607866 0.006691108852080992 -0.10106221538774379; 0.10245654775777437 0.027603437805590814 -0.20275493284402082; 0.11242798012527427 0.04223740180344729 -0.3040245573579564; 0.05495270879349681 0.02388461680330817 -0.18554068825016437; 0.03798690208270001 0.017996867333401903 -0.15217111307119952; 0.02672008672995809 0.013746664661065803 -0.12253976743280685; 0.013728722136508914 0.006787402309511104 -0.07137971907395212; 0.003705063731868864 0.0022127186231565557 -0.025778615933674132; 0.004709603987041745 0.0026717777604588393 -0.030846339550864136; 0.0008039147770512855 0.0004852994180251026 -0.005311138698342659; 0.0021863441094023056 0.002879337243519373 -0.025060207318566036; 0.005375740294373193 -0.007822437130176055 -0.0018318705031555352; 0.0028926368980103957 0.0033098576012612494 -0.0035613079432064085; 0.0002648174714165605 -0.0003001110028281011 -0.0029114784877159435; 0.0014794164276860713 -1.600929210497778e-5 -0.0003166136385592908; 0.00040566059113200745 -0.0023069437876330305 -0.009964117145257186; -0.004529039727919417 0.011210374138604956 -0.004559796822997753; 0.003365115604822975 -0.000589785714033994 -0.0022765702436815076; -0.002222009466224641 -0.0011768251839163598 0.007327420079728997] %
+
+Mass Used: 96.15437470530287 kg
+Launch C3: 100.16757580522783 km²/s²
+||V∞_in||: 0.0022326065590764087 km/s
diff --git a/archive/ES_0.5832930932260469 b/archive/ES_0.5832930932260469
new file mode 100644
index 0000000..fe6bcb8
--- /dev/null
+++ b/archive/ES_0.5832930932260469
@@ -0,0 +1,22 @@
+archive/ES_0.5832930932260469---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T22:49:48.479
+Launch V∞: [7.17415946556144, -6.079077224967064, 0.35129300595308277] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.070439372190904e-5, 3.665569879353335e-5, 0.0024124115445847494] km/s
+ V∞_out: [-0.0021566166322200668, -0.00072951053557448, 0.0007903903856787062] km/s
+ time of flight: 1.6400638516419512e8 seconds
+ arrival date: 2029-07-12T04:09:33.479
+ thrust profile: [0.8855195776172327 -0.1343424588844533 -0.19948701422226744; 0.49603405316955035 0.2188821773745121 -0.3370824015501917; 0.17170698280409843 0.1371294239089547 -0.2145283985449164; 0.09131460741262248 0.09845252580281103 -0.16509439651978158; 0.02207727638737124 0.027923802590742845 -0.05140735600526308; 0.01777103447270519 0.026222200193388525 -0.05043991784666739; 0.03644138791746561 0.06396112951782705 -0.12494116518251179; 0.0034782907212025046 0.00704774904639657 -0.01273426668832305; 0.00107131513966046 0.0039902850608255856 -0.009600307362669147; 0.0014308820486396351 0.0061392243545294 -0.0030291505686524615; -0.00023605680269885368 0.003258189138125593 -0.004010318930873298; 0.004320733066496149 0.002202126270302211 -0.002575424706978242; -0.0027541267093943566 0.012747402502270576 -0.003102241376971501; -0.0006870573780991388 0.006965836195951609 -0.004574874995769284; 0.002560873820158213 0.006892176631345988 -0.01186286689402671; 0.0008435124512423536 0.0006825067809182669 -0.0026719794037174914; 0.009760290440643948 -0.005706802706602435 -0.011085931065018753; 0.004702658584845202 -0.017243016497428883 -0.0196958084168236; -0.008325139250051369 -0.010732143891844795 -0.018161333225685507; 0.009287726664180682 0.018350690702663076 0.00507763538385945] %
+
+Mass Used: 163.983562894432 kg
+Launch C3: 88.54715072044962 km²/s²
+||V∞_in||: 0.002413222748989932 km/s
diff --git a/archive/ES_0.5833679252071045 b/archive/ES_0.5833679252071045
new file mode 100644
index 0000000..81420d9
--- /dev/null
+++ b/archive/ES_0.5833679252071045
@@ -0,0 +1,22 @@
+archive/ES_0.5833679252071045---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T12:50:23.438
+Launch V∞: [5.245505562432167, -7.961212016467484, -0.2698944340326502] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010325447873818335, 0.009802015911013462, -0.0001754730467932912] km/s
+ V∞_out: [-0.004933362128480479, 6.651679127781902e-5, 0.013356149741328677] km/s
+ time of flight: 1.41758816855038e8 seconds
+ arrival date: 2027-10-16T06:17:19.438
+ thrust profile: [0.8891940300734374 -0.5078192943488519 -0.340837523697907; 0.2541421848896437 0.00034078879414783714 -0.228143368763621; 0.1463843614783434 0.034462862489859546 -0.20200158067026283; 0.15243604904578167 0.05933926806622374 -0.2745670845329639; 0.09615673135028523 0.04751756870675241 -0.21271983697208396; 0.05656745372469595 0.0313365740055867 -0.1461436486868077; 0.042876703121840165 0.027614056291482766 -0.12627549047835365; 0.024764102571629483 0.017500470333071 -0.08230709751436507; 0.0067711681225873345 0.0046448711927421045 -0.023846543261390876; 0.0022451543671950995 0.0017793197442340578 -0.009517701866887577; 0.00048522711203529485 0.0004661082387417524 -0.0024485193278797903; 0.00017581925611133366 0.00013649099351652045 -0.0005060571850142145; -0.00026433113749037746 0.00010158105214906517 -0.00033006865708210724; 1.2566975495725146e-5 -0.00018140374382436114 -0.0001592391008977512; -0.0001841976448784157 -0.00018198983669457562 -0.00019334173794086822; 7.11983386213632e-5 0.0005110222355614066 -0.0002717812765577815; -2.117680035956755e-5 -0.0006414681296958035 0.00011292153178535527; -0.00016601641486006923 -0.00023510194455428907 0.00011681852964721528; -0.0001569534047394125 0.0005699748631579811 6.063153477748278e-5; -0.0007871227814128843 0.00027569515843485276 -4.247579063023838e-5] %
+
+Mass Used: 149.94301384560185 kg
+Launch C3: 90.96906838217487 km²/s²
+||V∞_in||: 0.014238159308873165 km/s
diff --git a/archive/ES_0.5835112048445641 b/archive/ES_0.5835112048445641
new file mode 100644
index 0000000..fafc3ab
--- /dev/null
+++ b/archive/ES_0.5835112048445641
@@ -0,0 +1,22 @@
+archive/ES_0.5835112048445641---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T21:45:42.850
+Launch V∞: [5.421888599163137, -8.22911780427435, -0.9008887914344487] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.904132542115946e-5, -6.346433270074422e-6, 7.814394004161982e-6] km/s
+ V∞_out: [-2.8610650551182913e-5, 1.1328890843310886e-5, -4.908456686567276e-6] km/s
+ time of flight: 1.4047120764679328e8 seconds
+ arrival date: 2027-10-04T17:32:29.850
+ thrust profile: [0.328952317793298 -0.20893123212256529 -0.15240220426998338; 0.20988755649950513 -0.0224489226171541 -0.22369398270710714; 0.1519527058156663 0.013900547236071351 -0.25559857659969193; 0.11223714482817408 0.023773032791713715 -0.25667588926881885; 0.08326300242347456 0.025124041778841998 -0.23578431766347752; 0.043068232980385916 0.016976542021279 -0.141667396602088; 0.02379035181376009 0.009799196819085981 -0.08864037436160947; 0.011950127592082877 0.0062535026334105005 -0.05273235469340242; 0.009526635099168243 0.005471383525993499 -0.04301738174503762; 0.0049545945774349 0.003235129274310057 -0.024043059864987178; 0.0009897620014317587 0.0020318202631152455 -0.0019508926546552559; 0.0004071550504283646 0.0006350790447696128 -0.0016316357457708815; -0.0002655152094510086 0.0003309917890502073 0.002080636223181331; 0.0008434478483661184 -0.003602250005591364 0.0013706935678198442; -0.00024162647206948972 0.004067007904742431 -0.00011933540553214837; 0.0007349720561843308 -0.0010449205291827004 -0.0014308647387532127; 0.0007157342015430537 0.0023682500853475404 0.0007972977572714584; 2.8117974116969625e-5 0.0010373127166919216 -0.003129601257196543; -0.0046454095027601595 -0.002667995650558942 0.00020917975762849692; -0.007793270407744834 -0.0042826928463759245 -0.00010294735357617847] %
+
+Mass Used: 109.52307646011832 kg
+Launch C3: 97.92685643289254 km²/s²
+||V∞_in||: 3.073663207186944e-5 km/s
diff --git a/archive/ES_0.5835778772549098 b/archive/ES_0.5835778772549098
new file mode 100644
index 0000000..36a097c
--- /dev/null
+++ b/archive/ES_0.5835778772549098
@@ -0,0 +1,22 @@
+archive/ES_0.5835778772549098---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T02:09:55.736
+Launch V∞: [5.256951659771486, -8.208582407887262, -0.2942202069192856] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.013698168199421325, 0.081049785914478, -0.09279734639732773] km/s
+ V∞_out: [0.08283829950957351, 0.07677326021113387, 0.05110769702899295] km/s
+ time of flight: 1.4096223332166478e8 seconds
+ arrival date: 2027-10-10T14:20:28.736
+ thrust profile: [0.5830537670597051 -0.34055783551534025 -0.25703029824895757; 0.15223402982969694 -0.008635235440471059 -0.1592688884826209; 0.11883557686420305 0.018099669630913612 -0.19059168633831614; 0.10065297548649697 0.02782637648578475 -0.21246968531616922; 0.0773089967152946 0.027826858977120245 -0.19848503050473063; 0.0451616828055423 0.019006546599185575 -0.1364671825662787; 0.08825208874712913 0.04282026756772713 -0.29187041439746; 0.019855814547761946 0.00994510030485527 -0.0755634859423359; 0.005231235806168217 0.0025294520885524776 -0.022589856272477424; 0.001440725082434323 0.0008093804242115252 -0.007175655756496186; 0.0030863438239339463 0.0009207506393073715 -0.014137789153397081; 0.001810166873787336 0.0008627619458907016 -0.009432163960763327; 0.0011247178261767727 0.0006468497597273875 -0.00608340600175394; -0.0007325625363115294 0.0002454369363931314 -0.0031543222517472283; -0.00030319187838689617 0.0004285449931151 -0.0003307260809439841; 0.003570212474245219 -0.0044420487936737574 -0.006775727549660515; 0.0004672388821193702 0.0015162371723405847 -0.004188521184546123; 0.0016702685663078911 -0.0028065236731550664 0.0024803716410246564; -0.0009727784760530875 -0.0034612660103738057 0.00769134473858054; -0.0007375171931468401 -0.00045738149971646166 0.0036120399028921413] %
+
+Mass Used: 126.07375678666949 kg
+Launch C3: 95.10293143041005 km²/s²
+||V∞_in||: 0.12396796000252641 km/s
diff --git a/archive/ES_0.5836023058773819 b/archive/ES_0.5836023058773819
new file mode 100644
index 0000000..59da725
--- /dev/null
+++ b/archive/ES_0.5836023058773819
@@ -0,0 +1,22 @@
+archive/ES_0.5836023058773819---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T20:58:59.973
+Launch V∞: [5.24408157619438, -8.36648130480884, -0.8703192339694675] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5183975047313196e-6, 6.491312607873647e-7, -1.2447927041937399e-6] km/s
+ V∞_out: [-6.051207435408254e-7, 1.4255230231633415e-6, 1.290490158686459e-6] km/s
+ time of flight: 1.3965322599606046e8 seconds
+ arrival date: 2027-09-27T05:32:44.973
+ thrust profile: [0.38420671618184377 -0.24387909945966468 -0.2032828399264675; 0.10061373559688162 -0.011120941558110336 -0.12052830751123536; 0.16362757498663383 0.0137930960952015 -0.29943772180356715; 0.14202401899428663 0.027277501472372383 -0.34463212063511367; 0.08636915591065017 0.02269745085791518 -0.2585483586849657; 0.03288742957867669 0.010176593052563453 -0.11532861795070952; 0.012937483149861208 0.0048804230979123345 -0.052868735440523694; 0.007686907020873927 0.004532948060712718 -0.03795688115115253; 0.0028540459971386923 0.001098169415140539 -0.014495787327466913; 0.0029882642877978333 0.0009037315762688608 -0.01597720296698041; 0.0020343135946102667 0.0006905794656843734 -0.010437435916898831; 0.0012130178981114772 -0.0004506356642877881 -0.0017765788891956481; -0.0011690644118621317 -0.0012397260342190356 0.0016169431090409907; -0.00038150409631951753 0.00020654896093627313 0.0019524628118901726; -0.0014055579654216532 -0.005243776717393511 0.0003523916379681467; -0.0003252382649520055 -0.00024332308462744195 -0.00036255566233959146; 0.0005440633430416136 -0.003037453469639295 0.006413532064637939; -0.0018556390840925834 -0.0006321402651668557 0.008260725847476212; -0.0004841280078030723 0.00018981462531617206 0.006677114610171954; 0.0005109908277338565 -0.0011436795945085443 -0.0012234636362016974] %
+
+Mass Used: 107.71019352894518 kg
+Launch C3: 98.25585657051435 km²/s²
+||V∞_in||: 2.0679485613814613e-6 km/s
diff --git a/archive/ES_0.5836206869278149 b/archive/ES_0.5836206869278149
new file mode 100644
index 0000000..344d3e7
--- /dev/null
+++ b/archive/ES_0.5836206869278149
@@ -0,0 +1,22 @@
+archive/ES_0.5836206869278149---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T11:19:45.218
+Launch V∞: [6.140108690067465, -7.818188890137462, -1.3073015023912071] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2539135578402913e-7, -1.0195488079685129e-7, 1.974653494937612e-7] km/s
+ V∞_out: [9.774581070271732e-8, -2.1786909275726222e-7, -1.9998494783117757e-7] km/s
+ time of flight: 1.5535311871957248e8 seconds
+ arrival date: 2028-03-23T12:58:23.218
+ thrust profile: [0.1538888043389632 -0.08112485678251849 -0.07011709678869205; 0.11483646906409001 0.004041413829374428 -0.12635873808826734; 0.12830338712392547 0.030759974651131627 -0.22665412261109066; 0.0774044524580308 0.03163464690663023 -0.18420387259571527; 0.08507108531172648 0.04088917012365145 -0.2508360501738828; 0.05482879776118257 0.03273925800424725 -0.19055652512438945; 0.027009199546512264 0.01961597848222198 -0.11032884907891023; 0.012589868877835954 0.010149108249030243 -0.059113239832344545; 0.00450394889556553 0.004050926431954526 -0.024689877114885173; 0.001250546747442878 0.0012871218180597684 -0.007868615873498217; 3.861698177483417e-5 0.00043147073974372655 -0.003919648695855239; -3.6931683905472865e-5 0.00028946575325340684 -0.00261128040341694; -0.001142885188302707 9.493842024565948e-5 -0.0005835462680430386; 0.0009513689090222288 0.00017951491764914805 0.0004113919462089891; -0.001410138893481388 0.0003772334817803505 0.0009513774426884089; 0.00017120975391651932 0.00022759585164369646 -0.0030037265205417702; 0.0007654497077483197 0.0007840896573547435 -0.0018813033969754813; -0.0031651273566446854 0.0010951028790589941 0.001522078338436552; -0.0006055010146499939 0.0017073068676188253 0.00036714324903358055; 0.0018519558820531746 -0.002806547730719111 -0.0004767795193973566] %
+
+Mass Used: 94.44217953157067 kg
+Launch C3: 100.53404946586515 km²/s²
+||V∞_in||: 3.165258681864031e-7 km/s
diff --git a/archive/ES_0.5836887802815129 b/archive/ES_0.5836887802815129
new file mode 100644
index 0000000..071805b
--- /dev/null
+++ b/archive/ES_0.5836887802815129
@@ -0,0 +1,22 @@
+archive/ES_0.5836887802815129---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T10:59:08.489
+Launch V∞: [5.493243418645344, -8.526692412312716, -0.4037314929240687] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.839868108191796e-8, 1.4621045885003993e-8, -3.335442546255656e-8] km/s
+ V∞_out: [-1.2833026394620982e-8, 2.940295964500071e-8, 3.746461220433429e-8] km/s
+ time of flight: 1.583241830827849e8 seconds
+ arrival date: 2028-05-08T21:55:31.489
+ thrust profile: [0.09628828919337534 -0.05999881228560261 -0.05912190072509313; 0.03538275115113839 -0.00936153668079697 -0.06105703686119175; 0.05589371254408512 -0.01238862306355105 -0.15554900985992787; 0.054221753998534926 -0.01403516517157097 -0.20634563520200846; 0.0480527227856829 -0.015449217330490322 -0.22706736264554422; 0.032817888763827324 -0.013030337547006892 -0.18276738626485647; 0.012516328949239933 -0.006205929219069255 -0.08236551556706007; 0.018060791213876253 -0.009202523157144428 -0.12140791902351719; 0.0028374744398323454 -0.001511268153696226 -0.025386290522862568; 0.0012602005830362642 -0.0008329601951447458 -0.012527117368617228; 0.002084395704217156 -0.0008722174495242608 -0.011955450588985546; -8.128133066596536e-5 -9.430183442400781e-5 -0.00017305428411801683; 9.275998586288786e-5 -0.00022477917816823682 -0.0010990923783583682; 0.0011964045785625612 0.0012769864488040464 -0.00015040141111417275; 0.0009358579886933273 -3.574423147563839e-5 -0.0009939932036032361; 0.0005810752101600767 0.0018840977517383985 3.0391889203103023e-5; 0.0019268882615346718 -5.9545476762271616e-5 0.0012736153958048378; -0.0008964749217075308 -0.0023824236607088074 -0.00042448030111051535; -5.375114896856339e-5 1.9556098578651102e-5 -0.00011421583773027664; -0.00011915955191573093 0.001192743993834525 -0.0003582667541234169] %
+
+Mass Used: 79.88487609224649 kg
+Launch C3: 103.04320586906033 km²/s²
+||V∞_in||: 5.292212570881368e-8 km/s
diff --git a/archive/ES_0.583813887336553 b/archive/ES_0.583813887336553
new file mode 100644
index 0000000..33a93e0
--- /dev/null
+++ b/archive/ES_0.583813887336553
@@ -0,0 +1,22 @@
+archive/ES_0.583813887336553---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-10T19:29:14.933
+Launch V∞: [6.240939542208852, -8.119700829112025, -0.4172663958760832] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0007202317760092951, -0.0008671224001293319, -0.0007365801413814644] km/s
+ V∞_out: [0.0008668703801398506, 0.0004418416216594311, -0.0009320891185111944] km/s
+ time of flight: 1.8377350339439833e8 seconds
+ arrival date: 2029-03-06T19:40:57.933
+ thrust profile: [0.04010916835237247 -0.02003982285808131 -0.024235794336383502; 0.010710876644732505 -0.0034090120961749503 -0.021680511589763283; 0.024164036688840394 -0.010469146676572106 -0.08199127112906676; 0.029534821155880592 -0.018755339106262647 -0.13260984044089216; 0.023507447633315536 -0.01910472908785715 -0.13078999393299587; 0.026530118000713462 -0.025473087178202868 -0.1651632432989897; 0.013022351162398086 -0.013658275604520053 -0.09091388979295233; 0.008855094310082695 -0.010063602313766077 -0.0667833891111591; 0.013026608360763674 -0.015098922394373045 -0.09605611148257373; 0.0008546738111948548 -0.0029944439835628426 -0.01403779283262764; 0.0006745673926982206 -0.0010879454811759258 -0.0067384149368115605; 0.0013951668200795153 -0.0021160607741852397 -0.015008412581983956; -8.351558997529864e-5 0.00020096314504409172 0.0012719467247458535; 0.0024185002758954992 0.0028577188319896716 0.0008627359645322651; 0.0022991679583647985 0.0025829081112655264 0.003186640702475643; 0.0005046944193023469 0.0026892862718545744 0.0008814804107958743; -0.0005435873688337336 -0.002522410362089286 -0.0003261188452060985; 0.00889249896930735 -0.0006945141039691692 0.002862321186084044; -0.00046674748224704286 0.0011101630186817859 -0.001192669844605124; 0.009195199554770899 0.0003548175207497734 0.0020864994931838847] %
+
+Mass Used: 68.30715674063549 kg
+Launch C3: 105.05297916891597 km²/s²
+||V∞_in||: 0.0013465457187400267 km/s
diff --git a/archive/ES_0.5838744572748303 b/archive/ES_0.5838744572748303
new file mode 100644
index 0000000..690d7f0
--- /dev/null
+++ b/archive/ES_0.5838744572748303
@@ -0,0 +1,22 @@
+archive/ES_0.5838744572748303---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T08:11:15.155
+Launch V∞: [5.6728877009779515, -8.34485134571389, -0.8428678656232316] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.846556087690508e-6, 0.008757084191035101, -0.0029179838518313453] km/s
+ V∞_out: [-0.007486759036999347, -0.004092366773335758, 0.003521670002916212] km/s
+ time of flight: 1.5019171024433386e8 seconds
+ arrival date: 2028-01-30T16:06:25.155
+ thrust profile: [0.03493914294397491 -0.0241649791939514 -0.020901127240890414; 0.04242444986931142 -0.008952064176163557 -0.06262463006631976; 0.0565766734968723 -0.007180128445983821 -0.14111658128661816; 0.052014772933356226 -0.006372581386922036 -0.17944365489045158; 0.04444241259396148 -0.006498489505910236 -0.1916443861370839; 0.035894383866374724 -0.006350380342112578 -0.1812967723175921; 0.02734608970905313 -0.005625260881460439 -0.1548456986482449; 0.02019564249359045 -0.004732065416424391 -0.12481555730339161; 0.011671760628656252 -0.003005265954187342 -0.0753363880776184; 0.0049390852913840716 -0.0018699308168766402 -0.030024305202656427; 0.002240256369627856 -0.0001274441269402131 -0.016296125463579787; -0.003036639340017806 0.0030885100920935685 -0.009080664590475573; -0.0015539035460527598 0.0024543176241988043 -0.020282705986412262; 0.009692681516686008 -0.007923491750403308 0.005793653538518826; -0.005736395257116187 0.0030123814706328684 -0.010102530930735393; 0.003787217961063529 -0.0032540502038494695 0.0026081989998519104; -0.005019016554605379 0.006119105239581826 -0.027297814901854164; -0.012312881425439704 0.005500477679446816 -0.0036198994066769484; 0.00465867687965833 -0.005052610111701096 -0.028589133391627324; -0.003458887962152434 -0.0012616063524272946 0.0021869956649622803] %
+
+Mass Used: 83.10322046889314 kg
+Launch C3: 102.5286250888701 km²/s²
+||V∞_in||: 0.00923045131886735 km/s
diff --git a/archive/ES_0.5839205841011454 b/archive/ES_0.5839205841011454
new file mode 100644
index 0000000..1355155
--- /dev/null
+++ b/archive/ES_0.5839205841011454
@@ -0,0 +1,22 @@
+archive/ES_0.5839205841011454---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T04:09:40.261
+Launch V∞: [5.338281659441219, -8.21803659629134, -0.40680925739030804] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.019266754938533234, 0.013634131661194407, 0.042987070608714525] km/s
+ V∞_out: [-0.023178113515550523, -0.03460936099775379, 0.025878551387582042] km/s
+ time of flight: 1.432408710936911e8 seconds
+ arrival date: 2027-11-06T01:17:31.261
+ thrust profile: [0.39007652962076594 -0.21548720840677485 -0.16692986789796893; 0.24461499217661276 -0.006013669614591751 -0.23996167423598447; 0.12497175110773397 0.022912049660546427 -0.19055381381239847; 0.10373423270417043 0.034417422616766745 -0.21111646091441721; 0.06786943326482375 0.02801151460725189 -0.16960501986447232; 0.08627084898843637 0.04150674316600442 -0.24258556632259887; 0.028672753433235387 0.014868599348192844 -0.09495686239469944; 0.029138437393470412 0.015581670172269661 -0.10762160468197697; 0.006784593839831548 0.003921184104515294 -0.02824835110877117; 0.007394916849490058 0.0049674201475221206 -0.03409685174327999; -0.0038703132051354236 -0.002330455622657334 -0.0024555511244442664; 0.0014109031612047481 0.0021870167088916953 -0.00495991268017895; -0.0006054905167257083 -0.006955485335849002 -0.006029548756661629; 0.00025019530549049253 0.00024411557443285723 0.000194943029106295; -0.0008071199356736061 -0.0013754855210233344 0.0040616598185955945; 0.0022784854581066475 -0.0011402563683170345 -0.01020823483949282; -0.007801434937218396 0.0035412338529055053 -0.008305005056912446; 0.01509716437286038 -0.003310377768160268 -7.471324540701363e-5; -0.00845822470883001 -0.005265531291826737 -0.013581593054656293; -0.017249756167254528 0.0017209283821661636 0.00173314333766594] %
+
+Mass Used: 120.08060443645218 kg
+Launch C3: 96.19887034540871 km²/s²
+||V∞_in||: 0.04904065284572471 km/s
diff --git a/archive/ES_0.5839409102779352 b/archive/ES_0.5839409102779352
new file mode 100644
index 0000000..e63e7c7
--- /dev/null
+++ b/archive/ES_0.5839409102779352
@@ -0,0 +1,22 @@
+archive/ES_0.5839409102779352---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T03:43:37.925
+Launch V∞: [5.523967747544116, -8.398981348232988, -0.6624967508893882] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6750400513918484e-6, -4.2947175801509817e-7, 9.50406392877734e-7] km/s
+ V∞_out: [-2.754711436762988e-6, 7.366241078256641e-7, -3.169383028119767e-7] km/s
+ time of flight: 1.5469583726405385e8 seconds
+ arrival date: 2028-03-24T14:47:34.925
+ thrust profile: [0.11193571306452216 -0.06357714929742223 -0.06018855351721368; 0.04233755682429911 -0.004877548669413603 -0.05638417480830268; 0.05127977638734266 0.002309675983647236 -0.11406827698483837; 0.04341944782599642 0.004078678528226674 -0.13051440842557677; 0.08523535084051617 0.02271033588826551 -0.32408055701560773; 0.021486839084266934 0.001582309922610981 -0.0928191945968546; 0.014475214241821098 0.0009406662659764738 -0.07603098959036575; 0.04318595174491504 0.0004300054528447992 -0.23058150840777084; 0.013619490487873455 0.0009951088491581763 -0.0746659838905675; 0.0034789230359057975 0.0020788779750088742 -0.027893178795930337; 5.592077750571311e-7 0.003343110630083961 -0.004552788911808473; 0.0017591434669518501 0.00034168134678326485 -0.003821473568332329; 0.02302596995185054 0.004895184351130577 -0.00607046759023667; -0.0005786769620807694 0.000905291330176437 0.00013063302913721888; -0.006325817895541895 -0.010129634884230188 0.007685481208266285; 8.023969076836157e-5 -0.0003880065334624632 -0.00140070478479501; -0.0018639529137539899 0.005146010821742043 0.008904211665275576; -0.004220352217034773 -0.004930306205513199 0.022165703974936727; -0.00831112348557783 -0.0037000978221127263 -0.0009487364951519096; -0.007050793613363905 -0.012594671415887888 0.02836254376351622] %
+
+Mass Used: 89.20434102285299 kg
+Launch C3: 101.49600930881225 km²/s²
+||V∞_in||: 2.8711596227144786e-6 km/s
diff --git a/archive/ES_0.5839476374569075 b/archive/ES_0.5839476374569075
new file mode 100644
index 0000000..5f77a8f
--- /dev/null
+++ b/archive/ES_0.5839476374569075
@@ -0,0 +1,22 @@
+archive/ES_0.5839476374569075---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T07:42:51.235
+Launch V∞: [7.128935389342506, -6.924375611272405, -0.849081287728507] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0443306122642861e-5, 2.8247005572891275e-5, 1.4287114860109724e-5] km/s
+ V∞_out: [2.459025441824638e-5, -1.8881205909940463e-5, -1.2241464675870153e-5] km/s
+ time of flight: 1.4136376334740674e8 seconds
+ arrival date: 2028-10-29T11:25:34.235
+ thrust profile: [0.2608132744824838 -0.09006249543038877 -0.12016725302991846; 0.1487014973411549 0.01934963331464867 -0.17292431732219865; 0.095075559613888 0.03196814940247515 -0.18027844047633879; 0.06698913102501199 0.031014786419621965 -0.17229145422558015; 0.06197597663315511 0.033745406217724705 -0.20099347145359592; 0.05530172949233382 0.03339459394368057 -0.21143818030637926; 0.022709575857232663 0.01611144042206957 -0.09895733490818562; 0.028466270432626728 0.019886830669683827 -0.13750754487629963; 0.006368421667849616 0.007038601416022496 -0.04474295088851109; -0.0022032432865858645 0.00630614947056097 -0.010890519694786807; 0.0054666167660472895 -0.0021364664428610665 -0.0063459924548353265; 0.004082041753076653 0.003030947493904761 -0.02271407407462264; 0.006740819635405076 -0.00705093972349292 2.0169009807825128e-5; -0.0034371066954555322 -0.004563549015335934 -0.004566103611076908; -0.001781028272794643 0.0040415649445208635 -0.000419219205844484; -0.003945922949769072 -0.0041189794347444905 -0.004564859172828619; 0.012547786417152176 -0.008225421708726735 -0.0017835594348521132; 0.01259562165522743 0.004851752515968906 0.004648290205531096; 0.016295140670391492 0.015234798834997863 0.000986496686562122; -0.012622940124363432 0.01472063337129927 -0.002189856221886846] %
+
+Mass Used: 100.91603122303923 kg
+Launch C3: 99.48963642457477 km²/s²
+||V∞_in||: 3.333283092736272e-5 km/s
diff --git a/archive/ES_0.5840059933791106 b/archive/ES_0.5840059933791106
new file mode 100644
index 0000000..407117b
--- /dev/null
+++ b/archive/ES_0.5840059933791106
@@ -0,0 +1,22 @@
+archive/ES_0.5840059933791106---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T02:28:16.546
+Launch V∞: [5.3238691690452296, -8.261091360084308, -0.7229620986853839] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.0199064837913986e-5, -1.2204347918255126e-5, 1.4752052152950245e-5] km/s
+ V∞_out: [-5.850557699473924e-5, 2.1562441976072187e-5, -9.97968186165852e-6] km/s
+ time of flight: 1.388722858040593e8 seconds
+ arrival date: 2027-09-16T10:06:21.546
+ thrust profile: [0.4392217633293593 -0.2720918501771761 -0.21482227008403415; 0.1870302189906836 -0.015862761705897444 -0.20566515146159953; 0.14073519372932963 0.01723637812542228 -0.2381836498533952; 0.09973880150241513 0.024316009219573113 -0.2243736491732876; 0.06397616746930261 0.02110553688431948 -0.1756431879911053; 0.03871536064697026 0.014975948102334375 -0.1228479073944343; 0.04779271590358959 0.020478590020707142 -0.17608891145299904; 0.020009460860022414 0.009466268292996325 -0.0829475137970483; 0.005378631331400895 0.0025645927598694587 -0.025709425603941682; 0.017260763365039938 0.007301525664892351 -0.07731805056399066; 0.002794212508123716 0.0018465960762581674 -0.016699292672189576; 0.0005881201963055054 0.00027934581341850813 -0.00011590973878811158; -1.2813107665124484e-5 -1.3311117100913203e-5 -0.00020177750857339096; -3.0947861619798404e-5 8.187171032002273e-5 0.00044675497877750994; 0.00020712333926688816 0.0001787573814315101 -0.0002917454389688417; 0.00016122838092423963 0.001219632815953324 -2.8477928822495172e-5; 8.842460185654494e-5 -1.9522095382071226e-5 0.0003777030467786368; -0.00044443571950451453 0.00011009095040827955 -0.00014447660444314716; 0.0004973099074754636 -4.436087311598166e-5 0.00027012974154254517; -0.00015170239387121974 -0.00021063675974004607 0.0004018014214001276] %
+
+Mass Used: 114.8543146970137 kg
+Launch C3: 97.1118875849055 km²/s²
+||V∞_in||: 6.317037722059727e-5 km/s
diff --git a/archive/ES_0.5840428844047884 b/archive/ES_0.5840428844047884
new file mode 100644
index 0000000..96ec396
--- /dev/null
+++ b/archive/ES_0.5840428844047884
@@ -0,0 +1,22 @@
+archive/ES_0.5840428844047884---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T11:22:01.962
+Launch V∞: [5.596496457274629, -8.12461373192675, -0.8691747238487011] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.821602603698161e-8, -1.7071157466830994e-8, 3.599043673085171e-8] km/s
+ V∞_out: [1.2889487780640541e-8, -3.154870148609804e-8, -4.4505289105074043e-8] km/s
+ time of flight: 1.472847676123327e8 seconds
+ arrival date: 2027-12-23T03:48:08.962
+ thrust profile: [0.27519424233706863 -0.15853739616888535 -0.13428306761733635; 0.1734566777078493 -0.0042237405288235025 -0.19391965962605195; 0.1208589934633617 0.023425031738028516 -0.2145616347886165; 0.08179910032003292 0.026844294911393212 -0.19828344616260174; 0.05720882921242473 0.02420686368360365 -0.1728110970650799; 0.038011260635033635 0.01915323494529492 -0.13675128276572748; 0.0193897140289991 0.010587924472564675 -0.0806341224462918; 0.02566900454324969 0.014766391737413924 -0.1187055460461138; 0.019152514044611147 0.013053674874530078 -0.09227145387105141; 0.008433197797401072 0.004744703219406496 -0.05007982609569652; -0.003099538815311899 -5.434994851100561e-5 -0.011336926624495305; 0.00047586531868558385 -0.0004385402938327182 0.0055651342967133945; -0.0020728439391293073 0.002694161289856199 0.005439389415732133; 0.002847045376294549 -0.004878939162674384 0.00588069023000995; 0.000914145139221457 0.0020242654841065673 0.008391195496338374; -0.0153859199104731 0.004518869678571608 -0.0016245404303360574; 0.003586032684524021 0.003128669675807237 -0.0033848280252690446; -0.003541798175463058 -0.010679837393944349 -0.023059586265803594; 0.007088554150968972 0.0032087758903282396 0.007706049291370358; -0.0045665323243649384 0.011223737697720854 -0.009798927988927184] %
+
+Mass Used: 109.21744919796674 kg
+Launch C3: 98.08558558987765 km²/s²
+||V∞_in||: 5.520145468548846e-8 km/s
diff --git a/archive/ES_0.5840520029220837 b/archive/ES_0.5840520029220837
new file mode 100644
index 0000000..5a1c40d
--- /dev/null
+++ b/archive/ES_0.5840520029220837
@@ -0,0 +1,22 @@
+archive/ES_0.5840520029220837---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T05:12:16.278
+Launch V∞: [7.0812538274497, -6.98591469640875, -0.9995952714388469] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1184971107280832e-5, 2.908717753269955e-5, 1.578020258584907e-5] km/s
+ V∞_out: [2.5297166838520594e-5, -2.0286384677398596e-5, -1.2987820420454432e-5] km/s
+ time of flight: 1.384503575764124e8 seconds
+ arrival date: 2028-09-25T15:38:13.278
+ thrust profile: [0.30809516004762344 -0.10226291252535302 -0.14719039942914247; 0.16933848807716967 0.020434778150894055 -0.20698468816170748; 0.06020792505857611 0.02064882996348949 -0.12075193197787239; 0.05651643948901615 0.02738491121971577 -0.15249979000628228; 0.03058912747568533 0.017352178268836994 -0.10310415812216477; 0.0513928025292868 0.04202023031635593 -0.2240977852232771; 0.03733458607269716 0.025717299451682305 -0.17940978775297323; 0.020570053299446764 0.015615495436387043 -0.10742579544505412; 0.012390954866814387 0.009566510943179871 -0.0703224545570248; 0.007934582892280044 0.006639041769583909 -0.04974951548689718; 0.01855802823181277 0.009508963709533911 -0.07312488274754898; 0.0006233920049012541 -0.00018336754183800153 -0.0022890327947069564; 0.00032793427589523883 0.00012428427239294322 -0.0012953491587607239; 0.00032443199318843815 0.0007372933192641367 -0.0010585648735689703; -0.0011840868533158407 -0.000743576056725078 -0.0011990312738872138; 0.0015557601171657998 0.0038615627934173494 -0.001650057314596768; -0.0005073025470505432 -0.00042527043813521653 -0.0008378956229053911; -0.0024400809414788734 -0.0008058671229040659 -0.0017776950198654308; 0.0006459091062429138 0.0002975417725972748 -0.0009955501996787386; -0.000540377479794228 0.002084847795397646 -0.0039009829401979727] %
+
+Mass Used: 98.37362478686782 kg
+Launch C3: 99.9463506209537 km²/s²
+||V∞_in||: 3.49311074708479e-5 km/s
diff --git a/archive/ES_0.5841050422674947 b/archive/ES_0.5841050422674947
new file mode 100644
index 0000000..59d720b
--- /dev/null
+++ b/archive/ES_0.5841050422674947
@@ -0,0 +1,22 @@
+archive/ES_0.5841050422674947---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T14:29:16.586
+Launch V∞: [6.924493893513153, -6.932027543186846, -0.5250342433725128] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0011148542724778018, -0.001637154649231128, -0.00013828756060747178] km/s
+ V∞_out: [0.00010592828846692411, -0.0005447461682113032, -0.0019063657009348053] km/s
+ time of flight: 1.4015200528834122e8 seconds
+ arrival date: 2028-10-14T17:36:01.586
+ thrust profile: [0.561963435469234 -0.17635469508976837 -0.22125731629473636; 0.12436621513821337 0.019221842609166352 -0.13939910835969388; 0.1155694000606088 0.04470249721419241 -0.21004336130465184; 0.13734355024279565 0.07466401874497329 -0.3258461027956862; 0.06880157321577783 0.0442528871526817 -0.21199574030242754; 0.02743203559062482 0.018121228153638754 -0.09938656623972997; 0.011910018158329812 0.008439082762366663 -0.052969298707179494; 0.019204688284379247 0.014710218448078547 -0.09048820136709818; 0.02667941819675808 0.022170798829589496 -0.13315381850778585; -0.0005523291504986329 0.00024676442396957474 -0.014323411109577971; 0.003373954450026205 0.0019196090112190347 -0.007059441082702051; -0.0006898050943388318 0.0003541867762789036 -0.008066040564458829; 0.0016652538190471745 0.0011168303548969548 -0.005723828883166831; 0.00320425767819105 9.126564608391119e-5 0.003445856212848283; 0.0010599125104601653 0.002699013214476473 0.00783082487418751; -0.007511322809772626 0.004493620582153032 0.01368907401640369; 0.002457793705401292 0.001986777067528328 -0.002844415126169228; 0.000305143814806173 -0.00807881873454513 0.01992646494207457; -0.0021001222477177446 -0.0015375943104883902 0.0018083821201843923; 0.009634482108164047 -0.007434542589239831 -0.0008973074141645047] %
+
+Mass Used: 119.83840140990196 kg
+Launch C3: 96.27728249751576 km²/s²
+||V∞_in||: 0.00198552231006853 km/s
diff --git a/archive/ES_0.5841167919197257 b/archive/ES_0.5841167919197257
new file mode 100644
index 0000000..5a49cc1
--- /dev/null
+++ b/archive/ES_0.5841167919197257
@@ -0,0 +1,22 @@
+archive/ES_0.5841167919197257---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T04:04:18.763
+Launch V∞: [5.420127444655009, -8.259000957581899, -0.21459885702340384] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.660134438436192e-6, 0.0037752648565353695, -0.0019598727014866705] km/s
+ V∞_out: [-0.0033814855379454617, -0.0019488912468428711, 0.0016863307024334046] km/s
+ time of flight: 1.407890814493945e8 seconds
+ arrival date: 2027-10-08T16:08:59.763
+ thrust profile: [0.30400094613440737 -0.18325808580454622 -0.15183303054757008; 0.21877839886812744 -0.015541313534562083 -0.24860132499490326; 0.14202195252887992 0.01661631141068752 -0.24847244773731061; 0.11677372033236681 0.02754027451200153 -0.2700777724764724; 0.0591085149375909 0.01812284541376595 -0.16786303618513787; 0.04806883750255361 0.017562703763130082 -0.15925010349225407; 0.045365409869726224 0.018365535950674867 -0.1688572282500319; 0.024199497263682784 0.010897986911768036 -0.10104871932101758; 0.0050415642973277355 0.0022045927576481513 -0.02323159683893459; 0.0003565727498859097 0.00036423716194873096 -0.0008854282003067017; 0.0015992536534073756 0.0005728379476606467 -0.010032466373852661; 0.00047024793642323173 -0.00028670857408060564 -0.0026091588017239805; -7.65241835500287e-5 0.00020448706133035285 0.0006229058972359773; 0.0007907646381991306 -1.2726519670898232e-5 -0.004140080557484268; -0.0008029181481878978 0.00021270223659271 -0.0002625988405177337; -0.0005763957609301856 -0.002233667914624841 0.0008671143995418835; -0.0004077393513665708 -0.006760880408828141 0.00018660019344117961; -0.008975715204357741 -0.0037248470625280694 0.0034769779188601447; 0.0004950009854428666 4.3970351176110816e-5 0.00013523852497170715; -0.006485649370967062 0.00030485201456639067 0.0020798662138589224] %
+
+Mass Used: 111.9324930550647 kg
+Launch C3: 97.6349310030769 km²/s²
+||V∞_in||: 0.004253682999615868 km/s
diff --git a/archive/ES_0.5842289470411822 b/archive/ES_0.5842289470411822
new file mode 100644
index 0000000..89ea8f0
--- /dev/null
+++ b/archive/ES_0.5842289470411822
@@ -0,0 +1,22 @@
+archive/ES_0.5842289470411822---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T11:50:58.597
+Launch V∞: [5.323521764502469, -8.139988747941674, -0.45087041096025987] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.773435578164886e-5, 2.478895197983636e-5, -4.6631190365408856e-5] km/s
+ V∞_out: [-2.2723292790751607e-5, 5.46840143051044e-5, 5.1132146758131104e-5] km/s
+ time of flight: 1.4087387362142813e8 seconds
+ arrival date: 2027-10-07T23:28:51.597
+ thrust profile: [0.5016322596826909 -0.29905321152016434 -0.22520358629247442; 0.28931828858873754 -0.014052141139504013 -0.2923397508518239; 0.17777924888106378 0.029848636268367087 -0.2767859048137781; 0.134120952301845 0.0399222893102901 -0.27644434692279013; 0.1156836177883983 0.0452577399552462 -0.2909984878508409; 0.04943499982532904 0.022529066457692707 -0.1465554856520526; 0.013039487911419477 0.0065860768687865225 -0.04474820688284926; 0.0022089445407402516 0.001500107790458154 -0.010118041851893965; -0.0007558042265164355 0.00218882944788165 -0.005617616785234312; 0.0016662702364213394 0.0016864011756081492 -0.009332399759176626; -0.003235941182540559 0.0010406440533853906 -0.001138591682201133; -0.0007221572942379273 0.001066535481330328 0.001631696380572676; -0.0023821087925587907 0.001742289581387679 -0.002174389691392003; -0.0017628398924204535 -0.0032927955815934434 -0.0013324933345127067; -0.0008187841751410069 0.004686178915845586 -0.006206979762735984; 0.005615576768134071 0.0008132569387885282 0.0027599214552572315; 0.0027797515925253573 -0.0018058345218757987 0.004521632401027062; 0.004187974782772495 -0.00902878538999069 0.004842708239123873; 0.001573792521175982 0.0018350094669692214 -0.0020169709586055767; 0.019569947860243464 -0.002041141455932408 0.008600959532643986] %
+
+Mass Used: 128.58535950754913 kg
+Launch C3: 94.80258492122802 km²/s²
+||V∞_in||: 7.82445901815304e-5 km/s
diff --git a/archive/ES_0.584249486816655 b/archive/ES_0.584249486816655
new file mode 100644
index 0000000..1f04a4d
--- /dev/null
+++ b/archive/ES_0.584249486816655
@@ -0,0 +1,22 @@
+archive/ES_0.584249486816655---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-25T16:02:12.649
+Launch V∞: [8.158020052371132, -6.305072337860401, 0.4884564142024518] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.113332777951334e-5, 0.00238565602748521, 3.8321553724769055e-5] km/s
+ V∞_out: [0.0009125840083335089, -0.00013925366224299497, 0.00020311952545004898] km/s
+ time of flight: 1.8749577787735155e8 seconds
+ arrival date: 2030-05-04T18:11:49.649
+ thrust profile: [0.008909494276257628 -0.0030637696128019386 -0.0048903165896552634; 0.0009719860042006991 -8.378726887412662e-5 -0.001727678639858371; 0.020906031171164616 -0.016476033060155614 -0.06566559557574252; 0.032352956471328485 -0.033433778520902194 -0.12290988288775201; 0.028409761907389145 -0.032626896047694434 -0.1174057479175101; 0.019210195149470415 -0.022980569822151735 -0.08345033435189617; 0.03515655156854363 -0.0433143743916089 -0.1521301914237708; 0.01618241371582327 -0.020363183541785013 -0.07223427257283836; 0.017532940467665303 -0.02240236155003003 -0.07870775239692711; 0.00316526209943519 -0.0038831700446436933 -0.014287316902214535; 0.005631834793525197 -0.006906199325295597 -0.02503440227992857; 0.0009550062429801496 -0.0011127944989192894 -0.004002185491239538; -0.00044700139921122954 0.0002821676086448468 -0.0009286432407508527; 0.00015239146165799816 -0.0001002542660323862 -0.0006092673973602655; 0.0002812204565943145 -0.0003307253985846175 -0.0010147622869266096; 0.0005202983848045607 -0.00031105947727359156 -0.0008356050546843521; 0.0008839273528940713 -0.0001940942128404435 -0.00011432090592918627; -0.0002599620783561604 0.0001297311402965635 0.0008920021300332854; 4.6432249158079075e-5 -0.00025925641854143363 0.001764758246919408; -0.00015316534213180295 -0.0003032386807406602 -0.0003315339844132245] %
+
+Mass Used: 60.10712944957913 kg
+Launch C3: 106.54581802911741 km²/s²
+||V∞_in||: 0.0023877036052216707 km/s
diff --git a/archive/ES_0.584347065078072 b/archive/ES_0.584347065078072
new file mode 100644
index 0000000..9889d7b
--- /dev/null
+++ b/archive/ES_0.584347065078072
@@ -0,0 +1,22 @@
+archive/ES_0.584347065078072---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T23:12:34.418
+Launch V∞: [5.369026216272462, -8.237646372792598, -0.6640630046943041] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00044249195713637145, 0.00019444743885918808, -0.0003593910302633509] km/s
+ V∞_out: [-0.00017431526684604442, 0.0004200937616110434, 0.00039480439481190144] km/s
+ time of flight: 1.399594052876951e8 seconds
+ arrival date: 2027-09-28T20:49:19.418
+ thrust profile: [0.4346094790375816 -0.2625682639789058 -0.2003568108117971; 0.16033532172929815 -0.010433549638684649 -0.1730887337001554; 0.13111779771264775 0.01933059579583079 -0.21649503864335423; 0.08889033078143746 0.02436564145077502 -0.19582753885372664; 0.06375467636952928 0.02296452402831988 -0.17245412246687739; 0.059939794618115154 0.025168816297874718 -0.18730009303489487; 0.024123897151650493 0.010636825964176776 -0.08697364667202195; 0.022456506075053322 0.011326456587483122 -0.08907168290453428; 0.011881637796968159 0.008565144813857877 -0.04710245808167095; 0.03734311387213543 0.02528049407793161 -0.1721724562974029; 0.0016122913036430075 0.000982332372684533 -0.007879323695284343; 0.00023027707330497426 0.0003136194630776781 -0.0013714428952216928; 7.399354454635566e-5 0.00033361571118093033 -0.0013237050665936357; -0.000508874300535063 -0.0005743213685553972 -0.0013113250102134168; 0.0006337188194377827 6.828486701063001e-5 -0.0014924319995866806; -6.26284154434017e-5 -0.0002761381727953271 -0.0008200241494667091; 0.00026926788613844356 0.00069059977049573 -0.00033513172634061766; -0.0009480242335798601 0.0011157700093529658 -0.002094508639412487; 0.0001513270372727622 0.0004253797205527539 -3.888620111295411e-5; -0.0007337004408345339 -0.0002452256011606878 0.0009053405041818618] %
+
+Mass Used: 115.16850955870586 kg
+Launch C3: 97.12623994840767 km²/s²
+||V∞_in||: 0.0006023046166542532 km/s
diff --git a/archive/ES_0.5843941096820578 b/archive/ES_0.5843941096820578
new file mode 100644
index 0000000..49cc422
--- /dev/null
+++ b/archive/ES_0.5843941096820578
@@ -0,0 +1,22 @@
+archive/ES_0.5843941096820578---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T16:26:18.464
+Launch V∞: [5.444005578641176, -8.545103942330087, -0.518546309090332] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.6726139895589134e-6, -1.1487555383053403e-6, 1.31986657763476e-6] km/s
+ V∞_out: [-3.809293064840044e-6, 1.3160267240427651e-6, -5.408173064135109e-7] km/s
+ time of flight: 1.5606671349237156e8 seconds
+ arrival date: 2028-04-12T00:18:11.464
+ thrust profile: [0.09797187015429194 -0.05996020706417293 -0.05847168136039344; 0.034737655654863635 -0.0075097252247751985 -0.05365821729611891; 0.05789351252188242 -0.008487740706079704 -0.15128301160278934; 0.06334589393812827 -0.00960886239353838 -0.22681026179041086; 0.05266228608365772 -0.009807767527540975 -0.2346885249369594; 0.03554293212065194 -0.0083162948802197 -0.1864217573209762; 0.018006300843000547 -0.005152993214355291 -0.1062005306694962; 0.01009957517113032 -0.003280577405743403 -0.06432449336600672; 0.004462351168480746 -0.0016826357948243975 -0.030101103245644398; 0.0035206279662412746 -0.0020595896641716948 -0.017527536534810515; 0.0008858746808152458 0.0002837057466277167 -0.008741607508625135; 0.0010282327736716123 -0.000582833611160552 -0.006874723982155823; 0.0020744368454911934 -0.0009875612721180632 -0.00736353616377044; -0.0009716624724322425 0.0006001708777416096 -0.00788593076361447; -0.00199607689493546 0.00010793464607512692 -0.00239749656892627; 0.0017803509374916104 0.0002357194469027775 -0.004084112414773065; 0.0004201670932178735 -0.0008101443360435891 -0.002872746818898042; -0.004994506438294771 -0.010852458158877594 -0.008825984779807434; 0.00015878784318195738 -0.0011846236380162194 0.0011316644042683845; 0.0011855823177636502 0.005729520117910154 -0.005370847464365322] %
+
+Mass Used: 81.39794562806037 kg
+Launch C3: 102.92488840017263 km²/s²
+||V∞_in||: 4.0681421540856125e-6 km/s
diff --git a/archive/ES_0.5844705007615787 b/archive/ES_0.5844705007615787
new file mode 100644
index 0000000..c69a8f6
--- /dev/null
+++ b/archive/ES_0.5844705007615787
@@ -0,0 +1,22 @@
+archive/ES_0.5844705007615787---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T03:10:58.050
+Launch V∞: [6.273888415406446, -7.2611779773729355, -1.0617540902787022] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00349874405057, -9.692497787597924e-5, 0.0024008348362546854] km/s
+ V∞_out: [-0.004037245244817113, 4.552042985358211e-5, 0.0012936661429445357] km/s
+ time of flight: 1.7774121864654619e8 seconds
+ arrival date: 2028-12-07T07:44:36.050
+ thrust profile: [0.5996812580596965 -0.18380443608381872 -0.18503273237525075; 0.24646975563420145 0.0737817623674849 -0.20738630187158616; 0.1543055461624406 0.09587973035123738 -0.2149803683495653; 0.11693694615896227 0.10222552200999875 -0.22768263169562059; 0.06153685741157381 0.06717742169671254 -0.155830724257393; 0.02914678979642355 0.037688694334599745 -0.09159947904284378; 0.011949849656470807 0.01776572613123438 -0.045661726679842994; 0.005423081902161183 0.009088774542369752 -0.02468541100578862; 0.0010720498614006342 0.0019199568645034625 -0.005743176801740262; 0.003356009825235024 0.006539017984873033 -0.019187463076147715; 0.0005503725205888807 0.0019198183865840896 -0.005116653772364957; 1.822529574868049e-5 -0.00010684969023354632 0.00025451505306361207; -0.0006258808160411967 0.0016473132630121625 -0.0008328413524337178; -0.001069535363874011 0.0005396148936248466 0.0008504461730488593; -0.0004971647132968051 -0.00020075262856855105 0.0007307483166004072; 0.0008891390313353843 -0.0009160935595054764 -0.0009450299416932874; -0.0022276768134077782 -0.0013664275946509677 -0.0010360548612482036; -0.0010901067580359317 -0.00043128111116780114 0.0007651623474178728; 0.001850680778690304 0.0015500312751140157 -0.0012966824571082685; -0.0008477303919121641 -0.002155909122872067 0.003153028586660132] %
+
+Mass Used: 138.13564879353908 kg
+Launch C3: 93.21370321628046 km²/s²
+||V∞_in||: 0.004244362413096847 km/s
diff --git a/archive/ES_0.5844830460863794 b/archive/ES_0.5844830460863794
new file mode 100644
index 0000000..a152288
--- /dev/null
+++ b/archive/ES_0.5844830460863794
@@ -0,0 +1,22 @@
+archive/ES_0.5844830460863794---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T22:47:59.844
+Launch V∞: [5.2767534041607815, -8.095152340143207, -0.45186443495622886] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7929109094608683e-7, -2.7914489648318414e-8, 3.782083831383665e-8] km/s
+ V∞_out: [-1.8403229429222557e-7, 1.7249874111949938e-8, -2.2571353803000036e-8] km/s
+ time of flight: 1.4011999537279135e8 seconds
+ arrival date: 2027-09-28T17:01:14.844
+ thrust profile: [0.6741756666453782 -0.39463395127346024 -0.2716915486330256; 0.2683487100630184 -0.006237592730915228 -0.2570043397660399; 0.13752507780855314 0.028111767108811216 -0.20619370229935066; 0.10888637248947705 0.03773075136673941 -0.21477802509008145; 0.0654520127074445 0.028889969248889258 -0.15912407175060336; 0.058078791033772496 0.029512513897478044 -0.1627199235406265; 0.07102405119603483 0.04173696852180939 -0.21753889564319773; 0.02148951293592413 0.013606271485094152 -0.07893285953988599; 0.005847859502882349 0.003555850449047893 -0.019503771065999754; 0.006229516826065072 0.005130681295128397 -0.028306940194158366; 0.0037860171954020336 0.00020712611955330537 -0.009120478380784964; -0.0008921308380056656 0.0001553283504622663 -0.0006336661649505066; 0.00024655676890692987 0.0005070038226954615 -0.0006568211853918149; -0.00016368919830580988 -0.0003408306853624329 0.0003779264389616962; -0.0008681984070967464 -0.0007041858974755409 0.0016282996480864547; -0.00040463504975488574 0.0026532880631572574 0.004270581759814751; -0.00034444180239051093 -0.0005855196326192767 -0.0017474104756779242; 0.0010414695286879814 -0.0038127484449128847 -0.000527138640506626; 0.0002452126705276565 0.0008568318450092403 -0.0005274036540408554; -0.001742965597880856 -0.0024024392668315726 0.002983005495902543] %
+
+Mass Used: 136.01472413228657 kg
+Launch C3: 93.57979936602675 km²/s²
+||V∞_in||: 1.8535082906673343e-7 km/s
diff --git a/archive/ES_0.5845534724044223 b/archive/ES_0.5845534724044223
new file mode 100644
index 0000000..e6407cc
--- /dev/null
+++ b/archive/ES_0.5845534724044223
@@ -0,0 +1,22 @@
+archive/ES_0.5845534724044223---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T16:34:41.669
+Launch V∞: [5.2760490487237135, -8.186634249036091, -0.25785893381437996] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.727144016029119e-5, -0.0001156595072289948, -1.0159150061696834e-5] km/s
+ V∞_out: [6.427924137947185e-6, -3.53063909962269e-5, -0.00013474517425891578] km/s
+ time of flight: 1.4069433567462415e8 seconds
+ arrival date: 2027-10-06T02:20:16.669
+ thrust profile: [0.4965299058718585 -0.2822978736751913 -0.201951185502525; 0.2633688072473747 -0.0019283956145598668 -0.24668507574199364; 0.168434141427945 0.03762893827889604 -0.2399656611509588; 0.14178209929299332 0.05188432471344884 -0.2648693180812429; 0.08783097604413417 0.041940367041893654 -0.20547001651876454; 0.053530028381263244 0.02832245040592969 -0.15011965856335105; 0.04763274782387939 0.028656050225121927 -0.14968278155200718; 0.025348145608215192 0.01594156929086847 -0.08983764689960844; -0.00046291889699377043 -1.6434831992673434e-5 0.0003244629724830138; 0.005902220872651534 0.004185154889145962 -0.02355406017275758; -0.0018230827978288583 0.0033198009216050986 -0.004230739003521333; -0.0018984530253005534 0.002357484744440916 0.0007597731545036204; -0.00046411359485426886 0.001575508508916044 -0.0020737471093563494; -0.0022378323811891704 -0.0010588550814774216 -0.002360813203411631; -0.00010463443297841499 0.0003703225545541322 -0.0013974127081543466; -0.004710270551145946 0.0009223073598150989 -0.009349944573136938; -0.00018823984768479674 0.0053950294172704786 0.002325780873728829; -0.00572624776522067 -0.0014564174210074494 -0.002594089417610411; -0.004292710947740213 0.000232701745400401 0.0002490586697645714; 0.0057102779949140875 0.0012023984854935216 0.008006278016889098] %
+
+Mass Used: 128.25475459479367 kg
+Launch C3: 94.924165121777 km²/s²
+||V∞_in||: 0.0001394675783358822 km/s
diff --git a/archive/ES_0.5846834913032632 b/archive/ES_0.5846834913032632
new file mode 100644
index 0000000..ab2cc4f
--- /dev/null
+++ b/archive/ES_0.5846834913032632
@@ -0,0 +1,22 @@
+archive/ES_0.5846834913032632---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T21:09:11.341
+Launch V∞: [6.3834786164452515, -7.187982603493122, 0.4662196671415851] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.029984179536096e-7, 0.00022675700585172488, -0.00015872394793222083] km/s
+ V∞_out: [-0.00012605016100773815, -0.00024257752617207906, 4.213230079950815e-5] km/s
+ time of flight: 1.780357205932485e8 seconds
+ arrival date: 2028-12-09T11:31:11.341
+ thrust profile: [0.6744577972445072 -0.20041122236456269 -0.16258381386067525; 0.26772077997005383 0.08077413795385453 -0.19719548017439603; 0.15953707445570034 0.09812691414371869 -0.19620030082150092; 0.11331648320708892 0.09686306857400097 -0.19453741124838855; 0.04568213361381692 0.04803493562694223 -0.1035840892681397; 0.04059989101793906 0.050299587362497906 -0.11117722141540069; 0.006916990388194327 0.009658669528619487 -0.02086576785176686; 0.007694370800072042 0.01200153175649953 -0.02727031656450856; 0.0021131866995993138 0.0006752774376518413 -0.003529637912003197; 0.004416872738821181 0.002501379817275601 -0.006798678978921947; 0.003339616341953523 0.005304703714196351 0.002760565193640451; 0.002726531573996919 0.004016098287962119 -0.001922842901137672; -0.0017498815071714132 -0.008065676618550774 -0.0036571500092017367; -0.004631122661067284 -0.006137294008374192 -0.0029424020538641573; -0.0019033076352309285 -0.0006261301794739577 -1.0012382598614464e-5; 0.00200701271065044 -0.0046685262331176616 0.0028350735854621514; -0.013760458121446247 -0.011602467047854153 -0.009227900615917954; -0.006897876967251043 0.002743957010585209 0.015194314037641937; -0.014627121241298497 -0.009565175538559897 -0.009541261879353592; 0.005047408526110209 0.0030490828740994563 -0.0005528155632350707] %
+
+Mass Used: 141.7700919126887 kg
+Launch C3: 92.63325393276315 km²/s²
+||V∞_in||: 0.00027678967747516375 km/s
diff --git a/archive/ES_0.584696118939017 b/archive/ES_0.584696118939017
new file mode 100644
index 0000000..ab82bf4
--- /dev/null
+++ b/archive/ES_0.584696118939017
@@ -0,0 +1,22 @@
+archive/ES_0.584696118939017---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-17T23:39:35.386
+Launch V∞: [5.689833803116961, -7.657636822532883, -0.21746946274513368] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008148309790368501, 0.0008010254451711994, 0.0007526441016943612] km/s
+ V∞_out: [-0.0008727636967876823, -0.000500362138173157, 0.0009263377770313637] km/s
+ time of flight: 1.572556226781417e8 seconds
+ arrival date: 2028-04-11T01:46:37.386
+ thrust profile: [0.7524434838169923 -0.3323325279000106 -0.21390980453376168; 0.27369631706722697 0.04003786987517772 -0.20609185573312036; 0.21558492878377195 0.09087463119145514 -0.2535695526457892; 0.16999426630682715 0.10419306499308208 -0.26808384058704415; 0.043495486793062144 0.03297032028875481 -0.09049188329587031; 0.03401374418628395 0.030192215239155898 -0.08339330045741004; 0.021270339015770683 0.021198958311415286 -0.059474976085117086; 0.04363852586924994 0.048863848386041166 -0.13784159759950584; 0.009830688834080248 0.01249351787665495 -0.034974429064029575; 0.005039445311621377 0.007018029664336912 -0.019731852833206; 0.0017945823757230391 0.0015143553286257625 -0.001997107471653349; 0.000747209367663726 0.0012805502050772853 -0.00423784182229427; 0.000982441535788144 -0.0008001111916488184 -0.00041474324721456086; 0.0013245593812664207 -0.004806316732201225 -4.587984992327821e-5; 0.004469327260332024 -0.005698690835647353 2.348991064360232e-5; 2.4966916749740727e-5 -3.55626233188689e-6 0.0004984307630243462; 0.004676985411969252 -0.0017792053767009199 -0.0032559195242899686; -0.011647823088347815 0.0021842578071045817 -0.006094742951284654; -0.0010238264320762626 0.00024569138998304643 -0.0070750421939904246; 0.001399347944683798 0.006998600772637985 0.005210308674154445] %
+
+Mass Used: 150.95686904475815 kg
+Launch C3: 91.06090338013057 km²/s²
+||V∞_in||: 0.001368234056009856 km/s
diff --git a/archive/ES_0.5847250124677476 b/archive/ES_0.5847250124677476
new file mode 100644
index 0000000..615b6a3
--- /dev/null
+++ b/archive/ES_0.5847250124677476
@@ -0,0 +1,22 @@
+archive/ES_0.5847250124677476---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T17:45:50.110
+Launch V∞: [5.29540854602193, -8.232894882045024, -0.5870873398686426] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.346779930285867e-6, -4.718745858582826e-6, -8.94198387803576e-6] km/s
+ V∞_out: [6.17237682289032e-6, -8.282222273684707e-6, 9.073121981356061e-6] km/s
+ time of flight: 1.3736065029809335e8 seconds
+ arrival date: 2027-08-28T13:30:00.110
+ thrust profile: [0.4506055055671192 -0.2746237497739096 -0.2064942967109274; 0.28199260308123686 -0.017763615943355873 -0.2828176586035415; 0.176344690196345 0.026994131828299628 -0.2707111326826436; 0.1293858032854282 0.0365840125048256 -0.26139727707425997; 0.09974570169229373 0.037222029653830646 -0.24552031710369138; 0.060794061334901894 0.026920689606839132 -0.17795262179594612; 0.028226924291773134 0.014567795633257696 -0.09821675801121474; 0.0033164150348201004 0.001646683266873219 -0.012738640629518395; 0.0039149816295686035 0.002063347060173018 -0.01585197880241444; 0.003997488949855029 0.002382710104598096 -0.017702247962007308; 0.003594251837998153 0.001725874663205502 -0.015623296733743722; 0.0002107849242377356 0.00013921205132453327 -0.0007426532486741903; 6.668141628379915e-5 0.0001547565192394853 -0.0008936971963503719; 0.0001649779585416925 0.00010700853931301386 -0.0007197865903728411; -0.00022653368346729178 0.00011067490151586415 9.116565647237151e-5; -0.0002504228147951318 -0.0006273355589292912 0.0007749298892675801; -0.0008823548292026223 -0.0005518273792105881 5.8286887605582625e-5; -0.00023861467070511954 0.0002956827964506681 0.00038812835198732943; 6.5586183524589045e-6 8.281285088743043e-7 -1.588650068600427e-5; -0.0004814287037867239 -0.0010107906045111862 0.00022700746839754904] %
+
+Mass Used: 121.2074566548431 kg
+Launch C3: 96.16658135271928 km²/s²
+||V∞_in||: 1.3769093405817926e-5 km/s
diff --git a/archive/ES_0.5847704656387733 b/archive/ES_0.5847704656387733
new file mode 100644
index 0000000..b26ef9c
--- /dev/null
+++ b/archive/ES_0.5847704656387733
@@ -0,0 +1,22 @@
+archive/ES_0.5847704656387733---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T00:56:15.494
+Launch V∞: [5.3657079975699595, -8.353887698967858, -0.7007566135168738] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0027055037705765827, -0.016921561912182904, 0.01831912014013213] km/s
+ V∞_out: [-0.01778540524748712, -0.014912820753266626, -0.009773339887581901] km/s
+ time of flight: 1.4151814057583192e8 seconds
+ arrival date: 2027-10-18T23:31:55.494
+ thrust profile: [0.27314739520893877 -0.16782411427274782 -0.1446141105581369; 0.14455420823091242 -0.013855710287992297 -0.1746146447826754; 0.10528194487487418 0.010262984623282439 -0.19781564656934408; 0.09156160430243918 0.01894081847669063 -0.22877473248463445; 0.06503442364135487 0.017898594952387294 -0.19904447727466926; 0.05561326612440844 0.01797850744479696 -0.1980912685523137; 0.0323903436216977 0.011633042060691195 -0.1314552599883858; 0.017013478752970327 0.006486213954717177 -0.07326925575762502; 0.007183263742023051 0.002991654644606523 -0.03260635734861084; 0.007797023918848459 0.003322805431317001 -0.0384893585163205; 0.001991084883871736 0.004022111616908821 -0.01166073473470406; -0.0020843154013866164 -0.004373167573957442 -0.00821686833719927; 0.0033930282143013603 -0.0022776658514503836 -0.005561766125180818; 0.002502979852464172 -0.0022864067504967753 -0.012434065063198281; 0.001242181461416161 -0.0025676999615271753 -0.002204064699289553; 0.000836043275064922 -0.0017108826802727886 -0.005437348630569881; 0.008316379310166627 -0.00185888175262391 0.0013610946426935461; -0.004708146268779216 0.0012237297296986594 0.0007311606030368043; 0.002244906889249968 -0.00012033921254609489 -0.0030636647156719885; -0.02277809389198511 -0.011884961723423175 -0.018341085450753962] %
+
+Mass Used: 104.32783254958349 kg
+Launch C3: 99.06932183354034 km²/s²
+||V∞_in||: 0.025084839463489453 km/s
diff --git a/archive/ES_0.5847733391581955 b/archive/ES_0.5847733391581955
new file mode 100644
index 0000000..fad2072
--- /dev/null
+++ b/archive/ES_0.5847733391581955
@@ -0,0 +1,22 @@
+archive/ES_0.5847733391581955---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T15:18:27.982
+Launch V∞: [6.253695361827035, -6.943780147710702, 0.4014177053361235] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8466473805124434e-8, 3.444997506943234e-8, 1.8328348675711003e-8] km/s
+ V∞_out: [-1.104818535822629e-8, 2.27842263824173e-8, -3.637157734904861e-8] km/s
+ time of flight: 1.8749577787425214e8 seconds
+ arrival date: 2029-03-28T17:28:04.982
+ thrust profile: [1.0 -0.268144588134159 -0.19726708669303664; 0.3853529098854959 0.1474172230872678 -0.22640177178767087; 0.1704422186444106 0.12134737066490052 -0.1661475441241329; 0.09078792949482013 0.09139288733916705 -0.12592775080155041; 0.035184629798345114 0.048339217635488235 -0.073412287328289; 0.01740197895735654 0.02840807025268415 -0.04751699492684095; 0.013940076302860982 0.02052568264211501 -0.037313055156526824; 0.0037449085375595615 0.007677497843349048 -0.013845819411886232; 0.013693607765265872 0.035222416465352596 -0.06038559352049568; 0.001284330203264647 0.004094390289100634 -0.00754741911355958; 0.0018980296706683764 0.00035897892035385447 -0.0024075770364478007; 0.0018411971450875302 0.00349005231013191 -0.00046746955410491287; 2.4668101285664353e-5 -1.4657137543080717e-6 -0.0027287840229512587; -0.00019213125255426985 0.000829141153815178 -0.0015533073670665242; -0.0014045654966402363 0.0007734829215081301 0.0010493668564173328; 0.00037313582877122995 0.0003548315017113347 -0.006437573301168174; 0.0023366522569223864 0.004852781454670416 -0.0016220040925928583; -0.004100789858358721 0.002760295687892455 -0.005103110777109628; -0.00028522817487662154 0.0009562086246936805 -0.0019020889553362813; -0.0002448638903290702 -0.0017197183745205858 0.0011191932297372682] %
+
+Mass Used: 171.9010022286875 kg
+Launch C3: 87.48592459243554 km²/s²
+||V∞_in||: 4.317105282777215e-8 km/s
diff --git a/archive/ES_0.5847979896541323 b/archive/ES_0.5847979896541323
new file mode 100644
index 0000000..c4773f6
--- /dev/null
+++ b/archive/ES_0.5847979896541323
@@ -0,0 +1,22 @@
+archive/ES_0.5847979896541323---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T13:43:04.555
+Launch V∞: [7.7036565018647325, -5.730829769896251, -0.1204191584196557] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002267337133674003, -0.0007017552606821041, -0.001470596386399493] km/s
+ V∞_out: [-0.0016272487266323409, -0.00020347447326838182, 0.00014683170062198558] km/s
+ time of flight: 1.7564679608104798e8 seconds
+ arrival date: 2029-11-24T12:29:40.555
+ thrust profile: [0.6189725589390798 -0.03852484647576183 -0.13036273467427645; 0.3638912365903042 0.21362814946221767 -0.2463552065634988; 0.1920699314457935 0.19609811455098947 -0.23630085800828812; 0.09769291699361035 0.1381863101505246 -0.18433392026329418; 0.038160784027849205 0.06940916920369959 -0.10439593048275704; 0.009568598445864931 0.0224969183621575 -0.03854156512046677; 0.005914430220503221 0.017626356602641374 -0.030642512666922583; 0.0016020439252918592 0.004923227420688253 -0.01376968112968827; 0.0016238701093428953 0.007054625509112443 -0.013831909903341716; 0.003246736640486276 0.017003031262137175 -0.03261268267401837; 0.00177617544548523 -0.00011142513713530166 -0.0014277356561470645; 0.004211306976869363 0.002702381522244142 -0.004981672524354624; -0.00032659350090086497 0.0007506484042520659 0.001167813745794448; -0.0029630694311504717 0.0004857530931977568 0.0023321507582920857; -0.0005540850437860839 -0.0009998863212517346 2.0899791572027548e-5; 0.0029512702918485668 -0.0009969186770017982 0.005541984387622444; -5.616486219476007e-5 0.0019329631019013851 -0.0005819953758883054; 0.004341951248866982 0.0016280963748656866 0.00610224908292605; -0.0014801397501495658 -0.0019087334045949362 0.009798591958585418; 0.004261556749896976 0.006396947766794406 0.003357147595460534] %
+
+Mass Used: 144.41212220668376 kg
+Launch C3: 92.20323412396638 km²/s²
+||V∞_in||: 0.0016451511645935838 km/s
diff --git a/archive/ES_0.5848100822098353 b/archive/ES_0.5848100822098353
new file mode 100644
index 0000000..29382b0
--- /dev/null
+++ b/archive/ES_0.5848100822098353
@@ -0,0 +1,22 @@
+archive/ES_0.5848100822098353---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T21:26:30.297
+Launch V∞: [5.29088865984384, -8.406716570939606, -0.7583269269541655] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1367815165021175e-5, 4.371055608638805e-6, -5.3699103670234984e-6] km/s
+ V∞_out: [2.0520648126800262e-5, -8.280249793506465e-6, 3.739246682324735e-6] km/s
+ time of flight: 1.416771329224912e8 seconds
+ arrival date: 2027-10-21T16:12:02.297
+ thrust profile: [0.27857586515926736 -0.17423366060958026 -0.1494676283967728; 0.15016079498925508 -0.017173661077763684 -0.18803625305982627; 0.10997266061219088 0.007816704373062151 -0.215437542485516; 0.0729432025121485 0.011832171455338885 -0.19069980434568434; 0.08218051877290167 0.019759792461134622 -0.26456627537472044; 0.03756183802201897 0.01006532303011203 -0.14388167834046114; 0.02541702150740786 0.007223813655703205 -0.1103030233363754; 0.030151404734567643 0.009374991712073347 -0.13201539578926313; 0.0027673825044944836 -0.0006255249722637566 -0.011600366390195536; 0.0016660992572221645 0.004688189621470896 -0.0126920990083948; 0.002080549675099429 -0.0005172811904758901 0.00018278081550787348; 0.001597760301345033 -0.0045215185584552165 -0.0012461681592443926; 0.006538372275364913 -0.0015268427615351666 -0.006176449440611366; -0.00520427017325314 0.0034604646778913957 -0.0008135699198834993; 0.005778476426314861 -0.004800289688888256 -0.008903322968342084; -0.0062434489710335205 0.0006332061935687002 0.0017542268420320823; 0.0034814642467048216 0.0032872018908494884 -9.035425600023225e-6; -0.0038718881446360627 0.0036888746472426097 -0.010981110035241584; 0.007085042970530812 0.0040646132317903386 -0.004209730422486905; -8.943063124967031e-5 -0.0018024690637798064 -0.015063563519911137] %
+
+Mass Used: 103.36999399328352 kg
+Launch C3: 99.24144604311846 km²/s²
+||V∞_in||: 2.2461647076966286e-5 km/s
diff --git a/archive/ES_0.5848669860904722 b/archive/ES_0.5848669860904722
new file mode 100644
index 0000000..1d5993a
--- /dev/null
+++ b/archive/ES_0.5848669860904722
@@ -0,0 +1,22 @@
+archive/ES_0.5848669860904722---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T22:24:27.889
+Launch V∞: [6.9927368464885555, -7.177753684179866, -1.283982411641439] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0028679855508965246, -0.004303158611899343, -0.0003675290857126061] km/s
+ V∞_out: [0.000349381906485708, -0.0015306815747929232, -0.004940962471306103] km/s
+ time of flight: 1.3560605139369228e8 seconds
+ arrival date: 2028-08-25T10:45:18.889
+ thrust profile: [0.2782017109849068 -0.1096580262101373 -0.14925737356480093; 0.06182609614837517 0.0022991548105492266 -0.08283893095644336; 0.09696453566265842 0.02036268368610981 -0.20735830748984038; 0.09673275062491356 0.02920884459557083 -0.28094151585733007; 0.075833926821854 0.026999518279598067 -0.2748901607127358; 0.04020464635656415 0.015364501698632368 -0.17313741328222657; 0.018683466659120698 0.0074603213568497475 -0.0927000202921659; 0.0040609516576528 0.0019240731896538266 -0.025031137824864203; 0.004583285898644454 0.0019796153291653067 -0.027107378181863418; 0.0023229906043881828 0.0011477684469134108 -0.01655956515992787; 0.0007081342281428059 0.00022075632030523683 -0.004421642342503268; -0.0003136387018629125 3.4700463022184535e-5 -0.0019667724614909894; 0.000682031658266603 0.0003352806388291832 -0.0009625237904800798; -0.0001161174973535015 0.000277967054225285 -0.00037467683500977617; 0.0009392108279249071 0.0005284911290577734 -0.0006609995827213692; 0.0007350068726558875 1.1830296484351718e-5 -0.0015408607605001108; -0.00025280397117051533 0.00130845779784211 -0.001311446290713474; 0.00022734035674599795 -0.00020817860147890384 0.0007235336499821551; 0.000404252304324696 -1.3530362931396566e-5 -0.00018332162927110263; -8.134364046553889e-6 0.00026230299885641453 -0.000587744220346526] %
+
+Mass Used: 86.95324067321235 kg
+Launch C3: 102.06712738840089 km²/s²
+||V∞_in||: 0.0051843604029966385 km/s
diff --git a/archive/ES_0.5849294942279506 b/archive/ES_0.5849294942279506
new file mode 100644
index 0000000..8d69f28
--- /dev/null
+++ b/archive/ES_0.5849294942279506
@@ -0,0 +1,22 @@
+archive/ES_0.5849294942279506---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T18:42:10.491
+Launch V∞: [7.004576136760054, -6.941480701799398, -0.9250150677034402] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.552279805581022e-9, 2.364410021753795e-9, 7.661208388678574e-10] km/s
+ V∞_out: [2.751539267391444e-9, -2.239716730438617e-9, -1.7184908237161145e-9] km/s
+ time of flight: 1.357745960158499e8 seconds
+ arrival date: 2028-08-24T05:52:06.491
+ thrust profile: [0.4851049118078009 -0.17818253568558867 -0.2270120433524158; 0.1663438410151283 0.019062552801759218 -0.19141084017230114; 0.11733426528587042 0.03858558728287333 -0.217249959633487; 0.09833894936172376 0.04539655581646944 -0.2470115263367621; 0.07774952831541221 0.04315050017367931 -0.24326082791288384; 0.055331258425155 0.0345500693401984 -0.20503799480736185; 0.01138256684159394 0.007599545619859227 -0.05095139321503011; 0.01868220483605907 0.013636165656281231 -0.0892974341393877; 0.005005708812842291 0.003866656224515014 -0.02592949914613618; 0.0033665304314196153 0.002146818580564745 -0.01832228378306794; 0.0005135939573414016 0.00020592333893063594 -0.0027731249783161955; 0.0011025056781858076 -0.00014980600276951633 -0.004236407807977078; -0.000459627484405428 -0.0020826195646589567 0.0012414226923093022; -0.001998918426921295 0.0008781245734650459 -0.0010008837003471903; 0.0017199973943291388 -0.00013697998638175098 -0.0013119242576615866; -0.0009395837489933988 0.0004990934542984541 0.002922449099057162; -0.002255744197113036 0.0010671814168041565 -0.003842233667835231; -0.00552233618667756 0.0024124695290842386 -6.846281139915038e-5; -0.0025382082782616144 0.0017792932356834393 0.0011237095377500056; -0.002407749225687271 -0.0016055022285294217 -0.0009469180461341249] %
+
+Mass Used: 110.1450278891075 kg
+Launch C3: 98.10389406460027 km²/s²
+||V∞_in||: 3.562514294244175e-9 km/s
diff --git a/archive/ES_0.5850058266590924 b/archive/ES_0.5850058266590924
new file mode 100644
index 0000000..928582e
--- /dev/null
+++ b/archive/ES_0.5850058266590924
@@ -0,0 +1,22 @@
+archive/ES_0.5850058266590924---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T09:06:26.804
+Launch V∞: [5.397766545854249, -8.506086318951501, -0.9854474306350138] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008516018240136562, 0.05021402001996721, -0.05866705181613159] km/s
+ V∞_out: [0.052259733593035644, 0.047527771891076875, 0.032336681524021034] km/s
+ time of flight: 1.3948978446680114e8 seconds
+ arrival date: 2027-09-26T20:16:10.804
+ thrust profile: [0.08687863869326995 -0.05841284195791471 -0.05103067970815739; 0.10817660765749094 -0.018449290343668136 -0.14271954040239698; 0.09585289451561431 -0.0009737196227423254 -0.19825083273505878; 0.08273319617100464 0.0053441336139855794 -0.2286276998075908; 0.06705617415268063 0.007106034081358622 -0.22783594844952434; 0.05085924460491692 0.006746308077669741 -0.20218108877478996; 0.03493869802388664 0.00532347409359948 -0.15730289921851956; 0.019705231807271524 0.0032700468377488087 -0.0985813538298331; 0.005460974106238616 0.0008888655347146366 -0.03054714410346313; 0.000385063758703991 -3.871698833301413e-5 -0.00296464882788919; -0.0002694381820241693 0.00030539914556647574 -0.0023914322392541085; -0.001355265174827276 0.0006592420667444873 -0.0002422553472142086; 0.0003614526803733637 0.00015005591228469165 -0.004189178406524935; -0.0004254731981029568 -1.3976961897441869e-7 -0.00033812488755086123; -0.0002867433222341936 0.00033442421495596887 -0.004671268226006857; 0.002080336164057678 0.0012671471940168978 -0.0002018032647402412; 0.0021125640025925064 -0.000662295193268609 0.0027596923960579354; 0.003474108789628106 0.0016775794674696964 -0.001019500701823394; 0.0007714855963557219 0.00029498898848486356 5.5155136905339804e-5; 0.0008403978618301059 0.0003959861755671294 -0.00026904095223357206] %
+
+Mass Used: 84.82057817494388 kg
+Launch C3: 102.46049478754237 km²/s²
+||V∞_in||: 0.07769036839936258 km/s
diff --git a/archive/ES_0.5850081546873639 b/archive/ES_0.5850081546873639
new file mode 100644
index 0000000..7da58e6
--- /dev/null
+++ b/archive/ES_0.5850081546873639
@@ -0,0 +1,22 @@
+archive/ES_0.5850081546873639---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T04:09:27.598
+Launch V∞: [7.670837034817989, -6.148425678964583, -0.026052299896945026] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004341382916288548, 0.0002863397293297581, -0.00020520906415495924] km/s
+ V∞_out: [8.82498884374066e-5, 0.000551595558160614, -2.2390766627461803e-5] km/s
+ time of flight: 1.7137570058666894e8 seconds
+ arrival date: 2029-10-15T16:31:07.598
+ thrust profile: [0.3364448302917076 -0.04377929679022329 -0.12648038483023677; 0.04727104941800721 0.01754819737795552 -0.0629583849079137; 0.06510216999977955 0.04386941463182695 -0.14074484213238012; 0.05916115983782605 0.05181600024043731 -0.17956307934217564; 0.04282240790586712 0.04459542334011079 -0.1709632031088716; 0.019680986160326933 0.021405248962663964 -0.09981688777048663; 0.012035012970091123 0.011292967349718866 -0.06177466849257987; 0.008524308819930592 0.011766594023206607 -0.06665779967278394; 0.0011378334182409093 0.005369959211988932 -0.0497370649123441; 0.0060361139946663615 0.013079803235240975 -0.07928732085287649; -0.003539446993403998 -0.0036258811176241696 0.010283323913805719; -0.004743018212327013 0.005424931083318505 0.009048556595201585; 0.002603947178175255 0.011862966032171442 -0.00951665987600994; -0.0015664749030548956 0.014007278161170075 -0.011281367217526312; 0.0179096225235372 0.006045959590021063 0.02372807837368943; -0.002332593056467282 0.0021506037746803213 0.005668788365774541; 0.013472196182015755 -0.08523328447063944 0.05891928195023282; -0.0037144031943385798 -0.009853871445090593 0.03813739825139269; 0.01844869732304928 0.008855742951286856 -0.07921029604467998; 0.005576632553129769 0.04168142292824986 0.0589115007084743] %
+
+Mass Used: 118.74375957882967 kg
+Launch C3: 96.64555786681626 km²/s²
+||V∞_in||: 0.0005590860907431107 km/s
diff --git a/archive/ES_0.5850279886939524 b/archive/ES_0.5850279886939524
new file mode 100644
index 0000000..54c0904
--- /dev/null
+++ b/archive/ES_0.5850279886939524
@@ -0,0 +1,22 @@
+archive/ES_0.5850279886939524---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-12T11:11:29.319
+Launch V∞: [6.331876803368434, -8.082354541523815, -0.5117607848641802] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.014116564711113552, 0.007030608925425516, -0.015959119687696633] km/s
+ V∞_out: [0.01440323655715906, 0.005864885220709553, 0.016189888229315885] km/s
+ time of flight: 1.8749577784020436e8 seconds
+ arrival date: 2029-04-20T13:21:06.319
+ thrust profile: [0.034806893303350836 -0.01790151429351889 -0.021375708198013807; 0.048552702305885334 -0.019355651513393506 -0.09594840888537902; 0.02714821905636405 -0.0165287715415053 -0.09510857602777133; 0.018245273031317785 -0.015912101591461215 -0.08774667675663647; 0.015836738007054558 -0.01721082969819425 -0.09255011861663262; 0.013142748914842755 -0.017016399003794622 -0.08836951068168199; 0.013087620638989035 -0.020195435759063136 -0.09931790800599405; 0.017733600075172978 -0.025598011961414896 -0.12715872315463603; 0.010546107615011378 -0.015935152186378667 -0.07920527473997174; 0.0008259595238089549 -0.00127432540660414 -0.006596041368899087; 0.0016941879848943542 -0.002423153662254753 -0.013464039022430856; 0.0013101074721040865 -0.0021693481915400817 -0.01013212415381171; 0.0004639367880903761 -0.0003841941174703565 -0.0016403288835353182; -9.642221642160666e-5 8.941228114674571e-5 -0.00021179955409212617; -0.00010171447477787688 -0.0001645243340404029 -0.0010409861769664897; -0.0004953703783901545 -0.00029655509858664123 -0.0010898812938271352; 0.0005894547886017849 0.00011520124065744948 -0.0001347493793548549; -8.706495848316556e-5 0.00013994147794480684 -0.0003469857419499076; -0.00035644392676202944 -0.0005158585007553671 -0.0006752645029387597; 0.0015562818097260163 0.0003760379891465743 0.00021523643501437538] %
+
+Mass Used: 66.07171579131546 kg
+Launch C3: 105.67901788885071 km²/s²
+||V∞_in||: 0.022436585353202827 km/s
diff --git a/archive/ES_0.5850808362794151 b/archive/ES_0.5850808362794151
new file mode 100644
index 0000000..d3bd5ec
--- /dev/null
+++ b/archive/ES_0.5850808362794151
@@ -0,0 +1,22 @@
+archive/ES_0.5850808362794151---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T08:39:17.454
+Launch V∞: [5.324672268139166, -8.277137466371492, -0.7302341936555017] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.6552759612300425e-5, -6.075963158884375e-5, 7.2087086354267955e-6] km/s
+ V∞_out: [-6.104878805603734e-5, 2.3463813956648676e-5, -1.0678005397734148e-5] km/s
+ time of flight: 1.3933517586928e8 seconds
+ arrival date: 2027-09-22T00:52:12.454
+ thrust profile: [0.45577087115632514 -0.26546366537107835 -0.21526323231327674; 0.13783396490232214 -0.0065803602762054695 -0.15188973061477393; 0.08872160843073557 0.014533930056603883 -0.1506491459201571; 0.11019183248607736 0.03315689704963453 -0.23933212750947244; 0.05334512003062379 0.02021282085199927 -0.1455701120695099; 0.0640076698244604 0.028818145347432513 -0.2004781996404627; 0.05141620664373258 0.026897929445930516 -0.17693574432000056; 0.018356693906698637 0.008862001598643452 -0.07689321027654553; 0.024290821398207582 0.013435959413318911 -0.10080179668461187; 0.014279935351283432 0.008962106894630768 -0.06620122563240342; -0.001301847321129298 -4.8864223590451355e-5 -0.003007738218926901; 0.0018789829808020212 0.0010139661770503375 -0.007367733864922527; 0.0019523542525202954 0.0010553470235904047 -0.0029568075569471382; -2.6815400303418146e-5 0.0011698712291662006 -0.001982306184454186; -0.001663040455455408 0.0017283980207935883 0.0021061885350086443; -0.0009849502258006274 -0.0013521206882595757 -0.002470717898360054; 0.0011110678274803612 -0.0008463061036923412 -0.004630780147555258; 0.0004002190771777763 0.0025372532927605412 0.0012235541291393658; 0.0001539991263961975 0.0012903644554102824 0.0022017594658273383; 0.0022761834370725116 0.001209132974140109 0.00560975222889427] %
+
+Mass Used: 114.44875095499037 kg
+Launch C3: 97.39638137788468 km²/s²
+||V∞_in||: 6.669893068131683e-5 km/s
diff --git a/archive/ES_0.5851465956472344 b/archive/ES_0.5851465956472344
new file mode 100644
index 0000000..52ca670
--- /dev/null
+++ b/archive/ES_0.5851465956472344
@@ -0,0 +1,22 @@
+archive/ES_0.5851465956472344---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T09:37:38.193
+Launch V∞: [5.265382657521519, -8.523851314601776, -1.041422052386574] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0020804033348022816, -0.012848224101702128, 0.012801562789578736] km/s
+ V∞_out: [-0.012081211120968242, -0.011525068164554505, -0.007385411516221] km/s
+ time of flight: 1.4400592061862472e8 seconds
+ arrival date: 2027-11-20T03:16:18.193
+ thrust profile: [0.22998666901313314 -0.14902541396442937 -0.1363227739354028; 0.04779879693920396 -0.008375975682808371 -0.06859146407498301; 0.07540112091033067 -0.001392949077047262 -0.17046274888558222; 0.08628390981477328 0.00462995625089262 -0.2605160039087567; 0.0698453578185754 0.006096192944132973 -0.26176407124246814; 0.041821368976035875 0.004114314206205249 -0.18569551103782792; 0.013592497974162416 0.0010141494628886076 -0.06973395766375817; 0.007529535648546422 0.0003395728601995413 -0.04247439075565467; 0.010875769858123597 0.0006354954660491976 -0.06805802257278845; -0.001066609640389401 0.004488203674195161 -0.009026793921275353; 0.0011123175751195215 -0.0015254835850950733 -0.008868271390928202; 0.005646531923320305 -0.002105223112623238 -0.0029369273316609597; -0.00023355021053104988 0.0005463677306586383 0.0003095663641837929; 0.00033771827379020826 -0.0016620347915996781 -0.0029351152158628054; -0.00019175105797298718 0.0007184345601442269 -0.0023796531614183967; 0.006909056198894426 0.006610441141869977 -0.01485421305368669; 0.0035947056921611003 0.002245574850510288 -0.015636113875363122; 0.00044622225113085854 0.0006630898130831567 -0.0012485630576439663; 0.001925298886670579 -0.008492899008814102 -0.005396344427145395; -0.0004467123198917418 -0.009819653146524296 -0.00017895435423313886] %
+
+Mass Used: 90.79270360231749 kg
+Launch C3: 101.46485565476387 km²/s²
+||V∞_in||: 0.01825609351582487 km/s
diff --git a/archive/ES_0.5851555348359743 b/archive/ES_0.5851555348359743
new file mode 100644
index 0000000..80ba3a5
--- /dev/null
+++ b/archive/ES_0.5851555348359743
@@ -0,0 +1,22 @@
+archive/ES_0.5851555348359743---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T16:44:09.415
+Launch V∞: [5.543984822346024, -8.159359204072905, -0.5794912103129193] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9931590090353731e-7, 8.04231998843074e-8, -1.616688342570285e-7] km/s
+ V∞_out: [5.076762365417753e-8, 1.8991076537840808e-7, 1.8472355212069605e-7] km/s
+ time of flight: 1.433338166776757e8 seconds
+ arrival date: 2027-11-06T15:41:05.415
+ thrust profile: [0.3764230021164297 -0.2075363102326892 -0.17084399243739384; 0.13944871562189012 -0.002360265701293058 -0.15613595097517913; 0.091147400457627 0.01821995221626877 -0.16145620435008387; 0.07116694204572173 0.024975898895296087 -0.16435368586042526; 0.06728505054594358 0.03109927339632969 -0.19184149615094706; 0.036891896244635285 0.017021783467762588 -0.11941986322800753; 0.046543520235884504 0.02843903846547537 -0.17783485826342169; 0.019910769321437517 0.011352113811040745 -0.08283275802319744; 0.019122864662558556 0.013683031963324675 -0.08722599832001016; 0.013933391714086061 0.00867541563933366 -0.06925019132479313; 0.02469167656670278 0.018013597409598257 -0.13272548903729398; 0.00039167470538296954 -0.000606888644263268 0.0014795938689004136; -0.0007548192371054205 -5.492970942778707e-5 0.0015582353307683823; -0.005184072849432991 0.0014168880616133946 -0.0006031251056148313; 0.0010863640767900886 -0.0024137754121644935 -0.0005268682986014744; -0.0003337400795044037 -0.0003542936552144388 0.0013032074015825188; -0.0003885657777875375 -0.004491238590845041 -0.007551258367376823; -0.0025717773332726178 0.000838770613534396 0.0012093990618877927; -0.007725855925213881 -0.00029253139160576925 0.005435440605599811; 0.005743391971414278 0.0016568020931949238 0.002814968096546249] %
+
+Mass Used: 113.07558834175688 kg
+Launch C3: 97.64672039432224 km²/s²
+||V∞_in||: 2.689452200777075e-7 km/s
diff --git a/archive/ES_0.5851910255096334 b/archive/ES_0.5851910255096334
new file mode 100644
index 0000000..f4e5ab4
--- /dev/null
+++ b/archive/ES_0.5851910255096334
@@ -0,0 +1,22 @@
+archive/ES_0.5851910255096334---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T07:01:13.033
+Launch V∞: [6.092520453231594, -8.237743089736895, -1.065310727619139] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007747548528841879, 0.003576899223135753, -0.00851706942728192] km/s
+ V∞_out: [0.007858383773936675, 0.0029892950955808023, 0.008649030751120754] km/s
+ time of flight: 1.7708129877207664e8 seconds
+ arrival date: 2028-12-17T20:16:11.033
+ thrust profile: [0.01343138386362536 -0.008655079767215901 -0.009171290640394642; 0.010364992538997019 -0.005908993116905651 -0.024104556825926375; 0.027359569120943318 -0.025180201654265683 -0.11791305733509903; 0.017025172423799376 -0.02172559377403855 -0.10157287860273914; 0.01859719070314952 -0.029794587139660503 -0.13657979674799287; 0.01130597914517879 -0.02031326975619058 -0.09272390871712831; 0.014120756706472668 -0.026247156520417064 -0.12454046431799279; 0.009769468969442969 -0.019993934147057423 -0.09017157590843515; 0.008734665131361214 -0.019512577945804303 -0.08646945497720798; 0.003943501006459424 -0.0077723449801612625 -0.03550652225403761; 0.003115781392621162 -0.0066495519654080504 -0.030106184285836255; 0.00046752333164908153 -0.0015619412499343261 -0.008237290006143176; 0.00045033160549715946 -0.00024163619012709873 -0.00019695844193068747; 1.0694356422877977e-5 -5.1006879187660695e-5 -0.0012847811828370604; 0.00010617541465970945 5.191807464736904e-5 -0.0006489342602647348; 0.0006131363256836819 -5.671220790393617e-5 0.00011859411286997386; -0.00026966851903133043 0.0001727145843439978 -0.0008977604244850205; -0.0005988156718989093 5.748486411870756e-5 -0.0007031536683959031; -0.0001700033179035565 -0.0003750896860997243 0.00042502508000223584; 0.00034275292771669956 -0.0012874792168824883 0.0002544017493287515] %
+
+Mass Used: 63.72392524162569 kg
+Launch C3: 106.11410363193369 km²/s²
+||V∞_in||: 0.01205649981911705 km/s
diff --git a/archive/ES_0.5852282554516601 b/archive/ES_0.5852282554516601
new file mode 100644
index 0000000..0aec680
--- /dev/null
+++ b/archive/ES_0.5852282554516601
@@ -0,0 +1,22 @@
+archive/ES_0.5852282554516601---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T23:31:56.864
+Launch V∞: [8.123014244922107, -5.573593167386492, 0.21573523360156358] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0001404259629409732, -0.0009395485970806483, 0.01673192828679159] km/s
+ V∞_out: [0.00271477814317017, -0.01657157138954197, 0.0001908392152741276] km/s
+ time of flight: 1.8749577787473074e8 seconds
+ arrival date: 2030-04-22T01:41:33.864
+ thrust profile: [0.2744161601013272 0.0010623218259048542 -0.07957455732399155; 0.10144944268997518 0.058069002470691806 -0.09743860903441223; 0.04939797563082563 0.04537157840741775 -0.08551395625724197; 0.033160649800265625 0.03906537898759418 -0.0842259674946067; 0.025029078533457552 0.03697224365487035 -0.08621905726685551; 0.021835938098750344 0.03744544236788991 -0.0984384184568232; 0.008826973736536004 0.013874897628668984 -0.045302752544233285; 0.007415841615444474 0.013402378433440183 -0.039615439243576606; -0.013760021081123484 -0.001386328429050206 -0.01654539002655716; -0.008823654644926265 0.007686417837886268 -0.016296844209218807; 0.013005612810872235 0.01086125657398158 -0.021277900254587725; 0.004264427810344153 0.0077755500436402225 -0.03542486670202241; 0.009123911888290426 -0.0014671557975614417 -0.012810033792732335; -0.03142413456724888 -0.038859099920184506 -0.0417269735904832; -0.04610001203084492 0.07293718619415854 -0.03181144886355448; -0.004476170061211015 -0.002982946078901658 0.00673950969057752; 0.00036715394647918 0.015886598559706422 -0.093579352992069; 0.0016634513927383313 0.02107569495251183 -0.009795223959602998; 0.05738115400418709 0.05113999916599288 -0.04135239292766759; -0.005414790860200796 0.07458128293150633 -0.10140315213632169] %
+
+Mass Used: 116.37971438665863 kg
+Launch C3: 97.09484290976198 km²/s²
+||V∞_in||: 0.016758875117730325 km/s
diff --git a/archive/ES_0.5852302891524188 b/archive/ES_0.5852302891524188
new file mode 100644
index 0000000..6c66dfe
--- /dev/null
+++ b/archive/ES_0.5852302891524188
@@ -0,0 +1,22 @@
+archive/ES_0.5852302891524188---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:47:46.198
+Launch V∞: [7.169628030508947, -7.010365059204245, -0.4076858951089892] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006276685610696598, -0.0022368966953083278, -0.0008839876737136239] km/s
+ V∞_out: [-0.0021703639500043163, -0.0002144588965736618, 0.001192494178941659] km/s
+ time of flight: 1.5740828936688808e8 seconds
+ arrival date: 2029-05-10T14:19:15.198
+ thrust profile: [0.23403626455081816 -0.06983758631340482 -0.11405044385084968; 0.07852665551642934 0.007445341918519602 -0.11097556020611764; 0.02992443494580147 0.006112975115934758 -0.07035370026905328; 0.03304140324242877 0.008065034771130871 -0.1081209431408518; 0.045321489532162036 0.011830483530446271 -0.1841924412604245; 0.06584069887856207 0.013867262262799678 -0.3105211528438787; 0.018139339929388213 0.0037794566503823114 -0.0979718375096634; 0.007361826156318573 0.0013838444807285407 -0.04195571851475729; 0.011858460478031553 0.0018928338779058266 -0.07586201719865351; 0.002935441940916283 -0.0043521145276160895 -0.012075011686537417; 0.004674676983321728 0.0013174837180267285 -0.014367696680476815; 0.0005942919575675674 -0.000965233276012133 -0.005368829439347754; -0.0034812806575690984 0.004515158291303666 0.001558951799932168; 0.0004594303646448419 -0.0009191055678619529 -0.005131130853159459; -0.005925099789173275 0.01064617405837443 0.006330468545702606; -0.018723527114363526 -0.021120041103687603 0.009114237452574687; 0.0011169124372174938 -0.0003658252587193558 0.016641319599067374; -0.02346117739625095 -0.013601971812901341 0.009136923321940837; 0.018412077107499387 0.021284089832742964 0.008995739649105838; 0.00946809148903327 0.008826790041943668 -0.03147319278649591] %
+
+Mass Used: 95.26454981307597 kg
+Launch C3: 100.71499214824217 km²/s²
+||V∞_in||: 0.002485781336987266 km/s
diff --git a/archive/ES_0.5852711481266492 b/archive/ES_0.5852711481266492
new file mode 100644
index 0000000..b372047
--- /dev/null
+++ b/archive/ES_0.5852711481266492
@@ -0,0 +1,22 @@
+archive/ES_0.5852711481266492---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T16:29:44.641
+Launch V∞: [7.726891543579024, -6.789595240791773, 0.14445119472283752] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0014269478827001359, -0.0009040551388469603, 0.00044677837154183007] km/s
+ V∞_out: [4.036453718007818e-6, 7.276284459621588e-6, -4.755551904334882e-6] km/s
+ time of flight: 1.7642346559209853e8 seconds
+ arrival date: 2029-12-24T15:00:49.641
+ thrust profile: [0.029143341731859236 -0.008509129256159719 -0.015620988637133907; 0.04319399252934566 -0.006431187221302353 -0.07835526372597137; 0.02384479323074335 -0.006245165777296808 -0.07020547900201372; 0.024132745270596435 -0.010363827855044007 -0.09224200860981999; 0.03260164848567943 -0.01789279689391221 -0.14808901761456622; 0.02529971470905028 -0.01758927381955604 -0.12893137297085372; 0.0296076504046573 -0.02153455329012083 -0.1560059226277092; 0.016907071778627374 -0.013420044907083716 -0.09173679103711788; 0.007989916763892043 -0.006953123524435683 -0.046532959614896216; 0.006210085775915808 -0.005413299852980462 -0.03615299476258149; 0.0002620396979839813 -0.000305720340854756 -0.0021312548034067113; -9.81241449639259e-5 -0.000713895038455927 -0.00016441999356442627; 0.0005311170667891342 -0.00023549304047180183 -0.0025728059962632065; -2.2059615075193848e-5 0.0010433641243738192 3.0464460136170064e-5; -7.873871814107966e-5 -3.9012345068734165e-5 -0.0019138465332561919; 0.0004122750524483125 0.0002325214577807099 -0.0016742551056517952; 0.00014625354460468033 9.361847873044847e-5 -0.0005316787506374418; -0.00014952084577517536 0.0009234210547999883 -0.00015904523490793565; -0.000380586083010127 -0.00013420073836569986 -0.00075630684980802; -0.0001860062727671106 0.0011452167422078842 0.000226454866353798] %
+
+Mass Used: 65.50779093633628 kg
+Launch C3: 105.82432260767219 km²/s²
+||V∞_in||: 0.0017473141867722492 km/s
diff --git a/archive/ES_0.5852803233506905 b/archive/ES_0.5852803233506905
new file mode 100644
index 0000000..d2d9c36
--- /dev/null
+++ b/archive/ES_0.5852803233506905
@@ -0,0 +1,22 @@
+archive/ES_0.5852803233506905---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:58:46.587
+Launch V∞: [6.886444651179056, -7.12392475231159, -0.9770647948307688] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003755153976226587, -0.005688551658070446, -0.0004858753248510053] km/s
+ V∞_out: [0.0014940132305663431, -0.006497583627756458, 0.0014192068422640507] km/s
+ time of flight: 1.374546178572247e8 seconds
+ arrival date: 2028-09-15T21:49:03.587
+ thrust profile: [0.526157105653939 -0.20137970818448453 -0.23923571076096736; 0.043082115772445334 0.0031757902062799 -0.05825889665108642; 0.07349531428680384 0.017792718738699042 -0.15540504472437353; 0.08310147502775436 0.027461187511563907 -0.2235028344020194; 0.06894233281930508 0.025995565107990372 -0.22963556554223308; 0.024542545571309242 0.011153429482089857 -0.10456522369560571; 0.026983980958230756 0.01216143759997511 -0.12928883401372593; 0.01197912408857134 0.006455989600332709 -0.06578674604307659; 0.006207691111416852 0.003040676980297735 -0.03757081344152543; 0.027468537752260748 0.01026155379040996 -0.163658630690003; 0.007965994448134145 0.0031031870895025654 -0.04765783446379717; 0.0001073271172545824 -0.00014854090627973505 -0.001215240987416025; 0.00032209265651106465 0.00022324789128687255 -0.001162105042521783; 0.000991930320974199 -0.001166664101928362 -0.0010386220077405462; -5.1507216128203144e-5 -6.13622396144622e-5 -0.0011806756474182485; 0.00180921185820494 -0.000926668211940221 -0.00028542930751462143; 7.815188125244712e-5 9.080128635764823e-5 0.0010216276466948823; 0.00019076403255518067 -4.951968426302822e-5 9.129012650178556e-5; -0.0010128654850741744 -0.00012073705025953925 -0.0005945763478003754; -0.0003140422151407219 -0.0013911948870054263 0.0002925518799637932] %
+
+Mass Used: 104.57991393785869 kg
+Launch C3: 99.12807942364805 km²/s²
+||V∞_in||: 0.00683351126310665 km/s
diff --git a/archive/ES_0.5852961099874154 b/archive/ES_0.5852961099874154
new file mode 100644
index 0000000..b580f54
--- /dev/null
+++ b/archive/ES_0.5852961099874154
@@ -0,0 +1,22 @@
+archive/ES_0.5852961099874154---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T23:03:16.093
+Launch V∞: [6.902040436585938, -6.949804315292927, -0.9104556189617435] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0108781320536625, -0.01782422900279045, -0.0013797637914292294] km/s
+ V∞_out: [0.004570486145032777, -0.01995916500011597, 0.004326818353707338] km/s
+ time of flight: 1.3482010353876624e8 seconds
+ arrival date: 2028-08-13T09:04:59.093
+ thrust profile: [0.7181899480105266 -0.25584698981470355 -0.315024465623887; 0.11582938680578019 0.013914668391653002 -0.13776524087764844; 0.08227363719516195 0.027769834874417067 -0.15670363915359617; 0.058364200839103146 0.027419493228515737 -0.15230942003372955; 0.05519437574098582 0.031593480853812146 -0.1783033356155746; 0.056537637231321346 0.03591629511970372 -0.21128455130577925; 0.05723673264530008 0.043473645234818954 -0.2512735876681798; 0.020384513110071896 0.015262619419100338 -0.09925503602286048; 0.010134179282300556 0.007733941307513834 -0.05435397251466765; 0.001313315849195161 0.0008666555627883461 -0.007661474580254139; 0.0019850673026744216 0.0016038405765721004 -0.012326253778462698; 0.00021677924953026378 0.00013784030849748471 -0.0007692927956473; 4.2265495822824844e-5 6.157786888593293e-5 -0.00030021150570966256; 0.00011095233784100958 -3.915548671283598e-5 -0.00036170313827494445; 0.0002566459096403467 -0.00010614103636492848 -0.0004418317779132877; 0.0001542273607561741 1.6348655923449903e-5 -0.0003911605686235276; 0.00013439692969422038 -6.335582880196802e-5 -1.3265385482822992e-5; -3.6043012031450645e-5 7.691518192553425e-5 -0.0003949176687634687; -1.4840176569477911e-5 4.850783802064977e-5 -0.00034177724218558515; -0.00026161815312249486 -5.53373820349608e-5 -0.0005615029625038374] %
+
+Mass Used: 118.37204373313944 kg
+Launch C3: 96.7668716432306 km²/s²
+||V∞_in||: 0.020927031434032274 km/s
diff --git a/archive/ES_0.5853838564576374 b/archive/ES_0.5853838564576374
new file mode 100644
index 0000000..be3e6f5
--- /dev/null
+++ b/archive/ES_0.5853838564576374
@@ -0,0 +1,22 @@
+archive/ES_0.5853838564576374---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T05:12:34.991
+Launch V∞: [6.750713704504415, -7.292269059582717, 0.2357099961661554] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6376641927278243e-9, 1.2344698640374212e-9, 9.094681811035515e-9] km/s
+ V∞_out: [-5.267355312061267e-9, -7.237651213069212e-9, -3.7000810317173003e-9] km/s
+ time of flight: 1.7589594307584354e8 seconds
+ arrival date: 2028-11-15T01:11:37.991
+ thrust profile: [0.21815945248837704 -0.07097073335464232 -0.06011217597948974; 0.21870305637714643 0.05800335336319152 -0.1688751791265909; 0.15829714117734928 0.08838531870159 -0.203469287962189; 0.08492767971319914 0.06594365257041475 -0.15142135747955288; 0.11475935048034137 0.11076326458875174 -0.2580618127654285; 0.028863081278486278 0.03317166958591074 -0.08172097355107795; 0.010189183377053213 0.01338270594501332 -0.034997644861906596; 0.0030556222468187373 0.006503786824232801 -0.0164515083335911; 0.002510237147575226 0.004935374008124959 -0.009054378773609557; 5.708029026070885e-5 -0.0014944963347439245 -0.004975609508234135; 0.0026276237864266035 -0.0036728054538329095 -0.00419932594497419; -0.004945755863840158 0.0023670394982788236 -0.0023419397663144654; -0.0002151831119479844 0.004214614803599779 0.0010074779281482992; 0.0006536350261816578 -0.0016978378360324163 -0.010972772668128537; -0.00025376379108872865 0.003942178237062704 0.00024806539895399875; -0.0013224476097544523 0.0010824614300009334 0.003938899784704646; 0.001419701637955421 0.007496210917783654 0.0041444531542144895; 0.010140542737596948 0.002929780225490302 -0.000130662076548513; 0.0008659586934152878 -0.008094376192059712 -0.0134535510906298; 0.004250193539921988 0.0004067477954298015 -0.0013718773632484295] %
+
+Mass Used: 106.5860164349383 kg
+Launch C3: 98.80488275982376 km²/s²
+||V∞_in||: 9.32304119358805e-9 km/s
diff --git a/archive/ES_0.5854069540880208 b/archive/ES_0.5854069540880208
new file mode 100644
index 0000000..c55104f
--- /dev/null
+++ b/archive/ES_0.5854069540880208
@@ -0,0 +1,22 @@
+archive/ES_0.5854069540880208---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T03:34:58.491
+Launch V∞: [7.203857104359667, -5.950157600945323, 0.1531486974331141] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.756379688541211e-5, -7.511933434006434e-5, -6.20216962282819e-5] km/s
+ V∞_out: [-1.1185683290119766e-5, 8.511872436338681e-5, -0.00010772549396062187] km/s
+ time of flight: 1.7697923528305304e8 seconds
+ arrival date: 2029-12-11T12:28:53.491
+ thrust profile: [0.8621851752821028 -0.01992283383736194 -0.109405464996004; 0.37797275059721924 0.24790493672350056 -0.2035561392402044; 0.15110933703809445 0.17182757078274807 -0.1601276291020514; 0.09189605752447053 0.14807658642976868 -0.1494501117447803; 0.05221520371260537 0.10804076066391419 -0.11819688435350434; 0.03466601717710626 0.09040350367328097 -0.10379174415356307; 0.007675055820416813 0.022025511344540883 -0.02630001727132268; 0.009235907375553786 0.03280862505989651 -0.041586893166528166; 0.0018739796756477725 0.006555655833767352 -0.010045006921519627; 0.0037158510051892545 0.006311092947207933 -0.007790068084024661; 0.0008026748172079859 0.0021044383167203445 -0.002025515999560336; 0.005494152772742896 -0.0025764545497655913 0.002347379469785353; 0.024493127488334685 -0.0035565442879095435 -0.008423788320135418; 0.00012464007157140787 0.008283453142650428 -0.0009379912831221637; -0.010130111515914853 0.003240541642977872 -0.004605078010879804; -0.025464949155808735 -0.01269432166487523 -0.014090359020531355; 0.008163482329492622 -0.008102260138183407 0.0032607449103248904; 0.0023448918526621557 0.00036686345676648514 0.009393395229854254; -0.01683340376827106 0.002893342733745595 -0.01770855416402521; 0.023092723186908137 -0.006409085849414404 -0.02352141014165815] %
+
+Mass Used: 173.58835455475537 kg
+Launch C3: 87.32338717964609 km²/s²
+||V∞_in||: 0.00013787059025559294 km/s
diff --git a/archive/ES_0.5854673303650568 b/archive/ES_0.5854673303650568
new file mode 100644
index 0000000..201c32c
--- /dev/null
+++ b/archive/ES_0.5854673303650568
@@ -0,0 +1,22 @@
+archive/ES_0.5854673303650568---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T21:22:59.666
+Launch V∞: [5.856688476638626, -8.086167882274049, -0.7026837072819238] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0075924820318278565, -0.044524220643748315, 0.06726021804877728] km/s
+ V∞_out: [-0.054784494610594967, -0.05016049216865898, -0.032339628171582674] km/s
+ time of flight: 1.4316522220048943e8 seconds
+ arrival date: 2027-11-02T21:30:01.666
+ thrust profile: [0.16961290664892503 -0.10442887669343622 -0.07712562003689051; 0.1289991689748484 -0.00829902549750792 -0.13538992577502038; 0.12369198241196525 0.01730729857460066 -0.20176633231935356; 0.10730385249186625 0.027726961355929673 -0.23285312228298516; 0.08699052740242762 0.02980288866294427 -0.23168947453877584; 0.06534358226956936 0.026843114715149784 -0.20320591833725807; 0.05068900662663335 0.023514554792848717 -0.1785414895728487; 0.02776215671770824 0.014441705939326598 -0.10801793255872061; 0.00993088704803799 0.005735184558891147 -0.04222588236484243; 0.0010722713686752497 -0.0003205009020796674 -0.004614192795679777; 0.0013346294399933546 0.0005022544123065443 -0.003250269150542311; 0.0005585928574213727 -0.0003960114578618225 -0.0005685278284498149; 0.0002725508388941 -0.0003989902720176802 0.0001900280741167549; -0.00042050974079149445 0.0006087977145326264 -0.0017692248917807033; -0.0002734260453417462 0.00036737276102517526 -0.0023843645131706864; 0.0012694023535933965 -0.0016008408957967606 0.0016039210251962196; -0.0023339540708737683 -0.0003004046742325294 0.0015170031273755349; -0.0002369793719273712 -0.0008159345567566204 0.0030958677267937536; -0.0001758387277642687 0.0016351504580164088 -0.0013628830651221304; -0.0007100276704026113 -0.0001165823717712955 0.002046088552766602] %
+
+Mass Used: 98.65794602894903 kg
+Launch C3: 100.18067532519152 km²/s²
+||V∞_in||: 0.0810184481418021 km/s
diff --git a/archive/ES_0.5854947559934834 b/archive/ES_0.5854947559934834
new file mode 100644
index 0000000..268c15e
--- /dev/null
+++ b/archive/ES_0.5854947559934834
@@ -0,0 +1,22 @@
+archive/ES_0.5854947559934834---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T15:25:53.191
+Launch V∞: [5.2830929412952505, -8.22262880828009, -0.6449580878713865] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00048762898521608665, 0.0002198589792195527, -0.000403914372836684] km/s
+ V∞_out: [-0.0001935374088728506, 0.0004698621811953779, 0.00043708377612935745] km/s
+ time of flight: 1.383563615446518e8 seconds
+ arrival date: 2027-09-09T23:45:14.191
+ thrust profile: [0.5421901088484485 -0.341447777663755 -0.26614890464039087; 0.19022585103104744 -0.016567882705879777 -0.2100405511314549; 0.11641049690450704 0.014171873018417805 -0.19856926730337518; 0.13963881016746207 0.03350068323028438 -0.3109683917196301; 0.07291735940940254 0.023903680427298898 -0.20075483459821716; 0.051349830666042484 0.019807221631921883 -0.16415746917789983; 0.04959269230579655 0.02113932669771142 -0.17732855522232865; 0.004386724952462449 0.002034277634025488 -0.016449203057513927; 0.006008390860169128 0.0029734788363884827 -0.02567901296793384; 0.0018507425608604655 0.0009046704871314708 -0.0068778697387564276; -0.0005030384177829514 -0.0009585969317809986 -0.005217155550941467; 0.003160421958723361 0.0003339902326476448 -0.004709747956294958; -0.001730584992118759 0.0007844115325824009 -0.00517356319246973; 0.002385120455777553 -0.0005022189047193108 -0.0009764898268317963; -0.0034536507635257573 1.640002616075533e-6 -0.0032018137763031914; -0.005456268015187223 0.0005459617971283197 -0.0007515592933985699; 0.0008883332874296181 0.0012375746525422875 -3.453092919454299e-5; -0.006404419549950791 -0.0010498766739082737 0.0012967746374861321; 0.0018322088840616332 0.01346613423479847 0.008894123899855323; -0.010810082845752404 0.0010667566802633705 0.004220969174367071] %
+
+Mass Used: 123.43499419104364 kg
+Launch C3: 95.93866648023207 km²/s²
+||V∞_in||: 0.0006702736892869851 km/s
diff --git a/archive/ES_0.5855101811287566 b/archive/ES_0.5855101811287566
new file mode 100644
index 0000000..5e7aa24
--- /dev/null
+++ b/archive/ES_0.5855101811287566
@@ -0,0 +1,22 @@
+archive/ES_0.5855101811287566---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T09:09:22.258
+Launch V∞: [5.297744932836332, -8.252716886134142, -0.6467059690216442] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005555976288777734, 0.0002535123955974307, -0.0004584158045270107] km/s
+ V∞_out: [-0.00023741496169930095, 0.0005573198832827357, 0.00046492474988708436] km/s
+ time of flight: 1.3714639651973343e8 seconds
+ arrival date: 2027-08-26T17:22:38.258
+ thrust profile: [0.4845536325076008 -0.2998099601976581 -0.23364910133699965; 0.22002947133736042 -0.016791822931597485 -0.2355462862124501; 0.12410317481305899 0.016784739239712222 -0.20449531003237958; 0.12343416021622268 0.0322619681101506 -0.2650701173689392; 0.06608890887473269 0.022997494290493126 -0.17551655380520317; 0.09190054159010898 0.03820009274058684 -0.27855586652709163; 0.03530821281696002 0.01622933282950216 -0.12356437298285365; 0.01180943496230803 0.006350898831551192 -0.047498473781181605; 0.0044249163592949645 0.002719433889639034 -0.021627811186400222; 0.0019012320725275609 0.0011303715646594533 -0.008853264853426008; -0.00011731026428541639 -3.288523526363257e-5 -0.00013477510801393564; -0.000150861315037959 -2.5019061187875525e-5 0.0005321062015885557; -0.0018996956800738929 8.021890570723149e-5 -0.0015453350470471699; 0.00021095696008452733 -0.0008901746683634395 -0.0009054272155378575; -0.000494067482193535 -0.0004942853292093904 0.0016875492770491696; -0.0006489962428183916 -0.0010416997259807739 0.0021725657375384526; 0.0032871640917828304 -0.0003486079393929872 -8.292557767922951e-5; 0.002206057525195616 -0.0024481306143705633 -0.00024277545173035644; 0.00043456970150137597 0.0016926409203308374 0.0011686318143347449; -0.0025127937735805453 0.0011063677274079948 -0.005067182565764685] %
+
+Mass Used: 119.64382639595442 kg
+Launch C3: 96.59166598644485 km²/s²
+||V∞_in||: 0.0007636113604290463 km/s
diff --git a/archive/ES_0.5855309311091853 b/archive/ES_0.5855309311091853
new file mode 100644
index 0000000..184244f
--- /dev/null
+++ b/archive/ES_0.5855309311091853
@@ -0,0 +1,22 @@
+archive/ES_0.5855309311091853---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T15:51:09.022
+Launch V∞: [5.479344727520746, -8.138904231884458, -0.48218346246359345] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5760155576489843e-5, 0.013323677899314197, -0.004377458506290019] km/s
+ V∞_out: [-0.009212596676283484, -0.007881018493196255, 0.007050326223178087] km/s
+ time of flight: 1.4878418309811616e8 seconds
+ arrival date: 2028-01-10T16:47:32.022
+ thrust profile: [0.41552152388380353 -0.2313534610447309 -0.19214024492224263; 0.07483069768870301 -0.003012640139587212 -0.08217456177697818; 0.09625816648622128 0.015072430274636318 -0.16821148312476972; 0.13932188458476844 0.03686714699641414 -0.33126919766231994; 0.07477247411101051 0.026019393257905893 -0.21576312981463522; 0.05541711324445222 0.02250341475697751 -0.18689820238141885; 0.02429690130623498 0.011152570676988063 -0.09232422416864554; 0.0088558122697708 0.00550719065291755 -0.038691039740758604; 0.0066666715583907485 -0.002256021257568146 -0.010753158165107746; -0.0004596745823283125 -0.0026806807426638895 -0.01148728384789247; 0.006704378627640053 -0.0006805345264217998 -0.012462392655583996; -0.002758180761211448 0.006167049640951038 -0.0014522635203642227; 0.010787856064087322 0.010848135345961985 -0.03019021561652897; -0.006510256733051081 0.0012021535900102421 -0.019869153224332647; -0.0033424805510258067 -0.023535669352500108 -0.019050885880465655; -0.014568885788917624 -0.02455654644646521 -0.01622771211820963; 0.017519044736562808 0.022102134393338538 -0.005106159326579376; -0.0021047483479732995 -0.001678732622751664 0.011166408325437424; -0.016516012959570135 -0.005605984282770111 0.026381314412775234; -0.012221654169798245 0.025383586532085965 0.04317440876982496] %
+
+Mass Used: 120.2174434508106 kg
+Launch C3: 96.49748163026952 km²/s²
+||V∞_in||: 0.014024378750040223 km/s
diff --git a/archive/ES_0.5855361487178694 b/archive/ES_0.5855361487178694
new file mode 100644
index 0000000..54b6d77
--- /dev/null
+++ b/archive/ES_0.5855361487178694
@@ -0,0 +1,22 @@
+archive/ES_0.5855361487178694---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T11:01:20.988
+Launch V∞: [5.197563310138749, -8.1691374129181, -0.5415831960616811] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.26495035511287e-7, 4.0687609133117883e-7, 4.654034529595424e-6] km/s
+ V∞_out: [-3.211418591728938e-6, -3.1575336703793765e-6, -1.4819683807518532e-6] km/s
+ time of flight: 1.3914845858285686e8 seconds
+ arrival date: 2027-09-18T23:22:18.988
+ thrust profile: [0.6834270819477122 -0.4197349306476915 -0.322469993475215; 0.2221008399054511 -0.01710504958710124 -0.24536963211812937; 0.14028568175496856 0.018276569007301603 -0.240303528593865; 0.10626631705164367 0.026662558872622935 -0.24110207179105708; 0.08249348171108255 0.027544288776074365 -0.22904463063265784; 0.03831448413228602 0.01529571456306112 -0.12649638695279447; 0.037957240277999876 0.01623617523771914 -0.13945383607372006; 0.013849374133884073 0.006994908722045767 -0.05825318668871531; 0.0034676996914662257 0.00082858377424895 -0.01734414459511392; -0.0027943095824628445 0.004236960827880304 -0.020460220717757938; 0.0015178512245032551 0.0009610854071813447 -0.007461362481344437; -0.0003010064520411182 -4.0538657241891984e-5 0.002673662066017467; 0.001567569483852849 0.0007715056007407896 0.00269213074878111; 0.0015018175482064899 0.0006543741174526172 -0.0006526584177383573; -0.0027312608669192145 -0.0014129788885499973 0.005766156792939646; -0.012810550935223566 -0.006550873201625023 0.006249979592377966; 0.006954673880854486 0.002082375477717815 0.0019521760977204154; 0.0009749489746953858 -0.001468889453921894 -0.004173392661182343; 0.00536620185507384 -0.0012762848774890336 0.007553325527997542; -0.001085594399897412 -0.0005346924788920959 -0.007094251950186812] %
+
+Mass Used: 134.54260721579294 kg
+Launch C3: 94.04278279229509 km²/s²
+||V∞_in||: 4.713606006645415e-6 km/s
diff --git a/archive/ES_0.5855869779204634 b/archive/ES_0.5855869779204634
new file mode 100644
index 0000000..e28b341
--- /dev/null
+++ b/archive/ES_0.5855869779204634
@@ -0,0 +1,22 @@
+archive/ES_0.5855869779204634---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T05:44:32.285
+Launch V∞: [5.28133513121894, -8.530203980144364, -1.1156868372482447] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.3193003859584796e-5, 2.0776572289880076e-5, -3.718415785503794e-5] km/s
+ V∞_out: [-1.8453017836534405e-5, 4.3158416688718566e-5, 3.842994023486839e-5] km/s
+ time of flight: 1.40174146872957e8 seconds
+ arrival date: 2027-10-05T15:00:18.285
+ thrust profile: [0.198383624040361 -0.13311011665335468 -0.11865137673744817; 0.07211574138084743 -0.012654461978339972 -0.09798012610720785; 0.09092668112344864 -0.0015792418974509542 -0.1951762296039883; 0.0939037469575908 0.0054987281672764935 -0.2708618808334655; 0.0736931275884019 0.007248241244602308 -0.2621854307600669; 0.04394035796853016 0.00523584775098408 -0.18291316722746484; 0.016328851407064932 0.0023953838723619753 -0.07619790638855314; 0.01670224474544129 0.002311905362139431 -0.0858646507869481; 0.0022068146922249576 0.00041280120175877903 -0.013241722957644173; 0.00039213755443650916 -9.510329431301865e-5 -0.012708624177159327; 0.0010561944142773515 0.0003265463005888811 -0.007262680227373574; 0.0008461763420073017 -0.00019379202306819945 -0.003485576857246967; 0.0006192695947283248 0.0004783469395142953 -0.003996695644140921; -0.006105652838847213 -0.0014096326128371732 -0.00195464752296305; -0.0016928423481935547 -0.0018812044343647582 -0.0035766545546529766; -0.0016653752514212508 -0.0006787531595290317 0.00013722940263821617; -0.0016504788609823019 0.002058181423664096 -0.00658513413156702; -0.0032879355807534337 0.002152640890052143 0.0050616681994976424; -0.00030970694746274723 0.00041616534813800586 0.0008996917208219891; 0.0011456206549556262 0.002756595856367476 -0.003419822227731486] %
+
+Mass Used: 88.75858689929919 kg
+Launch C3: 101.90163782992713 km²/s²
+||V∞_in||: 6.066269969197794e-5 km/s
diff --git a/archive/ES_0.585589874603734 b/archive/ES_0.585589874603734
new file mode 100644
index 0000000..5e9dd10
--- /dev/null
+++ b/archive/ES_0.585589874603734
@@ -0,0 +1,22 @@
+archive/ES_0.585589874603734---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T11:22:11.692
+Launch V∞: [5.20166410618111, -8.31597682119166, -0.6457453074927706] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0003478066979934746, 0.00017283553071660392, -0.0003425853192837624] km/s
+ V∞_out: [-0.00017570244983548708, 0.00034816352024182257, 0.0003407251731312561] km/s
+ time of flight: 1.379736396033645e8 seconds
+ arrival date: 2027-09-05T09:22:50.692
+ thrust profile: [0.3760703651760788 -0.21223550745701455 -0.16484563449832867; 0.26137981399205346 -0.006570589088953146 -0.247170944522638; 0.22744021055465172 0.04716115839127187 -0.32055709967735724; 0.1805664360436198 0.06305964990205475 -0.3331483888603231; 0.08211007173893069 0.035869567925314025 -0.19509967064206304; 0.05119342734436428 0.025452977295771347 -0.14215406504882672; 0.024485231397602412 0.014224948871261541 -0.07995401377824086; 0.013445762490951432 0.008324110545372855 -0.04897942818471615; 0.0025503438518060264 0.0029558853305026154 -0.013790269704600287; 0.0006522101933919286 0.0010951489883565338 -0.0030270921463284323; 0.002089337595814031 0.0035656867485715613 -0.012499366372399488; -0.0012933473136756022 -0.003709992559421056 0.00015551952759522382; -0.0005108916099957007 -0.002290376157012575 0.001694080309534551; -0.001635281240281098 0.0011702850164451502 0.004190871813565002; -0.007012679815413923 -0.0025935247698990857 0.001677389294415112; 0.00027652170633005456 0.0006634010950795385 0.0004346188587493593; -0.0016963166390311735 -0.0010209808791570543 0.005982040850731132; -0.0036919108227371307 0.0037235494284369244 0.006519834536654459; 0.0011053596104937558 0.0009737229273410542 -0.0015992546062328728; -0.0011373418212891034 0.00021597964362433963 -0.0010115685894533416] %
+
+Mass Used: 119.5145464010634 kg
+Launch C3: 96.6297669662788 km²/s²
+||V∞_in||: 0.0005178863976162838 km/s
diff --git a/archive/ES_0.5856614147301125 b/archive/ES_0.5856614147301125
new file mode 100644
index 0000000..5b61f7f
--- /dev/null
+++ b/archive/ES_0.5856614147301125
@@ -0,0 +1,22 @@
+archive/ES_0.5856614147301125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T02:41:28.401
+Launch V∞: [6.1876952936576, -7.593410349821977, -0.005720720471904409] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8783762828154024e-8, 5.7983900647317494e-8, 3.0599939496122e-8] km/s
+ V∞_out: [-1.827444091680065e-8, 4.144319602121436e-8, -5.6311822041681146e-8] km/s
+ time of flight: 1.638270395218995e8 seconds
+ arrival date: 2028-06-26T06:12:07.401
+ thrust profile: [0.31835443397168045 -0.1252761307564233 -0.09214472238900961; 0.33321859633394596 0.0653757138834635 -0.2451321307421011; 0.20945104131480768 0.10117308480929264 -0.24944380027574073; 0.14303850122673012 0.09845107557621989 -0.23155598140182812; 0.08663814486051899 0.07345140352085934 -0.17653930137428855; 0.049722805170905604 0.04861568932975814 -0.12127805241265763; 0.015703423690062782 0.018267885421033917 -0.047028465779013796; 0.0033541717192753172 0.003901303162170431 -0.010523717816217405; 0.0016319292364258928 0.004592632199268019 -0.010601795890217708; 0.003960410108211202 0.005005119427653436 -0.01622853289159059; 0.003410581775039952 -0.0003387585208588957 -0.003622765892616864; 0.0005147165547763975 0.0017116823858772407 -0.0009349875247199851; 0.001562340615831671 0.0019792375968015795 -0.005906240960311451; 0.0005444023163836553 0.00036715943258226573 0.0022664982145906105; -0.000947272549598231 -0.0010339516497535704 0.0027433236137959735; 0.0002963001813633931 0.0011495037225646588 -0.0027559883172173683; -0.0015574344581705233 -0.004705655626344944 -0.0008871540019549844; 0.0007235450605335666 -0.0020859057592490134 0.0015391233618292947; -0.0014890068051372145 0.008657785900783574 0.0014533774929295037; 0.00177082150664492 0.0013468673176803808 -0.008588163131504574] %
+
+Mass Used: 123.57797918342249 kg
+Launch C3: 95.94748651457864 km²/s²
+||V∞_in||: 7.160303089947892e-8 km/s
diff --git a/archive/ES_0.5856833879551792 b/archive/ES_0.5856833879551792
new file mode 100644
index 0000000..210a164
--- /dev/null
+++ b/archive/ES_0.5856833879551792
@@ -0,0 +1,22 @@
+archive/ES_0.5856833879551792---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T14:39:50.886
+Launch V∞: [7.083103108920234, -7.036646890567586, -0.782867770879004] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.191951863101544e-7, -1.072325319046507e-6, -6.023232247282941e-7] km/s
+ V∞_out: [-1.0103571573677101e-6, 7.929894530389316e-7, 4.640099110597637e-7] km/s
+ time of flight: 1.3806186591163245e8 seconds
+ arrival date: 2028-09-21T13:10:55.886
+ thrust profile: [0.2515332108002227 -0.0901585482558572 -0.12243734171605632; 0.1072355632194432 0.011576009153383254 -0.13110008836697584; 0.1080788898953615 0.03345591906177744 -0.21186769229787678; 0.09430333895861948 0.040430249543781084 -0.25053025508296806; 0.06660137887305441 0.0339076681113679 -0.22129196481736535; 0.040423663537266286 0.022703737705303026 -0.1595025082213809; 0.023597551751574946 0.014036899264840075 -0.1064816047296549; 0.02214114469294878 0.013821714881137887 -0.11108999376264633; 0.010317095709006133 0.006646415714526148 -0.0567696843421143; -0.0009817291012388456 -0.0008093801610538143 -0.0025570860169846577; 0.006869502518266343 0.004472544366015247 -0.04140393656249353; -0.001679745545305562 0.0015005952004748233 -0.01224906152985009; 9.204855847425714e-5 0.00013947984612106592 -0.008567921835494503; -0.00012529759457044444 0.0008998514188365117 0.000190597870081256; 0.010458266989329655 0.001593238910048464 0.003693067887181706; 0.0002537319486286015 -0.00024212943242198594 0.0036162518986100406; 0.0015434875958848047 -0.0014600032910639497 -0.005032104910198947; 0.01147364312387361 -0.0003757249584638358 -0.005912491284353031; 0.00033837231401791495 0.0012838279677246294 0.009631171264108767; 0.01255725119112288 -0.016044977977632036 -0.0007662779181030121] %
+
+Mass Used: 98.22777142631139 kg
+Launch C3: 100.29763106081103 km²/s²
+||V∞_in||: 1.2993842623107642e-6 km/s
diff --git a/archive/ES_0.58571882148881 b/archive/ES_0.58571882148881
new file mode 100644
index 0000000..aadb135
--- /dev/null
+++ b/archive/ES_0.58571882148881
@@ -0,0 +1,22 @@
+archive/ES_0.58571882148881---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T01:08:00.134
+Launch V∞: [5.3520335789721685, -8.395663748868325, -0.8284611505699448] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0001325563942180895, 0.00029799559258193037, -4.52357448240095e-5] km/s
+ V∞_out: [0.0003014098692256144, -0.00010371089876367578, 5.262109900389394e-5] km/s
+ time of flight: 1.3720053970816663e8 seconds
+ arrival date: 2027-08-29T00:23:39.134
+ thrust profile: [0.25768751233725246 -0.16099589693362004 -0.1343570501788042; 0.14726291359812813 -0.013974787559628169 -0.16976778684064442; 0.09113501084245325 0.009342729272119812 -0.1629030429008655; 0.16036355433747917 0.036405954544376506 -0.3586019782162702; 0.0762354524266405 0.022572496525335918 -0.21575590264716268; 0.06141807434983343 0.02137733441833797 -0.20271471460792204; 0.032738784104667545 0.012687212544639243 -0.12486857705843195; 0.00906650063817782 0.0036399227041161884 -0.0394026829180677; 0.00889550874917758 0.003745987612640092 -0.04176324373422952; 0.002764675643073128 0.0014746432385411739 -0.01550370260027053; -0.00020654965364313473 0.0010326728911784658 -0.0022019300284423886; 0.0019510239896230362 0.0008654478743051788 -0.010965320532861445; 0.00137446956623129 8.638698679190114e-5 -0.0032123983642962013; 0.001285198876773174 0.001839625629564399 -0.0010009031352108768; 0.00024867487220303934 0.002480149548977819 -0.0009187560583253525; 0.00025047591263086097 0.00015527864503113117 -0.0016538566205305033; 0.00042408091925779734 0.002944687515888658 -0.0006049553524603206; 0.0005699464626612611 0.0004620560878074579 -0.00020989584209205612; 0.00088398675794398 0.0016629172966440195 0.005317770285667235; -0.0033798453884718877 -0.0025011787297730646 0.004308242121828903] %
+
+Mass Used: 101.06823536396405 kg
+Launch C3: 99.81778109251104 km²/s²
+||V∞_in||: 0.00032927016788063306 km/s
diff --git a/archive/ES_0.5857221940878403 b/archive/ES_0.5857221940878403
new file mode 100644
index 0000000..6598719
--- /dev/null
+++ b/archive/ES_0.5857221940878403
@@ -0,0 +1,22 @@
+archive/ES_0.5857221940878403---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T10:58:51.971
+Launch V∞: [5.2878110715706725, -8.18964528169801, -0.4596393686208779] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6562630345097145e-5, -4.014263452433237e-6, 4.712398174437548e-6] km/s
+ V∞_out: [-1.5901082647170455e-5, 7.116254073739491e-6, -3.0206934295100044e-6] km/s
+ time of flight: 1.367786270845341e8 seconds
+ arrival date: 2027-08-21T13:02:38.971
+ thrust profile: [0.6299963743079998 -0.3692612788355339 -0.27045983345436736; 0.15871765448036831 -0.010229463619323477 -0.16878673799016705; 0.17070771286969288 0.026667933416424223 -0.27089488124422956; 0.132477873202106 0.038062582036203774 -0.27759441885093317; 0.07965023486453392 0.029147457255083917 -0.2039380277645287; 0.07156011420770783 0.03259350358441856 -0.21575525037848872; 0.05152785106517228 0.026837084102749816 -0.17570599692843616; 0.005228694603790373 0.0027435595695320903 -0.020074339352091325; 0.006306630723724357 0.0035624440642287015 -0.026220475893778676; 0.0009552678737993534 0.000735670932862776 -0.005756476684502978; -0.0002632723216880808 -1.662739278238923e-5 -0.000535370226856605; 0.001093181363815783 0.0008381857790621 -0.005055325538322193; -0.00016275124510778527 0.0005547136157355 -0.0007698492047847714; 0.0013742420448173951 -0.0003167620267998892 -0.001206143780690513; -0.0001758042405186887 0.00010233162905597133 4.247633822238698e-5; 0.0003587065775220239 0.0002500456129680477 0.0008292361145656123; 0.00036574259954789745 0.0002192100807091894 0.0003494044004807097; 0.00022738962690489802 -0.0002649514750065942 -0.0013376156134396848; 0.0004481050703518244 -0.00047311212754424815 -0.001186044032570633; -0.00034362786393204764 -0.00020062137240567162 0.0011952728152480451] %
+
+Mass Used: 127.76128574835502 kg
+Launch C3: 95.24250411785006 km²/s²
+||V∞_in||: 1.7681677849353446e-5 km/s
diff --git a/archive/ES_0.585733911854561 b/archive/ES_0.585733911854561
new file mode 100644
index 0000000..9854532
--- /dev/null
+++ b/archive/ES_0.585733911854561
@@ -0,0 +1,22 @@
+archive/ES_0.585733911854561---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T01:39:24.355
+Launch V∞: [6.930988639707802, -7.047052015188235, -0.3162896376437397] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0019803160967085333, 0.0015515535972811935, -0.0010535268178715116] km/s
+ V∞_out: [-0.0011919039433967665, 0.0024460826702535176, -0.00010946493698168348] km/s
+ time of flight: 1.3738791506007054e8 seconds
+ arrival date: 2028-09-13T04:57:59.355
+ thrust profile: [0.36580804326882527 -0.13229839871934204 -0.16494406164469583; 0.27105502780612084 0.028469017604482262 -0.30320397340686067; 0.12538480195123097 0.03790014216752889 -0.23237176617850047; 0.09914161224878307 0.041496669128892084 -0.24885977117256414; 0.07134487225581192 0.035656107203334494 -0.22374858470766287; 0.03169421876019095 0.017136149706644704 -0.12241383541578697; 0.026842969547555034 0.015232121109010894 -0.11800383247442069; 0.009028693023700886 0.004127001786061946 -0.043577431931159774; 0.008078299766418573 0.003493410201926607 -0.04442619906235195; 0.004527495832434544 0.004045919379734808 -0.027891384212336664; 0.006198957768345317 0.0018534510419850978 -0.03869455200730842; 0.0016141107076485537 0.0004246983665049289 -0.0051710285313674815; 0.0028589939640266283 -0.00037684908287846116 0.0013774451819655933; -0.0040290993860074235 0.005229363000326665 0.0007437624722770812; 0.001595491853946316 -0.00047028489764993476 -0.002608474653617586; -0.0008010415730501891 0.008306173220564487 -0.0012276851537911491; -0.005345478269815781 0.0008743615902976924 -0.008671767423996732; -0.000451414721329587 -0.0005824838992406307 -0.002823591713760092; -0.003774916837607247 0.0027774058026928854 0.0031130314046154337; -0.0003892261472351453 7.470079451042066e-5 -0.0044760838928231865] %
+
+Mass Used: 112.85865271044122 kg
+Launch C3: 97.79958476340799 km²/s²
+||V∞_in||: 0.0027274327056947905 km/s
diff --git a/archive/ES_0.5857402350910488 b/archive/ES_0.5857402350910488
new file mode 100644
index 0000000..162ad4e
--- /dev/null
+++ b/archive/ES_0.5857402350910488
@@ -0,0 +1,22 @@
+archive/ES_0.5857402350910488---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T04:19:21.879
+Launch V∞: [7.0336895840607125, -7.140316373064522, -1.1014210984522943] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001767986668361346, -0.010255071632496515, -0.010354435857055335] km/s
+ V∞_out: [-0.013102076487306102, -0.0014486452108213477, 0.006522391555596863] km/s
+ time of flight: 1.3508728924244887e8 seconds
+ arrival date: 2028-08-18T16:34:10.879
+ thrust profile: [0.25234193560836515 -0.09923932129309335 -0.12998133461951736; 0.08730533045221095 0.0052760267147638545 -0.11008735586625441; 0.09481264323533549 0.02307730355980579 -0.1922293236264007; 0.08729509621650035 0.03018584793118997 -0.24005984716617695; 0.09231072716522187 0.03802831412759585 -0.3136332991585055; 0.05124024758562479 0.02314112041607643 -0.20636489203508868; 0.023392717142520943 0.010775653328759677 -0.10656926816150053; 0.007453881457005219 0.003906853782986809 -0.03946559666076687; 0.001752050799387213 0.0004368047231949208 -0.022012004672477752; 0.00284038392485181 -0.00045751535773871005 -0.015617067109577543; 0.0004396095552531768 9.075541417476402e-5 -0.0044374490595968765; 0.0005774577819362883 0.0004269222957302268 -0.004725012006628277; 0.0012284524192219199 0.000494217744131776 0.0007076901915737416; -0.0019309995488982486 0.0037272995548116496 -0.0014747530788319356; -0.004398356826056252 -0.0001701990321460792 -0.0004529597832389279; -0.0005568803073753747 0.003376479628554669 2.1677059920763883e-5; 0.0008757873820567439 0.0006223201347950989 -0.0003292889363419888; -0.004191146592122074 5.228833951420219e-5 0.00021148291104048972; 9.406562947620914e-5 -0.00023898407326223908 -0.0006021972612706874; 0.002400162851577539 -0.0006401898269819853 -0.003664108374455369] %
+
+Mass Used: 90.28840047334597 kg
+Launch C3: 101.6700355084933 km²/s²
+||V∞_in||: 0.0146801434926574 km/s
diff --git a/archive/ES_0.5857598853874391 b/archive/ES_0.5857598853874391
new file mode 100644
index 0000000..4426959
--- /dev/null
+++ b/archive/ES_0.5857598853874391
@@ -0,0 +1,22 @@
+archive/ES_0.5857598853874391---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T20:54:50.642
+Launch V∞: [5.36687670343982, -8.280674551760992, -0.892384289060717] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.347182064815168e-5, -5.0838659211559744e-6, 6.062594019514203e-6] km/s
+ V∞_out: [-2.285890671847028e-5, 8.610353254260532e-6, -4.115708215435735e-6] km/s
+ time of flight: 1.384341124592649e8 seconds
+ arrival date: 2027-09-11T02:50:02.642
+ thrust profile: [0.356388326790828 -0.21528612953292248 -0.17855877363640704; 0.18213811893739157 -0.011458752440323112 -0.20338806287734254; 0.1544422917732652 0.02374113346343128 -0.26226304575234904; 0.12373588971517258 0.03505340164598111 -0.27711507836801397; 0.08259322167351814 0.030682425858442556 -0.22844262942736468; 0.04458705663974611 0.0195393610186798 -0.14589940045892502; 0.021386846075042314 0.010173976626289646 -0.08107023436039637; 0.014541024721858229 0.007684709013680933 -0.06444341235983055; 0.008724160470754588 0.008237882427213475 -0.04266503857421873; 0.0003242580677784443 -0.0003980594235443735 -0.005176856558472446; 0.003785421680084526 0.0022406558485675958 -0.016799679702627593; 0.001039643433454346 -0.003374127173684224 -0.003179928174297155; 0.0008310260827389192 -0.001953437302986112 -0.0013317338700678549; 0.0010422102725390803 0.004703838607231311 0.0007220491526137764; 0.0008505255964001969 -0.002770242070182849 -0.0005635406178883674; 0.0005105256252535741 -0.001946337973098418 -0.004039788152245006; 0.002718177322291718 0.011354064183750442 0.00223502081240128; -0.0018198776261322278 -0.0010370984479911344 -0.007866587086856634; -0.000666580774291407 0.0006047003408471455 -0.004414732646243858; 0.007718363112470187 0.0037328746774758317 -0.00704100657106773] %
+
+Mass Used: 110.7323628601066 kg
+Launch C3: 98.16928630146955 km²/s²
+||V∞_in||: 2.4769479273669443e-5 km/s
diff --git a/archive/ES_0.5859516773868749 b/archive/ES_0.5859516773868749
new file mode 100644
index 0000000..e509970
--- /dev/null
+++ b/archive/ES_0.5859516773868749
@@ -0,0 +1,22 @@
+archive/ES_0.5859516773868749---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T23:38:49.112
+Launch V∞: [5.446573880621776, -8.592197281296398, -0.6754715561300401] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005091201406075148, -0.00023841056598501432, 0.0004233967208250639] km/s
+ V∞_out: [0.00020049988629962408, -0.0005395309670600524, -0.00040537044039063705] km/s
+ time of flight: 1.561933381380242e8 seconds
+ arrival date: 2028-04-13T18:41:07.112
+ thrust profile: [0.04420610814391255 -0.025829916912270476 -0.02897337699082828; 0.03567435078977178 -0.006339286775918131 -0.06218607210062825; 0.05868468634662061 -0.00445757144337131 -0.15310466941446046; 0.042047429407748846 -0.00037020331983928173 -0.14730338966118983; 0.04107184833404949 4.911222850909126e-5 -0.1813250129073439; 0.022079156945478098 -0.0017030385645195691 -0.11359628465684742; 0.019269433257398876 -0.0023528533051154024 -0.10697774578205148; 0.00977097601852312 -0.0028844441729712006 -0.07380933936750741; 0.03166147391467055 0.002206445832335043 -0.2034245549135355; 0.0027868185217649233 -0.0005954565851155829 -0.021240490773499255; 0.007482525159860796 -0.0008487851844483001 -0.052372626146008246; 0.0006802411199213213 -0.00039849430953234203 -0.006728665368860448; -0.0008192138939664589 -0.0006108336807108951 -0.0017078739598391643; -0.000945177907936118 -0.0004783982551335186 5.630573248702718e-5; -0.0017479479712163735 -0.00010956072969545844 0.0010933658823035295; -0.00031263497160684967 -0.0023605703594535158 4.7087374820037765e-5; 0.0002584462773446228 -0.0004649327605618555 0.0003933108780371586; -0.000584123151291463 0.0015860494031610121 -0.006454341031361903; 0.0009326172528966127 0.0027094012749977856 0.0002522097911309548; 0.0038329419393360233 -0.0015704436554435227 0.0016893017649095158] %
+
+Mass Used: 77.25113956259975 kg
+Launch C3: 103.94728298092932 km²/s²
+||V∞_in||: 0.0007037810019820993 km/s
diff --git a/archive/ES_0.5859887345424953 b/archive/ES_0.5859887345424953
new file mode 100644
index 0000000..eee7aa4
--- /dev/null
+++ b/archive/ES_0.5859887345424953
@@ -0,0 +1,22 @@
+archive/ES_0.5859887345424953---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:18:35.702
+Launch V∞: [6.968139874180042, -7.170507979651499, -0.7768056810368565] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001302282912571322, 0.0010494841342642582, -0.0006995919124101446] km/s
+ V∞_out: [-0.0008027688239114246, 0.0016236222899405225, -7.565489457992768e-5] km/s
+ time of flight: 1.358892983276911e8 seconds
+ arrival date: 2028-08-28T11:20:13.702
+ thrust profile: [0.3280436939954187 -0.12395726179789959 -0.16289066917433134; 0.09645302566833093 0.007513935519816117 -0.12257703467075132; 0.07950522805442334 0.02062681925773068 -0.16150752239932972; 0.06131812561390408 0.022195452326883844 -0.16973176673812707; 0.06933699673068226 0.02926821478322771 -0.23500132959907016; 0.06417813090683383 0.02969055334998906 -0.2517343295105408; 0.03491082431377057 0.017385332343711805 -0.15675833564943392; 0.020397795483793012 0.010583492968055948 -0.10409743052759403; 0.005548656519927645 0.00298565233637468 -0.033810565472661376; 0.007667565608924806 0.004434125001771413 -0.044742813516925314; 0.002332561499315748 0.0008202051084797543 -0.015299168346552275; 0.0002501962798862797 0.00017748004988195083 -0.0009718043655338076; -0.0003656076376251377 -0.0006337953151015229 -0.0016868594564379228; -0.00020891177837572552 0.0004894485881370655 -0.001037156360263675; 7.658332237428227e-5 -2.644680859683029e-5 -0.00026174946907838153; 0.0002120465447698947 0.00018243783990115023 0.00039647423232202995; -0.0012142375836722195 5.711338806172237e-5 -0.0038418415614928474; 1.8616060443245948e-5 0.000925781693209257 -0.0009534137649955213; 0.0004955238952311972 -0.00034753764561597233 -0.0019591125821201826; -0.0020598344774715085 0.0005507477356100955 0.0002841860635743911] %
+
+Mass Used: 96.96844412514156 kg
+Launch C3: 100.57458505847481 km²/s²
+||V∞_in||: 0.0018129496894170364 km/s
diff --git a/archive/ES_0.5860413597545535 b/archive/ES_0.5860413597545535
new file mode 100644
index 0000000..a9f4102
--- /dev/null
+++ b/archive/ES_0.5860413597545535
@@ -0,0 +1,22 @@
+archive/ES_0.5860413597545535---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T14:13:08.656
+Launch V∞: [5.0539407800028515, -8.181088724260869, -0.6029857407263165] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0007030638357782636, 0.00032875011902777185, -0.0005993284686285944] km/s
+ V∞_out: [-0.0003043100929796941, 0.0007160070115094261, 0.0005963162108018284] km/s
+ time of flight: 1.3848860704637384e8 seconds
+ arrival date: 2027-09-11T11:16:35.656
+ thrust profile: [0.7611867017278515 -0.47288228901496704 -0.34226721299450863; 0.34189250201460764 -0.022708189767841194 -0.3502915551946991; 0.11647645824803206 0.018277104552965696 -0.19873814690497751; 0.08782377396784281 0.024722113536545152 -0.19617811686758677; 0.05087487324350029 0.018547520476641273 -0.1416459932888816; 0.05312419606529649 0.02109064749289245 -0.16602435204174396; 0.044449855336951234 0.023932497481430774 -0.16083831865243778; 0.015683832220822504 0.008742080492948345 -0.08067333993640212; 0.003277611328388116 0.001335708908636457 -0.015482461429742538; 0.0024578175154065995 0.001258256515572899 -0.02092786073723369; -0.00041777833053057356 -0.00015094710105809724 -5.490432943975731e-5; 0.000972202204074347 0.0004743203224047202 -0.009451586135294395; -0.001556129283224291 -0.001340651832505277 0.001656839956150363; 0.003657626903149983 -0.00433599152968086 0.003239838160460355; -0.0006414257744515699 0.0004254865367806604 0.008339367381633947; 0.0017592521016832601 0.0012161179883020132 0.0005235030938526479; -0.008284780235313635 0.000527991792270247 0.0033556743943902157; -0.007057250689327077 0.009384078641606475 -0.004989242769039339; -0.0005176275763435269 -0.0022169558086486485 0.0005845657711865482; 0.009203075987525863 0.007991244264835206 0.0008361325295851707] %
+
+Mass Used: 142.17087514809236 kg
+Launch C3: 92.83612192552343 km²/s²
+||V∞_in||: 0.000980596762817783 km/s
diff --git a/archive/ES_0.5860472956953119 b/archive/ES_0.5860472956953119
new file mode 100644
index 0000000..ce5c9ea
--- /dev/null
+++ b/archive/ES_0.5860472956953119
@@ -0,0 +1,22 @@
+archive/ES_0.5860472956953119---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T15:12:48.856
+Launch V∞: [6.255446919005408, -7.7449617863859626, -1.5831720072950022] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.587696117907315e-5, 5.990985754247909e-5, 7.71966145350109e-5] km/s
+ V∞_out: [9.737333873281597e-5, 5.651317764522078e-5, 2.750075312898966e-6] km/s
+ time of flight: 1.5991702188330328e8 seconds
+ arrival date: 2028-05-16T12:36:29.856
+ thrust profile: [0.11850094610983951 -0.05783966515380132 -0.05564473983025659; 0.07099270322555219 0.0055991278553495435 -0.08327136153288403; 0.09179116700036685 0.02843835105273035 -0.17366403188667107; 0.08611964669812373 0.039736025199937616 -0.22416821628504033; 0.0688676110964089 0.040102412511130434 -0.22587998107708962; 0.0480438102943189 0.03307189010653607 -0.18744399024292527; 0.03373328924691605 0.026412656667337376 -0.15205357822856885; 0.015298376157041623 0.013758060588464953 -0.07882505569476513; 0.00120336075416296 0.0018030097299385278 -0.009738953293830233; 0.0001537830034382087 -0.0011369966071210328 0.001090965743653684; -0.0001624701501889539 -0.0003425050726173429 0.0005474240315588379; 0.0019812991781719322 -0.001143414574026492 0.0006109134743132814; -0.00021134748907128572 -0.001390688848691629 0.0016367942562045487; 0.0028766627876702514 -0.002231721014149142 0.0034546335999786184; -0.0010546894992495381 0.0018430583265112458 0.0009615133066471979; 0.0031391608988798874 -0.0013481674068205004 0.006343047681783072; 0.00028055352524005545 -0.001849806471933019 -0.0011536561760390634; 0.003171290932860674 -0.0031446476498299793 0.006992448491324963; -0.0012354101631782235 0.003729650077965641 0.013844515275485404; -0.0013536134794841044 0.0011857094807686901 -0.0006970010487197394] %
+
+Mass Used: 90.92986178095634 kg
+Launch C3: 101.62148283375558 km²/s²
+||V∞_in||: 0.00011256439542339684 km/s
diff --git a/archive/ES_0.5860641102799522 b/archive/ES_0.5860641102799522
new file mode 100644
index 0000000..96b7453
--- /dev/null
+++ b/archive/ES_0.5860641102799522
@@ -0,0 +1,22 @@
+archive/ES_0.5860641102799522---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T22:38:27.634
+Launch V∞: [6.99399375317705, -7.056547688127551, -1.2080638276642062] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0034525887608107906, -0.002794877800865325, 0.0017747181282901795] km/s
+ V∞_out: [0.0021440236287691445, -0.004272897126118312, 0.0001776583132271079] km/s
+ time of flight: 1.347189379136208e8 seconds
+ arrival date: 2028-08-13T04:34:04.634
+ thrust profile: [0.3481478914213944 -0.13545761866463288 -0.16993206183480528; 0.1621498682280152 0.013600819885297264 -0.19048756755832108; 0.13254251648016174 0.03774956691647811 -0.25077367846491727; 0.09944735590393444 0.04019777131384743 -0.257049211991898; 0.06652593512191773 0.03240581628143211 -0.21569751752615562; 0.04620644603283587 0.02544122990389985 -0.17814091997245896; 0.0162323244073008 0.010510149479733269 -0.07345036849435309; 0.013891123685687347 0.009498144426454948 -0.07070176285366347; 0.000925358944092833 0.0010241812710992317 -0.007949184545943653; 0.0023325380728224034 0.00023493103952505835 -0.010749296676377218; -0.0002708076575180273 0.0011600159106663042 -0.007378419203743255; 0.0010884179088873384 0.0014082451963845907 -0.0058396322736705385; -0.002577698073330457 0.00047842496542681843 0.0005489576893224519; -0.003018090257676784 -0.002791360342145604 -0.000840582932619855; 0.004064859944946058 -0.0016477130554290254 -0.002389563941099626; 0.0023760020713427914 -0.002367628982293403 0.0014158090312449524; 0.0014670886076076123 -0.003035080877886752 0.000745726294580674; 0.0030372709882122866 -0.0012322404840087488 -0.003127692969478859; 0.004693366442468679 -0.0006749624001191883 -0.00024225383507244782; -0.0019866924628317113 0.00217182657043165 0.0031218650877870248] %
+
+Mass Used: 99.41510804156087 kg
+Launch C3: 100.17023210600857 km²/s²
+||V∞_in||: 0.00478344389618281 km/s
diff --git a/archive/ES_0.5861060876806972 b/archive/ES_0.5861060876806972
new file mode 100644
index 0000000..e485a8e
--- /dev/null
+++ b/archive/ES_0.5861060876806972
@@ -0,0 +1,22 @@
+archive/ES_0.5861060876806972---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T15:58:36.343
+Launch V∞: [6.9837604463320755, -7.225739211558022, -1.2030194886565346] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.666807007632703e-6, 6.775961843314174e-6, -3.2537694858329116e-5] km/s
+ V∞_out: [-1.5359094283006773e-5, 2.8621529076535386e-5, -1.000133996779172e-5] km/s
+ time of flight: 1.3697632469591594e8 seconds
+ arrival date: 2028-09-11T00:57:20.343
+ thrust profile: [0.21301597667330022 -0.08099317613906876 -0.1134905405162546; 0.0968383594943344 0.006087309497574112 -0.13008031383081017; 0.09055493493929923 0.02191683705875426 -0.1936796039361584; 0.07610834509167867 0.025841226778355306 -0.2206121772340682; 0.05162120458245228 0.02051571242020801 -0.18958009424370773; 0.03223779168403654 0.014021986136445366 -0.14501176066415214; 0.020702288137717663 0.009728647616106334 -0.10877215938339244; 0.01608137817913103 0.008067115093103532 -0.09335543785827717; 0.012528979686944402 0.006043861545980827 -0.07570874772949318; 0.009707737112842701 0.004793518906666987 -0.06192069772450403; 0.0007089169576185779 -0.0005351543189717939 -0.0018583701769247837; -0.0015760086245371532 -0.0001747876491946068 -0.00047892549242020563; -2.176136902481919e-6 -4.631022074632966e-5 -0.00034752366502382027; 0.0012869778187199873 0.0001568196305173139 0.0006822759493170707; 0.0005318043994936793 -0.00041006326300600815 -4.248153934185322e-6; -0.0013997861505150272 0.000979721105222116 0.0019499482150143912; 0.0008226346624609512 -0.0005284807338319197 -0.0005572068971957326; 0.0022104438966849605 -0.0006281755146948867 0.0019444417920844994; -0.005224384119192713 -0.00021457939057453317 -0.005630970595375592; -0.0013950318587943476 0.0005762130307957177 -0.0008412529580390409] %
+
+Mass Used: 86.27350970497264 kg
+Launch C3: 102.43147301528697 km²/s²
+||V∞_in||: 3.356179871881536e-5 km/s
diff --git a/archive/ES_0.5861258322383213 b/archive/ES_0.5861258322383213
new file mode 100644
index 0000000..a184a06
--- /dev/null
+++ b/archive/ES_0.5861258322383213
@@ -0,0 +1,22 @@
+archive/ES_0.5861258322383213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T20:26:35.799
+Launch V∞: [6.962393488504835, -6.99557146403108, 0.4256731709368662] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3087328440494884e-5, -1.9279753679009408e-6, 3.2308328951178314e-8] km/s
+ V∞_out: [1.917697324911891e-6, -4.264622704733637e-8, -1.3082588411052836e-5] km/s
+ time of flight: 1.8749577787440196e8 seconds
+ arrival date: 2029-03-29T22:36:12.799
+ thrust profile: [0.3572796949437131 -0.0749888652585419 -0.07067346148978004; 0.26623718547584513 0.10930436286444341 -0.16362874883419376; 0.12393682015247763 0.09638001082982911 -0.1395273288016616; 0.07984298309304658 0.08801525466687639 -0.13182358075379186; 0.06399256991816439 0.08611367259391758 -0.1368696977674556; 0.037826942892873756 0.06109801593613328 -0.10339439369390446; 0.013396720228751642 0.025876921302763402 -0.045451962988377684; 0.006708608349833358 0.014378331973667986 -0.026678503601793434; 0.006135055158524516 0.014623319238644315 -0.027687393961394142; 0.0023636082107651637 0.005571092350530313 -0.010347522316365071; 0.00032899084317292496 0.0007833182673253195 -0.0018807652082800858; 0.00011318873158300033 -0.0001167345564484414 -0.0011109140580971041; 0.000442674834208964 0.0002698905081856523 -0.00017963833290490306; -0.00027503420423085994 0.00011643476773539634 -9.047474341838057e-5; 0.00010374404728584962 0.002041423535585521 -0.0016406853776833622; 0.0010032571552662834 -0.0003064937836098939 0.0003807694919171964; 0.00026486901513760193 0.0032320446453761925 -5.896606729486773e-5; -0.0008021819938407494 0.0004507332204094379 0.00045905426793736107; -0.0001720128305756204 -0.001300254686984987 0.0015808221336786443; -3.603614998524206e-6 -0.0003621419363803179 0.0004073467758859879] %
+
+Mass Used: 114.51431601206514 kg
+Launch C3: 97.59414084559594 km²/s²
+||V∞_in||: 1.3228616653178012e-5 km/s
diff --git a/archive/ES_0.586175904600408 b/archive/ES_0.586175904600408
new file mode 100644
index 0000000..d508144
--- /dev/null
+++ b/archive/ES_0.586175904600408
@@ -0,0 +1,22 @@
+archive/ES_0.586175904600408---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T11:32:59.570
+Launch V∞: [7.071733270993034, -7.055379134959886, -1.0832906001509621] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.2720022461960696e-6, 3.5063586176113195e-6, -1.879309424375735e-7] km/s
+ V∞_out: [-3.692561980104223e-6, 2.3625751709800565e-6, 1.9601505844693848e-6] km/s
+ time of flight: 1.3389280673221868e8 seconds
+ arrival date: 2028-08-03T03:59:45.570
+ thrust profile: [0.25182520135933 -0.09657249576914922 -0.12218322990273142; 0.14331084908388378 0.01332764276800744 -0.16688621800426237; 0.14140349283147893 0.04213491742090912 -0.26161901842640106; 0.11533587915392322 0.048529046491944096 -0.28886957029282573; 0.08334630417915845 0.04229518008150219 -0.2602799849020873; 0.04676603176491759 0.026904380732468466 -0.17379992193445368; 0.012247088584825516 0.007921824548214065 -0.05435333828857076; 0.012804878285226064 0.008877239956940416 -0.060694422579210705; 0.005208433014778059 0.004623601019240369 -0.033174850493705596; 0.0030387680244965375 0.0023677890473405364 -0.018688513975618493; 0.0007479689182426473 0.0005014918000071115 -0.004423233060933709; 0.000512521882091709 0.0001677428306636431 -0.0008029652180239191; 0.00030510460361276714 8.55836614970519e-5 -0.0005090041304570769; 9.359663561860348e-5 3.5781373079582556e-5 -0.0008095940426055284; 0.00021163989197928802 -0.0006005146933843544 -0.000820393607195337; 0.0003259662565609442 0.0024757213330550846 -0.0012637270825702753; -1.804469699892867e-5 -0.00017006643632532675 -0.0004045409234912922; 0.001776052519639713 -0.0008793174066423911 0.002753109054850892; 0.0023235429915971044 0.0004392073186779928 0.0019151653660729588; -0.0007471096367451225 -0.0001630766592406734 -0.0004279268646038832] %
+
+Mass Used: 94.93094450938588 kg
+Launch C3: 100.96130471847259 km²/s²
+||V∞_in||: 4.799569511272314e-6 km/s
diff --git a/archive/ES_0.5861761758707542 b/archive/ES_0.5861761758707542
new file mode 100644
index 0000000..3f1f576
--- /dev/null
+++ b/archive/ES_0.5861761758707542
@@ -0,0 +1,22 @@
+archive/ES_0.5861761758707542---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-16T22:44:16.318
+Launch V∞: [5.638996538070276, -7.728145316519666, -0.17189133916228744] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.286692175056582e-9, -1.9129814164987284e-9, 1.975139928349681e-9] km/s
+ V∞_out: [1.0428830317615285e-9, -2.3619993284503235e-9, -3.342661720384263e-9] km/s
+ time of flight: 1.5100104562178263e8 seconds
+ arrival date: 2028-01-28T15:28:21.318
+ thrust profile: [0.7685542995595018 -0.388701880280168 -0.2486952876899872; 0.28733702564481794 0.022466593575212333 -0.22731786449254293; 0.2138836157838151 0.07200627873944314 -0.26244220877607105; 0.16400032958447214 0.08349110853668057 -0.2678554812219021; 0.13633242829392245 0.0875878640303536 -0.2740262381418591; 0.06248226066729022 0.04692209717571413 -0.1495157856476385; 0.004392714549515612 0.0039674779263744 -0.013158498572839626; 0.0014625293273693406 0.0004735215915737265 -0.005079187134559247; 0.0037014148639155165 0.003987148158311812 -0.013420919409957325; 0.00023751365200040198 0.0010187003864564185 -0.0028085422319078382; 0.0006339810500900905 -0.0003083761464280693 -0.004931454240521581; -0.00026891209101003464 0.0023053774095589457 -0.003975540565414748; -0.00014937283998331678 0.001470557724142629 -0.0009220223782477294; -0.0006709795209379596 -0.0008871963553061342 -0.0001465369772066811; -0.0007955504442286467 -0.0006407947686682743 0.003773266720944704; 0.0008710193760014968 0.002246463477617416 -0.0005901189901177757; -0.0012056631880774107 -2.0783087538421303e-5 0.0006426645539794919; 0.001446267551906593 -0.00015351183479225588 -0.0009457714148785243; 0.0018934016635499887 0.001031010992125001 -0.0048237156539586885; -0.0005562681336314815 -0.000678694665870571 -0.005500552131014004] %
+
+Mass Used: 149.81852988700757 kg
+Launch C3: 91.55205862209242 km²/s²
+||V∞_in||: 3.576260161103449e-9 km/s
diff --git a/archive/ES_0.5861880058052843 b/archive/ES_0.5861880058052843
new file mode 100644
index 0000000..df77264
--- /dev/null
+++ b/archive/ES_0.5861880058052843
@@ -0,0 +1,22 @@
+archive/ES_0.5861880058052843---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T06:42:19.376
+Launch V∞: [5.37696024385663, -8.277336704219465, -0.43206471019368947] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9967522402070552e-7, 8.410097632686375e-8, -1.7115455497189635e-7] km/s
+ V∞_out: [-3.773433391381044e-8, 7.912412608570816e-8, 2.6265127107722594e-7] km/s
+ time of flight: 1.3925030618870008e8 seconds
+ arrival date: 2027-09-20T23:20:45.376
+ thrust profile: [0.36927008367171577 -0.23223178642250605 -0.185170142292161; 0.14962212283381252 -0.014894963257115179 -0.1694049056555433; 0.14567005290370014 0.014144168734880995 -0.25445238327579; 0.12280199354271222 0.025512573758331887 -0.28338276059564077; 0.0846525888260315 0.023726766037676573 -0.23820793879894867; 0.0702976672930579 0.023262217171258974 -0.23150895807046515; 0.025254150198304917 0.01019795587756843 -0.09387219507037675; 0.015898815660890412 0.005067947342217486 -0.06454139885869224; 0.002511444898017699 0.0033037933901794046 -0.004387572102105238; 0.00453029237096453 0.0008998507603235156 -0.012814200158546323; -0.0024400630657121754 -0.005042141430871293 -0.006726277491417058; 0.006441158174945153 -0.001551083764278333 -0.0028066447011690426; 0.007281791578188711 0.002718034495534725 0.0007272873603352192; 0.00014765561950361205 0.0007007919513574217 -0.0014923192112951686; -0.01207312891053153 -0.0020741762103145102 -0.0018830333488378203; 0.002767850593942477 -0.0008065712485071223 0.0049723554435522595; -0.0062824457562153605 -0.005303223528645807 -0.0034089210510786783; 0.005459931542065196 -0.00850948323687727 0.005310971506257163; 0.0030634954494851542 0.003914715761340025 0.0016015916193555246; -0.0003187175606454366 0.0023494627592232694 0.010353688216103614] %
+
+Mass Used: 114.47868173133338 kg
+Launch C3: 97.61268429282828 km²/s²
+||V∞_in||: 2.7611057747663076e-7 km/s
diff --git a/archive/ES_0.5862076686912056 b/archive/ES_0.5862076686912056
new file mode 100644
index 0000000..93eb976
--- /dev/null
+++ b/archive/ES_0.5862076686912056
@@ -0,0 +1,22 @@
+archive/ES_0.5862076686912056---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T13:43:29.668
+Launch V∞: [7.038382581019894, -6.993009020669396, -0.8219080995468192] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.288991158237453e-6, 1.3467876614832761e-6, -1.9892851460939926e-7] km/s
+ V∞_out: [-1.388387187343557e-6, 9.717151603883223e-7, 8.054744677700702e-7] km/s
+ time of flight: 1.3635335521815756e8 seconds
+ arrival date: 2028-08-31T17:39:24.668
+ thrust profile: [0.4065119761047128 -0.14378662515329066 -0.18713019899095573; 0.09301905353412525 0.012075018442969928 -0.10987519084562404; 0.10252537871356054 0.033495858372471383 -0.18888748008703599; 0.09741042867489035 0.04438881836579867 -0.24381318064786198; 0.089019459266825 0.04915850043330689 -0.2723911790657849; 0.03693626437646569 0.024805812648303418 -0.13521324598973203; 0.04641403452700974 0.030531838987936065 -0.19426240870530992; 0.011575663719215961 0.013156417968677059 -0.06894470488396955; 0.007332139771742151 0.004246401123449867 -0.04105201025124171; 0.001217310136205978 0.0017284204057084012 -0.011587730622516586; 0.005699594797104952 0.004359190996061731 -0.03414734469630009; 0.0014280646755045869 -7.733323245689007e-5 -0.005352502130074124; 0.0004931400990516157 -0.0027076841551218265 -8.79638631468599e-5; 0.0009468255753089603 -5.714352196120034e-5 -0.0004645793744481046; -0.005573846180309676 0.0017780275608375218 0.005034649133794763; 0.0008727021455579537 -0.00567084333002129 0.008368542493696993; 0.0008152479866979687 -0.0014689700014824372 0.0032571412248926807; 0.005364696100413162 -0.003054618688241126 0.00395882741747742; 0.0003858068367062474 -0.004650533755728113 -0.0030067290678364514; -0.0033118479390958425 0.003833130627438143 -0.009054369319802837] %
+
+Mass Used: 105.72914504934033 kg
+Launch C3: 99.11653744406847 km²/s²
+||V∞_in||: 1.8748087275939976e-6 km/s
diff --git a/archive/ES_0.5862119163804547 b/archive/ES_0.5862119163804547
new file mode 100644
index 0000000..fd56ec7
--- /dev/null
+++ b/archive/ES_0.5862119163804547
@@ -0,0 +1,22 @@
+archive/ES_0.5862119163804547---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T23:02:40.577
+Launch V∞: [5.3425618058394635, -8.001695135220135, -0.11743163783223227] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0017481177646513995, 5.124032677116529e-5, -0.001129470455818687] km/s
+ V∞_out: [0.0020070775059509616, -1.877812285775531e-5, -0.000546822281189927] km/s
+ time of flight: 1.4322540712358308e8 seconds
+ arrival date: 2027-11-01T15:52:47.577
+ thrust profile: [0.6457314757683639 -0.33942489449266844 -0.21757556832578284; 0.29442666607835344 0.009116563024263065 -0.23354470730178575; 0.27110209249483685 0.07561877401687132 -0.3249893914853776; 0.1232920223471194 0.054084281330484284 -0.20139036831217644; 0.1152700344756621 0.06378567800322314 -0.2267810457967411; 0.06691151371018328 0.04378301010379576 -0.1567654516033935; 0.042257445527458394 0.03130313660598379 -0.11406723962798833; 0.015722544919524493 0.013166048134259659 -0.051485124947312874; 0.009502937690881516 0.007856163318437902 -0.03249579368687374; 0.0018610118215612258 0.0014442567213840928 -0.0072679398282481985; 0.002847407531331855 -0.0009705912842484466 0.000663939710640432; 0.002828286808713382 0.0027798858173443937 -0.012975864402745335; -0.0036907672977410716 -0.0020552894958217154 -0.0011937975583692483; -0.0013011372391476855 0.00028304294692568506 0.0006606903818856478; -0.0021115403523841634 -0.00017064994358190026 0.0010097045425447116; -0.0010688340893889392 0.002912974547219586 0.0042113221559792816; -0.0025672094538417263 0.00041778074638456134 0.005940780921990773; 0.0008489702545397028 0.0006463492925592783 -0.00302328089506186; -0.0007117198490866768 -0.002401009566829372 0.002086463031203914; 0.002128535840142552 -0.0005241267672454375 0.0077819581312236] %
+
+Mass Used: 143.84125816845608 kg
+Launch C3: 92.58388187578417 km²/s²
+||V∞_in||: 0.0020818849153458733 km/s
diff --git a/archive/ES_0.586212357012543 b/archive/ES_0.586212357012543
new file mode 100644
index 0000000..b1d76f2
--- /dev/null
+++ b/archive/ES_0.586212357012543
@@ -0,0 +1,22 @@
+archive/ES_0.586212357012543---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T13:10:04.523
+Launch V∞: [5.332529351412621, -8.396688282854248, -0.992609687013547] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5144085970588618e-6, -1.7897522184062892e-6, 3.9481690817338445e-6] km/s
+ V∞_out: [3.3791600502987446e-6, 3.2785765985834052e-6, 1.5982446346768508e-6] km/s
+ time of flight: 1.3782753063433367e8 seconds
+ arrival date: 2027-09-05T18:35:34.523
+ thrust profile: [0.2972296573469899 -0.18833592443516184 -0.15153449917483736; 0.13522616749766778 -0.010857584857155806 -0.16533087607372052; 0.11067894189359456 0.01326462294637515 -0.2059724711182207; 0.07907933791573227 0.019932914092742445 -0.19686379718256383; 0.05325681911642062 0.01860467682288166 -0.1633292585410638; 0.03464406723928635 0.013904367337235718 -0.12177777712183877; 0.03275749069105015 0.017099913182461117 -0.1304620458661488; 0.027661279706678487 0.016439520943365368 -0.12611598480410569; 0.020215042676937914 0.009608905499551366 -0.11661585971462095; 0.02123834120380655 0.010821465931888919 -0.09984257858730346; 0.0005703773739325596 4.766510468099809e-5 -0.002032681945379782; 0.00026620096199522205 -0.000250836992807925 -0.0011151618104441748; 0.000369987924219253 0.00047299460135933886 0.00016398586243973167; -0.00013195547429257004 -0.00024262447968780644 -0.0003522428396439531; -0.000721768766532926 -0.0006704632746821464 -0.00011132850919098808; 0.0005830970509261384 -0.0010188879423864196 -0.0009413613209134594; 4.813483058306296e-5 2.592082384507736e-5 0.00041425911694041714; -0.0002520596492438248 -0.0003670119354001861 0.0006329672709232637; -9.030477557408489e-5 0.00025899986937181487 0.00026828856323725544; -0.00026783994833862656 -0.0003736710023557252 -0.0003827207231135284] %
+
+Mass Used: 101.01556505049666 kg
+Launch C3: 99.92551739385205 km²/s²
+||V∞_in||: 5.0113374157217564e-6 km/s
diff --git a/archive/ES_0.5862418913766625 b/archive/ES_0.5862418913766625
new file mode 100644
index 0000000..a209d3e
--- /dev/null
+++ b/archive/ES_0.5862418913766625
@@ -0,0 +1,22 @@
+archive/ES_0.5862418913766625---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T12:58:40.870
+Launch V∞: [5.79539408009025, -7.726214399984576, -0.1395995034777524] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3585141503475305e-6, -2.4242904420333667e-7, 2.8539680390689033e-7] km/s
+ V∞_out: [-1.349454539647019e-6, 3.3783943420543643e-7, -1.671939034842982e-7] km/s
+ time of flight: 1.565254434783821e8 seconds
+ arrival date: 2028-04-03T04:16:03.870
+ thrust profile: [0.5827605296761496 -0.2554734663295583 -0.1736068713514338; 0.23539180106668253 0.03239971316855312 -0.17558993820445948; 0.1637961173360818 0.06530747464572094 -0.19000222633235522; 0.10989645378323372 0.06365546094367443 -0.17019968472382807; 0.10536417737529638 0.07741850206378009 -0.20269950712058984; 0.09764399180796988 0.0842201750905936 -0.22076731800705557; 0.04339311098118294 0.04172241026674845 -0.1131100022136818; 0.013551484889784514 0.011460311790515283 -0.03282337630144143; 0.003058483082542773 0.0031296465273750115 -0.009465262556982408; 0.0031367703210769173 0.004836408732157246 -0.009568194667408284; 0.002843540847722335 0.005740388950400124 -0.006242414934356079; 0.010252336809921115 0.003959727292027515 -0.008794202400493199; 0.0013208589989021418 -0.0028443324030604953 -0.01985830737435711; 0.0038554612757560275 0.004271467071991879 -0.012270641962035405; -0.0013321468651292668 0.0004418017204977406 -0.005096353543748491; -0.013712767222308853 -0.006207220623548629 0.0001225511967519223; -0.012846249544908728 0.011565505723646716 0.013802588775226086; -0.0010550724607849503 -0.004758221156876615 -0.010914826360653227; 0.005557436090936339 0.009777398417293722 0.0027564317191145233; 0.002257100841695055 0.0065534481285205535 -0.004314763136839452] %
+
+Mass Used: 139.69613440934154 kg
+Launch C3: 93.30046951944537 km²/s²
+||V∞_in||: 1.4091784393213247e-6 km/s
diff --git a/archive/ES_0.5862559403868968 b/archive/ES_0.5862559403868968
new file mode 100644
index 0000000..2ad49c8
--- /dev/null
+++ b/archive/ES_0.5862559403868968
@@ -0,0 +1,22 @@
+archive/ES_0.5862559403868968---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T16:48:11.287
+Launch V∞: [5.4244373359856395, -8.217717615618517, -0.8000474784600824] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.983759557395411e-8, 2.873773898768437e-8, -6.419975653064653e-8] km/s
+ V∞_out: [-3.1951888515541486e-8, 7.188969349491243e-8, 6.777426064852946e-8] km/s
+ time of flight: 1.3855418485405228e8 seconds
+ arrival date: 2027-09-11T08:04:35.287
+ thrust profile: [0.3704308389775659 -0.22276055336799266 -0.1732289521588152; 0.20506673438581188 -0.01059714276151379 -0.20867202175679264; 0.14864742283632854 0.02519767181380856 -0.23008473621106246; 0.1504202588356057 0.0459371330683652 -0.3051701501977805; 0.09915568505808185 0.03954482556710333 -0.2457925532231094; 0.05261060850406391 0.024655165490032483 -0.15123620508078872; 0.035781190465782306 0.01880854578159604 -0.11559007949349731; 0.010000843602526134 0.006018412617735984 -0.035878262033062526; 0.003803333526255801 0.0026817110474446374 -0.014891156254195067; 0.0027906603258417125 0.0023889415270535895 -0.013147154521219718; 0.004532634283097934 0.0033037165971339802 -0.019769722059826394; -0.0002065546017417083 -0.004651978186846014 -0.007480506715697476; 0.0014561373287574468 0.0009759070333280042 -0.007590767170689554; -0.0006878600845145917 -0.0019164164750092496 -0.0023285403659292895; 0.0010187247860545564 0.0010600243098362358 -0.005340607385396842; -0.0015371854192721126 -0.002403061405269246 0.0007689432774349182; 0.0054564439626192465 0.005273565804214033 -0.009182617060483332; -0.0022328254666180705 0.005612166972464393 -0.0009627820917316532; -0.0010923454617940021 0.0027532694645505417 -0.0034623232997912324; -0.0026805358220152193 -0.0038353559023046636 -0.009579967491398413] %
+
+Mass Used: 114.65830184379183 kg
+Launch C3: 97.5954791898722 km²/s²
+||V∞_in||: 9.911990787056726e-8 km/s
diff --git a/archive/ES_0.5862582191301065 b/archive/ES_0.5862582191301065
new file mode 100644
index 0000000..b17a3bf
--- /dev/null
+++ b/archive/ES_0.5862582191301065
@@ -0,0 +1,22 @@
+archive/ES_0.5862582191301065---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T00:19:28.070
+Launch V∞: [5.54126792582904, -8.307415924640395, -1.3974150895125645] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.0147298647377e-6, 2.027265918771094e-6, -2.5282501919065356e-6] km/s
+ V∞_out: [8.813551960606488e-6, -3.4715396123839315e-6, 1.4567541245834316e-6] km/s
+ time of flight: 1.4083763314433816e8 seconds
+ arrival date: 2027-10-10T01:53:21.070
+ thrust profile: [0.15226858521445483 -0.09482530874042268 -0.08208500044253966; 0.09498984317128288 -0.007654388079300717 -0.11335078001564594; 0.1142583952800958 0.013674899756525694 -0.2108252726193468; 0.1070345964175074 0.025329940025229446 -0.2632273464157932; 0.08354260359283898 0.02661940281737571 -0.252477747987681; 0.05517469180821982 0.021181388229863058 -0.19509575782327654; 0.028330563565989404 0.012686294326074784 -0.11419064089558104; 0.0019200783621533993 0.0008521615819166003 -0.009428841281166472; 0.0030450531059056543 0.0014556119786109428 -0.010423676590446747; 0.005266100966673742 -0.003371138473996053 -0.015571643011286345; 0.002390505024145724 0.0036724611712237584 -0.02654202415491834; 0.008832367953037724 0.005103169284564118 -0.04672608456161955; -0.001071438669087502 0.001271541027717601 -0.0020744848686790425; -0.0017423004661365098 0.002259888465951828 -6.815696714037103e-5; 7.929712621466934e-5 0.004031863036878637 0.0041183150206172085; 0.0003334429567267524 0.003275368912855076 0.002310229289871131; 0.00019453921262761745 -0.004492889747235555 -0.0013984819017018718; 0.004040945404309075 -0.012570318599737153 -0.001277218593664789; -0.0025479379676734875 -0.002030253387787259 0.0009844702526419563; -0.00041932460334446185 -0.0038853586098226466 0.010834174764169143] %
+
+Mass Used: 90.88371438319473 kg
+Launch C3: 101.6715785031879 km²/s²
+||V∞_in||: 9.579520377998058e-6 km/s
diff --git a/archive/ES_0.586295906302167 b/archive/ES_0.586295906302167
new file mode 100644
index 0000000..de3b5b3
--- /dev/null
+++ b/archive/ES_0.586295906302167
@@ -0,0 +1,22 @@
+archive/ES_0.586295906302167---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T21:46:16.551
+Launch V∞: [5.370922510324983, -8.634591406135154, -0.6987183629245866] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002077564910593365, -9.376091654417097e-5, 0.00016925268797772866] km/s
+ V∞_out: [8.28455056115095e-5, -0.00019967108342335861, -0.0001842124938537222] km/s
+ time of flight: 1.5124635353075004e8 seconds
+ arrival date: 2028-02-15T10:38:49.551
+ thrust profile: [0.046049181010790745 -0.029778591468404038 -0.02861572681385055; 0.056401810855590165 -0.013273058058798916 -0.0881854691170024; 0.05237435316404056 -0.00867753431798696 -0.13539525198556032; 0.05808242517336029 -0.008878707227984318 -0.20234867055757835; 0.04867034544741464 -0.008760840000315632 -0.21082296850998739; 0.04192112406476742 -0.009415166437596574 -0.21241849657844294; 0.029192641221098936 -0.00767650505867762 -0.1676521003071266; 0.012450641880242301 -0.004144861221862066 -0.08483778859057416; 0.0026585503035170058 -0.0006756430535906804 -0.017414714605252374; 0.003916074668645158 -0.001322218930180463 -0.026456432080674587; -0.0013148773534460154 -0.0006870190916840142 -0.002697865231678512; -0.0002650346344802493 0.0007053328093701877 -0.0006595772347459675; 0.0023857642587582764 0.0010889983321158416 -0.00023423846230439822; -0.00022653220465439246 0.00043229230602879104 -0.0008494026623655317; -0.0004540468382675775 -0.0006567347777667702 -0.0028862654268565586; 0.0007185362597547648 -0.0015183451929974847 -0.0025692704811303207; -0.0016979911387240154 -0.0022886989599657636 -0.0032394713950141814; -0.001514104750597263 -0.007644904419270464 -0.0029477398118355124; 0.00025379971351236787 -0.0007532044700026763 0.0038712548993779248; 0.0013678313682954366 -0.003322892112827788 0.006098900225250715] %
+
+Mass Used: 77.97997985707252 kg
+Launch C3: 103.89118471350669 km²/s²
+||V∞_in||: 0.0002839019926597514 km/s
diff --git a/archive/ES_0.5863064938299247 b/archive/ES_0.5863064938299247
new file mode 100644
index 0000000..86dab82
--- /dev/null
+++ b/archive/ES_0.5863064938299247
@@ -0,0 +1,22 @@
+archive/ES_0.5863064938299247---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-10T18:13:05.853
+Launch V∞: [6.125413616183972, -8.252970721147008, -1.0301419493951354] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.069311318793241e-8, -5.789740142868467e-8, -3.130483747974621e-8] km/s
+ V∞_out: [1.7686136115736376e-8, -3.706450608507827e-8, 5.574922057854532e-8] km/s
+ time of flight: 1.8132926198024985e8 seconds
+ arrival date: 2029-02-06T11:27:26.853
+ thrust profile: [0.004637960694363234 -0.0016284977834921158 -0.0048408406879539585; 0.0042013390813392315 -0.0011835280026481372 -0.008376821277351712; 0.021356486645750055 -0.007707935333594569 -0.07115917182389314; 0.030254731449033852 -0.015676082757405996 -0.1394951024643831; 0.030226630473940877 -0.020442860164320533 -0.1721941515489541; 0.024838394594230477 -0.02037055335174785 -0.16378880380477878; 0.01575261655304219 -0.014877632020203828 -0.11538316641001416; 0.008602288582913072 -0.009013075222821765 -0.06834194363348918; 0.0023317200383223147 -0.00208905547728088 -0.01733981966051602; 0.0011389183679453318 -0.0014617721466067264 -0.006529601874786409; 0.001418508315748298 -0.0017324869612105696 -0.00909664753340993; -9.979271570508853e-5 -0.0011787145331738067 -0.006242945033347111; 0.0005203444163735014 -6.908967202324574e-5 -0.0044426772089326706; 0.0002808943531492879 -0.0002762427463111382 -0.0071193034697342415; -4.3963789449865016e-5 0.0005929486965603288 -0.004016493346689728; 0.0006457328109164274 -0.0005383023270201473 -0.0018054841393939291; 0.003139974602606478 -0.002790464028097846 -0.00045077338294739235; 0.0002681570627769132 -0.0009927099562293575 -0.0027522235670212475; -0.004831170708497218 0.004120873035236537 -0.004676358904114665; 0.016425895528097752 -7.339227055437191e-5 -0.0017121819613615781] %
+
+Mass Used: 61.646017047064106 kg
+Launch C3: 106.69341012934538 km²/s²
+||V∞_in||: 7.262347512337048e-8 km/s
diff --git a/archive/ES_0.5864153008238882 b/archive/ES_0.5864153008238882
new file mode 100644
index 0000000..8c6d9d0
--- /dev/null
+++ b/archive/ES_0.5864153008238882
@@ -0,0 +1,22 @@
+archive/ES_0.5864153008238882---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T13:46:26.581
+Launch V∞: [5.222325316627576, -8.499203126289746, -1.5627174654834366] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0015477693825770285, -0.009391333064834674, 0.010901729444088966] km/s
+ V∞_out: [-0.010166126498107426, -0.008765290842346599, -0.005402221646835337] km/s
+ time of flight: 1.384585435660909e8 seconds
+ arrival date: 2027-09-15T02:28:49.581
+ thrust profile: [0.2725618411310739 -0.17527220337105462 -0.16141077177739258; 0.11948497165175066 -0.017364903531902322 -0.1650144022116404; 0.10373727331272421 0.003994233838890155 -0.2265269430198721; 0.06622163281979063 0.008883967075660835 -0.19462621537092037; 0.04952905598854194 0.009643605478208979 -0.18057580012797442; 0.04198771596811607 0.01004599408605975 -0.1798062922656683; 0.02597577210216266 0.00675989971493854 -0.1278037603410659; 0.010667597769705401 0.002706950613516964 -0.05730126329098197; 0.0021247606580075346 0.000542523103264557 -0.012014607852986388; 0.0007919473006018713 0.00020390522589063968 -0.004750930429785868; 0.00038408206100998466 0.0003207515744324265 -0.002307191166729538; -0.0003947041576354322 -0.0005867691604849273 -0.0011414992622353604; -0.0007705921428550089 0.000484516068230562 -0.0029134454437270032; 0.00015898692403772943 -0.00010491586490317829 -0.0020487631585506152; 0.00021332446243394138 -0.000329878759818286 -0.0008443215215638606; 0.0001079093141929271 0.00023002224281491474 -0.0007015573633640856; -0.0034910245864272615 0.003616355146264725 -0.002251372535197586; -0.000905019734378082 0.00022684237641675063 0.002165619733522436; -0.00028222222810710617 -0.0019491160468832957 7.344259144940058e-5; -0.0003442516544107171 -0.0016056654566917782 0.0011720965622835822] %
+
+Mass Used: 89.4357262938297 kg
+Launch C3: 101.95122137154969 km²/s²
+||V∞_in||: 0.014472056925966544 km/s
diff --git a/archive/ES_0.5864398180569425 b/archive/ES_0.5864398180569425
new file mode 100644
index 0000000..618d381
--- /dev/null
+++ b/archive/ES_0.5864398180569425
@@ -0,0 +1,22 @@
+archive/ES_0.5864398180569425---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T21:15:28.316
+Launch V∞: [7.0350042381035065, -6.998955495629282, -0.7658008665330811] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01057546028487307, -0.017470839605517, -0.0013568355669692953] km/s
+ V∞_out: [0.004381930147565444, -0.019534165303369072, 0.004248035996501232] km/s
+ time of flight: 1.372813889178253e8 seconds
+ arrival date: 2028-09-11T18:58:36.316
+ thrust profile: [0.4034902439641279 -0.13850837338394212 -0.17962815074922828; 0.10023248290340563 0.014229549176042673 -0.11639794131192627; 0.0807831767458812 0.029287227837493067 -0.14970542242521337; 0.06431310873884684 0.03225885380911561 -0.16145340289086751; 0.07083454378257886 0.045379709169015604 -0.2160875783709554; 0.061588983024107626 0.0370413741453252 -0.21832374595677226; 0.033553482377256603 0.022668971021607094 -0.14232526102473755; 0.026628384936571783 0.021806456127025132 -0.12701967278078224; 0.015896791859767233 0.01155937395993365 -0.08293616427687525; 0.00045574923426012245 -0.00017737409869593153 -0.0075816307966825765; 0.014644432993279187 0.012861421560226674 -0.09114271242396071; 0.0011454888090581465 -0.00014800012371567477 -0.0007222748221090659; 0.0015791681678784548 0.003938514677371959 0.0007501266754622001; -0.0005503218482509133 0.0005598710220488293 0.001212743878357337; 0.0016736491542848147 0.004082253842006393 0.0032514649669156074; -0.003260393688596201 -0.00547065367014848 -0.00443693217714705; -0.00019872395804279976 0.00046403184013103294 0.0013656855877207915; 0.0010192788932983834 0.0008445752958031805 -0.0016216977799410615; 0.010537396887945815 -0.005349231482766887 0.0006996527322039434; -0.003701375820134951 0.0030863949438447334 0.014427866004212975] %
+
+Mass Used: 106.31162490825363 kg
+Launch C3: 99.06311362711644 km²/s²
+||V∞_in||: 0.020467330053390496 km/s
diff --git a/archive/ES_0.5865034425974505 b/archive/ES_0.5865034425974505
new file mode 100644
index 0000000..69fc804
--- /dev/null
+++ b/archive/ES_0.5865034425974505
@@ -0,0 +1,22 @@
+archive/ES_0.5865034425974505---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-10T20:50:17.523
+Launch V∞: [6.102468310778494, -8.186876136632021, -1.0348534609516122] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.479688749581993e-9, -1.9770957861472406e-9, 3.99087925964167e-9] km/s
+ V∞_out: [1.6254430246705348e-9, -3.6892119699134833e-9, -5.117116735065345e-9] km/s
+ time of flight: 1.822484977812527e8 seconds
+ arrival date: 2029-02-17T05:25:14.523
+ thrust profile: [0.10842060292390285 -0.058892764260312765 -0.06637993010104128; 0.025325790278299804 -0.00897257854853764 -0.049905220923907416; 0.025084103737339193 -0.0135562227953395 -0.08723291807477347; 0.01793300560597018 -0.014319445124417659 -0.09230359341346694; 0.017607949138126133 -0.01700534071103247 -0.10556138090647038; 0.015652226297098937 -0.018383838854878858 -0.10896940967293077; 0.013814019714622263 -0.01772312583322701 -0.10251563113033016; 0.008912051324800664 -0.012386258193382712 -0.0710915874550989; 0.008960254318743453 -0.012863118070613211 -0.07150434407916403; 0.003381175253202274 -0.005151438703552369 -0.03119085577559545; 0.004277537005813076 -0.010228168832772638 -0.05176512330561503; 0.0013452173602686822 -0.0033997829173727703 -0.018929873435973812; 2.0283694734150534e-5 -2.699242704181701e-5 -0.00036190110797182796; 0.00010372073849947589 -6.69993222804084e-5 -0.0005532041545996435; -5.662694194711671e-5 -5.461157525323118e-5 -0.00014517086597643912; -0.00015459561542893827 -0.00023328133144393957 -0.0005068166709614852; 5.001431229711833e-5 2.0926635637810178e-5 -0.00016053948905936694; 1.0605889380862032e-5 0.00014081801963701122 -0.0005666732885587703; -8.56851982842979e-6 0.0003187425337093749 -0.00037918787333006605; -0.00011574324767257615 -0.0002416070251263407 0.00015203636160441024] %
+
+Mass Used: 69.79412109387658 kg
+Launch C3: 105.33598204625409 km²/s²
+||V∞_in||: 6.316932507615598e-9 km/s
diff --git a/archive/ES_0.5865135720084855 b/archive/ES_0.5865135720084855
new file mode 100644
index 0000000..ee84d2f
--- /dev/null
+++ b/archive/ES_0.5865135720084855
@@ -0,0 +1,22 @@
+archive/ES_0.5865135720084855---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T06:45:34.049
+Launch V∞: [6.954961644882968, -6.992528255860103, -0.8265199655417461] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0011460464540408916, 0.0008741687614091145, -0.0006081230904563696] km/s
+ V∞_out: [-0.0006947326357820446, 0.0014003197458283007, -6.177452941019749e-5] km/s
+ time of flight: 1.39234658758008e8 seconds
+ arrival date: 2028-10-04T19:03:12.049
+ thrust profile: [0.4147768194930661 -0.1456627288731942 -0.18966491101649735; 0.2157313149350953 0.02697428001075888 -0.2469691115720899; 0.09485224539619284 0.03300742437768493 -0.1821777159156981; 0.07337858431296414 0.03536774795350499 -0.1930452218245362; 0.0874795890653305 0.047966752406696414 -0.276376105100788; 0.03196575664451079 0.021630828322814804 -0.12753124838185906; 0.019098914145675046 0.013523707683969018 -0.08549667352939462; 0.0027171631798059304 0.009060456682461039 -0.04629644204011122; 0.010908180801134322 0.0062689613393100896 -0.04416402020214554; 0.006907983036793089 0.007050364271287893 -0.03820834621462422; -0.00265793675955469 -0.0008390224932074877 -0.018914007704096587; 0.0038839947037768506 0.001166206818990777 -0.004525511912829941; -0.007564530760434986 -0.014514954548987226 -0.0033073531642211617; -0.003614320184659169 0.000827662428339431 -0.011385520105035693; 0.010993270877884582 -0.0012751044078814508 -0.0011505124913850362; 0.0012578069357029682 -0.0006245427204903532 0.0004948297861581148; 0.022261964423943487 0.004091023384739711 0.0014729152979900302; 0.002387018571133966 0.0017512073009629042 -0.030297022264371726; -0.0029501771947619076 -0.007986992423187456 0.0007182802659321487; 0.019636087936065718 0.018226983814489228 0.021449101992268335] %
+
+Mass Used: 112.89037816853306 kg
+Launch C3: 97.95007814423428 km²/s²
+||V∞_in||: 0.0015644191226744362 km/s
diff --git a/archive/ES_0.5865372145298974 b/archive/ES_0.5865372145298974
new file mode 100644
index 0000000..6e04f8f
--- /dev/null
+++ b/archive/ES_0.5865372145298974
@@ -0,0 +1,22 @@
+archive/ES_0.5865372145298974---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:21:08.944
+Launch V∞: [7.012396806121214, -7.049304867734982, -0.8332722364638923] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0019490170703489282, -0.0028592294362500457, -0.0002447731052354326] km/s
+ V∞_out: [0.00023428128277537733, -0.0010235074408066868, -0.0033058299780941345] km/s
+ time of flight: 1.3703996783651978e8 seconds
+ arrival date: 2028-09-09T22:00:35.944
+ thrust profile: [0.3913372489990067 -0.1463023837812146 -0.19462879542323366; 0.10791585502673917 0.00931368958226535 -0.13938506219255442; 0.07887548360194292 0.021365571279120706 -0.16416513213003786; 0.06820622605689165 0.02590237925061606 -0.19272212586455859; 0.04174458627105844 0.018313552559341376 -0.1472361363275947; 0.0520780071434651 0.027015583044454804 -0.2307773471764427; 0.06049659142797175 0.03627813003488118 -0.2941337608396053; 0.005266843923125521 0.002865652312767792 -0.028271386989772256; 0.00784648819955644 0.004304000033176072 -0.04874957329762546; 0.0019387707398539292 0.0015161259092711572 -0.013379996483795599; -0.0006776534211703844 -0.0009096903092797955 -0.0035249688308099693; 0.004100786581676891 0.0024444712343758145 -0.027546598849824102; -0.0003985946034922809 -0.00028924967826976777 0.0042722376683367175; 0.003915865055709116 -0.004157750336316393 0.006720320912617777; 0.0010048007749216793 0.0008023183944682972 0.00904345485940133; -0.003324540292527098 4.648743889425962e-5 0.002471839395974617; -0.00278376813252794 0.002235091358706671 0.011174219713234722; -0.000245266079639384 0.0001393522265865627 0.00040980389190782194; 0.00041349347520688694 0.000720101934641657 0.00024254505749691938; -0.00015039419679169057 0.00218475150814789 -0.01211083041917693] %
+
+Mass Used: 103.52237117335653 kg
+Launch C3: 99.56075070483264 km²/s²
+||V∞_in||: 0.0034689731020399782 km/s
diff --git a/archive/ES_0.5865489549679401 b/archive/ES_0.5865489549679401
new file mode 100644
index 0000000..9293011
--- /dev/null
+++ b/archive/ES_0.5865489549679401
@@ -0,0 +1,22 @@
+archive/ES_0.5865489549679401---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:09:12.946
+Launch V∞: [5.371758143281311, -8.290620941337803, -0.6732939253037817] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00025349224090342315, 0.00012601392286257427, -0.00017194016075761784] km/s
+ V∞_out: [-9.773833626439485e-5, 0.00022690457122989235, 0.0002206272568049521] km/s
+ time of flight: 1.3992244592788088e8 seconds
+ arrival date: 2027-09-29T02:29:57.946
+ thrust profile: [0.37009778465317117 -0.22233823802035457 -0.17759983944057678; 0.13971352101002302 -0.009887371258598867 -0.15397921934157457; 0.12207095728828721 0.016770923786597357 -0.20572941509910664; 0.09449864546754995 0.024387037652632136 -0.2103087332416819; 0.05772292908718969 0.01978091611185111 -0.1537680523858044; 0.04044729509096669 0.01629765760897954 -0.13511063694288322; 0.07066948200160128 0.032232818792975355 -0.24811320324303243; 0.024794841531836063 0.007147401433028591 -0.09800652070180549; 0.016893672183853375 0.008557633991696062 -0.06271165301011696; 0.005335152833363996 0.005651190859453926 -0.051285629838676905; 0.002780143277485029 0.01082894368840026 -0.01105281556757403; -0.005100899234730304 -0.00027442427625789276 -0.009004030566619822; -0.004281492775748118 -0.004271189192563042 -0.006471529711997747; -0.0015355183286008608 -0.0017842915791715039 -0.0009331704481588899; 0.0002507129866750312 -0.003341470808263361 0.0036952986654992413; -0.004018814302753577 -0.0027011415215932315 0.004124702324546697; 0.0013575284732482975 -0.005117357925014861 0.00018495857567461132; -0.00234741697754279 0.006675142319973364 0.011194988392194287; 0.0019683962686120843 0.001993872316363294 -0.005371632184109484; -0.003316234624042411 0.007900671899522678 0.006821234661571538] %
+
+Mass Used: 112.38666332179446 kg
+Launch C3: 98.04350585270898 km²/s²
+||V∞_in||: 0.00033121178094205737 km/s
diff --git a/archive/ES_0.5866646176320427 b/archive/ES_0.5866646176320427
new file mode 100644
index 0000000..c67f7ef
--- /dev/null
+++ b/archive/ES_0.5866646176320427
@@ -0,0 +1,22 @@
+archive/ES_0.5866646176320427---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-12T04:33:25.778
+Launch V∞: [6.21870125886596, -8.109035681164963, -0.09624279379362027] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00047079586551192215, -0.0005635538982253748, -0.0004758019668513827] km/s
+ V∞_out: [0.0006516004834080366, 0.00034891552163094795, 0.0004632153901479001] km/s
+ time of flight: 1.8749577783298695e8 seconds
+ arrival date: 2029-04-20T06:43:02.778
+ thrust profile: [0.11256312536707394 -0.04948052592639932 -0.06166104494368965; 0.05555072219513833 -0.012341076379942214 -0.09752940603950694; 0.03009011641286861 -0.00946277991591809 -0.09295537181249003; 0.026200422700664645 -0.01139336546648866 -0.10918989561976208; 0.027586395715073535 -0.015955153081284965 -0.1384562301795149; 0.02413377301876515 -0.017469779509596415 -0.13874366555305997; 0.009906675583900784 -0.008013885172770659 -0.06306578857697803; 0.00913929948114553 -0.008375052364095891 -0.06269979383646632; 0.006823838294022687 -0.006553170779421678 -0.049950907155672256; 0.0058969285782948435 -0.006250382255960872 -0.04413112695651483; 0.00028336050064003423 -0.0005119103680974609 -0.0030227516690135826; 0.0004667048658622291 -0.0018681295112350973 4.174579468298862e-5; 0.0012214258194656034 0.0018235626438315817 0.0022593693536209136; 0.00017221191157890212 -3.481669876528141e-5 -0.0022086219632452375; -0.0018367681732870558 -0.001510775990291579 0.00116854102795509; -0.0005997019323165766 0.0012999035224523536 0.001824286739170754; 0.003196957545840676 -0.002313120551692383 0.005547907579408695; -0.0009746494464827028 -7.344241821040326e-5 -0.005842970909894467; -0.0049397403750015565 0.0024614042731796086 -0.006970066998145435; 0.0007113195964147842 0.0007386738013699849 4.903021778565917e-5] %
+
+Mass Used: 75.22057564947181 kg
+Launch C3: 104.4379677007848 km²/s²
+||V∞_in||: 0.0008750024313382107 km/s
diff --git a/archive/ES_0.5866967976557018 b/archive/ES_0.5866967976557018
new file mode 100644
index 0000000..1cf8c30
--- /dev/null
+++ b/archive/ES_0.5866967976557018
@@ -0,0 +1,22 @@
+archive/ES_0.5866967976557018---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T04:08:16.983
+Launch V∞: [6.586842296003094, -7.42181405358058, 0.11442577986974597] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.4305524804764715e-9, -5.915681835595225e-11, -5.7781633051973e-9] km/s
+ V∞_out: [-1.930243084877084e-9, 4.8897901918261465e-9, 6.830129894988432e-9] km/s
+ time of flight: 1.8749577787492767e8 seconds
+ arrival date: 2029-04-10T06:17:53.983
+ thrust profile: [0.17754528916080134 -0.04137977495166316 -0.06517997255333143; 0.060824156881070825 0.01634792850926413 -0.07166485482514798; 0.05572510592086458 0.02939820839558583 -0.10766569406318395; 0.03432110968559608 0.02137836461043596 -0.08710908091460406; 0.04302903461680222 0.045492393110244674 -0.17968065589400198; 0.016993315189499165 0.012069959696856567 -0.06764808694423013; 0.012605759907662894 0.025413845323093022 -0.08656430033446169; 0.017821797581597333 0.01778861476433365 -0.05404731077180517; 0.032274310014547135 0.029330975958285196 -0.11427769146668192; -0.009998276846339037 0.0074064245240680554 -0.027338941924464438; -0.005547978257815558 -0.013909733077611165 -0.03632375083088625; 0.022403480819278516 0.0032970292149076307 0.0071551389381055985; 0.014629855114922371 0.0032140947815503806 0.014906815127692182; -0.007017586984638346 -0.005331242769377908 -0.00459309321173543; 0.00598351353709654 -0.008585015616689371 -0.020763185925908367; -0.008775488394111873 0.034963625893579334 0.01703497953330605; -0.032631520003106027 -0.00886757224982922 0.02245834235970348; -0.0320736674117473 -0.018532296937779243 0.03164940627679727; 0.0035262139853383676 0.013539893461589746 -0.049646139008764426; -0.06722686350885707 0.06990331198891363 0.029082239550216833] %
+
+Mass Used: 109.99596412991696 kg
+Launch C3: 98.48290853744031 km²/s²
+||V∞_in||: 8.6453846597389e-9 km/s
diff --git a/archive/ES_0.5867953217117674 b/archive/ES_0.5867953217117674
new file mode 100644
index 0000000..2ef9aeb
--- /dev/null
+++ b/archive/ES_0.5867953217117674
@@ -0,0 +1,22 @@
+archive/ES_0.5867953217117674---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T20:11:57.166
+Launch V∞: [7.511848854748719, -6.449763144302209, -2.2854465265311648] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00030762309871904057, 0.0011249425067979856, 0.001722040774411411] km/s
+ V∞_out: [0.0018301083221979899, 0.00018522848783850517, -0.0009717603925800608] km/s
+ time of flight: 1.5443806876786837e8 seconds
+ arrival date: 2029-03-30T07:39:45.166
+ thrust profile: [0.1708549242029957 -0.049950985534759955 -0.0773696999458113; 0.050272903955751805 0.009812858533728892 -0.06901476391836951; 0.0688255061617738 0.027765332091811853 -0.15304763749239408; 0.05325006323212145 0.027775950685948316 -0.1615149659230807; 0.05723979051469992 0.038346738913809374 -0.23213728683194756; 0.03809277801739796 0.02775524785931258 -0.19327661519355735; 0.012142277571302604 0.010650230698685946 -0.07724045549257094; 0.010551857223437825 0.009819587714191445 -0.07617233201402375; 0.0029561773250928102 0.0031811090401716374 -0.02637221478007954; 0.0017202536363161464 0.002008081824493556 -0.017965443989195383; 0.0016134173623204716 0.004660104573689275 -0.0055674016933573165; -0.0009705171724982677 -0.001967920210909575 0.001775098072505634; -0.0003419180041922585 0.0014902522090680232 -0.003961627406836488; -5.917514418428784e-5 -0.0030236239963353576 0.007576489815484892; -0.0008577210821852783 -0.00045387821950970946 0.004998463915850447; -0.0011354254442987976 0.002841236227034501 -0.004936097335187364; -0.0040313448211973125 -0.008031118057250864 -0.00878973455455366; 0.00043468898731237836 -0.004816323170026846 0.004398972798424866; 0.0015031412803042776 0.004074961585121937 0.009896284736426671; -0.00023718241607216178 0.00962818934376203 -0.0025223942391061913] %
+
+Mass Used: 82.29947064809949 kg
+Launch C3: 103.25058365982213 km²/s²
+||V∞_in||: 0.0020797961542425 km/s
diff --git a/archive/ES_0.5868487797576025 b/archive/ES_0.5868487797576025
new file mode 100644
index 0000000..9bdfbfe
--- /dev/null
+++ b/archive/ES_0.5868487797576025
@@ -0,0 +1,22 @@
+archive/ES_0.5868487797576025---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T14:12:04.683
+Launch V∞: [5.287140078165014, -8.242740145939704, -0.4989103534520129] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00768116964574363, 0.046783556458929856, -0.04924689942954263] km/s
+ V∞_out: [0.04809114115048156, 0.04067216192657724, 0.026567608617057332] km/s
+ time of flight: 1.4499074154629397e8 seconds
+ arrival date: 2027-11-27T17:24:25.683
+ thrust profile: [0.42127697067467634 -0.24188601035391183 -0.19288743614876877; 0.2265511005718297 -0.011033489689193588 -0.24498705334511034; 0.09666877772092917 0.013651793024424742 -0.1651203071281782; 0.09063111369236461 0.02438007609572594 -0.20768477705677732; 0.04454721152619856 0.014117406813414968 -0.12362396221942706; 0.07361955109465565 0.03069949562275182 -0.23990166098518356; 0.05000447741098992 0.02113854877849638 -0.18034467638228963; 0.01484621046509132 0.006645283219236979 -0.057038321638809744; 0.0005776577128047901 0.0016491832834019922 -0.009599711934365082; 0.0029899124116668082 0.0013062447139633362 -0.015837336452887957; 0.0054000273221741744 0.0002781723930706248 -0.020397312294185045; -0.007499431393528443 -0.006172539350031486 0.009727683931434809; 0.0018325203240522362 0.0006620960459014984 -0.009474022138086707; 0.002661069592679268 0.00013594745388678707 -0.010402267415427883; -0.009824826013168886 0.0012890353198453924 -0.003654828627299828; 0.026409378198227633 0.024048947468426392 -0.004238801815672329; 0.004692683373233707 -0.0029104233159847823 -0.02035884419420319; -0.02843928933717151 0.0023920987176607425 -0.0005186815846200815; 0.00010050713200058289 0.004127544412491992 -0.012878714416578002; -0.00284584978110725 0.01609299575840372 0.04158589407855917] %
+
+Mass Used: 123.80800303149863 kg
+Launch C3: 96.14552686040646 km²/s²
+||V∞_in||: 0.06835904201710302 km/s
diff --git a/archive/ES_0.5869440601660734 b/archive/ES_0.5869440601660734
new file mode 100644
index 0000000..154bc01
--- /dev/null
+++ b/archive/ES_0.5869440601660734
@@ -0,0 +1,22 @@
+archive/ES_0.5869440601660734---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-29T03:20:13.487
+Launch V∞: [7.123216398657931, -6.284460765284241, -0.04105175889434693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9079320162611607e-6, -2.9403458981907246e-6, -2.872961471462293e-7] km/s
+ V∞_out: [2.539333181783197e-7, -1.211195327456287e-6, -3.2888617174360745e-6] km/s
+ time of flight: 1.505252634741649e8 seconds
+ arrival date: 2029-02-04T07:54:36.487
+ thrust profile: [0.9819905722153244 -0.2316978241213828 -0.25361738732093203; 0.4050066696120086 0.13458253931465428 -0.3103147010772016; 0.11564599475957868 0.07447986983481863 -0.15833767958825307; 0.12679437159998055 0.10978626341620662 -0.2336953777887607; 0.06944653553255048 0.0748136891491065 -0.16969892209016244; 0.04022169441942357 0.05068371977270528 -0.12215187912722539; 0.03232674495829103 0.04581155043485796 -0.114486446823989; 0.012262842291734943 0.018787396606340056 -0.051257381342931896; 0.0046579705537010225 0.007533577952619922 -0.02043570543852701; 0.0008621494095746283 -0.0007427668433782201 -0.00032670245870450076; 0.00019027869281481054 0.0007692186433819323 -0.0014348329989578204; -0.0006891234623380626 0.001266691288315548 -0.002507576029260975; 0.00010808304381685358 0.0007546522566024747 -0.0015454646475159472; -0.00018489041632417267 0.0016946371346402754 -0.0013667190621489867; -0.0002765688894129626 -0.0003269288389728479 1.393795104840794e-5; 0.0010958419155518337 -0.003465950234110685 0.0008779893341680554; 0.0027915797652275855 -0.0023757694982543915 0.0032778178051171064; -0.00011225527942277969 -0.0004619287520830083 0.0038521818996111092; -0.0016762000197095522 -0.00416113549341274 -0.005194036027592737; -0.0005514586080027679 -0.0021613845044513727 -0.005282050381255514] %
+
+Mass Used: 158.3893955805006 kg
+Launch C3: 90.23634421941458 km²/s²
+||V∞_in||: 3.5168704348961256e-6 km/s
diff --git a/archive/ES_0.5870450590132673 b/archive/ES_0.5870450590132673
new file mode 100644
index 0000000..dc96edb
--- /dev/null
+++ b/archive/ES_0.5870450590132673
@@ -0,0 +1,22 @@
+archive/ES_0.5870450590132673---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T07:27:41.406
+Launch V∞: [6.994639315741821, -7.030777146212681, -0.9270941332749156] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6431296568134006e-5, 3.9902790882011653e-5, 2.310113963226838e-5] km/s
+ V∞_out: [3.635778610731123e-5, -2.9031063728737982e-5, -1.5196662596439652e-5] km/s
+ time of flight: 1.3718104460014954e8 seconds
+ arrival date: 2028-09-11T01:18:25.406
+ thrust profile: [0.38276361748643517 -0.13954779768542197 -0.18106774537551806; 0.13580124597204402 0.013065940505845475 -0.16450986332601358; 0.11504617051061947 0.0343557330369023 -0.2216753058026978; 0.09538218008985062 0.041278811815384835 -0.24944237241891343; 0.053906490034874334 0.030431577532012165 -0.1855266038651906; 0.03806969897522765 0.026540062916614628 -0.16509788733441264; 0.029757768184184116 0.016366816961783975 -0.12450838689383847; 0.01606511994407525 0.009958693235930946 -0.08633127667930002; 0.0030194447221563786 0.006776109155477116 -0.02714520434825097; -0.0047519441025726545 0.00026290645626062784 -0.012916650083365018; 0.0036586451875318523 0.0009812651544938498 -0.01742448448931927; 0.0017492889599911644 0.0001433529851803284 -0.004835840869443883; 0.0031461067631151805 -0.0006250529294088299 -0.001089170430434245; -0.0008124772748737026 0.0011085371544297404 -0.014672667730424837; -0.006963833357077398 0.004147528763277553 -0.004130168244858255; 0.0035554581962312353 -0.0010693476819013522 -0.004050387527366813; 0.003941176943866444 0.0014017536646518912 0.012815192587887566; 0.0030081937641283085 -0.001737697883546805 -0.019461980740516038; 0.0040012615862296055 0.0003053751754113042 -0.02529393964203411; -0.00022433229201706336 -0.005910679914323585 0.019052826977449484] %
+
+Mass Used: 106.12409402975891 kg
+Launch C3: 99.21630996898051 km²/s²
+||V∞_in||: 4.894775663289468e-5 km/s
diff --git a/archive/ES_0.5870880126574745 b/archive/ES_0.5870880126574745
new file mode 100644
index 0000000..6fd8138
--- /dev/null
+++ b/archive/ES_0.5870880126574745
@@ -0,0 +1,22 @@
+archive/ES_0.5870880126574745---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T16:54:28.601
+Launch V∞: [7.025059520552432, -7.094200404979433, -0.5804896476779443] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001536154041211486, -0.0022498178766434014, -0.00019739885148857021] km/s
+ V∞_out: [0.00017446093989923356, -0.0008025612163386776, -0.0026041118548108984] km/s
+ time of flight: 1.3323888215995851e8 seconds
+ arrival date: 2028-07-26T19:42:30.601
+ thrust profile: [0.2880886844809709 -0.11101785823157319 -0.14289078844642444; 0.15373065553968346 0.010114633091138085 -0.18044199489218934; 0.15568909429992378 0.0392051321964491 -0.29685175737026775; 0.12723774394868165 0.04663992217260911 -0.3288519900926632; 0.09231185169158677 0.03900664007241174 -0.29406772324977154; 0.046248998396580726 0.024461826406338368 -0.16506871764859654; 0.013943485378167352 0.00742562134973484 -0.06202805989674682; 0.007858412892011368 0.004429058998746406 -0.03783750912479688; 0.0011189370941590319 0.00034701374643114874 -0.005294941582229349; 0.002513992850146318 0.0011718530338887488 -0.014001417556930826; 0.005542201227655393 0.00291097534957128 -0.027998236749860086; 0.000442187956059743 0.0005478447475436404 -0.00242242155185461; 0.00015989698572697848 7.089106088205974e-5 -0.0004413856523069949; -5.0074167650252834e-5 -0.00013787665684290113 -0.0006892126294737868; -0.00015923741309599888 0.0004500074160027895 -0.00035038744761195734; -0.00015689918591301635 -3.837158177264735e-5 -0.0006897374334616459; 0.00012169518024477999 -9.311630715672277e-5 -0.0005752607647110562; -0.00015794462023412456 0.00021021813500805543 -0.0006621017358096255; 0.0005223178404118793 -0.000987415749347447 -0.0001049061398671752; 7.159175441246476e-5 -4.7084920317722555e-6 -6.504563756027561e-5] %
+
+Mass Used: 101.50871294152694 kg
+Launch C3: 100.01610888437598 km²/s²
+||V∞_in||: 0.0027313762141022626 km/s
diff --git a/archive/ES_0.5871010591824615 b/archive/ES_0.5871010591824615
new file mode 100644
index 0000000..c83eb64
--- /dev/null
+++ b/archive/ES_0.5871010591824615
@@ -0,0 +1,22 @@
+archive/ES_0.5871010591824615---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T12:08:30.504
+Launch V∞: [5.702532258142802, -7.97101945578485, -2.070800932954386] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00037379354385837845, -0.0004227187593740235, 6.8485445398975115e-6] km/s
+ V∞_out: [0.00011469469819627729, -2.453671107535359e-6, -0.0005529111810290667] km/s
+ time of flight: 1.5393009354510796e8 seconds
+ arrival date: 2028-03-08T02:30:03.504
+ thrust profile: [0.2051943154450812 -0.09199391565222995 -0.08620992620622436; 0.15457467072400632 0.0198199703146028 -0.14316464380196256; 0.15814709077043934 0.06485604769329552 -0.2247077246109251; 0.11371447620867209 0.06846096487383022 -0.21732961349448332; 0.09054688052983166 0.06881327523511381 -0.21538872072852977; 0.05563625631976844 0.049668001073634484 -0.15927165642624228; 0.0313156618316156 0.031664606906935684 -0.10445732172726017; 0.016196796222452924 0.018089409797854297 -0.061764650543097516; 0.004923002870972141 0.005671859370771181 -0.020409376004757333; 0.0002751388174772155 0.0002838703247848019 -0.0013769937020144817; 0.0013918278028810299 0.0018911218101140832 -0.007227703473042857; 0.0001449060150881737 0.00015863449466338813 -0.000561062316391852; 0.000230390919991136 0.00013283258453745858 -0.0008000722146894638; 0.0002971811833406765 0.00012446756217126837 -0.000734555171787941; -9.558937519243537e-5 -0.0001632204489278086 -6.865421613408415e-5; 0.00018026939811649912 0.0002207283152559668 -0.0007058582279342151; 0.00010912696073808182 -0.0008752923383268758 0.0008671113427477712; -0.00039405201202145587 1.8015626934318353e-5 0.00037971050443452584; 0.0001161760994992082 -0.00014418978415565325 4.762457376864882e-5; 0.00013299592831089062 -0.000133540469871162 0.0003171526755466255] %
+
+Mass Used: 99.6098250752948 kg
+Launch C3: 100.34424182358461 km²/s²
+||V∞_in||: 0.0005643223064164964 km/s
diff --git a/archive/ES_0.5871335311441194 b/archive/ES_0.5871335311441194
new file mode 100644
index 0000000..df2f846
--- /dev/null
+++ b/archive/ES_0.5871335311441194
@@ -0,0 +1,22 @@
+archive/ES_0.5871335311441194---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T18:37:46.516
+Launch V∞: [5.434343739772278, -8.212917129717072, -0.7403733728070155] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.019662043728641457, 0.1255944863199075, -0.13572184302075557] km/s
+ V∞_out: [0.13615701897437688, 0.1003305357159408, 0.07728507691061051] km/s
+ time of flight: 1.4148629942285344e8 seconds
+ arrival date: 2027-10-16T08:22:45.516
+ thrust profile: [0.37682387922207594 -0.21891311730772137 -0.17902714355703855; 0.15415126274582155 -0.005416960287735494 -0.16678631807328212; 0.13036821615828403 0.024132321995784117 -0.21542128563353863; 0.11052095434538506 0.035324945599927285 -0.24047337669744778; 0.05721057732124583 0.023283079984866947 -0.15787997904086562; 0.07268249404699917 0.03544635727270839 -0.2263864219318075; 0.04166960552685103 0.02256407854163417 -0.14918501892664363; 0.009749060669011744 0.006826660265779007 -0.03909799773918236; 0.00671917421548799 0.0034783294656849624 -0.03298193426222902; 0.0029383572004964237 0.003134352310952803 -0.014279896287292638; 0.011662687619831035 0.0003523386014060055 -0.05415743975281455; 0.0038795486855688305 0.0032113817633140024 -0.007324073426322785; 0.0002530858140196463 -0.0017624065260941424 -0.004362504118313877; 0.0025135881948391047 -0.0003896080488081989 0.004219273452918323; 0.002300150320482518 -0.005250979432100936 -0.00936601854486158; 0.003637956531264446 0.01743361482185268 -0.006871228140843697; -0.0011968867521599516 0.006345102503423985 -0.02159772076671898; 0.010661667170167088 0.0052295963857143645 -0.0035010076998165255; -0.020514263400430326 0.00040153255699844825 0.005613484656213998; -0.0010337330419041618 -0.015563296708115106 0.01998157518732921] %
+
+Mass Used: 116.0509807103499 kg
+Launch C3: 97.5322523927639 km²/s²
+||V∞_in||: 0.18595964516663033 km/s
diff --git a/archive/ES_0.5871336232045764 b/archive/ES_0.5871336232045764
new file mode 100644
index 0000000..58013db
--- /dev/null
+++ b/archive/ES_0.5871336232045764
@@ -0,0 +1,22 @@
+archive/ES_0.5871336232045764---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T10:23:19.722
+Launch V∞: [5.319197877519394, -8.397078125119375, -0.7848700092724712] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007053486372812435, 0.04238568347448679, -0.046732213658788775] km/s
+ V∞_out: [0.044922382681443905, 0.03755655658009345, 0.024511890937854167] km/s
+ time of flight: 1.3523249182508004e8 seconds
+ arrival date: 2027-08-05T14:58:10.722
+ thrust profile: [0.27892444662869503 -0.1790374920097793 -0.14082075012074832; 0.1848288569871863 -0.018237674003271996 -0.20165212981214692; 0.1538400008677427 0.016467187786634814 -0.25426210878580857; 0.12130741871783762 0.02747161580555401 -0.26354511110135714; 0.09031592093410543 0.027787109696515037 -0.23953470442134753; 0.06291419765221175 0.023056935308834438 -0.19478564928062714; 0.03732815824125178 0.015306752437202286 -0.13083100769462602; 0.020515183152628604 0.009166773365435395 -0.07943107783982513; 0.0033980145091457178 0.0018695732819432895 -0.015438970468370183; 0.001875546883136823 0.0010838469056476026 -0.008770898988571795; 0.00028133986903778674 0.00015557079218911861 -0.0013328018446382187; 6.785683346973454e-5 0.0001516947896483965 0.0002571849247149981; 0.00023894539086243157 -0.00039406008439232896 -0.00020038264876162584; 0.001360988206599158 -0.0007918998722132787 0.00030667357609654843; -0.0002877722505114118 0.00044402222126468623 -0.0006033906324530405; 5.7539285625601844e-5 -0.00107727823362955 -0.0024687139998020432; -0.0013010918241127666 -0.0025997541548285538 -0.0014901962487895441; -0.0022875649962175205 -0.0010810252208368755 -4.82349665352033e-5; 0.002155058818139158 -0.0024431035930886713 0.003936340016684936; -0.0007857298181606476 0.00028430851825127554 -0.000794549248910594] %
+
+Mass Used: 105.03451355771949 kg
+Launch C3: 99.42080803102051 km²/s²
+||V∞_in||: 0.0634838375262674 km/s
diff --git a/archive/ES_0.5871903550507221 b/archive/ES_0.5871903550507221
new file mode 100644
index 0000000..17daefe
--- /dev/null
+++ b/archive/ES_0.5871903550507221
@@ -0,0 +1,22 @@
+archive/ES_0.5871903550507221---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T19:05:01.841
+Launch V∞: [7.088421156954299, -6.975489494349887, -0.80148045216545] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007224440271207444, 0.0005677846046856201, -0.0003516412419599153] km/s
+ V∞_out: [-0.0004346943575991335, 0.000842340157925527, -3.824562936668763e-5] km/s
+ time of flight: 1.3546195650890318e8 seconds
+ arrival date: 2028-08-20T15:24:17.841
+ thrust profile: [0.3352370895446169 -0.11546660315813603 -0.15362620037762428; 0.15285636390815047 0.023681555232934238 -0.17845232573093656; 0.12213638838345178 0.04706544188875587 -0.22635361266771048; 0.09151263529795518 0.048930819513588485 -0.23102983451469777; 0.06101680274228552 0.03877838847186064 -0.19481909404613715; 0.040618034156796504 0.029643565092288226 -0.15591145464265688; 0.030762477933444998 0.025993589694268005 -0.13804697789815587; 0.022293647054501646 0.021473203351553508 -0.11572185298652919; 0.007807426386541235 0.005958790051705803 -0.04214229853104192; 0.005681234131241292 0.008486324667453617 -0.0392941798805577; 0.0012691703166792842 0.003105996119129498 -0.007917126464851815; 0.0057475772503747455 0.0017738579874662626 -0.03421951699148612; 0.00018826485889510825 -0.0005532587310184737 -0.0004632409445926456; -0.0028503715511171623 0.0010358530625785797 -0.0005934369794444917; 0.0014082783258548746 -0.0016180346245335034 -0.005948593892572408; -0.002293771582455866 -0.0015921876209596278 0.0032890899607043783; 0.0015708080367689875 0.002603307667116842 -0.003009484421725671; -0.0007664074788990146 0.0018988146390461495 -0.005930723677535307; -0.0026677233773920307 -0.000736437400685161 0.005741700462427616; -0.00033338907579319845 -0.00044853607254642067 0.003814171772481679] %
+
+Mass Used: 104.37310281298915 kg
+Launch C3: 99.54553909934629 km²/s²
+||V∞_in||: 0.000983847697912414 km/s
diff --git a/archive/ES_0.5872419214594738 b/archive/ES_0.5872419214594738
new file mode 100644
index 0000000..7035aa6
--- /dev/null
+++ b/archive/ES_0.5872419214594738
@@ -0,0 +1,22 @@
+archive/ES_0.5872419214594738---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T11:38:32.976
+Launch V∞: [5.340504987183825, -8.224300339561971, -0.13765926093749256] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.540494549933454e-5, 5.575921579041713e-5, -6.847557571158832e-6] km/s
+ V∞_out: [5.77632746982925e-5, -1.8994291719634104e-5, 1.0039891581637654e-5] km/s
+ time of flight: 1.4015103323474765e8 seconds
+ arrival date: 2027-09-30T14:29:05.976
+ thrust profile: [0.49202613117064536 -0.28815227776135593 -0.1924290673013202; 0.09480975706925467 -0.00481363892964938 -0.08895116695839571; 0.08448498943697964 0.013713354663275322 -0.12092396929146748; 0.17768217847026455 0.048585176818527746 -0.3025401419792236; 0.11657968741839793 0.04668519174668606 -0.27142272488185193; 0.08683034409454765 0.03977484946730231 -0.23928653639227612; 0.04909299962233201 0.026427165875105133 -0.14737907335159198; 0.028806221836989332 0.018826689074838768 -0.10117588692666218; 0.00854386842703269 0.005263378075881462 -0.026963928592319095; 0.007017639537693465 0.0015391938907645837 -0.028190958960820935; 0.002795502496233725 0.0011130064151390917 -0.013453634523673983; 0.0027930768694294232 -0.004647941198540529 -0.010741911780621883; 0.0042885252083490165 0.004980212921682232 -0.009406399716022371; 0.007407732260719664 -0.004645276048324009 -0.005004923035388808; 0.0032450114226991542 -7.462623499761897e-5 -0.008215615583945055; 0.00028203172908743135 0.0009873566521714466 -0.006266704910431176; -0.002112842084415683 -0.0021837719842784896 -0.005255305656665377; -0.00682948324416217 -0.008294182431912708 0.0021397407672075867; -0.0004764554971933661 -0.01987734441633915 0.006211085438317512; -0.0010088744065065852 -0.002560659258777259 -0.009159149678373044] %
+
+Mass Used: 124.07106032019101 kg
+Launch C3: 96.1790596655763 km²/s²
+||V∞_in||: 6.165541700513262e-5 km/s
diff --git a/archive/ES_0.58724946614164 b/archive/ES_0.58724946614164
new file mode 100644
index 0000000..2c1c79b
--- /dev/null
+++ b/archive/ES_0.58724946614164
@@ -0,0 +1,22 @@
+archive/ES_0.58724946614164---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T05:20:01.620
+Launch V∞: [5.381568149174851, -8.301527803146614, -0.6220385158876829] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0004760371522594299, 0.00022181553971162602, -0.0003866479279687488] km/s
+ V∞_out: [-0.00020490189288705556, 0.00047011526444789886, 0.000402879770151921] km/s
+ time of flight: 1.3923103546111512e8 seconds
+ arrival date: 2027-09-20T16:37:16.620
+ thrust profile: [0.3614509294605178 -0.20975072923487723 -0.16225106166692668; 0.10733791067898005 -0.004032163658307875 -0.11357273688926146; 0.13905272779349928 0.02652058072598768 -0.21641627930585952; 0.060602498343172356 0.01886443656596032 -0.12863658104068806; 0.09851324420339179 0.04086881597209262 -0.24102407401949624; 0.06361585381320023 0.03137698928067069 -0.1852710714357286; 0.04113023797451792 0.022549509623507567 -0.13792567720082696; 0.037986899770937804 0.022500124383622602 -0.1387228194393616; 0.011864846690634404 0.007140365806880642 -0.048307054861153824; 0.005346604030272115 0.0035106575403509553 -0.02314754835263354; 0.03183101377608104 0.016153462927532617 -0.1339719094787327; 0.0010621473876780882 0.00026467190267676576 -0.004821636572403318; 0.0006479487481009035 0.0004935835133503467 -0.004131653549167258; -0.0006996271070900702 0.00023236705064370855 0.0007609912003690351; -0.002100429188202211 -6.408558198607855e-5 -0.002862853701941437; -0.00040824311052360326 0.0007418167385275762 0.0033016828773880453; -0.0020371474374236464 -0.0003351761646556774 -0.004750533727767753; 0.007826882298640928 -0.006181985854725657 -0.002019967658236592; -0.005326196883693883 -0.004289382234669235 -0.00424092722491771; 0.0020297782542239196 0.003938315937414761 0.0030474129587132904] %
+
+Mass Used: 111.92020993096276 kg
+Launch C3: 98.26357152587724 km²/s²
+||V∞_in||: 0.0006521580515422272 km/s
diff --git a/archive/ES_0.587475649629954 b/archive/ES_0.587475649629954
new file mode 100644
index 0000000..ed00633
--- /dev/null
+++ b/archive/ES_0.587475649629954
@@ -0,0 +1,22 @@
+archive/ES_0.587475649629954---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T13:03:20.831
+Launch V∞: [5.6028898849242195, -8.135206115349094, -0.26492330330412195] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8154115792873048e-5, 0.007555901879262898, -0.003301573493212997] km/s
+ V∞_out: [-0.006428054084834493, -0.003969934910233601, 0.003294900948207906] km/s
+ time of flight: 1.4009596575098857e8 seconds
+ arrival date: 2027-09-28T00:36:05.831
+ thrust profile: [0.350689749501578 -0.2110666489320849 -0.1576327769662877; 0.12480915580761856 -0.004708780694328318 -0.1262832682785294; 0.17451853555109692 0.032140325809441456 -0.26491829576621034; 0.18464747769006656 0.058498734308616726 -0.3651257662705193; 0.08557397554108605 0.03420937181755089 -0.20660354245110066; 0.08939364995787147 0.044168132144936145 -0.25472637566033357; 0.014021124490191259 0.00813609307039863 -0.04690121706812565; 0.007463810066732202 0.005221980173642294 -0.029102182470152598; 0.01526415869146019 0.011986434811937877 -0.0661973396559592; 0.0010391260994623299 0.00217982687922056 -0.007515222878506892; 0.004810488064946394 -0.0008501610961998891 -0.00564291278111605; 0.004175684349248286 -0.003662905805063484 -0.0024685046903618066; 0.0011885990652421427 0.005334084936177805 -0.007604402591042559; -0.0023721521323691102 -0.0010417721658118417 -0.005302884694610023; 0.003060317191932239 0.0008842391233483764 -0.013277478426517853; 0.001931003888907587 -0.00032426113037487903 -0.0031886018300005194; -0.0004958395474389729 -0.0004363521170284623 -4.135979248233619e-5; 0.0017882050492073987 0.0005027818399420049 0.0013929422164365675; -0.0022158221350470817 -0.004839153956970652 0.012617430398629574; -0.002566932350306996 -0.007119935471435216 0.0015638468301562404] %
+
+Mass Used: 115.79745314408729 kg
+Launch C3: 97.64413795843298 km²/s²
+||V∞_in||: 0.0082457486204744 km/s
diff --git a/archive/ES_0.5875221490356028 b/archive/ES_0.5875221490356028
new file mode 100644
index 0000000..2a3c932
--- /dev/null
+++ b/archive/ES_0.5875221490356028
@@ -0,0 +1,22 @@
+archive/ES_0.5875221490356028---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T22:20:40.852
+Launch V∞: [6.997746240115246, -7.01843845950281, -0.5480170337198678] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.360362230630519e-6, 2.4722894227505347e-6, -1.371222617469146e-7] km/s
+ V∞_out: [-2.6715256354024598e-6, 1.6227541635231763e-6, 1.336392941717017e-6] km/s
+ time of flight: 1.3496158837527803e8 seconds
+ arrival date: 2028-08-14T23:40:28.852
+ thrust profile: [0.33433206380352953 -0.12428755833876916 -0.14849383233765298; 0.23808243068747784 0.024852169375450674 -0.2572883461123531; 0.1703010593380481 0.05313910720779421 -0.2944099517133572; 0.12066513827941046 0.05268851268467941 -0.2840183096860096; 0.07650934414282501 0.039813683929050686 -0.2267147332355557; 0.04258033242540771 0.024935337619821873 -0.15384266329218377; 0.00984205487468929 0.005542345153231448 -0.04024439475833449; 0.007049986553286167 0.005716557144650251 -0.030393223195510292; 0.008693533387252065 0.006062836997193367 -0.04897764260127011; 0.00702644468180808 0.005283008794315109 -0.040452764458504833; 0.007551077488564864 0.0037621165712028786 -0.03793185320136479; 0.001661281793936104 0.0039522129484272075 -0.003857066671678965; -0.002387122042388981 0.0018752184673702802 -0.005304796594135328; -0.00434508571799011 -0.003671708927425365 -0.008348686047960512; -0.0018767273424862643 -0.0002711035153953915 8.128848038816035e-5; 0.0010581536983730222 0.004730410948965699 -0.004422599098488261; 0.0053194595894452785 0.0020364060146013723 -0.0046436671879734855; -0.0008830179843281613 -0.0006338319564395236 0.0045024392810675395; -0.0013290367213886277 -0.0007089674290926709 -0.0018553778964596765; -0.006678405976139001 0.0004836341118140666 0.009954011311058553] %
+
+Mass Used: 110.70019500748958 kg
+Launch C3: 98.52725352012236 km²/s²
+||V∞_in||: 3.420866463967549e-6 km/s
diff --git a/archive/ES_0.5876106029527403 b/archive/ES_0.5876106029527403
new file mode 100644
index 0000000..1a6e05c
--- /dev/null
+++ b/archive/ES_0.5876106029527403
@@ -0,0 +1,22 @@
+archive/ES_0.5876106029527403---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T12:26:37.038
+Launch V∞: [6.376963717404572, -7.825527498033723, -0.7541169334913732] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.345712733249316e-9, -2.095474962761537e-9, 3.904000356341046e-9] km/s
+ V∞_out: [1.7726084497393406e-9, -4.1427386098238845e-9, -5.6872127374823865e-9] km/s
+ time of flight: 1.874957778174724e8 seconds
+ arrival date: 2029-04-17T14:36:14.038
+ thrust profile: [0.14104724760999796 -0.062036088467992696 -0.07490319183931321; 0.023469706747297096 -0.002939902668166221 -0.03405423061300008; 0.026815223876682143 -0.005818360810532937 -0.07520871685185823; 0.0355315070381621 -0.01543573506549324 -0.1497618815431327; 0.024137975681429884 -0.012386069635731016 -0.12228627186254458; 0.02550982420433353 -0.017896811802832452 -0.1519314323519654; 0.015780073987216155 -0.011391223641779675 -0.10121174673292674; 0.01061826959329044 -0.004037184404287067 -0.05158082570650626; 0.008039943747744404 -0.0005036309827766683 -0.02336596458087505; 0.001497441956175567 0.0015594184356928728 -0.00876021345549085; -0.003124407780314793 -0.005551893612426439 -0.018681022725958292; 0.0026062128853348186 0.0005253334060891779 -0.011083611416698648; -0.0009551454602862362 -0.011980752883654841 -0.00493242662525284; 0.012383418073714418 0.03783087026639973 -0.012233840346329215; -0.002819141472720911 0.011968909140408133 0.012868209051872047; -0.03699717421962144 -0.01882886689196205 -0.02079112533884447; 0.0019385616930314975 -0.046944834999783386 -0.004392141015643987; 0.008587186978589468 -0.00392515503282104 0.004067837662979893; 0.00944602174441575 -0.007768507257622726 0.01883270933561124; 0.011749091803813658 -0.025427781674786452 -0.0045299074971458155] %
+
+Mass Used: 87.78514129929454 kg
+Launch C3: 102.47323922495471 km²/s²
+||V∞_in||: 6.943261389886985e-9 km/s
diff --git a/archive/ES_0.5876109836621777 b/archive/ES_0.5876109836621777
new file mode 100644
index 0000000..e492c38
--- /dev/null
+++ b/archive/ES_0.5876109836621777
@@ -0,0 +1,22 @@
+archive/ES_0.5876109836621777---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T11:20:40.350
+Launch V∞: [6.490047970410877, -7.363726176752687, 0.20370412907279356] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1204230343560037e-7, 3.384300248423264e-8, -3.7627177419548915e-8] km/s
+ V∞_out: [1.1851611207342117e-7, -3.1660115418599534e-8, 1.4468143864657162e-8] km/s
+ time of flight: 1.844382067367015e8 seconds
+ arrival date: 2029-03-03T04:10:46.350
+ thrust profile: [0.3219880458907638 -0.08445183640904218 -0.11352502647072078; 0.05674226102310718 0.018133658217102885 -0.06749360848743301; 0.0907918009364825 0.05094255575402814 -0.16747046762847492; 0.07128313498914195 0.05361624297608657 -0.1848761694793651; 0.04624033465613945 0.04348107402295378 -0.1582476129421223; 0.024005699646025468 0.02807390334459613 -0.10484384522789157; 0.010125046752561305 0.01574010001742128 -0.05597001107577407; 0.012151806539231555 0.02098401580939068 -0.0777048828241573; 0.009271642126509065 0.007643426424658796 -0.038751563222599796; 0.006314384395733605 0.007954012536408279 -0.03862355030320349; -0.0037800087816584746 -0.002087832171965509 0.016452156095331967; 0.007554183805401041 -0.004247050628187845 0.012166149156028608; -0.004683449855739402 -0.011092015576674545 -0.006203805444796965; -0.005424075559329889 -0.010142207923884554 0.01648723848154191; 0.0247155768087311 -0.042569457444300705 0.021525595685764044; 0.022719822975129852 -0.020717782839158164 0.045085785728060074; -0.004547366610558983 0.0030836547269037103 0.046021433338166225; 0.008783101604753565 -0.0015411778450925297 0.00156871680222699; -0.08483041881919946 0.013104696047582017 0.0505362748456507; 0.0003662263729561129 0.0014954536014915513 -0.0026672409957398677] %
+
+Mass Used: 123.29050705887494 kg
+Launch C3: 96.3866812366284 km²/s²
+||V∞_in||: 1.2294157578648948e-7 km/s
diff --git a/archive/ES_0.587619467818496 b/archive/ES_0.587619467818496
new file mode 100644
index 0000000..99a05c4
--- /dev/null
+++ b/archive/ES_0.587619467818496
@@ -0,0 +1,22 @@
+archive/ES_0.587619467818496---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:11:29.566
+Launch V∞: [5.282446789688896, -8.345532588086082, -0.9117346808778791] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.990974973693761e-5, -4.0269215278928476e-5, 7.538489151922915e-5] km/s
+ V∞_out: [3.691698865967849e-5, -8.70991348682141e-5, -8.08367262396709e-5] km/s
+ time of flight: 1.3621654570453858e8 seconds
+ arrival date: 2027-08-17T05:07:14.566
+ thrust profile: [0.4147194874224143 -0.26769376214210217 -0.20863238189762054; 0.14568127772112816 -0.016217089269032575 -0.16301925315745153; 0.14243012291230195 0.01290392611400898 -0.24022449335553386; 0.11663061198252647 0.023921205638560095 -0.25889259807265047; 0.08065943975889472 0.02263273792250198 -0.22088424825303904; 0.04008254366162411 0.013496399115937602 -0.1327116837462905; 0.013029243258631727 0.0044251119561997 -0.04699955632833107; 0.01496581163304265 0.005693758985427617 -0.059957069718933005; 0.025239713418578856 0.015245101933375006 -0.15358360978897248; 0.0009000598193690409 0.0004229230283876055 -0.004193153666108957; 0.011288727159493955 0.005389617350988261 -0.056857303138472266; 0.0009410811601568664 0.00012642217823583945 -0.0024105570305039264; 0.0011699821345492445 -0.0010299219209579207 -0.0034014942735868118; -0.0006490707675196334 0.000341548181697216 -0.00019356917357177185; 0.0009197477253103844 -0.0018481148125351677 -0.0023635081554443985; 0.000500700522890472 -0.00025978974985882636 -0.00021454066274077338; 0.000660694521186315 0.007857318975519528 -0.0058207068020781575; -0.0007560365648782628 -0.00043098175379869554 0.0020683678909006386; 0.001218595357741587 -0.0011068325046563212 -0.006624138497987249; 0.001799141532553321 -0.00316952056930625 -0.00039350171625693385] %
+
+Mass Used: 111.6527718289808 kg
+Launch C3: 98.38341839301678 km²/s²
+||V∞_in||: 0.00012404940413522907 km/s
diff --git a/archive/ES_0.5876239762742427 b/archive/ES_0.5876239762742427
new file mode 100644
index 0000000..4c9171e
--- /dev/null
+++ b/archive/ES_0.5876239762742427
@@ -0,0 +1,22 @@
+archive/ES_0.5876239762742427---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-26T22:00:12.428
+Launch V∞: [8.064565329010236, -6.546023258044971, -0.4337419050692399] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004789724132661742, -0.003706741659808378, -0.00019985411341236776] km/s
+ V∞_out: [0.0038286666879398996, 0.003503513144397028, -0.003118690279843935] km/s
+ time of flight: 1.8749577787490013e8 seconds
+ arrival date: 2030-05-06T00:09:49.428
+ thrust profile: [0.003879970379186265 -0.0010045634378490112 -0.0024845359139390047; 0.0008690001702806418 0.00027048385317025945 -0.0014503313422658225; 0.013022494740163837 -0.0060964624207567285 -0.041404377074196655; 0.035084910014527904 -0.024407559257817905 -0.1396582523676014; 0.027947332780930804 -0.02417040209992932 -0.1273456813129668; 0.022826997344250036 -0.02203855977480838 -0.11231912205834155; 0.015545985637459158 -0.015658076538465845 -0.07981748236570974; 0.01847672783664985 -0.019541756392960727 -0.09614429776565461; 0.007545297222160959 -0.007878259906054745 -0.039938680943588906; 0.0005514660684677168 -0.0006738824102885414 -0.004084065646941377; 0.005822136876698727 -0.0063532943300500765 -0.03134220860420231; 0.0015941178038776276 -0.0006166684797156863 -0.004899041382362702; 0.0018566132144785933 -0.0005735268835403598 -0.003368549137523787; 2.0789674808400355e-5 0.0013557949469839496 -0.0017988150138165378; 0.001572753036139327 -0.00200662229607482 0.0005133982008152464; -0.0007993072547170671 -0.0019195191928981807 -0.0023263581680429105; -6.332286129514828e-5 -0.0034851810439320294 0.001999748139861677; 6.912591571777284e-5 0.00045812431461448016 0.00017845765071620903; 0.0027150261579313327 0.0035742967332480047 0.004235405377839336; -0.0025382737823596508 -0.0027486356706450115 -0.0018909065804951456] %
+
+Mass Used: 55.119334514391994 kg
+Launch C3: 108.07576648095277 km²/s²
+||V∞_in||: 0.006059812923367279 km/s
diff --git a/archive/ES_0.5876701828801765 b/archive/ES_0.5876701828801765
new file mode 100644
index 0000000..57f2ffb
--- /dev/null
+++ b/archive/ES_0.5876701828801765
@@ -0,0 +1,22 @@
+archive/ES_0.5876701828801765---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T14:09:34.221
+Launch V∞: [5.287684590798862, -8.29599785580204, -0.31798764889378445] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3445681142936726e-9, 4.6542757744533606e-10, 5.636503296126571e-9] km/s
+ V∞_out: [-3.6623787438099427e-9, -4.939098896184667e-9, -2.656500679888658e-9] km/s
+ time of flight: 1.361701660676542e8 seconds
+ arrival date: 2027-08-15T15:12:20.221
+ thrust profile: [0.4574616530084792 -0.28566825230118814 -0.21708028406506016; 0.18893667164774372 -0.017040395217775305 -0.20277057461685014; 0.12084637610010353 0.013714478869992023 -0.1990135406981672; 0.19551669549432096 0.047023196693100934 -0.4102185107483236; 0.06404890768685452 0.01980348837048263 -0.16927298456378012; 0.04314068415497713 0.015947256485400203 -0.13382962419565328; 0.053467237291627945 0.022392442592082725 -0.1834465083857183; 0.014719759864253527 0.007070729438027969 -0.0598333474220876; 0.0041827537362000445 0.0018967374460835177 -0.017102900651095945; 0.008233339265880574 0.0037733786794650094 -0.037571841571258535; 0.0011472108322006444 0.0007904229121012175 -0.005992153990644185; 0.00020834558810818414 0.0001891591560427856 -0.0020537336362127226; 0.0008556136145383923 -5.675234998340318e-5 -0.004117978642326993; 0.00021274184447811592 0.0003165225661183533 -0.0021393750359353543; -0.0035906739460122685 -0.0001961175864057627 -0.0009023602581768081; 0.0014945771931277971 0.00015800581667458965 -0.0007863150630316095; 0.0037805418205688387 -0.0024725853138127377 -0.0009013208711390104; 0.004099006289828198 0.0006617087030847355 -0.005521999297868666; -0.0009959919363125183 -0.0012434717897445388 0.0031271564506127197; -0.0018876454647498223 -0.0013681864981480792 0.001951813818385103] %
+
+Mass Used: 120.45676810966461 kg
+Launch C3: 96.88430490009277 km²/s²
+||V∞_in||: 5.813317095348195e-9 km/s
diff --git a/archive/ES_0.5877350040123602 b/archive/ES_0.5877350040123602
new file mode 100644
index 0000000..dd529dd
--- /dev/null
+++ b/archive/ES_0.5877350040123602
@@ -0,0 +1,22 @@
+archive/ES_0.5877350040123602---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T22:58:45.286
+Launch V∞: [5.567408427233346, -8.43074839583921, 0.024221668358586378] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.438018529867879e-5, 0.00011080939866735872, -1.9886802862441055e-6] km/s
+ V∞_out: [-2.5428495050707477e-5, 6.22400655273789e-7, 0.0001433825315336232] km/s
+ time of flight: 1.639466966364862e8 seconds
+ arrival date: 2028-07-13T11:43:41.286
+ thrust profile: [0.11021774701446428 -0.05294512170167461 -0.06022045937116576; 0.0674416705245199 -0.005912360461478923 -0.1021022889919595; 0.05567698683402974 0.0011123285674858737 -0.13744058132599332; 0.045936197860629836 0.0023813225715780336 -0.15444087516450092; 0.0375988790053221 0.002041045379080714 -0.15719904366875118; 0.0298419652524815 0.0011192718664364426 -0.1479166816934236; 0.023074133804422338 0.00015136512806196672 -0.13130449588663667; 0.017228043743203324 -0.0007315351138280396 -0.1101659118722958; 0.011616605698211893 -0.0013069180667619517 -0.08270833264055401; 0.006679586103756905 -0.0016513192883728632 -0.05303562174435912; 0.0020813688530389816 -0.001584875283885682 -0.021091035621979996; 0.00466688356089039 0.008218566836787983 0.008020347198562521; 0.00287039815647797 0.00010934160176277155 0.007980513616417804; -0.001014918263918404 0.010647509611446934 -0.004348266759928096; 0.0028438513555024327 -6.388154091969237e-5 -0.009945272699438693; 0.007574381792703813 0.0089518157977591 0.007789000796468489; -0.004864914316683182 -0.00430990238439375 0.013879899134334087; -0.0036735675481732706 -0.003743304255471485 -0.0011377086373578968; -0.005207618456308721 3.5039274883886596e-6 -0.007937334015481584; 0.004219103837514216 -0.003101605478842572 0.01043931078417229] %
+
+Mass Used: 90.25834418813156 kg
+Launch C3: 102.07414179879235 km²/s²
+||V∞_in||: 0.00014556887393710058 km/s
diff --git a/archive/ES_0.5877556860646004 b/archive/ES_0.5877556860646004
new file mode 100644
index 0000000..28013da
--- /dev/null
+++ b/archive/ES_0.5877556860646004
@@ -0,0 +1,22 @@
+archive/ES_0.5877556860646004---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T07:15:13.217
+Launch V∞: [6.793208517938518, -7.0345793499318985, -1.0502955511580199] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8594757874969025e-5, 4.5655612490137956e-5, 2.6409368363511268e-5] km/s
+ V∞_out: [4.10353825482144e-5, -3.308581079304935e-5, -1.86791627674398e-5] km/s
+ time of flight: 1.3395825260181607e8 seconds
+ arrival date: 2028-08-04T17:52:45.217
+ thrust profile: [0.8143805121050784 -0.31344483279154206 -0.43644460040077987; 0.07687899050162308 0.002985714316108446 -0.09993509299783564; 0.0924197640921758 0.019811722586205043 -0.1930820442747955; 0.07752136369368534 0.024504978995472815 -0.22178474681599214; 0.06000393762186709 0.02257751218752992 -0.21377589267176286; 0.03946841437204346 0.01635432954609944 -0.16409521871327454; 0.019473960269648 0.008770075334412538 -0.0912892424263396; 0.018237250482658614 0.008058409197622839 -0.09853380021879145; 0.006165192217753728 0.004124515713912097 -0.038566585415833035; 0.0038222096139718777 0.003352201427456575 -0.019162459481222846; 0.0003031668646422233 -0.0003807715839408074 -0.0014412386460561245; -0.0003265078406976883 0.0009265936588669179 -0.009110742325113554; -0.002404579862493575 -0.0025192516510051614 -0.005521663691375231; 0.004895868860335554 -0.0019702287695623944 -0.005322874943003731; -0.0030093179578691465 -0.00315862268818065 -0.005228283740327397; -0.002767158920280768 0.004779827569848848 -0.009586748435864366; 0.0011097733554330587 0.006636440601209132 -0.014107969348120803; -0.0005238811110486901 -0.0037668790585485214 -0.011701907560419477; 0.0013951077631002618 -0.0039877315094371995 0.0013939212767938498; 0.000877710824103292 -0.0020344569333479684 0.00026654544987380225] %
+
+Mass Used: 121.42099590516591 kg
+Launch C3: 96.73610934346306 km²/s²
+||V∞_in||: 5.5925438841711326e-5 km/s
diff --git a/archive/ES_0.5877692601479333 b/archive/ES_0.5877692601479333
new file mode 100644
index 0000000..afc066a
--- /dev/null
+++ b/archive/ES_0.5877692601479333
@@ -0,0 +1,22 @@
+archive/ES_0.5877692601479333---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T04:48:17.664
+Launch V∞: [5.428385069567149, -8.331843129286396, -0.8921769530087665] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0050294755948135424, -0.03162250520393209, 0.14419237154777056] km/s
+ V∞_out: [-0.09942515468930979, -0.09446792119067594, -0.055503834220356804] km/s
+ time of flight: 1.4005605988824677e8 seconds
+ arrival date: 2027-10-01T05:15:56.664
+ thrust profile: [0.299836767454938 -0.17345659026387844 -0.1491654378040652; 0.1007098030679579 -0.00248821156701048 -0.11724520476907416; 0.07027877171561749 0.012901895271075513 -0.1240827248450685; 0.05506244186694557 0.016009157697996768 -0.13384630037647857; 0.06486108877588243 0.029289760727702275 -0.1885071648853948; 0.06427769059406858 0.0201106229396255 -0.20343374790074426; 0.046577998265559716 0.021579492563134652 -0.16432517263532972; 0.027682078938341022 0.018029401332272495 -0.11585800668340046; 0.0325097791637575 0.017215474091872685 -0.13814279886692754; 0.015972446535804943 0.00914358595531908 -0.08441111738822926; 0.004794546355779733 0.0033079419764365453 -0.02998121420639762; -0.0008871280549923319 -0.0023229042748672446 -0.008212496104230487; -0.0033814708306613515 0.0027247027415167966 -0.01121728203786432; 0.007931024868884091 0.010412742465525666 5.747080735072317e-5; -0.006354084918065729 -0.001847713790276785 -0.005770347450285889; 2.131484725227098e-5 -0.00411299967792499 0.0006501966087222762; 0.0017931658085539822 -0.012515612067397106 -0.0019724345331578455; -0.0032080615125533235 -0.0040313790047564356 0.0007898140556946405; 0.006690488944395884 0.0025062902416226546 0.00598229347510228; 0.001032509057734241 -0.0009266330148378181 -0.0063047457290113075] %
+
+Mass Used: 104.24690453082621 kg
+Launch C3: 99.68295411001645 km²/s²
+||V∞_in||: 0.1477048356442735 km/s
diff --git a/archive/ES_0.5877951509947534 b/archive/ES_0.5877951509947534
new file mode 100644
index 0000000..c74ddca
--- /dev/null
+++ b/archive/ES_0.5877951509947534
@@ -0,0 +1,22 @@
+archive/ES_0.5877951509947534---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T04:52:54.753
+Launch V∞: [5.321900065315947, -8.526094787978664, -1.1542119703964275] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.011576798567096862, -0.015991536555684655, -0.017031035050145173] km/s
+ V∞_out: [-0.023516076249853475, -0.011241012578612349, -0.0005939175454007159] km/s
+ time of flight: 1.5254553520473862e8 seconds
+ arrival date: 2028-02-29T18:38:29.753
+ thrust profile: [0.19858094639671744 -0.11602024856198974 -0.12232070175534669; 0.034796547650796664 -0.00554754419526135 -0.055132523611150175; 0.057582818587808345 -0.00046234091408299305 -0.14529660652776602; 0.05876301680992861 0.0037592248669640086 -0.20136959065353577; 0.04739646973691721 0.004097065815949764 -0.20308133408147916; 0.03262615133372114 0.002269169691850391 -0.1665281065635678; 0.01969279186770556 0.0006008776763659544 -0.11577354307324342; 0.01094403805511427 -0.00039592298820386536 -0.07157346788261566; 0.005994065963497518 -0.0005180185005326573 -0.04290637103420542; 0.0045630490505028775 0.0001793181308453758 -0.036822865210484945; 0.0007059530885150209 0.0009323582135174618 -0.011798057436239386; -0.003120519606736847 -0.00026766597204659496 0.003237029905876547; 0.004291878432412178 5.630062607029999e-6 0.0056615084257402885; -0.0007412468966935583 -0.002539667198095684 0.0039432365283457345; 0.013689415937024942 -0.013431289913484447 -0.0024014162334286835; -0.004419760998427755 0.0021483388881819027 0.0035237807508764867; 0.00036712704936613246 0.021073518624820296 0.002374176817064696; -0.013169718083558145 -0.0010872695819115822 -0.0025905060578057257; 0.0008053562724540266 0.0012950374174076475 -0.00044352269050866285; -0.008042689730283851 0.01737828165133715 -0.023401585346544705] %
+
+Mass Used: 88.72448834396846 kg
+Launch C3: 102.34911791141323 km²/s²
+||V∞_in||: 0.026073121434807302 km/s
diff --git a/archive/ES_0.5878493318737004 b/archive/ES_0.5878493318737004
new file mode 100644
index 0000000..f3064f8
--- /dev/null
+++ b/archive/ES_0.5878493318737004
@@ -0,0 +1,22 @@
+archive/ES_0.5878493318737004---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T13:20:10.661
+Launch V∞: [5.770486844276475, -7.319346771610055, 0.8054333732713086] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1031851239860446e-6, -4.441606795780888e-6, -1.6758575694498199e-6] km/s
+ V∞_out: [1.6678277716179099e-6, -2.6768085899928735e-6, 4.201927619708983e-6] km/s
+ time of flight: 1.857206022325752e8 seconds
+ arrival date: 2029-03-08T02:23:32.661
+ thrust profile: [0.7115433312522236 -0.14472940649871202 -0.08282619017976722; 0.4108651613941364 0.17496410811422292 -0.1564173653677649; 0.3030917379600468 0.23957362888029762 -0.19054733112098388; 0.19876756919203342 0.22182353971698174 -0.18160748886180542; 0.08696152266897758 0.12006675765240443 -0.10723789566392701; 0.041312997967539886 0.06835853276526209 -0.06608512801603908; 0.016228363728713464 0.031982083172371806 -0.033054847069723316; 0.003911769022390089 0.008810909493169693 -0.009777759760662807; 0.0014637710087401566 0.003628240121974433 -0.004182516467279149; 0.0006403578344734796 0.0018696191513407987 0.0016148474507031055; 0.0005243039969645143 0.0023734759314182593 -0.0028591710990931505; 0.0010302306601529965 0.0015538088810148293 -0.0040754020046716855; 0.0016650527208108474 0.0007590809979201114 -0.0023050878859275275; 0.0005490563022836575 0.0013755834104769642 -0.0006261968346007265; 0.0028465533590845923 0.0015680141138486423 -0.0036619559125701667; 0.0002783432989654515 0.0006876293278919071 -0.0018629564203839753; 0.00010612778971516796 0.0011761326161021201 -0.00214459650120637; -3.015121964084443e-5 0.0023237505929494936 0.0010100811048522366; -0.00016615492221421575 0.0012515792109614645 0.00025188317791723135; 0.0024623379697758965 0.002125963313129268 -0.0006936809602060293] %
+
+Mass Used: 175.2904292586677 kg
+Launch C3: 87.52007850182561 km²/s²
+||V∞_in||: 5.192278612243898e-6 km/s
diff --git a/archive/ES_0.5878857311825758 b/archive/ES_0.5878857311825758
new file mode 100644
index 0000000..a56df34
--- /dev/null
+++ b/archive/ES_0.5878857311825758
@@ -0,0 +1,22 @@
+archive/ES_0.5878857311825758---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T17:33:36.408
+Launch V∞: [5.831861236286562, -7.917702911537771, -0.9073657749905406] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8391233480802835e-7, -1.1616112706820877e-7, 2.2951835002799378e-7] km/s
+ V∞_out: [1.1528269295453213e-7, -2.5720725369207796e-7, -2.501801076875186e-7] km/s
+ time of flight: 1.4756565235390463e8 seconds
+ arrival date: 2027-12-21T16:01:08.408
+ thrust profile: [0.36132236016396424 -0.185341842431525 -0.13997535068671121; 0.1945073884599691 0.01320624214321814 -0.17773899719405828; 0.16601890812913686 0.054062451177752754 -0.23093784337830298; 0.16301736248787127 0.08075664246223135 -0.2942754278138857; 0.08082846927886403 0.050439280772943254 -0.1872124434595423; 0.04624239449598787 0.03363805270277066 -0.12590213900552796; 0.03102612835142616 0.025365704290679143 -0.09692143785689808; 0.02869151377614748 0.025673120295561635 -0.09995625884754088; 0.017038098860218145 0.016647756376741464 -0.06496530609424969; 0.0007861343186175914 0.0004820689681229403 -0.00401865559100323; 0.002645923460745232 0.002834761407042443 -0.012221306897962345; 0.0010571033753149007 0.0008228812374866481 -0.002361363147918292; -7.186128224226238e-5 -0.0001314565464782617 -0.00040625944921618895; 6.398203249829499e-5 -2.690056272367403e-5 -0.0005097962640743265; -0.0005822665466796248 0.0010862042906005522 -0.0006555481977400087; -0.00025525873989900867 -0.00033898887548162895 0.0011811472295606977; -0.0006783575185867418 -0.00018328655274806914 -0.002856359558793368; -5.796468271128521e-5 -0.00036828127953824404 0.0001445995983387605; 0.001769457138356034 -0.00038723034358846163 5.1566013508342896e-5; 3.0059087643897163e-5 0.00042180504275473197 0.003990841778323479] %
+
+Mass Used: 116.97705082125685 kg
+Launch C3: 97.52393752429971 km²/s²
+||V∞_in||: 3.831165544550055e-7 km/s
diff --git a/archive/ES_0.5879551084880944 b/archive/ES_0.5879551084880944
new file mode 100644
index 0000000..c736b64
--- /dev/null
+++ b/archive/ES_0.5879551084880944
@@ -0,0 +1,22 @@
+archive/ES_0.5879551084880944---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T16:29:03.858
+Launch V∞: [7.1890298444671945, -7.245487224892431, -0.3428505256852976] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0023398111935554987, 0.015699490789199654, 0.017506583914699992] km/s
+ V∞_out: [-0.00891162205719708, 0.007859895780825044, -0.02038331131601699] km/s
+ time of flight: 1.5224750865426576e8 seconds
+ arrival date: 2029-03-12T19:27:31.858
+ thrust profile: [0.057355396117663215 -0.02286039398087026 -0.030291954841162184; 0.02275376459383009 -0.0018032075539191983 -0.036711747006461896; 0.04325478636902658 -0.0034340741356861893 -0.11543343385998285; 0.04874610953197543 -0.006105984791755139 -0.17701378371571685; 0.055526590836069055 -0.00992714323721755 -0.24496474422985579; 0.030728960700558285 -0.008479457782797562 -0.1568233543499943; 0.014641997116331958 -0.005034539282598311 -0.08100430572428076; 0.00530282389947947 -0.001249174730503159 -0.031883525875646475; 0.02297510434638341 -0.012721567266663594 -0.15205760196249832; 0.018721229296432256 -0.011308379630587485 -0.12296069890183421; -0.00031929681895618775 0.0009877274442038543 -0.0009176413326926341; 0.0011159831434986046 -0.0025334044174988132 -0.018927705752929784; 0.0015598181892728402 0.0022429774822271984 -0.008030953562354476; -0.0005447962044633173 -2.0511114483966328e-5 0.0002930406779725085; -0.000617345064673746 -0.0005808644911148378 0.0006944232986638898; -0.0008578874536170349 0.004320528043948229 -0.000629456593156474; -0.0011429534074640715 -0.000823221238064655 0.003511064189568088; 0.00031774234826440964 0.0040189169577213284 -0.0007354360388970201; 0.0047480729542994276 0.007968495385545886 0.003500462883686735; 0.0005013717847111063 -0.0016114004208623895 -0.0006159486997017974] %
+
+Mass Used: 77.54973323963122 kg
+Launch C3: 104.29678171368211 km²/s²
+||V∞_in||: 0.023631106783730736 km/s
diff --git a/archive/ES_0.5879861912044293 b/archive/ES_0.5879861912044293
new file mode 100644
index 0000000..d340be4
--- /dev/null
+++ b/archive/ES_0.5879861912044293
@@ -0,0 +1,22 @@
+archive/ES_0.5879861912044293---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T15:05:13.078
+Launch V∞: [6.320460556915011, -7.346912371281554, 0.14594891637131926] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.598550157999952, -1.2267859252568578, -0.9529416113027122] km/s
+ V∞_out: [-0.2200533467145585, 1.3968296624118044, -1.7031744209035213] km/s
+ time of flight: 1.8565129628629407e8 seconds
+ arrival date: 2029-03-16T08:53:29.078
+ thrust profile: [0.4761464079779835 -0.12030121376378572 -0.12359814618987991; 0.049517694506139256 0.011623807237521004 -0.04334684462407362; 0.18543479126369714 0.09229975654526054 -0.2614212941170441; 0.03828715670084675 0.025642046267162495 -0.08144543132527071; 0.021915782787430074 0.01672347101778244 -0.05879046477753872; 0.05763412698383061 0.06516230854968351 -0.18421731309694198; 0.014388604612700272 0.014947542410379884 -0.06445480378045824; 0.0072017033768258095 0.007150665948203085 -0.028235697554389913; 0.012906545704129871 0.009804331384621636 -0.034842122830919635; -0.009630488290725792 0.01248538914227981 -0.01779688308891388; 0.0032662886290951 -0.0029628905865989722 -0.03869711880992485; -0.004951061329939893 0.0010456043899422284 -0.0005668931264501355; 0.005562056065859692 0.005280232757434361 -0.008453500520679488; 9.608205230637076e-5 0.007531326933473446 0.010841424616729054; 0.03591540782799729 0.09258475064616871 -0.024951030632962383; 0.037625568668723755 -0.002400500630985856 0.028298454483890893; 0.0032500410199702754 0.017733961370507846 0.004175976333451013; -0.06675112549183895 0.04218679455160857 0.006640777914866796; -0.0028385732953571385 -0.00850684516165263 0.014585447490310585; 0.06690913208326718 -0.06809563109682061 0.041871310082745514] %
+
+Mass Used: 137.96179898601076 kg
+Launch C3: 93.94664412899832 km²/s²
+||V∞_in||: 2.229005165674186 km/s
diff --git a/archive/ES_0.5880849198824235 b/archive/ES_0.5880849198824235
new file mode 100644
index 0000000..af0aecc
--- /dev/null
+++ b/archive/ES_0.5880849198824235
@@ -0,0 +1,22 @@
+archive/ES_0.5880849198824235---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:31:45.370
+Launch V∞: [6.929157601626344, -7.127176822917762, -1.1958201887428574] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.577149966936001e-5, 3.6517428382718346e-5, 2.184342167573952e-5] km/s
+ V∞_out: [3.331296791081039e-5, -2.664769982255694e-5, -1.550546555668426e-5] km/s
+ time of flight: 1.3241970374888825e8 seconds
+ arrival date: 2028-07-17T23:46:48.370
+ thrust profile: [0.4568379840079166 -0.17552613963875585 -0.2309988062401103; 0.1185418152778006 0.00902948817443577 -0.14744638431694843; 0.10395243734540073 0.0290398196599878 -0.20571756725195126; 0.08052720460385811 0.032127995886008134 -0.2161441784710249; 0.06489059721682534 0.031110276415948084 -0.21608441828947147; 0.04126504843465956 0.021921852188316663 -0.16342501493951964; 0.031333812432787655 0.017825105672312186 -0.13993652416182045; 0.022104379501131078 0.013779945686532036 -0.11030585626761384; 0.00491564491540745 0.002851482627354574 -0.027487009608895607; 0.0032208834382773948 0.0018610968721680166 -0.01890823705708026; 0.00010025173277068092 0.0005741920496134894 -0.0032957795012641955; -0.001349117117168038 0.0006851210610725175 -0.006720127818621266; 0.0007300109119602652 0.000440271025685588 -0.0007643690869239392; 0.00044207883176349255 0.0005677633378099932 -0.001508063207733507; -0.0002932435569011866 -0.00016112003996753983 0.001088519143197489; 0.0006995717802045155 -0.0009651345400159802 -0.0003936661864284822; 0.0011520697375579222 0.0008259965946969287 -0.0023891362503312965; 0.00024198473490185724 -0.00018814393342716715 -0.0016363302088735613; 0.0005104747069197921 0.0006167357692437622 -0.0004982108234645736; 0.002404934400166954 -0.001435191688056333 -0.0008049324125672858] %
+
+Mass Used: 101.36655386297662 kg
+Launch C3: 100.23986045711727 km²/s²
+||V∞_in||: 4.538058889009434e-5 km/s
diff --git a/archive/ES_0.5881346979776001 b/archive/ES_0.5881346979776001
new file mode 100644
index 0000000..9a39289
--- /dev/null
+++ b/archive/ES_0.5881346979776001
@@ -0,0 +1,22 @@
+archive/ES_0.5881346979776001---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-11T13:06:08.105
+Launch V∞: [6.165279653055087, -8.191449137514265, -0.5530207858026364] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.057234353550474e-8, -7.294453665485141e-8, -4.36052649429434e-8] km/s
+ V∞_out: [2.4751190731959606e-8, -4.696009086879631e-8, 7.294449907377311e-8] km/s
+ time of flight: 1.8425779974302396e8 seconds
+ arrival date: 2029-03-13T03:49:27.105
+ thrust profile: [0.04872360809907552 -0.024301252174468074 -0.028231697220742705; 0.06549901122112 -0.020092090250594313 -0.12206309558624565; 0.022200309466829937 -0.009596801744883006 -0.0701385247535255; 0.022859704511551733 -0.01356288666429087 -0.09855108428549314; 0.021782773285265965 -0.016828783411527364 -0.11602196022189916; 0.020502832200457004 -0.019517049150484068 -0.12545733049629293; 0.0127905285861837 -0.013634683469365437 -0.08453263610740164; 0.014596084674257747 -0.017432046227703387 -0.10696306758426542; 0.007650179759331478 -0.008535879908001481 -0.05464692674245026; 0.0028749483232906495 -0.004626709288934975 -0.01884753569716842; 0.001151562816694818 -0.0010158889705799941 -0.007069172359502132; -0.0004266161283238034 -0.0013294261500720345 -0.007409634064099115; 0.00016216764996385648 -0.0002626265793106578 -0.004084320140615394; -0.0007176202028790114 0.0010101184572064554 0.0031160987954064957; -0.0013024610567726302 0.0075351480391367175 -0.0029487186217245966; 0.0009494232838441577 -0.002352212049587603 -0.005108460889812174; -0.0008989841560133106 0.0028915800711441005 -0.007477651933165913; -0.0025298751098531027 0.014861649123081603 -0.0058000228282746695; 0.0001204486702440174 -0.0038695384149114533 -0.011637209692238824; 0.00016028145483156907 -0.001208270572184195 0.000689117344368011] %
+
+Mass Used: 71.22847335993674 kg
+Launch C3: 105.41634416238801 km²/s²
+||V∞_in||: 9.417239308044722e-8 km/s
diff --git a/archive/ES_0.5881900744058318 b/archive/ES_0.5881900744058318
new file mode 100644
index 0000000..a3c82f2
--- /dev/null
+++ b/archive/ES_0.5881900744058318
@@ -0,0 +1,22 @@
+archive/ES_0.5881900744058318---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T15:36:21.919
+Launch V∞: [5.322919909006078, -8.391581561793814, -0.8851297157409431] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.877306319148255e-6, 1.7573277684381683e-6, -2.021153131331497e-6] km/s
+ V∞_out: [7.546482358533391e-6, -3.268417084044634e-6, 1.2929933488285149e-6] km/s
+ time of flight: 1.4138891976537317e8 seconds
+ arrival date: 2027-10-18T02:18:20.919
+ thrust profile: [0.2659943744748036 -0.16902921360440534 -0.14705572026868594; 0.1489803784991123 -0.018078503124249724 -0.18949847865277036; 0.10947964561568409 0.0066452834312867295 -0.2180579090009927; 0.08835949737939927 0.0136145117797691 -0.23568912713834408; 0.06573478263500526 0.014020241030582373 -0.21756216501266423; 0.04113259852779329 0.010327937448534276 -0.16121034594363742; 0.023048906976591784 0.005935133647125926 -0.10965353199956135; 0.012435427291821385 0.002928549698571101 -0.0668870466406178; 0.004633966281845522 0.003322774418346526 -0.01735558091692046; 0.0033274165202467985 0.0020614092125300137 -0.042667170103246624; -8.874341371316536e-5 -0.003955221993962108 -0.019602597793581925; 0.004269785771630961 -0.0030325336615558522 -0.0027672375644738076; -0.006164785761830263 0.005893464963702232 0.0019928965301411845; 0.002262949625466486 0.01482279651381569 0.003541275723966425; 0.0021203174299352606 -0.0031575265529039695 -0.005904192144684753; 0.02264365422726708 0.010410274395210087 0.005370827922345557; -0.01428121876555273 0.004281408489407024 0.015562752506639329; -0.0009367736861763114 -0.013524260736003138 -0.024718814521769005; 0.0016383423841580549 0.0055950574385797164 0.0002815989561630585; -0.011940188985448864 -0.003927779865650648 0.009831328689884598] %
+
+Mass Used: 105.5975830090274 kg
+Launch C3: 99.53557207961882 km²/s²
+||V∞_in||: 8.320169211723282e-6 km/s
diff --git a/archive/ES_0.58827896673426 b/archive/ES_0.58827896673426
new file mode 100644
index 0000000..35733c2
--- /dev/null
+++ b/archive/ES_0.58827896673426
@@ -0,0 +1,22 @@
+archive/ES_0.58827896673426---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T17:48:26.900
+Launch V∞: [6.943461495525909, -7.147965539801306, -0.9668508767839115] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.407751711091242e-6, 1.1459495854169248e-5, 6.272417210725171e-6] km/s
+ V∞_out: [9.56864766942824e-6, -8.531543233428322e-6, -5.072567734122857e-6] km/s
+ time of flight: 1.3268265210849933e8 seconds
+ arrival date: 2028-07-21T10:05:58.900
+ thrust profile: [0.427162127101795 -0.1718177250797117 -0.21734131840344115; 0.09309752610301635 0.003962846439004311 -0.11648308600846365; 0.09386955722919525 0.020914782041336222 -0.18782908586406005; 0.11538639345770005 0.03665849229567188 -0.3085157238843405; 0.07098927459385079 0.02696368122681624 -0.2370820236868931; 0.04031200376142896 0.017024011374798628 -0.1589020879848777; 0.035016614694068464 0.015714445858979936 -0.15577465743738284; 0.013842461122977488 0.006347796388363867 -0.06782317313406525; 0.004837687121468958 0.002124427013572115 -0.027449990538283217; 0.0006109919208952199 0.0006027395951012969 -0.003655084314670202; 0.001051175969569048 -0.00021092697143239433 -0.005342291440534335; 0.0021771743056630895 0.00020072652030647556 -0.013425866715690819; 0.00023551957716384385 0.0005413220003928282 -0.003292751905511771; -0.0003973570681130396 0.0007918980465253418 -0.0036035478286654717; -0.00011486017438593348 -0.0003483282484767502 0.00042850371066587966; -0.00037821586881616105 1.0927459326752834e-6 -0.0018492995883161295; 0.0007659224558897479 -0.002011849520121732 0.00018698638328115387; -0.0002068682702732052 0.0031444031956191576 -0.00794778424952907; 0.001376872875306963 0.00034142386872971695 -0.0008620196839591083; 0.0002875702458422013 0.0023230478032396926 -0.005316944461310216] %
+
+Mass Used: 101.59288901344507 kg
+Launch C3: 100.2398695159757 km²/s²
+||V∞_in||: 1.3787368786093714e-5 km/s
diff --git a/archive/ES_0.5882790888759154 b/archive/ES_0.5882790888759154
new file mode 100644
index 0000000..9b01fbc
--- /dev/null
+++ b/archive/ES_0.5882790888759154
@@ -0,0 +1,22 @@
+archive/ES_0.5882790888759154---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T11:48:48.445
+Launch V∞: [6.894699293185804, -6.986329155051416, -0.8557595909742116] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.833218979531691e-6, 7.865215552837517e-6, -4.4019101439907756e-7] km/s
+ V∞_out: [-8.375787436979905e-6, 5.477543024349753e-6, 4.813052216364082e-6] km/s
+ time of flight: 1.3236865764316982e8 seconds
+ arrival date: 2028-07-15T12:53:05.445
+ thrust profile: [0.6705800046222018 -0.2578716165847157 -0.30341354182955643; 0.15484269605250883 0.015627214036796195 -0.17128026577227196; 0.1294871845968662 0.04087077703434802 -0.22720923112289185; 0.08548161225788405 0.03816876390666102 -0.20379293726002268; 0.07819124754017921 0.04191091296207891 -0.22979717280924888; 0.048679950454953345 0.029941870512492082 -0.17074625485605918; 0.042402945804863236 0.028069916703257067 -0.1673341826335061; 0.012073551715893874 0.009381687606446008 -0.056434395063088755; 0.005073696203051399 0.0037955972795215625 -0.026273675178175932; 0.009434067680814628 0.007960959571605775 -0.05528112521419601; 0.003202531897829612 0.001345427321420659 -0.021779961612143697; 0.00048464064674553586 0.00041921158392913216 -0.0027453980087597724; 0.00038234226212993704 0.00024936129051811166 -0.00043158811968387; 0.00010043003351074237 -0.00054982103015502 -0.0008291234869873255; -0.00016270475779199214 -0.0005691173619469714 -0.0007130775685492276; -0.0008274539866999398 1.563476838209262e-5 0.00015513635013374963; 0.0009828886290281064 0.0009612813674212878 -9.526575549309254e-5; 4.1805397570243176e-5 -0.0010186923435747198 0.0006700346495230136; -0.0003632440297328379 -0.001025456580268471 0.0016572395296867032; 3.560834797524603e-5 0.0008210150680470984 0.0002586531805521017] %
+
+Mass Used: 120.0372827001861 kg
+Launch C3: 97.0779978837226 km²/s²
+||V∞_in||: 1.1109217047256317e-5 km/s
diff --git a/archive/ES_0.58827928873153 b/archive/ES_0.58827928873153
new file mode 100644
index 0000000..7c7fb79
--- /dev/null
+++ b/archive/ES_0.58827928873153
@@ -0,0 +1,22 @@
+archive/ES_0.58827928873153---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T21:08:16.342
+Launch V∞: [6.7790504067927095, -7.002680441567542, 0.4347945371704661] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.905866654157461e-6, 3.7167909344662316e-6, 4.083501408576955e-6] km/s
+ V∞_out: [5.65194340241746e-6, 3.70545280028129e-6, 1.1258326808982643e-7] km/s
+ time of flight: 1.8749577787478676e8 seconds
+ arrival date: 2029-03-28T23:17:53.342
+ thrust profile: [0.5339369044214768 -0.11420077474391374 -0.09117161361358554; 0.2330750619711122 0.1014563651863294 -0.13451611116072384; 0.20375667875956185 0.16585271632756104 -0.21997150703299126; 0.08514448363366585 0.09284821420062239 -0.11855461236037558; 0.03780827708608113 0.05508195866657985 -0.07505234646329184; 0.038812679179508904 0.06341232299848695 -0.09097929149098742; 0.03330722915896628 0.06354796958477575 -0.0929204961807148; 0.0025694239947855564 0.00578697925805684 -0.00911488983365253; 0.006611390263338745 0.017085610575008608 -0.02828787662040357; 0.0009464805643286446 0.0005039261228757326 -0.0018807481904300426; -0.0006182308970539149 0.0009467574744617867 -0.0017316021220975199; -1.8871728156404045e-5 0.0012763421920172595 -0.0021995086363794845; -0.0003883316628353144 0.0002759761765830568 -0.001591205395683574; -0.00014842149179146528 9.439292194051764e-5 -0.001704394998913415; -0.00019330019622375424 5.5866751582289145e-5 -0.0004222045740234577; -0.0013338933373450899 0.0015701803201340152 0.00095039045942094; 0.0005754727888155469 0.0006966101203389726 -0.0002070343498931026; 1.6958112819414912e-5 0.0017243646714553526 -0.0022065711217757224; 0.0003130486654894292 2.249188566629252e-5 -0.0007640063429310744; -7.155090143424393e-5 -0.0004345227422227442 0.0014506703202071727] %
+
+Mass Used: 131.09689642118838 kg
+Launch C3: 95.18210407410227 km²/s²
+||V∞_in||: 6.7635281417644405e-6 km/s
diff --git a/archive/ES_0.5883493793059769 b/archive/ES_0.5883493793059769
new file mode 100644
index 0000000..dc967a4
--- /dev/null
+++ b/archive/ES_0.5883493793059769
@@ -0,0 +1,22 @@
+archive/ES_0.5883493793059769---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T01:47:41.596
+Launch V∞: [5.419786215543627, -8.289265637068192, -0.0020657576392596935] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.161164750702714e-6, -1.463888310896484e-6, 1.654993561748891e-6] km/s
+ V∞_out: [-6.101258784533251e-6, 2.15281182058014e-6, -1.0387937532699166e-6] km/s
+ time of flight: 1.4151815878523672e8 seconds
+ arrival date: 2027-10-18T00:23:39.596
+ thrust profile: [0.3158341671790177 -0.19411013448313336 -0.1533769229961102; 0.14085854096655703 -0.012122292184143586 -0.16170948913599642; 0.11416909051867283 0.01187282230882455 -0.2026190731296829; 0.0910778955447482 0.0189628997744898 -0.2135652019504951; 0.060288984046339936 0.015604664298892488 -0.17536630959958527; 0.04951911878968661 0.01221198156277643 -0.16753448613166508; 0.0371952919293616 0.009141506844431943 -0.15157536753114248; 0.0420120209722062 0.016917157221253403 -0.17971479736607066; 0.022416216236115023 0.007793791598300929 -0.10830127573460327; 0.006735956030313833 0.005354054966782673 -0.03584292848273948; 0.0034906356837027626 0.0036174744995413196 -0.0018663734949127654; -0.003147990911669273 0.007623002820296206 -0.004384197134235372; -0.0003073432382579943 -0.0011345739170768754 0.003441432131168547; 0.0027842673652073674 0.0004055886442456239 0.0023543222830475575; -0.0023981206931910025 -0.010478701263508342 -0.009191452504519072; -0.001061397663093174 -0.0006074731399077147 -0.0022971485217594657; 0.002490481019995189 0.018320156559691835 -0.007070850255174286; 0.0005927447887669559 0.0022613858711372364 -0.0008393766717568762; -0.003239625774743335 0.020535015016540148 -0.002229934046527776; 0.0024450624376769602 -0.008197348614526633 -0.009646600833896566] %
+
+Mass Used: 114.23920765695948 kg
+Launch C3: 98.08601169143088 km²/s²
+||V∞_in||: 6.545374226238808e-6 km/s
diff --git a/archive/ES_0.5883610744157816 b/archive/ES_0.5883610744157816
new file mode 100644
index 0000000..cf15f9f
--- /dev/null
+++ b/archive/ES_0.5883610744157816
@@ -0,0 +1,22 @@
+archive/ES_0.5883610744157816---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T19:41:26.557
+Launch V∞: [7.71907523890771, -5.8783384096799205, -0.4711082084660886] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000267012045285173, -0.0007080164503659133, -0.0016781352782599197] km/s
+ V∞_out: [-0.0016858628985917344, -0.00021333717581857868, 0.000710695310194687] km/s
+ time of flight: 1.7949792806126526e8 seconds
+ arrival date: 2030-01-09T08:13:34.557
+ thrust profile: [0.34140349362860384 0.009022484557997357 -0.060089438533399146; 0.23278048298903048 0.16605761859381438 -0.1222193333239506; 0.15942314992323084 0.19733764066286189 -0.1486094299073268; 0.10464705473705802 0.18407350078444132 -0.1484613982284591; 0.07341392168665653 0.1733387094837713 -0.14822431168034364; 0.04200532428610232 0.12898608170612183 -0.11873749218037727; 0.0232749611067237 0.09133876908095497 -0.08998958081066014; 0.012529702269279524 0.06294263123019316 -0.0652849340809753; 0.002036591539095545 0.01340619318364361 -0.015188416000398402; 0.0008398020372132063 0.003237754517175385 -0.006329767580531509; -8.374091369788965e-5 0.0002277029058453668 -0.0006606909092421924; 0.001538846804579399 0.000685905499253096 -0.001838151610308862; 0.00015892174258018275 -0.0009914443085456705 -0.0019303076946173454; 0.0004976819934314964 0.0016727039035092934 0.0004130053543508032; 0.00016179776062234108 -0.00027327355180400146 0.000740196893192363; 0.001052113024760056 0.0008823652496722177 0.0012855303525359527; 0.002162323105796712 0.004807819052123604 0.0023110663303801703; 0.0005626720770508301 0.0028760941857206026 0.00099949776395543; -6.221235864148708e-6 -0.0008825589628298517 0.0014128382437994507; -6.443783179567682e-5 0.001392288992532386 -0.0021435364385037035] %
+
+Mass Used: 135.9825071292089 kg
+Launch C3: 94.3609279467205 km²/s²
+||V∞_in||: 0.001840847831423504 km/s
diff --git a/archive/ES_0.588454441140699 b/archive/ES_0.588454441140699
new file mode 100644
index 0000000..001f76b
--- /dev/null
+++ b/archive/ES_0.588454441140699
@@ -0,0 +1,22 @@
+archive/ES_0.588454441140699---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-12T19:18:29.391
+Launch V∞: [6.218511807174369, -8.121596234238922, -0.6596846129156447] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.426815953567997e-6, -9.829881475575027e-7, 2.224173347165342e-8] km/s
+ V∞_out: [1.4344204894772163e-6, -3.104785583124528e-8, -7.352697291453586e-6] km/s
+ time of flight: 1.874957778140453e8 seconds
+ arrival date: 2029-04-20T21:28:06.391
+ thrust profile: [0.15450132586796395 -0.07592658018862748 -0.08393020021981017; 0.005834741746978498 -0.0012367282537425468 -0.011151704629734194; 0.031028477372374436 -0.018662245082555713 -0.10632242126031669; 0.03568979298742148 -0.030978345001829666 -0.16599165198839275; 0.02308985134274039 -0.02307062478650833 -0.12604534056794287; 0.01990373086559234 -0.023099103132258884 -0.1222241769532323; 0.011812140934162779 -0.012159275903530341 -0.07622409104079049; 0.008470898831932697 -0.008566788875905004 -0.05879286734796722; 0.004508752594849701 -0.005277144842552985 -0.0342774090556578; 0.0030335930200541643 -0.004095991742576776 -0.024552499281814046; 0.0006501445052312128 -0.002079422304599382 -0.006502822986839963; 0.0009696274644446688 -0.00028446640144015833 -0.00036579377375517376; 0.0007637103339681141 -0.0009546232727890675 -0.0010494544942610219; 0.0019264496482193447 0.001043699869526909 -0.0019683106174001874; 0.0024049888765963114 0.00041481855073450375 -0.004123448034764388; -0.0011575140548834052 -0.001678817157921625 0.0016448894541098837; -0.0017085712704895469 -0.00010031300820180196 0.0033292955162559173; -0.004809942189863329 -0.0063313665742167225 0.005853905522038688; -0.0029524992921800193 -0.006603875499492249 -0.002556619148593945; -0.0006195211546807244 0.0016595505041068913 -0.0006311398259254336] %
+
+Mass Used: 73.64869138463246 kg
+Launch C3: 105.06539827648854 km²/s²
+||V∞_in||: 7.491619024024011e-6 km/s
diff --git a/archive/ES_0.5884679824641951 b/archive/ES_0.5884679824641951
new file mode 100644
index 0000000..db19efc
--- /dev/null
+++ b/archive/ES_0.5884679824641951
@@ -0,0 +1,22 @@
+archive/ES_0.5884679824641951---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T00:25:42.542
+Launch V∞: [5.333846075043146, -8.34450394911474, -0.9019907515228539] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.020139403466977453, -0.04526087021144644, 0.006586149063842206] km/s
+ V∞_out: [-0.046355998684804826, 0.01623046933913006, -0.008040587597871747] km/s
+ time of flight: 1.357957259634547e8 seconds
+ arrival date: 2027-08-11T17:27:47.542
+ thrust profile: [0.3870745127857515 -0.23467671962221498 -0.17796461748608833; 0.1286604971340104 -0.007271977841580822 -0.1369389856794853; 0.10795984801321463 0.018239491701627777 -0.17243289225578176; 0.09715709152770233 0.03027599540897891 -0.20168217488954; 0.09381616139186309 0.03801652262008244 -0.24216762383419305; 0.054890448332697184 0.024378007102427112 -0.16041020425628633; 0.054882481995222464 0.028413240210588254 -0.17888346322802778; 0.044128781225791794 0.024551109562401485 -0.16038683993347225; 0.013852550992125828 0.007921560383418961 -0.05535544530366155; 0.005651108515218556 0.002341032118728559 -0.02201476197963978; -0.0003226155412202256 0.0011126442159344232 -0.0026851774156031903; 0.0010678182147855495 0.0006528990165561668 -0.00533849984463439; 0.0010195564811096834 0.0006096684833622511 -0.004723649860887644; 0.0017683764401252304 0.00255688411811952 -0.002242584849093783; -0.0026904812613436566 -0.003911523036174444 -0.003925476479673239; 0.0002887776738085008 -8.093159215767642e-5 -0.002642582279118849; 0.0017043127863533693 0.0016782614847239091 -0.011680798099865242; 0.004594060634934005 -0.0028818374953099553 -0.006019920797781986; -0.0016186171086611792 -0.0014030964989128801 -0.004911375654891994; 0.0004892623172561088 0.00023490614967586372 -4.1612805279947224e-5] %
+
+Mass Used: 109.66286956310933 kg
+Launch C3: 98.89424742487742 km²/s²
+||V∞_in||: 0.0499751868810338 km/s
diff --git a/archive/ES_0.5884958453229425 b/archive/ES_0.5884958453229425
new file mode 100644
index 0000000..a1ba8ef
--- /dev/null
+++ b/archive/ES_0.5884958453229425
@@ -0,0 +1,22 @@
+archive/ES_0.5884958453229425---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-29T15:04:20.218
+Launch V∞: [7.276494332386138, -6.3812848524117145, -0.2862982740819264] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.931274652227238e-6, 5.085255093295321e-6, -3.972821614114196e-6] km/s
+ V∞_out: [1.6787247757586115e-6, 8.587558137856495e-6, -4.1891822751591244e-7] km/s
+ time of flight: 1.4959489258587867e8 seconds
+ arrival date: 2029-01-25T01:12:32.218
+ thrust profile: [0.5771077251828379 -0.13860002368672278 -0.16481891331665627; 0.38401274557502796 0.12679446277872047 -0.29834197279118835; 0.22225017843378278 0.14241693822068457 -0.29022859928205913; 0.14544701858007236 0.12726997725179365 -0.26713394306993166; 0.0800771090290568 0.08553872509390227 -0.19079033749973567; 0.03363216079832967 0.04175606988875678 -0.10029579493370179; 0.022210758557567906 0.030543141920234877 -0.07492252124165509; 0.0020390187967272706 0.00328533111557706 -0.010244232266628621; 0.00011618727959836163 -0.0013732385882614458 -0.005184939411101974; -0.0006037509062280242 0.0001785140940420586 -0.0012761900831617418; -0.00023085533018759436 -0.0028607090939215957 0.0021339686824153967; 0.00021179544500142273 -0.0006899944352314951 0.002983650324348844; -0.002869268065439091 -0.005643242187585641 0.0011271596482343997; 0.00077729116576668 0.006106718288844121 0.00033585802829691393; 0.0041396772333491625 0.0009330069290358078 -0.012372139915769818; 0.0010898773783343443 0.0014016670144303446 0.0004924296566118959; -0.007290697306341517 0.00196203334729474 -0.003979314480390338; -0.00031535446612841137 0.0008390994539393421 -0.0026467267587199717; 0.009325038768950591 0.00883176448050758 -0.010378166538567768; 0.0004505775975028896 0.0015883356156765841 -0.0030517936307959837] %
+
+Mass Used: 139.70271131821346 kg
+Launch C3: 93.75013283860906 km²/s²
+||V∞_in||: 8.764881627358824e-6 km/s
diff --git a/archive/ES_0.5885230256243036 b/archive/ES_0.5885230256243036
new file mode 100644
index 0000000..574514a
--- /dev/null
+++ b/archive/ES_0.5885230256243036
@@ -0,0 +1,22 @@
+archive/ES_0.5885230256243036---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T23:36:39.542
+Launch V∞: [5.4091048971290325, -8.282590969507776, -0.6255449435324507] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00014378701822437702, 6.294780148211312e-5, -0.0001143721107105596] km/s
+ V∞_out: [-4.476106496964864e-5, 0.000148217297878191, 0.00011722583059952925] km/s
+ time of flight: 1.4168809102950296e8 seconds
+ arrival date: 2027-10-19T21:24:50.542
+ thrust profile: [0.28401907544873073 -0.17257200332475836 -0.14181944028908064; 0.18792140754967596 -0.01457482488937606 -0.21147975256250678; 0.13443089839344366 0.01647063571085265 -0.2334268582092854; 0.09602689958411072 0.022675507679729427 -0.2206825610180166; 0.071906508838992 0.02244574412842954 -0.20154271479513863; 0.04093916314469986 0.014462538374285733 -0.13173828063849394; 0.04092574693162532 0.016854228630554653 -0.15059646991754827; 0.016519914172355588 0.00793333603168905 -0.06338110700009074; 0.009748154953515846 0.0047279806894455 -0.04056029248701161; 0.007354597770878847 -0.01528087215524838 -0.02918014035112078; 0.011603430766262166 0.007856208046630052 -0.05210487473933107; 0.005443736085037319 0.0016114769325810204 -0.011260584634345004; 3.206362068602735e-5 0.00696174799996511 -0.014552496409168912; 0.0008814437027630214 -0.0015926866890717047 -0.0007501052905642556; -0.01071236580684505 -0.018017885723490577 0.0002303189226686847; 0.007470193230944855 0.007393746849426102 -0.004583280281227701; -0.01515661116614821 -0.027326755771587007 0.008686480877564247; 0.02889954516824374 -0.017464265584072852 0.028442999036586716; 7.424303492133735e-5 0.004700637077320282 0.0012886034573628127; 0.0012254343244031706 0.0008994950156763605 0.0037475116243666567] %
+
+Mass Used: 113.4791565376272 kg
+Launch C3: 98.25103543269606 km²/s²
+||V∞_in||: 0.00019421151363829424 km/s
diff --git a/archive/ES_0.5885491399301148 b/archive/ES_0.5885491399301148
new file mode 100644
index 0000000..c50a971
--- /dev/null
+++ b/archive/ES_0.5885491399301148
@@ -0,0 +1,22 @@
+archive/ES_0.5885491399301148---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T06:39:57.886
+Launch V∞: [6.853114859011112, -6.958442375959705, -0.7951400610039125] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002054030686794056, -0.0030837063334903806, -0.0002651324083885203] km/s
+ V∞_out: [0.0002499016232107122, -0.0010966744336936944, -0.003539742349474433] km/s
+ time of flight: 1.3346985161238495e8 seconds
+ arrival date: 2028-07-28T01:37:28.886
+ thrust profile: [0.7038531595437564 -0.26596221825827904 -0.31064931109850985; 0.205978186020037 0.02216416514732568 -0.22331697901972597; 0.14590284355971936 0.046387267970144815 -0.25260961543256116; 0.11221412264085154 0.05133210270373155 -0.2660630696132619; 0.07130927186627481 0.040004710122528375 -0.213791941141409; 0.034095575487007555 0.022060733666885636 -0.12195337331506252; 0.019429280887465487 0.015114875803381103 -0.0837766352247928; 0.0066322649803207435 0.005193258444748451 -0.03211416221317009; 0.0034373584231382056 0.002949176267639961 -0.018968238962636007; 0.008476101696915159 0.00833978339106682 -0.04963849475372428; 0.014918711929270237 0.01075288533963455 -0.07737605025517431; -0.0014625877757463495 0.0005871010344317975 -0.008254159468221074; 0.0012311260050494892 -0.00017832700433896825 -0.006911809391233204; -0.001392374678926772 -0.0033443354035571724 -0.0016626922306088822; -0.0026333510883196068 -0.000663230773866512 0.0006766258295893765; -0.0005797831569415782 0.0025578821341191347 -0.0019145575674585132; 0.0029628345673053972 0.0031405102572948 0.009438686885195715; 0.0006342229734072574 -0.00040370402261871523 0.0005153745799120694; -0.000597599694170737 -0.0027027362595706712 -0.0022865626748837034; 0.004292552050792009 0.0010565989258274025 -0.002887592611144349] %
+
+Mass Used: 126.53944741117766 kg
+Launch C3: 96.01735128696393 km²/s²
+||V∞_in||: 0.003714644263920604 km/s
diff --git a/archive/ES_0.5885685218242064 b/archive/ES_0.5885685218242064
new file mode 100644
index 0000000..7763bea
--- /dev/null
+++ b/archive/ES_0.5885685218242064
@@ -0,0 +1,22 @@
+archive/ES_0.5885685218242064---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T21:01:10.762
+Launch V∞: [5.374078448658603, -8.356990740994235, -1.2763555140768466] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.04573310475192974, -0.08383381249758345, 0.012113109025249136] km/s
+ V∞_out: [-0.08993976123275164, 0.03028780464042054, -0.016174377148768966] km/s
+ time of flight: 1.3435725697898695e8 seconds
+ arrival date: 2027-07-25T22:28:46.762
+ thrust profile: [0.28740686850103736 -0.19656686825726172 -0.15465801338228807; 0.19348196061009965 -0.018692490532582064 -0.21097286323687375; 0.12594869308045353 0.016329470337208964 -0.21028750908936675; 0.11020162399250591 0.027931823713581664 -0.2419894074668802; 0.0851182808740708 0.029728004513129257 -0.22800807395762812; 0.058110297564519506 0.025439913205032638 -0.1811201559428191; 0.03810893043680676 0.01941674006905791 -0.1339654138926768; 0.017275972856585307 0.00900677749794284 -0.06840246061725054; 0.004728460860029149 0.0023158408490319532 -0.019964019562718427; 0.00569923333144435 0.00239302905460394 -0.028555172174777273; 0.0004057670673765963 -8.557627593130772e-5 -0.0019118896244690125; 0.0008420237143985636 -0.0006957810803577011 -0.001810589133370478; 6.124542554183048e-5 -0.00010381562612189413 0.00022173106919044067; -6.785340407604036e-5 0.0008910857441100532 -0.0011382827508062238; -0.0001775961613162487 -0.00032737743758590594 -4.6726512903354364e-5; 4.4255529959272635e-5 0.00016749452724795994 0.00012393737659724792; 0.0007011153953433175 0.0002960224233373163 -0.0025544222131648826; 0.0006721496254319557 -0.00029285757613665996 -0.0004311945404152529; 0.0020731775745733917 -0.00122943047453837 0.0021436168893406633; 0.00013129136926422167 4.512835560399104e-5 -0.000624687140194243] %
+
+Mass Used: 101.29354403657226 kg
+Launch C3: 100.3490968157146 km²/s²
+||V∞_in||: 0.09626189484104565 km/s
diff --git a/archive/ES_0.5885932693951594 b/archive/ES_0.5885932693951594
new file mode 100644
index 0000000..e01a3dc
--- /dev/null
+++ b/archive/ES_0.5885932693951594
@@ -0,0 +1,22 @@
+archive/ES_0.5885932693951594---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T10:39:06.556
+Launch V∞: [6.935273317858108, -7.0781430642738625, -0.7979033083983202] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.014875903622766137, 0.08250078208714183, 0.08507276463372289] km/s
+ V∞_out: [0.10482660447822807, 0.012485097542691836, -0.05582437084451779] km/s
+ time of flight: 1.3279622639445615e8 seconds
+ arrival date: 2028-07-21T10:29:32.556
+ thrust profile: [0.4618936075918331 -0.1702741617302844 -0.2017121415639156; 0.17819944211105468 0.018978298873513683 -0.19652848468358336; 0.1302800578172851 0.03989465866783174 -0.22983525718279416; 0.039074852249387323 0.017634932639303835 -0.09798393668218232; 0.10448814739613892 0.051197810137969355 -0.2921882189814004; 0.059423441556405394 0.03536254139348183 -0.206862259469803; 0.023033247041602027 0.01514713810024229 -0.09451425635102052; 0.02190003225416716 0.015656934369976748 -0.09892185026587264; 0.022888203912114193 0.016944983914482042 -0.11265893969243862; 0.0016975837279681457 0.001143236487798912 -0.009439907254499754; 0.004989503472494281 0.0016280780536392248 -0.022752540691966732; 0.004362551213042076 -5.407740664995869e-5 -0.018375977325447337; 0.00033860408983785135 0.0003614412973383717 -0.000776437468917864; 0.0014551869671008241 -0.0002620470454686086 -6.895474954574435e-5; -0.0005506265257454443 0.00033277100515650753 -0.0008284735385107912; 0.0004918939218725756 -0.0011811597483456047 -0.0001566023489916942; 0.00023786526126320774 -0.0010999351200844363 0.00033512493480729604; 0.0002400725003090439 0.0009520430299618552 0.0008212352837237861; -0.00024279061567074529 0.0002609708424807604 0.00031134249001895737; 0.0016975016559710664 0.00034101014575427593 -0.0001411938309979] %
+
+Mass Used: 110.15596058691062 kg
+Launch C3: 98.83477492127578 km²/s²
+||V∞_in||: 0.11943637149549001 km/s
diff --git a/archive/ES_0.5886891649276189 b/archive/ES_0.5886891649276189
new file mode 100644
index 0000000..64fa412
--- /dev/null
+++ b/archive/ES_0.5886891649276189
@@ -0,0 +1,22 @@
+archive/ES_0.5886891649276189---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T04:10:16.091
+Launch V∞: [7.041066522314854, -7.095198285094309, -0.9885419372187442] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.0432885463164185e-5, 7.931392305602057e-5, 4.5763666272748306e-5] km/s
+ V∞_out: [7.002783837006835e-5, -5.685401101802162e-5, -3.520506632123199e-5] km/s
+ time of flight: 1.3396808031058851e8 seconds
+ arrival date: 2028-08-04T17:31:36.091
+ thrust profile: [0.29104801391286506 -0.10984623464198079 -0.14337503016664216; 0.1344114298917115 0.011674312393343388 -0.15912205572547114; 0.10939392814662358 0.03148147823142224 -0.20684767999470047; 0.08326665655010038 0.033778954224853046 -0.21317867664781714; 0.05052802875950683 0.024505709715847576 -0.16219576066161023; 0.03438915921265553 0.018650411595974515 -0.12957190883706177; 0.02098675055130835 0.012214481065454256 -0.09347956478952904; 0.04774748666437371 0.030464885234235167 -0.22768510520929594; 0.019793648627909628 0.013012689645822825 -0.10367555297465711; 0.00397582800599255 0.00242694348525209 -0.017832341575681046; 0.004073118990722538 0.002669038541176956 -0.023513176116459103; 0.003210962421162122 0.0017935170618974313 -0.00030316506619371304; 0.001661237336263652 0.0022445398587709517 -0.003429773885718009; 0.00047146460664553936 0.0003850740632591961 0.0026812835049744585; 0.0007215530840255302 4.099883300069532e-5 -0.0023977560281703398; 0.0006477551916712173 -0.003433249317384951 -0.0026074100760618167; -0.005789718492357704 0.0012391004528196985 -0.0030930088650613155; -0.0020194175157446145 -0.002441710434106014 -0.0008937227639049254; -0.0008145261488592451 -0.001318289178107956 -0.0009788700315737577; 0.005474111132012174 -0.0026983360819546496 -0.002494659174822112] %
+
+Mass Used: 98.24594119325639 kg
+Launch C3: 100.8956716381084 km²/s²
+||V∞_in||: 9.649441465118021e-5 km/s
diff --git a/archive/ES_0.5887182296621868 b/archive/ES_0.5887182296621868
new file mode 100644
index 0000000..d673658
--- /dev/null
+++ b/archive/ES_0.5887182296621868
@@ -0,0 +1,22 @@
+archive/ES_0.5887182296621868---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-12T17:27:16.256
+Launch V∞: [6.255955503892355, -8.07530697763814, -0.2822732349176518] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008846803979823591, -0.0010542946613089814, -0.0009071451573117381] km/s
+ V∞_out: [0.0010899081207049997, 0.0005419861246243071, -0.001112794826389207] km/s
+ time of flight: 1.8746150361263677e8 seconds
+ arrival date: 2029-04-20T10:05:39.256
+ thrust profile: [0.17419080598013437 -0.08941916475078808 -0.09308596956897426; 0.008770931655852557 -0.0038199555839672247 -0.017283862738088733; 0.023005141556845535 -0.01816729418065593 -0.08114904018591944; 0.029452663855245788 -0.033292570308648954 -0.140987320855788; 0.023315303742795897 -0.031793843060566374 -0.13155558012980836; 0.02032418470183216 -0.03112912423534157 -0.12683015817092128; 0.019226744655813817 -0.0319039103822194 -0.12784162165905152; 0.008918295056795368 -0.012430807656490054 -0.058899348118119726; 0.00533624661774494 -0.006245615087063564 -0.035682610584309035; 0.00280836000663635 -0.003107237436028278 -0.018906761724127686; 0.0010720066958530687 -0.001482513894675018 -0.007401029368018728; 0.0006271583631380213 -0.000720361270954579 -0.002859328808928264; -0.0010695060006075219 -0.005016393100224828 0.0008700619833848476; 0.00020112080208066645 0.001570077616255957 -0.00038918043093766645; 0.0003498722508136566 0.0018728407510114479 -0.00022060182806565057; 0.0033794035573170055 0.007315058113564917 -0.0027693306730730673; -0.0029490650645706933 0.006788747981049089 -0.00032408698285445214; -4.388198840299748e-5 -0.0011714621200090392 -0.00016482531189169905; -0.00038058288008744365 -0.004521895348625492 -0.005499753543580395; 0.0006243974527007343 -0.002919790043643994 -0.006160077014874602] %
+
+Mass Used: 77.67903327049953 kg
+Launch C3: 104.42724022892315 km²/s²
+||V∞_in||: 0.0016483655467987017 km/s
diff --git a/archive/ES_0.5887554927192112 b/archive/ES_0.5887554927192112
new file mode 100644
index 0000000..b0ddf4b
--- /dev/null
+++ b/archive/ES_0.5887554927192112
@@ -0,0 +1,22 @@
+archive/ES_0.5887554927192112---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T16:00:50.782
+Launch V∞: [5.200127520955945, -8.604314071930965, -1.0977269817271313] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00012743571202710111, -5.772597395540228e-5, 0.0001089878671985255] km/s
+ V∞_out: [5.3814136422936455e-5, -0.0001252633145323811, -0.00011355632597007012] km/s
+ time of flight: 1.4136554456720027e8 seconds
+ arrival date: 2027-10-20T20:13:14.782
+ thrust profile: [0.2265639663107417 -0.151741844227649 -0.1395083242903824; 0.06899520540233794 -0.01380511769359962 -0.09993987325092121; 0.0639860881160052 -0.0033251841543845972 -0.14572832648250986; 0.05838309393118599 0.00048290383572946563 -0.17945957347475647; 0.04983259074174701 0.0021544494016322536 -0.18742461023920387; 0.03361806038408487 0.0014963602827225595 -0.14823980012982738; 0.056075538676948596 0.003844759093164175 -0.28546128073106586; 0.01823671661171182 -8.513825902903066e-5 -0.09836330278211397; 0.0025055717297464445 -0.0005520152336688615 -0.012138225795350817; 0.0010295076406640594 -0.00013945714678735436 -0.006435790006987718; 0.0003900680217891329 -0.0006138067214328407 -0.004973522925312346; 0.004833515913080591 0.0017939956087599505 -0.006693883054882268; 0.0007263922579074131 0.0006931026420518606 -0.00249316369053937; 0.002865665657762205 -1.036644479133846e-6 -0.0015679614534093401; -0.002136585016274595 -0.0004028285372768103 -0.002172405974788133; 0.0019111812707580823 0.0018869103222690954 -0.0004404193678824212; 0.0017304032024919214 -0.01621315977991884 -0.001136920955582669; 0.013869199209189057 0.013803156053064859 -0.0014975164120173273; 0.0003409426170761789 0.00015446817941772335 -0.0016873817374753694; 0.0024128317210864773 -0.007237912836209127 0.0023271285889694105] %
+
+Mass Used: 90.24485828632078 kg
+Launch C3: 102.2805514090444 km²/s²
+||V∞_in||: 0.0001773428993939071 km/s
diff --git a/archive/ES_0.5888442156346572 b/archive/ES_0.5888442156346572
new file mode 100644
index 0000000..c3f1fc3
--- /dev/null
+++ b/archive/ES_0.5888442156346572
@@ -0,0 +1,22 @@
+archive/ES_0.5888442156346572---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T18:21:59.337
+Launch V∞: [5.160804432457689, -8.319396565241894, -1.0915016193944564] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.09650657246428035, -0.13965519419100247, 0.0236088699413768] km/s
+ V∞_out: [-0.16080483425247655, 0.05245958080997644, -0.02770174114034697] km/s
+ time of flight: 1.3298463837657912e8 seconds
+ arrival date: 2027-07-09T22:32:37.337
+ thrust profile: [0.5495814637369861 -0.3646397616074327 -0.2886177687068413; 0.2880761046392441 -0.03148156014121733 -0.3214318749155335; 0.13848751534697012 0.012477512184039986 -0.23820984680174231; 0.11232232902953046 0.023670615138462102 -0.2536839446958042; 0.08030898669517052 0.02330581238505747 -0.2215777306110603; 0.04578608516179332 0.01591959222784688 -0.14794423417108232; 0.028271817865164597 0.011155896432151025 -0.10287242920561028; 0.007729212304251916 0.0034095750371749165 -0.031084171247266895; 0.0014271518438871624 0.0005233985974736133 -0.003214164011004759; 0.0006748098412849379 0.00046807140913138044 -0.0010062192913086725; 0.0005532071508328309 0.0004813893519374541 -0.0029157620492732744; 0.000655346347671226 0.0006366251040709792 -0.004314698926732561; -0.0017221297911344249 -0.003087401951698278 -0.0016778428969908376; -0.001948849777232357 -0.0003153642447199556 -0.0015673388766876458; 0.0010150227902874366 8.217241618545322e-5 -0.007076816232676062; 0.003047868477126874 0.000602972935572018 -0.002716714806402113; 0.0014478899846579788 -0.00038535521249446255 0.00010177469338272255; 0.0003086448735601176 0.0016134192932857122 -0.002311301134921234; 0.0007870020652304237 -0.001948214185689816 0.00335354491905095; -0.0017065567558616785 0.005924108810497555 0.0020586964967437477] %
+
+Mass Used: 120.93203349475016 kg
+Launch C3: 97.03763738497427 km²/s²
+||V∞_in||: 0.17138982038977357 km/s
diff --git a/archive/ES_0.5888528519925602 b/archive/ES_0.5888528519925602
new file mode 100644
index 0000000..1ca43e4
--- /dev/null
+++ b/archive/ES_0.5888528519925602
@@ -0,0 +1,22 @@
+archive/ES_0.5888528519925602---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T02:37:27.717
+Launch V∞: [5.267684348552341, -8.197841548377838, -0.8821870965599184] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.352891781237275e-5, 1.632903844282723e-5, -3.4446073374660225e-5] km/s
+ V∞_out: [-3.153754194756755e-5, -2.85161493271989e-5, -1.4120784263663675e-5] km/s
+ time of flight: 1.3527960109552908e8 seconds
+ arrival date: 2027-08-03T20:17:28.717
+ thrust profile: [0.5393599486904936 -0.35712996944676073 -0.26883361538168565; 0.29742267579647436 -0.02394276948943351 -0.3059254311013942; 0.24755302069269922 0.0359924206241751 -0.3809531317492946; 0.1072119464120183 0.02938071777570599 -0.22019970804336192; 0.06800133679117999 0.025300651675554318 -0.17134749275504052; 0.03797726377705747 0.017465993225988224 -0.11317418181537299; 0.016020314604056632 0.008483061907337613 -0.05621744662245576; 0.006952045298417296 0.003980832382437469 -0.02738021239717933; 0.025833929494253834 0.0184027332831743 -0.10803593923450697; 0.002171455903151392 0.0018713016033863722 -0.009662927296216562; 0.0012417800663505122 0.000918558959831764 -0.006265980078980217; -0.000344903205040618 -0.0006085370632093638 0.0013401142178187924; 0.0026370362199356254 -0.003955904869064004 0.0018262275068962274; -0.0013278448217617228 -0.00014419244858103095 0.002439700112194483; -0.00039238810479692117 -0.0005759094597725476 0.00021778819280418127; -0.0003797590516184118 0.001008728497547782 -0.00036982859201764183; -0.0010019111844155324 -0.001180734649466829 0.0053248844053624955; 0.0031669274669118637 -0.0023411608789319265 0.003594025776332428; -0.0016369587477519116 -0.006346473063365101 -0.006941160137846113; 0.00016557801060221672 0.00042556575162043487 -0.0011663861499509748] %
+
+Mass Used: 128.56206928181155 kg
+Launch C3: 95.73135852163006 km²/s²
+||V∞_in||: 4.4797091879062835e-5 km/s
diff --git a/archive/ES_0.5888530318408061 b/archive/ES_0.5888530318408061
new file mode 100644
index 0000000..e58afbd
--- /dev/null
+++ b/archive/ES_0.5888530318408061
@@ -0,0 +1,22 @@
+archive/ES_0.5888530318408061---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T02:00:41.242
+Launch V∞: [6.339642592635319, -7.612267285242757, 0.07953131801695895] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9864206605367527e-8, -7.94184043190271e-9, 4.4762973957768724e-8] km/s
+ V∞_out: [1.1366521618015507e-9, -2.8932149410470934e-8, -4.084630908483494e-8] km/s
+ time of flight: 1.771779589711684e8 seconds
+ arrival date: 2028-12-08T18:06:39.242
+ thrust profile: [0.18188824400274547 -0.06005415940392548 -0.06543652421359285; 0.05596458797862444 0.016002762059500998 -0.06720656559225786; 0.07505942982085059 0.03626172613428585 -0.13260647269836012; 0.03665276844612773 0.02822818202358731 -0.09059438494485884; 0.04127194031710369 0.03320381121367031 -0.12408951812787374; 0.04561215234648457 0.03739855649336838 -0.1660215699817481; 0.026858870522457952 0.02300039490441737 -0.0982624332837128; 0.024783113782619208 0.018615094012239878 -0.12256765730014998; 0.0013550550999985138 0.01089026373735854 -0.07279589578121262; 0.008125379865900855 0.010236455696753008 -0.042590442188336346; -0.00035475635731627413 0.010122316846556838 -0.01317145572775127; 0.0035867385468119012 -0.027882366320263835 -0.004455671142172454; 0.0004882636650544239 0.006029214042982384 -0.012995046800154928; -0.0029937415308226604 -0.004161411272053167 0.01246296026823653; -0.0013798314054096785 0.022893551937231704 -0.0027363827957438552; 0.008454989458459966 -0.03619164978271958 0.013432315729985076; 0.020709726391536742 -0.022338390925936622 0.030146194362560587; 0.046974081210926895 0.028035077823028276 -0.033752808168156456; -0.028064835037787682 0.008704089080120901 0.09020794446354102; 0.02684164408302446 0.018707367655037898 -0.06799423826282468] %
+
+Mass Used: 114.48849832748238 kg
+Launch C3: 98.14400665487852 km²/s²
+||V∞_in||: 4.961233083670241e-8 km/s
diff --git a/archive/ES_0.5888786457319948 b/archive/ES_0.5888786457319948
new file mode 100644
index 0000000..f8edf75
--- /dev/null
+++ b/archive/ES_0.5888786457319948
@@ -0,0 +1,22 @@
+archive/ES_0.5888786457319948---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T23:00:16.662
+Launch V∞: [5.7443850544082595, -7.959578165659558, -1.404730077267632] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1618359887916891e-5, -0.0049382890130615364, 0.0019879532640413966] km/s
+ V∞_out: [0.004343404869831403, 0.0022698076388324153, -0.0020856362054744657] km/s
+ time of flight: 1.4932742555089974e8 seconds
+ arrival date: 2028-01-13T06:50:41.662
+ thrust profile: [0.3317473020845338 -0.16820890520781537 -0.1393242639419583; 0.14897475904320914 0.011145918830755105 -0.14451593422967782; 0.15046294428588972 0.04952420705053534 -0.22146326155811; 0.12002176107577213 0.06024140056831761 -0.23536074938210583; 0.07064542759512785 0.04548011494031744 -0.17482429981070133; 0.022854685460724028 0.016227883064633967 -0.0675579314174597; 0.035077087652919295 0.02835851340434199 -0.10668131026882502; 0.014589062679556243 0.013270037774716623 -0.06553484081138362; 0.010695375563988356 0.012107641757406513 -0.05417301088254766; 0.03521710320950254 0.03796631484624017 -0.15809423569268263; 0.0014865979398368352 0.00013056357223985987 -0.006511423067625171; 0.0003339959270212791 7.320891287930585e-5 -0.003172180812810452; 0.0023834299446063166 -0.0007645223655648063 -0.0034614433357422697; 0.002547434152995507 0.0015495734737264873 -0.002249660779752757; -0.0022324568797529747 -0.006793186942289883 -0.0017714543432086206; -0.012651797205217244 -2.1391191051433624e-5 -0.005871357969398161; 0.004944082244653586 0.011444972367170073 -0.002928446441573439; -0.009022628918399035 0.0030275257526750548 -0.011650667179420104; -0.0001744758617612436 -0.0007815759987568637 -0.0016119516937088104; 0.00020384116019902732 -0.002747090440304088 -0.01644573182732307] %
+
+Mass Used: 113.45610691254751 kg
+Launch C3: 98.32611081853368 km²/s²
+||V∞_in||: 0.005323419159039011 km/s
diff --git a/archive/ES_0.5890134341345311 b/archive/ES_0.5890134341345311
new file mode 100644
index 0000000..5811952
--- /dev/null
+++ b/archive/ES_0.5890134341345311
@@ -0,0 +1,22 @@
+archive/ES_0.5890134341345311---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T00:35:11.316
+Launch V∞: [6.060748795546946, -7.02284772766499, 0.8793667878530054] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.273429052125157e-8, 2.3537665448314546e-8, 1.3178333020867948e-8] km/s
+ V∞_out: [-8.356449642990049e-9, 1.5998668363543848e-8, -2.5514724536410456e-8] km/s
+ time of flight: 1.8588530769777626e8 seconds
+ arrival date: 2029-03-08T11:23:38.316
+ thrust profile: [1.0 -0.2870433761243202 -0.14656508368321852; 0.5517320380821598 0.21407659210083801 -0.24481952700294787; 0.12817002782121897 0.10037835116418233 -0.10735433422520717; 0.07223404897933801 0.07918252782734327 -0.08697679860030841; 0.056909332183098474 0.07752779086081234 -0.08815371091099074; 0.05670176476195414 0.09180410122800144 -0.10006289712948908; 0.02026430585800436 0.039537444662333956 -0.04828196805412515; 0.01527805980563801 0.03386296011288465 -0.0439874854851632; 6.470499902291651e-5 -0.00012059476597107099 -0.001172492447237603; 6.13370619746419e-5 -0.000367129080343012 -0.0003963769204695348; 0.0009527925866138642 0.0007838874250798182 -0.0037547944087145766; -7.743946359321547e-5 -2.4258465720393982e-5 -0.00012493318619508258; 0.0002758872690000482 0.0013065068893948137 -0.0016445688573596766; 0.00015310149089193398 0.0007788387912236059 -0.0009124384848686854; -0.0002545704498683138 9.92091104431208e-5 -3.2319177378820345e-5; 0.0009541401039754142 0.00037400617966563965 -0.0012303564916985967; 0.0006638441607587481 0.0010806532552031928 -0.0003950557380835544; 0.0010438546663093864 -0.00015224833786793698 -0.0013952736372062026; -0.00019183755851160712 7.942315646864944e-5 -0.0005222059337982921; 0.000771325902079558 -0.0012776801238698855 -0.0006318912048264932] %
+
+Mass Used: 180.69528581203303 kg
+Launch C3: 86.82635211627199 km²/s²
+||V∞_in||: 2.983039240515144e-8 km/s
diff --git a/archive/ES_0.5890470790308832 b/archive/ES_0.5890470790308832
new file mode 100644
index 0000000..cbb483c
--- /dev/null
+++ b/archive/ES_0.5890470790308832
@@ -0,0 +1,22 @@
+archive/ES_0.5890470790308832---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T17:24:42.717
+Launch V∞: [5.78393163490458, -7.774543915810993, -0.27655446727913263] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.879436231919089e-6, -1.4207635639234276e-6, -2.412696724233466e-6] km/s
+ V∞_out: [1.7498313990320384e-6, -2.3474268128707435e-6, 2.7307613006287343e-6] km/s
+ time of flight: 1.5978150449553832e8 seconds
+ arrival date: 2028-05-15T01:09:46.717
+ thrust profile: [0.5141161146657894 -0.2241618955843603 -0.18906630353460138; 0.15641830162224651 0.018646330614442135 -0.15336999106484767; 0.13751451325968825 0.05084704433091266 -0.21238509694370306; 0.08839045836671862 0.047479829757073884 -0.18615907163648981; 0.053655698184356115 0.03597450222908641 -0.14194262447239753; 0.022454421239497258 0.017744516167174765 -0.07005779810931241; 0.024357967537625914 0.021016844108337422 -0.08546817261750461; 0.022753871293104945 0.02188511690503566 -0.09161418001594582; 0.04243962463627496 0.0410637308108166 -0.18047618671109342; 0.002691328531857797 0.004290522032411982 -0.011053140552437698; -0.002707658738794016 -0.0028842302372494395 0.008007585161595249; -0.01656123040299403 0.009334468729506253 -0.0013307543425603889; 0.009336386092049447 0.003151093753981147 -0.0057536712980068155; -0.010310279847293168 0.0024759738202700934 0.022216218826722103; -0.004201421150601408 -0.01981495569752506 -0.01608251854666295; -0.0005783571821720918 -0.005342217780482729 0.016207049561314857; 0.0032830016660725238 -0.00537443852651159 0.01705919125283197; -0.034490698218916704 -0.04414702494279176 -0.004266632404052617; -0.004360020617575873 -0.040041436330654476 -0.003388633564643347; -0.003328714951147501 -0.05842459380753311 0.015111786177118931] %
+
+Mass Used: 139.04062186397186 kg
+Launch C3: 93.97388062949574 km²/s²
+||V∞_in||: 4.016320156733984e-6 km/s
diff --git a/archive/ES_0.5890476498969882 b/archive/ES_0.5890476498969882
new file mode 100644
index 0000000..f4e3b5b
--- /dev/null
+++ b/archive/ES_0.5890476498969882
@@ -0,0 +1,22 @@
+archive/ES_0.5890476498969882---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:48:25.790
+Launch V∞: [6.844721540247395, -7.141834699355073, -1.165513060391505] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3610267849806987e-5, 3.182145147888321e-5, 1.9187508131623852e-5] km/s
+ V∞_out: [2.8728705700428497e-5, -2.350264068688987e-5, -1.3725381272913305e-5] km/s
+ time of flight: 1.3104455576737478e8 seconds
+ arrival date: 2028-07-02T02:04:20.790
+ thrust profile: [0.5918997937261679 -0.24197230671961842 -0.3036800939706503; 0.1245382728791843 0.005356972316855233 -0.15611945693014667; 0.11267754141046586 0.02648737661537488 -0.22476344937837034; 0.09640969057990546 0.03326373583747185 -0.25926785961893195; 0.05905190316014118 0.024160201053806524 -0.19912536310661932; 0.05071021948337738 0.023064910210099075 -0.20056232031531954; 0.017112494743988498 0.009073315107302065 -0.07658018467876758; 0.00939024845854818 0.006225482308585202 -0.04984252623780039; 0.009272669041707721 0.0038999773522782697 -0.04577333864947188; 0.001900027550531043 0.001202002081153077 -0.012459456559213846; 0.0024708916295673802 0.0015218790599629433 -0.015728410232754342; 0.0011537866967205664 0.0004385415396603575 -0.005979614073507062; 0.00018951949024988856 -0.0003870845972858461 -0.0006050741485532261; -0.00023625867431787903 -5.7001879332157536e-5 -0.0009763448746184897; 0.00029933140409221847 0.00024158750145078273 -0.0018363302312749824; -0.00030430280244700923 0.00011543500705460569 -0.0013675282269613297; -0.0010728514436010817 0.0013371698113865595 -0.002909456309860066; 0.000485832872848427 -0.0004130133793297003 -0.001475788394192421; -0.00025720476566263055 0.0001850705795383866 -0.0005806365125549508; 1.6179484208399784e-5 -6.355419932032929e-6 -2.5504753189130075e-6] %
+
+Mass Used: 108.47137845259113 kg
+Launch C3: 99.21443653038202 km²/s²
+||V∞_in||: 3.957277641848673e-5 km/s
diff --git a/archive/ES_0.5893914069079493 b/archive/ES_0.5893914069079493
new file mode 100644
index 0000000..03cbe30
--- /dev/null
+++ b/archive/ES_0.5893914069079493
@@ -0,0 +1,22 @@
+archive/ES_0.5893914069079493---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T12:09:19.159
+Launch V∞: [5.333396129306407, -8.347990137080002, -0.4847466889801349] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000615830191701056, 0.00027078771143401097, -0.00030303542894680673] km/s
+ V∞_out: [-0.00023836898070226693, 0.0005325046827979439, 0.0004510630681372761] km/s
+ time of flight: 1.347476787575261e8 seconds
+ arrival date: 2027-07-30T02:03:57.159
+ thrust profile: [0.35987213533626383 -0.21997824030921087 -0.16687529248357127; 0.20201978065447307 -0.0135340150811031 -0.21044363708797567; 0.1401864671296817 0.021086332779179304 -0.22348897451324354; 0.10133430751331227 0.028690721961125144 -0.2127395673543173; 0.07134481300492317 0.02708791471720115 -0.17855494592800697; 0.06863972848047271 0.03082355549000277 -0.19738630579980598; 0.051945353005348346 0.025307631111236014 -0.16451344464657103; 0.01784337746878693 0.00860845754159137 -0.0663185105151399; 0.0460555507977816 0.022576859476979898 -0.1692189313412078; 0.009737749498601643 0.005797516712958256 -0.04237653406751723; 0.00018522986445554417 9.146289759928354e-5 -0.000876170721922778; 0.00019820463849757982 0.000166798572014475 -0.0004562260831906489; -9.726183892591253e-5 7.018627461258213e-5 -0.00026883161029391705; 2.760214641640407e-5 7.80999445854427e-5 -0.00017748501489472707; -5.772032342825653e-5 0.00015369960700790087 -0.0001899914496608798; 1.3781732727895512e-5 0.0004648830065392681 -0.00033613267154734914; -5.589905317541247e-6 -0.00018343843830399896 -0.00018881930981597808; 0.0001263907562539151 0.00022933207530518223 -0.0003234060625252365; 4.757514938271833e-5 0.0001549429764076826 0.00010156548594543815; 9.703739877221784e-6 -4.422124762536411e-5 3.881517861306573e-5] %
+
+Mass Used: 113.8039491646582 kg
+Launch C3: 98.36903295336275 km²/s²
+||V∞_in||: 0.0007378368931350639 km/s
diff --git a/archive/ES_0.5894526745167243 b/archive/ES_0.5894526745167243
new file mode 100644
index 0000000..962770a
--- /dev/null
+++ b/archive/ES_0.5894526745167243
@@ -0,0 +1,22 @@
+archive/ES_0.5894526745167243---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T04:44:16.892
+Launch V∞: [8.016766687178407, -5.694219410646237, 0.7623366907092116] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.631140627243251e-6, 2.1439270997023666e-6, -1.6064327215309717e-6] km/s
+ V∞_out: [5.390724672196697e-7, 3.608614148636824e-6, -1.7917575993548583e-7] km/s
+ time of flight: 1.6907976764413273e8 seconds
+ arrival date: 2029-09-08T03:20:23.892
+ thrust profile: [0.5880670864338533 -0.062288122576664225 -0.12934036413767153; 0.17976445960934664 0.09636925065912591 -0.1331722571815116; 0.10176337368967059 0.09181205928409167 -0.1312989864034026; 0.06880210982504617 0.08405713127370575 -0.13040710028461397; 0.07632837372114037 0.10721114317230585 -0.18215229444115874; 0.04864783555000435 0.08244086897110639 -0.14815334224710672; 0.015605719545276493 0.03247358823594312 -0.06322990618926606; 0.004555139402525179 0.010606015337607399 -0.02196997877849411; 0.002815264256091323 0.007464162994648846 -0.01601336629988196; 0.001177573630016665 0.0035671544404088855 -0.0076921708644896395; 0.0007658168964259656 0.0020549874236344256 -0.003972785749149593; 0.0017688251413735423 0.001053014116367879 -0.0028266165331824675; 3.175155080284641e-5 0.0015454986195529645 -0.0026087733169710037; -0.001480095684653114 0.003280769586011763 -0.0018085326686182294; 0.0017878108506774436 -0.0003470670746474231 -0.0026345792233328; -0.005597232007110723 0.006366198181868408 -0.004109489492334692; 0.0028828021892154704 -0.001374365348756962 0.0013046524829244182; 0.0053831326750422084 -0.003161477845252839 -0.006835194330225831; -0.00035781319035979727 0.0017827186912603447 -0.006594336027060973; 0.004392833199024441 0.002041835255481339 0.002445725399644526] %
+
+Mass Used: 120.26405335063919 kg
+Launch C3: 97.2738400432353 km²/s²
+||V∞_in||: 3.754990079610546e-6 km/s
diff --git a/archive/ES_0.5894548171832104 b/archive/ES_0.5894548171832104
new file mode 100644
index 0000000..4d6bae8
--- /dev/null
+++ b/archive/ES_0.5894548171832104
@@ -0,0 +1,22 @@
+archive/ES_0.5894548171832104---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T12:23:52.953
+Launch V∞: [7.194651891685596, -6.81260209585645, -0.5796273304401126] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006544664323325019, 0.0033992664903978544, 0.0002313834156297204] km/s
+ V∞_out: [-0.00539521380754203, -0.003010976497136895, 0.004033376646559652] km/s
+ time of flight: 1.483292859287872e8 seconds
+ arrival date: 2029-01-19T06:58:37.953
+ thrust profile: [0.266633502725883 -0.0773926965485505 -0.12023176668292347; 0.1352327929958962 0.02357701864990149 -0.16344443562205113; 0.08507389343480079 0.03149759533845064 -0.16975302866390238; 0.06069993945689674 0.029687462124953934 -0.16958178973684587; 0.04187714761732323 0.024003343426494173 -0.15624029917127324; 0.031738237238559515 0.02146214495729778 -0.15044667646775767; 0.022725036625689178 0.01630969867419624 -0.10199547504065884; 0.00872589863720472 0.0068632699867542364 -0.03511059210426845; 0.03930333438154605 0.03208405936100281 -0.2068236423576905; 0.00029278823758720207 0.00023885147701877072 0.005698449673470026; 0.005527705304415199 0.0034000227916140325 -0.04735863227203936; -0.006319633641407704 -0.002856677748891902 0.0014112433564950513; 0.0003001028033059088 0.005850786270476296 -0.015348141186493155; 0.002409041098956072 -0.004028461801076663 -0.010813896472772153; 0.007863782639211253 0.0029515720166886986 -0.007049167344589819; 0.04092235049381231 -0.020105262272511908 0.01809568783436828; -0.021437888724122705 0.011147762203950506 0.008336123126411686; -0.00466678649955791 0.010223203906949098 -0.013826100212171906; 0.00942336314584752 0.002749445867265338 0.07361756085649288; -0.07026924041234288 -0.002741193329893629 -0.042722424233878384] %
+
+Mass Used: 113.05252254010247 kg
+Launch C3: 98.51053100119594 km²/s²
+||V∞_in||: 0.007378426801342788 km/s
diff --git a/archive/ES_0.5894804489259996 b/archive/ES_0.5894804489259996
new file mode 100644
index 0000000..f8201d4
--- /dev/null
+++ b/archive/ES_0.5894804489259996
@@ -0,0 +1,22 @@
+archive/ES_0.5894804489259996---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T02:42:50.050
+Launch V∞: [7.699586735235467, -5.4453703213145666, 0.28299923309939207] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3530844421197193e-7, 1.0032963479607221e-7, 7.113579853150682e-6] km/s
+ V∞_out: [-6.209571701762495e-6, -2.2146766878252854e-6, 2.1722301645561397e-6] km/s
+ time of flight: 1.8569707543434975e8 seconds
+ arrival date: 2030-03-20T09:14:05.050
+ thrust profile: [0.961521055921349 -0.002512499208346687 -0.11447574980916284; 0.31666041568567804 0.2330693299999456 -0.1598487355768165; 0.1840812113243043 0.2182051088904153 -0.17122764272347718; 0.03753438263406574 0.06698111537287185 -0.06396773408155866; 0.025848422756210566 0.06431090694329854 -0.06502278710762213; 0.061793127855433734 0.15135966762733896 -0.15806735935150165; 0.0077309276640209505 0.034603774663952515 -0.04218991725918114; 0.003877716496483847 0.023826379488268063 -0.030159922950696017; 0.0012694001430035564 0.008310916304025022 -0.010750185632673525; -0.0003166155323480593 0.002057179515853609 -0.002318300220987576; -0.0008600866823634003 0.0005681283136654339 -0.0012579451986178645; -0.0004975161798758619 -0.0006714416882420884 -0.0006720143693666088; -9.015089152029015e-5 -0.00012778768894315196 -0.0007598006666563687; -0.0002853956566893729 0.002585857784955674 -0.0018386333482309826; 1.891816980977587e-5 0.0008470800820391576 -0.0013276303245550647; -0.0006242355446770878 -0.00033253814628292724 -0.0013852115156354416; -0.001214732469279501 0.0010385611257048629 0.0009609161209540693; -0.0016071764873849808 0.0023305760257253992 -0.0024890889770848123; 0.001470062877050953 0.0003520557701819439 3.792308077269803e-5; 0.000411932185065798 -0.0028326219911685106 0.000434762161857287] %
+
+Mass Used: 168.46845977265275 kg
+Launch C3: 89.0157823956023 km²/s²
+||V∞_in||: 7.115573957021643e-6 km/s
diff --git a/archive/ES_0.589516896466656 b/archive/ES_0.589516896466656
new file mode 100644
index 0000000..d70f60d
--- /dev/null
+++ b/archive/ES_0.589516896466656
@@ -0,0 +1,22 @@
+archive/ES_0.589516896466656---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T21:44:58.899
+Launch V∞: [6.309138414526355, -6.940878836350607, 0.04791911372765001] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006239178875504326, -0.00019688697966170892, 0.0045627994271363655] km/s
+ V∞_out: [-0.0074090220378798585, 7.492247112740074e-5, 0.002182736031840039] km/s
+ time of flight: 1.8749577787457627e8 seconds
+ arrival date: 2029-03-27T23:54:35.899
+ thrust profile: [1.0 -0.2512864962179378 -0.1918668614568964; 0.4033505587826501 0.16206508007499162 -0.23522050064171543; 0.13830954126255884 0.1080615757073157 -0.14537528724688223; 0.05085822686250046 0.05448156270938653 -0.07989117975791948; 0.04766808533719872 0.06513237665901307 -0.09975407496862532; 0.03163508476262691 0.053104874373775326 -0.08415854261082191; 0.03787908170941457 0.0745483422442083 -0.11477093719520509; 0.005675086769589734 0.01239852117561865 -0.021697817637278627; 0.0018206662407927315 0.004899938530151696 -0.009371384905003612; -0.00028703627392237963 0.0026517975938881826 -0.0032317963222799405; 0.0010867387436437083 0.0013060260121337676 -0.0015794455046678805; 0.00021120200870206653 0.00043195730665589367 -0.0007305652069470902; 0.0005135355123615816 0.0007412395753080932 0.0011050490149337824; 0.001244423944789357 0.00915131703996859 -0.011385800894824811; 0.003938338432795248 0.0012763092116258952 -0.008504378393116043; 0.0017588074438896991 0.002248995106907485 -0.000987850406303655; -0.0011027858947762368 0.0016687504199366784 -0.0017388432954475379; -0.0005662956403200367 0.0017994869134813373 0.0002708000205155121; -0.0013514009222248668 0.0026519083115140885 -0.00165308293993533; -0.0017451754848901307 -0.0012025487536091199 0.0013791368997427493] %
+
+Mass Used: 174.53366290102667 kg
+Launch C3: 87.98332279601235 km²/s²
+||V∞_in||: 0.007732092610385346 km/s
diff --git a/archive/ES_0.5895181523204561 b/archive/ES_0.5895181523204561
new file mode 100644
index 0000000..4f69d44
--- /dev/null
+++ b/archive/ES_0.5895181523204561
@@ -0,0 +1,22 @@
+archive/ES_0.5895181523204561---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T17:19:50.818
+Launch V∞: [7.091556008628809, -7.057992088889828, -1.1541294670498623] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.196737170058394e-6, 5.462643019531629e-6, -3.0356695947818434e-7] km/s
+ V∞_out: [-5.608805452603857e-6, 3.570273108887507e-6, 3.569027327140962e-6] km/s
+ time of flight: 1.3387240948409271e8 seconds
+ arrival date: 2028-08-03T04:06:39.818
+ thrust profile: [0.27165398552396464 -0.10121474715240872 -0.14045410103533565; 0.11799235098445407 0.015505237320200383 -0.14856376201462537; 0.09649509061396608 0.03341130764029768 -0.19203757163994373; 0.07864662654096799 0.037742409716360316 -0.21162979610624227; 0.06218414767036316 0.03627526240518545 -0.2078316461912466; 0.04603661501488753 0.03144070320564457 -0.18348882376863082; 0.03191278014710114 0.025429397175940036 -0.14661438207393662; 0.01950859973068496 0.01765912384459369 -0.10007480523313439; 0.009342969053010741 0.009169902138678241 -0.04952941609916895; 0.0023130053860860407 0.0003150446352258398 -0.009961770973310535; 0.007657765726072033 0.005397990674317187 -0.0450775006435555; 0.004761668013129769 -0.001648807741901668 -0.00476415475366029; 0.0018363171027078672 -9.0266194514727e-5 -0.002578587201100047; 0.0008054727261438326 -0.0021023247432641196 -0.00044631475647291877; 0.0015895656487789 -0.008838803949955166 0.0014990704804265101; 0.0017925118178553426 -0.0011073177555888125 -0.005848343067653786; 0.0005410704915868869 -0.0002216355937248698 -0.008813010531591142; 0.001991508972188342 -0.007674161330749572 -0.005729615336024312; 0.001856707206088666 -0.009827866473560678 -0.011194004603658169; 0.0011535240516143967 0.0059750569624172824 -0.0029803998020422762] %
+
+Mass Used: 96.05281400766125 kg
+Launch C3: 101.43743377706357 km²/s²
+||V∞_in||: 7.545773576803837e-6 km/s
diff --git a/archive/ES_0.5895353129764109 b/archive/ES_0.5895353129764109
new file mode 100644
index 0000000..5e10d83
--- /dev/null
+++ b/archive/ES_0.5895353129764109
@@ -0,0 +1,22 @@
+archive/ES_0.5895353129764109---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T00:41:22.983
+Launch V∞: [7.266945700505106, -6.67185811789665, -2.011675873045772] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0033096572937572947, 0.05022709213826992, 0.00606713285352165] km/s
+ V∞_out: [0.04853978643581027, -0.009151132157506922, 0.011440614038946568] km/s
+ time of flight: 1.495604371992908e8 seconds
+ arrival date: 2029-02-01T01:15:19.983
+ thrust profile: [0.23234674638158354 -0.06131618420638582 -0.12501640277806914; 0.10637178771688127 0.03461488704998971 -0.14412415365435632; 0.0913799039224637 0.05817540951061147 -0.2055015538662869; 0.0691225986138912 0.05916490188910284 -0.19554743928907747; 0.05035107115137417 0.056043359675623926 -0.19284001054091707; 0.017455045957670886 0.02618443391046762 -0.08567620024793846; 0.011941569513575149 0.019794056527844224 -0.0692691976462596; 0.020427664626872503 0.03750258412494752 -0.137052308160946; 0.004658586589147692 0.007554114709235298 -0.03273507563143771; 0.0014226128747636905 -0.0017763504026006255 -0.006832368716221795; -0.0001200552087916706 -0.0004290434688384308 -0.0012177803310451786; 0.005730695506075446 0.003535302962682275 -0.003917062842525396; -0.0008277881712201088 -0.00024212542766734733 0.004551291375684942; 0.0005619930786391407 -0.0024132336161284086 0.0034554842621838822; -0.012773153821689693 0.004469013671498103 0.001821766477546795; 0.008465132668120188 -0.01385967029134728 -0.0025484385675230976; -0.016793773081505446 0.019998409261702554 0.007889640636399053; -0.010976893326556957 0.020634401425277026 -0.020597117457677876; -0.016233130269880908 0.005717461474629913 0.02375920749621587; 0.023792610389069706 0.008600237846198875 0.008777847456265768] %
+
+Mass Used: 96.47185460298533 kg
+Launch C3: 101.36903037762755 km²/s²
+||V∞_in||: 0.050700342376858346 km/s
diff --git a/archive/ES_0.589544660591182 b/archive/ES_0.589544660591182
new file mode 100644
index 0000000..fe5985c
--- /dev/null
+++ b/archive/ES_0.589544660591182
@@ -0,0 +1,22 @@
+archive/ES_0.589544660591182---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:43:09.908
+Launch V∞: [6.904665638705983, -7.180422753587562, -1.015811809729799] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8040122941752823e-5, 6.323943764207405e-5, 3.848195523488127e-5] km/s
+ V∞_out: [5.697973234338846e-5, -4.815712672929948e-5, -2.6275369866443308e-5] km/s
+ time of flight: 1.3082309296924296e8 seconds
+ arrival date: 2028-06-29T12:28:01.908
+ thrust profile: [0.4062227705052456 -0.16739978712712314 -0.203336799955629; 0.1841958028501209 0.00878456916726064 -0.22032321222024173; 0.11174269183082262 0.026782401367167193 -0.21590721849095734; 0.08171574083923618 0.028600152575450222 -0.21387259239605605; 0.12497882534973995 0.05079701088596074 -0.38947461339801087; 0.039135609362634986 0.017872098559214965 -0.1482248011480145; 0.00801748043139522 0.0039406664478119045 -0.03479901588289752; 0.009349018399448909 0.004820024003508098 -0.04477032691401221; 0.00592521551791943 0.003226820793149428 -0.03136969555948708; 0.004237576963130275 0.002265700057722091 -0.023769692071477347; -9.302268035817638e-5 -5.808882344827612e-5 -0.0040726701667035585; 0.0006206950410036823 0.0005060069272996247 -0.003322659815281383; -3.1805335390128306e-5 0.00042083907734661056 -0.0022173189759246933; 0.00014580986704439808 9.476983795068798e-5 -0.002009945472509482; 0.0010470216367443603 -0.0009598201204406734 -0.0015031651143381825; 0.0022996038558820435 0.00021091231618974567 -0.001103190130610796; 0.0009585782950519732 0.0016848977749475058 8.095745317095171e-5; -3.545898899926002e-5 -0.0010272316582982922 -0.0003502521279099707; -0.0017316452266881886 -0.0003192171241276911 -0.000640082832681713; -0.002140858499581809 -0.001994781011039397 0.0005353298911795455] %
+
+Mass Used: 102.92438323349461 kg
+Launch C3: 100.26475213535161 km²/s²
+||V∞_in||: 7.916019104685e-5 km/s
diff --git a/archive/ES_0.5895739246929481 b/archive/ES_0.5895739246929481
new file mode 100644
index 0000000..018a3bc
--- /dev/null
+++ b/archive/ES_0.5895739246929481
@@ -0,0 +1,22 @@
+archive/ES_0.5895739246929481---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T19:52:51.444
+Launch V∞: [7.065213654115197, -6.81946860284571, -0.37821132552302117] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0011705102660922561, 0.0009131984075375477, -0.0006296887141013159] km/s
+ V∞_out: [-0.0006584742362298304, 0.001470669198345538, -6.188674193643014e-5] km/s
+ time of flight: 1.449222683038369e8 seconds
+ arrival date: 2028-12-09T04:03:59.444
+ thrust profile: [0.40625568951285207 -0.12242996639024804 -0.16625308157730898; 0.15764843983770896 0.030801283505457817 -0.1684219402665254; 0.1629496348096897 0.06884378605793583 -0.28241371721518194; 0.08596326131212799 0.04980763619993601 -0.2049105717685213; 0.04978757809479194 0.03570091332092871 -0.14996566010949566; 0.033799043891635974 0.028323968605567514 -0.1214026522139231; 0.031604719044021415 0.02839980121263225 -0.13003881969165457; 0.0189985768421718 0.01932661980927816 -0.08769080256919709; 0.01631614701855344 0.017463971572498432 -0.08204729766930484; 0.02656914742585607 -0.011334603209521621 -0.010108024181956212; 0.02559228261681316 -0.017411508670955277 -0.008465034095557562; 0.002590492254812974 -0.012109767248148735 0.0033700446085488936; 0.008811194870387128 -0.0010411121999654898 -0.0016708289046214186; -0.020102262636007714 -0.013080592908656463 -0.021634877759375067; -0.007515736160686406 -0.007484518200322093 0.0031767488214937607; 0.0007976618246405649 0.0007208600660960755 -0.007635828638777769; -0.015774788194942317 -0.020900863087644952 0.0028438131023209154; 0.003375201949185231 0.04987335620247204 0.021700371869787124; 0.0042295368274461245 -0.04373812732226054 0.009204019101545963; 0.008665642556893846 -0.012444991462500405 -0.03930163312600045] %
+
+Mass Used: 124.5378465819922 kg
+Launch C3: 96.56543981024811 km²/s²
+||V∞_in||: 0.0016126169697801911 km/s
diff --git a/archive/ES_0.5896653506106615 b/archive/ES_0.5896653506106615
new file mode 100644
index 0000000..64940b7
--- /dev/null
+++ b/archive/ES_0.5896653506106615
@@ -0,0 +1,22 @@
+archive/ES_0.5896653506106615---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T13:56:56.266
+Launch V∞: [5.400868251914133, -7.755385233892186, -1.4003452441483646] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.563605961382197e-5, -1.0244734025856567e-5, 1.7341516923166753e-7] km/s
+ V∞_out: [1.239004965235126e-5, -2.759607632212186e-7, -6.519781922405066e-5] km/s
+ time of flight: 1.5388204836914074e8 seconds
+ arrival date: 2028-03-03T14:57:44.266
+ thrust profile: [0.7135398211641973 -0.33327008834505406 -0.2379631249106818; 0.47869018506551525 0.06224467085722595 -0.3602408634136414; 0.19996356848394495 0.08464459127195778 -0.25146566804026843; 0.11231534157067932 0.07071032216621004 -0.19718312493589293; 0.05875803665953852 0.04474773504081369 -0.12710395070664565; 0.06629713384046196 0.06162681028547666 -0.17359238980156438; 0.016171716176930268 0.01643380283835966 -0.049758141754108615; 0.01762622263140621 0.019534551646892002 -0.05852588168093389; 0.007283926142082699 0.009342116359853853 -0.029710561618521224; -8.073297907240803e-6 0.002225417033075741 -0.0017885821642796976; 0.0009627934479617238 -0.0021771128893066137 -0.0009695116385645237; -0.0017946627293306911 -0.0016108910598664707 -0.0027718886467825955; 0.002211144524183348 0.0030547692678358817 -0.0006253372105614642; -0.0007637675136734509 -0.000796620855656777 0.0037805642591134986; -0.001202076637824045 -0.0005266601116469957 0.0028852760468445772; -0.0011441059433021812 -0.00045062698835127797 0.00369066899899029; 0.0026859860044442163 0.0015366234009837926 6.684489724433345e-5; 0.0006697074607021198 0.0010921372990341366 0.002692053218088203; -0.0023469668280017785 -0.0024292051301344855 0.007906317812702398; 0.0009661841048069421 -0.009730591713316987 0.0035580211208501456] %
+
+Mass Used: 155.4975643591788 kg
+Launch C3: 91.27634480341592 km²/s²
+||V∞_in||: 6.643099404427616e-5 km/s
diff --git a/archive/ES_0.5896657296413151 b/archive/ES_0.5896657296413151
new file mode 100644
index 0000000..779b03b
--- /dev/null
+++ b/archive/ES_0.5896657296413151
@@ -0,0 +1,22 @@
+archive/ES_0.5896657296413151---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T18:44:19.146
+Launch V∞: [7.001848046816012, -7.045837706946944, -0.9201580745014829] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.024025427177167366, 0.01257687953368017, 0.001601985312821286] km/s
+ V∞_out: [-0.021324166395499552, -0.010784994899672827, 0.01292099659670304] km/s
+ time of flight: 1.318423877745671e8 seconds
+ arrival date: 2028-07-09T17:37:26.146
+ thrust profile: [0.41335470062334023 -0.1558462014979932 -0.19398873881553536; 0.1720485258532752 0.018068964128167227 -0.1979464920614577; 0.1432888834408833 0.0462764797887572 -0.2596435215426349; 0.10077232515527308 0.045855552160739485 -0.2486254902825513; 0.06675344711104111 0.03622466020109717 -0.20683304682572215; 0.04474540275903096 0.027175650243889467 -0.16442456346386564; 0.043067291995535044 0.029102439353900826 -0.17669144019625746; 0.012179325600177716 0.008171673954331571 -0.0569542409562201; 0.005667434879027989 0.00368686399608829 -0.02693941142928098; 0.004785960882387214 0.0031264810130678987 -0.023177689942361777; -4.161934349628438e-5 0.00014452332822241794 -0.00036361243872236305; 0.003000693476931437 0.002085635440204722 -0.018901469510811605; 0.00026312285754675677 -0.0007994754416309998 0.0012963883258208038; -0.0004704316420942469 -0.0007314112254692513 0.0026171918218027275; -0.00047598392245241033 0.0022020714729467077 0.0011577358358657432; -0.0008274812672216701 0.0038823359740393216 0.004090696261493948; -0.001013399769566442 -0.0006597662054160903 0.0007356849053256149; -0.0018056719161519469 0.0026348220651829916 0.0038745933537818267; 0.001492502450575095 -0.00022503942727159464 0.0009610356036300967; 0.0003453568120165996 -0.00035123765952827814 -0.0005743605040835753] %
+
+Mass Used: 107.43104156666095 kg
+Launch C3: 99.51639594540686 km²/s²
+||V∞_in||: 0.027165518710169523 km/s
diff --git a/archive/ES_0.5897039995372967 b/archive/ES_0.5897039995372967
new file mode 100644
index 0000000..64833d3
--- /dev/null
+++ b/archive/ES_0.5897039995372967
@@ -0,0 +1,22 @@
+archive/ES_0.5897039995372967---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T20:50:09.150
+Launch V∞: [6.54948734981762, -7.532193646806535, 0.07654576941153662] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.313528874747668e-8, 1.3564034924692055e-8, -1.7335061608587957e-8] km/s
+ V∞_out: [6.35171844216727e-8, -5.609067482130913e-9, 7.465605465578315e-9] km/s
+ time of flight: 1.8469565951910508e8 seconds
+ arrival date: 2029-03-09T13:11:08.150
+ thrust profile: [0.09533050940557465 -0.029538424197268473 -0.042076049681484824; 0.0739206439434111 0.011987666819188395 -0.09879792350626772; 0.04780941685092913 0.01636063679964265 -0.10631172260973953; 0.03262816966307084 0.013028576534456838 -0.1051509207954831; 0.028506068811644285 0.013598793328802546 -0.11732358834331488; 0.034991014511562446 0.01927018560875751 -0.15950966794442112; 0.030346170400190723 0.017510799820646825 -0.15951591521516095; 0.010416487491718411 0.002389379751780655 -0.06424860417685956; 0.013847565303166604 0.01048336926058707 -0.09341262902751944; 0.0029283237364744565 0.0007935938213065011 -0.02820166071142221; -0.001030314683229959 -0.0005621766464723606 0.020233000245134393; 0.0026383075259783827 0.0077922669345688676 0.015815651350772144; -0.007828604250227042 -0.00320605297684375 0.04899528227990637; 0.022162828404843134 0.0034383759284187577 0.01034009609347785; 0.008712712648830426 -0.015756242876494967 -0.012987263743304481; -0.02831346240047993 -0.00014385499907084223 -0.0018314544878067027; -0.017580162555771973 -0.0199458451844252 0.02332854442256388; -0.014918525195156664 0.04097813970819163 0.07687061755432259; -0.0139321940369844 0.031149199231264163 0.003931390968827962; 0.02026510773376419 0.024842062097933163 -0.0020010537676198033] %
+
+Mass Used: 106.78042068301284 kg
+Launch C3: 99.63558493322857 km²/s²
+||V∞_in||: 6.686218729326062e-8 km/s
diff --git a/archive/ES_0.589726466012788 b/archive/ES_0.589726466012788
new file mode 100644
index 0000000..384b60b
--- /dev/null
+++ b/archive/ES_0.589726466012788
@@ -0,0 +1,22 @@
+archive/ES_0.589726466012788---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:24:43.559
+Launch V∞: [6.9578285342023465, -7.256940688809084, -1.146547864425468] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0024993144692306134, -0.0037876449984671668, -0.00032961469893600395] km/s
+ V∞_out: [0.0002992322873862866, -0.001338535535921813, -0.004338167122849132] km/s
+ time of flight: 1.3272211051145136e8 seconds
+ arrival date: 2028-07-22T22:39:53.559
+ thrust profile: [0.2558750955390311 -0.10480985648507957 -0.13739292619342472; 0.0861857494527859 0.002443399930217527 -0.11267637504037391; 0.12161010773951528 0.02531039120410122 -0.2535510232989823; 0.10344687672405799 0.03133274551605662 -0.2920312661540672; 0.07805589259297771 0.02799380024335257 -0.27346075248463414; 0.03113477608553876 0.011640342049808483 -0.13022726076766525; 0.025631072979846667 0.010338797956805344 -0.11693264982541368; 0.009401542647375492 0.003575149397551719 -0.05126793044973125; 0.003135227316257716 0.0023741958260695218 -0.016284791383724986; 0.0011042753526398332 0.0015384827431491567 -0.006634939207418159; 0.0017531214187727377 0.0007641809945651166 -0.01071129775633082; 0.0003308098198811503 -0.0004984438817623763 -0.002481171898927965; -0.0009448910737236696 -0.0008795877276942701 0.001372961534795595; 0.00023775815023775761 0.0004672475154673638 -0.0015654611056298375; -0.005636132104405717 0.005993694511139838 0.0022702777649691395; 0.0057590843435188135 0.003147498411275979 0.001962709768521656; 0.0029813089216697963 0.00019181940390386354 -0.0017848150871068833; 0.003019942995164588 -0.005587830685862247 -0.005521229041736336; 0.00442374094009712 0.0016903538687081715 0.0011001238221795512; 0.0004254300878097834 -0.007241046070776508 -0.001223029725443866] %
+
+Mass Used: 90.74423822850031 kg
+Launch C3: 102.38913807767183 km²/s²
+||V∞_in||: 0.004549887174455375 km/s
diff --git a/archive/ES_0.5898160717843356 b/archive/ES_0.5898160717843356
new file mode 100644
index 0000000..dd33dfd
--- /dev/null
+++ b/archive/ES_0.5898160717843356
@@ -0,0 +1,22 @@
+archive/ES_0.5898160717843356---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T14:43:59.534
+Launch V∞: [5.830899207068519, -7.58161256779221, -2.355621256190533] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00030384500699891026, 0.0019165861868648555, -0.0025988425962458236] km/s
+ V∞_out: [0.002280649315785183, 0.0018224086007803824, 0.0014226732256072292] km/s
+ time of flight: 1.859073606148835e8 seconds
+ arrival date: 2029-03-22T07:39:59.534
+ thrust profile: [0.5586818988974238 -0.1159193346701789 -0.1811779538963124; 0.13612090367421803 0.056506862186420065 -0.12939798119224347; 0.07986689416180741 0.06247731309025485 -0.12891642631380282; 0.06605794209543248 0.0719651770985428 -0.15162096546710477; 0.0355409543578572 0.04906832118905217 -0.11059131890656258; 0.027755096046049622 0.04648378274242405 -0.10945922311193194; 0.012114113879197348 0.023784485749931746 -0.0595458849165059; 0.014916107684475634 0.03446601070452413 -0.08736187032626773; 0.0063258828202287145 0.01669153256456788 -0.04455564765130192; 0.0018344556125305827 0.005290785595466915 -0.015528072914067522; 0.0003149028520368775 0.0018146654044896558 -0.0006411798735663846; 0.00020998028192442957 0.000773782837600094 -0.0017657552282097037; -0.0013081429895223276 -0.004357663574581781 -0.0022345704815438685; -0.0029023365604173186 -0.0010712663310649343 -0.002679960473220391; 0.002962687254422274 0.0018378889407734498 -0.0014161428922144525; -0.0006663342144350058 0.0005519500485970312 0.00012519669741684102; 0.006015795794255109 -0.006536595387370751 -0.0031245153280396788; -0.0003386998192368068 -4.2926550245477426e-5 0.000776779331000667; 0.00030127088843167954 3.6533240047537184e-5 -0.00043415350263658904; -0.0041656944320452565 0.0025271209393313973 0.007442918178966593] %
+
+Mass Used: 122.11516428506138 kg
+Launch C3: 97.02918619371374 km²/s²
+||V∞_in||: 0.0032433944009357027 km/s
diff --git a/archive/ES_0.5898879510445467 b/archive/ES_0.5898879510445467
new file mode 100644
index 0000000..377449d
--- /dev/null
+++ b/archive/ES_0.5898879510445467
@@ -0,0 +1,22 @@
+archive/ES_0.5898879510445467---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T10:09:59.719
+Launch V∞: [7.394566822713527, -6.566633768854008, -0.3229340961794596] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.556789702262437e-9, -5.266010395898999e-9, 3.5677779061255483e-9] km/s
+ V∞_out: [-3.307664307451278e-9, -6.16666764105167e-9, -2.0886034200964996e-10] km/s
+ time of flight: 1.6141504395526576e8 seconds
+ arrival date: 2029-06-22T15:40:42.719
+ thrust profile: [0.3015963305719811 -0.06517732636462512 -0.1309125782733191; 0.036969644431812644 0.0075398469376151715 -0.0488741201530361; 0.04026441559968304 0.015526253648625756 -0.08009431403024732; 0.05830713496346692 0.0287928519679726 -0.16686732251810332; 0.05423767365899912 0.0308262714020388 -0.19544916501277884; 0.030630493991675643 0.017276247504120833 -0.13093829083846067; 0.019532331434997746 0.012680421882764623 -0.09628824484269871; 0.01284464250375277 0.007551791466358717 -0.07908316357043321; 0.015400793486779005 0.00956880493691594 -0.0604693770294089; 0.0030073993506558876 0.015771207784196772 -0.06268978868470552; -0.016771296431581522 -0.005580749894867549 -0.01757169872136574; 0.004094648064131801 0.0009319227011665786 -0.019781366215302514; 0.026315612014013275 0.030187563146803237 -0.0225370589610351; -0.010772259162598802 0.005117844229481583 0.0011682503138150616; 0.012541531073946628 0.014509275927227854 -0.01581925339285002; 0.09493325586564601 0.0023220152931684333 -0.09251500101569866; 0.0364594531944011 0.040854518809211794 0.02779399315708793; -0.01331297742378704 -0.0157155286595288 0.0502958604910551; -0.027550358031469324 -0.012992403908951193 0.04342469843273468; -0.0769101667236664 0.004046531928362205 0.006982570955961117] %
+
+Mass Used: 117.09253633352728 kg
+Launch C3: 97.90458398030466 km²/s²
+||V∞_in||: 9.877498432365026e-9 km/s
diff --git a/archive/ES_0.5899363137042115 b/archive/ES_0.5899363137042115
new file mode 100644
index 0000000..16e953d
--- /dev/null
+++ b/archive/ES_0.5899363137042115
@@ -0,0 +1,22 @@
+archive/ES_0.5899363137042115---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T12:38:42.975
+Launch V∞: [5.165526869508538, -8.551129846609962, -1.5689701781491987] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.7323204751019943e-7, -9.88804403135156e-8, -1.2266465917191002e-6] km/s
+ V∞_out: [8.72977920543628e-7, 8.550732645074367e-7, 2.1601679473935734e-7] km/s
+ time of flight: 1.3630310350425935e8 seconds
+ arrival date: 2027-08-21T02:37:05.975
+ thrust profile: [0.266071855790255 -0.1780631148642582 -0.15662053652084726; 0.13387971332680162 -0.020243328882140213 -0.17237414406039406; 0.11174756315246724 0.003578696237637245 -0.22245110403384785; 0.09033948932293566 0.011808223111831866 -0.2396861227690501; 0.06161931760271175 0.01208612351047246 -0.20246913775276157; 0.03854926824168146 0.00950590164266555 -0.15062986282207658; 0.01833632810618721 0.005290134349458724 -0.08400833258279941; 0.005403042248331851 0.0035664603771545667 -0.037204440438354955; 0.003958601242809992 0.0015095738502652351 -0.021516020234815875; 0.005694379599782496 0.0018778584946344996 -0.03919301848622355; 0.0007778295718920436 0.0002668534997586488 -0.008234827378861626; -0.0019140205943687701 0.0032763483103847727 -0.00023311878445859448; -0.0009676585624448332 -0.0044202694424831865 0.0013888309366730483; 0.0011200994834267323 0.004239528898235425 0.001576791595664359; -0.0003950017953978282 -0.0003097092106336737 -0.0014176139822833233; -0.0008158015686743217 -3.361080216367988e-5 0.003369854069527673; -0.0049361285830747635 -0.0018131987024575594 -0.009041735787752959; 0.0008457105396326431 -0.001133128741093579 0.0030178634970938114; 0.004022911561240622 -0.009918567118799848 0.003697698486368849; 0.0008189233170522452 -0.0016682363059792066 0.003399680605212126] %
+
+Mass Used: 91.70645066171392 kg
+Launch C3: 102.26615691311991 km²/s²
+||V∞_in||: 1.2427584418290048e-6 km/s
diff --git a/archive/ES_0.5899587725915019 b/archive/ES_0.5899587725915019
new file mode 100644
index 0000000..9f68690
--- /dev/null
+++ b/archive/ES_0.5899587725915019
@@ -0,0 +1,22 @@
+archive/ES_0.5899587725915019---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-17T17:32:36.184
+Launch V∞: [5.342930503025384, -7.931841046428157, -0.2918804007114494] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.55950469782564e-6, 2.1278451646600234e-6, -2.362858983924629e-6] km/s
+ V∞_out: [9.274281789903106e-6, -3.5831456875789714e-6, 1.58301790450966e-6] km/s
+ time of flight: 1.4005459827214777e8 seconds
+ arrival date: 2027-09-24T17:35:54.184
+ thrust profile: [0.8192509672223941 -0.4765507962954766 -0.29554029352556704; 0.3710097426720235 -0.0024347114547476176 -0.3131510147238676; 0.21747027063945548 0.05245309668683482 -0.28490571037162715; 0.15841381870785232 0.062063584464194695 -0.2754956051491808; 0.0902816348686908 0.04597691163156357 -0.1943367618008118; 0.03284955974528799 0.019660487728924477 -0.08571427802567828; 0.027606133433039377 0.01895578328560034 -0.08244595477034891; 0.037378515023444345 0.02609456360719204 -0.11179371148790243; 0.0066064587760467286 0.006497386805485747 -0.026602005414555777; 0.0008369165147659106 0.0009384725194920683 -0.003521524218054721; 0.0021461812343055203 0.0016267317515406303 -0.008949844449258637; -0.0012173643410965944 0.0003771980326859137 -0.0015137985793435133; -0.0013533035012637095 0.00015901533699734624 -0.0015566429623188683; -0.00092232029019288 -0.002088588047619206 0.0030731004140657314; -0.00016088467807584008 -0.0016392953380612427 -0.00370711643368219; 0.00259155214261344 0.0027201528219705827 -0.002116341803026101; 0.0034727794828908367 0.00232135240904824 0.00018357193299552892; 0.005225846319897098 0.003642541904217742 -0.004504966916357846; -0.004024602803592593 0.0027107705532204906 -0.004120348495059323; -0.0003454623067053567 0.00248474454603036 0.002075571329620824] %
+
+Mass Used: 154.26571769011252 kg
+Launch C3: 91.54620291428107 km²/s²
+||V∞_in||: 1.0074470591074791e-5 km/s
diff --git a/archive/ES_0.5899634516922193 b/archive/ES_0.5899634516922193
new file mode 100644
index 0000000..7a4bd8a
--- /dev/null
+++ b/archive/ES_0.5899634516922193
@@ -0,0 +1,22 @@
+archive/ES_0.5899634516922193---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-12T14:36:59.546
+Launch V∞: [6.19592265179746, -8.116416721547518, -0.9091601978445636] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.237400132175331e-6, -9.704790172683058e-7, 2.0638281784635755e-8] km/s
+ V∞_out: [1.401573254415877e-6, -3.138373468619588e-8, -7.165973861270507e-6] km/s
+ time of flight: 1.859332986072711e8 seconds
+ arrival date: 2029-04-02T14:45:17.546
+ thrust profile: [0.18376914586566578 -0.08848983127828046 -0.08529434257625745; 0.018273578858399243 -0.014229112662916073 -0.043985205920541864; 0.02654099337945779 -0.03174295417627659 -0.11357316453977011; 0.028386064482625206 -0.03665448362326449 -0.15144599008769044; 0.014452965688632047 -0.035054719197848916 -0.11025218409345275; 0.013300726175168687 -0.03522591945375091 -0.11362200288856487; 0.009342834558518032 -0.02202335397142438 -0.07070057643388361; 0.007514723518955823 -0.012393576300633913 -0.050002303016924605; 0.006269783949815011 -0.010888833724510195 -0.0428461599532051; 0.004061842760225661 -0.006288806813819623 -0.028263484750333936; 0.0019651465809609613 -0.003600026404119085 -0.015684057286202896; 0.00018225389555026768 -0.0006808462944853546 -0.002521546750291288; -0.0005170887895137253 -0.00039677226389806187 0.0008112716452980402; -0.0006795924657438362 -0.0006171342288930076 0.0010212957512467826; -0.0007817025138683787 -0.0008624893589581678 0.000718819420400243; 0.0005756762471328422 -0.0009003015939848826 0.0011096508159155558; 0.0007087945018518878 0.0012148754536605146 -0.00029468358884485223; 0.000691216146229686 0.0014718154630783246 -0.0006829202111126993; -0.00018422221671592938 -0.0002937197679358948 -9.314201605401356e-5; -0.0009144051988661322 -0.00035119571571011384 0.0014888299653206271] %
+
+Mass Used: 75.25256764798542 kg
+Launch C3: 105.0922501702178 km²/s²
+||V∞_in||: 7.302206251184951e-6 km/s
diff --git a/archive/ES_0.5899643501263658 b/archive/ES_0.5899643501263658
new file mode 100644
index 0000000..112e86f
--- /dev/null
+++ b/archive/ES_0.5899643501263658
@@ -0,0 +1,22 @@
+archive/ES_0.5899643501263658---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T22:49:23.440
+Launch V∞: [5.434076178040938, -7.979693140203385, -0.07712934292812236] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012740279775658543, -0.008252512263887884, 0.010739344343287209] km/s
+ V∞_out: [-0.009212668453232648, -0.00796346184096177, -0.006041504053892505] km/s
+ time of flight: 1.4299743601522648e8 seconds
+ arrival date: 2027-10-30T00:19:59.440
+ thrust profile: [0.624569623969961 -0.3463664026638817 -0.23073327149732795; 0.30200197080123614 0.002216588598689522 -0.26182658059181435; 0.20320975437601843 0.04995151850989129 -0.2720178514847521; 0.17400990715203205 0.06826763530654072 -0.3063256272083458; 0.08308298671557825 0.04243074398217934 -0.18139518266186044; 0.07358028351246339 0.04345038095168517 -0.1882024712046909; 0.026327607783156445 0.017788572346872974 -0.0782128030981825; 0.0073603367484816615 0.004505841736960029 -0.026275986051737206; 0.0059436731707851066 0.003903150330670683 -0.024463364933745894; -0.00413222345689058 0.003679473870973932 -0.00794895282983389; -0.0018808232164782687 0.0018568538758748112 -0.007604848836423978; -0.002584940595285602 -0.009477909980555407 -0.0028250240033203837; -0.006090818800361347 0.007916512253406232 -0.004224944897594681; -0.0027262334039234596 0.007904409059371904 0.002401370897181415; -0.0037312426932496648 -0.004273875881696598 0.0014258999464953023; -0.005356136716000218 0.018163830272481245 -0.008630740291992001; -0.006918285953910273 0.01160086391731915 0.013999261984470678; 0.0016424747127163227 0.0010939163012213112 0.0006075698725872374; 0.019469006798194213 0.0018424852055686823 -3.5268423277903804e-5; -0.01138107127242136 -0.009976080644856992 -0.017465451027837725] %
+
+Mass Used: 144.56303498683474 kg
+Launch C3: 93.21063545610149 km²/s²
+||V∞_in||: 0.01360369886747481 km/s
diff --git a/archive/ES_0.5899800598856852 b/archive/ES_0.5899800598856852
new file mode 100644
index 0000000..f3dafc2
--- /dev/null
+++ b/archive/ES_0.5899800598856852
@@ -0,0 +1,22 @@
+archive/ES_0.5899800598856852---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T07:11:11.186
+Launch V∞: [6.913464720791236, -7.129146932822747, -1.125804474376391] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7542040549628174e-5, 5.85116509243658e-5, 3.6803617729493364e-5] km/s
+ V∞_out: [5.3043741279179864e-5, -4.6229126617751535e-5, -2.416238661223346e-5] km/s
+ time of flight: 1.3192446411694112e8 seconds
+ arrival date: 2028-07-12T04:52:15.186
+ thrust profile: [0.47605855722948803 -0.1890577052960038 -0.24184060738936763; 0.16101813465569512 0.010597384812339508 -0.20045902181764247; 0.09365598506061924 0.024226645863436442 -0.18789339763289856; 0.06608461311125272 0.024634095184079708 -0.1792595467828747; 0.06462886701726939 0.028362006075328777 -0.21488947322100918; 0.04188637437134701 0.020939760436866912 -0.16559205366961538; 0.041982112381928276 0.021933902006764715 -0.19059161751273904; 0.01954138775618921 0.010698757711203237 -0.09748136373701145; 0.005294788658380809 0.00308083159798465 -0.02968855633801009; 0.0018320808145290354 0.0003778309353407003 -0.008860747291801935; 0.0003458558073165275 -0.0008523450755197728 0.0010147439474757392; -0.0011904056435402387 -0.001187170877260201 -0.002129414586678507; 0.000602822230094241 0.0005405140247667843 -0.0025000150474752203; 0.0029422359776553816 0.002200702532347175 -0.003295906748694403; -0.00010965007414807503 -0.0014136079165767662 0.0024879146561359346; -0.0010711182956617566 0.0003278100217381155 0.0023730000743289676; -0.006903590653283586 0.004419228455117855 -0.0026091928013373678; -0.0031136415154230995 0.0002755942526141258 -0.009035805268510604; -0.0023858009011804154 -0.0014159002634316785 -0.0021549620562924176; 0.004599263638129972 0.0031060528737404686 -0.0085640615194378] %
+
+Mass Used: 105.62910065872575 kg
+Launch C3: 99.88816614992692 km²/s²
+||V∞_in||: 7.440889442473177e-5 km/s
diff --git a/archive/ES_0.5900281753621921 b/archive/ES_0.5900281753621921
new file mode 100644
index 0000000..cdd9289
--- /dev/null
+++ b/archive/ES_0.5900281753621921
@@ -0,0 +1,22 @@
+archive/ES_0.5900281753621921---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T14:32:40.556
+Launch V∞: [5.53281141062898, -8.27175715293136, -0.8442721764092375] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8587701775103036e-5, 1.2756680443359475e-5, -2.7040610854525832e-5] km/s
+ V∞_out: [-2.4876280463540284e-5, -2.2432573987555458e-5, -1.0836894631416861e-5] km/s
+ time of flight: 1.3663549032396308e8 seconds
+ arrival date: 2027-08-20T00:50:50.556
+ thrust profile: [0.2582614454138998 -0.15140253309391785 -0.12214386796826729; 0.16670315447182144 -0.006641219943224454 -0.17491178807160598; 0.1410162632568493 0.026345728316206286 -0.22081325649777483; 0.11513651761731412 0.037646533813722176 -0.23353553749203193; 0.08056134679253196 0.03461123905209739 -0.2015403122451276; 0.044696161023196505 0.023239553091239994 -0.13415356451177088; 0.018382521169721704 0.010817838798341282 -0.06541841619065371; 0.03859485927250446 0.020567207015184386 -0.12342694103342516; 0.024687418256429953 0.016110500374175867 -0.09799068905774799; 0.028523180504272837 0.01770363307020038 -0.10640357056798973; 0.018248423106926467 0.00927202669703629 -0.07513930814062164; -0.00016486032594411265 0.0002257281307711463 -0.0008025578444435992; 0.00014068390965869774 2.894510939207133e-5 -0.000952986320909017; 0.0006542907814487287 0.0010588426154270027 -0.001512058468220935; -0.00010881023181353718 0.0002975330427135824 0.0004254197812999558; -5.00143338169317e-5 1.03146819363032e-6 -0.0005811251291030759; 0.00034040199276465824 -0.0012473976446151875 0.0006291944611611583; 0.00019508020130488556 -0.0013765096159604711 0.0007318501182105284; -0.0008740007986599422 0.000727546552960441 0.0010536892801507197; 0.001069049096018013 -0.0015029169837595811 -0.0010799504232178003] %
+
+Mass Used: 106.51008119454673 kg
+Launch C3: 99.74676401051613 km²/s²
+||V∞_in||: 3.5205542015427894e-5 km/s
diff --git a/archive/ES_0.5900801647758911 b/archive/ES_0.5900801647758911
new file mode 100644
index 0000000..7d313b0
--- /dev/null
+++ b/archive/ES_0.5900801647758911
@@ -0,0 +1,22 @@
+archive/ES_0.5900801647758911---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T20:53:04.646
+Launch V∞: [5.281441630152116, -8.350664189822583, -1.0975557937662475] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.06683291459722639, -0.09979310849619753, 0.017174122639314945] km/s
+ V∞_out: [-0.11378842147420241, 0.03721886170842599, -0.019713254112366168] km/s
+ time of flight: 1.3410806680837198e8 seconds
+ arrival date: 2027-07-23T01:07:30.646
+ thrust profile: [0.3649020220001632 -0.23970778591558875 -0.1915776464512217; 0.21845223645730594 -0.024231117046569887 -0.2423267335883603; 0.18165840570074404 0.017680815942393836 -0.3058385862085774; 0.14785495111465333 0.03221459819222867 -0.3271046433113824; 0.09517742542994201 0.02848050023593541 -0.25716070127502205; 0.03500016790186748 0.012719160352283708 -0.11134787027197035; 0.008628591707006155 0.003664389471003544 -0.032798485358814605; 0.008356028425479556 0.004187773638795079 -0.036039614490409946; 0.00012893180810251464 -0.00028472188498329903 -0.002629735164908159; 0.0015183920326732 0.0022797465792363937 -0.013599487716299184; 0.0034719473306975995 0.0019945518489426417 -0.017968963549720367; 0.0015537820275147675 0.0006003061086463429 -0.0018121869369487247; 0.0017566872439863295 -0.0019765478571272905 0.0037045623418636283; 0.00923459974252569 -0.004508473712880936 0.0028812042375063753; -0.00023034891254501352 -0.0024022120014553635 -0.008634284297026158; 0.004748406468201949 0.0028743108068275533 -0.0013016717288454704; -0.009346667409344474 -0.0032460030577201957 -0.007198084441635029; 0.004286811768540103 0.0025625387821969605 -0.007160013984122027; -0.0006646569793679158 -0.006453205269628652 0.0015661175988709005; 0.0016965947369911895 -0.011740928491828399 0.01038558755530628] %
+
+Mass Used: 111.90775243001235 kg
+Launch C3: 98.83184682431896 km²/s²
+||V∞_in||: 0.12132705166336252 km/s
diff --git a/archive/ES_0.5904035063558207 b/archive/ES_0.5904035063558207
new file mode 100644
index 0000000..d67a7d7
--- /dev/null
+++ b/archive/ES_0.5904035063558207
@@ -0,0 +1,22 @@
+archive/ES_0.5904035063558207---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T10:05:07.987
+Launch V∞: [5.239598106899442, -8.496583547486258, -1.0152804008456984] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0035036200535848, -0.0022142507896770356, 0.0020139905134589986] km/s
+ V∞_out: [-0.0027542364754951686, 0.0033065006799395938, -0.001908395347139841] km/s
+ time of flight: 1.3211075236293542e8 seconds
+ arrival date: 2027-07-01T11:30:59.987
+ thrust profile: [0.3330762005871614 -0.21788007266013784 -0.18350264284790918; 0.10830335121917552 -0.015159971981119735 -0.12912171380547588; 0.1497816674553335 0.010474570833719195 -0.2652379416904857; 0.12098008814812877 0.02152753842530706 -0.27893434443194925; 0.07846658340691136 0.018967650630853535 -0.2211625501653504; 0.045475614559518915 0.013019409212840595 -0.15148419634988824; 0.027155936021892278 0.009195311391686252 -0.10230320176147038; 0.025038405270160546 0.009150009686416336 -0.10344833761526723; 0.013879796470547092 0.005696376404312933 -0.06444882460324178; 0.0029341155384330292 0.0011456476897700571 -0.016564787129323345; 0.0033314088449101216 0.0014391397431539874 -0.017440076333560803; 0.00018139243920155143 1.1438779012331159e-5 -0.0009220001348893478; 8.52265653588126e-5 -5.127920114149243e-5 -0.00012088536347653017; 0.00014400956365626441 4.377613294150715e-5 -0.0008172621857909176; 8.326810313856236e-5 0.0001469430624901061 -0.0007100274278203394; -6.939757770829376e-5 -6.919882122662888e-5 -0.00025868073924823485; 0.00010234435870014151 -5.917889696433745e-5 -0.00011288072263134375; 2.333473983682691e-5 0.0005744539117598141 -0.00025642291042214275; -0.00037794259765590917 0.00044898418417850484 -2.0493348787493362e-5; 0.000302543839881721 -0.0003939085142243676 0.0001941484425008361] %
+
+Mass Used: 101.52675561924207 kg
+Launch C3: 100.67611459357978 km²/s²
+||V∞_in||: 0.004608081794821982 km/s
diff --git a/archive/ES_0.5904198903780923 b/archive/ES_0.5904198903780923
new file mode 100644
index 0000000..b327175
--- /dev/null
+++ b/archive/ES_0.5904198903780923
@@ -0,0 +1,22 @@
+archive/ES_0.5904198903780923---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T02:28:55.060
+Launch V∞: [5.193220500373245, -8.442197655802035, -1.265499242320365] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0023721709434486628, -0.014582060897466697, 0.01583376176823264] km/s
+ V∞_out: [-0.014768241599258498, -0.013443262242553676, -0.008340719257132416] km/s
+ time of flight: 1.4213370566614693e8 seconds
+ arrival date: 2027-10-28T04:04:00.060
+ thrust profile: [0.39196692494301566 -0.25000858250094893 -0.2210860134145036; 0.061780732009116046 -0.007651044251294587 -0.08370238137602218; 0.08337695673141726 0.004671405021258258 -0.17380555205152587; 0.0853776389908601 0.012882975209712776 -0.2352472296119473; 0.05982747090252652 0.012834756019674948 -0.2055732589888375; 0.02788778267962956 0.007071722659639229 -0.1165908445601354; 0.022927717103027816 0.006103310138958586 -0.10622737353205775; 0.016168205450104795 0.0037021147770893636 -0.0933021869027551; 0.014415778270757768 0.007403684379915382 -0.06316606927161625; 0.0056969636814845105 -0.0003969154064920027 -0.03167013784862273; 0.0014750607089635951 -0.0007189829544481208 -0.010228223403794697; 0.0016873396627856252 -0.0021718581943318853 -0.007704511089493899; -0.0018390232440798136 -0.002734018519174375 0.004638504023316198; -0.00045577761121507257 -0.0045276586335476115 -0.014329113368495603; 0.0009785021540973946 0.0005181413519173709 -0.009854666167227364; 0.0118142093483147 0.017562432464469594 -0.014249189385876207; 0.009435643933085686 -0.004783272875364466 0.009645915740020869; -0.02133313761301503 0.01080820480272518 -0.0075706097199137855; 0.003898717490095143 -0.01296124188121153 0.010664904283915403; 0.03973616080080265 0.009993153877326591 -0.029982995876924004] %
+
+Mass Used: 106.41312102270922 kg
+Launch C3: 99.84172875743974 km²/s²
+||V∞_in||: 0.021655754587072577 km/s
diff --git a/archive/ES_0.590802372545698 b/archive/ES_0.590802372545698
new file mode 100644
index 0000000..dd2705c
--- /dev/null
+++ b/archive/ES_0.590802372545698
@@ -0,0 +1,22 @@
+archive/ES_0.590802372545698---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T10:02:26.129
+Launch V∞: [6.839153737873967, -7.0814497604194635, -1.1165090995786258] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001460482346443163, 0.0027049898767629366, 0.0009847868223291922] km/s
+ V∞_out: [0.001306206100680898, -0.0016341300305706173, 0.0024584178694345526] km/s
+ time of flight: 1.2988617637473796e8 seconds
+ arrival date: 2028-06-17T17:32:02.129
+ thrust profile: [0.6952341337693616 -0.28710619076464267 -0.34702954151509274; 0.14534102525940293 0.007645184935406783 -0.17580366197980093; 0.1155053351248405 0.028701805151153767 -0.22217716844718532; 0.08793001901200424 0.03193392753017209 -0.22853270609797255; 0.07041093919398807 0.030928884524091815 -0.2264034458628068; 0.049282639613547 0.02456063283272249 -0.1865863022124448; 0.027182520258393534 0.015125730390607987 -0.11785044190244255; 0.013298036426131551 0.007988979552284298 -0.0648705764797446; 0.0013714413603525982 0.001024665292448475 -0.007567337841565579; 0.005556367263614177 0.003635959007569165 -0.03210734945223991; 0.0011487625272607925 0.0008733090824147935 -0.007305905587664379; 0.0020608215819633733 -0.0015972508787041877 -0.002646239738058426; -0.0010094701295438463 0.0010246858075966467 -0.0009129682543860449; 0.0008346704821795177 0.00015922117815941785 -0.0016034739149775185; -0.0022373039140783585 0.001003477502361458 -0.00013977162562369512; 0.0022838681628790073 0.0008863911337749367 -0.0026943791582068224; -0.0044537152584810885 0.003494100748049299 -0.002116224192793223; 0.00020492855555322002 0.0007660963956580977 -0.00017762099352709422; -0.0002877824486077845 -0.001739939611578599 0.005798293524782463; -0.001049355290861611 -0.00018821501473152322 -0.002686475842108756] %
+
+Mass Used: 116.62540971711815 kg
+Launch C3: 98.1675471290622 km²/s²
+||V∞_in||: 0.003227969021396476 km/s
diff --git a/archive/ES_0.590871893605786 b/archive/ES_0.590871893605786
new file mode 100644
index 0000000..94fb163
--- /dev/null
+++ b/archive/ES_0.590871893605786
@@ -0,0 +1,22 @@
+archive/ES_0.590871893605786---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T21:09:07.530
+Launch V∞: [7.717193815350357, -5.397761945697821, 1.5045365435154732] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4783532575036413e-9, -1.4779001725070837e-9, -1.4786564573350336e-9] km/s
+ V∞_out: [-4.6878345405216574e-15, -9.923557230683473e-15, -4.107772615895777e-16] km/s
+ time of flight: 1.8749577772800547e8 seconds
+ arrival date: 2030-04-10T23:18:44.530
+ thrust profile: [0.8343196560028684 0.026906466103142932 -0.07479854910499349; 0.4603006386920117 0.34234652638985497 -0.18729816436243268; 0.1511402742915892 0.1949188318195279 -0.1302252197323976; 0.06099373559289805 0.11320377097607329 -0.08837789750175297; 0.011618632561646018 0.02861219487074135 -0.02544365098784529; 0.009666419721307367 0.03132888082082753 -0.029510188326420498; 0.010755209766874309 0.045753025019650576 -0.04490174830108756; 0.007446937460197477 0.04128477679556508 -0.04204661814930944; 0.0003767435583490181 0.002317351573537131 -0.002911525168453627; 0.00012671877137541583 0.0010290427863767304 0.00018005905479620825; 2.494265673402425e-5 0.0018701553149250223 -0.0019628658842927617; 0.00017116865773375323 -0.000910760979690951 -0.0005092629758762044; 0.00042480304114447576 0.0006094794207108735 0.0011250864869035131; 0.0025574004809512494 -0.0013170770007642535 -0.0013242056227490066; -9.733647450314132e-5 0.0007306406796311279 -0.0009708285664512852; 0.000805236030069103 0.0028070866110458297 -0.000526376110432035; 0.0003943571248241859 -0.0014913343246606662 0.0010631018349369647; -0.0007348422336156272 0.002893795469587463 0.004036119519464739; -0.006718624464429363 0.0013665676281898462 -0.004502644075526852; 0.00508965336997583 0.006536644424692354 -0.004405844121235425] %
+
+Mass Used: 158.78236560829055 kg
+Launch C3: 90.9545446168788 km²/s²
+||V∞_in||: 2.5604964738672627e-9 km/s
diff --git a/archive/ES_0.5908797533582762 b/archive/ES_0.5908797533582762
new file mode 100644
index 0000000..799e2cd
--- /dev/null
+++ b/archive/ES_0.5908797533582762
@@ -0,0 +1,22 @@
+archive/ES_0.5908797533582762---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T12:14:59.957
+Launch V∞: [7.184803650487908, -6.911736799111855, -0.7768033038116386] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.54496020536813e-6, -2.3250202996113062e-5, -1.2092342488024806e-5] km/s
+ V∞_out: [-2.0489538843694724e-5, 1.5699065844250794e-5, 9.842882618204777e-6] km/s
+ time of flight: 1.441754485499593e8 seconds
+ arrival date: 2028-12-02T04:59:07.957
+ thrust profile: [0.2290761239604694 -0.07114296959792446 -0.10210885048838161; 0.09188776525353826 0.008113991807386972 -0.11141955310376211; 0.06553383537794752 0.020442392390956264 -0.1261279573350389; 0.06045404330829421 0.028074754338896883 -0.16234921901104327; 0.04234549625372765 0.022351046099425717 -0.14032492588239118; 0.05147201279621019 0.03142738550552454 -0.17465316699477884; 0.03767502927442125 0.01659814608732946 -0.14572814692000105; 0.02515187257007958 0.014188190249052454 -0.13872221703012427; 0.0017184421452800143 0.009506587003545602 -0.03030429344745951; 0.00021750700976427492 0.001644633519434676 -0.0035713036027916183; 0.03447736910810915 0.019756574714810834 -0.16572182849345587; 0.008394826571171923 -0.005699817870296133 -0.0016837227253425683; 0.01938590603305058 -0.006113614094864731 -0.01251357852374059; 0.030634506070486164 -0.012371020233843148 -0.013710711787721106; -0.01823068656814876 -0.02576155748762314 -0.02845228060353481; 0.01909014950031684 0.030212707228252336 -0.030931170664343515; -0.009821561661862621 -0.03277346741467453 0.0019757860629261155; -0.001677104845812355 0.03312436403054824 -0.03538069006882937; -0.01921854878327398 -0.02001259519746267 0.03144317759869096; -0.0044835227516083435 0.0021900042393963553 0.003327779782811945] %
+
+Mass Used: 106.04427296505719 kg
+Launch C3: 99.99693244907402 km²/s²
+||V∞_in||: 2.7564706258537922e-5 km/s
diff --git a/archive/ES_0.5909110127623465 b/archive/ES_0.5909110127623465
new file mode 100644
index 0000000..6f14a86
--- /dev/null
+++ b/archive/ES_0.5909110127623465
@@ -0,0 +1,22 @@
+archive/ES_0.5909110127623465---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-11T16:13:18.106
+Launch V∞: [6.071584360446247, -8.206714398693823, -0.7894255582671011] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.180919414225473e-7, 4.4954621992144113e-8, -6.254623019884117e-8] km/s
+ V∞_out: [2.2504233068876613e-7, -1.923387031238481e-8, 2.630789960155167e-8] km/s
+ time of flight: 1.840297350218607e8 seconds
+ arrival date: 2029-03-10T15:35:33.106
+ thrust profile: [0.17227261602713076 -0.07650978789628801 -0.09120092815216935; 0.00997353043532647 -0.004217632979969365 -0.02112814961277336; 0.029855353585460685 -0.014627565409466617 -0.10218798026287076; 0.02961816899426294 -0.019792325627943974 -0.14140639145274309; 0.022579653422570102 -0.020383068707433376 -0.13203588877371894; 0.014329542072031272 -0.015708050324264266 -0.09342261302491808; 0.013903188875078342 -0.01687994007894972 -0.10003509271958923; 0.010353731900913437 -0.01355622001912823 -0.07829234161507637; 0.004545055040348892 -0.006879444232151856 -0.03632860535018345; 0.002768451679362776 0.0016864778966367128 -0.01085335850998458; 0.004903915630277261 0.005011489077371432 -0.013440627003184047; -0.00036184723489939333 -0.003159226787301318 -0.009974173804498134; 0.0030818988642053935 -0.005008040008574397 -0.028448054464862385; 0.0032092349398872384 0.010749049698290412 0.0004025187761694292; -0.0019512861267525837 -0.0023346341105673256 -0.00968403339043482; -0.0023414334337437553 -0.0007505165944133062 0.003558360634854295; 0.0006513343663690542 0.0024454474945811502 0.003992459420603074; 0.0009672039378086066 -0.0012258162379004964 -0.002271449252641008; -0.0020147754558248864 0.000873831241714093 0.005166440055261328; -0.01031947658928298 0.0028649135733193162 0.01687055279496451] %
+
+Mass Used: 77.84415317396679 kg
+Launch C3: 104.83749057978929 km²/s²
+||V∞_in||: 2.3129427979091658e-7 km/s
diff --git a/archive/ES_0.5910389799691018 b/archive/ES_0.5910389799691018
new file mode 100644
index 0000000..02135fd
--- /dev/null
+++ b/archive/ES_0.5910389799691018
@@ -0,0 +1,22 @@
+archive/ES_0.5910389799691018---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T17:19:20.511
+Launch V∞: [5.183603114069906, -8.771999289885844, -0.9506517505838098] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.3880712417568236e-8, -2.1301779802513984e-8, 4.703173720894914e-8] km/s
+ V∞_out: [1.9787745764388402e-8, -4.6907621544864777e-8, -5.520620501233965e-8] km/s
+ time of flight: 1.4848155801481804e8 seconds
+ arrival date: 2028-01-15T06:11:58.511
+ thrust profile: [0.12185262066568023 -0.08422028545886971 -0.08029130554209607; 0.03801735853875402 -0.012244278186315226 -0.06751629606876616; 0.06863358276538582 -0.01767348493762632 -0.19398053524473352; 0.0719093532129225 -0.019483809937839606 -0.2716003313151306; 0.05490495117510288 -0.01764253660740588 -0.25953888230135097; 0.025467152412148242 -0.010216578542034036 -0.1456997842815586; 0.009810005466230797 -0.005312014322915187 -0.0672777401893721; 0.005275864086647413 -0.0032652402358622516 -0.03900590180474228; 0.003753590548676911 -0.00228978670486875 -0.04564919817956047; 0.0005402694248682692 -0.0006931691874787411 -0.0062543961162308745; 0.0005590919841963226 -0.00026342083067091876 -0.004179687969818841; 0.0002061565797163046 0.0005379794496291512 -0.002014345351198642; -2.484282416081009e-5 -0.00021807655560936244 -0.0013051387781349245; -0.0001413385751118079 6.72488630850134e-5 0.00040087036505778847; 0.0004920042469477436 0.0005245125091177505 -0.0004175749310996579; -0.0004679680441531833 0.00013043612678296693 0.0005587521522066037; -0.0025889874185939877 -0.00032633329256550215 0.001064549478058409; -0.0005399875203663813 -9.847906564475536e-5 0.00014695885048640394; 0.0006980145736851383 -4.602435282044878e-5 0.004618466239374396; -0.001023661018540636 0.0014689132298162596 0.0033625812836588784] %
+
+Mass Used: 78.67034266571272 kg
+Launch C3: 104.72145153684104 km²/s²
+||V∞_in||: 7.462493750932818e-8 km/s
diff --git a/archive/ES_0.5910663991779802 b/archive/ES_0.5910663991779802
new file mode 100644
index 0000000..c308f0f
--- /dev/null
+++ b/archive/ES_0.5910663991779802
@@ -0,0 +1,22 @@
+archive/ES_0.5910663991779802---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T22:53:39.984
+Launch V∞: [5.53489895494837, -8.164027027303785, -0.47688286306622657] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.422524954265037e-7, 2.285420586431058e-7, -4.7256296553469235e-7] km/s
+ V∞_out: [-3.2447217703803623e-7, 4.86378358915335e-7, 4.7487113078512695e-7] km/s
+ time of flight: 1.472960475375054e8 seconds
+ arrival date: 2027-12-23T18:27:46.984
+ thrust profile: [0.3122514510355738 -0.17473666944140312 -0.13950901791882445; 0.09413731011221599 -0.0038220088401207694 -0.09941321587281185; 0.11796135447427665 0.019504269585181477 -0.19482784450140633; 0.09993287013198066 0.02851137730525523 -0.21998811239273963; 0.07722924444320646 0.02864803254299917 -0.20901466204841032; 0.0583126006739788 0.02530479123300413 -0.18279810959107726; 0.035917888673987 0.017022461655761757 -0.12871827635549393; 0.018280137923489367 0.008592239755697475 -0.075089012748169; 0.007818923483342746 0.01832623812358357 -0.0267328816104278; 0.006316480308948315 0.0024469181546095072 -0.03128669691476894; 0.006693648851903999 -0.00036372751718291856 -0.012886532456213498; 0.01828452805697619 -0.0039290052276981045 -0.014401990918196564; 0.017858137475671332 0.012925496971484911 -0.014845339866453412; 0.0027762296179612185 -0.00041335572414389227 -0.008309206384077557; 0.009859498636696851 0.040119767321220745 -0.010403789769500203; 0.01973171133003853 -0.05155954770693353 -0.10516987803411852; 0.005866145790729259 -0.00756509411908177 -0.0007828389194845177; 0.014764089048751648 -0.0016020228511775183 -0.003061397497764653; 0.0636619949437642 0.035394192088581404 0.011881832930538308; 0.017967925834544974 0.004675704601749376 -0.03123905348253886] %
+
+Mass Used: 120.74660982110163 kg
+Launch C3: 97.51386100912148 km²/s²
+||V∞_in||: 7.547085515349896e-7 km/s
diff --git a/archive/ES_0.5911016714202526 b/archive/ES_0.5911016714202526
new file mode 100644
index 0000000..c704708
--- /dev/null
+++ b/archive/ES_0.5911016714202526
@@ -0,0 +1,22 @@
+archive/ES_0.5911016714202526---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T10:22:46.142
+Launch V∞: [6.932355096921818, -7.156597527179111, -1.18441744539177] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010197884772783255, 0.05483994377086775, 0.056513355754998246] km/s
+ V∞_out: [0.0698315270845466, 0.008239038245227382, -0.036909177497499] km/s
+ time of flight: 1.297703685064945e8 seconds
+ arrival date: 2028-06-16T09:42:14.142
+ thrust profile: [0.3839514948152567 -0.14438002633206914 -0.18002354305014068; 0.17534446880412038 0.017647774386171027 -0.19434360433222125; 0.12412360188882658 0.03884112024510855 -0.2162035797279671; 0.15540125773991365 0.07219021036713812 -0.35347850922280666; 0.07103778385795556 0.038611330125535234 -0.2073677351409536; 0.04123281133612903 0.02573648281424359 -0.14608622282150124; 0.02295008953896382 0.015019926889368646 -0.09278268715990763; 0.012537111784116746 0.008807544352440794 -0.057238275655441095; 0.004817154936712663 0.0034492616863335754 -0.026018101449807977; 0.004741995575502483 0.0040970453939830785 -0.02471345666096534; 0.0023964630903119686 0.002268777771033406 -0.014837307144283444; 0.0013908241490836917 -0.0007307252947715915 -0.000886086836027697; -4.9771984449373035e-5 -0.0007327166024326151 -0.0010220286813140728; 0.001357198118872286 0.0017612889474323352 -0.007595788211086429; 0.0009331005252415404 0.003208253069455983 -0.002093987939579653; -0.00021109600703906294 -0.001462561219476203 -2.7735238106074006e-5; 0.0008048308753775665 0.0005128079667946763 -0.0012796622558359854; -0.0017881512076664758 0.0014361318499811297 0.004583167053031942; -0.000572295860633613 0.0003019526384146773 -0.0005752271299452865; 0.0010324997183073091 -0.0002679593904317914 1.672792858180256e-5] %
+
+Mass Used: 102.33448308567222 kg
+Launch C3: 100.67728004079244 km²/s²
+||V∞_in||: 0.07940513626536948 km/s
diff --git a/archive/ES_0.5912289746683409 b/archive/ES_0.5912289746683409
new file mode 100644
index 0000000..e7f0152
--- /dev/null
+++ b/archive/ES_0.5912289746683409
@@ -0,0 +1,22 @@
+archive/ES_0.5912289746683409---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T09:37:31.258
+Launch V∞: [5.163451689743984, -8.336040433260855, -0.9709753754623087] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.12334092076295844, -0.17468894451876504, 0.031057309342998215] km/s
+ V∞_out: [-0.20173930744641036, 0.06836359415619367, -0.03635714566090429] km/s
+ time of flight: 1.3089493414149739e8 seconds
+ arrival date: 2027-06-15T09:19:45.258
+ thrust profile: [0.6346150112192495 -0.4079708475378032 -0.2924126083646776; 0.20001381919949446 -0.018425907009554095 -0.21238548687745862; 0.11900294165835239 0.014429358307087378 -0.19160760132795718; 0.08863974941664883 0.022126695889915497 -0.18642551530581578; 0.09760385217966439 0.032068147562305575 -0.2387556990707881; 0.08678677685222069 0.03571272795079391 -0.2474267310843815; 0.04355381024788421 0.01985361717542317 -0.14300052730271534; 0.022117612837069978 0.011051742709365731 -0.0816337451611818; 0.012522296810777489 0.006585575516385236 -0.05032383898598876; 0.002026250827956467 0.0016406150666078126 -0.010176850150560104; -0.00017401490377968608 -0.00024490121484243297 -0.0003291663684363838; 0.0009833951414583559 9.118953230000275e-5 -0.0014573673635635402; 0.0001710449973107019 0.00011699850813369947 -0.0008117685453488458; 0.0004158230756040553 0.00015501942255731225 -5.9545882944670976e-5; -0.0001076173464999179 -1.4501964768936251e-5 0.00022773724029932484; 0.00040587791798220725 0.0011655925654392063 -6.32373398843372e-5; 0.0001799310296728477 -8.615191150848189e-5 -0.0003901167299511011; -0.000988372427515061 0.0005622408273608379 0.0015521197487873384; -0.00029918430714296154 0.00035440261917256134 -0.00018769418760870938; -4.094109971947721e-5 -0.00022881371306647963 0.0009635623811757317] %
+
+Mass Used: 123.38782339703266 kg
+Launch C3: 97.09359663703401 km²/s²
+||V∞_in||: 0.2160874048512806 km/s
diff --git a/archive/ES_0.5913646500408956 b/archive/ES_0.5913646500408956
new file mode 100644
index 0000000..4e54c1d
--- /dev/null
+++ b/archive/ES_0.5913646500408956
@@ -0,0 +1,22 @@
+archive/ES_0.5913646500408956---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T13:34:44.176
+Launch V∞: [6.896845945180638, -7.184269529108743, -1.113139555022501] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2057581910804737e-5, -1.1547431298844493e-5, 6.655679866100547e-7] km/s
+ V∞_out: [1.253420602180203e-5, -8.36108254382742e-6, -7.199488221200787e-6] km/s
+ time of flight: 1.3514657443926468e8 seconds
+ arrival date: 2028-08-19T18:17:38.176
+ thrust profile: [0.3532207771609318 -0.14009610109678833 -0.1756349373408019; 0.148191850410202 0.007730975669725036 -0.17917597042537906; 0.12263622745766395 0.028332455273510245 -0.23855384925448825; 0.0971874996262243 0.03198063098324516 -0.2572458435402679; 0.07478062401831756 0.0291618795405659 -0.24649779286557597; 0.03847747417886953 0.016447970147448795 -0.15164851829413922; 0.009622896391031316 0.0036528698769296517 -0.04160746851374081; 0.008430579391332457 0.002779910747633921 -0.018154016132401495; 0.002946715169276251 0.0037425425112401897 -0.048005376500835646; 0.006692792922327743 -0.0021914279722822475 -0.027064408891296275; 0.007544835144000261 0.0031751205388577232 -0.03460069680089372; -0.0037039310492194217 0.0012730765982513176 -0.004699631119002529; 0.0022107561614545944 0.002954779947054594 -0.009462593036601526; 0.0016963072075229452 -0.0029102973587126144 0.005323261132629942; 0.012241960694014342 0.0028050136606203534 0.007532657440740142; 5.7316757831015855e-5 -0.0006089599242196826 0.0009549611102047642; -0.017128415091765957 0.010211239783762371 -0.016135480138160182; -0.011812221787875369 0.005307084054164357 -0.030604998538700065; -0.009483400961911978 -0.01406663419456836 0.0063393309596036975; -0.026663299180001817 -0.015264709554328185 0.0007286726306021852] %
+
+Mass Used: 104.14621980459924 kg
+Launch C3: 100.41929232739066 km²/s²
+||V∞_in||: 1.6708423979600807e-5 km/s
diff --git a/archive/ES_0.5914505122398476 b/archive/ES_0.5914505122398476
new file mode 100644
index 0000000..80d11db
--- /dev/null
+++ b/archive/ES_0.5914505122398476
@@ -0,0 +1,22 @@
+archive/ES_0.5914505122398476---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T23:26:04.948
+Launch V∞: [6.991745215762482, -7.095469546207976, -0.9501941413342277] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004653730953681454, -0.00432981458607621, 0.0031527733012884193] km/s
+ V∞_out: [0.003133022783241109, -0.006360137029048016, 0.00027004425736987725] km/s
+ time of flight: 1.3330883864398673e8 seconds
+ arrival date: 2028-07-27T21:40:02.948
+ thrust profile: [0.36554077276449526 -0.14168779217994656 -0.1645483460679727; 0.1395714495735207 0.011095163410010768 -0.15270588079746844; 0.12297688941089284 0.03290370902345106 -0.20762373829600245; 0.08849992499798814 0.03314075898612289 -0.2050550997539409; 0.054582510820490954 0.027191235035495413 -0.16701255848480703; 0.0447805644746967 0.024490848956362162 -0.1548086611823253; 0.010016278931306579 0.008049778220501114 -0.05411361674604914; 0.030423655999797766 0.018835986301314406 -0.1359629431740928; 0.023248617561838457 0.016688274942591733 -0.12194147528698211; 0.024797689490400312 0.016035353738165455 -0.12537185855965177; 0.007918645402672009 0.0012063395564631003 -0.01789813763682523; 0.0061941087818102565 0.004475326124937932 -0.013008867103301083; -0.001892270313823693 8.292665914490412e-5 -0.0005860421594865838; -0.010452257776862624 0.000919052405419092 -0.0032469118097835205; 0.0002451932318381482 0.0007421683788467054 -0.010832667678343528; 9.67400886120772e-5 0.003493245960127481 -0.007370250410547871; 0.005744651807918029 -0.013812540413333504 -0.00428040972076621; -0.008977021197173089 -0.010866375613908637 -0.0021706778590811298; 0.0032795142322821613 0.0003058627534467442 0.001574008168914588; 0.0003632630031608295 0.0023837018674221838 0.00018133829906513254] %
+
+Mass Used: 105.91609174090718 kg
+Launch C3: 100.13305814952828 km²/s²
+||V∞_in||: 0.007095384811859626 km/s
diff --git a/archive/ES_0.5914908352373625 b/archive/ES_0.5914908352373625
new file mode 100644
index 0000000..cf087e9
--- /dev/null
+++ b/archive/ES_0.5914908352373625
@@ -0,0 +1,22 @@
+archive/ES_0.5914908352373625---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T09:44:41.524
+Launch V∞: [6.9857649581073185, -7.266745849582478, -1.4732413139581821] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8213164408907634e-5, 4.096238139756621e-5, 2.554553403795548e-5] km/s
+ V∞_out: [3.725874380580779e-5, -3.1296688955432695e-5, -1.7183296530175158e-5] km/s
+ time of flight: 1.2972461651295185e8 seconds
+ arrival date: 2028-06-17T20:21:37.524
+ thrust profile: [0.2433789030432709 -0.10475996319332966 -0.14121824278109396; 0.12525854052589805 0.0030436759368883534 -0.17484144157345433; 0.10892483581242836 0.022356730237287722 -0.2449992293053004; 0.07274198429280475 0.02237439792833811 -0.2219816568157435; 0.06066805198363636 0.023001186616413632 -0.23371928439785403; 0.03451222065061334 0.01312181457080856 -0.15201574832899958; 0.02392823550487185 0.009054303241152022 -0.11907543149685079; 0.006525985666331172 0.002887794652092739 -0.03759295726858248; 0.004680544136162498 0.0021234505386229187 -0.03056574989220681; 0.0035594287263398467 0.002101201738007017 -0.023181440846752093; 0.00030301625681129806 0.00012897191170882798 -0.0025935582709934956; 3.298501884370033e-5 8.74346757247768e-5 -0.0025711198438728247; -0.0001402232378385322 -8.435312243640475e-6 -0.0003772290211065163; -6.586774245581846e-5 3.286210637672793e-5 -0.00020126429306949894; -4.9663805959100865e-6 -3.664859820802827e-5 -4.539190651812325e-5; 0.00010726401257525973 -8.496027567036251e-5 -0.0006987248161123644; -0.00011562118401098158 -1.3608039311018076e-5 -0.00015609970953828277; 1.017430842068965e-5 0.0001117046322333149 0.00010279028524390696; -7.101292354264255e-5 7.700748832904737e-5 3.983126704383327e-5; -0.00011394797703568101 -2.8938845268437438e-5 -0.00011327722286094309] %
+
+Mass Used: 84.70711541818719 kg
+Launch C3: 103.77694726149755 km²/s²
+||V∞_in||: 5.159661187355154e-5 km/s
diff --git a/archive/ES_0.5915125899325326 b/archive/ES_0.5915125899325326
new file mode 100644
index 0000000..e4ef275
--- /dev/null
+++ b/archive/ES_0.5915125899325326
@@ -0,0 +1,22 @@
+archive/ES_0.5915125899325326---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T18:29:06.935
+Launch V∞: [6.485921189009788, -7.388745051476015, 0.24113312366023495] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2563252479870891e-6, 0.0003948084914098055, -0.0002946331286379544] km/s
+ V∞_out: [-0.00023351961619618738, -0.00042773164933003385, 7.170156567777677e-5] km/s
+ time of flight: 1.844514108066306e8 seconds
+ arrival date: 2029-03-03T14:59:16.935
+ thrust profile: [0.30429273067808804 -0.08056822759907678 -0.09887741253316544; 0.06236630360044868 0.017291997770420363 -0.05324929800400836; 0.07024322239710698 0.03855346681432963 -0.11250914948883141; 0.04383580632142736 0.031380718374884556 -0.08940353066553494; 0.045407438538179835 0.041678201111027526 -0.1336184839125876; 0.0377996237344507 0.034626112231828245 -0.11781122221422284; 0.022036356609691967 0.026998955255950054 -0.08315739584605128; 0.0055129064724458166 0.01317812302650826 -0.029864906377753134; 0.006106867263902334 0.008013234435518195 -0.018642732497393472; -0.0018904926593582426 0.011063477122971097 -0.015344106943569646; -0.0020436378990615154 0.007900276082164034 -0.014451664695721449; 0.0022812672822184314 0.0017181829332282093 -0.016635139813986132; -0.002527602861849736 -0.005693624473139151 -0.007279230570793067; -0.04457307987591259 0.010835273192901817 -0.06968745451153646; 0.012728032823257412 0.01111279433496502 -0.03652418756178407; 0.026985087287126723 0.00841470734045494 -0.010064134508007307; 0.05231776527830545 -0.05166644174744767 -0.11597147804418648; 0.02192557274918387 0.023430820064725834 -0.0951684271351102; 0.10487890521776855 -0.026905931196884187 -0.04657005075680092; 0.03492131950867737 -0.030140014827868676 0.04789856745251152] %
+
+Mass Used: 125.9045999016339 kg
+Launch C3: 96.71887228908358 km²/s²
+||V∞_in||: 0.0004926296821481676 km/s
diff --git a/archive/ES_0.5917516635974417 b/archive/ES_0.5917516635974417
new file mode 100644
index 0000000..3258885
--- /dev/null
+++ b/archive/ES_0.5917516635974417
@@ -0,0 +1,22 @@
+archive/ES_0.5917516635974417---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T21:36:31.611
+Launch V∞: [5.225338330626346, -8.349991754209581, -1.044305823446515] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.15390805101623292, -0.22169613989691747, 0.03482854451348475] km/s
+ V∞_out: [-0.2707579876018591, 0.025784220791250964, -0.013668510237845849] km/s
+ time of flight: 1.2970389063738799e8 seconds
+ arrival date: 2027-06-01T02:28:01.611
+ thrust profile: [0.49507330985639897 -0.32799664571512244 -0.25287305957678713; 0.28672798561927193 -0.03185232663325978 -0.3038503209493755; 0.16723875029026555 0.017893860578857522 -0.26661784212436146; 0.12698340163777586 0.028921198104143533 -0.2629824550323952; 0.11197603661718944 0.037565799484120935 -0.2836697390907341; 0.05844514329179356 0.02000115762155762 -0.16977420211711466; 0.017543577977856557 0.00751232144124141 -0.06018318362311829; 0.011005772332583161 0.005153797237133772 -0.04152660226485185; 0.001616418731314999 0.0008014702621001477 -0.006608834816230826; 0.0017672950765616196 0.0009345394440713248 -0.007897916705963544; 5.6759487641734186e-5 0.0001068379270630031 -0.00023659267983312712; -4.748652465976188e-6 -4.8604794761682326e-6 -0.00042018606906586275; 0.0003201239315560826 -1.7398924182094146e-5 -0.0001601511821663002; 0.00016818076355088024 -7.01745009378918e-5 -0.00022691213760389704; 0.00030024530925747974 1.564386820976231e-5 -0.00024758863240240386; 0.00016571467357877714 0.00011734572684483621 8.37878682291614e-5; 0.00014879905802503898 0.0001440123923645932 4.043577489640208e-5; -0.00017302326750298023 -0.00016048535977744273 -3.43543466636102e-5; -6.493222013447737e-5 -0.00012164000078098512 0.00020669680153728422; -2.1979561364002626e-5 7.696828593372245e-6 0.00013265955316032145] %
+
+Mass Used: 118.02720476005152 kg
+Launch C3: 98.11709761776522 km²/s²
+||V∞_in||: 0.2721211019486301 km/s
diff --git a/archive/ES_0.5917862304930874 b/archive/ES_0.5917862304930874
new file mode 100644
index 0000000..908364b
--- /dev/null
+++ b/archive/ES_0.5917862304930874
@@ -0,0 +1,22 @@
+archive/ES_0.5917862304930874---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T04:07:17.276
+Launch V∞: [6.9574978000525745, -7.211538259492107, -1.0815928758618907] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.734070890978425e-5, -5.311533986828647e-5, 8.472949630154062e-5] km/s
+ V∞_out: [4.3627978027111034e-5, -8.114854807024388e-5, 5.366744965300897e-5] km/s
+ time of flight: 1.2881647618401118e8 seconds
+ arrival date: 2028-06-06T02:28:33.276
+ thrust profile: [0.32243045605646653 -0.13566456076366334 -0.1675148631937159; 0.15769823923002316 0.006448139403784514 -0.19325455131447206; 0.15107106030506204 0.034942831860299166 -0.2909452571157083; 0.1264630878024337 0.042930368211037594 -0.3266396657170984; 0.08752655195582947 0.03583801687649339 -0.28049806862292087; 0.032756280451115526 0.014376828076980253 -0.1265768722165246; 0.011807134855786406 0.005886927150182477 -0.05274366696234771; 0.0052192651342306 0.0028487335068322676 -0.026439435604981985; 0.009186370225268612 0.004817695205599373 -0.0490587215293057; 0.001996495439269738 0.000890727860787298 -0.007366786146156793; 1.381583955179419e-5 -2.434758940100725e-5 -0.0018406078463720048; 0.001178984681911136 0.00019667064048282913 -0.00425727463901016; 0.0015827026299541822 0.00019613399647989635 -0.004461050600990646; 0.0004349651824836861 -0.0003904398343463285 -0.0008370515482012391; -0.0003444430804640611 0.00018250158414203846 -0.00014538087009683624; -0.0006684518271396801 -0.00019526614327071976 0.0003112379500667742; 0.0013957445208624384 -0.002504788662392482 -0.0005583885773977699; 0.0002757128844231415 0.000908308788602361 -0.001361913698751901; 0.0003177238143592862 0.00033095668092681865 -0.000854119907435533; -0.0004247900324275529 -0.00033833564523737237 0.002050967288667918] %
+
+Mass Used: 97.85033558794339 kg
+Launch C3: 101.58290285497006 km²/s²
+||V∞_in||: 0.00010674575127245865 km/s
diff --git a/archive/ES_0.5919423017914568 b/archive/ES_0.5919423017914568
new file mode 100644
index 0000000..12d9d46
--- /dev/null
+++ b/archive/ES_0.5919423017914568
@@ -0,0 +1,22 @@
+archive/ES_0.5919423017914568---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T16:26:38.937
+Launch V∞: [6.0086728363155615, -7.941885229603921, -0.3035233963765462] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6777735264993453e-9, 1.5348022216225403e-9, 1.0573402274976945e-8] km/s
+ V∞_out: [-5.849798877989978e-9, -8.273330597559968e-9, -4.32813387541666e-9] km/s
+ time of flight: 1.738648748543882e8 seconds
+ arrival date: 2028-11-04T00:14:32.937
+ thrust profile: [0.19907029683434227 -0.08163453743786252 -0.08026736397875653; 0.054746228798407966 0.013803232656798135 -0.057007400538345826; 0.030364121192261475 0.011350447348182476 -0.09687322386245957; 0.03540460934116981 0.018423768194328234 -0.1137775747481928; 0.032984753070924605 0.019814391294381867 -0.14199228514326032; 0.021199503261446068 0.009763173766390448 -0.13167686063382253; 0.0029410710184291766 0.012482900600656995 -0.09925432604544507; 0.03288631761693622 0.010205101041604922 -0.10017395342153808; 0.005326082577026774 0.01486278577728484 -0.06270338749139805; 0.015532981200551457 -0.029981062692909358 -0.025493960752778322; 0.00781350004159747 -0.004828873412124639 -0.0838893027758178; 0.005892015573105774 -0.0004264632040991976 -0.01151112288659136; 0.019095693137620297 0.0028637427556045198 -0.006477902670683863; 0.0202272613814264 -0.007677782644817991 -0.036740814634793534; -0.0010322586519483142 0.009679982460693893 -0.011215974057354802; -0.008696436695846521 -0.004427199327357705 -0.00013588037607492956; 0.027673570464197897 0.07281948339646653 0.0367514556566594; 0.019825179535532794 -0.08558191040523308 -0.03447722814259399; -0.03439582352441298 -0.055789134522390704 0.021924223664371134; -0.017536914914442737 -0.032042283708299105 0.03403197761146399] %
+
+Mass Used: 111.5254213037183 kg
+Launch C3: 99.26981670622537 km²/s²
+||V∞_in||: 1.081514574724757e-8 km/s
diff --git a/archive/ES_0.5919817818910145 b/archive/ES_0.5919817818910145
new file mode 100644
index 0000000..e715e73
--- /dev/null
+++ b/archive/ES_0.5919817818910145
@@ -0,0 +1,22 @@
+archive/ES_0.5919817818910145---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T11:15:25.776
+Launch V∞: [5.433196431875212, -8.20989512280162, -1.0259988537180573] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.279972520401413e-5, 2.2092805794145907e-5, -4.6524864043128364e-5] km/s
+ V∞_out: [-4.2089714460262975e-5, -4.002182526982225e-5, -1.8814310948931737e-5] km/s
+ time of flight: 1.341837679045974e8 seconds
+ arrival date: 2027-07-21T12:31:32.776
+ thrust profile: [0.47021580593137274 -0.2870697796056673 -0.21241766228834588; 0.22460669935100228 -0.008442030677492395 -0.2222514748209112; 0.15580849246406703 0.03143197823086419 -0.23248486537746135; 0.10689645121913567 0.037385236887866116 -0.2086166332156052; 0.05998156769080315 0.026336891133705402 -0.14334133330478585; 0.05448318663934777 0.028451251584730414 -0.15012635683238454; 0.043968813973648505 0.02542886588491097 -0.136519045542206; 0.03770259330355747 0.022636617543097762 -0.12196299166816366; 0.032041873622800796 0.0189618305408614 -0.11277850587532665; 0.02131375181516738 0.014522793978335533 -0.08422830476880211; 6.209543259872732e-5 0.00010961156776624747 -0.00015883434831862015; -3.634075424361415e-5 4.4511714453296784e-5 1.1103005564420607e-6; 0.00011954932721310217 0.00011902122345927369 -0.0002893039870708124; 7.168641097771802e-5 -0.00010005756219991303 -8.139091735964797e-6; -5.967004657078381e-5 -0.000257530016065044 -0.00014050571879505247; -4.892182339434365e-5 0.00010390920050300866 4.51915590528223e-5; 0.00012387110079608042 -7.089498629768534e-5 1.5096242612244936e-5; -8.059462443186233e-5 0.00019333601045739917 -3.33597772417265e-6; -6.232011106455832e-5 -5.024235038809511e-5 -0.0002013726281740537; 9.948632196675393e-5 -0.00028316973939640163 7.018070756950076e-5] %
+
+Mass Used: 119.12647445783432 kg
+Launch C3: 97.97467504257415 km²/s²
+||V∞_in||: 6.106125625589655e-5 km/s
diff --git a/archive/ES_0.5919926678348422 b/archive/ES_0.5919926678348422
new file mode 100644
index 0000000..d686150
--- /dev/null
+++ b/archive/ES_0.5919926678348422
@@ -0,0 +1,22 @@
+archive/ES_0.5919926678348422---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T20:46:21.822
+Launch V∞: [5.264887446600826, -8.443587611386427, -1.113059939343177] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0509594669616634, -0.07328009026847351, 0.00863367121532994] km/s
+ V∞_out: [-0.08418049473605421, 0.027520356843418414, -0.014202583040468585] km/s
+ time of flight: 1.359922616406626e8 seconds
+ arrival date: 2027-08-15T20:24:02.822
+ thrust profile: [0.31240543920466884 -0.20595570552780076 -0.17242106141289504; 0.1301464479768052 -0.018619042352511814 -0.15890949393083498; 0.12296698926829872 0.006022665000565209 -0.23035482555339146; 0.10665520189526193 0.016399980150599514 -0.2643065303308962; 0.07444888488858685 0.016049734884878538 -0.22665805443472176; 0.041431041006380905 0.010027820481742824 -0.14863412828216482; 0.027220734047005972 0.007103442345306205 -0.11127897961215688; 0.02046797076415716 0.005506884748736423 -0.09299911350119072; 0.0051017718016328414 0.0008685790821681557 -0.04311119833646336; 0.003515112278793793 0.0019905368019623826 -0.005385984210501397; 0.00011044224935086925 0.003480571823154014 -0.0015592990914620906; -0.0023370920006122783 0.003524062688901911 0.003939282749808411; -0.0013823880860980831 -0.0025258866632355023 -0.0024421683160258875; 0.009859881250738115 0.005401250150354307 0.004141426224825992; -0.00436789783497253 0.0007583420656595783 -0.005019022184529766; 0.011493811777636578 0.01542908117831537 0.00029944160012513547; -0.014864632605325888 0.011580327541231342 0.0033695648654956008; -0.003740445594902473 -0.014872918585474036 -0.02242799663801186; -0.005203948829541802 0.006723204664318151 0.006079095893847236; -0.001053181928876148 0.02062425523256412 -0.018568862206514252] %
+
+Mass Used: 105.85411411087625 kg
+Launch C3: 100.25211400510395 km²/s²
+||V∞_in||: 0.08967373741194747 km/s
diff --git a/archive/ES_0.5920373755474004 b/archive/ES_0.5920373755474004
new file mode 100644
index 0000000..ebe7300
--- /dev/null
+++ b/archive/ES_0.5920373755474004
@@ -0,0 +1,22 @@
+archive/ES_0.5920373755474004---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T13:21:06.011
+Launch V∞: [5.44663600766938, -8.036169687469437, -0.2251165652312841] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5409317837501933e-5, 5.816408232639481e-6, -6.6543299535352085e-6] km/s
+ V∞_out: [2.485495129116588e-5, -9.417897990867582e-6, 4.049127265255758e-6] km/s
+ time of flight: 1.3876150890501872e8 seconds
+ arrival date: 2027-09-10T14:12:54.011
+ thrust profile: [0.6197739570585918 -0.3542164604911386 -0.22879208587558697; 0.32424750045698914 -0.0020912684100528006 -0.27072371255817806; 0.17803606906685854 0.03980066629872261 -0.2304964141318202; 0.10861555833428053 0.039872603444332085 -0.18703854033750658; 0.0799047716537806 0.03785463756277086 -0.16894193933368348; 0.05984302898520357 0.034483504911159105 -0.14857444909712972; 0.07926776136361442 0.050407019359536065 -0.21080733367556742; 0.03144986194937119 0.020992832651475803 -0.09697239955238424; 0.020897250161588804 0.014177546792434778 -0.0689064350156096; 0.0014163250765975377 0.0033499723020685617 -0.014331016890923219; 0.003946612072176863 0.004481948731317132 -0.02491623163061042; 0.0020844356819726224 0.0022145798033047126 -0.011398265982408836; -0.0031764795303401076 0.007063211225709888 -0.0008859406606694701; 0.004809666897197086 0.0011186305190779232 -0.0017819708983002527; -0.001973560661981829 -0.0009142802327692951 -0.0059854417469772025; -0.00025371850062969525 -0.0030961000953424233 -5.440396443821263e-5; -0.00015814435404065599 0.0014452940471473075 -0.003929834301688279; -0.003173986704543028 0.002012911956062675 -0.00393780996584994; -0.0034679884623927335 -0.004593614381561789 0.002344076478175255; -0.004334757459759584 0.002581475663528692 -0.003610135750565282] %
+
+Mass Used: 140.64709514155584 kg
+Launch C3: 94.2965445137848 km²/s²
+||V∞_in||: 2.690249328271315e-5 km/s
diff --git a/archive/ES_0.5920873073105016 b/archive/ES_0.5920873073105016
new file mode 100644
index 0000000..496b70b
--- /dev/null
+++ b/archive/ES_0.5920873073105016
@@ -0,0 +1,22 @@
+archive/ES_0.5920873073105016---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T14:58:49.544
+Launch V∞: [6.993130405901637, -7.034433852986766, -0.8521860565686825] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.3307642667731287e-8, 8.882349467428377e-9, 1.056182191395288e-9] km/s
+ V∞_out: [2.161110500300586e-8, -1.3157605841429375e-8, 6.266313071237803e-9] km/s
+ time of flight: 1.344677056715114e8 seconds
+ arrival date: 2028-08-09T23:07:14.544
+ thrust profile: [0.4727298270332539 -0.1724889978004512 -0.20984364674239844; 0.10820293797072121 0.011943505725956146 -0.12714111031022246; 0.09130690214979878 0.030163920042321754 -0.16829372273107845; 0.049477364888873276 0.02215228016569579 -0.12635040834529793; 0.05751407750871886 0.03236802245292962 -0.17603779209668777; 0.033423945786482875 0.019607071278754825 -0.12512216315895086; 0.019020783403952902 0.010742846861306509 -0.07420158688054133; 0.025575822811873428 0.016125135111801622 -0.09319753080466385; 0.02171852337519436 0.02003104658709447 -0.11094170479354529; 0.0855193244129416 0.06701346622397393 -0.34924479998533325; 0.004557604064278197 0.0029438798922875498 -0.027014143144203716; 0.0006464400146759437 0.0009077598161225079 -0.002936278008585847; -0.0036177513595290808 0.007207075148043738 -0.002176228275363905; -0.010423187909493674 0.0033175955825490264 -0.002345497571534211; -0.0002806160441534279 -0.0008192968908694422 -0.00012382808552533365; 0.004244831933461913 -0.0016126468131087846 0.0007932727283327957; 0.00142755049536242 0.001234683485318033 0.000892130679918599; -1.7880852663612742e-5 -0.0006454169841735777 0.00042736771212507733; -0.002859388992074258 -0.001630149726601895 0.011646095457022668; -0.004654352725951865 -0.0034713287610600653 0.01231406575227182] %
+
+Mass Used: 112.60729597307181 kg
+Launch C3: 99.1133535810023 km²/s²
+||V∞_in||: 2.4965132877867757e-8 km/s
diff --git a/archive/ES_0.5921076541786988 b/archive/ES_0.5921076541786988
new file mode 100644
index 0000000..c2bce02
--- /dev/null
+++ b/archive/ES_0.5921076541786988
@@ -0,0 +1,22 @@
+archive/ES_0.5921076541786988---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T15:00:10.423
+Launch V∞: [5.825722618573639, -7.950881143384623, -1.3679349860922545] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9037705535718617e-7, -1.241814917699412e-7, 2.4755180591186003e-7] km/s
+ V∞_out: [1.1971078858453453e-7, -2.732219726405683e-7, -2.607269914316648e-7] km/s
+ time of flight: 1.4655407320338693e8 seconds
+ arrival date: 2027-12-09T20:28:03.423
+ thrust profile: [0.26881173098575595 -0.14293495651495083 -0.10794217463659833; 0.19597257654469807 0.010519202809005769 -0.17406947428438624; 0.20584789922631685 0.06386893466772291 -0.2763243690167065; 0.1744872533571729 0.0839711818333015 -0.3097216107707499; 0.12411689729638392 0.07616825273589743 -0.27221551383816345; 0.05899917766148721 0.04279719497353119 -0.15639830141500546; 0.014126201164270841 0.010708823350544112 -0.042942744456196204; 0.014271713872909078 0.011442119657714652 -0.04522204275412616; 0.0005907529135386782 -0.0010564651091572504 -0.005579137794679151; 0.001212910308057631 -0.0012509349556438644 -0.005844409468162653; 0.0015543392653902853 -0.0003902340904231498 -0.003136116803531955; 0.0008486472011421844 0.0008859700938949883 -0.004198330158789738; -6.496702324288969e-5 0.004014251163383302 -0.0016915131825640086; 0.0011010833716162713 0.0017056459382440987 -0.002797037506968654; 0.0025191353708805438 0.004044526731521077 -0.004538062896654444; 0.00632015303648395 0.0034138004843081798 -0.0023320375820274856; -0.0008024667489490833 0.007670310835181607 -0.0012428280223566678; 0.00014105714901386146 0.0001339208278076957 -0.0015789751893512819; 0.0006988864730354716 -0.0014991002564718875 0.0006466154692937312; 0.0074461394704069955 -0.002265587085433589 -0.0029117288476997335] %
+
+Mass Used: 113.13592339451998 kg
+Launch C3: 99.0268011109649 km²/s²
+||V∞_in||: 4.012751846131798e-7 km/s
diff --git a/archive/ES_0.5921406866518387 b/archive/ES_0.5921406866518387
new file mode 100644
index 0000000..348887c
--- /dev/null
+++ b/archive/ES_0.5921406866518387
@@ -0,0 +1,22 @@
+archive/ES_0.5921406866518387---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T11:30:00.601
+Launch V∞: [6.677007680646578, -7.536411002879351, -0.7826064137722698] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0028281834185406303, 0.012297324135476828, -0.015374568259246567] km/s
+ V∞_out: [0.013616055460672289, 0.011737037784700371, 0.008530884024626534] km/s
+ time of flight: 1.6167585011027578e8 seconds
+ arrival date: 2028-06-02T17:27:30.601
+ thrust profile: [0.1794425428528199 -0.08717427025355076 -0.10211596930253737; 0.083388229287086 0.009715603770174224 -0.11544014147127152; 0.09755948295444222 0.032480356033074906 -0.20914966921959188; 0.08332339025693214 0.04090670928682598 -0.2433014261074568; 0.02025882940465054 0.011456320239389356 -0.06523278284818032; 0.05405683693557012 0.04197625765466678 -0.25124005104395375; 0.03033469411497295 0.026568146138813867 -0.13942628679949778; 0.009891409764616395 0.00697779253106301 -0.04401559897340629; 0.0047370253765943926 0.003588066866760337 -0.022939553354867415; 0.004391626264914847 0.0036655182173482605 -0.023268406214329584; -0.0011073447430067337 0.004544767424729758 -0.013226604312762024; 0.001701101757556355 0.001303893329834725 -0.0032765031785711735; 0.0014865220049916402 -0.0007087670928615259 -0.010465643148905954; 0.0006461777998162051 0.0019463336431347238 -0.0028739097587386206; 0.0003522861643928722 0.0011486309627098121 -0.005825019983703659; 0.0007584224235290989 -0.0021081005435852336 0.0003906107416503943; -0.0040729769828599695 0.003425073847954812 0.0027823322504561166; -0.000570382703748266 -0.0026344514795573837 0.002925254062984297; -0.0004037746272158903 -0.0005872533746821975 0.004025613874339726; 0.00139824013432848 -7.603540619579992e-6 -0.006321059137173034] %
+
+Mass Used: 95.87516259857603 kg
+Launch C3: 101.99239517061184 km²/s²
+||V∞_in||: 0.019889699633230288 km/s
diff --git a/archive/ES_0.5922734837832436 b/archive/ES_0.5922734837832436
new file mode 100644
index 0000000..75bfa17
--- /dev/null
+++ b/archive/ES_0.5922734837832436
@@ -0,0 +1,22 @@
+archive/ES_0.5922734837832436---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T15:08:58.670
+Launch V∞: [7.017142268220831, -7.0939849798348105, -0.7952643741056876] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01785307933522944, -0.021927043404858695, -0.002066476333354484] km/s
+ V∞_out: [0.006112071602101323, -0.027063654233729233, 0.005875943045115589] km/s
+ time of flight: 1.2988887289548552e8 seconds
+ arrival date: 2028-06-16T23:23:30.670
+ thrust profile: [0.33269558278229183 -0.13025464044095753 -0.1557464191184227; 0.19563694120334654 0.016795991263086296 -0.21399599482815324; 0.16689787284526925 0.04891399569120785 -0.28650006767490716; 0.12771398849547141 0.0534250017824769 -0.2947755194276623; 0.077079043918814 0.03864725635185741 -0.2218537581761075; 0.05533759815285962 0.0306959596966398 -0.1894425734646497; 0.03566578238832616 0.021742122215327425 -0.1388487118487265; 0.012162828189109551 0.007682093667664697 -0.056215743446094216; 0.003920221146561904 0.004835391206240337 -0.023561526089683073; 0.0021358008570481896 0.0011533925525170179 -0.014841086986342344; 2.9528062534371255e-5 0.0002000748863588786 -0.0028054703900339956; -0.0022261554083841946 -0.0015172228882781526 0.0011431838849776301; 0.0020589085175763884 0.0030397178295763555 -0.007571838620707209; 5.2011018680603316e-5 -1.3571526571036214e-5 0.004354612151039329; -0.0022872632484991643 0.0008676719068450665 0.0015251581130445906; 0.002784706200385121 0.0012913247449952109 0.0010483074742171465; -0.00040232035568109315 -0.0021834350071699106 0.0017666403406173927; 0.0007360232964690341 -0.0028504038147194118 -0.0045750845944181355; -0.0013568509097527464 0.002172123344959716 0.0020966312669670876; 0.001012262972297813 0.0011881950477084355 0.0007927259646657513] %
+
+Mass Used: 106.50116648123003 kg
+Launch C3: 100.197353931295 km²/s²
+||V∞_in||: 0.02835133151484896 km/s
diff --git a/archive/ES_0.5922872558498665 b/archive/ES_0.5922872558498665
new file mode 100644
index 0000000..07c2034
--- /dev/null
+++ b/archive/ES_0.5922872558498665
@@ -0,0 +1,22 @@
+archive/ES_0.5922872558498665---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-26T17:21:15.280
+Launch V∞: [7.9768398900301305, -6.6666324803975066, -0.41182749927299167] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5612704982986504e-6, -1.0296428181128228e-5, 0.0002371218684492652] km/s
+ V∞_out: [1.083594866612814e-5, -0.0002380428667944745, 8.634607148360052e-7] km/s
+ time of flight: 1.8457984806009242e8 seconds
+ arrival date: 2030-04-02T01:32:03.280
+ thrust profile: [0.03115207413681073 -0.011204150572185632 -0.018630579681735496; 0.016935395245713268 -0.007043458560215429 -0.03447225336527243; 0.014268864953001493 -0.011061917320619693 -0.05023558985823083; 0.01053110994860135 -0.010510433008567084 -0.043546213203131706; 0.02160870745038874 -0.02454054910032699 -0.09691640276586713; 0.014841410335816164 -0.019196892074280818 -0.07432488770648005; 0.017126010461430922 -0.02190680882785131 -0.08274992534837783; 0.0431380676550189 -0.05573216506495628 -0.20061401874070545; 0.013315771622965294 -0.017666981152572214 -0.06697403680708527; 0.005224269647339337 -0.006753054650797656 -0.02447782132612204; 0.008158898643004479 -0.010615389830041367 -0.03934701134433845; 0.0013595314614878353 -0.00188944057313891 -0.006712047541516864; -0.000601674550683244 -0.00022322596337876862 -0.0005675361659496811; 1.2081236677139525e-5 -0.00012724852008420536 -0.0008202023466874476; 0.00028710912577160094 -0.00035342996538402754 -0.0006536612189927893; 0.0009405504838016162 -5.9168100756833554e-5 -0.0012762047174402543; 0.0005364925016212701 -0.0006384557966746265 -0.0006234880719858954; -2.869909713773994e-5 -0.002655700339130179 -0.0010147648789883452; 0.00017181481988865619 4.24003754133302e-5 -8.890795689073456e-5; 0.00034279203877137963 -0.0003418766053295949 -0.00023196793656038694] %
+
+Mass Used: 59.58100178886889 kg
+Launch C3: 108.24356514902436 km²/s²
+||V∞_in||: 0.00023735044658843306 km/s
diff --git a/archive/ES_0.5923265383137258 b/archive/ES_0.5923265383137258
new file mode 100644
index 0000000..201b0b8
--- /dev/null
+++ b/archive/ES_0.5923265383137258
@@ -0,0 +1,22 @@
+archive/ES_0.5923265383137258---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T22:12:43.566
+Launch V∞: [5.288811578878017, -8.408359580296166, -1.3696543262936889] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.05800566147395305, -0.08412155229811488, 0.013148773764925323] km/s
+ V∞_out: [-0.09370230434269199, 0.03984940425713443, -0.015746031270764717] km/s
+ time of flight: 1.3030659339908919e8 seconds
+ arrival date: 2027-06-09T02:29:16.566
+ thrust profile: [0.3555094182858045 -0.24701674368841847 -0.195656367283101; 0.21784471983429995 -0.030414016811003947 -0.24396835109853143; 0.1580994382331329 0.010435576589713178 -0.26788882806652975; 0.1298989534314825 0.023827233705812353 -0.2885535268732595; 0.09103859045280487 0.023715251972321955 -0.24634028291120347; 0.048945122635681106 0.01541071194016459 -0.15517706720714539; 0.014066442932844156 0.005545544429828585 -0.05023887811861206; 0.0032722455715597934 0.0006542023639898942 -0.010090923327027691; 0.004881520715912073 0.0025986276576196185 -0.021795359623972606; 0.002815836957370991 0.00029140342142213306 -0.015226313563640468; 0.006186383933818189 0.0022728835164639075 -0.029873917246277564; -0.00016975766958630956 0.0003619431621939277 -0.0054061754311694335; 0.00034770880736440695 0.0001651849890692929 -0.0022396497483506026; 0.00048028537564057285 0.000572186414564515 -0.001968345530635406; 0.00033359186554771754 -0.000433153374952869 -0.0026180847870148974; -5.845134702137252e-5 -0.0004218112400465584 -0.0020052297939007796; -0.0013297179821219526 0.000512618925038622 -0.001249707692592983; -0.0011216264508243285 0.0008325284500321668 0.00027587541672535396; -0.0001597889524161967 0.0030826691355738635 -0.0002618213522705497; -0.0017985515104251152 0.0015639869533496682 0.0006820607117167155] %
+
+Mass Used: 104.517676321203 kg
+Launch C3: 100.54799172196752 km²/s²
+||V∞_in||: 0.10302418442092373 km/s
diff --git a/archive/ES_0.5924596310991499 b/archive/ES_0.5924596310991499
new file mode 100644
index 0000000..20ecc62
--- /dev/null
+++ b/archive/ES_0.5924596310991499
@@ -0,0 +1,22 @@
+archive/ES_0.5924596310991499---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T06:46:26.994
+Launch V∞: [7.2085428789754005, -6.685827641157164, -2.585302127734139] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.94256676138444e-7, 1.312272463118975e-6, -2.327649367848471e-6] km/s
+ V∞_out: [-1.3026463786839166e-6, -2.5311527388812546e-6, -8.360173765269153e-8] km/s
+ time of flight: 1.5758953156576154e8 seconds
+ arrival date: 2029-05-08T05:38:37.994
+ thrust profile: [0.1780275693720993 -0.029379192347150144 -0.08007085693176112; 0.1112470251432109 0.04388837543205216 -0.12840713026244893; 0.08260584628233383 0.060463038098056754 -0.16088826085117167; 0.06042618875140289 0.06104329271346609 -0.16983957720835957; 0.04477948361673734 0.05728645621778691 -0.16869630757402798; 0.026773810948488828 0.04017910672490176 -0.12951979431840224; 0.014102066693660889 0.0240638118818441 -0.08700958857153188; 0.008445215431651295 0.016390965834723124 -0.06387757123869137; 0.0025647697094296784 0.005765608202084596 -0.02779086257448114; 0.00027527237630467353 -0.0019417399617750691 -0.0007178539400732181; -0.0029971787395612955 -0.005675562693615126 -0.0033545069459004276; 0.00016119475029023543 0.0013854748757635876 -0.0039053922633826388; -0.0002998816991798475 0.000884265782581629 0.00609528307339166; -9.667240016371567e-5 0.004502922325557001 0.010250802489801447; -0.0023865931159661002 -0.0066038628954552744 0.01950282718767214; -0.005481856380635384 -0.013723916562404518 -0.0061613081218909365; 0.008946635293480353 0.012537638570407642 0.008728507444612415; -0.003266447403447758 0.017918404365765694 -0.012537873650019248; -0.016296517384037153 -0.0033765496706526918 -0.02345824617154785; -0.0008919231436814746 -0.008289931313800803 0.004618009447449087] %
+
+Mass Used: 88.34441841677199 kg
+Launch C3: 103.34716877695479 km²/s²
+||V∞_in||: 2.851062422177318e-6 km/s
diff --git a/archive/ES_0.5924741164138336 b/archive/ES_0.5924741164138336
new file mode 100644
index 0000000..24418ff
--- /dev/null
+++ b/archive/ES_0.5924741164138336
@@ -0,0 +1,22 @@
+archive/ES_0.5924741164138336---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:28:48.720
+Launch V∞: [6.985598468293329, -7.262156454701254, -1.4834288947605476] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.7394674476812734e-5, 8.40299245991407e-5, 5.3166001859386044e-5] km/s
+ V∞_out: [8.133400192268784e-5, -6.0112446285523256e-5, -3.2558336929739306e-5] km/s
+ time of flight: 1.2947654025992994e8 seconds
+ arrival date: 2028-06-14T20:11:08.720
+ thrust profile: [0.25567350983451437 -0.10841107750961151 -0.1436968549567269; 0.11414702819240846 0.0033088860923358447 -0.15203420288452968; 0.10084777116025144 0.021509175463958797 -0.2138435277986795; 0.08899662321496807 0.02809605978319851 -0.2546696063003482; 0.06599479016614535 0.025086829458858956 -0.23475202610734403; 0.032783110368598614 0.013598357489532307 -0.1385011907685108; 0.015137477599720643 0.006338148473722183 -0.07297052278986998; 0.010115407118831245 0.0043678256821325905 -0.05316265570683199; 0.012102893054333702 0.005521648158036151 -0.06986081963602765; 0.008004474707919122 0.0036811484007338423 -0.04935457335991399; 6.0546851570097775e-5 0.00014402469095893016 -0.001886639334401192; 0.001140331072662501 0.0007052218514601847 -0.008073490300960382; 4.663605876239563e-5 7.08603856406506e-5 -0.0014262378944897517; 0.000826760352479415 -0.00019480349336272254 -0.00025096890250070314; 5.343125381466045e-5 -7.497550797813874e-5 -0.00045453360714165425; 0.000617328154021702 -8.344539031882267e-5 -0.0006058194700078998; 8.575432987191134e-5 0.00017280225101292432 -5.783486421743816e-5; 0.0014736501867322375 -0.0002556562359361118 -0.0001726628925527255; 0.000720191918891436 0.0012724194147851206 0.0010129919173322924; 0.0006256719182427582 0.0023953153983276992 -0.0004891040754744451] %
+
+Mass Used: 86.08109804102105 kg
+Launch C3: 103.73806361859168 km²/s²
+||V∞_in||: 0.0001062356515538748 km/s
diff --git a/archive/ES_0.5925901998716979 b/archive/ES_0.5925901998716979
new file mode 100644
index 0000000..d4ff763
--- /dev/null
+++ b/archive/ES_0.5925901998716979
@@ -0,0 +1,22 @@
+archive/ES_0.5925901998716979---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-16T10:32:58.384
+Launch V∞: [5.555845266501148, -7.353214582488667, -0.5016691139456144] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0001429439184628796, 0.000898389565162631, 0.0009803487747504546] km/s
+ V∞_out: [-0.00023032400478334477, 0.0002120054169909753, -0.0013010117473548101] km/s
+ time of flight: 1.7409346161829466e8 seconds
+ arrival date: 2028-10-21T09:50:39.384
+ thrust profile: [1.0 -0.33089959721888296 -0.182197960838206; 0.5698803002202204 0.1828232003484188 -0.2821890185149354; 0.2221565569792587 0.14715801158571615 -0.19846406861502147; 0.12995056525556622 0.11990417294336368 -0.16613230634417842; 0.0733267522308837 0.08594321574110354 -0.12178802884335739; 0.053599289346726274 0.07650458841654428 -0.11256547124121598; 0.014241265964682845 0.02228437614621948 -0.03519797155564454; 0.01634999060594948 0.029415115368765333 -0.04663160657005649; 0.01836057670953262 0.03637009612531314 -0.05870061686748673; 0.0018118464895489244 0.0039281844837425585 -0.006929219850140925; 0.00012020012051291098 0.0006648359378171855 -0.00025616259077797856; -5.4809749738151916e-5 0.0002762571369646748 -0.0005026782910879254; 0.0002214149287067575 0.00039522798901268046 -0.0007278385451809412; 0.0003319185287922979 0.0005035673962723642 -0.0003584661453709606; -0.0001765475721379194 0.0006293518326829177 -0.0004737226515482699; -1.7330978182144265e-5 -0.00027668654133282156 7.11395246600229e-5; 6.153640175814761e-5 0.00016465099346579513 -0.00040918188946757164; 7.280385840191331e-5 0.00018280619343591224 -0.00040740403805581023; -0.0002511555780525667 0.0004975620853019632 -0.000110829685632587; 2.692356215945832e-5 5.866311187682831e-5 -5.934220589841766e-5] %
+
+Mass Used: 194.42025605931485 kg
+Launch C3: 85.18885322131418 km²/s²
+||V∞_in||: 0.0013373931713498994 km/s
diff --git a/archive/ES_0.5925963867041968 b/archive/ES_0.5925963867041968
new file mode 100644
index 0000000..76468c7
--- /dev/null
+++ b/archive/ES_0.5925963867041968
@@ -0,0 +1,22 @@
+archive/ES_0.5925963867041968---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T13:58:18.804
+Launch V∞: [7.060955584835781, -7.120963669135326, -1.1387727764584996] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0048126972420244165, -0.0041836076537387, 0.003144455440690706] km/s
+ V∞_out: [0.003120346662208031, -0.0063089495001504075, 0.0009893553062094117] km/s
+ time of flight: 1.3035197586306307e8 seconds
+ arrival date: 2028-06-23T06:51:13.804
+ thrust profile: [0.28325155805754454 -0.1146545449222216 -0.14590074221063892; 0.1266212308157487 0.008481957437017473 -0.1551528105829839; 0.12614764001713952 0.033583649417395764 -0.24249729085213417; 0.11420425920218304 0.0437935168546058 -0.29459103920737106; 0.07674768090523475 0.03558676619094092 -0.24671381548866894; 0.025342091003699725 0.013179722678698451 -0.09646349786368269; 0.027717571869510894 0.015288973401547576 -0.12326971114228637; 0.02090332657817576 0.011560692508395082 -0.1078386064770125; 0.00847885703551786 0.0056696586886137365 -0.037620069636767235; 0.003377566386452716 0.002296853107129235 -0.016546980592486566; 0.004871057409077895 0.0033822272122216034 -0.017536419826074783; 0.0012458713937479862 0.0007183867045675623 -0.007067103555451632; 0.00034838269324351256 0.0007535808009187647 -0.0018978198980477328; -0.0008213540768804758 0.00010010659142001927 -0.004820442641824128; 0.004764414327031738 -0.0006375802991880111 -0.008895104141573726; 0.005220381320592189 -0.0016869219092660055 -0.006994493971466932; -0.0050223114497462956 -0.003852201581679546 0.011388980574214731; 0.0021598967750670515 0.002340984716022401 -0.002892861370806116; 0.004397766315490281 0.0022295687767852914 0.0006928027936584798; 0.001372682510938585 -0.000446364977136385 -0.009314327492012959] %
+
+Mass Used: 97.1673299115605 kg
+Launch C3: 101.86202078457185 km²/s²
+||V∞_in||: 0.0071100089846848884 km/s
diff --git a/archive/ES_0.5927208682470759 b/archive/ES_0.5927208682470759
new file mode 100644
index 0000000..d908bc3
--- /dev/null
+++ b/archive/ES_0.5927208682470759
@@ -0,0 +1,22 @@
+archive/ES_0.5927208682470759---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T18:54:54.439
+Launch V∞: [7.061042582461715, -7.137178453372955, -1.4586995624468768] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005367311484540544, -0.004775474985884387, 0.0035871586327918315] km/s
+ V∞_out: [0.0032711227913015573, -0.007265749461450176, 0.0009968304259374543] km/s
+ time of flight: 1.2925315611987047e8 seconds
+ arrival date: 2028-06-10T18:34:10.439
+ thrust profile: [0.28730817593259794 -0.12173064542907532 -0.15294460468018303; 0.14037685833858915 0.007048286259825752 -0.17474255935319719; 0.10495674768080553 0.025943788986153515 -0.20677905110113062; 0.08335960383454288 0.030240771556268163 -0.2223521376096642; 0.05965803114816345 0.026248106785306646 -0.19783930847584089; 0.02627209079132878 0.01296022566457369 -0.1041836726746995; 0.03597363877535828 0.01880210799486713 -0.15982624742563842; 0.03191425210497097 0.01771110596343373 -0.15535256830754626; 0.006850715090216529 0.003912017561670733 -0.037467434308249926; 0.0020730830295158454 0.0014786594393280423 -0.013310334331245233; 0.002827720080480995 0.0017415262659607792 -0.017980108587537697; 0.0004598674494069141 0.0003372444818380288 -0.002519276128726075; -0.0002615232450969735 -3.683403558780925e-5 -0.0003615227605913296; 0.00039395075514035135 0.00016732454882948956 -0.0017222197973295263; 0.0007104306663171319 0.0003132901749916773 -0.0022201125582451756; -0.00020769898150766884 0.0004932158507961435 -2.8768819697484347e-5; -0.0008927349829246541 0.000985247765436753 0.0004764734362873112; -0.0016020308666608368 0.0002920687215984972 -0.00252493299927408; -0.0005494130662241775 -0.0003797877110960668 -0.0004499042024278064; 0.0001228757769877755 0.0004463490493200082 -0.0016476380709787033] %
+
+Mass Used: 91.10926188760504 kg
+Launch C3: 102.92544304011147 km²/s²
+||V∞_in||: 0.008030000060379905 km/s
diff --git a/archive/ES_0.5927482898322378 b/archive/ES_0.5927482898322378
new file mode 100644
index 0000000..aa3251e
--- /dev/null
+++ b/archive/ES_0.5927482898322378
@@ -0,0 +1,22 @@
+archive/ES_0.5927482898322378---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T01:01:47.939
+Launch V∞: [5.223933735845216, -8.211879042554218, -0.5367205898407849] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0015463373694961245, -0.009321033139717484, 0.012078112241868126] km/s
+ V∞_out: [-0.010266122111525576, -0.008414975492536293, -0.00765105413718782] km/s
+ time of flight: 1.328041512923027e8 seconds
+ arrival date: 2027-07-05T03:04:18.939
+ thrust profile: [0.5876369951597449 -0.3678270374898011 -0.2432945503275429; 0.35407551966188144 -0.02166344222640557 -0.3170813506505142; 0.22499840018377143 0.03765837125948192 -0.30497619356994576; 0.16102307377417724 0.04821668909650629 -0.2859946903360653; 0.11139428743076724 0.045064697604780005 -0.23914161492677824; 0.0360475947466797 0.01795881102052873 -0.09679692928656052; 0.047580107861953845 0.026263809982021578 -0.1346580671446631; 0.011760347521124459 0.007110149519548021 -0.03857953552958628; 0.004440266000890385 0.0025529535735381312 -0.017250688480995407; 0.0034552850247579724 0.00251567896297561 -0.014479103835673114; 0.0048506326049059575 0.0030864879938418094 -0.01787252176445304; 0.000573390293775239 0.001553844240478823 -0.007046847205196912; -0.00039759197430876917 -0.0007037718221671596 -0.00919009819372623; -0.0008677627012320479 -0.0019034532290746788 -0.007703216104443978; -0.0010811854735385418 0.0014623393169348438 0.001719965360386844; 0.0007337653034506812 0.003241811355784116 -0.005039273484246813; -0.005895372460693734 0.003917877595164274 -0.005698186454385107; 0.006279907426116159 0.00015975313077146972 -0.005179421555961834; 0.0007620203988815367 0.0027851099343319825 -0.001597516387655111; -0.008842495196180133 0.0012012871929690302 0.0024603465910122517] %
+
+Mass Used: 137.30002935159928 kg
+Launch C3: 95.01251007760196 km²/s²
+||V∞_in||: 0.015334719214226794 km/s
diff --git a/archive/ES_0.5928140537466178 b/archive/ES_0.5928140537466178
new file mode 100644
index 0000000..5a046ac
--- /dev/null
+++ b/archive/ES_0.5928140537466178
@@ -0,0 +1,22 @@
+archive/ES_0.5928140537466178---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T22:48:50.751
+Launch V∞: [6.95150133328016, -7.074242171316408, -0.8165534760229406] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.018125289017188715, -0.02112185780056179, -0.002028989262262979] km/s
+ V∞_out: [0.006050453645316473, -0.02653854844211463, 0.006144241419095122] km/s
+ time of flight: 1.3105628796506484e8 seconds
+ arrival date: 2028-06-30T19:20:17.751
+ thrust profile: [0.4762582643606595 -0.18268140332141933 -0.22700445927283422; 0.1648497967354603 0.015156615044665544 -0.19144771016759643; 0.10888118701823482 0.03145287801566783 -0.19556389564823284; 0.1546872646961942 0.061365307383741116 -0.3519999965308015; 0.07076953293275645 0.038303207840863614 -0.21535304564534385; 0.04442464214615289 0.027460513227120332 -0.15981257618913858; 0.031812292143940074 0.02001130090044775 -0.12441598851689181; 0.018955064123943863 0.011121859554556753 -0.08467933705727435; 0.004517161257510445 0.0038545987126242347 -0.021745434784814194; 0.002779851349658756 0.0037205098866079623 -0.021981548579785407; 0.0009314428062908084 0.0023368854354230474 -0.005358861876292236; 0.00103982323586757 -0.002089771566758921 -0.0006243729525700508; -0.009221534882208587 -0.0018508687490115432 -0.004143152962960904; -0.010658264662827554 0.0012690070592375159 -0.004376185276701921; 0.00557094840086385 -0.00020643038902857223 -0.010492454709905778; 0.0003762698636737777 -0.005586985804180086 0.007018475651454181; -0.0035365588624035717 0.0060714601832293925 0.00041976988416646873; 0.007667324517297404 0.009410867118270626 0.007487742423113146; -0.004302177251112113 0.0018770627375967706 -0.003521763197219074; 0.0003811804404091453 0.016984722735540428 0.003296805093125816] %
+
+Mass Used: 113.91203882969785 kg
+Launch C3: 99.03503266423249 km²/s²
+||V∞_in||: 0.027906554361478476 km/s
diff --git a/archive/ES_0.5928285267911135 b/archive/ES_0.5928285267911135
new file mode 100644
index 0000000..7ffb8d6
--- /dev/null
+++ b/archive/ES_0.5928285267911135
@@ -0,0 +1,22 @@
+archive/ES_0.5928285267911135---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-14T23:46:34.597
+Launch V∞: [5.757519123096506, -7.533189064557868, 0.2672859519183228] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.5458033380949173e-6, 3.3490469205231343e-6, 3.9459407784603235e-6] km/s
+ V∞_out: [5.404681597920618e-6, 3.175267163890716e-6, 1.0224756365267144e-7] km/s
+ time of flight: 1.5871889704343683e8 seconds
+ arrival date: 2028-04-25T00:21:31.597
+ thrust profile: [0.8408341257099874 -0.38156579436004673 -0.21922071322703346; 0.44231998632152175 0.06561230770541548 -0.3001969378274401; 0.34429594352571524 0.1473874003565868 -0.36773921908149004; 0.13921540784967618 0.08752356292087639 -0.2039076341297916; 0.06177281595841471 0.04873456267069207 -0.11494755575086726; 0.018473249437316437 0.016522896321052593 -0.040487117404496675; 0.015707373918484792 0.016209720413390093 -0.041014029928865145; 0.017004687936409454 0.0193602913991636 -0.04990782248299909; 0.0012450060601876156 0.0018377023345953199 -0.004145317722738576; 0.0026999919517415884 0.002756549978370517 -0.010530832478413611; 0.0005901344859666072 0.002767015397493253 -0.0013499042934584796; -0.00227337450532517 0.003527164421697329 9.014040818739215e-5; -0.0011211528392458378 -0.0002583968277229721 -0.002351142653008891; 0.002521967038768264 -0.011662755009613977 -0.0026951526502986033; -0.002102928573877897 -0.00045438142518712445 0.003169088671939453; -0.00039200319792165046 0.0016873229591619274 -0.0021827774332144672; 0.003459776633395713 0.0006390461231648468 -0.01140121943419526; 0.0035035660429071293 0.005770495374747669 -0.0077336622566255946; 0.0007799134291477919 -0.0019127764728355493 0.000390669288267823; -0.003488612381469885 -0.0006546758674479062 0.005089398131120058] %
+
+Mass Used: 166.81174791711283 kg
+Launch C3: 89.96940571528908 km²/s²
+||V∞_in||: 6.273697890034761e-6 km/s
diff --git a/archive/ES_0.592860002544233 b/archive/ES_0.592860002544233
new file mode 100644
index 0000000..37ceef5
--- /dev/null
+++ b/archive/ES_0.592860002544233
@@ -0,0 +1,22 @@
+archive/ES_0.592860002544233---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T04:04:13.988
+Launch V∞: [5.160027437959798, -8.493830565721277, -1.1269770969357622] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1629970261681117e-5, 8.108444239610808e-6, -1.6853564876985705e-5] km/s
+ V∞_out: [-1.5005417250877417e-5, -1.4624487523586076e-5, -6.656263070814865e-6] km/s
+ time of flight: 1.3264629665530653e8 seconds
+ arrival date: 2027-07-08T10:15:49.988
+ thrust profile: [0.436594443405259 -0.29843902366780667 -0.24459138765291913; 0.13278850167366843 -0.021899485456626372 -0.16842982689869404; 0.11070624515781223 0.002439919252321082 -0.21493559115440725; 0.08050905837733831 0.009653367142252399 -0.20814736346186655; 0.054531841949443056 0.009551197575437438 -0.17282152017024646; 0.05120618901183044 0.011650335673276791 -0.18728873858845224; 0.012847512248060284 0.0032650373880872834 -0.051108980267165226; 0.025885182717942726 0.007566049366504678 -0.1150777119626882; 0.026845065169343162 0.007691433739974001 -0.1330675639584549; -0.0016810389589335265 0.0012988528491027541 -0.01127540998826698; 0.001974663579161628 -0.0009670049761406978 -0.014273045809231378; 0.004182295008692734 0.0005250795165035521 -0.020894723096914522; 0.0018022897684174945 -0.00035711257134841636 -0.0016008934900148082; -0.0005742600131222924 0.007079239437690718 -0.005121309279605534; 0.003150404695495124 -0.0012447622341177442 -0.0006016054406039516; 0.002538606616559663 -0.008625521792262393 -0.0013063447668219576; -0.0007431336046014572 -0.0007510023846216809 -0.00024388368340730413; -0.0019353136326584978 -0.0023167931738105807 -0.0032678623726020116; 0.00331352745259012 -0.0013369854485649518 0.0005725520083343641; -0.012538588881594691 0.011214600133300242 -0.010983529202275955] %
+
+Mass Used: 108.09681337087432 kg
+Launch C3: 100.04111821669673 km²/s²
+||V∞_in||: 2.202375366138186e-5 km/s
diff --git a/archive/ES_0.5929678242159205 b/archive/ES_0.5929678242159205
new file mode 100644
index 0000000..a38ee6b
--- /dev/null
+++ b/archive/ES_0.5929678242159205
@@ -0,0 +1,22 @@
+archive/ES_0.5929678242159205---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T22:13:08.536
+Launch V∞: [7.016964503868408, -6.859586751406349, -2.393720129000665] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.94058251730632e-6, -1.0235768444667896e-5, -6.329730658913e-6] km/s
+ V∞_out: [-9.028163906652137e-6, 8.001613475422184e-6, 3.876164009130056e-6] km/s
+ time of flight: 1.400632053321556e8 seconds
+ arrival date: 2028-10-13T00:39:53.536
+ thrust profile: [0.34151257104515625 -0.1012780924691812 -0.1575982648927579; 0.19298399658776372 0.04379569419177694 -0.20948043458202228; 0.13871516151138283 0.06973868194272247 -0.24369464248378594; 0.0967516901116657 0.06768836548849243 -0.23587403053632894; 0.05705245584800834 0.04881037495076276 -0.17833065010745774; 0.029990026219615374 0.02988791452745487 -0.11436128341406639; 0.01177260738695077 0.013604663183053482 -0.05435571726514873; 0.0013974939886506753 0.0033414778103997393 -0.017642717761860157; 0.0004661698468206246 0.0004349687597036561 -0.010865043373584926; 0.0004241074384399889 0.0011410106174212873 -0.000721404036566379; -0.0010050133008201248 -0.0022944168020115337 -0.015431164736100617; 0.0016782238354267002 0.007096566248442457 -0.014970002587487216; -0.002229963108191313 4.659128429572489e-5 -0.003418875840188065; 0.0033785625423658067 0.004451384113113044 -0.005122597934484765; -0.000389163649935884 -0.005259612921452945 0.011430562760717092; 0.0030093872669101217 0.0010825759347859022 -0.011290498079873906; -0.00021102064919522592 -0.0009214367612167228 0.0024383490868266715; -0.0015167286368213827 0.0022383751506528365 -0.0011729408314905595; 0.009990520950996895 0.0008001157940022994 -0.0047480156218003035; -0.0023885284091752887 -0.008774098396118073 -0.011875144144609159] %
+
+Mass Used: 96.66969397506409 kg
+Launch C3: 102.02161730460169 km²/s²
+||V∞_in||: 1.266351595896426e-5 km/s
diff --git a/archive/ES_0.5931817125663514 b/archive/ES_0.5931817125663514
new file mode 100644
index 0000000..c900dbe
--- /dev/null
+++ b/archive/ES_0.5931817125663514
@@ -0,0 +1,22 @@
+archive/ES_0.5931817125663514---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T00:57:31.292
+Launch V∞: [5.272672983012078, -8.428765374184438, -1.25863865392458] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.06680124713841415, -0.0968208088668788, 0.015785692125436988] km/s
+ V∞_out: [-0.11114196639782799, 0.03731000977360971, -0.01853944574252354] km/s
+ time of flight: 1.3087422440581664e8 seconds
+ arrival date: 2027-06-15T18:54:35.292
+ thrust profile: [0.34168711114029227 -0.224645275230386 -0.17426982770508678; 0.21663664289202916 -0.02322263998497671 -0.2287976602306669; 0.15675044229243226 0.01685289862481742 -0.24966940525297582; 0.1192171991358809 0.0279400881548228 -0.2489464258037702; 0.0742561378987882 0.02406983959343771 -0.1926243069069755; 0.028182245125195845 0.011143743389641561 -0.08999763068806577; 0.02545900087340555 0.013641786163220801 -0.09993959707020465; 0.023759983543122733 0.013305598363133922 -0.0852188694913378; 0.02638319840564274 0.014874616031820111 -0.1069331924761196; 0.014464488717605152 0.008145599431508317 -0.0737001230307219; 0.000735899079944842 0.00035370276520458514 -0.0025097380217738337; 0.0003503191136975014 -0.0004250794927786638 0.0006758314463510956; 0.0009904937460661714 -0.0011168926392084357 -0.0023462915671688764; -0.0011301960727518603 0.0019597884833895997 -0.00021379411578971766; -0.0011712380387176818 0.00021466670863118823 0.0017857574472284693; -0.001631706486277636 -0.0016401841733447073 0.0014210092024538822; 0.0001435781705763819 0.00022793852726920658 0.002861037444530571; 0.0002610711754194864 0.0035930847239901594 -0.00041676087023806343; -0.0006630598870115771 0.0008763290727969657 -0.0007080047660698329; -4.721831784497484e-5 0.0006514432452461442 -4.318904276066107e-5] %
+
+Mass Used: 106.20752994414033 kg
+Launch C3: 100.4293373799891 km²/s²
+||V∞_in||: 0.11868388148675979 km/s
diff --git a/archive/ES_0.5932353074102352 b/archive/ES_0.5932353074102352
new file mode 100644
index 0000000..5c5b1c9
--- /dev/null
+++ b/archive/ES_0.5932353074102352
@@ -0,0 +1,22 @@
+archive/ES_0.5932353074102352---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T02:42:50.139
+Launch V∞: [5.2275774630061544, -8.423307725876079, -0.9903796131024453] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0763313527406979, -0.09542028155935268, 0.017875952124028115] km/s
+ V∞_out: [-0.11610176947024584, 0.03704215074666436, -0.019946229498363735] km/s
+ time of flight: 1.3094793163564016e8 seconds
+ arrival date: 2027-06-16T17:08:21.139
+ thrust profile: [0.40824666022160455 -0.26358049623277185 -0.2168476400663488; 0.21345303258305318 -0.022676187061925424 -0.2401287390879965; 0.16618285523936707 0.01753924564236687 -0.2806359923579943; 0.12602257779936227 0.02875632526599014 -0.27905532138646555; 0.08390340519572213 0.025631252194998917 -0.22863342974686285; 0.03420834255001937 0.011487906405316238 -0.11028317228765291; 0.022974415194229 0.008622738589444543 -0.08170879678564691; 0.022537168349043228 0.00921300055147264 -0.08949354338701179; 0.013352517318336827 0.005990096180358613 -0.05577491625313846; 0.0017246059539523435 0.0014494604746407133 -0.008016625878344437; 0.004693411664709964 0.0022567353019255208 -0.023606087035782243; 5.629025409637834e-5 -0.0011819548030400522 -0.003111702907776297; -0.004819474586164649 0.0008057103919443692 -0.0016693846436376227; 0.000418562405434757 0.0005575607136412253 0.0018640139578288187; -9.653353484209248e-5 0.001232541165803166 0.0023470953873478907; -0.002646132874864995 0.002649857282874455 0.002283619080563135; -0.0004238155372832938 -0.004662134005889981 0.0024708866871850223; -0.00042096581710816025 -0.002064486423064107 -0.0014669842107340322; 0.008253950057889719 -0.0007720673480298851 -0.008205566126065017; -0.0013820574522187903 0.013299278934910789 -0.004979598029415571] %
+
+Mass Used: 113.08809474354348 kg
+Launch C3: 99.26053095458245 km²/s²
+||V∞_in||: 0.12349516269243721 km/s
diff --git a/archive/ES_0.5933702059854733 b/archive/ES_0.5933702059854733
new file mode 100644
index 0000000..65bae58
--- /dev/null
+++ b/archive/ES_0.5933702059854733
@@ -0,0 +1,22 @@
+archive/ES_0.5933702059854733---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T08:36:28.043
+Launch V∞: [5.280850752872226, -8.445225775047234, -1.2888091762063236] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004174755249018222, -0.0015144067514947152, 0.0013719056262559916] km/s
+ V∞_out: [-0.0026983308103363008, 0.0032230853653038914, -0.0019848936678008885] km/s
+ time of flight: 1.3403810192563969e8 seconds
+ arrival date: 2027-07-23T17:24:49.043
+ thrust profile: [0.3078822149445696 -0.20430845662280997 -0.1699276115990732; 0.12500458345876947 -0.015964094584926588 -0.1507245214047607; 0.14301929787021214 0.01025089980260391 -0.25884898668336764; 0.11886631448831558 0.02191508108695321 -0.28324505105931586; 0.0791567228845652 0.020548404496585123 -0.23269302299915776; 0.043895363004692704 0.01391750784650861 -0.1516996131488698; 0.02308314252917589 0.008236010432505258 -0.089934474392422; 0.01070704850225262 0.004335258338993099 -0.045322565279762764; 0.002839666252973659 0.000902192900927281 -0.013802053427722298; 0.0038412477724697877 0.002051505850916847 -0.01861211457377757; 0.0034068356889480726 1.5742481832152965e-5 -0.018502926833882407; 0.0018242581971640319 -0.0029197651818665053 -0.00155356360290921; 0.0021728472254678955 -0.002233142492802997 0.0030345296388666863; 0.0001943138929112162 0.0014565169382778531 -0.004836138834864446; 0.006864798304922451 0.008806402201934061 -0.01940962893163582; -0.011595668578552883 -0.01204794305435655 0.0024248782206575145; -0.006062965112970626 -0.00111170522747314 -0.0017503058582414442; -0.00494772578021377 -0.01168911108270239 -0.03522879757318401; 0.0032768105022168747 0.0007591418433387845 -0.00022472674351482422; 0.0282045382100743 0.01702034184914292 -0.025903705373166955] %
+
+Mass Used: 103.85543605959492 kg
+Launch C3: 100.87025215830695 km²/s²
+||V∞_in||: 0.004648024768170973 km/s
diff --git a/archive/ES_0.5934297788610224 b/archive/ES_0.5934297788610224
new file mode 100644
index 0000000..9b9a9c3
--- /dev/null
+++ b/archive/ES_0.5934297788610224
@@ -0,0 +1,22 @@
+archive/ES_0.5934297788610224---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T03:33:39.840
+Launch V∞: [5.251365189958864, -8.376107237871743, -0.7568996766210271] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0022721139565908834, 0.0021035627734235663, -3.680686890725109e-5] km/s
+ V∞_out: [-0.0010800280116283663, 1.4898593126194728e-5, 0.002904129928083424] km/s
+ time of flight: 1.3077708279039906e8 seconds
+ arrival date: 2027-06-13T18:31:41.840
+ thrust profile: [0.40197714509337223 -0.2707152555830266 -0.1976393074556257; 0.24490222001420106 -0.030681204056781968 -0.24931466780953584; 0.23443448843989573 0.019036946197039238 -0.35727664679420146; 0.12229189085416865 0.024557891815528653 -0.2441479832526934; 0.10897274045496909 0.030498674179681974 -0.262485713108441; 0.06950104249210784 0.023664912971031536 -0.1943497888890084; 0.008088813236374693 0.003479083751753721 -0.028027317533158506; 0.00835388206514774 0.0035883976954005554 -0.031244434391831166; 0.009013633094344565 0.0037069459629804043 -0.03478819910090445; 0.005320909963797327 0.0018032089181528085 -0.02194323786126064; 0.0065176763576936724 0.0037715590684332147 -0.02855580261894979; 0.004951052010523913 0.0039699153427181074 -0.0023479073925088533; 0.0017167928349648746 0.0016176074219790759 -0.004816227609344658; -0.001193794335998821 7.951249257175021e-5 -0.002266909451017266; -0.0041788949629959025 0.0029187194643443826 -0.0077306883346256825; -0.0007129050199033843 -0.0004864838859905189 -0.006382911875137825; 0.0013404748364610002 0.0008365796250102071 -0.007242108364944445; 0.00033055882333728366 0.0009107390224873805 -0.003108032355596235; -0.0023244923764255696 -0.002761115215101398 -0.01270062690207675; -0.0011892067615845538 0.002681044162006035 -0.007891105161294324] %
+
+Mass Used: 118.86612402639548 kg
+Launch C3: 98.30890593910812 km²/s²
+||V∞_in||: 0.003096584072662533 km/s
diff --git a/archive/ES_0.5934846643500131 b/archive/ES_0.5934846643500131
new file mode 100644
index 0000000..fe9bd1b
--- /dev/null
+++ b/archive/ES_0.5934846643500131
@@ -0,0 +1,22 @@
+archive/ES_0.5934846643500131---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T08:07:56.898
+Launch V∞: [5.189420502889784, -8.445916472515794, -0.9439562380609151] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.03176861285877689, 0.023263137738941213, 0.02464995749537951] km/s
+ V∞_out: [-0.02144721137672497, -0.03370911559420884, 0.02368829983056442] km/s
+ time of flight: 1.3016142706085531e8 seconds
+ arrival date: 2027-06-07T20:05:03.898
+ thrust profile: [0.4305932270690652 -0.2906011387896286 -0.22782382185932282; 0.20423311910650938 -0.0249941979407412 -0.22872036316433303; 0.17497959678248523 0.013434982353309907 -0.2895942172036349; 0.12127652626177661 0.024145243817039502 -0.26549444686636603; 0.08895272828548408 0.02428810500312093 -0.23696657543326854; 0.030381687070827747 0.009347080224336444 -0.09602239317507404; 0.040776889030947186 0.01821915394538188 -0.14889076985197044; 0.0070354470615983855 0.0030178134174101852 -0.027735131992563875; 0.023321711825734576 0.010428290858152696 -0.09772237108839839; 0.0009283364422430895 -0.00021832015427905105 -0.004139019699323744; -0.0022897171109264275 -0.0028756411894441023 -0.003646873193334911; -0.0003319592202386917 -0.0002851325613757739 5.3597241891257304e-5; 0.0007531638742631313 2.836784508332955e-6 -0.004002790055087257; 0.00577609384249048 0.0010098059956826556 0.0021228008732628034; -0.003423894002746955 0.00653350033960237 -0.00019374608950976078; -0.0005014374238281275 0.0021751789521295673 -0.005903802747556816; 0.0007395601290418832 0.0013610274181955779 -0.0024772732244422195; 0.00427151826086424 0.000596436425407768 0.0019837788472765565; 0.0011330293921381605 0.0008975814363211823 -0.0025457745113134102; 0.0031501664932766845 0.0012433868238183434 -0.007220261257264749] %
+
+Mass Used: 113.99668743226175 kg
+Launch C3: 99.15464359590061 km²/s²
+||V∞_in||: 0.04645469561794385 km/s
diff --git a/archive/ES_0.5934888214184667 b/archive/ES_0.5934888214184667
new file mode 100644
index 0000000..21d954f
--- /dev/null
+++ b/archive/ES_0.5934888214184667
@@ -0,0 +1,22 @@
+archive/ES_0.5934888214184667---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T11:55:22.487
+Launch V∞: [5.383957037715122, -8.284851845614584, -0.8508961753984616] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.828516509116639e-5, 1.2391959328036227e-5, -2.8378033354446248e-5] km/s
+ V∞_out: [-2.5101560345838475e-5, -2.3086241251314013e-5, -1.1410713230024937e-5] km/s
+ time of flight: 1.3341697574594368e8 seconds
+ arrival date: 2027-07-13T16:11:37.487
+ thrust profile: [0.3701724687937596 -0.24432525484662884 -0.18416140469439107; 0.23856044097757992 -0.0252693200401675 -0.24895837027577705; 0.21817771486108603 0.022872676846348257 -0.345220819510482; 0.11533881107907508 0.02678660660481926 -0.23737805390937253; 0.09905460240180207 0.03131116849358728 -0.2470668577110569; 0.0629627327451391 0.023999808378584005 -0.1808819171580618; 0.02738612320479166 0.012233843786660155 -0.08685466048783357; 0.006479772199042 -0.0021030797966517184 -0.01586931016760348; 0.0035931833511722282 -0.0031713534590607478 -0.01175430656279951; 0.008613731959954792 0.0019962031589148004 -0.02114353903360717; 0.0036907246547225494 0.002786357149390457 -0.014217567916231697; -0.0007215102928557924 -0.0012742251101514968 -0.00897710255066328; 0.0009902232530533874 0.0003409651400996406 -0.0013432899500748058; -0.001974878835932083 0.002928022202101357 -0.001973673618202401; -0.0006936557629617112 -0.004229566433320363 -0.010394219562867159; -0.0012286725309032325 -0.0014383231946236785 0.004631619651556061; -0.026640821263203485 -0.009895051758423843 -0.01701831894511583; -0.006337129239355251 0.00789638304143281 -0.00998524793857611; -0.0020306758940976783 -0.018818158756755545 0.0003375681312353403; -0.00160250573335269 -0.006979489523815926 0.014156233202143823] %
+
+Mass Used: 118.69652955206675 kg
+Launch C3: 98.34978778905332 km²/s²
+||V∞_in||: 3.59613778304583e-5 km/s
diff --git a/archive/ES_0.5936146482434607 b/archive/ES_0.5936146482434607
new file mode 100644
index 0000000..bb83f0c
--- /dev/null
+++ b/archive/ES_0.5936146482434607
@@ -0,0 +1,22 @@
+archive/ES_0.5936146482434607---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T14:40:37.546
+Launch V∞: [7.053991654862541, -7.171454059421256, -1.2836902590021948] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0048904948010158955, -0.026115211218060798, -0.02824651307568185] km/s
+ V∞_out: [-0.03380623655062841, -0.0041227397835841475, 0.018540419215276695] km/s
+ time of flight: 1.2817796000088018e8 seconds
+ arrival date: 2028-05-29T03:39:57.546
+ thrust profile: [0.2541061450369371 -0.10958181665259469 -0.14389243670439628; 0.15731069088471233 0.009599201103935282 -0.183745867915023; 0.12171666849341094 0.03206486126223185 -0.2239594583315935; 0.0888688682161833 0.03422269165482775 -0.22143047359413912; 0.06988978046921289 0.03269960728751742 -0.2155951180996103; 0.05155919166752659 0.027305620301131893 -0.18780171935927048; 0.03382436110797547 0.019525065853194187 -0.14155210356865577; 0.021043422163052272 0.012842412762867931 -0.09794532670835825; 0.01005568205474514 0.006324617983210141 -0.050582364921846666; 0.0028690356968743167 0.0018648269160799619 -0.01571660733093748; 0.0011334702022760931 0.0012107639770654887 -0.011594296597490887; 0.0005098831204631122 -1.3420450061373684e-5 -0.000767414807593605; -0.0009029729503510468 0.000635766393146392 -0.0007906627304370042; 0.0005554185702005439 0.000391715102913938 -0.0009713051370460169; 0.00013362374662889535 7.35408822916503e-5 0.0012615398657446935; 0.0001641160455669176 -2.8889981858704015e-5 0.0005193738528324766; 0.0013614026058389652 -0.0017259278735075614 -0.0007395056091172935; -2.3543100946193734e-6 0.0002744705830220118 -0.0008158801680039657; -0.00028226118896062017 0.0002433899603437642 0.0005602668964041826; 0.0011893901023071441 -0.0002664808570053187 -0.0006625230500551196] %
+
+Mass Used: 92.67135135052104 kg
+Launch C3: 102.83641227431711 km²/s²
+||V∞_in||: 0.038778688700075434 km/s
diff --git a/archive/ES_0.5936563710355502 b/archive/ES_0.5936563710355502
new file mode 100644
index 0000000..fd7bc14
--- /dev/null
+++ b/archive/ES_0.5936563710355502
@@ -0,0 +1,22 @@
+archive/ES_0.5936563710355502---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T01:35:08.799
+Launch V∞: [6.973725002380063, -7.158167609948747, -1.0388599044252125] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.160569454447477e-6, -2.966562926174621e-6, 5.641722104319764e-6] km/s
+ V∞_out: [2.7914010598117373e-6, 6.121313408047263e-6, 1.9470905809043898e-7] km/s
+ time of flight: 1.2771817287411655e8 seconds
+ arrival date: 2028-05-23T06:51:20.799
+ thrust profile: [0.3705829679172081 -0.14776443421316432 -0.1778072001123787; 0.2022780007949641 0.014849316352127821 -0.22517063190280773; 0.13697535103555694 0.03855886794881133 -0.24027367786337808; 0.11330237027004908 0.046351230478299345 -0.26630848339732993; 0.08084657520312467 0.04006272244882264 -0.23532561849902353; 0.05758214825750237 0.03211719079397182 -0.19789757387350176; 0.035065586374655566 0.020810547402573418 -0.13649118893757034; 0.016460576984779495 0.009690084515159831 -0.06878416334532059; 0.003491797046822365 0.0014409646857884671 -0.014272562965927965; 0.0018821226102872415 0.0013228126310332953 -0.010076950236730255; 0.0003689336433919133 0.0002452359265749096 -0.002397699580956381; 0.0013638427761715742 0.0010968617973255914 -0.008051805334504602; 0.0008057640329301467 -7.321943666510817e-5 -0.0030349644658107674; 0.000458944670562283 -0.00010586894451104561 -0.0013335137137603786; 0.00019615681649058663 0.00037957979262535045 -0.0014725250468680734; -0.0008939886581959997 0.0017570344700703771 -0.001575218257305235; 0.002460434705932481 -0.0008361813419322742 -0.0002379030671999507; 0.0004992127665537029 0.00038744879886640525 -0.0021767267235628003; -0.0002632214263660833 -0.0020730805761533743 0.0007853657459420036; 0.001112249282311455 0.000571004665119698 -5.07568953521379e-5] %
+
+Mass Used: 103.71573546336049 kg
+Launch C3: 100.95143384196254 km²/s²
+||V∞_in||: 6.730348004733145e-6 km/s
diff --git a/archive/ES_0.5936747535450996 b/archive/ES_0.5936747535450996
new file mode 100644
index 0000000..43d6f80
--- /dev/null
+++ b/archive/ES_0.5936747535450996
@@ -0,0 +1,22 @@
+archive/ES_0.5936747535450996---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-17T11:46:39.560
+Launch V∞: [6.215875356358792, -7.157222442424506, 0.17815331063371914] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004518953937718152, -0.00013622728313362125, 0.0031486817305718825] km/s
+ V∞_out: [-0.005301989399702681, 4.726928559993709e-5, 0.0014738052115971353] km/s
+ time of flight: 1.849139571698521e8 seconds
+ arrival date: 2029-02-24T16:45:56.560
+ thrust profile: [0.7053559407955765 -0.17174624724012297 -0.10998972139268744; 0.45776742991070835 0.1812813452670398 -0.21306022162263924; 0.22682845817233516 0.17271318963291907 -0.1833353561118374; 0.14916541321458204 0.1584924935222779 -0.17162457826960018; 0.08750338432965618 0.117284985406468 -0.13317632950033453; 0.039398907488896545 0.06380545430031329 -0.07705471380390319; 0.015913196121395374 0.02989257561815591 -0.03764315398596718; 0.002506529935024408 0.007018310621458685 -0.008722600368849726; 0.0016847954566007537 0.00522421620816193 -0.007292930882040773; 0.0016120653039666277 0.005185201843217569 -0.007051756203084842; 0.0003540232235875635 0.0002386330181562508 -0.0008186925408989557; -0.00015795485443240864 0.000786752920891885 -0.001566293153216231; 0.00045000326696430053 0.0014595179296725534 -0.0015699274930502766; -0.0002515770454893986 0.0014102994079326732 -0.0003668468492673421; 0.00017645112958828384 0.0007331354988024644 0.00011645750768445864; -4.59236126917449e-5 -9.61457405227306e-5 -0.00013725844111335555; -0.0004723372337817419 0.0011577969793203427 -0.00018013185994573098; 0.0008287228643312685 0.0006547076183490695 -5.822994407320175e-5; -0.0003660519471426647 0.0006359968056648135 -0.0005188682970155562; -5.1554494824016385e-5 0.0003154163030880667 -0.0019280068032981718] %
+
+Mass Used: 168.2349233296468 kg
+Launch C3: 89.89467813822331 km²/s²
+||V∞_in||: 0.005509419134929336 km/s
diff --git a/archive/ES_0.5936807370078058 b/archive/ES_0.5936807370078058
new file mode 100644
index 0000000..358765b
--- /dev/null
+++ b/archive/ES_0.5936807370078058
@@ -0,0 +1,22 @@
+archive/ES_0.5936807370078058---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T23:05:05.841
+Launch V∞: [7.089544606695962, -6.798081472517144, -0.9386073387897826] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0007021531526370137, 0.001868032101876442, 0.00016518924830750132] km/s
+ V∞_out: [-0.00014157828340630838, 0.0006016087349115263, 0.001906133588557686] km/s
+ time of flight: 1.328325563611278e8 seconds
+ arrival date: 2028-07-17T09:01:01.841
+ thrust profile: [0.5583087621146718 -0.19346458944678394 -0.22454189639720643; 0.271423228556157 0.04893368798923968 -0.2622970048801325; 0.1812679757619422 0.0795156960063673 -0.2786730596634351; 0.1467283740621483 0.09016250062386583 -0.30263016517521774; 0.08122491617875645 0.06013164160703718 -0.21644378593555264; 0.03663214122423786 0.03125381125788394 -0.1188236564814611; 0.03586703012616281 0.035664877104801214 -0.13180639161171345; 0.014350334654105056 0.014732772298381425 -0.05802773862213092; 0.006187393928650218 0.005960985037535871 -0.026386391294755965; 0.004764856851486372 0.004846090961962075 -0.022835131765288515; 0.00024244990878550477 0.0007171023275788532 0.0006878933823539487; 0.0006525781419467191 0.00030219900565102014 0.0016400602642988428; 0.003064512270161207 -0.0019067297529605045 0.0011878147753100685; 0.0006856854726491099 0.0011635325829219515 -0.001452857159594518; 0.0001335403044897028 0.0007206526719332344 0.0021034132782842734; 0.0005499406095937658 6.925680467494583e-5 0.001335479684264586; 0.0038323523648402386 -0.002820389574907911 0.003977693193726115; 0.001600148413778542 -0.003676261176776359 -5.207546322827112e-5; 0.0023506848549227793 -0.0022624900515054915 0.0063727260380839; 0.003863268705566118 0.0012522517910134026 0.0005481130432578353] %
+
+Mass Used: 124.7143871622743 kg
+Launch C3: 97.3565381737427 km²/s²
+||V∞_in||: 0.0020024611035312054 km/s
diff --git a/archive/ES_0.593793498765206 b/archive/ES_0.593793498765206
new file mode 100644
index 0000000..a33d3f0
--- /dev/null
+++ b/archive/ES_0.593793498765206
@@ -0,0 +1,22 @@
+archive/ES_0.593793498765206---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T17:20:36.416
+Launch V∞: [6.99304278643665, -7.1656629244307055, -1.4252776714308286] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0036821459552727103, -0.05256849867260131, -0.006112304643929364] km/s
+ V∞_out: [-0.050720346984171376, 0.009567272585364234, -0.012256117336090685] km/s
+ time of flight: 1.2838218609210908e8 seconds
+ arrival date: 2028-05-31T15:03:42.416
+ thrust profile: [0.3456277040959277 -0.14242720910679546 -0.1796923436907986; 0.15405548745735825 0.009254773573156136 -0.1845711534351395; 0.12927676226454454 0.03408384156535639 -0.24431439884867695; 0.09777774265830672 0.037580963745592194 -0.24924885583728948; 0.07264002832776364 0.033902729282422966 -0.22944884676160196; 0.024355289352779835 0.01252212546040605 -0.0917291219219958; 0.01766554293607679 0.011474534458728597 -0.0779263205410512; 0.03684359341166368 0.02262228134677881 -0.16921534621569037; 0.008372321602920571 0.005187030364106932 -0.04385353988451567; 0.002714143077647011 0.001304616633524269 -0.008239427125867295; -0.0010419126713411885 -3.804924670120928e-6 -0.0009636442147779932; -9.584928877742218e-5 0.0008859568024885095 -0.0020403784666044294; -0.0011060171254399583 0.0012521333788689157 0.0007088845181577865; 0.0002042882719275851 -0.00046341356032143246 0.0007489535065443485; -0.0012163859766113681 -0.0040261006596902064 0.0026824804963739924; 0.0013128883510086778 -0.0008873604390162294 -0.0008716342276416871; -2.231010868378381e-6 0.0003563736066616968 0.0006474170072767059; 0.0024280330782022594 -0.0036431959527991314 -0.00031866046500340895; -0.0015788707854989675 -0.0012703958128135171 0.0032163297069826113; -0.0048146011021498215 -0.003636717204325676 0.0008093997975028485] %
+
+Mass Used: 96.1211460583936 kg
+Launch C3: 102.28078900017375 km²/s²
+||V∞_in||: 0.05305059396074108 km/s
diff --git a/archive/ES_0.5938088720081811 b/archive/ES_0.5938088720081811
new file mode 100644
index 0000000..caad7c3
--- /dev/null
+++ b/archive/ES_0.5938088720081811
@@ -0,0 +1,22 @@
+archive/ES_0.5938088720081811---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T00:32:46.328
+Launch V∞: [6.7906057130011765, -6.894163422890962, -0.6360363837185424] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.855995027855733e-10, 1.0882315980957123e-9, -1.6750419259354234e-9] km/s
+ V∞_out: [9.875047912920991e-10, 2.061426184328612e-9, 5.560600549496966e-11] km/s
+ time of flight: 1.3162413767309725e8 seconds
+ arrival date: 2028-07-04T10:48:23.328
+ thrust profile: [0.7724526602611458 -0.28875736672786767 -0.3050433582026466; 0.40988245689504177 0.052650152486488536 -0.3837731465152244; 0.23839580921476014 0.08736440396032724 -0.357019333288811; 0.12038145226216894 0.06326777246411294 -0.24997549217344678; 0.05429689927549694 0.034381079763908876 -0.14438275719951554; 0.029402180315311666 0.021073429199020242 -0.0934098056781729; 0.019569679552744013 0.015264817345107144 -0.07107219889803645; 0.011425268354437605 0.0094649618331271 -0.046664060241420335; 0.011806740847302388 0.00996903118681477 -0.05335219225324943; 0.010478509529737504 0.0107493474343361 -0.0494458611808448; 0.0011973218105881963 0.0027949536163874985 -0.00838502154035478; -0.002677571486022121 -0.003597161244224775 -0.001191083791284581; 0.0021879368529266873 0.002289993972306651 -0.0017933214697654926; -0.0009032862546082535 0.00452922730743809 -0.003033427808057875; -0.007175883468469604 0.012478816008564257 0.0027474743349833047; -0.007341636941873325 -0.004331474137513357 -0.0014636670097971439; -0.006305104280932295 0.00017440703105379095 0.0069533279169810515; 0.004436179020229377 0.0045635591504901525 -0.016695460757843127; 0.0026433040169782365 0.0024114765798169575 -0.017296989534991133; -0.0014257253507889076 -0.003601013158145492 -0.0017910439761899847] %
+
+Mass Used: 144.17326507062853 kg
+Launch C3: 94.04635753238561 km²/s²
+||V∞_in||: 2.1850171496053425e-9 km/s
diff --git a/archive/ES_0.5938202364909837 b/archive/ES_0.5938202364909837
new file mode 100644
index 0000000..0405ab3
--- /dev/null
+++ b/archive/ES_0.5938202364909837
@@ -0,0 +1,22 @@
+archive/ES_0.5938202364909837---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T20:17:03.291
+Launch V∞: [7.338868564817435, -5.816236195582114, 0.4681529305640815] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4172826906165642e-9, -1.462453811205201e-9, -1.516208685483757e-9] km/s
+ V∞_out: [3.0714657311758194e-10, -2.691243108772798e-10, 1.0222152077048442e-10] km/s
+ time of flight: 1.8502846724179867e8 seconds
+ arrival date: 2030-03-12T09:04:50.291
+ thrust profile: [0.6882289986904133 0.0011208001872334403 -0.0734294244713941; 0.43905503704937854 0.308623965093201 -0.16503106812914098; 0.24529185241554113 0.30300103912822096 -0.17254166305199964; 0.15575749039723202 0.27631664766705016 -0.1711063708060746; 0.08025376269743956 0.19175321479262442 -0.1302272316739733; 0.024229528182876194 0.07517886199302003 -0.056728884101559345; 0.0016963069908747233 0.004239501029044149 -0.0054931850620610805; -0.0003204176346410894 0.0015794557702571374 -0.001456358610241956; 0.0018170918594260397 0.006952032326675308 -0.006087133126873277; 0.0011317101428398291 0.006878670268198909 -0.0035268093971886237; -0.0004984057978778444 0.0035649962699371225 -5.4793485604510625e-5; 0.0020311143519811045 0.0017119938989496397 0.000769494174654199; -0.002203283370922122 -0.0013136980607298685 -0.001739286601039917; -0.0002958859538867526 -6.530729295442771e-5 -0.0014727065285514284; -0.0004991362128949627 0.0005396275876357584 -0.0021757613518704633; -0.006095344176850572 -0.0011174622852345314 0.0005318507316617296; 0.00028714084884792356 -0.004666045708154429 0.002393321059374124; -0.0008880204240207127 0.0015519150007126566 0.0013855589202260966; -0.00359368627479118 0.0014550278903132697 0.002426452908503767; 0.00022351210593939559 0.0015719299880303684 0.0014213049264585054] %
+
+Mass Used: 180.00082821779324 kg
+Launch C3: 87.90676246086075 km²/s²
+||V∞_in||: 2.538966355225356e-9 km/s
diff --git a/archive/ES_0.5938481779673737 b/archive/ES_0.5938481779673737
new file mode 100644
index 0000000..ca2ff0c
--- /dev/null
+++ b/archive/ES_0.5938481779673737
@@ -0,0 +1,22 @@
+archive/ES_0.5938481779673737---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T13:41:03.097
+Launch V∞: [6.968562782062135, -7.275629583584221, -1.1527357318526512] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.997390739606952e-5, 0.0001317172545687753, 7.943769135053333e-5] km/s
+ V∞_out: [0.00012574192207934012, -9.548594154276599e-5, -5.0449457635588534e-5] km/s
+ time of flight: 1.3051733469291157e8 seconds
+ arrival date: 2028-06-27T04:29:57.097
+ thrust profile: [0.2621166917202911 -0.11061739574027105 -0.14250545804597553; 0.12668714860510472 0.00308424095481381 -0.16058159612585765; 0.08552275616606232 0.016789755212205472 -0.17161534436215908; 0.06959074290167659 0.020208801720388376 -0.18792160458845125; 0.06006057521839096 0.020353335830590277 -0.20295012867840143; 0.038884500317630334 0.014086787607386408 -0.1551881640708535; 0.047780877396053606 0.022852794754255286 -0.21518443675923712; 0.031785065935954995 0.013565874383049641 -0.16062781663404763; 0.003596671131258046 0.0011597522016735377 -0.016903657500094968; 0.0036543630157858504 0.0024981643962717504 -0.019612380334608312; 0.0016806553823710347 0.00024531419417211844 -0.009717721538511229; 0.0023238030877150563 0.0014775235138032635 -0.014044429429013317; 0.0010387425101413147 0.0006124943801486463 -0.004938423022869826; 0.005740412146199279 -0.0028272810268630266 0.000884504416917729; 0.0005232486119766685 0.0025883394044432222 -0.0033988634863348346; 0.0016874669277907033 -0.00034991020273669304 0.0015525271319570342; -0.0012874958121158193 -0.0006791076371076533 0.008321106284874476; -0.001605523961539904 -0.01225996252065743 -0.002295927438229306; 0.005636655897444166 -0.005097182299828947 0.003994500565872698; -0.0013538355394760089 -0.004086548364815445 0.0015049338138043667] %
+
+Mass Used: 93.01356657201814 kg
+Launch C3: 102.82445275255733 km²/s²
+||V∞_in||: 0.00016509588585603965 km/s
diff --git a/archive/ES_0.5939066484013086 b/archive/ES_0.5939066484013086
new file mode 100644
index 0000000..0abe48f
--- /dev/null
+++ b/archive/ES_0.5939066484013086
@@ -0,0 +1,22 @@
+archive/ES_0.5939066484013086---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-16T11:57:33.066
+Launch V∞: [6.126711260700956, -7.02627176671172, 0.7041076548015559] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013117179485996108, -0.006317957465119664, 0.01483279141848955] km/s
+ V∞_out: [-0.013241174646215829, -0.005526138445469178, -0.01503467127268625] km/s
+ time of flight: 1.8409989287459084e8 seconds
+ arrival date: 2029-02-14T06:49:05.066
+ thrust profile: [1.0 -0.29472843402314414 -0.1635513083341974; 0.49554621039302216 0.18419161121849825 -0.24509008170383212; 0.27485959804452326 0.19890571744092597 -0.23165437188367638; 0.11289424171968312 0.11442207263223063 -0.1386839036033489; 0.0505179566259846 0.06496775369016264 -0.08334437234645214; 0.013143896814665995 0.021068349314727734 -0.028148094332977065; 0.005582919433898472 0.010346612400449703 -0.014663376890295761; 0.005036901326868118 0.013724034110725923 -0.019107558655156436; 0.0016420776674595176 0.0005332139081565524 -0.0015008337913855869; 0.0013757483882854615 -0.00011977289029006279 -0.001942782386223218; 0.0021718338920675546 0.0030484855645293344 -0.005558240866583919; 0.0004399637053272632 0.0007418486346301708 -0.0006103162067661851; 0.0015890720485384785 0.0018399303232700167 -0.0033970730591397903; -0.00033824357217226 0.0008206371966668034 -0.00036426441434534384; 0.00143881782866472 0.001838184720416943 0.0017573658955683526; 0.00027958275026443273 0.001662157399423402 -0.0022927849488543015; 0.0014664550655698288 -0.001355383636827543 -0.003211156690565024; 0.003970896653251876 -0.004948283471421881 -0.0008661688000964321; 0.00015854096149695842 0.001077837045876471 -0.0031107111998189066; -0.0006601919050270963 0.0011979784186945273 -0.0008763440734319461] %
+
+Mass Used: 183.05277829429178 kg
+Launch C3: 87.40085340124027 km²/s²
+||V∞_in||: 0.02078433750359428 km/s
diff --git a/archive/ES_0.5940513432898027 b/archive/ES_0.5940513432898027
new file mode 100644
index 0000000..845a540
--- /dev/null
+++ b/archive/ES_0.5940513432898027
@@ -0,0 +1,22 @@
+archive/ES_0.5940513432898027---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T07:45:20.886
+Launch V∞: [7.973057079180379, -6.032306646084787, 0.15883716818576069] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00031642107229713843, -0.00028970206981836504, -0.0002663855200157686] km/s
+ V∞_out: [4.783139520897065e-10, -4.5990978019925646e-10, 1.7150616849993708e-10] km/s
+ time of flight: 1.8452392011420587e8 seconds
+ arrival date: 2030-03-24T00:24:00.886
+ thrust profile: [0.17902819038342382 -0.016560540600647718 -0.07897757228471833; 0.008297454204044416 0.0058660795620747025 -0.0171823937701842; 0.03840587251741653 0.02050203719862748 -0.10445205838748453; 0.030861450150619016 0.018959621742192234 -0.11576349954293513; 0.047593790138428224 0.023026431577536147 -0.19674700935780423; 0.02419122894750535 0.017699056976879474 -0.14472651166944425; 0.01168019597828495 0.008383700503304545 -0.0811731046415208; 0.008994345139158253 0.00739051724724717 -0.07303898724470517; 0.0037095209388160115 0.006841977958533957 -0.026426921080539064; -0.0030236834381235974 0.012375539067935662 -0.01410086401011728; -0.0019801047686471645 -0.0022062833686309303 -0.005990260816309725; -0.018744238945247786 -0.0012414452304286812 0.04366617788299673; 0.0317317165411851 0.006397474544719496 0.00697427623053501; -0.005332409815045945 0.002517070831854714 -0.033133426360341375; -0.01915768238691615 0.013451090176075821 0.0451418913918341; 0.004231891128927282 0.010951051700635712 -0.007872204627869611; -0.04068555835905237 -0.03495635056613406 0.01505633343413533; 0.04958724193936363 -0.11520963559700724 0.06663732411693934; 0.05862772614732249 -0.006141358593468023 0.05177366883822202; -0.023009190724913982 0.013082681080734779 0.0064038827321138995] %
+
+Mass Used: 109.82228105156128 kg
+Launch C3: 99.98359190626432 km²/s²
+||V∞_in||: 0.0005049859696316198 km/s
diff --git a/archive/ES_0.5940720637686657 b/archive/ES_0.5940720637686657
new file mode 100644
index 0000000..6a4f8c2
--- /dev/null
+++ b/archive/ES_0.5940720637686657
@@ -0,0 +1,22 @@
+archive/ES_0.5940720637686657---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T13:42:29.794
+Launch V∞: [7.24908666441492, -5.69273504302348, 0.31859088252171686] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4165869758267268e-6, -3.096751860166736e-6, -3.0316599412487135e-7] km/s
+ V∞_out: [2.442475929700426e-7, -1.2361333329595843e-6, -3.719211391368041e-6] km/s
+ time of flight: 1.8749577787308362e8 seconds
+ arrival date: 2030-04-09T15:52:06.794
+ thrust profile: [0.9459700937815455 0.00866116295414477 -0.10608976677549627; 0.592751306147782 0.43125526260847813 -0.22550084497172393; 0.1284255756999979 0.16972801967954015 -0.102245129289238; 0.07836200575514078 0.15090119694715215 -0.09918315606273058; 0.061160239272843905 0.16068160585568597 -0.11220797847310726; 0.03223695417442165 0.11459047635892465 -0.08641893151922245; 0.014817395733145097 0.0703546252567591 -0.057363943727099256; 0.0010982001794546563 0.006602472847974517 -0.0056317733181114145; 0.0007820282131692237 0.0038337716419191105 -0.0036242143854839704; 0.00013611283293167863 0.0033365936553658914 -0.0031119842438944124; 0.0035400752265991276 0.0032198424299769647 -0.002329360393657753; -0.001262155427298444 0.000790689757987569 -0.002913774365240401; -9.731347521171704e-5 0.0016595166077602737 0.0010066116748277615; 4.1434312877197156e-5 0.0006018117767069605 -0.0009400902772036352; -0.0004661078977509078 0.0014868674987711936 -0.0018006957008801358; -0.0006774454342085516 -0.0006214664078479425 0.00029861341317584844; -0.00035184282843898776 0.0009742032140907669 -0.0024863067989954342; 5.095660373466925e-5 0.0007927781325643335 -0.00014069534597370165; 0.00018515238157293645 0.0016772176092949478 -2.6680929478876524e-5; 0.00021623929131710598 0.0006599550808550534 -0.002324662884962604] %
+
+Mass Used: 196.91246671274166 kg
+Launch C3: 85.05798988869172 km²/s²
+||V∞_in||: 3.939755616174083e-6 km/s
diff --git a/archive/ES_0.5941173824751748 b/archive/ES_0.5941173824751748
new file mode 100644
index 0000000..25be26a
--- /dev/null
+++ b/archive/ES_0.5941173824751748
@@ -0,0 +1,22 @@
+archive/ES_0.5941173824751748---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T06:58:13.802
+Launch V∞: [5.306558192132715, -8.192565757883214, -0.3307870529401668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.161703138260608e-6, -9.931207874924512e-6, -1.3266714367793127e-5] km/s
+ V∞_out: [-1.6253411255710156e-5, -9.672776493002324e-6, -4.603542249595669e-7] km/s
+ time of flight: 1.4017267470131984e8 seconds
+ arrival date: 2027-09-30T15:49:27.802
+ thrust profile: [0.557451007160547 -0.3248024439562486 -0.23633156601205474; 0.16180788785228395 -0.006475995126772797 -0.15997797072898212; 0.12405078411352473 0.022401627956949544 -0.18724593942530704; 0.10334777479212583 0.03228059466241336 -0.20487851308315289; 0.06716235481681823 0.027034805724804694 -0.16377100721918533; 0.08861378949462582 0.04144145591990235 -0.2442523828686116; 0.07002625610699469 0.03758432111977204 -0.21761229386234343; 0.011757255144668247 0.004075199065131241 -0.03684929488505356; 0.009990928382363895 0.011566381218812177 -0.036167623272682636; 0.022856475403590586 0.012345774185536007 -0.08372929966589249; -0.00015555315091651117 0.0012813826928093994 -0.012812843423539718; 0.0012107859702959745 0.0011518877674398659 -0.007005564092238386; -0.004428320387062187 -0.002547100209960524 0.003875203233521198; -0.000808790142238721 -0.0008679150021288049 -0.0016860884175704492; -0.0016196457368066759 0.0034526548360214737 -0.016566488880133613; 0.009131145357340428 0.002014607169922757 -0.013797124391080468; -0.04536417410512167 -0.018619603770292648 0.004375717203667225; 0.004399575680103693 0.0153461573164118 -0.0028292332005749217; -0.02207092599386822 -0.005826564291587746 0.05311254528608121; -0.017739021178888516 0.024266841714902464 0.042472501819404096] %
+
+Mass Used: 136.71211678197915 kg
+Launch C3: 95.38711361812425 km²/s²
+||V∞_in||: 1.8935981737559462e-5 km/s
diff --git a/archive/ES_0.5941678898067859 b/archive/ES_0.5941678898067859
new file mode 100644
index 0000000..ca48a63
--- /dev/null
+++ b/archive/ES_0.5941678898067859
@@ -0,0 +1,22 @@
+archive/ES_0.5941678898067859---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T03:17:32.227
+Launch V∞: [5.281614747896973, -8.395627209689025, -1.1709504136820044] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.06510997022866781, -0.0941450393584687, 0.015279571627856887] km/s
+ V∞_out: [-0.11017271793557397, 0.02898427525778063, -0.01894730684669426] km/s
+ time of flight: 1.3137913093731187e8 seconds
+ arrival date: 2027-06-21T17:29:42.227
+ thrust profile: [0.39360450070362885 -0.2751378427082948 -0.20741868205827443; 0.2049100801344828 -0.029958609842151204 -0.22892782434080608; 0.14256628769210963 0.009743969407202022 -0.24743779156605994; 0.11058101731809578 0.02081003205749549 -0.25291172919137467; 0.07131498596552968 0.020061765952418854 -0.20134417912757346; 0.044314841545830985 0.01592507436277627 -0.14659188019763092; 0.01784809348061421 0.006442012500207772 -0.0681833965071394; 0.009262892911292779 0.0030140541392715196 -0.03692986684592725; 0.025488159174463627 0.007195249500761481 -0.11438668656269343; 0.006281821563553564 0.002444358026296893 -0.03260316883797847; 0.005302141161957858 0.0028782050868719294 -0.03029823450893937; -0.0012231058971121332 0.004998603530352575 -0.0034109163205112377; -0.0009001579770716343 0.0007199462235274034 -0.0006947067206334633; 0.00020498586257759727 0.0015123044240867775 0.0006717879706686814; -0.0016197979173412994 0.0004306286939156116 0.0027532214283311944; -0.00886660106569203 -0.005169099941964978 -0.009974783573591045; -0.004319427659812729 0.00817212096331596 -0.00509862330857711; -0.0012271554880425042 -0.002986978415665208 -0.004924052393863353; 0.008342201921955717 0.006301156434095921 -0.014578578253705208; 0.007011933944360392 -0.010862356613131424 0.0017444352468976604] %
+
+Mass Used: 111.3025812545593 kg
+Launch C3: 99.75313546057558 km²/s²
+||V∞_in||: 0.11548186856869107 km/s
diff --git a/archive/ES_0.5941831582885944 b/archive/ES_0.5941831582885944
new file mode 100644
index 0000000..339574d
--- /dev/null
+++ b/archive/ES_0.5941831582885944
@@ -0,0 +1,22 @@
+archive/ES_0.5941831582885944---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T09:10:33.447
+Launch V∞: [6.959790660503949, -7.152615288462578, -0.8357142444578902] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012726145252335114, 0.06860663874025932, 0.06897734878990783] km/s
+ V∞_out: [0.086637629859042, 0.00935838024942844, -0.044738832328615655] km/s
+ time of flight: 1.2859769624465302e8 seconds
+ arrival date: 2028-06-02T18:45:29.447
+ thrust profile: [0.41768977426602183 -0.16607242065927474 -0.20215194830046404; 0.19680502662130345 0.013232361542022246 -0.22422539463563326; 0.1299856525505042 0.03474026449280414 -0.2347590272880694; 0.0757292297460857 0.029182167855409866 -0.18552785732462768; 0.05251394003487327 0.02458592809045597 -0.1589173967591942; 0.04305415254910575 0.022625028874238735 -0.15297250959851025; 0.03147924543995272 0.017399312865691036 -0.12799876378925662; 0.03867809844696833 0.02369603403907747 -0.16743848296432992; 0.04008833588484199 0.025926609258377573 -0.1898206594891538; 0.0018120116516037402 0.001004565989273658 -0.008535416799502565; -1.2628903831593758e-6 4.6096387267969565e-5 -0.0005191346894994729; -4.389496016151914e-6 8.074164721692451e-5 -0.0004024729098464309; 0.00010161257833555974 0.00019570594491402128 -0.0005388818407094864; 3.055077871179384e-5 4.481844350628827e-5 -2.145457180732931e-5; -0.0004790439146754095 4.879263450110353e-5 0.0003919072360785026; -2.1041710128001315e-5 0.00010525122680820625 0.0005027918889817188; 0.0001441004755893413 0.0003390455987538421 -0.00014922459236543106; -0.0008181953026241775 -0.0007467951172411251 -0.0001750162811528658; -0.00025315887105670774 -0.0008903343394193992 0.0001710198764555561; -0.0014722225857969353 0.00033937629565696154 0.000583204511297867] %
+
+Mass Used: 108.14779416316424 kg
+Launch C3: 100.29700980117643 km²/s²
+||V∞_in||: 0.09811574949163147 km/s
diff --git a/archive/ES_0.5942009620889349 b/archive/ES_0.5942009620889349
new file mode 100644
index 0000000..87f6e0d
--- /dev/null
+++ b/archive/ES_0.5942009620889349
@@ -0,0 +1,22 @@
+archive/ES_0.5942009620889349---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-14T14:53:52.282
+Launch V∞: [5.888449776497493, -7.404857616579212, 0.29657711711654683] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012850525618090124, -0.006139078919664487, 0.014207649223691308] km/s
+ V∞_out: [-0.012658333760111341, -0.005404333136606458, -0.014651756768075246] km/s
+ time of flight: 1.6496876667531085e8 seconds
+ arrival date: 2028-07-05T23:33:18.282
+ thrust profile: [0.8971010058900005 -0.3612570725517416 -0.19515579558736784; 0.5146332341056754 0.10820875361517551 -0.30631794476588753; 0.23142389091640908 0.11921949376154893 -0.22928282793284188; 0.117941984568841 0.08672782387096413 -0.16449483101294032; 0.04455241199120103 0.040997617686823244 -0.0800332532653118; 0.040849396659508805 0.04525706153039011 -0.09128943960339872; 0.03328258995523972 0.04213193197840527 -0.08465340447942768; 0.0217210442657529 0.02968775968568085 -0.06297542670462425; 0.00687103179933509 0.0102295591216046 -0.022028205821749365; 0.0017383901389747289 0.0014248583463145632 -0.0022052818224169274; 0.0009039931806577329 0.0011059395351789827 -0.0026546356253162513; 0.0012634806018541308 0.0018850671250977495 -0.003500710060505724; 0.001558453298229459 0.0005170348498035658 -0.003344769302166046; 0.0007016531689279136 0.001755304228105584 -0.0015115912230505247; -0.00048355065771049535 -0.00031676188593314806 -0.0002446990559841658; -0.0014056214473564489 -0.0005156409590105102 -0.001293343899731391; 0.0005983890716223983 0.0006953870960181579 -0.0008644051341112995; 0.0002297579737709889 0.0003124392678216727 -0.0008604791128037446; 0.00019640193475390822 1.5720836883482427e-5 0.0010479379938517508; -0.0008770664153953309 -0.00224672764051487 -0.0031200332444528333] %
+
+Mass Used: 170.60445114559752 kg
+Launch C3: 89.59371507854169 km²/s²
+||V∞_in||: 0.02011669940886217 km/s
diff --git a/archive/ES_0.5943222753505251 b/archive/ES_0.5943222753505251
new file mode 100644
index 0000000..5bc3164
--- /dev/null
+++ b/archive/ES_0.5943222753505251
@@ -0,0 +1,22 @@
+archive/ES_0.5943222753505251---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T12:19:03.396
+Launch V∞: [7.049967987873092, -6.764985270461756, -0.1711741563186178] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.957086880924596e-6, 5.268478710005971e-6, -2.1263604601065433e-5] km/s
+ V∞_out: [-1.0164179671773654e-5, 1.8515283384193795e-5, -6.447757677315843e-6] km/s
+ time of flight: 1.3552923261163583e8 seconds
+ arrival date: 2028-08-17T03:19:35.396
+ thrust profile: [0.5718262878729239 -0.18720521378177796 -0.19781386970932943; 0.287883048577213 0.05428205548753924 -0.25338589777816284; 0.23669963086189047 0.10445395085912255 -0.328457026940585; 0.18517470133798944 0.1114925821496072 -0.3228213242950982; 0.07387369978155592 0.05523020760768866 -0.18016434511949334; 0.05204780930220573 0.04760226790736798 -0.14756154465511784; 0.010712272640786422 0.01083628965469341 -0.03828485537266677; 0.023262882698321625 0.024939207995180922 -0.08794912328146498; 0.01841472818435396 0.02079643855286581 -0.07725254145733021; 0.009298828469782017 0.011613393727562014 -0.04358294390461181; 0.0005206414114222689 0.00013603286200654656 -0.004186466612830868; -0.006685557233450096 -0.0029471478044540964 0.002541946857679677; -0.00333162848906477 -0.0006766249717515138 0.0009545514444526579; -0.004640574616775468 -0.004582259271693286 0.0041172704761904605; 0.0030312129617031287 0.0011353734589810366 -0.0012978807973549088; 0.00278809290453634 -0.006356099438101502 0.0014746784585631639; 0.004801303058591459 0.0017792354945964516 0.009406758723932; 0.0012533717781996621 -0.003919822287360698 0.011570796559234606; -0.000481780662987994 -0.003453694852760483 0.010149147388738594; 0.0013184919105204613 0.00030781227751469273 0.0004558771433107061] %
+
+Mass Used: 136.31380080916324 kg
+Launch C3: 95.4963749313913 km²/s²
+||V∞_in||: 2.2105250764684248e-5 km/s
diff --git a/archive/ES_0.5943937736503155 b/archive/ES_0.5943937736503155
new file mode 100644
index 0000000..6964814
--- /dev/null
+++ b/archive/ES_0.5943937736503155
@@ -0,0 +1,22 @@
+archive/ES_0.5943937736503155---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T19:00:55.442
+Launch V∞: [5.405345204434152, -8.39581540426038, -1.339982008356526] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.06761818733937937, -0.10031035197925604, 0.01625347995389304] km/s
+ V∞_out: [-0.11415850372713592, 0.038287596840285876, -0.02004974517554302] km/s
+ time of flight: 1.3146041398495483e8 seconds
+ arrival date: 2027-06-22T07:47:48.442
+ thrust profile: [0.2814442244810004 -0.19727431277777838 -0.15029318504309855; 0.1428114095231844 -0.01898779003937858 -0.1593394831680275; 0.1424767304111736 0.009941626373755926 -0.2368382123404071; 0.1164776934716537 0.021789824289087916 -0.2538891528600108; 0.08716088123763657 0.023445373075395622 -0.23158984140690508; 0.057083382099321456 0.019381474255838905 -0.17732800435427176; 0.03121407486915182 0.012992584785223894 -0.11059731612914993; 0.006784230785919465 0.002115876094184599 -0.02589338811994058; 0.017444411306170006 0.007574245702305216 -0.07367673795836253; 0.012733199141891178 0.0068521963543271 -0.05667329002384886; 0.0009532177703154381 -0.0008485045830507728 -0.002468817452801175; -0.0006087476641691221 0.004206743747663104 -0.0014370650610811217; 1.501350638025427e-5 0.0007616797628599917 -0.00318606164562138; -0.002334177563805723 -0.00026188965877517066 -0.008185214614283566; 0.0005247158487685981 0.002141120674330426 -0.0013419953788875653; 0.0017303236690289167 0.003994578933863831 -0.0008178495031128568; -0.002087774802063465 0.008989046872220767 -0.016882862249414935; 0.0025592580551483095 0.0020494987008744516 -0.019386171163250865; -0.0069792146708415655 -0.004874287522341985 0.005854704249928239; 0.00017606281612003467 -7.904208450898215e-5 -0.001371720502722577] %
+
+Mass Used: 101.35842421733423 kg
+Launch C3: 101.50302486423438 km²/s²
+||V∞_in||: 0.12205966403311638 km/s
diff --git a/archive/ES_0.5945231673065475 b/archive/ES_0.5945231673065475
new file mode 100644
index 0000000..bd085d9
--- /dev/null
+++ b/archive/ES_0.5945231673065475
@@ -0,0 +1,22 @@
+archive/ES_0.5945231673065475---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T11:20:59.335
+Launch V∞: [6.877006512028762, -7.082372348277422, -0.8831377801069816] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.8235584641586487e-6, 1.9487574662387404e-6, -1.07067006168044e-7] km/s
+ V∞_out: [-2.069292674715672e-6, 1.2839407731885462e-6, 1.0972824829847972e-6] km/s
+ time of flight: 1.3123532116561559e8 seconds
+ arrival date: 2028-07-03T09:36:20.335
+ thrust profile: [0.6042395199129295 -0.24059021278751616 -0.2894935567848454; 0.15099238971998352 0.009808809605829551 -0.17673653461587907; 0.10872061997525302 0.028310016083342424 -0.20327760516333804; 0.09607640922265072 0.036042622814816495 -0.24148382838706847; 0.056812163069052284 0.02694590283751522 -0.18037871823537938; 0.07234356795658393 0.036778697896216336 -0.2640198068977246; 0.02316555100908181 0.013171741681127091 -0.09748083232958782; 0.020136472308129632 0.010541828898524383 -0.0923274212393552; 0.003145020248435133 0.00039757691285248063 -0.00976356821661713; 0.006851168963233263 0.003039424881108175 -0.041872985712462854; 0.004618928537762431 0.009155800236843717 -0.011135446722807472; 0.004357213666516837 0.005706780382166387 -0.0034233253150308734; -0.0014692910554878111 0.005566259135294694 -0.015151114153883222; -0.0082030456378667 -0.005108620697980969 0.0012739360079574626; 0.013630695880300643 0.023755474149576343 0.002307102607541099; 0.0003876372395977788 -0.007931300599706757 -0.010238895883064985; 0.00027071485227537866 0.0012284897226106503 0.008070170866562348; -0.021403437892916776 -0.025169809773345236 0.0058814671276099725; 0.005704552084572618 -0.013650032265196978 -0.007201951925610772; 0.0016757949315348059 0.0017471601772001259 0.0037692322135945934] %
+
+Mass Used: 120.58365944640491 kg
+Launch C3: 98.23314898478294 km²/s²
+||V∞_in||: 2.671045577715901e-6 km/s
diff --git a/archive/ES_0.5945578847991702 b/archive/ES_0.5945578847991702
new file mode 100644
index 0000000..de0b05d
--- /dev/null
+++ b/archive/ES_0.5945578847991702
@@ -0,0 +1,22 @@
+archive/ES_0.5945578847991702---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T17:01:07.351
+Launch V∞: [6.869477779448048, -7.035081026076903, -1.115189806694935] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005358598711634707, -0.033708264321065724, -0.005022853989147682] km/s
+ V∞_out: [-0.032848731192499654, 0.006510689682389105, -0.008288521386368031] km/s
+ time of flight: 1.2671232767047401e8 seconds
+ arrival date: 2028-05-10T06:53:14.351
+ thrust profile: [0.7053239957714865 -0.2898185226492952 -0.3334301118113054; 0.25515534596797274 0.018026725490442666 -0.28195819395296706; 0.16861925622669166 0.04791562837230195 -0.29397725060774615; 0.11122662774582484 0.046023985748355714 -0.26161205606810045; 0.06143838167044292 0.03113742433060056 -0.18076640247591866; 0.053658800478000895 0.030850232876102404 -0.18454680236225673; 0.018831184589763968 0.011985151902216738 -0.07509432548401176; 0.012637338972618973 0.008490352875736748 -0.05566613759854974; 0.004332926298646975 0.002640202795696034 -0.021765026153557125; 0.0009534724578994236 -0.00019563893505138098 -0.0033423178184190513; 0.0007288234440392253 0.0013239648128779474 -0.007779472840147423; 0.0002396243790132224 0.00030112802579827504 -0.0025919845745754296; 4.218342204400619e-6 0.0005991732642317974 -0.0064750511237870526; -1.94683681401409e-5 -0.0005850901964516574 -0.004029372516697159; 0.0006828489916271094 0.0004238758255084448 -0.0034208307320943133; 0.0014212952463152416 0.0039308287527318585 -0.0016626311912093935; 0.0003334823055520171 0.0018699653436293536 -0.0005146068747766946; -0.0001765276050535074 0.0005236533683379423 0.00024267180395731486; -0.00014153628990523875 -0.00013845195469519458 -0.00010087375393416165; 0.00010038275912824105 -0.0005396181294084321 -0.000989811010022564] %
+
+Mass Used: 122.4173921196334 kg
+Launch C3: 97.92573831075401 km²/s²
+||V∞_in||: 0.03449914094419544 km/s
diff --git a/archive/ES_0.5946647125886267 b/archive/ES_0.5946647125886267
new file mode 100644
index 0000000..17f8c6f
--- /dev/null
+++ b/archive/ES_0.5946647125886267
@@ -0,0 +1,22 @@
+archive/ES_0.5946647125886267---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-17T07:21:46.489
+Launch V∞: [6.367577588268499, -7.0831709083419945, 0.3361212594169347] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.934426859218278e-8, 2.511798858474229e-8, -3.264965523246944e-8] km/s
+ V∞_out: [1.0380714277330518e-7, -2.7774505297052966e-8, 1.3362474098288573e-8] km/s
+ time of flight: 1.856295965153089e8 seconds
+ arrival date: 2029-03-04T19:08:22.489
+ thrust profile: [0.7258968795842917 -0.1847696729986004 -0.10265074169141086; 0.4424206315844121 0.17199466395018218 -0.19771856386105674; 0.16902081993610416 0.13130200571303774 -0.14787006239854397; 0.18043626895772055 0.19012179530494988 -0.20945606779011172; 0.078517489350667 0.10753455579432926 -0.12803951570368227; 0.027499463630528825 0.04712820459013554 -0.06113785774581906; 0.011177923553285061 0.021682387732792217 -0.02950682755367616; 0.0016078885280501995 0.0035256939555137084 -0.005088850312694682; 0.005893360005382827 0.01394471343673791 -0.020142640075674987; 0.0005814230195868483 0.001646609398035615 -0.00234064015493265; 0.001931386336834468 0.0056642645593629375 -0.00893765783106512; 8.345816876242297e-5 0.00013257772331491956 -0.0002546339104865126; 3.9909855646392064e-5 -3.0875087805004022e-6 -8.363856422941487e-5; 0.0001374369720853893 0.00011664917723697626 -0.00014794204423541224; -4.8244167350951694e-5 1.3356342875673938e-5 -9.578731473266594e-5; 4.856621559128674e-5 1.709403590676531e-5 1.3378546754088517e-5; -5.542493784747969e-6 0.000137453042880943 0.0001474665534228906; 0.00021150518249481867 8.7381697603749e-5 -0.0001016253200255684; -9.637757583864974e-6 -7.669034155294887e-5 0.0001438588215496624; 3.513186829794622e-5 0.00026628283148673397 3.3018974496926406e-5] %
+
+Mass Used: 163.93189491753492 kg
+Launch C3: 90.83033196043365 km²/s²
+||V∞_in||: 1.0754625534837612e-7 km/s
diff --git a/archive/ES_0.5947245949623232 b/archive/ES_0.5947245949623232
new file mode 100644
index 0000000..1ed5606
--- /dev/null
+++ b/archive/ES_0.5947245949623232
@@ -0,0 +1,22 @@
+archive/ES_0.5947245949623232---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T21:44:24.057
+Launch V∞: [5.362598515276957, -8.348333643281977, -0.776372250228771] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000292343272592071, 0.00013378748795479046, -0.0002220514637887479] km/s
+ V∞_out: [-0.00012079816263451195, 0.00028284444797555507, 0.0002430750653838161] km/s
+ time of flight: 1.357234687646591e8 seconds
+ arrival date: 2027-08-10T18:42:12.057
+ thrust profile: [0.3280095299905399 -0.19991539142761675 -0.15934243087208166; 0.16862746487337257 -0.008547553126307464 -0.18475952286574093; 0.14154465750414585 0.0237825495458724 -0.2317587372257111; 0.11327972357444105 0.034433170909092654 -0.2429200685137673; 0.08046376511403754 0.03294629838699637 -0.2149705572949485; 0.04266961631948488 0.02095252286614412 -0.14268422678761553; 0.020144256540936652 0.009681395929124419 -0.07779899669325956; 0.052620829402590774 0.025521622870376834 -0.18881751018793927; 0.007289326032762365 0.004233267806853538 -0.023513937638720842; 0.017402853302208626 0.01132790464648803 -0.08264547362270185; -0.001274516750973233 0.0018674403332543795 -0.0037307843393803693; 0.0010236030695100244 -0.005492213430446194 -0.0004632101357039623; 0.0006168222785202409 0.004095192301600111 -0.01216557170119033; -0.0014367800461508324 -0.010622733700613254 -0.005492570752251066; -0.005203650923073251 -0.0017025717076995922 0.00979605801755405; -0.00780967968956735 -0.001041315391581062 0.019567993761741474; -0.0020707176806010223 -0.0033989181810017972 0.007655351510735503; -0.006291442321733949 -0.006156608667478943 -0.037491167912285905; -0.0015217921015313108 -0.0026603615569353077 -0.002419666060023121; -0.0016371156279457884 -0.035150554740405876 -0.033465211238050574] %
+
+Mass Used: 116.02516138462079 kg
+Launch C3: 99.05489132652966 km²/s²
+||V∞_in||: 0.0003907307686039337 km/s
diff --git a/archive/ES_0.5949099006712119 b/archive/ES_0.5949099006712119
new file mode 100644
index 0000000..ad62f29
--- /dev/null
+++ b/archive/ES_0.5949099006712119
@@ -0,0 +1,22 @@
+archive/ES_0.5949099006712119---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T15:30:28.367
+Launch V∞: [6.8097784447331735, -7.269318315791284, -0.6846831333653798] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0014716097077492921, -0.0011050635895581014, 0.0007912399852278299] km/s
+ V∞_out: [0.0009198290047352273, -0.0017883331744697343, 7.982772526631928e-5] km/s
+ time of flight: 1.346531931467243e8 seconds
+ arrival date: 2028-08-15T03:10:21.367
+ thrust profile: [0.48776398905632423 -0.20143865226670263 -0.24901643991366101; 0.08787051120380952 0.0004686166851987147 -0.11844756821071346; 0.09263088408060448 0.014965438883870027 -0.20037869170892247; 0.08498767837969964 0.019853708580835697 -0.24760029960542526; 0.07014254015652653 0.018813163041714296 -0.2528526163867438; 0.04938444936131178 0.013356320369759067 -0.20714839903154908; 0.025851322970824802 0.006768878977941097 -0.12466769081054242; 0.007942466601541232 0.0013487540806366388 -0.041656946196395574; 6.8068522350858e-5 0.004388156858324355 -0.008251811715062134; 0.011440387013274444 0.0023838538477423473 -0.06912495341661422; 0.0018895546477249764 0.002130447600809217 -0.010681997309718853; 0.0026677769136969117 -0.000349751929468184 -0.0052145740954703135; -0.0007381522003818046 -0.0014080489000292554 -0.009898382563403443; 0.0043530340491547284 -0.0027191181422858324 -0.0052221033824253315; 0.0023973671144477656 -0.00020816068853895565 0.010535369133382346; 0.008663396570018732 0.020937511089231472 0.0036847946665282995; 0.006135602883124205 0.005436738410409035 -0.003928023350707845; 0.0026762586401173675 0.0006866196600506159 0.0051620462958029655; 0.035773274470033825 -0.01429831615186297 0.022887096725862636; -0.01674344878322959 0.005912438854248883 0.025428446737603798] %
+
+Mass Used: 112.56652107444415 kg
+Launch C3: 99.68486223576623 km²/s²
+||V∞_in||: 0.0020032127653178355 km/s
diff --git a/archive/ES_0.5949232766163359 b/archive/ES_0.5949232766163359
new file mode 100644
index 0000000..eb66caf
--- /dev/null
+++ b/archive/ES_0.5949232766163359
@@ -0,0 +1,22 @@
+archive/ES_0.5949232766163359---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T21:24:54.192
+Launch V∞: [5.241032464145165, -8.398074244427168, -1.1550699466274361] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000281915212945559, 0.09305022438020114, -0.051880159315280706] km/s
+ V∞_out: [-0.08475110229766643, -0.049481985796061945, 0.04144637462292053] km/s
+ time of flight: 1.3114851710782783e8 seconds
+ arrival date: 2027-06-18T19:33:31.192
+ thrust profile: [0.41570639378448726 -0.27328047236156733 -0.2166583541150133; 0.21833069307695482 -0.02325496414994115 -0.2400054438801901; 0.16879921044956395 0.018077356615803595 -0.278806373722169; 0.12513509281841692 0.029181064742764922 -0.2714974970099794; 0.07067383626880577 0.02273844261450825 -0.19040659600650814; 0.031632997021400336 0.012519421965642059 -0.10372793921100665; 0.028421004697717477 0.012674025085451509 -0.10309752616205997; 0.014306160485578905 0.006768229017344902 -0.0640962299682167; 0.01319105508649567 0.00815479137108106 -0.06516321000513069; 0.01598364139440984 0.00813322796651096 -0.06947432215006837; 0.003949855888811072 0.002348601256293204 -0.0008355389989130623; -0.0011026573827573245 -0.00042231213321676454 0.002946262445421586; 0.002329741636711755 0.001363335047459979 -0.00037054026801198623; -0.0005945677427031297 0.0018915838258039908 -0.0010265337079757137; -0.0013172620641172437 -0.0005256025713056387 0.005773115651928691; 0.00022850472939139343 -0.004094733568085619 0.007049792900521078; -0.005471882551307763 0.0009524227495198857 0.0077760650298697425; 0.002561776902741762 -0.011836806005456498 0.008094480184360937; -0.005348442844669874 -0.0004986693878490064 0.01153134822086426; -0.010635224179371277 0.001594450041473245 -0.0023906110370650155] %
+
+Mass Used: 114.65064587976303 kg
+Launch C3: 99.33025888673639 km²/s²
+||V∞_in||: 0.10653625985537493 km/s
diff --git a/archive/ES_0.5950697628482039 b/archive/ES_0.5950697628482039
new file mode 100644
index 0000000..7b4f82e
--- /dev/null
+++ b/archive/ES_0.5950697628482039
@@ -0,0 +1,22 @@
+archive/ES_0.5950697628482039---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-14T08:10:17.559
+Launch V∞: [6.334629040071359, -8.225235995280448, -0.5048257124509161] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004657970625391244, -0.0002187547810844129, 0.0005609035311246854] km/s
+ V∞_out: [-0.0004944820355904124, -0.00020440314248796335, -0.0005433588686863161] km/s
+ time of flight: 1.874957778597082e8 seconds
+ arrival date: 2029-04-22T10:19:54.559
+ thrust profile: [0.005928217115823312 -0.0034977695294723513 -0.004321176958493136; 0.011148735514665494 -0.007271290950533603 -0.025002215623986412; 0.019356095759573734 -0.020190067825943656 -0.07520407466867006; 0.014398741223296138 -0.01996347093742039 -0.07321053519346798; 0.038280803082199326 -0.061835486096886515 -0.2189426104442483; 0.010619160976707563 -0.01911065937199848 -0.06884907777673895; 0.009553952185973788 -0.01817863037515052 -0.0646254687431009; 0.010691258594110523 -0.021691036921891338 -0.07722997065941888; 0.012872327158798448 -0.0260348337446231 -0.08921193112486484; 0.008649978298117445 -0.017823198094542254 -0.06260435811183243; 0.0013149870369926707 -0.001721281963932007 -0.007814318995354765; 0.0012489001136268899 -0.0015451221046815676 -0.007441727756241013; 0.0017757453331341646 -0.0019376795453361364 -0.0023146048356540256; 0.0006204161666235544 -0.00017650288000368563 -0.0037604527978113873; 0.0012896297366036434 0.00023454574611893038 -0.0074387073406977046; -0.002903284530310749 -0.0019587202468156935 -0.005417805651424766; 0.0010914927257959974 0.0010081656079203162 -0.0037905033590119623; 0.0022855327907227254 -0.003323614090749609 -0.002256721738922662; 8.363910716255275e-5 0.001134989243864364 0.00046248940260630155; 0.0034026106705841224 0.0031463814203988427 -0.0030085650818880098] %
+
+Mass Used: 64.03291601184719 kg
+Launch C3: 108.03688125332411 km²/s²
+||V∞_in||: 0.0007612051818961215 km/s
diff --git a/archive/ES_0.5950836735429921 b/archive/ES_0.5950836735429921
new file mode 100644
index 0000000..3ec4843
--- /dev/null
+++ b/archive/ES_0.5950836735429921
@@ -0,0 +1,22 @@
+archive/ES_0.5950836735429921---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T18:40:48.678
+Launch V∞: [6.570969343649459, -7.005286888262635, -0.87384344856414] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1767774797679523e-7, 7.41246934022116e-5, -6.453231105765377e-5] km/s
+ V∞_out: [-4.8482130262974704e-5, -8.34499015146955e-5, 1.8142137866945707e-5] km/s
+ time of flight: 1.8749577787468815e8 seconds
+ arrival date: 2029-03-28T20:50:25.678
+ thrust profile: [0.7233544849173715 -0.16720361144578724 -0.1569517634380552; 0.17386767325823071 0.07443148053178504 -0.11817868173606151; 0.11481941201131841 0.0930262631116215 -0.13227278659950617; 0.19035625227628447 0.2104827986048239 -0.2834396678593243; 0.06320067634016147 0.09173830219813854 -0.13697213856546983; 0.03687408535434103 0.06514380007133147 -0.10269352780892198; 0.013422746103365277 0.027743837196593304 -0.046888901458362095; 0.012095508318115275 0.02924112291537583 -0.05072816237301822; 0.00414025137742399 0.011642212942128664 -0.020852352998882974; 2.261089424384173e-5 0.00016804502348990717 -0.00032043131721111245; 0.0004277743142633861 0.0014053865150177455 -0.002703679239528404; 0.00010380485548396267 0.00018097073542271356 -0.00012599183767992016; 1.723324532796348e-5 6.990640376372122e-5 -0.0004310413141171654; 7.777891062441767e-5 -0.00019903401246268361 -0.0001800118292059585; 3.936087840195176e-6 0.00010558859864524794 -2.6483804946032298e-5; 0.000251168229980817 0.0003337162718486203 -0.00029684263289811636; 0.00037105961568284 0.00035990030515868296 -0.0003178879023390724; 0.00011363639012155249 8.717295394627481e-5 -0.00029994961922380736; 0.0002505311927190137 -0.00026174934423593926 0.00027780649801057507; 1.6597124952071856e-7 -4.341718414241357e-5 9.74019250509885e-5] %
+
+Mass Used: 151.67512403140154 kg
+Launch C3: 93.01528487464387 km²/s²
+||V∞_in||: 9.827988973343233e-5 km/s
diff --git a/archive/ES_0.5950873272306814 b/archive/ES_0.5950873272306814
new file mode 100644
index 0000000..6c84f9c
--- /dev/null
+++ b/archive/ES_0.5950873272306814
@@ -0,0 +1,22 @@
+archive/ES_0.5950873272306814---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T02:03:18.064
+Launch V∞: [5.090267173313352, -8.353082632733752, -1.0569531543947648] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.609382630001616e-5, 1.0536146903114536e-5, -2.197691424951296e-5] km/s
+ V∞_out: [-2.078035498740908e-5, -1.8363406702493447e-5, -9.09735309777092e-6] km/s
+ time of flight: 1.3019759502743064e8 seconds
+ arrival date: 2027-06-08T00:03:13.064
+ thrust profile: [0.7017384188284962 -0.4721624908798447 -0.36179124264389256; 0.22003757074643038 -0.02899414229738172 -0.24330451348141424; 0.10208157808046613 0.007177970364539154 -0.17111948141106187; 0.08456065166898062 0.015863695723201524 -0.18500874292835195; 0.08622873242341877 0.022945758780129808 -0.22746676477884933; 0.06876614555855895 0.022123658554953955 -0.2100490899737593; 0.01906161419375614 0.007054136162734147 -0.06717363776408819; 0.03417292064073816 0.01381510106959681 -0.12941986854896637; 0.0038300464516790077 0.0006226095003240219 -0.01955383993417543; 0.00434952552815527 -0.0032836581709765043 -0.021272419268462503; 0.0018594262285659196 -0.00021756315274225162 -0.014937723505245684; 0.004411362596379011 0.001708335808645344 -0.012953237730027265; 0.006136184497856283 0.0012012535557659153 -0.027977443568746718; 0.01664740071612785 0.004174780575169212 -0.015823795301086373; -0.0020904521817622064 -0.0005069306186709325 0.0043562399474371205; -0.0009607186746955008 -4.7404131656434475e-5 0.0019233729676209066; 0.002503482237466637 -0.0057032715879500664 -0.0033851906361304276; 0.000615202884347989 -0.0031335977376583616 -0.00897645701898867; -0.0031690385231792767 -0.001258639220228497 0.004257159512146717; -0.0002291292680820209 0.0003205415483476127 -0.023930196320259556] %
+
+Mass Used: 129.59045231160871 kg
+Launch C3: 96.80195933557478 km²/s²
+||V∞_in||: 2.9206273238288167e-5 km/s
diff --git a/archive/ES_0.5952010574956446 b/archive/ES_0.5952010574956446
new file mode 100644
index 0000000..795d834
--- /dev/null
+++ b/archive/ES_0.5952010574956446
@@ -0,0 +1,22 @@
+archive/ES_0.5952010574956446---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T06:40:06.780
+Launch V∞: [7.127614416730511, -6.810610163635551, -0.052485989059423886] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.2549583324191145e-6, -2.090453090151052e-5, -1.2287459917686518e-5] km/s
+ V∞_out: [-1.803243053218878e-5, 1.4967275133289028e-5, 9.368098207537498e-6] km/s
+ time of flight: 1.445878270250646e8 seconds
+ arrival date: 2028-12-04T17:57:13.780
+ thrust profile: [0.3217400662671566 -0.09350977776289462 -0.12973359371789195; 0.15296311760043566 0.027763833133805458 -0.1563021641754511; 0.1364960709386313 0.05638595557729807 -0.22010511731802873; 0.12212859987513972 0.07078223025584947 -0.2767969386187854; 0.0958820516155292 0.0681668609646376 -0.2802950255119349; 0.04481652275839624 0.03597370434331885 -0.16141485078469803; 0.024667634397208354 0.02072365665243097 -0.09937734753897624; 0.004357572108181913 0.0005718700928754529 -0.02391888707907248; 0.003074990525094739 0.005087747256157774 -0.00711245960008755; 0.010015961923983683 0.02694508333194178 -0.03263776689454961; 0.0323953150319235 -0.002954606973658538 -0.03610799127949517; 0.0026114384463291444 0.002153684857765456 -0.019775739351124363; -0.034402626053980624 0.007220465135049346 -0.012035147914345295; -0.019461675821778646 -0.01137225549178269 0.005977251620747548; 0.017044309684760662 -0.022015634034093946 -0.0008746388601200759; 0.06438362342949096 -0.02327397917516657 0.01235683983891152; 0.015141796540454099 -0.003929415739835258 -0.008776086940869355; -0.008292796950983868 -0.009476390953203526 0.03509463351864552; 0.054204985919651213 -0.05063028031220439 0.0787366509585106; 0.0005480998615516668 -0.010239654627426735 -0.005219435438993147] %
+
+Mass Used: 127.4592587653051 kg
+Launch C3: 97.19005285364804 km²/s²
+||V∞_in||: 2.5310383320805287e-5 km/s
diff --git a/archive/ES_0.5953191438748493 b/archive/ES_0.5953191438748493
new file mode 100644
index 0000000..e3b7839
--- /dev/null
+++ b/archive/ES_0.5953191438748493
@@ -0,0 +1,22 @@
+archive/ES_0.5953191438748493---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-22T09:39:00.957
+Launch V∞: [7.438031825209451, -7.075420463901206, 0.5708059600810373] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1000408651148465e-8, -7.1672920231840554e-9, 5.9985997235939285e-9] km/s
+ V∞_out: [-4.790732990827385e-9, -9.806070497129114e-9, -3.220362547535419e-10] km/s
+ time of flight: 1.7302421641725045e8 seconds
+ arrival date: 2029-11-14T23:55:56.957
+ thrust profile: [0.13833754946681262 -0.029130934101461232 -0.06673455221913402; 0.026788935774498798 0.0013051549713919554 -0.04343232038707069; 0.051058452052430564 0.004900384009453241 -0.13111772511721512; 0.05624887917441935 0.004195620796145116 -0.18997351699702666; 0.04633020913234402 0.0005704044208760369 -0.19016142442847056; 0.029783898486519602 -0.002425127598773673 -0.14306423589438172; 0.0192819411035022 -0.0033868320977372673 -0.10351205334936364; 0.008569191577526423 -0.001994840578136331 -0.04635417872904315; 0.0032097066560042376 -0.0011784599081872207 -0.02033144509660351; 0.00389112552480151 -0.0013842131526036069 -0.02213834026868258; 0.002035506267029393 0.00012350902977195438 -0.012669083213594026; 0.000320249780993379 -0.0011757308145596 -0.005605289610042788; 0.0016441374692380357 -0.0014847472987589388 -0.0030549891780773716; 0.0006774925665722039 -0.0006046957430592445 -0.0004631778038135737; -0.0002804548806291634 0.0023532873899775215 0.004471606839477712; 9.612670197192309e-5 -0.0011509591409819885 -0.0010695352066484652; 0.002962067419985674 0.001866581766113899 0.00404897042171797; -0.0009522065089301919 0.002740143601766911 0.0050580610386123355; -0.0007706318790306407 0.0033583258540856196 -0.001661805674808765; 0.0008638630173857776 -0.0004160315589168078 -0.0012892562809561684] %
+
+Mass Used: 77.88735008299727 kg
+Launch C3: 105.71171161788462 km²/s²
+||V∞_in||: 1.4434758885473665e-8 km/s
diff --git a/archive/ES_0.5953289083397839 b/archive/ES_0.5953289083397839
new file mode 100644
index 0000000..32a1f97
--- /dev/null
+++ b/archive/ES_0.5953289083397839
@@ -0,0 +1,22 @@
+archive/ES_0.5953289083397839---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T08:29:41.342
+Launch V∞: [6.829135561580384, -7.150150659571372, -1.110846905842727] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004998194889673123, -0.027979322210256594, -0.028560691439682612] km/s
+ V∞_out: [-0.03427320550719938, -0.004302867733996686, 0.02068426756227076] km/s
+ time of flight: 1.265972465183682e8 seconds
+ arrival date: 2028-05-10T14:23:47.342
+ thrust profile: [0.6718324051930901 -0.28888916136405374 -0.33517396568902774; 0.17628944231196336 0.007093305474476398 -0.20931112283885392; 0.1526362393156711 0.0361019142552571 -0.2834871953146502; 0.08775768444127639 0.030970879512233093 -0.2231789538951412; 0.07301382988576835 0.031255040821917844 -0.2280393594771722; 0.04444182051780962 0.021558296913548776 -0.16540007029428214; 0.02059485969720806 0.010790339727201427 -0.08745360782485355; 0.010316119305502747 0.00571186938534855 -0.048263076854387875; 0.002875828259234113 0.0018760206961437882 -0.014331609127726392; 0.010177768164920154 0.006066746133244101 -0.058605453724421344; 0.0018133046838529553 0.0010122266794396733 -0.009413112145602557; 0.00043119957074794386 0.0012834718608794285 -0.00706417538392598; 0.0006582469124956726 0.00128489521335043 -0.002479798697069144; -0.0011406155205644824 -0.0018816015334047953 -0.0029351158673162027; 4.424531857069895e-5 -5.585593351584866e-5 -0.0021584581030374152; 0.0012353964077840831 0.0002149552648740647 -0.0011891684469379701; -0.0010656789619169172 0.0022073079870184665 -0.00044873656194306926; 0.000826089884371842 -0.0031394672668208956 0.0004462196238346125; -0.003705257555315293 0.007100063957835121 -0.01083443675495236; 0.0007857073955533163 0.0016463935082297503 -0.002597419316006469] %
+
+Mass Used: 117.0753141058999 kg
+Launch C3: 98.9957278212311 km²/s²
+||V∞_in||: 0.04029314481414018 km/s
diff --git a/archive/ES_0.5955587301122375 b/archive/ES_0.5955587301122375
new file mode 100644
index 0000000..8a53df6
--- /dev/null
+++ b/archive/ES_0.5955587301122375
@@ -0,0 +1,22 @@
+archive/ES_0.5955587301122375---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T17:21:48.518
+Launch V∞: [6.993285930553688, -7.218330266148821, -1.6155843043455236] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005263392391950906, -0.001173008593258874, -0.0007050502960261097] km/s
+ V∞_out: [-0.0012027895075062097, 0.0007482847284586742, 0.0003972296809138844] km/s
+ time of flight: 1.2874126791304106e8 seconds
+ arrival date: 2028-06-05T18:49:35.518
+ thrust profile: [0.3257543572999228 -0.13460035270834425 -0.1702419506051774; 0.10027845455859656 0.005112200728452351 -0.12721786404446916; 0.09126111512409897 0.022692209991838953 -0.1815079929310063; 0.07766567040839806 0.028313640234013993 -0.20758333881658192; 0.04946923371542896 0.02191019983027581 -0.1667482955682678; 0.025460943206235234 0.012433268809865845 -0.10442970238243793; 0.015775088110777446 0.007487882919672221 -0.0646151430596309; 0.055817079282999484 0.024024450579242247 -0.25894488808264243; 0.010393980409831903 0.004963517315526232 -0.05919319528629673; 0.0057700381702585615 0.0025864885794241706 -0.03502863944193692; 0.00383109013663747 0.0013424641716865784 -0.021760757415947053; 0.0014301699803086966 0.0031688162386442737 -0.005986695863816893; 1.3126458921225046e-5 -0.0013299135570439605 -0.004047223764295886; -0.0034713811315452633 0.004114681597051255 -0.0011539699076694929; 0.0018557912059463076 -0.00038958282766286215 -0.004099490001894453; -0.004686363679004944 0.0011114928434276551 0.006199089250370927; 0.00031632414805722906 0.0006087749031789807 -0.0027102838021167822; -0.0006692843826136274 0.00020901373688195392 0.001178927311865965; -0.0019969524217108487 0.0024775876597860793 0.0020463717916606007; -0.00486497181956858 0.004587906066423983 0.007364904333546588] %
+
+Mass Used: 90.36587840186439 kg
+Launch C3: 103.62045258212788 km²/s²
+||V∞_in||: 0.001466314452804082 km/s
diff --git a/archive/ES_0.5956723706813029 b/archive/ES_0.5956723706813029
new file mode 100644
index 0000000..0711e5f
--- /dev/null
+++ b/archive/ES_0.5956723706813029
@@ -0,0 +1,22 @@
+archive/ES_0.5956723706813029---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T23:10:19.860
+Launch V∞: [6.825388881950522, -7.085797726008605, -0.8430980080788211] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.2660360795590416e-6, 8.628259695290288e-6, 4.403549727144423e-6] km/s
+ V∞_out: [6.792186344671509e-6, -6.548246702318261e-6, -3.924543753009015e-6] km/s
+ time of flight: 1.2594173937972498e8 seconds
+ arrival date: 2028-05-01T14:59:18.860
+ thrust profile: [0.7157198614285645 -0.29593050426262424 -0.3269235880624811; 0.2789842082527448 0.018922750182891093 -0.29463975299664086; 0.15889237567603842 0.04511564087955214 -0.2713820744242524; 0.11690435023039154 0.04827575762964935 -0.26656119096783215; 0.05705198361587375 0.028089105779735352 -0.16256379881620828; 0.056425098315272294 0.03163865391415634 -0.18644939249966583; 0.040894923653830705 0.024743228136761653 -0.15302776493157158; 0.020817553410329388 0.013389513474436074 -0.08621415206573264; 0.0043572428793530234 0.0028841913329038854 -0.01955646025481836; 0.0006654051279549227 0.00038768239278871885 -0.0030313983982689836; 0.000607271033576677 0.00019243345612164213 -0.0014306251367948181; -0.00021349803653264015 0.00029779866028681367 -0.0015128100154990335; 0.00020690158779687362 0.00035263830875700966 -0.0009489043592325753; -0.00020579073107682708 0.0012126659443711563 -0.0007343233928336816; -3.029167079783373e-7 -0.0006344385281962907 -0.00043767805404016616; -0.00048260307156927987 3.759732003167386e-5 -0.0005869118609781135; 0.0013948307576220008 0.00018301325324260426 -0.0003534388640075769; -3.5772022182533e-5 0.0006659541868153723 -0.0009879384998670317; -0.0002612742328503597 -0.00014717855853141223 7.2981505668388e-5; 0.000170095730199924 0.0003863507497613637 -0.000842617230245494] %
+
+Mass Used: 126.17031630741758 kg
+Launch C3: 97.505277054989 km²/s²
+||V∞_in||: 1.0222773950439576e-5 km/s
diff --git a/archive/ES_0.5956779740327541 b/archive/ES_0.5956779740327541
new file mode 100644
index 0000000..6b0a78a
--- /dev/null
+++ b/archive/ES_0.5956779740327541
@@ -0,0 +1,22 @@
+archive/ES_0.5956779740327541---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T12:45:57.326
+Launch V∞: [6.931178881646875, -7.184050701574216, -1.0707622405583332] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0031753988019572106, 0.005091084794469405, 0.001879513884764942] km/s
+ V∞_out: [0.002556059224481238, -0.003346658451898492, 0.004666125295852059] km/s
+ time of flight: 1.2660565602652285e8 seconds
+ arrival date: 2028-05-10T21:00:13.326
+ thrust profile: [0.4936043487221016 -0.2065410177813583 -0.2334647261394002; 0.15360243489770858 0.006587960907226349 -0.17386438621972053; 0.10138111607772402 0.023990337929965994 -0.1811813036332727; 0.10934570035613377 0.038797169977259495 -0.2569411311543819; 0.05137480451950326 0.021362522508806946 -0.15216188369907346; 0.03381419450156962 0.019908402427384123 -0.11306972969231292; 0.09509357019051752 0.054351115520474225 -0.39104314155598874; 0.012417920618084242 0.0069416107901697326 -0.05379330409508974; 0.005937648444712911 0.0038822117532931123 -0.02924376827747681; 0.004781140176118514 0.003074648993147421 -0.028672447458791026; -0.00020165691120426952 0.001016231622972486 -0.000455168401465751; 3.11485822549172e-5 0.00043926650425164603 0.00012613495921237486; 0.00046704922605625383 -0.00032913510589327607 0.0001678403719735477; -0.0012606716846038602 3.769923014626452e-5 -0.00032559300151269166; -0.0013882923541625569 0.00041360493700722954 -0.0006023436369237599; -0.000453758247195053 -6.136380401391178e-5 0.0007376703551857617; -0.0008384008436871993 -0.0005834500384074164 5.284681913666654e-5; -3.750427799256321e-5 -0.0005058479412578831 0.0015986376766306144; 0.0003799085195402156 -0.00040114438343813897 0.0006556146363569449; -0.0010560091906396743 -0.0010949113452212017 0.002313230499873805] %
+
+Mass Used: 106.96722084165094 kg
+Launch C3: 100.7983569479821 km²/s²
+||V∞_in||: 0.0062876763894918345 km/s
diff --git a/archive/ES_0.5956948006011608 b/archive/ES_0.5956948006011608
new file mode 100644
index 0000000..d06bb04
--- /dev/null
+++ b/archive/ES_0.5956948006011608
@@ -0,0 +1,22 @@
+archive/ES_0.5956948006011608---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-16T14:17:21.954
+Launch V∞: [6.247262106428834, -7.057645591877084, 0.3924711871828387] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7097148838168694e-7, -3.7577380176221295e-8, 4.831556305530027e-8] km/s
+ V∞_out: [-1.617328717948557e-7, 5.01593663159963e-8, -6.670053903543956e-8] km/s
+ time of flight: 1.8130995966007408e8 seconds
+ arrival date: 2029-01-13T02:10:00.954
+ thrust profile: [1.0 -0.28688397345811323 -0.1801852422214826; 0.3567436200480765 0.12241345855665 -0.20181221072794409; 0.22016390801452984 0.15082928657100594 -0.2082889392088262; 0.13290025585475293 0.12751541694556426 -0.17812299347157293; 0.057413135289341846 0.06985719377512374 -0.10319767421124856; 0.020294765400264373 0.029055481635404928 -0.04717330658245772; 0.0018690072835466753 0.005238115935663572 -0.008755844694394832; 0.0029956977456323934 0.00372802165385207 -0.007621095233336588; 0.015794606871839055 0.03657246009539222 -0.06408760803572328; 0.0008097499524907473 0.0037524714767616456 -0.00898590283272459; -9.76517693633095e-5 0.001390434351436343 0.00456561966037099; 0.0006379142201982441 0.001379047517075781 -0.0022841696133755873; -0.004564809053723797 -0.003837477822473053 -0.005896043139015926; -0.0003766663536321575 -0.00047057683839060466 -0.0022021717465478515; -0.004534708520879539 0.0038583128498449835 0.0016761064478543644; -0.001235294939456667 0.0005164606527116246 -0.0024659419245934523; 0.005232766908905466 0.0035271292645891036 0.007229315902151304; 0.00018317532147543942 -0.0005285880025094104 0.0006545394937069475; 0.00032765079532586676 0.004164415288075093 -0.006931794977578011; 0.005727809793337908 -0.008044900785165055 -0.004593776300059459] %
+
+Mass Used: 175.8533079362487 kg
+Launch C3: 88.99267875973237 km²/s²
+||V∞_in||: 1.815976403307826e-7 km/s
diff --git a/archive/ES_0.5957003959757823 b/archive/ES_0.5957003959757823
new file mode 100644
index 0000000..6191823
--- /dev/null
+++ b/archive/ES_0.5957003959757823
@@ -0,0 +1,22 @@
+archive/ES_0.5957003959757823---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T00:38:57.510
+Launch V∞: [7.669223438723989, -5.598481207010977, 0.8058147660006377] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0032741701683695864, -0.0022470395006127784, -0.0001454984999460818] km/s
+ V∞_out: [0.002865224241655093, 0.0013370604018347945, -0.0024025270181138934] km/s
+ time of flight: 1.844155094751959e8 seconds
+ arrival date: 2030-03-04T11:10:46.510
+ thrust profile: [0.7726694046942043 -0.00897137409497115 -0.059002831839060355; 0.37289367985603183 0.2623687475452811 -0.13647174154380012; 0.13192400172281982 0.17181498362846082 -0.09979904914277228; 0.08195593610522277 0.15108345919749747 -0.09625430926806403; 0.08240455312482832 0.2060216147762746 -0.14294291487294472; 0.03880302145181413 0.1321108691382824 -0.10026820940073945; 0.011440000851109565 0.04913947960750074 -0.04070912706157649; 0.009333958896470084 0.04435297927194687 -0.03730643053497973; 0.0002086274581818504 0.0007929552155788145 -0.0006795799851012982; 0.0001011647406669015 0.0007356664826011221 -0.0008246041996673386; 0.0003011379769227358 0.0012510983593228297 -0.0005344938939987519; -0.00022497042112798736 0.0005994144628635439 -0.0006464416880702709; 8.372085621103395e-5 0.0001895004580354518 -0.00025312567431622383; 5.841237934479655e-7 0.00019568139983730504 -0.00012556595567981887; -9.807960136387685e-5 -2.7313120425038134e-5 -2.8652802940011784e-5; -0.00025546018773121317 9.554701847480174e-5 -0.00025527810259686466; 2.2687249962074986e-5 4.37178911124745e-5 7.133206892231709e-5; -9.669774472691021e-5 -0.00012229901177496683 -6.397443395422811e-5; -5.205974675566709e-5 -7.740144511653404e-5 0.00014146427923982085; 0.0002861780676577276 5.028791157686135e-5 0.00024920060720160257] %
+
+Mass Used: 165.26277704838594 kg
+Launch C3: 90.80931741543316 km²/s²
+||V∞_in||: 0.003973732077309945 km/s
diff --git a/archive/ES_0.5959455358507482 b/archive/ES_0.5959455358507482
new file mode 100644
index 0000000..577f2a7
--- /dev/null
+++ b/archive/ES_0.5959455358507482
@@ -0,0 +1,22 @@
+archive/ES_0.5959455358507482---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T08:44:44.153
+Launch V∞: [5.0682157916778605, -8.718254454961702, -1.4698677690901343] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.425449414577252e-6, -3.897833383235377e-6, 7.875218988193161e-6] km/s
+ V∞_out: [7.2392709502544506e-6, 6.618814431517102e-6, 3.2407942571113223e-6] km/s
+ time of flight: 1.3378058528996277e8 seconds
+ arrival date: 2027-07-24T18:01:09.153
+ thrust profile: [0.3070669990449886 -0.2267254287532432 -0.2033169395614772; 0.053394192184164725 -0.01297330747850261 -0.07891343619738905; 0.06262641058208886 -0.006818168624053732 -0.14476543240531578; 0.07000462816649453 -0.004089960644571232 -0.21805589786825028; 0.06220842105878026 -0.0023591885601685807 -0.23960390836508214; 0.03928428344217824 -0.0009975618551525667 -0.1766457671794588; 0.024291268216188606 -0.00021804074905566512 -0.12426734231889527; 0.007438477366299939 0.00013661773074031023 -0.04277747654792876; 0.00537074953980116 0.00019922667310537384 -0.0330009235632911; 0.010147861356360964 0.0010648896203309288 -0.057602029655171076; 0.0021831692379525964 0.002920189507492962 -0.005478751998554491; -0.00033121785157278567 -0.00582681743778468 -0.003604101857836982; 0.0005536131786905143 -0.0002698624942858622 -0.001870442768821797; 0.004253451375196143 -0.0017743101863321913 -0.002212353037765446; 0.003246401644065232 -0.0005529694025896562 -0.0009694132586180047; 0.002096798603057738 -0.008501700890910971 -0.006657228598957307; -0.003885466096574146 0.010922397567382084 -0.007049953465481948; 0.005570349264205668 -0.006648172140235055 -0.0023366571427929717; 0.006077080152926502 0.0014968633821158617 -0.007905378212664141; 0.001220017135600339 -0.0015982342164947596 -0.005094189870033527] %
+
+Mass Used: 89.44730584455874 kg
+Launch C3: 103.85528331108243 km²/s²
+||V∞_in||: 1.032703638734748e-5 km/s
diff --git a/archive/ES_0.5959841937393395 b/archive/ES_0.5959841937393395
new file mode 100644
index 0000000..e9fef01
--- /dev/null
+++ b/archive/ES_0.5959841937393395
@@ -0,0 +1,22 @@
+archive/ES_0.5959841937393395---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-28T18:57:27.811
+Launch V∞: [7.063018999440516, -6.586553923567343, -0.8548593939619805] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.975706547105286e-6, -3.4865332954194145e-6, 2.595191168683858e-6] km/s
+ V∞_out: [-7.424958706229598e-7, -5.834004094929282e-6, 2.6784583625856384e-7] km/s
+ time of flight: 1.382374013422373e8 seconds
+ arrival date: 2028-09-14T18:14:08.811
+ thrust profile: [0.7412123742662655 -0.22443541926248053 -0.2245675337665; 0.4067520755029994 0.10338121540822348 -0.3151497947929597; 0.2324893882321524 0.12763080450055866 -0.2947920935409859; 0.19559727479773906 0.14906259317800044 -0.33356744867887084; 0.06038626789735257 0.0563275690803408 -0.13896036523881805; 0.03321141796935336 0.03566823062633622 -0.09254908651603637; 0.034455671283817324 0.04167354049849755 -0.11037544823571624; 0.010340348749791159 0.014560815910299228 -0.041650111489499445; 0.014026962242130785 0.02005207466937086 -0.054666888680186335; 0.003167960354032383 0.004465981991209341 -0.013454679121067006; 0.0005621560207995576 0.0003070414323871818 -0.0018317325846660213; 0.0012614513295488585 0.00204972620635454 -0.006364100425539747; 0.00022800959859121158 0.0009396928410749 -0.002482930491497593; 0.00022819200745308337 0.0005573983489872751 -0.0007380139582821494; 0.0002017504455961586 3.487532733947819e-5 0.00017653262827932838; 0.0005055646390369833 0.0012185233840694364 -0.002499857113487604; -0.00013322350743593693 -0.0015175467284510294 0.0002253580683559029; 8.754514350499144e-5 -0.00019074763462704689 -0.000869186826489848; 0.0009249596983722796 0.000724810223333947 -0.00011963997772142053; 2.779278879003731e-5 3.261789278595083e-5 -0.0001287374142690651] %
+
+Mass Used: 146.98322444111136 kg
+Launch C3: 93.9997145579631 km²/s²
+||V∞_in||: 5.89043072879893e-6 km/s
diff --git a/archive/ES_0.5960141234672478 b/archive/ES_0.5960141234672478
new file mode 100644
index 0000000..9804ae0
--- /dev/null
+++ b/archive/ES_0.5960141234672478
@@ -0,0 +1,22 @@
+archive/ES_0.5960141234672478---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T02:23:53.443
+Launch V∞: [7.046437092063469, -7.2089757064785935, -1.4627978796753067] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006448973518255781, -0.020174682589153503, -0.038239910937294924] km/s
+ V∞_out: [-0.03767383172207147, -0.0044000616609133425, 0.021729337090181385] km/s
+ time of flight: 1.286697762289087e8 seconds
+ arrival date: 2028-06-04T08:00:09.443
+ thrust profile: [0.18801501825975872 -0.07786972044415982 -0.0908831566768427; 0.12734002713724377 0.005703674517571738 -0.1408405632125048; 0.13264570194687947 0.030913500380285192 -0.23016879631353426; 0.11252264236131002 0.0379704250403839 -0.26392666942395304; 0.10520010649022447 0.03772129905812393 -0.26272717010572727; 0.05034916954835846 0.022946430597639338 -0.17146128369212008; 0.012418721209206248 0.007644175862733411 -0.052700107089156734; 0.0024133494060696896 0.002260598527558651 -0.01989047189095842; 0.012396811843070411 0.008047390021348215 -0.061372383452868884; 0.003924925187727372 0.0016444559076790389 -0.021411671560993772; 0.011956402218220138 0.008518647812124493 -0.06471900939622877; 0.002427809140295817 0.0004578024657071742 -0.013648328959553022; 0.004501987614946074 0.00478147524178411 -0.03474277341539879; -0.00292260058311565 -0.00022203500197910653 0.00558380671180967; -0.0032197537132039574 0.006568369227467345 -0.00714385187973331; 0.0027960908783311628 0.0010346462552707665 -0.00011948166671842033; 0.0029195669180241786 -0.0041566378066607125 0.005956122620854722; 0.001186770820018939 -0.0022657314133435187 0.0020820334349927368; -0.0074690572942339925 0.009299358671505852 0.0048070782775263875; 0.0008398794305224432 -0.0008473456076799646 0.0036170972133223985] %
+
+Mass Used: 90.07507032802005 kg
+Launch C3: 103.76138406578899 km²/s²
+||V∞_in||: 0.043713817786879536 km/s
diff --git a/archive/ES_0.5960339108989462 b/archive/ES_0.5960339108989462
new file mode 100644
index 0000000..7df9cee
--- /dev/null
+++ b/archive/ES_0.5960339108989462
@@ -0,0 +1,22 @@
+archive/ES_0.5960339108989462---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T10:25:17.867
+Launch V∞: [5.219458158334036, -8.386402483313827, -1.028222411827361] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.1504923931839651e-5, -5.88993516207493e-6, -1.0949439229080734e-5] km/s
+ V∞_out: [7.64896736294576e-6, -1.0025520050228373e-5, 1.1312592470542966e-5] km/s
+ time of flight: 1.2951884212536103e8 seconds
+ arrival date: 2027-05-30T11:52:39.867
+ thrust profile: [0.4552214523375577 -0.3005738715043063 -0.22745876654870428; 0.3210302919769732 -0.04169424764638085 -0.3373897563642838; 0.1427001339915422 0.011129436208133668 -0.24124311666215906; 0.10621059415605254 0.020027841699450266 -0.23603693871321627; 0.07857172047493323 0.02084560439230256 -0.21262796650650823; 0.05075786845508491 0.01607601932661163 -0.15963123320559358; 0.029437303555305383 0.010446048967952672 -0.10539987613016258; 0.012828061278849256 0.004291147562170183 -0.05162041205446713; 0.014747373123871576 0.005209304910460757 -0.06116793174722028; 0.00033511393753868596 0.001748806606954674 -0.008223259300825056; -0.0005571513672230665 -0.0014931134137906642 -0.002950886919581154; 0.0059733648955843975 0.006416813209182857 -0.004306363174189865; 0.002401106681616522 0.009402401738118366 -0.0021749141709498966; 0.002410495452246436 -0.0042706079763131285 -0.0034136587824933357; 0.005523768738532655 0.006753848986628622 0.0042060577068187; 0.01311756632516415 -0.0014943001964895439 -0.006015704128230352; -0.0023954412376229555 -0.0015920317154385797 -0.0032026950727622617; -0.004010509344384905 -0.002914700148694919 -0.012055184087123647; -0.0004152357653059135 0.0009034919807148774 -0.008809852617673085; 0.0118081758702987 -0.01316152477455432 0.004651516633174084] %
+
+Mass Used: 120.02112950842638 kg
+Launch C3: 98.63173140691613 km²/s²
+||V∞_in||: 1.693944598628289e-5 km/s
diff --git a/archive/ES_0.5960392396505929 b/archive/ES_0.5960392396505929
new file mode 100644
index 0000000..0f08874
--- /dev/null
+++ b/archive/ES_0.5960392396505929
@@ -0,0 +1,22 @@
+archive/ES_0.5960392396505929---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-28T04:25:07.971
+Launch V∞: [6.908920469497952, -6.432033511370469, -0.2107970313527219] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.633544200612353e-10, 5.198345943105177e-10, -1.715033909082935e-9] km/s
+ V∞_out: [7.814342256617533e-10, 1.5860427479706272e-9, 4.221755180240778e-11] km/s
+ time of flight: 1.4623565118947822e8 seconds
+ arrival date: 2028-12-15T17:25:58.971
+ thrust profile: [1.0 -0.27606715663914666 -0.2564109981175104; 0.5220309364487055 0.1672214042725095 -0.33840173926980494; 0.19880359369193976 0.13018988308176252 -0.22305564468101083; 0.08346001832427619 0.07464364279841938 -0.1358678386118018; 0.09842590613196367 0.10998147421531765 -0.19790482759880487; 0.0426997702655608 0.05444762441010149 -0.10946331664536743; 0.03541474642832718 0.05125293564134893 -0.10043214914455266; 0.034046028859196706 0.05578773712577198 -0.11149820824025042; 0.006967631505575468 0.014773636774562508 -0.03588554539804964; 0.008922797477456048 0.016457573079998036 -0.037135363659906905; -0.0020691397625938477 0.0032257482317710985 0.0008306738746136962; -0.002485043753164735 -0.00346644388066058 0.0015257205004371105; -0.004758132436158863 -0.0040198694696349565 0.003932106804018499; -0.00355272947293355 -0.00576928488874058 0.006362180517757519; -0.0025875019288642853 -0.002755349627119374 0.00806483432388357; 0.0021550820620843576 -0.008916253638358785 -0.0002705728246261978; -0.015242034598043228 0.0024618231576650504 -0.004034927687260226; 0.00027903714416170915 -0.0018649852244165645 0.0016791663326371133; 0.009525770332109591 -0.0008639193158410212 -0.01258712081926153; 0.008236063496139864 0.011421223455907126 -0.0014002890853492718] %
+
+Mass Used: 175.34518981263045 kg
+Launch C3: 89.14867253366764 km²/s²
+||V∞_in||: 1.9892084278389595e-9 km/s
diff --git a/archive/ES_0.5961430955096102 b/archive/ES_0.5961430955096102
new file mode 100644
index 0000000..0d19f84
--- /dev/null
+++ b/archive/ES_0.5961430955096102
@@ -0,0 +1,22 @@
+archive/ES_0.5961430955096102---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T04:01:53.210
+Launch V∞: [5.0326084249743435, -8.664481964821299, -1.7302933199085473] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9563322520723244e-6, 1.515035834336135e-6, -1.711518630469716e-7] km/s
+ V∞_out: [-1.4363062653228103e-6, 1.9371633823428783e-6, -2.2875352157635977e-6] km/s
+ time of flight: 1.3067654608802025e8 seconds
+ arrival date: 2027-06-17T15:04:19.210
+ thrust profile: [0.41452347568516695 -0.2983009906455403 -0.2618484773358798; 0.0859503014374467 -0.018133133895168674 -0.12144551610826658; 0.07287672762102723 -0.0026236313294906205 -0.15845777695973873; 0.07499074684802241 0.004613217803137509 -0.2137732977055978; 0.06060625832729684 0.006759648356303127 -0.21225030620713622; 0.030318358145214677 0.0037255159515055423 -0.1268260177736224; 0.01681911003041658 0.0029544743901593834 -0.08093353682371199; 0.020874236218281206 0.003478016910461007 -0.11019577644521046; 0.004243697188128544 0.0002725379887488661 -0.029949931955726077; 0.004128251754063157 0.00043111875022672035 -0.028637219272092628; 0.0023246148859199615 0.002342096529425295 -0.01105030129746838; 0.0009736557185053831 0.0012602200356916658 -0.00018500319618115378; -0.0012875690562450283 -0.0001911059860505379 -0.0016032664486442007; -0.0010089938973419947 0.0036812714422627965 -0.0023594668966532596; 0.002895597778036647 -0.0015382498217572762 -0.0030175989796193924; 0.00015399417420204706 0.00192726426347361 0.001701238751445881; 0.0022129003466220894 -1.8954346480178216e-5 0.003994700241049582; -0.002661100953294204 -0.0025993310634299027 0.0015356995625468092; -0.002609276740229847 -0.007002399926296919 -0.0013865684327873991; -0.001890278973771893 -0.0003235164791624031 0.0005008283808004578] %
+
+Mass Used: 92.36680163179926 kg
+Launch C3: 103.39431025075645 km²/s²
+||V∞_in||: 3.326338365859682e-6 km/s
diff --git a/archive/ES_0.5963887716219519 b/archive/ES_0.5963887716219519
new file mode 100644
index 0000000..f420572
--- /dev/null
+++ b/archive/ES_0.5963887716219519
@@ -0,0 +1,22 @@
+archive/ES_0.5963887716219519---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T05:00:56.291
+Launch V∞: [7.011487950417386, -7.117358294775939, -0.757161806936276] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0016467691810449787, -0.0024048490232819438, -0.00020717494822872242] km/s
+ V∞_out: [0.000200992264811486, -0.0008655113761102934, -0.002782769179083603] km/s
+ time of flight: 1.335875825563321e8 seconds
+ arrival date: 2028-07-31T08:40:38.291
+ thrust profile: [0.28554413327408984 -0.11508326713315696 -0.14055934302722195; 0.13648733388367143 0.0066068031679179205 -0.16435026053112423; 0.14680624722352129 0.03469527696520539 -0.28082173080904854; 0.10971569833532088 0.03718815986462758 -0.28529065170434836; 0.08080740321344694 0.032247554942476525 -0.2599606447748864; 0.037111413122227765 0.014987882356965162 -0.1483753115973338; 0.025838570554138653 0.01014598374217167 -0.10674979020841012; 0.010524757702274219 0.0034511295306207464 -0.0480616787476587; 0.0032488696311354912 0.0014322823060051125 -0.012595756842288346; 0.0011081823042616104 0.0014451042165710332 -0.005212735606448593; 0.008962139366939091 0.002990208841480919 -0.012529370331029197; 0.01169865270108456 0.006037688821901882 -0.021180483535722543; 0.005378953101465552 0.0020630476916940537 -0.017872711768067255; -0.0032424657628334873 0.01235504984746131 -0.006676886842680394; 0.022251929958626713 -0.0018690659671189648 -0.016546831506810987; 0.01317141196092022 0.017134816332986167 -0.028465509133290774; 0.004648445513632489 0.004436325325618905 -0.008068827445290729; -0.01942395896743254 0.006134415908413947 -0.008388562814471088; 0.03053292994360723 0.009115478768416615 0.04270167360477278; -0.01535302078508303 -0.009291498481595632 0.06069431637632982] %
+
+Mass Used: 110.17246302675267 kg
+Launch C3: 100.39104637694707 km²/s²
+||V∞_in||: 0.002921997436616474 km/s
diff --git a/archive/ES_0.5964101449058266 b/archive/ES_0.5964101449058266
new file mode 100644
index 0000000..4453d1d
--- /dev/null
+++ b/archive/ES_0.5964101449058266
@@ -0,0 +1,22 @@
+archive/ES_0.5964101449058266---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:36:12.945
+Launch V∞: [5.572780505928083, -8.081080244275931, -0.3632695625181301] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.434681389051895e-5, -0.00011729639099541345, 2.17847520372116e-6] km/s
+ V∞_out: [2.6938536495178668e-5, -6.687638697199765e-7, -0.0001481138380764024] km/s
+ time of flight: 1.5020209292322063e8 seconds
+ arrival date: 2028-01-26T02:24:24.945
+ thrust profile: [0.35363518469169386 -0.1863585086957668 -0.15103546755776245; 0.13624494959029732 -0.0020161390311520364 -0.13917533725084746; 0.1100100268732051 0.023699593061482265 -0.16944790864712306; 0.10629342409101525 0.041195697369030525 -0.22295686066891013; 0.06424970214337128 0.026701707062407678 -0.17044602683118712; 0.04586993974969475 0.021262866461783547 -0.14376091218629533; 0.05299383958558698 0.029700816870782347 -0.1886820385955805; 0.025341374091532656 0.014282705353814776 -0.09926111730474754; 0.0023343460827907865 -0.0008272998021145036 -0.016641653861658143; 0.0049747999655983125 0.0017602619628351625 -0.0027412767573704233; -0.0010522655459844965 0.004810522815632512 -0.022361375608036436; -0.00963378379986123 0.007473672126207137 -0.00965863739817157; 0.0008059961157241137 0.00528272675155275 -0.015445829140486525; 0.033219252849465405 -0.03489551067220842 -0.0208485856807965; -0.037466553256678074 0.040120484283361076 -0.014655422716409983; 0.01333931848603116 -0.003220956477568987 -0.019036676169461638; 0.002288314898470265 0.020457086419450817 0.01861548521507564; -0.005350674161607055 -0.003958465601347505 0.028334046227197575; -0.009940998022594365 0.04538376961243448 -0.13901874353233531; 0.08608437546627436 0.0397912350815904 0.004768938608028814] %
+
+Mass Used: 132.94355505920066 kg
+Launch C3: 96.49170525673092 km²/s²
+||V∞_in||: 0.00015054736924321977 km/s
diff --git a/archive/ES_0.5964472862235195 b/archive/ES_0.5964472862235195
new file mode 100644
index 0000000..6091cbe
--- /dev/null
+++ b/archive/ES_0.5964472862235195
@@ -0,0 +1,22 @@
+archive/ES_0.5964472862235195---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T01:30:41.548
+Launch V∞: [5.265150405857412, -8.345074515525926, -0.8323829757154275] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005103396916061823, 0.00023829086333596394, -0.0004334235358639524] km/s
+ V∞_out: [-0.00021519267273469592, 0.0005220578354136177, 0.0004318260357655975] km/s
+ time of flight: 1.3188795249076246e8 seconds
+ arrival date: 2027-06-26T13:03:13.548
+ thrust profile: [0.4779743697897607 -0.3000569976657377 -0.22660612408101743; 0.18512730363172467 -0.0159577214660203 -0.18995291328998087; 0.16180184729326638 0.021580834515384763 -0.24721139547964258; 0.11642517369100235 0.030203946568829985 -0.2322515658090639; 0.08707170984284562 0.0292077993063987 -0.21142147015382426; 0.08078269732212041 0.033884628585001075 -0.22360344296293777; 0.040561500190092574 0.01874690000993488 -0.12346710245157323; 0.026024351884164146 0.013619029040196174 -0.09073505410907663; 0.024871290261276803 0.01218628769383932 -0.05515097834393379; 0.0046718240480463375 0.004658925320965253 -0.027641541190754584; 0.004578946903996012 -0.005753282479661795 -0.01543957397786435; -0.00032309273953959284 -0.0013947512559876391 0.0005506076385619714; 0.0003701889886632519 0.01449494386991814 -0.006391344126098801; 0.0006640153514495847 0.0071672188714415885 0.0028975638865641026; 5.789313998358058e-5 0.013994592689060595 0.010793739222129927; -0.002272192208801865 -0.00122612764224693 0.008472080034566343; 0.0025117721187585458 -0.03152551604658635 -0.007850222123648044; -0.0005878369434969908 -0.0014059125238589272 -0.003785385390837962; -0.004027541229868683 0.004988387041628754 -0.009655329642613654; 0.01083487176012471 0.004033872434533771 -0.019294374606222537] %
+
+Mass Used: 123.86802376936339 kg
+Launch C3: 98.05493888424161 km²/s²
+||V∞_in||: 0.0007106933922718736 km/s
diff --git a/archive/ES_0.5964866396445795 b/archive/ES_0.5964866396445795
new file mode 100644
index 0000000..f69087e
--- /dev/null
+++ b/archive/ES_0.5964866396445795
@@ -0,0 +1,22 @@
+archive/ES_0.5964866396445795---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T00:53:53.724
+Launch V∞: [6.817589062966904, -7.091329894618812, -1.1981882120497747] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.010088810957996033, -0.06292774597297182, -0.009811199644319998] km/s
+ V∞_out: [-0.061023611576309714, 0.012696619200924292, -0.016571005681280646] km/s
+ time of flight: 1.2552838989304623e8 seconds
+ arrival date: 2028-04-26T21:53:42.724
+ thrust profile: [0.6933926353976514 -0.2927182118790695 -0.33179060729509735; 0.30272034512407703 0.019861282399492714 -0.32915004696011907; 0.19049497356130057 0.05397686122779385 -0.32654687769458224; 0.10979574911864197 0.04624653227846334 -0.2559715075531304; 0.050260049383958595 0.025980604280938027 -0.1484422233691622; 0.04128001004180082 0.02435485011342914 -0.14416522386317984; 0.018169617726738967 0.011276647825628181 -0.074788103153549; 0.015575797904569366 0.010558909944717797 -0.06617029491821932; 0.00378516807747915 0.002513238839362016 -0.017225185209015288; 0.0006771646559185431 0.0004413435769175856 -0.003707881753153241; 0.0008742054985625672 0.0008078032486129997 -0.004422514663109164; -0.0004721744819875572 -7.578925972351498e-5 -0.00271095024840785; 0.003476593706699802 0.003092077256624708 -0.001726693982942288; 0.00041326246934997324 -5.100627507751126e-5 -0.0017398725390598965; 0.0017568563719410311 0.0051176512805228645 -0.0022876483312369265; -0.0038677807380777126 0.005272359198048261 -0.008125304981408508; -0.0006113797033830003 -0.007931937728288336 -0.0050479520632566045; 0.000428358911880367 0.0006257466528371769 0.00026366293617070824; -0.0018578680123475834 0.00017015243997325468 -0.0031591624106571178; 0.0011272772698247865 0.0017712654518572124 -0.003685366637715003] %
+
+Mass Used: 123.05529035111931 kg
+Launch C3: 98.20213529729544 km²/s²
+||V∞_in||: 0.06448212898350796 km/s
diff --git a/archive/ES_0.5967421022017981 b/archive/ES_0.5967421022017981
new file mode 100644
index 0000000..54ac117
--- /dev/null
+++ b/archive/ES_0.5967421022017981
@@ -0,0 +1,22 @@
+archive/ES_0.5967421022017981---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T20:44:18.171
+Launch V∞: [5.217267051141379, -8.430167274744292, -1.203596981774283] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0425213956851405, -0.0006707526893705986, 0.035175450807750294] km/s
+ V∞_out: [-0.05402008459876342, 0.00041472202767273007, 0.011286844781493244] km/s
+ time of flight: 1.2762198794257878e8 seconds
+ arrival date: 2027-05-08T23:17:25.171
+ thrust profile: [0.5105810737825203 -0.345775023025223 -0.2538052677362472; 0.19691489902855405 -0.025153453057483885 -0.21423301002085562; 0.14547817853033196 0.012204661825746995 -0.2372069578422002; 0.09653933688602627 0.01995026985208311 -0.20754312486771692; 0.046582872415822256 0.01342216076375355 -0.12289417721359291; 0.04959648958834092 0.01714151713803171 -0.14790576646493706; 0.05759198811430635 0.02504159940717969 -0.19496470413501815; 0.02750300117131905 0.012345871868157294 -0.10284486646695729; 0.029338117200462806 0.012270219146666221 -0.11332128998223318; 0.008621119249900755 0.003928567300198417 -0.03731933534388745; 0.0019981513650798016 0.00010975317155130634 -0.004174911620906844; -8.263685781556492e-5 0.0012569323795211017 -0.0016935399525314706; 0.0023499254568899665 0.001599657668653675 -0.0017676366967583831; -0.0019177642380359045 -0.0014210607352125432 -0.001616750291128866; -0.000783904596307148 -0.0005978174793958891 0.00014775287138480298; 0.0012385689510512937 0.002273100533461608 0.0011142569941966487; 0.0006976169009579843 -0.0022701060656794246 0.0008202549611895866; 0.0009661355238366044 -0.0022933403448611744 0.0010208418548107569; -0.000523633604981704 -0.0012449589888477934 0.0005829416566635246; 0.0005632906005423953 -0.00035832599862657645 -0.0032816906696735136] %
+
+Mass Used: 114.40437739924892 kg
+Launch C3: 99.73624145763124 km²/s²
+||V∞_in||: 0.05518905090424227 km/s
diff --git a/archive/ES_0.5967544060097144 b/archive/ES_0.5967544060097144
new file mode 100644
index 0000000..5f9edf3
--- /dev/null
+++ b/archive/ES_0.5967544060097144
@@ -0,0 +1,22 @@
+archive/ES_0.5967544060097144---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T14:01:00.791
+Launch V∞: [5.031615322302218, -8.663275702419796, -1.83149011179091] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.031309442688618565, 0.042248255295729904, -0.00789227716579378] km/s
+ V∞_out: [0.049721974895221205, -0.016414910179246418, 0.00921648990140098] km/s
+ time of flight: 1.324959855980591e8 seconds
+ arrival date: 2027-07-09T02:27:25.791
+ thrust profile: [0.37526002063051594 -0.27035487168420147 -0.24391972057801461; 0.08851485894428605 -0.019696474537547005 -0.12727148770958768; 0.08617098600611241 -0.004845201155353824 -0.1922685520490268; 0.07038594133678101 0.0016065095132766771 -0.21029877161574598; 0.05047433528034595 0.003182785204217535 -0.1867573138726059; 0.029497819193346476 0.0023546989474325535 -0.12920453764896161; 0.02267129170617417 0.001906972429799395 -0.11416909597257702; 0.013534476816878955 0.0011471604812835186 -0.07498702261307122; 0.0006623861772320015 0.00024335928342799883 -0.006198459526521875; 0.002466586223670273 0.0023813672777289125 -0.00671162990982398; 0.0013310735604986621 -0.005070724317441176 -0.005301770126566955; -0.0023058504075107265 0.000505245918533759 -0.012439253948398694; 0.0024379337769019163 -0.0026335654233745473 0.0009877268426528873; 0.003378525699260152 0.0034591429227939707 0.001635853248803304; -0.00016439168246922963 0.001754695256195517 -0.0005672130181069257; 0.009060332539585781 0.005890956812300277 0.0018404956800409998; -0.00435720876566846 -0.00018177269224051813 0.0007418347419612856; 0.004220511829960239 0.0019396188574651355 0.013482477274574824; -0.0043221931457955946 0.001641294657967845 0.011697812595937393; 0.0036200284515560373 0.002109788417919749 0.009839077002529086] %
+
+Mass Used: 91.15765472678277 kg
+Launch C3: 103.72385467735154 km²/s²
+||V∞_in||: 0.05317409440570446 km/s
diff --git a/archive/ES_0.5968678377373694 b/archive/ES_0.5968678377373694
new file mode 100644
index 0000000..36c5215
--- /dev/null
+++ b/archive/ES_0.5968678377373694
@@ -0,0 +1,22 @@
+archive/ES_0.5968678377373694---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T21:18:39.893
+Launch V∞: [5.2791811724558695, -8.515547804698087, -1.2261217086624399] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.4503071440052758, -0.29758836174870235, 0.27670961812054506] km/s
+ V∞_out: [-0.37994451328007384, 0.383707582480457, -0.2761413763148648] km/s
+ time of flight: 1.2836937548851357e8 seconds
+ arrival date: 2027-05-18T15:28:14.893
+ thrust profile: [0.30742393634183196 -0.21638364830176426 -0.1793201968017284; 0.16359891425042195 -0.027347566547360983 -0.19895345898936448; 0.15148411146938098 0.004462654790474189 -0.2759273066046457; 0.12143199575463691 0.016675386588295267 -0.2895393832929802; 0.08242606498056916 0.016998587903696655 -0.24032860157404815; 0.042101409396809966 0.010641726810151094 -0.1433582800840092; 0.020481919958783325 0.005884673519962427 -0.0777483266747172; 0.009549634595303516 0.0029358727945928507 -0.03939536952565291; 0.0055780369507211 0.001868666819035878 -0.02445380840600733; 0.012854007706006624 0.004700401287967586 -0.06033079622361069; 0.0007911101130697935 0.0003218944304449709 -0.0038961823683788767; 0.0006798378934142208 -0.0013021595448505724 -0.003894916913073792; -0.006405415907531654 -0.0006893106486996963 -0.0085763949224146; 0.0005555232701756211 0.0007274868121270243 -0.00031287577568359787; -0.004910442724189073 -0.0026744953600541634 -0.006040651429561203; -0.004481679522890471 0.0018735539441037336 -0.002649253542749087; 0.011781075319514778 0.009753789996240703 -0.0012224304578214835; -0.008453761604708598 0.0019055542980762588 -0.010001859249074012; -0.0022085035124571016 -0.0003154416590740636 0.007748713486095373; -0.006521867692685127 -0.004080612986270702 0.001162212591751078] %
+
+Mass Used: 102.00099488430624 kg
+Launch C3: 101.88768271016424 km²/s²
+||V∞_in||: 0.6065505500375732 km/s
diff --git a/archive/ES_0.5969810078869175 b/archive/ES_0.5969810078869175
new file mode 100644
index 0000000..af7aa8a
--- /dev/null
+++ b/archive/ES_0.5969810078869175
@@ -0,0 +1,22 @@
+archive/ES_0.5969810078869175---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T16:52:49.952
+Launch V∞: [5.167893990099941, -8.341664803503186, -0.9256462521014904] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.688497292515603e-5, -8.335217507609037e-6, -1.511989336993254e-5] km/s
+ V∞_out: [1.0935632581466075e-5, -1.4329907545889938e-5, 1.6119376714485723e-5] km/s
+ time of flight: 1.277628296770616e8 seconds
+ arrival date: 2027-05-09T10:33:18.952
+ thrust profile: [0.5912900410215833 -0.4079573206096007 -0.29780212701302194; 0.3738758438739481 -0.052141057921659864 -0.38487442970069585; 0.1443532928998149 0.009692096598048164 -0.22501556578455148; 0.10024096113577433 0.017716502922312926 -0.20261788937390712; 0.07870680016289923 0.021091319234073688 -0.1925508224236466; 0.06445561203813654 0.021311764200734693 -0.18226638834299275; 0.0376517663765774 0.014392570432150711 -0.12189942305840638; 0.007833214673628174 0.0028041929621888404 -0.028522131049878822; 0.02707908079570212 0.010588639064174342 -0.08040263534830726; 0.009419242941084477 0.005031311234858065 -0.02599344830013561; 0.0023059787075841833 0.00516850892451092 -0.025914312649741606; -0.0010899766456618225 0.0007650752163904436 -0.0042184146102645795; -0.00040332858981827717 0.002266916215507701 -3.711956216350212e-5; -0.002896404631339463 0.00012284992114915062 0.003653047058971589; -0.0016875542655744999 0.00259239246594714 0.0012345358330277418; -0.0010583030721913128 -0.00035940459665283116 0.0007157080864058081; -0.0046229367230857694 -0.0013191732209086476 0.0038933738193428565; -0.0023615444806445764 -0.0012377924180520202 0.0019672368419541234; 0.003726476922468226 0.002496398243911094 -0.008969246746795478; -0.002134983091254046 0.0016473730062525874 -0.0002790984819236778] %
+
+Mass Used: 129.78513687089435 kg
+Launch C3: 97.14732097094448 km²/s²
+||V∞_in||: 2.4149313387766003e-5 km/s
diff --git a/archive/ES_0.5970900144418456 b/archive/ES_0.5970900144418456
new file mode 100644
index 0000000..1ba4e52
--- /dev/null
+++ b/archive/ES_0.5970900144418456
@@ -0,0 +1,22 @@
+archive/ES_0.5970900144418456---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-17T17:22:18.691
+Launch V∞: [6.668002850626561, -6.920129218347537, 0.09616775938749506] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.648950293234561e-7, 2.5881313055579116e-6, -1.502579121385935e-7] km/s
+ V∞_out: [9.303791722611566e-7, -2.123252178080448e-6, 1.2142914500837824e-6] km/s
+ time of flight: 1.874957778744895e8 seconds
+ arrival date: 2029-03-26T19:31:55.691
+ thrust profile: [0.775858142499582 -0.17973354545556802 -0.14820115872774167; 0.4232033233096468 0.1749032275800544 -0.25412504657287127; 0.1474559937709578 0.11551969868148715 -0.1623466594371238; 0.07406085154911887 0.0803389926418673 -0.1187643801579875; 0.042029351976312405 0.05794716543364806 -0.09025610316458844; 0.03257429311107901 0.05350563232826355 -0.0866569761294171; 0.01637172815156068 0.03175949525047562 -0.05363837376035075; 0.009396305841998204 0.020983632590199697 -0.03695361767280588; 0.0025619123196766293 0.006014880732161713 -0.010910527994361867; 0.0006846439324467562 0.0011231526275895737 -0.0023563741072820522; 0.0005070680090722675 0.002725985740254106 -0.0030670030086276585; -0.000744624071881602 0.002191705921704209 -0.003030564255051472; -0.0005811566459670717 0.001432708011016622 -0.0013851702422750221; 0.000321909536535154 0.0007412595636662848 -0.0011542197799879635; 0.00035308392266010253 3.8228438229363646e-5 -0.0012413971649327578; -0.00041172875277690655 -0.0018577434970071462 -0.001946786768077821; -0.0026480504148324647 -0.002158759572382837 -0.0005959410373807463; 0.0015819989696857824 0.0012739747100080014 -0.0019987625777110538; 0.0002364482853675178 6.309527848222078e-6 -0.0006231801744104285; -0.0017334456103084367 -0.0012901978209123458 -0.002294362800141501] %
+
+Mass Used: 157.84010804235504 kg
+Launch C3: 92.35969865253684 km²/s²
+||V∞_in||: 2.6180430625553346e-6 km/s
diff --git a/archive/ES_0.5972556007851729 b/archive/ES_0.5972556007851729
new file mode 100644
index 0000000..3798d32
--- /dev/null
+++ b/archive/ES_0.5972556007851729
@@ -0,0 +1,22 @@
+archive/ES_0.5972556007851729---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T05:35:26.522
+Launch V∞: [6.840607961260415, -7.159961212766199, -1.0363098266248076] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3953699414624682e-6, -3.3675615007014774e-6, 6.377222980458383e-6] km/s
+ V∞_out: [3.1608495614508112e-6, 6.903311594202884e-6, 2.1998480349714274e-7] km/s
+ time of flight: 1.2610055803494503e8 seconds
+ arrival date: 2028-05-04T17:31:24.522
+ thrust profile: [0.6483432106665384 -0.27535419626244434 -0.3159185023120223; 0.1765204204320841 0.005809975110953081 -0.2033113237102074; 0.14999604668572933 0.03742252267167359 -0.272591170316287; 0.10492274001142467 0.03794510647241921 -0.258578474666885; 0.09852423952957896 0.0408319243266261 -0.29299754898373964; 0.04037564875422541 0.016906577806718257 -0.14501513933963978; 0.024115651452106993 0.013808289001748212 -0.09600745513829062; 0.01108466909728727 0.006491430742589133 -0.05161192303389214; -0.0004509690482477238 -0.0007807013283352306 -0.0045480711335978705; -0.00043339367701276986 0.0014062062501228776 -0.003307939132895722; 0.004084976754494162 0.0027226609511953144 -0.022672996225174758; 0.0014418716623849923 0.0008704990753413396 -0.008067201571738396; -0.0004735144483436974 -0.00045447879438069785 -0.0038880630027999293; 0.002053507829895033 -0.00015055318491089423 0.00046021711072621093; -0.014330469964727633 0.0004551833619190271 -0.008698964859508116; 0.00810082880686059 -0.004639055054488233 0.000741502238330288; -0.0074039220526363105 -0.003250953241474146 0.0037556357470548644; 0.0005080947751886625 0.0014930989043935783 -0.0012621476675807848; 0.00017473402186726382 0.0033560303097553853 -0.011318907676716682; 0.01130400119058467 0.006071578363813813 -0.0026373510580887023] %
+
+Mass Used: 118.522951471748 kg
+Launch C3: 99.13289990473493 km²/s²
+||V∞_in||: 7.599160516790996e-6 km/s
diff --git a/archive/ES_0.5972703128456229 b/archive/ES_0.5972703128456229
new file mode 100644
index 0000000..82dde32
--- /dev/null
+++ b/archive/ES_0.5972703128456229
@@ -0,0 +1,22 @@
+archive/ES_0.5972703128456229---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T16:08:28.312
+Launch V∞: [5.198117754466881, -8.378119491566544, -1.1339288189599017] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.060156839358366986, -0.08881018892868299, 0.014522143425721838] km/s
+ V∞_out: [-0.10124091241315801, 0.03411673940427801, -0.017483725320505492] km/s
+ time of flight: 1.2887282640236183e8 seconds
+ arrival date: 2027-05-23T06:08:54.312
+ thrust profile: [0.5705552848210671 -0.3904961324265945 -0.30247903000401727; 0.19249188563251193 -0.025530283321352626 -0.21416244175453955; 0.15690344661857988 0.012004464325661 -0.26102166071752037; 0.12056471946252692 0.023726712460911938 -0.2618860160789653; 0.06308212762231843 0.017643966906452646 -0.16803458829316162; 0.06825043879403463 0.02305414709714029 -0.2081507130099579; 0.030770107467808668 0.011283463430873168 -0.1010422737996132; 0.004045882656694978 -0.00015947337189484156 -0.02331574249755408; 0.022678393370591046 0.010210406847469263 -0.09181507187005954; 0.004234621409139057 -0.0048445007262904955 -0.018018443041880324; -0.0032705214394177515 -0.005616706787889026 -0.007440587223435457; -0.011334667562395373 0.004674702816210564 -0.006258989131575777; 0.0007376318597268399 0.0016468228586726294 0.005966452445110729; 0.0006486729424642012 -0.0013759361309651878 -0.0018780423007430445; 0.0050543539875699045 0.006045302619485096 -0.00585318304925743; -0.00630711093937331 0.0016392733636995112 0.007563454328007217; -0.0011229903594963681 -0.0017364229863519216 -0.0037461503662097537; 0.0031312944172328743 -0.006482341653013724 0.00195630995784027; 0.0018818605889618228 0.0005175229773990387 0.00014187969008269815; -0.013433065416765155 0.006618680171607831 0.030173097868340416] %
+
+Mass Used: 122.23722932391684 kg
+Launch C3: 98.49910897073885 km²/s²
+||V∞_in||: 0.10824503512315922 km/s
diff --git a/archive/ES_0.5973893156965236 b/archive/ES_0.5973893156965236
new file mode 100644
index 0000000..8a21425
--- /dev/null
+++ b/archive/ES_0.5973893156965236
@@ -0,0 +1,22 @@
+archive/ES_0.5973893156965236---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:59:01.553
+Launch V∞: [6.915646715424492, -7.31442926761283, -1.694719034352717] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.23733390154667697, 0.12303782023813505, 0.016725895036364354] km/s
+ V∞_out: [-0.20916536784275322, -0.1090352883025935, 0.12689281742689032] km/s
+ time of flight: 1.2525266549986333e8 seconds
+ arrival date: 2028-04-26T22:23:26.553
+ thrust profile: [0.39766953910857483 -0.18370543869861194 -0.2300387046500324; 0.11597010821752696 -0.002580565339585322 -0.15206537498916387; 0.10613317643798262 0.015684044555260183 -0.22234266146679824; 0.08639384420866165 0.02035183795568129 -0.2444431694037414; 0.05557287008533183 0.015919139941417772 -0.1929066224337836; 0.03760630936976746 0.01178646166046708 -0.15148340812638025; 0.0225126124762735 0.0074314682680828295 -0.10178579058794501; 0.015964216945519107 0.005184591344511622 -0.07877934894216802; 0.0039275878782250445 0.0005228481389367031 -0.015392735494206035; 0.0020661627874564593 0.0006117355288080354 -0.006718577232902657; 0.0004874715121776236 -0.0001221446112220396 -0.0028648952420400548; 0.0008470712693477104 0.0007086488302536199 -0.004621966408692222; 2.9566069859386472e-5 0.0001574464642850582 -0.002313037788057989; 4.500649324723358e-5 0.0006845634826117267 -0.004415641220720359; 0.0012044194074972978 0.002675646322058309 -0.004506829609084162; 0.000360868274530303 0.0008728064972410498 -0.002969951797027407; -0.0008111130767270089 0.0005722554879770644 -0.00020096638424934492; 0.00010007232543292159 0.00017211391601213355 -0.000615956080994678; 0.00022595022894487168 -0.0006443764565098792 -0.0012389850343804498; -0.001533222809285707 -0.00035517374806457976 0.0013983786972184293] %
+
+Mass Used: 89.12601559420182 kg
+Launch C3: 104.19911760887014 km²/s²
+||V∞_in||: 0.2678533957169236 km/s
diff --git a/archive/ES_0.5974370531477315 b/archive/ES_0.5974370531477315
new file mode 100644
index 0000000..d0fa51f
--- /dev/null
+++ b/archive/ES_0.5974370531477315
@@ -0,0 +1,22 @@
+archive/ES_0.5974370531477315---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:23:47.617
+Launch V∞: [7.008577708802243, -7.24339410305414, -1.4827442774693211] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.016672022838085603, 0.0198585995121597, 0.0019992609343009605] km/s
+ V∞_out: [-0.00620096893811789, 0.024653645090367916, -0.005471990763376649] km/s
+ time of flight: 1.2592764873743322e8 seconds
+ arrival date: 2028-05-03T20:17:55.617
+ thrust profile: [0.34518273173809566 -0.14950648779338446 -0.18798385970487794; 0.11830121008791014 0.004892648338145269 -0.15197695668319186; 0.07940007890804146 0.018155303081763392 -0.15912083176543634; 0.05924926911973652 0.019374486201813926 -0.15903675592429084; 0.055094149117796656 0.02376122876354265 -0.18220780655011284; 0.0566978649994305 0.027433031783400535 -0.21867062170399468; 0.05068914356612722 0.029295635242965343 -0.2127366222989168; 0.00900535505498619 0.00450398537893813 -0.045169730047523046; 0.019131353239445172 0.011803948978226717 -0.10832261291743511; 0.00779245170793874 0.004099298103731792 -0.04458099976182206; 0.0012703190849581369 -2.509665249091688e-5 -0.001669220470551026; 0.0013793708578174195 7.933535395565947e-5 -0.0026705405345446714; 0.00087292185596598 0.00047961640155697537 -0.002552864828667778; 0.0002929217574793345 -6.119395141325522e-5 -0.0017622449377395016; 6.31725638469971e-5 -0.0004972335385536211 -0.0013935680432891743; -0.00015838966910885956 5.7825620620737374e-5 -0.0005783717304539806; -0.0004274518981959603 0.0018781052898626978 0.0007297333910501602; 0.0020936885438640656 -0.0022675481610253878 0.0012418275754894482; -0.0031054030121196773 0.0006593976450430968 0.0006168363189325779; -0.0005962260582375864 -0.0010230860968620536 -8.857123997825381e-6] %
+
+Mass Used: 91.59476902741153 kg
+Launch C3: 103.7854502248472 km²/s²
+||V∞_in||: 0.026006102445030464 km/s
diff --git a/archive/ES_0.5974881841662303 b/archive/ES_0.5974881841662303
new file mode 100644
index 0000000..9d52544
--- /dev/null
+++ b/archive/ES_0.5974881841662303
@@ -0,0 +1,22 @@
+archive/ES_0.5974881841662303---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-16T23:39:52.384
+Launch V∞: [6.390723168657973, -7.813868562227099, -0.6297870414698227] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0015005718016113901, 0.00905884066869838, -0.011340399239611746] km/s
+ V∞_out: [0.010051081512889875, 0.008425801354302861, 0.006414976060829528] km/s
+ time of flight: 1.488512889192994e8 seconds
+ arrival date: 2028-01-03T19:14:40.384
+ thrust profile: [0.1682163764251951 -0.09538353830582488 -0.0679845625912573; 0.11936799760737468 0.0027019887872229745 -0.1161639859761281; 0.13352533597890165 0.033810537417817206 -0.20623323808224045; 0.1222709115622082 0.05023807182446713 -0.26858642634344304; 0.09065103419298205 0.04646466105712525 -0.23005185616355628; 0.07537116545932686 0.045199678621707096 -0.22473681937544976; 0.043740914220727053 0.030250068051154922 -0.14614635611568974; 0.02224998050640749 0.017203576643434446 -0.08272212611504631; 0.0043044950127000495 0.0038119394628154404 -0.01779591172174194; 0.00116093631245786 0.00112091401113177 -0.005769075167393068; 0.00024128331409966708 0.0005056397886453301 -0.0043566453087006355; 0.00016740473364714137 0.00014151719838385605 -0.000838686250092911; 5.698741031304188e-5 4.872935392270062e-5 -0.0006225192421620763; -0.00016953851171326817 -7.494288478631912e-5 -0.0002781966309087329; -0.00011743383858754878 -0.00023274430435047736 -0.0006552158464470246; 0.0007687176426352134 0.00036494435255131417 0.0009181438166446435; -0.0005606215838116744 -0.00041649700180723876 -0.0012655491503995048; -0.0001420888157853625 -0.0006510300158578109 -0.0005009630573554424; 0.0007586961344328497 0.000996729462109617 0.001953265696632049; -0.00043620617943296227 -0.00043574392311661423 -0.0006609667173248209] %
+
+Mass Used: 100.35153677184962 kg
+Launch C3: 102.2945162437861 km²/s²
+||V∞_in||: 0.014591743038665452 km/s
diff --git a/archive/ES_0.5977085400531784 b/archive/ES_0.5977085400531784
new file mode 100644
index 0000000..1044d58
--- /dev/null
+++ b/archive/ES_0.5977085400531784
@@ -0,0 +1,22 @@
+archive/ES_0.5977085400531784---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T01:27:53.106
+Launch V∞: [6.768873158870772, -7.016247537835063, -0.947516536868481] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000495813423119562, -0.002462972075637481, -0.002475891987126096] km/s
+ V∞_out: [-0.00347298830652278, -0.0004203670901944956, 0.0004357007239428386] km/s
+ time of flight: 1.2509324701842394e8 seconds
+ arrival date: 2028-04-20T21:35:20.106
+ thrust profile: [0.9364663387031461 -0.3904301826141752 -0.4144398718071081; 0.27066949102823545 0.02333812117307297 -0.27435295439580654; 0.14897742874416361 0.048149709639948184 -0.23895473332559058; 0.14111592181308247 0.06533150831016077 -0.2987068368520294; 0.05534926877365657 0.03174329029754172 -0.15124562594790356; 0.012215223912645469 0.007711231780052445 -0.04073830362329088; 0.036808290511135676 0.02515627346743983 -0.12321274686214508; 0.06833853277596527 0.043273295113134554 -0.22319144812797123; 0.012386042769948896 0.010267451966091516 -0.05677556679812984; 0.0027860668827288044 0.002049087576394262 -0.012509955555174942; 0.0013982828054144112 0.0013314710613007476 -0.007018664541666103; 7.354509580363057e-5 3.6956657697112256e-5 -4.732646550128876e-5; -6.732097231693684e-5 -0.0001087045491710195 0.00013466585567261811; -0.00019519658186092166 0.0005974083825763209 -0.0002539801790777447; -0.0005901205793563787 -3.926272749518092e-5 -0.00030072547130283113; 2.7301549958476852e-5 0.00014745840678965182 0.0001239214404028143; -8.251744507247895e-5 -2.4707946451009476e-5 0.00010367983877245197; 7.729759976981786e-5 4.451600627072307e-5 -0.0004751104586185491; 7.397821581728352e-5 0.00013012568449713945 -0.0008883983152210377; -0.00018271539384291007 -0.0006573081978852378 3.449542787942498e-5] %
+
+Mass Used: 137.65819124130894 kg
+Launch C3: 95.943160940697 km²/s²
+||V∞_in||: 0.0035273366054050966 km/s
diff --git a/archive/ES_0.5977350712837249 b/archive/ES_0.5977350712837249
new file mode 100644
index 0000000..9642405
--- /dev/null
+++ b/archive/ES_0.5977350712837249
@@ -0,0 +1,22 @@
+archive/ES_0.5977350712837249---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T14:48:41.860
+Launch V∞: [6.911898049212096, -7.282397639062246, -1.4398579558377331] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.021550932907767887, 0.022171528662406473, 0.002286209924949576] km/s
+ V∞_out: [-0.007192894317651903, 0.02944061701624035, -0.006517260748354634] km/s
+ time of flight: 1.2460661398617409e8 seconds
+ arrival date: 2028-04-18T19:45:34.860
+ thrust profile: [0.48106669966109944 -0.2156137578851718 -0.2604588381794199; 0.09848182485574648 0.0008814274148173284 -0.12515734442887588; 0.10249807739702478 0.0199904068891324 -0.2027798795489369; 0.08617097876698034 0.025624402594811826 -0.2278886558979246; 0.07640903351412304 0.02781546797065258 -0.24763751211336874; 0.05606894066540806 0.022776382853360342 -0.21254024118787995; 0.03999246707312864 0.01783431231212736 -0.17046011521729806; 0.004499871124875498 0.0020035618104483964 -0.0212204309003207; 0.002403377118564343 0.001120606399772145 -0.012107278463478121; 0.003925333742276671 0.0015598870062717661 -0.019576702575830194; 0.0002585151453987313 0.00015197606267803546 -0.0021046506595249386; 0.0006042849506475477 1.928735975978977e-5 -0.002779072281558558; 0.00018482121845688084 0.0010755538218280296 -0.00179068544198697; 0.00021686084348679986 6.984003728934939e-5 -0.0005800956030587176; -0.002225944934216108 -0.00042694406910430513 -0.006330431732041508; -0.0012310570487071965 0.0013483815043469783 -0.0020093404832321835; 0.00023825462114244962 0.0018598711741496534 -0.006037211318711444; -0.0002424455274898903 0.00011771829786051159 -0.000605593533601699; 0.0003191935155296144 0.00012943078137201943 -0.0010997052687056223; 0.00030502951597392473 0.0007640066715890638 0.0017666816521613254] %
+
+Mass Used: 97.21934429453404 kg
+Launch C3: 102.88084094911058 km²/s²
+||V∞_in||: 0.031003969878774598 km/s
diff --git a/archive/ES_0.5977677415706997 b/archive/ES_0.5977677415706997
new file mode 100644
index 0000000..219bd19
--- /dev/null
+++ b/archive/ES_0.5977677415706997
@@ -0,0 +1,22 @@
+archive/ES_0.5977677415706997---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T05:38:09.885
+Launch V∞: [5.653060278327063, -8.097547683993966, -0.5092694893144512] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9132803143441837e-6, -0.0010344067819704635, 0.0003267047754027273] km/s
+ V∞_out: [0.0010265643813329893, 0.0005687066611583606, -0.0004652123360369906] km/s
+ time of flight: 1.5073907914630803e8 seconds
+ arrival date: 2028-02-01T21:36:08.885
+ thrust profile: [0.25374564052730103 -0.1332826455219214 -0.11745789322790351; 0.12010723802893786 0.0019821406475745264 -0.1325729071448225; 0.12188863309956832 0.027664683156499153 -0.21117248777585645; 0.11039337481735709 0.039483820854335966 -0.2554593254860309; 0.07783671758859335 0.03575276438193023 -0.2225841668911706; 0.04211123243480923 0.024174766933770887 -0.13902610618594297; 0.02054514749050947 0.015709634134541815 -0.07083595211780556; 0.03343492304449999 0.02227677000339744 -0.1394178669834246; 0.012364682470237259 0.007001995579630691 -0.03582127899044971; -0.0001978164463812054 0.010086449098529855 -0.011737187882915844; -0.01793438055135168 -0.009787567832624739 -0.005779118460067993; -0.0070532418374413324 -0.019115473940926123 -0.019114808592509015; -0.010506433075638198 0.007446837457087397 -0.018518012645822635; 0.019064343757080816 -0.034482423281060444 0.0012059137978984256; -0.020316793709405992 0.012800445577016812 -0.018239639171043553; 0.009776812110750658 -0.06682589716325403 0.044387636922934286; -0.010772547206448933 -0.014761947468033432 0.037978666603074376; -0.016583639912405784 0.0291278737479326 0.01528499140976484; 0.029965450317199775 -0.04005097327598379 0.03821463831177026; -0.050299712467098454 -0.036088337276051555 0.04402609730311666] %
+
+Mass Used: 126.97313939588867 kg
+Launch C3: 97.78672441770189 km²/s²
+||V∞_in||: 0.001084775120243361 km/s
diff --git a/archive/ES_0.5977784055592229 b/archive/ES_0.5977784055592229
new file mode 100644
index 0000000..e9cb901
--- /dev/null
+++ b/archive/ES_0.5977784055592229
@@ -0,0 +1,22 @@
+archive/ES_0.5977784055592229---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T22:23:44.246
+Launch V∞: [7.120238443587189, -7.197570095607403, -1.5444555160776525] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0063974367676005025, -0.019610857838420905, -0.03879655713616294] km/s
+ V∞_out: [-0.03763777561874944, -0.006382821264592266, 0.021754082471458054] km/s
+ time of flight: 1.2764409352864647e8 seconds
+ arrival date: 2028-05-23T07:05:17.246
+ thrust profile: [0.15471857684832752 -0.06408080148788192 -0.08341337999394031; 0.11571694262534393 0.006641856994533093 -0.14104863906643506; 0.10513275300803562 0.02701014484512657 -0.20100971740430623; 0.08874723931366207 0.033246308297173593 -0.22789917838480778; 0.07005130179128816 0.03194683626755763 -0.22248074338869583; 0.05122020249287685 0.02657388143766509 -0.19158120317240362; 0.03184564427126756 0.01818491054552756 -0.13657442383363436; 0.014511878283648853 0.008713604702279727 -0.07063504463498099; 0.0019970189514724296 -0.0005043707594605624 -0.008543093413023752; 0.011672635914140568 0.00757077853310222 -0.06520364953217964; 0.00604138548442423 0.005052854942561176 -0.03986714148680711; -0.0009223021593931279 0.0017220835602773305 0.001080814294845842; 0.00031113763051296363 5.725148739432664e-5 -0.0019274023467398052; -0.00913354289420075 0.0029652299338728976 -0.008753867057107546; 0.002343756558702503 -0.011714930360197103 -0.0056581131643170055; -0.008300717990120759 0.0009681050236014092 -0.002303481649705781; -0.001615207624058903 0.001481746971995275 0.003543828692860483; 0.007094729366324155 0.008663237639180596 -0.00026912130800515067; -0.0005057286942833383 0.0038709556214957105 -0.004469457402411888; 0.012059168922121298 -0.002826095195318622 0.0011740856042949015] %
+
+Mass Used: 85.56057705990088 kg
+Launch C3: 104.88815361586157 km²/s²
+||V∞_in||: 0.043939569729046696 km/s
diff --git a/archive/ES_0.5980694091265737 b/archive/ES_0.5980694091265737
new file mode 100644
index 0000000..dcbcbb9
--- /dev/null
+++ b/archive/ES_0.5980694091265737
@@ -0,0 +1,22 @@
+archive/ES_0.5980694091265737---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T14:23:59.623
+Launch V∞: [7.385316633683307, -6.490108053517322, -2.535304024068354] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.109080748393523e-7, -1.2752295619791193e-6, 6.5654680466272885e-6] km/s
+ V∞_out: [3.224558885906815e-6, -5.583459334371057e-6, 1.9961367818059867e-6] km/s
+ time of flight: 1.4738008106601536e8 seconds
+ arrival date: 2029-01-03T09:18:40.623
+ thrust profile: [0.27453343929599094 -0.06804233269620226 -0.11779620379239825; 0.1327485466358725 0.04197536402802199 -0.14002467423736667; 0.11892215918333997 0.0762040326069679 -0.20553072946738057; 0.09219422730375308 0.08234478297412828 -0.22351082409558465; 0.058655549332562826 0.06475173823993305 -0.1865933213823312; 0.0339915855989555 0.043553981276977585 -0.1350962057476489; 0.026608170757824994 0.03939081494952149 -0.12525335828594913; 0.010086154378389103 0.016398279511989317 -0.05494770158155884; 0.010897503403360188 0.021182183444964545 -0.06797352717522856; 0.00015984939423095468 0.0006895300346480397 -0.0017467992903366664; 0.0002746518157768821 -0.000137700215297039 -0.0011464493649944252; -0.0009350766524665445 -4.1664809425653036e-5 -0.0006034154900460835; 0.00045507825713901536 -0.001099386610287727 -0.001693918697504871; -3.350014430667407e-5 0.0002873363842090044 -0.0006221935951639373; -0.0002812037239262036 0.0023624329596408063 -0.0010611201930701723; 0.0001916426295563223 -0.0010244289162361425 0.0007560596137581714; 9.528180353892469e-5 -0.0020321004296698247 0.0007982957677904655; -0.0008423660649710283 0.003023535400963915 0.001703100436255041; -1.1559800056273234e-6 -0.0004835793114109459 0.00012303399055627919; -0.0003062585240302643 -5.0526458987775965e-6 3.8474538970101444e-5] %
+
+Mass Used: 96.37664752781211 kg
+Launch C3: 103.09217082054693 km²/s²
+||V∞_in||: 6.749913675584076e-6 km/s
diff --git a/archive/ES_0.5980959224848409 b/archive/ES_0.5980959224848409
new file mode 100644
index 0000000..147b54b
--- /dev/null
+++ b/archive/ES_0.5980959224848409
@@ -0,0 +1,22 @@
+archive/ES_0.5980959224848409---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T23:47:22.226
+Launch V∞: [5.0316890637092495, -8.801023909135106, -1.7974336825875668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.017181516010362517, 0.030370314857581685, 0.002378310388045036] km/s
+ V∞_out: [-0.002413356816158297, 0.011016665004201575, 0.03453765642880554] km/s
+ time of flight: 1.3743280919888178e8 seconds
+ arrival date: 2027-09-06T15:34:11.226
+ thrust profile: [0.19405563215144386 -0.1382082026820478 -0.1330901666477496; 0.07170034825495913 -0.01888283865846923 -0.11278038833378892; 0.06223891783600811 -0.0076988195717394145 -0.15518142406381036; 0.06166902493733631 -0.003947995033034324 -0.20704302371582942; 0.04905451411279472 -0.0022727961439371696 -0.2046420479399074; 0.039623748039949405 -0.002361449784391524 -0.19679743563019023; 0.014696835209363638 -0.0007879383900295428 -0.08384764667155721; 0.005209272206842588 -0.0008515735314823257 -0.0337098359762899; 0.002433816101808353 0.00041173479437380607 -0.012345688368742681; 0.0010809877042956418 -0.001670590419241232 -0.010796388660512147; 0.0031857349125772633 0.004277648066969603 -0.006456221415826497; -0.0050906834787751605 0.0035327201724722414 -0.0036124921076976157; 0.0014918701259518524 0.002693589160144793 -0.00020158877531697; -0.0015068588251849748 0.0027623570410097806 0.0005088593108802685; 0.0055192587536964976 -0.005932473035157293 0.0007210957307218103; -0.0026911154219771095 0.004322767000989875 -0.0028260680322049862; 0.003280562143767145 -0.001766874816318375 -0.005083175825876791; 0.0006592302405852938 0.002070686564534705 0.002440441136696065; 0.021627882380152057 0.017161703290590642 0.00037466625001806507; -0.012677443403543582 -0.006610290961542122 0.02942998278607742] %
+
+Mass Used: 79.4062498287849 kg
+Launch C3: 106.00668452631933 km²/s²
+||V∞_in||: 0.03497451754155979 km/s
diff --git a/archive/ES_0.5981519777527469 b/archive/ES_0.5981519777527469
new file mode 100644
index 0000000..a1b1043
--- /dev/null
+++ b/archive/ES_0.5981519777527469
@@ -0,0 +1,22 @@
+archive/ES_0.5981519777527469---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-26T21:52:11.031
+Launch V∞: [6.911438956695627, -6.46372187482994, -0.0539990769561579] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.03791031676833e-7, -1.0316176236110757e-6, -1.0443973110013281e-7] km/s
+ V∞_out: [9.006799954177279e-8, -4.5919965381427304e-7, -1.1611097200488487e-6] km/s
+ time of flight: 1.4039424668096623e8 seconds
+ arrival date: 2028-10-07T20:16:17.031
+ thrust profile: [1.0 -0.32624834727612406 -0.29572793254114943; 0.654829815386789 0.16480360611475084 -0.4720751246667168; 0.27789910572625764 0.1466743437711769 -0.3327942595157556; 0.14487793021958417 0.1072686073347805 -0.2401471633535569; 0.06704391231387039 0.06087441664747686 -0.141698653413025; 0.04019025129013853 0.042486924565128294 -0.1030092846313379; 0.014999140957103172 0.018056895214164006 -0.04548713578208928; 0.010539434019781722 0.014007210665520655 -0.03626678511181862; 0.002495139801595825 0.0035421763010983227 -0.011158107009364213; 0.0030174904272191826 0.0033643851443641236 -0.00835515317009334; 0.0008796783468604596 0.002589892016258188 -0.0048552170245358146; 0.003479854062376061 -0.0006551324473285892 -0.004483511869029194; 0.002680843526500013 0.0005672320615212902 -0.005148786435434884; -0.004771306593806214 0.004318833553882571 -0.005014911645953424; 0.002276825395764557 -0.0005001141283607032 0.003055931872719308; -0.003183300010099896 0.003671070770921277 -0.0012063729065096428; 0.007330327546278659 0.0006957957715862462 -0.0019219439806944542; -0.0016360787854347765 -0.0025718988827613323 0.004965243577620902; 0.003445037397099623 0.00302234338756423 -0.001848159580496782; -0.003274054770181941 0.01065444821549973 0.0047366202619951265] %
+
+Mass Used: 175.46544588388815 kg
+Launch C3: 89.55060482759713 km²/s²
+||V∞_in||: 1.2531817087102622e-6 km/s
diff --git a/archive/ES_0.5982068067212952 b/archive/ES_0.5982068067212952
new file mode 100644
index 0000000..f0bafc7
--- /dev/null
+++ b/archive/ES_0.5982068067212952
@@ -0,0 +1,22 @@
+archive/ES_0.5982068067212952---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T23:27:32.973
+Launch V∞: [6.918394825581146, -7.233609179462674, -1.3669062401425232] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00722787543040675, -0.02125095920145806, -0.04526167768963136] km/s
+ V∞_out: [-0.04345859007386818, -0.007300778357790125, 0.02469410749977047] km/s
+ time of flight: 1.2644184427811788e8 seconds
+ arrival date: 2028-05-09T10:11:36.973
+ thrust profile: [0.413899737675993 -0.17158831619273845 -0.2061026961010861; 0.14882796479866775 0.007754631204378096 -0.16956815939401512; 0.14596759374806334 0.03713621738775954 -0.25844479820831195; 0.11426023647518091 0.04272970458039185 -0.27106179522604434; 0.05609487063534826 0.025483039231953032 -0.16677377067860216; 0.025762130467566372 0.01282325344082042 -0.09176511409716542; 0.039818627999377 0.022956945303574235 -0.15128572714217856; 0.03300470929420637 0.020036403103071268 -0.13731236992908924; 0.006603223049351581 0.003688540045187687 -0.031209083576143083; 0.002352198917156097 0.0014080888510768627 -0.014818766123511453; 0.0062079525836866226 -0.0010051432556635906 -0.0058606697909034; 0.0008313722887524593 -0.0047477201017454935 -0.001487323587011191; -0.0009476400544963862 0.006597640421987057 -0.008007240220984497; -0.005031979359019497 0.003597719414887907 -0.008786032891982236; -0.003931123868945837 -0.003701333389873453 -0.011090090223053007; 0.0036190350322340375 -0.0018044888568931276 0.00735377868716045; 0.006446614904011011 0.0006379929513190484 -0.013203410488330885; 0.0032477641792464894 0.00837037065678827 0.0007058598970322866; 0.003770993648941307 -0.005690511724481475 -0.0020179873497572754; 0.00947069582607907 -0.00932243620416881 -0.0032153437348800213] %
+
+Mass Used: 102.57123304798915 kg
+Launch C3: 102.0577213931752 km²/s²
+||V∞_in||: 0.05052192511672121 km/s
diff --git a/archive/ES_0.5982428022915881 b/archive/ES_0.5982428022915881
new file mode 100644
index 0000000..937d857
--- /dev/null
+++ b/archive/ES_0.5982428022915881
@@ -0,0 +1,22 @@
+archive/ES_0.5982428022915881---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T04:28:06.857
+Launch V∞: [6.964102241495984, -7.213954519365799, -0.9855597777793474] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.244897182727895e-5, -0.000137449765881311, 0.00021432709951248096] km/s
+ V∞_out: [0.00010956271072164041, -0.00020826002386819953, 0.00013379503795696713] km/s
+ time of flight: 1.2766283933328502e8 seconds
+ arrival date: 2028-05-23T18:22:05.857
+ thrust profile: [0.3974542524837446 -0.1715159693704761 -0.2052313407899532; 0.11178554919612052 0.0022580200406941385 -0.13694807765307737; 0.11178025444428921 0.022376534416535185 -0.21529935347619766; 0.10114342914015148 0.03042839029702654 -0.2609324237942659; 0.11211377807159058 0.039644776494405544 -0.3537593573171522; 0.04422498149888246 0.018108134262368385 -0.16567288279559053; 0.031438546296959156 0.013887072934593181 -0.13417025792121515; 0.01036864933555085 0.0047413872355253775 -0.04963985489176474; 0.0036371527228002618 0.0038245440337382275 -0.03365920823273222; 0.0020360775050874344 0.0011376426551912733 -0.010330652606620732; -0.0007070811897572581 -0.0035178574516612254 -0.0036982440522238926; 0.0002723144772297714 0.0020094290946226284 -0.0015294483115102812; 0.0005174274884007 -0.007838269462592064 0.003829194033106568; -0.00605317379842396 -0.0014227916993050705 -0.008398642167155464; 0.002020781653253725 0.01003013957451827 -0.007108163294038546; 0.013801094195027983 0.007281764657219596 0.0006660078565297596; -0.0008848924719455798 0.0043119541366540655 0.0030385749149680844; -0.00025335431870618754 0.003854375002299795 0.013884279426922939; -0.009052591641979588 0.015619915678547456 -0.011984676823023142; 0.004682182149835904 -0.02361062642972136 0.002523773953281392] %
+
+Mass Used: 105.80133984731219 kg
+Launch C3: 101.5111879130641 km²/s²
+||V∞_in||: 0.00027087885875088356 km/s
diff --git a/archive/ES_0.5982849901109346 b/archive/ES_0.5982849901109346
new file mode 100644
index 0000000..b0aa1ad
--- /dev/null
+++ b/archive/ES_0.5982849901109346
@@ -0,0 +1,22 @@
+archive/ES_0.5982849901109346---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-17T21:07:08.009
+Launch V∞: [5.765590955750343, -7.431394610294562, 0.19765537916069162] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.886126240329825e-6, 9.476424300663753e-7, -2.0212546692040312e-8] km/s
+ V∞_out: [-9.44537930068929e-7, 2.181765834372008e-8, 6.8827063746003225e-6] km/s
+ time of flight: 1.7049941781363446e8 seconds
+ arrival date: 2028-09-11T06:04:05.009
+ thrust profile: [0.8041008453925047 -0.27589928142049525 -0.16887574244269904; 0.37525947185336 0.09846597398297963 -0.22273202822610236; 0.284695266908296 0.16079110477660977 -0.26780039829104973; 0.15716410416897272 0.12533286098032848 -0.20819520460592353; 0.051405654298640274 0.04936835582716407 -0.08652094990231554; 0.06349246637209642 0.07366112824927631 -0.1306813796938049; 0.0037299060421941525 0.009072018892518845 -0.010746720286684629; 0.008981604861366427 -7.37900439298951e-5 -0.00940262290390684; 0.013920260812505547 0.013306382925415326 -0.02404661324299785; 0.003937183545367523 0.015958016168487243 -0.015738639387589074; 0.0031258249684491058 0.003317978125033389 -0.01115672860360669; 0.007597992155588984 0.008312646309288636 -0.004774763395915763; 0.0015180196784893782 0.011375243103035438 -0.01920065099895852; 0.006401088359147093 -0.0015477452016836278 -0.014837774626683956; 0.006315875991275156 -0.04436325596949304 -0.005924982883485329; 0.010403646895284491 0.025603889390510958 0.03489369555774466; 0.002871769455335888 0.0044373157022383316 -0.001175062002603382; -0.01786865439978212 -0.029984013588929735 0.05241193493638647; 0.008727077207765301 0.013568999554626565 -0.014857205219468705; -0.028067362078186005 -0.037140071936095 0.02163832855501009] %
+
+Mass Used: 181.70988179359483 kg
+Launch C3: 88.50673257185638 km²/s²
+||V∞_in||: 6.951055266653032e-6 km/s
diff --git a/archive/ES_0.5983225791675284 b/archive/ES_0.5983225791675284
new file mode 100644
index 0000000..ae45435
--- /dev/null
+++ b/archive/ES_0.5983225791675284
@@ -0,0 +1,22 @@
+archive/ES_0.5983225791675284---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T14:50:48.893
+Launch V∞: [7.410739955824226, -6.598097260385953, -0.33617091134673077] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9898784011835205e-6, 8.619194403630882e-6, 4.342941959252076e-6] km/s
+ V∞_out: [6.718229536199727e-6, -6.516306885647056e-6, -3.8072045266903237e-6] km/s
+ time of flight: 1.5749854748006052e8 seconds
+ arrival date: 2029-05-06T12:26:35.893
+ thrust profile: [0.19466435227480128 -0.04903598712847481 -0.0819946516702128; 0.07709144738164249 0.014555546316139631 -0.09631625776439894; 0.07036628978971893 0.02788771289306502 -0.14484893483102285; 0.061836272296093744 0.03246538329077081 -0.1762274587838413; 0.05122523357249926 0.031067847126277567 -0.18433966344006858; 0.04335697337839737 0.029357645106746124 -0.1851787079111372; 0.01739579787420964 0.009238171683799578 -0.09454291659838257; 0.012839248799106057 0.007492873265839386 -0.08664200083315038; 0.011132515949867444 0.007763146673020802 -0.08443859667758488; 0.0180337513332236 0.02227090677861899 0.00046608725595965246; -0.004622560691910593 -0.026885021069995768 -0.011026482002068745; -0.006103495000391105 -0.006328757371299473 0.022285530176135483; -0.008909571768840401 0.036174512994782936 0.019537183294601898; 0.039579913068326256 0.007373463902466199 -0.0019454798374241213; 0.02997877180788698 0.038316152514129856 -0.02020622674519129; -0.026552021055347888 0.034993398845312225 -0.029503066325646917; -0.03830022612828207 0.038484205383846615 -0.08229651316931313; 0.006309346245924817 0.07318335582780251 0.03413013218170738; -0.03262222861072614 -0.048724648535531725 0.023451011363220916; 0.008662731226298423 -0.017751886615998302 0.09729413668729402] %
+
+Mass Used: 123.06904634212833 kg
+Launch C3: 98.56696503199797 km²/s²
+||V∞_in||: 1.0104010584064028e-5 km/s
diff --git a/archive/ES_0.5983273962230247 b/archive/ES_0.5983273962230247
new file mode 100644
index 0000000..83a09eb
--- /dev/null
+++ b/archive/ES_0.5983273962230247
@@ -0,0 +1,22 @@
+archive/ES_0.5983273962230247---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T05:53:53.477
+Launch V∞: [5.202744710355805, -8.533671105088647, -1.3268020150691169] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0021071813978848454, -0.0013972729126318633, 0.0012966059140731914] km/s
+ V∞_out: [-0.0015029976518713087, 0.0017721635336981757, -0.0016356999100904004] km/s
+ time of flight: 1.2701183219659445e8 seconds
+ arrival date: 2027-05-03T06:57:45.477
+ thrust profile: [0.44173758740871466 -0.310009499335961 -0.24757960889580294; 0.11827673593164424 -0.019240646081889846 -0.14154751957363695; 0.11856149544984163 0.004177906912461441 -0.21134032748820336; 0.09130142636199591 0.013199451522446611 -0.21262497766054583; 0.07833675459699468 0.01695194553044987 -0.2182158234300311; 0.03954779698853175 0.010488909883671965 -0.12901570120818862; 0.04027263678642777 0.012455070112323009 -0.14782242095907988; 0.022121166152170336 0.0077341034547854836 -0.09328324437227793; 0.025717566688983617 0.0092876073314393 -0.1131157224497235; 0.00963835169065387 0.003108037449965503 -0.04333724874546103; 0.001460792864269558 0.000621818018035229 -0.005539593936069647; 0.00025309134646317043 0.0004212851303379856 -0.002937245237817608; 0.0015148696809172474 -0.0006993975072957367 -0.003166760508611634; 0.00010138171061036677 0.0004497611821672404 -0.0025722025678365885; -0.0018749528438441179 0.00444497357687161 0.003463544502434957; 0.00035279716773601016 -0.000363075362500532 0.005231848477961059; 0.0004477267888200649 9.78835408282498e-5 -0.0017432590053874245; -0.002072076778176931 -0.0006414955585424651 0.0060343773219910905; -0.004736784773744255 0.0019067499930970964 -0.001095777893155409; -0.0013656659742288 -0.0008808170766109479 0.005905073840862916] %
+
+Mass Used: 105.07572020431053 kg
+Launch C3: 101.65249863815168 km²/s²
+||V∞_in||: 0.002841438356251326 km/s
diff --git a/archive/ES_0.5983614952628341 b/archive/ES_0.5983614952628341
new file mode 100644
index 0000000..f22b72f
--- /dev/null
+++ b/archive/ES_0.5983614952628341
@@ -0,0 +1,22 @@
+archive/ES_0.5983614952628341---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T12:08:32.634
+Launch V∞: [6.234691109402424, -7.412776318889148, -1.2357913116132542] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.653008401830663e-7, 8.438838467084371e-7, 9.380689989399774e-7] km/s
+ V∞_out: [1.2854043539452602e-6, 8.309938801031214e-7, 2.4939344374250876e-8] km/s
+ time of flight: 1.7010772898592132e8 seconds
+ arrival date: 2028-09-09T08:17:20.634
+ thrust profile: [0.506426997967529 -0.19282267799652264 -0.1774181491691947; 0.19012831726494558 0.03893837277060346 -0.17409423589131595; 0.1538400552104348 0.07646922925953978 -0.23103442913779848; 0.11221724416322543 0.07932337417602167 -0.22865288338109543; 0.06275369840297848 0.05503322998404768 -0.15992286391708138; 0.0522282002322299 0.0548664524227372 -0.16205397495930884; 0.015027782217934459 0.017769384963650894 -0.05755995128949702; -0.0010617348676573222 0.0013472023898250967 -0.0041241694497937765; -0.0041483442335153685 0.0029349272716044134 0.0018594233089939032; 0.0121402037800497 0.009303108697132 6.079202149454621e-5; -0.0003645404676771379 0.00032924219904291604 -9.369868139382648e-5; -0.0015211142901271988 0.002531511998491418 -0.006676978383857914; -0.007670508458623546 0.009694009875169388 -0.015025926781558046; 0.0022955332944369074 0.0002279669853333708 0.00103081846480787; -5.601789809324962e-5 0.0008763194020335399 -0.0020817313623553765; 0.028388400612052982 0.015599337746872312 -0.02726099833127351; 0.0008657005064057238 -0.0011034039494317873 0.000738287630865443; -0.02862055397568956 -0.02773649302748853 -0.03187363869295464; 0.0421773913272852 0.030055123578403023 -0.07256143652254131; -0.0062604248002982145 0.0014593984479189688 -0.046087056824217196] %
+
+Mass Used: 141.89287526844873 kg
+Launch C3: 95.34780614940418 km²/s²
+||V∞_in||: 1.5299865808330478e-6 km/s
diff --git a/archive/ES_0.5985553750966206 b/archive/ES_0.5985553750966206
new file mode 100644
index 0000000..8d032a0
--- /dev/null
+++ b/archive/ES_0.5985553750966206
@@ -0,0 +1,22 @@
+archive/ES_0.5985553750966206---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T07:28:27.200
+Launch V∞: [6.760278221285599, -7.31129889572438, -1.2463158183641123] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.08492230263794293, 0.08345555926523161, 0.0060859088539110245] km/s
+ V∞_out: [-0.0916617260149856, -0.04996289003369081, 0.05725866173781597] km/s
+ time of flight: 1.2411486245112169e8 seconds
+ arrival date: 2028-04-12T19:49:29.200
+ thrust profile: [0.5314848745228871 -0.22874822103838308 -0.27241310465818763; 0.3318585413246817 0.012293661380908462 -0.3884285449036383; 0.15458036384311766 0.03534778164625429 -0.2908660132231824; 0.09048630144096724 0.029320443802590572 -0.23317898113503033; 0.05830480360484461 0.023106396578804148 -0.18765517244314597; 0.028488666430237182 0.012436632935559537 -0.10904687904789623; 0.015772671997346745 0.007312065109582436 -0.06885212500146684; 0.005328248123054796 0.0024325809605320763 -0.02545860577401632; 0.013684655196358126 0.006386446572162652 -0.06913535992443576; -0.0002702771151784838 0.00014181240767805156 0.00023325553746781063; 0.001093921827176721 0.0005996566565296601 -0.006425549582052087; -0.00010104677032060934 0.00037283965390285095 0.0009225669737778761; -0.000557076095358381 -0.00036614467242128727 0.0024836005707304038; 0.0016116366574282157 0.0005007093295193273 0.001503255307938435; -0.0005799888338078236 0.0007185614859863913 0.0014494469603191327; -0.0037504973926167097 -0.0022960324165816693 0.0007388540652291341; 5.394675729889788e-5 0.0003381928080482674 -0.00014495201199370614; -0.0005738279972542847 0.0028791393357974807 0.0002821266838239849; -0.0004803856623749929 -0.002891685801689105 0.0007451468132048398; -0.00249230717707902 0.0001663249843374386 0.003920260122797262] %
+
+Mass Used: 110.84102591572855 kg
+Launch C3: 100.70975629091353 km²/s²
+||V∞_in||: 0.11922108095542948 km/s
diff --git a/archive/ES_0.5985708803486643 b/archive/ES_0.5985708803486643
new file mode 100644
index 0000000..b752c55
--- /dev/null
+++ b/archive/ES_0.5985708803486643
@@ -0,0 +1,22 @@
+archive/ES_0.5985708803486643---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T23:06:00.246
+Launch V∞: [5.176665949578994, -8.498616219737661, -1.1152955411074585] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.619859413623618, -0.398776369634238, 0.3691961762250679] km/s
+ V∞_out: [-0.5398613743840441, 0.5030720246935244, -0.36789861808576096] km/s
+ time of flight: 1.2677046742128678e8 seconds
+ arrival date: 2027-04-30T05:07:07.246
+ thrust profile: [0.5687784935987774 -0.3893820907244048 -0.2898284548115007; 0.0928247159683622 -0.01408059273263601 -0.11025301409533371; 0.11756945714656993 0.00429102061637079 -0.2009586090713254; 0.06670494867684339 0.011705979715562228 -0.15468193658039647; 0.049947708587009414 0.012517057087616716 -0.1413089533494274; 0.04917583579282467 0.011091563650835166 -0.16499540802781615; 0.06354996053232995 0.017157624028964213 -0.20834835916241706; 0.029523625256639447 0.011468567208100262 -0.12063949963875116; 0.028389123433030784 0.01458537236308825 -0.126756692276581; 0.033033906774850276 0.01396311030559254 -0.14317439866695397; 0.0003903024208167359 0.0001384397020170784 -0.001937922530812329; 0.0001508019762832374 3.5856081371827696e-6 -0.000838172630294128; 7.398671902041236e-5 0.00023157409119540031 -0.00024458947856037186; 2.5310246892334146e-5 0.0004426678501375594 -0.0010026794497169785; -2.5783382947658048e-6 9.656711550043082e-5 -0.0010232160757872627; 0.00028665015780126213 0.00010269996459538917 -0.0004630705747940186; 0.00026294831119170233 -0.0013050892247959372 -0.00010440803294442405; 9.92741233966064e-6 -0.00012250235346467097 -0.0005281213684638763; -0.00011898977281679386 -0.00010499076698693578 0.00045065567552119313; -6.600620537706559e-5 -0.0001221734758961684 0.00016914567001281313] %
+
+Mass Used: 113.43467287716703 kg
+Launch C3: 100.2682321479328 km²/s²
+||V∞_in||: 0.8243507155183947 km/s
diff --git a/archive/ES_0.5985926001231624 b/archive/ES_0.5985926001231624
new file mode 100644
index 0000000..212dfb5
--- /dev/null
+++ b/archive/ES_0.5985926001231624
@@ -0,0 +1,22 @@
+archive/ES_0.5985926001231624---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T11:29:29.794
+Launch V∞: [6.985623934294317, -7.111472091302516, -1.5823999636971693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00812554849117714, -0.022497067408455966, -0.0478648923800933] km/s
+ V∞_out: [-0.0466693025303671, -0.007652156726708057, 0.025027436671249945] km/s
+ time of flight: 1.2526102691619231e8 seconds
+ arrival date: 2028-04-24T06:13:15.794
+ thrust profile: [0.46030609888635016 -0.20541568317598297 -0.24028521146221732; 0.2155546919021136 0.010794790150872303 -0.24201664021205316; 0.14205782482757565 0.03756627012341658 -0.25091240280503707; 0.10881284522399273 0.04276198089638569 -0.2580260196203469; 0.0748931468608537 0.03630448790473356 -0.21979100269157348; 0.0411094650068248 0.022789142753543396 -0.1426623883989226; 0.021656578338103673 0.01283357147534485 -0.0852516055288537; 0.011595845465055113 0.008512277264434265 -0.04998707390827107; 0.0050572806720306975 0.0038284731460709555 -0.02942142942832111; -0.0028457507252150935 0.0014664443570219508 -0.0065671741522973105; 0.0028923350297858025 -0.00014540863609357807 -0.006723374922084555; 0.0020928613153572513 -0.0016158326732205986 -0.004205269649236993; 0.006598818256114946 -0.0008430473317130648 -0.0055810949320911855; -0.00030502286320169963 0.007087357042565152 -0.003720836154592574; 0.0031441131028526245 -0.0006843569932289285 0.002457374957176683; 0.00323669919478288 -0.0032463815309950496 -0.004935417307641571; 2.2384466193320026e-5 -0.00010754630603107627 -0.0012933216920473466; 0.00166683060521809 0.0019699718610872484 0.0021184876502956555; -0.008195336302979507 0.0018522754986495314 -0.004837377029115207; -0.008518053585134872 0.008949603241500483 0.0006253667726429895] %
+
+Mass Used: 104.08156104945374 kg
+Launch C3: 101.87596670186899 km²/s²
+||V∞_in||: 0.05350878902405656 km/s
diff --git a/archive/ES_0.5986067796567638 b/archive/ES_0.5986067796567638
new file mode 100644
index 0000000..b17a445
--- /dev/null
+++ b/archive/ES_0.5986067796567638
@@ -0,0 +1,22 @@
+archive/ES_0.5986067796567638---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T08:30:41.008
+Launch V∞: [5.240402806755151, -8.541351304331615, -1.2198622984172507] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.6976057099199e-6, -3.4182938420614364e-6, -1.3191288219631661e-5] km/s
+ V∞_out: [6.692310125316013e-6, -9.908881795434798e-6, 1.0099349057530767e-5] km/s
+ time of flight: 1.2700102357592855e8 seconds
+ arrival date: 2027-05-02T06:34:24.008
+ thrust profile: [0.28177588788917945 -0.18770659339984092 -0.15332601691177264; 0.22548103425953855 -0.02563152754977117 -0.23717761276092442; 0.1576215629713342 0.017042434008820505 -0.24645746892499923; 0.12358411603030678 0.029297335680100275 -0.24946681683673752; 0.09769958555743827 0.031942515976345155 -0.23703833954753378; 0.06449824868755982 0.025793080461528922 -0.18115968560349743; 0.03199090481413329 0.013991346690530778 -0.10634638021893887; 0.011744951783950384 0.0055869773321682555 -0.04230759183996897; 0.013694765841164608 0.0060358533455970205 -0.054141763868900884; 0.006474293533572518 0.00412270899994477 -0.023983400361958233; 0.006128012605710843 0.0038859714423048726 -0.01855883568635669; 0.0060266544317307555 -0.002690129692151708 -0.00952170687931705; 0.000856834048085733 -0.002443361128114889 -0.006352455568082673; 0.0006232638072185237 0.003998525182974718 -0.005608335586252018; -0.0010490115142383059 -0.002433907389267783 -0.006679113566434039; -0.0003754125236947086 -0.0016886032317566177 0.0034627625095592076; 0.007057390544467955 0.0002827875974943982 0.003630054005852935; 0.0030949001663077066 -0.004836267073420711 -0.00350699730511167; 0.004618201924010536 0.006514709908083189 -0.003976662210680491; -0.0018589516927347226 0.00425337294931813 -0.011487760983313968] %
+
+Mass Used: 103.93126463532326 kg
+Launch C3: 101.90456770815447 km²/s²
+||V∞_in||: 1.565081312103175e-5 km/s
diff --git a/archive/ES_0.5986111182112066 b/archive/ES_0.5986111182112066
new file mode 100644
index 0000000..84c5ec6
--- /dev/null
+++ b/archive/ES_0.5986111182112066
@@ -0,0 +1,22 @@
+archive/ES_0.5986111182112066---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:51:51.306
+Launch V∞: [6.8632440668733565, -7.324401104062177, -1.3717501183839558] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0030044083904655233, -0.0016376594886373648, -0.0002223192411889302] km/s
+ V∞_out: [0.0026237841124457434, 0.0014445628363670099, -0.0015974910100874276] km/s
+ time of flight: 1.2406080495474406e8 seconds
+ arrival date: 2028-04-12T16:11:55.306
+ thrust profile: [0.45370402041733215 -0.2045985443568357 -0.2504115403762296; 0.20734917583762236 0.00034820281255463755 -0.25704934893571746; 0.1061032455124076 0.019759944154175594 -0.20870424051276973; 0.08437325108851489 0.0243035403971794 -0.22211667814692293; 0.06909114104865063 0.024217736018579305 -0.22391000035423647; 0.04226210626515833 0.017025429174340884 -0.16052669965261138; 0.03412978675130931 0.014767756462477103 -0.1465851064600815; 0.00865244101810191 0.0038869472498127902 -0.04361346590943256; 0.005488269906140299 0.003283163891397904 -0.02881557915433648; 0.0017704581611707607 0.0009255783282763013 -0.00997872439145559; -7.641361134725071e-5 -0.0002556030798249368 -0.0027339318093794257; 0.0002236539165079329 3.2586832490132415e-5 -0.002441141257502959; 0.0003547184337259654 -6.462002727215463e-5 4.680133708634014e-5; -0.001068023056687249 -0.0002164119458339288 0.00039357539243949514; 4.900010596254043e-5 -0.0019077944311832796 0.0007008650933219359; -6.589103951396675e-5 -0.00022606163376062368 -0.0016642497145282656; 0.0008272831083889312 0.0003274265985563221 0.0021152712688223703; -0.0021752979559775147 -0.0009108680645078891 -0.0005001550630459037; 0.000109553965093245 8.478687208730536e-5 -0.0006156375664648315; 0.0025254794231920072 0.0002881279146816468 -0.001650539402452705] %
+
+Mass Used: 99.68906850172289 kg
+Launch C3: 102.63266904194596 km²/s²
+||V∞_in||: 0.0034289683904093447 km/s
diff --git a/archive/ES_0.5986528463095059 b/archive/ES_0.5986528463095059
new file mode 100644
index 0000000..1ae50bd
--- /dev/null
+++ b/archive/ES_0.5986528463095059
@@ -0,0 +1,22 @@
+archive/ES_0.5986528463095059---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T16:34:51.487
+Launch V∞: [6.790865481553807, -7.174334374451076, -1.3725466286350656] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9439505639484004e-6, -3.096510326689972e-5, 4.457570148525192e-6] km/s
+ V∞_out: [-4.8124938837210106e-6, 1.8890634513876083e-5, 2.4640042116496113e-5] km/s
+ time of flight: 1.2261443969301781e8 seconds
+ arrival date: 2028-03-24T20:08:50.487
+ thrust profile: [0.7053725370615991 -0.31527689830836453 -0.3497557209178022; 0.2967414036641203 0.008210918895457692 -0.32241591146367876; 0.18838317233184182 0.04347864446180019 -0.3197957185299845; 0.12484658140309415 0.04383596656731288 -0.28437429279735044; 0.08085195478955838 0.03505302142476021 -0.22852634901941382; 0.00998959051957153 0.004972937708244582 -0.03716426503987571; 0.01593122702748507 0.009110394894044964 -0.061008400292615304; 0.011169384540054441 0.006586291332256533 -0.05213976911131546; 0.007124923616282812 0.004493338995584689 -0.03163179791883278; 0.0014428541627682981 0.0010240343007048886 -0.008023795256368937; 3.533597340346211e-5 -6.152273478726242e-5 -0.00014619835225383916; -7.872472273815921e-5 6.639618436123405e-5 -0.00021325189032055753; 7.98017999161188e-6 -2.6225603834559537e-5 -0.000649871410102955; -0.00011954970223022172 -0.00011297855844015427 -0.0008730083561750029; 0.00027065146336980954 -0.0001462695287708578 -0.00030965085327219614; -8.618584837945714e-5 6.500586348622347e-5 -0.0002474576675454122; -0.00019884154089658994 -1.371388791753062e-6 -0.0010074361878138686; -0.0001396175415035103 0.0001638568833418929 0.0001230792912404094; 1.392656056073329e-5 2.529941482386699e-5 -6.351870396463112e-5; -0.0006256422766060142 -0.0003129722247783176 0.0002773845256530069] %
+
+Mass Used: 118.18191763661707 kg
+Launch C3: 99.47081195276682 km²/s²
+||V∞_in||: 3.142251417187617e-5 km/s
diff --git a/archive/ES_0.5986586580249758 b/archive/ES_0.5986586580249758
new file mode 100644
index 0000000..14bb7b9
--- /dev/null
+++ b/archive/ES_0.5986586580249758
@@ -0,0 +1,22 @@
+archive/ES_0.5986586580249758---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T15:04:16.108
+Launch V∞: [5.265121722879929, -8.241543304660084, -0.866989162702637] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0016176979167900664, 0.0009894914426390414, -0.0008802424732416584] km/s
+ V∞_out: [0.0012040765278016046, -0.0014789532982123342, 0.0008496692572421488] km/s
+ time of flight: 1.2800415354955015e8 seconds
+ arrival date: 2027-05-10T03:46:49.108
+ thrust profile: [0.6332862458045747 -0.41428934089818426 -0.2791409126859315; 0.35760274761331046 -0.03222320650429066 -0.32044596488595517; 0.20096600812024007 0.02767882771164066 -0.2708328828223096; 0.1709963023108417 0.04695162657345682 -0.2963626296593271; 0.08701805079007123 0.03299616268771934 -0.18897349721109216; 0.04897026904013178 0.020680134039103043 -0.11829483865235005; 0.03383915618763045 0.020110500879149305 -0.10799601719764113; 0.019467377885175777 0.011883267363046904 -0.06514398562991955; 0.03923486985240049 0.021829454242930875 -0.12597624016115147; 0.0022516404191542283 0.0010749077921422853 -0.005256299318741722; 0.001002860180260202 -0.00024015842362721867 -0.00029044588025501023; 0.001602158896857782 0.0013728670767129416 -0.0077874549189613975; 0.00034417918961580793 0.0007454699719835518 0.0002884165722750981; -0.0030878549111378424 -0.0015034303139348755 0.0007516774526733554; 0.0031573359039019375 0.0004682569943524592 -0.00040763108463680016; 0.0003407806277742121 0.0010636901377173839 -0.0008639725926481212; 0.0003573659480624028 -0.002742718172795298 0.0010440896984389783; 0.002279313733317458 -0.006980730422114462 0.0008020332419956317; -0.0018414067317347876 -0.002655191993346414 -0.002677340580065101; -3.3624253539097813e-6 -0.002387759322902335 0.0007652799351370618] %
+
+Mass Used: 136.12385848496024 kg
+Launch C3: 96.3962130075734 km²/s²
+||V∞_in||: 0.0020906617796146282 km/s
diff --git a/archive/ES_0.5986939385377901 b/archive/ES_0.5986939385377901
new file mode 100644
index 0000000..69b993f
--- /dev/null
+++ b/archive/ES_0.5986939385377901
@@ -0,0 +1,22 @@
+archive/ES_0.5986939385377901---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T14:07:35.102
+Launch V∞: [6.851303691578958, -7.267769998644214, -1.3927418927296953] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003506545067142969, -0.005353215374814117, -0.0020548363290666502] km/s
+ V∞_out: [-0.003773890931666329, 0.004786414087847798, -0.0025084876233438373] km/s
+ time of flight: 1.2497219757018319e8 seconds
+ arrival date: 2028-04-23T00:37:32.102
+ thrust profile: [0.5971410134709557 -0.2567478087655488 -0.3044207547941086; 0.12317876276893887 0.0034601709470618775 -0.14990092798840848; 0.08681981585786161 0.018939903721290216 -0.1659873073137941; 0.06208791596538946 0.020590300793646033 -0.15876312149252148; 0.05377066060230741 0.023241938202550695 -0.17494865877660648; 0.040582046541717716 0.01855789641900417 -0.16079333250681152; 0.03634626316152526 0.017391763928696347 -0.156638425349386; 0.018982347356666207 0.00923875716946143 -0.09016416754103804; 0.029993149092489065 0.01616658572067459 -0.15334752850641062; 0.0110905216857121 0.005857467227131326 -0.05981534867969696; -9.247800592963222e-6 0.00030005681633175706 -0.004959354955018858; 2.5246918650030973e-5 -0.0003492634130231048 -0.0009557127237180046; 6.743681560412532e-5 -0.0008142381902967264 0.0004277711029651277; 0.00044426048287979575 -1.5210229345307961e-5 -0.0005357973630345962; 0.0009199614750635191 0.00021898696408164195 0.0027765154859527292; -2.29670501512281e-5 -0.0001339191943840112 -0.0007829586546411874; 0.00017613766958962237 0.0012943844322676125 -0.000845000068999049; 0.0001426145661550974 -0.00014351692571131966 -0.0013449136758243707; -0.0007462939592298595 0.00024366961934695308 -0.0006417014916395101; 0.0007253633566101306 0.0028863895891480117 -0.0018969176187018013] %
+
+Mass Used: 105.22291908541774 kg
+Launch C3: 101.70057300720067 km²/s²
+||V∞_in||: 0.0067212443413629175 km/s
diff --git a/archive/ES_0.5989991042638805 b/archive/ES_0.5989991042638805
new file mode 100644
index 0000000..96f518c
--- /dev/null
+++ b/archive/ES_0.5989991042638805
@@ -0,0 +1,22 @@
+archive/ES_0.5989991042638805---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T21:05:19.330
+Launch V∞: [6.2474214021130745, -8.067240723265066, -0.8347870641855368] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.7602493834372487e-6, -3.2049034128934805e-6, -4.190962903884704e-6] km/s
+ V∞_out: [-5.357905030365592e-6, -3.6416172805128577e-6, -1.1271009127420109e-7] km/s
+ time of flight: 1.824043666701237e8 seconds
+ arrival date: 2029-02-18T00:58:05.330
+ thrust profile: [0.04949144048809151 -0.02753430002654548 -0.03259192592010108; 0.0076551174543095625 -0.009034200543099804 -0.005588525824221991; 0.030659741541326734 -0.018565050645622815 -0.11425631765619562; 0.029069747565192375 -0.024858606932824732 -0.1483164247707209; 0.02866924790625323 -0.03116625548389966 -0.17758061680512108; 0.022833371461126614 -0.028825789170603053 -0.16159727375521196; 0.014988484307794054 -0.021008093027653208 -0.11785744272597648; 0.008329494723808385 -0.013004876119662927 -0.07347404660500387; 0.0007739291693410899 -0.0037364848817186963 -0.013205957942475213; -0.004393306324843696 0.0055292475381934925 -0.007542338522283197; -0.009499547912520353 0.0018822234490810802 -0.005524954969564207; -0.0026553975451405415 0.01074125897220953 -0.0044059804330134145; -0.007042131305106356 0.005264159361039049 -0.003233487114974675; -0.01983608877654345 -0.010593947762147438 -0.0026471128928277124; 0.014988995031183637 0.010294861146459708 0.03438138878008516; 0.02961426193038183 0.015716730331016976 0.018306343954408073; 0.001340575129297307 -0.031984663204170156 0.0024855731014599937; -0.00690118929740849 -0.0028264774631946397 0.03354901019181288; 0.010178529353082152 -0.03279625505965856 0.06624231139704183; -0.007586255491724788 0.0057910226043832915 -0.006210986190269121] %
+
+Mass Used: 87.45510869408736 kg
+Launch C3: 104.80751650521826 km²/s²
+||V∞_in||: 6.478815584144543e-6 km/s
diff --git a/archive/ES_0.5991457873583721 b/archive/ES_0.5991457873583721
new file mode 100644
index 0000000..58c3205
--- /dev/null
+++ b/archive/ES_0.5991457873583721
@@ -0,0 +1,22 @@
+archive/ES_0.5991457873583721---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-29T05:03:45.690
+Launch V∞: [6.894018331539838, -6.670558855782909, -0.4908221619892425] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00028812557032546846, 0.0001957104939371217, 0.011920698230619524] km/s
+ V∞_out: [-0.010967477645898508, -0.004259484278187728, 0.001913936781759534] km/s
+ time of flight: 1.3201851587665051e8 seconds
+ arrival date: 2028-07-05T04:52:20.690
+ thrust profile: [0.9928616767222912 -0.35302958851510224 -0.3322308853033288; 0.46235132799627154 0.08130356883329344 -0.36890104953631236; 0.2263588487803102 0.10000346416162303 -0.2907939471181301; 0.14334591124110968 0.08981552536896407 -0.2521234403871596; 0.08234018367988621 0.06404531068229623 -0.18614025911102164; 0.04261996107371319 0.038850445881000985 -0.11844562075909089; 0.023845160528623916 0.02149446779607285 -0.07172482625140694; 0.02558897033725825 0.026801346956111364 -0.0882117359740128; 0.01884449329560733 0.021663968779192185 -0.07475806978385467; 0.0027670751767013627 0.0030389786429611495 -0.013627474227451407; 0.007708540719874245 0.008898270287502615 -0.03449997075183284; -0.00045871677493380773 0.00025369975175076 -0.0014075955523061366; -0.0012170303583389393 -0.002046421182688242 0.002105640519423737; -0.0015232451647321857 -0.0007851961100236174 7.029709019514799e-5; 0.0008100597656400564 0.0005794022523737733 0.0011647091559395003; -0.0012689440852218122 0.0014389801378663367 0.0018360374593221736; 0.0026685009846480374 -0.0004821322432083065 -0.004587376127676205; 0.001138814613485767 0.0021164713775399507 0.0007224653241856983; 0.000714093031057949 0.00038174300763375065 -7.733711047039978e-5; -0.0008253519316542174 -0.0014915002979011978 -0.0009412700141427472] %
+
+Mass Used: 160.7923734252704 kg
+Launch C3: 92.26475059877093 km²/s²
+||V∞_in||: 0.011925785728714394 km/s
diff --git a/archive/ES_0.5991809033842304 b/archive/ES_0.5991809033842304
new file mode 100644
index 0000000..8733491
--- /dev/null
+++ b/archive/ES_0.5991809033842304
@@ -0,0 +1,22 @@
+archive/ES_0.5991809033842304---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T14:43:19.017
+Launch V∞: [5.136342433789489, -8.55222762348232, -1.3273318190697085] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.06206734341856261, 0.030204610928978814, -0.06926749615005712] km/s
+ V∞_out: [0.06342274693629982, 0.026953133506262546, 0.06938095511094719] km/s
+ time of flight: 1.238111278369049e8 seconds
+ arrival date: 2027-03-26T14:42:06.017
+ thrust profile: [0.44662646209506335 -0.3193325328469056 -0.250851781923931; 0.24744939658934828 -0.04167860525603252 -0.2730248716798363; 0.19677911177525653 0.00698942823695555 -0.3208040931172953; 0.14432252934267004 0.021596312677037637 -0.30559751231050347; 0.08832554306773242 0.01987649746172563 -0.22741209437064966; 0.030665320381381832 0.008677461974850727 -0.0949073501479498; 0.010689497915769803 0.003515955499976541 -0.0387703813957571; 0.01343044870629815 0.004633591279277838 -0.05224284469711237; 0.0063050732309983225 0.002041274415980011 -0.026268620918844094; 0.006044038149716004 0.0025373387269761022 -0.028008457385666173; 0.00010954017299494176 0.0002771394585931576 -0.0012431837863755746; 0.0005678488331852658 -0.00018074241796362826 -0.0012870736692272367; -0.000424816139156574 -8.202967710443953e-5 -0.0006593131351197525; -0.00010627713797255135 -0.00021986764205947823 -0.00036052224383656135; 0.0006513937213597188 0.0006839678314786085 -0.000932869311521351; 6.387028291839682e-5 8.712151024714232e-5 -0.00046527457545983875; 0.00016112720291000816 0.0012584852300524163 0.0003183870270631272; 7.392496558837825e-5 0.0004645491635502263 -0.0011798532512912662; 0.00015193225704898195 0.00018397623599230429 -0.0019198390041330815; -3.056725348256047e-6 4.369808567414497e-5 -5.2022064848675784e-5] %
+
+Mass Used: 108.21859998792843 kg
+Launch C3: 101.28442067891548 km²/s²
+||V∞_in||: 0.09778885244907495 km/s
diff --git a/archive/ES_0.5992096463376915 b/archive/ES_0.5992096463376915
new file mode 100644
index 0000000..40d6a28
--- /dev/null
+++ b/archive/ES_0.5992096463376915
@@ -0,0 +1,22 @@
+archive/ES_0.5992096463376915---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T01:21:17.808
+Launch V∞: [5.526780288757444, -8.396173966500028, -2.5487775660892105] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.635484900229575e-6, 2.242128388078699e-6, 4.3997651934303995e-6] km/s
+ V∞_out: [-2.7540754024200216e-6, 4.769452941969774e-6, -3.945736029579941e-6] km/s
+ time of flight: 1.3212908593466939e8 seconds
+ arrival date: 2027-07-01T07:52:42.808
+ thrust profile: [0.15150800760623334 -0.11741002187847568 -0.10595214238353973; 0.09189218592558765 -0.01864274469914185 -0.13977688921548873; 0.06929066299627686 -0.000848088262025098 -0.16716444806911301; 0.0538147240495583 0.005002509358548839 -0.17587170084043774; 0.04249942967886129 0.006902932028327731 -0.17268096016556383; 0.03198557578289044 0.0072259029076712075 -0.15267857443798874; 0.022422933975251087 0.006498835837866391 -0.12096928760797608; 0.013820713023228697 0.004942216095582018 -0.0822227194259518; 0.0073924507403355265 0.0033271514937765084 -0.048711518234119976; 0.0019331005516376137 0.0009473536175712625 -0.013333794376588022; 0.0003506734881117731 -0.0002494884244852475 -0.0010166673662445756; 0.0002480388668826417 -0.00032345469579598673 -0.0007982788532820354; 7.581603221462275e-5 -5.193832119157867e-5 -0.00035858091483331213; 0.0002837308086183737 8.450151301796872e-5 -0.000569837850517104; 0.0005013595300941225 -0.0006842926805427772 -0.0007222905706286508; 1.25545935752078e-5 6.854131859745496e-5 -0.000868236752399392; 0.0007459615137347453 -0.00036780296233088823 0.0003854086801323713; 0.00010189825052189219 -8.310417765836184e-5 -0.00013396869743851898; 5.1166147239670656e-6 0.0004903784794466368 0.0012412152149844607; 0.00035863679342035184 0.0004939068479473858 -0.0005291609710345807] %
+
+Mass Used: 71.77697654288022 kg
+Launch C3: 107.53730471733026 km²/s²
+||V∞_in||: 6.772945720010343e-6 km/s
diff --git a/archive/ES_0.5992111513324264 b/archive/ES_0.5992111513324264
new file mode 100644
index 0000000..2b286a3
--- /dev/null
+++ b/archive/ES_0.5992111513324264
@@ -0,0 +1,22 @@
+archive/ES_0.5992111513324264---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T09:59:05.148
+Launch V∞: [5.241858839152541, -8.603570082767353, -1.6249422712188244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.038088064512798614, 0.031458757690160336, 0.032465838610435116] km/s
+ V∞_out: [-0.028326609438025546, -0.04251796931078148, 0.029730469848357435] km/s
+ time of flight: 1.2453378262372766e8 seconds
+ arrival date: 2027-04-04T18:42:07.148
+ thrust profile: [0.3353897368255639 -0.23862129405745205 -0.1983440938035086; 0.1281677538397507 -0.021378038869630852 -0.1555922608075841; 0.11142862762988325 0.004135596339369866 -0.20011973350205486; 0.09203858624157021 0.014168550081087326 -0.2144806402569531; 0.11219785143993988 0.0246636065940947 -0.30487957033364693; 0.07204940184698272 0.01928520506286245 -0.22850964354667805; 0.013476486758291932 0.003991348864825883 -0.051129979802600506; 0.007395855260333477 0.0024832690964221482 -0.031316683439817285; 0.012105489951641903 0.003038639535671754 -0.056964569935063755; 0.0012913407809352056 0.000486942129841489 -0.006403333566913525; 0.0005216543668741347 0.00017866017701333208 -0.002216034057083558; 0.00026706338333028093 9.138002010847991e-5 -0.0014385396141667853; 1.759116443098951e-5 3.810261879920256e-5 -9.636776937160227e-5; -8.346412173351877e-5 0.0004963678616094637 -0.0002486516929714015; -0.00025985354445432667 -6.915537801034218e-5 -0.00026393909769527487; -0.00026488124618793605 -0.00030785869929688715 -0.0003066832974831223; -0.0006833091291738422 -0.00011368609289182319 -0.0006827190439627869; 0.0003796839036405757 0.0004821521383753714 0.00021032682119906282; 0.0002071990123347505 -0.00022247704079207296 -0.0011332517910338181; 5.9096013447060595e-5 0.00014212706254076833 0.0002431400522833037] %
+
+Mass Used: 91.60252863416918 kg
+Launch C3: 104.13893964348486 km²/s²
+||V∞_in||: 0.059113321429421904 km/s
diff --git a/archive/ES_0.5992159529810388 b/archive/ES_0.5992159529810388
new file mode 100644
index 0000000..bc041c7
--- /dev/null
+++ b/archive/ES_0.5992159529810388
@@ -0,0 +1,22 @@
+archive/ES_0.5992159529810388---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T14:50:17.682
+Launch V∞: [5.158386839940779, -8.447881171932783, -1.307115212999274] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.057856351293094216, -0.0008501032206261111, 0.04589361548385528] km/s
+ V∞_out: [-0.07235420794516043, 0.0005546065517560757, 0.014629994342044938] km/s
+ time of flight: 1.2347590022116846e8 seconds
+ arrival date: 2027-03-21T17:41:57.682
+ thrust profile: [0.608123179447982 -0.4363969265967851 -0.33742539950438; 0.24118685786405342 -0.0403476856423528 -0.2667845173718201; 0.18446026175988836 0.007368708630582928 -0.30196628393331965; 0.14748641944146643 0.02309345149665805 -0.3124570966148996; 0.06689697270614918 0.01577088576234645 -0.17577865763909367; 0.0601474482917046 0.017576772032799042 -0.18042116668113223; 0.009044090915263828 0.003141456787926879 -0.03377820430735577; 0.008932535956598058 0.0034273443799387026 -0.037410549323775376; 0.005351699350980903 0.002797317048825311 -0.02812898153208307; 0.005858063296804965 0.002923054610984397 -0.02130181722625558; 0.0001852967205235357 -6.46829264513766e-5 -0.0006933029462258668; -0.00024723034607541965 0.00021416958100468417 -0.0001805537487466617; 8.27606462388722e-5 -2.12886990114691e-5 -0.00033717625053212956; -5.850790841525063e-5 0.00014266705408869248 2.352007765532521e-5; 5.376557110783466e-5 -4.4994847610816384e-5 -9.190493047749309e-5; -8.730766597808888e-5 -3.0581749270460466e-5 -0.0002726392550571851; -0.00010275969550365759 0.00015247928707120423 -0.0001641549991612895; 0.00011065631371251115 0.0001055012743336563 -0.0002207048454945387; -0.0010887605875989882 -0.000501125683816588 -0.00040073917179225485; 8.069864049229725e-5 2.31936395609201e-5 -0.0002695672387692835] %
+
+Mass Used: 117.5941044284009 kg
+Launch C3: 99.68420126562476 km²/s²
+||V∞_in||: 0.07385325993221697 km/s
diff --git a/archive/ES_0.5993859435975466 b/archive/ES_0.5993859435975466
new file mode 100644
index 0000000..8d7db46
--- /dev/null
+++ b/archive/ES_0.5993859435975466
@@ -0,0 +1,22 @@
+archive/ES_0.5993859435975466---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T00:21:57.464
+Launch V∞: [6.942701462644465, -7.349996504635006, -1.8278973462519703] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0037274670470788594, 0.02392419199034287, 0.003652521028534153] km/s
+ V∞_out: [0.023029991728284214, -0.004807086462871893, 0.006788292942116456] km/s
+ time of flight: 1.2410253482909894e8 seconds
+ arrival date: 2028-04-13T09:17:31.464
+ thrust profile: [0.2804210382129802 -0.1189328659233723 -0.15463571336566237; 0.17386013288939775 0.006105753828407551 -0.21038927738575028; 0.1142752172447953 0.02611733099015187 -0.21781677312875963; 0.08201122328998675 0.027938969409006923 -0.21069746934690056; 0.05384760889123144 0.022112419301025973 -0.1728830330425638; 0.029308474193326627 0.013302119562136193 -0.11356414014331623; 0.01841287674322346 0.008884371925274031 -0.0821157813855865; 0.026484828761730327 0.014072559612659961 -0.12496633044994283; 0.0054353972230863825 0.0035853156780190245 -0.03242036933521141; 0.0031240561503031007 0.0022770071155636 -0.018381060354790636; 0.00466419782094518 0.0029079968870824656 -0.02840266993859852; 0.0001645581012013649 0.00015190913414122573 -0.00174655907070976; 0.00011107596656380542 8.181732544394038e-5 -0.0008296256049900222; 9.678086458314724e-5 -0.00019958065473880038 -0.000417925404158987; 8.81380195903063e-5 0.00017078570270263408 -0.00044134927249415805; -0.00039508431828992293 -0.0003442127299920208 -0.000593838993199177; 0.00021458784003263788 -6.400448443040924e-5 -0.00015568294592449214; 6.75288956625428e-5 -3.096551460227191e-5 -0.0004442356572418511; -6.558621629876447e-5 -1.9889119360718072e-5 2.61491894946429e-5; -5.035751797464819e-5 -9.178444768066221e-6 0.0002004743801424225] %
+
+Mass Used: 83.48916212887798 kg
+Launch C3: 105.56476092598739 km²/s²
+||V∞_in||: 0.024486769546874267 km/s
diff --git a/archive/ES_0.5994336160622684 b/archive/ES_0.5994336160622684
new file mode 100644
index 0000000..830032f
--- /dev/null
+++ b/archive/ES_0.5994336160622684
@@ -0,0 +1,22 @@
+archive/ES_0.5994336160622684---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T09:44:33.144
+Launch V∞: [6.958746050750891, -7.28681658688551, -1.4373354635145432] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003930630988231351, -0.0061549944405772695, -0.0023024097890985223] km/s
+ V∞_out: [-0.004388031776405925, 0.005540731818021872, -0.00293867920985069] km/s
+ time of flight: 1.2384094270192859e8 seconds
+ arrival date: 2028-04-09T18:00:15.144
+ thrust profile: [0.39942392363337753 -0.17515309416709016 -0.2189126975556924; 0.14249848098486617 0.002423341103418647 -0.18083904129800224; 0.116204392551405 0.023832588862760237 -0.22824383566458148; 0.07931456790541075 0.02372751212241348 -0.21194772377288437; 0.0525738196290669 0.019466431078934903 -0.17239786621580938; 0.053370962589811013 0.021270891428420688 -0.1997664160899521; 0.027505475163947756 0.012562580208732303 -0.12140994183879023; 0.014604269297034917 0.006882517818283089 -0.07109003129110758; 0.01369540339821729 0.006785531204794758 -0.07175791066666942; 0.0065234790055494095 0.0028326261739431225 -0.03486148699003512; 0.0032240496321616465 0.0016379816388720806 -0.01870827044402656; -0.0003783557277377285 2.8595373203905693e-5 -0.0017155649063309618; 0.00027869118074856945 -1.9376597571821303e-5 -0.0001440900172165855; -0.0007483997952411014 0.00011129647377013971 -0.0011246229588077318; 0.000861919748458388 -0.0002987802960050477 -0.000494614044787326; 0.0005934583879486188 0.00016596211331868708 -0.00010029083614545263; 0.0007359506717537967 -4.974483599299185e-5 -0.0013886167169704954; 0.0002454742069543156 -0.0010412522449122267 -0.0016984340841128716; 5.227083221432226e-5 -0.0004024259614220561 0.0006803858728623889; 0.00019279625574503698 0.00012958550255825606 -0.0003443835524107766] %
+
+Mass Used: 95.07719321348623 kg
+Launch C3: 103.58777580442748 km²/s²
+||V∞_in||: 0.007657343362166696 km/s
diff --git a/archive/ES_0.5994822563370993 b/archive/ES_0.5994822563370993
new file mode 100644
index 0000000..be2adc1
--- /dev/null
+++ b/archive/ES_0.5994822563370993
@@ -0,0 +1,22 @@
+archive/ES_0.5994822563370993---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T12:58:45.728
+Launch V∞: [5.124720209962984, -8.50019016952248, -1.3073174187719718] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.44221020335132416, -0.2819795219433783, 0.2632536529263409] km/s
+ V∞_out: [-0.3827991760868826, 0.3553684417922819, -0.2676374390361384] km/s
+ time of flight: 1.2484907988225591e8 seconds
+ arrival date: 2027-04-07T13:16:44.728
+ thrust profile: [0.5384497612118461 -0.3897635123768337 -0.30660404886136594; 0.20878347627141935 -0.03664596117734242 -0.24390699730494275; 0.19468640252728572 0.0047230772967786555 -0.33546097863783514; 0.13776127315617512 0.018945614418007538 -0.31143690835800253; 0.07683896013014474 0.016730055540273795 -0.21552127954742342; 0.024589825138908537 0.006412417806334509 -0.08070679286872477; 0.016066473714314227 0.003862285826107704 -0.05943431354554541; 0.007908004050221462 0.0018313865484550333 -0.031937948901728325; 0.007023537200749181 0.002664237477480572 -0.03373551432086069; 0.0005915291745425467 -0.0013050651781010007 -0.0045997977028861825; 0.00250323547644085 -0.00011031911344262292 -0.0092172285987594; 0.002333018704485554 0.003030325593303005 -0.00433787349519738; 0.005147149829534907 0.003142071598035646 -0.0018736259091763218; 0.00262346786071519 0.0017144048366105587 0.0007182463467450234; -5.431035408202795e-5 -0.0053528723950014906 -0.0098353094400419; 0.004360669815550305 -0.0041844065562337 0.002463065005584882; 0.00047327981436929916 0.00035920586319472775 -0.003005907246160657; -0.0019518794737961524 0.006953785012548304 -0.011438066525174973; -0.0046701518776795055 0.0020283512078770206 -0.0023494393200187234; -0.004925088738590884 0.00433182396465368 0.009128008598437463] %
+
+Mass Used: 114.74972999901593 kg
+Launch C3: 100.22506898187426 km²/s²
+||V∞_in||: 0.5868260394039259 km/s
diff --git a/archive/ES_0.5995073566193987 b/archive/ES_0.5995073566193987
new file mode 100644
index 0000000..590aa23
--- /dev/null
+++ b/archive/ES_0.5995073566193987
@@ -0,0 +1,22 @@
+archive/ES_0.5995073566193987---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-26T20:47:12.411
+Launch V∞: [7.349123649218939, -6.357299758505361, -0.426769110183095] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.3991977325651592e-9, 4.021468973138122e-9, 2.0329743646970904e-9] km/s
+ V∞_out: [3.5777526380649435e-9, -3.5238612927901026e-9, -2.106654777448208e-9] km/s
+ time of flight: 1.4638210148086542e8 seconds
+ arrival date: 2028-12-16T02:28:53.411
+ thrust profile: [0.6063801047547058 -0.15917207661538121 -0.16950275466271625; 0.4759961149953566 0.1494318729208779 -0.3456524785296762; 0.2642128368064794 0.165651256499126 -0.3165225987550461; 0.1427587540212567 0.12350504602332911 -0.2392528615425819; 0.07031339906919555 0.07413632919575552 -0.15284439318509574; 0.042498330160916684 0.051962411515109615 -0.11185513242780508; 0.018980381550357816 0.02758000649297998 -0.06234378142974916; 0.005124772302248903 0.008036959279281648 -0.019077075550095423; 0.003385624175897528 0.005860707412841911 -0.014240854032268655; 0.014574867300768292 0.03368020268926038 -0.07314159975315826; -0.000104184876197011 0.0009273760832962845 -0.0022944177040071833; 0.0009218982468857087 -0.00038602226387054117 0.0004560606284191981; 0.00020705084768623204 0.0009197738439554711 0.0003998630074395228; 7.704929288679776e-5 -0.001286750129389684 -0.002528518118727459; -0.0005395606282853585 0.0029613381061359217 -0.002002925718564608; -0.001425125915985785 0.0006577932588769497 0.0017632975126009968; 0.000616134293173895 -0.00011852514466531051 -0.0007306095046734659; -0.00010386324740566978 -0.00193967796845418 2.8677478186048006e-5; 0.000672820847631994 0.0016940303323053699 0.004212278482255555; -0.0010247349718412388 -0.00018337512727843947 7.746797162302358e-5] %
+
+Mass Used: 147.5510214469191 kg
+Launch C3: 94.60701050440788 km²/s²
+||V∞_in||: 5.105031560076188e-9 km/s
diff --git a/archive/ES_0.5996281078669147 b/archive/ES_0.5996281078669147
new file mode 100644
index 0000000..5ff2a90
--- /dev/null
+++ b/archive/ES_0.5996281078669147
@@ -0,0 +1,22 @@
+archive/ES_0.5996281078669147---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T00:24:58.320
+Launch V∞: [6.958212260833227, -7.177891123396403, -1.330186453692607] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.518435501614669e-5, -0.0001098125735306066, 0.0001817458682222153] km/s
+ V∞_out: [8.703789326435875e-5, -0.00017478703037164062, 0.000112323880593009] km/s
+ time of flight: 1.2906180428648965e8 seconds
+ arrival date: 2028-06-08T18:55:02.320
+ thrust profile: [0.35313458417412497 -0.14882856411352016 -0.17879923667087677; 0.14432461215752648 0.005960952972241493 -0.16608043176792656; 0.14226689484223654 0.033262290054166026 -0.26209408938685125; 0.12191450791563424 0.04194524928012698 -0.30324695529126877; 0.0933860985353457 0.0387946053424587 -0.2865755382416035; 0.036257007776570975 0.01671375787271805 -0.12546595290231768; 0.01377400630734258 0.006512043481056393 -0.04992001349773717; 0.01013569676798938 -0.012858691056754697 -0.025184275435964253; 0.005941843238848258 0.0019141909429420758 -0.012426535362098264; -0.002238740478130283 0.00034159645091215603 -0.012365523739496039; 0.0014008295967599905 0.0007540812810806858 -0.0031543811378454203; 0.0007895862614431434 -0.0004240907424198446 -0.004242801517285118; 0.005074263044643449 0.0012875739266383114 -0.011887162597510428; -0.005754601857583852 -0.0066669053350760085 -0.006084002814651888; 0.03901210292851673 0.010725771048823367 -0.01585083033124762; -0.004776018006901389 -0.010733597662915272 -0.01860789930088765; 0.028218929503309897 0.01492084394236322 -0.03748721596948616; 0.03299558132512431 0.006562127619748614 -0.0017222580235756106; 0.0035529919384135415 0.016587467487796635 -0.0563208580936701; -0.00787611476662084 0.006317101707344034 0.006896799961967107] %
+
+Mass Used: 106.2680892329754 kg
+Launch C3: 101.70823484773003 km²/s²
+||V∞_in||: 0.0002252621787172798 km/s
diff --git a/archive/ES_0.5997331399117586 b/archive/ES_0.5997331399117586
new file mode 100644
index 0000000..fff3ca8
--- /dev/null
+++ b/archive/ES_0.5997331399117586
@@ -0,0 +1,22 @@
+archive/ES_0.5997331399117586---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T16:17:02.782
+Launch V∞: [5.269718829809199, -8.429788295721007, -0.7207798405957383] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001487112137641511, 0.5380893180577437, -0.26977219314368167] km/s
+ V∞_out: [-0.47945549160468487, -0.27292672356719255, 0.23593430395459725] km/s
+ time of flight: 1.2922514253713897e8 seconds
+ arrival date: 2027-05-27T08:09:24.782
+ thrust profile: [0.4044381398104036 -0.27120002537144255 -0.20626103874343582; 0.22842191260619868 -0.02876436762077471 -0.2411996384097507; 0.1514319422666137 0.012404204839846007 -0.24042364637090413; 0.1057015483667008 0.021551438702885128 -0.21978426104704282; 0.05483131370913662 0.015908968789897636 -0.14106668250875704; 0.053507987152072 0.018462603659325696 -0.1577644678129633; 0.03364455093127981 0.01351091924297925 -0.11316828404473572; 0.04401060395383242 0.01971790949979763 -0.15726563802799423; 0.02597162349012859 0.014456195323510852 -0.09899226580133828; 0.013323156606994933 0.0023962904728512674 -0.05973809170099369; 0.008773686191132297 0.008946399485805705 -0.0633713568574883; -0.0009472501439925871 0.0023862300385758583 -0.0033171913048099543; -0.0013381568176992105 -0.0025570103042887636 -0.0047093886651960295; -0.001921774166513852 -0.0004681702013152342 -0.002799496204309271; 0.0009406291823851097 0.0006787365108699044 -0.009557371305311629; 0.012218046517635882 0.006617684995374851 -0.023217489096472206; 0.007585888397287224 0.003104338289703564 0.006675544604554254; 0.018061485782341905 0.00041487326253731433 -0.01945144343964853; 0.01087911420990224 -0.00047349953440723597 0.003297959708156684; 0.009712262586359367 0.007227578467569249 -0.0037568319864655832] %
+
+Mass Used: 120.14238336229482 kg
+Launch C3: 99.35079083452975 km²/s²
+||V∞_in||: 0.6019296984730936 km/s
diff --git a/archive/ES_0.5998447553899962 b/archive/ES_0.5998447553899962
new file mode 100644
index 0000000..f5aca9f
--- /dev/null
+++ b/archive/ES_0.5998447553899962
@@ -0,0 +1,22 @@
+archive/ES_0.5998447553899962---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T03:19:34.644
+Launch V∞: [5.187329847181283, -8.556458584671253, -1.5049392362795044] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.024974327640585808, 0.021346899780534216, 0.02184754386071919] km/s
+ V∞_out: [-0.018622590588788363, -0.029816917166685452, 0.017914526093106797] km/s
+ time of flight: 1.25628082128256e8 seconds
+ arrival date: 2027-04-17T04:00:56.644
+ thrust profile: [0.3960220954681478 -0.28072220305429463 -0.230111628575694; 0.17126328746518632 -0.029389704184153386 -0.20384255273805008; 0.15094834430868118 0.004563948298544828 -0.26626720867950754; 0.11561556626732979 0.016431441580913794 -0.26546641243060676; 0.10747697451951979 0.023342719472082694 -0.29397427691458844; 0.03471536052600072 0.010167706871399104 -0.11622646101789474; 0.0158770280865164 0.005190408477654651 -0.05976474561524449; 0.011587094697821338 0.004492867093325361 -0.04752941243807997; 0.004649961285997002 0.0023020997469404944 -0.020708892528596746; 0.0003959236435187868 0.0005242460820776932 -0.0026366373391597565; 0.0002413114188798784 -0.0008331663197822878 0.0013106805554317417; 0.004570182425050714 -0.0005323684818647924 -0.0042371593951775356; -0.0038188159923949155 -0.0058709389519151795 -0.002100727666282738; -0.007442263988493224 -0.001304368696750954 0.0008681127311751064; -0.01017610071556886 0.0007156010948947856 -0.002784107342638129; -0.0003055047105672442 -0.0003453665124052139 -0.002144245931159404; -0.0025612807363913845 -0.0026111185514708533 0.000446099914930719; 0.012408939056475115 0.010474158068854622 -0.004752838069945361; 0.008254848382250896 -0.0032906714158006047 0.005219098220507787; 0.008809976704915207 0.007084049838264494 -0.0036461042512210473] %
+
+Mass Used: 102.56595135764564 kg
+Launch C3: 102.3862165595457 km²/s²
+||V∞_in||: 0.03945532085898617 km/s
diff --git a/archive/ES_0.5998727882475705 b/archive/ES_0.5998727882475705
new file mode 100644
index 0000000..dcba0a3
--- /dev/null
+++ b/archive/ES_0.5998727882475705
@@ -0,0 +1,22 @@
+archive/ES_0.5998727882475705---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T10:18:44.650
+Launch V∞: [5.138908088936597, -8.599021117927911, -1.4303381523226224] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6160616338267035e-9, -1.2620373883937977e-9, -1.582411898546074e-9] km/s
+ V∞_out: [-2.3938904566974035e-10, 5.474782520769284e-10, 7.688676734162997e-10] km/s
+ time of flight: 1.2351988771349241e8 seconds
+ arrival date: 2027-03-24T01:23:31.650
+ thrust profile: [0.42551907731523597 -0.3164223770619033 -0.25484620665280844; 0.23775310397506694 -0.04848926723671529 -0.2820172182978853; 0.13665584310619058 -0.0010854907131914683 -0.2446718828588937; 0.1023944148445721 0.009988611763653154 -0.23946273555269; 0.07499739523125501 0.012497337290798025 -0.2131333389235751; 0.06844006916303932 0.014378298428194079 -0.22303680248087454; 0.011010835999498338 0.0028803927262781837 -0.043617192091024694; 0.006537744997529704 0.0017826945677049634 -0.028045489449314835; 0.0022452691785567022 0.0006232920661925506 -0.010348733880476633; 0.001059342070098734 0.00032698994037716727 -0.005012396851191678; 0.0052570016974753655 0.0019483457282697752 -0.02857394230765446; 7.750960497493878e-5 0.00011897003999819316 -0.0005878309596615511; 8.011007738257516e-5 -0.00011029584269788614 -0.0006673758499033467; 8.958024288830817e-5 -6.1909122775965575e-6 -0.0005163831975146734; 0.0002599463723267937 1.9417158081490498e-5 -0.00045817110185853815; 0.00018371239508404322 -6.21145763825822e-5 -0.000638708189115326; -0.00022910072982619924 -6.376603392982061e-5 -0.0003294718997868868; 0.0001293572784471518 1.3849592502164183e-5 -0.00023213359316935595; -0.0005036845390981201 0.00041494010175237447 0.0001854824731126382; -0.00022832296444138438 -3.5068838416806776e-5 -7.576775239305543e-5] %
+
+Mass Used: 102.53337433742809 kg
+Launch C3: 102.39740776309786 km²/s²
+||V∞_in||: 2.5900619665735147e-9 km/s
diff --git a/archive/ES_0.5999195459953728 b/archive/ES_0.5999195459953728
new file mode 100644
index 0000000..082fc6e
--- /dev/null
+++ b/archive/ES_0.5999195459953728
@@ -0,0 +1,22 @@
+archive/ES_0.5999195459953728---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T11:09:39.273
+Launch V∞: [5.201284225210998, -8.186736204551094, -0.2639699750216843] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.1349450071639801, -0.18872283693609418, 0.03038190878795008] km/s
+ V∞_out: [-0.2959000471764254, 0.029400282801974598, -0.015437619169804408] km/s
+ time of flight: 1.3109040059244588e8 seconds
+ arrival date: 2027-06-14T17:09:39.273
+ thrust profile: [0.7287314574151093 -0.4517553071898804 -0.28436595205371107; 0.36120862081088406 -0.023029087893686167 -0.31569983184708267; 0.12874006774113705 0.01979519098736216 -0.17650380531189722; 0.1662535049684736 0.049154563388085035 -0.28748102216228855; 0.15580854611549366 0.06497951202916129 -0.3238726069171766; 0.06916553576527146 0.03050589089797591 -0.16958548949252372; 0.0549767303572832 0.026692308628690476 -0.1500999197265713; 0.02088748545111169 0.009590025928177353 -0.058107673993874155; 0.0032246824167098606 0.0009495843507505665 -0.0020892198649673176; 0.0073162147507302225 0.004407590242239905 -0.019150459714172507; -0.006916079165807197 -0.0018557425603812883 -0.013137761561594973; 0.007402931753700963 0.004748285869200413 -0.009961106764701603; -0.005029695646667741 -0.002189152519558534 0.004789361678981986; 0.0015626130737990192 0.0015819050393360385 -0.00594123436167719; 0.004671887817688136 0.020949486602003235 0.003358293500773887; 0.003788487420142364 -0.02273962687527002 -0.005599813939054729; -0.0053087079677953996 0.0171488549681535 -0.014375857553156863; 0.013423110031930028 -0.008966813343613936 0.011249577763232438; -0.00711612132345568 0.0027337383911758507 0.00910055692072655; 0.006063110369797149 0.0024565254908954027 -0.00013225201010168253] %
+
+Mass Used: 150.72296036598027 kg
+Launch C3: 94.14568742204936 km²/s²
+||V∞_in||: 0.23398616309793527 km/s
diff --git a/archive/ES_0.6000228583691603 b/archive/ES_0.6000228583691603
new file mode 100644
index 0000000..7790929
--- /dev/null
+++ b/archive/ES_0.6000228583691603
@@ -0,0 +1,22 @@
+archive/ES_0.6000228583691603---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T19:59:31.070
+Launch V∞: [5.1191055052148355, -8.533576249624883, -1.202939267794544] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.9495229782253104, -0.6436028067176001, 0.38627257154508543] km/s
+ V∞_out: [-0.8258864607156182, 0.6737470327384717, -0.5709536759249361] km/s
+ time of flight: 1.2377879999999183e8 seconds
+ arrival date: 2027-03-26T10:59:30.070
+ thrust profile: [0.5418311719599728 -0.4021999399773504 -0.31702958078225324; 0.20153165567288306 -0.04014780926506632 -0.23890630843479382; 0.19327247709528486 -0.0016844420098731327 -0.337685722522743; 0.12162846975727809 0.011740300060837129 -0.2804794689593306; 0.0732447224985234 0.012370902282590617 -0.20412410390079422; 0.05103905306848368 0.010822308322839244 -0.16318785697237428; 0.014230722405918038 0.004085367626904767 -0.05122416890283713; 0.007480468892647297 0.0025593945241169386 -0.031117798751994677; 0.0025473815268516812 0.0007117582403258759 -0.010775614140866224; 0.0007681770736994963 0.0026858004960751657 -0.021365619142572106; 0.00045881839392764414 0.0004309142693680341 -0.0031263548501640737; 0.0025559858675377974 -0.0009182111758483796 -0.008575073559556624; 0.0009003186405231983 0.0012067532508404956 -0.007643524356140457; 0.003033492736786707 -0.004058794280451243 -0.007553972958362254; -0.00028361661741447457 2.0713803162005005e-5 -0.0029137652753137523; 0.0007007381094524071 0.0006481106331828473 -0.004307677670999525; -0.0019627511612205044 -0.00014718739154365943 -0.002068159635930882; 0.0012982970769392795 0.00228183570413349 -0.0022068568482618714; -0.0012900160794444596 -0.0013210265681961857 0.0021652453419019994; -0.001146263019666834 -0.002438465212107034 0.0024052098228874233] %
+
+Mass Used: 113.92700672585897 kg
+Launch C3: 100.47422766368479 km²/s²
+||V∞_in||: 1.2103821539169721 km/s
diff --git a/archive/ES_0.6000352109134487 b/archive/ES_0.6000352109134487
new file mode 100644
index 0000000..5f4e56d
--- /dev/null
+++ b/archive/ES_0.6000352109134487
@@ -0,0 +1,22 @@
+archive/ES_0.6000352109134487---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T04:16:07.639
+Launch V∞: [5.11618821318498, -8.390780537132626, -0.9994926264235664] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2139180175658068e-5, -5.720664417974935e-6, -9.890521484547409e-6] km/s
+ V∞_out: [7.818043540582588e-6, -8.27819220319534e-6, 1.217657224774146e-5] km/s
+ time of flight: 1.237273101949897e8 seconds
+ arrival date: 2027-03-24T04:57:57.639
+ thrust profile: [0.72923445320924 -0.5245424961554875 -0.3809068221382714; 0.32926925696621284 -0.05344491410195287 -0.3581298790965337; 0.13637148125124532 0.006818974030675804 -0.22938230892211411; 0.11088097309495647 0.018791508596289582 -0.24110600954840952; 0.05682400100681967 0.012883774616651718 -0.15155983545762178; 0.06031128686406608 0.017764348124472293 -0.18435054471363777; 0.031005714524914855 0.010209936187148409 -0.10616399039143001; 0.023779426660954808 0.00835327852224757 -0.08971570653072455; 0.005610217851028055 0.0024147745533927337 -0.023762426133163816; 0.013649023548668609 0.005311404142087008 -0.06419412631390461; 0.000715818365112032 0.000297542194429272 -0.003293849558219409; 2.404600029667621e-5 -5.784019280823768e-6 9.117810372697192e-5; 8.982325866669227e-5 9.001812502162489e-6 -0.00028002813961929105; -0.00010066558912083062 -0.0001279788623867249 -0.0001516088396680982; -8.147786565495911e-5 4.8948901450482084e-5 -3.8082855699160284e-5; 0.0004117457424654249 5.8410685363613604e-6 -0.0003731979363618421; 8.344234745866642e-5 0.00012490056813358618 -7.078475109284605e-5; -8.14783883957322e-5 1.7152444958062557e-5 0.00013374908866962975; -7.874070751989282e-6 5.350952892163889e-5 0.00012320867088696895; -0.0003908786035132934 1.3709272123837351e-5 0.00020604495453750203] %
+
+Mass Used: 130.8269481012553 kg
+Launch C3: 97.57956536533167 km²/s²
+||V∞_in||: 1.6670576233485998e-5 km/s
diff --git a/archive/ES_0.6000809895652897 b/archive/ES_0.6000809895652897
new file mode 100644
index 0000000..ad47ed0
--- /dev/null
+++ b/archive/ES_0.6000809895652897
@@ -0,0 +1,22 @@
+archive/ES_0.6000809895652897---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T07:22:05.686
+Launch V∞: [6.815917736271848, -7.287973338947647, -1.1320954628507747] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0028715099958648064, -0.004534048779544907, -0.0016732661646040765] km/s
+ V∞_out: [-0.0031749619700619466, 0.004112377163497022, -0.0021475799686639803] km/s
+ time of flight: 1.2324999889687148e8 seconds
+ arrival date: 2028-04-02T19:28:43.686
+ thrust profile: [0.6129484125149874 -0.27418870510024196 -0.31914242025120615; 0.2024185458106484 -0.003318929880978117 -0.24521476483157195; 0.11240913036901574 0.020751646070124037 -0.20992029577505408; 0.0969599535386258 0.02625715290834373 -0.24518789792197698; 0.08490273939874428 0.026790186962068488 -0.2527846093608613; 0.04520743737213905 0.016020181970686748 -0.16339162045310282; 0.018462769046450413 0.007856356193853718 -0.08021941268417623; 0.013036465091464312 0.005938860528606677 -0.061605154935129997; 0.0106475041280543 0.005320531467271616 -0.055969997971382995; 0.00293926022438498 0.001304280159346915 -0.016273023503575183; 0.006295467940898515 0.0031107694516608855 -0.03519392584700241; 0.000790615181533531 0.000250069424491554 -0.004536491833937262; 0.0007289549928593981 0.00021380075742523288 -0.0015906880333815742; 0.00016239398922466498 -0.0004244191715014327 -0.001936954274522479; 0.00024755510938331165 8.110282958972809e-5 -0.00040799050319226043; 2.6585246195094127e-5 0.00016053533766640719 -0.0011512324758778238; 0.0015607367434873752 0.0018724609418825193 -0.0030939019739053635; 0.00023016088140709106 -0.0001665710808973506 -0.0013652995355841685; -0.0007916087771667403 -0.00012099591152311495 -0.0012565626963275166; 0.0001280129045853251 -0.0011387962238807471 -0.0010604355857246083] %
+
+Mass Used: 111.78572882874687 kg
+Launch C3: 100.85293011384417 km²/s²
+||V∞_in||: 0.005621653462216698 km/s
diff --git a/archive/ES_0.6001440467000037 b/archive/ES_0.6001440467000037
new file mode 100644
index 0000000..e327dbe
--- /dev/null
+++ b/archive/ES_0.6001440467000037
@@ -0,0 +1,22 @@
+archive/ES_0.6001440467000037---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T03:09:52.951
+Launch V∞: [5.160126087262539, -8.459125322025274, -1.2778203893189304] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.2839770287792195, -0.18693008425766597, 0.16999102835449637] km/s
+ V∞_out: [-0.24659492097101376, 0.2354545848952991, -0.1681586985734455] km/s
+ time of flight: 1.2424120623392904e8 seconds
+ arrival date: 2027-03-31T02:36:38.951
+ thrust profile: [0.6287650839774382 -0.44909363335121466 -0.3494551699536723; 0.21788712182185233 -0.0370267933546462 -0.2517280867835949; 0.11536853651913868 0.003930604336252165 -0.19827194419844135; 0.07063064082569502 0.010251002176484628 -0.1619799543676474; 0.08642866481347744 0.019066874232215855 -0.2356849500877566; 0.051422316046182096 0.015138341906779235 -0.16303866085136942; 0.056575630115177945 0.017009054768195284 -0.19666160408877617; 0.019313362726029897 0.007274766489024753 -0.07795982272094193; 0.0034331376182557367 0.0010624866782224366 -0.01353958801620453; 0.004980515418422013 0.0019001883581816741 -0.020680247795604893; 0.0027194819492535223 0.0031107510637097386 -0.006292551491664585; 9.871416115915478e-5 -0.00031186030037855554 -0.004607613334375191; 0.0007355222789496843 0.000253800870025956 -0.0036845757104985205; -0.0019880188218966348 0.0038843337842148227 -0.006004577410928058; -0.0020368899149500403 0.001073511391735832 -0.002063891820656171; -0.00327968426702505 -0.001825032925165355 -0.007192164306734959; 0.0016815064298425792 0.0017793553153086427 -0.0014909388967349196; 0.0004505467489677084 -0.0024683131671900185 -0.0029664846221484223; -0.0021981278606855083 0.003203603772041547 -0.0038163690814907603; 0.0008537501299714159 -0.0019506315206547688 -0.001035489257131495] %
+
+Mass Used: 117.9049779977122 kg
+Launch C3: 99.8165273975358 km²/s²
+||V∞_in||: 0.3801088778177523 km/s
diff --git a/archive/ES_0.6002994913029281 b/archive/ES_0.6002994913029281
new file mode 100644
index 0000000..c4ae5a3
--- /dev/null
+++ b/archive/ES_0.6002994913029281
@@ -0,0 +1,22 @@
+archive/ES_0.6002994913029281---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T04:57:32.970
+Launch V∞: [5.348460418684848, -8.38805668791681, -1.5455765775333665] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.09393551889826776, 0.05987570225811923, -0.040278782940184506] km/s
+ V∞_out: [0.08325821881889606, -0.0644342860846203, 0.057560728849533845] km/s
+ time of flight: 1.2523432196893708e8 seconds
+ arrival date: 2027-04-09T16:16:13.970
+ thrust profile: [0.39723478327297984 -0.27201104838922036 -0.2097959177992466; 0.2713912330204403 -0.033079648613872276 -0.27683644247667805; 0.21018400254038147 0.021091948520625098 -0.31552856654563677; 0.15588614830849595 0.0361430940284501 -0.3026256949457838; 0.10124343574902059 0.03281394305183911 -0.23757392911705444; 0.051320860611066416 0.020359328697470293 -0.14032915835187318; 0.013326057603230848 0.005979842546726168 -0.03796764266340185; 0.006234796511459645 0.0015781823650210058 -0.017091630216573832; 0.007612243058539392 0.003957443652741409 -0.02583966978901857; 0.004852437629508717 -9.857359469024043e-5 -0.009662636925117464; 0.0022431221526560702 -0.0003451196949186184 -0.005034771144821344; 9.744015921276912e-5 -0.0009707095535048767 0.00019484809896007024; 0.0008097202711733588 0.0008779914682733986 -0.006572954307537888; 0.0013016159536312316 -0.000500678201742784 -0.008281709485118147; -0.0006289777676910012 -0.002653751858298231 -0.0027197671896183567; 0.004014215511789406 -0.002606954107323752 -0.0020369331773899086; 0.0007516958610168884 -0.0012660314423740447 -0.001556511353062351; -0.0003863617393194722 -0.001233076349676912 -0.0029506557906321647; 0.0002047313805179179 0.000436975026731132 -0.002690261338517224; -0.0007928140042644168 -0.0049100773406143645 -0.0003902489177255321] %
+
+Mass Used: 109.11581014612511 kg
+Launch C3: 101.35433080696419 km²/s²
+||V∞_in||: 0.11845404926270889 km/s
diff --git a/archive/ES_0.60052933502594 b/archive/ES_0.60052933502594
new file mode 100644
index 0000000..f595007
--- /dev/null
+++ b/archive/ES_0.60052933502594
@@ -0,0 +1,22 @@
+archive/ES_0.60052933502594---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T13:18:06.972
+Launch V∞: [6.985163253375173, -7.259270554913578, -1.518073568067026] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006780592097517537, -0.006362587246222585, 0.0046649997133003905] km/s
+ V∞_out: [0.004144099374546102, -0.009454482618329867, 0.001289785611325459] km/s
+ time of flight: 1.2240565614977361e8 seconds
+ arrival date: 2028-03-23T06:52:22.972
+ thrust profile: [0.36280241328325374 -0.16017146619340386 -0.19662207938541007; 0.19730819372995514 0.0055574370310493264 -0.23471221076972387; 0.1503641033739421 0.0342951097629831 -0.2786588950111128; 0.10988079590794396 0.03811977949840011 -0.27256208557728284; 0.08544135630917743 0.03650548129166371 -0.2609250162745197; 0.03598378212137467 0.018047125922656584 -0.13171873593729347; 0.01613960219203715 0.00856202038640507 -0.06799245506157031; 0.010401146614972311 0.006072136153375239 -0.049432752648020946; 0.0017644824133157125 0.0010919960206697964 -0.009068592681738782; 0.00469914043731478 0.0028219702929433523 -0.025580344145387398; 0.00010539833087666166 0.0007577534630192047 -0.00023095088475307002; 1.2542788471009935e-5 -4.029782445032172e-6 -0.0003291674592921642; -0.00034943424636574733 -0.000677247639622009 8.239560956506349e-5; -0.0003832769997249696 8.833422773527554e-5 0.0007361529113673183; 4.8983493914084384e-5 -0.00013601399308019044 -0.004304775741326915; 0.0002877538160548081 0.000211482096571071 -0.0008081519763280678; -0.00046834536493579496 -0.0011725568017613716 0.0023914002692368144; 0.0003346940990511401 -0.002688958150474874 0.0006598107502555205; -0.000557798746595464 0.0003702195246623474 0.00019345639588720838; -0.0003914358543645429 -0.0012240505434104763 0.002126342097037783] %
+
+Mass Used: 95.15219572475235 kg
+Launch C3: 103.79406202380189 km²/s²
+||V∞_in||: 0.010402940352794699 km/s
diff --git a/archive/ES_0.6005597041817916 b/archive/ES_0.6005597041817916
new file mode 100644
index 0000000..8e8a40e
--- /dev/null
+++ b/archive/ES_0.6005597041817916
@@ -0,0 +1,22 @@
+archive/ES_0.6005597041817916---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T07:24:08.471
+Launch V∞: [7.081730221135395, -6.97990883802505, -0.34495214550189346] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012088976845900637, -0.001874558341116873, -0.00015708064711286176] km/s
+ V∞_out: [0.00013696247575591266, -0.000598769585951651, -0.002149048810407676] km/s
+ time of flight: 1.3410826652752629e8 seconds
+ arrival date: 2028-08-04T11:41:54.471
+ thrust profile: [0.3668646417753433 -0.1285777356678351 -0.1572161462703569; 0.14048326714487466 0.018516647842600875 -0.14367677973184506; 0.11785744975730811 0.04135702083460774 -0.19340927182989034; 0.11059399751391098 0.05374016681385697 -0.24353396568350205; 0.1224734609576633 0.07092505210256037 -0.3264402737785977; 0.04252288193632347 0.028567981595594323 -0.13422658368700352; 0.047347052453195385 0.034277924923237744 -0.17296129379661268; 0.03646908823271428 0.028274720168209325 -0.14326857922541336; 0.002603652094113066 0.004907621762976997 -0.007539216458750549; -0.009221163711354756 0.0063682917245234455 -0.019709177287876987; 0.0052767761116772295 0.00937733681277282 -0.022065507388660137; -0.01284034392638404 -0.016105426711114396 -0.014761494755461796; -0.002358113613467914 -0.010472029049028804 0.0006261033771630127; 0.004996243394216589 0.009521884087316614 0.01169684452757043; -0.031058600341027708 -0.018209503284612863 -0.011251963537264343; 0.03259914715851722 -0.0037117123152394012 -0.06740866567280145; -0.018112086875760915 -0.010536833548005862 0.013023094529220586; -0.016027301078634704 -0.009165854396038554 -0.0023435031618895433; -0.00021149997536968604 -0.022499428605509846 0.008058996896194257; 0.03621262443344786 -0.03696725581053931 -0.034566237657884] %
+
+Mass Used: 123.2170248259381 kg
+Launch C3: 98.98902229476893 km²/s²
+||V∞_in||: 0.002236085176319421 km/s
diff --git a/archive/ES_0.6006384650724077 b/archive/ES_0.6006384650724077
new file mode 100644
index 0000000..0a1df8e
--- /dev/null
+++ b/archive/ES_0.6006384650724077
@@ -0,0 +1,22 @@
+archive/ES_0.6006384650724077---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T14:31:24.853
+Launch V∞: [6.884293729437408, -7.1510295566181, -0.8691797974228392] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0012785086408760005, -0.009610968273576773, 0.00530267489140552] km/s
+ V∞_out: [0.0033722329619392463, 0.008820188197906764, -0.005737608174059752] km/s
+ time of flight: 1.2484122829117154e8 seconds
+ arrival date: 2028-04-19T12:38:32.853
+ thrust profile: [0.6288011423107275 -0.2598342842398304 -0.2887888191461988; 0.19748514600741238 0.013904385105699116 -0.2233889769696347; 0.141806623925528 0.04043534394072893 -0.2534116059591889; 0.10822742414658276 0.04550217263724914 -0.2614027168939032; 0.08294582267244269 0.042944498419406084 -0.2526731105135281; 0.047743948467822046 0.025160409678809333 -0.16464861103508194; 0.024078530707733834 0.012596138619693501 -0.09247248197834362; 0.029238531066426293 0.0173530119754044 -0.12463012762645068; 0.005184045687678874 0.0035296271847013445 -0.02387649200418879; 0.002077058225070542 0.000802887230791838 -0.006800950184794597; 0.010267023893791822 0.006752500818386062 -0.041905676635944335; 0.0015040010954155726 0.0014259754842548703 -0.00994413000666066; 0.0030060010197758575 -0.0035069969174849024 -0.006125551784120598; -0.005757633002962476 0.005577067307280697 -0.005187997859283271; 0.0012900361934372428 -0.0006156462500838114 -0.0004896212286910218; 0.008847856574822835 0.010123763841877976 -0.005519094036536081; -0.0023354152445510612 -0.0015763612038677717 -0.0035240156806423907; 0.0015290017700120423 -0.007932929092897289 -0.00012100172589850876; 0.006176038131180658 0.006263425476747318 0.00642449055605953; -0.005765929930048593 -0.014620912949885895 0.008054806239974323] %
+
+Mass Used: 121.57539112504719 kg
+Launch C3: 99.28619739304487 km²/s²
+||V∞_in||: 0.011050957266428843 km/s
diff --git a/archive/ES_0.6006427079416543 b/archive/ES_0.6006427079416543
new file mode 100644
index 0000000..ee8d8b2
--- /dev/null
+++ b/archive/ES_0.6006427079416543
@@ -0,0 +1,22 @@
+archive/ES_0.6006427079416543---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T07:12:31.584
+Launch V∞: [6.90975949624345, -7.21283407997676, -1.2500996484058717] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005873794844463288, -0.0038068543553197737, 0.0026108769068951283] km/s
+ V∞_out: [0.001455485119065987, 0.0036868784129668775, -0.0024360085787388614] km/s
+ time of flight: 1.2236043656764263e8 seconds
+ arrival date: 2028-03-22T12:13:07.584
+ thrust profile: [0.5887647925085919 -0.26405194649880265 -0.2978998454789028; 0.18967948092307696 0.0017473317094505714 -0.22010143696904472; 0.1369272546281159 0.027470789992069113 -0.24787679373519186; 0.10050726935536798 0.031121814739625785 -0.244033367812166; 0.06903589674519243 0.02611011775150014 -0.20797049767544865; 0.03200131481405216 0.014349010429574236 -0.1146591084012081; 0.038354702687189844 0.015557069697627279 -0.1492171772219807; 0.023511085068755842 0.01063523286779682 -0.0968538812033736; 0.01974559679422825 0.008496902633997072 -0.08984725666097956; 0.0007252340978358804 0.00045452906899949303 -0.00469656994945989; 0.00021690994188213044 0.00012935865646000418 -0.0015478478846569729; -2.4080852039435046e-6 -2.3240788465100923e-5 -0.0003979709237553234; 0.0002521829616071024 0.00016679043566813386 -0.001605270207226127; 6.075020290102078e-5 6.0756289789026135e-5 -0.00046942581785282733; 6.719878821377032e-5 -7.782336526260914e-5 9.382506776691444e-5; 0.0002898020921154297 -0.00013223401616388922 -0.0002235676581473045; -6.095560998219579e-5 -6.907861771938232e-5 0.00010176374665327338; 0.00038583150405146593 0.0005755219033574557 -0.00021833628122877656; 4.3680127060955116e-5 6.331200297718994e-6 -0.00026062840464870923; -0.0001734358527973347 -0.0001704905869982095 -0.00010423855491237567] %
+
+Mass Used: 109.64357072774965 kg
+Launch C3: 101.3325008921452 km²/s²
+||V∞_in||: 0.004653367916286422 km/s
diff --git a/archive/ES_0.6006528530435701 b/archive/ES_0.6006528530435701
new file mode 100644
index 0000000..0c2d165
--- /dev/null
+++ b/archive/ES_0.6006528530435701
@@ -0,0 +1,22 @@
+archive/ES_0.6006528530435701---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T20:18:00.094
+Launch V∞: [6.939694652422336, -7.361312438060483, -1.3203380120927288] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003284228299013627, -0.005014103851371504, -0.0019306209260854857] km/s
+ V∞_out: [-0.0035602249175383702, 0.004589579431587916, -0.0024315473794149444] km/s
+ time of flight: 1.233343939738607e8 seconds
+ arrival date: 2028-04-04T07:51:13.094
+ thrust profile: [0.35031367611278696 -0.14631111235092792 -0.18308609329050585; 0.15850473459879816 0.011993372487135256 -0.19417364331619746; 0.0916478613029878 0.019325757930905338 -0.174626923959689; 0.05397050247008275 0.01748918994916867 -0.13978173313646647; 0.048775755148691965 0.019402932298709156 -0.15519613205689836; 0.07928432465104325 0.04120704875798435 -0.2897823619201835; 0.05979304102111059 0.028453157970958015 -0.24537222200969017; 0.016357608555208954 0.008782928529005326 -0.0738445937579221; 0.011770761919555896 0.005815300494530442 -0.06106724507490666; 0.0029747983858490552 0.0018424846096734197 -0.017019153183855416; 0.0002907015570565931 9.629081156092111e-5 -0.0018331977184753642; 0.00010771271090868189 0.00018675633806387146 -0.0003286507364693072; 0.0001348394118105771 3.997910005289657e-5 -0.0003803959118089231; 6.661768951911194e-5 -0.00010858418229334683 -0.00038896823365406014; 6.840435541158622e-5 -0.000118369577776095 -0.0002680464559449468; -0.00045549539249408643 0.0001268931173395016 0.0002687781143148004; -0.00047914078318691904 0.000237214585565389 -0.00011160136861189466; -6.792136505597406e-5 0.00017763735167810677 -0.00027442713555400736; 3.218725566480254e-5 0.00027603487586948396 -0.0005872940395317294; 0.00043001887294035244 -0.0005796712617445296 -0.0007133557381163448] %
+
+Mass Used: 93.56080686711448 kg
+Launch C3: 104.09157514578011 km²/s²
+||V∞_in||: 0.00629719700443139 km/s
diff --git a/archive/ES_0.6006669305190429 b/archive/ES_0.6006669305190429
new file mode 100644
index 0000000..2f538a1
--- /dev/null
+++ b/archive/ES_0.6006669305190429
@@ -0,0 +1,22 @@
+archive/ES_0.6006669305190429---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T23:36:24.785
+Launch V∞: [5.193364103614192, -8.394944160558737, -1.0037956770534266] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010089263809412385, 0.059553705745275326, -0.06437667523361812] km/s
+ V∞_out: [0.06071484872599605, 0.054101948107792015, 0.0343295416154221] km/s
+ time of flight: 1.2483666086284705e8 seconds
+ arrival date: 2027-04-05T20:27:24.785
+ thrust profile: [0.626151628587569 -0.43272649010596287 -0.31769406241974757; 0.30488090734219153 -0.04273105669408849 -0.318091127559063; 0.11359031293321856 0.007377340275963639 -0.18671498569135883; 0.09430683975918319 0.017541516709710783 -0.20016319225456258; 0.0835336131874138 0.021093328699732888 -0.2128069289037252; 0.07247228261964599 0.023849780876042337 -0.20281763229780925; 0.055252682125062645 0.01871661135604312 -0.18317594467707551; 0.01883495756566014 0.007064147771916043 -0.06903088233920693; 0.013018616939076256 0.005655086992044847 -0.0505582810947693; 0.0009587334129820308 -0.0001516556940261819 -0.006114219697142785; 0.0005104802374078744 0.0013445631227219565 -0.00984522739544777; 0.001205146486050366 -5.975777660651663e-6 -0.008559637627289916; 0.001473895296642515 0.0026658776824989294 -0.004925102249262205; 0.0066908705395429015 0.0028197537609858424 0.0001780060170271929; 0.007036732613001378 -0.0032395729914393087 -0.002554316478499246; 0.0016101089271986224 0.003289933662490639 -0.003903484507420836; 0.0009432322818989494 -0.0028199801548778156 -0.004514657172739429; -0.0016199226270250623 0.0013324726141167365 -0.0025592599712939397; 0.008465662971887392 -0.004903216198739338 0.002982175166676841; 0.0024786827610268963 0.0012349618081691459 0.00042676276761863165] %
+
+Mass Used: 126.46469599709008 kg
+Launch C3: 98.45372393287883 km²/s²
+||V∞_in||: 0.08827680004590957 km/s
diff --git a/archive/ES_0.6006756887106035 b/archive/ES_0.6006756887106035
new file mode 100644
index 0000000..0e4c682
--- /dev/null
+++ b/archive/ES_0.6006756887106035
@@ -0,0 +1,22 @@
+archive/ES_0.6006756887106035---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-28T02:06:49.236
+Launch V∞: [7.16659970787893, -6.5391567537551385, -0.9079786456729247] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1095741857688323e-6, -3.169814211919034e-6, -3.0908314754027525e-7] km/s
+ V∞_out: [3.1623183646695837e-7, -1.545415011497144e-6, -3.476629671018551e-6] km/s
+ time of flight: 1.3795384979773235e8 seconds
+ arrival date: 2028-09-10T18:37:38.236
+ thrust profile: [0.7380361766974842 -0.21515322011430435 -0.2424190369394306; 0.40546723850154825 0.10164379859162705 -0.3156337435319574; 0.1972181030479797 0.1063193214193906 -0.24908021009348758; 0.14601525566233406 0.11008545150003035 -0.2566232975234499; 0.09530899215419805 0.0884514514487463 -0.21096875247961014; 0.07959549961426092 0.08585193991587925 -0.21332578669514324; 0.008871171472235984 0.010607751491569506 -0.028692106158220678; 0.008382174641367323 0.01074398835607248 -0.032834509650166564; 0.015504686110258459 0.022518101818552773 -0.06069839918340568; 0.00786462665845851 0.011791502194816296 -0.03627268429631185; 0.0011268690728932333 0.001524299292744062 -0.0057053285032616745; -0.00013178555595174627 3.72088241663562e-5 -0.0013312550643026647; -0.00024487645957250775 -0.0020304449066268536 -0.00016186825936502134; -0.0004533576793173766 0.0011006147895099231 -0.0009561302953355294; 0.001085589375496232 -0.0009407992871552544 -7.63531975174858e-5; -0.002334898411603728 0.00041597532489262123 0.007040304596073613; -0.0007951753594432551 -0.00045872435057590477 0.0012878731621087554; -0.00176458107215579 -0.0021447322006449966 0.003654088539789414; 0.0012434842059512686 -0.0023589104920113896 0.0014567144773585399; -0.0008190034459781732 -0.0011116700873729651 0.0012967220690692414] %
+
+Mass Used: 146.94160890483 kg
+Launch C3: 94.94514764414986 km²/s²
+||V∞_in||: 3.820151538282156e-6 km/s
diff --git a/archive/ES_0.6007320274897645 b/archive/ES_0.6007320274897645
new file mode 100644
index 0000000..0728fe5
--- /dev/null
+++ b/archive/ES_0.6007320274897645
@@ -0,0 +1,22 @@
+archive/ES_0.6007320274897645---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T14:02:54.454
+Launch V∞: [6.9580090174196, -7.243338611718252, -1.1629831750726403] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007746783925027988, -0.007199170486229537, 0.005498310286420704] km/s
+ V∞_out: [0.004672475851578134, -0.010851715523929011, 0.0014805146657871832] km/s
+ time of flight: 1.2361484116183504e8 seconds
+ arrival date: 2028-04-06T07:30:15.454
+ thrust profile: [0.4096380868879887 -0.18425854570351005 -0.2131281331011206; 0.19396351320145194 0.0012919285317933651 -0.22583313986573317; 0.1390361317324009 0.02720104570366372 -0.25189837429251943; 0.10609980669846138 0.03176020799293684 -0.2550530328511224; 0.10455658552119493 0.036824275144143936 -0.3082234303342823; 0.04199144401283904 0.019372877245353005 -0.1410648952143776; 0.02860625391015791 0.015310539002058709 -0.11589508783010816; 0.009488807975771502 0.005389894612844323 -0.04222083469035703; 0.005674845685198983 0.0011267677956416462 -0.021698329289274704; -0.0008846716133150438 0.001378037960594871 -0.009723043814755757; 0.0015337831138560255 -0.0006539801842270384 -0.0053438962657424375; 0.006272471937921957 0.0030222741797498523 -0.03541665673065643; 0.0003123693446192853 0.0017953677249002774 -0.009631144162019035; 0.004474054695014292 -0.0012879086043558522 0.0028851390524234017; -0.004481771941391067 -0.0018722209623141862 0.00047209721558452104; 0.000669226314448724 0.005977250337031727 -0.008890239468918867; 0.005696162129929867 -0.004295980986112353 0.002731497104143107; -0.00011332952293516036 -0.0016108549450344943 0.004573586690724949; -0.00021751876063575738 6.482943312690389e-5 0.0008188665102887376; -0.0004916024310257067 -0.0011838821574483482 0.002550918308854664] %
+
+Mass Used: 104.49851942804116 kg
+Launch C3: 102.23237359600299 km²/s²
+||V∞_in||: 0.01191940153181485 km/s
diff --git a/archive/ES_0.6007757211899667 b/archive/ES_0.6007757211899667
new file mode 100644
index 0000000..65e4d7f
--- /dev/null
+++ b/archive/ES_0.6007757211899667
@@ -0,0 +1,22 @@
+archive/ES_0.6007757211899667---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T09:34:45.107
+Launch V∞: [6.830995940080655, -7.248464180396846, -1.3823534190485838] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001828922318636797, 0.011707229532233982, 0.001794609674651792] km/s
+ V∞_out: [0.011004597759399595, -0.0022175087007834603, 0.004222634155802362] km/s
+ time of flight: 1.2537807236622174e8 seconds
+ arrival date: 2028-04-27T12:49:17.107
+ thrust profile: [0.58110309758445 -0.25945427887479483 -0.30667924047234724; 0.16802302360503252 0.0005734229760685917 -0.20182568084054345; 0.12953256846924857 0.0239360973013075 -0.24508197602532159; 0.09386334548495502 0.026436689340251958 -0.23689285555007078; 0.06547731915352974 0.02130514265122886 -0.19526614096722283; 0.04009697033118278 0.013018424998096741 -0.15020885640456552; 0.016715535624386806 0.0066866817534110825 -0.0730757538159746; 0.015306509037707382 0.007717486460979309 -0.07272737348262621; 0.010358307203739144 0.004583975251442758 -0.05451109660843019; 0.00028629384333560054 0.002004953095619341 -0.01805273372929339; -0.00481872773324199 0.0009144483242081703 -0.0016949194979436338; -0.004501043514742062 -0.00274415828020073 -0.009608560692167685; 0.006362120465236593 -0.004520038068950362 -0.0038403724717737996; 0.0013994864439349345 0.00828423565445132 0.0002455200524018458; 0.003801980220440253 0.002679696307058172 -0.009813624345929577; -0.005312382359234855 0.0011145171628298863 0.005291539783839521; -0.018610975119210928 0.009317041992312716 -0.01340783434544987; -0.012457786064772373 -0.018620316747028538 -0.009833527236678376; -0.00035703254627331035 -0.0060166059036280365 -0.019585121956355672; 0.0010338884675468825 0.011979600663831348 0.005235502967449987] %
+
+Mass Used: 111.07544440383708 kg
+Launch C3: 101.11363948304982 km²/s²
+||V∞_in||: 0.011984356639067995 km/s
diff --git a/archive/ES_0.6007955756096419 b/archive/ES_0.6007955756096419
new file mode 100644
index 0000000..c3488f5
--- /dev/null
+++ b/archive/ES_0.6007955756096419
@@ -0,0 +1,22 @@
+archive/ES_0.6007955756096419---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-16T16:30:51.752
+Launch V∞: [6.304095648283078, -7.012982167992597, 0.3315122099274524] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00081008065495844, 0.0009045844221178806, 0.0008914047675335548] km/s
+ V∞_out: [-0.0010098669059475868, -0.0004794068351040046, 0.0010082868083402122] km/s
+ time of flight: 1.8749577787476075e8 seconds
+ arrival date: 2029-03-25T18:40:28.752
+ thrust profile: [1.0 -0.24616536145353737 -0.12982687578216892; 0.28380389647488474 0.12643045766021505 -0.12396119196641057; 0.16206423395093827 0.13349722549745197 -0.1201694681889574; 0.12949907327531252 0.14892783588011307 -0.13511353564822204; 0.0818793723763144 0.12174635225540509 -0.11633822217998012; 0.05049365623644884 0.0926358664882541 -0.09351125079390647; 0.029238263008366138 0.06509723458420325 -0.06895234259485318; 0.023023392548559198 0.061974170026896404 -0.06673443985570335; 0.009541104555820861 0.02611127812815129 -0.029812504360058875; 0.0006148508228833342 0.000829764513534773 -0.00012699738534689535; 0.0005971200912344972 0.0005456504025879297 -0.0018253585027508765; -0.00015119042597361965 0.00120428694904014 0.0006030842642785247; -0.0008445695390676902 0.000999286912119334 -0.00012192500113250939; -0.0018426465783427136 -0.0006266461348533854 -0.000762002449443639; -4.262725021635756e-5 0.0014094429596303907 9.643118124695637e-5; -2.136946949242237e-6 0.0016182538053450542 0.001469320259721435; -0.0010179758472387214 -0.0015415366889768261 -0.0013817475745741834; 0.0010195871608452375 0.0008420132615949181 3.8449651782027246e-5; -0.0005890142987096223 0.0005363428861297643 -0.00019314820375804405; 5.4419370893862574e-5 0.00012825628903297972 -0.0002940011855877241] %
+
+Mass Used: 181.56643134766273 kg
+Launch C3: 89.03344117661477 km²/s²
+||V∞_in||: 0.001506355238268114 km/s
diff --git a/archive/ES_0.6008186954678758 b/archive/ES_0.6008186954678758
new file mode 100644
index 0000000..36e8645
--- /dev/null
+++ b/archive/ES_0.6008186954678758
@@ -0,0 +1,22 @@
+archive/ES_0.6008186954678758---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:09:15.466
+Launch V∞: [6.927727960526041, -7.292070085680889, -1.658736998697838] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0003453169261416539, -0.000527111687702812, -0.00020200280730061398] km/s
+ V∞_out: [-0.0004049658381372186, 0.00039955235954418036, -0.00030125758977354893] km/s
+ time of flight: 1.2619800465472451e8 seconds
+ arrival date: 2028-05-07T13:09:19.466
+ thrust profile: [0.35757438577964706 -0.15362190625589578 -0.19606163296422832; 0.1213177254432395 0.001841365897054457 -0.15367741344467883; 0.11142150054273836 0.0228230976631355 -0.22320964771333687; 0.12128913066673057 0.03885430055015188 -0.33050891974395724; 0.05982342112174477 0.02215311433044405 -0.1995355071085453; 0.027092063292290303 0.011078267899887355 -0.10560175311682699; 0.012381439251368696 0.005934279180465829 -0.05800974699428331; 0.011116002591989608 0.006359460210943819 -0.05827279936325949; 0.011771155682680019 0.00593635520789457 -0.06422723881390162; -0.001313007635887352 -0.003136665139312346 -0.01876395394601856; -0.001855040180663145 -0.001493154568463612 -0.001762790335764452; -0.002573572778061514 0.0008958803666999693 -0.01453231148176346; 0.0025909066446160485 -0.00429827971487994 -0.001964410002205471; 0.0002226675034122475 0.002600295467793349 0.005179396836491448; 0.017031797388475683 -0.0012112061200875383 0.008914801755253353; 0.0027204024747398974 0.001034348943553838 -0.002732398543621048; 0.00017851631747280064 0.003006312925739502 0.010197084009268899; 0.002853062881776676 0.01576972923035561 0.013557332613678915; 0.004984468894422492 -0.0007104585106259062 0.006428453293517556; 0.0065702010821324566 0.030745486214218968 0.01419232545140766] %
+
+Mass Used: 94.7603406936064 kg
+Launch C3: 103.9191092603855 km²/s²
+||V∞_in||: 0.0006617368396501409 km/s
diff --git a/archive/ES_0.600865266511571 b/archive/ES_0.600865266511571
new file mode 100644
index 0000000..109706f
--- /dev/null
+++ b/archive/ES_0.600865266511571
@@ -0,0 +1,22 @@
+archive/ES_0.600865266511571---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:03:56.241
+Launch V∞: [5.130174602050293, -8.501195378692314, -1.3428362031793544] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.4385738029759562, -0.28114015497788175, 0.26946828772801135] km/s
+ V∞_out: [-0.3794971081827469, 0.36036901470205757, -0.2648307511912442] km/s
+ time of flight: 1.2526757376570013e8 seconds
+ arrival date: 2027-04-12T11:36:49.241
+ thrust profile: [0.5142236063604431 -0.3733113065183223 -0.29465841085189076; 0.21484326033602935 -0.03895050039391626 -0.24295153757036236; 0.18421247069129537 0.0031517915021853447 -0.31112276076258033; 0.13423743279427108 0.016942920038835074 -0.2947784229362305; 0.0842294523523638 0.01657618162791397 -0.2229155419891791; 0.02639803149669603 0.006588331671583467 -0.07866351853484262; 0.015326280051897382 0.004999795876490894 -0.045678524071068566; 0.00828690782953469 0.00284747600619255 -0.030672761166640534; 0.01095110049926177 0.005372649197868452 -0.022691988014408325; 0.0030620478181077656 -0.0019496984579241462 -0.029269184357574838; 0.005425109428273896 0.0008442186343713242 -0.03121386958851895; 0.0037399739431154527 -0.0024020808296219653 -0.009003442700527588; 0.002858796563189124 0.0012582870536890693 -0.009720330084691722; -0.00409921697903344 -0.00808953151523419 -0.014168996061329809; 0.0014465223037846053 -0.004760518896341815 0.003967352467710637; 0.004334555183805609 0.012967373050360687 -0.005291696803989908; 0.0005523763984976876 -0.003858125205882726 -0.007808742463169498; 0.002456266592263419 -0.0028081961379624633 -0.005632319711245932; -0.0029596023162856352 -0.015835250452688104 -0.01290939280340982; -0.01549572943363619 -0.0060771034373318464 0.0006924482146386532] %
+
+Mass Used: 115.38817453055435 kg
+Launch C3: 100.39222338279059 km²/s²
+||V∞_in||: 0.5865150684243726 km/s
diff --git a/archive/ES_0.6010053028772363 b/archive/ES_0.6010053028772363
new file mode 100644
index 0000000..1b05cff
--- /dev/null
+++ b/archive/ES_0.6010053028772363
@@ -0,0 +1,22 @@
+archive/ES_0.6010053028772363---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T22:42:06.797
+Launch V∞: [6.970130354761212, -7.197174912286732, -0.8238560820120506] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003282958149685322, -0.020056084838985033, -0.022548184613217327] km/s
+ V∞_out: [-0.026428931681616655, -0.0031651303898360787, 0.014568330642387354] km/s
+ time of flight: 1.268279174591209e8 seconds
+ arrival date: 2028-05-13T20:40:43.797
+ thrust profile: [0.4162517786774398 -0.1931244562750332 -0.2323660083026409; 0.11593792066347039 -0.0032201736028088473 -0.14463102138018138; 0.18512906767150433 0.028121128415170563 -0.3773082546814197; 0.10796980955272041 0.02359778051659937 -0.29059019853285417; 0.0565646217791756 0.014350737451974866 -0.183634080306787; 0.05002983290113128 0.014747929196407068 -0.18237299001984952; 0.038398220433342574 0.011223368238968969 -0.16019442991501018; 0.008595056019507432 0.002300405539973562 -0.03610498785362696; 0.00862902048880273 0.010072025266844396 -0.011638149211832847; -0.002337210354908512 -0.004159218992748094 -0.006991213008722248; 0.0003323741280830672 0.010793290161141878 -0.007647671618324201; -0.003984893793986306 -0.005914517641578973 -0.008266231194738372; 0.004763508985484636 0.0014009467991105428 -0.007507897119593957; 0.0015073033845580425 -0.008465883027915296 0.0006497596275963609; 0.0071179792911824115 0.00829062520120184 -0.0021129678141004462; 0.000118523785089548 2.021987138632058e-5 -0.0005208787445527944; 0.014547828654657029 0.012968946172293175 -0.02391457307518382; 0.005000646362828825 0.0014202935308509016 -0.007098748096234688; 0.0011468725975988933 -0.021105081197082144 -0.021687367432286497; 0.04328878812964633 0.010011142443127802 -0.006066354516669056] %
+
+Mass Used: 111.65162079846732 kg
+Launch C3: 101.06078272428144 km²/s²
+||V∞_in||: 0.030355312263801226 km/s
diff --git a/archive/ES_0.6011180446132398 b/archive/ES_0.6011180446132398
new file mode 100644
index 0000000..9239aab
--- /dev/null
+++ b/archive/ES_0.6011180446132398
@@ -0,0 +1,22 @@
+archive/ES_0.6011180446132398---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:14:17.035
+Launch V∞: [7.051192028522879, -7.315181110364433, -1.648644903639051] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002875226569798559, -0.004481434760495258, -0.001689603831213231] km/s
+ V∞_out: [-0.0036049781309065417, 0.0036105497360748194, -0.0022743593921231006] km/s
+ time of flight: 1.2318368425695133e8 seconds
+ arrival date: 2028-04-02T08:55:41.035
+ thrust profile: [0.2534752154585925 -0.11393739431508884 -0.14477340271487377; 0.10646325133521464 0.001023200424988197 -0.14018846488574538; 0.09574516835658395 0.01900722096342257 -0.19662252693109555; 0.08125830300354515 0.02482052967123603 -0.22349871899092139; 0.060711535106841095 0.02281593790932112 -0.2061785312135962; 0.04434552654728971 0.01873880462015383 -0.1765499049922982; 0.029049260526966558 0.012602243572384451 -0.13077857420396252; 0.018394780379046717 0.008309112702867636 -0.091740517651937; 0.011580573170594622 0.005527358514660916 -0.05724309161269026; 0.004903857081301038 0.0035984915685607416 -0.030100492514163593; 0.0019513912459301387 0.0005985569745287622 -0.011530217918628224; 0.00027122278144640357 0.00045835558901234717 -0.0027230405039693007; -0.00014537341379989265 0.0002918256987646182 -0.0015195946960014244; -0.0021911974108240247 0.00107021489170882 -0.0034563334452947033; 0.001052302965842255 -0.0008374426874581677 -0.0016149443610555792; -0.001587129361248172 -0.000672955674723837 -0.004189381143876283; -0.0005396921651223685 0.0014551896291887714 -0.0015129699591535564; -7.504546583442153e-5 -0.0003634143949393762 -0.00042763724305489785; -0.0007358733815784292 0.0011920508862764698 -0.0007383177983459846; 6.681543941961508e-5 -0.0013030010813352027 0.00034982896799569277] %
+
+Mass Used: 83.26730535559182 kg
+Launch C3: 105.94921371883221 km²/s²
+||V∞_in||: 0.005586138777966513 km/s
diff --git a/archive/ES_0.6011898287785594 b/archive/ES_0.6011898287785594
new file mode 100644
index 0000000..6dae724
--- /dev/null
+++ b/archive/ES_0.6011898287785594
@@ -0,0 +1,22 @@
+archive/ES_0.6011898287785594---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:35:54.519
+Launch V∞: [6.994851746944507, -7.282818308749511, -1.4770368161843295] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.532188309807999e-5, -7.844639096968179e-6, 5.318939644332918e-5] km/s
+ V∞_out: [5.2923636957349774e-5, -4.141479334298105e-5, -2.0712461299616155e-5] km/s
+ time of flight: 1.2837566274881537e8 seconds
+ arrival date: 2028-06-02T01:30:16.519
+ thrust profile: [0.23470684712710246 -0.09907785031141245 -0.12624385456688444; 0.11181040690684563 0.003023603317039842 -0.13732054402793392; 0.09945543923242695 0.021237466783611422 -0.1944131874898018; 0.08270059655024156 0.026308035495394337 -0.21827687940203552; 0.07304485322758425 0.02812815255017701 -0.2381743307092364; 0.035316297925830804 0.014115695591724467 -0.13265655810820984; 0.020710835179463212 0.008071329756898775 -0.08219570827762147; 0.00907741339594293 0.010602584288350236 -0.044175826477148905; 0.023053073211431394 0.008269084425716338 -0.1104994859835432; 0.003950939022759319 0.0022295834728367544 -0.017825844525540462; 0.021385260740278772 -0.011963456901074337 -0.02361073003778721; 0.03634598419812403 0.003098806234868822 -0.0453869341893546; 0.00013760407999745264 0.0006218104681208665 -0.001342093892024796; -0.003141282121564606 0.004163447359767771 -0.010321795577513199; 0.027352592310183416 -0.022454974811436254 -0.038100975333131684; -0.014493014630194048 0.002920387689237923 -0.01799638693107283; -0.004998765896556496 0.00748969453605579 -0.01381483908758343; -0.010618118606815044 -0.024123803455492247 -0.018797524821627568; 0.0245886674809317 0.010014392614232086 -0.02097831674638007; -0.004967058920575934 -0.0013088523609310458 0.0007680989327698488] %
+
+Mass Used: 93.85211802958975 kg
+Launch C3: 104.14903123635365 km²/s²
+||V∞_in||: 7.031872683804328e-5 km/s
diff --git a/archive/ES_0.6014032487985833 b/archive/ES_0.6014032487985833
new file mode 100644
index 0000000..a9785f9
--- /dev/null
+++ b/archive/ES_0.6014032487985833
@@ -0,0 +1,22 @@
+archive/ES_0.6014032487985833---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T07:16:29.491
+Launch V∞: [6.838451157254024, -7.341210659194764, -1.6410319292724511] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00025986192101561004, 0.0003121121062498679, 0.00015958920690737678] km/s
+ V∞_out: [0.0002522059557836996, -0.00033448227163156955, 0.00016119307065127757] km/s
+ time of flight: 1.2390795039421137e8 seconds
+ arrival date: 2028-04-11T10:08:59.491
+ thrust profile: [0.5308980289973667 -0.24402180772597346 -0.29700207239450377; 0.10868309372092291 -0.0010189610205503681 -0.14038498654537376; 0.11764288280825065 0.019146224299551477 -0.23917481953028816; 0.09083453614239279 0.023429753666887942 -0.24818731316204937; 0.06037674972487871 0.020983502305485336 -0.20299827842469667; 0.0364193619991554 0.01103620694074306 -0.1555195818607895; 0.014682390046624486 0.005765819098602078 -0.06887729460551278; 0.010747032898701341 0.0038627683932905333 -0.05407188748451836; 0.0028278631311308903 0.0009142826038802899 -0.009749981025037456; 0.005245838870013861 0.0018125234511588207 -0.031095297090659786; -0.002044911914392147 -0.0005817510454380784 -0.006101304364760778; 0.0005820033747609872 0.0012579474690971903 -0.004512833942542695; -0.0011141497947309152 0.001656095910773841 -0.004698929375783692; 0.009633953688044067 -0.0048205350544516905 -0.006557577243010372; -0.007736223500217082 0.0005792465629212908 0.0015900824211508126; 0.003999257770323814 -0.009408339401993007 -0.015261113182500105; -0.0034723344493765886 0.006213492377931536 -0.007075130819454555; 0.007023916567758422 0.01367335936286424 -0.006070376762468913; 0.002886812424323062 -0.006419042488656259 0.00461534769389769; 0.003239729484666331 -0.00030996640373026835 0.004146513062219045] %
+
+Mass Used: 98.7576087983407 kg
+Launch C3: 103.35077396571539 km²/s²
+||V∞_in||: 0.00043636097422085937 km/s
diff --git a/archive/ES_0.6016033784436293 b/archive/ES_0.6016033784436293
new file mode 100644
index 0000000..f093e15
--- /dev/null
+++ b/archive/ES_0.6016033784436293
@@ -0,0 +1,22 @@
+archive/ES_0.6016033784436293---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T09:12:58.163
+Launch V∞: [7.112802140242451, -6.9341175580960055, -1.1801701231784298] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010255512322577867, -0.009290490678266797, 0.007299313975046156] km/s
+ V∞_out: [0.007449257155479421, -0.013546215739914706, 0.0024059381062106785] km/s
+ time of flight: 1.2511196592546636e8 seconds
+ arrival date: 2028-04-19T10:32:23.163
+ thrust profile: [0.529897670924023 -0.21200560437942031 -0.23542175354840783; 0.24084814898875676 0.024438239381453404 -0.2399725834076938; 0.20383639862186495 0.06846275676579508 -0.31433940011482364; 0.1608445045267596 0.0782291280763439 -0.33059938477771794; 0.10744705748137205 0.06429619276638866 -0.2730223715565856; 0.051696657527001574 0.03595935904481663 -0.15746165078176066; 0.014576660810056296 0.010187127790557814 -0.04992101090258716; 0.009613035120113538 0.007878833002416817 -0.038439482739457013; 0.009886937671405227 0.007951567757195587 -0.04113168003011997; 0.00277839606437027 0.002230854757867412 -0.01215343226272442; -0.0012838004754974642 0.002529735357482528 -0.005930013776064803; -0.0017059244075051244 0.0020573980806853995 -0.0014556995677187533; 0.002999742040990125 0.000660635789019518 0.0010967051363883805; 0.002026067067538836 0.002016665439107954 -0.0023501210889202433; 0.0025962841720212366 -0.0011690638409354247 -0.0039602798597815694; 0.00034623245544793525 -0.001631384589398294 0.000703468669779027; 0.0016429929653524406 0.001556353110023315 0.0006946163535019893; -0.0012175361501437912 -0.0013961917647229757 -0.003966009167930655; -0.0016627015701751128 -0.0008386810847256549 -0.0013564454751037146; -0.0013397678295868159 -0.001338043492930244 -0.004863266533144383] %
+
+Mass Used: 118.14794584454148 kg
+Launch C3: 100.06674211537589 km²/s²
+||V∞_in||: 0.015645086594449163 km/s
diff --git a/archive/ES_0.6018170231825046 b/archive/ES_0.6018170231825046
new file mode 100644
index 0000000..94a733a
--- /dev/null
+++ b/archive/ES_0.6018170231825046
@@ -0,0 +1,22 @@
+archive/ES_0.6018170231825046---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T06:53:19.260
+Launch V∞: [7.1709865991702495, -6.933390667235636, -2.6095732446691065] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0031481883284778245, 0.0026918964337883824, -0.0020560299216179057] km/s
+ V∞_out: [-0.0013934446441620518, 0.0043872117399306135, -0.00043559236044147457] km/s
+ time of flight: 1.3187212434463185e8 seconds
+ arrival date: 2028-07-09T14:02:03.260
+ thrust profile: [0.23049536153302627 -0.0857042851098696 -0.12314733254731561; 0.13080935909166347 0.018663679372417478 -0.15999868167299847; 0.11035665373437167 0.043473360136497025 -0.21528999196960252; 0.08879839650780288 0.04967812236565422 -0.2345886756225333; 0.0601807318699617 0.04244947354747645 -0.20189556905035455; 0.027559021757934794 0.022774113487262892 -0.11480217189134506; 0.020327758352552534 0.018450417473951295 -0.09716728822222585; 0.007033137813284499 0.006734454870319986 -0.039418274763290746; 0.0016081735278865054 0.0012839164651713849 -0.010140468485888416; 0.0032225861309984408 0.0036861524123193955 -0.022735674062311365; 5.322499607412438e-5 -6.532003864148547e-5 0.000388850177225941; 0.0035711513368500113 -0.001322390231452355 -0.0015688512652214117; 0.002025300456682969 0.0028651779667328552 0.005604509159022973; 6.19171208687504e-5 9.92705514832866e-5 0.00538394151216798; -0.003262835559895946 -0.001600792767890178 0.0057786893685105; 0.0052866804922629684 -0.006954137635092958 -0.006551068129693196; -0.0034988749809532404 0.0002576865909992447 -0.004775310725782995; 0.0010613124266788039 0.0008082699850426038 -0.003638275523456862; -0.0042877742706157835 0.011801546717215085 -0.004821244497078287; 0.008234792635052385 -0.004150453440989854 -0.003560722309268915] %
+
+Mass Used: 82.00836680877501 kg
+Launch C3: 106.30482746928236 km²/s²
+||V∞_in||: 0.004624354571223398 km/s
diff --git a/archive/ES_0.6018526501411726 b/archive/ES_0.6018526501411726
new file mode 100644
index 0000000..cc1a517
--- /dev/null
+++ b/archive/ES_0.6018526501411726
@@ -0,0 +1,22 @@
+archive/ES_0.6018526501411726---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T12:49:48.596
+Launch V∞: [6.976247746675405, -7.329038218124173, -2.0502609604649153] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0029958207096124124, 0.008330169810000723, 0.016758135027233476] km/s
+ V∞_out: [0.01635765258841025, 5.980897759614838e-6, -0.00953404471346666] km/s
+ time of flight: 1.2627121705063778e8 seconds
+ arrival date: 2028-05-09T00:10:05.596
+ thrust profile: [0.25774549603033464 -0.10862563784943217 -0.14162328373526312; 0.08568100740903303 0.0025447872501228068 -0.11505082345712024; 0.09489581178818694 0.020699573488119433 -0.18483129222362846; 0.040671182079915894 0.012022359874455078 -0.10746440259783425; 0.07751367168004493 0.03117560388473918 -0.2523097931681853; 0.024142979391607026 0.007805628045719717 -0.09270660583159603; 0.018251126012940037 0.01115894357960719 -0.08337711543022104; 0.017814945378189638 0.009332793477119069 -0.09502787982597072; 0.005982697695134282 0.005200240448564396 -0.04059118393653847; 0.0006176767071166887 0.00395073070034316 -0.015369447814884226; 0.02480187075840147 0.015328574428039497 -0.14993972177240647; 0.0010796605190646381 0.0005753167232384231 -0.005163487587416649; -0.0013423210825475643 0.0003986163490420692 0.0028622277689078213; 0.001729345846835829 -0.0012716168413768427 0.002155804842300813; 0.0032093892209711862 -0.0001326258924696798 0.0011316860328980996; 8.046915647015877e-5 -0.0030960379086537775 0.0012241556041198845; -0.010638692554169866 0.005591117338050433 0.002220218805721976; -0.007261584195964886 -0.01015259510755033 -0.0010127014463741427; 0.005284041670098868 -0.004700403217212065 -0.001541259020870852; 0.0037242517562446737 0.01116334079905133 0.00430094756448877] %
+
+Mass Used: 80.40740281297258 kg
+Launch C3: 106.58640383172494 km²/s²
+||V∞_in||: 0.018952618826393878 km/s
diff --git a/archive/ES_0.601910979702 b/archive/ES_0.601910979702
new file mode 100644
index 0000000..9acef32
--- /dev/null
+++ b/archive/ES_0.601910979702
@@ -0,0 +1,22 @@
+archive/ES_0.601910979702---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T23:18:38.770
+Launch V∞: [6.924589520718285, -7.289501556362635, -1.3651229281918889] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0037532439388189296, -0.005739326476639454, -0.0022886860802992207] km/s
+ V∞_out: [-0.004108540254076438, 0.005224041181453235, -0.002798980195192278] km/s
+ time of flight: 1.2299968023996776e8 seconds
+ arrival date: 2028-03-30T13:53:18.770
+ thrust profile: [0.4352124096243086 -0.18710630986384721 -0.2237913929206574; 0.17962496016726548 0.009154707105593577 -0.20943908958434113; 0.129973320157749 0.03383955254171924 -0.2364181495406397; 0.09946598712527639 0.038480277285653675 -0.24110884735564297; 0.05892475485346143 0.02852655988401916 -0.17817026841308173; 0.025397140258159513 0.011683182396594455 -0.09137750067963821; 0.01168464966230514 0.006765214037513014 -0.04821984676784531; 0.03747617558033711 0.021107767349819246 -0.16568169725116477; 0.03183304753616005 0.019779579504070367 -0.1531773187784987; 0.006211712324671462 0.006078778598730011 -0.03844667934676977; 0.003432955687091531 0.0010900184944272152 -0.014875939841457426; 9.550009142320015e-5 -0.00046490032544070224 0.0017644692962890376; 0.0016681815695509313 -0.0014066588590892451 0.0023527309467495632; -0.00033678531855758497 -0.00047919760433914584 0.002047070000932863; -0.0005778911838576444 0.0008568045876810044 0.0008392658278053469; -0.003285856474119711 0.0022629609771680852 -0.00038205867160134854; 0.0004431002613270792 0.000182278599739983 8.842995311133492e-5; 0.0003383126279543681 0.000190491232202175 -6.122027965061176e-5; 0.004186706210242535 0.0016854095030531921 -0.001825903625599767; 0.0015490999532712468 0.00194602779266467 0.002235073044698804] %
+
+Mass Used: 101.68586377057545 kg
+Launch C3: 102.95033357972994 km²/s²
+||V∞_in||: 0.00722943928972995 km/s
diff --git a/archive/ES_0.6019209206822032 b/archive/ES_0.6019209206822032
new file mode 100644
index 0000000..cd58614
--- /dev/null
+++ b/archive/ES_0.6019209206822032
@@ -0,0 +1,22 @@
+archive/ES_0.6019209206822032---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-29T04:45:29.896
+Launch V∞: [7.832474686033116, -5.553137050614067, 0.05427461168257872] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003390644799961223, -0.0009036453585205838, -0.002203414866394154] km/s
+ V∞_out: [-0.0021858155390700653, -0.00027027902377907545, 0.0009618165568659515] km/s
+ time of flight: 1.8563181497103426e8 seconds
+ arrival date: 2030-03-17T17:09:03.896
+ thrust profile: [0.6027139000982589 0.0003908802398016478 -0.08015283194157702; 0.4040079749520144 0.2895046268323944 -0.18424139286580726; 0.23188951238356287 0.29197523320103264 -0.1971509094231793; 0.12825586096502475 0.23289327223697665 -0.17242025403693204; 0.06277002570827696 0.1546284149915695 -0.12517338635607203; 0.016066249123775217 0.054059826292612745 -0.04860127854068414; 0.0012357033094907975 0.006514698421397765 -0.006730156042621377; 0.001975094063972443 0.011914719364570147 -0.012586488414601105; 0.0019471835823346932 0.013877732364552758 -0.014703377511068014; 9.996158291289225e-5 0.0012880945059018315 -0.001396875481546852; 8.114344891260912e-5 0.0012559171144498837 -0.0012068494876938795; -3.509698476889976e-5 0.0015900164093969578 -0.0019691121564390994; 0.0001678111416307485 0.0009051143620491058 -0.0011853754873635608; 0.0004490681290824342 3.8871520667324794e-5 -0.0008081932419444252; -0.00018866134469328372 0.0013281379673112748 -0.0029212014589594364; 4.6382248265085875e-5 -0.0004915118213249877 0.0004697882871141407; 0.0008623028989741799 -0.0014738720114025792 -0.0008798524178626468; -0.0008491268430587573 0.0002455609567022475 0.0003071327996701047; 2.68502080239444e-5 -0.00040824533711150603 -8.61711441465312e-5; 0.00040677823957949866 -0.000645318675470417 0.0022601337080375193] %
+
+Mass Used: 164.47811095750467 kg
+Launch C3: 92.18793654372556 km²/s²
+||V∞_in||: 0.0024055304464956585 km/s
diff --git a/archive/ES_0.6020459671988759 b/archive/ES_0.6020459671988759
new file mode 100644
index 0000000..8f5802f
--- /dev/null
+++ b/archive/ES_0.6020459671988759
@@ -0,0 +1,22 @@
+archive/ES_0.6020459671988759---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:56:49.225
+Launch V∞: [6.973745826872197, -7.307740389867658, -1.6298918154057516] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.9962206343840485e-6, 9.096674358988588e-6, -1.4737390206042831e-5] km/s
+ V∞_out: [-7.574955180442123e-6, -1.6680984255856396e-5, -5.312345054621359e-7] km/s
+ time of flight: 1.2420710740864338e8 seconds
+ arrival date: 2028-04-14T05:55:16.225
+ thrust profile: [0.3123588517036486 -0.13910230991236927 -0.171937430149435; 0.1540987017071667 0.0018061512478550687 -0.19262359849405658; 0.1170542310086142 0.02337785449417321 -0.23002209994629869; 0.08871860371459524 0.02713744627271403 -0.23446288072052004; 0.05413457453925238 0.020454155038995198 -0.1789926052820671; 0.020187580325511115 0.008884721997485646 -0.0789459530224343; 0.016473943383011152 0.009488166836985997 -0.07887235978726923; 0.025018446096191565 0.01222468528376352 -0.12429620142849429; 0.021636791461697613 0.008713899780318201 -0.10649528528482034; -0.0003806717362378298 -0.000668963215138962 -0.004413246876597701; 0.004402269577346702 0.0009613065441098377 -0.0160473884544604; 0.003450900030799625 0.006635014447300071 -0.01913110465368705; 0.005239532694484737 0.0009357651245982374 -0.006051555168765077; 0.0005574291926272314 0.006286643855164186 -0.009307919816242394; -0.0028391241130955236 -0.0034323903894136866 -0.006740892625770745; 0.019526467663961433 0.0012423341724524344 -0.006930508048558516; -0.007370211421270134 0.0009598946183913006 -0.005753838963976536; 0.00015177542939115454 -0.00474236228272345 0.0004919983502629866; -0.001641917516748831 -0.0010103952436007317 0.0016403273088129756; 0.0005819293209976154 0.017359359963637293 -0.007242657185958127] %
+
+Mass Used: 91.6792662702469 kg
+Launch C3: 104.69274779344714 km²/s²
+||V∞_in||: 1.8327433436650662e-5 km/s
diff --git a/archive/ES_0.602070271952896 b/archive/ES_0.602070271952896
new file mode 100644
index 0000000..b43cde0
--- /dev/null
+++ b/archive/ES_0.602070271952896
@@ -0,0 +1,22 @@
+archive/ES_0.602070271952896---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T11:53:57.360
+Launch V∞: [6.916148078533005, -7.324510235394433, -1.6927326252865023] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002719055136025705, -0.004431468477026187, -0.0015990229394976909] km/s
+ V∞_out: [-0.0030844717490515093, 0.003909291847313249, -0.0021898221184744188] km/s
+ time of flight: 1.216367318231079e8 seconds
+ arrival date: 2028-03-15T07:52:48.360
+ thrust profile: [0.49943294190630266 -0.1929649082905348 -0.2412515502971063; 0.12890268124043672 0.0016835676475057322 -0.16175141318022657; 0.09920361746469109 0.02065446762317536 -0.19395627657764467; 0.0791402592066587 0.02529840254294084 -0.2061146946852897; 0.06009655727930593 0.0238094414902127 -0.19326366362164213; 0.044403829805956724 0.019735931676925916 -0.16617024728755814; 0.03067602730241053 0.01462169034197622 -0.12916121081918902; 0.019391639204074187 0.009732843361291273 -0.08937090524149781; 0.01593025202411274 0.008838899424831964 -0.08162778324205394; 0.0004492302503770482 0.0004082023026083631 -0.004046102063545382; 0.0001800607406125387 8.311059731571124e-5 -0.0010222959898289808; 0.0008733180104672107 0.0005383000526344295 -0.006163050411186611; -3.921399047885811e-5 -2.3234996609532908e-5 0.00013629979553031257; -1.1692181128969756e-5 6.756484777303118e-5 -0.00013364460761754334; -7.266649448349418e-5 0.00021289802604466756 -0.0002853826884806036; 1.658978329879872e-5 -2.57581523035289e-5 -0.00010321417122187836; 0.00018029085226268533 0.0002248275524132476 -0.00020109120419767857; -8.332548195957596e-7 5.6860088612028123e-5 -0.0006682655187666225; 0.0004394354942597778 6.695913864400931e-6 0.0002884634328003267; 6.271430637144287e-5 -0.00012169988338451009 -7.765469318676322e-5] %
+
+Mass Used: 93.7250779341116 kg
+Launch C3: 104.34689817330292 km²/s²
+||V∞_in||: 0.005439489687154889 km/s
diff --git a/archive/ES_0.6023426466966257 b/archive/ES_0.6023426466966257
new file mode 100644
index 0000000..f40ef45
--- /dev/null
+++ b/archive/ES_0.6023426466966257
@@ -0,0 +1,22 @@
+archive/ES_0.6023426466966257---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T03:55:47.116
+Launch V∞: [5.134960166107679, -8.565940888343693, -1.4913456964024823] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.867904901042362e-7, -1.517920488942624e-7, -2.573278749903228e-7] km/s
+ V∞_out: [1.8083085609235276e-7, -2.3944246664119825e-7, 2.864417733037593e-7] km/s
+ time of flight: 1.2282239489386255e8 seconds
+ arrival date: 2027-03-15T17:15:41.116
+ thrust profile: [0.5083218869676989 -0.3770802985103609 -0.30623949791864347; 0.2351978596642658 -0.047269866095388385 -0.28259139162562075; 0.15221036596655674 -0.0005683103757469166 -0.27290793505235095; 0.09345200500004301 0.009640545139583455 -0.21930831316851185; 0.04388829692132831 0.00750612581401018 -0.12657539530972278; 0.02689721164480621 0.005811875489582777 -0.08984889157904243; 0.01984209821303589 0.005277415726478084 -0.07463434275093733; 0.027375122681677386 0.007781702518731596 -0.11112199038047899; 0.026615039260375124 0.005841952607763109 -0.10313764536439923; 0.005006082575400798 0.0016936894371029985 -0.02450616530356027; 0.0015168370288608946 -0.0007550814269965503 -0.001112612937053716; 0.0007279756104302978 0.000400293125898443 -0.002263245847764008; 0.0005725465845402171 -9.465892178208324e-6 -0.001913953151360846; 0.00016556063877058724 0.0006351190486379983 -0.0010246527282338916; -0.000767884784480246 -0.0001419540520238512 0.00019645842354282185; 0.0014051530959654792 -0.0011423800110013128 0.0010195783125061114; 0.0019901338520725426 -0.0001552216585765945 -0.005697650094509248; -0.006074436509098995 -0.0021205200630933395 -0.0009550375450240738; 0.0012663233514080261 -0.0020524443804578836 -0.0024935557141587544; -0.0002754458641241887 0.0012470367162505372 0.003051761798460232] %
+
+Mass Used: 107.92400583437666 kg
+Launch C3: 101.96727119628915 km²/s²
+||V∞_in||: 4.1413433396517775e-7 km/s
diff --git a/archive/ES_0.6024074029295066 b/archive/ES_0.6024074029295066
new file mode 100644
index 0000000..21fbfe3
--- /dev/null
+++ b/archive/ES_0.6024074029295066
@@ -0,0 +1,22 @@
+archive/ES_0.6024074029295066---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-12T04:41:06.326
+Launch V∞: [5.754058452595725, -7.532874457627389, 0.46441052521328907] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.5796821855028133e-8, 4.174350562176307e-8, 2.806038236173698e-8] km/s
+ V∞_out: [-1.3124090738455408e-8, 2.8782678614316412e-8, -4.768534160657505e-8] km/s
+ time of flight: 1.575639099396067e8 seconds
+ arrival date: 2028-04-08T20:26:15.326
+ thrust profile: [0.9105240335242143 -0.4101551736183483 -0.18825077201848936; 0.5755994364199659 0.09484647308728561 -0.3204173012478086; 0.28496552070465947 0.1278114320983278 -0.2578177594547806; 0.14963115141888195 0.09670773701885502 -0.18357127155004088; 0.14962682227210578 0.12121916256037266 -0.22440971842404162; 0.06250192054715682 0.0591534515790273 -0.11426712350959982; 0.004852660503010888 0.005243873737932251 -0.011130359736819823; 0.0012957899577895188 0.001518841876019449 -0.0030716150715334204; 0.000602123290991732 0.0008840076704174376 -0.001843036345517137; 0.00026889863936727624 0.001383426301585648 -0.0018656275067745003; 0.004436697467133754 0.0069830804877764096 -0.014346547104830359; 0.0005585440784365953 0.00091973362953976 -0.0009652289127217215; 8.36472515602934e-5 -0.00011443304412171523 -0.00022072337883428358; 7.507875863484409e-5 0.0005831679683395602 -0.0009016896463449372; 0.00014296543864330917 0.0007781540793295084 -0.001228474953369584; 0.00047710583650942176 0.001091361031346176 -0.00038497883099050613; -0.0007017626228268141 0.0007785931799908742 5.0905801190880114e-5; 0.0002195360738797657 6.048796590402985e-5 1.9471255292509643e-5; 2.2250354809343607e-5 -7.574055233329057e-5 -0.0006408427713357314; -0.000430319837562948 -0.0007948404961209969 0.00021484845656184965] %
+
+Mass Used: 177.40576688163583 kg
+Launch C3: 90.06906340619233 km²/s²
+||V∞_in||: 5.652770416089001e-8 km/s
diff --git a/archive/ES_0.6024228158131731 b/archive/ES_0.6024228158131731
new file mode 100644
index 0000000..e7ad505
--- /dev/null
+++ b/archive/ES_0.6024228158131731
@@ -0,0 +1,22 @@
+archive/ES_0.6024228158131731---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T13:52:01.227
+Launch V∞: [6.935527712148012, -7.291942683187331, -1.6293584198160416] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005632149874066867, -0.00540831720179902, 0.004041550948350789] km/s
+ V∞_out: [0.0036274271329115107, -0.007929216767863422, 0.0011314011621535586] km/s
+ time of flight: 1.2093940451247914e8 seconds
+ arrival date: 2028-03-06T08:08:45.227
+ thrust profile: [0.39895540319362505 -0.17972168769389996 -0.20520327111265926; 0.23398942286171948 0.006376192394470249 -0.2547753349460687; 0.17267515729269442 0.03984555183556466 -0.29172174151992314; 0.1221803053430131 0.043209860685483846 -0.2770603318537095; 0.07664938334801814 0.034025737783984794 -0.21924403329740025; 0.02126269660348685 0.011055689228290769 -0.0746811810567742; 0.01830909263867623 0.010906010014817552 -0.06979908105900069; 0.008629343444022207 0.005112041690386154 -0.03875979520702858; 0.01101584081437867 0.007246408584377032 -0.0493608007582389; 0.009971379111591771 0.004874483697620686 -0.04482734720840291; 0.00011888219828421834 0.0002699118069128798 -0.0009992014202771238; 0.00011971817321923742 0.00012588604863029594 -0.0008270175188377507; 6.643068350238881e-5 0.00024119057616381296 -0.0007967416851470444; 0.0003738529257801311 -0.00011891766283687416 -0.0005826844200835747; 0.0003961789698512289 -6.09673257773543e-5 -0.0001294547184223654; 0.00011016506598173283 0.00010278364450015083 1.1528582725909967e-5; 0.0003567648636928244 0.0002760612908239078 -0.00046915912426759494; 8.788746121804518e-5 -1.8342786511635112e-5 -0.0003371949174231643; 0.00010753149791813859 0.00013112219562784317 -0.0001880476511278838; 0.00020792053405762376 -9.469641963501246e-5 -9.615829695828793e-5] %
+
+Mass Used: 96.57539244235704 kg
+Launch C3: 103.92878160108772 km²/s²
+||V∞_in||: 0.008792334230870764 km/s
diff --git a/archive/ES_0.6027069615442054 b/archive/ES_0.6027069615442054
new file mode 100644
index 0000000..bfea99e
--- /dev/null
+++ b/archive/ES_0.6027069615442054
@@ -0,0 +1,22 @@
+archive/ES_0.6027069615442054---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T16:52:41.729
+Launch V∞: [6.954512979798792, -7.349714829079589, -1.5868979833091759] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0016077199967610763, -0.0027576777805695903, -0.0010046039812585616] km/s
+ V∞_out: [-0.001991586378887332, 0.00234195792476222, -0.0012576776969370686] km/s
+ time of flight: 1.2280299470375873e8 seconds
+ arrival date: 2028-03-29T00:49:15.729
+ thrust profile: [0.32189571104922776 -0.1439590218822073 -0.1667909500308057; 0.15219689390983268 0.003409438889793617 -0.17648085640641722; 0.12184979914608905 0.026013522594045893 -0.21835907402869367; 0.09423204676209625 0.03074587082355086 -0.22501438281840797; 0.06624637420525112 0.027202835138196664 -0.19568483921199178; 0.026669779654204286 0.013286751339180686 -0.09833373862094412; 0.016801711858460095 0.009235388423505537 -0.06880568821621914; 0.018935825097889235 0.008499805031839084 -0.08744531953871221; 0.021316002272142483 0.010536764164257587 -0.10119450506895597; 0.015503063748596627 0.00922305130884722 -0.0780080750537034; 0.013497513037461257 0.008611550140919036 -0.06612913541478535; -0.0028550398433748623 0.0006852724650217546 -0.0017104247938474792; 0.00048818790167942064 0.00014354906767491223 -0.0005345237429570503; -0.00010879975004508106 -0.0013048151518584177 0.0006475509747499112; 0.00047462821534855534 -5.372517374014788e-5 -0.001426056072790317; 0.000850862165777628 0.0001440135631279893 -0.0004660278047201023; 0.0005029971752495622 0.00446432763800756 -0.0027688340110529792; -0.0011742282638619681 -0.00193330027469864 0.00021095145694581194; -0.00014807634955535956 -0.0022473610598425417 -0.0024776506838803405; 0.00043561110931167107 -0.0014097352009981548 0.0010430647681004298] %
+
+Mass Used: 91.23093142583048 kg
+Launch C3: 104.90180406441301 km²/s²
+||V∞_in||: 0.003346457752399275 km/s
diff --git a/archive/ES_0.6028110113503995 b/archive/ES_0.6028110113503995
new file mode 100644
index 0000000..829294e
--- /dev/null
+++ b/archive/ES_0.6028110113503995
@@ -0,0 +1,22 @@
+archive/ES_0.6028110113503995---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T09:54:48.074
+Launch V∞: [6.948767983341534, -7.2927018351338955, -1.6246767106159448] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-8.150577900802553e-5, -0.0005276406246748535, 0.00035714583416169594] km/s
+ V∞_out: [0.00019190017495580579, 0.0004889069358507439, -0.0003306237906445153] km/s
+ time of flight: 1.2380420465728493e8 seconds
+ arrival date: 2028-04-09T07:58:12.074
+ thrust profile: [0.3710811467244181 -0.16455714536714655 -0.20185033611842396; 0.16859715995053762 0.0022915608203793094 -0.20557184876171836; 0.11436230251416053 0.023259466996208573 -0.21947044563179352; 0.07630843987653232 0.02363797649790727 -0.19890918662539042; 0.07705169475898628 0.028306591631420287 -0.23050494631161678; 0.030962301774100937 0.012784868584838942 -0.11468770444825388; 0.03993108929218097 0.018197416223105046 -0.16715437325741792; 0.008565397328645133 0.00388309686667725 -0.04857848111164984; 0.010443499684526536 0.00631380992019242 -0.05757633929688253; 7.870180513982333e-5 0.002221571613376087 -0.006677025482030578; 0.0019473323479437393 0.00016653992174638522 -0.007094849130935689; 0.0010846348000348423 0.002410715225273632 -0.00673678943681273; 0.0046492784547352405 0.005675938077386102 -0.009557178068144328; 0.0004126107307680102 0.00013931037706461664 -0.0017173059275271089; 0.0011710567429093679 -0.0029812112301497613 -0.005455336478289193; -0.005713202943273529 0.00834228524474773 -0.00014046173585751526; 0.0008362710444444856 -0.00266527457892203 0.011155068254928995; -0.0008276355275001809 0.002122917581252979 0.004170472581308546; -0.008316824314383846 -0.010475042734835521 0.022735164297037584; -0.006227625552847721 0.002198464105755724 0.024077575112003494] %
+
+Mass Used: 95.98021599590902 kg
+Launch C3: 104.1084509564955 km²/s²
+||V∞_in||: 0.0006423402273546538 km/s
diff --git a/archive/ES_0.6031075958189711 b/archive/ES_0.6031075958189711
new file mode 100644
index 0000000..f59860b
--- /dev/null
+++ b/archive/ES_0.6031075958189711
@@ -0,0 +1,22 @@
+archive/ES_0.6031075958189711---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T18:54:33.497
+Launch V∞: [5.179127012489045, -8.634992182371706, -1.6096925421528554] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0062021362977216785, -0.00496580733750475, 0.00010629843900572071] km/s
+ V∞_out: [0.0027423629836488233, -3.858056741219662e-5, -0.007458032298671812] km/s
+ time of flight: 1.2215321943419984e8 seconds
+ arrival date: 2027-03-08T14:21:32.497
+ thrust profile: [0.4183769009107767 -0.3194682419863599 -0.26637182151221833; 0.14945325445869795 -0.03323117559631843 -0.1877433997059386; 0.14899764335546725 -0.005372719249664638 -0.2781624728765809; 0.11006617948320997 0.007006331241359465 -0.26786161340907055; 0.06607339890295921 0.008578405768570503 -0.19612838765281526; 0.031182577147265956 0.005168760959095714 -0.10760833358957653; 0.02145392107054954 0.004640361751503673 -0.0840226917988472; 0.01302562182791434 0.0031354804792389016 -0.056568175029940486; 0.004218678272656548 0.0014661033517603202 -0.028069410073144004; 0.0009878492635584742 0.00040025174920607675 -0.001759698413787789; 0.0006872917614508729 0.0003326130875922046 -0.001968517844059129; 0.008595745873470884 0.0022745935269059786 -0.0456539407436729; -0.0011475049127200538 0.0008306998707234517 -0.00029424542121529815; -0.0009152163972095144 -4.9623739870856146e-5 -0.0007934394839432739; 0.0002583160836697455 -9.752310972473404e-5 -0.0008515401746955157; 0.0021324806881584946 -0.0005999767949572244 -0.0009743677550886629; 1.495679229884819e-5 -4.807653773483502e-5 -0.0005275667338280159; 0.0005374616970412198 4.9334316487618934e-5 0.00021511570349350367; 0.0032756202060667218 -0.0013940761690014953 0.0010794366846151103; 0.003267049866498795 -0.00027069342309243654 -0.002946718370757423] %
+
+Mass Used: 97.08978114743559 kg
+Launch C3: 103.9775566813767 km²/s²
+||V∞_in||: 0.007945881733757924 km/s
diff --git a/archive/ES_0.603431259200211 b/archive/ES_0.603431259200211
new file mode 100644
index 0000000..642e28b
--- /dev/null
+++ b/archive/ES_0.603431259200211
@@ -0,0 +1,22 @@
+archive/ES_0.603431259200211---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T18:24:17.121
+Launch V∞: [6.884633731750392, -7.2264973760144615, -1.327914181921072] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00286897248173562, 0.004632852607489017, 0.001756645694249566] km/s
+ V∞_out: [0.0022346718596305574, -0.0029006592766153507, 0.004401063851617478] km/s
+ time of flight: 1.2523909668352017e8 seconds
+ arrival date: 2028-04-25T07:02:33.121
+ thrust profile: [0.49569430710458534 -0.21415735978303252 -0.253791688689836; 0.17637387598320473 0.007664882107693436 -0.2067222243461754; 0.15782739620910352 0.03794535866387577 -0.2874887527381602; 0.12167216317509882 0.04361481486408058 -0.29686732999514265; 0.05602895924751222 0.025166854609451204 -0.17197013913604955; 0.032664665983021215 0.018482236600186865 -0.11084459578493432; 0.027618380181974746 0.01683417920547968 -0.12543626461653945; 0.015248148903035016 0.009298776617847395 -0.04950960510052746; 0.009456041742520434 0.0003774045054009186 -0.039747993981346756; 0.002543400344488674 -0.005341968260250801 -0.009633584892796018; -0.0053099891145019455 -0.005322027196568262 -0.023570466127770997; 0.01083152111538387 -0.011975893358524023 -0.003964552923936304; 0.002478935051317947 0.0209218890073326 0.0033922466584178947; -0.0013016992320418642 -0.002115107366644436 -0.012683205260767515; 0.00022317558833977874 0.0018138169883757786 -0.004387657581362613; -0.00896312636885739 -0.007295387652327675 0.008746160983844207; -0.0030721149989998333 0.0066326279457483645 -0.006073216569882017; 0.012034722061566897 -0.006286297696061215 -0.003341630959256994; -0.02359405033180132 -0.007816086302460536 0.021606688743343344; -0.04476448754853958 0.013644909234080859 -0.018082294239086482] %
+
+Mass Used: 112.59762394764266 kg
+Launch C3: 101.38380202044632 km²/s²
+||V∞_in||: 0.005725393478076382 km/s
diff --git a/archive/ES_0.6034409405098868 b/archive/ES_0.6034409405098868
new file mode 100644
index 0000000..b229b7b
--- /dev/null
+++ b/archive/ES_0.6034409405098868
@@ -0,0 +1,22 @@
+archive/ES_0.6034409405098868---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T00:59:52.432
+Launch V∞: [5.313017971391461, -8.352170320618889, -0.6818852077366573] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.09343199999865491, -0.10795817117510247, 0.023947486737157592] km/s
+ V∞_out: [-0.13088615781136348, -0.05736721540450638, -0.0231222563424899] km/s
+ time of flight: 1.3497387387884116e8 seconds
+ arrival date: 2027-08-02T05:44:25.432
+ thrust profile: [0.3999243692344135 -0.2561298160056433 -0.19755400970708287; 0.143178756974432 -0.01684581728153864 -0.15969973814354485; 0.1291197498212529 0.011145708928860503 -0.21788729372819132; 0.08326572029272203 0.015919871187915366 -0.18678585760591082; 0.0893912498280836 0.025002111005176703 -0.24070079709911588; 0.04484778833309347 0.013643391902480042 -0.1421425300056081; 0.05219547268691606 0.01931580575186822 -0.18303210067966835; 0.041298976107274524 0.017095061730501605 -0.164672578913591; 0.0066620959850750144 -6.560682574559447e-5 -0.03204559742760619; 0.0030605777876958717 0.001753369557989899 -0.006766818327989919; 0.008248537163270286 0.006625111915320178 -0.016184294213738543; 0.005309401522850924 0.006812732129915846 0.006150658661822533; 0.023961127437411273 0.015320122171649362 0.010946175629643852; 0.04956289785106356 0.02935935998376863 -0.03854862716359985; 0.022608926893061817 -0.0038428473121193993 -0.029363605204673168; 0.0015286073944890432 0.009476990217424671 -0.0005599467934834365; 0.003374272942006291 0.02889251794354967 -0.049496265950256274; 0.06059650660865727 -0.023411156864094434 -0.004480068752032868; -0.041838607992111615 -0.000298454175652119 -0.02542947623789535; -0.008754154965341482 0.06541700244831933 -0.0129721285788977] %
+
+Mass Used: 129.71181787953446 kg
+Launch C3: 98.45187646548574 km²/s²
+||V∞_in||: 0.14476873788303785 km/s
diff --git a/archive/ES_0.6035095793298881 b/archive/ES_0.6035095793298881
new file mode 100644
index 0000000..f1c7e63
--- /dev/null
+++ b/archive/ES_0.6035095793298881
@@ -0,0 +1,22 @@
+archive/ES_0.6035095793298881---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-28T19:51:55.251
+Launch V∞: [7.087452010284046, -5.7693559917033195, -0.39114936675269624] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.664139637505441e-7, -3.1582166884550016e-6, 6.82391206796164e-5] km/s
+ V∞_out: [2.9731845803454757e-6, -6.836322013681447e-5, 8.079120889113218e-7] km/s
+ time of flight: 1.8749577786843583e8 seconds
+ arrival date: 2030-04-07T22:01:32.251
+ thrust profile: [0.9786393222985765 -0.006551083130072152 -0.12207884329348018; 0.5425468861093125 0.397997696482861 -0.23221558187848634; 0.3220934829601056 0.41368522003975 -0.2583312694594252; 0.15042858693076439 0.2802768852065273 -0.19656344904647627; 0.05055275842944206 0.12873889717507242 -0.10249173201430714; 0.004597731547987946 0.015018479626294615 -0.012967449613649155; 0.0027337751799008823 0.011725989290983542 -0.010325411738879638; 0.0013951710403802494 0.007537613022870186 -0.005522687769868457; 0.0002435076094798857 0.0012818587131554402 -0.001796664605490697; -0.00014992082446709472 0.0009183360370159174 -0.000976860301992107; -0.00016169644023129382 0.001245467031041073 -0.0011007202070789596; 0.0007478184746439859 0.0010913212634563727 -0.002078456059124409; 2.9822758711271855e-5 0.0007136308666281609 -0.0006666491751639646; -0.0005054605555128407 0.0015151008323897107 -0.001520250002132309; -0.0006920945855154748 -0.00045317369911119284 0.0005148458226679244; 0.0003646043923797248 -0.00077536947200751 -4.5971108123091546e-6; -0.00027234864078186263 0.0021791501930812536 -0.0009128993650161411; -9.015193882306888e-5 0.000438921246013528 -0.0005356827476450778; -0.0017770238151840658 0.0002874593634827557 -0.0025207080685736797; -0.00011778003994204322 -9.285677102595434e-5 0.0001295756552480528] %
+
+Mass Used: 216.01692864374127 kg
+Launch C3: 83.67044238419341 km²/s²
+||V∞_in||: 6.831375751460366e-5 km/s
diff --git a/archive/ES_0.6035189100082798 b/archive/ES_0.6035189100082798
new file mode 100644
index 0000000..3680f12
--- /dev/null
+++ b/archive/ES_0.6035189100082798
@@ -0,0 +1,22 @@
+archive/ES_0.6035189100082798---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T13:29:17.583
+Launch V∞: [5.219753096070866, -8.607661841392003, -1.7263381006920138] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.039198547916476194, 0.03396728015502974, 0.03434496959063286] km/s
+ V∞_out: [-0.028610424972422825, -0.04464035127779677, 0.0325417820023217] km/s
+ time of flight: 1.229983970045493e8 seconds
+ arrival date: 2027-03-18T03:42:34.583
+ thrust profile: [0.42364984964800656 -0.302051341084336 -0.24399078197341412; 0.15050274943749933 -0.026270875314884458 -0.18468865284601554; 0.08520553760871875 0.0027539091820965055 -0.16125418432651048; 0.059877419771671755 0.009013161641534144 -0.1496581821551958; 0.0570328258533468 0.012626541891934953 -0.169687206145462; 0.04923127312897379 0.012998102623136228 -0.16429584796971902; 0.026339440504732747 0.008079978403749959 -0.0965934278207046; 0.015179180167807754 0.005582586051988903 -0.06869161591511233; 0.03983110735871537 0.01423061222735567 -0.16840500350104476; 0.008260716686650295 0.0038815943790526633 -0.04044778134988733; 0.008641367926194025 0.0037133271070896204 -0.04720193164034929; 0.0004522611010557149 0.0002847327406691754 -0.000687426758238909; 0.0002120652866019275 -0.00030844112970661406 0.0005576953345401533; 0.0005261971263183399 0.0004969177654228758 -7.347537940476911e-5; 0.0002563717268384684 -0.0003959848101208276 -2.4604367032190458e-5; -0.00021598029900731522 -4.58661597045532e-5 0.0010612983908407725; -0.000648563380021437 0.00020055942339052552 0.0007669215630272479; -4.089884073269092e-5 -7.171798626184108e-8 0.00010977596975920241; -0.00046688258782125376 -0.0010284323477122567 0.00033367168845524584; 0.0008019977679761926 0.0013248297446380327 -0.0001962925426487092] %
+
+Mass Used: 95.58426502367001 kg
+Launch C3: 104.31790799759827 km²/s²
+||V∞_in||: 0.06220835326603698 km/s
diff --git a/archive/ES_0.6035382576275503 b/archive/ES_0.6035382576275503
new file mode 100644
index 0000000..f9efbf4
--- /dev/null
+++ b/archive/ES_0.6035382576275503
@@ -0,0 +1,22 @@
+archive/ES_0.6035382576275503---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T07:32:21.148
+Launch V∞: [6.9277162726399535, -7.2560318386358675, -1.2653422404459986] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005949374899873088, 0.003791060847788914, 0.0005855714547759362] km/s
+ V∞_out: [0.003671717055257765, -0.0007155368690284013, 0.001085598104712141] km/s
+ time of flight: 1.2187203306167832e8 seconds
+ arrival date: 2028-03-16T20:52:54.148
+ thrust profile: [0.4487443635719456 -0.200439222053129 -0.22917480844381913; 0.2593465443873552 0.005172858285770245 -0.290435496300751; 0.12385676450716705 0.027244918939226988 -0.21597804939199713; 0.15149947030936814 0.049483640200533835 -0.34714288576105184; 0.08361985073702899 0.034520618083357775 -0.23794915879197454; 0.038737887942013424 0.018206308832011946 -0.13197632049554073; 0.016077296668214336 0.008888402831080944 -0.060580015176191604; 0.004534922801214632 0.002366579812498842 -0.022226257005028453; 0.0033138172722410597 0.004146651750812284 -0.025206966084018317; 0.01573690070665311 0.012129307960274302 -0.08386905906916496; 0.001958403488071115 -0.004736137550562368 -0.006824676206869384; 0.002760556482783806 -0.0028031198659972784 -0.002076435442246256; 0.00043591486639804394 0.00036529752809882476 -0.0015291767773407293; -0.003976269414649712 -0.0015347453977164088 0.002410977882352333; -0.0029515512366171054 0.0002495920321678688 -0.0009795856409910708; 0.010470738297869172 -0.0021246098228649233 0.00505045092153549; -0.0031424706132675336 0.0005801340030927658 -0.002155659661673398; -0.00029926952849398687 -0.007669799532647544 -0.0063054223031339274; 0.0100706883928342 -0.0009020265381064672 0.005747179201047132; -0.0025914466243057714 0.002346830426540279 -0.001963356791120082] %
+
+Mass Used: 107.70264016490637 kg
+Launch C3: 102.2443417829547 km²/s²
+||V∞_in||: 0.0038818792996793195 km/s
diff --git a/archive/ES_0.6036395827617569 b/archive/ES_0.6036395827617569
new file mode 100644
index 0000000..4d1fe50
--- /dev/null
+++ b/archive/ES_0.6036395827617569
@@ -0,0 +1,22 @@
+archive/ES_0.6036395827617569---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-13T06:37:57.369
+Launch V∞: [5.65851486869059, -7.678401424676238, -0.048224219254990604] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.022032477581489e-8, 4.672230598851757e-8, 3.149322679294283e-8] km/s
+ V∞_out: [-1.2190961833252936e-8, 4.875721512259791e-8, -4.041814423476301e-8] km/s
+ time of flight: 1.5056826608945364e8 seconds
+ arrival date: 2028-01-19T23:09:03.369
+ thrust profile: [0.914096346115709 -0.44662532692369267 -0.22322004483586907; 0.3895671830210289 0.05324753253343308 -0.23315700428091646; 0.2427927560886469 0.10292642652859632 -0.22409333596187025; 0.16008226170508238 0.09981828420342875 -0.1992966409072268; 0.08852881643017743 0.06883787348550965 -0.14079537447157658; 0.058895401776867994 0.05245958624637962 -0.10915483217834766; 0.08021365426670321 0.08015940723150983 -0.16632806393138758; 0.03455077225933552 0.03855614529187786 -0.08430399900017004; 0.03954539270755793 0.044347839880281334 -0.09761415337352766; 0.0003621828299731388 0.0006117007803055875 -0.0021709389255177803; 0.0004344720221725702 0.00048661350218414594 -0.0014693212512682284; -2.4077605467819822e-5 0.0002516811225402272 0.0006773508599822154; 0.0015800709764094943 0.00023996679334650252 -0.00032754885941944857; -0.000854768162271266 -0.0008503864822340117 0.0020628279431842145; 0.0010077942378146972 0.002474366366924255 0.005315837220760026; -0.0005331103169386149 -0.0020859155107391045 0.0013707499740690582; 0.0020031930282076458 -0.005451060561943577 -0.0010661116176241903; -0.0006332116521423382 -0.0027084803072493623 -0.008476578466999993; -0.0015324815409629205 -0.002955596213963201 -0.007425676256820258; 0.0010310528128993947 -0.0022805421848122506 0.005420311052548392] %
+
+Mass Used: 173.53555344630195 kg
+Launch C3: 90.97896453298533 km²/s²
+||V∞_in||: 6.39379796386477e-8 km/s
diff --git a/archive/ES_0.6036479637243589 b/archive/ES_0.6036479637243589
new file mode 100644
index 0000000..eb1733b
--- /dev/null
+++ b/archive/ES_0.6036479637243589
@@ -0,0 +1,22 @@
+archive/ES_0.6036479637243589---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T12:35:03.781
+Launch V∞: [6.938375717895406, -7.237353999614936, -1.4468110275737054] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002946955026275499, -0.00471871010414966, -0.0019269572459289105] km/s
+ V∞_out: [-0.003616508815525624, 0.004133805191632748, -0.0021209030595563576] km/s
+ time of flight: 1.2242189523757732e8 seconds
+ arrival date: 2028-03-23T10:39:58.781
+ thrust profile: [0.5024440358553797 -0.22297079090922128 -0.2604721281178429; 0.1698726182276575 0.0027154773910507564 -0.1980636039899221; 0.14373706629037367 0.0302160934592916 -0.26138431509116583; 0.10940779900838976 0.035179646680988295 -0.26554238293838145; 0.0475908338069899 0.019539607407126777 -0.1472651127058939; 0.07013441717518726 0.030962105365793146 -0.24314926145410787; 0.029777675382067326 0.013900385318871498 -0.11273256974564617; 0.002306620822613674 -0.0004467201783064027 -0.00943407150766348; 0.005980347121892974 0.0030647151800800424 -0.028054258900023794; -0.005245633490428181 -0.003567539393223738 -0.012925363593792753; -0.0044499807625419975 0.0021452258331578194 -0.0027152411646191874; 0.0067383837161017306 0.0028926429831707804 -0.01609271639078414; -0.000585593617920648 0.005538425860468774 -2.3295576110165216e-5; -0.004213108269466442 0.0005076404398965273 -0.0251798087954448; 0.002457973049369385 0.005600561142736957 -0.010015288238582143; 0.00040632329158659243 -0.0008861719667882908 -0.006992552480872867; -0.00034266796670492233 0.0020054181203690187 0.0011002326705785272; 0.0009598889013573237 -0.0021243338361681165 -0.005065522747987279; 4.762143612427967e-5 0.012995980513113374 -0.025189441112139086; -0.018044040138051637 -0.0016975488581471875 -0.004416157424631398] %
+
+Mass Used: 105.67655044881667 kg
+Launch C3: 102.61361266793179 km²/s²
+||V∞_in||: 0.005887608444991265 km/s
diff --git a/archive/ES_0.6037859242658309 b/archive/ES_0.6037859242658309
new file mode 100644
index 0000000..5bc9f5a
--- /dev/null
+++ b/archive/ES_0.6037859242658309
@@ -0,0 +1,22 @@
+archive/ES_0.6037859242658309---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:06:16.503
+Launch V∞: [7.260384643151612, -6.762176164072271, -0.5981937445706389] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7827880306065407e-6, -1.444028021126212e-5, 0.0002777721803042009] km/s
+ V∞_out: [1.06176458091231e-5, -0.0002777334527260198, 2.9237301030689283e-6] km/s
+ time of flight: 1.5042531856702298e8 seconds
+ arrival date: 2029-02-12T11:54:54.503
+ thrust profile: [0.205206402985353 -0.06032490424871861 -0.08743482081766465; 0.15601840208542692 0.029241495140086005 -0.17469517246681707; 0.05701166187507685 0.01996342681681732 -0.09509756885756206; 0.03846441663227825 0.013652533405069374 -0.07885842132835709; 0.04449685788151257 0.02464313699079541 -0.1350284149063206; 0.07930930442852263 0.05475824181060508 -0.3401505043070907; 0.03671064053643111 0.022917576317655865 -0.15833108125409015; 0.01956868489481968 0.02028169630938638 -0.04958205176637321; 0.002321883574107003 0.0013407011867336636 0.010084833822106315; 0.013440881617212318 0.003060868607661637 -0.04468238222051281; -0.008150599649176549 0.009903333422646987 -0.027787540207336186; 0.00794664524136059 0.031954292168629564 -0.0565448008760237; -0.016242050725662753 0.05473750006952291 -0.034149009174019834; -0.0004144217825673734 -0.010420520310390344 -0.01625473455090532; 0.09400203445039604 0.013645726486190973 0.04572820963624893; -0.09560924317547961 -0.0045227712135865955 -0.06858332052375656; -0.05365306551880167 -0.05194459255900537 0.04907072258864195; -0.005241036213011236 0.003979870042378138 -0.006207132727806121; -0.014434985783471868 -0.06024678547562859 -0.06643846617030615; -0.054001135921913225 0.022155265547837075 0.08056918081670089] %
+
+Mass Used: 128.09496849720563 kg
+Launch C3: 98.79804739650237 km²/s²
+||V∞_in||: 0.0002781529869994053 km/s
diff --git a/archive/ES_0.603995760708997 b/archive/ES_0.603995760708997
new file mode 100644
index 0000000..e487991
--- /dev/null
+++ b/archive/ES_0.603995760708997
@@ -0,0 +1,22 @@
+archive/ES_0.603995760708997---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T23:47:45.650
+Launch V∞: [5.21733028317509, -8.587879672301739, -1.4517726180341113] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.09986355794613296, 0.04781076286928513, -0.10862953338083808] km/s
+ V∞_out: [0.09648221208684583, 0.04216270238924335, 0.11388774326813043] km/s
+ time of flight: 1.2176244094572255e8 seconds
+ arrival date: 2027-03-03T06:41:45.650
+ thrust profile: [0.44701291782279634 -0.32761846519093485 -0.2625881152844669; 0.1985991026919163 -0.040660658048002694 -0.2363050712309434; 0.1334925607235602 -0.0020911913464839106 -0.2377646591413742; 0.09429087438062544 0.008370445239483859 -0.2187972740270373; 0.06314514283335376 0.009761478451181832 -0.17705897504388743; 0.05310365177460688 0.01004368570148369 -0.1703998280683148; 0.032216951905748005 0.00823776852613566 -0.11718529122725596; 0.02408307684482816 0.006930284549586455 -0.09426610838240658; 0.011416678012822272 0.0037505084651544103 -0.04907512869860884; 0.0031762916108004696 0.0004770337036162507 -0.013169131062783255; 0.000855962534437796 -0.0006126579060202359 -0.004612409931051596; 0.0024596858841242682 0.0011883623539890881 -0.012316930706266672; 0.00025699018611612166 0.00021748795891585976 -0.000978308201246148; 0.000748638464371686 0.00029393957344725843 -0.0033454974351610728; 0.000942231192532251 -0.0007153177978503895 -0.004044649069128431; 0.0017879695231671137 -0.0016955006086225798 -0.0025701315695949812; -2.4672764529809574e-5 0.0008478589961947529 -0.004438474900185673; 0.0012170922209674034 0.0033406262609254043 -0.0007814009166919034; -0.002125080561374576 0.0014383858961171223 0.004151326205905638; 0.0005224491250794599 0.00017944914425234752 -0.003041063334209838] %
+
+Mass Used: 103.36255916966275 kg
+Launch C3: 103.0798562841429 km²/s²
+||V∞_in||: 0.1551095573275299 km/s
diff --git a/archive/ES_0.6040208065083343 b/archive/ES_0.6040208065083343
new file mode 100644
index 0000000..510a66c
--- /dev/null
+++ b/archive/ES_0.6040208065083343
@@ -0,0 +1,22 @@
+archive/ES_0.6040208065083343---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-27T07:24:33.864
+Launch V∞: [6.703288370549707, -5.970617605544571, -0.23748971011122802] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4798535099098836e-9, -1.0326489184801556e-9, -1.7764152085438303e-9] km/s
+ V∞_out: [4.650365457937631e-10, 9.730075229873963e-10, 2.3883981999578016e-11] km/s
+ time of flight: 1.8300007870126346e8 seconds
+ arrival date: 2030-02-13T08:45:51.864
+ thrust profile: [1.0 -0.07301585804258892 -0.1237770015414152; 0.7833754746348144 0.4879445849891755 -0.3031070721848283; 0.44152773467870926 0.4936362415172658 -0.31328399124279827; 0.16303610530006965 0.2627481053363735 -0.1853472278989174; 0.0366366496208964 0.07230053068229489 -0.051197006322581465; 0.004207588588797904 0.012362420992971154 -0.010736936454929836; 0.002653335881393658 0.009577160006273209 -0.008678458842714848; 0.0005365132027809979 0.0029451672353898906 -0.002954814588082504; 0.00016975666856170499 0.0010119806994246432 -0.0009690293070953282; 0.00019861924424318918 0.0009134572808424962 -0.0010298475397176386; 4.0676257195770935e-5 0.0008380085353454198 -0.001055517552855304; 0.00016422150049238157 0.0005940827428346881 -0.000478511895983275; 2.188115950585868e-5 0.0004547900285850854 -0.0005294372767527854; -0.00012435220841089612 0.0004130711489118855 -5.091536087009613e-5; -1.3785463372680723e-5 0.0005668710515434858 -0.0006969063772872974; 0.00042190563493814805 0.0006368181306577059 -0.0005397840111106373; 2.266809112684005e-5 0.0007853012047203283 -0.0007558872241779837; -8.305818302526276e-6 -2.0346978512382203e-5 0.00011400178788656011; 0.0007592395754721524 0.0002605500178852354 0.00032490700809416177; 0.0002090651713523722 0.00024729137043951886 -0.00012815012925504655] %
+
+Mass Used: 234.29822715175578 kg
+Launch C3: 80.63875093279445 km²/s²
+||V∞_in||: 2.5321890120559045e-9 km/s
diff --git a/archive/ES_0.6040242901619046 b/archive/ES_0.6040242901619046
new file mode 100644
index 0000000..632435f
--- /dev/null
+++ b/archive/ES_0.6040242901619046
@@ -0,0 +1,22 @@
+archive/ES_0.6040242901619046---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-29T11:49:25.704
+Launch V∞: [8.007039362556998, -6.800564683114872, -0.24868571183973304] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.8158171785525086e-6, -4.110036650500258e-6, -4.1961521963052843e-7] km/s
+ V∞_out: [3.513900545311201e-7, -1.7402747212619549e-6, -4.6738647945280575e-6] km/s
+ time of flight: 1.8749577787367094e8 seconds
+ arrival date: 2030-05-08T13:59:02.704
+ thrust profile: [0.06739569923563209 -0.02391219278525224 -0.0390473305028688; 0.009852282202471717 -0.005213823606093633 -0.020918125733079655; 0.0243827596324672 -0.02023166374639446 -0.07461976278332225; 0.02325561066380988 -0.026663647354937713 -0.0926191662403106; 0.02580822431938147 -0.033305749924684526 -0.11176618872099525; 0.023099673488236983 -0.03144423061378721 -0.10492778013999152; 0.019145152182254734 -0.026088949095453104 -0.08586211949317361; 0.020076961243505283 -0.02779339987001067 -0.09206585716112987; 0.007814336270987772 -0.009950854026772291 -0.03353301599142446; 0.01196995980545403 -0.014344134527102936 -0.051478309451175694; 0.0019969345447322664 -0.002639429973076289 -0.009034211216673239; 9.930199423038017e-5 -0.00020886477456894716 -0.0005946847354176037; 6.609819848463017e-5 -0.00010135748847935847 -0.00030752011888985514; 5.7012229223808285e-5 -0.00013778315186928312 -0.0005309978820451436; 7.815149756724223e-5 -0.00011983555224870222 -0.00036202431521813855; 0.00023109427838912316 0.0002068433938058587 -0.00043962083083127373; 0.00013319366555003166 0.000162228771645882 -0.000200637718729872; 0.000280181390671892 -0.0010163872117368 -0.0002520406961079556; -4.88941495873023e-5 -4.2065261087015165e-5 0.00011802139749590913; 0.0001839361300099517 0.0001585000963664053 -8.770078583883933e-5] %
+
+Mass Used: 60.565482170323776 kg
+Launch C3: 110.4222039460397 km²/s²
+||V∞_in||: 4.999730451137578e-6 km/s
diff --git a/archive/ES_0.6040882803659875 b/archive/ES_0.6040882803659875
new file mode 100644
index 0000000..064ca99
--- /dev/null
+++ b/archive/ES_0.6040882803659875
@@ -0,0 +1,22 @@
+archive/ES_0.6040882803659875---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:15:11.067
+Launch V∞: [7.021169296893441, -7.274909697895246, -1.5964082305970542] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.478796972807892e-5, 0.0001108156953930105, 6.128709271000475e-5] km/s
+ V∞_out: [0.00010307086911285556, -7.551583621951129e-5, -4.143689857992215e-5] km/s
+ time of flight: 1.2842806287250681e8 seconds
+ arrival date: 2028-06-02T15:42:53.067
+ thrust profile: [0.19562652582896284 -0.08653185342449694 -0.11242246156786663; 0.10878267615247399 0.001623728349160418 -0.14600517210265695; 0.11520301792383919 0.02034705265550588 -0.24496253648810648; 0.08514991302462548 0.023230598346186175 -0.2458523698031939; 0.0686235787582623 0.022588222695104524 -0.24545360265050925; 0.04445947948059071 0.017289170233175666 -0.18756123953622028; 0.03385871320264033 0.01430788209178934 -0.16225184997877795; 0.004416095797497975 0.006122711226738951 -0.02482640126066667; -0.00074458023427395 0.004304083673837732 -0.011088989181841848; -0.0021094130763006144 -0.002818489932049655 0.0008347747092335772; 0.0016479779468649863 -0.0019026142587929107 0.0056097624515142; 0.001306932306378097 -0.002222017352588878 0.016292715491717537; -8.40837442610742e-6 -0.0033397678479929406 0.00940999111761028; 0.002817641812742079 -0.014742110390947211 0.019734422452226598; 0.011486961366169756 -0.015450088560525925 -0.008601464408179136; 0.011161290841270533 -0.002435897606314549 0.04267444607317161; -0.010780402779457524 0.0037949461630044055 -0.011439427393859794; -0.026478309405420498 0.017073390376162397 -0.0006181270260694958; -0.010293831929547243 0.019560441354900163 -0.010060094235577811; -0.01947894662016747 0.0018115951427675474 0.010618545171343648] %
+
+Mass Used: 93.61337665347537 kg
+Launch C3: 104.76964864688745 km²/s²
+||V∞_in||: 0.00013432121318185196 km/s
diff --git a/archive/ES_0.6041223453441731 b/archive/ES_0.6041223453441731
new file mode 100644
index 0000000..3c5382d
--- /dev/null
+++ b/archive/ES_0.6041223453441731
@@ -0,0 +1,22 @@
+archive/ES_0.6041223453441731---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T02:01:16.817
+Launch V∞: [5.4106742281187605, -8.560771155327604, -1.6487048159700552] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.07269474418991348, 0.037890819608352964, -0.08272490838023971] km/s
+ V∞_out: [0.07167996423991978, 0.03147301924447186, 0.08621316866119894] km/s
+ time of flight: 1.2279463813127756e8 seconds
+ arrival date: 2027-03-14T07:38:34.817
+ thrust profile: [0.24079365820977222 -0.17055479196904563 -0.14434133421998013; 0.15499394002006261 -0.024533890145431655 -0.18060123516353987; 0.14265642596962425 0.007662063185946109 -0.24283494903031974; 0.11560044666241798 0.02019103375322602 -0.25405379249568244; 0.08060200014812138 0.020562929839960456 -0.214628358516296; 0.04777187983538088 0.014817064448262073 -0.14940526507269078; 0.030546223906737086 0.010882769499585252 -0.107754202985213; 0.020081213314743503 0.00806444820683961 -0.0768201232282381; 0.012720747375282048 0.00460463285062007 -0.05388098963926079; 0.012413202379354907 0.003663192009461988 -0.050952569571078715; 0.0010114660809710926 0.0008357822014899483 -0.0027185568085014745; 0.0012395790889759434 0.0006366443549451518 -0.005602969946518978; -0.0003670578957066209 0.0040277074167817985 -0.00012198085162826286; 0.0004128481182238085 -0.0017929699852396782 -0.002828092040110736; 0.0013081105320291813 -4.2808266771331344e-5 0.0020353979903894037; 0.0015835824976393775 0.0013546187499268922 -0.005506687764916795; -0.00030582497691842127 -0.0016606103829677286 0.00032426187930703274; -0.0008399081394418017 -0.0006009016473803724 -0.00027208179855269616; 0.0033548373104878406 -0.00045678830838013183 -0.003131025660440834; -0.004239712889877038 -0.0025042092027132224 0.0007370567675679652] %
+
+Mass Used: 90.67358487783213 kg
+Launch C3: 105.28042594692053 km²/s²
+||V∞_in||: 0.11646308646927042 km/s
diff --git a/archive/ES_0.6042235879435702 b/archive/ES_0.6042235879435702
new file mode 100644
index 0000000..6bc897e
--- /dev/null
+++ b/archive/ES_0.6042235879435702
@@ -0,0 +1,22 @@
+archive/ES_0.6042235879435702---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:10:28.644
+Launch V∞: [7.000812557280067, -7.381665940872247, -1.8971378278592748] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0037564527321693165, 0.024632164621732275, 0.003773180415578436] km/s
+ V∞_out: [0.02372664148065939, -0.004979051058458382, 0.006877268354394219] km/s
+ time of flight: 1.2073443464853175e8 seconds
+ arrival date: 2028-03-05T07:31:02.644
+ thrust profile: [0.2583971823566804 -0.12430325645612508 -0.1399685164768842; 0.1587659766831901 -0.0027828583028863822 -0.1858178715010441; 0.11379435872918862 0.01880652173723014 -0.20870638722955; 0.08592909012672124 0.022205719764922343 -0.21163584973985386; 0.06184433606316573 0.02034763660310051 -0.18882248499380747; 0.044911878657693215 0.016648170073705375 -0.16138503759142767; 0.029822310914707512 0.011908130575655538 -0.1223986155695469; 0.017882495719979484 0.007511044920499353 -0.08218722037066568; 0.006772366448908816 0.002985398862332285 -0.03451824442930253; 0.0008334168169851116 0.0005358332840901125 -0.00412909064580398; 0.0005548508251462213 0.0005282799901250078 -0.0038409096989501573; -0.00015390007094199772 6.546964850395531e-5 0.0005538816357901997; 0.00011678436388967077 8.067320864390073e-6 -0.0005700101659666353; 0.0005494267367765988 4.1091027921672654e-5 -0.0022675343460555925; 0.00033314405401436796 -0.0013871654481448436 -0.0013491790045247881; -0.0005461624419377799 -0.0004858032673693322 9.005557723281219e-5; 0.001257039293188147 0.0015259473417035558 -0.00050484670547355; -0.00011005072658396638 -0.0007443582766954516 0.00038191288942466704; 0.0013421280573398026 -0.00032396456593695544 0.002234469155548143; -0.001652700315336939 -0.000863497221374292 0.0010240118435153522] %
+
+Mass Used: 80.1804332350921 kg
+Launch C3: 107.09950046269824 km²/s²
+||V∞_in||: 0.025201019057364448 km/s
diff --git a/archive/ES_0.6042501616091084 b/archive/ES_0.6042501616091084
new file mode 100644
index 0000000..0f5fb70
--- /dev/null
+++ b/archive/ES_0.6042501616091084
@@ -0,0 +1,22 @@
+archive/ES_0.6042501616091084---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T18:29:17.885
+Launch V∞: [5.15153904380604, -8.648666924666726, -1.5893863360747502] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.019243203173615265, -0.009845096545361653, 0.022124409881152288] km/s
+ V∞_out: [-0.019501766378826058, -0.008824578854409546, -0.022424983134729723] km/s
+ time of flight: 1.2016588640092482e8 seconds
+ arrival date: 2027-02-13T13:54:03.885
+ thrust profile: [0.490737169158833 -0.37573637154885686 -0.31632100392460444; 0.16118621636041658 -0.038057097873725854 -0.20414626323797916; 0.1478664447362914 -0.006752025447597476 -0.2776269994506896; 0.11520546126451274 0.005869796427365373 -0.28136142812612386; 0.08342247903311047 0.00872291606515773 -0.24688100721014022; 0.0377473450968801 0.0057964503345738945 -0.13021366728054615; 0.012198732835586054 0.0026092134535794986 -0.048161996244575615; 0.006723137635042669 0.001642080301480474 -0.02866163322917561; 0.002456341007350783 0.0005413406085566956 -0.011779676525988726; 0.00021086747975040723 4.595526344303197e-5 -0.001088680815265214; 0.0007641921750911609 0.00022636679239099888 -0.003991593704131887; -0.00013286558443445094 -4.0612294221571894e-5 -0.00027315299302072384; -4.2052011954974604e-5 -3.0080002706819398e-5 -0.00016807343059293924; 1.505468343019435e-5 6.086528550339448e-5 -7.664400880475075e-5; 8.97252207994569e-5 -6.383420837056567e-5 -0.00020692941194600648; 0.00015523969556981734 -3.714674020907803e-5 -0.00018165385219379133; 1.5012406319092153e-5 0.00015280356043062668 -0.00011968062066934305; 0.00020568374607611776 8.309108575650364e-6 -0.0002627132691652288; 8.316389665892371e-5 -2.0610453052602684e-5 -0.0002996394575005357; -6.445034194600745e-5 1.638392091523095e-6 -8.236929543332881e-5] %
+
+Mass Used: 99.0855209332235 kg
+Launch C3: 103.86394301898336 km²/s²
+||V∞_in||: 0.030930831009815394 km/s
diff --git a/archive/ES_0.6043787307197046 b/archive/ES_0.6043787307197046
new file mode 100644
index 0000000..5cbec20
--- /dev/null
+++ b/archive/ES_0.6043787307197046
@@ -0,0 +1,22 @@
+archive/ES_0.6043787307197046---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T02:29:57.596
+Launch V∞: [6.95671195955316, -7.328698601526264, -1.7603965543310485] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005619300752297209, -0.01635586796361646, -0.03494254610466107] km/s
+ V∞_out: [-0.03304849418051822, -0.006034268634005412, 0.019789014387563406] km/s
+ time of flight: 1.1946065718284126e8 seconds
+ arrival date: 2028-02-18T18:00:54.596
+ thrust profile: [0.41907563265398323 -0.19381439108845844 -0.2331714478197763; 0.19030190212590148 -3.997676405924866e-5 -0.23028710239008532; 0.1499093324304352 0.02910600107220976 -0.28088980847410966; 0.11370831792386597 0.03470925821902978 -0.2840079590726127; 0.06363820159856225 0.02382612732451416 -0.19714204868879; 0.036056873470525566 0.015207249853442904 -0.13118849862602192; 0.01635873766419658 0.007625151736549703 -0.06787340615122078; 0.006710678199703054 0.0034090454881635 -0.030946560956611347; 0.002872438887693317 0.0017133176821455826 -0.015046461154907391; 0.00025282696818188096 0.0002197932579658309 -0.002304573331358953; 0.00038168153099676314 8.240388148248086e-5 -0.0022636325174059516; 0.0003328729828610608 0.0001068747496797539 -0.0018209814034449217; 0.00031986794254119347 0.00019701782451045954 -0.0017668574975580648; -9.123273518154933e-5 -0.0002864596551771458 -0.0008510555347307594; 6.088166839900871e-5 3.3765656040749624e-5 -0.00047252931190009534; -0.0011848789486995186 0.0011580231174697021 0.0001645510840507647; -0.000664240367737047 -9.168678946555115e-5 0.000126153577543202; 0.0004728132470615624 4.330141454492535e-5 0.000360745747536841; 0.000532722905470738 0.0004362091609792716 -0.0008738058827008776; 0.0007788522301934581 -0.0005646375917650485 -0.00116971116620657] %
+
+Mass Used: 91.41466620555093 kg
+Launch C3: 105.2046605087036 km²/s²
+||V∞_in||: 0.038988106982314336 km/s
diff --git a/archive/ES_0.6047715644548125 b/archive/ES_0.6047715644548125
new file mode 100644
index 0000000..68059de
--- /dev/null
+++ b/archive/ES_0.6047715644548125
@@ -0,0 +1,22 @@
+archive/ES_0.6047715644548125---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T21:05:35.337
+Launch V∞: [7.033828796790316, -7.370447494905316, -2.061378054096614] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005386434739957887, -0.0008474335206836757, -0.00032367244920265104] km/s
+ V∞_out: [-0.0004921220519515826, 0.000817962389988839, -0.0004480964888189865] km/s
+ time of flight: 1.2035754052446212e8 seconds
+ arrival date: 2028-02-29T21:44:35.337
+ thrust profile: [0.25527069060320007 -0.1182605433534718 -0.1528087316194936; 0.12691814531288867 -2.4690793721373195e-5 -0.1674807088629229; 0.10380597801578656 0.020351120058437523 -0.21294062057381408; 0.09080638292107977 0.027800583327261496 -0.2546531341034432; 0.05404955490093706 0.020857128714530757 -0.18732567249001855; 0.039519366953872676 0.017411245416729355 -0.16099208635781073; 0.019164119613640243 0.009514050654370755 -0.09147531497878181; 0.005513115850103169 0.0025609262119657846 -0.02743594872237362; 0.0037982976193944545 0.0017246340967601791 -0.020723245897072206; 0.0007401151671107793 0.00029880151538530346 -0.002969945302013836; 0.00042208586802355846 0.0001301040285689991 -0.00498718110886904; 0.00044012825488606004 -0.0007882705571006171 -0.002477508040678484; 0.0002559787637313156 -0.00023686314206263002 6.563024805805381e-5; -0.00029504401650951267 0.00036475626171971983 -0.0006691786725474881; -0.0015537612027600456 0.00018607905231493658 -0.002340803297592371; 0.00014222317087607232 0.00017198783154176033 -0.0023531302103984913; -0.0015115413138558093 -0.0006368392987602112 0.0019293319237936842; 0.00022221523075131196 -0.00015018153214754054 -0.001900295775741705; -0.00017065090331625258 -0.0012040916411061114 3.3030569904977675e-5; 0.0007894657467818311 0.00019380088461592098 -0.0023095732802645612] %
+
+Mass Used: 75.28960594947512 kg
+Launch C3: 108.0475232996239 km²/s²
+||V∞_in||: 0.0010550091082210734 km/s
diff --git a/archive/ES_0.6048179364286307 b/archive/ES_0.6048179364286307
new file mode 100644
index 0000000..473e00e
--- /dev/null
+++ b/archive/ES_0.6048179364286307
@@ -0,0 +1,22 @@
+archive/ES_0.6048179364286307---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-11T11:13:15.700
+Launch V∞: [5.2567223565083205, -7.7127941664356365, 0.061977981919811485] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4895465883740399e-7, 3.815558091355197e-8, -4.803873497969189e-8] km/s
+ V∞_out: [1.5498327553797648e-7, -4.1710457493091804e-8, 1.949036071246389e-8] km/s
+ time of flight: 1.440228513404117e8 seconds
+ arrival date: 2027-11-03T09:34:06.700
+ thrust profile: [1.0 -0.5876713541943641 -0.2594537782360904; 0.8192970985462552 0.05303712660219369 -0.46633944035225955; 0.43756498178760167 0.1447211611907666 -0.387963617853224; 0.1882190534925838 0.09695374739616194 -0.22760481739659932; 0.08794572908911283 0.05804588344869697 -0.13496767193381742; 0.04428174303226459 0.034225189570907075 -0.07991807050830457; 0.044663934791049034 0.03898293534082657 -0.09070693891532618; 0.003246017903773114 0.0031024141583279844 -0.0076460186437215475; 0.0010666530377590946 0.001065134774688363 -0.0027233363031135193; 0.00023941280909702678 0.0002586761968927437 -0.00040959572368285345; 0.00015877811281782278 0.00014075086989364218 -0.0005477109696789111; 0.0002061596364479495 0.00013466617759496486 -0.0004703210511433988; 0.00016387401937042263 8.181187020969908e-5 -0.0001497542441999857; 6.610235980357209e-6 3.735638096707131e-5 -0.0002745456655734031; 0.00018684099172095272 0.000561068970285152 -0.00045209015424501833; 0.00037688065480195133 0.0005114422287583937 -0.000997615784635865; 0.0005993380467394295 0.0007027746274486747 -0.0009109831381786489; -1.5532899960657063e-5 -8.886930130169944e-5 0.000254822794938224; 0.00014764274460698018 0.0004499710180248051 -0.000930748577034534; -5.163702615456364e-5 0.0001250264312168702 5.463723717113295e-5] %
+
+Mass Used: 197.39662966488095 kg
+Launch C3: 87.12416505746083 km²/s²
+||V∞_in||: 1.6109332327153442e-7 km/s
diff --git a/archive/ES_0.6049041102343498 b/archive/ES_0.6049041102343498
new file mode 100644
index 0000000..e49290d
--- /dev/null
+++ b/archive/ES_0.6049041102343498
@@ -0,0 +1,22 @@
+archive/ES_0.6049041102343498---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T18:11:39.079
+Launch V∞: [6.944289356414305, -7.275764050006921, -1.555722986129214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008186711755878666, 0.04187637190092657, 0.04452271516479019] km/s
+ V∞_out: [0.05443897818083312, 0.006400639848648938, -0.028250111497595008] km/s
+ time of flight: 1.2067194271870306e8 seconds
+ arrival date: 2028-03-03T10:10:41.079
+ thrust profile: [0.4991525083063028 -0.2243662740914889 -0.27080730953985993; 0.18053646298712944 0.000943501460448203 -0.21606526472371337; 0.13744687804306174 0.027211852908165652 -0.2554136137488395; 0.09836781352956239 0.03025828633864496 -0.2436492938690229; 0.059181914256501975 0.022520180049216618 -0.18067480108376915; 0.03827668787036922 0.016544180774954644 -0.1373522438334226; 0.02135315982106469 0.010015603969909956 -0.08729022295766266; 0.03061733221528395 0.015030342946270184 -0.13507598841789506; 0.002127833820483405 0.00118585247659375 -0.010221007575661993; 0.0006030809824226618 0.0009633260117145736 -0.005540220996152408; 0.0034240182055521426 0.001838316223102984 -0.017761570909568893; 0.0009074677771506768 -0.0026764518218210607 -0.002197218971306434; 0.0003908055493036427 7.674893147680062e-5 -0.002091482958585788; 0.0036392583874421654 0.0027938467971973576 -0.0033727314750810764; 0.0010929542350791347 0.002283724216865997 -0.00358532472563065; 0.011448565057850819 -0.0007967226015047101 -0.014515236706200849; -0.0041937590782783795 -0.0028291626233563215 0.0005438847032918045; 7.57384910445592e-5 -0.0015433009675069665 -0.014206977345691311; 0.001194380487595006 -0.0012122060918073184 0.004751510896906428; 0.00423649531812591 -0.0031495987991424614 -0.004077241442680957] %
+
+Mass Used: 101.5037966851828 kg
+Launch C3: 103.5801711865529 km²/s²
+||V∞_in||: 0.061667859851008235 km/s
diff --git a/archive/ES_0.6049695638818965 b/archive/ES_0.6049695638818965
new file mode 100644
index 0000000..986cef6
--- /dev/null
+++ b/archive/ES_0.6049695638818965
@@ -0,0 +1,22 @@
+archive/ES_0.6049695638818965---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T19:16:20.103
+Launch V∞: [5.311962927244481, -8.625803678688081, -1.3868805165816982] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.276078443144522e-5, -7.78957502852737e-5, 1.1074863422068796e-5] km/s
+ V∞_out: [-7.991315192424545e-5, 2.6660863575629645e-5, -1.3680572663632632e-5] km/s
+ time of flight: 1.2103470654304633e8 seconds
+ arrival date: 2027-02-22T16:01:26.103
+ thrust profile: [0.29984915324058675 -0.22273975784017208 -0.17943965838310016; 0.19346949619024903 -0.03870241331993966 -0.2294621042504906; 0.14730713433921497 -0.00015495629777161705 -0.26027167676351404; 0.11514099531098249 0.012462997045146576 -0.2649642793318919; 0.07831289371638997 0.014186991107739163 -0.2194677730107365; 0.04948493112376398 0.011567357268255918 -0.16051561211535842; 0.027907104281536307 0.007437174759142598 -0.10129263794415248; 0.016678090680427193 0.005388286884307993 -0.06763844058322488; 0.010089350430834077 0.0032477641802292844 -0.042381501727759584; 0.008296685607426494 0.0030001195048337294 -0.041801342378480315; 0.0032344135428056166 0.0016645353511721352 -0.018393131518625136; -0.00029021234401248634 -0.00027874715446810566 0.00042697221795181465; -1.280722713041076e-5 5.301164941181039e-5 0.00026350641863194274; -2.0565636523262362e-6 0.0003334277343684683 0.0002588482103062509; -7.355052473374409e-5 7.916020357554701e-5 0.0004337248456208532; 6.592424870329807e-5 4.2916040710483074e-5 -0.00019124166941623762; 8.677494245904214e-5 0.00035142243619120197 0.00014842424276153204; 0.00010549384808470185 -6.698607342670642e-5 2.4736262243506118e-5; 3.434596781420914e-5 -0.0001756294616746038 0.0005857960446392487; 1.573963252990698e-5 -0.00023199756143000216 -0.0003678339165398033] %
+
+Mass Used: 95.95270979826455 kg
+Launch C3: 104.5448768109625 km²/s²
+||V∞_in||: 8.522716414903653e-5 km/s
diff --git a/archive/ES_0.6052816983303517 b/archive/ES_0.6052816983303517
new file mode 100644
index 0000000..52484db
--- /dev/null
+++ b/archive/ES_0.6052816983303517
@@ -0,0 +1,22 @@
+archive/ES_0.6052816983303517---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T09:02:40.565
+Launch V∞: [6.7821676751008235, -7.18091857931432, -1.1474158673554502] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.7253303921235606e-6, 2.889065949448591e-6, -1.4880392408215778e-7] km/s
+ V∞_out: [-3.0384844824920355e-6, 1.983761728753147e-6, 1.6155649909088067e-6] km/s
+ time of flight: 1.2070857596584031e8 seconds
+ arrival date: 2028-03-02T11:12:15.565
+ thrust profile: [0.7792239466781532 -0.343295628573487 -0.3793980135994161; 0.35264517123840033 0.009933608395697697 -0.3844111020480519; 0.17914052183980314 0.04061499686299357 -0.30912625907851204; 0.10861426441414522 0.03729775246026584 -0.2533064216975441; 0.06330337966831433 0.026575486062285728 -0.18476069252403246; 0.03504968336976887 0.01635698483873564 -0.12071280508878356; 0.02429110051323683 0.011953245145682448 -0.09454437027835993; 0.004824910991651244 0.004492491564507815 -0.026567898045945892; 0.005904751320259594 0.0050436542468319644 -0.026692944059025968; 0.003004221593178218 0.0013808634165841656 -0.016493682130994693; 0.0002614823631951102 0.0005915018258020224 0.0014735876526847432; 0.0018765089676540394 0.0011872106013952686 -0.011075843659776484; 0.011850520398700801 0.010071664577092637 -0.0026366905019582967; 0.0026023495894895708 -0.0012412686287502593 -0.009543726818838248; 0.002836064840094442 0.0015562435600566377 -0.012213510016249887; 0.003568169910138144 0.0008119650372821828 -0.006442901731288202; -0.006250331900773542 0.010076494255770618 0.003965110149389493; -0.005604997413070289 0.0014671610602552635 -0.010124621759760592; -0.017698425076464255 -0.0004127612304071467 0.004309212512564538; 0.0012585256333427618 -0.003684115095417316 -0.002180626981424629] %
+
+Mass Used: 129.36225445200853 kg
+Launch C3: 98.87995318858317 km²/s²
+||V∞_in||: 3.974452215628953e-6 km/s
diff --git a/archive/ES_0.6054025307926165 b/archive/ES_0.6054025307926165
new file mode 100644
index 0000000..11fc20b
--- /dev/null
+++ b/archive/ES_0.6054025307926165
@@ -0,0 +1,22 @@
+archive/ES_0.6054025307926165---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T21:26:57.636
+Launch V∞: [6.838628793899197, -6.898978272783599, -0.6106335335610582] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01580590156033693, -0.014064975230748091, 0.01132370505022331] km/s
+ V∞_out: [0.011776015888171931, -0.020597034747489123, 0.003690406547681624] km/s
+ time of flight: 1.2340164693373594e8 seconds
+ arrival date: 2028-03-29T03:41:03.636
+ thrust profile: [0.9753748434694 -0.37753329185099715 -0.35005156458398207; 0.4389604769522197 0.058165464559647405 -0.36813502379528973; 0.20755263033532556 0.07899281481932738 -0.28028304127653425; 0.1671575038286653 0.09677380672536735 -0.29768394269074755; 0.07965796145350632 0.053195074687566235 -0.18085143181079633; 0.06617056433999127 0.04672323973520175 -0.17680203104253878; 0.04879202667051493 0.044578480074897606 -0.14542428192172052; 0.014856529189548905 0.015363575981108699 -0.06130774304948961; 0.012354553261035434 0.011731598573847559 -0.047245390635681325; 0.012291191073666536 0.012294016068369901 -0.052203830015104355; 0.00010513938295488771 4.95126239839961e-5 -0.0010461301590236982; -7.982808092218082e-5 1.2746658194905889e-5 -0.0006618069826641981; 0.0001870582292697586 4.954124496375496e-6 -0.00013274109558015997; 9.014480414769945e-5 0.00023621817604643633 -0.00036424840702500296; 0.00011115634426532383 -0.00022695445563457222 -0.0006280166369655609; 2.076327643335844e-5 0.00039002066596249515 0.0002438392405272378; 0.0005473509925481464 -0.00026112010390272214 0.0004003715848125745; 0.0004284610553117913 0.00022297163937139264 -0.0013807562943116958; -0.0001468195801133369 -0.00012437901585196927 -0.0007480517080875307; 0.0002503758426324722 -0.0006769785411904195 -0.0003186448124392545] %
+
+Mass Used: 153.67851249990554 kg
+Launch C3: 94.73561830139663 km²/s²
+||V∞_in||: 0.023997423787587527 km/s
diff --git a/archive/ES_0.6056582753274979 b/archive/ES_0.6056582753274979
new file mode 100644
index 0000000..501951f
--- /dev/null
+++ b/archive/ES_0.6056582753274979
@@ -0,0 +1,22 @@
+archive/ES_0.6056582753274979---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T17:17:31.459
+Launch V∞: [5.110381512431422, -8.80719799854362, -1.8013901946659463] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.290530793202509, -0.20208759751608216, 0.1213362762966032] km/s
+ V∞_out: [-0.2374529494004705, 0.23879734672700562, -0.16630022258674837] km/s
+ time of flight: 1.212865001662126e8 seconds
+ arrival date: 2027-02-28T11:59:11.459
+ thrust profile: [0.3364581214008297 -0.2630209967594028 -0.22970561545752416; 0.09420914496597357 -0.024566564421824262 -0.1303425654025707; 0.11486190187533601 -0.010083277827717507 -0.23642420618492493; 0.09065100992931002 -0.00020967619742728226 -0.24462857822044173; 0.06556783429925978 0.0030785611509012026 -0.2149181781202595; 0.038310092616467756 0.0031408121450847174 -0.14690849681638748; 0.011639144086266547 0.0012901115198203086 -0.05217268388690956; 0.008687100619989686 0.0009200995149919203 -0.04267167530335652; 0.009141477150529416 0.0011294406036204162 -0.04793318518589735; 0.0017300839424551754 0.0002713398190972808 -0.010616741763870913; 0.00013074611234363737 -0.0003325816907696187 -0.0008038872256270528; 0.0001452468444730885 0.0002590561005717388 -0.0010697703687817066; 0.00031304818336928386 2.437916785313408e-5 -0.0020106217802135155; 1.0752440419987204e-5 -0.00011919108134704557 -0.00011207835800987093; 0.0006005639853772557 -0.0007237013586208864 -0.0005681910906775424; 0.0001671367893940395 -5.024580832756721e-5 -0.0005550275338539961; -0.00024295138401528153 -0.0005574059039421815 5.987897490137141e-5; -0.0010268516324261838 2.4735503130758965e-5 0.001955449456675653; 0.0007188565366102176 -1.581344551224769e-5 -0.001274042519759787; -6.60119342243572e-5 -0.00046253093171733984 -0.0005988510726416289] %
+
+Mass Used: 82.85615708947125 kg
+Launch C3: 106.92774242159022 km²/s²
+||V∞_in||: 0.374125688524895 km/s
diff --git a/archive/ES_0.605676468092856 b/archive/ES_0.605676468092856
new file mode 100644
index 0000000..5017daa
--- /dev/null
+++ b/archive/ES_0.605676468092856
@@ -0,0 +1,22 @@
+archive/ES_0.605676468092856---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T21:36:59.591
+Launch V∞: [5.268835690485806, -8.624426763610941, -1.686079447723638] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.10512642318360958, 0.044467574181495405, -0.1077872274495968] km/s
+ V∞_out: [0.10550555330612775, 0.04519249212689019, 0.10712841689925622] km/s
+ time of flight: 1.1993286602330302e8 seconds
+ arrival date: 2027-02-10T00:18:05.591
+ thrust profile: [0.35562734766338056 -0.26893540539543725 -0.2172180836150227; 0.20283799483599943 -0.04260282143751493 -0.23595240261709524; 0.16095941209621606 -0.001942245130950047 -0.2755733544908144; 0.12416392160187423 0.01182555494199196 -0.27455616942304945; 0.07472689104008655 0.012344850242877495 -0.2000679360603106; 0.04512557290328032 0.009716217248899057 -0.1403123863597956; 0.03389530359947059 0.008546264814218033 -0.11790748030041213; 0.00293845677111338 0.0007635790578714924 -0.010846040394567692; 0.005539138152176342 0.001696994444697473 -0.023552662589650993; 0.0004827879293935016 0.0006005870656533138 -0.0022922303077508466; -0.0012086657005233395 -0.0003024451207917517 -0.002568106659264442; 0.0001389310273714251 0.000248711759868223 0.0006927964223471944; 0.0005915853304151459 0.00024385929144798003 -0.002966024613648726; 0.0009231184664529433 -0.00010613135734344409 -0.0013042048213108095; -3.606088431370896e-5 9.855126844558043e-5 0.0015132663564690909; 0.00010255782560982131 0.0014663595189476754 0.00010938336870138128; 0.003772981429548427 0.002543680297347495 -0.0010357433713171814; -3.531703041974177e-5 9.990288274832707e-6 0.00034855349434816693; 9.20205114702242e-6 -0.00014632345856091273 -8.597152648049766e-5; 0.001977055834101608 -0.0019475232172054178 0.0014569370065954498] %
+
+Mass Used: 94.21453521847161 kg
+Launch C3: 104.98423043826179 km²/s²
+||V∞_in||: 0.15699368269531508 km/s
diff --git a/archive/ES_0.6059170728778938 b/archive/ES_0.6059170728778938
new file mode 100644
index 0000000..96c7ff7
--- /dev/null
+++ b/archive/ES_0.6059170728778938
@@ -0,0 +1,22 @@
+archive/ES_0.6059170728778938---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T21:42:10.205
+Launch V∞: [5.117822270188072, -9.058688140488078, -0.9330107302067995] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.126613950241338e-8, -2.2048372476921808e-7, -1.1493910027285914e-7] km/s
+ V∞_out: [-1.8222032040458563e-7, 1.6352373504104118e-7, 1.0635086828419407e-7] km/s
+ time of flight: 1.482018702276426e8 seconds
+ arrival date: 2028-01-15T04:53:20.205
+ thrust profile: [0.0463352441091516 -0.037344136991952284 -0.035812999116119064; 0.015297788898952353 -0.008469334569277816 -0.03246801946431062; 0.027100372622507987 -0.01832864079453671 -0.09765100411464141; 0.04239514640529159 -0.03700558497822139 -0.21256659231346312; 0.032380740910434025 -0.03517935027767808 -0.20510041814678912; 0.035554449510817314 -0.045782725768143094 -0.26591852709748737; 0.014026118075469206 -0.020585987322965797 -0.12072799417147864; 0.011673234524926853 -0.01870750601028276 -0.10789522497835573; 0.0029020638397167517 -0.005118373342624577 -0.02972286838154042; 0.0001357261018558731 -0.00013304881368511647 -0.001453145272539427; 5.590570352805512e-5 -0.0002770709020246194 -0.001739570645017011; -0.0003713872287316634 -0.00015851308327136907 -0.0005976827129343589; 0.00016032804309495992 -0.00041210079430079483 -0.0023283650668819503; 6.183426019859987e-5 -0.00018254997764351703 -0.001481995351006672; -0.0003713633320630446 -0.0007297354364444075 -0.0010636118394542846; 0.0004807416699031471 -0.0004845598657338235 9.747911729591965e-5; 0.00010666351550856526 -0.00013440262336631196 -0.0014046363933076377; -0.0005678196209178612 0.00020481120818676297 0.0007349663660962862; -0.00100727472040338 -0.00027736787581767613 -0.0001953742480875452; -0.0022432045709762658 -0.002282761924278006 -0.0006822631527947531] %
+
+Mass Used: 70.35565796609808 kg
+Launch C3: 109.12244463853337 km²/s²
+||V∞_in||: 2.6158794905207005e-7 km/s
diff --git a/archive/ES_0.6062533234212564 b/archive/ES_0.6062533234212564
new file mode 100644
index 0000000..11fbe85
--- /dev/null
+++ b/archive/ES_0.6062533234212564
@@ -0,0 +1,22 @@
+archive/ES_0.6062533234212564---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T19:41:15.654
+Launch V∞: [5.234368172470938, -8.537903136795425, -1.5342120820573242] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00013358924211671205, 5.920078273611722e-5, -0.00010929636880843868] km/s
+ V∞_out: [-5.6709607065353934e-5, 0.00013321076773752447, 0.00011105612470960076] km/s
+ time of flight: 1.1915249628671718e8 seconds
+ arrival date: 2027-01-30T21:36:11.654
+ thrust profile: [0.5072141730753754 -0.37578602091057184 -0.2969742475336528; 0.27961195527510674 -0.05254664293533599 -0.31153486185096557; 0.19068298356177799 0.0036492475531291627 -0.3122096520172019; 0.1533533235944399 0.020788003869678356 -0.322713398878909; 0.0706355229399079 0.014876198033625313 -0.18092074242771708; 0.03661423540443243 0.009692050464716752 -0.10860844702401667; 0.00835794942532661 0.0025884705009133415 -0.02836359151955675; 0.011122698678979111 0.0038045703524954 -0.041128007406446426; 0.00888494859648247 0.0032515516923357418 -0.0347912593324202; 0.0013379909474087151 0.0007931337400083647 -0.007550635449059043; -0.0007775229694201872 0.0004056287550516567 -0.0029163780007019214; 1.1130652132592539e-5 0.0006503852562108965 -0.0006779528607270231; -0.0003630824907187659 0.0011799197401985942 -0.0006001004158386846; -0.0002604129150574026 -0.0007549786131114532 -0.0002776024414051536; 0.0005066338489858622 -0.0005806523840887291 -0.0007479463789282821; 0.00015736995601183497 2.4645820130347564e-5 -0.0008362690710721091; 0.0004189654253574064 0.0008776557072735815 -0.0014487914325307316; -0.0013867854511966022 0.0008031482655707611 0.002659477634333312; 0.0011458756535207121 0.003286708875430698 -0.0016512892608011901; -0.00047282595013164975 0.0004522882039614834 0.0007602478102259123] %
+
+Mass Used: 108.51433736058243 kg
+Launch C3: 102.64820685100857 km²/s²
+||V∞_in||: 0.00018247332550429588 km/s
diff --git a/archive/ES_0.6062890058102056 b/archive/ES_0.6062890058102056
new file mode 100644
index 0000000..63b2bf0
--- /dev/null
+++ b/archive/ES_0.6062890058102056
@@ -0,0 +1,22 @@
+archive/ES_0.6062890058102056---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:31:29.922
+Launch V∞: [6.969049236822743, -7.3945455935107836, -1.511127039897749] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001020041596570256, -0.0015200343529773166, -0.0005737346626213739] km/s
+ V∞_out: [-0.0008148340880010631, 0.0015283115594991786, -0.0008248944662913007] km/s
+ time of flight: 1.199058110505233e8 seconds
+ arrival date: 2028-02-24T14:41:40.922
+ thrust profile: [0.3558867970377261 -0.1645591266515927 -0.19232336664940447; 0.12795322908691917 -0.0017609793282506044 -0.15892781152025712; 0.15083257816597925 0.024910932519099552 -0.2789724431057115; 0.10719561470588145 0.028448280608534993 -0.26804869596796144; 0.05543529802056861 0.017783423341576076 -0.1868669813085231; 0.044224092431353584 0.018191762097930504 -0.16477016641353126; 0.016257221500380187 0.006110492804491137 -0.06849724146923629; 0.012369442341164672 0.004998745309192237 -0.05626111288457356; 0.016158582687222554 0.006979561627480917 -0.07726721510936424; 0.010571912786472704 0.004414062452437501 -0.05547290186857737; 0.000620489809715422 0.0013157361608980996 -0.0005116649229346628; 0.0003767749990329542 0.00045305290208128165 -0.006790251538811279; 0.0009202277070379231 0.00015453547084687527 -0.0026159726594100472; 0.002022998175234436 0.002525836974137126 -0.00849427171861107; 0.0009314420495671569 -0.002600040995947044 -7.858361445901071e-5; 0.0006682962103027471 -0.0002526929527523164 -0.0008134735741905843; -0.001763767500940809 0.0028220864007451937 -0.001115219061179726; 0.00044219395649115767 0.0003797118515325729 -0.003130242327023556; 0.002010093285016865 0.0013202116661618385 -0.0016386624954070812; -0.0014463313879182229 -0.0018389288497138614 -0.0068037040745696515] %
+
+Mass Used: 91.74284251744257 kg
+Launch C3: 105.53045673047953 km²/s²
+||V∞_in||: 0.0019183745088115689 km/s
diff --git a/archive/ES_0.6064091115459018 b/archive/ES_0.6064091115459018
new file mode 100644
index 0000000..4f2273d
--- /dev/null
+++ b/archive/ES_0.6064091115459018
@@ -0,0 +1,22 @@
+archive/ES_0.6064091115459018---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:45:29.876
+Launch V∞: [7.018570409605985, -7.372741605740578, -1.9159956855545517] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00396284562109681, 0.025303015122939657, 0.004588719442973315] km/s
+ V∞_out: [0.02461784684663712, -0.0048936527493256285, 0.006847632969378571] km/s
+ time of flight: 1.1934519225704366e8 seconds
+ arrival date: 2028-02-17T23:12:01.876
+ thrust profile: [0.30342249361303714 -0.1385945639302207 -0.17679215809111073; 0.16215748348887343 -0.0005439613286980285 -0.20096410223326705; 0.11421175496007573 0.02159681363761257 -0.21963208705908882; 0.08217166806434308 0.02483910671297194 -0.21206363393959615; 0.04740962928566611 0.01815726005928236 -0.15320756536384106; 0.03389295080776203 0.015150936158260657 -0.12969125870547235; 0.02139155680564094 0.009373104506343929 -0.09640538613476532; 0.016308398928213313 0.009001762953055837 -0.0809482231817081; 0.014205320338776386 0.00818047121266047 -0.07469740530202257; 0.007190872673890113 0.003083442040912525 -0.03879039311046088; 0.0009886909335347683 0.00053702572374211 -0.0059907250794644235; -0.0005671507170141386 -0.0002928016355843765 0.0003737669399165634; -2.704942667847173e-5 -8.375281682424678e-5 0.00027636025730687385; -0.00011652050702958447 0.0002269537665817279 -0.00012469632528684584; 7.424251475849098e-5 0.0001373980730515591 -0.0005311047661639614; -0.00031280843427226835 -0.000572220337126472 0.000257046798171232; 2.9382040685271556e-5 1.4125105585145368e-5 2.8656871675283174e-6; 6.366443036586407e-5 -0.0003042002810354234 -0.00023710141259743504; -0.0002146467778174392 0.000283733223381621 -0.0003936716461916149; -0.00030954751495292174 1.178344787522955e-5 0.0002531570172803948] %
+
+Mass Used: 81.626611864594 kg
+Launch C3: 107.28868884667853 km²/s²
+||V∞_in||: 0.026019282577632315 km/s
diff --git a/archive/ES_0.6066834789043594 b/archive/ES_0.6066834789043594
new file mode 100644
index 0000000..fd8b3c6
--- /dev/null
+++ b/archive/ES_0.6066834789043594
@@ -0,0 +1,22 @@
+archive/ES_0.6066834789043594---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T21:36:52.157
+Launch V∞: [6.909532559670502, -7.346832382101816, -1.8382145850152902] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.439554558628483e-6, -4.409600722033941e-6, -2.1245902034668836e-5] km/s
+ V∞_out: [-1.3539766929297374e-5, -2.4787449314414947e-5, -7.877702300450102e-7] km/s
+ time of flight: 1.2100969430477864e8 seconds
+ arrival date: 2028-03-08T11:25:06.157
+ thrust profile: [0.5357432117940519 -0.2192165983334239 -0.250927369015748; 0.10494527590011034 0.0004992496642411198 -0.13321030864892525; 0.07857160403240744 0.015458352561775822 -0.15532155884645524; 0.052988263159799036 0.016466289101433555 -0.14008391378461; 0.03640798859504035 0.013954519226647049 -0.11889689868261591; 0.05056814416354358 0.020701354205579215 -0.19014796933858646; 0.02502692142524609 0.011022448715493195 -0.11267429469761328; 0.02127609347914766 0.010332496335627543 -0.10292620510125598; 0.03818972126857839 0.02055063029603885 -0.19516469818629564; 0.0011084990962502066 0.001121713002106746 -0.006611882036094869; 0.006907156228368453 0.003974448681824003 -0.03760249787078654; -0.0012885411352905529 -0.0005674726144614449 -4.002051230423721e-5; 0.001120627683749104 -0.0030027754832668476 -0.0009985506883262644; 0.002119698326133129 0.0007215807267816649 0.003343175802241172; -0.001173592063412028 -0.0005440848384955352 0.003972899636846062; 0.0035268209466354644 -0.0030728509952259227 -0.0020148847258227203; 0.0007413557773390598 -0.00048791829944205335 0.0026419781428220265; -0.0017879260714908224 -0.00022854356670309336 -0.0009281528161727884; 0.010982776990827121 0.0019073615324015952 -0.0058709279116003245; -0.0026627994586191166 0.005096036966918439 -0.01382854397629489] %
+
+Mass Used: 94.73378061269659 kg
+Launch C3: 105.09661910440958 km²/s²
+||V∞_in||: 2.328216083061395e-5 km/s
diff --git a/archive/ES_0.6068674357346588 b/archive/ES_0.6068674357346588
new file mode 100644
index 0000000..450581f
--- /dev/null
+++ b/archive/ES_0.6068674357346588
@@ -0,0 +1,22 @@
+archive/ES_0.6068674357346588---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T12:41:12.189
+Launch V∞: [7.01551371079001, -7.094836006285612, -1.086282705015104] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.098298156493432e-6, -4.66639429310052e-6, -2.343200428633769e-5] km/s
+ V∞_out: [-1.2228560157304639e-5, -2.2421382932932492e-5, -7.198420657793533e-7] km/s
+ time of flight: 1.2274086412235907e8 seconds
+ arrival date: 2028-03-25T03:22:16.189
+ thrust profile: [0.5554940060044721 -0.23473990315837073 -0.2672384973757036; 0.21777511546683423 0.011492984109197616 -0.2398603797817463; 0.17168652174483606 0.04539301028081328 -0.29311570723009656; 0.1132305707969382 0.043998135101096625 -0.25826183668019403; 0.052401623013116294 0.024064028955634413 -0.14849183553457107; 0.06479901358967807 0.03466157215194204 -0.2190874575605731; 0.02817171135279529 0.016859719886583965 -0.10202734487090874; 0.017399412154140936 0.010096925036629224 -0.07590087074473316; 0.01937525114324487 0.011957192790912358 -0.08644739448764821; 0.0018595031100929697 0.0021717606419237997 -0.015367626038787864; 0.002320024558189423 0.004690894651349101 -0.032525240590424005; -0.0022328135807899918 -0.005034185460295144 -0.0026027947300104916; -0.0036221445364239494 0.0008042578964641154 -0.006428900029892952; 0.004924461900015265 0.0190875142346664 -0.010321713715721059; 0.018813549718471927 0.01558222697736872 -0.005674730803124126; 0.0022155195472634967 -0.003910171095658916 0.00703887722287222; 0.004110948486011616 -0.011387329992745837 -0.006161637322999605; 0.004290437669090388 0.0063063245204715655 0.015170997831373547; -0.0009599474036822695 0.023155919112589216 -0.00804663778301222; -0.0014074796186164555 0.0015243098974741481 0.01296449489383537] %
+
+Mass Used: 120.39618762119335 kg
+Launch C3: 100.73414069758432 km²/s²
+||V∞_in||: 2.5565857895210183e-5 km/s
diff --git a/archive/ES_0.6068957552660158 b/archive/ES_0.6068957552660158
new file mode 100644
index 0000000..80039b2
--- /dev/null
+++ b/archive/ES_0.6068957552660158
@@ -0,0 +1,22 @@
+archive/ES_0.6068957552660158---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T14:03:44.361
+Launch V∞: [5.084312220410106, -8.564818326789013, -1.5895948842057834] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005301095832550173, 0.002401455908061269, -0.0047216357330097086] km/s
+ V∞_out: [-0.0020685294774595684, 0.006027770202757849, 0.004265745672083723] km/s
+ time of flight: 1.1853745119633944e8 seconds
+ arrival date: 2027-01-24T13:07:55.361
+ thrust profile: [0.7303322252583472 -0.5157403660621248 -0.3485170686054565; 0.19849970283367738 -0.033199605699102686 -0.21039728372961303; 0.1355195343531665 0.0062979297691541265 -0.21180684701527877; 0.11070942977831416 0.018800352835931913 -0.2221014888047501; 0.09636152432640588 0.023388820313038818 -0.2275562516291139; 0.09012065529897026 0.022716059000675207 -0.23024892199121236; 0.02007744252023575 0.006928272742857018 -0.06412499047867228; 0.015327947035624317 0.006628238136933993 -0.0544456576346224; 0.007464737144929428 0.00281128389027974 -0.02882477724341923; 0.0038352731267336424 0.0016446756592050126 -0.015102828324201385; -7.300874709269647e-5 -0.0004138852913526898 -0.0001538828653135252; 0.00025707407506032215 0.0007012334463612027 -0.0020324064655016837; 8.548550294291664e-5 3.6936464335029845e-5 -0.0013778045254076872; -0.0007241765117737621 0.00011474172449694516 -0.0003662928841942504; 0.00032056146162505233 0.0005000084805575834 -0.001303558414573244; 0.00013419890903184663 0.00020157478155699658 -0.0007067468550805201; 0.0003373917658438953 -0.0004306656300463391 -0.0008576505839014426; 7.594148018473789e-5 0.00022600036245811958 -0.00014201572895529598; 0.0004156947747791348 1.778973529882491e-5 -0.000623769031193215; 0.0007181092267357883 0.0009287336911332211 -6.065215768430259e-5] %
+
+Mass Used: 114.60164001881867 kg
+Launch C3: 101.73315562140569 km²/s²
+||V∞_in||: 0.0074941611604953705 km/s
diff --git a/archive/ES_0.6069247253106476 b/archive/ES_0.6069247253106476
new file mode 100644
index 0000000..eb2a161
--- /dev/null
+++ b/archive/ES_0.6069247253106476
@@ -0,0 +1,22 @@
+archive/ES_0.6069247253106476---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-12T04:54:57.498
+Launch V∞: [5.8524003945900445, -7.6549350737779465, -0.4459923493644513] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00862531280179509, 0.011821099304665841, 0.012185124686361657] km/s
+ V∞_out: [0.017256258452043878, 0.008071202533803097, 0.0004043512418145332] km/s
+ time of flight: 1.549486792354712e8 seconds
+ arrival date: 2028-03-09T14:12:56.498
+ thrust profile: [0.6336441874553369 -0.30644379655727283 -0.16051849598900667; 0.5064580939086286 0.06943417754318293 -0.3029886330269146; 0.36757596783306656 0.15572596144160036 -0.34064287328661125; 0.2498651888749275 0.15620145251945408 -0.3099651758965332; 0.1381583154245436 0.10883661358684456 -0.2142509326570666; 0.03304014813932945 0.030957992605779583 -0.06316556215285468; 0.006174759772617598 0.006852576378554774 -0.0143758840317424; 0.007124553476478183 0.009048120700531312 -0.018800763834665727; 0.0022608879729786816 0.0028875521195052233 -0.006686582029887532; 0.0008791429029181331 0.001235163420801001 -0.0030198256657251277; 0.0004143947010924598 0.0003077134446903906 -0.0006779676649386065; 2.6241679491617197e-5 0.00012993683349414193 -0.0003560528286848905; 0.00014768046035904057 0.00020006240720788407 -0.0007837311937847217; 0.00016070231820566855 0.0002459390834099463 -0.0006516281516300531; 0.00023560807406733316 0.00029557008757216837 -0.00036379358472368164; 0.0006342846705154926 -0.0002306839171692309 -0.0002047623294853409; 9.313231287481799e-5 0.00012693200256954826 -9.940078890975456e-5; 0.00046991902880634594 0.0003086033307036304 -0.00025398406505432224; -0.00011892248544097131 -8.87772789509491e-5 -0.0002390616958756679; 2.2383574421934324e-5 -2.2344618750113132e-5 0.00039279184389751694] %
+
+Mass Used: 165.30158472382573 kg
+Launch C3: 93.04753053804511 km²/s²
+||V∞_in||: 0.019042365223935858 km/s
diff --git a/archive/ES_0.6070400768433122 b/archive/ES_0.6070400768433122
new file mode 100644
index 0000000..d42cd6f
--- /dev/null
+++ b/archive/ES_0.6070400768433122
@@ -0,0 +1,22 @@
+archive/ES_0.6070400768433122---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T07:24:39.627
+Launch V∞: [5.176106012540697, -8.641653894537843, -1.5007540371554267] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.035909677034180375, 0.017302091828241765, -0.03836235635092976] km/s
+ V∞_out: [0.03299860408216827, 0.014731300088295275, 0.04192509838531821] km/s
+ time of flight: 1.2053452502393213e8 seconds
+ arrival date: 2027-02-17T09:13:24.627
+ thrust profile: [0.39643304015832165 -0.291745731723021 -0.23319053084955188; 0.32772181922063454 -0.06488661706752616 -0.36946021890811875; 0.10033810702665251 0.00064006197280217 -0.17866454315302896; 0.06679220104425751 0.006552309116124056 -0.1519427942607618; 0.05735967926266707 0.012251910150011284 -0.15192185195368; 0.07061613371327018 0.015251435323463316 -0.22511947094977694; 0.01687917771559986 0.004637695575871582 -0.06021991289161818; 0.010105058659809431 0.0028237072251886567 -0.040432185297427765; 0.020676761183295898 0.007746427267030722 -0.09531952149634473; 0.004588595870501599 0.0016581238205014527 -0.02018175525395574; 0.01683352727996938 0.005442000382553478 -0.07733712951852699; -0.00032559445020236813 0.00012719498710790227 0.0005400859670185078; 0.0001757112665529883 -0.00028452127107318694 -0.0033411356725133383; 0.0002639436443696315 -0.0019319039498576934 -0.0028107844491875914; -0.0004543643220326545 0.0002399299185000438 -0.005149043964094429; -0.0029437463835212917 -0.00010672480137388375 0.0018984471968591335; -0.0010268042901338632 -0.0005195903608329073 0.0005444140360584496; -0.00042517553000666407 -0.0030305924583687227 -0.009001667204482755; -0.0004503119920863773 -0.0022612201823325384 -0.000801643234476434; 0.0015409820424554868 -0.004057794056469109 -0.0016944670201108] %
+
+Mass Used: 103.16540034840136 kg
+Launch C3: 103.72251816607934 km²/s²
+||V∞_in||: 0.0553221264154567 km/s
diff --git a/archive/ES_0.6070419032696779 b/archive/ES_0.6070419032696779
new file mode 100644
index 0000000..79827ed
--- /dev/null
+++ b/archive/ES_0.6070419032696779
@@ -0,0 +1,22 @@
+archive/ES_0.6070419032696779---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T09:19:52.516
+Launch V∞: [5.141123081908811, -8.505884071690092, -1.016791157424616] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.986873235564151e-6, -1.2899389011233296e-6, 2.393360378591598e-8] km/s
+ V∞_out: [1.6256606267256314e-6, -3.4087103512054084e-8, -7.926979137831744e-6] km/s
+ time of flight: 1.1907111454958642e8 seconds
+ arrival date: 2027-01-29T12:38:26.516
+ thrust profile: [0.6425990664712564 -0.4727675969805771 -0.34363794879874165; 0.26103554630029857 -0.05046725286686487 -0.2748405328673646; 0.31942894909741415 0.003983625994198995 -0.48051285059251164; 0.14461652090035484 0.01788287391241126 -0.2870860607530267; 0.07903518915929579 0.01591488277426477 -0.19050640269949431; 0.035010377067943105 0.009421905482447694 -0.09957365476584253; 0.01675226367606266 0.005113577161996974 -0.053400038907865106; 0.007746681834887433 0.002640502474534435 -0.027149112504384773; 0.016502251487102156 0.006921806462352796 -0.06113191367320145; 0.00395104979925693 0.001565643263129243 -0.015713695418480878; 0.0035515546983129124 0.001396566861923678 -0.014610143753490469; 0.0005358635414963561 0.0007446633913700285 -0.0022202056166737536; 0.0010755499729548455 -0.00028982558920362996 -0.0016179136304127703; 0.0006232007160428609 -0.00037831348604307885 0.00012093857609755292; 6.768772840790721e-5 -9.057716588643143e-5 -0.0015764036146624861; 0.000495782644780839 0.0008312424820859062 -0.001566314634150958; -6.38797257849208e-5 0.0002346591153371398 -0.0013055579270065194; -0.002320835830250394 -0.00024575721647442843 -0.00013260590108922716; 0.0009757701998892761 0.0004925147816945597 -0.001044767435417145; -0.00019957187387774009 -9.034716665513908e-5 0.0004661197180078106] %
+
+Mass Used: 125.96095173521962 kg
+Launch C3: 99.81507464218365 km²/s²
+||V∞_in||: 8.090405383353324e-6 km/s
diff --git a/archive/ES_0.6071133489206663 b/archive/ES_0.6071133489206663
new file mode 100644
index 0000000..bd5c2ac
--- /dev/null
+++ b/archive/ES_0.6071133489206663
@@ -0,0 +1,22 @@
+archive/ES_0.6071133489206663---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T16:49:51.889
+Launch V∞: [6.91875264860367, -7.313778646739232, -1.5615870805047403] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0024803459929143143, 0.003999354722283162, 0.0014635049509521643] km/s
+ V∞_out: [0.0016126944082535634, -0.002714502441608998, 0.0037835569405451973] km/s
+ time of flight: 1.1799276142920916e8 seconds
+ arrival date: 2028-02-01T08:35:52.889
+ thrust profile: [0.559666135904219 -0.2586492489854562 -0.2880132398703075; 0.22679512457537174 0.00023511310503036853 -0.25453042907002704; 0.14008286074687473 0.02771840975450435 -0.2456384197727401; 0.1003664516012483 0.03143471889850129 -0.23497782738608144; 0.06971400668787961 0.027585409553824065 -0.20207071197759235; 0.04543815261836773 0.021098038364691832 -0.15613348917012793; 0.0267068416471906 0.014588552681906968 -0.10966305141335199; 0.007172706760076231 0.003688596659870096 -0.03056890559544739; 0.012662460167826226 0.006297047716691672 -0.05931681049942549; 0.005695810163191458 0.003391125468369739 -0.030363648338020494; 0.00013891711199209367 -6.977854124420456e-5 -0.0006062064639174573; 0.00031944239728597134 0.00013972536388827956 -0.0009693997846737942; 3.130683923109102e-5 6.988024459599832e-5 -0.0007182613231324497; -0.0004303354191982677 0.0007309557773036131 -0.0017973689365602219; 0.00018863518574024454 3.7563393479854445e-5 -0.00048191865189691814; 0.00027338247554584854 -0.0005785291691003759 0.0007597228970796227; 0.00031396426037638193 0.00016203083257781482 -0.0002077405441298077; 0.00022596481905780307 0.000163089720424722 -2.8041559603529448e-5; -0.00018838613269812313 -9.463189629282205e-5 -4.1287055171958405e-5; 0.00024885749305525234 -0.0012713536907949462 0.00034820907591891367] %
+
+Mass Used: 102.80444573043678 kg
+Launch C3: 103.79905051605837 km²/s²
+||V∞_in||: 0.004928366989244634 km/s
diff --git a/archive/ES_0.6071194351241658 b/archive/ES_0.6071194351241658
new file mode 100644
index 0000000..20bd64d
--- /dev/null
+++ b/archive/ES_0.6071194351241658
@@ -0,0 +1,22 @@
+archive/ES_0.6071194351241658---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T08:30:46.806
+Launch V∞: [6.8614720793646375, -7.136919047117658, -1.231700553077713] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0032468868676570053, -0.018756201015243223, -0.018649458753243676] km/s
+ V∞_out: [-0.023241118391708396, -0.0027783919811899993, 0.012739911967036244] km/s
+ time of flight: 1.2830131351498644e8 seconds
+ arrival date: 2028-05-30T07:45:59.806
+ thrust profile: [0.5358383247699218 -0.22343097826620895 -0.2664342281127527; 0.20136938596259357 0.011962115788858882 -0.23067120962439158; 0.18590757408055825 0.04829741122738177 -0.3358256680306362; 0.11851392373234403 0.0455332743616649 -0.2886697042605426; 0.07584314020555505 0.03628910549243672 -0.22806527530234505; 0.028697814312891163 0.016012066311687202 -0.09173635732587737; 0.01231026028216555 0.011051536678492725 -0.05109673813059871; 0.010373960216824761 0.0013120219376822305 -0.029436727999627432; 0.010450055496758958 -0.001229008548022568 -0.028767663542272615; 0.004784877215202192 0.0052807403843686115 -0.015397397979199869; -0.0027452660277187905 -0.0002521494809360137 0.0054142631844949305; 0.006375125438379687 0.01056167515233939 0.0001162110051871456; 0.0021187818837244735 -0.002316996688826605 -0.004463161702850272; -0.02888208859681157 0.005256966427447242 -0.028542687569237096; -0.0011244992917833325 -0.0076292339395021645 0.004526476518433936; 0.007287886596390235 -0.0380293985173365 0.01624222848945407; -0.010649658412650366 -0.03078045189037336 -0.01837446785579771; 0.053298577917110845 -0.089763536290072 -0.007626589903701353; 0.03030029039241435 0.030507179884578916 -0.03981156459089273; 0.004364734420482723 0.044751931027971405 -0.04365904364314321] %
+
+Mass Used: 127.69976444965778 kg
+Launch C3: 99.53249883346325 km²/s²
+||V∞_in||: 0.026648445782906583 km/s
diff --git a/archive/ES_0.6072167222229141 b/archive/ES_0.6072167222229141
new file mode 100644
index 0000000..97db505
--- /dev/null
+++ b/archive/ES_0.6072167222229141
@@ -0,0 +1,22 @@
+archive/ES_0.6072167222229141---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-11T19:26:14.755
+Launch V∞: [5.627154384159391, -7.716112415839473, -0.025141713950428128] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.914259182298835e-9, -4.86821633184514e-10, -3.790107351335492e-9] km/s
+ V∞_out: [-1.4024266508134213e-9, 3.0185983277748346e-9, 4.082164670420206e-9] km/s
+ time of flight: 1.477139639482875e8 seconds
+ arrival date: 2027-12-16T11:05:37.755
+ thrust profile: [0.875872925629536 -0.44294764764327527 -0.20758758488273096; 0.5222227789668694 0.055974526285647294 -0.2993793980857768; 0.2701939573024362 0.10502764253821831 -0.24664077504221651; 0.2592833860834162 0.1492548342380094 -0.30218673068639607; 0.11741287923631279 0.07797178511325982 -0.18074589842046113; 0.09654113579344803 0.08228376710017783 -0.1725563963931798; 0.021864451911230754 0.019298847027573028 -0.046061031916526794; 0.01186336226920956 0.014024700034450116 -0.03815547413935111; 0.0045401199314081655 0.00352629992859618 -0.00997653284597182; 0.0019425160037034336 0.0031737311913620143 -0.0051031021836618895; 0.0038850953314268563 0.005308896739180209 -0.012860635384061053; -0.0011386535641422465 -0.0015673271432473646 -0.0009097199897970133; -0.001882290391134185 -0.0008553535974604857 0.0006712100450528065; -0.00018805927086201085 0.00047482057308340347 -0.0014205833495161348; -0.0006722144196584517 -5.223192863720486e-5 -0.00040444776104943403; 0.0009759762225154562 -0.00011758812806229085 -0.00071908120228847; -0.00020481067113721897 0.001792773588727716 -0.0005950749394429326; 0.0011919865710909995 -0.00028956437025234644 0.001036896204994343; -0.00025681690141931635 -0.0005449326394728511 0.00018901750990847643; 0.00039458607040134637 0.0002845379874177967 -0.0007875408687659038] %
+
+Mass Used: 176.3968211936358 kg
+Launch C3: 91.2038893828167 km²/s²
+||V∞_in||: 5.470222480246532e-9 km/s
diff --git a/archive/ES_0.607276504435345 b/archive/ES_0.607276504435345
new file mode 100644
index 0000000..16ed080
--- /dev/null
+++ b/archive/ES_0.607276504435345
@@ -0,0 +1,22 @@
+archive/ES_0.607276504435345---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T09:10:22.197
+Launch V∞: [6.648958255574604, -7.276086059989854, -0.4838239171463976] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.012944995922842395, -0.07256286771366612, -0.06935296684591977] km/s
+ V∞_out: [-0.0875016842717659, -0.010393737506334188, 0.049732506441325264] km/s
+ time of flight: 1.24258332149009e8 seconds
+ arrival date: 2028-04-13T13:22:34.197
+ thrust profile: [0.6120971828958033 -0.2622085426747974 -0.2812706243560107; 0.5002959485104139 0.01570919813324393 -0.5155067088363603; 0.2243654553490654 0.04851334978795942 -0.3749975163047343; 0.1031852408665787 0.03338577308680061 -0.23395157342450032; 0.047727592821915084 0.018963322021968442 -0.1324320622863597; 0.061457811044686464 0.027173493275750926 -0.19807405648952722; 0.01363049045206987 0.006257153407227552 -0.04780629231084236; 0.007656634322303588 0.0035163361249656412 -0.02925442347348308; 0.009137655265677442 0.00442508493494298 -0.03774749280474823; -0.004883501053154543 0.002045859556013451 -0.012468741689917531; -0.0020735058514244065 0.004585409625901111 -0.006097950499441356; 0.006391008245805305 0.005717572707385089 -0.01007395901618454; -0.004344634869936345 -0.020700384360015506 -0.01560197175324967; 0.013912400859028189 -0.010094215800195813 -0.01543139369978888; 0.0041954050905069415 0.0034494555320512556 0.003970529957865104; -0.0013615454173809254 -0.002903467740553424 0.010816346420791892; 0.0026220621916912584 -0.009608506263706235 0.00014422847166062867; 0.011267175071637698 0.008579598741019519 -0.048860566365426586; 0.01122239251557657 0.019680786472300073 0.013136362835312929; 0.003968557605775789 0.013184266776802386 -0.03651464743549988] %
+
+Mass Used: 140.4149895604969 kg
+Launch C3: 97.38415981955524 km²/s²
+||V∞_in||: 0.10120660403651859 km/s
diff --git a/archive/ES_0.6073214481503905 b/archive/ES_0.6073214481503905
new file mode 100644
index 0000000..dd85770
--- /dev/null
+++ b/archive/ES_0.6073214481503905
@@ -0,0 +1,22 @@
+archive/ES_0.6073214481503905---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T19:08:05.590
+Launch V∞: [6.984284740094169, -7.2947474077246675, -1.6691038160563472] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0036053545463971296, -0.00564270660146997, -0.0020426005974703647] km/s
+ V∞_out: [-0.003950349093441326, 0.0050311929426458315, -0.0025943498621223107] km/s
+ time of flight: 1.1932516654786085e8 seconds
+ arrival date: 2028-02-16T21:00:51.590
+ thrust profile: [0.45136680940875507 -0.20698010982785162 -0.25209353612881485; 0.20393703467727908 0.0005037752000904962 -0.250145210739176; 0.13057711443162318 0.02573971964049164 -0.24965261024789828; 0.08385869582870469 0.02595164220846345 -0.21469676323252737; 0.05741148158429099 0.021954493739961237 -0.18016314689504956; 0.03226932234646881 0.014258447100683835 -0.12102190916498448; 0.026413293903631146 0.012475295318190176 -0.11138512864900561; 0.02371693337983308 0.01227759942279881 -0.1075405935190379; 0.006410389356087022 0.002392779449640125 -0.030275084545736283; 0.0014479445067725732 0.0007636773596940568 -0.013958876811365602; 0.0016989283500218702 0.0013066062745529362 -0.013763736893398697; 0.0027911486763287237 -0.0051892351615145365 -0.00039262703447025846; -0.006335534641967003 0.002457081233265849 -0.002695190377985467; -0.002886043138886544 -0.0003672462130230532 0.006488783031097024; -0.001223655455898413 0.0026897363207718647 -0.006486421966654086; 0.0003150954823484683 0.0005817723536840843 -0.0006518532237688858; 0.003611407065927516 -0.0003461751246259343 0.0032242484999729397; -0.00647516313613216 0.0029597363521009523 -0.00258046223170158; 0.009073492795751516 -0.003338039434188875 0.0023165627220675267; 0.0008400223466303685 0.0005678593668460622 -0.0014340651577670195] %
+
+Mass Used: 97.32805254716959 kg
+Launch C3: 104.77948062199188 km²/s²
+||V∞_in||: 0.0070007811275803735 km/s
diff --git a/archive/ES_0.6073441884655674 b/archive/ES_0.6073441884655674
new file mode 100644
index 0000000..af4ba21
--- /dev/null
+++ b/archive/ES_0.6073441884655674
@@ -0,0 +1,22 @@
+archive/ES_0.6073441884655674---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T22:53:45.323
+Launch V∞: [5.092224085362439, -8.557107674138392, -1.3400927312070439] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.09373814149222456, 0.061789839893666675, -0.05741414560635351] km/s
+ V∞_out: [0.0777088462693189, -0.08115733054964697, 0.05662038492848845] km/s
+ time of flight: 1.2734409831177181e8 seconds
+ arrival date: 2027-05-07T20:15:23.323
+ thrust profile: [0.5134621582501597 -0.3641852473159378 -0.2992466295170964; 0.12952750802214882 -0.024571474550202067 -0.16318748775125597; 0.11572320867751906 0.0007244646345141111 -0.21979916772269537; 0.10418501341013447 0.011813242538449453 -0.2578952559532013; 0.06899756180048436 0.011953788682384567 -0.20831689553136448; 0.03478773921478129 0.006832454958532339 -0.13274100789928955; 0.04409129432599481 0.012236318082252383 -0.17699704793153578; 0.01714747201607733 -0.004264215127454446 -0.060948469845180944; -0.004281002408041461 0.0006835686339603427 0.006144186232958749; 0.00434706850527624 0.0001812291945845854 -0.01291421477907188; -0.00015686492679264116 0.0002943245014451059 -0.002552997135475279; 0.019464343695961832 0.018196014690353635 -0.03484865438702381; -0.0026816006499486666 -0.00736052755347202 -0.006121359189623799; 0.02588073636587005 -0.008242685992232462 -0.017867019036745695; 0.02017090632539628 0.030210379491603222 -0.009163012763347796; 0.007817356186106288 -0.02126663330619328 0.02250572675497805; -0.021660692371756305 -0.017596918077625062 -0.013785521082280067; 0.0028447347025758077 -0.0021503007357242436 0.0274339215060799; 0.0059391399969717104 0.00021779895587114288 0.05094116610286477; 0.00816594609357071 -9.454398293471403e-5 -0.032841203632025424] %
+
+Mass Used: 119.68921581479344 kg
+Launch C3: 100.95068641057745 km²/s²
+||V∞_in||: 0.12609999048457074 km/s
diff --git a/archive/ES_0.6073653732505351 b/archive/ES_0.6073653732505351
new file mode 100644
index 0000000..bd481af
--- /dev/null
+++ b/archive/ES_0.6073653732505351
@@ -0,0 +1,22 @@
+archive/ES_0.6073653732505351---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T08:44:02.092
+Launch V∞: [5.340895230849307, -8.622879323218138, -1.7202911521671664] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0376380762698394, 0.021934971874777796, -0.022787943311909593] km/s
+ V∞_out: [0.03319267660469806, 0.013570053694191595, 0.03363334455153026] km/s
+ time of flight: 1.1883059980334337e8 seconds
+ arrival date: 2027-01-27T17:14:01.092
+ thrust profile: [0.2888882530627831 -0.2253417815077565 -0.17772287059321104; 0.21468680706382434 -0.04331329381695168 -0.23640499476654028; 0.17853666612850627 -0.0006538699045496645 -0.28833896713892826; 0.13826446891016106 0.017246377818549673 -0.28659211208827806; 0.09572085575161289 0.0211451005507203 -0.23629564480118892; 0.04845589193857699 0.01363956217307902 -0.1400819778619227; 0.014164475977024327 0.005268863974320275 -0.05028778052420481; 0.01049907992706732 0.006372209310127278 -0.041904385485960906; 0.0050865530345211 0.0016499325105249463 -0.020024827494264114; 0.0034193749128958867 0.0016400232457399033 -0.01437299345342373; 0.00014508627308892214 -5.3462819658033935e-5 -0.0005488610829190433; -6.136285169010703e-7 5.802739037377366e-6 -0.00031567419413870414; 7.096175587424758e-5 7.514613716875021e-5 -0.0005065073671581948; 4.231859036310184e-5 9.932813115273937e-6 -8.729123746390171e-5; -4.720631416397104e-5 3.546354568344053e-5 -0.0001610464446300257; -3.1985150258701436e-5 0.00017629649801387072 -0.00034889888567024704; 0.00011204776600837855 0.0002078049777886341 -0.00020939769600001148; -1.5385372705939613e-5 0.000823578366199079 -0.0004436720098518036; -0.0002437201025310923 0.00017162356307106949 7.774828319345186e-5; 1.5592742638641537e-5 -5.908472086394233e-5 -6.636519323921974e-5] %
+
+Mass Used: 91.2010359877786 kg
+Launch C3: 105.8386113379164 km²/s²
+||V∞_in||: 0.04916358547571918 km/s
diff --git a/archive/ES_0.6074999299534034 b/archive/ES_0.6074999299534034
new file mode 100644
index 0000000..0b82411
--- /dev/null
+++ b/archive/ES_0.6074999299534034
@@ -0,0 +1,22 @@
+archive/ES_0.6074999299534034---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T10:27:28.824
+Launch V∞: [7.016217371188453, -7.260864506406918, -1.4705168382751477] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004161091989459715, -0.006474251794305621, -0.0023700814505703835] km/s
+ V∞_out: [-0.0045600780612651, 0.005790885162639786, -0.00309959754926144] km/s
+ time of flight: 1.206959096484183e8 seconds
+ arrival date: 2028-03-03T09:05:57.824
+ thrust profile: [0.3950670921842973 -0.17855481403849974 -0.21364442360053584; 0.2121958015561598 0.0051806246846001665 -0.2556411528703032; 0.1272394232670884 0.027945622848619314 -0.23786611109322814; 0.09372226612069359 0.031194599906688436 -0.23414316179549702; 0.05942297209121284 0.022686840281171124 -0.17892576347156935; 0.033637976690250676 0.013997194053468495 -0.11633495699932703; 0.02840548592553487 0.012393398531235287 -0.10840970618609477; 0.020669628585117426 0.009745248949201668 -0.08678253913130869; 0.010441933585887058 0.0055288690220520525 -0.04838817789527196; 0.013724432281743568 0.008105114062314775 -0.07238937969914892; 0.002636418072654501 -0.0016528486493500307 -0.002773166060922568; 0.00043670348830791416 -0.00021322319895657627 -0.0035468628810877505; -0.00139142799389993 0.0016201684929142341 -0.004182656526277287; 0.010342427723444843 -0.008407992012101295 -0.026777683109370717; -0.0062739301565703 0.0026107040114029516 -0.010168583324553712; 0.0004871581392893552 0.009203140804895617 -0.02610326965960978; 0.0008316209302065302 0.0019282928805012965 -0.004422231693675072; 0.00570681709175676 0.011298228433097171 -0.02053329489091729; 0.0018575995801338554 0.002068945028752177 -0.01092575758767069; -0.0020798943325316746 0.0037430848622667084 0.007945936976151834] %
+
+Mass Used: 101.44228872670419 kg
+Launch C3: 104.10987935181711 km²/s²
+||V∞_in||: 0.008052819936094012 km/s
diff --git a/archive/ES_0.6075189426060998 b/archive/ES_0.6075189426060998
new file mode 100644
index 0000000..6e58379
--- /dev/null
+++ b/archive/ES_0.6075189426060998
@@ -0,0 +1,22 @@
+archive/ES_0.6075189426060998---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T09:20:21.301
+Launch V∞: [5.0755965474074545, -8.315834578621132, -1.1211191584094164] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.1835950124456465, -0.002795527126174243, 0.12921165435228169] km/s
+ V∞_out: [-0.21974622894678145, 0.0016858295288806812, 0.04597599742134121] km/s
+ time of flight: 1.2093990795184588e8 seconds
+ arrival date: 2027-02-19T03:45:28.301
+ thrust profile: [0.9999999675115404 -0.7378443704733226 -0.5263020213477659; 0.2541891699213068 -0.04289812891695836 -0.2639834155138137; 0.19711490775040583 0.010374526358148286 -0.3002640656536643; 0.1236378943919692 0.02082197059345698 -0.2424569186870479; 0.10400603161662919 0.02526992042751154 -0.24699593886764093; 0.026646964210459805 0.008182770403316273 -0.07668779335706206; 0.025297235835872445 0.013134547963638332 -0.07704781984395598; 0.01240017900880719 0.0064994572740645195 -0.04280808293106805; 0.03024196942374006 0.012713888118778063 -0.11360627930462215; -0.003336377887599268 -0.009978115872523449 -0.0075164713478981255; -0.003432328778575815 -0.007195779461743524 -0.0032801812392130557; -7.609341722853054e-5 0.006672106085416775 -0.0029561038801229718; -0.0024775384045503026 -0.006571425896391123 -0.00016976714689331384; -0.0018525679916165387 -0.004786386978146895 -0.0073724787374607244; 0.006611523313737617 -0.002099696815107837 -0.006433915868039805; 0.011658671510112493 0.0023467114761503995 -0.006469841496083071; -0.004728909949642193 -0.003621023459974302 -0.007796872011730904; 0.0031639313073775935 -0.003465437469810517 0.011551883695065634; -0.012486951066636321 0.009185870245874372 -0.010816370750851397; 0.012175048091384987 0.00032666601149099363 0.002260832747023344] %
+
+Mass Used: 147.77055593312798 kg
+Launch C3: 96.17169321839802 km²/s²
+||V∞_in||: 0.22452303932399406 km/s
diff --git a/archive/ES_0.6075282151475832 b/archive/ES_0.6075282151475832
new file mode 100644
index 0000000..98576aa
--- /dev/null
+++ b/archive/ES_0.6075282151475832
@@ -0,0 +1,22 @@
+archive/ES_0.6075282151475832---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T22:52:43.954
+Launch V∞: [5.254100589741985, -8.571186047812771, -1.2057034773608293] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.2113250579518638, -0.003991717975395232, 0.1503547371663183] km/s
+ V∞_out: [-0.2606851085115988, 0.002191940343200249, 0.05412973687164365] km/s
+ time of flight: 1.191891421207004e8 seconds
+ arrival date: 2027-01-31T10:58:25.954
+ thrust profile: [0.4647671945500343 -0.3395867873998096 -0.26477354551875054; 0.27874760650712804 -0.05131960823266019 -0.30684280534942976; 0.16487466776503026 0.003384376221570926 -0.2716018489594142; 0.10000357107042113 0.013100154467454925 -0.21739471196928156; 0.10256042897377542 0.021931987642688208 -0.2600347461883963; 0.07061250459369135 0.01921662033589416 -0.204706176029134; 0.014273841413863224 0.004622086218855583 -0.04815809391640561; 0.02039458559846296 0.007059571737846483 -0.07547345985616362; 0.016984454304113286 0.0056973086584735655 -0.06313586736043898; 0.0032938314345519987 0.0011548435020271046 -0.013501936260321794; 0.0005985246222527392 0.0002925610491794593 -0.001982810194468892; 0.0011358929296443417 0.00041527572402464286 -0.004815213046587604; -0.0011081099316503336 0.00042827973394841577 -0.0009025435045771235; 0.0005359343262512885 -0.0003888818272976763 -0.0010121822566764825; 0.0008920388360605931 -0.0004619211883589371 -0.001666817923039222; 0.0011204976046511302 -0.0008040650827022796 0.00018627897241179974; 0.0018942606948803345 -0.0005122562486975867 -0.0005433912159460274; 0.0010635092188805593 0.0006129406155646426 0.0004965916915052944; -0.0009835458687692837 -0.00016399362259938142 0.00044772410875315105; -0.0003562992363662105 0.0002260805006932921 9.990031128580219e-5] %
+
+Mass Used: 110.72319347162056 kg
+Launch C3: 102.5245241486674 km²/s²
+||V∞_in||: 0.2593853521675932 km/s
diff --git a/archive/ES_0.6077579154053965 b/archive/ES_0.6077579154053965
new file mode 100644
index 0000000..e139f81
--- /dev/null
+++ b/archive/ES_0.6077579154053965
@@ -0,0 +1,22 @@
+archive/ES_0.6077579154053965---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T04:22:03.444
+Launch V∞: [6.8619893954167175, -7.488091486407256, -1.8701012821825105] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.206159365927722e-6, -5.268851411671263e-5, 7.0102485792215825e-6] km/s
+ V∞_out: [-7.5083077609588175e-6, 3.2176503276599484e-5, 4.1821867239323965e-5] km/s
+ time of flight: 1.2119343032324457e8 seconds
+ arrival date: 2028-03-11T21:12:33.444
+ thrust profile: [0.3667033824216045 -0.170539548409718 -0.2179002403071028; 0.15248094864199288 -0.003388575415779415 -0.20156046876151062; 0.10822522462185084 0.016360049735987474 -0.22507663675416237; 0.07669100616408404 0.018434784711139206 -0.21482579937301766; 0.045853671610355945 0.012401941058038612 -0.1585222657757351; 0.03152635814474691 0.009089865490055742 -0.12735159756172118; 0.024005769038277246 0.007554975446115674 -0.10945645252025087; 0.006915467100934756 0.00021970989001472143 -0.04498721933530838; 0.004223291204489494 0.0039006967263936036 -0.030948911087512132; -0.0012707118950174914 0.0020089973239763087 -0.006246944701283884; -0.0052551957636440255 0.0022900813037943528 -0.011530615628415505; 0.004563110156334068 0.0080425758135981 -0.005663576507767515; 0.00321909756088505 0.003184446126740405 -0.004478479882913897; -0.004682908894998081 0.0008543664595049554 0.0037174320078374517; -0.0015873591358084962 0.004021986595974056 0.008484343621918421; 0.001197905773180504 -0.0019033657174101402 -0.0043645616552015955; -0.005042738256700605 0.01664192889895099 -0.004848624173883797; -0.018401509977059482 0.008458121480952761 -0.008100462749667966; -0.0003239430045747476 -0.0059211169935099025 -0.007125373535366913; 0.00795881531450998 -0.013740099607567943 0.004921555467933184] %
+
+Mass Used: 86.89270160574688 kg
+Launch C3: 106.65569137723698 km²/s²
+||V∞_in||: 5.331899175323072e-5 km/s
diff --git a/archive/ES_0.6077940731589664 b/archive/ES_0.6077940731589664
new file mode 100644
index 0000000..22d919a
--- /dev/null
+++ b/archive/ES_0.6077940731589664
@@ -0,0 +1,22 @@
+archive/ES_0.6077940731589664---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T21:45:12.105
+Launch V∞: [6.928242013209511, -6.9710714444111845, -0.765998272552484] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0035457569015971578, -0.02382810582038529, -0.0036510569897177337] km/s
+ V∞_out: [-0.02289138010602505, 0.00491527653428043, -0.006917926649476388] km/s
+ time of flight: 1.218386170259404e8 seconds
+ arrival date: 2028-03-12T01:48:49.105
+ thrust profile: [0.7797444500591432 -0.3232421245089172 -0.3226860038007953; 0.3844889647824366 0.03219502063874458 -0.3515915399471788; 0.2523048322825511 0.07923739457431411 -0.35622616483013975; 0.17395817798469002 0.07996823379429288 -0.32677938094805675; 0.08146584943225219 0.046397765223108296 -0.19272575330603847; 0.07086970300568952 0.04618745870421907 -0.1928228820402303; 0.032646138350693424 0.022847003701602253 -0.10700118153888744; 0.007590735272219815 0.007006431773133535 -0.03186383747309959; 0.0075004778055157775 0.006593133757465739 -0.032443427445073676; 0.0014230604330623584 -0.0012595577104342673 -0.004094734987766773; 0.000574052247536957 0.008497924264600328 -0.0008907123708959339; -0.008840512321756264 0.007170356962759519 -0.0025972998704900533; 0.002666105480430589 0.002587048444693183 0.0059856410525999815; 0.00034887897492021655 -0.0011782116023683403 -0.0027721584007768456; 0.00103711586312248 -0.0017519101228358857 -0.0010554341217713307; -0.009590601820851249 -0.0006559473744415109 -0.0061994019183835404; -0.008981306742640902 0.0077420988918033935 -0.0002009410437164088; 0.0024606204139128447 -0.0029171918997506667 0.005341717494183762; 0.0004596958720599594 -0.00230722659594564 0.0012644745064267094; -0.003871017806763176 0.0026572889350316656 -0.004715323210559597] %
+
+Mass Used: 142.19150634239531 kg
+Launch C3: 97.1831278302398 km²/s²
+||V∞_in||: 0.024365574816426348 km/s
diff --git a/archive/ES_0.6079206429907853 b/archive/ES_0.6079206429907853
new file mode 100644
index 0000000..dbd522e
--- /dev/null
+++ b/archive/ES_0.6079206429907853
@@ -0,0 +1,22 @@
+archive/ES_0.6079206429907853---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-25T08:47:08.372
+Launch V∞: [7.770790690225183, -6.0090600390833595, -0.08950092240093478] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.145290713223777e-9, -2.933176809097247e-9, -1.0104688385626834e-9] km/s
+ V∞_out: [-5.3146413935752474e-9, 3.951776675281598e-9, -1.7977811772021462e-9] km/s
+ time of flight: 1.6230264289047036e8 seconds
+ arrival date: 2029-06-16T20:51:10.372
+ thrust profile: [0.47063964441951506 -0.07278893308470717 -0.09221418458193828; 0.4433727750631946 0.21554901091068004 -0.2624150038649794; 0.24405422385630282 0.216197546413266 -0.23617303803484888; 0.15057419427222343 0.18471558736734553 -0.21429219761999974; 0.08764639079116684 0.13533927483397096 -0.16969917062200413; 0.042772091256126174 0.0788465009603445 -0.10809082618773955; 0.011222704954091355 0.023924747703226584 -0.0349601481815257; 0.007607159296555922 0.018536460104682732 -0.027797667772392863; 0.0009128346298441116 0.002591795056176021 -0.00406715612412624; 0.0037414852111585166 0.01170177645513621 -0.018709424221360425; 0.00032985201050669805 0.0016833434923172706 -0.002843816261652172; -6.40262291332662e-5 0.0010710631405581052 -0.001226874654073871; 0.0006442405754773794 0.0016752424082709405 -0.002381031765305016; 0.00046109154170531023 0.0011043224425623434 -0.002040490815147703; 0.0002559913959126486 -4.191233052310369e-5 -1.2287192099435032e-5; -5.416944017288454e-5 -0.0009551740814313647 -0.0007353714922952433; 3.945442136754061e-5 -0.0018951355103909474 0.000448390472877955; 0.00013466343775220637 0.0006358769847240576 -0.0010049175209348427; 0.0001429766415002498 0.0003849041662347644 -0.0008884462077124299; 0.0004461056641955042 -0.001224105946987149 0.0006879584954529194] %
+
+Mass Used: 146.31241145761078 kg
+Launch C3: 96.5020009197095 km²/s²
+||V∞_in||: 6.88397933009437e-9 km/s
diff --git a/archive/ES_0.6081986584335951 b/archive/ES_0.6081986584335951
new file mode 100644
index 0000000..75276f0
--- /dev/null
+++ b/archive/ES_0.6081986584335951
@@ -0,0 +1,22 @@
+archive/ES_0.6081986584335951---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-27T13:28:24.724
+Launch V∞: [7.174990566505607, -5.694087640464849, 0.8578181550236185] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00010731512670546547, 0.0002044312798660693, 7.386928221469432e-5] km/s
+ V∞_out: [2.1341489092229188e-5, -0.00014095415584044037, 0.00019622390115699907] km/s
+ time of flight: 1.8749577775411496e8 seconds
+ arrival date: 2030-04-06T15:38:01.724
+ thrust profile: [1.0 -0.013608272016363556 -0.06960117252550028; 0.7024223120474911 0.5022965160005906 -0.19521222761637097; 0.21845030602416263 0.28735545698690423 -0.13460034643178953; 0.09620472423491433 0.17808098937912153 -0.09404826546889444; 0.034836991664896386 0.08959803257331578 -0.05327219426214073; 0.01599948110692474 0.05475355836311866 -0.03516715691182709; 0.025808155581409108 0.12227596534769072 -0.07726790004531667; 0.005942051113859677 0.03697504770508425 -0.026257978320049724; 0.00026818624930169583 0.0026552080581827365 -0.001969170348985645; -0.0006196309521831435 0.0005244217632303331 -0.00012637016858935013; -0.0004208295055710943 -0.001674078618666114 0.0004330792279821934; -0.0021178584619240904 0.0007050023638117534 -0.0006292942241252686; -0.00022515420712526245 0.001910036556055803 -0.00031668643814923895; -0.0005102111605426109 0.002567358610240745 -0.000896808862900387; -0.0002424389956418133 0.00016657016856833952 -0.00010375527781257424; 0.00026803707718483377 -0.0004099831248584704 -0.000588122470995352; -0.0013033253524049704 -0.0022463024164360813 -0.00033366915648349216; -0.0023338558135953293 0.002104799081277624 0.0015176093099419099; 0.00029240656975961334 -0.0003907985744752917 -8.000255081271727e-5; 0.004283986410085579 -0.0002511408376240179 0.001323065549584771] %
+
+Mass Used: 215.83774340853597 kg
+Launch C3: 84.63897567382713 km²/s²
+||V∞_in||: 0.00024241566670164577 km/s
diff --git a/archive/ES_0.6082455015634521 b/archive/ES_0.6082455015634521
new file mode 100644
index 0000000..03db02b
--- /dev/null
+++ b/archive/ES_0.6082455015634521
@@ -0,0 +1,22 @@
+archive/ES_0.6082455015634521---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T12:01:34.416
+Launch V∞: [7.018000014777629, -7.380670619947144, -1.8673986455385359] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.876598943722913e-6, -6.085898854794221e-6, -2.1023174338906713e-5] km/s
+ V∞_out: [-1.0942003757027275e-5, -2.0515275503938693e-5, -6.32770161602574e-7] km/s
+ time of flight: 1.1825406501827969e8 seconds
+ arrival date: 2028-02-05T04:22:39.416
+ thrust profile: [0.3117901670366257 -0.14607905301084417 -0.17758620138036385; 0.17374247314830987 -0.0016925672478246463 -0.21076004914432428; 0.1322521545878883 0.023900543122878183 -0.2478608113177583; 0.10108693795503729 0.029206425133939066 -0.25196950717542227; 0.07145217759040434 0.02578913751422765 -0.21886012829978707; 0.045461579614368586 0.0190187238202465 -0.16348204377213016; 0.01740955219130278 0.009487388302654675 -0.07392281081097492; 0.001572929342222436 -0.0007914536004605964 -0.022173070223628834; 0.0004707453697678399 -0.0004947078878005994 -0.025777787966595602; 0.0027557259672371616 0.0014862263154449414 -0.010431505008687406; -0.0001913981366904985 0.00028138442817979455 0.0004193963381649399; 0.00033890980712584 -0.0010396141221447749 -0.0015960508723873246; -0.00027180175909078405 1.4626483488618396e-5 -0.0009567576530985413; -0.000691271590423897 -0.0003623152533640825 -0.003888412978790931; 0.000413086515606959 -0.0028102290530730807 0.0036746442254137488; -8.451466797208178e-5 8.922333880587651e-5 0.0017370893289217352; -0.0026733550631715466 0.0005791417847498927 0.007339183596904508; -0.00662275834149005 0.001728810386689566 0.004081096474127652; 0.0002072373913003286 0.0027568160944772932 -0.001414462631186938; -0.00012827951276588387 -0.0020323088775342185 -0.0005523849465524605] %
+
+Mass Used: 84.20591435527558 kg
+Launch C3: 107.2138007089289 km²/s²
+||V∞_in||: 2.326054245014738e-5 km/s
diff --git a/archive/ES_0.6085078053733604 b/archive/ES_0.6085078053733604
new file mode 100644
index 0000000..f1a9654
--- /dev/null
+++ b/archive/ES_0.6085078053733604
@@ -0,0 +1,22 @@
+archive/ES_0.6085078053733604---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-28T17:35:25.746
+Launch V∞: [4.913782209390837, -8.83779187186539, -1.7141915848824187] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.619133285634739e-6, 7.776270474752482e-7, 1.5025112530017774e-6] km/s
+ V∞_out: [-1.04303119178226e-6, 1.424287597582803e-6, -1.5361541646193329e-6] km/s
+ time of flight: 1.2768319711053216e8 seconds
+ arrival date: 2027-05-15T13:08:42.746
+ thrust profile: [0.41494280672288514 -0.32926731090594924 -0.2899268547279687; 0.10406127500885595 -0.03223158819009261 -0.16115117861788616; 0.06285677912646444 -0.010841709049576813 -0.15456184184077948; 0.05744393405502837 -0.0067258455906955015 -0.18744341648871185; 0.04535858004530885 -0.00474602734233373 -0.18204694663700483; 0.025958543861617504 -0.003082651845781198 -0.12276663665941959; 0.006631735545664945 -0.0036380351962112967 -0.05783544966181063; 0.011574749092896042 -0.003809065349663699 -0.09813902796903183; 0.015899685928972066 0.0019168855525381705 -0.08171435874657568; 0.003866248102762587 -0.0036526585793931433 -0.01941437188893337; -0.0006077290471860751 -0.0012783035962520815 -0.004309763612802112; 0.001495274968407237 -0.0002321507269152476 -0.004661073382966592; -0.0001649903282756834 -0.0012894760162043938 -0.00835214372477312; -0.0011959764982461837 0.0011860184783421494 0.002079485141297888; 6.155666390982354e-5 -0.0013616370880803158 0.003092212448135221; -0.005827744231716031 0.011855827234827705 0.0054242913860048396; 0.010947882238519427 0.017711802521779313 0.011350427969759595; 0.006732244135609141 0.008609807029814676 0.016319424911546473; 0.02376509797265459 -0.005061378638363485 0.00951909457334257; 0.0487698954728457 0.008471757431673065 -0.012944192465995392] %
+
+Mass Used: 96.31584382731808 kg
+Launch C3: 105.19027356141756 km²/s²
+||V∞_in||: 2.341759271789564e-6 km/s
diff --git a/archive/ES_0.6085826519710863 b/archive/ES_0.6085826519710863
new file mode 100644
index 0000000..2c803fb
--- /dev/null
+++ b/archive/ES_0.6085826519710863
@@ -0,0 +1,22 @@
+archive/ES_0.6085826519710863---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T19:53:42.119
+Launch V∞: [6.9288378385022344, -6.932296929474642, -0.6272507119793395] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0006540043280140148, 0.010335295201574921, 0.0012636841871836993] km/s
+ V∞_out: [0.009970177063103049, -0.0018775525643173496, 0.0024163117243714196] km/s
+ time of flight: 1.2545233723819087e8 seconds
+ arrival date: 2028-04-22T19:45:59.119
+ thrust profile: [0.6766222879169989 -0.26275890136979607 -0.2694575737970667; 0.4706779395130115 0.05160804592616034 -0.4284346106773904; 0.24007827627314093 0.08225936365459138 -0.3535708590478782; 0.13250846133120917 0.06484167791640218 -0.26521221816938556; 0.08630723986891489 0.05194767126897858 -0.21428201795933388; 0.03135269731281294 0.020892643530730563 -0.08684998107495757; 0.038702631582269074 0.02795167803000577 -0.12043061202638346; 0.023484675558078327 0.0187803778464983 -0.08020830361730642; 0.006517445914842709 0.005258409111744439 -0.018751505861503634; 0.001966343980861023 0.0030900323716984033 -0.0067143375620641425; 0.0016461788338894927 0.0011757462105019237 -0.00500515718309082; -0.00012125980581636012 0.004142593569484734 -0.0021003146958198625; -0.005903335235263755 -0.006404052756831293 -0.00859528923310483; 0.009351113951543208 0.007125927156346439 -0.013754064651403875; -0.024677929979790576 0.0025222331038079375 0.0008814484951532257; 0.002652686497304141 -0.0037116294564064046 0.002323962311049017; -0.00191982786871298 0.005759846737925936 -0.048116958398040116; 0.018767577404707723 0.015408567310608648 0.022172026291963704; -0.009408527473103018 -0.014856953811632243 -0.015459519526258965; -0.028961023950217223 -0.029160195700332864 0.02472838743240286] %
+
+Mass Used: 147.33572249593635 kg
+Launch C3: 96.45897796634246 km²/s²
+||V∞_in||: 0.010432782289001184 km/s
diff --git a/archive/ES_0.6086933854732902 b/archive/ES_0.6086933854732902
new file mode 100644
index 0000000..b4070f2
--- /dev/null
+++ b/archive/ES_0.6086933854732902
@@ -0,0 +1,22 @@
+archive/ES_0.6086933854732902---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T01:47:27.429
+Launch V∞: [6.803261030682565, -7.002450103950251, -0.9584372928671265] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001159673872884207, 0.007985805142288423, 0.0011908891187109474] km/s
+ V∞_out: [0.007663695413882288, -0.0015425504398251567, 0.0023017000248419265] km/s
+ time of flight: 1.2176064462835109e8 seconds
+ arrival date: 2028-03-12T08:11:31.429
+ thrust profile: [0.9500650608846835 -0.4077207637722796 -0.4257521095427006; 0.35482322808869904 0.022283403381848903 -0.35436622371425874; 0.2259963585481711 0.06416604034604659 -0.35037662164716493; 0.14360119360116613 0.06001325974979258 -0.2975363838509709; 0.08488860518528274 0.04270885918301855 -0.21622060150150452; 0.05229394708020579 0.029091764170039107 -0.15385025361296278; 0.010035553412126964 0.006124579486449699 -0.02986211996342262; 0.00788048554676666 0.008925404838000943 -0.03223218567126896; 0.0016090097715044114 0.006442471970529289 -0.03178364530503541; 0.00660612320609679 0.007283604812538718 -0.03381833797764928; 0.0006834383146989798 0.007108577683689971 -0.0056574584856835365; -0.0019327652848920992 9.834333367963243e-5 -0.006297625143696719; 0.0004908956714398625 -0.000600837488093864 -0.003953876073890269; 0.0009972184493909672 0.0009648172480932879 -0.002342944561572823; 0.0021132247446151234 0.0014422750637196155 0.006981766662352605; -0.003665577869565931 -0.0031034421550640012 0.009647713955255759; 0.0016699819713638926 -0.002689198254708128 0.0048123405484184305; -0.017584118701162887 -0.0045707895542629 0.03055213225452212; 0.031657298706786234 0.028793823369328973 0.016781773030549833; 0.0033733536809650126 -0.02392062632837231 0.012428880429734022] %
+
+Mass Used: 148.75820715223244 kg
+Launch C3: 96.23727015427534 km²/s²
+||V∞_in||: 0.0081569690544414 km/s
diff --git a/archive/ES_0.6088191858566046 b/archive/ES_0.6088191858566046
new file mode 100644
index 0000000..e034f86
--- /dev/null
+++ b/archive/ES_0.6088191858566046
@@ -0,0 +1,22 @@
+archive/ES_0.6088191858566046---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:57:26.377
+Launch V∞: [5.246759713369285, -8.604891561875407, -1.427872389890995] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.04329888329283081, -0.020635597978565835, 0.045408786399703] km/s
+ V∞_out: [-0.04168326874363807, -0.01809671134018266, -0.04803086224114027] km/s
+ time of flight: 1.2017272433834955e8 seconds
+ arrival date: 2027-02-12T13:16:10.377
+ thrust profile: [0.4542631251307327 -0.32648275863784476 -0.2509608971244409; 0.17307108946996302 -0.02867236744627385 -0.19909204328980962; 0.10900926033148423 0.004053696053725871 -0.1844699345612186; 0.11772876458586407 0.020639775892783964 -0.24397152979335346; 0.08827739116286513 0.02023266225049762 -0.22552596275088263; 0.06277307106319187 0.017517918421186725 -0.19061130624426667; 0.0380514288738743 0.011655407079645092 -0.13118064908314178; 0.02366649501518596 0.006360135223165293 -0.08769053485341262; 0.012464291339734755 0.0042921202595775304 -0.051652737163436616; 0.010448001715991166 0.00164716018700366 -0.038277537350315756; 0.0015962387539938902 0.000267768484143908 -0.005878611135638668; 0.0026255833757613542 0.003046256915068132 0.0005582532527339855; -0.002368603254071656 -0.0010366182589204708 0.003860843823183973; 0.000755484179561155 0.0021087525467564025 -0.0076164775458993925; 0.0033757854217730953 0.0018443993859689302 0.002286935654762231; 0.00902973282567265 -0.004480646039327371 0.0004893396618890333; 0.003492145529915905 0.00039365271904354354 -0.002300911993921971; 0.006777918908161273 0.01006267245012836 -0.0038710042096590943; -0.006489003256137361 -0.009710412929005388 -8.558079548837702e-5; -0.014609853495569206 -0.0013654876692138214 -0.00824045895416092] %
+
+Mass Used: 105.88883274689033 kg
+Launch C3: 103.61146584328256 km²/s²
+||V∞_in||: 0.06604982271462223 km/s
diff --git a/archive/ES_0.6088706611271432 b/archive/ES_0.6088706611271432
new file mode 100644
index 0000000..54d2871
--- /dev/null
+++ b/archive/ES_0.6088706611271432
@@ -0,0 +1,22 @@
+archive/ES_0.6088706611271432---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-12T11:23:36.718
+Launch V∞: [5.852827281362403, -7.769456009807147, -0.28497092106407024] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8702004897362585e-8, 5.570559070514117e-8, 3.060322637418535e-8] km/s
+ V∞_out: [-1.86094652054188e-8, 3.857547624750443e-8, -5.582272032388791e-8] km/s
+ time of flight: 1.4702920838227352e8 seconds
+ arrival date: 2027-12-09T04:50:24.718
+ thrust profile: [0.5861277992213259 -0.3085042612351793 -0.17230424154805915; 0.5651485754728522 0.0478658006895689 -0.37812819870625697; 0.29571360257274737 0.10711109657965083 -0.3099109067389964; 0.18551489399633234 0.10189313192086129 -0.2590696855998165; 0.11027542493819886 0.07625874279567989 -0.1910314432626897; 0.052405267381170205 0.04189081022509487 -0.1073635617563516; 0.02221298258323142 0.020407890091718936 -0.05352094066982543; 0.014241629211580899 0.01411411721703723 -0.03829956835173391; 0.009705740990908823 0.010457305338698443 -0.029132517872525222; 0.0016601151061282349 0.0042774275957689865 -0.004450109102354523; -0.0004453254571646279 0.0009168189323069903 -0.005070287623135236; -0.0010184197190996405 -0.0010283303877948054 -0.0006545850951261566; 0.002800116743669756 0.001569682907156901 -0.0069537884323244105; 0.0038751823239666573 0.004867949567997014 -0.0016214517786063481; 0.0024029260596928424 0.0013050406915094824 -0.001338531594187434; 0.0032504696860366 0.006476912943123525 0.0004260078117647335; -0.0035370463618094087 -0.00258288883495965 0.002366669697652604; 2.924309595046367e-5 0.0005737187255067944 -0.0007269956720351092; -0.0018970524331346974 -0.0022275672337519615 0.006409668564676413; 0.002570629219923609 -0.00019059235613303426 -0.0072872676780062606] %
+
+Mass Used: 157.92519123376405 kg
+Launch C3: 94.70124229964051 km²/s²
+||V∞_in||: 6.973862190670655e-8 km/s
diff --git a/archive/ES_0.6089448755986142 b/archive/ES_0.6089448755986142
new file mode 100644
index 0000000..dd33c3d
--- /dev/null
+++ b/archive/ES_0.6089448755986142
@@ -0,0 +1,22 @@
+archive/ES_0.6089448755986142---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T20:12:58.596
+Launch V∞: [6.881465467800674, -7.395849966781769, -1.6919707244322244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004590724099799008, -0.00024301796463371882, -0.0011329253860395717] km/s
+ V∞_out: [-0.0005867151966618886, -0.001098883272408855, -3.4889553717530483e-5] km/s
+ time of flight: 1.1711248265953682e8 seconds
+ arrival date: 2028-01-23T07:27:40.596
+ thrust profile: [0.6123307006160796 -0.2958916520839874 -0.33523911083725627; 0.15042515679353016 -0.005625844058502369 -0.18651390345736085; 0.12570039626519294 0.017674910230147237 -0.23923407898913032; 0.09000821670736966 0.021368165665098585 -0.22940288379224655; 0.058161142850830065 0.017579399098094604 -0.18509689674813407; 0.03974673387591901 0.012350949334193083 -0.13111959565820192; 0.02910568686272571 0.014252614506106598 -0.1217794942677109; 0.015410957526158058 0.006214211744984875 -0.06333646584930559; 0.0048686569367343375 0.0022582717563632976 -0.027116185627980932; 0.004616050281294538 0.0013346644801333339 -0.022506599365381436; 0.0009942675560534763 0.0006478829200507713 -0.006339219251216806; 1.1845138006015814e-5 0.00012494447190158786 -0.0013153026738948771; 0.0005496934099264001 0.0014702637631130075 -0.001420428712536715; 0.000236849893192261 -0.00028141246796314695 -0.0015030302388339128; 0.00011026293642654229 -0.0004858547204459338 -0.0014882053449763592; 0.00021816565715289808 0.00023963066668149604 -0.0004618246241610024; 0.00042351279611242795 1.3647098721728153e-5 0.0002708936788322668; -0.0006393507432914999 -0.0007455517694051508 0.0004016234053489257; -0.002748223630697707 0.0004276619270847256 -0.0010475857672058045; 0.0009521884847865131 -0.0009028787749704799 0.0014266710545593258] %
+
+Mass Used: 98.4261044182972 kg
+Launch C3: 104.91592864801476 km²/s²
+||V∞_in||: 0.0012463246523568335 km/s
diff --git a/archive/ES_0.6089695777669062 b/archive/ES_0.6089695777669062
new file mode 100644
index 0000000..c672505
--- /dev/null
+++ b/archive/ES_0.6089695777669062
@@ -0,0 +1,22 @@
+archive/ES_0.6089695777669062---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T13:35:38.880
+Launch V∞: [6.946026629852249, -7.383958131945116, -1.7175974214224592] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001596591842529211, -0.0026417678521379762, -0.0010190299621863606] km/s
+ V∞_out: [-0.0018838615934041068, 0.0023456402251730746, -0.0012294593625590468] km/s
+ time of flight: 1.176201230834942e8 seconds
+ arrival date: 2028-01-28T21:51:01.880
+ thrust profile: [0.46932381880645957 -0.22315287848655543 -0.2653793372901713; 0.17115261476978644 -0.0037430348766327804 -0.2108890931761313; 0.13299120925156466 0.021750591407700585 -0.2522610766327505; 0.11077244868925318 0.029183978984310865 -0.27850222461368795; 0.06797574904840695 0.022288599307955726 -0.21201978835001348; 0.02952188736706386 0.011289915634240725 -0.11012381289362842; 0.017495953838031694 0.0076880399219143815 -0.07402678462436409; 0.01121467754813128 0.006245267106184422 -0.054431602791226344; 0.007230494629087217 0.004129669331962779 -0.042858859965053765; 0.0010555046191058624 0.0025511172402055736 -0.004923431878686807; 0.0006684316403659189 0.0006266168406957001 -0.0033443560225607715; 0.00033335953251503725 0.000104698105004971 -0.0017775239684613524; -0.001314177235304928 0.0021422904291223065 0.0005609440044920286; -0.003936571554795186 -0.003398523448067063 0.00010687080490246175; -0.0005352222030659096 0.00013130134048715774 -0.0007205741612600254; 0.0025174615233629783 -0.002077044663764081 0.0023248893928070995; 0.0026613616250547676 -0.0034814171124642893 -0.0015391274509225757; -0.007612902453201492 0.00435787098316954 -5.272789361999823e-5; 0.0012719291553884527 -0.0019458473046124313 0.004340777481210475; 0.0018696260149410554 0.0006519191587086881 -0.0027234065732886473] %
+
+Mass Used: 93.76296425048668 kg
+Launch C3: 105.72026453901208 km²/s²
+||V∞_in||: 0.003250609936620211 km/s
diff --git a/archive/ES_0.6089964013025696 b/archive/ES_0.6089964013025696
new file mode 100644
index 0000000..fb1ea8c
--- /dev/null
+++ b/archive/ES_0.6089964013025696
@@ -0,0 +1,22 @@
+archive/ES_0.6089964013025696---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T23:22:30.871
+Launch V∞: [7.003803223609787, -7.238145018475076, -1.625777195394748] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00044341312963920825, -0.0028511918392853694, 0.0027611356758563965] km/s
+ V∞_out: [0.0012894400334243492, 0.003082632175678958, -0.0021871773968472584] km/s
+ time of flight: 1.184901249212823e8 seconds
+ arrival date: 2028-02-06T09:17:54.871
+ thrust profile: [0.5643156663313327 -0.24335417956723035 -0.278337652527385; 0.1855986210755885 0.007708360041412881 -0.20936766269551524; 0.09789686002917602 0.024862059141083692 -0.1742434282515355; 0.07647307844855192 0.029034762520102824 -0.18188885963284349; 0.06772759426865287 0.03136112089343187 -0.19445019455517187; 0.049086521382880145 0.027203664986850368 -0.16406106695758194; 0.023397457784281227 0.013309734029455466 -0.0900342763356063; 0.02546549314278935 0.015210710632966484 -0.10545474116560581; 0.039538084785593036 0.026527678155024777 -0.17032938348277507; 0.007231649615628299 0.00428433664346593 -0.031989753272087376; -0.0013942845951794391 0.00041897819925670833 0.000719133630501943; -0.002050656655219463 0.0018051968543787238 -0.0060237400634842835; -0.0003705237951622368 0.00024882325275605904 -0.0004467909530783084; -0.0002133749895878365 -0.0004914744527837155 0.0007516664878346375; 0.0005738662715063601 0.00114726981615473 -0.0059647740330060015; 0.0005747415506890382 -0.00022200455025742368 -0.0033254680030251906; -0.0029374771809278256 0.00015458010316316925 -0.007122009025278653; 0.003577762325079211 -0.0044927278673106644 -0.005046334330162708; -0.0004138731904037823 -0.002886141211035565 -0.0003530261005188738; -0.00019043485151301089 -0.001689921308310444 0.0005213365473049434] %
+
+Mass Used: 103.32073422956773 kg
+Launch C3: 104.08715439258802 km²/s²
+||V∞_in||: 0.0039937176074969155 km/s
diff --git a/archive/ES_0.6091362303248621 b/archive/ES_0.6091362303248621
new file mode 100644
index 0000000..8d736f2
--- /dev/null
+++ b/archive/ES_0.6091362303248621
@@ -0,0 +1,22 @@
+archive/ES_0.6091362303248621---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T22:35:34.906
+Launch V∞: [6.977065721754441, -7.3542683231404045, -1.5507006313496363] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008840911845675472, 0.05639404822248715, 0.010296542045022818] km/s
+ V∞_out: [0.05476149013269202, -0.010854703010383885, 0.01573964152073887] km/s
+ time of flight: 1.1811802884861027e8 seconds
+ arrival date: 2028-02-03T01:09:22.906
+ thrust profile: [0.4740015645504973 -0.2078848676218471 -0.22456284839117352; 0.10001199680929469 0.0033939551892024655 -0.11420113693985448; 0.1158650057985214 0.029883036254289175 -0.2028386980525096; 0.09769960129224116 0.038875173300470814 -0.22675501133283799; 0.12688292058781167 0.05861509717115287 -0.32239109094848667; 0.04804120452968353 0.025256774468484542 -0.1560442627242486; 0.01991351954156398 0.01119521066702248 -0.07455386364583703; 0.024910117156440627 0.014462419568240844 -0.09737247628603807; 0.012470713961600962 0.008981875319099976 -0.05554639174366375; 0.01590564265163793 0.008833384892348086 -0.06317119820861924; -0.0008995384587794843 0.003982228483735773 -0.008443048819330612; -0.00037586027308866127 -0.004184967459822105 -0.006819855688520764; 0.00036365503323083654 0.0021175745943819027 -0.0025844653213464843; 0.001875569480571762 -0.0017514507515183548 -0.003493601814928397; 0.002197242791741884 0.005972747983007183 -0.0017088473570212983; -0.0033891515566946634 0.0009001436344680308 -0.001094857526479518; -0.0009413418620288741 -0.0032214161982202787 0.002348620480927446; -0.0011795363477038845 0.00018765493855722097 0.0010273145926878295; 0.0008293637231254273 0.00024720764828525853 0.0016589329974564162; 0.0005365280436559995 0.0002975216001347757 -0.00203021764190554] %
+
+Mass Used: 97.17087894778297 kg
+Launch C3: 105.16938110249535 km²/s²
+||V∞_in||: 0.05800404447336525 km/s
diff --git a/archive/ES_0.6096388242960569 b/archive/ES_0.6096388242960569
new file mode 100644
index 0000000..bc63774
--- /dev/null
+++ b/archive/ES_0.6096388242960569
@@ -0,0 +1,22 @@
+archive/ES_0.6096388242960569---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T08:24:37.948
+Launch V∞: [7.040380990085368, -7.075384823457944, -0.8941709194153271] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0010524807870050292, 0.007084406936231533, 0.001116999392589253] km/s
+ V∞_out: [0.006754868561289984, -0.0013747063528088581, 0.0022229807765969823] km/s
+ time of flight: 1.1913015052564856e8 seconds
+ arrival date: 2028-02-11T04:07:07.948
+ thrust profile: [0.6564065351993765 -0.27836462461247174 -0.312683334404916; 0.27331044476135624 0.014805652046969459 -0.27099712376646584; 0.17588029353786955 0.04803917141457098 -0.26779614134006846; 0.12045621759699712 0.049101050263142106 -0.2424026692144669; 0.08480689534610732 0.042496087649040636 -0.2082910654614186; 0.06252285423367902 0.035180765670532174 -0.18003993090543577; 0.0885939537734484 0.05445873900843833 -0.26419405449765127; 0.02494484710222177 0.01566419627931851 -0.08693417430484093; 0.01427619804740799 0.009244080286617959 -0.05266630213495681; 0.002377813762146218 0.002346123249574157 -0.013727538325507367; 0.0003060623760813121 0.0002693561667547757 -0.0011658727086582533; -0.00020846669745960594 0.0007253029306878349 -0.0005171731231332103; 0.0009103284671902114 0.0002840590964033079 0.00035565948380738384; 0.00010771751690372269 0.0001737678131190824 -0.0009868507934381891; 0.00028064503511123135 0.0002868264867256989 -0.0008110794216423113; 0.0002518889441255445 0.00011491382020994772 -0.0009160497151327572; 0.0004753706265053226 0.0011817768998617071 0.0008550050130249633; -0.00030028176825658883 -4.8424370477917586e-5 -0.0004915833582421491; -0.0021137242548533207 -0.0003362126896764675 0.0026902632568126484; 0.0009902488465022908 0.0011002053330372798 -0.0007757386158517815] %
+
+Mass Used: 125.41776531963524 kg
+Launch C3: 100.4275765187025 km²/s²
+||V∞_in||: 0.007248739551686551 km/s
diff --git a/archive/ES_0.6096741792802488 b/archive/ES_0.6096741792802488
new file mode 100644
index 0000000..075d03a
--- /dev/null
+++ b/archive/ES_0.6096741792802488
@@ -0,0 +1,22 @@
+archive/ES_0.6096741792802488---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T17:43:15.256
+Launch V∞: [5.0607899777812, -8.706627065091237, -1.7261362343749493] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.009587544162696977, -0.007853802352039845, 0.00017657046519704432] km/s
+ V∞_out: [0.004159185431189846, -5.882930887531882e-5, -0.01167333772839226] km/s
+ time of flight: 1.1907079281489468e8 seconds
+ arrival date: 2027-02-01T20:56:27.256
+ thrust profile: [0.596609477949358 -0.4689451532241415 -0.3873110146458073; 0.10350894019883058 -0.02499935755192187 -0.13391271246557743; 0.13518945036678043 -0.008474214341183907 -0.2578762758658503; 0.10137625985901713 0.003605418379032479 -0.2516958095811859; 0.0674373929332891 0.0067645447932886005 -0.20238174731889816; 0.03471259085063107 0.0050776992078593345 -0.1213710779021852; 0.020430550979369595 0.004508698636004886 -0.08666650267159014; 0.006776010955950052 0.00489225082639212 -0.032460888248994915; 0.003981757719211417 0.0035369894241351514 -0.01627156650759; 0.003781057854419936 -8.209357397890985e-5 -0.005183998990705378; 0.004228821483672396 -0.0026117939937752134 -0.007118957257345894; -0.006105829982458507 -0.005671530041800336 0.0027261998872120255; 0.0011126681428182494 -0.0004932796843986595 -0.003550214723759832; -0.003376162107528706 -0.00021468967087017897 -0.0029933444370258836; -0.008907750405400395 0.00429936906674155 -0.00623502609301401; -0.003518658526974778 -0.01233190126332175 -0.002977038596992337; 0.005020712809812211 -0.002980872802974106 -0.0025473613942700226; 0.008494216071042766 -0.011434274796318152 0.0036674785387187203; 0.0016249319252735273 0.0010831373614605966 -0.0009576182653389888; -0.00776334015355064 0.002659698285961596 0.00910034443128487] %
+
+Mass Used: 102.30698045538702 kg
+Launch C3: 104.396496349412 km²/s²
+||V∞_in||: 0.012394934109778535 km/s
diff --git a/archive/ES_0.6097847985764514 b/archive/ES_0.6097847985764514
new file mode 100644
index 0000000..606ee29
--- /dev/null
+++ b/archive/ES_0.6097847985764514
@@ -0,0 +1,22 @@
+archive/ES_0.6097847985764514---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:38:01.306
+Launch V∞: [6.959245761946217, -7.397199725949876, -1.639588173741903] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00034224612847714455, -0.00015680596768685704, -0.0007367247654754538] km/s
+ V∞_out: [-0.00036386502980938695, -0.0007426785518139596, -2.2188002548902494e-5] km/s
+ time of flight: 1.1887663396449593e8 seconds
+ arrival date: 2028-02-12T16:55:14.306
+ thrust profile: [0.40449241723137236 -0.18690672249022564 -0.22204548412157832; 0.16344832639523582 -0.0011490641986651757 -0.19950875210575011; 0.13364740359642943 0.024242748967100127 -0.2509717791440859; 0.08016064120973812 0.02295916670116365 -0.20319991686371713; 0.026470853286563314 0.008953868043111619 -0.08201096703002689; 0.03203877501699258 0.012138278943638989 -0.11034953005558149; 0.013864373113199196 0.005585127300801435 -0.05416727960069102; 0.014993199587048128 0.007675637659318844 -0.06708410381735225; 0.039448515333088095 0.018739908825926545 -0.18426059043286752; 0.03093724614363416 0.015194494946797052 -0.15416348088434123; 0.002480352253002639 0.0013797312062318388 -0.014110979463682276; 0.00025471504405810523 0.0001762206705077363 -0.0028826037911057105; 3.460399125947475e-5 -0.0021984135558215556 0.0005850698133815805; 0.00023158339437775988 0.0011748465638870293 -0.002156715257939143; -0.0013673425545168922 -0.0017742849569812404 -0.0007697176426983598; 0.0035888538600998164 -0.0003545953754769118 -0.0033880942323091454; 0.0011047449540935402 -0.00044739831054452624 -0.004982462437263425; -0.000808426797310744 -0.0008978386294580133 0.0007600473585296105; -0.0020963698946085863 -0.007964579823798109 -0.0025903851958976967; 0.005696019788604883 -0.0005962410247612555 0.002416780602267036] %
+
+Mass Used: 94.0277623544971 kg
+Launch C3: 105.83791474023363 km²/s²
+||V∞_in||: 0.0008273354241325994 km/s
diff --git a/archive/ES_0.6098152944713977 b/archive/ES_0.6098152944713977
new file mode 100644
index 0000000..c1d4097
--- /dev/null
+++ b/archive/ES_0.6098152944713977
@@ -0,0 +1,22 @@
+archive/ES_0.6098152944713977---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T23:50:03.587
+Launch V∞: [6.998234136766537, -7.292540991009043, -1.409236669305668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.019500351327355e-6, 5.188482571588288e-5, -6.857497607977737e-6] km/s
+ V∞_out: [6.753024483749795e-6, -3.609488615931606e-5, -3.766317101060774e-5] km/s
+ time of flight: 1.1690305292407072e8 seconds
+ arrival date: 2028-01-19T00:54:15.587
+ thrust profile: [0.47897977333330827 -0.21867548879035775 -0.24780907936567428; 0.230995776775426 0.00100219972973367 -0.2530506465484781; 0.15412301953776347 0.031175189240446877 -0.25935319400017937; 0.16858959112607233 0.054392020358707396 -0.3685283412505978; 0.08399863486452087 0.0331451717235659 -0.22752108009431923; 0.06200077884186229 0.027678064909527903 -0.19457925087760064; 0.014588239162913026 0.007277451481060739 -0.05462124989588544; 0.009978429852967739 0.00532380967336667 -0.0413679282543596; 0.0034840816937433544 0.002037903868810703 -0.015941377949863233; 0.0006767631898801767 -0.0002620145180645609 -0.0018206495850751755; 0.000729699992288578 0.0009847955584885717 -0.004278143832096134; 0.00038562299390128567 0.0004935920826716582 0.0007341410755406811; -0.0009719667282851678 -0.00042768046645165123 0.0006109193489414457; -0.0006907420440077454 -0.00014387204831444475 0.0037646162701382; -0.003240475834152043 0.0006596735245466554 0.0024456444516442123; -0.0017668535272392337 0.0007318189137065072 -0.0002513863728668455; 0.0012411943468816882 -0.0016639093360780208 0.0015074775524324781; -0.001848696978469547 -0.003749538852654347 0.0029473338004181076; 0.00022428999003400746 0.00024430726667904287 -0.00024993592587083243; -0.0015026681547839027 -0.0006534643477183384 0.0020848292059576744] %
+
+Mass Used: 103.95394196607094 kg
+Launch C3: 104.14238312866736 km²/s²
+||V∞_in||: 5.249015904038854e-5 km/s
diff --git a/archive/ES_0.6099522657894692 b/archive/ES_0.6099522657894692
new file mode 100644
index 0000000..4f47cbd
--- /dev/null
+++ b/archive/ES_0.6099522657894692
@@ -0,0 +1,22 @@
+archive/ES_0.6099522657894692---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T01:12:32.438
+Launch V∞: [5.105636336301099, -8.475120727479611, -1.015956082939769] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.0311157538252299e-7, 2.6039519536807e-8, -3.344016271480586e-8] km/s
+ V∞_out: [1.083282987198814e-7, -2.820471720254683e-8, 1.3117841748594639e-8] km/s
+ time of flight: 1.17352598933978e8 seconds
+ arrival date: 2027-01-09T07:09:10.438
+ thrust profile: [0.8040674179648942 -0.5847953446833526 -0.36631498944970237; 0.4036575153607385 -0.05595485876435686 -0.40137430411775227; 0.08954678783147955 0.0019598004310697656 -0.13944372286838336; 0.15719451356227723 0.025747203677485283 -0.300413914966152; 0.12064692334034922 0.030193976609134317 -0.27515928955048724; 0.07992862271050084 0.016096951186487712 -0.21319227068791546; 0.024430984229267705 0.006652367347097307 -0.07346826055281547; 0.03462397866716282 0.011365658088812338 -0.11269046820777948; 0.0005384857516255453 0.00014864560451054433 -0.0016775063374066285; 0.0016377093360764828 0.0005128656640496648 -0.005496193700450086; 0.00029126115555479183 -0.00010312364986906288 -0.00018218295192775036; 0.00022940837499205158 0.00045944711947071 -0.0008995764081167071; 0.00045406534975154546 -0.0002458650564361215 -0.00020598454879472422; 0.00012489520835574488 0.00010356979667153757 -0.0005089119491434341; 2.114164609731136e-5 0.0003145379679783827 -0.000903831836669761; 0.0005798830538413192 0.0004139139046036139 -0.0010530550164060926; 0.0001223656063359254 0.0005121803842329111 -0.0015454154655744593; 0.00039674053612452414 0.00016248325706632439 -0.0009177054102380897; 0.0001439711377697688 7.43011180985862e-5 -0.0003623138704003687; -4.430053617010326e-5 -7.366558615095166e-5 3.8369500800397366e-5] %
+
+Mass Used: 134.53470713386014 kg
+Launch C3: 98.92736050637497 km²/s²
+||V∞_in||: 1.114822767885827e-7 km/s
diff --git a/archive/ES_0.6099674879639945 b/archive/ES_0.6099674879639945
new file mode 100644
index 0000000..95327ba
--- /dev/null
+++ b/archive/ES_0.6099674879639945
@@ -0,0 +1,22 @@
+archive/ES_0.6099674879639945---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T04:26:27.926
+Launch V∞: [6.868355941648812, -7.236965852786452, -1.4178035391213963] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002509473017442759, 0.014361704291149892, 0.00297855513020153] km/s
+ V∞_out: [0.01407334716251354, -0.00270978796792141, 0.003992735660008248] km/s
+ time of flight: 1.2046577717783831e8 seconds
+ arrival date: 2028-02-29T11:09:24.926
+ thrust profile: [0.6723617295171194 -0.29886392139373885 -0.3239160398777676; 0.21798904738962735 0.009216823195718786 -0.23127267841328644; 0.14212050934527568 0.03629621580565465 -0.23421948967029055; 0.07532013069795115 0.029813498560612953 -0.1693098703502441; 0.04320303596971588 0.02150747455309281 -0.12106890201826453; 0.017563740284206902 0.008968606551837573 -0.059517821629149883; 0.021280553101793418 0.01421546252130412 -0.08407036029342223; 0.03078718986294763 0.0184380797933441 -0.11810310135642565; 0.02440954839965342 0.015146255118606407 -0.09632550996799472; 0.031460516004181246 0.021197617396810725 -0.141613183771836; 0.03505960481060556 0.02249372213068219 -0.11853572060625488; 0.005738683722108295 0.002066313374401332 -0.03720047769772082; 0.0009210504831306909 0.000551421742974076 0.0011176991421318096; 0.0017864270504755562 0.0030340746182078585 -0.003873324933343735; 0.0036851994224643765 -0.005331127741526187 0.0023982360081669842; -0.002946878374639487 0.0037521528565832214 -0.0075042515597157295; -0.005591942318214298 -0.009483594780924316 -0.0076543786548671985; 0.0037780311510431487 -0.01323306078975446 0.006102341276779945; -0.02125126899372959 0.00025202548724962673 -0.0022080056132001355; -0.009159574073971897 0.001011194839248821 -0.007591855954623021] %
+
+Mass Used: 119.20616529309882 kg
+Launch C3: 101.55815497112482 km²/s²
+||V∞_in||: 0.014880450115347867 km/s
diff --git a/archive/ES_0.6101523283580422 b/archive/ES_0.6101523283580422
new file mode 100644
index 0000000..18f7f03
--- /dev/null
+++ b/archive/ES_0.6101523283580422
@@ -0,0 +1,22 @@
+archive/ES_0.6101523283580422---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T06:44:20.208
+Launch V∞: [5.200009448341123, -8.724664108335558, -1.7853438403683561] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002567174936696909, 0.001892614357438595, -4.1461069860305144e-5] km/s
+ V∞_out: [-0.0010508941599171302, 1.4139159050844228e-5, 0.003022357617465739] km/s
+ time of flight: 1.1902069579729517e8 seconds
+ arrival date: 2027-01-31T20:02:35.208
+ thrust profile: [0.4103704973292187 -0.3109453348920484 -0.2523583651123407; 0.10063318540693525 -0.02248754150344318 -0.12207640329206905; 0.07828868198636886 -0.0023988023959391654 -0.14004292492048917; 0.10221938698451676 0.006903013928902229 -0.23219700066766036; 0.09316357977950256 0.011909010172223304 -0.25197086778963806; 0.09045525138806311 0.015805981301226943 -0.2784766534760272; 0.0219712868445156 0.004496180901248233 -0.07985710990660753; 0.003294879606569054 0.0032935347168965047 -0.0056027722771646435; 0.005486921153082192 0.000757556020320425 -0.023520942125846055; 0.0029215873788786518 0.0014251793930889754 -0.00847466208536998; -0.0034584920699797608 0.007605420654549548 -0.01078894498978428; 0.0007670157314603467 -0.0008750790976250942 0.00038577861844548344; 0.0036486492625631 0.001636834961223589 -0.0008192183039701465; 0.001790674239659321 0.0005424684410436659 -0.002540899318069917; 0.006534794938609657 -0.011872151109556228 -0.008752029492438137; 0.013641168124623293 0.0076542145593287494 -0.019782202220290188; 0.0011701075715791962 -0.0014891521045254227 -0.00048668420487169587; -0.0005138601511221715 -0.008634010506035482 -0.005387802189636442; 0.006184950729150128 -0.0018910188505391924 -0.009893213488037483; 0.0085406534067035 0.0028891858265006356 0.004039886391749662] %
+
+Mass Used: 91.48504736671748 kg
+Launch C3: 106.34731469445688 km²/s²
+||V∞_in||: 0.003189685765385275 km/s
diff --git a/archive/ES_0.6102261806390123 b/archive/ES_0.6102261806390123
new file mode 100644
index 0000000..0ce169c
--- /dev/null
+++ b/archive/ES_0.6102261806390123
@@ -0,0 +1,22 @@
+archive/ES_0.6102261806390123---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T04:11:30.566
+Launch V∞: [6.818173249382493, -6.899935509337474, -0.8998919020597711] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.000203834594826883, -0.001331639317571617, 0.00128800180736454] km/s
+ V∞_out: [0.00042861294840794184, 0.0016486177242398601, -0.0007562054979062415] km/s
+ time of flight: 1.2040455960043265e8 seconds
+ arrival date: 2028-02-22T17:54:09.566
+ thrust profile: [0.8930604271658427 -0.37917900533053384 -0.35945483871886497; 0.7323020726346531 0.06282960171728273 -0.6256167094723473; 0.34397430523216377 0.11174050055205194 -0.45386400744064587; 0.16510939737494112 0.0796723534900452 -0.2915489689978123; 0.07895757529887401 0.047965020297634914 -0.1740597031125118; 0.02058328733168109 0.014909302529120434 -0.055291785760170825; 0.010872448054535628 0.009008171469616012 -0.03520516925885512; 0.006202708674572545 0.005210407186332057 -0.018545377471256137; 3.888501897993503e-6 -0.0001153012683397603 -0.004416175974485402; -0.0011808065393654227 0.0016861492371607334 -0.0047299219276190265; 0.0017959928810018266 0.0006460171874986345 -0.005672658506928413; 0.00022400348927053158 0.0031046209288588004 -0.00064387149698104; 0.002049752889403668 0.0011648467179830532 -0.0023856344089679244; 0.0008371924541034071 0.001043819158343319 -0.004963823737946805; -0.004002932213202093 0.003598553125812795 0.0003002995755170433; 0.0007700820452260466 -7.309562361286753e-5 -0.008342278184996062; -0.002300821921597318 -0.006054852536465375 0.0004005326575632557; -0.0033055290334170957 -0.0009598314356263653 0.005344689587149946; -0.0012786967167899214 0.0002049137376518446 0.0016638748164771078; 0.003836340458525269 0.0035552275911713217 -0.0010223080076512394] %
+
+Mass Used: 158.30986617132476 kg
+Launch C3: 94.90640192700394 km²/s²
+||V∞_in||: 0.001863802690717331 km/s
diff --git a/archive/ES_0.6102814020471705 b/archive/ES_0.6102814020471705
new file mode 100644
index 0000000..cd3371a
--- /dev/null
+++ b/archive/ES_0.6102814020471705
@@ -0,0 +1,22 @@
+archive/ES_0.6102814020471705---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-15T23:03:58.854
+Launch V∞: [6.748833281183011, -6.975298121218271, 0.35870741924971916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.571362837208836e-7, 3.29350036427557e-6, -1.9640642311550106e-7] km/s
+ V∞_out: [1.2218585365316583e-6, -2.7075340191075255e-6, 1.504876596111603e-6] km/s
+ time of flight: 1.8749577787472335e8 seconds
+ arrival date: 2029-03-25T01:13:35.854
+ thrust profile: [0.7290363015465763 -0.16649547946913995 -0.10377476558618758; 0.31424235154310975 0.13623246005269085 -0.1516063022879467; 0.20998779089423417 0.17196194621953723 -0.174351314729158; 0.11097391690848354 0.12693589654606469 -0.13402117619656845; 0.0666712962360805 0.0965877987664073 -0.10660004212686562; 0.0518035009622446 0.09098881663211264 -0.10511666070249967; 0.027100241377176544 0.05549202742704175 -0.06813041291496512; 0.0014327583004571606 0.003948793436653997 -0.0044772636029997105; 0.00631904222777057 0.017020778951385967 -0.022174230317173728; -0.000618940884259982 0.0022383581027004586 -0.0015900844150276718; -0.0008368636598012539 -0.0008008979254829182 0.0008069924721025399; -0.0015779960205178 0.0003747454108628238 -0.00012010886984310798; -0.00010116817603197465 0.0015636465994621868 -0.0016999169370357284; 8.375189223660824e-5 0.0009545932030658733 -0.0014344305512523695; 0.007783396370859124 0.002661094443873308 -0.001358229714447163; -0.00040974114212981137 -0.003040085178884467 0.0026630997782431855; -0.0023106681575134325 0.0091342057989337 0.00304308626509603; 0.0006170195961876043 -0.004824526935505307 -0.009979611548676338; 0.0005945933421552045 -0.001525257495952612 -0.014557324166446856; -0.0022240394097180535 0.0035027357176987987 -0.00589938569976111] %
+
+Mass Used: 161.7354366817858 kg
+Launch C3: 94.33020554969939 km²/s²
+||V∞_in||: 3.330869813489935e-6 km/s
diff --git a/archive/ES_0.6102986758630466 b/archive/ES_0.6102986758630466
new file mode 100644
index 0000000..5d35ef2
--- /dev/null
+++ b/archive/ES_0.6102986758630466
@@ -0,0 +1,22 @@
+archive/ES_0.6102986758630466---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T22:42:44.152
+Launch V∞: [7.1839415946069085, -7.04334923487983, -2.340258018189192] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.08082532268683867, -0.0768218703902094, 0.05842868480336358] km/s
+ V∞_out: [0.06493198739220828, -0.10594332592710859, 0.020272164144611853] km/s
+ time of flight: 1.1990174210834546e8 seconds
+ arrival date: 2028-02-20T16:45:06.152
+ thrust profile: [0.41898351069989487 -0.1784189223686859 -0.21870414163053398; 0.17987459979136927 0.012961053661052099 -0.195618537064066; 0.15224238968838377 0.046700643092705725 -0.2529813015410517; 0.11862826325920785 0.0540629694076069 -0.26207605845829945; 0.07739950063889439 0.04268916479790155 -0.21063017752485494; 0.045959253473847536 0.02678290480721076 -0.14516583692289664; 0.012522121572700568 0.008600810811602065 -0.046682441534331154; 0.01099487269973996 0.008321663625153042 -0.04576455375434935; 0.0033631556547646596 0.002810272519759345 -0.010989150665403983; 0.00033052878480927797 0.00027227605192773545 -0.001761100836919925; 0.0016794481116361424 0.00027917398701119106 -0.003421058290091425; 0.0006257882317385122 0.0004122663168056739 -0.0016008766890721917; 0.00036616234335609395 0.00027006629828042555 -0.0017102237222726294; -0.0018381866439588215 0.002346802032953017 -0.0025663702340889705; -0.0002787883825304629 0.0007724081729917848 -0.0022088093311978764; 0.0006927405815235781 -0.0003620311274767536 -0.0013135254469069813; -0.00038348004868758853 0.0009446817116879225 0.0002597311271154417; -0.0006030301242724912 -0.001129310027563659 -3.878340263133479e-5; 0.00010947308759932955 -0.0001291246099070476 -0.0011867392871577186; -0.00039435888179114404 0.001802998520846661 0.0011139521373021] %
+
+Mass Used: 89.6299967599457 kg
+Launch C3: 106.69459287090434 km²/s²
+||V∞_in||: 0.12588980802881758 km/s
diff --git a/archive/ES_0.6103163157079277 b/archive/ES_0.6103163157079277
new file mode 100644
index 0000000..8518520
--- /dev/null
+++ b/archive/ES_0.6103163157079277
@@ -0,0 +1,22 @@
+archive/ES_0.6103163157079277---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T05:11:08.522
+Launch V∞: [6.987930831986175, -7.229322951287226, -1.1935828128373298] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.787228440005132e-6, -4.1467494627304394e-5, 5.491576421221566e-6] km/s
+ V∞_out: [-6.010359496120685e-6, 2.318022373083626e-5, 3.449909517702027e-5] km/s
+ time of flight: 1.177187424301052e8 seconds
+ arrival date: 2028-01-27T16:50:10.522
+ thrust profile: [0.5498646881017623 -0.2463666643687584 -0.26061768082419656; 0.23952398666666488 0.005885994560276317 -0.24583773713218451; 0.1827422993322251 0.04196236554464462 -0.2886073879422915; 0.17104320620364213 0.0635416392062743 -0.3579504131546097; 0.053238869748760305 0.023814184897150033 -0.14301998751355635; 0.06308368476468483 0.03198802792429159 -0.1915629215017643; 0.015113023903571663 0.0083202903136098 -0.05277873926260069; 0.01484798834358603 0.007924903342209438 -0.05927922500016291; 0.007212807179343726 0.003915573784672463 -0.02683951948643246; 0.031498836113456795 0.019178248657413226 -0.12811392580067352; 0.004621001626300745 0.0036096683798408336 -0.0202446703318647; 0.0010205621649511357 0.000428423527638451 -0.004421585908375909; 0.0003677124614705966 0.0005021770314871299 -0.002066843461400936; 0.0017642794594645377 0.0004999742609476325 -0.002660642383700885; 0.0011006422276623085 0.0006682783768146059 -0.004132851268968936; -0.0005916507111666997 -0.000876371451790085 -0.0018103276523876426; -0.003127210587197995 0.00019700310928755772 0.00024827628332740014; 0.0013581561891740767 0.0013166156565810705 -0.0032201497255307347; -0.0022448964028413945 0.0013886663681483367 0.0024438386072784075; 0.0001926965817305624 0.00010456666421735804 -0.001374690565858737] %
+
+Mass Used: 114.00862412247943 kg
+Launch C3: 102.51892757773192 km²/s²
+||V∞_in||: 4.20006383464873e-5 km/s
diff --git a/archive/ES_0.6104749169195323 b/archive/ES_0.6104749169195323
new file mode 100644
index 0000000..1835902
--- /dev/null
+++ b/archive/ES_0.6104749169195323
@@ -0,0 +1,22 @@
+archive/ES_0.6104749169195323---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T18:10:24.974
+Launch V∞: [5.271838468431311, -8.637700702789552, -1.472134409648316] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.24385449179552618, 0.07046641844524318, -0.15755353384607787] km/s
+ V∞_out: [0.20443720003027713, 0.0893130437403247, 0.1991143743811737] km/s
+ time of flight: 1.1766290957476273e8 seconds
+ arrival date: 2027-01-14T14:18:53.974
+ thrust profile: [0.45207813249894385 -0.3335573089115966 -0.26748552176214085; 0.20756370081689535 -0.041390445072239844 -0.24083241060815028; 0.14527531077703648 6.131284174352663e-5 -0.2487080810845082; 0.10361589640186177 0.011454487744260004 -0.2300164263555721; 0.05309432303651473 0.009918768638992766 -0.14360214689821504; 0.040604227730093596 0.009659470516768912 -0.12143858168270942; 0.0804786918880946 0.020717305771988322 -0.2612530827326141; 0.02056469096414211 0.006510249837995999 -0.07261472624368932; 0.00624143405457918 0.001970353176734452 -0.024774769918525112; 0.004670062043064294 0.0013827375480596 -0.02025432810418868; 0.000973645841399585 -0.00032660306894699174 -0.00041199717301539085; 0.00013452125601980542 -9.885466043426213e-6 0.0006852863386448593; -0.0008138452663007082 0.00044837147792137737 -0.000997714289194004; -0.0013313534921328037 -0.0006290199232054067 0.0012332784826954927; -0.0019975600347426695 -9.28327428647933e-5 3.627218835371447e-5; -0.002024635173049751 -0.0003102587958342066 -0.0016254424363204307; 0.0023770288635043694 -0.00016458235642021412 0.0015567115173562441; 0.0014315321711782189 -0.0022890240599584204 -0.003109675178069808; -0.002071989926283146 0.001140047797876443 -0.0010796167964180216; 0.0005611220335221212 0.0007617734127800094 -0.0006374154284680443] %
+
+Mass Used: 102.23295480785646 kg
+Launch C3: 104.56933398827391 km²/s²
+||V∞_in||: 0.29875348587881223 km/s
diff --git a/archive/ES_0.6106586329967547 b/archive/ES_0.6106586329967547
new file mode 100644
index 0000000..73c5064
--- /dev/null
+++ b/archive/ES_0.6106586329967547
@@ -0,0 +1,22 @@
+archive/ES_0.6106586329967547---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-11T14:28:10.526
+Launch V∞: [5.858969384585324, -7.633503926892442, -0.3893853130376541] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.3450017067365225e-6, -1.673648546475885e-6, -3.271392444982287e-6] km/s
+ V∞_out: [2.2061847021507362e-6, -3.0137355522946335e-6, 3.2767488220673643e-6] km/s
+ time of flight: 1.539853877548489e8 seconds
+ arrival date: 2028-02-26T20:11:17.526
+ thrust profile: [0.7058235426607004 -0.3461976997226757 -0.18131529785982617; 0.5611505475488603 0.07430865056082324 -0.344863231443956; 0.36273073955349616 0.15260014902660562 -0.3470769425446846; 0.22486767817760098 0.1396859479105632 -0.2889352285352831; 0.10098665526169939 0.07918759034419014 -0.16383310878723292; 0.03780589913817085 0.035818210476941253 -0.07460480832494136; 0.0077430908809969735 0.008534870916754598 -0.01929298572294412; 0.004352284228941166 0.004305290897372293 -0.013551934024257849; 0.0018985200111739044 0.0025923241783661556 -0.0069368005459326375; 0.004315578543490248 0.007227259027239016 -0.019408749864824024; 0.0032489032358142007 0.0044952129270026155 -0.010563396907208901; 0.001475536306567392 0.00304409339584404 -0.000795055475248471; -0.0017219482398607264 0.002030616555024724 -0.00010029413942724179; 0.0007217585938557734 0.0006394496483559014 -0.0024005283580308353; 0.002645454192033702 0.0005294225549888293 -0.0024443058998975054; 0.0011395867997151389 -0.0017406634845500706 -0.005453440283693891; -0.0009530918448540226 0.0005230145930268965 -0.0008579301834266096; 0.0021116228847229057 0.005351469267282982 -0.005817557001895195; -0.0010496776351643223 0.0023774425794176805 0.0028138443730927813; 0.0001329349762662032 8.634461703158286e-5 -0.0003012112731855621] %
+
+Mass Used: 171.39617381804783 kg
+Launch C3: 92.74952537339989 km²/s²
+||V∞_in||: 4.9691190772890805e-6 km/s
diff --git a/archive/ES_0.6106862560555789 b/archive/ES_0.6106862560555789
new file mode 100644
index 0000000..42a6f47
--- /dev/null
+++ b/archive/ES_0.6106862560555789
@@ -0,0 +1,22 @@
+archive/ES_0.6106862560555789---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T17:22:14.184
+Launch V∞: [7.038454888426516, -7.401652678477544, -2.0824946491905227] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0027536636766527615, 0.016444117501673655, 0.0030738557199614185] km/s
+ V∞_out: [0.016127536307716014, -0.0030987911122724045, 0.004214551270082276] km/s
+ time of flight: 1.1677714408958614e8 seconds
+ arrival date: 2028-01-19T07:27:58.184
+ thrust profile: [0.32515443469504984 -0.15294217412079358 -0.19037561280941187; 0.16550128516485527 -0.002190747652733339 -0.20574819535996564; 0.11511553840960144 0.02059730155449899 -0.22111089378501708; 0.07971267090016179 0.02297607191646287 -0.2043245614197608; 0.05228738720019107 0.01891952603230751 -0.16594969130304127; 0.036202556913980354 0.015116694879419842 -0.1357165158870325; 0.011526525690262576 0.005131135654795633 -0.05091874828636382; 0.012495363763497545 0.005704794799309889 -0.055945346668598926; 0.0035702668719048893 0.0019963726283890974 -0.017438561580293215; 0.014503184906022315 0.007197478622457862 -0.07535697702478397; 0.003238821243998986 0.00185068580783851 -0.019083267019679623; 0.0001265846779097358 1.5218948630574486e-5 -0.0006293457861797228; 6.47054014380042e-5 -0.0005213660107446329 -0.00044736627183192967; -0.00021716639455476026 0.0002383523674257599 -0.0012883628248584636; -0.00021986657132196954 0.00014201137872660365 -0.001197004926333302; -0.00011395184047101174 -1.0878974490837823e-5 9.829366567683142e-5; 0.0003577579165408595 -4.868391287696927e-7 -0.002195586870510847; 0.0003563939817074925 0.0011396398871618282 0.0001546627419028686; -5.414098665946677e-5 -8.201473352378966e-6 0.00023595874361729023; 0.0005069516576732907 -9.518644934140556e-5 0.0004979203344932029] %
+
+Mass Used: 78.61091967154834 kg
+Launch C3: 108.66109355313607 km²/s²
+||V∞_in||: 0.016954063024540937 km/s
diff --git a/archive/ES_0.6106948250634456 b/archive/ES_0.6106948250634456
new file mode 100644
index 0000000..12e2694
--- /dev/null
+++ b/archive/ES_0.6106948250634456
@@ -0,0 +1,22 @@
+archive/ES_0.6106948250634456---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:37:11.820
+Launch V∞: [7.051685348801974, -7.4004623549177495, -2.0946515773180314] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.11637748024041863, 0.11859443775038199, -0.09019761441935017] km/s
+ V∞_out: [-0.09728005048591104, 0.15945304050017337, -0.029069631745967297] km/s
+ time of flight: 1.1669535202185242e8 seconds
+ arrival date: 2028-01-18T10:59:43.820
+ thrust profile: [0.34071013818404283 -0.1626388583646131 -0.20531399757783358; 0.1349385787225787 -0.002586888627278459 -0.1728195547405391; 0.09612023869569214 0.016509554001287733 -0.19051656048393825; 0.0748140869736537 0.020895879485923505 -0.19758108935900395; 0.05266829990505869 0.018294331480524288 -0.1703772766634782; 0.03133702830660905 0.012321256272020875 -0.11891757383114163; 0.018195499553299178 0.007809987048979347 -0.07831599313532213; 0.02289916727728894 0.010909068811044566 -0.10925897356220246; 0.015435051858104272 0.007420063640693044 -0.07831078019798089; 0.0011095525957952892 0.0005217872426770995 -0.006124747301153985; 0.00020841098029929285 0.00030380074224339165 -0.0015191895734427282; 0.00043932492455931295 -0.00017161702312655129 -0.0008107211513309212; 5.915486665299726e-5 -3.6341039581860206e-5 -0.0009912883705061098; 0.00012629996443065065 -3.8693807110864434e-5 -0.0008795457970097724; 0.0001313322113710537 0.0005962322994822497 -0.0004732346097414791; 4.156713800461284e-5 -1.732211435168747e-5 -0.0003952695051732711; 0.00013283279969156022 -0.00013359255082958304 -0.0002030342803209399; 3.6750789694880924e-5 6.88377270489166e-5 -0.00011589692593879427; -0.00011405781199061801 -3.5064519819540245e-5 0.00024062790289702644; -0.00038949901092148525 0.00011854116084625201 -0.0004326607291232744] %
+
+Mass Used: 77.34002766737922 kg
+Launch C3: 108.88067455542411 km²/s²
+||V∞_in||: 0.18906075272086492 km/s
diff --git a/archive/ES_0.6107672569126363 b/archive/ES_0.6107672569126363
new file mode 100644
index 0000000..e41a0d7
--- /dev/null
+++ b/archive/ES_0.6107672569126363
@@ -0,0 +1,22 @@
+archive/ES_0.6107672569126363---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T20:08:30.451
+Launch V∞: [6.992300498175121, -7.32347805404374, -1.7949241898258101] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0069094774355442055, 0.044098786601998424, 0.007901336382469757] km/s
+ V∞_out: [0.04270727893750867, -0.008622023794592232, 0.012525257412429963] km/s
+ time of flight: 1.1660018727700119e8 seconds
+ arrival date: 2028-01-16T09:04:57.451
+ thrust profile: [0.5410505009279586 -0.24483850616942135 -0.2812457301420471; 0.1267185991897189 -0.0015828235843637656 -0.1478483115420268; 0.1443311267588557 0.027829112466592174 -0.2513730711738802; 0.09589294959983195 0.028603876985958922 -0.22126079745909244; 0.09585500267334676 0.03671761123729378 -0.26930352464831786; 0.021733451232939262 0.007557947486568485 -0.07707367162549822; 0.012074536247480713 0.00514366040331456 -0.048966307548620434; 0.020943444358905647 0.00985666720112158 -0.08863709349582752; 0.026714083097047786 0.012144985933458375 -0.11977250474359431; -0.00011064837320198654 0.0008788219231309264 -0.005420112326031538; 0.002185778726562689 0.0013228159733247574 -0.005909492515786661; 0.0021348983215040145 -0.00040108833701051126 -0.0002316647264039829; 0.00031187573779370523 0.0005399127602229215 -0.0016952664974884896; 0.003129405220704368 0.0001993738134064087 -0.0004084247949279966; 0.0009305099305229369 0.0002998084568987607 -0.004566897886105795; -0.0006830716819182392 -0.0010075742433263042 -0.0021675424892472817; -0.0002826916367424919 -0.0020343884162151407 0.0012388162565392952; 0.005440536619575286 0.0010343322780797962 -0.0012845226814754572; 0.0001377478264578467 -0.0008340771206100195 0.0013556122433887468; -0.0016258872014961378 0.002398230872243044 -0.004338603153818813] %
+
+Mass Used: 95.70225857771311 kg
+Launch C3: 105.74734991206216 km²/s²
+||V∞_in||: 0.04533072881423627 km/s
diff --git a/archive/ES_0.6109058294115555 b/archive/ES_0.6109058294115555
new file mode 100644
index 0000000..fa9bf0e
--- /dev/null
+++ b/archive/ES_0.6109058294115555
@@ -0,0 +1,22 @@
+archive/ES_0.6109058294115555---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T23:52:55.228
+Launch V∞: [6.947432881662912, -7.442249488073751, -1.9100141215000375] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0007750762362078995, -0.004739529294009297, 0.004834575404903192] km/s
+ V∞_out: [0.003318241218406067, 0.004703991117983363, -0.003646652506880867] km/s
+ time of flight: 1.1732287836305524e8 seconds
+ arrival date: 2028-01-25T21:34:13.228
+ thrust profile: [0.3459903158539925 -0.16517571311009596 -0.1972968191052418; 0.20993297172079153 -0.005707395849821104 -0.2523265576290467; 0.15572949625280874 0.024458731942898743 -0.28872978716019726; 0.11542631342103396 0.029818102413813257 -0.28502912292690263; 0.05635737393123275 0.018504348624670857 -0.1735623627382708; 0.030268885912069752 0.011448262281794878 -0.11044719767943793; 0.01076011905824854 0.00433860164002126 -0.04686395075088573; -0.0007488940586422763 0.00041349065253223796 -0.00887587151095824; 0.0016216056168053812 0.0009333284354740173 -0.011147981485837143; 0.0011424909458689501 0.001833715662205976 -0.005689068697411504; 0.00011437779703934401 -0.0012479608919720789 -0.004614258900232536; -0.0001955740072723961 0.0007888499893649128 -0.0033861029113131345; 0.003451985254969139 0.0056845091862055535 -0.001087198000263356; 0.0007606061898229881 -0.000784263756653344 0.002685018914322629; -0.0003707888424722117 -0.00021080780237651086 0.000662374180304709; 0.002720212217192216 -0.0035583855840124667 -0.014804049336089396; -0.003685648097391904 0.013454602275136453 -0.0016537352818202533; -0.0032466104928402144 -0.005253437285299117 -0.013183253982929471; 0.0017279454234950672 -0.00031151668687405006 0.011837998381017793; -0.001926706342286228 0.004086953206684936 0.011846729268384981] %
+
+Mass Used: 86.79481329187956 kg
+Launch C3: 107.3020550322746 km²/s²
+||V∞_in||: 0.00681446993143277 km/s
diff --git a/archive/ES_0.6114786097013363 b/archive/ES_0.6114786097013363
new file mode 100644
index 0000000..625b790
--- /dev/null
+++ b/archive/ES_0.6114786097013363
@@ -0,0 +1,22 @@
+archive/ES_0.6114786097013363---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:00:40.778
+Launch V∞: [6.953424136513991, -7.4390977364673185, -1.6727374781545443] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004589872116713477, -0.0002429276598402826, -0.0011274066812662356] km/s
+ V∞_out: [-0.0005998737406470219, -0.001086150622292008, -3.4994938130208056e-5] km/s
+ time of flight: 1.1553077999044529e8 seconds
+ arrival date: 2028-01-04T21:53:39.778
+ thrust profile: [0.4508485793598639 -0.2176127512103883 -0.24944461062735074; 0.18012303341479144 -0.006055747990662437 -0.21263659794931117; 0.16511906967252551 0.025536661400275367 -0.3009761231742261; 0.12575871732609473 0.032648987918155264 -0.305735265299572; 0.0655952951903353 0.020567285644187108 -0.1953293757911294; 0.04877812397687888 0.018381335202039658 -0.17505547416382555; 0.006453175597608125 0.0025080638429275885 -0.0262833643197896; 0.003226071541833782 0.001275575883190813 -0.014376037005499373; 0.002489380082572425 0.0010196405345356905 -0.01197456055567128; 0.0008845993542564295 0.00030387790938639223 -0.0045015398250993046; 0.005459781983879778 0.0025242869191955987 -0.02840853802992789; 0.0005020864692912417 5.788807743954867e-5 -0.0025145895531604855; 0.00023101963969061667 -0.0008560876082369906 -0.0014178591198170903; 0.00013300288897843742 0.00010234819292520873 -0.0006559873362999457; 0.0011151188103203458 -0.0002214112925572105 -0.0016941648042166709; 0.0003624984230108854 9.197337464656352e-5 -0.0012063533414792722; 2.7386231671402573e-5 0.001296964586287346 -2.047914485765875e-5; -0.000150887871707942 -8.169045963890936e-5 0.0006935718908139021; -0.0010050506158637944 0.0015415741324672108 -0.0003670274601037237; 7.89255724815269e-6 4.1138657879940654e-5 0.0002025857034041507] %
+
+Mass Used: 92.20976866777619 kg
+Launch C3: 106.48833302579135 km²/s²
+||V∞_in||: 0.0012412610254725078 km/s
diff --git a/archive/ES_0.6115574152153169 b/archive/ES_0.6115574152153169
new file mode 100644
index 0000000..7f35ba1
--- /dev/null
+++ b/archive/ES_0.6115574152153169
@@ -0,0 +1,22 @@
+archive/ES_0.6115574152153169---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T12:31:32.336
+Launch V∞: [5.076985182092764, -8.628263228201353, -1.3785756466322183] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.013146021900010333, 0.010841638531466908, -0.0002101527496183567] km/s
+ V∞_out: [-0.005318206540586729, 7.72191813070247e-5, 0.01619071582089726] km/s
+ time of flight: 1.1781738371475771e8 seconds
+ arrival date: 2027-01-16T03:34:35.336
+ thrust profile: [0.46435955126762446 -0.33881368170202664 -0.2514071711194702; 0.5705569910069326 -0.10441155690064116 -0.5223144390514709; 0.09379847735905224 0.00041498014852522013 -0.1527665361570952; 0.11707214850067624 0.011157737708456874 -0.24340054815329046; 0.10406288313135471 0.02135583047371533 -0.24547427754672646; 0.04085073024392603 0.009999265398340744 -0.11588787876740743; 0.04057749768893497 0.01123393243418854 -0.12686437599079417; 0.006040783404295965 0.0016779205174168156 -0.021376494720500287; 0.0025912661619068183 -0.0005587430315417597 -0.005567335859413782; 0.00026588461206478544 -0.0012920863355615519 -0.002958636634628788; 0.0013642364069495498 0.001034552773662024 -0.002668386687363128; 0.00018535717087964624 -0.0006189810675979805 -0.0014916183447154165; 0.0009957533822266909 0.007695765193074151 0.0009904942538402775; -0.004781048710950915 0.007642453439411653 -0.005590456819588641; -0.0006589310040899848 0.010017820363641475 0.0009384095765926042; 0.00011728197100930164 -0.0007912808769223429 0.000484739450347045; -0.009304486679922848 -0.003609612136748302 -0.013315446725854637; 0.013344567658411324 -0.011995092544280831 -0.007545011963484926; -0.005431227914288155 -0.004985979676832375 0.00721416972973074; 0.0050241991116936596 -0.0037897426230343663 0.014645232618642343] %
+
+Mass Used: 117.76512623898634 kg
+Launch C3: 102.12317568780857 km²/s²
+||V∞_in||: 0.017041220086035837 km/s
diff --git a/archive/ES_0.6117031976770865 b/archive/ES_0.6117031976770865
new file mode 100644
index 0000000..fd78656
--- /dev/null
+++ b/archive/ES_0.6117031976770865
@@ -0,0 +1,22 @@
+archive/ES_0.6117031976770865---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T06:40:24.603
+Launch V∞: [6.932669325118014, -7.307266158171279, -1.477008196376694] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.23856759833984e-6, 2.448468323542552e-6, -1.361762141523318e-7] km/s
+ V∞_out: [-2.5594105197702974e-6, 1.6157645302153212e-6, 1.3641629039301332e-6] km/s
+ time of flight: 1.1488057812312019e8 seconds
+ arrival date: 2027-12-26T21:56:42.603
+ thrust profile: [0.6775094985906326 -0.31907950072953395 -0.3607248459798086; 0.22192135489295534 -0.0025584934336246373 -0.2522110876595947; 0.17421537591527148 0.0319199183889729 -0.3011096153456628; 0.1432691995235557 0.04219389900156774 -0.32411870179485147; 0.0937578972377296 0.0347093610171688 -0.2606982146537726; 0.03383440805636428 0.014619557454614442 -0.11411920526799894; 0.013199316821996864 0.0060626918479108425 -0.05306320803004519; 0.0064716675251982525 0.003191931342110589 -0.02799733041203152; 0.0024580375710733264 0.0012800927922117873 -0.010432364478495217; 0.0011199035248172875 0.00019652263577416275 -0.004570878299853772; 0.0005227786459333767 -0.00023896326662780883 -0.0010820913081097388; 0.0010130980182538468 0.00045308348063577956 -0.004353085315338876; -1.2144122817314869e-5 -2.2785326550497925e-5 -0.00024657374833861366; 0.0005599245306924041 0.00034342812304793133 -0.0015769716092334754; 0.0008591686869920587 0.0011357431427965329 -0.0009979583178779151; 0.0005959163476833401 7.183541294379533e-5 -0.0006158034093282677; -0.00016500053936515432 -0.00011651496733629154 -0.0006569527849975409; -3.408421297069751e-5 -0.0005674442224085288 0.00016745976923649258; -0.0002169267559905127 0.0001341579329568613 -0.00013297025557525448; -0.0007242731536023833 -0.0004895691196655304 0.00037460396211793853] %
+
+Mass Used: 109.08942126521742 kg
+Launch C3: 103.63959588995144 km²/s²
+||V∞_in||: 3.320350280471796e-6 km/s
diff --git a/archive/ES_0.6117213705369561 b/archive/ES_0.6117213705369561
new file mode 100644
index 0000000..7eee258
--- /dev/null
+++ b/archive/ES_0.6117213705369561
@@ -0,0 +1,22 @@
+archive/ES_0.6117213705369561---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T17:39:45.120
+Launch V∞: [8.032916681693266, -5.88204568642774, 0.11369629500124487] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.4944540877267257e-10, 3.7770652204567785e-9, -2.03375716071431e-9] km/s
+ V∞_out: [1.9656694366437923e-9, 3.8982999126018485e-9, 1.009071005691834e-10] km/s
+ time of flight: 1.8283850075421798e8 seconds
+ arrival date: 2030-02-28T22:08:05.120
+ thrust profile: [0.13841724152901114 -0.02063518782232371 -0.03470158580348169; 0.051945990853507915 0.015807907701595007 -0.027632001879158846; 0.03738427405624033 0.019491486436448366 -0.04308529150014944; 0.0483371890483239 0.026406941044061927 -0.0870393987855877; 0.028569517321018964 0.031082483565284112 -0.06401495803224416; 0.05455144305427673 0.010540407493897064 -0.08183275463200856; 0.021885127070835748 0.007688399112402626 -0.03666878600772322; 0.01770604902073007 0.024753259805852017 -0.028547607944822483; -0.0065641744227252705 0.01875142749869436 -0.005242632994522949; 0.003248885949188068 0.01804757635326809 -0.09283984463316443; 0.0016598095972677265 0.021201412459267852 -0.08726595920349162; -0.008420915034377884 0.01616670619779939 -0.06120540207516184; 0.006714422578568971 0.008157247211620101 -0.06953340684631394; -0.014749024821016456 0.005760653969711521 0.0015468437319235712; -0.0371889494514954 0.0036631171379771796 -0.08724051436071775; 0.07719708408590266 -0.03501710194976123 -0.14438050957254692; -0.21286225818556037 0.02421643966537354 -0.08005228338981252; -0.16688004759944963 0.09277039450297639 -0.011317365265107083; -8.800220315306837e-5 -0.001998979753387732 0.001011633150205471; 0.08964873165705384 -0.11873589931950987 -0.11899646573250612] %
+
+Mass Used: 135.36328976126288 kg
+Launch C3: 99.13913871974616 km²/s²
+||V∞_in||: 4.3040099862864215e-9 km/s
diff --git a/archive/ES_0.611873444138075 b/archive/ES_0.611873444138075
new file mode 100644
index 0000000..61cfc8b
--- /dev/null
+++ b/archive/ES_0.611873444138075
@@ -0,0 +1,22 @@
+archive/ES_0.611873444138075---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T12:00:15.457
+Launch V∞: [7.308024176492567, -6.628260629496219, -2.9795168331093094] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.315626520497783e-7, 9.349483787102037e-7, -1.6120912631285965e-6] km/s
+ V∞_out: [-8.724873415192694e-7, -1.7272890837299536e-6, -5.049363814171187e-8] km/s
+ time of flight: 1.4081468850285977e8 seconds
+ arrival date: 2028-10-19T07:11:43.457
+ thrust profile: [0.2218396878828242 -0.06737600508240285 -0.10034181206476024; 0.14199628156531557 0.03548061026264634 -0.14689296058453946; 0.11667929875276183 0.06416972360018061 -0.19459211373327; 0.09017210221016432 0.06978105798042981 -0.20864647610183829; 0.0711405370318369 0.0677151685592068 -0.20768777075586056; 0.04719636336884134 0.05285505145602351 -0.17042869663204105; 0.026174038233550304 0.03276252383247709 -0.11255669860839608; 0.009983982764668149 0.013226917298970877 -0.05116486971039365; 0.0043448667665824964 0.00013517980475511067 -0.001855050358878224; 0.001551964828611808 0.016969603797770048 -0.021292295631394315; -0.0010187375092880367 -0.0032257045990007993 0.001217606814604272; -4.376780711467593e-5 -0.0011184940242701313 -0.006588320996507893; -0.005240949452821532 0.01762073400509557 -0.005779427916423687; -0.004735639784935898 0.0068131862418123286 0.0033717920290136207; -0.0001399758724866827 -0.0006509718854854913 0.0062973845033944395; -0.0024319903412072176 -0.014631678759147938 -0.020262892868435925; -0.0018384283614997275 -0.009141646304461997 2.1309610839973393e-5; -0.006974323849672297 -0.0013027851117255007 0.008682478234311225; 0.00040708355997499626 0.0005191015611695905 -0.006074493452205319; 0.005229649925548788 0.017890167124590677 -0.024066659363048644] %
+
+Mass Used: 94.24398627060555 kg
+Launch C3: 106.21857689551119 km²/s²
+||V∞_in||: 1.9379178425729473e-6 km/s
diff --git a/archive/ES_0.6120836180743843 b/archive/ES_0.6120836180743843
new file mode 100644
index 0000000..8cd7cca
--- /dev/null
+++ b/archive/ES_0.6120836180743843
@@ -0,0 +1,22 @@
+archive/ES_0.6120836180743843---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:57:59.250
+Launch V∞: [7.658084142853147, -6.321895002379468, -0.012279562350438818] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.416953915773279e-6, 2.9535490233994052e-5, -0.0008190428696605087] km/s
+ V∞_out: [-3.112938940837806e-5, 0.0008189252900581209, -8.579064548566166e-6] km/s
+ time of flight: 1.7380415359254447e8 seconds
+ arrival date: 2029-11-16T15:53:52.250
+ thrust profile: [0.24394615652207832 -0.03735924756004142 -0.11213244794295354; 0.048275231233777346 0.013177250736391206 -0.05240161130839063; 0.03810218932135369 0.013056490859728343 -0.08916649785016366; 0.031299006502301455 0.018802427513464268 -0.12873668457403367; 0.03129853340991558 0.019413183782137567 -0.13316582624324988; 0.02694366199488546 0.017520992586301347 -0.13890571306861116; 0.015812232522190595 0.011898553125818015 -0.10235772173251126; 0.003749841813251123 0.011542566405946822 -0.09076824467588501; -0.026524760476139452 -0.0016015316521026286 -0.06542527979696014; 0.0030663799085280286 0.001441576675446463 -0.032972444139136706; -0.004169122454652547 0.0007274365784344984 -0.0030381686493449155; 0.011486613304611145 0.01063733104031456 -0.04905447680796658; 0.016507742158845325 0.004671347730870878 -0.010918637145078928; 0.008792752430269155 -0.00016776068697985327 0.030838201522367686; 0.05054275017368446 0.06613596458139412 -0.04332568126754463; 0.15266395894827237 -0.027137138802308572 0.07530745950523841; -0.02416578706645786 0.02319681208682423 0.05486211073869489; -0.019839949514823197 -0.00010165998160619666 0.0348083988233716; -0.16870517490481277 -0.016450310383649504 -0.017592738620180157; 0.045183053774494115 -0.0204737031490481 -0.1945664928752513] %
+
+Mass Used: 138.85645472472697 kg
+Launch C3: 98.61275994778082 km²/s²
+||V∞_in||: 0.000819587138141502 km/s
diff --git a/archive/ES_0.612199583758607 b/archive/ES_0.612199583758607
new file mode 100644
index 0000000..6fc1c7b
--- /dev/null
+++ b/archive/ES_0.612199583758607
@@ -0,0 +1,22 @@
+archive/ES_0.612199583758607---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T11:22:31.631
+Launch V∞: [6.919061800333212, -7.332887085108811, -1.4653451306298764] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0030714473399989853, 0.003845386902965003, 0.0021994559263211217] km/s
+ V∞_out: [0.002238009689400683, -0.0028561631576993164, 0.00398612193585256] km/s
+ time of flight: 1.1492781701084149e8 seconds
+ arrival date: 2027-12-27T15:46:08.631
+ thrust profile: [0.6607084374637039 -0.3070745333357583 -0.339984398260612; 0.23463162329654896 3.225592225533362e-5 -0.2626126567320814; 0.13722609540841296 0.02708119265431969 -0.23702185212420857; 0.17084458027092722 0.053513088352498704 -0.37512976058689995; 0.07921615035403531 0.031872473894395 -0.22241541149515287; 0.02524492160609009 0.010946336527918916 -0.08257549496992418; 0.026015996357581093 0.011313862175358127 -0.0894583519951123; 0.00829881506816444 0.004257061282224452 -0.034426944762492855; 0.010563192154586534 0.005621434296751198 -0.04681335022197253; 0.003476171611083488 0.001997252459391464 -0.016176686953002752; 0.0003817151697072379 0.00016353388235385805 -0.0013374325946653965; -0.00014265247235865407 0.0001506340363249474 0.0004443990779705211; 0.00014745772294138095 0.0002455647381329395 -0.0007798443692708144; 0.00014676566764318394 0.00040952615071789943 -0.0009429526905759503; -0.0006113533634815749 -0.000779879919779515 -0.001083844548632067; 2.0073299068381668e-5 4.357999488916245e-5 -0.00030045143616672364; -0.0005831945217532682 0.00021631977525523785 -0.000652022428701424; 0.0009218129486090172 -0.00092614459622695 -0.0017798920740086013; -2.797203443690146e-5 0.0002981086167597837 -0.0006034656328370205; 0.0004065513718315846 0.0005883895515099833 -0.0005207608959198263] %
+
+Mass Used: 108.78018200043653 kg
+Launch C3: 103.79188555164656 km²/s²
+||V∞_in||: 0.0053905839727909554 km/s
diff --git a/archive/ES_0.612226016818451 b/archive/ES_0.612226016818451
new file mode 100644
index 0000000..e9dba59
--- /dev/null
+++ b/archive/ES_0.612226016818451
@@ -0,0 +1,22 @@
+archive/ES_0.612226016818451---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T22:23:46.068
+Launch V∞: [7.012075416874902, -7.286948315801661, -1.3357696211950443] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.018189566225946856, 0.11516757667426948, 0.02117264427658696] km/s
+ V∞_out: [0.11192015601017768, -0.021305704763777616, 0.03253727516688339] km/s
+ time of flight: 1.1666382249972408e8 seconds
+ arrival date: 2028-01-16T05:00:48.068
+ thrust profile: [0.5612084798862934 -0.250230774207382 -0.2599014011470888; 0.16371031286568322 0.00774981675345332 -0.17947802852717198; 0.10472020911841169 0.02713524765059542 -0.1774433350498336; 0.12120368401277715 0.047410453175901986 -0.2592675196098854; 0.054626696692870014 0.026155676842724684 -0.16040614164042488; 0.08541687845153773 0.05118449443947083 -0.2606795581733406; 0.046528845821193016 0.030881647025339545 -0.17351400445346998; 0.028429872741722657 0.02134329991279772 -0.1130629571525591; 0.015956258326999262 0.01007209916150333 -0.06785191990752151; 0.014228850681249051 0.008383875610673634 -0.05619906067942411; -0.000378449928263742 0.00017919554288822965 -0.0009622136478328012; 0.0006005518552596429 -0.0020798298862710206 -0.0014209203509601082; -0.0004839724706610578 0.0005693608914803434 0.00035884979677848353; -6.81940944575872e-5 -0.00014091006505823533 -0.0010742728524634425; 0.0008016644950075123 0.00011745902487644101 0.002849405718642582; -0.0022485933098003383 0.001080385907406345 0.001283836483472699; -0.00017963761367975793 0.0012529701244243035 0.0036620030785389623; -0.0008501106795456876 -0.000675771273180092 0.00040785119485013395; 0.0030516085235812256 -0.000776230028068637 0.0015567812490662667; -0.0001728686678901037 0.00013356616537727218 0.0011733544551206449] %
+
+Mass Used: 107.28728192978042 kg
+Launch C3: 104.05309789001355 km²/s²
+||V∞_in||: 0.11850194893829695 km/s
diff --git a/archive/ES_0.6122427338364573 b/archive/ES_0.6122427338364573
new file mode 100644
index 0000000..de4ee0b
--- /dev/null
+++ b/archive/ES_0.6122427338364573
@@ -0,0 +1,22 @@
+archive/ES_0.6122427338364573---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T13:11:18.836
+Launch V∞: [5.214397604950424, -8.51687335131269, -1.1937157814072734] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.4593313740899503, 0.30386226506842423, -0.2925294788686496] km/s
+ V∞_out: [0.3808200410323478, -0.37420377615480394, 0.32405056733923715] km/s
+ time of flight: 1.2684259189374132e8 seconds
+ arrival date: 2027-04-30T15:14:29.836
+ thrust profile: [0.368742406130296 -0.26304698154166656 -0.20494771891991445; 0.19386326017436653 -0.03527120741629748 -0.21905854301102456; 0.16803469238517296 0.0026024440413413277 -0.2843156466761935; 0.14045264726621748 0.017210132335311424 -0.3094798615465888; 0.07908826144258034 0.013345075183631294 -0.21271768536806104; 0.03139824469520224 0.0044549280454465314 -0.0944781838002854; 0.031921133045712015 0.005917865524962546 -0.107880321736629; 0.01585798099153281 0.0011900302812390701 -0.06401383454311847; -0.0011515059177495883 -0.0007321437660087481 -0.02629001366727238; 0.007537187541984683 0.0004878502375764652 -0.025403302588704928; 0.01594752637585167 0.005679229780403849 -0.02991781157508339; 0.06244839695928571 0.04147719603413458 -0.02813340802700682; 0.0020063534033125598 -0.009330524127720053 -0.011383601274718783; -0.016200327599442406 0.019618402946950438 -0.010727084799838593; 0.009931335357004472 0.005454758158024322 -0.01312109954364298; 0.006620871483731237 0.02568921430169304 0.009990978858568146; -0.028561913443214158 -0.02394566903717996 0.023884886161704026; -0.011921735279354487 -0.014693406989596808 0.025081110070875677; 0.003596940256067654 -0.005082746759749567 0.020193940964661088; 0.12742157551203165 -0.025960485505756817 -0.05022612870157567] %
+
+Mass Used: 124.22967279157001 kg
+Launch C3: 101.15203143159374 km²/s²
+||V∞_in||: 0.6236113239535014 km/s
diff --git a/archive/ES_0.6123629886298775 b/archive/ES_0.6123629886298775
new file mode 100644
index 0000000..bf01630
--- /dev/null
+++ b/archive/ES_0.6123629886298775
@@ -0,0 +1,22 @@
+archive/ES_0.6123629886298775---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T23:01:35.712
+Launch V∞: [5.2751298113412, -8.661216821294703, -1.6354570434824398] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01154274470772458, -0.005957846816868132, 0.012549618987269454] km/s
+ V∞_out: [-0.011760586468874507, -0.0046695039337949495, -0.012880726200106482] km/s
+ time of flight: 1.1807226110600024e8 seconds
+ arrival date: 2027-01-19T12:52:36.712
+ thrust profile: [0.3714942769127498 -0.27514235457329284 -0.22284221348905592; 0.18648733513038335 -0.03538852611871538 -0.21336187522148525; 0.19399856639202537 0.002395803568838406 -0.3190282385205687; 0.11879730601555455 0.015360834365879166 -0.2536335710049435; 0.061944569057803066 0.012278706304360275 -0.1603952797122025; 0.040754334443318836 0.009956774580258716 -0.12153411323468802; 0.03303341403005917 0.009994889344157806 -0.11027086809253993; 0.022364533552884217 0.007144663061859577 -0.07970432734795593; 0.012776520278712816 0.004248825454391784 -0.04873564064475559; 0.0012224822532464015 0.0006528045961139463 -0.0038460504721996433; -0.00013158334363123263 0.0008176666035273955 -0.002173344303387432; -0.0015396795249455603 0.0032375271513952423 -0.005774382568315981; 0.0020239467634099164 -0.00011097400726251309 0.002091456524580368; -0.010595843830076116 -0.0016228707229629718 -0.0070115426272450085; -0.0018101688639026465 -0.008530610582666982 7.25461848864184e-5; 0.007112486587430833 -0.018868632717278334 0.004748899252526461; -0.0028405403359501955 -0.003667808517621758 0.002714351818314977; -0.001877010194078971 -0.0009806000966933919 0.010868224429106538; 6.9873350714433e-5 -0.0010129123470532001 0.0021041113454130156; 0.016529522267189442 -0.010178609074635334 -0.013426797189122201] %
+
+Mass Used: 98.89953869203464 kg
+Launch C3: 105.51839109305527 km²/s²
+||V∞_in||: 0.018061667442586898 km/s
diff --git a/archive/ES_0.6123989637921698 b/archive/ES_0.6123989637921698
new file mode 100644
index 0000000..9a2abe4
--- /dev/null
+++ b/archive/ES_0.6123989637921698
@@ -0,0 +1,22 @@
+archive/ES_0.6123989637921698---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T13:17:06.046
+Launch V∞: [7.199058811117145, -7.112606612177662, -1.3022498732497818] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0019389425548452758, 0.012465282030413291, -0.012696139849209693] km/s
+ V∞_out: [-0.007512076645348998, -0.012912635704910393, 0.009839660987398743] km/s
+ time of flight: 1.1854939192252366e8 seconds
+ arrival date: 2028-02-04T15:40:17.046
+ thrust profile: [0.3778174272819815 -0.15575337146178583 -0.1810601388516894; 0.26064938955355516 0.019712922335365174 -0.2625697073489866; 0.10945233877711706 0.03384181686971391 -0.1773064563508309; 0.14716464680359015 0.06676348809735413 -0.29874314314578687; 0.09820702671109621 0.053279359107359314 -0.246563274330295; 0.07917902409167883 0.05090979631667745 -0.23201071116774732; 0.05226069223248452 0.0369735014031712 -0.17868554920990184; 0.023544486006976787 0.022383625738918465 -0.09634883530481467; 0.0024704709981230193 0.0019295793833755365 -0.01173766922014238; 0.00884276015625155 0.005646659405718567 -0.03504348879386549; -0.00012591505676826488 -0.0010057501346543516 0.0003625910421989299; 0.0009930402323760743 -0.000367599603789933 0.0001145329720683816; -0.0009443083038480817 0.00039005327947059967 0.0027496112181675477; 0.00028241019025675266 -0.0005631088153295347 0.005681582522924842; 0.0010013997458631746 0.0018454057265351585 0.003909256340668356; -0.002912798117068447 -0.0015537269014756305 0.00436618672808518; 0.0004276174213435462 0.005225394937522225 0.0013024105204280023; -0.0019424565808519583 -0.004439625392495859 -0.0016439958270096063; 0.0011140381346436165 8.10107826976296e-5 0.007179327696844127; 0.00035659128093852837 4.453484043448247e-6 0.0018045841540324213] %
+
+Mass Used: 107.14851840313895 kg
+Launch C3: 104.11147531789587 km²/s²
+||V∞_in||: 0.017897897122271786 km/s
diff --git a/archive/ES_0.612664189675028 b/archive/ES_0.612664189675028
new file mode 100644
index 0000000..a23e6b9
--- /dev/null
+++ b/archive/ES_0.612664189675028
@@ -0,0 +1,22 @@
+archive/ES_0.612664189675028---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T08:49:54.456
+Launch V∞: [5.373280848182256, -8.469989635642333, -1.5783363324374255] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005567944739853739, 0.004447955425619383, -8.664718757448897e-5] km/s
+ V∞_out: [-0.002203663209739744, 3.133266098763222e-5, 0.006777310064364877] km/s
+ time of flight: 1.1667226676919687e8 seconds
+ arrival date: 2026-12-31T17:47:40.456
+ thrust profile: [0.5761734862813073 -0.41848605556675206 -0.31746954860045434; 0.28135053964815954 -0.046720590059888156 -0.29214746289803867; 0.19526352789829468 0.009910155611575188 -0.2937248468446873; 0.14593612268099623 0.025557674469183948 -0.2802656329638481; 0.09567497342128638 0.024739356185376628 -0.22036539853947923; 0.030620227608953735 0.009842738163300538 -0.08257782357120592; 0.028607501529969204 0.010942663792765702 -0.08751781013866443; 0.015198165932838136 0.005843028028439444 -0.04718928243722446; 0.019954867824801395 0.008845635128062614 -0.06869252931639087; 0.0026185080239745236 0.0013174745653979976 -0.009718176101749715; -2.9763604287984377e-5 -7.289155941996397e-5 -0.0029559241378108074; 0.0011995013431472972 0.00054618076488127 -0.0055906924034915635; 0.0007141799723285829 -0.0006305873850354277 -0.003401973726108147; 5.533026828684069e-5 -0.000543526214949251 0.0010419366622122974; 0.000576796207844274 0.00034739626931062765 -0.002495187155985703; 0.0007016199206875209 0.0002640761363060316 0.0006348426454047092; 0.00038800288416370615 0.0003679241043382162 0.0017771758561417324; 0.0015025523190234896 0.0007401090739327774 -0.0015918064036567845; -0.0028367154636783523 -0.0001690203017953001 -0.002294365903882231; -0.0011305286898223852 0.001003405523085631 0.0011674624524069567] %
+
+Mass Used: 113.33478832306628 kg
+Launch C3: 103.10401707962279 km²/s²
+||V∞_in||: 0.007126978590502177 km/s
diff --git a/archive/ES_0.6128554767654095 b/archive/ES_0.6128554767654095
new file mode 100644
index 0000000..3121663
--- /dev/null
+++ b/archive/ES_0.6128554767654095
@@ -0,0 +1,22 @@
+archive/ES_0.6128554767654095---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T17:27:56.732
+Launch V∞: [5.233700595169207, -8.618770214167217, -1.59679771538208] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.08290077065306264, 0.03863758802628622, -0.08507413863315881] km/s
+ V∞_out: [0.080980033150994, 0.034113603685948096, 0.08876948419730218] km/s
+ time of flight: 1.1677395936473536e8 seconds
+ arrival date: 2027-01-04T06:40:35.732
+ thrust profile: [0.5813888622120683 -0.4220758784397678 -0.314570653480976; 0.21253660206560934 -0.038313532424705345 -0.23564733389648504; 0.10419201327614452 0.0016329780466527888 -0.17512988453261216; 0.0749321645821939 0.009758411079134555 -0.16472398202292635; 0.0722549783544596 0.01598457864912253 -0.18442945634059804; 0.02726516338625706 0.007490406755609311 -0.08018772525133112; 0.05924492341418444 0.020654775358319246 -0.1864602384591598; 0.04013523308338373 0.013727971274889093 -0.1469709990318152; 0.01776603676371936 0.006248368050692797 -0.06712212572321664; 0.01779100358735948 0.007472383825972397 -0.07052417913253525; 0.0011501163555698694 0.0008573564812033099 -0.00243672871416602; 0.0023110492346481073 -0.0014137542154239974 -0.003192244593203505; 0.0002781022494194865 -0.0019471917467004426 -0.0015766877565642032; 7.129068324039005e-6 -0.0013743973099148484 -0.0017323157954280046; -0.00020907146938066207 0.0008170331606198291 -0.0025217601714625205; 0.004623804058750491 0.0010230989808976444 -0.00016264839982604021; 0.0019948583912729966 0.0056210942842660015 -0.001513227439368129; -0.0011355673212411453 0.0012588823349836487 -0.0036612162368566017; 0.001065734880542802 -0.002492721742007725 -0.0043671367204564954; 0.0010419119348191498 -0.0010639372430963914 0.0012020081567456072] %
+
+Mass Used: 107.02131116099463 kg
+Launch C3: 104.22458486833996 km²/s²
+||V∞_in||: 0.12491200922062952 km/s
diff --git a/archive/ES_0.6128844194406428 b/archive/ES_0.6128844194406428
new file mode 100644
index 0000000..a70b9a1
--- /dev/null
+++ b/archive/ES_0.6128844194406428
@@ -0,0 +1,22 @@
+archive/ES_0.6128844194406428---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:30:52.668
+Launch V∞: [6.936741878291603, -7.364547710284286, -1.8846016686832903] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.210997392604311e-6, -4.055207836754732e-6, -0.00012171829937562922] km/s
+ V∞_out: [-5.867956649068752e-5, -0.00010697390254212778, -3.41180640269389e-6] km/s
+ time of flight: 1.1988884296134329e8 seconds
+ arrival date: 2028-02-24T05:58:14.668
+ thrust profile: [0.4053247575991922 -0.1905890261878043 -0.22600721931930573; 0.16485856378311906 -0.00527438994467179 -0.19447588435755522; 0.12457050536039381 0.018179958719183237 -0.22921203006661955; 0.09016578058646352 0.02140508754151519 -0.2205636272677331; 0.0631988969297893 0.018102914142457387 -0.18798163371841115; 0.04598994964610142 0.014397814071754791 -0.1575653227546421; 0.01755904042546645 0.00520919234466833 -0.06048520900698482; -0.0009213541152498059 0.010353412167433141 -0.010477167864958442; 0.029620549191497245 0.0009028914925720759 -0.03515401577725818; 0.006059376924549134 0.012745475628749472 -0.021198771760250167; 0.004490988709109368 0.0023602099574126004 -0.018411551804955174; 0.004129735636484534 0.0006012460523171487 -0.017210973849523626; 0.00028320175285141724 -0.0012719042505887168 -0.012454423875067686; -0.004517171294055565 -0.0006146852461640131 -0.013948751881472933; -0.016066010752220725 0.016187319994423528 -0.00503840902166848; 0.0005528049389630359 7.991690572049218e-5 -0.001400495934074492; 0.020314640959213526 0.04107346918752426 -0.046273520237300816; -0.0028244657217852925 0.00025075070776429953 -0.0006101322671101981; 0.003886849347548166 0.012041930771207346 -0.05322832729800691; 0.018942042623166323 0.00020040461187784172 -0.05123388794193527] %
+
+Mass Used: 97.242889189989 kg
+Launch C3: 105.90667431270187 km²/s²
+||V∞_in||: 0.00012206231847575209 km/s
diff --git a/archive/ES_0.6129290165935635 b/archive/ES_0.6129290165935635
new file mode 100644
index 0000000..3516064
--- /dev/null
+++ b/archive/ES_0.6129290165935635
@@ -0,0 +1,22 @@
+archive/ES_0.6129290165935635---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T04:42:50.659
+Launch V∞: [5.267034603982971, -8.675822172030903, -1.7156128818776775] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004721854865650386, -0.004627254807057149, 9.501327866015847e-5] km/s
+ V∞_out: [0.002433726993043409, -3.989064027240599e-5, -0.006146791126682538] km/s
+ time of flight: 1.1700844132626404e8 seconds
+ arrival date: 2027-01-07T11:03:31.659
+ thrust profile: [0.4154974505424245 -0.3162124052469467 -0.25250238174709105; 0.18364697640933908 -0.039481417600870525 -0.2086865588201028; 0.14273257690334187 -0.002224269699324146 -0.2364089000149072; 0.11273058755489845 0.010131814215563474 -0.238985683638427; 0.10272126375259895 0.016000014874600243 -0.2601869344733268; 0.05797255754690406 0.012282167086884824 -0.17108677931392113; 0.008814643376719096 0.0017140350475899485 -0.02870588067715477; 0.007866699956858444 0.0049390633059234615 -0.04848060135050763; 0.00870827872375467 0.005379549046145936 -0.04380296422355442; 0.005713289568073498 0.0010296607821239899 -0.03463300706136644; -0.0036198629519530916 -0.00034679740969931476 -0.0015691077995197648; 0.0007117717362962622 0.00038766022417132155 -0.0005549693181114736; -0.00527258778107066 0.0032253112525230075 0.005796538403258503; -0.0007356308608630078 0.0024058279010761097 0.0012045779800462274; -0.005895705379346461 -0.003687654272277741 0.006937125967844806; 0.001388658329223475 -0.000502854895342405 0.0003125657564412871; 0.0008574880654322605 0.0006164246110659526 0.0022427267832519898; 0.002341492153073438 0.00011796797470523706 0.008013572343313846; -0.0012717473511997261 -0.0006480948958996629 -0.0004577931901248969; -0.01710968207829291 -0.0073692647225678184 -0.007812244928495943] %
+
+Mass Used: 97.01376928828086 kg
+Launch C3: 105.95487144072169 km²/s²
+||V∞_in||: 0.006611839981791867 km/s
diff --git a/archive/ES_0.6130547999230875 b/archive/ES_0.6130547999230875
new file mode 100644
index 0000000..f632865
--- /dev/null
+++ b/archive/ES_0.6130547999230875
@@ -0,0 +1,22 @@
+archive/ES_0.6130547999230875---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T13:19:18.100
+Launch V∞: [5.181544432894631, -8.570401412915517, -1.558651711893994] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.39192553695000276, -0.2581492836877503, 0.1600685707320186] km/s
+ V∞_out: [-0.34400515734785775, 0.2863588405887236, -0.2137048546616306] km/s
+ time of flight: 1.1932727327171053e8 seconds
+ arrival date: 2027-02-02T15:47:11.100
+ thrust profile: [0.6002755426705882 -0.43733757163915016 -0.32483928466594836; 0.19427086831456122 -0.03195260167145284 -0.21234422931203437; 0.14165527846960124 0.006647610886468134 -0.2277420969497376; 0.08141975356965571 0.01354257836538839 -0.17532673194633347; 0.029743180640155423 0.006889470357366115 -0.08215520172624902; 0.04214334109524121 0.01635114920597344 -0.13103567704407373; 0.0637886366758754 0.016598257645137317 -0.19156830068439473; 0.03455754381600401 0.01235497985959638 -0.12302617025571018; 0.011826846675370439 0.0033269735929245137 -0.04320081875408666; 0.01791218175356807 0.007685683795005503 -0.07439434388645494; 0.01072171586093655 0.0039535528292616124 -0.045577759896884895; 0.0013196660502485529 -0.0007926516863474564 -0.002810473259562586; 0.008331290921202394 0.004919626532212589 0.008770681714527148; 0.007054009545880925 0.005029849603423647 -0.011780742207641555; 0.003866943225317666 0.0050434425540520295 -0.0046108401484192315; 0.009058706109668118 -0.0013302463182748169 -0.006476235999676245; -0.0007173190456160193 0.0001101811879668812 -0.0073794653834652404; 0.028340989180504948 0.017108515828246743 -0.02433829262264613; 0.0028738418179495087 -0.006337460067992736 -0.018896463281240214; -0.010640436314667032 0.018339198612194747 -0.02645209220772827] %
+
+Mass Used: 115.97472679952716 kg
+Launch C3: 102.72957824755571 km²/s²
+||V∞_in||: 0.49585141576710035 km/s
diff --git a/archive/ES_0.6134391188932258 b/archive/ES_0.6134391188932258
new file mode 100644
index 0000000..2e81711
--- /dev/null
+++ b/archive/ES_0.6134391188932258
@@ -0,0 +1,22 @@
+archive/ES_0.6134391188932258---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:44:55.088
+Launch V∞: [7.018339582579531, -7.464919273040811, -1.9032829703537275] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013384136997136576, -0.029748063316834633, -0.018257869923206115] km/s
+ V∞_out: [-0.03058581011739269, 0.018598190850617258, 0.010760370485521866] km/s
+ time of flight: 1.1506925995269506e8 seconds
+ arrival date: 2027-12-31T01:25:54.088
+ thrust profile: [0.4000153105498981 -0.19235618185857709 -0.23359570319961234; 0.14330901393942994 -0.003947503637705983 -0.1865419672428885; 0.076524767178574 0.01026235793998067 -0.14862432925997832; 0.07060936001246312 0.01748325878760521 -0.18359019407516586; 0.06999122870263819 0.020813514495015034 -0.21521626497978338; 0.0631534504214206 0.020771312301724548 -0.21756290520226357; 0.025495293702459832 0.009619455204441981 -0.10619220349489657; 0.011212338941723531 0.004272077948210038 -0.051475828994668175; 0.002869135069622039 0.0011083674317429336 -0.014045457752287395; 0.004324947738055469 0.0018816864695174204 -0.019171779216095777; 0.007551456898888728 0.0019389068876655828 -0.03468106442458536; 6.88173363899425e-5 9.804682721787959e-5 -0.0003749630455356327; -4.199578230704436e-5 -5.966591623067903e-5 -0.000545504128771855; 0.0005125213235212448 0.0003104435385624365 -0.0007395692241494833; -0.0002690192097187447 -1.0176422919534048e-5 -3.868737307978162e-5; 1.9634170045303937e-5 -9.912957082087446e-5 -0.00033027423641354095; -1.2321577815319008e-5 0.0002549829889314185 -0.00020754682682477203; -0.0005593833879130468 -0.0001780758661559187 8.836663752970902e-7; -5.5790298004206496e-5 0.00014722775675794422 -0.00030191146856983986; -9.980248303074953e-5 -3.7368438680524305e-5 0.0004484639447616339] %
+
+Mass Used: 82.15216020659591 kg
+Launch C3: 108.60459631465729 km²/s²
+||V∞_in||: 0.03738224456066325 km/s
diff --git a/archive/ES_0.6135038202485792 b/archive/ES_0.6135038202485792
new file mode 100644
index 0000000..278aa0d
--- /dev/null
+++ b/archive/ES_0.6135038202485792
@@ -0,0 +1,22 @@
+archive/ES_0.6135038202485792---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T06:37:06.702
+Launch V∞: [5.474538436552993, -8.64375343212144, -1.9278979168207633] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.045427238415002034, -0.0008531877779234282, 0.03322727445508061] km/s
+ V∞_out: [-0.05507153556718313, 0.00046388659353478425, 0.011659321332444112] km/s
+ time of flight: 1.1644321560338825e8 seconds
+ arrival date: 2026-12-30T23:57:21.702
+ thrust profile: [0.25902005223915875 -0.19269423015921627 -0.16575329041697967; 0.1709292135449643 -0.033613062100065254 -0.20360527100560463; 0.14068052235433134 0.0017488664962963534 -0.2432417895394372; 0.11040920241753252 0.014391216266190235 -0.24523995552500458; 0.07690555903671736 0.016041551283860457 -0.2060264420622446; 0.05176893566966967 0.013135095054262106 -0.15802500504430167; 0.03300534347308805 0.009099541719109731 -0.1083680028951355; 0.009420718427822456 0.002532536538335413 -0.037329822442185565; 0.004781181730293025 0.001628815875270554 -0.01834721282731855; 0.007743313459518287 0.0028361770989002084 -0.032320085453963886; 9.379171511853012e-5 0.001423760054072556 -0.003082428169712336; 0.0007411709613559403 3.682462009501241e-5 -0.0017062578280264474; 0.00020973696426396227 0.00012406724571751982 -0.0034663101084456997; 0.00043872538058149877 4.476262423569683e-5 -0.0011979890439457576; -0.0001368676779693014 -2.3820809096965993e-5 -0.00011265454911072413; -0.001380318683549747 -0.0010358763402151263 0.002267981354270303; 0.0007993158127090807 0.0002364201479942321 -0.0009234438312467133; 0.0007110073305852693 0.0007177466438188632 0.00020904310476371128; 0.0008697294745241185 -0.000545853289342793 0.0027919217941983904; 0.0015145391202897242 -0.0011166441600782885 -0.007296808812526631] %
+
+Mass Used: 83.41042023665614 kg
+Launch C3: 108.40183486628908 km²/s²
+||V∞_in||: 0.056288663930769284 km/s
diff --git a/archive/ES_0.6137622338667643 b/archive/ES_0.6137622338667643
new file mode 100644
index 0000000..37feb28
--- /dev/null
+++ b/archive/ES_0.6137622338667643
@@ -0,0 +1,22 @@
+archive/ES_0.6137622338667643---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T01:57:12.225
+Launch V∞: [6.95681539529832, -7.301210757601386, -1.3958961331502622] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03421842113348254, 0.036163405548063646, 0.0037329232183364123] km/s
+ V∞_out: [-0.011698229283626788, 0.04738194626481474, -0.010498549371403201] km/s
+ time of flight: 1.152683809228407e8 seconds
+ arrival date: 2027-12-31T04:56:52.225
+ thrust profile: [0.6194167887277492 -0.2836751523984755 -0.3185342473741647; 0.2594906699850456 0.0006031064585068574 -0.28561681089481894; 0.18867430161871596 0.03790585784841473 -0.3160343097631475; 0.07947138748797195 0.023984357847884885 -0.17683272590707258; 0.05515486826242256 0.02053708700038448 -0.14889704296182282; 0.044607108973833236 0.018659828237600037 -0.1400295079187934; 0.08069765737778382 0.03988627690682431 -0.27746964726675766; 0.0053311655978942754 0.0027955524916269178 -0.022306034826752093; 0.001435126873812045 0.0018138302015802098 -0.012385740634888119; 0.0034624932228178437 0.0024745933677858484 -0.014141923895646754; 0.003203739668355991 0.0012832422013601178 -0.007930565639052081; 0.003821223258966593 0.004121158018637952 -0.0137692440797843; -0.00036510889909633444 0.001832884105069106 -0.0021684430120085156; 0.003393217680237838 0.0014416771786222391 -0.01739181799781713; 0.004276337919654783 0.0022924040702853136 -0.004482378536593152; 0.003060136470614076 0.0010191495487561495 -0.005372176068177683; -0.0006604071772390508 0.0015931390195660805 0.0014475354670690013; -0.003007224724014057 -0.0030484591642563254 -0.007929110740666215; 0.002528698436695918 -0.0023957238905453534 0.003005235734891514; 6.876109640436287e-5 0.0006212122897793857 0.00020013660558872593] %
+
+Mass Used: 111.41061042787123 kg
+Launch C3: 103.6534849857178 km²/s²
+||V∞_in||: 0.04992621517255319 km/s
diff --git a/archive/ES_0.6139835192414976 b/archive/ES_0.6139835192414976
new file mode 100644
index 0000000..09571f7
--- /dev/null
+++ b/archive/ES_0.6139835192414976
@@ -0,0 +1,22 @@
+archive/ES_0.6139835192414976---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T05:28:18.842
+Launch V∞: [5.243509041474849, -8.612969223314876, -1.403071014707571] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005423677438018456, 0.004367861642321219, -8.634945125021406e-5] km/s
+ V∞_out: [-0.0019970134677177527, 2.8869832022595695e-5, 0.006673683562476494] km/s
+ time of flight: 1.1623910800510256e8 seconds
+ arrival date: 2026-12-28T14:06:46.842
+ thrust profile: [0.500656300742652 -0.37890283435365635 -0.28412628208710444; 0.26466990178308525 -0.0564835613458414 -0.2874184110840779; 0.26914949853833686 -0.0025768770240130914 -0.4125254018140872; 0.08189913022529448 0.008195925805472442 -0.16921384764666242; 0.07339532375878874 0.013274560999171287 -0.18562168981044502; 0.057248068523528865 0.013566357640829639 -0.16813085503046515; 0.024258863977897067 0.006318390159410209 -0.0804314344677277; 0.02166531720617584 0.005052886413979821 -0.0693585725807921; 0.0003490997222090949 -0.0002833130444405037 -0.0050035303531965085; -0.00035497534223904027 -0.0009024017959767215 -0.00534922126749446; -0.003081145453761407 0.0003718158134712572 -0.004924748723093153; -0.0006554566979812631 -0.0006590362141474357 -0.007747223225457208; -0.0011400137916556395 0.0019401416042793436 -0.00752023537143988; 0.002989484812589472 -0.0020651015732325753 -0.009449116189635377; 0.0011203069867087836 -9.536110265173235e-5 -0.001296215835125121; 0.01729345714531601 0.013952870007995959 -0.019840788281359562; 0.018610405303594455 -0.008236556148836532 -0.011379364173869339; -0.002417418713422134 0.008434439328331796 -0.002630953926856012; 0.000947339705602636 -0.004262461926910625 -0.0031555802732760553; -0.0016175974855561564 0.0008059552281868071 -0.0011801268034032867] %
+
+Mass Used: 111.71107305277064 kg
+Launch C3: 103.64623418211028 km²/s²
+||V∞_in||: 0.006964334031755131 km/s
diff --git a/archive/ES_0.6141767968241654 b/archive/ES_0.6141767968241654
new file mode 100644
index 0000000..4fc22a1
--- /dev/null
+++ b/archive/ES_0.6141767968241654
@@ -0,0 +1,22 @@
+archive/ES_0.6141767968241654---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T04:08:59.394
+Launch V∞: [7.136634655337771, -7.045254471736178, -1.2032440557650375] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0020022139904941113, -0.012503611708135545, -0.002397613155078456] km/s
+ V∞_out: [-0.01229637520688261, 0.0023926242143178147, -0.0030559097460044174] km/s
+ time of flight: 1.1753938948470293e8 seconds
+ arrival date: 2028-01-22T13:58:48.394
+ thrust profile: [0.5478184382093398 -0.22744810237541457 -0.23421409831882511; 0.3363420179780516 0.027230365800426277 -0.3067960481180026; 0.22703615705484553 0.07177306054143508 -0.3182133583366914; 0.1564235699658163 0.07392566900119239 -0.29286866980921394; 0.11306249675528642 0.06684788164013306 -0.26021189474936574; 0.07134240536469122 0.05032083797261292 -0.19399658641484258; 0.035081013101943725 0.025462932977608172 -0.10763496462944314; 0.025198899285182562 0.01713547638357689 -0.082474567701942; 0.0015809502587933095 0.00165517081847312 -0.011832789408146267; 0.0016011325474623841 0.0009857763587852234 -0.007027884215675552; 0.0015092053393990484 -0.000590717763962132 -0.0020274967033076345; 0.0021815941517990094 -0.0006053341514209982 0.0014807090586726984; 0.0034186345369047926 0.0038378838027332924 -0.005236948176609619; 0.0017610342919540576 0.002698557898251626 -0.0032599523290054704; 0.0015837972641681221 0.00291445135869165 -0.0016438871079851472; 0.000411209617812833 -0.0024269415168879185 -0.003440327160824169; -0.0011835966711058704 -0.0004309926102214355 -0.0001742449020427422; -8.421165898949996e-5 0.0035632182393575784 -0.004062873017900307; 0.002884242898333675 -0.0009327597377030537 -0.0023552221858836376; 0.00041000990493121267 -7.15331007044575e-6 -1.3973560542390062e-5] %
+
+Mass Used: 121.45232360223963 kg
+Launch C3: 102.01496103302057 km²/s²
+||V∞_in||: 0.012887890263846907 km/s
diff --git a/archive/ES_0.6141974249887072 b/archive/ES_0.6141974249887072
new file mode 100644
index 0000000..156297d
--- /dev/null
+++ b/archive/ES_0.6141974249887072
@@ -0,0 +1,22 @@
+archive/ES_0.6141974249887072---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T02:49:43.637
+Launch V∞: [6.952941930866745, -7.3571292190333235, -1.8183095482521725] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008058556068315566, 0.05060478488658707, 0.009096694627135773] km/s
+ V∞_out: [0.049184578801518976, -0.0095918255230548, 0.014068510909278492] km/s
+ time of flight: 1.1457124308095372e8 seconds
+ arrival date: 2027-12-24T04:10:26.637
+ thrust profile: [0.6251564130386759 -0.29478617483228636 -0.3379359713887913; 0.23491069949077314 -0.001832089401596985 -0.27508104103036773; 0.12509951257138238 0.02338489743301193 -0.23143011167706246; 0.05754442966618814 0.01646396382907718 -0.14407962298964613; 0.038225562132790096 0.014103498952297558 -0.11764519134669704; 0.023490164050963977 0.00858804225067972 -0.08506119487519495; 0.049255088986503076 0.017721893349396268 -0.18297311047769427; 0.025125210335162483 0.013900803360730098 -0.12066016148597607; 0.006898668059311821 0.0034282717567410605 -0.03294509226095917; 0.0053367164301404285 0.00288259499165693 -0.026601470662228607; 0.0025045732365629805 0.0012095905382590241 -0.013339157028731502; 0.0008455621556880829 0.0007968975219897123 -0.0020237690254136234; 0.0004120558854805467 0.00016633571086153247 -0.001859124334566239; -0.0004898395963475828 -3.9844083337914186e-5 -0.0005651581091232353; 0.0001643929891709619 -0.00016417739928522614 -0.0011617571941283762; 0.0023167797136080127 -0.00016791299403187153 -0.0037980580822372842; 0.0004269966208950284 0.0019143569506107731 -0.003421821078088917; 0.0021898961322244755 0.0002802385638823378 -0.004761255082872242; 0.000562429756601113 0.0004799660161929416 0.002267025500318812; -0.004727912826730981 -0.003509238760800627 -0.0011165726592757348] %
+
+Mass Used: 99.53115401201921 kg
+Launch C3: 105.77700145282388 km²/s²
+||V∞_in||: 0.0520435820487339 km/s
diff --git a/archive/ES_0.6143804999000733 b/archive/ES_0.6143804999000733
new file mode 100644
index 0000000..ae49ce9
--- /dev/null
+++ b/archive/ES_0.6143804999000733
@@ -0,0 +1,22 @@
+archive/ES_0.6143804999000733---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T13:45:50.410
+Launch V∞: [5.144290684153762, -8.932780032399156, -2.3837928719217003] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.035215101939862346, 0.0005324458062813415, -0.02455580690235806] km/s
+ V∞_out: [0.04199803470299132, -0.00030371341206576974, -0.00880397053358371] km/s
+ time of flight: 1.1705539813860537e8 seconds
+ arrival date: 2027-01-11T09:09:08.410
+ thrust profile: [0.25740868439543474 -0.20336335506941097 -0.1848979461532705; 0.12297242973492925 -0.03475539632702736 -0.17836099959754115; 0.08272210435591136 -0.00904946407689569 -0.17942266643449395; 0.05506080247243054 -0.0013668583086879006 -0.15625405652088778; 0.03563880030905678 0.0010529653994713552 -0.1253934817585411; 0.020934119125848916 0.0009767909397468133 -0.08543687795556228; 0.013604987231335318 0.0007109554814020223 -0.060651689059021956; 0.00960575297758471 0.0005592968169470996 -0.04772257044806299; 0.008119350919754345 0.00025336636154383197 -0.04476898073741377; 0.0009469019896265363 0.00017454322305492722 -0.005313939389897156; 8.138023767658669e-5 -0.00026051019414724834 -0.0010735130246280484; 0.0023320777237576347 7.507516008786264e-5 -0.012488949326315802; 0.0012680747982861719 -0.001066822075892447 -0.0014463586764328152; 0.0004053968299088871 0.001290707993329661 -0.0020144248796060207; 0.0006431465545332112 -0.0020239299745011784 -0.002422758617963883; 0.0023783072243289895 0.0004972980596987883 -0.0007829914935127915; -5.9236946224322684e-5 6.74225321365478e-6 0.0006350731558012342; 0.0003303063244012972 0.0013573562404429454 -0.00012479425064193398; -0.0002367445769294091 -0.0003644994841046843 8.230532386816446e-5; 0.0017717183941055484 -4.086721333948352e-5 0.0015480812129589055] %
+
+Mass Used: 63.789517012023225 kg
+Launch C3: 111.94075420652497 km²/s²
+||V∞_in||: 0.042934538029393295 km/s
diff --git a/archive/ES_0.6145201066831925 b/archive/ES_0.6145201066831925
new file mode 100644
index 0000000..f84cf4f
--- /dev/null
+++ b/archive/ES_0.6145201066831925
@@ -0,0 +1,22 @@
+archive/ES_0.6145201066831925---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T14:42:29.992
+Launch V∞: [5.304670799986197, -8.65157683763653, -1.7007051899455505] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.013281858048009267, 0.012660357283267476, -0.0002433538265677906] km/s
+ V∞_out: [-0.005628202916512181, 7.38043568832248e-5, 0.017474015876214728] km/s
+ time of flight: 1.1624159282093708e8 seconds
+ arrival date: 2026-12-29T00:02:21.992
+ thrust profile: [0.4119110269329402 -0.3027318628950225 -0.24255403873798095; 0.25078151322430375 -0.04740852883568603 -0.27356598718392994; 0.13231956043041543 0.0018577658493511037 -0.21381848623291427; 0.11490678007088424 0.015129629905673648 -0.23591035215921458; 0.06119188887091948 0.012271370254497373 -0.1537078405795853; 0.058237921395587075 0.013734240870169058 -0.16742781152819342; 0.06793041824938803 0.020029871727787873 -0.21163715667090974; 0.006758253882078983 0.0021283985977374694 -0.023910205126894506; 0.004551776973309636 6.408613643479183e-5 -0.008467797599320401; 0.0023882154788791607 0.0024473527676910738 -0.006442424278538805; 0.002522712621411576 -0.00034134348908153235 -0.005479257616980981; 0.0016060534763518352 -0.00180971725431532 -0.008813669923592208; -0.00024215361664483345 -0.0024863857153623412 -0.008667219740183906; -0.0015196862525379512 -0.0012463768314298043 0.004748522716620872; -0.0007754808129560441 6.585224731481379e-5 0.006989791507134144; 0.0009605115788089099 -0.0015238555231044347 0.0023704110044715787; -0.000888749054568907 -0.002820471359984391 0.0033460263888259317; -0.006794045902177847 0.0038000615897875157 -0.0037712835212130986; 0.005000512884485272 0.0026710229119683757 -0.005560286911936275; -0.007790660380066714 0.012136176059027573 0.016484779382880635] %
+
+Mass Used: 99.29680319869158 kg
+Launch C3: 105.88171221686281 km²/s²
+||V∞_in||: 0.018350793466015508 km/s
diff --git a/archive/ES_0.6146883413198825 b/archive/ES_0.6146883413198825
new file mode 100644
index 0000000..a27cf53
--- /dev/null
+++ b/archive/ES_0.6146883413198825
@@ -0,0 +1,22 @@
+archive/ES_0.6146883413198825---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T21:57:26.424
+Launch V∞: [6.841580619156293, -7.171585378886346, -1.5089388616960149] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000546077524269397, -0.0008599698442722224, 0.0012825698621709075] km/s
+ V∞_out: [0.0006580840846508552, -0.0012540659276935708, 0.000821427897708738] km/s
+ time of flight: 1.1540179051966211e8 seconds
+ arrival date: 2027-12-31T14:00:36.424
+ thrust profile: [0.9385797120654645 -0.43233452328009786 -0.45389363974432406; 0.34145934298867336 0.007532072537267565 -0.35076642334699715; 0.18469321626851448 0.04428212267544858 -0.29448674152257726; 0.09378378866051085 0.03544588862066277 -0.20181361861543393; 0.06621367525538556 0.03097120192334612 -0.17307408370363353; 0.05432980826306566 0.028866728716572296 -0.1645173144253687; 0.026379263593673943 0.015301609049311255 -0.08989915792543496; 0.016167702635264194 0.009921743157015455 -0.059363596951707086; 0.004935535225307634 0.0037829684642298684 -0.01831274957571881; 0.0018807625045030585 -0.0011900535882452697 -0.006380470885833451; 0.002832990891074276 -0.0037542076990978715 -0.001007383024908509; -0.001011100170280786 -0.0014275168708635573 0.00022793507208368567; 0.005497452954698015 -0.003181545023247454 -0.009713943435802026; -0.0022813907134935528 -0.0007313388636645775 -0.0012605985263052098; -0.0028253420666433976 -0.006205312623678157 0.007362225986341602; 0.0021933521098682243 -0.0026699523106760627 0.004573902302590381; -0.0013206696484176262 -0.0019613115616161202 0.0019561047906468585; -0.005721388291249583 -0.01870867465428642 0.005242877057817087; 0.004397574275283456 -0.005244060992683625 -0.01637587986275651; 0.011915549107066912 -0.008891608393700495 -0.0234129360285463] %
+
+Mass Used: 130.79447243665027 kg
+Launch C3: 100.51575870340787 km²/s²
+||V∞_in||: 0.0016379054450483047 km/s
diff --git a/archive/ES_0.6149900357631537 b/archive/ES_0.6149900357631537
new file mode 100644
index 0000000..8ca02c9
--- /dev/null
+++ b/archive/ES_0.6149900357631537
@@ -0,0 +1,22 @@
+archive/ES_0.6149900357631537---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T07:02:39.224
+Launch V∞: [5.318695874299197, -8.390949749704607, -1.4410989517109989] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0035589403357548536, -0.003254962033680741, 6.695027322293945e-5] km/s
+ V∞_out: [0.001478207616767999, -2.0008846849254725e-5, -0.004594166759714334] km/s
+ time of flight: 1.1513715621124017e8 seconds
+ arrival date: 2026-12-12T21:35:15.224
+ thrust profile: [0.7847008129340732 -0.5662524360225842 -0.39658304500420555; 0.39022198882157516 -0.058972694686100946 -0.3669798857034913; 0.231747798186564 0.01806736197887999 -0.3218757196108825; 0.1520202742244629 0.03218615185387281 -0.27452161191469415; 0.0789829306652466 0.024558080726905428 -0.1797023919017729; 0.049394442499758155 0.018748611237081943 -0.1319426416708259; 0.04082532960494575 0.016673305705027588 -0.11718897371270323; 0.01322799787903632 0.0054747737564119145 -0.037424227573240064; 0.0005561447079883272 0.00027118763414963904 -0.0018163391065005533; 0.00320152958777087 0.001786437228600385 -0.012906774016226795; 0.0022057890319404218 0.000995762478228858 -0.00731794504193586; -3.0429410719080216e-5 -0.0001911235264031225 -0.0006821711482554336; 0.00017015407436116945 0.00012972100323302476 -0.00020415655211641616; 0.00015942205212657199 3.715595538383806e-5 -0.0003456086458429094; 8.693977952139785e-5 0.00013870664473707457 -2.9152112282293036e-5; 7.671459670062633e-5 -6.651552872623904e-5 -0.00020120837183559387; 8.849816353486664e-5 -4.232357045982134e-5 -6.464832937955111e-5; 3.7220447966480424e-7 -9.480598525046948e-5 -0.00013207258665062343; -3.1015853364289708e-6 -2.085979935435327e-5 0.00011835074182745453; 9.00799667795453e-5 -5.2861817967776975e-5 9.325801694891931e-5] %
+
+Mass Used: 129.643951842143 kg
+Launch C3: 100.77332969397764 km²/s²
+||V∞_in||: 0.004823413365372137 km/s
diff --git a/archive/ES_0.6150038131133948 b/archive/ES_0.6150038131133948
new file mode 100644
index 0000000..be04964
--- /dev/null
+++ b/archive/ES_0.6150038131133948
@@ -0,0 +1,22 @@
+archive/ES_0.6150038131133948---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T11:03:22.781
+Launch V∞: [7.027152981809334, -7.406420304358917, -1.9538759832534929] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.20157176204689092, -0.9208116432682754, -1.5224887257530697] km/s
+ V∞_out: [0.7952142192810217, 0.3483120509420316, 1.5653073422051718] km/s
+ time of flight: 1.1403100382837072e8 seconds
+ arrival date: 2027-12-18T06:20:05.781
+ thrust profile: [0.446989576894254 -0.2134345350520252 -0.25006569034664544; 0.21399186344401677 -0.005271652443550418 -0.2524040583140104; 0.13287619931617198 0.021777610517350037 -0.24573777104449995; 0.07817375248402149 0.022477735367780433 -0.19720434851261376; 0.05028988583262667 0.019417066173013628 -0.15745796284291452; 0.02344108317435889 0.00940330428574845 -0.0842690515224091; 0.020003877282075224 0.008800507734632469 -0.08034884219864273; 0.01905197214320953 0.008216257454651424 -0.08184459503762676; 0.007585889900120993 0.002918913603254794 -0.03717580037183831; 0.010172564653924585 0.0038467150608258232 -0.048521624941137424; 0.0036995154202205138 0.0017656919946203934 -0.01945663105563392; 0.0010066570375616556 -0.0004757805478173817 -0.002415661677619462; 0.0002114874354711367 8.33920497849337e-5 -0.0008865913218920622; 2.129057341730689e-5 0.0003966353085192544 -0.0012171926289586028; 0.0015000651951672878 -0.0006840805827244623 -0.0016500041054550772; 0.00019975174956701378 -0.00035685963075092085 -0.0009810358775501436; -0.0002607366475761259 0.0010687407327939942 0.000182423192691072; -0.00012244795736987156 0.0002170006570655107 0.0007097059767027648; 0.0004405906818281671 -1.9582760324621483e-5 -0.0003514223021989259; 5.9978182825085394e-5 0.00021172646838532225 -0.0004083516829479012] %
+
+Mass Used: 87.19194464267184 kg
+Launch C3: 108.05357211250666 km²/s²
+||V∞_in||: 1.7906694775078722 km/s
diff --git a/archive/ES_0.6150490233876351 b/archive/ES_0.6150490233876351
new file mode 100644
index 0000000..f234fa9
--- /dev/null
+++ b/archive/ES_0.6150490233876351
@@ -0,0 +1,22 @@
+archive/ES_0.6150490233876351---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T18:54:55.703
+Launch V∞: [7.103036800411124, -7.295936178198388, -1.6729808467929037] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.001380243943999625, -0.0023039960819399986, 0.0031984913544706984] km/s
+ V∞_out: [0.00172066136978814, -0.003188883516296718, 0.002076850584345697] km/s
+ time of flight: 1.1425930061378807e8 seconds
+ arrival date: 2027-12-19T05:36:35.703
+ thrust profile: [0.40941467482677346 -0.19312663807398345 -0.21998666925449764; 0.2528635693737651 0.0023266240074359796 -0.2754424156551796; 0.1807410973778472 0.03903434185219869 -0.3004894550930182; 0.1307953946979623 0.044395529860082335 -0.28832079353326956; 0.08227068056354883 0.03511013290814091 -0.22642036881029365; 0.03793470405030494 0.01857221657088535 -0.12779224392124722; 0.01521319448819772 0.007529696824695987 -0.05692173017683395; 0.00560658104081968 0.00265311342610044 -0.022578650756891742; 0.004926901229169485 0.0031111599876439246 -0.022147423519875583; 0.007479776050538009 0.003316775683956578 -0.03407442659778734; 0.00026013412005322656 -0.0004080649443107305 -0.0012688544744728328; 0.006645409185975124 0.004948780686677127 -0.03563420846361463; 0.00021877979977516106 0.0007868891070770053 -0.0012180105046745875; -0.0003290069374339842 0.0005746689979115205 0.0009414881787738175; 0.0014407068602830075 0.00043451694339036363 7.463118596360294e-5; 0.0009234983296830426 0.00013196873515541993 -0.0004676899921963022; 0.00025489815880516535 0.0004158236717053814 -0.001078539914247708; -0.0016497985149070997 -0.0012957636934956295 -0.0007562590943123706; 7.634978461879588e-5 -0.0011553429697208884 0.0014686613592963284; 0.0010171898045450026 -0.0017865247283163814 0.0002265792086655669] %
+
+Mass Used: 96.40821901347181 kg
+Launch C3: 106.4826814180747 km²/s²
+||V∞_in||: 0.004176579729296007 km/s
diff --git a/archive/ES_0.6151730171112677 b/archive/ES_0.6151730171112677
new file mode 100644
index 0000000..4a8cb79
--- /dev/null
+++ b/archive/ES_0.6151730171112677
@@ -0,0 +1,22 @@
+archive/ES_0.6151730171112677---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T22:02:39.579
+Launch V∞: [6.994459916131606, -7.137077960314377, -1.138328639641013] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009974233464785718, -0.0072271966980426575, 0.004224217610587757] km/s
+ V∞_out: [0.002576498833585395, 0.006716560949969961, -0.004395717588913065] km/s
+ time of flight: 1.2742482929801439e8 seconds
+ arrival date: 2028-05-19T17:49:48.579
+ thrust profile: [0.4242396025552197 -0.18169662585543564 -0.20949676492511368; 0.14905117200784632 0.0033758394768708374 -0.17036961275175924; 0.11187892752754036 0.023543120417678497 -0.20227462437007715; 0.08816129751451712 0.027820871505268505 -0.21422288548127214; 0.07346725818130466 0.028084962671261305 -0.21956673200890325; 0.09144645826250722 0.04176209363453012 -0.3163109440669992; 0.03173630665404665 0.012289747563823703 -0.12598867070520042; 0.007534598914397333 0.006386818802660409 -0.019937459660593168; 0.013705369132533318 0.01679661725386431 -0.011514504993636982; 0.0070769927824472405 0.007066940027199163 -0.00963357905298762; 0.014067157283224444 0.008018234587689584 -0.028609954849393656; -0.004793770643346164 -0.004748993066317894 -0.007093037626670833; 0.029882232146376565 0.07082726098644249 -0.021999750961071964; 0.0014330561503985498 -0.0003899028070186057 -0.011485543712452806; -0.07666854926675086 -0.020731297692189204 -0.031513057602622914; -0.03051915700815499 0.0733536206380111 0.013099958728849392; -0.05893061770031688 0.013525533231363412 -0.05836497051867469; 0.006518127907456765 0.0016293291356173113 0.010947927692797309; 0.11486864153638138 0.047145098976679616 0.018516415159879653; 0.018543065331767604 -0.032217466288154716 -0.004817651401653376] %
+
+Mass Used: 127.62435000262258 kg
+Launch C3: 101.15614342180395 km²/s²
+||V∞_in||: 0.008430376021619614 km/s
diff --git a/archive/ES_0.6151917908849912 b/archive/ES_0.6151917908849912
new file mode 100644
index 0000000..542b491
--- /dev/null
+++ b/archive/ES_0.6151917908849912
@@ -0,0 +1,22 @@
+archive/ES_0.6151917908849912---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T13:22:03.080
+Launch V∞: [5.361050092952799, -8.649239501566797, -1.8778352787585908] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012544795553527017, 0.012400050863748804, -0.00022352281701899703] km/s
+ V∞_out: [-0.005237888610442462, 6.608118063440875e-5, 0.016843826045637028] km/s
+ time of flight: 1.1487806702408016e8 seconds
+ arrival date: 2026-12-13T03:56:30.080
+ thrust profile: [0.424181279457469 -0.3176938312515182 -0.2801345606492547; 0.2273630453366914 -0.044637667511407575 -0.2615379175879949; 0.1480254086997235 0.0019476054461486153 -0.2483851510073812; 0.10633097890750308 0.013867845354606952 -0.2291016504982638; 0.06670536886876559 0.013763410895227495 -0.17326923629138974; 0.038950240035779245 0.010044497422043896 -0.11738994954594958; 0.022126038299634884 0.0063112797189668 -0.0760792584894733; 0.019082118725069996 0.006619403403353046 -0.06800157733621943; 0.004572319208798853 0.0028210304988442497 -0.01564778633447132; 0.0074412553924747445 0.0031354372649880302 -0.029084481371924844; -0.0023622203709025395 -0.0003261643059254696 -0.005135997751886896; 5.574357609303116e-5 0.00046942746070940505 4.659467148054354e-6; -0.005554167227386235 -0.0021623281133868622 -0.0034957446647125596; 0.0014180787340080108 0.0007798661826363953 -0.007426533279612299; 0.0010870404540656337 5.229299319756359e-5 -0.0011613573174098695; 2.3769949506955573e-5 0.00014751701563241962 -0.0002825628730339768; -0.002219793462864104 0.0011697696518927795 -0.0024662332009862085; 0.001747030968163964 -0.0011131440572716032 0.00023324730990003512; -0.0031223765201508756 -0.00010343332492221522 -0.005052973194500859; 0.0010661374012485838 -0.0014832742511601733 -0.002413308416375633] %
+
+Mass Used: 93.11102959803884 kg
+Launch C3: 107.07646738876302 km²/s²
+||V∞_in||: 0.017640383197455683 km/s
diff --git a/archive/ES_0.6152666527592271 b/archive/ES_0.6152666527592271
new file mode 100644
index 0000000..6c5c26d
--- /dev/null
+++ b/archive/ES_0.6152666527592271
@@ -0,0 +1,22 @@
+archive/ES_0.6152666527592271---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T13:58:34.870
+Launch V∞: [7.002233831494184, -7.421383249953148, -1.6377957761072939] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.038380855547252256, 0.039508675435490796, 0.004072236270219351] km/s
+ V∞_out: [-0.013666788262223145, 0.05214709459019372, -0.011989993817502445] km/s
+ time of flight: 1.142557499408651e8 seconds
+ arrival date: 2027-12-20T23:41:03.870
+ thrust profile: [0.48089077118953877 -0.23467998711997717 -0.2747881871374101; 0.20881989424899597 -0.008966795855413823 -0.2531907592741493; 0.12865889771228578 0.017616784241867127 -0.24027272805031966; 0.07681214793121437 0.01795214803731033 -0.19060420811192716; 0.053138239351044524 0.0157169179248321 -0.16096489955275708; 0.05438314973160863 0.01825982556527916 -0.19025275566975353; 0.02573050045584782 0.011299634645116888 -0.10187209110913992; 0.029271741990789142 0.011117541995706961 -0.12436972861596092; 0.0036215438082382433 0.001556457252330129 -0.016912364498244997; 0.0030330764685599482 0.0012593737482559874 -0.015088879060721453; 0.001450999740069798 0.0008963997510682709 -0.007184894348433864; 0.0020166013528538224 0.0006679007022899715 -0.009171578455714263; 0.00023544612016495638 0.00046511822834271934 -0.001766186409080054; 0.0005047377487430679 0.0003580857267134656 -0.001678997931445032; 0.00024747125870592905 0.0002569295642011098 -0.0013107377817514502; 0.0006496035003032691 -0.0036392416808999836 -0.0015560265982304026; 0.001834033191533592 -0.0030329591446702844 -0.003535287411828448; 0.00010604959789185593 -0.000428278442784749 -0.0026169128227546325; 0.0009584686053815568 0.0003263086112279633 -0.0030054649901840574; 0.000489810539655299 -0.0012078420421275965 0.003361594848338833] %
+
+Mass Used: 94.86602751502141 kg
+Launch C3: 106.79058297784175 km²/s²
+||V∞_in||: 0.055232314956431876 km/s
diff --git a/archive/ES_0.6153836245611193 b/archive/ES_0.6153836245611193
new file mode 100644
index 0000000..8fcc80d
--- /dev/null
+++ b/archive/ES_0.6153836245611193
@@ -0,0 +1,22 @@
+archive/ES_0.6153836245611193---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T23:33:32.590
+Launch V∞: [5.162587976941726, -8.672478397331897, -1.338675418603251] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03991564665224908, 0.03899462689910086, -0.0015769784602150721] km/s
+ V∞_out: [-0.018098581528178993, 0.0002419551937519153, 0.056172784360132566] km/s
+ time of flight: 1.1426860913774806e8 seconds
+ arrival date: 2026-12-06T12:50:21.590
+ thrust profile: [0.5586363733037744 -0.4342996557294652 -0.317327786179777; 0.4091315874937162 -0.09695202993462239 -0.43154015787868893; 0.11204494725958734 -0.006548086023405969 -0.19483662517339354; 0.1401709471310796 0.012924396182312359 -0.2880306512022205; 0.07997740077857787 0.009036120864437999 -0.20603417515550598; 0.044840795247701626 0.00817634913429295 -0.13335562055379752; 0.02936716319700982 0.006491123829524912 -0.09961398170900937; 0.012780280648866804 0.0027553826501519113 -0.045642492167864375; 0.006346346896582329 0.0014670171165378609 -0.024195267494692186; 0.0007218247459507183 0.0002374531612768276 -0.0031070827565726094; 0.0006557087032407995 0.00016787178862582563 -0.002880436197586651; 0.0007350433066703172 -0.00042694200790379343 -0.0018862409880246547; 0.0008007674024683499 0.0006942810937481355 -0.002791230284385899; 0.0021227568312283556 0.0004551696838952237 -0.002264013797352823; -0.00019520291913927533 -0.00029592239864373836 -0.0038128290918299193; -0.0001113731453903906 -0.0010553750354290047 -0.0015752249461317407; 0.000983071237775597 -0.0014492229993742253 -0.001531785920645811; -0.00040895711972677704 -0.0002888857950568141 -0.0025133939903820004; -0.0005789977286120443 -0.0015945238508641272 0.0005833219602148828; 0.0003934154070810163 9.915934844355833e-5 -0.0007472168014534299] %
+
+Mass Used: 113.28611503999764 kg
+Launch C3: 103.65624804822427 km²/s²
+||V∞_in||: 0.05582406860603467 km/s
diff --git a/archive/ES_0.6164672426152712 b/archive/ES_0.6164672426152712
new file mode 100644
index 0000000..fef1f4c
--- /dev/null
+++ b/archive/ES_0.6164672426152712
@@ -0,0 +1,22 @@
+archive/ES_0.6164672426152712---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:03:40.666
+Launch V∞: [7.017372601675549, -7.4018023807023745, -2.115338014356229] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003396896639964625, -0.0005375612764859582, 0.0008216772364199983] km/s
+ V∞_out: [0.00040975462635790133, -0.0007906434945476415, 0.0005350055461275534] km/s
+ time of flight: 1.1434742602380303e8 seconds
+ arrival date: 2027-12-22T05:14:06.666
+ thrust profile: [0.4816245321855293 -0.24181888175887736 -0.2676169671109762; 0.17945289889416335 -0.008520574211222591 -0.22458094892914204; 0.10129506788456606 0.014612053700548225 -0.20230249577739504; 0.07390745847531592 0.01810181495602597 -0.1961619704289654; 0.05001166853635363 0.015142030139787755 -0.1599935853106951; 0.03294807538447283 0.011813729443046669 -0.11906990218683848; 0.021026198608028603 0.00870171376330378 -0.08076421833516295; 0.016640081106952195 0.007472221394709382 -0.06856378818449053; 0.005256167925329977 0.00252136882483011 -0.023581663843108294; -0.0005258240279119425 -0.0003187648901991528 -0.0056831886782240625; 0.0056059074525962 -0.0011440734835672334 -0.0064795217783976755; 0.001298520144661375 -0.0028654887858930657 0.0013663153669291068; -0.005345023656950363 -7.390302921599743e-5 -0.007703858709715331; -0.011485289599109858 -0.0027980308151428937 -0.007951043536831634; 0.011939631216257112 -0.001084427468487014 -0.011049849686259822; -0.00033382576870048033 -0.000381950993162284 -0.00024366761745711087; 0.000636110491614772 0.0001412180522086418 -0.003368973750191115; -0.010508738377805216 -0.003341191758484691 0.007716484875078856; 0.007564661415080946 -0.0036329522471193706 0.005588142169999448; 0.006587789231338555 0.0034492700915091283 -0.008625221386298952] %
+
+Mass Used: 86.26681521707496 kg
+Launch C3: 108.50485162869855 km²/s²
+||V∞_in||: 0.0010389969560369503 km/s
diff --git a/archive/ES_0.6166051135886023 b/archive/ES_0.6166051135886023
new file mode 100644
index 0000000..c81e9af
--- /dev/null
+++ b/archive/ES_0.6166051135886023
@@ -0,0 +1,22 @@
+archive/ES_0.6166051135886023---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T21:21:40.630
+Launch V∞: [7.081545070713602, -7.0729091815335625, -0.776577260159705] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.12569211342020387, -0.19700859876116908, -0.07680141452474583] km/s
+ V∞_out: [-0.14140915050284358, 0.1776207593128055, -0.09465864143283792] km/s
+ time of flight: 1.1821819752862304e8 seconds
+ arrival date: 2028-01-30T03:44:57.630
+ thrust profile: [0.5002588515718371 -0.19771825906394763 -0.20353209361576632; 0.4054390241694503 0.040029185349386 -0.34107058991699124; 0.2423569923140263 0.0807257949835226 -0.3112829839329478; 0.18065015960900016 0.08740742446155071 -0.30403025066127853; 0.10248875965132118 0.06063796192970542 -0.21497968792565086; 0.08338045120220135 0.056688096391749335 -0.20215894735742795; 0.07887004887583762 0.05941979023466609 -0.21235731456802007; 0.0229843245681633 0.018505422430265896 -0.06785506490478066; 0.01823578179497519 0.01548440305634518 -0.06101618314749655; 0.0002901538197337305 -0.0016223591992106942 3.205407219406334e-5; 0.002873873687006971 -0.004662918383876911 -0.0004510593494124414; 0.00430470582405602 -0.003009020159280036 8.728342550493647e-5; -0.0022794285403208527 -0.0009648491939429927 -0.006293626488579706; 0.0011637101927252833 0.001071312493633596 -0.004770915783360482; -0.00107065156804025 -0.002699694621590011 -0.004509154573100797; -0.0020216781866428837 -0.0024564512238648174 -0.006095482963089488; 0.012471230063607982 0.00011388168858744913 0.0076364691595693784; 0.0009647357382865877 0.0008229274087098732 -0.0024345158387460123; -0.010410373178908307 -0.0063652727719950425 0.011194511483434939; -0.000643184932303301 0.002595909436010302 0.003527348481835557] %
+
+Mass Used: 131.50448265472824 kg
+Launch C3: 100.77739711976703 km²/s²
+||V∞_in||: 0.2459864887242357 km/s
diff --git a/archive/ES_0.6166160120016827 b/archive/ES_0.6166160120016827
new file mode 100644
index 0000000..799075a
--- /dev/null
+++ b/archive/ES_0.6166160120016827
@@ -0,0 +1,22 @@
+archive/ES_0.6166160120016827---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-16T03:26:38.154
+Launch V∞: [6.78984188046747, -7.061671164117695, 0.3968908190976129] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005595369517045494, 0.0035546308839460856, 0.005290234728382895] km/s
+ V∞_out: [-0.003676153364721908, -0.006156489845913204, 0.00452847598605185] km/s
+ time of flight: 1.8136998694124848e8 seconds
+ arrival date: 2029-01-13T07:59:44.154
+ thrust profile: [0.6185853301371108 -0.17460324268517943 -0.12446785055997758; 0.22677772757378417 0.08061953852423408 -0.14150652506851957; 0.3321148289581088 0.23032797379028558 -0.3291070490447332; 0.10074312432188874 0.09844891521564511 -0.14856211424358867; 0.05740910584655088 0.07057320730640948 -0.1112123899864324; 0.02002606755928106 0.028470075500273764 -0.048760773995074905; 0.0086471110366893 0.013837106595653702 -0.026402876672936643; 0.0014265539609784046 0.003981499614614159 -0.004991593171845032; 0.004017652604239849 0.016659056604590654 -0.025775275495175717; 0.005753350807228488 0.0009711415070141555 -0.013906197339986211; 0.015173349537815817 0.0032097192446065613 -0.00877779903708288; 0.004446317473116489 0.00013207136899013672 0.003205383612978156; -0.000573420296805515 -0.012092225549907656 -0.01264626040716155; 0.012059990455496168 0.014566804630426594 0.021477119771260916; 0.00434033092498837 0.0081506384059375 0.0033086245115111256; 0.0023252806985154108 -0.00832555924735576 0.02508424197641599; -0.003356859832369942 -0.011610817404073125 0.023032704357998823; 0.0429792594342547 -0.03636118865672547 -0.022524808839899726; -0.014087275726044674 0.0026212577340985364 -0.03696458455897043; 0.017031717305988316 0.003998843952114248 0.0020925637809899953] %
+
+Mass Used: 158.64641150266516 kg
+Launch C3: 96.12667471416536 km²/s²
+||V∞_in||: 0.008481164084886797 km/s
diff --git a/archive/ES_0.6167317018496277 b/archive/ES_0.6167317018496277
new file mode 100644
index 0000000..5ced3c6
--- /dev/null
+++ b/archive/ES_0.6167317018496277
@@ -0,0 +1,22 @@
+archive/ES_0.6167317018496277---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T14:14:46.346
+Launch V∞: [6.9211107226494395, -7.260446424553024, -1.5849520274557676] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004508634303134923, -0.0007113346203308209, 0.001025105362003831] km/s
+ V∞_out: [0.0005463915887768562, -0.0010137120703511474, 0.000658058516376843] km/s
+ time of flight: 1.1407536032803085e8 seconds
+ arrival date: 2027-12-16T21:50:46.346
+ thrust profile: [0.7446136811317625 -0.3443768456690535 -0.3765670939912292; 0.32017578305700195 0.0036020179771916187 -0.33622798112145946; 0.19150597942923062 0.042402283869977526 -0.30894141999365443; 0.11359433682035322 0.0401475108011707 -0.24647991638462663; 0.07395980619097293 0.03290826425942262 -0.1988454175184542; 0.027220019645016327 0.014330339228684258 -0.08857924360545251; 0.012531797064778262 0.00718711036000441 -0.048269941104464704; 0.012891656736333154 0.007416949619074792 -0.05379742661231516; 0.007298545512678197 0.0017255693272446866 -0.018772457097138283; 0.0022920892986215114 0.0017048228729090696 -0.020161132806905138; 0.0044904676062675845 0.002064210260953539 -0.020287416047652652; 0.0037886084472614134 0.0031543395274858444 -0.016843515248004568; 0.004780217501741191 -0.0026340894965498404 -0.02022112323252926; -0.0026458446140145125 0.0019020591451808992 0.00972227756901935; 0.0011445306853236077 0.000845996372097965 -0.0050357695569011145; 0.005252863843951308 0.0010658292646911027 -0.017151974817575882; 0.009052114939009866 0.0028153824364224203 0.00047801078135745363; -0.005589059838849102 0.009865529552361578 0.0029685521280004247; -0.002135342708944216 -0.00031754187968954816 0.002461803018053991; 0.011579136728378087 0.011260875617633156 0.003878936112115692] %
+
+Mass Used: 117.9407338760675 kg
+Launch C3: 103.12792884831397 km²/s²
+||V∞_in||: 0.0013266935509318827 km/s
diff --git a/archive/ES_0.6167349241519442 b/archive/ES_0.6167349241519442
new file mode 100644
index 0000000..83b1eba
--- /dev/null
+++ b/archive/ES_0.6167349241519442
@@ -0,0 +1,22 @@
+archive/ES_0.6167349241519442---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T05:31:39.157
+Launch V∞: [6.854135962753329, -7.2366529597566585, -1.2292963523701004] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0014888462359538604, -0.002489143520865722, 0.004372600431114507] km/s
+ V∞_out: [0.0026039322233748015, -0.003282555048163961, 0.003158318860011338] km/s
+ time of flight: 1.129245447424227e8 seconds
+ arrival date: 2027-12-03T05:27:23.157
+ thrust profile: [0.9691402143717996 -0.45407609311724473 -0.4585838587451334; 0.291102556534841 -0.00036359344387672536 -0.30149570992955127; 0.22178868617045128 0.045141753727639906 -0.3462905625268208; 0.1489153956953765 0.048507197111703565 -0.30705113214364704; 0.09592689866293955 0.03917339675116007 -0.2426519376967512; 0.0390104273494662 0.017784787815749842 -0.11545999153162674; 0.015085585816644065 0.007488152145512291 -0.050446205291116195; 0.008893710970493296 0.00482651468756923 -0.03329778616722539; 0.017240654589172424 0.009527754331090908 -0.06686316154450024; 0.0010004625151025653 0.00044127602650006874 -0.003386455796815574; 0.0013350314978876126 0.0009555828041092613 -0.006627289570185069; 0.000143354187200401 0.0007323563963710521 -0.002567918218498551; -0.0008551111118079633 0.00031575555742023766 0.0007910473565601315; -0.000711936609610248 0.00022435937717013867 -0.002843694623597148; -0.002280992918543192 -0.0019472479572376369 0.00014275898390769348; 0.0003886049883313043 8.163722996485853e-5 -0.000876074467869969; -0.00017986833269844997 -0.00015601025154128503 -0.001293549608502312; -0.00014232478330291996 0.0019019477302579068 0.002334374861591556; -0.0008291419014921935 0.001335339758062108 0.001249510041920584; 0.0010312500626961708 -0.0011071299264829278 0.0028645433953236616] %
+
+Mass Used: 131.17702180668812 kg
+Launch C3: 100.85949537781374 km²/s²
+||V∞_in||: 0.005247107118400057 km/s
diff --git a/archive/ES_0.6168333797010791 b/archive/ES_0.6168333797010791
new file mode 100644
index 0000000..694989f
--- /dev/null
+++ b/archive/ES_0.6168333797010791
@@ -0,0 +1,22 @@
+archive/ES_0.6168333797010791---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T16:31:06.574
+Launch V∞: [5.324275881360735, -8.652645702510283, -2.014286421397355] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.04499644535589043, -0.0008315158566826979, 0.031296164456499506] km/s
+ V∞_out: [-0.05361147589291145, 0.0004381383812819933, 0.011404675210984212] km/s
+ time of flight: 1.1453124767763905e8 seconds
+ arrival date: 2026-12-09T06:45:13.574
+ thrust profile: [0.46015537877817303 -0.33965475218137625 -0.27796050235205394; 0.25074786264562066 -0.048559898442519935 -0.27566317748939934; 0.1360539107876334 0.002680333030324237 -0.21826860356691405; 0.08569925067990558 0.012241084279097666 -0.17614476944131852; 0.079695616441183 0.017638433302342535 -0.1936324408069221; 0.02983980357924878 0.008905417169028141 -0.08706055817856446; 0.028260634370504484 0.009788607601474313 -0.08925530265628367; 0.005603373312906546 0.0020659389269254923 -0.023479043244516957; 0.019704177185206926 0.009241249518327223 -0.07074412584904802; 0.007780449927415218 0.0034228920238898036 -0.030257772960855137; 0.004727881077415275 0.0007697100102487545 -0.01572184990456041; 0.003152586614620089 -0.00018632303454811866 -0.0036666760619731365; 0.0019380312354491027 -0.004467063604823459 -0.0004334207660250532; -0.0004908368896763017 -0.0007026000176763189 0.002066334719811494; 0.0010649704928370391 -0.00043895605270560865 -0.0036999607794577505; -0.0016167018221726471 -0.0015543659264777487 0.00244988095406104; -6.565738011712132e-5 0.0052915445864083486 -0.004579860266535878; -0.0015009465682379029 0.0015989608836109023 -0.007856556212471302; 0.0007504121205624723 -0.0038359445788372993 -0.003215016793608227; -0.008309522910571332 -0.002726566342304994 0.006782044056408714] %
+
+Mass Used: 93.8766198928879 kg
+Launch C3: 107.27354110143504 km²/s²
+||V∞_in||: 0.054816251449490885 km/s
diff --git a/archive/ES_0.6169094732262506 b/archive/ES_0.6169094732262506
new file mode 100644
index 0000000..4ef7a2f
--- /dev/null
+++ b/archive/ES_0.6169094732262506
@@ -0,0 +1,22 @@
+archive/ES_0.6169094732262506---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T15:13:49.186
+Launch V∞: [5.250333030678321, -8.389617183713884, -1.374157220127884] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.99026295328504e-7, -3.5979028846788946e-6, 6.909466388481232e-5] km/s
+ V∞_out: [2.8142852513363164e-6, -6.907031597221194e-5, 8.570040740357343e-7] km/s
+ time of flight: 1.1484191433514076e8 seconds
+ arrival date: 2026-12-09T19:45:43.186
+ thrust profile: [0.884313262190196 -0.6482861377756556 -0.4541869953070386; 0.36595433275240596 -0.06107153747536766 -0.34856078207695085; 0.2201173876389459 0.012148673719104932 -0.30484455577395064; 0.1718357658218055 0.03090567690538605 -0.3021136572246518; 0.08402958372214048 0.022049486282129622 -0.18365662416294648; 0.03296216541276766 0.011182508405305311 -0.0802395710245306; 0.015392168780455321 0.005302963383289735 -0.04044022869142685; 0.01782798713148226 0.007828891369327498 -0.05561516499948772; 0.02719041703668968 0.013587372202082866 -0.08724221517042446; 0.005162251874711955 0.0022371488277840175 -0.01569959961067255; 0.00041911090145239937 0.001718535739682516 -0.0035595017241478195; 0.004045299634768895 0.0019770102627409978 -0.013814241739239293; 0.0036601955812399665 0.0021877539638442945 -0.015058515227880955; 0.004303473217030137 -0.0030422485164794573 -0.00515595308705127; 0.009166911919576744 -6.33812163888136e-5 -0.011610032409385893; -0.0032229489484647857 -0.000501811976946684 0.0037152944847043687; 0.0035070284615286093 -0.001151031460762697 0.0003085263615116209; 0.0010289567580108578 -0.0011756953780785 -0.002031868700706826; 0.0029005084028485614 0.003518426715059614 8.143147721140827e-5; 0.004489751984909647 0.0053452283730648425 0.0033433046184348694] %
+
+Mass Used: 137.3278267510418 kg
+Launch C3: 99.83998148792867 km²/s²
+||V∞_in||: 6.919007522590358e-5 km/s
diff --git a/archive/ES_0.6170944451044339 b/archive/ES_0.6170944451044339
new file mode 100644
index 0000000..4265eb6
--- /dev/null
+++ b/archive/ES_0.6170944451044339
@@ -0,0 +1,22 @@
+archive/ES_0.6170944451044339---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T03:37:15.688
+Launch V∞: [5.182073060942285, -8.826120220520261, -2.1370388654416543] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.06435178511074396, 0.03956867649204588, -0.03684240454638238] km/s
+ V∞_out: [0.053913005780802256, -0.05120727051327693, 0.03869044618047655] km/s
+ time of flight: 1.136795600247473e8 seconds
+ arrival date: 2026-12-01T21:16:35.688
+ thrust profile: [0.4730980827275077 -0.3764099575633913 -0.31574267571401127; 0.17850411174559128 -0.04708069438120659 -0.2247124741027383; 0.1089015798738865 -0.008448017137241175 -0.20206658301158803; 0.06326456210624301 0.0010486301936406912 -0.1522485402626419; 0.03319235069326703 0.002332075612874784 -0.09636150053726368; 0.025490376092807136 0.0029585599126073546 -0.08464480083947408; 0.04384743088923659 0.0061880188846248265 -0.1592207396064638; 0.0140304989036149 0.0022057940800033955 -0.056654739665622726; 0.001654728329600542 0.00014958110863943185 -0.006675608065171396; 0.0005424349697651417 0.0005227371967671769 -0.004576777359336149; 0.0005452682998114419 0.00013766922392497317 -0.0027009312788715536; 0.00010445431031003315 -0.00038525354131743413 -0.0007594705258642674; 0.0016263143147679895 0.000698680205864439 -0.0067545232002250025; 0.00042191760465396726 0.00032064526181701576 -0.0037123594056836873; 0.0009768939996570272 0.00013451397567583657 -0.0019267055293463343; 0.00016370342319242632 -0.0004181981910948824 0.0014184660777256408; 2.4698709458427417e-5 -0.0006557320451506548 -0.0025955235556360113; -0.00014765304689418318 -0.000565182279534364 -0.001010842874582695; 0.0003718160086601005 0.00010824594199038053 -0.0014850255786703832; 0.00015559609731271304 0.0002496019021763925 -0.00012681935776182138] %
+
+Mass Used: 82.23643488933976 kg
+Launch C3: 109.32121446842854 km²/s²
+||V∞_in||: 0.08404876667168204 km/s
diff --git a/archive/ES_0.6172127745229339 b/archive/ES_0.6172127745229339
new file mode 100644
index 0000000..cd0402b
--- /dev/null
+++ b/archive/ES_0.6172127745229339
@@ -0,0 +1,22 @@
+archive/ES_0.6172127745229339---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T15:55:37.804
+Launch V∞: [5.290932289932037, -8.54031779169972, -1.6630262924142343] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.082735991958872e-7, -2.0622856935936785e-7, -2.466226965498633e-6] km/s
+ V∞_out: [1.807580466953884e-6, 1.484691667353327e-6, 8.532982821749979e-7] km/s
+ time of flight: 1.1764755877919678e8 seconds
+ arrival date: 2027-01-13T07:48:15.804
+ thrust profile: [0.5626069556226371 -0.4133489927235899 -0.31409508045197576; 0.2146694302177234 -0.035775497116974204 -0.22536988349669684; 0.11177347125755747 0.0055000148886058635 -0.17390707843396544; 0.15929100065879184 0.026552522890387852 -0.30600777773589694; 0.08097066822917719 0.020280672231568157 -0.1900102130724307; 0.03192749496697079 0.009091681476972287 -0.0858369265895917; 0.022248306910620644 0.008559793328858511 -0.06757437948601973; 0.02113112605394471 0.003399975510748975 -0.05625258991358665; 0.03214854787472136 0.01343809378478854 -0.10861983671151064; 0.019011481888869013 0.008153700467447638 -0.07320096771476632; -0.002220471997994663 0.0031069763725299166 -0.0021851450108322464; 0.0034788740118237875 -0.01193556154489526 -0.00908329909962683; -0.004592619634686778 0.024355737712130926 -0.027925168424950006; -0.014928300047447428 0.0030823920155251495 0.01108246652554149; -0.004865951422725458 -0.0030648291159050753 0.004378877592253064; 0.012199591423309078 0.022026060866967505 -0.016705260122721503; 0.016157712669144002 -0.0028457638720485318 -0.002063291342436463; -0.005618875552928799 -0.006456104897470824 -0.02932377870230641; 0.03277147974724182 -0.0026519353504302866 -0.006148162564976942; 0.009634379284881504 0.0011062098514064754 -0.006433330865944168] %
+
+Mass Used: 115.18445152350205 kg
+Launch C3: 103.6966489291293 km²/s²
+||V∞_in||: 2.493960360577889e-6 km/s
diff --git a/archive/ES_0.617497145325734 b/archive/ES_0.617497145325734
new file mode 100644
index 0000000..dd204c3
--- /dev/null
+++ b/archive/ES_0.617497145325734
@@ -0,0 +1,22 @@
+archive/ES_0.617497145325734---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T13:45:20.142
+Launch V∞: [7.086063528663971, -7.356071749317064, -1.651788853710744] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0014521614307489775, -0.0024170034296895466, 0.004039122319078711] km/s
+ V∞_out: [0.0024510191892153565, -0.003066771055946131, 0.0029693004846860567] km/s
+ time of flight: 1.1388694338615955e8 seconds
+ arrival date: 2027-12-15T17:01:03.142
+ thrust profile: [0.45688769933950685 -0.20273673282480448 -0.2166708631718007; 0.1755508983939818 0.002550704424541759 -0.1765220727761265; 0.09166268771383011 0.02070125362807938 -0.14453296109678296; 0.051257230906062434 0.01832396006071883 -0.1101123552411906; 0.052673188571433945 0.023850197623396262 -0.13583249262610594; 0.10153381917945158 0.03690518413832749 -0.23714976456125747; 0.1693307959260931 0.04023457965468357 -0.42698326649520396; 0.018973893336449697 0.010415304939478464 -0.06775798125403855; 0.014807803437123084 0.006441002183212401 -0.05430884033221492; 0.00011478186356925874 0.0007171212935958311 -0.0033853788428548294; -0.00011332689584898331 8.67964521519603e-5 0.0005162447265114996; 0.0020999043499940074 -0.0015297960841323213 -0.0007362182194820752; 0.0008068784512992836 0.0006501461057365284 -0.002679839947639354; 0.00015072301384266894 -0.0001519945726741333 -0.0003058523857702454; -2.8630896679201026e-5 -0.0006330011813061181 -0.0012822590444758635; 0.0027109145762523137 -0.00032786492487167103 -0.0009472011356537913; -0.0016352728349015478 -0.0004136863584587397 0.001603637320838653; -0.0026027376353133487 0.002445031947463804 -0.005489007733958256; -0.00015078453167875438 -0.0015379894842659197 -0.005299668430600533; -0.0006175530853770433 0.0006001934661590469 4.954373534284861e-5] %
+
+Mass Used: 95.94045261815836 kg
+Launch C3: 107.05249433060534 km²/s²
+||V∞_in||: 0.0049259707173881714 km/s
diff --git a/archive/ES_0.6175047465428108 b/archive/ES_0.6175047465428108
new file mode 100644
index 0000000..6b6c64a
--- /dev/null
+++ b/archive/ES_0.6175047465428108
@@ -0,0 +1,22 @@
+archive/ES_0.6175047465428108---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T10:24:29.092
+Launch V∞: [7.063660776668379, -7.401237435651786, -2.0157836423453364] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.15720249577233605, -0.7193480188791954, -1.2348131714123747] km/s
+ V∞_out: [0.629470343921383, 0.27581247557240374, 1.2627228335129035] km/s
+ time of flight: 1.1261038148268062e8 seconds
+ arrival date: 2027-12-01T19:04:10.092
+ thrust profile: [0.4568405053982184 -0.23437323301453575 -0.273467911273713; 0.21567134733569762 -0.014976915286796975 -0.26964210058137045; 0.15798851491978289 0.016873687640746832 -0.30298444037806754; 0.06130119485738677 0.013779338124301753 -0.15369871114708858; 0.05280781334203174 0.015039177761591103 -0.1606343466030387; 0.03765013434239772 0.012703976645910041 -0.13268602115659725; 0.016891434173495454 0.007092659799416947 -0.0682423759636451; 0.0065466066434333 0.00282465265898612 -0.026788636842114782; 0.0031342470834915034 0.0011672605702845761 -0.01621707611348508; 0.001077291458410153 0.00010194570193951148 -0.00441219293486844; 0.0069709176954646564 0.0031649688436233784 -0.028196854599507135; 0.0008528377226158621 0.00023312970358257815 -0.003880623724639225; 0.0012693133763235092 0.0009480304824455758 -0.001113087616247895; 0.00032419533257421794 -4.261469425481104e-5 -0.0010670124344250552; 0.0033519232003148543 0.0035258543324288654 -0.004503955469458963; -0.0004770788888290927 -0.00012472707631651982 0.0007493366921166888; 0.00039702948127824135 -0.0006401130087741957 -0.0020228575025892617; -0.002655503072846058 0.0029975868092866694 -0.001144750733525813; -0.0026227309666377206 0.0007810217568819434 -0.0031512305931160646; 0.0015244554705372891 -0.0013917942914635395 -0.002346128276698626] %
+
+Mass Used: 86.12302106962397 kg
+Launch C3: 108.73700283948378 km²/s²
+||V∞_in||: 1.437684862977962 km/s
diff --git a/archive/ES_0.6176155829974161 b/archive/ES_0.6176155829974161
new file mode 100644
index 0000000..11327a2
--- /dev/null
+++ b/archive/ES_0.6176155829974161
@@ -0,0 +1,22 @@
+archive/ES_0.6176155829974161---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T14:12:50.455
+Launch V∞: [5.284155876320824, -8.74777693481572, -1.7295853073296408] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004450015091116259, -0.004328098874704782, -1.0663320858590766e-5] km/s
+ V∞_out: [0.0018555217876617795, -2.5372619697857533e-5, -0.005887056571276364] km/s
+ time of flight: 1.1330979550410981e8 seconds
+ arrival date: 2026-11-26T01:09:25.455
+ thrust profile: [0.42847885206972086 -0.33392815667622294 -0.2699361064991671; 0.22711960336025802 -0.05444914864960813 -0.2621026727323627; 0.1619572014404048 -0.007088780396345962 -0.2708811820026917; 0.10378451693686211 0.006234125403197078 -0.22314349491588165; 0.10072996836352915 0.012745475207203316 -0.25616021883810675; 0.043657008219710795 0.0073280484094250045 -0.12901009909344793; 0.009793773066897628 0.0023482478091509788 -0.034112431890705924; 0.007008355976762468 0.0007664910752973068 -0.018766009304723177; 0.008211588703796747 0.002270281575436541 -0.03232555041216407; 0.002395937841118622 0.0008479558273601293 -0.010708217920635248; 0.001851488591670795 0.001732613896872366 -0.007655528568094768; -0.002285538169891032 -0.0008343295290301443 -0.006799872443483363; 0.0008951153133898672 0.0010544596766174016 -0.004604599732944333; -0.00015673320569108314 0.000916049144583939 -0.006129915723804824; 0.0015025576516505797 0.0006133358470853442 -0.0059264350121832655; -0.0007427886464117907 -0.0008748384401537003 -0.000498446670613828; 0.001397031345870566 -0.0037192551711003746 -0.003181600732737096; 6.820547399682552e-5 -0.0011618732223612135 0.0003482242321206086; 0.0005701819177667171 0.0005503264293733427 -0.0019473389112249512; -0.001526557591317966 -0.0013779446764172255 -0.005717070267639833] %
+
+Mass Used: 93.83352205268329 kg
+Launch C3: 107.43736996188038 km²/s²
+||V∞_in||: 0.006207671696118843 km/s
diff --git a/archive/ES_0.6177360477804267 b/archive/ES_0.6177360477804267
new file mode 100644
index 0000000..01ba692
--- /dev/null
+++ b/archive/ES_0.6177360477804267
@@ -0,0 +1,22 @@
+archive/ES_0.6177360477804267---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T20:40:05.023
+Launch V∞: [5.32800386919152, -8.721615038110999, -1.5386711729939877] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.022001281938764935, 0.01452195637843137, -0.0006928857666292247] km/s
+ V∞_out: [-0.007199905481891024, 0.0001139439554223504, 0.025379786728415024] km/s
+ time of flight: 1.1321333703795792e8 seconds
+ arrival date: 2026-11-24T04:49:02.023
+ thrust profile: [0.39195911532356914 -0.297584847505946 -0.23398349598689794; 0.26367086063144385 -0.057254032155884184 -0.28927418857371706; 0.1787210135708474 -0.0024815619765578517 -0.28577880223492547; 0.13047899910407748 0.013234079282670376 -0.26304667721247094; 0.08500057783555748 0.014136778957571651 -0.2074377920397077; 0.055360835530066765 0.013002309160187681 -0.14464018669771764; 0.036863164285305464 0.0084182165166477 -0.11409197961797127; 0.017356213812729962 0.004909359424314802 -0.059276778742835996; 0.0006982461460463465 0.00021511746707475357 -0.0030858781045980236; 0.003566316721079822 0.0010958589064471887 -0.013609681179807435; 0.0006109188822021932 0.00043418525813261393 -0.0011681150762362592; 0.0005527525633691365 0.0011522467118801206 -0.004242377721398292; 0.000408982821502114 0.00042799037730284527 -0.001304509074089614; 1.337675687972914e-5 0.00029714339388308976 -0.00045516952702224947; 0.0002070923121884598 2.0846265571404423e-6 -0.0005075988038644952; 0.000346516271540871 8.680207755398925e-5 -0.0016048649276752453; 0.00042581754109984743 -0.0009260197567012235 0.00017880102219947243; 0.0006198410649167242 -7.917324923935938e-5 -0.00035626621993844814; -0.0001550471399666102 -0.00016273933459518106 0.0001882147914257159; -0.0011072542695134838 -0.000542068755377877 -0.0001662390000981887] %
+
+Mass Used: 97.56545443376035 kg
+Launch C3: 106.82170308172643 km²/s²
+||V∞_in||: 0.026370887635642548 km/s
diff --git a/archive/ES_0.6177447574889972 b/archive/ES_0.6177447574889972
new file mode 100644
index 0000000..fab24ac
--- /dev/null
+++ b/archive/ES_0.6177447574889972
@@ -0,0 +1,22 @@
+archive/ES_0.6177447574889972---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T14:23:31.202
+Launch V∞: [7.009211720232806, -6.910079728508601, -0.29583880334338625] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002002926328147358, -0.00291568737765755, -0.0002499256460485314] km/s
+ V∞_out: [0.00023389895226943306, -0.0011331101284642803, -0.003350047578897057] km/s
+ time of flight: 1.3671747610867378e8 seconds
+ arrival date: 2028-09-02T23:28:07.202
+ thrust profile: [0.45323467708107074 -0.14603085212699762 -0.17789299465203323; 0.194601191561147 0.03538647420343979 -0.1921835776353357; 0.15677571442638022 0.07022456806562496 -0.2513737112547881; 0.10242811973127085 0.057743724351784854 -0.20594691650959446; 0.07849594012371368 0.04883576795327323 -0.19221469336562372; 0.06418527480898882 0.06258383798265342 -0.24550952038317905; 0.0371257975141477 0.04168273610744346 -0.1649246988157082; 0.013568688913991628 0.008094819470986642 -0.05576132748255236; 0.0027654002193214272 -0.0038639664331410195 -0.005334420439501602; 0.01918912392533797 0.025246532203011415 -0.013106827822836536; 0.01344935246260939 0.015897892756120743 -0.07387050620090202; 0.04417114420597643 0.00185690699040226 0.002454103944409791; 0.051808137692743624 -0.02903583967132867 -0.018572529656773366; -0.012170892487920654 -0.0036106248820859197 -0.004904064778645748; -0.009141744830228261 -0.0047834889674437005 0.039693272104181485; 0.027827659025466314 0.03947611651430098 -0.02796548302834502; 0.002235433338646868 -0.023950430356671146 -0.09437893777648805; 0.024569133965316032 0.028600363991244517 0.07649797757436146; -0.017947815702252654 -0.07315698893152581 0.06306861403985178; 0.039461504559884494 0.13541803167114475 -0.14169949395982326] %
+
+Mass Used: 155.0685506232412 kg
+Launch C3: 96.96577139095808 km²/s²
+||V∞_in||: 0.003546182396432845 km/s
diff --git a/archive/ES_0.6178043729695115 b/archive/ES_0.6178043729695115
new file mode 100644
index 0000000..2c3a113
--- /dev/null
+++ b/archive/ES_0.6178043729695115
@@ -0,0 +1,22 @@
+archive/ES_0.6178043729695115---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:42:48.671
+Launch V∞: [6.982733114004289, -7.385810325483184, -1.8998581175770215] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.18272713898168524, -0.853968100829557, -1.392103994521234] km/s
+ V∞_out: [0.7208070756594436, 0.3307693791563174, 1.438908180745001] km/s
+ time of flight: 1.1524925410305357e8 seconds
+ arrival date: 2028-01-01T06:23:42.671
+ thrust profile: [0.4920439515668175 -0.231800500032079 -0.2727196640298442; 0.20102398459587145 -0.0027561975802464587 -0.23787502392421467; 0.13599093915854116 0.02452712920299356 -0.2470520226411428; 0.08678497814883372 0.025278682552032156 -0.210103214417597; 0.04406724111085913 0.016132992880052533 -0.1338807171997987; 0.019115530644137717 0.0076994542399346595 -0.06908483721327534; 0.04689639468074737 0.021156707323317907 -0.18138078416958672; 0.014235243952081563 0.005632009652650433 -0.05412335448405364; 0.012996983200448323 0.0060248849367681885 -0.018315597517498765; 0.011302098035524103 0.001921049071479005 -0.028330397962502096; 0.007787320666757424 0.001012493634682999 -0.01912061706044051; -0.01042386000193872 -0.0031079100141048967 -0.012596086173531971; -0.0014210238772104132 -0.0019449703063715218 -0.004753857308754612; -0.002325897644596113 0.008323749050207399 -0.014418596878454447; -0.0011099686562403184 -0.001146933338762656 0.0061588702528537365; 0.003752968231207191 0.0008095045134824758 -0.009093598226234251; 0.007915846613858886 -0.016862932403528715 0.008259255830425223; 0.013802584986615817 0.0006732012045452926 0.03210602598192192; -0.013450433963045317 -0.0015574826932551167 -0.003911696955602434; 0.010339221560219823 -0.02291845582028199 0.007071896841008792] %
+
+Mass Used: 97.08217062572567 kg
+Launch C3: 106.91821677234934 km²/s²
+||V∞_in||: 1.643351531510178 km/s
diff --git a/archive/ES_0.6179214598954907 b/archive/ES_0.6179214598954907
new file mode 100644
index 0000000..168c05c
--- /dev/null
+++ b/archive/ES_0.6179214598954907
@@ -0,0 +1,22 @@
+archive/ES_0.6179214598954907---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T06:39:13.496
+Launch V∞: [6.96805366001703, -7.19880843953545, -1.2692246340175621] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0001129343474356995, -0.00018280392458995317, 0.0002589904769616217] km/s
+ V∞_out: [0.0001382186524056793, -0.00025735640354834934, 0.00016515507437462666] km/s
+ time of flight: 1.1998758314495814e8 seconds
+ arrival date: 2028-02-23T00:32:16.496
+ thrust profile: [0.5241736736304781 -0.23250733721351044 -0.262379125775258; 0.2869211342638839 0.007694232337893605 -0.3125899560734117; 0.11622599059206264 0.02516429288594473 -0.19879479314118617; 0.12368905643468946 0.0425270762576338 -0.2787265042549169; 0.09178824364487054 0.03851020817068409 -0.25281337617570654; 0.06437608905364228 0.02987575677913794 -0.2055234222286792; 0.026419749188884768 0.01505950116852254 -0.10069274659525891; 0.018521768613542954 0.008175358046956866 -0.07546290907181237; 0.006573189431908884 0.000696095389952283 -0.01939410000658206; -0.0006472336024761736 0.0038490674507362624 -0.020616781039609233; 0.003058401036959947 -0.005597323868539341 -0.002140501910538172; 0.009996557691183891 -0.0027341545964677545 -0.001689639000761607; 0.0019186325244763443 0.0007386909270148383 -0.004655212069736603; 0.04113986296505396 -0.004861980010866033 -0.001955820374297354; -0.02102154992073727 0.016900020161875005 0.004221955034428182; 0.04745247915242141 0.034557934838432974 0.015092883447743191; -0.0020839511132362248 0.004978267247909493 0.013768532257668442; -0.034517347099425055 0.032811270729571566 0.01525323584331855; 0.00506170395637936 0.01724242706206778 0.06938762827169456; 0.018903762010992406 -0.0008965728080391026 -0.03545148642930872] %
+
+Mass Used: 125.98101862206931 kg
+Launch C3: 101.98754592960056 km²/s²
+||V∞_in||: 0.0003365226720936122 km/s
diff --git a/archive/ES_0.6180997792539304 b/archive/ES_0.6180997792539304
new file mode 100644
index 0000000..3575ef1
--- /dev/null
+++ b/archive/ES_0.6180997792539304
@@ -0,0 +1,22 @@
+archive/ES_0.6180997792539304---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:26:18.563
+Launch V∞: [7.028727852528583, -7.502187771362353, -2.2116002848406295] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01828159400491918, 0.01833358538283514, 0.0019462933138332946] km/s
+ V∞_out: [-0.006343944393904071, 0.024637556510288615, -0.005183370516234557] km/s
+ time of flight: 1.1327194745605606e8 seconds
+ arrival date: 2027-12-10T16:52:05.563
+ thrust profile: [0.42759774454852506 -0.21054837932162176 -0.25505025892900207; 0.13434658546520423 -0.006401096893874312 -0.17524179198879317; 0.07918485727244545 0.010318656637443281 -0.15964030905117824; 0.04118903236222917 0.009330904127765237 -0.10817891727365993; 0.05865550815017231 0.020097552543446143 -0.18833393622861852; 0.026708852458693703 0.007399790090811946 -0.10201970895176253; 0.031804899212275965 0.012764140829250438 -0.14567969789133436; 0.005477006956802138 0.0021167941736661144 -0.02560005036632802; 0.002726278327142847 0.0009516371621638243 -0.014872316647269049; 0.01881903345467274 0.0068343221722517705 -0.09374364267368451; -0.00015874444750506368 0.000573852606287396 -0.005293931085460892; 0.001130810613913374 0.0007713485880952665 -0.009584539914522665; 0.0021579482015468584 0.0015108117243557888 -0.005060840726691624; 0.0002556433088711065 0.00013886473121933697 -0.0017751634201967196; -0.0010947329545319747 0.000864433575599605 -0.0008252962367469245; 0.00024689548928387114 -0.0021760692880348612 -0.0008567269957832297; -0.001332239524301732 0.00034494357661891755 0.0053398678889774; -0.002269480490016245 0.001010410005294112 -0.003918469372872107; 0.0001045158309786352 -3.430255578761184e-6 -0.00012968258790559475; -0.0018897758437510376 0.00086305763163752 0.002190752180724403] %
+
+Mass Used: 76.08383678693599 kg
+Launch C3: 110.57701240159705 km²/s²
+||V∞_in||: 0.025963919003376117 km/s
diff --git a/archive/ES_0.6181456702764109 b/archive/ES_0.6181456702764109
new file mode 100644
index 0000000..5b09d1e
--- /dev/null
+++ b/archive/ES_0.6181456702764109
@@ -0,0 +1,22 @@
+archive/ES_0.6181456702764109---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-15T13:08:00.440
+Launch V∞: [6.248835798053914, -7.9063350398399885, -1.884492949864358] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005568047307753941, 0.007576834156287118, 0.00809555319294696] km/s
+ V∞_out: [0.011249949517622555, 0.005248784068337825, 0.0002821360267803762] km/s
+ time of flight: 1.4220313464926758e8 seconds
+ arrival date: 2027-10-17T10:00:14.440
+ thrust profile: [0.17488134008634634 -0.10345489119450145 -0.0750560216321723; 0.17389601765031276 0.004485329940460383 -0.16066249385273437; 0.15510300860190387 0.045105471840070736 -0.21988542916310003; 0.12948306151090674 0.060207118943863165 -0.2430712922281511; 0.10286031356455907 0.06141754860355192 -0.2362887294859235; 0.07754411709969926 0.05456140041501062 -0.20754769015007085; 0.054195543581573365 0.042915413036091955 -0.16323237827831868; 0.03273108242798454 0.028326498343591654 -0.10783598287170273; 0.012869561537156774 0.011916002551528814 -0.04534438181238315; 0.0009698395053970867 -0.001291684648165914 -0.006595368138110605; 0.0051234866272308445 0.004198549506825252 -0.006020084609003883; 0.0009329032971965741 -0.0003392456570061866 -0.0031046476426567072; 0.00040519139489644644 0.001566789107168 -0.002744923279487322; 0.011182995232057886 0.0026311354076838976 -0.0076770391297292795; 0.0009555528930692878 0.0011571280621653923 -0.004044157352293331; 0.0073443292050816835 0.0026303170028273183 0.0009845144732395488; -0.00039385542568584923 -1.072047446493661e-5 0.0019205028832339696; 0.0014718811709779204 0.0004044145324653015 0.0001333477794523098; 0.0017343261377141862 -0.005738846154221854 0.008597568382900312; 0.000604122753932475 0.00035421466959746606 -0.0022752790631402862] %
+
+Mass Used: 108.03180373972009 kg
+Launch C3: 105.10939627133016 km²/s²
+||V∞_in||: 0.012407640716635002 km/s
diff --git a/archive/ES_0.6184123798799906 b/archive/ES_0.6184123798799906
new file mode 100644
index 0000000..f020eaa
--- /dev/null
+++ b/archive/ES_0.6184123798799906
@@ -0,0 +1,22 @@
+archive/ES_0.6184123798799906---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T01:06:11.429
+Launch V∞: [6.923517434781375, -7.4566388668759895, -1.8987259395165976] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4081332335422936e-5, -2.2558355688108144e-5, 1.2489031446493441e-6] km/s
+ V∞_out: [2.4809153289406036e-5, -1.657169193373931e-5, -1.4146732611273604e-5] km/s
+ time of flight: 1.1144429807722606e8 seconds
+ arrival date: 2027-11-18T21:51:09.429
+ thrust profile: [0.7111341838537062 -0.34820033154454055 -0.456663257313919; 0.2211028703454244 -0.012011827061518118 -0.27086065071335713; 0.1334773104946429 0.017343101262748798 -0.25077237089466103; 0.06878121958274577 0.016257938711498846 -0.17407416931069206; 0.06798027250494151 0.019261270869778697 -0.20703647500738967; 0.021930533973801854 0.0071405850583680245 -0.07951661543558673; 0.013989698896181091 0.0049450714797415 -0.057607695096439024; 0.00493243696055452 0.0017849614803778409 -0.023076686996936675; 0.00499750800131024 0.0018872655563703072 -0.025069333469431455; 0.0022526796806716168 0.0009657326555883888 -0.012794920056945231; 0.0007712475505480409 0.0003209215202511863 -0.003956777542573505; 0.0005004084983225022 -0.000237783051987706 -0.0013731095291589436; 0.0005352356781092649 -0.00013609010879476557 -0.002652915464998853; -0.0006381775319677226 0.0004385616418454717 -0.00025569977908970304; 0.0006274625349478951 0.0013248552035344246 -9.170382397266814e-5; 6.590792036278439e-5 3.53509519849496e-5 -0.0003056826164194808; 0.0007561451568191725 0.0014735215609668632 -0.0002931794904778813; 0.00046633226730294694 -0.00028711827967366796 -0.0005835437937212035; -0.00010244342199542116 0.00017755279186218995 -0.00040233276475552245; -0.000716541217719462 -0.00020620736682272804 -0.0002638502043871248] %
+
+Mass Used: 96.48776037761945 kg
+Launch C3: 107.14171705412049 km²/s²
+||V∞_in||: 3.30204442348222e-5 km/s
diff --git a/archive/ES_0.6188573297558272 b/archive/ES_0.6188573297558272
new file mode 100644
index 0000000..8e46da4
--- /dev/null
+++ b/archive/ES_0.6188573297558272
@@ -0,0 +1,22 @@
+archive/ES_0.6188573297558272---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:33:01.462
+Launch V∞: [7.033174361776047, -7.4841417087995605, -1.9620222027603256] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006876125367512917, -0.00030276203517407994, -0.0013698215282636557] km/s
+ V∞_out: [-0.000774693470088946, -0.00135360081469226, -4.434942950025981e-5] km/s
+ time of flight: 1.1300548105070315e8 seconds
+ arrival date: 2027-12-07T04:57:42.462
+ thrust profile: [0.435314326614676 -0.2113433348751757 -0.2560262603596453; 0.15943688597692593 -0.005937619223412703 -0.2058118949755255; 0.0958963392894623 0.013712965236449498 -0.19198352399992136; 0.06790158590834289 0.015618567182395543 -0.17123709508331478; 0.07635569077809795 0.023813829690141727 -0.23845659169486708; 0.058158334751456646 0.015087897944682722 -0.19306780940820398; 0.012143629706696265 0.0035483636373886238 -0.05242625940363559; 0.01054248458131623 0.0028562178295759274 -0.047153000745700314; 0.005571343305917273 0.0013155138536285337 -0.02672569973001984; 0.003351302782206228 0.00024180701591403194 -0.019414975082856823; 0.0020721451531261247 0.00213464371808469 -0.003545766584888324; 0.0004235941866779459 0.001478220670156889 -0.00023370718788333703; 0.00022214045816763847 -0.0006226601954158087 0.0031799579100995437; 0.00114670796456301 -0.004471045771727261 0.0014252689947936463; 0.001907644655007014 -0.0032279222776804353 -0.0037716324486017864; -0.00027519045846124144 -0.00040402932415683373 0.0017924625984423051; -0.0020374486740535715 0.001529937459135354 0.002226757715183142; -0.004518433855300525 -0.004680067709610268 0.004533671281582506; -0.0041843355120465345 0.0054373588999787874 -0.0010184914126646098; 0.013156447359932062 0.010954732251834055 -0.013682359001931724] %
+
+Mass Used: 84.2567606212724 kg
+Launch C3: 109.3274498446616 km²/s²
+||V∞_in||: 0.0015623337895388663 km/s
diff --git a/archive/ES_0.6189216499006169 b/archive/ES_0.6189216499006169
new file mode 100644
index 0000000..0ae6606
--- /dev/null
+++ b/archive/ES_0.6189216499006169
@@ -0,0 +1,22 @@
+archive/ES_0.6189216499006169---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T12:00:08.451
+Launch V∞: [6.8904636940825625, -7.203419360738443, -1.521016325650917] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00015924322087820995, 8.419091586634983e-5, 0.00038426135392234206] km/s
+ V∞_out: [0.00019630279993546474, 0.0003760419187550357, 1.2015955482092646e-5] km/s
+ time of flight: 1.1103421560189937e8 seconds
+ arrival date: 2027-11-10T14:50:23.451
+ thrust profile: [0.8589060583489085 -0.41243877214906866 -0.4334605763422914; 0.6080102556608613 -0.0035097537706040224 -0.6076160654586684; 0.25346214183940446 0.05130719758547452 -0.3831891805112581; 0.15427117566528162 0.050133755618707504 -0.3055458103498468; 0.030195502487283848 0.012362715243927605 -0.0756103515269886; 0.01024952070984544 0.0049522592597219485 -0.031887314140108265; 0.005931271034855006 0.0031855272120369336 -0.021266250965169268; 0.005089360645751848 0.0033937143867625126 -0.020025180039528377; 0.007351587583220793 0.004226921908446161 -0.02902923345473436; 0.0007101270493586906 0.0005327075149161732 -0.0036244886673398556; 0.000635343401288388 0.0004130227255121101 -0.003596036560932059; 3.285709097163318e-6 2.0975265960415185e-5 -0.0006449097337230723; -0.00019021952570271122 0.0003614428195442271 -0.0004084684133630012; 5.5777503869718455e-5 -0.0002421117149227823 0.0004086916521881945; 8.945112559706166e-5 5.61668436521483e-5 -0.000170394368412871; 9.206240162404225e-5 6.327117576730126e-5 -0.0006375703663613489; 0.00014747167487091798 0.0002403619736431041 -0.00024473250945557495; 0.0001451229679440954 -0.00013711414879736514 6.116420801926723e-5; -0.00027968648537263766 -0.00027073373705304994 -0.0004933608911973203; -0.00038633155530612504 -0.0006510589133968017 -0.00025698269683708966] %
+
+Mass Used: 128.9347436480566 kg
+Launch C3: 101.68123106902797 km²/s²
+||V∞_in||: 0.0004243857936221624 km/s
diff --git a/archive/ES_0.6189312885483579 b/archive/ES_0.6189312885483579
new file mode 100644
index 0000000..bbdd101
--- /dev/null
+++ b/archive/ES_0.6189312885483579
@@ -0,0 +1,22 @@
+archive/ES_0.6189312885483579---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T21:22:25.059
+Launch V∞: [5.308677945201174, -8.679334598094025, -1.8109929097534916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.371830537785893e-5, -3.0029079789173742e-5, 6.211077790842976e-5] km/s
+ V∞_out: [5.6967026490334976e-5, 5.291435211798441e-5, 2.50129287835988e-5] km/s
+ time of flight: 1.1278855479362004e8 seconds
+ arrival date: 2026-11-19T07:31:39.059
+ thrust profile: [0.5334163364081106 -0.40328178462939285 -0.3084411613863449; 0.26494539938381073 -0.055155214018164346 -0.28743222292157; 0.1409948184269815 0.0001752068277454904 -0.22889801343658142; 0.07975664614403824 0.009463955948754797 -0.16880527181270355; 0.06221267755138975 0.00953317968081812 -0.1533237188326397; 0.03201857758349155 0.00823258107929107 -0.09518909778045842; 0.035643167333223445 0.009857463743723077 -0.11009950190288575; 0.037741256887972564 0.009151333667332642 -0.12460355593870258; 0.018747204419742397 0.005464296987734811 -0.06513377647886133; 0.0017962427667271173 0.0009712649066233924 -0.004451569908983062; 0.0013215510607961648 -0.0016980304642316964 -0.005277743319280336; 0.00011573279281565656 -8.157423780403303e-6 9.260880279957724e-5; -0.0006515190219621156 0.0004905322283740183 -0.0007479236428737008; -1.2577169527490243e-5 0.003817184121494636 -0.010435705864253101; 0.000769592423616056 0.0005760843760710668 -0.0008810237403983601; 0.000396055215010582 0.0023308408044796715 -0.005213247987114863; -0.0015089340811950936 0.0007394549350498744 -0.002230458252733423; -0.0006621089531891992 0.001057467755718475 -0.001559840638097604; -0.0030077972930884793 -0.0005544997110879491 -0.0009925483799124051; 8.639109859044343e-6 9.096588537927338e-5 0.001089083867854554] %
+
+Mass Used: 99.12963549391498 kg
+Launch C3: 106.79260591071474 km²/s²
+||V∞_in||: 8.167487123030301e-5 km/s
diff --git a/archive/ES_0.6189941884454058 b/archive/ES_0.6189941884454058
new file mode 100644
index 0000000..35d1b6a
--- /dev/null
+++ b/archive/ES_0.6189941884454058
@@ -0,0 +1,22 @@
+archive/ES_0.6189941884454058---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T21:18:01.514
+Launch V∞: [6.925763641038587, -7.438546910714806, -1.9711894872554738] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006779346627394372, -0.0011440288269572582, 0.0020697566222685052] km/s
+ V∞_out: [0.0012806984491169798, -0.0015298071688469703, 0.0014448359054994322] km/s
+ time of flight: 1.1188362265148686e8 seconds
+ arrival date: 2027-11-23T20:05:03.514
+ thrust profile: [0.702287655995909 -0.35105312396918725 -0.40093058312518426; 0.20493583301981624 -0.009552292928480014 -0.24300880113370882; 0.12582312613619592 0.01775988229466986 -0.22750685769268758; 0.08312210129727507 0.0205046145913943 -0.1978895964370569; 0.03934242881001291 0.012856348344868734 -0.11335472331395847; 0.056739263146311225 0.01878943166989661 -0.1914200531789127; 0.008218795066807928 0.003655728668739949 -0.03134759656696314; 0.006499865162232568 0.0042363777613595825 -0.03217436088189269; 0.011972473482933456 0.01064665607787134 -0.041612593217994036; 0.0021866259622117783 0.0010327006046517524 -0.010020248630705397; 0.001146543099888062 0.0006267531995179764 -0.002729450271377884; 0.002157901160127619 -0.0003173328239713894 -0.007244530664626601; 0.0003088514078385585 0.0007168082780053131 -0.0037868968796365542; 0.00026371495334191666 -0.0020197059882809338 -0.007908684008331317; -0.0025011795955422467 0.001964105274458447 -0.0037418898824481336; -0.003549053182079657 0.0020485949161911906 0.0016103140467346342; 0.0019849677391676037 0.0021924632710727935 0.0009111686779345318; 0.0063642861924164094 0.00261374939415184 -0.0008900204533838249; 0.00481592349113711 -0.00428664902615554 0.00331181002116654; -0.002204122733787272 -0.006285791647202743 -0.005529413842144942] %
+
+Mass Used: 96.92122731653717 kg
+Launch C3: 107.18377014910335 km²/s²
+||V∞_in||: 0.002460140207239654 km/s
diff --git a/archive/ES_0.6190931418955685 b/archive/ES_0.6190931418955685
new file mode 100644
index 0000000..098cdf9
--- /dev/null
+++ b/archive/ES_0.6190931418955685
@@ -0,0 +1,22 @@
+archive/ES_0.6190931418955685---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T23:21:48.689
+Launch V∞: [6.908377562470089, -7.0482130596697665, -0.5455924491434989] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6393621562735776e-7, 1.0776460995965255e-7, 1.3359788456824117e-8] km/s
+ V∞_out: [2.3066385791756095e-7, -1.2498390599615395e-7, -1.144852828380335e-7] km/s
+ time of flight: 1.1905149280425197e8 seconds
+ arrival date: 2028-02-08T21:13:20.689
+ thrust profile: [0.7215522013954271 -0.31114677179492034 -0.29229129498894246; 0.36100091948539054 0.020400820123586995 -0.3166778604296829; 0.33671013332910876 0.09406268754314968 -0.4505288676631406; 0.376195537582839 0.1562603434275454 -0.6461447765009047; 0.050707128974306036 0.023846023838804464 -0.11828329986554657; 0.011068489805646535 0.0047128995732210735 -0.02569924377668968; 0.011062611747936175 0.004363879834688935 -0.018425668874506147; 0.006912713521130464 0.003388596187653725 -0.013235532681958059; 0.024388466067125934 0.01375329486506583 -0.07022176276294124; 0.002604508842157658 0.006872603176109329 -0.017904170418795978; 0.0062128358813079345 0.004725099311002928 -0.020265877494397164; 0.007086983597074981 -0.0031633569051921634 -0.018419202404913237; 0.015514758713847433 0.010091695727973518 -0.018956248993425424; 0.008122306307243763 0.0019227079925320315 -0.009398395905592997; 0.0034708686889825986 0.01195877490419616 -0.009287460210741144; -0.002286157154452406 0.017571523183050053 0.006429341738028373; 0.01698564176451474 0.012265224266056144 -0.01188071413304617; 0.031525392591684354 -0.023702431340212958 0.015557905885981285; -0.07260636788652898 0.035736213923095825 0.008431219284854952; 0.004507216012463065 0.0004257715848515702 0.004390166793519151] %
+
+Mass Used: 152.35482137406825 kg
+Launch C3: 97.70065900070202 km²/s²
+||V∞_in||: 2.854015084526678e-7 km/s
diff --git a/archive/ES_0.619118222235026 b/archive/ES_0.619118222235026
new file mode 100644
index 0000000..91a5f33
--- /dev/null
+++ b/archive/ES_0.619118222235026
@@ -0,0 +1,22 @@
+archive/ES_0.619118222235026---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T02:21:04.030
+Launch V∞: [5.269335031270047, -8.607430998623435, -1.5133043331683822] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8812372442455568e-5, -1.2391298126578548e-5, 2.644227248319296e-5] km/s
+ V∞_out: [2.4192319768674425e-5, 2.2484159280530372e-5, 1.0708349264223704e-5] km/s
+ time of flight: 1.1459825328679918e8 seconds
+ arrival date: 2026-12-09T11:11:57.030
+ thrust profile: [0.5650152958783824 -0.4199281244725106 -0.3232473156007239; 0.29093940209438346 -0.05904451353347396 -0.31691135227079253; 0.18759122962042757 0.00022690184184786198 -0.29991958195704316; 0.12864142246610094 0.014905201840253167 -0.2649119880441367; 0.06213692866865947 0.011948891127567552 -0.15586395117168794; 0.05997829047473379 0.014882305396990002 -0.16920499897085067; 0.03113769465039357 0.00905402248509142 -0.1000506785895003; 0.004409893524662506 0.001799660212552655 -0.01620593140501388; 0.01148750742871859 0.006884920303127208 -0.04132303006339174; 0.004047325187283573 0.0026482000205076297 -0.013519029801356136; -0.001090324945253116 -0.0002735323644904228 0.003524250835591477; -0.0011038264860359578 0.009559572580246686 0.0024207790201403265; 0.0037783135577831185 -0.0014580940130824902 0.004134012001254524; -0.00046100542139988944 -0.01790355086988308 -0.0003081237817791399; 0.01563435962789207 -0.011479293998346999 -0.00831649999047941; 0.005008142834195232 -0.016223059743061027 -0.00349015960215702; -0.003349619359908483 0.0007602328459833408 0.0010108743792267062; 0.021259908399246852 -0.0009483644296658677 0.0016498401555000287; -0.005663666753019887 -2.786149833174964e-5 -0.00014431915134601554; 0.014450461327452502 0.0028702567075078386 0.018536864220862] %
+
+Mass Used: 114.79880051724967 kg
+Launch C3: 104.14385007261954 km²/s²
+||V∞_in||: 3.473677302587035e-5 km/s
diff --git a/archive/ES_0.6191535652127245 b/archive/ES_0.6191535652127245
new file mode 100644
index 0000000..eba06a4
--- /dev/null
+++ b/archive/ES_0.6191535652127245
@@ -0,0 +1,22 @@
+archive/ES_0.6191535652127245---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-02T21:29:16.718
+Launch V∞: [6.391373033024575, -7.592661856037789, 0.016776871105339444] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8582078404865137e-7, 4.771853382365994e-8, -6.050637074266155e-8] km/s
+ V∞_out: [1.9373788652576166e-7, -4.86981150486479e-8, 2.426705491908171e-8] km/s
+ time of flight: 1.8393882525605264e8 seconds
+ arrival date: 2029-02-28T19:36:21.718
+ thrust profile: [0.1943793682912686 -0.07165834817253139 -0.06566090915334023; 0.09047049384753277 0.09050781000674532 -0.014568347073951039; 0.009155149658652863 -0.010438136550214507 -0.0454775278757411; 0.03085956560500499 -0.005659974100338611 -0.0792293743671805; 0.01746862680361731 -0.010235266198677494 -0.06675891753458289; -0.016566235872967662 -0.012976832412670558 -0.029510443239439254; 0.018613545928896094 0.09443033199544254 -0.04291213051103289; 0.01626878657591351 -0.01815668808466127 -0.12676480429510442; 0.08755921267457334 0.06090239318749957 -0.07737312322110973; 0.0035833214133381627 -0.014071289884522161 -0.05516592256339695; 0.024310948486015088 -0.023284759413780595 -0.07906206414242525; 0.022784713896892246 0.007197624325757373 -0.09724830083327111; 0.014653820681754 0.0018313212626211075 -0.10922530804976091; 0.02780955094951383 0.05518204193354144 -0.07520252771697132; 0.05917240146368348 -0.08051075088464868 -0.048835678961762434; -0.09202116666908824 0.05924482123158176 0.02049091020555114; -0.05228445457423975 0.02959557250742745 -0.06375392402544772; -0.017659901982860403 -0.04241609148742411 -0.022355613053700204; 0.024494692324692452 -0.01622294885938727 -0.0016651886595341059; -0.061499333793469044 0.20632657581804087 -0.06564171805862631] %
+
+Mass Used: 147.77156491845926 kg
+Launch C3: 98.49844477080903 km²/s²
+||V∞_in||: 2.0116521358123456e-7 km/s
diff --git a/archive/ES_0.6192980816159158 b/archive/ES_0.6192980816159158
new file mode 100644
index 0000000..abc4fe7
--- /dev/null
+++ b/archive/ES_0.6192980816159158
@@ -0,0 +1,22 @@
+archive/ES_0.6192980816159158---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-26T04:59:42.667
+Launch V∞: [7.445874511594667, -5.7069224663851115, -0.010962514675711034] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.6725416760896386e-6, 1.0636458296567344e-5, -0.0002602751428500439] km/s
+ V∞_out: [-1.0099374882463938e-5, 0.0002613423910286846, -1.733606579553523e-6] km/s
+ time of flight: 1.8749577786894897e8 seconds
+ arrival date: 2030-04-05T07:09:19.667
+ thrust profile: [0.7642869395363456 -0.02793413330746127 -0.07441178703173341; 0.59181197306459 0.4232937131431632 -0.1924129055479611; 0.26684980789017304 0.3368656154711377 -0.16595187235918094; 0.14333354027590434 0.26656416469822464 -0.1456691265993507; 0.057209805385207806 0.14986785007425105 -0.09329775272740924; 0.017567316454513388 0.06295073615388294 -0.042882288473135764; 0.029633291409569863 0.14338940889856683 -0.09904056760954605; 0.0016966418526899786 0.011350668098921622 -0.008910977693927052; 0.000529494430566517 0.005187831340621581 -0.004236322572289032; 2.2581736118913268e-5 5.648727415989772e-6 -0.00011414038444327972; 0.00026682687949475703 0.010320259309120934 -0.009164257099865463; -0.0007411523261552062 0.0008547454617194297 -0.0006495883888730384; 0.0002822661689473507 0.0005437803499406626 -0.0002564124504805558; -5.647054665621485e-5 0.0005026600235891568 -6.244140040316591e-5; 2.07857502028232e-5 -0.00021958652000673545 5.653609109191872e-5; -5.7188798955262255e-5 -0.0005545850749261187 -1.149286351481818e-6; -9.846015704974281e-5 -0.00010050822256095916 -0.0008129164790423952; 0.0010085759168341844 -0.0007248069842846883 -0.0007064746211673798; -0.00023336746698976007 0.00146146984153788 -0.0009522605256318738; 0.00023866860599722472 0.00029049361144651686 0.00027490330799377817] %
+
+Mass Used: 209.12199505580202 kg
+Launch C3: 88.01013145647426 km²/s²
+||V∞_in||: 0.00026049775743058445 km/s
diff --git a/archive/ES_0.6194188579955904 b/archive/ES_0.6194188579955904
new file mode 100644
index 0000000..5ec8a6e
--- /dev/null
+++ b/archive/ES_0.6194188579955904
@@ -0,0 +1,22 @@
+archive/ES_0.6194188579955904---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-25T01:33:56.219
+Launch V∞: [6.806626620957754, -6.672480918811857, -0.8620837961313945] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005000746203327658, -0.0029375331874407066, -0.00018287209378752472] km/s
+ V∞_out: [0.004048116499541846, 0.002369721039008859, -0.0034080254645129284] km/s
+ time of flight: 1.2433861678823818e8 seconds
+ arrival date: 2028-04-03T04:04:12.219
+ thrust profile: [1.0 -0.4486202129937568 -0.35288476047617234; 0.9289756557238491 0.1421873927579807 -0.6146145735255429; 0.4572021416016832 0.1962019305628204 -0.46795471331166144; 0.353285865370649 0.21785535470390427 -0.47903581390485817; 0.02801237804136243 0.021676897993061228 -0.052617164365858185; 0.02019975101600652 0.0180614707895361 -0.04435454956142894; 0.00492642402823496 0.00523905976240338 -0.012340249492414345; 0.004501260172014659 0.006068766692635806 -0.014254702561443277; 0.004572540411925846 0.001793806327330967 -0.008282312878524628; 0.00361782452064258 0.004292804757293138 -0.011770831089172422; 0.0033780880020819032 0.0012290888263201594 -0.0029349464027963734; 0.00280414114785176 0.00291667178894524 -0.003278508744881635; -0.0006786110207144134 -0.0014613755779116706 0.00223669314256218; 0.004956509451930663 0.0032774508522657266 -0.0030052766368503956; 0.0025152768891065535 0.0025682721176714133 -0.007962062867584522; -0.0007165937484077969 -0.0019071477152233876 -0.0003566790158322766; 0.0011822588868356575 -0.00018995843818382218 0.0019080977129715647; 0.003672561762739644 0.001099819117957055 0.0026697358962399892; 0.000606268421636144 -0.0031795725237413752 -0.002633857510860455; -0.0005530792567350464 -0.0033148575089456496 -0.00015249473270028866] %
+
+Mass Used: 188.34909075807218 kg
+Launch C3: 91.59535604059141 km²/s²
+||V∞_in||: 0.005802586149304272 km/s
diff --git a/archive/ES_0.6194727035208528 b/archive/ES_0.6194727035208528
new file mode 100644
index 0000000..f7c1ce6
--- /dev/null
+++ b/archive/ES_0.6194727035208528
@@ -0,0 +1,22 @@
+archive/ES_0.6194727035208528---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-12T11:36:47.842
+Launch V∞: [5.416124393411661, -7.9618433317626245, -0.7017066851631483] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6770994332124168e-7, -3.695296581554975e-8, 4.667159660845079e-8] km/s
+ V∞_out: [-1.7655231038191148e-7, 1.5968415349944315e-8, -2.0052413779649934e-8] km/s
+ time of flight: 1.2805098234706321e8 seconds
+ arrival date: 2027-05-03T13:19:49.842
+ thrust profile: [0.8941580816603716 -0.5822374912551341 -0.3051709098932181; 0.6477486733169223 -0.030454648095850974 -0.4333014662906207; 0.42903716632079053 0.08786846099787714 -0.4177030024599872; 0.26421010513695636 0.09565764569076611 -0.33136903901338943; 0.1290808812580578 0.06172505454223448 -0.19845044067985476; 0.03369692592072033 0.01947626217660608 -0.06248730450881942; 0.04660570347789164 0.03200001677392962 -0.10488692896603963; 0.012689308692200004 0.008744391960357296 -0.027422983443764076; 0.01692403501536663 0.012949746381915189 -0.040939391711532186; 0.0034226468943385755 0.00019853206193762817 -0.00037373097707492364; 0.0040107370117338365 0.0003849346043704074 -0.00790463058235696; -0.00038654497682250695 0.007442822846386516 -0.0072587611512366; 0.0017635060801495734 0.001431713485749963 -0.004484503436265238; -0.0012677283043391096 -0.0010750466596512612 -0.0014484054775492842; -0.0036229867122924988 0.005597297973910182 -0.006688253699895036; 0.0008451221315477183 -0.0020390196374016362 -0.0022919772978673113; 0.0018680883502543214 -0.005804889055660062 -0.004093849206984286; -0.004032388550731852 -0.0030929205487847423 -0.007034826456963689; -2.360134355793215e-5 0.0036273346900921564 0.0034115297546977903; -2.1593021739091086e-5 0.0015500396595708463 0.0002502567140031099] %
+
+Mass Used: 178.94797519506892 kg
+Launch C3: 93.21774495644446 km²/s²
+||V∞_in||: 1.7796175066952235e-7 km/s
diff --git a/archive/ES_0.6196296962786645 b/archive/ES_0.6196296962786645
new file mode 100644
index 0000000..82fc4fe
--- /dev/null
+++ b/archive/ES_0.6196296962786645
@@ -0,0 +1,22 @@
+archive/ES_0.6196296962786645---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T02:46:40.883
+Launch V∞: [6.961820668796883, -7.308563311732865, -1.5376607623355163] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0031000317405521787, 0.03189237917684226, 0.005864168875865819] km/s
+ V∞_out: [0.0308590016955306, -0.005718341865513546, 0.008795915721478446] km/s
+ time of flight: 1.150167769112744e8 seconds
+ arrival date: 2027-12-28T07:52:56.883
+ thrust profile: [0.5560681928510633 -0.26287560371148383 -0.2971498784772679; 0.288159756907154 -0.0009154849989224628 -0.3171321047850547; 0.23332453229887262 0.046223535434342516 -0.3901611120577437; 0.12244132604238601 0.037303399620185536 -0.27227538239765947; 0.0679946941477893 0.02659369308332404 -0.1843160319023183; 0.03356703955131876 0.014987999540774854 -0.10402640696999543; 0.014780670841239078 0.007108727824791311 -0.0484018166340518; -0.005152227221822439 0.0005257174850097946 -0.0187682320753811; 0.010364584025522495 0.005226074330992718 -0.03749636533923116; -0.003850957155209302 0.003798527613568595 -0.00948094431869657; -0.0014082931763195648 0.0005725497648462719 -0.004969009682935609; -0.0007689374739712836 0.0003221974150287828 -0.0020810144219073597; -0.0027847450993380455 0.009399980746367402 -0.01212882572501474; -0.0022712177987153337 0.0008330395839569101 0.00210404989554839; -0.01191835421834495 -0.02736130856317431 -0.022502896430096134; 0.016579181426874274 -0.011301452320816467 0.014556189497917961; -0.005567303339627783 -0.029830744014461674 0.013311396691912222; 0.009762310754973485 0.016040991138516605 0.014912218386524581; 0.027592420392474677 -0.0029085815621913984 0.020351904230536448; -0.009417976681013268 0.00637603654562314 0.025487765100156833] %
+
+Mass Used: 114.79704792273378 kg
+Launch C3: 104.24644532612139 km²/s²
+||V∞_in||: 0.032574875639925116 km/s
diff --git a/archive/ES_0.6197379133028889 b/archive/ES_0.6197379133028889
new file mode 100644
index 0000000..f83741d
--- /dev/null
+++ b/archive/ES_0.6197379133028889
@@ -0,0 +1,22 @@
+archive/ES_0.6197379133028889---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:01:19.224
+Launch V∞: [5.377263296903306, -8.667769506571515, -2.0779948600404463] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.009833998543408483, -0.00428530178727018, 0.009027840426149755] km/s
+ V∞_out: [0.003999519640078159, -0.010776251186896516, -0.008032747566003712] km/s
+ time of flight: 1.1296670373243934e8 seconds
+ arrival date: 2026-11-21T02:39:42.224
+ thrust profile: [0.4413775126603837 -0.3318663277035435 -0.2744734094532062; 0.22780431357326775 -0.04893221360478311 -0.25488628250579376; 0.16396868759029662 -0.001427159177562603 -0.2633424988666353; 0.11714233218444815 0.012062934264131388 -0.23957444333108183; 0.07587021842785142 0.012952768129971901 -0.18465875597596604; 0.03689603927171771 0.008170017222831678 -0.10311542465850018; 0.01358036262785314 0.003258193095068681 -0.04118712434758893; 0.00035786873808516147 0.0006268334929559325 -0.011711771134128343; 0.005481969575593809 0.0035143392252163087 -0.006152192863768672; 0.008892140697202311 0.0028080992055154403 -0.025878664513232008; 0.002725192922464344 0.0025496384020968696 -0.005576151456181658; 0.0009429195722240422 -0.0005873653171529049 -0.004037398395685701; 0.001382995002308395 0.002674101209775298 -0.008281435940836024; 0.0020288450510553835 0.0022650178414789133 -0.0032030236257271404; 0.0058471099875433965 0.004763379569876219 -0.003021840827330696; 0.0014477472729820056 0.003249865485417729 -0.0024959049027200534; 0.0026708791452489814 0.0015212148125591015 -0.009837686063231165; 0.0004940533357179776 -0.00513365206066411 0.0053253451322153224; 0.011444336075010221 0.00013121594780996957 0.00834978141509221; -0.005913823049167351 -0.001036335445840436 0.010103727668264336] %
+
+Mass Used: 90.9085988938682 kg
+Launch C3: 108.36325142162893 km²/s²
+||V∞_in||: 0.014020457963981239 km/s
diff --git a/archive/ES_0.6198153188223808 b/archive/ES_0.6198153188223808
new file mode 100644
index 0000000..be54009
--- /dev/null
+++ b/archive/ES_0.6198153188223808
@@ -0,0 +1,22 @@
+archive/ES_0.6198153188223808---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:24:45.752
+Launch V∞: [7.118509961549197, -7.443649508091692, -1.9954359181020098] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0034434351931082133, 0.020238878555284345, -0.019257938915034873] km/s
+ V∞_out: [-0.01348497986391928, -0.019767370488561014, 0.014821369307444345] km/s
+ time of flight: 1.1180571850336555e8 seconds
+ arrival date: 2027-11-22T16:33:23.752
+ thrust profile: [0.37983231815358187 -0.18588683932295438 -0.2224594082039009; 0.18979427455623374 -0.007042857893648176 -0.22834340550080381; 0.10792330224417294 0.016457331504750056 -0.19837715719327217; 0.08331141957281646 0.021090881285284094 -0.20051043953311745; 0.05695272800739882 0.017979688167876914 -0.16620111883579797; 0.03173956175668307 0.011464632820825937 -0.10741599953855147; 0.03389062202490294 0.01332242777408793 -0.1303082378783506; 0.02766045071872046 0.012151641739011721 -0.11450361617316268; 0.0046684776617816615 0.0017496783077833628 -0.020485088189341312; 0.0003105511536862762 0.00011081884791290042 -0.0034257491126939645; 0.0018181131175126907 0.0009797987546089106 -0.009021593631542337; -0.0005420596844586925 0.000529399328933945 -0.004798604454548319; 0.0016410356762775115 -0.000700301078985377 -0.003758659407735575; 0.0006083143451339295 0.0007418050878401909 -0.003662178088738261; 0.00041430634856011374 -0.0004072517340858073 -0.0021826476245911555; 0.0006422120329789434 9.768701941431299e-5 -0.002069662307436401; 0.001610105122743071 0.0001416694471857694 -0.0014945599820532873; -0.0009835542318193402 -0.0013464838416678538 -0.0022925286464374256; 0.0013682756295358444 -0.00021142332594156006 -0.0022227001284526493; -4.387240118831968e-5 0.0002378382042636639 -0.00018505554981645793] %
+
+Mass Used: 81.08448360387501 kg
+Launch C3: 110.06286657524045 km²/s²
+||V∞_in||: 0.028148493074406297 km/s
diff --git a/archive/ES_0.6198351984424324 b/archive/ES_0.6198351984424324
new file mode 100644
index 0000000..17e737d
--- /dev/null
+++ b/archive/ES_0.6198351984424324
@@ -0,0 +1,22 @@
+archive/ES_0.6198351984424324---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T00:23:53.729
+Launch V∞: [5.283230893338527, -8.513129332633389, -1.272787968646082] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013981697702263289, 0.00026900057053609155, -0.010495242030209911] km/s
+ V∞_out: [0.017003310862624552, -0.00014077308238908575, -0.0041655120218508195] km/s
+ time of flight: 1.1840300096454848e8 seconds
+ arrival date: 2027-01-21T10:07:13.729
+ thrust profile: [0.5084737523327386 -0.37164030595704706 -0.27569348625612233; 0.34768989496505853 -0.061345562992649025 -0.35686409853412093; 0.19262319813325185 0.006317965868242903 -0.29503651720287327; 0.10885418121414356 0.015347971833295091 -0.21411722030284647; 0.07162669111791939 0.015286158194477192 -0.16657010960170285; 0.03537204065584372 0.008966396009475712 -0.09412721845928468; 0.025868855194097474 0.007533784681390866 -0.07536463863910238; 0.07648086540802675 0.026091812831979297 -0.2431874163974692; 0.005424920234590775 0.004069472282931002 -0.011657516395521456; 0.0023176369659194066 -0.010671419626686753 -0.0018430391486262184; 0.005761497621506194 0.0026591820966728433 -0.01587182085394073; 0.015073626490580371 0.006405120247921748 -0.0026297434077549794; 0.009419234322665872 0.005188463629509881 0.002464283787493704; -0.022271304806211735 0.009234544958921457 -0.02244333595034894; -0.026970319306004745 0.025070507134574264 -0.012365488877387344; -0.0009624599201492438 0.0021611787434881397 -0.008645711852992968; -0.05152829090467263 0.0346699930713511 0.0034310505698039416; 0.032761313736758946 -0.03743568929045809 -0.013035645923991108; -0.0010062880227057318 -0.0044613625495107945 0.011364545549055758; -0.015199094446673712 0.022704092128762003 0.02847720996119663] %
+
+Mass Used: 128.10671281850546 kg
+Launch C3: 102.00588891959984 km²/s²
+||V∞_in||: 0.017484574264679937 km/s
diff --git a/archive/ES_0.6200800417823358 b/archive/ES_0.6200800417823358
new file mode 100644
index 0000000..0f42957
--- /dev/null
+++ b/archive/ES_0.6200800417823358
@@ -0,0 +1,22 @@
+archive/ES_0.6200800417823358---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T23:05:13.849
+Launch V∞: [6.922677907620728, -7.387693639488503, -1.5945277346778628] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005736140360580904, 0.026747266052495285, -0.03153019091144065] km/s
+ V∞_out: [-0.010363116019594222, -0.01580874329669709, 0.03721705108266193] km/s
+ time of flight: 1.1328481748558341e8 seconds
+ arrival date: 2027-12-09T03:05:30.849
+ thrust profile: [0.6204741956816301 -0.3005900693808897 -0.3212673960851518; 0.2805980343539431 -0.008694193043939844 -0.29550451491651697; 0.18419829405192412 0.028416512210808372 -0.29485536046487953; 0.1449172112089061 0.034999125237494565 -0.2989940259190829; 0.04882878800428147 0.019967935677339517 -0.12568031969136384; 0.015416576283374329 0.010908976639340895 -0.06336543688809128; 0.04263783252914405 0.02048055913453246 -0.13873194233090316; 0.013022722700036368 0.01579087786043716 -0.07685006168275038; 0.00510916520506718 -0.0021035282584095094 -0.04411813264320726; 0.00042530677743741205 -6.057329755654382e-5 -0.014823921144092473; 0.00023917419407020108 0.004449539453741973 -0.005681973995284578; 0.0008297703601994047 -0.008688472143338065 0.0036997910708328717; 0.0004577689142073693 -0.0013247606369173885 -0.0013360854528282695; -0.00940687887187629 -0.014503553098719105 0.00047366485905879496; -0.003329302124844427 -0.0033627384531568576 0.013551455776900019; -0.00154950772310036 0.00760844892091079 -0.003340335702470006; -0.015655884105637563 -0.006662865314973362 0.008054855996959525; 1.7931032306211852e-5 -0.00546190327695763 0.012409047927059314; 0.0016200905887551608 0.0014057292327927361 -0.004666466290165651; -0.0008023504601637142 -0.017254915329971695 -0.0056472216438097425] %
+
+Mass Used: 110.67001712789897 kg
+Launch C3: 105.0440054202559 km²/s²
+||V∞_in||: 0.041742933371184475 km/s
diff --git a/archive/ES_0.6201298638468931 b/archive/ES_0.6201298638468931
new file mode 100644
index 0000000..e1b107e
--- /dev/null
+++ b/archive/ES_0.6201298638468931
@@ -0,0 +1,22 @@
+archive/ES_0.6201298638468931---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:37:18.034
+Launch V∞: [7.053099882920187, -7.405586293552458, -1.9515074845500224] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.14700169645586283, -0.7207827790773084, -1.1239771400641954] km/s
+ V∞_out: [0.600279405614713, 0.24886739760471663, 1.174567392148775] km/s
+ time of flight: 1.1142618504531659e8 seconds
+ arrival date: 2027-11-18T00:20:23.034
+ thrust profile: [0.5633144680011748 -0.27500293685597493 -0.3156453188152409; 0.2033635268320033 -0.0063273004514192875 -0.24205478847060588; 0.12855266029283102 0.020196217249311546 -0.23528114032852943; 0.08500829551649301 0.022334838171553732 -0.20647438133334928; 0.052744719770482805 0.017763438559886505 -0.15605111645269307; 0.02577559825211394 0.01025059713013882 -0.09212216406217627; 0.014383867470787954 0.006133199247677627 -0.06197428066740225; 0.023442545964764007 0.011376892401943749 -0.0975397170825916; 0.006154767923193807 0.00374386506352586 -0.032100742662193205; 0.006332699395565755 0.004919081442138562 -0.043722551525888435; 0.0038995895518659546 0.002611631766466236 -0.02200208609880902; 5.476197330073836e-5 0.0001986649734021181 -0.0005811308881633849; 0.00038748232624513765 -0.0004056968072748159 -0.0007130234464736112; 0.00018841309089272175 -0.0009196003621078804 0.0010286312765503723; 9.637663860765028e-5 -0.0004469913757195671 -0.0002581406744550254; -0.0024119789813019125 -0.0014163027957420945 -6.36206506426897e-5; 0.00039556849438452096 0.003755968567650929 -0.0013524395799789464; -0.000756027327609432 3.739170487747107e-5 -0.000624669847243034; 0.0011347813109145028 -0.00028368534651212107 0.0009186222159480815; -0.000918834540491668 0.0022924748491677397 0.003276251984122577] %
+
+Mass Used: 91.16721248496788 kg
+Launch C3: 108.39730777195555 km²/s²
+||V∞_in||: 1.3433026184602623 km/s
diff --git a/archive/ES_0.6201587617977581 b/archive/ES_0.6201587617977581
new file mode 100644
index 0000000..b904e67
--- /dev/null
+++ b/archive/ES_0.6201587617977581
@@ -0,0 +1,22 @@
+archive/ES_0.6201587617977581---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T03:29:54.325
+Launch V∞: [5.2980725068271415, -8.620227473673, -1.9203226912974694] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.032759423207991405, 0.03268416756516539, -0.0013180869841676616] km/s
+ V∞_out: [-0.014511490717854672, 0.0001968902369554491, 0.046555677016387444] km/s
+ time of flight: 1.1152167465699174e8 seconds
+ arrival date: 2026-11-03T21:44:28.325
+ thrust profile: [0.5914453018116687 -0.45312926852306584 -0.34451702219046926; 0.3866785080237489 -0.08361216245534121 -0.4004362417176108; 0.2302793413134564 -0.0017644435637847987 -0.34748561768136527; 0.11743452880885308 0.013013465423302662 -0.23243933615811174; 0.031349443241595165 0.006071891653654598 -0.07682827728121013; 0.018296600671783726 0.004531961178551416 -0.051134837098614695; 0.010024456626504084 0.0030996159243289706 -0.030907191337334536; 0.018071361500366874 0.005694136794870337 -0.0601432651656302; 0.007417644650666009 0.002430442451089508 -0.026550147129440416; 0.000982292990101945 0.0006452535672461074 -0.0038442752081330545; -5.1416057396536183e-5 0.0010748283909803305 -0.0014490347145261128; 0.002434758315227997 0.001410416032737848 -0.0018691388361050034; -0.0016901233298322372 0.0005329200263046518 -0.0017438380615369571; -0.000964875814794146 -0.0006734931087132444 -0.0025986966863818808; -0.004296874294491593 -0.0019740136420051454 -0.003138628237242253; -0.003419638159698246 0.004397711230835681 0.001939746704775406; -0.0011916595186373547 -0.000431909952212285 -0.0026262406538103936; 7.801438388013423e-5 1.1182412817830039e-5 -0.0004699004110809877; -0.004465584603652865 0.004493251352141251 0.0036957601806125225; -0.0005480969678979596 3.469984732092815e-5 -0.0005311107151875698] %
+
+Mass Used: 104.80294495635553 kg
+Launch C3: 106.06553322417638 km²/s²
+||V∞_in||: 0.04629440540330902 km/s
diff --git a/archive/ES_0.6204818286951883 b/archive/ES_0.6204818286951883
new file mode 100644
index 0000000..a0efdd2
--- /dev/null
+++ b/archive/ES_0.6204818286951883
@@ -0,0 +1,22 @@
+archive/ES_0.6204818286951883---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T11:55:43.748
+Launch V∞: [5.140103261002849, -8.430881655472758, -1.203767650141755] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.36586637953728e-5, 9.52806031192489e-6, -2.044653342239975e-5] km/s
+ V∞_out: [-1.8775269440967942e-5, -1.6962475854187232e-5, -7.848835518776949e-6] km/s
+ time of flight: 1.1446324848024325e8 seconds
+ arrival date: 2026-12-06T07:16:31.748
+ thrust profile: [0.9255658976457736 -0.685173294137281 -0.4559817760654025; 0.4616564397479104 -0.08584533576595602 -0.4338580727255864; 0.20797795676172962 0.004730514445294462 -0.2994229880267105; 0.13353756499970726 0.01961334168719113 -0.25133850383257855; 0.039935230244399385 0.008437309351315371 -0.09267202656071707; 0.0543685709280829 0.02101169309474377 -0.1591347522583051; 0.013966641275585846 0.006363158946793345 -0.052039863272539254; 0.020528957220388895 0.003428333938252707 -0.06671820738955644; 0.0013635268830404679 -0.002321229278984644 -0.00580401003332866; 0.0405442749254807 0.0044389644021267435 -0.11682556364452248; -0.007116427561809968 0.006420016743032735 -0.010727785339598783; 0.008842253245837295 0.004282877556618913 -0.022623047709843615; 0.006621683457540343 -0.004003589729515595 0.0051875097553030595; 0.0008361536219769753 0.0021634519014299206 -0.0096676546883167; -0.016972891534131625 -0.008430810927934348 -0.008401406537585981; 0.009882936205171888 -0.004172167109347164 -0.001429245329365226; 0.00782782033120317 -0.0007652087607106642 0.002754910901238617; 0.002206648325771486 -0.0021800094686860376 -0.013275794913459012; 0.0008019551737344019 -0.0023169131457251467 -0.02040121474615112; 0.002419610408603493 -0.023477682245839394 0.023436064101709522] %
+
+Mass Used: 146.69014594004557 kg
+Launch C3: 98.949483577887 km²/s²
+||V∞_in||: 2.6370509266527562e-5 km/s
diff --git a/archive/ES_0.6207312322058048 b/archive/ES_0.6207312322058048
new file mode 100644
index 0000000..ecf9673
--- /dev/null
+++ b/archive/ES_0.6207312322058048
@@ -0,0 +1,22 @@
+archive/ES_0.6207312322058048---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T22:19:27.877
+Launch V∞: [5.293561046442225, -8.603704755069405, -1.397406455509181] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.10868731942970675, -0.001963975956801784, 0.07680796381346816] km/s
+ V∞_out: [-0.13039382870434635, 0.001279097318818294, 0.026787178076146213] km/s
+ time of flight: 1.1273241795418203e8 seconds
+ arrival date: 2026-11-17T16:53:04.877
+ thrust profile: [0.6578792373445894 -0.5033951074725119 -0.3769136484751559; 0.23571105068945658 -0.05234527477656523 -0.2504245093057617; 0.2049415426244908 -0.0034704939866051342 -0.31146972017364233; 0.15044715789838473 0.01384821738374757 -0.29113803382297904; 0.08309941544213463 0.013324891642476033 -0.19119023483312708; 0.049314900793695264 0.010558209740188026 -0.13036651005088307; 0.014701699974000896 0.000345847200440333 -0.03846082545135313; 0.055430359812328335 0.01524360346623496 -0.17239421984079337; -0.0004321245108132891 0.0046224795812992115 -0.014263475564434518; 0.00828102793523006 -0.000904219330313072 -0.006098964420536936; 0.0027149982899005035 0.002022445627822677 -0.002184967385018563; 0.0038744464890593123 -0.001610533208986802 -0.005364447179422059; 0.0014944939500994142 -0.0021683004177421813 -0.0014092830732979655; 0.0005527648171322961 0.0017985460531331754 0.002657300923936178; 0.0005201259892121032 -3.713721800050173e-5 0.001263671873787297; -0.0009362841175371906 -0.001989375299736471 0.004611725104260648; -0.0048329779602387345 -0.0031437347606773475 -0.00256423076025563; -0.0032318515652068214 -0.00036931649047449735 0.006999298432766767; -0.011399324657406534 0.0017804065079001787 0.009060234821944561; 0.006923562958098394 0.0033290794382848355 -0.006772577400915559] %
+
+Mass Used: 117.52986918427905 kg
+Launch C3: 103.99826886671312 km²/s²
+||V∞_in||: 0.13310241887939167 km/s
diff --git a/archive/ES_0.6209673027733036 b/archive/ES_0.6209673027733036
new file mode 100644
index 0000000..c2d0d4c
--- /dev/null
+++ b/archive/ES_0.6209673027733036
@@ -0,0 +1,22 @@
+archive/ES_0.6209673027733036---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-09T21:53:51.031
+Launch V∞: [5.813470157964658, -7.601539104542556, 0.08610260118554981] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.382556867975516e-7, 0.00027800296101951, -0.00019205119535979266] km/s
+ V∞_out: [-0.00014975997077878864, -0.00029624075363078334, 6.20129520743347e-5] km/s
+ time of flight: 1.596914026841645e8 seconds
+ arrival date: 2028-05-01T04:37:13.031
+ thrust profile: [0.7826478696773813 -0.36808996169937463 -0.11999198311650444; 0.5541568329642533 0.113442214298338 -0.2266586616844311; 0.3210027343266586 0.16741220828561598 -0.21795993813539813; 0.21333096693045994 0.16214121489447872 -0.19982468446197543; 0.13367979282877396 0.12746878684015328 -0.15918046508008474; 0.10148953548647283 0.11395694435902304 -0.14557396443342224; 0.06799327862759122 0.08928309871522316 -0.11656561517664296; 0.01540754137051998 0.020929718235311076 -0.029140366840984262; 0.017012322775656848 0.02552107087122194 -0.03541282307531978; 0.0022605084635928955 0.003548855624909469 -0.004523300256743538; 0.0012784687611026436 0.000718606233581609 -0.0005060235017903747; 0.0002378147165984256 0.0013368467287732235 -0.0010703587982217658; 0.0001358650811089553 -5.6763955301408276e-5 -0.0029123098124003597; -6.406705053809068e-5 0.0004894001066186016 -0.007599663555071543; 0.00248787078786601 -0.0018502128833913594 -0.0052466652858430786; 0.0008894517723038543 0.003140885300525014 0.0026358892938868833; 0.0029126610756021174 0.005896448190637281 -0.00022332340096942592; 0.0008733766307636994 -0.0013259465643059888 -0.003170540005297306; -0.002152359578132672 -0.003207150610964701 -0.0005638328666063851; -0.0027666881599893297 0.003750673090417775 0.001971734151610852] %
+
+Mass Used: 190.2029200242182 kg
+Launch C3: 91.58724569336617 km²/s²
+||V∞_in||: 0.00033789053056772233 km/s
diff --git a/archive/ES_0.6211761499601565 b/archive/ES_0.6211761499601565
new file mode 100644
index 0000000..9fce8b1
--- /dev/null
+++ b/archive/ES_0.6211761499601565
@@ -0,0 +1,22 @@
+archive/ES_0.6211761499601565---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-11T09:57:58.698
+Launch V∞: [6.261185829046477, -7.8373087912785495, -0.4921851180373086] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0032018042906465727, 0.0024406042367245257, 0.004126354478578602] km/s
+ V∞_out: [-0.0040359821734860645, -0.002125992460594664, 0.0035206947739894142] km/s
+ time of flight: 1.4439578251593703e8 seconds
+ arrival date: 2027-11-07T15:54:20.698
+ thrust profile: [0.42376035408567025 -0.22924914764987944 -0.13207029599276174; 0.25100978888623265 0.01647698944507434 -0.17647576466863524; 0.2419910246147703 0.08200897694431585 -0.26196558517149204; 0.3087247354413033 0.15675644784027115 -0.40306274975932294; 0.14529132609959117 0.09560262316958996 -0.25236082684696887; 0.08002175941476214 0.06178934840803381 -0.15966896460383603; 0.042742764218646714 0.037640703784144754 -0.09640680973782992; 0.003754280782572969 0.003397426759121623 -0.009591697337220621; 0.007213830374843624 0.007579534382572841 -0.02199065854637247; 0.0028729793800884858 0.003925896066358695 -0.011070739368629973; -0.00022731853910993314 0.0004818447391953674 -0.0007360279589683711; -0.0002873328871233566 0.0008217648678169446 5.328723169786755e-5; 9.812024607316541e-5 -0.0006879506524133795 -0.00010216687486592514; 0.0006821652408017338 0.00018902268002452528 0.0008565970077479485; -0.00010685954750320944 -0.001475189014287633 -0.00027846090350285566; 0.0009347425118248123 0.0006001797337585824 -0.002219842438863368; -2.7881836371369297e-5 -0.0003894645820009481 0.000648892047959035; 0.000520735645714574 0.0004475016044358907 -0.001458845684567298; 0.0006556886387436781 0.0006030028681923775 -0.0007081234489514103; 0.0004664578453104263 0.00040166611226120783 -0.00037717762791392493] %
+
+Mass Used: 136.30823923447178 kg
+Launch C3: 100.86810326612186 km²/s²
+||V∞_in||: 0.005764971902690089 km/s
diff --git a/archive/ES_0.6214863133031532 b/archive/ES_0.6214863133031532
new file mode 100644
index 0000000..bbde510
--- /dev/null
+++ b/archive/ES_0.6214863133031532
@@ -0,0 +1,22 @@
+archive/ES_0.6214863133031532---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:35:32.733
+Launch V∞: [7.0385280410635005, -7.477205626587277, -1.6597597995183497] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.19707636783298366, -0.9363064586308696, -1.4546227056041607] km/s
+ V∞_out: [1.1629963800808711, 0.26270999778677945, 1.2688400489466258] km/s
+ time of flight: 1.1251192464263995e8 seconds
+ arrival date: 2027-11-30T23:54:16.733
+ thrust profile: [0.44259619492520086 -0.21331583088941874 -0.23497787997368852; 0.1699910647965666 -0.005077927529590738 -0.19171712179015427; 0.08078273407731125 0.013793751295839084 -0.1470252778864181; 0.11962071356433458 0.0308941979140781 -0.26211767906798733; 0.10379524694871828 0.03343954696770303 -0.2721920470414983; 0.05935718229831423 0.022101390275252614 -0.18273017317106072; 0.0228118558534798 0.007255647131431187 -0.08496182278810196; 0.007247037713065086 0.004613423231750691 -0.038354583802624444; 0.030725174097988896 0.013033703305264474 -0.1112126249914464; 0.0029637785515797535 0.0007218776013393019 -0.008056991572161557; 0.002644713228925434 0.0003932133507571855 -0.009702140106046139; -0.0023343015735126176 0.006608642665549955 -0.003594184743274385; -0.0007118487600903602 0.0003110731780753993 -0.005347629123179026; -0.005020363899086222 0.002638720152652322 -0.0029701718758961783; 0.009617916292974968 -0.0014942433447515096 -0.007183073670972364; -0.0017181147431460945 0.011235455074802874 0.002862927458722321; 0.004707108278668766 0.002277603978808069 -0.00892040458763791; 0.003088453862457626 0.008759388882941678 0.015167526130018413; 0.002855689318571811 0.0007287553193569645 0.0025967887968322825; -0.010251543056477734 0.004688706818857405 -0.0036541335701235035] %
+
+Mass Used: 93.87571142499564 kg
+Launch C3: 108.20428355920282 km²/s²
+||V∞_in||: 1.7411019771659817 km/s
diff --git a/archive/ES_0.6215039308767007 b/archive/ES_0.6215039308767007
new file mode 100644
index 0000000..38f74d8
--- /dev/null
+++ b/archive/ES_0.6215039308767007
@@ -0,0 +1,22 @@
+archive/ES_0.6215039308767007---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T05:07:46.709
+Launch V∞: [6.972222322451992, -7.405686950501997, -1.9089774592723079] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008582806811424207, -0.00375843020338723, -0.01839439455082756] km/s
+ V∞_out: [-0.00509920645435309, -0.019992187971982423, -0.0006475517024348947] km/s
+ time of flight: 1.1153935137772502e8 seconds
+ arrival date: 2027-11-19T04:16:57.709
+ thrust profile: [0.6215390480307252 -0.300560413506932 -0.3312592813899667; 0.2843598399467368 -0.006351847188101548 -0.3089909226546048; 0.15411236472580006 0.027318611796615565 -0.2580311464332998; 0.09879481298770841 0.02914328368931205 -0.21910688262379718; 0.0457799302368613 0.018275685923705653 -0.12322714946393233; 0.0277868671889585 0.016499434001395755 -0.09029366077427714; 0.020398889642543248 0.004504478092524156 -0.06778665060343836; 0.009908665136960438 0.0022490694082987588 -0.053606388739733675; 0.01002441581264249 0.0034402927909777145 -0.04311674626193556; 0.0082354113674519 0.0043715918714552875 -0.038949378808418665; -0.002569069779921965 -0.0016299390704424867 0.0005160619744618081; 0.0022416593890862073 -0.003448671538962911 -0.005621299713182311; 0.000977506116007879 0.00035351118367866986 -0.0037999572314344455; -0.0003700644403379814 0.0022783955975227243 0.00018332652446630994; 0.001650699828944691 -0.0012742035014540458 0.004323378953594073; -0.0018443207001270867 -0.0014739093545269913 -0.013002987047243057; -0.003814764998650369 0.015935539307157312 0.002798771920911138; -0.010819935404675662 -0.006900923794525615 -0.007381869420813527; 0.003098092814382322 0.002163581641956379 -0.007770144052276243; -0.0051283293123260704 -0.009938377302818359 -0.01217876072721436] %
+
+Mass Used: 100.33629615798236 kg
+Launch C3: 107.10027826254318 km²/s²
+||V∞_in||: 0.02064325849393641 km/s
diff --git a/archive/ES_0.6216429429118717 b/archive/ES_0.6216429429118717
new file mode 100644
index 0000000..72e0515
--- /dev/null
+++ b/archive/ES_0.6216429429118717
@@ -0,0 +1,22 @@
+archive/ES_0.6216429429118717---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T20:50:27.656
+Launch V∞: [5.367064771422473, -8.7862574726055, -1.9649118434047923] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.04922279117251987, 0.04784640371969388, 0.04892671452550194] km/s
+ V∞_out: [-0.03835619778390436, -0.06109279053290622, 0.04361551474263967] km/s
+ time of flight: 1.1165958939513628e8 seconds
+ arrival date: 2026-11-07T05:23:36.656
+ thrust profile: [0.39976921616967936 -0.3055399263998768 -0.2560392972765571; 0.19416847197724035 -0.044866143373320094 -0.23147013443427014; 0.1162091528118251 -0.003969604647245967 -0.2014796961760575; 0.08149580558674992 0.00592662706164193 -0.1803423119226034; 0.06338815854996308 0.008642582238347208 -0.1679935051547003; 0.059405093227224016 0.011188579354503323 -0.17884684435789952; 0.020853640487709837 0.00428922250982772 -0.06979807500545324; 0.005399268255849369 0.0012215012657131436 -0.020823166157791822; 0.020825193814946023 0.005234455974271407 -0.08059163604701716; 0.003746748693193774 0.0009856421789192996 -0.016170326005521363; 0.001212768571442354 0.000544696207953755 -0.0045158576472504024; 0.0017752063972657224 -5.61094103494701e-6 -0.004311634446306008; 0.0010211481876421446 0.0006915603394568818 -0.0027694601905886443; -0.0008212861494568372 0.0017092090856168998 -0.0009758170604995359; 0.0008452529145233244 -0.0007650807029579258 -0.000650285597418857; 0.0007093725193625813 0.0027047438069722576 0.0007952575268368512; 0.0011178884268165932 -0.003288846440467375 -0.004131323444314142; -0.0002799813231492629 -6.137311533408848e-5 -0.00010278381091954067; -0.001007183364611551 0.002157928177271994 -0.00034609322361232376; 0.0005386811332518353 0.007060317023610653 0.0002506243639067866] %
+
+Mass Used: 84.37336480102704 kg
+Launch C3: 109.86458318791257 km²/s²
+||V∞_in||: 0.08429700418153303 km/s
diff --git a/archive/ES_0.6217407563927164 b/archive/ES_0.6217407563927164
new file mode 100644
index 0000000..1c54464
--- /dev/null
+++ b/archive/ES_0.6217407563927164
@@ -0,0 +1,22 @@
+archive/ES_0.6217407563927164---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T02:00:44.034
+Launch V∞: [6.902552406054916, -7.441826759965221, -1.9930057240557213] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008441570724876488, -0.02340801768312338, -0.053371081476947996] km/s
+ V∞_out: [-0.05160769524483469, -0.008291494703997461, 0.027124826574854526] km/s
+ time of flight: 1.1047080059269154e8 seconds
+ arrival date: 2027-11-07T16:20:44.034
+ thrust profile: [0.8405698601024619 -0.422126562460439 -0.4813622201883499; 0.23830501464397114 -0.0117047216601464 -0.2885908184921626; 0.09494704345845224 0.011792895056260215 -0.18170379339241782; 0.06780835011425185 0.014946944433124994 -0.17198354270180416; 0.041352163990138864 0.011730034442423262 -0.12972252495452669; 0.015489860742063497 0.004895488399869211 -0.05729690759228666; 0.0264589392637342 0.009383973889257689 -0.10801207370211968; 0.010564927101303563 0.0037436987932997156 -0.04828663140363828; 0.003854752643188142 0.0016631474826179263 -0.01654321009416952; 0.003902036745714087 0.0008771563471398412 -0.014565357421545813; 0.009137419879709325 0.003596719711521939 -0.04889975126698964; 0.0008595326109698583 -0.00038494096645835693 -0.004463865225932676; -0.003969459154940522 0.0007138839384852646 -0.0008584300920438546; -0.0003298962399676075 -0.00045587165965069534 -6.461411515980612e-5; -0.0007500076642162455 0.0008349626636711098 -0.002900712097202942; -1.43883604637583e-5 0.0014177267303550913 -0.0028932617931714186; 4.801915738462183e-5 -0.005870561729479994 0.00048300411762511455; 0.004132449419383545 0.004201689126950213 -0.0031481287117754815; -0.0010131692193685003 -0.0006082103093906444 0.006568573702114167; 0.0018570107012846416 0.004153656983549023 -0.0009104967016700092] %
+
+Mass Used: 101.20870794274015 kg
+Launch C3: 106.99808705978785 km²/s²
+||V∞_in||: 0.0588869064069045 km/s
diff --git a/archive/ES_0.6217852413282094 b/archive/ES_0.6217852413282094
new file mode 100644
index 0000000..aa9a699
--- /dev/null
+++ b/archive/ES_0.6217852413282094
@@ -0,0 +1,22 @@
+archive/ES_0.6217852413282094---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:42:05.852
+Launch V∞: [7.033525261106257, -7.421452179529519, -1.8395217720015442] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005982380024127472, 0.027678481918315484, -0.03390246121861206] km/s
+ V∞_out: [-0.011540191522463508, -0.016742427715974943, 0.03921267633380325] km/s
+ time of flight: 1.1214170286602215e8 seconds
+ arrival date: 2027-11-26T07:10:27.852
+ thrust profile: [0.48331469822535333 -0.2411197134297636 -0.2811435835076316; 0.21531453302900957 -0.010682756208847033 -0.2546668639794612; 0.18553269310746487 0.025032115146937286 -0.3331385924595506; 0.10762723818178765 0.02511710401997922 -0.2537744402967024; 0.06498503195018561 0.019180601442407557 -0.18593910089248905; 0.03144519520369182 0.010754923611005931 -0.10386041964522932; 0.009668347987931267 0.0038667742916291773 -0.03723970753806555; 0.0032751457190683853 0.0015160544195727155 -0.01683955555706326; 0.003601869155709022 0.0015048719624319257 -0.018160755181834756; 0.007951177040284502 0.0018313636961447995 -0.006514035669110175; 0.004849919555576636 0.003529789426832681 -0.011365351324559599; -0.0008110254183808867 -0.0007772561811870689 -0.003291510785448421; 0.007290561104970432 -0.01175670827992469 -0.016846337346852893; -0.004889533624687722 -0.007473361404949154 -0.004258481217988736; 0.010717861461032306 0.006060401575087776 -0.00322333963972443; 0.005011781562485882 0.022321258059590888 -0.005129924290179112; 0.0100606873331312 0.0013153841171723638 0.004393264067888982; 0.010235175140246269 -0.010155981023690263 -0.0008434784139479028; 0.01303670479593659 0.024560361302984193 -0.01779956906981076; 0.0011531348900721842 0.0059226653187922276 -0.007434708771841121] %
+
+Mass Used: 95.81120420848038 kg
+Launch C3: 107.93227040133098 km²/s²
+||V∞_in||: 0.04417311522561083 km/s
diff --git a/archive/ES_0.6218660873239162 b/archive/ES_0.6218660873239162
new file mode 100644
index 0000000..57a27c0
--- /dev/null
+++ b/archive/ES_0.6218660873239162
@@ -0,0 +1,22 @@
+archive/ES_0.6218660873239162---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T05:15:39.282
+Launch V∞: [7.038322495519857, -7.40365937773556, -2.1036924147274196] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008023053893030773, -0.0036026444748837837, -0.017823804905964087] km/s
+ V∞_out: [-0.004583193854299384, -0.019333210899633576, -0.0005034896372784994] km/s
+ time of flight: 1.1051532835754398e8 seconds
+ arrival date: 2027-11-07T07:57:47.282
+ thrust profile: [0.5979726343121171 -0.2737214781085545 -0.3194165584414532; 0.24415577248559736 -0.006789781129417244 -0.2778641232152444; 0.13544147586799685 0.022795261952806983 -0.23632504698619128; 0.10544736582438259 0.0296651330567957 -0.24172853272074954; 0.0538534656286178 0.019629941797330415 -0.15291841514169824; 0.026692652157685882 0.0114973701612072 -0.0886736739751308; 0.015011214637188876 0.007118125030318537 -0.061303390119504836; 0.010379596748885623 0.004939099071615515 -0.03842358796721676; 0.002128386153670713 0.001237436076066624 -0.010368378417888225; 4.781389789737284e-5 -0.0005060383766574174 -0.003056691062408033; 0.0024222498515346228 0.0016704264056110964 -0.011513385714528564; -0.001079483007637503 -0.0007677111508089308 -0.00044252172923244393; -0.0004962745860036485 5.914370563550944e-5 -0.00025979376649740973; 0.0010237034365234775 0.0006058322724623962 0.0010202303635661874; -0.0015410922721716266 -0.0006929501424958818 -0.0011803725563585745; 0.004701510543024071 0.002293750815458456 0.006904224216074717; -0.001339842204951758 -0.006091491360264278 0.010155612818072361; -0.001265515915562565 -0.0006471500664768746 -0.0005639611478866643; 0.0070079735654907886 0.008117846641132931 0.007978307712860708; 0.00012098395255731044 0.00047617680669163767 -0.0002714406114353676] %
+
+Mass Used: 90.97398307975254 kg
+Launch C3: 108.77767750825424 km²/s²
+||V∞_in||: 0.019875524202112416 km/s
diff --git a/archive/ES_0.6219208587010356 b/archive/ES_0.6219208587010356
new file mode 100644
index 0000000..c40cc7c
--- /dev/null
+++ b/archive/ES_0.6219208587010356
@@ -0,0 +1,22 @@
+archive/ES_0.6219208587010356---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T07:31:49.797
+Launch V∞: [7.124192090944672, -7.4863146048172275, -2.348774509206219] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01145809521142262, -0.024518927023433088, -0.01781437102866649] km/s
+ V∞_out: [-0.02600819558026439, 0.016630394744222832, 0.009834418494654974] km/s
+ time of flight: 1.1310674585594802e8 seconds
+ arrival date: 2027-12-08T10:04:14.797
+ thrust profile: [0.23376391561116722 -0.12312345707753568 -0.14286075845046647; 0.1505888415365108 -0.012420253191128812 -0.18807224935273265; 0.11000081666040584 0.009619754665992778 -0.2115780258308823; 0.07976380642974634 0.014116164576763245 -0.20373859039568262; 0.05219243686045718 0.012169270010518598 -0.16287241478780537; 0.030991169238962436 0.008305419370952387 -0.11013737733411046; 0.014294042708182377 0.0052204672599595004 -0.05308601302006346; 0.0047504980863207836 0.005435063344662465 -0.01852963647833359; 0.0044611038479464805 0.003940553011439767 -0.015129653166398548; 0.001254016560776281 -0.0006198313661816876 -0.010485969462289175; -0.006166641788769522 0.003403354612544212 -0.012658991426490301; 0.005911143616965224 0.01417856152326224 -0.020092137667160868; 0.003291843997020369 0.0018231007450239152 -0.01022589697724971; -0.0007155089862824924 -0.0011765230085701676 -0.0015810305990369452; -0.007191313434902527 0.02062515782638856 -0.020597933241293793; -0.0017940500614338998 -0.0010645882082535771 -0.00026081437275870785; -0.0033664185143014447 0.007544556425028333 -0.015825106844699236; 0.010104748691548301 0.006979166887899497 -0.0004047521792446829; 0.007453052649901454 -0.016973524958923143 -0.018242384312324684; 0.013500736261787681 0.027254572366124306 -0.016100819899474813] %
+
+Mass Used: 70.39906261576925 kg
+Launch C3: 112.31576100607525 km²/s²
+||V∞_in||: 0.032400888003285576 km/s
diff --git a/archive/ES_0.6220192775884026 b/archive/ES_0.6220192775884026
new file mode 100644
index 0000000..dfc4aae
--- /dev/null
+++ b/archive/ES_0.6220192775884026
@@ -0,0 +1,22 @@
+archive/ES_0.6220192775884026---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:01:30.746
+Launch V∞: [7.054201912508549, -7.444402112050435, -1.831617313388617] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.2717603154826195, -1.2966888115955462, -2.0523097799130547] km/s
+ V∞_out: [1.0529432772631935, 0.46048954398625325, 2.153830786735631] km/s
+ time of flight: 1.1050205899200465e8 seconds
+ arrival date: 2027-11-07T14:02:28.746
+ thrust profile: [0.5645717377628745 -0.27765866341773004 -0.3101237774326703; 0.22256322197972234 -0.008637123498431971 -0.2690918946767499; 0.10847544684118954 0.015387575364352687 -0.20663620694888235; 0.05409647829172579 0.011287020155828926 -0.1318405645928094; 0.10428159378147392 0.03582039347574809 -0.2945960936420912; 0.024668116800878336 0.008229704805631578 -0.0860553056891299; 0.03825351200195009 0.014143492562528096 -0.14230584709211927; 0.01056673701971534 0.0037414708007023354 -0.042275854544747374; 0.00872816852893627 0.0032771420560373417 -0.03791830107682412; 0.0005335012973305052 -0.00046993316649408725 -0.004952086647037995; 0.0024931919646125804 0.002043947610415965 -0.008217375026811798; 0.0011558203759025553 0.0007520161628437362 -0.002488343187750959; 0.0009509014565074643 7.475164649291505e-5 -0.004056786490670326; -0.00022847267559302073 1.7097147184172472e-5 -0.0022185167545614227; 0.0009893720580060337 8.404869827356498e-5 -0.0031498561027506347; -0.0018713796473418171 -0.0012988606436448143 -0.0020414272277837447; -9.763560279371338e-5 -0.00016025020510545933 -0.0006717213115483068; 0.00296920843065394 0.003049058181181039 -0.0015705272177933655; -0.0007266235799923981 0.0023014270718525126 -0.0016397694281840786; 0.002789996023738244 0.001619785842389464 -0.0003352347769302046] %
+
+Mass Used: 92.56418562203953 kg
+Launch C3: 108.53570941104518 km²/s²
+||V∞_in||: 2.442791635796032 km/s
diff --git a/archive/ES_0.6222593409318116 b/archive/ES_0.6222593409318116
new file mode 100644
index 0000000..c28b83c
--- /dev/null
+++ b/archive/ES_0.6222593409318116
@@ -0,0 +1,22 @@
+archive/ES_0.6222593409318116---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T11:49:20.919
+Launch V∞: [7.0412173613224605, -7.439739442347519, -1.44657224003273] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008554607784369088, -0.0003780361953835365, -0.0017129504446398284] km/s
+ V∞_out: [-0.0009300793414780111, -0.0017132727396664408, -8.690417137353546e-5] km/s
+ time of flight: 1.1422199491741097e8 seconds
+ arrival date: 2027-12-20T12:09:14.919
+ thrust profile: [0.39125003933327196 -0.2023025233050199 -0.20373479903686723; 0.17358606802830306 -0.006652096221880927 -0.19405759116719212; 0.1313818402734854 0.017799488975188307 -0.22190946628094768; 0.10578100602165189 0.024591627076532944 -0.23475968037075048; 0.07935171988322795 0.023180372883665604 -0.21420943509866316; 0.06491440660139883 0.021725091103560818 -0.20472222414641372; 0.014172674751077658 0.005220328896119617 -0.05015873640648483; 0.01858125354213002 0.007313055023247836 -0.07281727376965909; 0.037823368167515095 0.019988481218597882 -0.17283916304147148; 0.0011250562506769 -0.00021083964269057344 0.00016710961011600072; -0.0005682781503815918 -0.0010458211065310437 0.0010659454553513163; 0.013115384037173192 0.002661806043828467 -0.022098791394921928; 0.0060283939257188175 0.019846217030863936 -0.02432356819962304; 0.02275381740767647 -0.013560860236766406 -0.018805782194160802; -0.017938816223916618 0.0007072158125764342 -0.02030055575418844; 0.013682904994160729 0.022705507164106686 -0.013611289871448344; -0.016221279135000977 -0.009617547998259826 -0.022339476006027405; 0.0018986533510122851 0.011271302004684862 0.008267561678281994; 0.005045264402670151 -0.0037999059336098883 -0.01776420201637499; 0.00598807958248705 0.0062222842003346835 0.0029977030944179405] %
+
+Mass Used: 101.67985357435964 kg
+Launch C3: 107.02103614504352 km²/s²
+||V∞_in||: 0.001951646416299768 km/s
diff --git a/archive/ES_0.6223116392278726 b/archive/ES_0.6223116392278726
new file mode 100644
index 0000000..cea7921
--- /dev/null
+++ b/archive/ES_0.6223116392278726
@@ -0,0 +1,22 @@
+archive/ES_0.6223116392278726---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-10T06:33:32.316
+Launch V∞: [5.372420426610469, -7.843988028459589, -0.38087443663145] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01419367088143166, -0.006910910071660098, 0.017047081198137682] km/s
+ V∞_out: [-0.021046164752439343, -0.009331994823951655, 0.003054149286047312] km/s
+ time of flight: 1.3374478665688124e8 seconds
+ arrival date: 2027-07-06T05:53:18.316
+ thrust profile: [1.0 -0.6528940313637819 -0.26910017910267975; 0.7913351057556356 0.010562965971753421 -0.4281137938557103; 0.37236773775878335 0.1076271912642242 -0.3190912412709454; 0.21788170149644778 0.10092943386426159 -0.25152876441839184; 0.10263224849297432 0.05977494295305125 -0.14097374932977594; 0.09587546695203059 0.06541852294773816 -0.15448365419700824; 0.07968377798073958 0.0614633429055576 -0.14459437243122344; 0.031379707106680484 0.02483068779857565 -0.06132023065969933; 0.01240770585751716 0.012202792140637492 -0.028526132163346925; 0.002407529990517886 0.0016078942489215857 -0.00584068980612764; 0.021898881311594412 0.02211472790501695 -0.05167020950179148; 0.00012936432189583597 0.0002615375352025824 -0.0011852723953898392; 0.0001526124991814473 0.000529745728981118 -0.0005243676886507811; 0.0015225409089362125 -0.0007327739428200668 -0.0006778102963526894; 0.0007978993762295393 0.0017010475062167133 -0.002792720884283688; 0.0007037547672898666 0.000794540705111126 -0.0003511970464672759; 8.784961472307852e-5 0.0008071647609060209 -0.002018599352405255; 0.0002386997733594056 -0.0012992560312721215 -0.0016557488853193062; 0.0006867057983922041 -0.0005929125813406483 -0.0018852069774056212; -0.00028928463020527566 -0.00026916893509723464 -9.364401792864765e-5] %
+
+Mass Used: 197.9029096229292 kg
+Launch C3: 90.53611476735809 km²/s²
+||V∞_in||: 0.02323411174297122 km/s
diff --git a/archive/ES_0.6223415091716015 b/archive/ES_0.6223415091716015
new file mode 100644
index 0000000..043ddce
--- /dev/null
+++ b/archive/ES_0.6223415091716015
@@ -0,0 +1,22 @@
+archive/ES_0.6223415091716015---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T02:08:16.946
+Launch V∞: [5.317043012339535, -8.711762215060322, -1.7668618064801402] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.3941925921387527e-5, -0.00010088414753378728, 7.835958483125547e-5] km/s
+ V∞_out: [9.08955599878644e-5, 9.404965982453849e-5, 4.643218912491631e-5] km/s
+ time of flight: 1.1164170078758188e8 seconds
+ arrival date: 2026-11-06T05:43:16.946
+ thrust profile: [0.5199475314334485 -0.40088103659078383 -0.31770750622192784; 0.2543807998467037 -0.05797671279206473 -0.2809281134077516; 0.1607487646645184 -0.004357039886108957 -0.2569891036027722; 0.11417517823097427 0.009329485796262051 -0.2338284516340027; 0.07279517163658136 0.01064345661925661 -0.1806204298180591; 0.04372832421318083 0.00794031655166167 -0.12769641299351783; 0.017454697638247023 0.0033282881374645675 -0.06078692398798214; 0.017348029805486546 0.004152691615309944 -0.06364809196238602; 0.007389640790293674 0.0017806760153527609 -0.030872982025835848; 0.0008677233894465908 0.0011019585952769322 -0.0076112332927574244; 0.00023668723556932866 -0.004609271193976126 -0.00195396273270521; 0.007952895949624422 0.005487692845145926 -0.0017309754241993363; 0.0061811433516054965 0.007079663842032145 -2.6511674889376918e-5; 0.00020373072501736857 -0.0008147013355126664 -0.0012150137973696595; -0.0001658781368621008 0.00032965125779848355 -0.002439099387507226; 0.0010299542343131555 -0.002567048319633793 -0.005462253821612714; 0.01599009597000061 -0.0016378560438428218 -0.006982259684631706; -0.0062883546617625114 0.0071856104374524235 -0.0043168182042201625; -0.0015261202802543485 -0.007747460327757997 0.010764731943562887; -0.0007714072283464689 0.0014146683188287837 0.002876493331436655] %
+
+Mass Used: 100.2210644417537 kg
+Launch C3: 107.28754793001967 km²/s²
+||V∞_in||: 0.00013866350323951194 km/s
diff --git a/archive/ES_0.6223700326981212 b/archive/ES_0.6223700326981212
new file mode 100644
index 0000000..de7f100
--- /dev/null
+++ b/archive/ES_0.6223700326981212
@@ -0,0 +1,22 @@
+archive/ES_0.6223700326981212---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T02:16:46.675
+Launch V∞: [7.086997084814742, -7.182878709012564, -1.584749755980931] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.045665832636169926, -0.07550714584688666, -0.02974766052235243] km/s
+ V∞_out: [-0.0544830961067822, 0.0660652155791139, -0.036605291872818864] km/s
+ time of flight: 1.1245480409700514e8 seconds
+ arrival date: 2027-11-26T15:43:30.675
+ thrust profile: [0.6068487756167849 -0.2757034284822213 -0.2950086805404827; 0.4131405302773558 0.010625686428472907 -0.4008581225381666; 0.23753995926546606 0.05770897389785381 -0.3520411127363605; 0.1215998121889858 0.04579148293938962 -0.24327256304760814; 0.0530569554529403 0.02494627457702037 -0.13250074644786008; 0.045458846543541695 0.02481720351793118 -0.12784481782919688; 0.028822163683619745 0.016478011546530766 -0.09713921958277476; 0.015274228404990556 0.010259513503395589 -0.055676536394499154; 0.0028296421542346826 0.0017373496984325475 -0.00957486536969079; 0.012678326555735173 0.00865955454500329 -0.050737166924238165; 0.00492911911465686 -0.0004015204424438752 -0.004160950851311702; 0.004186365366447282 0.0015273295195060233 -0.004902852119500119; 0.004411834943626996 0.0003101092226316126 -0.0029118956043449077; 0.0019410028349994177 0.003336905721908611 0.002754675936878219; 3.2750455338814407e-5 2.9551756243514915e-5 -0.00023390101120381707; 0.018536947393015667 -0.0026251379817952237 -0.008869572826477434; 0.0006001097430826134 -0.001385350426768308 -0.002590399301052952; 0.004334193437312679 0.0003607312226022309 -0.02248035439788257; 0.0049025901992771495 -0.016632762771836753 -0.010444435763743157; 0.005638920792833051 0.013636739635493177 -0.009513432307628652] %
+
+Mass Used: 117.50258637823981 kg
+Launch C3: 104.33070601764027 km²/s²
+||V∞_in||: 0.093121536987159 km/s
diff --git a/archive/ES_0.6223895814924426 b/archive/ES_0.6223895814924426
new file mode 100644
index 0000000..b7c6d22
--- /dev/null
+++ b/archive/ES_0.6223895814924426
@@ -0,0 +1,22 @@
+archive/ES_0.6223895814924426---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:26:07.971
+Launch V∞: [7.09454889942954, -7.422992605938836, -2.0012112774238946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.2247577162268769, -1.0820192935387105, -1.7828856105099926] km/s
+ V∞_out: [0.9536465034346218, 0.3830420398906847, 1.8276900595999712] km/s
+ time of flight: 1.103306028724096e8 seconds
+ arrival date: 2027-11-05T07:49:29.971
+ thrust profile: [0.5148975957158566 -0.25099484085297163 -0.2911013788813192; 0.2000254874806276 -0.007515075668037637 -0.22795195721064707; 0.12435948306776562 0.01903019548795748 -0.21454402084397442; 0.10320820516551071 0.026962379706256066 -0.2319759229345618; 0.04388079450783942 0.014724423689195057 -0.12154245114210473; 0.06835963167853988 0.026233870483112157 -0.21404547779957103; 0.027065757670129458 0.011060890008824273 -0.09727401100756225; 0.0049450221122186964 0.002631272607208509 -0.02149718446441507; 0.0019552567344291267 0.00029632449472446755 -0.007009333291403577; 0.00534756644028348 0.0012338571719690684 -0.004510433980666491; 0.0037812818852312733 0.0019671366375683974 -0.004403811052694414; 0.0021250550548411397 0.0015088996967185936 -0.00997280587591733; 0.002000052999363791 4.159161265746003e-5 -0.00808409488729056; 0.0041827304921200695 -0.0017774550512474115 -0.0032380143391191685; -2.108878414606042e-5 0.0018302666467788725 0.00046055905936571084; 0.001284082964857547 0.0003825567952422109 -0.003973302188097082; -0.003974038114256387 0.00283085055531662 -0.00483702431681013; -0.0005235149803568904 -0.00021319274543513556 -0.0011962425163986748; 0.0005891913641242506 0.0012341601941117915 -0.0014392091057597676; 0.0031131445281283206 -0.0012550960707005507 0.004912792264389816] %
+
+Mass Used: 87.73115404305236 kg
+Launch C3: 109.4382898911081 km²/s²
+||V∞_in||: 2.097608848846019 km/s
diff --git a/archive/ES_0.6224669670704527 b/archive/ES_0.6224669670704527
new file mode 100644
index 0000000..bd7f43c
--- /dev/null
+++ b/archive/ES_0.6224669670704527
@@ -0,0 +1,22 @@
+archive/ES_0.6224669670704527---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T09:08:32.881
+Launch V∞: [7.0204710476822045, -7.260657806646562, -1.4110794766543246] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03395660225884843, 0.03476505742186212, 0.003673919017142387] km/s
+ V∞_out: [-0.010970676780211776, 0.04641486184833504, -0.010021997272996533] km/s
+ time of flight: 1.1389960134702523e8 seconds
+ arrival date: 2027-12-14T15:55:13.881
+ thrust profile: [0.6463091706663688 -0.2940021842083773 -0.31218000831664233; 0.2728364985040466 0.0037149638571731675 -0.2888802646758736; 0.1524977701575288 0.034855235297126454 -0.24560582180116847; 0.12133509095948629 0.045003598818379564 -0.26554230933566125; 0.0709398730577217 0.027991832055669488 -0.17946078510662303; 0.039437798972425595 0.018237127525837005 -0.11692868274581268; 0.03673872627187543 0.017971215778819792 -0.12289023101718766; 0.005376283825822016 0.005830160118584096 -0.020655555642703674; 0.00583032954186509 0.006389781843871052 -0.030408321647935655; 0.03722508542958123 0.02209886926565737 -0.15142674978093604; 0.008997576608797847 0.006589606742112521 -0.02049473553431362; 0.0008004438443934816 0.0003571920194258693 -0.0051010285802296695; 0.005671613093097696 -0.006998477297532006 -0.006420140385917444; -0.01845352429746947 0.006773955726576884 -0.01591484417631156; 0.00013542768476193165 0.00012900011566256827 -0.0006093317084257605; 0.008072756047945958 0.021840144772957065 -0.02392464017682386; -0.020222289563444924 0.01562831883056274 -0.016955619996527845; 0.024339509233296933 0.012500042532864141 -0.03187044670227086; 0.021756087784060265 0.012139159227834175 -0.03412523806708621; -0.0007314682641964489 0.0023938729131253575 -0.00042612179847438487] %
+
+Mass Used: 119.5721485472136 kg
+Launch C3: 103.99531080599677 km²/s²
+||V∞_in||: 0.048735590028802574 km/s
diff --git a/archive/ES_0.6227741614883939 b/archive/ES_0.6227741614883939
new file mode 100644
index 0000000..4315b70
--- /dev/null
+++ b/archive/ES_0.6227741614883939
@@ -0,0 +1,22 @@
+archive/ES_0.6227741614883939---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T04:48:12.739
+Launch V∞: [5.259136473816213, -8.623441711710665, -1.4286174531503464] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8516723505823597e-5, 1.880538714893776e-5, -4.2011493193433773e-5] km/s
+ V∞_out: [-3.828751056239522e-5, -3.478004833855106e-5, -1.609969783673578e-5] km/s
+ time of flight: 1.1129088599750957e8 seconds
+ arrival date: 2026-11-01T06:56:17.739
+ thrust profile: [0.734181872426339 -0.5618299724064635 -0.3875721315907973; 0.27080767810028883 -0.0604495104310005 -0.2819574450814761; 0.1701800716408916 -0.003316425708846793 -0.25891525093163104; 0.15360843360927798 0.01436694519960443 -0.2965551097070857; 0.13991905428973173 0.019133239361636648 -0.31064851634149365; 0.029068748365301367 0.007355245796486399 -0.08105081877969177; 0.015977064627540328 0.003311833651334138 -0.04972015082351031; 0.00843107014126218 0.0020105046913312242 -0.030280119943251412; 0.02483366750320592 0.008432987187675744 -0.08882363603263686; -0.0009463640459815165 -0.0007753811886897779 0.000958923238101733; 0.00047716486818266115 -0.0007604991076185694 -1.6869849520248937e-5; -0.001208839269498301 0.0008007593198985653 0.0017343604856903396; 0.0002101267956583271 -0.0003703291966543929 -0.002429254559319312; 0.0007395567310898026 0.0003828328696804811 -0.0014683037523347533; -0.001253948997688172 0.0014756393426107336 0.0045762021168420965; -0.0017385696617930747 -2.8437904505507926e-5 0.006916881004829263; -0.002135130807446761 -0.003005808137503961 0.0007105461976112118; -0.0022207915392946616 0.008673984116575204 0.005758205933578229; 0.005865940205370307 -0.002931765773218686 -0.003815632593725234; 0.006692215769403213 6.430480125834998e-5 0.00466047461936144] %
+
+Mass Used: 119.53445621096944 kg
+Launch C3: 104.06321123294117 km²/s²
+||V∞_in||: 5.4146206383004876e-5 km/s
diff --git a/archive/ES_0.6229539900273663 b/archive/ES_0.6229539900273663
new file mode 100644
index 0000000..8a21f61
--- /dev/null
+++ b/archive/ES_0.6229539900273663
@@ -0,0 +1,22 @@
+archive/ES_0.6229539900273663---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T13:16:44.850
+Launch V∞: [6.888601718844677, -7.390265931141149, -2.06856521315223] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.213483599007007, -1.0821969354577972, -1.9200856502485864] km/s
+ V∞_out: [1.0588883151336839, 0.3905704603803589, 1.9049973479427453] km/s
+ time of flight: 1.0911996083993073e8 seconds
+ arrival date: 2027-10-22T12:22:44.850
+ thrust profile: [0.9700545243460804 -0.4941204428979268 -0.55163353805475; 0.2887457829032858 -0.015197631898765029 -0.32805837315944053; 0.11521335853420495 0.016146828166718294 -0.2015371657252789; 0.0844988754151794 0.020885035069277975 -0.19373047129625873; 0.033597891146296334 0.010637350962738993 -0.09723352276176074; 0.014617521248202526 0.005405038174023768 -0.04939580453757178; 0.011213658178231944 0.0058829860500909 -0.04619240804054333; 0.015253620206588972 0.006447355700841873 -0.06196133927340085; 0.007624634110329716 0.0030740269473295083 -0.03396242343015363; 0.00080141386658674 0.001693224097442207 -0.005774560299995901; 0.0005488115054491502 0.0004475410632791535 -0.0009573393672202765; -0.0005791847684528165 0.0007355734686144028 -0.008761328827695793; 0.003949880963772915 -0.00016400202656134292 0.0013571943158942974; 0.0016403021809576937 -0.0013345506909143937 -0.002416396422573993; 0.0001809923380711422 0.00418261392395163 0.0001413875669468833; -0.0013122749762205566 0.005069481558218191 0.001919160402554694; -0.0012208240020966832 -0.0024709799764485642 0.004891270686236553; -0.0009774858601976372 8.264258087949892e-5 -0.002187875198208554; -0.0011062219353270616 -0.0019115437306923963 0.0005395145490859799; -0.00027025155712373603 -0.00019788600679444086 -0.0005307905803978341] %
+
+Mass Used: 106.41733544490035 kg
+Launch C3: 106.34782621491892 km²/s²
+||V∞_in||: 2.2143744846908278 km/s
diff --git a/archive/ES_0.6231004580258707 b/archive/ES_0.6231004580258707
new file mode 100644
index 0000000..fef3c01
--- /dev/null
+++ b/archive/ES_0.6231004580258707
@@ -0,0 +1,22 @@
+archive/ES_0.6231004580258707---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T19:43:03.530
+Launch V∞: [5.302086453359922, -8.673063289065977, -1.9987932572883964] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006061818355095913, -0.0032878456362436534, 0.008845890077202821] km/s
+ V∞_out: [0.0031296886885126074, -0.008728232787938002, -0.006309745167611832] km/s
+ time of flight: 1.1155552955415152e8 seconds
+ arrival date: 2026-11-04T23:21:52.530
+ thrust profile: [0.5458208306707537 -0.4263252877171058 -0.3375140407175874; 0.310695821956723 -0.07311223203468675 -0.3393630590445453; 0.19852099412931704 -0.006692599280490423 -0.31099221435188174; 0.11799547534867409 0.008905597283539924 -0.23510649331667924; 0.04922115670126822 0.007227576149418178 -0.1174203312640871; 0.020076719350499678 0.003909582326953639 -0.054887207267497067; 0.014312575702857901 0.0027563469163004997 -0.04336857524902208; 0.006170553896568759 0.0009374036222564541 -0.01982506900170405; 0.0022620624293063296 0.0008743013518632884 -0.005941352491568763; -5.9659188508014854e-5 0.0006663008220776114 -0.0030027816626621625; 0.006831937238370605 0.00505182796873982 -0.005834016484091844; 0.0011326289444031227 -0.0004859773579390979 -0.003865022752666389; -0.010546319305323902 0.0021695979070067268 -0.01019898522833834; -0.007294481066293409 0.011698422817159522 -0.011734857364905371; -0.009675338395273961 0.014109270443442 -0.007211303459516625; -0.004702864912490447 0.00367155709850474 0.002406581812854122; -0.0007987042179969752 0.000506470135380414 -0.01948785786408907; 0.006101390651178501 -0.0017953577116097182 -0.004867624306388022; 0.017097803692778232 0.009674488241242254 -0.006240568459413205; 0.010124079467300153 -0.008368143169793885 0.014461543841327227] %
+
+Mass Used: 100.86282234435066 kg
+Launch C3: 107.32932206042831 km²/s²
+||V∞_in||: 0.011216298050421961 km/s
diff --git a/archive/ES_0.6234010852872424 b/archive/ES_0.6234010852872424
new file mode 100644
index 0000000..0dfc582
--- /dev/null
+++ b/archive/ES_0.6234010852872424
@@ -0,0 +1,22 @@
+archive/ES_0.6234010852872424---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T02:52:12.541
+Launch V∞: [5.259766987346145, -8.645686585622462, -1.8251764655847904] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.7537892621428706e-5, 2.4033334111166497e-5, 4.385081257956424e-5] km/s
+ V∞_out: [-3.0710208807597355e-5, 4.1168226047031106e-5, -4.606605720608769e-5] km/s
+ time of flight: 1.09963847917711e8 seconds
+ arrival date: 2026-10-17T20:22:59.541
+ thrust profile: [0.8355591004262594 -0.6530259426690127 -0.4780150555596401; 0.23789555247320476 -0.06172027490388365 -0.2989428660667243; 0.14379008077413793 -0.009438374298222661 -0.2739767128161378; 0.11648218042878203 0.0040720033972590245 -0.2747415552407647; 0.031124033317323548 0.0031960275779960167 -0.08553628433116232; 0.012151499624271719 0.0015247712635114768 -0.03361868294272348; 0.041585341372301445 0.006898476049694552 -0.1397420268447881; 0.003811657798103933 0.0012956165627787898 -0.020192550691419026; 0.0009662807602249484 0.0008702679698277253 -0.01009975037403716; 0.0005266868801097522 0.0003741082966418216 -0.006354844395601971; -0.0009435115089419317 0.0007799445406316389 -0.004125665126675495; 0.003451910944250301 0.0016805472345207402 -0.0037455623215139136; 0.0035785822285886756 -0.0003523428738744478 -0.0007308017287937325; -0.002384172417668314 0.0013291071205391322 0.00030053388081288613; 0.002251559866551266 -7.288796480517867e-5 -0.005598277513711081; -0.0024193773125485178 0.0028764533706732384 -0.0007931564472864073; -0.005203296385920656 0.002575101537449541 -0.0010423102562098943; -0.008397759923011224 0.003696166255266172 -0.0013664292965811877; -0.000487671713135851 0.0004146210617554367 -0.0033694119822500444; 0.00605896579853292 -0.001599208376064272 0.0076654593158287125] %
+
+Mass Used: 110.45943200212287 kg
+Launch C3: 105.74431442851312 km²/s²
+||V∞_in||: 6.899526177407776e-5 km/s
diff --git a/archive/ES_0.623517606161271 b/archive/ES_0.623517606161271
new file mode 100644
index 0000000..4717da8
--- /dev/null
+++ b/archive/ES_0.623517606161271
@@ -0,0 +1,22 @@
+archive/ES_0.623517606161271---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T00:34:41.814
+Launch V∞: [7.050543423857025, -7.509932099657216, -1.7811350829802017] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2140383058546794e-5, -2.2198576499460874e-5, 1.616683335793803e-5] km/s
+ V∞_out: [2.772199432117306e-5, -1.6826534630977487e-5, -1.3882842009744631e-5] km/s
+ time of flight: 1.1011439429220013e8 seconds
+ arrival date: 2027-11-03T11:54:35.814
+ thrust profile: [0.4497303743176637 -0.2269773623468831 -0.2369604875539595; 0.2466421228998084 -0.018478658648197026 -0.26844908755817803; 0.16272004679866856 0.019869955789140373 -0.2704026378591649; 0.09479939211919627 0.021594084496344184 -0.21204380187954527; 0.04871967313766914 0.013312191533732929 -0.13695900657537802; 0.04906297958934214 0.015871509051888645 -0.15570073560127218; 0.02652633201438425 0.009730370424847454 -0.09634590831702046; 0.015252494988792635 0.006113598048954031 -0.06191321337655156; 0.016869281898893494 0.006217652932801823 -0.07084407952922503; 0.0018855942713555196 0.0007545220164630347 -0.0088123552866023; 0.0009141544268759 0.00034267469647846356 -0.00448517054960826; 0.00018611286740803385 0.00023317505888148233 -0.001388709752914883; 0.0002787528256136955 -8.829036842149501e-5 -0.0020429356861433956; -0.0015295368451018415 -0.00010947292106834616 -0.0014399746653427148; 2.2190988166981025e-5 4.63795614604242e-5 -7.693701013712531e-5; 0.0002072959703645987 0.00020495649124757534 -0.0020562358677361373; 0.0031821922165618816 0.0031618006114154428 -0.001457587821429347; -0.0007628846052273393 0.0003449939555344116 0.0019210717377764579; -0.00015395159971182278 -0.0006624437017792532 0.00084621659611866; 0.0005479938926295952 -0.0001780759584673339 -0.0036287357685301303] %
+
+Mass Used: 89.96071195577633 kg
+Launch C3: 109.28168489697828 km²/s²
+||V∞_in||: 3.5275201791129986e-5 km/s
diff --git a/archive/ES_0.6235715387321148 b/archive/ES_0.6235715387321148
new file mode 100644
index 0000000..5d3fea8
--- /dev/null
+++ b/archive/ES_0.6235715387321148
@@ -0,0 +1,22 @@
+archive/ES_0.6235715387321148---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T20:40:20.967
+Launch V∞: [5.402435379098303, -8.723387041560612, -1.9396334963981983] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.2905275825633515e-5, -9.917885165488272e-5, 7.862155379070784e-5] km/s
+ V∞_out: [8.486818577345279e-5, 8.7963901481467e-5, 6.227644110625647e-5] km/s
+ time of flight: 1.1012799183062015e8 seconds
+ arrival date: 2026-10-19T11:46:51.967
+ thrust profile: [0.44154029501541575 -0.3459210920825493 -0.2698543518336445; 0.2781212715585428 -0.06506221471893213 -0.29725233365371667; 0.20413472857811857 -0.005985375486126052 -0.3116903553186392; 0.14738166184154575 0.012407539496918944 -0.2874604526089084; 0.031783062718668244 0.005897170366935739 -0.0787771489971212; 0.03094656474326854 0.0069154520780365675 -0.08649874312606616; 0.024564522910399497 0.006980729629438695 -0.0758437067169532; 0.006142971274473671 0.00220453703802929 -0.02112688257541353; 0.012363372442800403 0.004045412054192194 -0.04408988437424982; 0.003597055150018334 0.0012780485532010626 -0.014703160085167769; -0.00010161946093013315 0.0005032763527495249 -0.00038932575243526486; 0.0009942312472599967 0.0013151158942396718 -0.0002821233256256871; 0.0012017495311819777 -0.0009616895946226561 0.000744706304445431; -0.0003220031209551611 5.8486939472038265e-5 0.001187803336955329; -0.001714505872938271 0.0001437701801592749 -0.0002792808091720757; -0.0006995474276036415 4.012038187701145e-5 0.0006788325475333016; -0.00232015541951366 0.0005168952867505386 0.0005940186486166163; 0.00016679750858273148 -8.941035014663708e-5 -0.00016626012979808168; 0.000704296709239376 -0.0006060095407137611 0.000570855154975577; 0.0004339699948920797 -0.0012292653632074609 1.5121298265944921e-5] %
+
+Mass Used: 91.39865083925588 kg
+Launch C3: 109.04596760255052 km²/s²
+||V∞_in||: 0.00013717420146016073 km/s
diff --git a/archive/ES_0.6236327790852165 b/archive/ES_0.6236327790852165
new file mode 100644
index 0000000..dea68fd
--- /dev/null
+++ b/archive/ES_0.6236327790852165
@@ -0,0 +1,22 @@
+archive/ES_0.6236327790852165---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-17T00:59:01.678
+Launch V∞: [6.637184931070404, -8.08918946668177, -3.1168333891456776] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.191435457086488e-6, 5.068342651231363e-6, 0.00033199366281753446] km/s
+ V∞_out: [-0.0003261776516041714, -4.090526982223216e-5, 4.575992976172937e-5] km/s
+ time of flight: 1.3066290299301694e8 seconds
+ arrival date: 2028-07-07T08:14:03.678
+ thrust profile: [0.10290162315873971 -0.060211077950617024 -0.07811599143463294; 0.026732238191692112 -0.009080454166142508 -0.055379154748485454; 0.017081723872657564 -0.006800168303046849 -0.06255708670251779; 0.014483913103081242 -0.007931991918229955 -0.07539578866856247; 0.009915927932217801 -0.007011942552339801 -0.06490724262445843; 0.007008520580139044 -0.006018728886022283 -0.05355968054706327; 0.004891917345146177 -0.0052833326431561975 -0.047741592696450404; 0.004388715553318156 -0.00510440280084205 -0.044712858541430964; 0.001565467075459792 -0.00186450746940328 -0.0172459012003725; 0.00093225185885863 -0.0006678184268432161 -0.006821854675249277; 0.0011480426817685086 -0.0009188106166257582 -0.0032308916046316595; 0.0003273386596738139 -0.0005061222492540602 -0.004201715337932164; 0.0012706460814422274 -0.0009453482464507859 -0.0033132962419314075; -0.0008410032951482586 -0.0011201186169594807 -0.003420213168947243; 0.00042720776162391083 -0.00017074223766861145 -0.002197653567151659; 0.00021368548211473767 -0.0003851560695896939 -0.0008099643880990785; 0.0009161027279946612 -0.00034623270064748553 -0.00494140183186101; -0.0022277093857651182 0.00308944929168941 -0.0015445292381004612; 0.0006465180676256575 0.0011620367499815313 -0.0022814260839224645; -0.0030059713392918113 0.0008822712974963686 0.002484620002251542] %
+
+Mass Used: 32.2273898581052 kg
+Launch C3: 119.20186041279669 km²/s²
+||V∞_in||: 0.0003320900692903242 km/s
diff --git a/archive/ES_0.6239789886367926 b/archive/ES_0.6239789886367926
new file mode 100644
index 0000000..a60d3d0
--- /dev/null
+++ b/archive/ES_0.6239789886367926
@@ -0,0 +1,22 @@
+archive/ES_0.6239789886367926---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T13:08:28.117
+Launch V∞: [8.134364036428657, -5.555779588736754, 0.009180844372489961] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.234586043328408e-5, 5.4284585525455524e-5, 0.00015558766488263674] km/s
+ V∞_out: [0.00015155405123625586, 1.947800383031772e-5, -6.589586781492263e-5] km/s
+ time of flight: 1.8749577787356722e8 seconds
+ arrival date: 2030-04-22T15:18:05.117
+ thrust profile: [0.3219322231641249 -0.005923965288510969 -0.09686854752903476; 0.0251879663498434 0.02854438215316678 -0.051904538155737055; 0.04425009017292406 0.03729073454759424 -0.048647911169621284; 0.04438197321373394 0.03415711093048795 -0.09822270307572893; 0.03327433414210843 0.039990131162612914 -0.10038212615169351; 0.014647327747814643 0.03672655894760129 -0.05984381743264699; -0.006643794317474898 0.015161236132961425 -0.06196918678435277; 0.015510243455108659 0.015039473080183142 -0.06922150402156656; 0.008042108927294296 -0.011834254405738988 -0.006726761799194935; -0.02192588337676572 0.022338648392483354 -0.06220738120380465; 0.021213205844300597 -0.022080577632027143 -0.020875621094027106; -0.009928708568704283 0.007148585451123875 -0.023052486394542892; -0.0036944136950641145 0.03200268442926007 -0.05029734019902518; -0.0004009984691047518 -0.0005374855028811663 0.0004910037204272856; 0.024786816361711164 0.08843438834483931 -0.025761023879435314; 0.029436078756993906 -0.08101016436591527 0.003929473282862857; 0.045052457345052824 0.14966136516845768 -0.10622472797251992; 0.10994128543502017 -0.09692056623202082 -0.1427462413460508; 0.07381873117981981 0.0698862207758787 0.15560857449715182; -0.015955905128397996 -0.02122216709354172 -0.2868417099660709] %
+
+Mass Used: 161.94003188817578 kg
+Launch C3: 97.03464940367124 km²/s²
+||V∞_in||: 0.00016629394206586713 km/s
diff --git a/archive/ES_0.6239897937417502 b/archive/ES_0.6239897937417502
new file mode 100644
index 0000000..84cd9ff
--- /dev/null
+++ b/archive/ES_0.6239897937417502
@@ -0,0 +1,22 @@
+archive/ES_0.6239897937417502---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T20:59:58.971
+Launch V∞: [5.1668551228007455, -8.629299770148712, -1.7621998954774272] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.780999898314965e-5, -2.312083312433854e-5, 5.252146471218003e-5] km/s
+ V∞_out: [4.643806942188045e-5, 4.666453838325826e-5, 1.970988949528607e-5] km/s
+ time of flight: 1.1414379314244689e8 seconds
+ arrival date: 2026-12-04T23:36:31.971
+ thrust profile: [0.6321515653851276 -0.4948814902966088 -0.3895957309892303; 0.3307444491494039 -0.07713896081950508 -0.3693607589230067; 0.1998044915414329 -0.006111357501056246 -0.324075717503181; 0.11358500729780999 0.00950802386635675 -0.237198855347183; 0.057926034937937756 0.009447490337252997 -0.1447219719775149; 0.021017950988379237 0.004375567267553137 -0.056639016760438206; 0.009191985516849672 0.0003539420937256881 -0.025197519181886938; 0.009403431609723754 0.0011983143467723175 -0.029228795750164595; 0.006829037158060397 -0.006757685812066384 -0.004384923805107337; 0.0010685112273438732 0.007234089137733941 -0.018955826001159373; 0.0030143264290768234 -0.0055973997803431055 -0.011796727794354214; 0.002440361996519853 -0.0007892789375984997 -0.007973687775816767; -0.014993425983271875 -0.012240007382011801 -0.007521061875531138; 0.007994188825695919 0.006330851053044063 -0.0034836963659541052; 0.009384203844647807 -0.002174527683818931 -0.00926935862433306; -0.020474655868498885 0.02497588017654908 0.013397644734645588; 0.03208588511715041 -0.02075408447377955 -0.029370081620567274; -0.016194388742752787 0.033117771488837044 0.026228789658801654; -0.024354200492569016 -0.002878281332517061 0.0035925916647632627; 0.03757704739031004 -0.019878083792696802 -0.05806521158107897] %
+
+Mass Used: 119.76652271283274 kg
+Launch C3: 104.26655485472159 km²/s²
+||V∞_in||: 6.872170838230129e-5 km/s
diff --git a/archive/ES_0.6239965396819411 b/archive/ES_0.6239965396819411
new file mode 100644
index 0000000..93703ab
--- /dev/null
+++ b/archive/ES_0.6239965396819411
@@ -0,0 +1,22 @@
+archive/ES_0.6239965396819411---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T11:55:58.797
+Launch V∞: [7.037120314582937, -7.204863338736107, -1.5485456478621984] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.022177785599963272, 0.15080387251878105, 0.026660303329056122] km/s
+ V∞_out: [0.14708279655554835, -0.02877513078968124, 0.03841251604717441] km/s
+ time of flight: 1.1097775481946407e8 seconds
+ arrival date: 2027-11-09T23:05:12.797
+ thrust profile: [0.7858636664376505 -0.3647601343458956 -0.37131349479904635; 0.39248174953617565 0.006022660943787856 -0.37078210860890004; 0.19807436062898287 0.0468433138805149 -0.28741559119058846; 0.09665154389384327 0.036593028047055484 -0.18900390556298916; 0.034789826355240853 0.01700218368138305 -0.08299587456036274; 0.04864276125266657 0.026675690350034153 -0.13566996769701833; 0.07076022970812103 0.04268340844295343 -0.2140262758830534; 0.03373531752658647 0.021389370385337066 -0.11271515167976859; 0.006690650721818402 0.0038333509268453393 -0.02455662087714139; 0.007958991983760525 0.005361531859759983 -0.031080929081526973; 0.0019135573909813564 0.001772575542189065 -0.010390003576141157; -0.0016932595692246424 -0.0025587079996445676 -0.005171476398845138; 0.005399614937164461 0.005570825922498854 -0.004916817263267807; -0.0011972375004180456 -0.0006735444672342755 -0.003203055479006454; 0.006601682696876377 -6.315077262196867e-5 -0.0014203467790544929; 0.0013714598212389742 -0.0005377403281480205 -0.0057955730301981374; -0.010295306197443337 0.002061800595522302 0.0025449540408378725; 0.0023497313229746733 0.0013639149132063993 -0.0012561240682424676; -0.0012630697136111948 1.1612019638730891e-5 0.0020242226628111445; 0.001992091523393115 0.01345291689785457 0.004266004868844663] %
+
+Mass Used: 122.32614485639215 kg
+Launch C3: 103.82911167529242 km²/s²
+||V∞_in||: 0.15473989115407827 km/s
diff --git a/archive/ES_0.6240551844281097 b/archive/ES_0.6240551844281097
new file mode 100644
index 0000000..917ae76
--- /dev/null
+++ b/archive/ES_0.6240551844281097
@@ -0,0 +1,22 @@
+archive/ES_0.6240551844281097---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T14:56:45.096
+Launch V∞: [7.010463398703812, -7.349444647149538, -1.888797704644153] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.023761349254054376, -0.03849890893819268, -0.015490206276722525] km/s
+ V∞_out: [-0.027904358887299367, 0.03373128385464435, -0.019205705276730944] km/s
+ time of flight: 1.0908120599581057e8 seconds
+ arrival date: 2027-10-21T03:16:50.096
+ thrust profile: [0.8201890513122863 -0.39763575870522416 -0.4284240429517984; 0.27760441336553193 -0.003507540566083995 -0.3012478140936091; 0.13479943106103115 0.02737536834799066 -0.22657552283011384; 0.08524720190683238 0.029513455550228433 -0.1926604875897965; 0.04749292311720123 0.020212718229455338 -0.12740398135418649; 0.04266181887597715 0.020760955412663 -0.13911914040908654; 0.03184174351525515 0.01737344984113528 -0.10839645682186538; 0.022150421887584832 0.008492485550314628 -0.07695203736216256; 0.004859979661988999 0.0027413514228097537 -0.020341439394040883; 0.0013310929025306274 0.0004358672992104207 -0.004033009638898061; 0.00010744888117634284 0.0006479657481746203 -0.0022849528452651997; -0.00028452426830090556 3.317781618556183e-6 0.0014322593524110643; -0.000470014669125946 0.00020083153703040967 -0.0015675578687764993; -5.0065813860279695e-5 -9.258842758465388e-5 -0.0009478389949774196; 0.0011771283003070621 0.0020575998043206346 -0.0005280749644341785; -0.0008528865045884758 0.005462850213238924 -0.0034426219972781605; 0.0017791191015717822 0.0021981537142447176 -0.0019029968906660111; 0.0004006453983178718 0.00047692582483454697 -0.0004676971672734455; 0.0031448792935225146 0.0015184703320114514 -0.00227557702476142; 0.004640406576788128 -0.0004158745373515329 0.002892380893738565] %
+
+Mass Used: 105.48152084442063 kg
+Launch C3: 106.72849045514982 km²/s²
+||V∞_in||: 0.047819600566083954 km/s
diff --git a/archive/ES_0.6241214306441089 b/archive/ES_0.6241214306441089
new file mode 100644
index 0000000..9311ed6
--- /dev/null
+++ b/archive/ES_0.6241214306441089
@@ -0,0 +1,22 @@
+archive/ES_0.6241214306441089---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T17:39:05.426
+Launch V∞: [5.240995269171102, -8.7001814592056, -1.9865199784355771] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004830806646253824, -0.004024940619352588, 8.963339571441347e-5] km/s
+ V∞_out: [0.0021528468731978347, -3.073319215626555e-5, -0.005909003059841316] km/s
+ time of flight: 1.1520795213209777e8 seconds
+ arrival date: 2026-12-18T03:51:37.426
+ thrust profile: [0.4936313742483307 -0.38038621164640735 -0.3161802296676532; 0.17297476709444726 -0.038275205828306125 -0.21075793449170077; 0.12149419587633663 -0.00221673124842179 -0.2170246815038619; 0.10982405689027756 0.00998863009789275 -0.24998316605675416; 0.08865598788647155 0.014519515691460289 -0.24043024487457276; 0.03241652614029359 0.007035404672523815 -0.10571439432991937; 0.012961557290907385 0.0014643322392124906 -0.03873958999282058; 0.014673358563725845 0.0037440929768316174 -0.0389839039616038; 0.012285673488781162 -0.005764100910900408 -0.014206496293595999; -0.000632303521775785 0.0034534729021310257 -0.00648219762970412; 0.006533585515685992 -0.004944203506209362 0.006250313200063307; 0.0006231540323463148 -0.0024920790536746363 -0.02566953707815866; -0.0008674479806068848 -0.010884654570266933 0.008431667813966972; 0.012362979166379622 -0.0279002574786595 0.012632751509964202; 0.008231611543093889 -0.02418742257175747 0.02570462742696893; 0.0019357501165303793 -0.00544273283837786 -0.007027209036136757; 0.010918687493579484 0.02495889723863366 0.0002874441357733754; -0.018126339311866246 -0.013484615028862147 0.028434361673165702; 0.006614088653067822 0.03431948532932626 -0.011434494038020835; -0.04419383033004783 -0.016499356360073936 0.01929034265677601] %
+
+Mass Used: 103.34820807219603 kg
+Launch C3: 107.10745045930246 km²/s²
+||V∞_in||: 0.006288471514480431 km/s
diff --git a/archive/ES_0.6241363451259188 b/archive/ES_0.6241363451259188
new file mode 100644
index 0000000..421201f
--- /dev/null
+++ b/archive/ES_0.6241363451259188
@@ -0,0 +1,22 @@
+archive/ES_0.6241363451259188---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T17:19:01.823
+Launch V∞: [5.409996823654991, -8.694922904056977, -1.9386407094899207] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.9329179826370947e-5, -2.010059647042532e-5, 4.168372004879799e-5] km/s
+ V∞_out: [3.8719801417548955e-5, 3.4840381497852106e-5, 1.7008940862319783e-5] km/s
+ time of flight: 1.1137224548449902e8 seconds
+ arrival date: 2026-11-02T18:03:06.823
+ thrust profile: [0.45842452581543625 -0.3444009781015379 -0.2768628253216421; 0.25524125253738406 -0.05504108364896737 -0.2852921362393034; 0.14761747584055004 -0.0023183934520700678 -0.24024600636721072; 0.0937212609912391 0.00883134950499034 -0.19505589117291636; 0.05720564485258532 0.009405098784965192 -0.1424203802484555; 0.047453474961210926 0.010123549065863421 -0.1337472084947584; 0.04807703527527697 0.01207427616052909 -0.14863273923691944; 0.011856597911178378 0.0029643379755866614 -0.040096175682167445; 0.0006120301555841156 -0.0003945239006812315 -0.0011338042787760402; 0.00322188899046992 0.0002233823292798443 -0.0012156967886400348; 0.005987014047783357 0.0017881794319711767 -0.012222110046604177; -0.0002924774326611802 -0.0014192568889754423 -0.002186449634129696; 0.0005495674170367122 0.0053405256260272834 -0.006784529246979731; 0.0003720544503694563 0.0008221006795156873 0.00045099802963671385; 0.00038620079995654974 -0.00171774925355079 -0.003937402008723253; -0.00019550107557127954 0.00015299506680271837 -3.824424324814916e-5; 0.004117881670231089 -0.006312139535279218 0.002343818506761647; 0.027602517772037122 0.012096679939669312 -0.005679717506308106; -0.012335742135365185 -0.026753123137951803 -0.020717595817076905; -0.0009277013193270082 -0.0036195541853763953 -0.0018584780711524218] %
+
+Mass Used: 94.49528249723608 kg
+Launch C3: 108.62807773994328 km²/s²
+||V∞_in||: 5.4788386404976766e-5 km/s
diff --git a/archive/ES_0.6242494238755424 b/archive/ES_0.6242494238755424
new file mode 100644
index 0000000..44e6bd3
--- /dev/null
+++ b/archive/ES_0.6242494238755424
@@ -0,0 +1,22 @@
+archive/ES_0.6242494238755424---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T06:56:42.455
+Launch V∞: [7.208958526607169, -7.363540632044457, -2.005384500495625] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0063048804088907656, 0.0358552388957396, 0.0065822978871746774] km/s
+ V∞_out: [0.03524384395182826, -0.006818037778479766, 0.008939973160323248] km/s
+ time of flight: 1.100604009554073e8 seconds
+ arrival date: 2027-11-01T03:16:42.455
+ thrust profile: [0.35053222872676526 -0.165760523685039 -0.19447357302386292; 0.2627378286263134 -0.0013126629345633785 -0.2799241009862816; 0.1701649400492179 0.03491228690073609 -0.27900926822223804; 0.11570780825947263 0.037954288432858856 -0.24903495105370288; 0.07274839737070915 0.029963057019619974 -0.19360664268533873; 0.038970638116385646 0.018033844393487045 -0.12104318389774756; 0.013924789712854376 0.007403611480422142 -0.050497278076024554; 0.01307332046913063 0.0076384681201700525 -0.053559759763628666; 0.004863928854438666 0.0028112616390287394 -0.02212012839465224; 0.0011158633055589986 0.002068257320045685 -0.008255556896126193; 0.002338595649891523 -0.0014094727438115856 -0.000589138964290812; -5.236464772852525e-5 -0.0010366478547772047 0.0028576112069410606; 0.0008514009654206641 0.0063990744132507455 -0.0062110884266154956; 0.0026041053567130235 0.0002631490819182942 -0.0007828039571116784; 0.001235387269995104 -0.0001911603445658662 -0.0014240202250793872; 0.0002709236572278059 -0.0007130568150293176 -0.0014208352733531835; 0.0046822925919600645 -0.0013011751932044376 -0.004285167725372502; 0.007623611814105781 -0.00015920766235786416 -0.0009123390679471569; -0.002114435306356748 0.00028534749586915165 -0.0012913329528838643; 0.0010776145084276565 -0.007347027354639515 0.006209197048109236] %
+
+Mass Used: 85.3854405959828 kg
+Launch C3: 110.21238067293999 km²/s²
+||V∞_in||: 0.03699562567002316 km/s
diff --git a/archive/ES_0.6242606477221507 b/archive/ES_0.6242606477221507
new file mode 100644
index 0000000..f8d682d
--- /dev/null
+++ b/archive/ES_0.6242606477221507
@@ -0,0 +1,22 @@
+archive/ES_0.6242606477221507---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T13:33:50.232
+Launch V∞: [7.171946864163408, -7.382972247332238, -1.8763772848291176] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008050427965255971, 0.0477882504296257, -0.04433636032033731] km/s
+ V∞_out: [-0.01652778671617609, -0.02406896602691627, 0.05475431936985144] km/s
+ time of flight: 1.0966357069673009e8 seconds
+ arrival date: 2027-10-27T19:40:00.232
+ thrust profile: [0.44288604075820914 -0.21039110326908228 -0.24129712190666677; 0.2561620796549788 -0.00234819349678405 -0.27996199666018284; 0.1409232319674781 0.027511271012105466 -0.23319464943044674; 0.10432176408030557 0.03302882956884905 -0.2253754072253928; 0.07144387714583174 0.027868312478421874 -0.18645671861139848; 0.046629363122830336 0.020152519457103394 -0.1409867842088911; 0.03610137883940576 0.016183253827757878 -0.12106625188257897; 0.015749237796607068 0.008035492553890924 -0.0597131455191619; 0.006908395878218165 0.003539565069846145 -0.02759332297310587; 0.0020049938491686777 0.0011805400320049591 -0.008674461243594103; 0.0003210817476995004 0.0002753391847992716 -0.001966826647147522; -0.0008902900247925922 0.0010184843211138023 -0.0049698483698461925; 8.605696873077847e-5 0.00023575379663820376 -0.0018497987361258835; -6.452385585554608e-5 0.000243216155731836 -0.0013864415248398846; 0.00024615248889172563 0.0003680054918530364 -0.0008325936962149429; 0.0011663302202311898 -0.0013007181969566328 -0.0015807198045001147; -0.0027344926693133233 -0.0013789933270717185 -0.0017806771898145161; -0.0013875150685115022 -0.002466619657927175 -0.0013166688468009276; 0.0005497597297017332 0.005143634092420461 -0.00022686492292453228; -0.00032691830125892996 -0.00040311960967990873 -0.0004945438744694622] %
+
+Mass Used: 89.75304801251878 kg
+Launch C3: 109.46589274228407 km²/s²
+||V∞_in||: 0.06568286775105954 km/s
diff --git a/archive/ES_0.6244481035888969 b/archive/ES_0.6244481035888969
new file mode 100644
index 0000000..fcd8473
--- /dev/null
+++ b/archive/ES_0.6244481035888969
@@ -0,0 +1,22 @@
+archive/ES_0.6244481035888969---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T01:02:46.367
+Launch V∞: [7.123006646917425, -7.415927412525764, -1.8005249597382649] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.026533107571427458, -0.18422954756274226, 0.008177979753823597] km/s
+ V∞_out: [-0.17847609333511585, 0.032536760442446425, -0.042520970319326265] km/s
+ time of flight: 1.0968974592261803e8 seconds
+ arrival date: 2027-10-28T14:25:11.367
+ thrust profile: [0.5178456048483437 -0.24747598845999197 -0.28287267950938033; 0.21436638615325265 -0.004849923023549568 -0.23835193586419876; 0.13600453263694734 0.023497148755215188 -0.2279734077323851; 0.09093511036227159 0.027313072428490508 -0.20102998292825233; 0.07448913842241704 0.02683661698434129 -0.1981225333627344; 0.04424876075147715 0.018192531550277023 -0.1383582963607561; 0.03842321563452931 0.01734410392863118 -0.1329261878311468; 0.012920094672035505 0.004855454628617325 -0.0468043162712091; 0.006127822251841985 0.0030808237977983295 -0.02635855198252333; 0.01796283195114347 0.009057159743083389 -0.07458801950345463; 0.0028205085227984536 0.0012671221692184406 -0.012101855996417468; 0.00044837488611115193 -0.00029378030664567044 -0.0005223635656655739; 0.0005684189361280434 -0.0001430200758162954 0.0006476252307179586; -0.0004619305108873567 -2.8830384096901983e-5 -0.0002877838396337899; 0.0005497084380836868 -0.0002329767717473096 -0.00027714560928442783; 0.0003269278433108057 0.0009909237273872929 0.00028778089724122756; -0.00042063942283853805 -0.0005177969265653961 0.002411773522729202; 0.0008700097773632442 0.000146652394748764 -0.0005827500915443235; -0.0014605629755208606 -0.0006285263789893709 -0.0002516482246790134; 3.902277418922681e-5 -0.001395811245507692 0.001583798522345843] %
+
+Mass Used: 92.83474379233849 kg
+Launch C3: 108.97509321052136 km²/s²
+||V∞_in||: 0.18630998724014664 km/s
diff --git a/archive/ES_0.6244881300787785 b/archive/ES_0.6244881300787785
new file mode 100644
index 0000000..c763316
--- /dev/null
+++ b/archive/ES_0.6244881300787785
@@ -0,0 +1,22 @@
+archive/ES_0.6244881300787785---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T03:06:32.534
+Launch V∞: [5.327732599529465, -8.705330159854102, -1.3126940398362243] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.6143406197916295e-5, 2.507235891682629e-5, -5.136022822233755e-5] km/s
+ V∞_out: [-4.655855321043633e-5, -4.4344116712227415e-5, -2.1014895303065973e-5] km/s
+ time of flight: 1.1073264758205144e8 seconds
+ arrival date: 2026-10-25T18:10:39.534
+ thrust profile: [0.47265619752882776 -0.34176146458726375 -0.2540989085065388; 0.41004550838728776 -0.07607920325895827 -0.3976408237727856; 0.16838231178142385 0.0012650253524190901 -0.2481679103547839; 0.17012202857308417 0.02340408883532267 -0.3067292157923956; 0.0898186981328882 0.018550428778551942 -0.1994709237285933; 0.055523762403340386 0.013079272190122802 -0.13855699721138948; 0.03298467323312504 0.0092106878346988 -0.09030254459081716; 0.03172657037798372 0.009591077571132632 -0.09238816595731916; 0.015270322394253752 0.004965880364730217 -0.047158920518527166; 0.001455772927654756 0.00070106763443128 -0.004565613740049851; 0.0018304027116857098 0.0005035195136599017 -0.005993118104959448; 0.00023778126513052632 0.00039139770106753555 -0.00278217335874798; 0.0007289748697695972 -9.265913423274854e-5 -0.002670302985926955; -0.0006952939595851089 0.0012164801388093631 -0.004874263159771287; 0.002388174465767519 0.0007767779692471608 -0.0028137656705623593; 0.00023783726895272898 0.003069619724462167 0.0005244156681022275; 0.0005428400240693639 0.0005038855427794884 -0.0034030789786503885; 0.00035037626592211626 0.0008703860030880045 -0.000893288046314094; 0.0005626838958756124 -0.0014973325793560342 -0.0024726219878149153; 6.575599154381908e-6 -6.300585958645896e-5 -0.0003349425634664553] %
+
+Mass Used: 110.87388975471504 kg
+Launch C3: 105.89067348637597 km²/s²
+||V∞_in||: 6.762279228405414e-5 km/s
diff --git a/archive/ES_0.6245428499469451 b/archive/ES_0.6245428499469451
new file mode 100644
index 0000000..6c94a84
--- /dev/null
+++ b/archive/ES_0.6245428499469451
@@ -0,0 +1,22 @@
+archive/ES_0.6245428499469451---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T17:38:27.209
+Launch V∞: [7.227531455925665, -7.196258838611113, -1.3753851911697703] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.027601320988704717, 0.12197257121814434, -0.15639676203442973] km/s
+ V∞_out: [-0.050175903948838134, -0.07366392107968162, 0.17930951848788898] km/s
+ time of flight: 1.1098164665635175e8 seconds
+ arrival date: 2027-11-09T05:52:33.209
+ thrust profile: [0.4982163566168093 -0.2196362858112838 -0.23597158968900123; 0.3289295658788341 0.012542089619347305 -0.31322726756019686; 0.22020039337070432 0.0561976950408463 -0.3155184047745515; 0.13000649159263716 0.048688699001851826 -0.24733347127583843; 0.10777055383718144 0.051204797715507545 -0.24694868773880072; 0.09608055833830768 0.05138651537506668 -0.24624902431704015; 0.043242001578434164 0.02544963228377547 -0.12794902232344071; 0.025176113768011564 0.015801548661057048 -0.08140153999367303; 0.00195842590050464 0.0013050605020503273 -0.007026872051108169; 0.001040328827322651 0.0007244052433174475 -0.003895728194506496; 0.0004633271449300937 0.00037196314607962464 -0.0011880267671464794; -0.00025483228263776766 0.0004590408507943115 -0.00029385798865704703; 0.00015199123082141924 0.0001933826504965616 -0.0006300306253190023; 0.0002285770422727705 -0.00022667367168037423 -0.0011107422240574027; -0.0002612719216985968 -0.0003405058293121488 -0.00023366332573667662; 0.00011843604785632836 4.9444138772499564e-5 -0.00039908231726105004; 0.0002465012956619489 0.0002713797319034931 -0.0014801469336549742; -0.0002141332446239978 -0.0007926375529581576 5.587408988538037e-5; 0.0004450313307157778 6.293412350925448e-5 2.7746695491861193e-5; -0.00018678182425728554 -0.00010183295673940487 -0.00016413194547855168] %
+
+Mass Used: 110.79561118859556 kg
+Launch C3: 105.91503664277263 km²/s²
+||V∞_in||: 0.20024756733788512 km/s
diff --git a/archive/ES_0.6246764083378422 b/archive/ES_0.6246764083378422
new file mode 100644
index 0000000..b30db5d
--- /dev/null
+++ b/archive/ES_0.6246764083378422
@@ -0,0 +1,22 @@
+archive/ES_0.6246764083378422---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-25T00:22:02.064
+Launch V∞: [6.976559531246028, -6.653076836933902, -1.1201220677718868] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7741163553166692e-9, 1.0613576109655874e-9, 1.536926031082528e-10] km/s
+ V∞_out: [1.374669959190586e-9, -1.3830415914014475e-9, -1.0603087280758674e-9] km/s
+ time of flight: 1.235633474299285e8 seconds
+ arrival date: 2028-03-25T03:31:09.064
+ thrust profile: [1.0 -0.3994121022051953 -0.3409844698502948; 0.7380861183460187 0.11479093923168135 -0.5150279501020387; 0.46881935260654367 0.20214288652103082 -0.5005924785711352; 0.20275031476771235 0.12586118617364606 -0.2913515611683158; 0.14263764420466743 0.10942586092651674 -0.25224733169147245; 0.021179218233155595 0.018613986774272312 -0.04526783934716405; 0.025181442561984586 0.025060307486796392 -0.060618520059936884; 0.002700775778058189 0.0023304630092294163 -0.006693197104400568; -0.0008364290899280456 0.002116411046127065 -0.003868392183203086; 0.0011699010483546548 0.003046044703176015 -0.0018322232888055212; 0.000979636926454793 0.0006311879106428732 -0.00305667872599816; 0.003865273038083529 -0.002088637563086101 -0.0026391659926929246; 0.0071623534093447384 0.0047177967780107355 1.663232950658341e-5; 0.009179642690697544 -0.006608842560396722 -0.0022789258975833534; -0.001201559547345227 -0.0026031912558523787 -0.0010369417050719156; -0.001625074928905945 0.007191092194405712 0.002939989243648985; 0.010146736030918029 -0.0034808553338461215 -0.0007058319402726146; -0.00040162229871433097 -0.001891716329698259 -0.0009512293581875647; -0.007515372765404829 -0.005115069814012822 0.009354699869684333; -0.0019028833454851428 -0.00012562061620441985 -0.0007041916984380191] %
+
+Mass Used: 179.34463125654065 kg
+Launch C3: 94.19048773787577 km²/s²
+||V∞_in||: 2.0730630084025114e-9 km/s
diff --git a/archive/ES_0.6247738667706106 b/archive/ES_0.6247738667706106
new file mode 100644
index 0000000..d87aeea
--- /dev/null
+++ b/archive/ES_0.6247738667706106
@@ -0,0 +1,22 @@
+archive/ES_0.6247738667706106---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:14:24.956
+Launch V∞: [7.050939930075023, -7.5516733345873, -2.173975635062726] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01264048776827068, -0.033888902053612315, -0.0445938934326561] km/s
+ V∞_out: [-0.05014271352995738, -0.008141023620612023, 0.026797541046488026] km/s
+ time of flight: 1.0920762482656027e8 seconds
+ arrival date: 2027-10-24T15:41:28.956
+ thrust profile: [0.44996544695166546 -0.23229107087688305 -0.27283695695288385; 0.22986456425107887 -0.017289472580939037 -0.27664247462316555; 0.145048719888001 0.014572206116499535 -0.26449402412240064; 0.09490434568389627 0.018256852505858394 -0.22788009356614633; 0.05465110607451868 0.013214017324091158 -0.1606549997294826; 0.012230632624294472 0.0033933026410690793 -0.04235427978318396; 0.0037516142987079016 0.0017024429107611427 -0.01630322118406576; 0.014005326917542835 0.005184658356821816 -0.026685059322208392; 0.004962401485378135 0.0011394914634059751 -0.012336123250558087; -0.0009713542812586011 0.0009489907035660107 -0.0035070009645528913; 0.0038856484189896123 0.00017524727522745217 -0.0024401806909506996; 0.0023210131704120692 -0.00024265011539719204 -0.0009385212481260322; -0.0006064528483435978 0.0016634147951383542 -0.0005745661638631521; 0.004507406756894105 -0.00016739438674776694 -0.004161339931730455; 0.0012634281929447561 0.000847586251313222 -0.005376626603698635; -0.004814668238618607 -0.003153274929817953 -0.001543347803795077; 0.0005030294006972821 -3.088418296691344e-5 -0.003609943746713284; 0.0023435178060470948 -0.0038945835878315795 0.0013269771040109444; -0.002193646685280784 0.0019173595024408615 0.0004725541719166124; 0.00039766617127262214 -0.005492912288630732 -0.004636606157632683] %
+
+Mass Used: 78.66296224752296 kg
+Launch C3: 111.46969411168963 km²/s²
+||V∞_in||: 0.057418245749084135 km/s
diff --git a/archive/ES_0.624884311973688 b/archive/ES_0.624884311973688
new file mode 100644
index 0000000..fb95fcf
--- /dev/null
+++ b/archive/ES_0.624884311973688
@@ -0,0 +1,22 @@
+archive/ES_0.624884311973688---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T18:47:36.731
+Launch V∞: [7.043162197883513, -7.343020009594216, -1.9613853070568605] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.022679401556106746, -0.036705403169079186, -0.01476009039159267] km/s
+ V∞_out: [-0.010306748990612367, -0.04381714286403396, -0.0072981605314292415] km/s
+ time of flight: 1.0820952854108685e8 seconds
+ arrival date: 2027-10-11T04:59:44.731
+ thrust profile: [0.8385953045261704 -0.4151838322250852 -0.47411850182904275; 0.2676477055324721 -0.015465826161184167 -0.312763208207593; 0.15029240285650702 0.019404517929441895 -0.26392793758185007; 0.09779646043761825 0.022916956155300143 -0.22452915019921918; 0.04769531916538674 0.014375196818838927 -0.13343280261724583; 0.025984375964332958 0.009021397012540695 -0.08519905488835985; 0.018793572424504437 0.007294447405886448 -0.0686591695672425; 0.004814666039619342 0.002075332647795547 -0.018796533385335337; 0.006824109690799399 0.002587414673053791 -0.026228718313433673; 0.001321148561202824 0.0006631131320350417 -0.006372836757598879; 0.0007941556084432523 -3.251929186326522e-5 -0.0012417483703924164; 0.00011468690101915812 -3.2283522405593423e-7 -0.0005232010699734302; -0.00014122067099282533 -0.00038762719820315146 0.0006706904397502947; -0.0006355699686086654 0.0013422077814637277 -0.00010452971139703645; -0.0005356863213567361 -0.002317581494663313 -0.0002554637389113122; 0.00035418496000788786 0.0004069093022650968 -0.0031245415175378257; -0.0007296709076820773 0.0006032353757003321 0.00046520324296869765; -0.0009807920411260805 0.002050020561218474 0.002107414904659705; 0.00016752982518836992 5.694248185560092e-6 9.80351353169564e-5; 0.000818740804618238 -0.0001405177447108807 -0.0005155177200793492] %
+
+Mass Used: 102.68856187918254 kg
+Launch C3: 107.37310892973488 km²/s²
+||V∞_in||: 0.04560155858208984 km/s
diff --git a/archive/ES_0.6249393577882304 b/archive/ES_0.6249393577882304
new file mode 100644
index 0000000..bf3a328
--- /dev/null
+++ b/archive/ES_0.6249393577882304
@@ -0,0 +1,22 @@
+archive/ES_0.6249393577882304---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-27T05:30:49.978
+Launch V∞: [7.950585231129742, -6.552996837711963, 2.2496692873386843] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3789247897784585e-5, 1.3536768914999826e-5, 1.3761243772838996e-5] km/s
+ V∞_out: [-9.049137944303693e-11, -1.8186447242242082e-10, -4.903916673662969e-12] km/s
+ time of flight: 1.85424811393809e8 seconds
+ arrival date: 2030-04-12T08:24:20.978
+ thrust profile: [0.09025530566921373 -0.025979145373303838 -0.04149659583033021; 0.02052447141850688 -0.0073868600824862395 -0.032620187798586664; 0.03273581681884311 -0.02425062641208491 -0.08451430789467215; 0.03282257038097454 -0.029766582392711703 -0.10213074869034672; 0.03834237941439092 -0.039180083284030304 -0.13068412169141314; 0.03625629136655113 -0.03916977073009307 -0.127671097734955; 0.028419117505362985 -0.031451808113906805 -0.10103838364178769; 0.021698674952154023 -0.02440244920797616 -0.07695630143667251; 0.023777611367704055 -0.02714143290876893 -0.0826437311084025; 0.038214174409117105 -0.04372702880805302 -0.15330983147432678; 0.000614753788204701 -0.000705792807287362 -0.002258211281046249; 0.0005454959668988728 -0.000516508064521244 -0.0016162181864127416; 2.2562202399163624e-5 -0.00014036116662088574 -0.0007028937598415497; -0.00010212887931015154 -0.00122918465659621 -0.0018393552095993808; 0.00045906504954893617 -0.00033333264770446817 -0.0017513311852390399; 0.0007852564165743584 -1.4220623567025282e-5 -0.00044561299758317944; 9.796785312204417e-5 -0.00011189666306341993 -0.0007261754118576291; -3.281049431400518e-5 0.0007705611399344676 -0.000573064158423641; 0.000823916301800618 -2.214665547429248e-5 0.0006424379071078353; 0.0003227737993880929 -0.0010033384467045983 -0.00016427692444934502] %
+
+Mass Used: 80.34417173259044 kg
+Launch C3: 111.2145849749163 km²/s²
+||V∞_in||: 2.3722548354259123e-5 km/s
diff --git a/archive/ES_0.6249500579574623 b/archive/ES_0.6249500579574623
new file mode 100644
index 0000000..e0ffea7
--- /dev/null
+++ b/archive/ES_0.6249500579574623
@@ -0,0 +1,22 @@
+archive/ES_0.6249500579574623---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T10:27:48.058
+Launch V∞: [5.256310990707662, -8.719873452984526, -1.7210143037572836] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.033149936052702986, -0.013628484285223452, 0.03179657933751515] km/s
+ V∞_out: [0.02306276373147887, -0.03367647524363837, -0.02509565903137321] km/s
+ time of flight: 1.1051652712992793e8 seconds
+ arrival date: 2026-10-24T13:29:55.058
+ thrust profile: [0.6612346585851221 -0.5182195737235102 -0.3951418916171103; 0.22689687930873875 -0.054596588035824394 -0.24999977387939443; 0.1683452527569421 -0.006705457841326005 -0.26590477794268647; 0.1442104871060748 0.009806463789106084 -0.28837976802455184; 0.04665432324260667 0.007490353332572588 -0.12212456221422083; 0.03313764489088043 0.00570255693035863 -0.09645617161835562; 0.02828073748120387 0.00906633267514161 -0.09263064603345764; 0.015081522629009168 0.002762224759851827 -0.05177119824156767; 0.0035737656043433384 0.000575605598407105 -0.010841816556029919; 0.004641524539082667 0.0013171748373376397 -0.018145070164073344; 0.0016888415417152117 0.0004555814701949746 -0.006780428161818119; 0.0024908056092994525 0.0006971962798348313 -0.006279166686796527; 0.001441435315689393 0.005596551558345443 -0.0050280726192186665; 0.0007885623272370218 0.002244494790830741 -0.0023925519978787047; -0.008190235155347975 0.0027514532595792943 -0.008977868738051797; -0.005361917364330457 0.0020932416978634858 -0.007435810851801328; 0.0013374799646959559 -0.018353917855543952 -0.0049733211378225695; 0.013247163924454802 -0.002716049927663451 -0.007212497136229965; -0.011226333498589917 0.00442611947799006 -0.007266678857926243; -0.008914622703810996 -0.010214012384377294 -0.009652941154467042] %
+
+Mass Used: 107.1182180288315 kg
+Launch C3: 106.6268885008356 km²/s²
+||V∞_in||: 0.047913216358096596 km/s
diff --git a/archive/ES_0.6249853306449479 b/archive/ES_0.6249853306449479
new file mode 100644
index 0000000..3df1c52
--- /dev/null
+++ b/archive/ES_0.6249853306449479
@@ -0,0 +1,22 @@
+archive/ES_0.6249853306449479---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T22:07:19.440
+Launch V∞: [7.129172166173349, -7.313859918483411, -1.9014848708833554] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.002836971251481484, 0.012286533182194396, -0.016598455703648003] km/s
+ V∞_out: [-0.0055544078027615065, -0.007681734420089628, 0.018564064547188015] km/s
+ time of flight: 1.1107665211100091e8 seconds
+ arrival date: 2027-11-12T12:44:51.440
+ thrust profile: [0.5856768636960292 -0.25135944328554144 -0.2636478295168621; 0.2010348613505112 0.006302847839357993 -0.20392179927380802; 0.10584440027169073 0.025558492786327033 -0.16783620194441165; 0.08104590715771903 0.029991855089468823 -0.16604540452742939; 0.052677214863992 0.025185023583550112 -0.1370331092779878; 0.11628621270845658 0.054247452539453164 -0.29964054634596865; 0.026311585575331076 0.016177552354249936 -0.09273924798208583; 0.021609688921875196 0.00963357813511994 -0.06624183764818681; 0.014966237424375894 0.013092621147877135 -0.0702250168466435; 0.014600652619711761 0.010222108284219617 -0.06453894883546522; 0.0004951640334740593 0.001367935660367688 -0.004821420117517227; 0.00544078660306042 0.006925392138553846 -0.005742570142627228; 0.014334296475552226 0.015601773925060135 -0.019633831976547816; -0.0049808344233851255 -0.0043617647487379195 0.00125137772046357; 0.0010749117637204636 0.0028195667693143404 -0.002331751800263823; 0.0018347379583543181 -0.0014727770680182822 0.004029602406190797; 0.00508597647474894 0.0020622862282030506 -0.005445582069930257; -0.006124285411626128 -0.005185120222457976 0.008754802777453302; 0.0006390657070505419 -0.0021389072204470753 0.0027367336047834745; -0.01851269623283422 -0.007617456675251503 -0.00747908844117237] %
+
+Mass Used: 99.53870927380513 kg
+Launch C3: 107.93328739633726 km²/s²
+||V∞_in||: 0.02084504821929806 km/s
diff --git a/archive/ES_0.6251526202443105 b/archive/ES_0.6251526202443105
new file mode 100644
index 0000000..f93b0be
--- /dev/null
+++ b/archive/ES_0.6251526202443105
@@ -0,0 +1,22 @@
+archive/ES_0.6251526202443105---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T19:21:36.746
+Launch V∞: [5.368159093763517, -8.670806508076442, -2.0080330833216316] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.6509202684784094e-5, -1.775409569597736e-5, 3.6508526265577296e-5] km/s
+ V∞_out: [3.350904170200645e-5, 3.154602026031152e-5, 1.5257780277894097e-5] km/s
+ time of flight: 1.0968872731275883e8 seconds
+ arrival date: 2026-10-14T08:27:03.746
+ thrust profile: [0.6274204070957015 -0.48545131584660767 -0.3840484235888666; 0.3014680368159275 -0.06922724637160707 -0.3347715036442002; 0.14630738615888786 -0.003559619538300777 -0.2404000954823709; 0.07995693659907234 0.00696969858086167 -0.17080779350200262; 0.06262906295764063 0.009556078672423923 -0.15822474752858337; 0.02148678504107497 0.0047178743337211015 -0.0635476690239041; 0.032868669782795186 0.006978625928366613 -0.10947504783913439; 0.005258587945789746 0.0017027486288632716 -0.021093813320137683; 0.0010411521669247458 0.0005289676792634628 -0.007449108720857103; 0.0017629534627441128 -0.00042366323980381083 -0.0013125006277025044; 0.008409086355585195 0.0034903012421790493 -0.03116801611873444; -0.0008704481562714025 0.00045905311424341655 -0.0010110060948948073; 0.00030039412581933265 0.0018979180806332158 0.0013894152303222077; -3.998387570972126e-5 -0.0003267335891423886 -0.0036243385122305396; -0.0019317062537527576 -0.007099166706157395 0.002658796164972407; -0.0015634984056495742 0.0010614267981880155 0.0050939966018624825; 0.0012383896029939387 -0.0011035912228380446 -0.008418544770753674; 0.0022846286221386764 0.0013305329238082074 0.007092002955004221; -0.005429614497249022 -0.0029570443189834727 -0.00043513911057045445; -5.041958481532909e-5 0.003245502830680121 -0.001595115016911812] %
+
+Mass Used: 99.15680616736518 kg
+Launch C3: 108.03221442017092 km²/s²
+||V∞_in||: 4.848523724856086e-5 km/s
diff --git a/archive/ES_0.6251528817426552 b/archive/ES_0.6251528817426552
new file mode 100644
index 0000000..d39d06a
--- /dev/null
+++ b/archive/ES_0.6251528817426552
@@ -0,0 +1,22 @@
+archive/ES_0.6251528817426552---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T04:03:52.399
+Launch V∞: [7.106050363366638, -7.476002488429209, -2.0071999378909156] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000775412529304845, -0.00029198060276984175, -0.001268628495753101] km/s
+ V∞_out: [-0.0007523430476286018, -0.0013144835628165566, -4.315686981846427e-5] km/s
+ time of flight: 1.1208754398247036e8 seconds
+ arrival date: 2027-11-26T11:29:35.399
+ thrust profile: [0.3720880172502553 -0.19234218261295652 -0.225261992299762; 0.15636876786485715 -0.011835358286164747 -0.20184369914456335; 0.10578890272144675 0.01047143493059053 -0.21005211407948024; 0.07651037575246945 0.01478966387838401 -0.20104724596126833; 0.07112644638389007 0.018132801880550904 -0.21840122606076187; 0.03651969300749086 0.012013388515413094 -0.13427592614505782; 0.019005154853275318 0.006753657664615955 -0.08591402073553993; 0.011665015548952731 0.005582100866264229 -0.05290440663242302; 0.00389649209505801 0.006324648825294755 -0.01543908325190361; 0.0089497000209143 0.003121594879368122 -0.0164836081306107; -0.011755320829136471 0.0026477521703256257 -0.01123821452653955; -0.011382396015222979 -8.664847937815589e-5 -0.0032826820472966417; 0.0018894113137932636 0.005184074574842396 -0.0028156889078332914; -0.003514104242498959 0.0001723985145894663 0.008772815797897768; 0.007431743718139761 -0.021252627338635973 0.009626877798488434; -0.011142443787184311 0.010438475008523483 -0.01700902440069823; -0.009076185987400658 -0.008264378802313892 -0.0007125160083141617; -0.008572315621954069 -0.03704687297157666 -0.010045268408856963; 0.017415377433298608 -0.012439600363765992 0.005865724317562935; 0.013563243612328017 0.002866535747547227 0.0003506193418021665] %
+
+Mass Used: 85.25509874092677 kg
+Launch C3: 110.41541656437215 km²/s²
+||V∞_in||: 0.0015152344779714964 km/s
diff --git a/archive/ES_0.6252585585664028 b/archive/ES_0.6252585585664028
new file mode 100644
index 0000000..9c95a31
--- /dev/null
+++ b/archive/ES_0.6252585585664028
@@ -0,0 +1,22 @@
+archive/ES_0.6252585585664028---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T13:16:55.872
+Launch V∞: [5.261859843043353, -8.520357682121888, -1.6866749631225642] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003722879579502955, 0.1336779020349591, -0.08576732052615861] km/s
+ V∞_out: [-0.12604638458033157, -0.07340839310468818, 0.06283762309105963] km/s
+ time of flight: 1.0846647661772485e8 seconds
+ arrival date: 2026-09-28T22:51:31.872
+ thrust profile: [0.9999984844980274 -0.7975686429068146 -0.5542167368393139; 0.4504495036660095 -0.09854860555302068 -0.45822739649346406; 0.1535186404456394 -0.0026297456774696686 -0.23316085159031566; 0.07999017536750175 0.008877139366505533 -0.15846177520576715; 0.09017558262758434 0.016116501618599198 -0.20632917756619287; 0.023950433270911047 0.005718382498131193 -0.06501916678283998; 0.02290853645206863 0.0062427490390373885 -0.06713882788423395; 0.018581200270114062 0.005769041501981472 -0.06025907299645882; 0.0017351276559014412 0.0002446650204638196 -0.0055023902032116535; 0.0051355469834805595 0.001453504443159088 -0.017733493119093016; 0.00039583037734472996 7.258062669395957e-5 -0.0012671405582632461; 0.0002564062503676864 4.530596511249217e-5 -0.000512024388888524; 4.064958473223065e-5 0.00010771286169900996 -0.0007275342558814758; 0.00016447187485785762 1.3513739851688802e-5 -0.0004129208737108776; -9.931503039923976e-6 0.0001502922714042979 -0.00029906664438683937; 0.0004962422118189201 1.9006758080008355e-5 -0.00046688363717033296; 0.000559912736775175 -0.000176147274943928 -3.8213553464061794e-5; 0.0002489858431218766 -0.0002116326902442654 -5.755395227467197e-5; 1.9967805208553466e-5 0.000294366998830979 -0.00020774808057748805; -0.0003033352378422943 -0.00030878837272376033 -0.00024180617573031757] %
+
+Mass Used: 127.88518891709373 kg
+Launch C3: 103.12853647035021 km²/s²
+||V∞_in||: 0.15882680303093866 km/s
diff --git a/archive/ES_0.6253736764440381 b/archive/ES_0.6253736764440381
new file mode 100644
index 0000000..47dcb52
--- /dev/null
+++ b/archive/ES_0.6253736764440381
@@ -0,0 +1,22 @@
+archive/ES_0.6253736764440381---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T19:40:47.353
+Launch V∞: [7.100629504819945, -7.417948033014746, -1.659471169503422] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.5836517680915827, -2.8381818213811374, -4.55881001405183] km/s
+ V∞_out: [2.2540882422261754, 1.7048495748500436, 4.604130651786638] km/s
+ time of flight: 1.0927313025165768e8 seconds
+ arrival date: 2027-10-23T13:19:37.353
+ thrust profile: [0.507132672421884 -0.24591319387012067 -0.27587601700989733; 0.31354088945573294 -0.007052796990438145 -0.33432266079064393; 0.14409018830317988 0.02422020553303166 -0.23735439752991475; 0.1067186659021063 0.02979336039315062 -0.22983509926194937; 0.08564154939205089 0.030224976793539308 -0.2221382205205891; 0.07319213165551017 0.02932927110364988 -0.21620814283195824; 0.012008465483178679 0.004808766673062114 -0.03963643730835134; 0.017553200884579706 0.007786529822772564 -0.06533367502443431; 0.003937231752484011 0.0020625301093083292 -0.016150524654141463; -3.2531240682182007e-5 3.0859207000003995e-7 0.0006258065215918492; 0.0008750167865874451 -0.00040591278610551773 -0.0014605513803340985; -0.0006091509136367337 0.0012584614544062485 -0.0033048514018343684; 2.3241116721634057e-6 -1.8510417110805297e-5 0.00032080727218060075; -0.0023947670831720247 0.0035201673623561887 -0.005667676390099682; 0.002011152873636661 0.00154688547579797 -0.002384111201669436; 0.00030285353173921457 -0.0033719380664404943 -0.009521011946993535; 0.003832910760864213 0.0049682125376015965 -0.003932121639903752; -0.00013612377409494064 -0.00047293327259621343 -0.002595568691501313; 0.0011762430380832252 0.0017000101861561476 -0.007133729124789772; -0.0014025660286589676 0.0006865916940591269 -0.00028783315529696467] %
+
+Mass Used: 98.44332365681157 kg
+Launch C3: 108.19873694763992 km²/s²
+||V∞_in||: 5.401728814169962 km/s
diff --git a/archive/ES_0.6254633075008535 b/archive/ES_0.6254633075008535
new file mode 100644
index 0000000..b1edf5e
--- /dev/null
+++ b/archive/ES_0.6254633075008535
@@ -0,0 +1,22 @@
+archive/ES_0.6254633075008535---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T22:38:16.970
+Launch V∞: [7.140408132992693, -7.345968661379715, -1.8371641823145113] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01398122279604099, 0.09313351836933677, 0.016803058494623022] km/s
+ V∞_out: [0.090552421588047, -0.018469835584759956, 0.02469987920995074] km/s
+ time of flight: 1.0927956303685217e8 seconds
+ arrival date: 2027-10-22T18:04:19.970
+ thrust profile: [0.5165068511398696 -0.24328528862415502 -0.26806597662784415; 0.30374686754693053 0.00013753467612703284 -0.30853435120789474; 0.19377105971388503 0.0419875135589103 -0.29633548642825175; 0.12261353371606964 0.043509486447873245 -0.24762357775301969; 0.06805696838420378 0.030977744535107085 -0.16931757070557457; 0.037448023366677616 0.01944162025498907 -0.10889576131478713; 0.02908613404541963 0.017204930066792766 -0.0942389151303107; 0.02906429531552546 0.017292465935472567 -0.09532660925746844; 0.0011535675132822944 0.0015561571433399188 -0.004737933425197225; 0.0009565150263741258 -0.00016488523652283737 -0.003448876134768729; 0.0006596642547287665 0.0008177867392957323 -0.001587897720215063; 0.0008054130926931373 0.0007302076669230429 -0.001762913636519663; 6.714665210949349e-5 0.0010755612157792875 -0.0019250591664696703; -8.323577485195438e-5 0.00029218813388989643 -0.0015749895907934686; 0.000979178159915981 -0.00074720650600547 -1.33926047889317e-5; 0.0009663824666331891 0.0016206369444296776 -0.0008007573459188645; -0.000793089751766008 0.003154535147497183 0.005188213889644999; -0.004149324786272385 -0.0013222030892855788 0.007678466064308569; -0.003134301923596314 -0.0015822569279584997 0.009028963255288241; -0.00016432075350826482 0.00010078062390542593 -0.00040548778308887977] %
+
+Mass Used: 97.81803142830995 kg
+Launch C3: 108.32385611246042 km²/s²
+||V∞_in||: 0.09566435913911642 km/s
diff --git a/archive/ES_0.6254923862396373 b/archive/ES_0.6254923862396373
new file mode 100644
index 0000000..2576678
--- /dev/null
+++ b/archive/ES_0.6254923862396373
@@ -0,0 +1,22 @@
+archive/ES_0.6254923862396373---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-18T22:33:34.009
+Launch V∞: [6.26255816063297, -8.657562954660278, -0.5085171682342315] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.229455191430612e-5, 6.376922284214943e-5, 6.238040429448604e-5] km/s
+ V∞_out: [-7.089604865378553e-5, -3.5505583510800814e-5, 7.450812573389958e-5] km/s
+ time of flight: 1.8749577787488282e8 seconds
+ arrival date: 2029-04-27T00:43:11.009
+ thrust profile: [0.00022210338245015013 -0.00017968003016736238 -0.0001729935987423843; 0.002256641300177536 -0.003039597565813839 -0.0062756013164473184; 0.00445195130798011 -0.011580513913294052 -0.024181757604574625; 0.022351535200054198 -0.06840974347181225 -0.14125763484744266; 0.021810441952888067 -0.07167084509155834 -0.14805017601886286; 0.019841089830495595 -0.06608649341912759 -0.13682769674188905; 0.019510023543322787 -0.06405665616635517 -0.13302697807286656; 0.01126069641772329 -0.03615445605710609 -0.07586434751653666; 0.008273824113005526 -0.026177196168121763 -0.055277160001838424; 0.0032434949597130005 -0.0072952298925341155 -0.016623536478346235; 0.0006908487844192296 -0.0019103799255535954 -0.004296265474309477; 8.944207448844418e-5 -0.00020912378576887027 -0.0005814138230092926; -1.989591136148839e-5 5.908147999031884e-5 0.00021715116035391955; -5.8416449164191475e-6 1.2028388561719842e-5 4.312457960304307e-5; 1.9575613126884666e-5 0.00015658066189877816 3.508897900924234e-6; -1.9306674976641617e-5 7.195544450735298e-5 0.0002737974407473169; -9.590901584873353e-5 6.853161463474299e-5 -2.2640951003343295e-5; -3.949327479729515e-5 -0.00012079352299633025 -0.0002223468860354006; -2.2984281553953602e-5 3.22353696176856e-5 6.871623194421771e-5; 0.0003189265372773812 -0.00011350991777074249 -0.0003184875123314486] %
+
+Mass Used: 62.22332963187773 kg
+Launch C3: 114.43162073960558 km²/s²
+||V∞_in||: 0.0001088045946641934 km/s
diff --git a/archive/ES_0.6255376104196589 b/archive/ES_0.6255376104196589
new file mode 100644
index 0000000..ad2f317
--- /dev/null
+++ b/archive/ES_0.6255376104196589
@@ -0,0 +1,22 @@
+archive/ES_0.6255376104196589---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:21:19.669
+Launch V∞: [7.06033036253148, -7.516495285748109, -1.991488673768472] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004756709771725644, -0.027299613300143865, 0.026344919085263856] km/s
+ V∞_out: [0.009937239893598085, 0.014519047237801942, -0.03394205096509021] km/s
+ time of flight: 1.0826362220696637e8 seconds
+ arrival date: 2027-10-13T06:35:01.669
+ thrust profile: [0.5415974195151004 -0.2752855822591742 -0.317845245232803; 0.26482079025771915 -0.01593008103303926 -0.31040345372064526; 0.14222709690072716 0.01780282820215822 -0.2552604741040436; 0.094732623272927 0.021551915983396064 -0.22412251147711826; 0.04888427733904299 0.013632220110231288 -0.1390342209450804; 0.033445402895923175 0.010471419315436447 -0.11011241181346415; 0.015496154090097655 0.005025643180896846 -0.05719557273724869; 0.004492687774324974 0.001691577983748843 -0.018881597289710582; 0.0017325082535759942 0.0006772021365870746 -0.007727205385026044; 0.0029869496132392055 0.0010228751350271508 -0.015183400724615582; 0.00017867590973087344 1.9855547141165584e-5 -0.00039248652696607147; 0.00016032490882344341 8.736423608089597e-6 -0.0006655165114074665; 2.433824018297935e-5 -0.00020994915268717352 -0.0004664493314964056; 0.0001830998369722323 8.025432193712596e-5 -0.00041065235930220367; 0.00014906924436326638 0.0006509669962232599 -0.00039364113325817665; 6.699280286904933e-5 -6.751563639411254e-5 -0.0003723856164942888; 0.00014879965303463025 0.0008305563841097696 4.286409395680467e-5; 1.9583942050260965e-5 0.00010948307686194905 -0.00032182460892592494; 5.0189762908049326e-5 0.00015986282541588254 -0.00030772801481036556; -0.0002670484750551293 5.534784516424531e-5 -8.493228736654907e-6] %
+
+Mass Used: 86.30725096831975 kg
+Launch C3: 110.31199334650555 km²/s²
+||V∞_in||: 0.038235453911244756 km/s
diff --git a/archive/ES_0.6256263402653749 b/archive/ES_0.6256263402653749
new file mode 100644
index 0000000..09fac7b
--- /dev/null
+++ b/archive/ES_0.6256263402653749
@@ -0,0 +1,22 @@
+archive/ES_0.6256263402653749---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-24T14:45:54.668
+Launch V∞: [7.530245082877718, -5.558403612276382, -0.2506990234241297] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.21192542412494e-6, -0.0001837009458752626, -3.4168345822806584e-6] km/s
+ V∞_out: [-0.0001775222563204087, 2.7296723879600207e-5, -3.9972448099307764e-5] km/s
+ time of flight: 1.874957777990453e8 seconds
+ arrival date: 2030-04-03T16:55:31.668
+ thrust profile: [0.9405168685690515 -0.0418051445405901 -0.11063533292341934; 0.6265502595287845 0.43149284649980885 -0.2549057293388314; 0.3208004732912881 0.39623436398012796 -0.24669239951465408; 0.15069185398231275 0.2702248988273789 -0.18492702947179593; 0.044485383396907684 0.10844015318224302 -0.08135302602077497; 0.005003610586458172 0.02749275693713115 -0.021790618697572164; 0.001777185942578947 0.010969398712163396 -0.010322066691563967; 0.0005375514483492882 0.00545313916754604 -0.00585686537919976; 3.730250128903951e-5 0.006370113096356143 -0.007246470914826857; 0.0016272679015168598 0.003475561100166138 -0.003207816021021002; 0.0003565955426401238 0.004391720483134491 -0.00561484714991707; -0.0007143518020042061 0.0035376222763304184 -0.003758874224473266; -0.0004170670200985379 0.0031173722117154162 -0.00025615308138085893; 0.0007410212063265965 0.0002562551892557409 -0.0003568533707296976; -0.00015344345543853312 0.0012876282590251848 -0.0030705528771220797; -0.00014864012231885338 0.001210956450704714 -0.00443963918993759; -4.03777519730413e-5 -0.0006106712931865383 -0.00019512003452212053; 0.0030577651894627546 0.0017511263406440095 0.00022048376896914687; -0.003999996145382249 -0.001083718175486333 0.0012128936123538942; -0.0006815153724543375 0.0003347330936975914 -0.0009280584858585518] %
+
+Mass Used: 218.52819524408824 kg
+Launch C3: 87.663291725517 km²/s²
+||V∞_in||: 0.00018391614391673238 km/s
diff --git a/archive/ES_0.6257402024165217 b/archive/ES_0.6257402024165217
new file mode 100644
index 0000000..543b0b2
--- /dev/null
+++ b/archive/ES_0.6257402024165217
@@ -0,0 +1,22 @@
+archive/ES_0.6257402024165217---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T00:44:16.469
+Launch V∞: [7.085231079437807, -7.503062009194196, -1.9151348263710108] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002208511127077274, -0.013125525297322154, 0.012235321625568434] km/s
+ V∞_out: [0.004787455840959621, 0.006850229687862494, -0.016028965707795616] km/s
+ time of flight: 1.095360338256164e8 seconds
+ arrival date: 2027-10-27T19:24:49.469
+ thrust profile: [0.4836263826269519 -0.23256471671923598 -0.2575869955046658; 0.2125248870218112 -0.005440771698363289 -0.2427335224406176; 0.11829527649670611 0.019020949238517722 -0.2093186259772827; 0.07438597196011104 0.021016632507819953 -0.1784216799591522; 0.06353319731300279 0.021356557909760904 -0.17166257282936367; 0.03944539668936802 0.014437902388733244 -0.13332942902650083; 0.016195901211231538 0.007191797224683942 -0.06324523338428957; 0.015913364213860522 0.0070733905425347 -0.06738076858798307; 0.015688981692835974 0.0073965400019861465 -0.07189908885811093; 0.01098987485530312 0.006804862759149898 -0.06416593232296587; 0.004993981256350916 -8.825825061013477e-5 -0.019231092019427718; 3.730204118454028e-5 -3.97582723982836e-5 -0.002717710617848556; 0.0009951560570891555 -0.0014310989427739587 -0.0013923393006865818; 0.002329599159189669 -0.0019981853907021785 -0.0033944153814252156; 0.0011568091012005076 0.002560410407901147 0.003272940720176723; 0.0005029755723904461 0.0033200384602751157 -0.0005550959219224856; -0.0010512693840799884 -0.0020744977700660893 0.0013660337688515523; -0.000938000120613257 0.0005814908347856798 0.004413854162466749; -0.0021332090972759512 0.0015103629678292737 0.0006861404904363812; 0.001439058860588371 -0.002021765437442933 0.0038621761811497724] %
+
+Mass Used: 87.40585068413657 kg
+Launch C3: 110.1641803660238 km²/s²
+||V∞_in||: 0.01807927075437974 km/s
diff --git a/archive/ES_0.625863309427717 b/archive/ES_0.625863309427717
new file mode 100644
index 0000000..577f7de
--- /dev/null
+++ b/archive/ES_0.625863309427717
@@ -0,0 +1,22 @@
+archive/ES_0.625863309427717---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T11:55:59.633
+Launch V∞: [6.969636553782927, -7.579764106066747, -2.2440665645405318] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0001096793735534888, -0.0005366632306976112, 0.0009031511415412365] km/s
+ V∞_out: [0.0005046525620835678, -0.0006985650776534033, 0.0006143087279477243] km/s
+ time of flight: 1.1052479434667493e8 seconds
+ arrival date: 2027-11-09T17:15:53.633
+ thrust profile: [0.6140792431236711 -0.3191099090142123 -0.3651266034227944; 0.09282965152491308 -0.008839808096285266 -0.11548252825204677; 0.09450241500197946 0.006735224520499269 -0.17962252616706467; 0.030148147294469442 0.0046105872351279225 -0.07630160864902827; 0.05031923900167212 0.010015478327881782 -0.15254867529803512; 0.03365042346003788 0.007609689699039278 -0.1177414870093367; 0.0340259996743015 0.008276620824864885 -0.1328981972209134; 0.010136095606534685 0.002191939909804512 -0.042554769556043086; 0.008955138492996515 0.005239362663706689 -0.0339021853346992; 0.00530725979564906 -0.0031188939596225648 -0.006043301288336065; 0.0047357132464245265 -0.0004697875548358272 -0.02825398867219476; 0.002909492840283615 -0.006197726088941861 -0.006007416560024144; -0.0008748044166554413 0.0029419427423020145 -0.016879671862116332; 0.0033447342062878716 0.003045901917369265 -0.012954812371078957; 0.008831274369646896 0.009212349084179606 -0.0077277959755211205; 0.01120538453953927 -0.0032099225822359604 0.003664228552963728; -0.0015009680863534735 0.0006681728050136647 0.0015216484427105562; -0.001838020197881362 -0.006692077969842442 -0.004915188704663175; 0.005185181744694757 -0.009234004821630344 -0.008502748571067411; -0.023480307498281585 -0.000354474242890345 0.007934209705893308] %
+
+Mass Used: 82.29765567338973 kg
+Launch C3: 111.06449234153374 km²/s²
+||V∞_in||: 0.0010562759926426057 km/s
diff --git a/archive/ES_0.6260096247536411 b/archive/ES_0.6260096247536411
new file mode 100644
index 0000000..65c3d31
--- /dev/null
+++ b/archive/ES_0.6260096247536411
@@ -0,0 +1,22 @@
+archive/ES_0.6260096247536411---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-21T07:40:05.209
+Launch V∞: [5.645006560060261, -8.46453817517259, -2.773039195030234] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005982586690826357, -0.0005046095589823177, 9.424064890303519e-6] km/s
+ V∞_out: [0.00023767941632163935, -3.4218787427344237e-6, -0.0007491449900598967] km/s
+ time of flight: 1.168460410609075e8 seconds
+ arrival date: 2027-01-02T16:54:06.209
+ thrust profile: [0.273719889823545 -0.196385184912888 -0.1669566411418677; 0.18975146803445672 -0.02761251394861203 -0.20703425232849346; 0.13203625183903173 0.011196446806953095 -0.2072856269375555; 0.10846912251118451 0.023830450953193683 -0.2171855743402001; 0.07731236227733282 0.02421146144426972 -0.1857489232331862; 0.039468260848443966 0.015128652270708328 -0.11036559684877328; 0.018595350021356753 0.00827287202110012 -0.05387433924310604; 0.01298665059029319 0.006165154823461074 -0.04082049945917161; 5.248202616504949e-5 -0.003287488597835174 -0.0054310654455023795; 0.005294827497335431 0.003507878281563574 -0.01520763411448333; 0.005884048104145867 -0.0016359369734933887 -0.009914792539706754; 0.0035799961936223736 0.0005850812175535754 -0.0026727828072233566; 0.004168220150522334 -0.0011437541354960264 -0.009218044977374319; 0.0026098670011270985 -0.0005622370405560532 0.007850265074266309; 0.004984420361683599 -7.852280608344558e-5 0.016741756972840676; 0.0006246550351025733 -0.00045729128257415496 0.0021631116850899506; 0.011867646631398783 -0.01952423026571848 -0.011267011156216781; 0.002998400664731384 0.016957214305822768 -0.001373449148585376; 0.006708274952309059 0.01475441154962444 -0.007591098390337428; 0.010542759802192294 -0.0028491016679026743 -0.04598992432422162] %
+
+Mass Used: 81.65309245028129 kg
+Launch C3: 111.20425195925144 km²/s²
+||V∞_in||: 0.0007827087933247669 km/s
diff --git a/archive/ES_0.6260941442661822 b/archive/ES_0.6260941442661822
new file mode 100644
index 0000000..dd4d8d0
--- /dev/null
+++ b/archive/ES_0.6260941442661822
@@ -0,0 +1,22 @@
+archive/ES_0.6260941442661822---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T22:25:48.099
+Launch V∞: [7.093850160606681, -7.328788326517714, -1.568656746343873] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00984319106913745, -0.004504375811035938, -0.022053774343516862] km/s
+ V∞_out: [-0.005828803849503971, -0.023855257787331472, -0.0006364828470102843] km/s
+ time of flight: 1.0945027811544238e8 seconds
+ arrival date: 2027-10-24T17:17:06.099
+ thrust profile: [0.664854442207384 -0.3118206247260238 -0.3361090433593194; 0.29766654614103555 0.0002959344007181869 -0.30984116936028683; 0.13307062756340593 0.024678980121455616 -0.2114068242423906; 0.11851784713153618 0.034712353602070395 -0.23804374776863646; 0.10372348594950004 0.041880121357889155 -0.2516515175841541; 0.05560454133879833 0.024339485456883667 -0.15592213459440962; 0.025106921208612024 0.009738051906717152 -0.08391819365588396; 0.02841858507754716 0.011186566491532957 -0.1023781743865156; 0.0031618856950016453 0.0017547749149376278 -0.011010288125859179; 0.004996155348891804 0.004734626930234678 -0.03819241991230383; 0.0040680508674236955 0.0005522629614557468 -0.004581049089861316; -0.002008540869277405 -0.00031030732511715185 -0.007027510335192174; 0.002356766975045878 -0.0006025762929279931 -0.0027657845897723597; 0.0004583402771694729 0.0014016972896841633 -0.0036574376427666567; -0.0006529439076140382 -0.000399944626447748 -0.014288898774694254; -0.0007626702804965644 0.005745217372961112 -0.0014198666993411047; -0.0019321991140581584 0.0014656308884186046 -0.002542668629642256; 0.0006041236165400473 0.004441322162433281 0.012086594580779736; 0.0015005254284036272 0.0018301538158531066 0.00044960138567431973; -0.0011580662960706464 0.0008316544793026911 0.0003653381384065655] %
+
+Mass Used: 109.22506250450988 kg
+Launch C3: 106.49453242389188 km²/s²
+||V∞_in||: 0.024567188985827326 km/s
diff --git a/archive/ES_0.6262853613636843 b/archive/ES_0.6262853613636843
new file mode 100644
index 0000000..2d1aa19
--- /dev/null
+++ b/archive/ES_0.6262853613636843
@@ -0,0 +1,22 @@
+archive/ES_0.6262853613636843---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-09T20:13:00.650
+Launch V∞: [5.20564854426115, -9.138325625165542, 0.03375606841753358] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.08112522708966774, -0.10231917372711821, 0.0017477040702311532] km/s
+ V∞_out: [0.01720521854306363, -0.000600157917122287, -0.13044060409253325] km/s
+ time of flight: 1.5626060830121014e8 seconds
+ arrival date: 2028-04-21T09:56:28.650
+ thrust profile: [0.06335755932464339 -0.052988226545069995 -0.047511637766285746; 0.0414355665284168 -0.03457327465407733 -0.09433036008272955; 0.04773837537467111 -0.056982289527211225 -0.18789096473858652; 0.025626554114940747 -0.03962976451046653 -0.14202246535822785; 0.023353189338335086 -0.04581791882016499 -0.16467759983668845; 0.025540625742612663 -0.06490635922183018 -0.22332201630356044; 0.013171921083370185 -0.03342847882364314 -0.11578868344292081; 0.006109017657824171 -0.015583903501107943 -0.05512224379164577; 0.01485252935969482 -0.03942340026551094 -0.13709953235765998; 0.008234166208904823 -0.020026652761430896 -0.07131963752050934; -0.0003176332471939036 -0.002711778421135324 -0.00411501661538251; 0.00024458038547203764 0.00011390877190053044 -0.00019822079849315965; -0.0005084196947458185 0.0009479496265702464 0.0007168844248053883; 0.0002954765355924107 -0.00010240805238316504 0.00036315015189517706; 0.000604544376669711 -0.0007216316781448061 -0.0005832629338782052; -4.286846332111941e-5 0.0015385910005280507 0.000683872068861638; -7.945823506787497e-5 0.00036953885545025977 0.00035271523162679015; 8.765308413799682e-5 -0.000636400331311096 0.0008031888582478114; -0.0007503190510673181 -0.0006034465856886839 0.0013775463389729744; 0.0002549688971857575 -0.0011956181093663804 -0.0002668553594352862] %
+
+Mass Used: 85.44760468216236 kg
+Launch C3: 110.60891147008044 km²/s²
+||V∞_in||: 0.1305893190581353 km/s
diff --git a/archive/ES_0.626379305298443 b/archive/ES_0.626379305298443
new file mode 100644
index 0000000..4996fa8
--- /dev/null
+++ b/archive/ES_0.626379305298443
@@ -0,0 +1,22 @@
+archive/ES_0.626379305298443---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T08:47:51.234
+Launch V∞: [5.408304270702902, -8.743812594497424, -2.180707880578458] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.54132498143821e-5, -0.00010667940882707948, 0.0001026993586217969] km/s
+ V∞_out: [0.0001032166243928711, 0.00010436223762339354, 7.85166781543103e-5] km/s
+ time of flight: 1.0913697107047422e8 seconds
+ arrival date: 2026-10-08T12:37:22.234
+ thrust profile: [0.4888617614415419 -0.38351700129483846 -0.31207329356311814; 0.2583314457364551 -0.062385569216167724 -0.28846040363273795; 0.16895795350710788 -0.00653243979321702 -0.26992391168575885; 0.11525907547906458 0.008215316217207088 -0.2343766786988071; 0.03637753141913267 0.004645967975641071 -0.0895743549249069; 0.021215805483795744 0.004027721931198392 -0.06002120441690467; 0.012981789395908855 0.0028560280814991373 -0.04133652925988223; 0.009459946148923514 0.0019805362056392467 -0.02976978902609066; 0.0038471310700120046 0.003304141779008289 -0.02232830341386636; 0.0018056964219016027 0.0010870599576444295 -0.0050361416742854635; 0.003481039004068949 0.001361452695296955 -0.015231579242469123; -0.0006428304801527645 0.00042452266904790403 1.2648772628603977e-7; -0.0022444735138082055 0.00015094361679745643 0.0015014299378302465; -0.00511521894361131 0.003585517628796636 -0.00544672863757952; 0.002543433089115722 -0.0008531087964355468 -0.0007313055276268452; -0.004348509871156881 0.001309296817059514 0.0010629288630821633; -0.0008663643270725113 0.0006772705000101531 0.0009351667667512791; -0.0004814672311302373 -0.00033633834907573245 0.005105502105205013; -0.00788828367394365 -0.0037253008314233017 0.0050460921126171615; 0.001566576583370093 0.0008621672437037314 -0.0059952624707459035] %
+
+Mass Used: 86.42876915794659 kg
+Launch C3: 110.45950063261202 km²/s²
+||V∞_in||: 0.00016617705249699795 km/s
diff --git a/archive/ES_0.626461838062805 b/archive/ES_0.626461838062805
new file mode 100644
index 0000000..cdab9c6
--- /dev/null
+++ b/archive/ES_0.626461838062805
@@ -0,0 +1,22 @@
+archive/ES_0.626461838062805---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T08:46:59.976
+Launch V∞: [5.598203708452922, -8.055060790956134, -0.4092056810853797] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005328101729173673, -0.0003546547452760865, 0.0002672949268688542] km/s
+ V∞_out: [-0.00035161227560696277, 0.0005016955608288436, -0.0003267989793541001] km/s
+ time of flight: 1.5443839936675316e8 seconds
+ arrival date: 2028-03-16T20:20:18.976
+ thrust profile: [0.37706053505999043 -0.193462617493502 -0.160870965263036; 0.05938234517589861 0.0023623445406309954 -0.05300847385179309; 0.09978065540289405 0.019956869063596817 -0.1571730595632127; 0.10625809107929994 0.034319122389059126 -0.2324530187168348; 0.06769096782760659 0.02684274557757831 -0.1762202435358548; 0.02985911454677757 0.01626200802224529 -0.08719435261798747; 0.04474482299925178 0.02196548074925249 -0.16722950991396113; 0.012775721674512196 -0.0067312333485375665 -0.043166239881520414; 0.029081163212316123 -0.019057231681223308 -0.07764752718671836; 0.020586113126807755 0.006701106166532529 -0.03254685456070806; -0.017316126322667467 0.01966559520848256 -0.012873179123236978; 0.0519763635966074 0.0035344120755091014 -0.05450752382016304; 0.029619327121220534 -0.01443454368144384 -0.06781704629883452; 0.019527365045497434 -0.07542755837260648 -0.013867769893992975; -0.07513400554552445 0.04114682592508424 -0.08571562048052853; 0.13672372471658567 0.015614860083181328 0.0035423907712768335; -0.1250401159877621 0.10930440219093122 -0.0726313790849129; 0.019827213404346507 0.013376661963941645 0.14988691879793342; 0.01744810976137554 0.015737877997633303 0.1559502178777067; 0.013765039827757416 0.01835605356031152 -0.12413591622366017] %
+
+Mass Used: 168.58933709212897 kg
+Launch C3: 96.39133839676745 km²/s²
+||V∞_in||: 0.0006936232742929744 km/s
diff --git a/archive/ES_0.6264906051086095 b/archive/ES_0.6264906051086095
new file mode 100644
index 0000000..3947a3c
--- /dev/null
+++ b/archive/ES_0.6264906051086095
@@ -0,0 +1,22 @@
+archive/ES_0.6264906051086095---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T10:07:30.861
+Launch V∞: [5.319467589906635, -8.635269678400435, -1.9115480343126157] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005847030733835989, 0.005171258136405466, -9.507264773696284e-5] km/s
+ V∞_out: [-0.002547657567531841, 3.535187432059063e-5, 0.007379896475296404] km/s
+ time of flight: 1.15893358233055e8 seconds
+ arrival date: 2026-12-24T18:43:28.861
+ thrust profile: [0.43371875021375234 -0.3193965699047928 -0.23583103150312276; 0.23230794571827632 -0.04024831557705442 -0.22730192852633382; 0.1403378230754866 0.006339631578421448 -0.1983006708489727; 0.0900408229608193 0.014993460096597327 -0.16406243984026017; 0.04979926742767573 0.012011581021689508 -0.10866420227293921; 0.053368243180258824 0.016589983046185204 -0.13156392616157667; 0.08701649972842321 0.021664543452853815 -0.23698417525633475; 0.02839907514949751 0.010586373169755347 -0.08406722796013222; 0.006167523533304134 0.0024634736181873597 -0.01823849818762692; 0.020098220188274764 -0.01878247099867209 0.002106415977145061; 0.0010998628647545285 0.0014036125676060753 -0.008197478026321984; -0.014355263999219495 0.022010510847329308 -0.011312886924610396; -0.0029154462513056156 0.013657786436670979 -0.006528272232030055; -0.0036107573274526505 -0.014255041946819962 -0.008761565054527524; -0.011515926651951336 -0.001914116901593742 0.005187296107596325; 0.009164871568650937 0.002886971029492069 -0.004156683943088492; -0.05348291627628574 0.037062333118293544 -0.0769318623972571; 0.027242302351659583 -0.02098943933114787 -0.07463174947619151; 0.02345862273425279 -0.0009272438367407525 -0.07730603695806824; -0.013782932610500008 -0.0025544346521570154 -0.011693344680338967] %
+
+Mass Used: 109.54700910689917 kg
+Launch C3: 106.51863374625349 km²/s²
+||V∞_in||: 0.007806325507183906 km/s
diff --git a/archive/ES_0.6266720267807728 b/archive/ES_0.6266720267807728
new file mode 100644
index 0000000..d7f9090
--- /dev/null
+++ b/archive/ES_0.6266720267807728
@@ -0,0 +1,22 @@
+archive/ES_0.6266720267807728---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:19:46.639
+Launch V∞: [7.091147428332447, -7.426429999726534, -2.0341189858544237] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008254922584992198, -0.0037265845293546988, -0.017703110859540152] km/s
+ V∞_out: [-0.00490504160829763, -0.01925344217190752, -0.000507332987324882] km/s
+ time of flight: 1.0832172752315252e8 seconds
+ arrival date: 2027-10-13T01:41:53.639
+ thrust profile: [0.6300387022557582 -0.3078850707675641 -0.3377324049690486; 0.22772474455385766 -0.008591399051920481 -0.2546091261772051; 0.12036222310577256 0.01983447821870939 -0.20459499344730822; 0.1241105033310463 0.03245806725905278 -0.26015624043766655; 0.0617101018455827 0.02242574575098926 -0.17037306006724298; 0.030358718007397752 0.01130089768062128 -0.09048906088122514; 0.021825112727784906 0.00893369175147129 -0.07542248526141135; 0.012430251852003917 0.006719465080031033 -0.04828102714413979; 0.0049222626931711855 0.0022175542915183846 -0.022765088801599283; -0.00019416941953942068 0.0006435852040014528 -0.0031093032440426523; 0.002044303970417877 0.0015219860775853393 -0.004331663905749706; 0.0017080178362791903 0.000508372073498313 -0.005774839740644212; -0.003438665540333565 -0.00159434793178634 -0.00224840650474861; 0.003994247215313967 -4.01086069612539e-5 0.0014415465627451679; 0.002124877081479842 0.001171528665418664 0.0007447334569721672; -0.00036404224825058184 -0.0006103117407978261 0.008990927590306702; 0.0003367971953935309 0.0005330602766946222 -0.005418742108870403; -0.002077817582021785 -0.0023279387619086957 0.004344719019134372; -7.389004174211081e-5 -0.0006970026141678266 0.0003667289983491891; -0.0036655859584000866 -0.004252833171089306 0.0009593449413684456] %
+
+Mass Used: 91.93643034541583 kg
+Launch C3: 109.57387443979756 km²/s²
+||V∞_in||: 0.01988545481611644 km/s
diff --git a/archive/ES_0.6268804980769853 b/archive/ES_0.6268804980769853
new file mode 100644
index 0000000..3231677
--- /dev/null
+++ b/archive/ES_0.6268804980769853
@@ -0,0 +1,22 @@
+archive/ES_0.6268804980769853---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T10:28:22.607
+Launch V∞: [7.24168989902164, -7.496277112230633, -2.864862739423626] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01164021645227144, -0.005294522697122461, -0.024512699255340196] km/s
+ V∞_out: [-0.0019343545113542776, -0.02757379741838209, -0.0005941151391258841] km/s
+ time of flight: 1.0958661617247981e8 seconds
+ arrival date: 2027-10-28T19:11:58.607
+ thrust profile: [0.20529314457726536 -0.10172996203990942 -0.12845503563054803; 0.12540846481653503 -0.004719159810476641 -0.152896744389151; 0.08854485357744514 0.014058820414622683 -0.16273785412284075; 0.06351235235906402 0.017383395856841594 -0.15329537316589006; 0.04289205774021682 0.015134846042040843 -0.1257655370095276; 0.02407645154984431 0.01004411681644815 -0.08181121772331336; 0.007203082653388907 0.003952211955442669 -0.028216411168150296; -0.00014466123865149156 0.0006459037990981864 -0.015043409528977389; 5.266423320897872e-5 -0.0009878288764857215 -0.008479271651722959; 0.0003669656694872663 -7.242367147441194e-5 -0.00485093490765721; -0.00394890567440183 0.0026916151440838114 -0.0025767454837893494; -0.003042198231664753 -0.0025920050361335715 -0.0011466329856368936; -0.0011789344218073737 -0.0007865728854130464 -0.0029395706203296777; 0.005289549866868837 -0.0026278310848700994 -0.0025457444333147087; 0.0014426826757629016 0.0010213837971348267 -0.009025354127627061; 0.0029319072671543647 0.0033484155325832544 0.000695234307071589; 0.0002994647395132506 -0.0001574649748970779 0.0004517979691435231; -0.005394162004744609 -0.007593490702961279 0.0040842208094771315; 0.0023312818113175376 -0.0016218768453361222 -0.002548226179202773; 0.00048425582003901397 0.0003873309153423119 -0.002437172083366037] %
+
+Mass Used: 49.772438115833666 kg
+Launch C3: 116.84368165268273 km²/s²
+||V∞_in||: 0.027647767259379757 km/s
diff --git a/archive/ES_0.6269107005617931 b/archive/ES_0.6269107005617931
new file mode 100644
index 0000000..f967d37
--- /dev/null
+++ b/archive/ES_0.6269107005617931
@@ -0,0 +1,22 @@
+archive/ES_0.6269107005617931---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T05:57:21.097
+Launch V∞: [6.969346588751915, -7.805275170907492, -2.270955528137578] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0533145888993304, -0.14329444529658053, -0.18667983687436054] km/s
+ V∞_out: [-0.21128527661015306, -0.034887745534567145, 0.11118304555205477] km/s
+ time of flight: 1.1038549020718753e8 seconds
+ arrival date: 2027-11-09T20:35:31.097
+ thrust profile: [0.31437766260672007 -0.18465998639822304 -0.21266198686962173; 0.1184866504365128 -0.012875361641511587 -0.15164816335196515; 0.08888646611900228 0.003883976726890677 -0.1758941995119292; 0.0695610923939607 0.008094684236613704 -0.18318589537166327; 0.047659188740978256 0.007384666247923672 -0.15450503265768567; 0.025706445503979356 0.003974316284690001 -0.09751003513150816; 0.012924091429975982 0.001939868512128739 -0.055474099843485884; 0.0067699191777520346 0.0008882177940503472 -0.03385048294187753; 0.0025178205770920617 0.0003714548141573522 -0.012135440450479953; 0.00018863244233746808 -4.171224256203443e-5 -0.005643995831509957; -0.0004684155386377336 0.0006954840786778687 -0.004107811136026392; 0.001985289363710471 0.0006905179183707652 -0.006774199618483805; 0.002741452680122357 0.0007684239674047187 -0.0034037077440645333; -0.000182831078873626 -0.0006230625463363665 -0.002403310667886277; 0.0018109718594615956 0.0008037758693256027 -0.0004200208003548202; -0.00026303934494403174 -0.0008966127145081677 -0.0020236613404085724; -0.002320255298745285 -0.0014656947851073795 8.973054864458755e-5; -0.001693452775378842 -0.007025053227798747 -0.002781112730112704; 0.0026042966884015062 0.0057468185548240165 -0.0003901544130260736; -0.00046777110800530334 -0.003782123902843917 0.0019773078692537833] %
+
+Mass Used: 62.596267614108 kg
+Launch C3: 114.65135137851155 km²/s²
+||V∞_in||: 0.2412987876840602 km/s
diff --git a/archive/ES_0.6270843037461292 b/archive/ES_0.6270843037461292
new file mode 100644
index 0000000..6b69595
--- /dev/null
+++ b/archive/ES_0.6270843037461292
@@ -0,0 +1,22 @@
+archive/ES_0.6270843037461292---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T23:13:54.638
+Launch V∞: [5.5039667724178605, -8.724734458685216, -2.4036783461059845] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01546796834834127, -0.006546468515988216, 0.0017984386698766295] km/s
+ V∞_out: [0.00817484620908194, -0.01195484318006706, -0.008698772754993029] km/s
+ time of flight: 1.0924223846766901e8 seconds
+ arrival date: 2026-10-09T08:17:52.638
+ thrust profile: [0.4002040566875019 -0.309349574405054 -0.25284172995793897; 0.22619330267654045 -0.05039615173514805 -0.24517339185663548; 0.15956258300537066 -0.0020090000508321427 -0.24592697448000478; 0.11390301948001652 0.01192532784042787 -0.2229536803809337; 0.05207417490441732 0.010005741441652484 -0.12525773612971697; 0.02127003153405365 0.005879415028842028 -0.06027497936755735; 0.006272393773026498 0.002022315912932619 -0.020529128709735243; 0.006578031601104167 0.0019953327070730675 -0.021926469676692206; 0.0018458153913679066 0.0014613043386469222 -0.004080327982216027; 0.0056719209292198725 0.0018096546663232725 -0.022145357889808676; 0.0020245800997329335 0.0009030297208668324 -0.008407446804779319; 0.0022847898768023492 0.0009370335855406099 -0.009502177649685327; 0.0007336073832542061 6.291525816487379e-5 -0.0035611299228882937; 0.00149496365383035 -0.00038626708937622857 0.0005202693474727683; -0.0007091750099284225 -0.00020814955388319596 -0.000807048167151318; 0.0002384492941274873 0.00026489655867743085 -0.001167970306998189; -0.004283803347791066 -0.0067467059239802365 0.002371349389801716; 0.006511677168520068 -0.003876440103675774 -0.0038711159923225744; -0.0022267902546023967 -0.001259368529017161 0.003958615338276987; 0.0024772682673741223 0.004455943483389832 -0.004383467784532797] %
+
+Mass Used: 77.14320571555481 kg
+Launch C3: 112.19231119798788 km²/s²
+||V∞_in||: 0.016892266766346663 km/s
diff --git a/archive/ES_0.6274822916716171 b/archive/ES_0.6274822916716171
new file mode 100644
index 0000000..6ae6fde
--- /dev/null
+++ b/archive/ES_0.6274822916716171
@@ -0,0 +1,22 @@
+archive/ES_0.6274822916716171---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T00:12:43.529
+Launch V∞: [7.070790192534306, -7.324135109052911, -1.688755732362668] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.3247052245720868, -1.51713814476956, -2.4623449045123156] km/s
+ V∞_out: [1.2830774703175876, 0.5367987490410827, 2.556341920566449] km/s
+ time of flight: 1.0774428420558536e8 seconds
+ arrival date: 2027-10-05T01:10:47.529
+ thrust profile: [0.7906847874605742 -0.3831752520306577 -0.3954386456136849; 0.30998598089106505 -0.008997197917907635 -0.3127629935314767; 0.2376021711209185 0.04039142694753022 -0.3548240577195777; 0.08606269474349089 0.024834127557987962 -0.17809401447390372; 0.04406668938427594 0.01555474259619146 -0.11225526932865848; 0.07509075780544475 0.029825413291589897 -0.20965688342825434; 0.0293792571180769 0.01326426453999108 -0.09815743530822522; 0.015414524395032568 0.0074518891216912055 -0.056253780194318176; 0.003228807482087646 0.0014961396730924334 -0.01204267481577363; 0.0034162707383563955 0.0017386181750763988 -0.01345255188745601; 0.0003095066526983783 -0.00012077928917337202 -0.0023272812340011627; 0.0008843433117552684 0.00022864782793859483 -0.001670197830182576; 0.0002776858796704638 0.0008235609715146332 -0.0009612522711436125; -0.00014157727229378576 0.00011818070520278387 -0.0005882833790315386; 0.0009197361202137823 0.0024020448053991435 -0.0013078727196241878; -0.0002527381095897245 -0.0008958802371909079 1.405955294211188e-5; 0.00018437941993059955 0.00028277233990014767 -0.0014128864075340954; 0.0002969740537983756 0.0002966611258922651 -0.00020744344595782609; 0.0020215653091910325 0.0012036189990295842 -0.0004052744394370012; -0.00013181987674087291 -0.0007136875627090141 -0.00251916494540296] %
+
+Mass Used: 110.86561131470307 kg
+Launch C3: 106.4909249660886 km²/s²
+||V∞_in||: 2.9103752441836424 km/s
diff --git a/archive/ES_0.6275963181749655 b/archive/ES_0.6275963181749655
new file mode 100644
index 0000000..06b69d0
--- /dev/null
+++ b/archive/ES_0.6275963181749655
@@ -0,0 +1,22 @@
+archive/ES_0.6275963181749655---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T16:49:16.137
+Launch V∞: [4.995664821343341, -9.161146483914006, -2.1618904093941076] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.10676420144506724, 0.10412121178970785, 0.10877717502397394] km/s
+ V∞_out: [-0.07838700612652452, -0.13063093562929998, 0.09831276380732112] km/s
+ time of flight: 1.1266168910213563e8 seconds
+ arrival date: 2026-11-23T15:44:05.137
+ thrust profile: [0.4140594940104961 -0.3635544559167869 -0.2851981257732725; 0.05023996710752862 -0.01918146416692347 -0.07362420307041287; 0.052761471484591274 -0.01258661441608643 -0.1142301375097114; 0.0654370089999682 -0.012494888021518843 -0.17692276575213353; 0.08650185208641696 -0.014181087554117792 -0.26977691442630636; 0.018707809886333904 -0.0033834502369520553 -0.074815305658313; 0.0032680525097651247 -0.0010036647498816455 -0.013398521063205484; 0.0025071998932856333 -0.0005692232123890534 -0.012780543295251447; 0.01241141482120715 -0.002427570263469519 -0.06471453501024634; 0.0017479263146385358 -0.0015836655156314732 -0.008393556236309172; 0.002859783657497096 0.001357354814078618 -0.005845124357115042; -0.0002333148883432543 0.0023855385450346042 -0.004235883463364718; 0.00032099732167147543 -0.00020085159103452196 -0.0012394552027943152; 0.0004946010086567959 3.063080477401373e-5 -0.0018527841407135729; -0.0037921665868571285 -0.0001261169969797959 0.00030110166635085277; 0.0007386475190066136 -0.00030967348588135555 -0.0025498608692983635; 0.010208429997327947 -0.001583585177538668 0.004093744721088832; 0.0006691737731418961 0.013182499807154458 -0.004196278663973681; -0.00012815460686963235 -0.00030147881583130257 -0.001953358562951996; -0.004038025992767452 -0.01135075394295316 0.013129017656534583] %
+
+Mass Used: 69.77962591731557 kg
+Launch C3: 113.55704204916758 km²/s²
+||V∞_in||: 0.18458682309676483 km/s
diff --git a/archive/ES_0.627689585329696 b/archive/ES_0.627689585329696
new file mode 100644
index 0000000..0affb13
--- /dev/null
+++ b/archive/ES_0.627689585329696
@@ -0,0 +1,22 @@
+archive/ES_0.627689585329696---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T23:32:58.048
+Launch V∞: [7.009689971484963, -7.3932207946453055, -1.7736704055316912] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.09612521378088307, -0.4560772025470917, -0.7083982665673141] km/s
+ V∞_out: [0.3720891296695338, 0.14854532630793596, 0.7477186681684018] km/s
+ time of flight: 1.0960412913926068e8 seconds
+ arrival date: 2027-10-27T13:08:27.048
+ thrust profile: [0.7093968643803817 -0.3530312841084937 -0.3859464790503683; 0.267479446079563 -0.012436784813791393 -0.2831810284833134; 0.16378325281007808 0.023978673160969487 -0.25688508466323473; 0.10709273489387319 0.027734835108117282 -0.21803975420102298; 0.06357122366034634 0.021318467215104206 -0.15832433259593434; 0.02879805095439297 0.012321319452389956 -0.08502425554848925; 0.012795608690592798 0.004835367139954864 -0.04392070581521092; 0.00925811702298308 0.004644037757345446 -0.039310880033312894; 0.009020068051086221 0.0038669794006979696 -0.04215578124357944; 0.018790311548139878 0.011116484279606617 -0.07459988126594887; 0.008483775850242544 0.0050986327965627815 -0.0376746598448588; 0.0016272981838904054 0.0005103483467993257 -0.007946707083435964; 0.0055485296192144375 0.0022454020947806404 -0.023253168752432347; 0.005499637283425595 -0.0039709063122051564 -0.009840788337674735; -0.017341406233905128 0.013107402555262179 -0.009727595808687936; 0.006268910933947618 0.00266615602015654 -0.024210405654572522; 0.001473357442544983 0.0019205756202255817 -0.0022850437735614064; -0.011488304977931926 0.006119280701564745 -0.008489225670508298; 0.0001761836546232094 -0.014688614393304399 -0.0011204489268782248; 0.0026011145707817438 0.028289526311686096 -0.0029976554144777222] %
+
+Mass Used: 108.47983500531109 kg
+Launch C3: 106.94137392217158 km²/s²
+||V∞_in||: 0.8479826504611854 km/s
diff --git a/archive/ES_0.6280718656719757 b/archive/ES_0.6280718656719757
new file mode 100644
index 0000000..b636008
--- /dev/null
+++ b/archive/ES_0.6280718656719757
@@ -0,0 +1,22 @@
+archive/ES_0.6280718656719757---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T22:23:07.238
+Launch V∞: [5.431585305008251, -8.799147193347148, -2.166869333225424] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.03786663851265877, -0.015556347448130467, 0.037535099848929214] km/s
+ V∞_out: [0.026346515622725906, -0.03955200492643315, -0.028746571309839566] km/s
+ time of flight: 1.0926854190036365e8 seconds
+ arrival date: 2026-10-10T14:45:28.238
+ thrust profile: [0.41325779363821463 -0.33017008830987704 -0.26826531834262707; 0.2158259882493113 -0.05395384283253299 -0.25420802172635676; 0.11944809183844442 -0.007101550379624603 -0.2048331434400177; 0.07865780853797938 0.0026866337079761013 -0.17112292336747395; 0.046351785450002604 0.004549558143952048 -0.11946643774770398; 0.047746954966107764 0.006538012063955757 -0.14002532909388163; 0.026929046980898184 0.004137833939064945 -0.0858985817299082; 0.011426193971934282 0.0017366645050151184 -0.038034404283573645; 0.0053340720229604 0.0021937486980292157 -0.020109372308926586; 0.0028838827682955933 0.003117250852487669 -0.008691857988240622; 0.0020190293081622287 0.00032049489399713495 -0.004863173983901615; 0.002206116129224859 -0.0007885046178802943 -0.007702913409273912; 2.7138470510148648e-5 -0.002147597716683577 -0.0008044838041602594; -0.00024002250739227804 -0.0015747692815327428 1.0401553533681942e-6; 0.005090812884537857 0.003024468957847978 0.00011932757426903035; 0.0021328887227798307 -0.005641045863941041 0.001943904695755756; -5.891976118532207e-5 -0.003458463547052879 0.0005042571395337315; -0.0012321878617215808 -7.792234691398855e-5 0.0021438396383611667; -0.0064966033669019065 0.012693311656798024 0.01578195337186034; 0.009106724759621558 -0.013189177192560542 -0.020387489379661727] %
+
+Mass Used: 81.61965099955205 kg
+Launch C3: 111.62243296304335 km²/s²
+||V∞_in||: 0.05554066959305058 km/s
diff --git a/archive/ES_0.6284827654668783 b/archive/ES_0.6284827654668783
new file mode 100644
index 0000000..2db3a30
--- /dev/null
+++ b/archive/ES_0.6284827654668783
@@ -0,0 +1,22 @@
+archive/ES_0.6284827654668783---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T09:43:06.924
+Launch V∞: [7.016745979840573, -7.511000116684496, -2.0175066656192024] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.015734213115392286, -0.04310735695912713, -0.05661225194186543] km/s
+ V∞_out: [-0.06567799537300407, -0.009959134635615308, 0.02994485528636576] km/s
+ time of flight: 1.1041304851038346e8 seconds
+ arrival date: 2027-11-07T08:00:34.924
+ thrust profile: [0.5453992876564552 -0.2757168835159165 -0.3199232840794357; 0.1820883390804258 -0.01043437808506137 -0.21826045435153937; 0.12229422490835817 0.01529485741912821 -0.22228435121233397; 0.09120901559109461 0.020555456920657668 -0.2176882474455471; 0.05851237167853354 0.017227405249393334 -0.171541256204216; 0.027621761437156084 0.009375931628842976 -0.09711413156177767; 0.022402843675860318 0.00843171660566944 -0.08822247779310372; 0.011884157683227238 0.007292005526676728 -0.06440239011407017; -0.003039529611794015 -3.812431940925865e-5 -0.00881366168436691; 0.002334407665988557 0.0017800861279957218 -0.015785550789354737; -0.0003903122109911595 -0.0015062383427097913 0.007133700228981299; 0.011101941770125336 0.0006227769244231435 -0.01321260654299615; -0.001073170461635939 -0.0014065697216406653 0.013499663567208733; 0.0007741170472023687 0.004907071601353832 0.009335306475058446; -0.013339264473857613 0.011808701255578839 0.010262914228710365; 0.00695606334740745 -0.003735367160117133 -0.024777429134597243; 0.0010716310292445278 -0.003541343239663233 -0.0050784874046317175; 0.02462893004820857 -0.018768437643812235 0.01213382827249624; -0.012884540194258064 -0.02357694219157754 0.004456529088900422; -0.00893379097602384 -0.02254587733424483 -0.009842711167602453] %
+
+Mass Used: 93.19550945316723 kg
+Launch C3: 109.72018004426128 km²/s²
+||V∞_in||: 0.07287493915120229 km/s
diff --git a/archive/ES_0.6286971275698795 b/archive/ES_0.6286971275698795
new file mode 100644
index 0000000..a27cbab
--- /dev/null
+++ b/archive/ES_0.6286971275698795
@@ -0,0 +1,22 @@
+archive/ES_0.6286971275698795---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T14:14:51.189
+Launch V∞: [5.37241275789251, -8.762070169507512, -2.1314326426997474] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.029878841515005982, -0.012356543965887652, 0.05110651120631338] km/s
+ V∞_out: [0.02839540008114274, -0.04348920758354154, -0.03098374903582591] km/s
+ time of flight: 1.1027274655057807e8 seconds
+ arrival date: 2026-10-21T21:33:57.189
+ thrust profile: [0.46239119673581575 -0.3474228418898296 -0.29502243166506537; 0.24389315253361843 -0.05674463147822839 -0.28448312976876367; 0.16232360585856695 -0.0036175989236228666 -0.27188410600421703; 0.0801103238045437 0.006699828990065196 -0.17335792572332848; 0.04979146931088337 0.0076892554461877585 -0.12941058304477338; 0.02190161550633427 0.00434025213896133 -0.06351691124158189; 0.010276837906198452 0.0017656567667785174 -0.029063807218205007; 0.01039123869436296 0.0026241671075431005 -0.03380697782117173; -0.0003389392482107713 0.005614080961706047 -0.005884557256935057; 0.0017558268022467812 0.0021045687497760275 -0.006305266881154736; -0.0032294287677907406 -0.0004206947730629665 -0.005653107822979329; -0.00033164710295969894 0.013580525181329309 -0.020492839884070437; 0.00400160586583747 -0.01206124224552611 -4.791758706191749e-5; 0.021145263998977017 0.005761277906335526 -0.03408590478011505; 0.01055315061606328 0.006124867362501654 -0.03786103414148012; 0.0031490718654429966 0.004477520441741728 -0.0517883876000193; -0.0030556834029497482 -0.003473188715616312 -0.006753603222709768; 0.0015213707990114475 0.0038672697464624942 0.003517349746714078; 0.008775780023484636 0.013457779047850853 -0.0311764563905894; -0.0018978367097975354 0.01809201792936819 -0.00392652371351235] %
+
+Mass Used: 90.7650794579099 kg
+Launch C3: 110.17969760690563 km²/s²
+||V∞_in||: 0.06047565490956501 km/s
diff --git a/archive/ES_0.6288634346076166 b/archive/ES_0.6288634346076166
new file mode 100644
index 0000000..c688a67
--- /dev/null
+++ b/archive/ES_0.6288634346076166
@@ -0,0 +1,22 @@
+archive/ES_0.6288634346076166---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T09:09:00.064
+Launch V∞: [6.857756903013526, -7.073620566072388, -0.7311612001503004] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.470431613757702e-5, 7.728880903559551e-5, 4.894063354043117e-5] km/s
+ V∞_out: [7.861393826581835e-5, -4.8811819551158367e-5, -3.154264379219726e-5] km/s
+ time of flight: 1.2841266936893831e8 seconds
+ arrival date: 2028-05-30T15:20:09.064
+ thrust profile: [0.6021409681622913 -0.24926594336635255 -0.29806039419598435; 0.27890997857151295 0.018921771377111887 -0.33002535784243037; 0.1773940826821541 0.04937283583659445 -0.3368176300847316; 0.12191831933024712 0.05009923226155275 -0.3162701070687687; 0.0705893725993233 0.037359754809030477 -0.23918722417541116; 0.056838180210491904 0.032608773067137435 -0.23111312852123242; 0.02392823410992539 0.01791457034590311 -0.12345170181726962; 0.009397544422432307 -0.0018081358606091072 -0.024058179735579176; -0.006633480699649801 0.007933605197648134 -0.01588670309376034; -0.008121947645908567 -0.008645180775377563 0.04869259071968447; 0.029732116455928458 -0.008314090889131726 -0.0342909802143726; -0.02036916567186852 -0.018697976112701575 0.08432160338462086; 0.015043560754596591 0.019477562554229014 0.009489892982630432; -0.03464412765528386 -0.020929561536000167 0.04589378746826858; 0.018994425549130646 -0.015649943722253944 0.09531892995898653; -0.011980803762260817 -0.005070874123107369 -0.025104930186459047; -0.038486855058684884 -0.016487841565447248 0.04245933541642105; 0.00286223408596669 -0.0053131446326502175 0.12344738827455082; 0.011077329721218224 -0.010276671178672998 0.00776896976550802; 0.05519037096021724 -0.04254658399231445 0.026786778525883164] %
+
+Mass Used: 164.34338997606937 kg
+Launch C3: 97.59953435419715 km²/s²
+||V∞_in||: 9.784239966423767e-5 km/s
diff --git a/archive/ES_0.6288914934475236 b/archive/ES_0.6288914934475236
new file mode 100644
index 0000000..7d35229
--- /dev/null
+++ b/archive/ES_0.6288914934475236
@@ -0,0 +1,22 @@
+archive/ES_0.6288914934475236---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T21:36:39.173
+Launch V∞: [7.1353305376901615, -7.4681503861099, -2.252700739055532] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0015932222963960755, -0.009480200520718535, 0.008859298888457786] km/s
+ V∞_out: [0.003507067813178063, 0.005048905668937872, -0.011538480936164794] km/s
+ time of flight: 1.0733385131857361e8 seconds
+ arrival date: 2027-10-02T04:34:10.173
+ thrust profile: [0.5665128146437406 -0.2794498494860527 -0.32515252521496824; 0.23543924737080207 -0.01173360373337231 -0.2718773558542784; 0.11844787297575408 0.01620321677543144 -0.2070559255134533; 0.06647483048174542 0.01598283169555415 -0.15200201921823753; 0.04534939665132452 0.013795389458060525 -0.12445259062903437; 0.03986042187782257 0.014014060633476981 -0.12600895102002818; 0.007019930894459117 0.0026482377320206714 -0.024821398979505548; 0.01213369449291348 0.0048612727167513985 -0.046599654509061346; 0.008785903197895099 0.0035480889237055717 -0.03551663886352069; 0.0016896828828689469 0.0008040623760794839 -0.008166359676991551; 0.001514423389196686 0.0014126315237087167 -0.003627342500392298; 0.0031304696431863187 -0.0010964560699176337 -0.0059529520123677414; 0.0013650034859198855 0.0009402632833293055 -0.0039369639167318084; 0.0017508766679559858 -0.000793312725077835 0.0006623670550555683; 0.002258049304579072 0.00031912953309511474 -0.001822488561834325; -6.155507837148208e-5 -0.0007354805678724758 -0.0013710754192449485; -0.003963393716949483 0.0016695306054626813 -0.007682933105490935; 0.001537093879073196 0.0011480943939520469 -0.006939084878616929; -0.003815367407832797 0.005934041933922805 -0.007467362827146036; 0.0005085129723561843 0.0001417091169378082 -0.0034896203399576234] %
+
+Mass Used: 81.76831832234438 kg
+Launch C3: 111.76087269138856 km²/s²
+||V∞_in||: 0.013072862578402442 km/s
diff --git a/archive/ES_0.62889850581948 b/archive/ES_0.62889850581948
new file mode 100644
index 0000000..f86ae5c
--- /dev/null
+++ b/archive/ES_0.62889850581948
@@ -0,0 +1,22 @@
+archive/ES_0.62889850581948---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T11:02:52.923
+Launch V∞: [7.003693270178538, -7.397648663578596, -2.0752343545014535] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007403485868996078, -0.0035363312403127165, -0.015918969777076568] km/s
+ V∞_out: [-0.004289264503029566, -0.017381427928268633, -0.00044177763626630816] km/s
+ time of flight: 1.0702782503380673e8 seconds
+ arrival date: 2027-09-28T04:59:57.923
+ thrust profile: [0.9174382222996879 -0.4599543166811552 -0.5049183259953562; 0.30249108331911595 -0.01456903084560784 -0.344620669342029; 0.0833764969689437 0.011334104882525096 -0.14482975747877155; 0.08136380010741465 0.01815341612189804 -0.18130292836194423; 0.06096131282270098 0.018354708392613 -0.16291407198427094; 0.01998977885773129 0.006932762371740476 -0.06182693039374801; 0.007173799693413479 0.0026043430977783343 -0.021137706258014467; 0.005978449376793666 0.0022535976477644696 -0.01740888360281275; 0.018828442996461737 0.007964343976969105 -0.07477161327206211; 0.007983893107926522 0.005069025580956833 -0.005333332029652977; -0.0012813327283531216 -0.0015678159164677263 -0.03242943439629965; 0.0015402572794855833 -0.005057380073034067 0.000605986119164301; -0.0007885891742788549 0.0006843492418159506 -0.003372445993210225; -0.001871380509693642 0.00048152162396631124 -0.0047632699704582135; 0.0033102782091377174 0.002157131524159671 -0.011608153811550132; 0.0014189415861047246 -0.0021807679676307296 0.0003014116418459531; -0.002045004071161275 0.005581379219571851 -0.005490580029711372; -0.005044869843309317 0.005080149786264938 -0.006366472388014081; -0.0009507228387752101 -0.0009285501866099647 0.0009947990410962351; 0.0003460562282541473 -0.0015817671040958062 -0.0015687744654482461] %
+
+Mass Used: 103.22770713093178 kg
+Launch C3: 108.0835227985934 km²/s²
+||V∞_in||: 0.01790895978043151 km/s
diff --git a/archive/ES_0.6288989627517104 b/archive/ES_0.6288989627517104
new file mode 100644
index 0000000..b5c1d7a
--- /dev/null
+++ b/archive/ES_0.6288989627517104
@@ -0,0 +1,22 @@
+archive/ES_0.6288989627517104---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T10:00:29.362
+Launch V∞: [7.020026430070455, -7.339342873094656, -1.858218873801259] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006735949122171115, 0.039852745249993736, 0.00717159467080325] km/s
+ V∞_out: [0.03909581160693881, -0.007722148619280704, 0.009892255523880364] km/s
+ time of flight: 1.0791861782449988e8 seconds
+ arrival date: 2027-10-07T11:24:06.362
+ thrust profile: [0.8393070805582664 -0.4078523254231997 -0.4307012484805916; 0.3499713805521075 -0.00819118831053599 -0.3634082082805942; 0.1580229417226976 0.026905190542022173 -0.2521524149151259; 0.10219879776076901 0.02859622716403051 -0.21208572185457292; 0.06222524928510507 0.021591965535501145 -0.15448574255745728; 0.039490230094122614 0.01497620543217558 -0.10516010113259718; 0.013455934584442702 0.005805302235045258 -0.03813282923063145; 0.019500763842366698 0.010609761921671677 -0.06669463596646269; 0.0036043576391859723 -0.00016227992511616204 -0.014095496736474561; 0.004941991253760378 0.002335548637895747 -0.01890041343029695; 0.004445949395206785 0.001615383672918753 -0.012056873837819976; 0.0013838068074139651 -0.00023898099600280645 -0.007545941034022934; 0.003866978157915169 0.00034420275503598084 -0.003324986541655733; -0.0038668456169946783 -0.000693272541656036 -0.005304202636279425; 0.0047017795436443644 -0.00585840855175428 -0.0021242953962279203; -0.0010952902164544417 0.0002528495106468697 -0.0001569698501073767; -0.004375838101259487 0.0006552620594858722 -0.0040486973955804655; 0.017820341230962336 -0.006570661672292611 0.011281649519808853; -0.021590548796097526 -0.023320118968956735 0.009229478746894657; 0.0024124720718944046 0.004393317433201566 0.0037235021066580245] %
+
+Mass Used: 111.88385996467059 kg
+Launch C3: 106.59970227068428 km²/s²
+||V∞_in||: 0.04104931284028601 km/s
diff --git a/archive/ES_0.6289855339642355 b/archive/ES_0.6289855339642355
new file mode 100644
index 0000000..37d784e
--- /dev/null
+++ b/archive/ES_0.6289855339642355
@@ -0,0 +1,22 @@
+archive/ES_0.6289855339642355---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T03:05:15.125
+Launch V∞: [7.029307123250313, -7.444605956945374, -1.7616279721673602] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008335889552006145, 0.05994014928664119, 0.00968240911483088] km/s
+ V∞_out: [0.05848754960129273, -0.01127185676604545, 0.014452457627843352] km/s
+ time of flight: 1.0693681766411296e8 seconds
+ arrival date: 2027-09-26T19:45:32.125
+ thrust profile: [0.6679036092896419 -0.3276188929988097 -0.353147863177197; 0.4054935017876527 -0.018268034872495325 -0.42124592697151686; 0.2300194521035486 0.03310416988246467 -0.36080644635808073; 0.12085704540341817 0.030095765115177395 -0.2521322770210471; 0.049245637385805736 0.015508401406026934 -0.1293380104631318; 0.017664997784610063 0.006239798808261826 -0.05378391714530369; 0.010261333948578455 0.0038242606943008155 -0.03444495738858315; 0.00861684922619267 0.003300356394270068 -0.030889297315890595; 0.002328192638378415 0.0012352306769234482 -0.009835892825415637; 0.004262481774606309 0.0014592545785760335 -0.013594133325344657; 0.0015677781040801364 0.004519660147672619 -0.0075596850498764485; 7.575317910360393e-5 0.00023135569555416736 -0.0024938211400350407; -0.0007302188650548651 -0.0007053827312706815 -0.0019193974290602316; 0.0003281089125421912 0.0009113813919272427 -1.7245747358590746e-5; 0.0043448826620704145 -0.0014100300555945978 -0.0009177816749994406; 0.0038332034999238223 0.0015285920790895553 -0.0012984304320997043; -0.0029892841030401307 -0.0001211317636298286 -0.0010256657469355959; -0.00019737157354001627 -0.0005667060858383231 -0.004788241481045405; 0.000302140437086873 0.00015707131199116722 -0.0015403215620709418; -0.00090333645450461 -0.005434909074379511 -0.0012466893507793717] %
+
+Mass Used: 104.18600029460276 kg
+Launch C3: 107.93664959948663 km²/s²
+||V∞_in||: 0.061286683687364236 km/s
diff --git a/archive/ES_0.6290450555638839 b/archive/ES_0.6290450555638839
new file mode 100644
index 0000000..919643e
--- /dev/null
+++ b/archive/ES_0.6290450555638839
@@ -0,0 +1,22 @@
+archive/ES_0.6290450555638839---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T13:25:49.936
+Launch V∞: [5.59813284696576, -8.702547108578397, -2.605598135307093] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.575783200696531e-5, -4.769428892357694e-5, 1.619320347981363e-5] km/s
+ V∞_out: [3.556215053075273e-5, 3.597190224180701e-5, 2.5358706864436643e-5] km/s
+ time of flight: 1.0908701300544226e8 seconds
+ arrival date: 2026-10-07T03:22:42.936
+ thrust profile: [0.32647879713243033 -0.25221359889359707 -0.20391476293106992; 0.21856752200050547 -0.04677701463606081 -0.23057240843346777; 0.15132537907199803 0.0002882953534254493 -0.2259972190238962; 0.1059204546896639 0.013273639246511483 -0.20061244403816303; 0.04780407159175337 0.010710310897180298 -0.1114724227398999; 0.02212345552057535 0.006416644447348326 -0.06136936201028851; 0.010855428428338762 0.0028917416093403995 -0.03013627693067593; 0.004107586888579765 0.001438920105780598 -0.014188486536856589; 0.007076572841717434 0.0028020567074327875 -0.025957483579403126; 0.0047427509326534115 0.003028519908000195 -0.021625512726811187; 0.0011773984256092966 -9.627844866218118e-6 -0.004478984291851692; 0.0015230558957043258 0.00013237402726507495 -0.0036331256715911816; -0.0009661251676337108 0.0016896237496072995 -0.002908119122058936; -0.00011391290812300391 -0.0008261699114829956 -0.003865391869671716; 0.0014536582849289741 -0.00036048426877004745 0.0030112911243858065; 0.002942173068391289 0.0023797622549801356 -0.00020043860814584428; -0.0017709732151211122 0.0010600422051383483 0.0018466758814673408; 0.0006122679380314521 -0.001995786689738336 0.0031201381733883186; 0.0010389678560763908 -3.767931548601577e-5 -0.00398110991137042; 0.0005292067151629061 -0.0034619052770737298 -0.00516489237152798] %
+
+Mass Used: 69.68763620442041 kg
+Launch C3: 113.86255919201899 km²/s²
+||V∞_in||: 5.6572351414479215e-5 km/s
diff --git a/archive/ES_0.6290938577119098 b/archive/ES_0.6290938577119098
new file mode 100644
index 0000000..1b194c4
--- /dev/null
+++ b/archive/ES_0.6290938577119098
@@ -0,0 +1,22 @@
+archive/ES_0.6290938577119098---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T07:50:33.493
+Launch V∞: [5.3142818597630805, -8.401570407143561, -1.1587833361668403] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.4323001149415608, -1.3442465247893642, -1.4539956541354755] km/s
+ V∞_out: [0.793151505767186, 1.4102779982955926, -0.9951128835804696] km/s
+ time of flight: 1.0967760000449966e8 seconds
+ arrival date: 2026-10-10T17:50:33.493
+ thrust profile: [1.0 -0.8166710532075767 -0.5038353125249835; 0.5148133388880103 -0.08906282776182026 -0.4402326702419359; 0.17728936963363898 0.0075182268512021255 -0.23367560410913205; 0.15308183571669332 0.026748394813402607 -0.25159425755905; 0.05679644805799902 0.013416077190416102 -0.11118524095993915; 0.10976779590780975 0.038327285622240054 -0.2399774397768107; 0.10162206110690675 0.03140764126366659 -0.226737345452707; 0.025488493262277867 0.009680299220854206 -0.0650425907365379; 0.0010911740617850691 0.0005623531801144358 -0.002624796727774563; 0.0011501809963381968 0.0007147647678963501 -0.001356955397911622; 0.0008257852952834393 0.0003109550240617494 -0.001971224546561709; 0.0004908649283765026 0.0019049031381954756 -0.00031562002718425394; 0.0018572554534586334 0.0006907033644521169 -0.0007078992455032464; -0.0022787574612374104 0.003041000810529779 -0.0013535172266842524; -0.0026053121768242395 -0.0093310895493239 0.0006563557459467013; -0.0036703749207311594 -0.004962991196767098 -0.0001979411014053568; -0.0047753600162294884 -0.00440605450339295 0.0005884115726305875; -0.0027099082444340165 -0.0001580632515395334 0.006567446328945507; -0.0009300291528827197 -0.0006482017569574611 -0.005039117577149453; -0.0011217109700735507 -0.0015211312967706877 0.004127857998783978] %
+
+Mass Used: 149.61342509753877 kg
+Launch C3: 100.17075581137533 km²/s²
+||V∞_in||: 2.443887415760951 km/s
diff --git a/archive/ES_0.6291474847232406 b/archive/ES_0.6291474847232406
new file mode 100644
index 0000000..9144dd0
--- /dev/null
+++ b/archive/ES_0.6291474847232406
@@ -0,0 +1,22 @@
+archive/ES_0.6291474847232406---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T09:27:58.600
+Launch V∞: [5.311368704105728, -8.800657967658047, -1.9990789856602607] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.1434364585395264, -0.04347854440077238, 0.09506084493934472] km/s
+ V∞_out: [-0.12366567763130952, -0.05208390150379153, -0.11672489524076878] km/s
+ time of flight: 1.1012229757002363e8 seconds
+ arrival date: 2026-10-20T22:59:35.600
+ thrust profile: [0.5869920623740854 -0.4539038110914409 -0.3507346898541814; 0.13529178654201954 -0.03217045886137604 -0.16660019889104183; 0.09320367333615483 -0.004304205106582237 -0.1663463468631132; 0.08011279119918083 0.005115164877172536 -0.18172038404433946; 0.05012939276127233 0.00683539840386369 -0.13751712771546787; 0.0509092233031922 0.00967409272213635 -0.15850457858361075; 0.030399104409315154 0.006751804061970659 -0.10809809865063581; 0.026473494180054773 0.008862104143362828 -0.10180019118344734; 0.009076318007207311 0.0036475466213676273 -0.03212918187916668; -0.0006305278384029493 0.0002260387500308111 -0.00010901404742115267; 0.003913669432643444 0.0023439974651811076 0.005114536598215056; -0.002667600498991659 0.0013466106464260664 0.005108577491519975; 0.0029319483058351313 0.002195016400525503 -0.0011842223279057234; -0.009348507112133923 -0.0026846642779726404 -0.0028934003135761828; 0.001774920917443279 -0.001279130258344403 -0.0017182948029002428; -0.007810946652462258 -0.01022837654019358 -0.025742377120837358; 0.029298421112782285 0.004908902244056016 -0.006937030040368627; 0.0036719537755199975 -0.03925428179488076 -0.004914769027613497; 0.0063331136785876084 -0.0074624687535488135 0.010107502570487328; 0.00088262014473347 0.0016470321641409934 -0.01573992792436288] %
+
+Mass Used: 94.33061154464986 kg
+Launch C3: 109.65853496556528 km²/s²
+||V∞_in||: 0.17748511402974998 km/s
diff --git a/archive/ES_0.6292531083633982 b/archive/ES_0.6292531083633982
new file mode 100644
index 0000000..73789da
--- /dev/null
+++ b/archive/ES_0.6292531083633982
@@ -0,0 +1,22 @@
+archive/ES_0.6292531083633982---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:41:15.306
+Launch V∞: [6.910967006096894, -7.468126388375691, -1.914405209303493] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.040031251562900064, -0.11013748062040402, -0.14284776939026103] km/s
+ V∞_out: [-0.16142027202860293, -0.0272032534465878, 0.08546070685302981] km/s
+ time of flight: 1.0946568414148554e8 seconds
+ arrival date: 2027-10-27T05:49:19.306
+ thrust profile: [0.8809810794544596 -0.4516218829825929 -0.5110316427081291; 0.1733344358743664 -0.01087316291367814 -0.2134911288695258; 0.10412003723068904 0.01179541381406742 -0.1962347625557354; 0.09003674560858861 0.019237234109206847 -0.22151714816891666; 0.06811241817388904 0.018633513533973543 -0.20386712466601534; 0.018961030582576883 0.005711227273739598 -0.07053679637437972; 0.025505306901690904 0.00848302660455071 -0.10207763178193402; 0.014592499138389198 0.005322636285510423 -0.06100428774938381; 0.004418246323328161 0.0003403923170917831 -0.018799881607077025; -0.0030558292117124084 -0.0015077618224450338 0.003255075699354549; -0.0005209484555572898 0.009641637341743038 0.005265930957655888; -0.0010432569393129202 0.004466913821215022 -0.0013022289584423675; -0.0010386264831748412 -6.532216705556289e-5 0.0015496598160963594; 0.001918027256151451 0.0008653252626584088 0.0031693815614120737; 0.01367684552078701 -0.009674790942877246 0.011970021507160053; 0.021923953239486135 -0.009042824839967458 0.007461078960552261; -0.006995021174513616 -0.007188054536062926 0.01731739776998855; -0.016566481356732925 0.006460050226907715 0.0255742410749676; 0.03223775337531509 -0.008837819451502187 0.011373039242108187; 0.0008127937691620199 0.0014516921085428608 -0.009344129489842423] %
+
+Mass Used: 108.79923632175542 kg
+Launch C3: 107.19932401752156 km²/s²
+||V∞_in||: 0.18476539437588213 km/s
diff --git a/archive/ES_0.629374645629282 b/archive/ES_0.629374645629282
new file mode 100644
index 0000000..0ae9012
--- /dev/null
+++ b/archive/ES_0.629374645629282
@@ -0,0 +1,22 @@
+archive/ES_0.629374645629282---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T08:05:05.333
+Launch V∞: [7.229813432183058, -7.382814020851059, -1.7637506147468323] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01653134959333548, 0.10483616838507034, 0.019808944238334184] km/s
+ V∞_out: [0.10146912780562117, -0.02021124776136239, 0.030812210771358966] km/s
+ time of flight: 1.0799387683525923e8 seconds
+ arrival date: 2027-10-08T06:23:01.333
+ thrust profile: [0.45121852858780437 -0.21360225383352743 -0.24101325866500625; 0.2462581405523047 -0.00355369108433551 -0.25830236455703764; 0.1651174886832139 0.03076380199147093 -0.2565298764311383; 0.11176234548338704 0.033993311001113344 -0.22864448066312856; 0.08190176623296536 0.03142360241291001 -0.2044292246528881; 0.055984061965556456 0.022379678797785362 -0.16016869451980426; 0.04836857029222993 0.022170841024642382 -0.14989411807519962; 0.0147595232961622 0.008092093568519164 -0.053591559466117135; 0.012737673660074281 0.00710138088171903 -0.0472976480426793; 0.0012399751528732609 0.000301971587421257 -0.0026624324540818834; -0.0011416452342553494 0.0004932183911466154 -9.304599348384959e-5; -0.002347879888903337 0.0002756898947537776 0.0001875795701111174; 0.0008978039214620624 -0.0013305339365800451 -0.0011829058275516526; 0.0005654636239535805 -0.0026106273301195965 -0.0016399123250462229; -0.0017132197822642826 0.0043712558694829345 -0.0009920372277816805; 0.0008771533300458128 -0.0017215200294374445 0.001419892229704167; -0.0021610379611336694 -0.0030944095642918877 -0.003797589771528563; -0.00047730951710488434 0.0010957724039095075 0.00027523488249702605; -0.006698734950832816 0.0021384197520107964 0.0007248217735735563; 0.0012028005971939115 0.0003587499662973083 0.003051270170221092] %
+
+Mass Used: 93.26314529109095 kg
+Launch C3: 109.88696136166938 km²/s²
+||V∞_in||: 0.10796435519595034 km/s
diff --git a/archive/ES_0.6293959423332177 b/archive/ES_0.6293959423332177
new file mode 100644
index 0000000..0227645
--- /dev/null
+++ b/archive/ES_0.6293959423332177
@@ -0,0 +1,22 @@
+archive/ES_0.6293959423332177---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T16:39:48.893
+Launch V∞: [7.2272126347090415, -7.462077082986928, -2.337809701759061] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0007215273361850834, -0.0037579433458820406, -0.0012099838202865377] km/s
+ V∞_out: [-0.002306909885389282, 0.002943143806923046, -0.0014578541123403267] km/s
+ time of flight: 1.0808310244637835e8 seconds
+ arrival date: 2027-10-10T15:44:50.893
+ thrust profile: [0.3562811620201016 -0.17600680604089664 -0.2100283339859095; 0.19645273428224733 -0.00791425170941861 -0.22812857334447803; 0.13328978595562746 0.02039944738289974 -0.23283845666349864; 0.08735082967302019 0.022853929154644872 -0.2007288099419831; 0.04591425004494321 0.014853387868167837 -0.12793981731589824; 0.026003088129929776 0.010743690220047784 -0.07703578436313925; 0.01834007967480061 0.006418879995530654 -0.06473704403787726; 0.005264669665873809 0.0012483981776601045 -0.018829781835828414; 0.013819533571368565 0.005261585609618511 -0.05655184815815462; 0.0009595862854967904 -0.003929801797477506 -0.008499549665611042; 0.005757826984796716 -0.0003609660667117771 -0.008515209237705199; 0.0011510968106669822 6.558078486170685e-5 -0.0033511987070755853; 0.0009343622742220526 -0.00011669715076562419 -0.002172163568259166; -0.00621973275236855 -0.0045145789424442355 -0.010484032233724919; -0.0007647692696820104 0.001316230930675239 -0.0014220783964016244; 0.017185281087704205 0.00856084347763603 0.0012093967899003202; -0.001033897721392528 0.0010837378962325755 0.0019000745132417953; 0.0033353083816779977 0.009562827609878876 0.004301728708110954; -0.001031792202967639 -0.0014413253135740246 0.008079747165441954; 0.0005422151140570236 0.0042299325502621245 0.00706626433088741] %
+
+Mass Used: 72.90871819739687 kg
+Launch C3: 113.3805510613755 km²/s²
+||V∞_in||: 0.004013327887561226 km/s
diff --git a/archive/ES_0.6294225365707344 b/archive/ES_0.6294225365707344
new file mode 100644
index 0000000..1f725fa
--- /dev/null
+++ b/archive/ES_0.6294225365707344
@@ -0,0 +1,22 @@
+archive/ES_0.6294225365707344---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T07:02:18.106
+Launch V∞: [5.572552655676807, -8.688845950035875, -2.3943368639536824] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.06566836271824578, -0.06519823848063475, 0.0026279940149808822] km/s
+ V∞_out: [0.013359561096050139, -0.0003993058408637147, -0.09161710223649654] km/s
+ time of flight: 1.079765549536193e8 seconds
+ arrival date: 2026-09-24T00:31:32.106
+ thrust profile: [0.40501766519462773 -0.31464495411220555 -0.25320520687469616; 0.2960050970966519 -0.06662805664300597 -0.31091362458272126; 0.19695209126674082 -0.002889041377119423 -0.29152860244975354; 0.11512264120066222 0.011895586283478966 -0.21585921163377308; 0.05311149996545366 0.009942522258270761 -0.12023955837913944; 0.010103590850277885 0.002569127241702531 -0.027319970931138342; 0.007323576531874739 0.0022098548019488986 -0.02046523341765262; 0.005249539914004513 0.001768456055793007 -0.01681957439392505; 0.0013690042296781461 0.0002547058828164704 -0.00440995160616705; 0.0014955006565122151 8.686054545927184e-5 -0.002701351944364763; 0.003507879793969194 0.0021934569760823867 -0.01175842868713119; 0.00031122354084093894 5.949860168185625e-5 -0.00046762753806646907; 0.0006273652225123084 6.045698458463098e-5 -0.0015426751143760437; -8.126241475971894e-5 0.0012027658332814648 7.580584002305526e-5; 0.002191774806455761 -0.0003560541137767244 -0.004250924867593804; -0.0003102800980686124 0.001868702951547484 -0.0005460802976773656; 0.0009535481704425424 -0.0004803658286645948 -0.0037433221787743194; -0.00011316318706128842 0.0007833893195496878 -0.0004778104592254688; -0.0029047100563859823 -0.000679658180304041 -0.0024747871926830965; -0.002252857742561432 0.00045043212935953335 -0.001243339519018114] %
+
+Mass Used: 79.34658230516425 kg
+Launch C3: 112.282236061833 km²/s²
+||V∞_in||: 0.09257456732610522 km/s
diff --git a/archive/ES_0.6294789595826884 b/archive/ES_0.6294789595826884
new file mode 100644
index 0000000..8b4a330
--- /dev/null
+++ b/archive/ES_0.6294789595826884
@@ -0,0 +1,22 @@
+archive/ES_0.6294789595826884---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-22T08:51:39.195
+Launch V∞: [7.496987213108732, -5.641116100304375, 0.012106454179974028] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.790999429261689e-7, -7.257586403534893e-7, -8.013260435551205e-8] km/s
+ V∞_out: [6.434210412465391e-8, -3.2961305336255997e-7, -8.693170209323173e-7] km/s
+ time of flight: 1.8160494801145855e8 seconds
+ arrival date: 2030-01-23T06:40:47.195
+ thrust profile: [1.0 -0.11697533327433789 -0.12607981354359105; 0.7619237843497473 0.4678233599831716 -0.2820207795111462; 0.3099344637931747 0.3516704960248328 -0.21642025384963806; 0.09046834318310792 0.15041544974174353 -0.10656653207316856; 0.03867791757546567 0.08626426152978771 -0.06647485622545368; 0.03275521104651064 0.0942084406361695 -0.0758024303635605; 0.013775709322309988 0.05174084580765969 -0.04458876525475742; 0.010207976679369027 0.04817504388633041 -0.04337856303768912; 0.00024997987224789067 0.0015614401760514814 -0.0014432137837976503; 7.970192852250033e-5 0.0008429726231114019 -0.0007659169473763791; 1.359040478769144e-5 0.0001140425421033242 -0.00011288204257971948; 1.868799683529695e-5 0.0001744316825570077 -0.00011696311900993256; -5.809459205652161e-5 7.891424075698033e-5 -0.00011311733033894159; -2.792981661137059e-6 0.00010427339446933737 -0.00010828581896482629; -4.782389535948171e-5 -3.26451723352506e-5 -3.4765492062222806e-5; 5.36974793343758e-5 2.7591655906605194e-5 -1.941469879041392e-5; 6.656815730737988e-5 1.815751153530917e-5 4.288384667485867e-5; 0.00010607066215585865 -0.00013754102885611702 -0.00021799458341033992; -0.00024093598066339463 -2.29667090166145e-5 -7.682162806045678e-5; 7.384679299931272e-5 1.009662146849878e-5 -2.41632086425422e-5] %
+
+Mass Used: 220.9003837814421 kg
+Launch C3: 88.02715469686188 km²/s²
+||V∞_in||: 9.319353959506177e-7 km/s
diff --git a/archive/ES_0.6296927211714508 b/archive/ES_0.6296927211714508
new file mode 100644
index 0000000..8146dbc
--- /dev/null
+++ b/archive/ES_0.6296927211714508
@@ -0,0 +1,22 @@
+archive/ES_0.6296927211714508---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T14:30:28.710
+Launch V∞: [7.0279126877691755, -7.515687898269922, -2.2071267399833543] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.02470394988034002, 0.02414235398624327, 0.002570576331924462] km/s
+ V∞_out: [-0.023246505167833637, 0.01876463882985475, -0.017527216407987593] km/s
+ time of flight: 1.0780418967085755e8 seconds
+ arrival date: 2027-10-08T08:06:57.710
+ thrust profile: [0.7080155586860498 -0.36228381444459473 -0.38649367706704074; 0.1838790363305148 -0.012077119331190812 -0.19865093386584243; 0.10785966003783416 0.01307807228708373 -0.17807794543718422; 0.05105720017906057 0.012809750436314027 -0.1172060361044748; 0.03190832814624064 0.011077489412065905 -0.09445289246960954; 0.021750046239202982 0.008643743081105444 -0.07360505749019648; 0.02150107366280138 0.007498989684706676 -0.07583118286225596; 0.018106509217044906 0.006252825674524482 -0.067248825704744; 0.03168587581544498 0.011682279743414526 -0.11786606410424157; -0.001961133158613112 0.002801468936445773 -0.01082384420430058; 0.009201142204839547 -0.003478273189399388 -0.012818662640715267; 0.0077967483016748145 0.0019469105054154986 -0.014463190620726173; 0.00046736789576933436 0.002064231717408436 -0.01019816434728086; 0.00996936265530296 0.0014440300698469314 -0.017802294745186485; 0.008152916212457605 -0.00024278976694560553 -0.005183991353573067; -0.0002468020031781964 -0.0012421830154705103 -0.008577450115841014; 0.002386175125606811 -0.001960751759988248 -0.005690734494234594; 0.0009981020368787486 -0.008655345884214065 -0.011140686662682682; -0.004582267391646233 -0.000777997041241578 0.0016409150396735905; -0.0031501717229959186 0.0020014798436745213 0.0007739068535776326] %
+
+Mass Used: 88.60841766485737 kg
+Launch C3: 110.74852977745746 km²/s²
+||V∞_in||: 0.03463735351272782 km/s
diff --git a/archive/ES_0.6298286028274559 b/archive/ES_0.6298286028274559
new file mode 100644
index 0000000..a4e9290
--- /dev/null
+++ b/archive/ES_0.6298286028274559
@@ -0,0 +1,22 @@
+archive/ES_0.6298286028274559---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T02:01:23.181
+Launch V∞: [7.038272121870429, -7.309319406413, -1.9092510581123816] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.605737679865584e-6, -7.129933029988679e-5, 9.411314084998497e-6] km/s
+ V∞_out: [-1.0289271173815534e-5, 4.449336870376596e-5, 5.584062500115702e-5] km/s
+ time of flight: 1.0702447961174785e8 seconds
+ arrival date: 2027-09-26T19:02:42.181
+ thrust profile: [0.9015717525023972 -0.44031757962587836 -0.4686861479319409; 0.37787434129185454 -0.00832448326234279 -0.3779069272037444; 0.18010913695647404 0.03422301719452855 -0.27116040036650285; 0.08661490335956445 0.027938168906107973 -0.17457598939981347; 0.03418458197625403 0.013299855648964737 -0.08602692918426685; 0.02534895372616799 0.012287620180821215 -0.07658427942850794; 0.02046976371024996 0.009088957328950962 -0.06033756277781505; 0.018973711720243664 0.01167375800174121 -0.06469586951135191; 0.026947743244961637 0.015617723800047011 -0.09697870657096024; 0.009521322845467086 0.005283388503755209 -0.03208242949623784; -2.270580261820197e-5 -0.0008038755573662342 0.0015216033787857834; 0.0003438470703866202 4.630793984441821e-5 -0.0008767120092075701; 0.00032908853552286797 0.00036313375348862096 -0.000839166682526785; 0.0023901886085611257 0.002037283735038977 0.001761389072318939; 0.0006916196115478931 -0.00019075288374752154 -0.0006532363755057167; 0.0017959295779990771 -0.0006787829603026017 -0.0008213603492346785; -0.00038646048610468465 -0.00924106784328052 0.003008998502889268; -0.000614761405842623 0.0036499706152863746 0.0033825640686170567; -0.007691725922209628 0.004861133219513316 0.007637128189047969; -0.0014612153766464771 0.0006857863493024347 0.0024754019688129495] %
+
+Mass Used: 112.9161618440553 kg
+Launch C3: 106.60866424936741 km²/s²
+||V∞_in||: 7.2135924676643e-5 km/s
diff --git a/archive/ES_0.629985501736359 b/archive/ES_0.629985501736359
new file mode 100644
index 0000000..38f2fc4
--- /dev/null
+++ b/archive/ES_0.629985501736359
@@ -0,0 +1,22 @@
+archive/ES_0.629985501736359---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T16:42:44.730
+Launch V∞: [6.949019595191274, -7.436954863584301, -1.7269702703961471] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006277966756031339, -0.002938799955620192, -0.00022618244997723354] km/s
+ V∞_out: [0.005369851364162304, 0.0031547233248626644, -0.0031762952699659537] km/s
+ time of flight: 1.0679504689016148e8 seconds
+ arrival date: 2027-09-25T18:00:10.730
+ thrust profile: [1.0 -0.507895241062905 -0.4961437043877561; 0.2978010697096091 -0.014680157485691953 -0.3160285129676147; 0.08361106786720089 0.010952556513752314 -0.1403229188092707; 0.043318078867723306 0.01029690650558378 -0.09491135689380478; 0.04521177705383894 0.013455134400380328 -0.11854831616348127; 0.09700588881678042 0.03449129408440244 -0.27587807542264614; 0.02951210516379105 0.01131870307778496 -0.09812271689327848; 0.01884289766447212 0.007585796371539501 -0.06789843845100807; 0.030064828809516955 0.012347580069696978 -0.11565628510661877; 0.0002528714703697247 2.008924321921532e-5 -0.002224487701901222; 0.0008942333882427968 0.00021315828302749691 -0.003506199933427547; 0.00015656972487322667 2.2692716627839012e-5 -0.001202806906068186; 0.0002768631173387274 -0.001377149137690686 -0.0014287252443154399; 0.00029386193122220294 0.0001731866501250988 -0.0013058023433537985; 0.0014027530624167498 0.0005056982178877268 -0.0008168532361024552; 0.00024100988915858631 7.103897609726253e-5 -0.0008954653186721683; -0.0008687964463143787 -0.00030054120388085283 0.0002555987382243537; 0.00021093521687028812 0.002937959483253178 -0.000913758577307058; 0.00019502602194053408 -8.130487256845055e-5 0.0002020837223171354; 2.8657858899720084e-5 -0.00018884851443383248 0.0005705214647017433] %
+
+Mass Used: 113.26876782140016 kg
+Launch C3: 106.57959729217463 km²/s²
+||V∞_in||: 0.006935457466502523 km/s
diff --git a/archive/ES_0.6301334640094225 b/archive/ES_0.6301334640094225
new file mode 100644
index 0000000..1a64fa5
--- /dev/null
+++ b/archive/ES_0.6301334640094225
@@ -0,0 +1,22 @@
+archive/ES_0.6301334640094225---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T12:04:30.721
+Launch V∞: [5.21268630810349, -8.711294745278524, -1.5848941376185777] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.6801091429141786e-5, 2.3478218141721417e-5, 4.677818659064862e-5] km/s
+ V∞_out: [-3.1843780224538785e-5, 4.140297859935455e-5, -4.634767906489332e-5] km/s
+ time of flight: 1.0660111747780736e8 seconds
+ arrival date: 2026-09-09T07:29:47.721
+ thrust profile: [0.9366081274610671 -0.7389995300606947 -0.53257262895888; 0.3110656700152331 -0.08240804268503064 -0.33901883171852004; 0.1835632567845992 -0.012871840752447919 -0.2885758497895396; 0.18211515470244719 0.006166597495858395 -0.35656258084144177; 0.03974436942628321 0.004129582826330137 -0.09426388050815986; 0.032858701755962574 0.005401289535203942 -0.08766828186661985; 0.00995493162178691 0.0015667513121186897 -0.03002637475902373; 0.0020959242685497743 0.00041703043077372955 -0.0070052766431191234; 0.010005779106341399 0.001941117432410282 -0.03414756282805354; 0.000765046631202701 0.0003003074038669925 -0.004108802022022229; 0.0009951868062424317 -0.00044779670569734483 -0.002648222733005473; 0.0004876273014321074 0.0002795109841450184 -0.0028859730583814056; 7.274567752751351e-5 -0.0003474749921793139 -0.0019663642135150385; 0.0010303142594105391 0.0004750651888611448 -0.0017434607935151183; 0.00037962866606615586 0.0011065597748442801 0.0008143803916339058; 0.0008072325863866187 0.0002695931959232091 -0.001000707492191452; 0.000782557444125243 0.00092755920676082 0.0004719559957332923; -0.0002331586506566552 3.127975203500138e-5 0.0009304554038957044; -0.0008969966757352947 -0.00033707568930487657 -0.002253216060674686; 0.00021503574635757956 -0.0010474088300893528 -0.0019469012236519095] %
+
+Mass Used: 119.32695068361636 kg
+Launch C3: 105.57064411326455 km²/s²
+||V∞_in||: 7.021230395577889e-5 km/s
diff --git a/archive/ES_0.6301678436848214 b/archive/ES_0.6301678436848214
new file mode 100644
index 0000000..c0b880b
--- /dev/null
+++ b/archive/ES_0.6301678436848214
@@ -0,0 +1,22 @@
+archive/ES_0.6301678436848214---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T00:58:23.035
+Launch V∞: [7.037095841505428, -7.506967193453809, -1.8202350373107252] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001487889077682079, -0.008684794692245328, 0.008336365957813112] km/s
+ V∞_out: [0.0032981703412377963, 0.004687616531534446, -0.010688059677811237] km/s
+ time of flight: 1.066575885785976e8 seconds
+ arrival date: 2027-09-24T12:04:51.035
+ thrust profile: [0.702233137848213 -0.35832433966908117 -0.3911138027740423; 0.27062181864271323 -0.015122920038972946 -0.2998753366679604; 0.1804567314863761 0.02359607025158851 -0.29615923025767643; 0.10928441224379037 0.0264349134073184 -0.23703861832706982; 0.04636620801316975 0.01429204947368954 -0.12656007658795493; 0.01133677775974653 0.004043366995193049 -0.03559581372052806; 0.0047595642987306175 0.0019602972184017296 -0.01842302602459253; 0.03916637632378543 0.015925400858335277 -0.1489467169140922; 0.009251169440825633 0.0036982319471618574 -0.03821065596350658; 0.005564611911583311 0.002311254965990716 -0.024150926567800535; -0.000483080817447284 7.030667213138553e-5 0.0008029729677552763; 0.0005051498948148397 0.00032388397236246953 0.000746572451447015; -0.00023852605228934467 0.00040759902645738806 0.0008205051139446385; -0.0002866218393540726 1.2311991323124986e-5 0.0003667678881633867; 0.00033697376025961054 -0.0002466029125385752 -0.000399498083650874; 0.00010206983801455457 1.7305736072389575e-5 -0.00035631027092084217; -0.0007477871264648419 -0.0006293668880644023 -0.0011328757410740652; 0.0008021737760124969 5.135923596496021e-5 0.00018263336972953158; 9.035859527382141e-5 -1.1923740429640398e-5 7.716887891013056e-5; 0.00024438240022514645 -0.0012820484557799412 5.649163478619579e-5] %
+
+Mass Used: 98.26272644875144 kg
+Launch C3: 109.18852991717831 km²/s²
+||V∞_in||: 0.012129899840333537 km/s
diff --git a/archive/ES_0.6302753871689412 b/archive/ES_0.6302753871689412
new file mode 100644
index 0000000..2bcb302
--- /dev/null
+++ b/archive/ES_0.6302753871689412
@@ -0,0 +1,22 @@
+archive/ES_0.6302753871689412---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T16:04:24.500
+Launch V∞: [7.155723081955582, -7.3555949822782605, -1.4430085268068047] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.3041316269038437e-9, -1.4122985434423852e-9, -7.27761239260288e-10] km/s
+ V∞_out: [1.961618327856383e-10, -7.064455374641521e-10, 1.221052455715304e-10] km/s
+ time of flight: 1.0788241021292719e8 seconds
+ arrival date: 2027-10-06T07:24:34.500
+ thrust profile: [0.606320109345905 -0.28044062901291794 -0.2809554685836365; 0.1881394588224232 0.0005042751999352697 -0.187124188747183; 0.22705972395376545 0.046455655588772675 -0.31834564595260584; 0.24172604188862135 0.07798583115639643 -0.4273957324268104; 0.08911660603571726 0.03658313002047458 -0.20582041604697357; 0.06550811279375385 0.031004545050305178 -0.16990766128491624; 0.022479328908929216 0.011843693513106787 -0.07071121792394819; 0.023477376497998168 0.01197688311734223 -0.07388066180695615; 0.014639677141202541 0.008488273070350183 -0.05230235209097439; 0.0017705935129304984 0.0008689891983483343 -0.0074439451249898; -0.0002489715514538886 -0.000527228197310009 0.0020192713527874984; -0.00018884823201733165 -0.00025419273632712247 0.0031380006855182105; -0.0012230272004996347 -0.00017694113828777556 -0.0004814771535704962; -0.0011138945901408473 -2.728844927824121e-5 -5.579836695190595e-5; -0.0008770464654992508 0.0010672281677640298 0.0011778873976696456; -0.0031107708967331696 -9.058117210298297e-5 -0.0006003624553729927; -0.0007753464579067412 0.0013822578372561026 0.0008280586957353685; 6.092974704716249e-5 0.002616633228155649 0.002577183903256941; -0.0021340883728219956 0.005365381746145653 0.003321113199256194; 0.00015044125597626955 -0.0002603123036971066 0.00016806909334077962] %
+
+Mass Used: 108.87131182901203 kg
+Launch C3: 107.39142397738617 km²/s²
+||V∞_in||: 2.0554763188784297e-9 km/s
diff --git a/archive/ES_0.6304871590387922 b/archive/ES_0.6304871590387922
new file mode 100644
index 0000000..6fce206
--- /dev/null
+++ b/archive/ES_0.6304871590387922
@@ -0,0 +1,22 @@
+archive/ES_0.6304871590387922---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T01:29:43.892
+Launch V∞: [6.992830459342908, -7.395874168211094, -1.9081260876242567] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.20680365593340339, -0.9800976944109879, -1.4792151891769305] km/s
+ V∞_out: [0.8005820566351382, 0.34680057479804444, 1.5591236520255265] km/s
+ time of flight: 1.0648947685789992e8 seconds
+ arrival date: 2027-09-21T13:54:19.892
+ thrust profile: [0.8653909622842979 -0.4355164450017822 -0.4642067622991213; 0.43426930864527136 -0.021747095751549716 -0.45305226294812784; 0.17126416104438336 0.024937336862999347 -0.2770909259551411; 0.07288999217357656 0.018703639775909872 -0.1572614620553635; 0.03633625757687732 0.0108962098890166 -0.09459558418906107; 0.02086473184670625 0.008050648885495233 -0.0622004914430809; 0.01712698251481001 0.007262800743707292 -0.056979815169680335; 0.010535696840205335 0.0047112893671195375 -0.03884060302654901; 0.00353833997218753 0.001663792178549119 -0.015290959977923207; 0.005123693712898513 0.004194740170064853 -0.027789042263036273; 0.003332884299523861 0.0019197537638867917 -0.015375791451832665; 0.0007471998413630374 0.0037012236678422563 -0.006703025893862461; -0.00011414122255659761 -0.0002157599570290561 0.00019010675561488945; -0.00016540371630980374 0.0004803205212161554 0.0017784709142164004; -0.0022721182151573746 -0.0006033620204440116 -0.010265364386920849; -0.003976695046141277 -0.0013031156285426915 -0.0021772030792745157; 0.004598921684439938 -0.0038747338187448076 0.005750155802450268; 0.00384795700010112 0.0021190900147722725 -0.0016972233285496255; 0.0011593904878203646 -0.0006026808777213239 -0.0034911215828645195; -0.011376977618298905 -0.011991022996499867 0.012046115297645047] %
+
+Mass Used: 110.0041488954339 kg
+Launch C3: 107.23957771139834 km²/s²
+||V∞_in||: 1.7864592966504718 km/s
diff --git a/archive/ES_0.6307666958785305 b/archive/ES_0.6307666958785305
new file mode 100644
index 0000000..ea1782e
--- /dev/null
+++ b/archive/ES_0.6307666958785305
@@ -0,0 +1,22 @@
+archive/ES_0.6307666958785305---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T21:29:44.513
+Launch V∞: [5.443887661728503, -8.724533619659661, -2.073238951449051] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.11560114055271156, -0.08319904289136124, 0.04845605120803724] km/s
+ V∞_out: [-0.0923023121660965, 0.08080711815335265, -0.08730368018997628] km/s
+ time of flight: 1.0789335953978708e8 seconds
+ arrival date: 2026-09-23T15:52:23.513
+ thrust profile: [0.5322076968344756 -0.4137537820028671 -0.3197196971967374; 0.3111842141851451 -0.07115975714555095 -0.32247588177105746; 0.17792431249018947 -0.003085142874276776 -0.2646338747220784; 0.08785394863520797 0.008837188648860466 -0.16989285386033515; 0.04409485763967314 0.00800455686702542 -0.10441761536130599; 0.033234961713608104 0.00708489967706902 -0.09149075779502425; 0.034461932609912316 0.00926856182127014 -0.10229944367552729; 0.017960833861601855 0.00509760903514001 -0.05146383009839909; 0.007159916540519267 0.004215703954873744 -0.017087801701039847; 0.0058861589523799916 -0.003872755069630771 -0.0036263488574638796; -0.000589997302961983 -0.004169122617814203 -0.002080861861349747; -0.0004764722243027037 -0.0006281399136031005 -0.003055746592580166; -0.0025001736930579 0.009137729640384291 0.002084181570973641; 0.0010604057878804247 0.0004279388442533426 -0.005463941286999064; -0.003263061682760627 0.00735979959157975 0.006534155121864997; 0.0017092203364188544 -0.00458126355927373 0.0015428437948541698; -0.002797789513436662 -0.002350393816272272 0.0027596496110866234; -0.01143529238272756 0.009815273044922182 0.003237614948333702; -0.0017266457189108234 0.009076856823661621 -0.0033997617388456984; -0.0006849303924505846 -0.002469374611448515 -0.005785058858691357] %
+
+Mass Used: 93.92611475221929 kg
+Launch C3: 110.0517195038971 km²/s²
+||V∞_in||: 0.15044498440892692 km/s
diff --git a/archive/ES_0.6309981219808931 b/archive/ES_0.6309981219808931
new file mode 100644
index 0000000..c74f210
--- /dev/null
+++ b/archive/ES_0.6309981219808931
@@ -0,0 +1,22 @@
+archive/ES_0.6309981219808931---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T02:46:16.522
+Launch V∞: [7.22135415118586, -7.5035030444492605, -2.537273422164054] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.625416781493175e-5, -2.6154875195917478e-5, 1.9183207073038403e-5] km/s
+ V∞_out: [3.279468917033276e-5, -1.990942393824358e-5, -1.6423858407559215e-5] km/s
+ time of flight: 1.0693184083950432e8 seconds
+ arrival date: 2027-09-27T18:03:36.522
+ thrust profile: [0.3576098928027137 -0.18054397220079813 -0.20943700549392597; 0.2080155273013785 -0.009145753120665416 -0.21682177962635063; 0.13631860236389987 0.02062196254085358 -0.211728951241052; 0.08546103821020244 0.022877571019101543 -0.1739538800476015; 0.04228037324716517 0.015414232762023316 -0.10727068538278019; 0.010981353283608017 0.004086519288432233 -0.03466874646565601; 0.011080457358825315 0.004959473962321262 -0.03679521223520994; 0.011539992676139773 0.006097066891805895 -0.044083824165366374; 0.0024931367477111443 0.0015359628614647646 -0.011078979194095175; 0.008431423804003073 0.0045819483329242695 -0.03830102204925243; 0.0030793361348772415 0.0010115249474148685 -0.011013296264497397; 0.0015273994074035757 0.0005398431975596257 -0.007737605279025183; 0.00017173332198434297 0.002289020360700495 -0.00320070740128383; 0.0007136935338336982 0.000294034476793938 -0.004443252694114923; 0.0007358697240940288 0.0005507865700086836 -0.0026576367899363088; 0.002836921403706472 0.0011153948060842296 -0.0032933179915302056; 0.0033625852882439664 0.001568494925923454 -0.0025719763447584424; 0.001493227166706585 -0.00018864535625797525 -0.0024340760334352427; 0.006491107379985571 0.0026530014538671486 -0.0072965968053107545; 0.00014578489577572398 0.002143801471540834 -0.007660851641087426] %
+
+Mass Used: 65.98289986429154 kg
+Launch C3: 114.88827013372865 km²/s²
+||V∞_in||: 4.172953699450413e-5 km/s
diff --git a/archive/ES_0.6311194169901555 b/archive/ES_0.6311194169901555
new file mode 100644
index 0000000..9a98232
--- /dev/null
+++ b/archive/ES_0.6311194169901555
@@ -0,0 +1,22 @@
+archive/ES_0.6311194169901555---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T04:49:28.729
+Launch V∞: [7.092812495055724, -7.49634739335776, -2.1246274702670576] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.450561033354945e-5, -4.353659731221766e-5, 3.3149955865196915e-5] km/s
+ V∞_out: [5.539009567925065e-5, -3.4145738513903954e-5, -2.7216405096973878e-5] km/s
+ time of flight: 1.0586420791218245e8 seconds
+ arrival date: 2027-09-15T11:32:55.729
+ thrust profile: [0.7104704551198637 -0.35855088339350927 -0.39937563474633925; 0.2576709233755325 -0.01425527555754195 -0.28930286152263884; 0.1381390449118911 0.018285611005162357 -0.23748413391909567; 0.06496314060472995 0.015263859031356389 -0.14995053291254776; 0.03373925522197413 0.009184521552001933 -0.094839532397349; 0.021847286623760544 0.006792140712309652 -0.0710358400873992; 0.025696351158589092 0.009051674853262593 -0.09189292669272663; 0.01756209239001395 0.006293729400336042 -0.06986265240085798; 0.002993594119062329 0.001020205388835677 -0.012753909374163245; 0.00142000004588857 0.00033624746986780164 -0.006144748763224511; 0.002627440498105952 0.000988121688926251 -0.013436357834787884; 0.0004565474701259104 7.279759512862688e-5 -0.002961885384552286; 0.0006774928196252255 -0.000667534541635629 -1.8958130667638897e-5; 0.0008023093952598003 -3.8433654220702585e-6 -0.00038847667588999134; 0.00027888985241617437 -4.098434985796566e-5 -0.000251747760413383; 0.0002443571036351006 0.00031023118256959703 0.0005487602581606154; -5.9191762917471246e-5 -0.0006403666210962757 -0.0002587431111142751; 0.0003189158436395329 0.00037245391477462255 -0.0007303458959457161; 0.00029941835027245007 -0.00027269177372306737 0.0006638014441130284; 0.00025010956749347326 0.0013728277712429235 -0.0004082596098898395] %
+
+Mass Used: 88.70533104240167 kg
+Launch C3: 111.01725521933368 km²/s²
+||V∞_in||: 7.053441876525563e-5 km/s
diff --git a/archive/ES_0.6312335981520919 b/archive/ES_0.6312335981520919
new file mode 100644
index 0000000..2903491
--- /dev/null
+++ b/archive/ES_0.6312335981520919
@@ -0,0 +1,22 @@
+archive/ES_0.6312335981520919---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T17:32:48.384
+Launch V∞: [5.539226239049194, -8.735870757151812, -2.2135249110905293] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006173969201359291, -0.003154863090514017, 0.006798997598812127] km/s
+ V∞_out: [0.0028408307148081726, -0.007554715095215591, -0.005400974247955221] km/s
+ time of flight: 1.0734960807405414e8 seconds
+ arrival date: 2026-09-17T04:52:56.384
+ thrust profile: [0.45066709112908304 -0.3408568556691963 -0.27212202527229423; 0.2644526007624513 -0.055955148436115335 -0.27217209176972645; 0.17251420813166032 -0.0006406214174787059 -0.2516658392341923; 0.1132045165333278 0.012686625993618314 -0.21005634552407887; 0.06436569794106382 0.012157136783513996 -0.1437802663858511; 0.024348869321226912 0.006134269046740829 -0.06383966764254838; 0.015019083439735688 0.0042847452454096 -0.04345658883975924; 0.009245349944631685 0.0029891276258063523 -0.027128164428063137; 0.006217137178531871 0.002554823991791927 -0.022847229184763767; 0.013479993939066936 0.005053606451491551 -0.045939316318686085; -0.0006184261096759615 0.0008747294207798425 9.171049367722242e-5; 0.0006264880884995448 0.0021504691150365275 -0.004335472358183928; 0.00017790147272180436 -0.0011879353083526496 0.00039898400533880125; -0.0005007891365291613 -8.230856327099529e-6 0.001349828543406311; -0.0010180665558280808 0.0044113330562044915 -0.0014798558983277529; -0.00024936434334441233 0.0028533644455422547 0.0033498333759715733; -0.00040874785876552364 -0.00014064801258332257 -0.0017187813696129227; -0.0006917448947617109 -0.0024401576242665244 0.0049558422247278095; -0.0024782344744438177 -0.0009576349145240062 -2.9675855677301858e-5; -0.0008239143269890307 0.0004962803391836538 0.0016218720467412774] %
+
+Mass Used: 83.69994433131797 kg
+Launch C3: 111.89815774504959 km²/s²
+||V∞_in||: 0.009710686132703178 km/s
diff --git a/archive/ES_0.6315091289402202 b/archive/ES_0.6315091289402202
new file mode 100644
index 0000000..a4b1ccc
--- /dev/null
+++ b/archive/ES_0.6315091289402202
@@ -0,0 +1,22 @@
+archive/ES_0.6315091289402202---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T01:16:28.534
+Launch V∞: [6.96722473402379, -7.54554735884985, -2.0585186409791287] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.019066085509177023, -0.04846447086609961, -0.0650528288236143] km/s
+ V∞_out: [-0.0737836777861822, -0.012269169468054486, 0.0368565380722199] km/s
+ time of flight: 1.0596348877451095e8 seconds
+ arrival date: 2027-09-17T11:34:36.534
+ thrust profile: [0.9774513887779439 -0.5128319675631914 -0.4951156897074363; 0.10173365781074517 -0.007513846641275736 -0.12342846666360091; 0.1382352717407799 0.016701761073509725 -0.24620957507636906; 0.051035761419255414 0.01028830364968153 -0.11775777641060697; 0.04402248975089272 0.011449565144692888 -0.12227871721018642; 0.043809545618992696 0.013145627914587345 -0.13879532382393944; 0.02480733374704302 0.008238680440782634 -0.08913683306037769; 0.005966429671236689 0.0019488554938249414 -0.025261622600706583; 0.017715196211148355 0.006579754274571271 -0.07473437679283548; 0.005294880436420229 0.0019273651191115335 -0.022045764892741092; 0.0016756562491188603 0.000850854023517641 -0.0057640657918566615; -5.834362079155096e-5 -0.0008246757484027172 -0.0016335686898746311; -0.00045347392447199036 0.00028224817196931793 -0.0007602292265771822; 0.00039390759238149887 0.00015718537002918568 -0.00012395728910009592; 3.0035303661002505e-5 -0.0003242155898115727 -0.0006273281006067979; -0.002082160815022345 -0.000817924402490417 -0.00012670967911357014; -0.0005350150055476511 0.0002495428494897878 -0.0009318859700145705; -0.00018364028330315567 0.00048330245857234884 -0.0009392354336803251; -0.0006322111983082271 0.0006792914874642765 7.131755530943612e-5; 0.0001341245445639076 0.0007633611423822249 0.0005690526502331499] %
+
+Mass Used: 96.75645789685541 kg
+Launch C3: 109.71500443429738 km²/s²
+||V∞_in||: 0.08333181319837418 km/s
diff --git a/archive/ES_0.6316686173939775 b/archive/ES_0.6316686173939775
new file mode 100644
index 0000000..9ad6ee3
--- /dev/null
+++ b/archive/ES_0.6316686173939775
@@ -0,0 +1,22 @@
+archive/ES_0.6316686173939775---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T02:48:49.820
+Launch V∞: [7.08384448473807, -7.397234871690406, -2.1488237378703356] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.948956394949959e-6, -2.01045206114956e-5, 2.8284171880437886e-6] km/s
+ V∞_out: [-3.1927316674226425e-6, 1.16453193612484e-5, 1.643679326269557e-5] km/s
+ time of flight: 1.103672385843783e8 seconds
+ arrival date: 2027-11-05T12:22:47.820
+ thrust profile: [0.5072880493159093 -0.253820960966798 -0.2863673430667896; 0.25767282299699534 -0.011708529628806258 -0.28300096476131503; 0.1618772980676784 0.023069342026857738 -0.26701684600891384; 0.09934445234300228 0.0244412390670609 -0.21308909334241646; 0.05538563099028093 0.017617657051355783 -0.14307936323511364; 0.03046224413547599 0.010157002055134262 -0.08378428348419069; 0.0014300317272078395 0.002314337239480731 -0.005059299787131035; 0.013133837459499614 0.004623119554451363 -0.0029460930448115454; 0.003941069577055751 0.0020715981368400996 -0.026033466773069974; 0.0009056657268709489 0.00041916407000584143 -0.005788910904067781; 0.009104526691994162 -0.005060612196308992 -0.04757920119996263; 0.007919396187899684 -0.0022048234432812835 -0.04631275263178014; 4.961094585435107e-5 -4.566941652936598e-6 -0.0006653185814705764; -0.003855004670278799 -0.001705132593113525 0.0003778714028539543; -0.05506437042015151 0.020490591444811183 -0.021256845322965418; -0.0036709304991170756 0.03687622495642042 -0.02088796416932815; 0.01933824298005653 0.0037423765858659273 -0.04318450134467988; -0.00045011519273596267 -0.003146871874612146 0.018817968328005905; 0.0016308624547182952 -0.020198395137854694 0.03646670037659651; -0.005414382386370362 -0.0029185435541588312 0.0535896607098458] %
+
+Mass Used: 98.0953376168145 kg
+Launch C3: 109.51737988734159 km²/s²
+||V∞_in||: 2.039583594357165e-5 km/s
diff --git a/archive/ES_0.6317424223240633 b/archive/ES_0.6317424223240633
new file mode 100644
index 0000000..35c115d
--- /dev/null
+++ b/archive/ES_0.6317424223240633
@@ -0,0 +1,22 @@
+archive/ES_0.6317424223240633---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T10:29:21.348
+Launch V∞: [5.135807736867101, -8.500475570450726, -1.6078292527467992] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.7806246312036199, 0.21748331395429965, -0.5372179094735652] km/s
+ V∞_out: [0.7079830042289732, 0.2769224603449566, 0.6230148360815422] km/s
+ time of flight: 1.1101166893228304e8 seconds
+ arrival date: 2026-10-28T07:03:49.348
+ thrust profile: [0.9845206088722515 -0.7724072165895721 -0.5496260529491717; 0.4374653116426381 -0.10227256308762384 -0.4303523746302623; 0.2854995090497823 -0.008391488718308762 -0.4010455436964456; 0.062207790763619424 0.005086553428116228 -0.10641979957951857; 0.02380056398158796 0.0036731005314260537 -0.04589087678977107; 0.01718859033196287 0.0033744537583986077 -0.037995487165822774; -0.0017728678729449 0.003104061351784532 -0.012844730992839108; 0.03347094955205633 0.008827767271274156 -0.09149434728866915; 0.02393233728545871 0.007151023669366723 -0.0594693154269624; 0.009303962190206568 0.010575528425227064 -0.0458035143263619; -8.69853890903547e-5 -0.00013550184270143023 -0.0013372775417645924; 0.010433734845349207 0.004969696933949109 -0.020376085950333602; -0.026554617810339826 0.019121736371532246 -0.048423886563496985; 0.03320934527477721 0.020949101734041457 -0.0038987296745958; -0.0011382042335788744 -0.0002181102631965374 -0.002524840448941452; 0.0005844480382808353 0.04136918641441972 -0.07292648987571036; -0.039532274480080856 0.02908909189589312 -0.04961034790236156; 0.025210819258729388 0.047245349782968134 -0.00392688263616893; -0.034631687618247205 -0.03789625989486359 -0.015567285095111651; -0.0012433735659417677 0.007049436228626401 -0.0031955206845195087] %
+
+Mass Used: 146.5844538954293 kg
+Launch C3: 101.21972093988191 km²/s²
+||V∞_in||: 0.9722535106388044 km/s
diff --git a/archive/ES_0.631848501640776 b/archive/ES_0.631848501640776
new file mode 100644
index 0000000..cd493a1
--- /dev/null
+++ b/archive/ES_0.631848501640776
@@ -0,0 +1,22 @@
+archive/ES_0.631848501640776---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T19:37:27.001
+Launch V∞: [7.116052274233412, -7.306139175612478, -1.7067672992597325] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004407230700135003, -0.011432878276170412, -0.015112092471713393] km/s
+ V∞_out: [-0.01697310223032343, -0.0027632418159850543, 0.009097051871487143] km/s
+ time of flight: 1.070368476826357e8 seconds
+ arrival date: 2027-09-26T16:04:54.001
+ thrust profile: [0.7835274827111219 -0.3824464337098166 -0.4162722775358894; 0.32986630020635754 -0.011109385513967248 -0.34287410230848464; 0.20508437170920457 0.03541810432972709 -0.31729783900232506; 0.10331686253891993 0.028192148779789247 -0.20651078918908267; 0.12303948167720237 0.04465168427170155 -0.2998151433262231; 0.020737246607925384 0.008150723871957135 -0.05362501073923455; 0.021254798244877793 0.008784959836909178 -0.06168969215898777; 0.004140778380192419 -0.0070546084915132385 -0.01516775614343192; 0.001320789700950539 0.0036446924470912175 -0.007949539648144275; 0.001617955053917636 -0.002476869296592934 -0.008511526061111576; 0.008491021715166644 0.0033772178784820008 -0.020418043021647403; 0.004022662834894551 0.0022441233786986902 -0.014991951270423045; 3.9892320988787176e-5 -0.0014856186332592005 -0.0086806857492854; 0.0015429921779013447 -0.000580834422225218 5.316896930122883e-5; -0.0027832753019503206 -0.0028696919366705464 -0.004960889980370713; -0.0020102842698071534 0.007878438812733096 0.008534929290863844; -0.0028453031372015023 -0.00018837793347807738 0.01453220311281838; -0.0004726328645909732 -0.0005067394581660086 0.0029478434626104676; 0.0033034454924981485 -0.0049243424392686145 -0.025576818360512482; -0.006470796798492839 0.005691678369703201 -0.00380828066634617] %
+
+Mass Used: 113.39286053253045 kg
+Launch C3: 106.93092423686426 km²/s²
+||V∞_in||: 0.01945532644279089 km/s
diff --git a/archive/ES_0.6320828681159689 b/archive/ES_0.6320828681159689
new file mode 100644
index 0000000..dcf331c
--- /dev/null
+++ b/archive/ES_0.6320828681159689
@@ -0,0 +1,22 @@
+archive/ES_0.6320828681159689---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T21:11:42.679
+Launch V∞: [5.247257384411783, -8.732952022417063, -1.9904253822706162] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.410866308139423e-6, 3.0494090403251926e-6, 6.4350018499122024e-6] km/s
+ V∞_out: [-4.351080574959967e-6, 3.9502390982223386e-6, -7.609956644518147e-6] km/s
+ time of flight: 1.0879106110922682e8 seconds
+ arrival date: 2026-10-05T00:56:03.679
+ thrust profile: [0.7401134604336186 -0.5957509247207357 -0.4728067314277311; 0.2746853800903356 -0.07335099413334985 -0.3235296859994092; 0.14546960957975819 -0.010177121435092414 -0.25276947582598464; 0.08926815550510779 0.00312941781013622 -0.20002274466711104; 0.04372446846645215 0.003927596430253329 -0.12034604745164772; 0.02183103245516967 0.002987995521748962 -0.0654032405391753; 0.017910935043018005 0.0023405921504051673 -0.06462471507884578; 0.00339457301252861 -0.0006940603593993377 -0.01072646285558686; 0.000595355913672062 -0.0010848553061308622 -0.0019136368130015834; 0.0020295195776514766 -0.0003517776150486064 -0.007143412601073099; 0.010245717007627914 0.004838894606270644 -0.011616323562460416; 0.005337635573991237 -0.0014382137148400253 0.013413035311459556; 0.009872479819901523 -0.004374215057309907 -0.008049777901249144; -0.0022507407023395847 0.005515292120705691 0.014806298826989178; 0.005699731488600106 0.0010911882232048102 -0.019776238883586823; 0.006128195762918112 0.009283298098061984 -0.0028121800920406044; -0.017724712432421366 0.03513923874038345 0.01909821946957637; 0.0034857280167647706 0.0013641641133756025 -0.002939072843019003; 0.012639431278231967 -0.021807228032350065 0.0009853733787526424; 0.013175770618384234 0.04965312783285156 0.02748572643960919] %
+
+Mass Used: 108.83027946410903 kg
+Launch C3: 107.75995428648937 km²/s²
+||V∞_in||: 9.581615266980181e-6 km/s
diff --git a/archive/ES_0.6321055477737177 b/archive/ES_0.6321055477737177
new file mode 100644
index 0000000..f6e4068
--- /dev/null
+++ b/archive/ES_0.6321055477737177
@@ -0,0 +1,22 @@
+archive/ES_0.6321055477737177---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T23:34:45.452
+Launch V∞: [7.124163879660523, -7.460809834663965, -2.2106267541139992] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0012965079405265706, -0.006446005977536644, 0.006231674118952618] km/s
+ V∞_out: [0.0024146204256544545, 0.0035106103911396406, -0.007994248921546621] km/s
+ time of flight: 1.0763511030543472e8 seconds
+ arrival date: 2027-10-05T18:13:15.452
+ thrust profile: [0.6444176801694259 -0.32273698487836056 -0.3168667017204979; 0.1879126636819547 -0.008355828099791126 -0.20066616527528186; 0.054332687971481 0.007595228401209972 -0.09765099474575153; 0.03456100935101083 0.00885603574680189 -0.08014710602196785; 0.062108767120091626 0.019891833681272154 -0.15828686724291832; 0.03688180997365028 0.01458306621211428 -0.11640441798276974; 0.023319280727451583 0.009768843033880474 -0.08415654768217662; 0.01713190693225483 0.0067759763068455875 -0.0796938152302083; 0.03734989471192597 0.014054035233791062 -0.13956945649821942; 0.017358213953412367 0.001552743234733281 -0.04008641724107614; 0.015201950740225201 -0.003971532009545002 -0.03891636595143448; 0.011011874564321716 0.004476891296752584 -0.014643077099790647; -0.0027432568099120327 0.005849696051373559 -0.0009061625738951036; 0.002979600820900666 0.0024077814293126205 -0.009889221088825064; -1.8062226059246955e-5 0.001810018450749158 0.0018364002134969998; -0.0012261763775138577 -0.0006070807487755297 -0.003803026630507322; 0.00021859782994220313 0.0014907556371992355 -0.0014911178827612583; -0.0034497925858060635 0.008585596657835468 -0.0064203268701843955; -0.02133811229795552 0.01500366703456316 -0.009537901957437894; 0.005872814312275999 -0.005984675238215945 0.014725189240539442] %
+
+Mass Used: 88.181593123521 kg
+Launch C3: 111.30426501928281 km²/s²
+||V∞_in||: 0.009059011437629962 km/s
diff --git a/archive/ES_0.6321308289109906 b/archive/ES_0.6321308289109906
new file mode 100644
index 0000000..9c682e0
--- /dev/null
+++ b/archive/ES_0.6321308289109906
@@ -0,0 +1,22 @@
+archive/ES_0.6321308289109906---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T19:21:40.461
+Launch V∞: [6.40699237199278, -7.55514233818836, 0.10587166388088436] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.923194539047502e-6, -2.5241239895557495e-6, -3.140691898906794e-6] km/s
+ V∞_out: [-4.254315006241427e-6, -2.6033467803852937e-6, -6.843027837381694e-8] km/s
+ time of flight: 1.874957778743831e8 seconds
+ arrival date: 2029-04-11T21:31:17.461
+ thrust profile: [0.13657915951322355 -0.047971723850063624 -0.05083070210358024; 0.16613862687538974 0.019364664490332896 -0.1812769624842148; 0.049862426390617935 0.006949420237068549 -0.09358591169810315; 0.04001472410512606 0.004990553545260851 -0.08824270105787395; 0.032042510293840316 0.004122767728403668 -0.0916118579577156; 0.027108668059105848 0.004762969784292463 -0.07935163874863546; 0.0235600529116236 -0.002516900325129178 -0.08890789076346417; 0.017571660322889184 0.0004500453262703127 -0.028537556802584546; 0.014717204257197688 0.012890066699470772 0.0035678331413217805; -0.006250952860847981 0.033863896043576446 -0.028775503562365544; 0.0025774666775360876 -0.0050861391107922226 -0.030914701831667588; 0.015189094435336928 0.030505078694326414 -0.014617195815765231; 0.00820052152285761 -0.001089950940440587 -0.015505813295891208; 0.11276892358820712 0.07329045651644898 -0.04221803126578747; 0.13404156597981404 0.1497298710843475 -0.05702883507916429; -0.030386829435099398 0.013505615557094005 -0.06366563972095626; -0.01483310437668009 -0.01828464191172599 0.020836386485661624; 0.15636058749633377 -0.1888281145778588 -0.14846400356669393; 0.071817119653274 0.22437791825762998 -0.07122959655024572; 0.13041124580222435 0.06170186846147662 0.07643106717746549] %
+
+Mass Used: 164.99717481289736 kg
+Launch C3: 98.14093581427285 km²/s²
+||V∞_in||: 4.977972863689268e-6 km/s
diff --git a/archive/ES_0.6322660599004979 b/archive/ES_0.6322660599004979
new file mode 100644
index 0000000..7e69447
--- /dev/null
+++ b/archive/ES_0.6322660599004979
@@ -0,0 +1,22 @@
+archive/ES_0.6322660599004979---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:39:45.618
+Launch V∞: [7.254509691341085, -7.488840562880133, -2.3580828811518644] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009723330647125673, -0.004810262110231404, 0.004681944071977159] km/s
+ V∞_out: [0.0017703449505209717, 0.002670106673558104, -0.0059783384399827045] km/s
+ time of flight: 1.0665946578842653e8 seconds
+ arrival date: 2027-09-24T07:17:30.618
+ thrust profile: [0.37536797022609597 -0.1794282132273924 -0.20430845661803707; 0.1922027552834289 -0.004272944156360478 -0.20332013898161339; 0.11993714374312114 0.021398373633288822 -0.18993159042665203; 0.07601086392276903 0.022461468244838936 -0.15798053731908454; 0.0473972171063043 0.01772018305231552 -0.12177891562788072; 0.0348294372794846 0.015224051777573949 -0.10794180378727627; 0.030148065653835515 0.014172715192055837 -0.09299954005864344; 0.018533794619811948 0.00921667428266149 -0.0724265954405679; 0.004612543522422386 0.002055670496137968 -0.01809415059743144; 0.005542693850817407 0.0027000656449729923 -0.02251390821559058; 0.005466358115354596 -0.0010026529879113692 -0.008280073633770015; 0.0009935380433825438 0.0010970619849964194 -0.008424177927394378; -0.0008749654976695411 -0.001047995275107362 -0.0037670935192688614; 0.0015702450287115731 0.005349962940427241 -0.008248613923063565; 0.0009393336459893165 0.0022545503418358497 -0.003565486969438293; -0.003005436168668535 0.0010351394585418402 -0.0003526373654848232; 0.0019685776802812246 0.0029047029217781793 -0.0027973545504874253; 0.0015227628816562176 -0.0025528726353555627 0.003152829826178311; 0.0002727175779996721 0.009724549902763654 -0.00755132634610829; 0.00045878582092410513 -0.0022001020873922946 0.0030282241821260668] %
+
+Mass Used: 71.06174406168566 kg
+Launch C3: 114.27119871238203 km²/s²
+||V∞_in||: 0.00678267303140755 km/s
diff --git a/archive/ES_0.6323660859645353 b/archive/ES_0.6323660859645353
new file mode 100644
index 0000000..c48e131
--- /dev/null
+++ b/archive/ES_0.6323660859645353
@@ -0,0 +1,22 @@
+archive/ES_0.6323660859645353---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T06:06:55.672
+Launch V∞: [5.428777295635992, -8.63433740885306, -2.0354044213827263] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.915840459079783e-5, 9.838133448777907e-6, -9.763921129437645e-6] km/s
+ V∞_out: [-3.162207398223452e-5, -3.2740195018376924e-5, -2.3537583349863486e-5] km/s
+ time of flight: 1.0622899927425869e8 seconds
+ arrival date: 2026-09-03T18:10:14.672
+ thrust profile: [0.8333743399556065 -0.6252515848665894 -0.4656654053990616; 0.33234581463537316 -0.0734223779319033 -0.33144542259183196; 0.13823751877850682 -0.0011233900839936767 -0.2032659715376126; 0.13030760726326296 0.014244570510876587 -0.23702860717166258; 0.04872796083201726 0.008897608606901811 -0.10736697911910557; 0.03149799643287016 0.0071139755872436415 -0.07714260912053336; 0.0253960149841122 0.007115334808249497 -0.06949854271963204; 0.01982226642326839 0.006085134735392963 -0.05853371527318575; 0.0013554625466232764 -0.0003586865833393831 0.0006247764592780558; -0.0009609707715594207 -0.0003615652488133268 -0.001614196172902163; 0.0004053797699357226 -0.00040216526947146707 -0.0007899195170559506; 0.000802833023965012 0.0009364772543747914 -0.002620512794072368; 0.0022044095705418282 -0.0027002328211821643 -0.0033624007458160597; 0.0002630394422776282 0.0011434200066028463 -0.002786278515575517; -0.0014182012152468473 -0.0003010747552525555 -0.010939547988884964; 0.0013491874406124996 0.0009348481207715033 -0.0020233582449547755; -0.000622626612388189 0.00102348348942637 -0.0017638091698732442; -0.0027122341774007365 -0.0037589614770834412 -0.008510212883989395; -0.0015202843915566905 -0.004177597829823361 0.0036063384634263057; 0.005544899855727037 -0.0030781489525088628 -0.0029958913038565663] %
+
+Mass Used: 106.79048694294443 kg
+Launch C3: 108.16627657411657 km²/s²
+||V∞_in||: 5.1075158027072366e-5 km/s
diff --git a/archive/ES_0.6324162877990706 b/archive/ES_0.6324162877990706
new file mode 100644
index 0000000..6e8518a
--- /dev/null
+++ b/archive/ES_0.6324162877990706
@@ -0,0 +1,22 @@
+archive/ES_0.6324162877990706---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T05:22:58.233
+Launch V∞: [7.312246648839169, -7.4136129054055955, -2.5253591018764068] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0018222865428430374, 0.010971504532545702, 0.0019456301176361576] km/s
+ V∞_out: [0.010766683497402278, -0.0021410807206837692, 0.0026569789884308254] km/s
+ time of flight: 1.0706002626014237e8 seconds
+ arrival date: 2027-09-28T08:16:44.233
+ thrust profile: [0.33663366854266635 -0.164163681356587 -0.1970676363895755; 0.19988342543785342 -0.005761273496826785 -0.22410428026883222; 0.12676409246486217 0.021745490851633888 -0.21279326807095603; 0.08048109147343285 0.02318227376252293 -0.17716198918204387; 0.04511241185678885 0.016481650513617954 -0.11997105896543105; 0.02313801605947938 0.009644775320212455 -0.0687635448016773; 0.011713610956034085 0.005346469940755378 -0.038305971971995006; 0.012165280345660391 0.005884070400557659 -0.04381801350924671; 0.0082021772251565 0.004127148452869554 -0.03081671109734316; 0.005260869384825703 -0.003438270885498801 -0.021070422774784298; 0.0009500036230104488 -0.00020190253146891977 -0.008637831274784777; 0.0015474551091267438 0.0018635022862602787 -0.013049645012667891; 0.0010642949878057104 0.0014152616245998028 -0.002495885836119316; 0.0003860512703267884 8.920835680013752e-5 -0.002080690244890041; 0.005742221284406289 0.001315152183384891 0.0013567973367030898; 0.010125142827623614 0.0017421748292343758 0.003964814670351301; 0.005248099872162074 0.0031790286449649187 -0.016480692992184017; 0.0044013299859229655 -0.001493392066247851 0.00017621237274792543; -0.0019525836485056042 0.0030258776189037006 0.009946317280821761; 0.00445464121916004 0.00795661033089101 -0.0029190452584980844] %
+
+Mass Used: 68.10540101008019 kg
+Launch C3: 114.80804595808607 km²/s²
+||V∞_in||: 0.011290709300418224 km/s
diff --git a/archive/ES_0.6324944474078025 b/archive/ES_0.6324944474078025
new file mode 100644
index 0000000..aeb96b6
--- /dev/null
+++ b/archive/ES_0.6324944474078025
@@ -0,0 +1,22 @@
+archive/ES_0.6324944474078025---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T22:18:32.474
+Launch V∞: [5.526322295608212, -8.719081888015847, -2.3429994348612415] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9402700713139044e-5, -1.3272851683426974e-5, 2.751109645643111e-5] km/s
+ V∞_out: [2.712446729660201e-5, 2.05356893515558e-5, 1.2352741366180788e-5] km/s
+ time of flight: 1.0613978884712046e8 seconds
+ arrival date: 2026-09-03T09:35:00.474
+ thrust profile: [0.5626868207562169 -0.4399447730470047 -0.34556362861566997; 0.3117398094450546 -0.07391517992171232 -0.32106659370820606; 0.15754472555844976 -0.0043943719450520195 -0.2301100945029662; 0.07251662937047645 0.006862583902061065 -0.13764484674814367; 0.04308060801152732 0.007538187148553454 -0.09777064082030049; 0.014630274410070546 0.0035113528895942842 -0.039102638605251754; 0.03288796078451618 0.00856813054475386 -0.0931306984749149; 0.004849554493889532 0.0014812083297312372 -0.015593098352459648; 0.006374957661593008 0.002295370819870497 -0.02348122659674098; 0.000773796105451245 0.0003028006891357248 -0.002887438700721199; 0.0014484156264527152 -0.0003022274886862479 -0.0021764023803382514; 0.0007115433849417908 0.0003130675749683801 -0.003453169020587515; 0.0004592298134796066 1.717452985743593e-5 -0.0019019622327741481; -0.00033451098697444346 0.0008962985020095755 -0.002656162262110366; 0.0022277593201588085 0.00035241749175051514 -0.0002954195600766937; 0.0003125225964823649 0.00012243910656434024 -0.0010162051124211462; 0.0007149322856966846 0.0006283547717434665 -0.0010401533542572423; -0.00048571029777142154 0.00039369729274421486 0.00032717271659293617; 5.934526472811067e-8 -0.00019910326058562476 0.0019215459532977274; -0.0011689422813679015 -0.0008488087317165965 0.0013038328718899856] %
+
+Mass Used: 84.27192692880499 kg
+Launch C3: 112.0522734366225 km²/s²
+||V∞_in||: 3.618692878663445e-5 km/s
diff --git a/archive/ES_0.6325403242910328 b/archive/ES_0.6325403242910328
new file mode 100644
index 0000000..5e6f1ea
--- /dev/null
+++ b/archive/ES_0.6325403242910328
@@ -0,0 +1,22 @@
+archive/ES_0.6325403242910328---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-23T12:37:14.074
+Launch V∞: [7.534415435995283, -5.595987423969257, -0.24960695010765369] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.249508758293161e-6, -0.00022015753414689722, -3.717357400224341e-6] km/s
+ V∞_out: [-0.0002128525796922433, 3.1035668768921484e-5, -4.764222558718151e-5] km/s
+ time of flight: 1.8749577782152024e8 seconds
+ arrival date: 2030-04-02T14:46:51.074
+ thrust profile: [0.9494211326996405 -0.04703840784347308 -0.10142663694701343; 0.6080998197164034 0.4192778686133571 -0.22466739594819643; 0.30852676186228434 0.3871613539195524 -0.21547983899422063; 0.14246850127420033 0.26536110615812625 -0.1612425994958122; 0.0545834101339623 0.14223379945641929 -0.09568821517551641; 0.023732620322848213 0.08418876885875397 -0.06147821608318318; 0.011856720188887945 0.05735418457427138 -0.04463371097492701; 0.0020108593662753415 0.01322647534960976 -0.011413361757990265; 0.00019200308200345123 0.0020534719570772107 -0.001723137413097313; -9.406498139018764e-6 -0.00012172165493775652 1.4281579170095612e-5; 5.879259066796433e-5 0.00022763487146242132 0.0004733959742870033; 0.0001933249903598083 -4.0013158572481546e-5 0.00015934757463106583; -9.299088390215683e-5 0.0006719659905682982 0.00024545117927306497; 1.7848932697456397e-5 -9.041229711043291e-5 -0.0006530097036888857; 0.0009402216044188088 0.0004235788478184052 0.0006684012573471951; 0.0001278991967094344 -5.903595768528189e-5 -0.0001847990472595579; -1.739165547895399e-5 -0.0010681371391068045 -0.0010542615168518796; -0.00011667298181183863 -0.0007244628488702855 3.4966197991606e-5; -0.00040931924775967167 -0.00020904353341806196 -7.380805987628183e-5; 0.0001553042331102952 8.705278659320561e-7 0.0006604764235104198] %
+
+Mass Used: 223.7857417674577 kg
+Launch C3: 88.14479484092811 km²/s²
+||V∞_in||: 0.00022021289220854767 km/s
diff --git a/archive/ES_0.6325888402572792 b/archive/ES_0.6325888402572792
new file mode 100644
index 0000000..f9aefe1
--- /dev/null
+++ b/archive/ES_0.6325888402572792
@@ -0,0 +1,22 @@
+archive/ES_0.6325888402572792---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T12:51:14.684
+Launch V∞: [7.230560603189056, -7.44677180072072, -2.2635334871986115] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007035671435872749, 0.03878005518955752, 0.040025097187009785] km/s
+ V∞_out: [0.048811671172869914, 0.005967834326271318, -0.02714912791310266] km/s
+ time of flight: 1.0563502708435306e8 seconds
+ arrival date: 2027-09-12T03:55:01.684
+ thrust profile: [0.545421683262815 -0.2636280727636558 -0.30349787652270055; 0.26827448471964127 -0.008878306860286598 -0.2901071449836555; 0.09324193032954133 0.015134410233176 -0.15614219700434973; 0.07084426366043602 0.019275302060209887 -0.15340952130879795; 0.044823545579268965 0.01619768150249544 -0.12176627076580931; 0.029986653755064655 0.011012812093430312 -0.08808282692287656; 0.030689580529322195 0.012952814828018105 -0.10091485399353659; 0.01837433281948747 0.00812099105479098 -0.06716650895677352; 0.00982614633145898 0.004786920405638673 -0.03927181525075287; 0.0039007510331453194 0.0015240448812389037 -0.017053848478766426; 0.0015401415985165764 0.0006384298016597111 -0.0057256598398216; 0.00024745260714834685 7.669322731367089e-5 -0.0005357301453262022; 2.1704085114539217e-5 -1.1600224858918583e-5 -7.162299418526306e-5; 0.00012522481782359414 -0.00019753189606069518 -0.00011402986799476545; 5.094804552220486e-5 -0.00026885330958854626 -0.00022271673071280534; -0.00036791750930843174 0.00014892362934551943 -0.00036381923204302643; -0.00041898296519330325 0.0003192467300064132 0.0005704328497074808; 2.9108106539445844e-5 -3.590231226592328e-5 -3.823613493136776e-5; 0.00028008522279371464 -3.371358079455081e-5 -0.00041633815327106943; -4.949361125943953e-5 0.0002556614008888485 -0.0004976245727630058] %
+
+Mass Used: 79.67614267309273 kg
+Launch C3: 112.85900073606851 km²/s²
+||V∞_in||: 0.056172962872615695 km/s
diff --git a/archive/ES_0.6326074515472915 b/archive/ES_0.6326074515472915
new file mode 100644
index 0000000..5e144d3
--- /dev/null
+++ b/archive/ES_0.6326074515472915
@@ -0,0 +1,22 @@
+archive/ES_0.6326074515472915---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-19T15:26:50.513
+Launch V∞: [6.053942663871926, -7.75787335082349, -0.8954090939646077] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2413327141582066e-6, -1.1187380207605594e-6, -1.8892705885870113e-6] km/s
+ V∞_out: [3.07942187865685e-6, -4.0137174789414755e-7, 4.337256611566162e-7] km/s
+ time of flight: 1.5649929630528867e8 seconds
+ arrival date: 2028-04-03T23:28:26.513
+ thrust profile: [0.31230009181042034 -0.14507517071179873 -0.1109127587109778; 0.16196849831184132 0.01705892450356684 -0.15382049363140668; 0.14649389947083885 0.05293273632884719 -0.20666903523953556; 0.13138526510449794 0.07100102555939396 -0.23947598350037194; 0.0884227168328481 0.05934787328281121 -0.20932335522131476; 0.032979047243451326 0.029498351395003945 -0.12183204854364776; 0.04685742838293943 0.060405621719852844 -0.13141210555658014; 0.021864074857883355 0.025525770864891592 -0.0778567553430435; 0.005739844543822382 0.011758496199014229 -0.020973220698547144; -0.005508268134433815 0.0022351875424058195 -0.002740632154001145; -0.008935564560123305 -0.03415586922936796 -0.003952409783786866; -0.004402660116607509 0.004436517438223065 0.024943014364053176; -0.011708072683526468 -0.02091574568506933 0.03634120772621851; 0.045516700194362235 0.05400180480869916 -0.003574012745101591; 0.009721950626811679 0.01616763771379539 -0.0473574351433496; 0.0072828665988345495 -0.003629292688263702 -0.03303709866673264; 0.04136207370066108 -0.038467322042712915 0.0010364520286586507; -0.03621757351235165 -0.17974900981628383 -0.13271610996248823; 0.04725612706285136 0.24128764125152674 0.013090112274600423; 0.06896550425790643 0.13859946481962915 0.005749343196023094] %
+
+Mass Used: 168.4953209277205 kg
+Launch C3: 97.6365781504205 km²/s²
+||V∞_in||: 3.1375930984675114e-6 km/s
diff --git a/archive/ES_0.6327562355263814 b/archive/ES_0.6327562355263814
new file mode 100644
index 0000000..f223272
--- /dev/null
+++ b/archive/ES_0.6327562355263814
@@ -0,0 +1,22 @@
+archive/ES_0.6327562355263814---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T03:03:01.023
+Launch V∞: [7.259428000337056, -7.507704715214684, -2.438014023259103] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00965445786501474, -0.02748206320066816, -0.034810503291773265] km/s
+ V∞_out: [-0.04043161466743907, -0.006614589021113873, 0.019532951944753792] km/s
+ time of flight: 1.0586242423144367e8 seconds
+ arrival date: 2027-09-15T09:16:45.023
+ thrust profile: [0.39302656995392105 -0.19178258437087298 -0.22490749971107524; 0.2159447299837044 -0.00865487395091492 -0.24324471497038938; 0.10260937603121852 0.016264891057378522 -0.1774718402751811; 0.07738120324009383 0.02097483247519083 -0.17606840147060962; 0.038689288993235094 0.013323003153074291 -0.10672048984711922; 0.042900501949092174 0.016690523487786837 -0.1295006809591917; 0.01818250721615795 0.007716535404286388 -0.06690057054687447; 0.0036767552887633295 0.0015388188099567613 -0.015636292009072985; 0.002216215911719568 0.000984108443762103 -0.010737537220924914; 0.0008526871683694698 8.692325597431448e-5 -0.006079488723073876; -0.0002456112513283958 0.0005705288191620871 -0.000788920745476253; -6.627484552023072e-5 -3.8500716251206946e-5 -0.0008171053880186383; -0.0010392573258244963 0.0003416468895733587 0.0006949031207873898; 0.004259399377774007 -0.00042378398777043544 0.0008487576541267009; 0.0008116184282705778 0.004035738504491743 0.0006184027714385689; -0.001603498172715265 0.002499945476652455 0.0021249502585603264; -0.0007797421866328691 -0.0003642455336294206 0.0033980333952804004; 0.00020442950972667634 0.0006051465900791713 -0.0019568318395277295; 0.0005439701835027431 0.001340356528326925 -0.0031960123835061277; -0.00047187800866056566 -0.001138206273386702 0.00141285884309275] %
+
+Mass Used: 67.33072351094688 kg
+Launch C3: 115.00883736054253 km²/s²
+||V∞_in||: 0.04538990519773555 km/s
diff --git a/archive/ES_0.632791587642847 b/archive/ES_0.632791587642847
new file mode 100644
index 0000000..b567a47
--- /dev/null
+++ b/archive/ES_0.632791587642847
@@ -0,0 +1,22 @@
+archive/ES_0.632791587642847---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T11:13:59.862
+Launch V∞: [5.4513331673617955, -8.800734681643041, -1.6659408896504662] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.029903802267665855, -0.01207739459954157, 0.02885751823464599] km/s
+ V∞_out: [0.020634434877164307, -0.03112683138327496, -0.02186237117202581] km/s
+ time of flight: 1.0670313095144995e8 seconds
+ arrival date: 2026-09-10T10:59:29.862
+ thrust profile: [0.501060758613414 -0.40668301782067934 -0.30595820673596336; 0.2809647021920911 -0.07535906653365937 -0.3079710787518376; 0.1868072236201683 -0.012378095162278871 -0.2927615173774346; 0.10486105025266092 0.003956541953017001 -0.21046612332406103; 0.07482476242180011 0.007903040518807228 -0.177600279662879; 0.05450311869042854 0.008086688474451164 -0.14686864517333506; 0.010013825649638052 0.0018063895541768108 -0.030445857131560082; 0.030773607539337573 0.0060981807723583074 -0.09617348313766678; 0.011801645092503829 0.0026722613228164927 -0.04060692140002576; 0.002144313350611365 0.00046596008856385115 -0.0076667634284976575; 0.0037665615886888926 0.0006723945422247095 -0.014338127890110084; 0.0003862084822488446 -0.0009489110416123947 -0.0010664406265904116; 0.0006877595572291976 9.710536166975456e-5 -0.0008157475529621856; -5.8554444240294394e-5 -0.000160999830027561 0.0001675761117631248; -0.00013043756170634605 -4.467799277196985e-5 -0.0005872407604124005; -0.0006842197675999235 0.0011077847841925352 0.0004396515379399607; -0.0003232580795736966 -8.753404827218565e-5 0.0010082573121545468; -0.001334236964299324 -0.001307798682032916 -0.0003474330500336992; -0.00024815530708625943 0.0005851632875226085 0.00036156723350763025; 0.0007556265739197206 -0.0025639279114446256 -0.002547238884235166] %
+
+Mass Used: 96.90913308128847 kg
+Launch C3: 109.9453232860628 km²/s²
+||V∞_in||: 0.04327652029726534 km/s
diff --git a/archive/ES_0.6328661645365032 b/archive/ES_0.6328661645365032
new file mode 100644
index 0000000..e9459eb
--- /dev/null
+++ b/archive/ES_0.6328661645365032
@@ -0,0 +1,22 @@
+archive/ES_0.6328661645365032---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:28:42.105
+Launch V∞: [7.354060512895208, -7.519527206992605, -2.700995415962017] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013252018555110536, -0.008656424736066906, -0.027393186854617627] km/s
+ V∞_out: [-0.004673878831341399, -0.03126122440917847, -0.0013342161067151884] km/s
+ time of flight: 1.0639403439514014e8 seconds
+ arrival date: 2027-09-21T21:22:36.105
+ thrust profile: [0.2115535065034037 -0.11646964840036456 -0.12998628384036037; 0.13325463151770056 -0.013772741632900848 -0.16127862417878486; 0.08348736777641928 0.007388243431813513 -0.15720871277576015; 0.05657610101245888 0.011897340418476886 -0.14286964670115493; 0.0399546559575297 0.01214783044615247 -0.12456408000090237; 0.02681375771049051 0.01076945683139737 -0.09873915755085914; 0.01626982223777768 0.008054022497192897 -0.06767489504612846; 0.007187492708261608 0.003712309844018723 -0.03234270129111504; 0.00010821787093048688 0.002230889747206798 -0.005897007186088087; 0.001046940681377975 -0.0001880299046358526 -0.001648169399231589; 0.003082378766737367 -0.0009571467187672834 -0.0042430096486657035; 0.0016448988111685081 -0.0014043334213909844 -0.00180007090805535; -0.00038873199419531756 0.0004805066105257793 0.0019177864564382569; -0.0010550720138998103 0.0022988899379424196 -0.0021944871449392517; -0.0013127508875860516 -0.00043022027786452234 7.389535133576672e-5; 7.966776475691912e-5 -0.0001508617055439544 -0.0004065212172498058; 0.0002612924757902733 -2.883370390597108e-5 -0.002022986353586549; -0.001005250034910537 -0.001556934784558104 -0.006079515359215509; 0.0007702221712370884 -0.000548381672914998 -0.0007966497247758842; -0.00014435767991971183 -0.0002548573817775904 -0.004257669035193493] %
+
+Mass Used: 50.47210715298661 kg
+Launch C3: 117.92087168107437 km²/s²
+||V∞_in||: 0.031637578463722234 km/s
diff --git a/archive/ES_0.6330049493465023 b/archive/ES_0.6330049493465023
new file mode 100644
index 0000000..cc54ff8
--- /dev/null
+++ b/archive/ES_0.6330049493465023
@@ -0,0 +1,22 @@
+archive/ES_0.6330049493465023---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T17:51:20.298
+Launch V∞: [7.120291107272075, -7.537157983000937, -2.3855123394904214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8893178556961358e-5, -1.873925721496395e-5, 1.3432370652120098e-5] km/s
+ V∞_out: [2.354663282731437e-5, -1.3891167601503896e-5, -1.1881273835509808e-5] km/s
+ time of flight: 1.0595876962059294e8 seconds
+ arrival date: 2027-09-17T02:50:49.298
+ thrust profile: [0.6166710383397533 -0.3181249155626466 -0.36913455169939696; 0.20589474838150557 -0.015381110077016856 -0.23844401874864918; 0.10861379539637074 0.01202667832054365 -0.18874440849257362; 0.06925335710540373 0.014909129578820223 -0.1576018546564178; 0.05290467171387655 0.014844498234911175 -0.14534139880411384; 0.016572119631713247 0.005768204869784337 -0.05468516538728079; 0.003610426003490314 0.0032557118881573364 -0.018140583486587973; 0.0029320737465281963 0.0014687744665556062 -0.015217538423018767; 0.009479481344967605 0.004115016571882336 -0.03220580795254923; -0.0014751606392081154 -0.0014417656583568827 -0.0031138556385186555; -0.0018246012537714246 0.00036529732999362655 -0.0018091143974699932; -0.0003746889353357409 0.00015677626122551734 -0.0037762167810793295; 0.00682974376308649 -0.002216224921834741 -0.003503138107821041; -0.00995574255276966 0.0008115258485727858 -0.002767716539021636; 0.0009628342029411519 -0.0006150869372054902 -0.0029709114755090468; -0.0018452526340172937 1.4615648932291253e-5 0.003730749729506824; 0.005113570499887423 -0.001496782845394221 -0.0017813865924829132; -0.0015778164264966343 -0.015249020496139694 0.00630118887997206; 0.002193177715999056 0.0013704701457121003 0.004864606580404629; -0.0074973723998939135 -0.004681108577848243 -0.013680473388549953] %
+
+Mass Used: 78.18431153415668 kg
+Launch C3: 113.1979650348736 km²/s²
+||V∞_in||: 2.9808397110373786e-5 km/s
diff --git a/archive/ES_0.6332198331498278 b/archive/ES_0.6332198331498278
new file mode 100644
index 0000000..29ded38
--- /dev/null
+++ b/archive/ES_0.6332198331498278
@@ -0,0 +1,22 @@
+archive/ES_0.6332198331498278---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T04:47:57.673
+Launch V∞: [6.989773513389125, -7.467286711575349, -2.0520792849886287] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.05797354866029982, -0.0938913105425284, -0.03881199084389681] km/s
+ V∞_out: [-0.06490302028898814, 0.08412325369919549, -0.04893196657614107] km/s
+ time of flight: 1.0520031220374751e8 seconds
+ arrival date: 2027-09-07T19:06:29.673
+ thrust profile: [1.0 -0.5320022511476978 -0.505009565508255; 0.2805936854895637 -0.017305114435209375 -0.289727896717502; 0.08459836496071341 0.011739483187858054 -0.13975880262596305; 0.04777959119114993 0.011185781507170913 -0.10329297160595148; 0.06866019602357527 0.021338323542369232 -0.16909742623340046; 0.04622898560222173 0.015186668170631723 -0.134531318852816; 0.02576813964044178 0.009344287525220858 -0.08403221113378492; 0.006514475765790843 0.0022385205388078078 -0.024827944390551356; 0.009901112460992312 0.0029969575297645458 -0.035994810166489234; -0.000619290821953767 0.0018189164477951164 -0.006901049586466941; 0.003457012304307172 0.0012398811560879745 -0.015408542142057063; 0.004007488063212801 -0.002133358450208144 -0.02505209954514764; 0.00134676537615771 0.0015743401832339094 0.0002607435179962515; 0.004031117894477251 0.0008921318097573773 -0.007774692232720667; 0.0037973602709887944 -0.0013154009560750438 -0.0026287500049547137; -0.005212886714773835 0.002555068852922119 0.0007853755087013237; -0.000489559452623088 -0.0007251786059948645 -0.0008654734867967568; 0.0005537889886005438 -0.0002968255725019687 -0.000832045853214303; 0.005786332845963816 0.001958397281565215 -0.0011080283115375647; -0.000844508656158113 -0.001177624004454373 -0.0013146755754315112] %
+
+Mass Used: 103.92452371431773 kg
+Launch C3: 108.82833399322539 km²/s²
+||V∞_in||: 0.11697384824364969 km/s
diff --git a/archive/ES_0.6333703028543001 b/archive/ES_0.6333703028543001
new file mode 100644
index 0000000..1474b63
--- /dev/null
+++ b/archive/ES_0.6333703028543001
@@ -0,0 +1,22 @@
+archive/ES_0.6333703028543001---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T13:00:48.935
+Launch V∞: [5.4767536378169925, -8.792683884162205, -1.9861359718684055] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.021210141129387454, 0.021601046081028738, -0.0009284643896018895] km/s
+ V∞_out: [-0.004361472915115342, 0.00013295868849951974, 0.02996627025659328] km/s
+ time of flight: 1.067581017106811e8 seconds
+ arrival date: 2026-09-11T04:02:29.935
+ thrust profile: [0.5032627904877223 -0.39742086420024864 -0.2932565130530492; 0.28269298297996415 -0.0700876474067189 -0.2910388713134298; 0.13666117483463983 -0.006066064194248401 -0.21456576640205902; 0.054918359436161655 0.004256052923483656 -0.11114558734158846; 0.045919136770568185 0.0072307192520502 -0.10681535337446679; 0.04110842627713044 0.006261259648648777 -0.10620166739482857; 0.04845780554062178 0.010851715262466257 -0.14241193731751622; 0.039348719716630925 0.00963128082498659 -0.12449876847728114; 0.004133267845800079 0.0010277794630461526 -0.013063978198681851; 0.010997661396555926 0.0031989524330066875 -0.037903956305626776; 0.0013839833514436599 0.0015741414738027761 -0.0037606745327893494; 0.0011114809217431514 0.00023741699963135323 -0.003951119135539156; 0.00013931333233479376 -0.0005629696152832915 -0.0010734601108817092; 0.003971407700505367 -0.004184670672800757 -0.005921161478925676; -0.0006997711778741027 0.0027814203784219445 -0.0051795904362837274; 0.006905332078351479 -0.003508828964967046 -0.005444654330069994; 0.0054365828157140585 4.853436712091687e-5 -0.009428286704621569; -0.0021405941949097632 0.0005223895955526136 -0.003804586827865129; 0.003239917854091979 1.5821773408531252e-5 -0.0005338520663867663; -0.002526559056830237 -0.0013688431787561932 -0.00206620326695267] %
+
+Mass Used: 89.96869102645041 kg
+Launch C3: 111.25085639489708 km²/s²
+||V∞_in||: 0.03028757706793363 km/s
diff --git a/archive/ES_0.6334547009805539 b/archive/ES_0.6334547009805539
new file mode 100644
index 0000000..5c0f707
--- /dev/null
+++ b/archive/ES_0.6334547009805539
@@ -0,0 +1,22 @@
+archive/ES_0.6334547009805539---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-30T05:56:47.025
+Launch V∞: [7.087421455952692, -6.959678515253398, -1.4582969474247536] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03750680570003266, 0.09117898348528423, 0.12986824285725865] km/s
+ V∞_out: [0.14143906271239218, 0.024991369024521815, -0.07727468281089832] km/s
+ time of flight: 1.0886061359366253e8 seconds
+ arrival date: 2027-10-12T05:00:20.025
+ thrust profile: [1.0 -0.4703797704551281 -0.4209208055188933; 0.7144203640761607 0.03782343953420779 -0.5536703967466609; 0.40824088353326016 0.11934820538766965 -0.4722220556379494; 0.19188050966514772 0.08526670254819683 -0.29659561356621095; 0.03414633004642302 0.018866341531829634 -0.0660555682102824; 0.07751612385828277 0.04915968175259043 -0.1674564819121221; 0.031598107849976395 0.022015608480623488 -0.07727420403718628; 0.008102143960729525 0.006350824620986025 -0.022798931111059344; 0.0015359222605675713 0.0011063247656120506 -0.0045644063447962055; 0.002529373867851257 0.0021098693749406054 -0.007792712678510696; 0.00046276349379172576 4.228760820021969e-5 -0.0013764257433551916; 0.00022511663633794114 0.00014460511177022146 -0.0006878813889710296; 9.8805759929242e-5 0.0001510210377415537 -0.0004352399476582058; -0.00041150186683815176 -0.0005374280503156083 -0.00032507329098560876; 0.00034231075113314176 0.000453330177227272 -0.0007639774102398086; -0.0001163140788240055 0.00017617062847507395 1.4793171701681985e-6; -0.00014912031236034043 -0.00020491086089878443 -0.00021552151347224317; -0.00021105280285549187 0.0001655564443660454 0.00043923575415034423; 2.2300540838628765e-5 1.3669788325106915e-5 -0.00013081530243826047; 0.0005265156980748978 0.00047959078178706164 7.750362965124674e-5] %
+
+Mass Used: 151.0579132957073 kg
+Launch C3: 100.79529791684666 km²/s²
+||V∞_in||: 0.16305253143101353 km/s
diff --git a/archive/ES_0.6335079918754154 b/archive/ES_0.6335079918754154
new file mode 100644
index 0000000..468097b
--- /dev/null
+++ b/archive/ES_0.6335079918754154
@@ -0,0 +1,22 @@
+archive/ES_0.6335079918754154---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T21:08:30.595
+Launch V∞: [7.132647834417839, -7.373245533158434, -1.3259215261016577] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.2883281006052844, -1.4149901475682585, -2.1750571081514027] km/s
+ V∞_out: [1.2129466679406338, 0.4949951105328101, 2.2578766362199594] km/s
+ time of flight: 1.0688699645121855e8 seconds
+ arrival date: 2027-09-24T23:58:26.595
+ thrust profile: [0.6234540621626037 -0.29033528707821754 -0.3088416491063665; 0.3610629725581831 -0.005116969086252566 -0.3549015199505563; 0.22544708956211845 0.03806012956025826 -0.32677181888411305; 0.14938104373250713 0.04037919446776804 -0.2820224574390334; 0.08340682154461421 0.029887781935105707 -0.19368228485449018; 0.06933361476495772 0.027987219157441123 -0.1823477719635774; 0.044852887393539216 0.019976728186637243 -0.13118764266645797; 0.017453626579969163 0.008899456106101449 -0.05941114037823994; 0.009970555173230733 0.005522403628692495 -0.035513939044300294; 0.007613003963306716 0.0018589267761728713 -0.01086046597856137; 0.0005992694256132633 0.000516366191877917 -0.004484182111591885; 0.0005476499375639396 0.0019721034216098176 -0.0013463823143594032; 0.004310558798418728 -0.005526873988916628 -0.005765857872090994; -0.000648290576247699 0.002089330891994627 -0.004409958010400932; -0.002414364523524839 -0.0034809193792834925 -0.006034586516611433; -0.0038671061480868175 -0.002168309568818712 0.0015893920442305324; 0.004115735063563547 0.005552892829437914 -0.00584165894942967; 0.00011849671862263433 0.0007166925692485208 -0.0020447245691422207; -0.006327973571658532 0.0032396750094710906 -0.0015766920237090048; 0.002108806759786898 0.003642532727298954 -0.0024932451848094393] %
+
+Mass Used: 114.94067468121602 kg
+Launch C3: 106.99748271544604 km²/s²
+||V∞_in||: 2.6107860186223295 km/s
diff --git a/archive/ES_0.6337487801990389 b/archive/ES_0.6337487801990389
new file mode 100644
index 0000000..439fb79
--- /dev/null
+++ b/archive/ES_0.6337487801990389
@@ -0,0 +1,22 @@
+archive/ES_0.6337487801990389---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T00:50:26.454
+Launch V∞: [5.36537204206634, -8.584324490805406, -2.0624808306688913] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0055054329825454, -0.005644926223596039, 0.00021969890813364754] km/s
+ V∞_out: [0.0007746035313254165, -2.410111534549276e-5, -0.00784570321317704] km/s
+ time of flight: 1.067365814206218e8 seconds
+ arrival date: 2026-09-09T09:53:27.454
+ thrust profile: [0.8859544679227652 -0.694068817587398 -0.5231082676625776; 0.4182491057482207 -0.09680691255099876 -0.41629979615702295; 0.18359024050749664 -0.0035543369461226893 -0.26306699746197393; 0.08520871919753278 0.008373900097163505 -0.15920555055679453; 0.029150632902161733 0.004612369328936946 -0.06668660032330044; 0.011296754018251335 0.0023637165687850122 -0.027500237007848045; 0.015288118501807196 0.0034391664575986985 -0.04087898549578193; 0.019707040323968587 0.007315088733300061 -0.057835795119388106; 0.0017792675675464102 0.0011351405304468008 -0.008885640310916255; 0.011950455094153462 0.003907771330596094 -0.03756739030736791; 0.006932228034886112 -0.00303037488721028 -0.005903522637282716; 0.0013964760325734988 -0.0009009086340945284 -0.004776799335777973; 0.012275351284664024 -0.008768281387733525 0.0007747557344589037; 0.00011158560863678982 -0.0008994318124620254 -0.0016640495877796105; 0.015682327384742144 -0.018465192559398373 -0.002354909033239527; 0.02117565972157187 0.010730072718707632 -0.020442976765934363; 0.011766735059085208 0.011290598492949748 -0.0026160644302134434; 0.000676864125452463 0.0022873084174629705 -0.0016840529406634778; 0.021092704643349194 -0.011130531774756564 -0.029466715810884628; -0.0015364635519436367 -0.0006634494468258229 0.005059960137153723] %
+
+Mass Used: 116.77216103993123 kg
+Launch C3: 106.73167129010527 km²/s²
+||V∞_in||: 0.007888171651617128 km/s
diff --git a/archive/ES_0.6338269921837102 b/archive/ES_0.6338269921837102
new file mode 100644
index 0000000..bf0294a
--- /dev/null
+++ b/archive/ES_0.6338269921837102
@@ -0,0 +1,22 @@
+archive/ES_0.6338269921837102---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:57:19.717
+Launch V∞: [7.248326318033971, -7.459729069694531, -2.2606364949537676] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.17530984104327216, -0.8305643534514996, -1.273860286327728] km/s
+ V∞_out: [0.6314987562048364, 0.2943718702997945, 1.364876393005239] km/s
+ time of flight: 1.0545271435969651e8 seconds
+ arrival date: 2027-09-10T04:22:33.717
+ thrust profile: [0.5203745851712702 -0.2557206286525877 -0.2958503756611839; 0.23506593290060462 -0.011833220422766499 -0.2658298003796411; 0.10166978173598049 0.014123124038586378 -0.1733965714377028; 0.0708715158201908 0.01769442494302087 -0.1617335354117042; 0.07974637203925704 0.027520069950647173 -0.20093150007460855; 0.02024816920506466 0.007206027553820969 -0.06250686443269998; 0.02748105848868385 0.011109426621624206 -0.09787815058707333; 0.007406923852975509 0.00279772214794747 -0.02716634096368752; 0.00456527240219435 0.0016816841789717043 -0.017809439604352675; 0.002280091910252864 0.0018061051192637032 -0.0010209433624435616; 0.00033967557785798 0.002142820834409711 -0.00504826664432331; -0.0007458232906885822 0.001418338172152122 -0.004887973602494348; -0.0008607621843056395 -0.00036186958350947047 -0.005829672843634616; -6.492996497777209e-5 0.0010655830754425766 -0.0021391107558212333; -0.0007116996090645201 -0.0006510353997444555 -0.0005503855665334781; 0.001118007882117065 -0.0007338171310359342 -0.004221708049026752; 0.007314467497462172 -0.000859577506812167 -0.004182129569753843; 0.001495400588748733 0.005118105107260569 -0.0008135640845934838; 0.0014268471138888408 0.002976858912844006 0.0052490697827287415; -0.0028826098950148174 -0.004718633516061259 0.00014380748906250808] %
+
+Mass Used: 78.56991839944112 kg
+Launch C3: 113.29626956826641 km²/s²
+||V∞_in||: 1.530781079930728 km/s
diff --git a/archive/ES_0.634118461501755 b/archive/ES_0.634118461501755
new file mode 100644
index 0000000..187b809
--- /dev/null
+++ b/archive/ES_0.634118461501755
@@ -0,0 +1,22 @@
+archive/ES_0.634118461501755---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T07:35:30.750
+Launch V∞: [5.494194230755124, -8.842572873673227, -2.30701908687604] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.043076075718950085, -0.017339937305334955, 0.04028609045031246] km/s
+ V∞_out: [0.028594031061308138, -0.043978512074944555, -0.03204976188256267] km/s
+ time of flight: 1.0528977262872636e8 seconds
+ arrival date: 2026-08-25T22:45:02.750
+ thrust profile: [0.5220203457754143 -0.4208037883311607 -0.34400812291418903; 0.22971646009886645 -0.05985872719184791 -0.25642564161693543; 0.13062011837157234 -0.00796920960739637 -0.20817100317852597; 0.07389805920916148 0.0035921621862474323 -0.1516001181527812; 0.04496327005824893 0.0056114437637947625 -0.10964198858900642; 0.03426175174543718 0.005792691449137582 -0.09498335771401863; 0.009284246270390121 0.0021719072391465934 -0.02959430060109461; 0.006904944012983864 0.0017130045265130386 -0.02385511753903347; 0.003939338893625163 0.0010896051477291319 -0.014399375605295138; 0.0008922677817656971 -0.000555356398262751 -0.002615929534585318; 0.000650425168693159 0.00026993126669898034 -0.002146521624755484; 0.00020358674790321805 -0.000804600020157465 -0.004266294196778931; 0.00024089493527202109 0.000282497911224744 -0.000394571010635419; 5.137820728883186e-5 0.0002691486911329098 -0.00017801620328090212; -0.0007066696181221949 0.00024622696288379423 -0.00020305187690377018; 0.0007052180413603247 5.387955736581681e-7 -0.00041367277623415824; -0.0005655196687893887 -0.0004823344639786286 0.0012928744389092894; 0.00010466640753597947 0.0001107964149284896 -0.0005515662910689898; 0.00016664775400209944 -0.0016991214079524 0.0006939219129878571; 0.0005730161527356867 -0.0005315609104894425 -0.0017205977173636708] %
+
+Mass Used: 76.55719144299428 kg
+Launch C3: 113.69960233869483 km²/s²
+||V∞_in||: 0.06147512349616245 km/s
diff --git a/archive/ES_0.6341882785404324 b/archive/ES_0.6341882785404324
new file mode 100644
index 0000000..a38b969
--- /dev/null
+++ b/archive/ES_0.6341882785404324
@@ -0,0 +1,22 @@
+archive/ES_0.6341882785404324---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T05:30:35.393
+Launch V∞: [5.418402944068042, -8.753341389805712, -1.771664425020414] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007845255753479247, -0.0008622779006941842, 0.0008331179727012417] km/s
+ V∞_out: [0.0008555649722149283, 0.0009040920978367148, 0.0007078749024635501] km/s
+ time of flight: 1.0645507731942804e8 seconds
+ arrival date: 2026-09-07T08:21:52.393
+ thrust profile: [0.6542247516868688 -0.5137710361309074 -0.3840726161224459; 0.26894467999105437 -0.06651002346073931 -0.2847175266633837; 0.16193940614087768 -0.0074201802858737485 -0.24657892706287662; 0.11902988839331456 0.007929184170409755 -0.22968064723196; 0.0827400583730536 0.012251640042193666 -0.190435704225508; 0.03689492739764308 0.007607192488984478 -0.0977918910937545; 0.01653834598336052 0.004987784206629023 -0.04868129163705679; 0.005242813654728597 0.0019961842492301164 -0.013949274805925825; 0.023170181565264167 0.006286616155008433 -0.07924954221447876; -0.00018600888868071288 -0.000647095842585944 -0.020612927672701058; 0.0028132720189929816 0.005309560315841967 -0.010792461133807177; 0.0029567172739333866 0.0006951752613467314 -0.006284684500532945; 0.004207814850379025 -0.0004191273359810035 -0.0067583538238759604; 0.004887899108973645 0.0020543164855594807 -0.007621772148067043; -0.002179368103105191 -0.0007161022643793302 0.0021321003108522255; 0.0017125903119495143 0.002264873087608303 -0.007220916658723316; -0.005064067432031354 -0.00344559864007388 -0.005481511814894931; 0.009133050751372544 0.006544577208679039 0.009095477414899928; -0.006546677603384512 -0.005293758145846409 -0.0040830723649632385; 0.005101300359872751 0.00678614683242924 0.0005189805099396834] %
+
+Mass Used: 103.35957871418987 kg
+Launch C3: 109.11887078565393 km²/s²
+||V∞_in||: 0.0014328604652367196 km/s
diff --git a/archive/ES_0.6341884403203293 b/archive/ES_0.6341884403203293
new file mode 100644
index 0000000..65b4810
--- /dev/null
+++ b/archive/ES_0.6341884403203293
@@ -0,0 +1,22 @@
+archive/ES_0.6341884403203293---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:50:31.313
+Launch V∞: [7.121282616491872, -7.481930690332086, -1.9791250169992214] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0063460138045520415, -0.017334958200818276, -0.022406336892354873] km/s
+ V∞_out: [-0.025715727592088237, -0.0039628895556821, 0.012872244411784766] km/s
+ time of flight: 1.0560426588704142e8 seconds
+ arrival date: 2027-09-12T01:21:36.313
+ thrust profile: [0.6870308373612164 -0.3409405846579187 -0.3530217401496541; 0.2593448223382976 -0.012224695923368622 -0.26459246453279767; 0.12713652195527714 0.01955067878762697 -0.20167214192079336; 0.0957668564017814 0.02511193156753083 -0.19692525360447988; 0.05895610912633805 0.023035365277476957 -0.15889280417053; 0.04056579096817745 0.016010148754339433 -0.1195350443096978; 0.03736914525608302 0.019308356465873616 -0.1246532485907526; 0.007066725312854221 0.0031089329748873284 -0.024050010682887788; 0.012341809761343837 0.006323629905563094 -0.04793310320768081; 0.0008089076914451999 -0.0015990452770909512 -0.003548037197678935; 0.004200246843808231 0.0028192914661205 -0.01760713712120856; 0.000601055196865113 0.0022598883815595455 0.0021278752895221046; 0.005300293599737653 -0.006270709785639799 -0.0003273919155163524; -0.00027908573326269654 -0.007051177674488824 0.003366916936304578; -0.0033618090748136044 0.005089372250016519 0.0009421817313714506; 5.5014762534991203e-5 -0.0012655476865718945 -0.002522117616379733; -6.912662580588972e-5 -0.007914815689632934 0.002048717925135281; -0.0009561250766342738 4.302364022788134e-5 -0.00010350396904490944; -0.0004930379991885548 0.003361530586965213 -0.003198237949141057; -0.0032510752186862574 -0.006553573704712583 0.0008686001678032574] %
+
+Mass Used: 94.66799575491541 kg
+Launch C3: 110.60888879179466 km²/s²
+||V∞_in||: 0.029031303793756576 km/s
diff --git a/archive/ES_0.6343539548119961 b/archive/ES_0.6343539548119961
new file mode 100644
index 0000000..8226e6f
--- /dev/null
+++ b/archive/ES_0.6343539548119961
@@ -0,0 +1,22 @@
+archive/ES_0.6343539548119961---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-21T14:45:25.277
+Launch V∞: [7.473211938294323, -5.685438185128409, -0.32406262021073373] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.769996985674197e-10, -5.4705918706626785e-9, -4.143214439696908e-9] km/s
+ V∞_out: [-1.5266667452511553e-9, 1.5127194755349298e-9, 1.2484231321208659e-9] km/s
+ time of flight: 1.8101255168232054e8 seconds
+ arrival date: 2030-01-15T16:01:16.277
+ thrust profile: [1.0 -0.10264633793817766 -0.12740764769992335; 0.6918965496933761 0.42470739092159443 -0.28653552145914535; 0.3593069207599869 0.4013518705213481 -0.2732146366805213; 0.15835522823664178 0.2550446440473887 -0.18804281990285315; 0.08503004474900652 0.18276346107708907 -0.14498545889435094; 0.006505927211677154 0.018068558379632862 -0.01714579395361096; 0.0012468862247601252 0.004280923514716375 -0.004121702395254169; 0.00036588365392897223 0.0015539328071533525 -0.0016011069877575885; 0.0001278365905605107 0.0006757683197418397 -0.0006903282252369992; 0.0005820306084223725 0.000910363737282687 -0.0005965637824065265; 1.722670133222305e-6 0.0008748576558242809 -0.0011467404601399256; 5.0422382627007145e-5 0.0005546543301036709 -0.0006060530305168968; 0.00014701767567332598 9.523608962610478e-5 -3.063881264012944e-5; 0.00014506836424228161 0.0006549028737236953 -8.1035871039502e-5; -8.925899952378285e-5 0.000396883953839062 -0.00048676249230035474; -1.597810726424939e-5 -8.080612839739883e-5 0.00012655964777649758; -0.0002792463833492289 0.00015548816574584284 -1.913883537920047e-5; 0.0005898169927245843 -0.0006964523317549166 -0.00020975820394034025; 6.466602016552949e-5 0.000518554282547793 -0.0003908409958206972; -0.0002235136903379966 0.00042771184996658203 1.417471725169157e-6] %
+
+Mass Used: 225.1239103691687 kg
+Launch C3: 88.27812061339885 km²/s²
+||V∞_in||: 6.931675823325437e-9 km/s
diff --git a/archive/ES_0.6345647544318233 b/archive/ES_0.6345647544318233
new file mode 100644
index 0000000..470ab7a
--- /dev/null
+++ b/archive/ES_0.6345647544318233
@@ -0,0 +1,22 @@
+archive/ES_0.6345647544318233---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T02:59:53.097
+Launch V∞: [7.039092442910931, -7.490382761186807, -1.9131538185504577] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0038880098306207766, -0.003634421857456162, 0.0025348497881336647] km/s
+ V∞_out: [0.002508485827801893, -0.005279383165997705, 0.0007647310104315949] km/s
+ time of flight: 1.1252218985004854e8 seconds
+ arrival date: 2027-12-01T11:09:42.097
+ thrust profile: [0.4025089331493394 -0.1975853491670476 -0.22944880322837338; 0.2002751591960826 -0.007598669077277881 -0.23238570934007172; 0.1313444522633056 0.01988867848735571 -0.2318072443985522; 0.09531827447722317 0.024525795619431585 -0.2213615080322209; 0.05616758138438103 0.018902631236374905 -0.15770434378930726; 0.02167911366705689 0.008320985051415108 -0.06780240475557305; 0.01866869973446077 0.008658879389807101 -0.060078937941149484; 0.00827195671301851 0.0027479865915509003 -0.02819939317612383; 0.007272934697692825 0.007724436050965625 -0.032083257533267504; 0.0034789702201984355 -0.00011750538645352582 -0.01674491430287186; 0.0017775800051237425 0.004797881044626931 -0.015609456305269238; 0.01674970498219288 -0.0005299487605108085 -0.04486079039337943; 0.005606362925433964 -0.014644474114879843 0.009242248865579993; -0.02610595305993348 -0.007393809525347939 -0.06276103491628057; 0.04856923940655544 0.0016731991469049988 -0.04271553347585663; -0.032607700486297304 -0.01171893333126964 -0.08016934386027194; -0.057901092484806856 0.03264733279033342 -0.0785363170630976; 0.01380738494651065 0.007261772941647497 -0.013304846803071969; 0.004866733569346289 0.020212175358483513 -0.08110320243095184; -0.011400114326867966 -0.010941315960805015 0.07542067954111921] %
+
+Mass Used: 102.65579930666763 kg
+Launch C3: 109.31481386236449 km²/s²
+||V∞_in||: 0.005895006881197017 km/s
diff --git a/archive/ES_0.634643844228394 b/archive/ES_0.634643844228394
new file mode 100644
index 0000000..e5a3121
--- /dev/null
+++ b/archive/ES_0.634643844228394
@@ -0,0 +1,22 @@
+archive/ES_0.634643844228394---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T20:35:33.853
+Launch V∞: [7.293330383864582, -7.505364128658179, -2.1662223827231823] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.010494951235682896, -0.008289342031037114, -0.025682784289963134] km/s
+ V∞_out: [-0.004370494728353856, -0.02858961774108348, -0.001283510916522157] km/s
+ time of flight: 1.0543768987167813e8 seconds
+ arrival date: 2027-09-10T04:50:22.853
+ thrust profile: [0.3878875558309441 -0.18829495406032673 -0.2178893293912202; 0.193900926135419 -0.009602197680064602 -0.2094977945112471; 0.10195487656899746 0.01599206979801368 -0.1667924919241261; 0.0930953993045587 0.025270994113003906 -0.19633534785217094; 0.050970943956608686 0.017362465327600246 -0.13075696435956058; 0.052696247932355875 0.02150071886698906 -0.15373283058558362; 0.0668699972370065 0.027924501958202258 -0.1989222052207457; 0.004087485553544651 0.0019071812679320396 -0.015247525092041482; 0.0032406311602094905 0.0014148917371595905 -0.012690748477940841; 0.0010382388902037824 0.0005019921436087147 -0.004056331586223157; 0.0007216918684726434 0.00038500266958996286 -0.0022460468130047983; 0.0013267082709048578 0.0021819222721459835 -0.004880535259532993; -0.00013343747338940594 0.0004875800208952812 -0.0036463387457185076; 0.0002310240312337591 0.0007374385471289905 -0.0015091416932251794; -0.0005877879025756792 0.00014801070625346284 -0.00020277981721809413; 0.000565981851244637 0.00035474773602585104 -0.0019022036762713626; -0.003316983538461289 -0.0017031783946951297 -0.0018744674741092912; 0.0015652465660522972 -0.0030425520004445285 -0.002716607194873524; -0.001848442091453934 -0.0015523163742988326 -0.0010796098274515427; 0.005142250014238023 -0.00021068156893524047 0.0012390068874555467] %
+
+Mass Used: 74.15969541351387 kg
+Launch C3: 114.21567820336213 km²/s²
+||V∞_in||: 0.028956218703961634 km/s
diff --git a/archive/ES_0.6348301584249437 b/archive/ES_0.6348301584249437
new file mode 100644
index 0000000..f7a114a
--- /dev/null
+++ b/archive/ES_0.6348301584249437
@@ -0,0 +1,22 @@
+archive/ES_0.6348301584249437---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-02T21:29:24.486
+Launch V∞: [7.175175700701762, -7.12985913233693, -1.3379412142837872] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00516841441664082, -0.0034458804912187177, -0.007816178271415194] km/s
+ V∞_out: [-0.001489799965378945, -0.00985305636150147, -0.0004127732777460182] km/s
+ time of flight: 1.0742880754700325e8 seconds
+ arrival date: 2027-09-28T06:49:31.486
+ thrust profile: [0.8198609633776256 -0.37682672496689756 -0.38437848331640034; 0.48287216377871234 0.007581817922041789 -0.441254562682009; 0.32388847431080076 0.07599246745185805 -0.4404310094474825; 0.17290384532256808 0.06226155896049881 -0.30796572110470416; 0.09088921192151388 0.03995997019453183 -0.1946676208979519; 0.06795206276709727 0.03390922110999609 -0.169842113328398; 0.008896361616988334 0.004639468676334631 -0.027316543942102114; 0.007395813289262249 0.0031923229639754594 -0.022849317973629848; 0.00327698511006219 0.0011135648676695487 -0.009162272587656917; 0.001246698684118812 0.004524008420119895 -0.016428072390077042; 0.0017872133263407393 0.0005880445198839666 -0.0054120587319473595; 0.0006912315323492273 -0.007687958584047147 -0.004602197074163808; -0.0008837213263607742 0.003546474857275424 0.0026115043129606814; 0.005643070016002708 0.0033539138977856935 -0.008832022656171667; -0.004567709779444214 0.003244136083179865 -0.001561392803448804; 0.0012910965001705745 -0.001013643665577717 -0.002495282419968127; 0.006464863397317595 0.006206787093383136 0.004990646441884204; 0.009201308744591857 0.007580566566309086 -0.01038202725616722; -0.0017275760703560961 -0.009337158161446552 0.0005319901564261099; 0.00925249778158428 -0.00039553483119386467 0.007843346751902708] %
+
+Mass Used: 133.3377932203348 kg
+Launch C3: 104.1081242757885 km²/s²
+||V∞_in||: 0.009983949254300396 km/s
diff --git a/archive/ES_0.6349730648198566 b/archive/ES_0.6349730648198566
new file mode 100644
index 0000000..49e8257
--- /dev/null
+++ b/archive/ES_0.6349730648198566
@@ -0,0 +1,22 @@
+archive/ES_0.6349730648198566---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T22:29:22.161
+Launch V∞: [7.180116960579566, -7.601492981437741, -2.064164994278147] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.023298123900821446, -0.10881016485915712, -0.17568043153498247] km/s
+ V∞_out: [0.08482061797288591, 0.039317717543159755, 0.18674980423187398] km/s
+ time of flight: 1.0735399562769012e8 seconds
+ arrival date: 2027-10-03T11:02:37.161
+ thrust profile: [0.33699850528888253 -0.16840082328950062 -0.2022720221493384; 0.18702976868836282 -0.014611613286823475 -0.22098099959972112; 0.0983411595411718 0.009292405597694972 -0.17554188111969365; 0.07214250937426424 0.013308151013734596 -0.16867215089564014; 0.06975709098005965 0.016773155207706704 -0.19362745328788616; 0.043494802185637955 0.011474397349952743 -0.1403753662811312; 0.02645847111666446 0.006562427033837446 -0.08867429574375933; 0.01173486898000651 0.0048516572489292155 -0.03744152207883444; 0.003269032790991646 -0.00012583195637893597 -0.01869271080822719; 0.00019697723803016815 0.00023416231394177275 -0.0005684535214205569; 0.0014790677956169442 -0.002784890564159347 -0.008665579250004152; 0.0088321996339963 0.0034394080185742447 -0.00597749039484158; 0.015738394760092672 0.0010403110774717633 -0.03062292287682462; 0.0035160078961190225 -0.00021610780787133883 -0.011429441552635993; -0.008947129362716407 -0.011542678217527674 -0.028025758657142505; 0.02357035072750574 0.01961435185385896 -0.01971431776909394; 0.02626144641759193 0.002798202742031768 -0.036615643486153295; -0.008633003425712896 -0.008866926160705727 -0.022861215606183365; 0.000684645370519383 0.0007041131957163129 -0.0013074377030049703; 0.008071386974312176 0.008231923269446436 -0.0027182949257643974] %
+
+Mass Used: 78.14952090119095 kg
+Launch C3: 113.59755223805288 km²/s²
+||V∞_in||: 0.20795689115365387 km/s
diff --git a/archive/ES_0.6350307078692827 b/archive/ES_0.6350307078692827
new file mode 100644
index 0000000..650c7bf
--- /dev/null
+++ b/archive/ES_0.6350307078692827
@@ -0,0 +1,22 @@
+archive/ES_0.6350307078692827---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:49:43.575
+Launch V∞: [7.181389554346585, -7.545996340111236, -1.9725672772641567] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001607121932398968, -0.009833737960756473, 0.004927740892932237] km/s
+ V∞_out: [0.00289226827079006, 0.004308221320839711, -0.009831408184681003] km/s
+ time of flight: 1.065570930548673e8 seconds
+ arrival date: 2027-09-23T13:01:16.575
+ thrust profile: [0.45852221520386777 -0.22414243848966278 -0.24860218557701533; 0.20147660577829019 -0.006392330461957223 -0.2171908177275059; 0.08411776326447276 0.013114610721590671 -0.14009259406366548; 0.07960971981702616 0.020366164042498913 -0.16805406255177577; 0.0921046328243092 0.032878720670181806 -0.22651276363748368; 0.03094711059255374 0.012012631161900187 -0.09163264966351746; 0.05140110372776015 0.022522470182675846 -0.16560988804415738; 0.03240522464948094 0.014316685133156102 -0.11260777013024127; 0.004783743889426229 0.0019882638318074793 -0.017117430465756665; 0.005511703635098295 -0.0001698062078491888 -0.007503507078159235; 0.003801594651614502 -0.0003542652335852517 -0.010554896508946416; 0.0003490958321429715 0.0002484003799841962 -0.009027767131823818; 0.0005251796540970775 0.0003200787397388781 -0.0033334170415074806; 0.004156584691891894 0.0010317764457594301 -0.005454067161684648; 0.0016462590060650484 0.0005804695895545331 -0.0012896391242483707; -0.011783166764010242 0.011845209095818092 -0.014873438539019363; -0.0015467049788123015 -0.0005793564646323765 -0.006654349150152516; 0.019362380584655024 -0.003750913608965654 -0.01870974881512801; 0.009374027590711698 -0.00506449280794859 -0.0067128180426059905; 0.012108161012908458 -0.0011183313943880877 -0.023265302575397676] %
+
+Mass Used: 85.17076874992472 kg
+Launch C3: 112.40543835958374 km²/s²
+||V∞_in||: 0.01111610873886619 km/s
diff --git a/archive/ES_0.6353062765535246 b/archive/ES_0.6353062765535246
new file mode 100644
index 0000000..2fd82b7
--- /dev/null
+++ b/archive/ES_0.6353062765535246
@@ -0,0 +1,22 @@
+archive/ES_0.6353062765535246---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T02:42:25.569
+Launch V∞: [5.387994991015565, -8.52939602628549, -1.7824665072303194] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.19615143223003048, -0.18105743063339919, 0.007782007279018541] km/s
+ V∞_out: [0.023168129445615863, -0.0006632088383921847, -0.16356479849476463] km/s
+ time of flight: 1.059251810603842e8 seconds
+ arrival date: 2026-08-30T02:22:06.569
+ thrust profile: [0.9944936180483686 -0.7693812482718979 -0.5290333811740231; 0.48750293688996016 -0.10748169759850106 -0.44567206723807307; 0.2206147897576449 0.00042925474797088055 -0.29356967889565017; 0.046218640017167176 0.006719863659445737 -0.08502807014512076; 0.039851457353081834 0.008446376093033468 -0.08402979766728211; 0.03840135379428145 0.008879312771346817 -0.09121185674611153; 0.02124127926042474 0.005597614938456778 -0.05767009436656085; 0.016285325692367392 0.0056534259740486465 -0.04686143833056467; 0.047828071432763186 0.017843053385809302 -0.13743971603203742; 0.003911388349687364 0.001334467734651019 -0.011327165814484936; 0.0125419461941731 0.011355236808589575 -0.0455943016618027; 0.0035797613654863073 0.0027385873199507337 -0.003099398350884333; 0.002890565553508503 -0.0024331170340930143 0.00038170816191247835; 0.0026249438618203094 -0.0010736298244985705 -0.0007790721475700443; -0.0008831717392306852 0.001671693463053142 -0.0028645829327100004; 0.0009751724745406095 0.003933704588366732 -0.002596127085792223; -0.0055797097132731085 0.002788626426935257 -0.0015053267676242875; -0.0013408204036443445 0.0002882376106241617 0.004100611220627763; 0.005813994611472171 0.008767301897300435 0.006123671621178366; 0.0017213627905455628 -0.00012805824093686796 0.0038782585815087768] %
+
+Mass Used: 128.93406087848734 kg
+Launch C3: 104.95827344582136 km²/s²
+||V∞_in||: 0.2670538095417309 km/s
diff --git a/archive/ES_0.6355259765311058 b/archive/ES_0.6355259765311058
new file mode 100644
index 0000000..1988832
--- /dev/null
+++ b/archive/ES_0.6355259765311058
@@ -0,0 +1,22 @@
+archive/ES_0.6355259765311058---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-15T17:28:01.493
+Launch V∞: [6.9546589202623945, -7.174810846268905, -0.7500129047133607] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.138959570219678e-9, 5.201047298026891e-11, -6.427193682881074e-9] km/s
+ V∞_out: [-1.2912563430556722e-9, 3.0432142103353773e-9, 4.114552212632997e-9] km/s
+ time of flight: 1.8279570135159373e8 seconds
+ arrival date: 2029-01-29T10:03:02.493
+ thrust profile: [0.3036095422666621 -0.07518571153093291 -0.06326544452097949; 0.24970132439214823 0.10076786145983235 -0.1414568533449631; 0.2009884836637603 0.15718546190037502 -0.18563790167076755; 0.15112172746670158 0.1655507961925028 -0.19588120690867464; 0.10451290496825659 0.14490374775073947 -0.17793657514639483; 0.07122355960132781 0.11931488750928605 -0.1526487010288201; 0.040159300130532746 0.07907609649719098 -0.10681184639065662; 0.016489200342817503 0.03805879751540265 -0.05406076591349519; 0.0012813707026118394 0.004301775977988875 -0.006397816131067182; -0.002473119431158756 -0.004283466296901427 0.0006432474110838098; -0.005607458746736986 -0.01265831066728459 0.017692788561714034; -0.007888631260682484 0.01277422380199924 0.011508195699845382; -0.020014103021523972 -0.011781964844367927 -0.000928796168148154; -0.002987242221644407 -0.010462766886559925 0.018728368869810757; -0.011679608683262855 -0.024226879806927906 -0.003730750445789025; -0.0006500675197867873 -0.0017599781962099798 -0.0004949001088808651; -0.013680109737262029 -0.045750880224089296 0.012223398094854659; 0.0013776456605903561 0.0043699164965250534 -0.0018314703613908237; 0.012652339594081494 0.015597343377026607 0.025173341063761356; 0.0015212232454925082 0.006969779244607658 0.021791489398645784] %
+
+Mass Used: 155.73532667035806 kg
+Launch C3: 100.40771073415978 km²/s²
+||V∞_in||: 9.606053688783815e-9 km/s
diff --git a/archive/ES_0.635736379477682 b/archive/ES_0.635736379477682
new file mode 100644
index 0000000..9c054b8
--- /dev/null
+++ b/archive/ES_0.635736379477682
@@ -0,0 +1,22 @@
+archive/ES_0.635736379477682---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:34:05.491
+Launch V∞: [7.179178549555544, -7.473099184993941, -2.2530450387985548] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9778558329039668e-5, -1.9727265680627837e-5, 1.4813056730200477e-5] km/s
+ V∞_out: [2.4454277419033055e-5, -1.547188786903779e-5, -1.2744354646442047e-5] km/s
+ time of flight: 1.0551552069404465e8 seconds
+ arrival date: 2027-09-11T04:26:05.491
+ thrust profile: [0.6303913728423709 -0.31613444910732297 -0.3535348100467629; 0.20847105014504003 -0.011333706373184774 -0.2272732441476094; 0.11044048058056172 0.014534935075004208 -0.17930418629117306; 0.10634886937064372 0.025508881046719976 -0.22293741093671993; 0.048905762889179125 0.01457096442837096 -0.12284865830400678; 0.016423629591220294 0.005748555192566112 -0.0478405502285177; 0.020832703109955785 0.007536348783861994 -0.06496416855873402; -0.0009203868914129179 -0.0024976544716921135 -0.03004404044459515; 0.015914663229644875 0.002947552089341513 -0.02217046255510288; 0.009642942893370945 0.00440785500003183 -0.03706699525632455; 0.00808888625950315 -0.00014290872671990254 -0.01118226894508694; -0.0009303949156858819 0.001749125030894911 -0.009693511326232343; -0.0007884394197721265 0.0023636229405079173 -0.0007322767744991068; 0.010581492372141076 -0.0001887376329840233 -0.0018030569213406018; -0.002200840702844504 0.0059320237316077 -0.00681369489221537; 0.0022102977437606403 -0.006236930495044523 -0.023857441404032533; -0.004776832206093987 -0.0035625922442455464 -0.009300399698577252; -0.009803818808494425 0.007324980163114309 -0.007619231741969796; -0.008783694175150564 0.008146360627754663 -0.01381675924579654; 0.005262983434786174 0.015991026378093704 0.006745148978636082] %
+
+Mass Used: 85.65227926223542 kg
+Launch C3: 112.46402802201033 km²/s²
+||V∞_in||: 3.161934582658912e-5 km/s
diff --git a/archive/ES_0.6357449506394436 b/archive/ES_0.6357449506394436
new file mode 100644
index 0000000..f44722f
--- /dev/null
+++ b/archive/ES_0.6357449506394436
@@ -0,0 +1,22 @@
+archive/ES_0.6357449506394436---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T04:34:59.494
+Launch V∞: [7.227343587892009, -7.526671798962445, -1.9209872697663508] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003436998725007878, -0.03073194053028371, 0.034489409499120785] km/s
+ V∞_out: [0.01208131816457008, 0.016982303562823972, -0.04135604065740594] km/s
+ time of flight: 1.0516668993115854e8 seconds
+ arrival date: 2027-09-07T09:33:08.494
+ thrust profile: [0.5094370982108212 -0.26099312412887327 -0.29705149773265777; 0.21806083946163213 -0.016045399390394875 -0.25188428391090806; 0.1253429550200553 0.013582922851324916 -0.21728804320205417; 0.06935169419172016 0.01453250740579421 -0.15863542899956765; 0.061822055347872586 0.017317367806893483 -0.16999554169122336; 0.045163677018129574 0.013953028867860229 -0.141261168875639; 0.031055347893760514 0.010288976157572146 -0.10931721759113495; 0.034415525695015894 0.012104815355612296 -0.12860404951914647; 0.0002465855554137171 -0.0005420930780691126 -0.0008779438477609963; 0.000469507910050856 0.00030266005549293816 -0.0027225281673046624; 0.0008516453315787451 0.0003921838839119857 -0.008510525342043681; 0.003276713689074477 0.0014781575417756566 -0.015338897714549616; -0.001665853327218087 -0.00037829759475333484 -4.141269107161725e-6; -0.0016032303154773341 0.00026657235021196205 -0.0024078660563321202; -0.001097930893087772 0.0013682293803677925 0.002223557018179882; -0.00028840841667634933 -0.00015899569227125374 0.0024954716702073553; 5.064088472299356e-5 -0.0008757485669565562 -0.00026641653404021033; 0.0011301613982675738 -0.0002433342514957739 -0.00316946159061093; -0.0005748033209069738 -0.0017576804509850349 0.004879253035513032; 0.00047176074698214156 0.00011785885160954166 -0.00033470450150565635] %
+
+Mass Used: 85.01216692817343 kg
+Launch C3: 112.5754757973447 km²/s²
+||V∞_in||: 0.04632261323145148 km/s
diff --git a/archive/ES_0.6359829539444091 b/archive/ES_0.6359829539444091
new file mode 100644
index 0000000..19ccf76
--- /dev/null
+++ b/archive/ES_0.6359829539444091
@@ -0,0 +1,22 @@
+archive/ES_0.6359829539444091---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:39:49.160
+Launch V∞: [6.949907227586401, -7.4319579039305745, -1.6913025090916591] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005587000463649713, 0.03250684434624626, 0.0057290940016596755] km/s
+ V∞_out: [0.03165788709647537, -0.0074140448362550885, 0.007970625136698077] km/s
+ time of flight: 1.1060226806090741e8 seconds
+ arrival date: 2027-11-08T11:30:57.160
+ thrust profile: [0.6522662341990142 -0.321791478725306 -0.3493391367767953; 0.31062214355419626 -0.013161472966139494 -0.336327593415947; 0.2051572437907151 0.02946985198315832 -0.33595257944781615; 0.06917003850867437 0.016379181486405044 -0.15377181165797907; 0.06002711776639275 0.01763006646880377 -0.1611524523250266; 0.017371481391164238 0.00213679544615688 -0.048405348004512086; 0.013333465291624387 -0.003579368893401583 -0.06585984515376914; 0.04119536788312672 -0.0001956733693003112 -0.09803704220161169; -0.005234356310737929 0.007403851926275752 -0.029499065590949645; 0.033480511132410413 0.0049894590374853325 -0.026572953526224817; -0.0015388179736015484 0.004656519935412127 0.0131640333197387; -0.0012681578645041768 0.0029675652771914292 0.006621348044754909; 0.0078928693125533 -0.007949223442634198 -0.015763635165710964; -0.0035489726909848996 0.0037334032462107113 -0.028228244017666063; 0.00017091056748318853 -7.66362451494946e-5 -0.011552463034079795; 0.008922893191771614 0.006751917200847635 0.01865431883671609; 0.06178863486173747 -0.012465913589133744 -0.11673652794466352; 0.06302524411477341 0.035927744847075 -0.07886736017038007; 0.06890657156659205 -0.0017071301723693263 -0.009920160708800644; 0.03063304496397255 -0.005436609991380565 -0.028241124470179235] %
+
+Mass Used: 121.33845414698135 kg
+Launch C3: 106.39571293511358 km²/s²
+||V∞_in||: 0.03347733593958393 km/s
diff --git a/archive/ES_0.6360031063628712 b/archive/ES_0.6360031063628712
new file mode 100644
index 0000000..c9642ff
--- /dev/null
+++ b/archive/ES_0.6360031063628712
@@ -0,0 +1,22 @@
+archive/ES_0.6360031063628712---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T11:02:56.489
+Launch V∞: [5.389440420251605, -8.628627111830383, -1.4767481034191958] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00804740298530706, 0.13942575978776747, -0.08498809082391795] km/s
+ V∞_out: [-0.13547834775086043, -0.06922863986393842, 0.06877964987980935] km/s
+ time of flight: 1.0565177959228145e8 seconds
+ arrival date: 2026-08-27T06:45:55.489
+ thrust profile: [0.8145576008807401 -0.6145960231490472 -0.41154440923435176; 0.5013789394508004 -0.10718409967497412 -0.4417548031813049; 0.1761562959492221 0.0028608309075988923 -0.23174831109649704; 0.11629910928835813 0.01715272376832428 -0.18800012186324108; 0.1466931223867749 0.029779038701629457 -0.2721499694599264; 0.06220583714646832 0.015187140446530533 -0.14044592275131787; 0.027332922037717963 0.006993989929185762 -0.06431638834951477; 0.04141768872884225 0.011872798528382281 -0.11586274673713147; 0.0014044316922980765 0.0003950276336531236 -0.0040042874683217785; 0.001649176997458303 0.0004244662582904362 -0.004722388760693514; -0.00039366821239333817 0.0009989156266432234 0.0018459772629754248; -0.0012071948461442879 1.0146182250744994e-5 0.0018245446157593563; -0.00041459794432096566 -0.0021826977977413074 0.0011237703879116874; 0.00010371371952744616 -0.00012211611088284432 -0.0010334643211890471; 0.0009385860664782985 -0.00016315794705484512 0.001257346759479644; -0.00033734872274604477 0.0007986120448988466 -0.002276402883627339; -0.001556552661167202 0.0011250479492536335 0.000709089787241312; -0.0002461425942960624 0.0020305285104986015 0.0020378960498102804; -0.0012338596201117331 0.0001871856542726793 0.003680747221218221; -0.0026487391230402488 -0.0023248745324523693 -0.004047480535033397] %
+
+Mass Used: 125.53661419346781 kg
+Launch C3: 105.68005883940832 km²/s²
+||V∞_in||: 0.1634847967521711 km/s
diff --git a/archive/ES_0.6360856007127665 b/archive/ES_0.6360856007127665
new file mode 100644
index 0000000..7434712
--- /dev/null
+++ b/archive/ES_0.6360856007127665
@@ -0,0 +1,22 @@
+archive/ES_0.6360856007127665---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T05:44:43.796
+Launch V∞: [7.0458619418530875, -7.600369858633737, -2.2234679706134304] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006972492917417402, -0.01096914388397279, -0.004179924850708164] km/s
+ V∞_out: [-0.007371532428769041, 0.009973031206275578, -0.005819949008284006] km/s
+ time of flight: 1.0817246117883028e8 seconds
+ arrival date: 2027-10-13T05:39:04.796
+ thrust profile: [0.5335326230312882 -0.2749326630980421 -0.30792239551387135; 0.1880499464199499 -0.014580277177597384 -0.2152903177180345; 0.093521215304389 0.010002471492976717 -0.16568558863855237; 0.03879370366274414 0.008043276220719268 -0.09584752202625063; 0.061461860165708794 0.015077118250424066 -0.1698395980507698; 0.01921100068696392 0.005957923702745419 -0.06736613605642613; 0.02339993673061011 0.009512150991035126 -0.0730339993997386; 0.01869044939621301 0.005904718326242538 -0.0834764410187733; 0.004416504874218505 0.014360239361430287 -0.023234363091902407; 0.0005706257038541229 -0.007269926068366867 -0.010749256102750264; 0.0038549916154363515 0.0031829126693550328 -0.018016491335156544; 0.01238358251583848 0.007388349352195178 -0.015893433944508664; 0.004365476601553973 0.005630433845533273 -0.026627807611538767; -0.010956928637309085 -0.016896412985854314 -0.0013113592815704404; 0.0033643241618906594 0.030278730413082742 -0.001233116679554714; -0.005916679178328922 -0.0003172650398535915 -0.013324110446907674; -0.010873178834467952 0.00860723017305162 -0.04133745345392584; -0.009373192065727376 -0.02017482924643727 -0.020497210952975558; 0.021791198626761932 0.031370278894615286 -0.012164187186763317; 0.02121938931177895 0.018090535426514318 0.04827629533077327] %
+
+Mass Used: 86.70385403474393 kg
+Launch C3: 112.35360230802577 km²/s²
+||V∞_in||: 0.013653188154724199 km/s
diff --git a/archive/ES_0.6361882005527693 b/archive/ES_0.6361882005527693
new file mode 100644
index 0000000..ff31a8e
--- /dev/null
+++ b/archive/ES_0.6361882005527693
@@ -0,0 +1,22 @@
+archive/ES_0.6361882005527693---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T10:50:49.296
+Launch V∞: [6.9508153468150695, -7.26979839462296, -1.6502320660399183] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.005098218565713915, -0.0016610660264147, -0.010890249703447347] km/s
+ V∞_out: [-0.0031601406738670217, -0.011714555993209778, -0.00033822429534721455] km/s
+ time of flight: 1.0974786702490842e8 seconds
+ arrival date: 2027-10-27T16:21:56.296
+ thrust profile: [0.9029887708114331 -0.43995537717185457 -0.43221242725595443; 0.38527388701614845 -0.00499858695778181 -0.37023008904129134; 0.19421082461187975 0.038244489355477064 -0.2871034135739451; 0.06670434561713144 0.01913476926579718 -0.13346614943200735; 0.04954644436184338 0.017152584429758387 -0.10955716395915083; 0.09200717916083377 0.03958854559283149 -0.23046910731571205; 0.021486108826095727 0.009767756567661887 -0.06442021553214226; 0.013623545413074855 0.005909944557209272 -0.04124134534119496; 0.013487816457774877 0.005224054328906441 -0.03642060223298417; 0.004112818440573129 -0.002743939651682478 0.004509105786610762; -0.005388692712447522 0.005317537935545251 -0.02583049009399397; -0.0037423949304666096 -0.003682532226583504 -0.000681548799863884; -0.0015704618443833276 0.003642282894144854 0.001149140680066156; 0.051545734091795074 0.04680044551420675 -0.01976193606003404; -0.05683906296787929 -0.005214510936954752 -0.0696278346482857; 0.0005432304275296996 0.030183747979982113 -0.059060588682757556; 0.06462454638944401 0.02622116546922943 -0.06158143478001278; 0.017854074182156714 0.04343445757324051 0.01839210077337771; 0.01679791044476623 -0.02016682232262136 0.017219963621619; 0.015344112324440481 0.0033828208110079326 0.01052075308837872] %
+
+Mass Used: 136.21166740291255 kg
+Launch C3: 103.88706855576883 km²/s²
+||V∞_in||: 0.012138719516132424 km/s
diff --git a/archive/ES_0.6361917950215027 b/archive/ES_0.6361917950215027
new file mode 100644
index 0000000..08c2b1e
--- /dev/null
+++ b/archive/ES_0.6361917950215027
@@ -0,0 +1,22 @@
+archive/ES_0.6361917950215027---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:06:56.494
+Launch V∞: [7.18515036936477, -7.468027744400397, -2.4188582332458153] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0013673858349398172, -0.007045961817111514, 0.005874020548463095] km/s
+ V∞_out: [0.0023198710512704244, 0.0035764496293293085, -0.008236564857237097] km/s
+ time of flight: 1.0543611554999787e8 seconds
+ arrival date: 2027-09-10T05:55:31.494
+ thrust profile: [0.6101751739611428 -0.3077219916868173 -0.332673355694027; 0.23314108233427056 -0.01289272756798796 -0.24297769089241192; 0.13814233109110668 0.01995786934713147 -0.21311358814457487; 0.05086589787521693 0.01282401274380075 -0.10913509073055087; 0.013404468277355301 0.0028046588075233986 -0.035302643534614195; 0.019117864066764422 0.004845679578212088 -0.05888597453773771; 0.01807971864505775 0.004587236002265855 -0.05602177632495229; 0.043573963441701294 0.02673580279623912 -0.14219713105270418; 0.0033351085191549055 0.005306150211939456 -0.017729176225361656; 0.0012484061283527161 0.0021910669657178405 -0.03287735774571251; -0.00018461415533232214 0.0028148888178447014 -0.005092207635594514; -0.004560786702420718 1.8699654975003546e-6 -0.012391097810682442; -0.0008638120957190477 0.002366463958526738 0.008772399980609427; 0.0006802074124496764 0.005142941280568469 -0.004143042555175983; 0.0066333856971005955 0.01096910907679181 0.0014137016362537839; 0.00060853992071344 -0.004235767082790002 -0.011688636549371119; -0.0020930371080619924 0.0031894714827141596 0.008035784545529046; 0.003676025562923571 0.01367853725071606 -0.008602964669913511; 0.0005543781138407483 0.01929648426462409 0.0025323127939187173; 0.0011383901166590674 0.001732719114483583 0.003322426009778511] %
+
+Mass Used: 81.6063478430824 kg
+Launch C3: 113.24869937405784 km²/s²
+||V∞_in||: 0.009274666535976058 km/s
diff --git a/archive/ES_0.6363471762546834 b/archive/ES_0.6363471762546834
new file mode 100644
index 0000000..b05ba5d
--- /dev/null
+++ b/archive/ES_0.6363471762546834
@@ -0,0 +1,22 @@
+archive/ES_0.6363471762546834---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:43:47.084
+Launch V∞: [7.176308085760775, -7.518389034887269, -2.2990946717349683] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01254894496355849, -0.00917784769072287, -0.028066247219754523] km/s
+ V∞_out: [-0.004824069482201882, -0.031693287260393714, -0.0013207660396163266] km/s
+ time of flight: 1.0472758446799558e8 seconds
+ arrival date: 2027-09-02T14:43:31.084
+ thrust profile: [0.6341300558153569 -0.32725290934115586 -0.36059876419914916; 0.24874545140696017 -0.017741672778118344 -0.28353850776507633; 0.09079614274249628 0.011339538393265616 -0.15982244769855558; 0.059754116656267536 0.01338555192611636 -0.135362519934207; 0.03902608775459515 0.010878676137677581 -0.10271067037149316; 0.03085966099919654 0.009775733257682597 -0.08953282952562877; 0.025644053919621306 0.007400804457648352 -0.08711854708237242; 0.001323914483302462 0.0024477456287086232 -0.02052944533736327; 0.0020202046036527053 0.0009388144685560808 -0.006421195673375077; 0.004176663096346267 0.0020148578143582953 -0.017885895166496805; 0.005924175748188329 0.0016870260974565906 -0.01600509055066046; -0.001468238232621823 -0.004885760504571108 -0.004010649644609982; 0.004101611475936795 -0.0009997308085569906 -0.006080124213118661; 0.004739593084753862 0.0034970669186070143 -0.009509326850053143; -0.007011848803592253 0.012410211628391564 0.001595693005653799; -0.003909404326574363 -0.010621816712159914 -0.006272294415601802; -0.007902436359328458 -0.009417199053421029 -0.022026057254677794; -0.0006763811705317946 -0.0003113057924062925 0.00264000351241531; -0.0007026224759981489 0.0003767150463998615 -0.00026855519400028303; -0.000729903676763342 -0.00014073255049103082 0.0013995042176697088] %
+
+Mass Used: 81.42182719806306 kg
+Launch C3: 113.31140773126873 km²/s²
+||V∞_in||: 0.032084624681191234 km/s
diff --git a/archive/ES_0.6363938755855825 b/archive/ES_0.6363938755855825
new file mode 100644
index 0000000..3baff80
--- /dev/null
+++ b/archive/ES_0.6363938755855825
@@ -0,0 +1,22 @@
+archive/ES_0.6363938755855825---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:19:50.495
+Launch V∞: [7.1611988084443725, -7.567761054961005, -2.251150375962956] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.026447700191122022, 0.026060439949272752, 0.0027684192647992266] km/s
+ V∞_out: [-0.024957647762533477, 0.020003939346347102, -0.018827878880164777] km/s
+ time of flight: 1.0483757746650116e8 seconds
+ arrival date: 2027-09-04T08:52:47.495
+ thrust profile: [0.6561183389005654 -0.3255592417981421 -0.3258129821927559; 0.16824007942245853 -0.00923235563448568 -0.21534429467928712; 0.07844142522259166 0.00907257224816314 -0.14346646248578293; 0.04359935710260104 0.009380879191536653 -0.10344493401660251; 0.04337845760528004 0.012558196160274027 -0.12789200805138987; 0.020208053187611045 0.006367271402582178 -0.06760679780762505; 0.023757344243304366 0.008214191298461798 -0.09110910319940117; 0.04004697541975076 0.01716215943191517 -0.14563069100261783; 0.006283684336683901 0.0015630130467841684 -0.022559221731956194; 0.012112463967702467 0.001972108674874784 -0.050574869593640326; 0.0009873334152109498 -0.00024186844245408691 0.00029439318729044335; -0.0005601391350839945 -0.0006719422460260689 0.002081683462628739; 0.0021741767108724 -0.0021229555700605115 -0.0001697539608698052; -0.002360795488948037 0.002847269654112986 0.0024459900640924326; 0.0005079697765580116 -0.00036958069434827267 0.0032727947972616125; -0.0008369960580998253 -0.00010349964258037328 0.0019054924295660068; -0.0007309147164711867 0.000172510738843201 0.002717167475883597; -0.0004802951512859293 -0.00048526363500378495 0.0018487582129523808; 0.0011347611289710465 9.815612219382706e-6 -0.0015196509890623147; 0.0008886263654270374 -0.0049788650908419545 0.0022273609165831005] %
+
+Mass Used: 79.66770783340098 kg
+Launch C3: 113.62145377424775 km²/s²
+||V∞_in||: 0.03723293597038566 km/s
diff --git a/archive/ES_0.6366940860347584 b/archive/ES_0.6366940860347584
new file mode 100644
index 0000000..1cc3b1e
--- /dev/null
+++ b/archive/ES_0.6366940860347584
@@ -0,0 +1,22 @@
+archive/ES_0.6366940860347584---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T15:58:50.542
+Launch V∞: [7.20778654215112, -7.43210285060424, -1.7919928599964754] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.016880013511534186, -0.028327212941797797, -0.01147085667283664] km/s
+ V∞_out: [-0.020678402148716857, 0.024077089214900566, -0.014492748381151152] km/s
+ time of flight: 1.0422734093221983e8 seconds
+ arrival date: 2027-08-26T00:01:10.542
+ thrust profile: [0.6169299111637596 -0.28641549679048994 -0.305300119598121; 0.32011738431194325 -0.003665255502874484 -0.3109280084267889; 0.22859451830827315 0.04398820019636157 -0.32601879942912393; 0.1589944045456591 0.04911400913995084 -0.2953643122438564; 0.06771854237935006 0.024922579712043987 -0.15552144691007688; 0.04284361278309365 0.017913232803832228 -0.11338134138847158; 0.03405359095126065 0.015716906215189994 -0.1000064709197106; 0.006938542519305834 0.003575824882411781 -0.02270823178976028; 0.0007471486557762436 0.0003452881825530414 -0.002542285332500878; 0.0011389215899811902 0.00017821326097209271 -0.0030515683116758415; 8.2502023505889e-5 3.340073989364792e-5 -0.0011489510411447493; 0.0016532449463641315 0.0012293834862879605 -0.006117322773363419; -0.00022220124660113241 -1.2046546292442828e-5 -0.0021986045220190324; -0.0005403925755056155 -0.00025257455433552614 -0.00063473854717643; 0.00022099832153198748 0.0004292378434405469 -0.001466627545365922; 0.0009624801008118774 0.002028264670119311 -0.0003604566134620111; 0.00031905795572610023 4.45652251946432e-5 -0.0009682298336984748; 0.00010393826121244212 2.9858919243792316e-5 0.0006739299724322532; -0.000512428663859579 0.00014028656686892603 0.0005645113800048006; -0.0004349761224413794 0.0013888623015489454 -0.000940595440631875] %
+
+Mass Used: 98.81222853541021 kg
+Launch C3: 110.3995780294528 km²/s²
+||V∞_in||: 0.034913412924094 km/s
diff --git a/archive/ES_0.6368102274112363 b/archive/ES_0.6368102274112363
new file mode 100644
index 0000000..691f3a7
--- /dev/null
+++ b/archive/ES_0.6368102274112363
@@ -0,0 +1,22 @@
+archive/ES_0.6368102274112363---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:14:53.829
+Launch V∞: [7.182235233972126, -7.495065334695048, -2.2648891364545407] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.05542319041148522, -0.08995903674337652, -0.03726695948423042] km/s
+ V∞_out: [-0.05933145024139285, 0.08258775423608003, -0.04704113694502684] km/s
+ time of flight: 1.0332107941072991e8 seconds
+ arrival date: 2027-08-17T01:32:52.829
+ thrust profile: [0.7266504622378762 -0.370962268505188 -0.40973774576804844; 0.3240636931425851 -0.020883098634372058 -0.3516411754761163; 0.0848149455057162 0.010317048472396928 -0.14413933739355594; 0.090530799505556 0.020655111031628655 -0.19631601575095683; 0.049010337420044355 0.012828652986161919 -0.1294349293842348; 0.018804777312496124 0.0063758287128166564 -0.06207490306622983; 0.00921724751462534 0.003465536783657117 -0.03160425821965883; 0.005886959718360705 0.001899305490687597 -0.020674605099098308; 0.0006400521667932185 0.00025414041266869823 -0.0027376741992796287; 0.00023308956798366332 0.00028645479455191786 -0.0024658250691883157; 0.0003564589522707827 -0.00010117040530659901 -0.0010846570096276413; 6.113169474149894e-5 0.0005046015479991073 -0.0003550787998150692; -0.00037549800725953525 -0.00023440216400363019 -0.0005017429073521462; 0.0008115826332464049 -0.0007224337441293962 0.0001700316121859877; -5.8582477371157444e-5 0.0005996838727860865 -0.0010494416867272514; -0.0009602752244622602 0.0001137487546488346 -0.0010868506523422643; -0.0010762933603946558 -3.7493757587072985e-5 0.0002532220408555596; 0.0009494583337658778 -0.000450063272435207 0.0006126464956036268; 0.0010158846749130817 0.0009684043652882835 0.00015017650469196077; 0.0010953317342817682 0.000968403064246231 -7.6049697514086e-5] %
+
+Mass Used: 84.41892290043006 kg
+Launch C3: 112.8902301278878 km²/s²
+||V∞_in||: 0.11204099515973243 km/s
diff --git a/archive/ES_0.6368513329737661 b/archive/ES_0.6368513329737661
new file mode 100644
index 0000000..734811e
--- /dev/null
+++ b/archive/ES_0.6368513329737661
@@ -0,0 +1,22 @@
+archive/ES_0.6368513329737661---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T00:49:36.458
+Launch V∞: [5.560013174225104, -8.676207824654057, -1.9121370486314961] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.5247502554283927, 0.4959265143885548, -0.02125820872954935] km/s
+ V∞_out: [-0.09919913498772553, 0.0028338543434880477, 0.7143295155514088] km/s
+ time of flight: 1.0487030368314916e8 seconds
+ arrival date: 2026-08-18T19:27:59.458
+ thrust profile: [0.6746167522305987 -0.5150550969302335 -0.3856416352707944; 0.33906517330770575 -0.07805684441520132 -0.3384921613176781; 0.20067834564808656 -0.004818333457209232 -0.2805120122026421; 0.11014227883264206 0.009738624326885137 -0.19335551022300262; 0.0714082009345179 0.011742500281831346 -0.14774037133495718; 0.040285347594091844 0.008828635108426344 -0.0940960889288425; 0.04961847215825204 0.012460164684330016 -0.12570639448319723; 0.002981626837142112 3.267523967224702e-5 -0.006624261102283555; 0.0030125814646942742 0.0021530901367982744 -0.01340511715753322; 0.002029106441229406 0.000814844029566197 -0.0082869507024944; 0.0017524233003595165 0.0008450669226832117 -0.002601866785420657; 0.0006285606496541781 0.00014986865476729512 0.000868517913299928; 0.0009480155588179476 0.0005455378069709913 -0.0036606571326792247; 0.0012372027140764425 0.000657784432019948 -0.0029936193412798424; 0.0010077837834336566 -0.0011756856838339674 3.956334030376146e-5; 0.0007037801546904351 0.0007799495234642236 -0.003281820477556862; -0.0005140742457622103 -1.5404064422105458e-5 -0.0024652507456779894; 0.005300225176357885 -0.00509692421733883 0.0013378335599673954; -0.00023275521996649323 -0.0008539161481887244 -0.0004524788213906963; 0.0007283119496949131 0.00021710078389169528 -0.002296815934780561] %
+
+Mass Used: 102.22140709584437 kg
+Launch C3: 109.84659680689417 km²/s²
+||V∞_in||: 0.7223280762120035 km/s
diff --git a/archive/ES_0.6370850789822546 b/archive/ES_0.6370850789822546
new file mode 100644
index 0000000..ce94c03
--- /dev/null
+++ b/archive/ES_0.6370850789822546
@@ -0,0 +1,22 @@
+archive/ES_0.6370850789822546---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-01T05:36:19.432
+Launch V∞: [7.845607303341686, -7.4709544860943025, -1.4421966627838825] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.217089617555473e-9, -4.28565102692583e-10, -1.5498333888339338e-9] km/s
+ V∞_out: [7.191585239981749e-10, 9.091567741651445e-10, 4.0100624555242725e-11] km/s
+ time of flight: 1.8191171480342913e8 seconds
+ arrival date: 2030-03-07T16:38:13.432
+ thrust profile: [0.004725165075078091 -0.002638964263823945 -0.0033527002780787928; 0.0025062219880532853 -0.0028970848687393503 -0.006266633287152016; 0.007435953775488162 -0.013115896098203513 -0.02818505421286008; 0.025084237973161522 -0.051213846770530626 -0.10732600854270818; 0.03150202962987133 -0.06601001814367198 -0.13869116904350048; 0.03004634613144765 -0.06298428149784709 -0.13289841766316027; 0.019617106746253436 -0.04126964195469426 -0.08730106744861542; 0.008478166753308574 -0.01746050698011293 -0.037398827808496744; 0.003978011669088891 -0.007944670562843032 -0.017395055524321502; 0.00042648285391913874 -0.000859058251766941 -0.0018498992161519797; 0.00023041967473201193 -0.0004630226165680695 -0.0009471089330530739; 0.0003906783412044017 -0.0007071033474662298 -0.0012370747827386839; 9.667756806215725e-5 -0.0001365997683559847 -0.00040728133426610097; 0.0001224916409959056 -0.00028779492134122474 -0.000525580758235625; 0.0001333904979763674 0.00011458883083793203 -0.00018962186389368717; 0.00011506910170612028 -0.0001310102748724242 -0.00022219906442989655; -0.00018372847254694434 -0.00013154418304527302 -0.00030173694134487665; -6.323080604497442e-5 7.39737441686148e-5 7.0191340336662e-5; -2.0806814785815454e-5 0.00011253358376213894 -0.00019424406974059404; 0.0001792320252199788 -0.0003826453683732218 7.759299969640836e-5] %
+
+Mass Used: 46.48215652946237 kg
+Launch C3: 119.44864610568595 km²/s²
+||V∞_in||: 2.0166702054504865e-9 km/s
diff --git a/archive/ES_0.6370864191196581 b/archive/ES_0.6370864191196581
new file mode 100644
index 0000000..ef0e8ab
--- /dev/null
+++ b/archive/ES_0.6370864191196581
@@ -0,0 +1,22 @@
+archive/ES_0.6370864191196581---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T01:43:25.359
+Launch V∞: [7.093583808302493, -7.2817664218560285, -1.6166906756674182] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002078205348437633, 0.0013885484712558229, 0.0044966138419545035] km/s
+ V∞_out: [0.0008828937167946559, 0.005055954318814147, 0.00023441426777004942] km/s
+ time of flight: 1.0455413450359857e8 seconds
+ arrival date: 2027-08-28T04:32:19.359
+ thrust profile: [0.922466411179631 -0.4347485819138162 -0.4072174699694943; 0.5070600790669074 -0.005235598935901079 -0.43459735619705425; 0.26762772260077894 0.052492035426498704 -0.35256897052354874; 0.10643555101694495 0.033803216841445674 -0.18875261450040126; 0.06573548276532466 0.0257416859267987 -0.13913255767007643; 0.06457044285629567 0.028908810261896466 -0.15441105609567563; 0.05360121231699443 0.026686778064533463 -0.14151293663629874; 0.011380367581643831 0.005274136414715049 -0.02941904965870037; 0.007561806133107849 0.007194505266233176 -0.016914791621221944; 0.0016613579419365258 0.0006578181751453257 -0.0029328810761339447; -0.0007286960041706847 -0.0007047613516365688 -0.003431849271012107; 0.0025051145882122204 7.018128269536527e-5 -0.0038918130881865527; 0.0011365546272832042 0.0004443899100696029 -0.0014038378350234866; 0.001715964967992665 0.0008562081128729692 -0.00435844613010913; 0.0011477095399796096 -0.0005477421851010772 -0.0004497282408386866; 0.0023637877036867374 -0.0006125566816168101 0.00026482069789449006; 0.002382387591735609 0.0013844551631039927 -0.00033316488642401443; -0.0004091642534857342 0.00025604670281013193 -0.0006944439513562281; 0.005561632403056418 -0.006015564111904914 -0.0019947947455491908; -0.004585126854587123 -0.0022006222591850672 0.009146173433020521] %
+
+Mass Used: 125.18649275568578 kg
+Launch C3: 105.95674220867122 km²/s²
+||V∞_in||: 0.005144564157531569 km/s
diff --git a/archive/ES_0.6371265412859313 b/archive/ES_0.6371265412859313
new file mode 100644
index 0000000..48b6a10
--- /dev/null
+++ b/archive/ES_0.6371265412859313
@@ -0,0 +1,22 @@
+archive/ES_0.6371265412859313---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:45:58.301
+Launch V∞: [7.2204977389315665, -7.560828133536247, -2.067100694380143] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004109460181838491, 0.026323468542874158, 0.004634313686339702] km/s
+ V∞_out: [0.02566983052221108, -0.004973235102710905, 0.0068902545234281656] km/s
+ time of flight: 1.0391815338439003e8 seconds
+ arrival date: 2027-08-24T05:55:11.301
+ thrust profile: [0.5168775161511707 -0.26407279636577796 -0.3012628286602604; 0.2680235990568061 -0.018981940837630648 -0.30062706117745136; 0.1552180206387273 0.01767378412658843 -0.2606152257255844; 0.09336781670464041 0.02022148124535703 -0.20602278123750045; 0.04719398159973376 0.013394347624104375 -0.12839129160022783; 0.01795851558558975 0.00585601860115389 -0.056648141684674996; 0.02428603145393642 0.008958563815361191 -0.08712279619763567; 0.008841240205477547 0.0034670691338330095 -0.033258700742488184; 0.006372716959801071 0.0020645722541739525 -0.025425005567679744; 0.0014681865450037964 0.0005110019956344129 -0.006183089508974899; 0.00010406280140238917 9.94495340094949e-5 0.0002036137539856865; -6.345912373788156e-5 0.00010593233431944813 -0.0012326096352088941; -8.706702954967903e-5 0.000309328743777494 -0.0005600493713435148; 0.00015849305030817711 0.00021595835896755087 -0.0005441542179247806; -0.0015601103261804945 0.00018607877880268676 -0.00040897341556240494; -0.0012747211287115888 -0.0008639895052096972 0.0007393038437240406; -0.00030685117523158957 0.0010306618683370349 -0.00014322677103135388; 5.8081288199570954e-5 -3.993631125920968e-5 3.184184125635571e-5; 0.0006032316731146686 -0.0007147292372250843 -8.347032590448248e-5; 0.0008054893608207691 -0.0005676243072162734 6.699159152115429e-5] %
+
+Mass Used: 80.79571099652685 kg
+Launch C3: 113.57461494349594 km²/s²
+||V∞_in||: 0.027042365326598133 km/s
diff --git a/archive/ES_0.6372667032899232 b/archive/ES_0.6372667032899232
new file mode 100644
index 0000000..46688b7
--- /dev/null
+++ b/archive/ES_0.6372667032899232
@@ -0,0 +1,22 @@
+archive/ES_0.6372667032899232---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T03:23:52.959
+Launch V∞: [7.228479633048054, -7.509960394140829, -2.324707057007697] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.05428030876164579, -0.0855659779012238, -0.03518795413577224] km/s
+ V∞_out: [-0.05863637564823906, 0.07760309624134833, -0.0452103518453615] km/s
+ time of flight: 1.0414757096516229e8 seconds
+ arrival date: 2027-08-26T13:16:42.959
+ thrust profile: [0.5338525105683414 -0.27092020430179264 -0.30412727716442906; 0.2927420723432636 -0.017312179572236405 -0.3102783024227552; 0.1313465281528356 0.018692090892274308 -0.20763841786068116; 0.07869294063024163 0.020453014444681752 -0.16301918513576535; 0.047103709910984504 0.01598840640421531 -0.1196091205070744; 0.012348691593713036 0.0046595096654525655 -0.03589149695685837; 0.017106792344394047 0.006674951656739307 -0.057836509461216754; 0.009388149511628722 0.004550421318814416 -0.03411247400428834; 0.006910013324730882 0.0034305074384050416 -0.022652218387812013; -0.0010358474852245063 0.0013051982836896968 -0.00413654430494191; 0.0003701376818794134 -0.0018824430068754361 -0.002225918312345196; -0.00026243421149228633 -0.00085030318938006 -0.004119965767453389; 0.0003300181745591808 0.0008767646997782392 -0.0012061894727340484; 0.0011734117199559044 0.000861719827194764 -0.0014090940552720162; 0.00097025873075964 -0.0075361725086330045 -0.014538124258227888; -0.0043341010654716185 0.00037049101014364105 0.00014203248162843532; 0.002779150592254659 0.00108243518261309 0.0032125338094356123; 0.008063555287156911 0.005827997585267794 -0.0064545989902726; -0.0035314752106976838 -0.0005052149141237331 0.0032211702597097595; 0.008965961335849926 0.008691906759491755 -0.0020447316768221315] %
+
+Mass Used: 78.15881984241832 kg
+Launch C3: 114.05468582785579 km²/s²
+||V∞_in||: 0.10726640018996411 km/s
diff --git a/archive/ES_0.6375806472704638 b/archive/ES_0.6375806472704638
new file mode 100644
index 0000000..db6ec1a
--- /dev/null
+++ b/archive/ES_0.6375806472704638
@@ -0,0 +1,22 @@
+archive/ES_0.6375806472704638---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:05:35.635
+Launch V∞: [7.161752291831886, -7.594696187286239, -2.0153386513712306] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.006582937344947125, -0.004189565548191936, -0.016296016749258596] km/s
+ V∞_out: [-0.0027286023071583327, -0.017835700964171662, -0.0007652137809617] km/s
+ time of flight: 1.0408485333393845e8 seconds
+ arrival date: 2027-08-26T11:33:08.635
+ thrust profile: [0.5502352311613862 -0.2792171166156014 -0.3089813777754755; 0.2940297518377967 -0.02236816129752549 -0.31923329060804473; 0.1608818234589802 0.01685322874658531 -0.2619188521355404; 0.07965217177059011 0.01637604306316858 -0.17012934798878693; 0.03145109049931313 0.008409352355677581 -0.08367517022055017; 0.04368052011364387 0.015056105751750992 -0.13807240530125633; 0.00860376016508424 0.004396864817347266 -0.031240294785579496; 0.01743664692828919 0.006383240124638949 -0.0653617121088275; 0.007485709706039308 0.001952590749296353 -0.030701968525511103; 0.005026006323881407 9.203467946022968e-5 -0.013982271611405797; 0.0006775677506997035 0.001454893031671482 -0.0037091809332017995; -0.0005349892176301414 0.0025175416841089066 -0.005091779787778902; -0.0007982302708328315 -0.00011631033365559502 -0.0027065106898485607; 0.00017872980745711124 -0.00061642369259572 -0.0027423469163897207; 0.001005606193868493 2.4535049214285433e-5 -0.005025062016168802; 0.0019456917238976114 -0.0018429700581824903 -0.003774115492682222; 0.0027357225341884898 -0.001162807751023484 -0.002349146539949253; -0.0009195361470908927 -0.00015827473434077463 -0.00011461489035826267; 0.0007678878925949097 0.0020961110464616526 0.001544734130220605; -0.0016373088845630444 0.0015111539320724317 -0.000995892163492349] %
+
+Mass Used: 84.49252879458163 kg
+Launch C3: 113.0316959464502 km²/s²
+||V∞_in||: 0.018067863334169123 km/s
diff --git a/archive/ES_0.6376754044113436 b/archive/ES_0.6376754044113436
new file mode 100644
index 0000000..6496b76
--- /dev/null
+++ b/archive/ES_0.6376754044113436
@@ -0,0 +1,22 @@
+archive/ES_0.6376754044113436---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T09:58:31.445
+Launch V∞: [5.525646346070744, -8.69900474363216, -1.9308640969958017] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002047217727101747, 0.034752970064074705, -0.02157944611175016] km/s
+ V∞_out: [-0.03425939384319266, -0.015413506510490864, 0.01634517715122317] km/s
+ time of flight: 1.0444058822259852e8 seconds
+ arrival date: 2026-08-14T05:14:59.445
+ thrust profile: [0.7132348676248904 -0.5573839623410453 -0.38604916571528164; 0.3596304588441567 -0.08241594803157927 -0.3301858983082671; 0.14798317261613134 -0.0008281109754713022 -0.20560580857730953; 0.05634367950076786 0.005138979539869171 -0.09939070237712867; 0.09706125107381763 0.0175903501211944 -0.1953483076344555; 0.10676555594325111 0.028151874320510795 -0.2402020508937326; 0.028263861472379283 0.00750496773598538 -0.07181552945953733; 0.005404475929330757 0.0011680634776306449 -0.01443091899331531; 0.0036153183098663914 0.0012492027446022503 -0.010371418248312473; 0.0020144041268301887 0.0007404972783945369 -0.00653193048433636; 0.001142531879109656 0.000825342726029351 -0.005725307817564535; 0.0006933982998718177 -0.0005806333172640014 -0.002562326018882911; 0.000716818007161355 0.0006333240521738909 -0.003226132446181373; -9.016593968476025e-5 0.0005096306166182886 -0.00248419612920674; -0.0011338882649637226 0.00016835519668607018 5.1755132843393846e-5; -0.0010952782811415932 8.450246674364793e-5 -0.0002766683393970581; -0.0013701675130235345 0.0002590558311144486 -0.000869848224726287; -0.00036680000669821774 0.00016266532506718128 0.0003441542223613873; 0.0020636166193511354 0.0016879282638988895 0.0030604649839579383; -0.0008940660920326973 -0.000126317570918305 -0.004761388298733968] %
+
+Mass Used: 102.67479628945875 kg
+Launch C3: 109.93368723264722 km²/s²
+||V∞_in||: 0.04095891262212122 km/s
diff --git a/archive/ES_0.6377650001167123 b/archive/ES_0.6377650001167123
new file mode 100644
index 0000000..d4bd0e1
--- /dev/null
+++ b/archive/ES_0.6377650001167123
@@ -0,0 +1,22 @@
+archive/ES_0.6377650001167123---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T13:34:27.096
+Launch V∞: [7.132536380912785, -7.612935183526518, -2.403627447682972] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.31968694677949044, -1.4725093688137205, -2.3199035687287455] km/s
+ V∞_out: [0.9618127513567427, 0.45040194521658555, 2.5547715696291315] km/s
+ time of flight: 1.0452939059617606e8 seconds
+ arrival date: 2027-09-01T09:30:57.096
+ thrust profile: [0.6654804273502327 -0.3489085285959744 -0.3910423644059652; 0.1658244768824275 -0.01485753247479188 -0.19692945073871854; 0.06332665167983732 0.00573529058613164 -0.11687826457043318; 0.03537647104500862 0.006489441292141261 -0.08635114604971249; 0.07174467652538438 0.0170529206532918 -0.19881353376069524; 0.01703128590016663 0.0046825232493924 -0.055944233180111616; 0.007301937549797466 0.0020425405957288497 -0.024388938033041114; 0.01807179245104681 0.005434364554817154 -0.07469692261310662; 0.0031120593810189455 0.0021822166676222134 -0.01187860827257883; 0.0013234943601057969 0.00039189895378515405 -0.0062228214952742104; -0.003485961273817226 -0.0006633438701772326 -0.003471131788660345; 0.0016644692959332913 -0.0006938711647226461 -0.004493838980275163; 0.002454200791089958 0.0023860717939250594 -0.001223590749729745; -0.0020683777870122745 0.0060929546006413815 -0.002232127684968553; -0.008120560209802166 0.002413287598001529 -0.0005337916286493102; 0.0033252793934690304 -0.006978189800828731 -0.005136896219314373; 0.011766346921108138 -0.00028839890794292444 -0.0021531222040669126; 0.0007808056768087551 -0.00033657456039856866 -0.004642218905087321; -0.01225033512281641 -0.009865191339989074 0.0045169297367818025; -0.005715650715386534 0.012373409484048558 0.014038297569597947] %
+
+Mass Used: 75.51668706439159 kg
+Launch C3: 114.60728224087534 km²/s²
+||V∞_in||: 2.7663036986899585 km/s
diff --git a/archive/ES_0.638042973082901 b/archive/ES_0.638042973082901
new file mode 100644
index 0000000..d89ca01
--- /dev/null
+++ b/archive/ES_0.638042973082901
@@ -0,0 +1,22 @@
+archive/ES_0.638042973082901---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T07:21:07.885
+Launch V∞: [7.237750192919666, -7.5050704822246805, -2.2653492462330327] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.010566118661657074, -0.029130597961274953, -0.036557464268320454] km/s
+ V∞_out: [-0.04046256093545524, -0.007019517026106484, 0.0247049375944655] km/s
+ time of flight: 1.0365180879883541e8 seconds
+ arrival date: 2027-08-20T23:31:15.885
+ thrust profile: [0.6799751880862689 -0.3410637441474138 -0.36303420929549757; 0.19067520831432458 -0.010389505400541538 -0.21022444604719884; 0.07702098389618994 0.011359958050956609 -0.13030819440338812; 0.04513673327630994 0.01148294778366075 -0.10065576330263068; 0.04500366002149642 0.014908699028006194 -0.11776467219886917; 0.039007074943200146 0.015012028681803109 -0.11596013002851788; 0.02763525192817354 0.011349055577771078 -0.09292637807574258; 0.04257950019001269 0.020386382595921217 -0.1394132407128378; 0.009503599446023768 0.004176194772243693 -0.03605077925708049; 0.00027291836326334587 0.00013902595718649657 -0.0002306957750001657; 0.003579154249871694 0.0013718762642626078 -0.014303283282257473; -0.0002645111534466292 0.0007080178738918283 -0.0006353266301974503; 7.871345274842271e-5 0.0005111307803479829 -0.0005163004247538328; -0.00023723365603347567 0.0001457378234315074 0.00014360730899092534; 0.00018538334064014054 0.00013388865898813048 -0.00041471165325255026; 0.00042702584414629896 -0.0001235080783540133 -0.0006392291891613941; -0.0003916833633348684 -4.650767874274142e-5 0.00020985387767990268; -0.000828983309155801 0.0007810894672522729 0.0006393620854111137; -0.0017586029780035243 0.0004604169208164213 0.0004979511978121269; 0.000655773183474881 -0.0007317898763241568 -0.0008764857760542468] %
+
+Mass Used: 80.29978023026615 kg
+Launch C3: 113.84291800567743 km²/s²
+||V∞_in||: 0.047923718500166294 km/s
diff --git a/archive/ES_0.6384090919103853 b/archive/ES_0.6384090919103853
new file mode 100644
index 0000000..706b617
--- /dev/null
+++ b/archive/ES_0.6384090919103853
@@ -0,0 +1,22 @@
+archive/ES_0.6384090919103853---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T20:34:42.612
+Launch V∞: [7.163345357205025, -7.50861149755505, -1.6273128290557846] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.028329980227434576, -0.12137584383562652, -0.20182285503551756] km/s
+ V∞_out: [0.07948686405282743, 0.03678342350065522, 0.2266673048168516] km/s
+ time of flight: 1.0542868017348957e8 seconds
+ arrival date: 2027-09-10T02:19:22.612
+ thrust profile: [0.6211203266269497 -0.31334368263078266 -0.34682498679202606; 0.1958527584719362 -0.012169323178432521 -0.21953488774461208; 0.15924117533379614 0.0194415669231716 -0.2626596137043327; 0.10639704011465488 0.023532442739180287 -0.22698913161675308; 0.10236014832575639 0.029176627872241106 -0.26266388987239575; 0.05673981426546835 0.018784917187895024 -0.16559850155464342; 0.034019527186168214 0.011448912507496623 -0.10734279264218743; 0.01935197091067146 0.007888469498636315 -0.06440718510231169; 0.0049878553681431135 -6.39932458662458e-5 -0.007992227353182493; 0.00013223772453055654 -0.0008133609294560464 -0.002371182186862371; -0.008700080489293556 0.0015480588322326564 -0.006303631519293949; 0.000929019436306802 -0.0025947411474329454 -0.010393496327373845; 0.0075502476570877995 -0.0006280109816555114 -0.004390176231332133; 0.000694099452554386 0.0003550790151403754 -0.0014199219063688769; 0.0007687361026093554 0.002033446287525873 -0.007984780474728679; 0.0025677271649707273 -0.008868281436915546 0.0066091032984461695; -0.01106036284832947 -0.010559105888931823 -0.007219037902319408; -0.010903189090755027 0.011704314695500213 0.007657354119671346; 0.017183586204796764 0.00479362797336538 0.003749117046865711; 0.004739244026393472 -0.00843685335397384 -0.01911514937522594] %
+
+Mass Used: 101.15529672885486 kg
+Launch C3: 110.34091037141621 km²/s²
+||V∞_in||: 0.23720697304502827 km/s
diff --git a/archive/ES_0.6384736706910974 b/archive/ES_0.6384736706910974
new file mode 100644
index 0000000..c88b431
--- /dev/null
+++ b/archive/ES_0.6384736706910974
@@ -0,0 +1,22 @@
+archive/ES_0.6384736706910974---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T15:56:32.150
+Launch V∞: [5.460667504532515, -8.669436228084356, -2.00974235054902] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.093522022636416, -0.03898497509412462, 0.08343958022624834] km/s
+ V∞_out: [-0.07591102776124158, -0.032982618053918646, -0.1019063840188087] km/s
+ time of flight: 1.034581199622097e8 seconds
+ arrival date: 2026-08-03T02:18:31.150
+ thrust profile: [0.8978071902296176 -0.70890035433184 -0.4931825011939288; 0.42740760498983116 -0.10504382756058955 -0.39977192951901175; 0.15704151934747568 -0.005081466769059337 -0.2177078264191571; 0.07069163111294159 0.0061008049737435125 -0.12763570676735694; 0.03292907707483025 0.005445603490086278 -0.07267084255638585; 0.021728299494833146 0.004937661429599367 -0.054276507959451825; 0.05337234669427278 0.013274774498164782 -0.13632481032743396; 0.009932712663590472 0.002800848735275518 -0.026063152748382584; 0.014027341030663667 0.00503286175362187 -0.038809167523222124; 0.00982571523101766 0.000841999337579725 -0.02920680312841346; 6.444324492516947e-5 -5.084139972769385e-6 -0.0005717398983189048; 9.528936354671712e-5 8.381964740069179e-5 -0.00023013736600277458; 7.358708882106369e-5 4.017140023845433e-5 -0.0001982611280793938; -4.1581925903959285e-5 0.00025336235013034706 -0.0004033317474319959; -0.00018550833690804283 -3.7566760171901215e-5 -0.0005755069616910969; 7.701162999035482e-5 1.848822420567383e-5 -0.00028140469322954063; -3.906398283599834e-5 -8.865953053237855e-5 -7.241439066182207e-5; 0.0005574407404513977 7.994682084833122e-5 -0.0006845342394529033; -8.439613396007235e-5 -3.0403254183948764e-5 0.00020583242041568185; -6.913268891285207e-5 -1.0802343679127958e-5 -0.00017065750496401727] %
+
+Mass Used: 108.95299166937684 kg
+Launch C3: 109.01707842346917 km²/s²
+||V∞_in||: 0.13125684953338 km/s
diff --git a/archive/ES_0.6385693777913546 b/archive/ES_0.6385693777913546
new file mode 100644
index 0000000..547806f
--- /dev/null
+++ b/archive/ES_0.6385693777913546
@@ -0,0 +1,22 @@
+archive/ES_0.6385693777913546---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T07:30:07.846
+Launch V∞: [7.251981215162856, -7.5255223080276785, -2.2658620402081984] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013396302779063608, -0.008955645684183234, -0.027737337740254105] km/s
+ V∞_out: [-0.004817496813443054, -0.03168318877521525, -0.0013897022040454783] km/s
+ time of flight: 1.0379154756877361e8 seconds
+ arrival date: 2027-08-22T14:29:14.846
+ thrust profile: [0.5720119368611363 -0.28165717443939287 -0.30983246130274966; 0.18117547001446618 -0.00967806265303234 -0.19823728492328868; 0.14181657772863504 0.019385616573418293 -0.2274258926520463; 0.08909553899814579 0.022096939270487052 -0.18734810151904646; 0.04777519084963486 0.015697170748769498 -0.1179863353334054; 0.026023408050521772 0.009923788490358165 -0.0774399937460102; 0.02107626477542639 0.008186157205352103 -0.06936118857529296; 0.007297058187946782 0.0034852580707649882 -0.027505517397484566; 0.009583427858439351 0.004597332709215299 -0.04044922136927759; 0.003270454121119142 0.001359829894200068 -0.01697590321522952; 0.0041592746390571745 0.0008723244596714214 -0.018599341860070107; -8.574700350050214e-5 0.00023618845675794356 -0.001362531762724078; 0.0011964210838726192 0.000991507962324624 -0.001314744549276813; 0.0009502944264150007 0.0001861383646331766 0.0017988679743168486; -0.005323436330805714 -0.0037964327019235134 0.007725858800071148; 0.003031609587077143 0.001269470109745902 -0.0036308686070235575; 0.003757608706142466 -0.0014004519367491262 0.0019950243434732604; -0.004708978149584169 -0.003926224754526728 -0.0006104265472774129; 0.0010340790963073944 -0.0010335144805593485 -0.004353999567490798; 0.0025553402831633445 0.0013705247138443167 -0.002587017169858983] %
+
+Mass Used: 77.90432544601754 kg
+Launch C3: 114.35884833895362 km²/s²
+||V∞_in||: 0.032078410538645796 km/s
diff --git a/archive/ES_0.6386359873242947 b/archive/ES_0.6386359873242947
new file mode 100644
index 0000000..9f0e06e
--- /dev/null
+++ b/archive/ES_0.6386359873242947
@@ -0,0 +1,22 @@
+archive/ES_0.6386359873242947---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T13:34:13.684
+Launch V∞: [5.59992838977432, -8.713682880175526, -2.157823149710712] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4146364707181254e-5, -1.162047562361014e-5, 2.2838681920237018e-5] km/s
+ V∞_out: [2.044132976253767e-5, 1.90228978667448e-5, 8.784649408239224e-6] km/s
+ time of flight: 1.0452168892786846e8 seconds
+ arrival date: 2026-08-15T07:22:21.684
+ thrust profile: [0.6063440131571218 -0.4673842218685536 -0.3549711014363349; 0.33825369300239716 -0.07872597486108103 -0.3369294343640745; 0.1662910580128762 -0.004144638968461731 -0.23866490008794647; 0.06762065800317085 0.005924357380955664 -0.12295497989891924; 0.03187144712078594 0.004344420549029251 -0.07434085859098706; 0.04563086453679867 0.009899009418737894 -0.11156580451777941; 0.009082793150065825 0.002293563855464224 -0.028054402952184587; 0.04834800157598571 0.014401710851998456 -0.13461235081169257; 0.002717985303667277 0.0010622487573373643 -0.008873855366504426; 3.123248966562962e-5 0.004714996430610947 -0.007700377981415674; 0.001057189618207301 -2.319777839825208e-5 -0.006485371705867633; 0.0012511353117566329 0.0005985112375641737 -0.004612171880282614; 0.0034467178021916436 -0.003257120432633073 -0.003723854791230829; 0.0033695881025881955 -0.0008792305696695493 -0.008439538104906328; 0.004621323919248839 0.001931146089813856 -0.009015304733692248; 0.0027990491507613436 -0.0002403993391858299 -0.004214145162523631; -0.006119797307870727 -0.004828758193719413 0.0011968879320738844; -0.0014308643385095208 5.324374331107245e-5 0.0029353561607031392; 0.0004974270534256944 -0.0007961255412163341 0.004115184701729875; -0.0013165934749154095 -8.279013821287443e-5 -0.0016989413448285575] %
+
+Mass Used: 92.07058823997431 kg
+Launch C3: 111.94366805229191 km²/s²
+||V∞_in||: 2.9270471127080652e-5 km/s
diff --git a/archive/ES_0.6389156899696262 b/archive/ES_0.6389156899696262
new file mode 100644
index 0000000..94e38dc
--- /dev/null
+++ b/archive/ES_0.6389156899696262
@@ -0,0 +1,22 @@
+archive/ES_0.6389156899696262---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T21:27:51.336
+Launch V∞: [5.5197412007307864, -8.818540938867452, -2.1972046045721094] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.08368552181416823, -0.026677412414506746, 0.058611220699012964] km/s
+ V∞_out: [-0.069268255414911, -0.031471698194994145, -0.07323800821485484] km/s
+ time of flight: 1.0601083191471799e8 seconds
+ arrival date: 2026-09-02T20:55:02.336
+ thrust profile: [0.5017052314903369 -0.3924459547210473 -0.3106317424210325; 0.1962765720985247 -0.0486873213112676 -0.21624555529851147; 0.11952261444409179 -0.005708162166705325 -0.18588651186103808; 0.08703217330894626 0.005205479736576204 -0.16998182709237153; 0.057526142984217765 0.0076617523267707415 -0.1360551385305403; 0.051798644593135545 0.008915747075714393 -0.1339638621043007; 0.034120180671170265 0.006907554667231069 -0.09972262397888426; 0.009245876273248526 -0.0003742906537485583 -0.021749564828182587; 0.002176670323973076 0.0012041487306144872 -0.005743661002403027; 0.002736132880009959 -0.0010557955677738856 -0.0005365458111925847; 0.0017874536207701007 0.011371555420296112 0.005210694541796118; -0.0039926314071677795 -0.001627697182513903 0.0023825874049376717; -0.002999025139249719 -0.0012496032462148924 -0.008204303200134763; -0.0005658470332159747 0.0034296606205130083 -0.0027706828728579435; -0.017363910206655876 -0.008111591510783807 -0.013173296429622358; -0.0031958179870377385 -0.0028530559152287697 0.0029262809357885407; 0.01793190006468404 -0.00901422312116172 -0.02965159870117034; 0.006094716669003412 0.006707118481995865 -0.023056597460784062; -0.021193828239129117 -0.018938584827686657 -0.021508902065245066; 0.015089189143837212 -0.02067015590523274 0.018625284972853817] %
+
+Mass Used: 85.87379911860262 kg
+Launch C3: 113.06191528787907 km²/s²
+||V∞_in||: 0.10559463095381182 km/s
diff --git a/archive/ES_0.6389703000558955 b/archive/ES_0.6389703000558955
new file mode 100644
index 0000000..f8ff8d1
--- /dev/null
+++ b/archive/ES_0.6389703000558955
@@ -0,0 +1,22 @@
+archive/ES_0.6389703000558955---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T17:13:16.694
+Launch V∞: [5.54208378823569, -8.81069708994911, -2.1245216106461395] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00016501286655528372, -8.307127596188176e-5, -0.0001480248923068756] km/s
+ V∞_out: [6.871906981284671e-5, -0.00015257186125209959, 0.00016744703381863906] km/s
+ time of flight: 1.0358213999934444e8 seconds
+ arrival date: 2026-08-05T14:02:15.694
+ thrust profile: [0.6012756863698142 -0.4755478332653828 -0.36132065142349007; 0.2882897567947109 -0.0743783709996493 -0.29901894546939944; 0.18560905996747282 -0.010206933412388446 -0.27220135540868884; 0.100807082827623 0.005984781785700649 -0.1908327485310513; 0.03127047401144991 0.00404430186568206 -0.072306162139094; 0.021185764294981188 0.00391092520353696 -0.05557210151785518; 0.013339991681812218 0.0026820719507609438 -0.03807029375604108; 0.013914261127789408 0.0037598772210041343 -0.0422109595645263; 0.006052734774243204 0.0017368478458283203 -0.020818989784913686; 0.011109540975404201 0.003040404882120947 -0.03761214901866845; 0.0005102796557171606 0.0003635296824101305 -0.000648886398815146; 0.0008502541561310757 -0.0004116583038957604 -0.001830559647800079; 0.0011682054832897722 0.0006992766562433582 -0.0019842899269410103; 0.000287813960416611 0.000171067525165991 -0.0018041586232467116; 2.0609272102477478e-5 -0.0003485830640410088 -0.0012712144842182839; -0.00045861609875647957 -0.0001600725856456613 0.00034221671497346; 0.0010824857420811923 -0.0011661723728762616 -0.0014363275586136532; 7.241319180752647e-5 -0.00042344983054037454 -0.0001587804563997695; 0.00032565994997643937 4.879275727156607e-5 -0.0008132261115724926; -9.221972774172717e-5 -8.730055165128998e-5 0.0003992000997389399] %
+
+Mass Used: 87.1347867274153 kg
+Launch C3: 112.85666800076504 km²/s²
+||V∞_in||: 0.00023673075795339546 km/s
diff --git a/archive/ES_0.6392167012601737 b/archive/ES_0.6392167012601737
new file mode 100644
index 0000000..04ad04b
--- /dev/null
+++ b/archive/ES_0.6392167012601737
@@ -0,0 +1,22 @@
+archive/ES_0.6392167012601737---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:25:45.724
+Launch V∞: [7.280061783056182, -7.570660237436771, -2.357991300276621] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0014871495924340806, -0.007822695497584523, 0.006575877202495587] km/s
+ V∞_out: [0.0026531067561072837, 0.004103836372155042, -0.009096432894116978] km/s
+ time of flight: 1.0335598193627316e8 seconds
+ arrival date: 2027-08-18T05:25:26.724
+ thrust profile: [0.5557287897862195 -0.28710862616012 -0.32861211571601; 0.14541121915579774 -0.011259511551564901 -0.1728097612414967; 0.06960691044044406 0.007229588113324386 -0.12402291380118206; 0.052947656077854066 0.010613039264819792 -0.12272064096933948; 0.03693285669928033 0.009856904642295588 -0.10182109548509888; 0.05852717452072546 0.018100819941120803 -0.17483248991709477; 0.03650713914203842 0.011647161992133255 -0.12125553869000817; 0.004470097584542942 0.00179928740315426 -0.01762298373052958; 0.005018587379676022 0.0013687746457053242 -0.014273405164758377; 0.0021851308748462683 0.0009340620892572023 -0.00861691523715418; -0.0009748725145063541 -0.0016111178416267993 -0.001551913321877544; 0.0009317068312866516 0.0017605169013949333 -0.0014767448724161383; -0.0003930585638976118 -0.00012262045573408202 -0.000687618700724069; 0.0008394750568674837 0.0008152671721842605 -0.0006676771355912433; -0.003734054773492338 0.0007891432447082864 -0.0008207064212481746; 0.0004676910025135546 0.0007596848434288033 -0.00040960924423435866; -0.0002617977809696063 -0.000997724009340407 -0.0038628781169408287; 0.0009239193667797015 0.000585386011369278 -0.0014435981908104759; -0.003246852394091076 -0.0019285361658294784 -7.001900366710562e-5; 0.0002040398834808393 -0.0017212260588339969 0.0013061097846144626] %
+
+Mass Used: 69.8192908235269 kg
+Launch C3: 115.87431896800156 km²/s²
+||V∞_in||: 0.010327068303275002 km/s
diff --git a/archive/ES_0.6392171118445151 b/archive/ES_0.6392171118445151
new file mode 100644
index 0000000..a87d1e7
--- /dev/null
+++ b/archive/ES_0.6392171118445151
@@ -0,0 +1,22 @@
+archive/ES_0.6392171118445151---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:57:54.650
+Launch V∞: [7.221734145211493, -7.499271148017723, -2.2881051990379833] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0014315836020733672, -0.008693676726313472, 0.007738735481295503] km/s
+ V∞_out: [0.0033799963987564113, 0.004740842391762185, -0.010180843061135642] km/s
+ time of flight: 1.031710442425714e8 seconds
+ arrival date: 2027-08-15T09:35:18.650
+ thrust profile: [0.7265772328346005 -0.37013724699689354 -0.3660534773555644; 0.23119392591424806 -0.014184125431307495 -0.23763572541141037; 0.0658478845073662 0.008910184035438366 -0.11694324256175659; 0.06565473479389815 0.019512893903954446 -0.145418770348245; 0.06939697572635357 0.01669606536643426 -0.16421277503355278; 0.040173480149126944 0.013914239318103672 -0.1221054695973037; 0.01855646946355524 0.008375884490585258 -0.0647660223523825; 0.014483509497522053 0.005787230600656969 -0.05295848088945668; 0.004091435919651241 0.0021154210719596727 -0.0133424076610954; 0.005689766705328764 0.0021865721121333997 -0.01981835585989157; -0.0009914445853404575 0.00036647160734337356 -0.0007690567989545906; -0.00029988244127247604 0.0008147153144849497 0.0014883557941125984; 0.0032415717598764156 -0.001651359646797999 -0.0014091708569348277; 0.0030329256697448352 0.0004624932595561571 -0.00011128826835848232; 0.0008452456519581174 -0.001185767820217989 -0.0025390036393769817; -0.0007373520656218761 0.002452966130665921 0.005376787351670629; 0.0012087870183623377 0.002128704534702381 0.0021212649382805196; -0.0008788539866174459 -0.002783661884668592 0.004102211811800564; -0.0012579202366012027 -0.0007768663821866873 0.0020159708682989438; 0.00017613913360996366 1.2374945771739679e-5 -0.0016284843090278102] %
+
+Mass Used: 82.92366338336342 kg
+Launch C3: 113.62793721746928 km²/s²
+||V∞_in||: 0.011726784447615289 km/s
diff --git a/archive/ES_0.6394619560747112 b/archive/ES_0.6394619560747112
new file mode 100644
index 0000000..ed5d81e
--- /dev/null
+++ b/archive/ES_0.6394619560747112
@@ -0,0 +1,22 @@
+archive/ES_0.6394619560747112---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T05:13:08.398
+Launch V∞: [5.5514865739075585, -8.854889554149125, -2.2497918640639387] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.04652430046224495, -0.01887614711558907, 0.04195441272738337] km/s
+ V∞_out: [0.03268870034229722, -0.049221418866777014, -0.03660160565179015] km/s
+ time of flight: 1.0439803510821712e8 seconds
+ arrival date: 2026-08-15T12:40:23.398
+ thrust profile: [0.5033493491091653 -0.39902538479430216 -0.3259671465608591; 0.22740779008226453 -0.05987171234254591 -0.2598938570060932; 0.1304445298082113 -0.008650938590313868 -0.21170155709337254; 0.09048917426356888 0.0036179469634899887 -0.18492113011538439; 0.0476570316361535 0.005008487747094898 -0.11576868704149833; 0.022540055261876576 0.0035867575046928954 -0.06201505350672197; 0.012755105935514727 0.002562136860839937 -0.040253574665788085; 0.0019215958378502786 0.0008326784028475425 -0.017344539808619535; 0.007517813769631114 0.002723883503884601 -0.029601869620585954; -0.00029821846276244235 -0.0015410156909694518 -0.003426583485016294; -0.00017932489297342938 -5.8627935903748495e-5 -0.004372504372454269; 0.0015836833856199212 -0.00194181969433809 -0.0036865108227648307; 0.007172851218241417 0.012572604012503926 -0.01176926952585447; -0.002189088147253576 0.006927850915498203 -0.0003235169176307121; 0.002000194076138689 0.0015966048318197862 0.0008406709027254768; -0.0012401049666516336 -0.003423831881257269 -0.0057740692644894995; 9.80740373733289e-5 -0.00016217284153380697 -0.0032082440742526603; 0.019542774622274106 0.006697277184086538 0.0005288799618768502; -0.0026479273692958504 -0.008764863535219415 0.016247611166866512; -0.0019927802739768976 -0.0017506129231353678 -0.010564922123103837] %
+
+Mass Used: 79.34940759012625 kg
+Launch C3: 114.28963562806346 km²/s²
+||V∞_in||: 0.0654292916875174 km/s
diff --git a/archive/ES_0.6395404574451427 b/archive/ES_0.6395404574451427
new file mode 100644
index 0000000..6a1bab4
--- /dev/null
+++ b/archive/ES_0.6395404574451427
@@ -0,0 +1,22 @@
+archive/ES_0.6395404574451427---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T17:03:50.360
+Launch V∞: [7.313491592802704, -7.533656672953613, -2.6746249999517837] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.4275403628428314e-5, -4.2875164348654144e-5, 3.2641651668140784e-5] km/s
+ V∞_out: [5.499306702643179e-5, -3.323085452367005e-5, -2.7135833932337865e-5] km/s
+ time of flight: 1.0265360564075133e8 seconds
+ arrival date: 2027-08-09T19:57:15.360
+ thrust profile: [0.5287624444298812 -0.2665574281357208 -0.30447767721271757; 0.2271391902123482 -0.012871610208954542 -0.2498913695663258; 0.09661230754544368 0.013138871678403177 -0.16461443085454774; 0.03550205652429336 0.008523891980159013 -0.08026245456103258; 0.031335370739495015 0.009840849219787005 -0.0846738599570083; 0.019530477444559633 0.007155283375337978 -0.060605593778642455; 0.006567913698783241 0.002607696193336615 -0.023190758368546855; 0.003705782677425856 0.0014818655644316444 -0.014000328234857933; 0.0034479458750077585 0.0014721050943931092 -0.013789944084147491; 0.0006966612948722255 5.1040043059632736e-5 -0.0011345901734461255; -3.565081189332918e-5 -0.00024737878646923916 -0.0007744016126855675; -0.00018191080279936916 9.598603006225096e-5 -0.0016326305484777824; 0.00016203195407409385 8.224751083990286e-5 -0.0009555699679074874; -8.930177732616523e-5 0.00020632089997702055 -5.539565366950705e-5; 1.3407247872129345e-5 7.049052371428677e-5 -0.00024071276534117918; -0.00019961877125023236 -0.00020491978214413393 -0.00034993297061517906; -0.00015336203979860168 -7.85801271829138e-5 -0.0003029860655058081; -0.0001723585267175022 -7.928903931800409e-5 0.0006157470490483439; 0.0003545823217069296 0.0001104952119683541 -0.0006442601995896829; -0.001264504146954962 0.0004107527300173236 0.000254049187186399] %
+
+Mass Used: 61.31609431924153 kg
+Launch C3: 117.39676103430142 km²/s²
+||V∞_in||: 6.974287424539215e-5 km/s
diff --git a/archive/ES_0.639727192789316 b/archive/ES_0.639727192789316
new file mode 100644
index 0000000..b0e709b
--- /dev/null
+++ b/archive/ES_0.639727192789316
@@ -0,0 +1,22 @@
+archive/ES_0.639727192789316---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T17:33:33.332
+Launch V∞: [7.343782988959307, -7.351004023157047, -1.7981895137253119] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.25708163735197626, -1.2074879733450843, -1.6892336239446062] km/s
+ V∞_out: [0.782126028369143, 0.3732795907923545, 1.9076268978699973] km/s
+ time of flight: 1.0440630097754923e8 seconds
+ arrival date: 2027-08-27T03:18:33.332
+ thrust profile: [0.49350897525403886 -0.23354918176003325 -0.25915641441240267; 0.3377513728723303 -0.0050283842237423704 -0.33026092535643636; 0.2012163978823817 0.03812710594101661 -0.2906136087749346; 0.14496611309990448 0.045702880971395875 -0.2689930079180943; 0.07271111091847328 0.027866230751217302 -0.16581159253552852; 0.06288417587223971 0.028526282508004156 -0.1649941954243617; 0.026280362946477707 0.013010383322725286 -0.07617969831042633; 0.02123564466806452 0.011219494447353416 -0.06650138252287473; 0.007710113016155386 0.004277032505783759 -0.024691997288138222; 0.0005861568793038292 0.00023620838537229786 -0.00023125361936939806; 0.0001887850894243427 -0.000395839620843179 -0.005894259433616872; 0.0010204621720964245 -0.0008937401348828164 -0.0036482172457028748; 0.008030799349029177 -0.0011768609505126283 -0.0020153020943686544; -0.004660875846921051 0.0007308804056154201 -0.0008842831865023373; 0.0008657547807207642 0.0021188475313515254 -0.0046271535191665806; -0.003596850000766841 0.00018520336074744916 -0.00616655128292687; 0.004308510558792553 0.0028538021493508306 -0.0006277827431638685; 0.0004913914265836704 0.00036072663034277875 0.005938024160723316; -0.011667517460149091 0.004492850656899303 0.0032069324307732465; -0.005341311513105598 -0.0007905294288573309 -0.005128709981421495] %
+
+Mass Used: 97.67067504362194 kg
+Launch C3: 111.20189426467086 km²/s²
+||V∞_in||: 2.0922782822324613 km/s
diff --git a/archive/ES_0.6397798113103933 b/archive/ES_0.6397798113103933
new file mode 100644
index 0000000..fa6b80e
--- /dev/null
+++ b/archive/ES_0.6397798113103933
@@ -0,0 +1,22 @@
+archive/ES_0.6397798113103933---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:20:37.530
+Launch V∞: [7.306403449382657, -7.5172576671338165, -2.369234292317667] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01619123158956564, -0.010813701297497005, -0.03472520782396455] km/s
+ V∞_out: [-0.006044681871529026, -0.039338714785693424, -0.0016853655751257457] km/s
+ time of flight: 1.0433947939468999e8 seconds
+ arrival date: 2027-08-28T20:31:56.530
+ thrust profile: [0.45141427089623437 -0.22462451364036717 -0.2553868472930192; 0.14605476072221737 -0.008546681604963286 -0.16006150777912803; 0.09458490154733708 0.01216756533113526 -0.15297624196263512; 0.11804366201913458 0.02785875455463677 -0.24420897253451757; 0.07564869644952182 0.022924785601743436 -0.1883140094481662; 0.04275078263792562 0.014902229871850314 -0.12070322134164556; 0.004009764983383543 -9.641013943211137e-5 -0.013463440590103905; 0.004978554530615051 0.0011042760853361678 -0.01134361906202901; 0.0029769539708229854 -0.0003704354810450123 -0.008767804668666484; -0.0029456051740471886 0.009265177211308635 -0.003454339631285969; -0.0009298035119040681 -0.00400262550520291 -0.009524240951397325; 0.0038711290320675674 4.764645303443086e-5 -0.006457936418381739; 0.0022450986525173974 0.0008187603327041065 -0.0006263863733643315; -0.0001855744440269845 0.004238678699360384 -0.003178203180850125; 0.013887047599262282 0.0037593975877986993 -0.008326259145196331; -0.01160359904553699 -0.007308203906267597 -0.0028682230798855973; 0.009539444536330897 -0.025788741068227355 -0.012324032817603756; 0.00019786851771479857 0.025082405843485915 -0.0030118579570079886; 0.002114605325944881 -0.005525355780290022 -0.0013496704481266637; -0.004439870347545449 -0.006284256912072374 0.014078781106924851] %
+
+Mass Used: 72.62498209721844 kg
+Launch C3: 115.50596533112693 km²/s²
+||V∞_in||: 0.0398112066453149 km/s
diff --git a/archive/ES_0.6399672091656989 b/archive/ES_0.6399672091656989
new file mode 100644
index 0000000..20d2e8d
--- /dev/null
+++ b/archive/ES_0.6399672091656989
@@ -0,0 +1,22 @@
+archive/ES_0.6399672091656989---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T02:11:52.393
+Launch V∞: [7.36635191856433, -7.118817607074705, -1.9722436842818047] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011204917969129806, -0.017270323431724615, -0.007023457856694601] km/s
+ V∞_out: [-0.01335681520751432, 0.015039882756654837, -0.008328761084906449] km/s
+ time of flight: 1.0531058942558977e8 seconds
+ arrival date: 2027-09-03T23:08:21.393
+ thrust profile: [0.7539834684070387 -0.3404509055202086 -0.3431072964580248; 0.4104990091098688 0.012583567525569486 -0.3500210275565169; 0.201841185094596 0.050484832781954876 -0.2595192584122504; 0.1047249600546336 0.042421248154364564 -0.17897728630015577; 0.12562742237453256 0.07587844595953822 -0.25232859354201886; 0.054633991418384195 0.030857310343856862 -0.12881552631508564; 0.023318407893996054 0.014159786731192543 -0.06600792127287541; 0.032695969499372944 0.0216219280012926 -0.08979841987965055; 0.01509975854373983 0.011008435040434583 -0.047823051037593524; 0.0038131149508552962 0.0028734931457480434 -0.012575404320154297; 0.00013399147903705113 -0.0012526636996768752 7.290799559425839e-5; -0.001098370506108827 0.00022798561542954803 0.00019233244245328736; -7.719304082274599e-5 0.0006964114614259001 0.0005770776635592185; 0.0002706094938889353 0.000305863396904728 -0.0012349114182952348; -0.002559035516644989 0.00123907271141633 0.000289733963763311; -0.00012392116132350364 -0.0010551298659811485 0.0017241409855169218; 0.000784195891077456 -0.0009193995640495534 -0.0008312655046201138; -0.0015154956009142172 -0.0014306817593855207 -0.0005655528100642862; -0.0011059348714948809 0.00010683824045616713 -0.0013241090059777708; 0.0010108100939938316 -0.0015252966178456527 0.0007797227323736541] %
+
+Mass Used: 111.78411983676642 kg
+Launch C3: 108.83044986112269 km²/s²
+||V∞_in||: 0.02175185551616389 km/s
diff --git a/archive/ES_0.6399928396689094 b/archive/ES_0.6399928396689094
new file mode 100644
index 0000000..953f8dd
--- /dev/null
+++ b/archive/ES_0.6399928396689094
@@ -0,0 +1,22 @@
+archive/ES_0.6399928396689094---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T22:09:22.409
+Launch V∞: [7.104764764806629, -7.501360442381106, -2.4061581724304753] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.06413076378031075, -0.2841596412332386, -0.47723061724743043] km/s
+ V∞_out: [0.1748264769676494, 0.08199165516932007, 0.5305270543125051] km/s
+ time of flight: 1.0343079690011168e8 seconds
+ arrival date: 2027-08-19T00:55:58.409
+ thrust profile: [1.0 -0.5472858187763153 -0.5682097146425757; 0.13517995569919478 -0.007647354433998667 -0.1564594292829399; 0.0564394448091932 0.005135243026698321 -0.09628592538705155; 0.04925882010813094 0.00989250971534181 -0.1113404276830967; 0.035902526608781134 0.00865249173440687 -0.09209439904076755; 0.027185088399229475 0.007837551006187025 -0.08292521620561133; 0.01948868666988035 0.0031295202924654917 -0.061092827717697314; 0.0034045936515255133 0.003492019005844974 -0.021164319880452268; -0.0009496198568587108 -0.0011529792571563836 -0.027076651538296033; 0.008539272155693625 0.00331596561785639 -0.03656371054530466; -0.0016515710478839998 -0.0006891950388333686 -0.0032265048588490577; -0.006800354788610324 0.008118139313851285 -0.016195792081369773; -0.003079467166086092 0.001106802704112897 -0.011646271253877615; 0.005168994044209997 0.005142622276805581 -0.013039344580445287; 0.0049689735990414785 0.01090968584760723 -0.004410398792136967; 0.002997512756236813 0.0015565082811343162 -0.015427885863858924; 0.01416809396255966 0.01248458387333928 -0.0009347024211431645; -0.013465564540197516 -0.012058128350402895 0.0024921499978176453; 0.0022494513775018 0.004457032646441996 -0.0030792786722686604; 0.002094895598723391 0.015846025466641902 0.0017059437649633697] %
+
+Mass Used: 90.18846627740868 kg
+Launch C3: 112.53768800051182 km²/s²
+||V∞_in||: 0.5591140479430045 km/s
diff --git a/archive/ES_0.6401340748600136 b/archive/ES_0.6401340748600136
new file mode 100644
index 0000000..fd6b488
--- /dev/null
+++ b/archive/ES_0.6401340748600136
@@ -0,0 +1,22 @@
+archive/ES_0.6401340748600136---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T19:51:37.281
+Launch V∞: [7.2810833591993385, -7.282005364683048, -2.2345940609450423] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.821472309608019e-6, -4.729222314027425e-5, 6.280352859110397e-6] km/s
+ V∞_out: [-6.711530760704573e-6, 3.030826535478928e-5, 3.6426510712692995e-5] km/s
+ time of flight: 1.0384475926340437e8 seconds
+ arrival date: 2027-08-20T17:37:36.281
+ thrust profile: [0.7458669086736448 -0.3659090002221249 -0.3904868706416344; 0.38908449189156064 -0.0205771332953384 -0.39359850335563873; 0.18741613912452051 0.02812489874425079 -0.2737187437840481; 0.1077452477118217 0.029716168809991707 -0.1979124911481328; 0.042663293140529114 0.018837329841919267 -0.08813790505539644; 0.01068655305287522 -0.0009830911421497912 -0.019416690384267868; 0.00738540624050569 0.004405591452340429 -0.030234471452306018; 0.009930050981404311 0.00521856782458911 -0.03199174700383081; 0.009677861717645678 0.005439324007519399 -0.034644684472493234; 0.006527732482732919 0.003951677733756884 -0.02053033709624918; 0.0025544229341792103 0.0006870226894287778 -0.0090408437626948; -0.0029469660337208773 0.00085511631026732 -0.0010742779255764714; 0.002966183858193007 -0.0058696501986009115 0.0001279937557410963; 0.005669601819480653 0.000433878073314976 -0.021236326254929147; 0.0014283072303085584 -0.005879983115365332 -0.009307535995924397; 0.0039627745894449794 0.004398543358400551 -0.006444093119591197; -0.009155834056416734 -0.0071122368746181774 -0.004325277200401245; 0.0012432041118161305 0.0001561428264228405 -0.003657674523742215; 0.00459317169782296 -0.0047613887923827584 -0.003359951008004433; 0.008690553377825786 -0.014951267305851109 0.030145194021296444] %
+
+Mass Used: 99.11782614947288 kg
+Launch C3: 111.03518763209307 km²/s²
+||V∞_in||: 4.786022202411443e-5 km/s
diff --git a/archive/ES_0.6402071089339856 b/archive/ES_0.6402071089339856
new file mode 100644
index 0000000..1e45a3b
--- /dev/null
+++ b/archive/ES_0.6402071089339856
@@ -0,0 +1,22 @@
+archive/ES_0.6402071089339856---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T21:59:55.595
+Launch V∞: [7.280817245198431, -7.299440279029123, -1.4591005279004658] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.16468283968148617, -0.8223995140554793, -1.2524177293064689] km/s
+ V∞_out: [0.3880397137473074, 0.39719194355092785, 1.4126865492014749] km/s
+ time of flight: 1.0443322825705612e8 seconds
+ arrival date: 2027-08-26T15:13:43.595
+ thrust profile: [0.6336245209726344 -0.29910732990112004 -0.31666859608817055; 0.39941387605223466 -0.00515857171813697 -0.37760962008942756; 0.2447322621597683 0.04688239130540107 -0.3350456386629171; 0.16016574031400038 0.048978534638791406 -0.28107323498691505; 0.12595353108277588 0.04859733148969786 -0.26410800816552094; 0.06251322049559552 0.02697278433011812 -0.1500804295434161; 0.032121208249886804 0.015287524005979885 -0.08603924494741812; 0.01611453957158236 0.008172177631329134 -0.047366025178637805; 0.008341362812599997 0.004462463884717296 -0.023860916434962475; 0.0021576040773709877 -0.0028091011299791937 -0.006213520389729202; 4.103154921423726e-5 -0.0004146918765616192 -0.001393481377862021; 0.008776873875507603 0.0034221879366412144 -0.011210082943019218; -0.0010446845317542083 0.0036635297798675278 -0.0018028154523247143; 0.004363481208310268 -0.001074862630431391 -0.004097544760362251; 0.0009628261418318695 -0.0020945058108351663 -0.0017310841777668819; -0.006117321787228329 -0.0005427373049026366 5.8900605883630236e-5; 0.003700127811149069 0.0022798672570879686 -0.005074838320802819; -0.0022892667588915745 -0.0036932964571092814 -0.0029193938295135596; -0.0015194069993460253 0.00040273227440006717 3.8576286707777546e-5; 0.0005053901366318483 -0.0007980408239857324 0.0017778936068100827] %
+
+Mass Used: 114.45186253191878 kg
+Launch C3: 108.42110249561104 km²/s²
+||V∞_in||: 1.5073193314906494 km/s
diff --git a/archive/ES_0.6403779135440479 b/archive/ES_0.6403779135440479
new file mode 100644
index 0000000..2a72d05
--- /dev/null
+++ b/archive/ES_0.6403779135440479
@@ -0,0 +1,22 @@
+archive/ES_0.6403779135440479---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T15:21:34.753
+Launch V∞: [7.075535334332883, -7.717296359847037, -2.418479635268792] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.16914295211575298, -0.8550976200528716, -1.298896385183228] km/s
+ V∞_out: [0.7423429210541358, 0.316169788108376, 1.3398721951805526] km/s
+ time of flight: 1.0280082086899102e8 seconds
+ arrival date: 2027-08-13T11:08:34.753
+ thrust profile: [0.7674825477495968 -0.4187186920415963 -0.46748702404151304; 0.21732150144619106 -0.027750427143893093 -0.263106277752172; 0.05490028643642201 0.0022003305835039313 -0.1024176366486881; 0.04907755318067111 0.005934957585304626 -0.11858511389774568; 0.034902561483129924 0.005898892956233376 -0.10144030417110661; 0.00973829895941773 0.002204458315998469 -0.03450069480222262; 0.004745207787902109 -0.0004034237455440606 -0.018717443810154572; 0.0020419421732629246 -0.00044749857576064365 -0.012058380762974264; 0.0007794291109171519 0.0012191214782150352 -0.004042435816321638; 0.002710268898107885 0.0030430149066632863 -0.01313215794767145; 0.00023962787087408085 -0.00022145117868503685 -0.0013637293053791084; 0.0008281529678125501 0.00010832272926734509 -0.0011875207641789765; 0.0004694740828519396 0.0003329773480458783 0.00035615171237385335; 0.0005314622848825669 -0.0004190473557307186 -0.007652287286537086; 0.00014558367723071418 0.00012374086529144072 -1.5714214318849782e-5; -0.0010043283251760131 0.0009264937855622477 -0.0007962760337748493; -0.0006246221602380873 0.0026314461338296357 -0.001038957291564473; 0.004203427086181531 -0.0020479319467280816 0.001231464967681189; 0.0018190144208695387 -0.001771350955091389 -0.000463170730060972; -0.0006663215240486699 -0.00030882358273777026 0.0016064224405814825] %
+
+Mass Used: 73.53894093873987 kg
+Launch C3: 115.46890711931133 km²/s²
+||V∞_in||: 1.5642675914026263 km/s
diff --git a/archive/ES_0.6407473237541413 b/archive/ES_0.6407473237541413
new file mode 100644
index 0000000..b43613d
--- /dev/null
+++ b/archive/ES_0.6407473237541413
@@ -0,0 +1,22 @@
+archive/ES_0.6407473237541413---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T05:14:05.271
+Launch V∞: [6.927559417952332, -7.569090516085685, -2.2821731052152496] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.015904314007761697, -0.02836591783100673, -0.038337229661424] km/s
+ V∞_out: [-0.043855442956137504, -0.009183353291864794, 0.022805327900470938] km/s
+ time of flight: 1.057960919728773e8 seconds
+ arrival date: 2027-09-15T17:02:16.271
+ thrust profile: [0.9237064659278043 -0.4619403771759089 -0.4853047668353974; 0.28137249720630453 -0.0255921381058225 -0.32711071439035005; 0.092924833614247 0.007382162301767951 -0.1725318017719568; 0.03694890755060943 0.005361486502024985 -0.09299026054602566; 0.034768658416956755 0.008370166781338109 -0.09986375406891529; 0.030723979365410464 0.01195823407506496 -0.10819513406386749; 0.003916571878015246 0.001765948779465983 -0.027672181887341905; 0.0011352105315345679 -0.0013912245754593095 -0.01626018089782727; -0.00099208683971788 -0.0018946989164626126 -0.0006130918556220208; -0.000739826992278524 -0.0035949412221354757 -0.004377842444694566; 0.0035908741793515223 0.023616008769999305 -0.022691139587619757; 0.005645989149442397 -0.002720553598768807 -0.004470752118123034; -0.002768095226340719 0.005783000708152421 -0.00253159971431767; 0.018017589795407293 0.0012579929774273512 -0.005883103277170013; 0.010238272042121074 -0.006138186545011755 0.005510960427473659; 0.008957821026866038 0.0034771473582216874 0.008384531777654006; 0.061263552455379254 -0.005195526839896145 0.03663320445704438; -0.0012310360092760639 -0.012549708834903939 0.0374209805234175; -0.06189709266413512 0.042604584260536205 -0.025680191863109995; 0.009368065093087559 -0.01108584280196948 0.015443457167088934] %
+
+Mass Used: 103.01048297576244 kg
+Launch C3: 110.49052481212614 km²/s²
+||V∞_in||: 0.0502724146681426 km/s
diff --git a/archive/ES_0.6408214057203925 b/archive/ES_0.6408214057203925
new file mode 100644
index 0000000..939d4c9
--- /dev/null
+++ b/archive/ES_0.6408214057203925
@@ -0,0 +1,22 @@
+archive/ES_0.6408214057203925---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T10:08:15.981
+Launch V∞: [5.476966515582343, -8.85617617612582, -2.1066235623821457] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00025831008686854153, -0.0001341798409903667, -0.0002641877734524912] km/s
+ V∞_out: [0.00011743349698679608, -0.00025303088300717856, 0.00027708884649863566] km/s
+ time of flight: 1.0259485982003188e8 seconds
+ arrival date: 2026-07-25T20:42:34.981
+ thrust profile: [0.675815441882618 -0.5481638926320629 -0.4114723991028489; 0.33650543434653357 -0.09255591617529779 -0.34206727373386114; 0.13923158036588143 -0.00966411222348672 -0.20312672412086774; 0.09548998085847349 0.0037944141528794845 -0.17532909009710293; 0.0623232575354997 0.00580595309948774 -0.12922579745334364; 0.011727313917054335 0.0011269073316063417 -0.030024265653222217; 0.008150500638445348 0.001597881436745435 -0.021573660512802465; 0.012064314416148714 0.0053633878978655 -0.041940831042622514; 0.0020803055094965306 0.0004750013181332192 -0.006575730646149477; 0.007911510353527789 0.002090318166593783 -0.02989495317280909; 0.00013527105731683494 7.140926247637193e-5 -0.0008985786370461176; 0.00023978280988034122 1.2769385065718629e-5 -0.0003864727654424022; 0.0004487793014930673 -8.726828864728963e-5 -0.000955226845075069; 0.00022838066756667743 -7.62865379878911e-5 -0.0009205997622806132; 8.560658842308847e-5 -6.432106065488714e-5 -0.0007888223983943652; 0.00034013929892331025 0.00020261429948467672 8.103142535453183e-5; 0.0002597913747166403 -0.00012589482894582473 2.5590929308790325e-5; 5.921720017638903e-5 -6.136751361970113e-5 -0.00010104065591734989; -0.0003696729940170359 -0.0007241591022198552 -0.00041058940665816243; 6.597901880981907e-5 2.146575654599634e-6 -0.0001923512320608418] %
+
+Mass Used: 89.23483120478568 kg
+Launch C3: 112.86688150897237 km²/s²
+||V∞_in||: 0.0003930947854500469 km/s
diff --git a/archive/ES_0.6408780933335794 b/archive/ES_0.6408780933335794
new file mode 100644
index 0000000..2554fd2
--- /dev/null
+++ b/archive/ES_0.6408780933335794
@@ -0,0 +1,22 @@
+archive/ES_0.6408780933335794---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T09:59:36.878
+Launch V∞: [5.756301975455712, -8.741845788970608, -2.495225838119645] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0005638064810550995, 0.010753368912733447, -0.004779010972597566] km/s
+ V∞_out: [-0.009194922453644581, -0.005464654472374795, 0.004961459903066318] km/s
+ time of flight: 1.039325367407597e8 seconds
+ arrival date: 2026-08-08T08:08:32.878
+ thrust profile: [0.393790909832668 -0.3021166430838973 -0.23917283591936614; 0.29281024924895427 -0.06528415399847465 -0.2869926863847661; 0.17078175809720142 -0.0016028043429340776 -0.23250444412783366; 0.10972571854832887 0.012162094873983766 -0.18682458518192377; 0.06340332821354275 0.01212056158993727 -0.12730315807967; 0.011693787317713486 0.0031057090777966614 -0.02827654143068637; 0.009630950271779749 0.003003075435779993 -0.02584767194352958; 0.002423937506240429 0.001717499084077537 -0.007068860957988678; 0.008651601626267123 0.0031304632609080512 -0.02549052210131559; 0.0028473323729982696 0.0012828854421875725 -0.00949515145833607; 0.0019314861975039306 0.0003595822933591442 -0.007776367096342939; 0.0012217516487069945 0.0004637842314666968 -0.004713348719995885; -0.0005445353779184061 0.00016713109951072428 -0.00034609059289157813; -3.541068042788747e-5 0.0001964962701479209 0.0016750584469734625; 0.0001908930003664568 0.0009572120780987261 0.0006765617906413172; 0.0006522437641413684 -0.0017986545735062017 0.0006704544206231317; -0.0001189205671670798 -0.00041467127580464944 -0.0011630768495742405; 0.00041869196329361865 -0.004274537295440792 0.0031367096566849925; 0.0018927926699553565 5.5046739966005626e-5 -0.0003514950512311525; 0.0006575362701309805 6.703084741485794e-6 -0.0023816127576274655] %
+
+Mass Used: 72.30175430751888 kg
+Launch C3: 115.78103221399836 km²/s²
+||V∞_in||: 0.01178099174932356 km/s
diff --git a/archive/ES_0.6409638040306193 b/archive/ES_0.6409638040306193
new file mode 100644
index 0000000..0514f65
--- /dev/null
+++ b/archive/ES_0.6409638040306193
@@ -0,0 +1,22 @@
+archive/ES_0.6409638040306193---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-01T00:24:37.592
+Launch V∞: [6.321857850306418, -7.363556698353377, 0.08454010492545729] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.869170878282828e-6, 1.099218520885994e-6, -2.4115302177553973e-8] km/s
+ V∞_out: [-1.6918328680222514e-6, 3.900506926292199e-8, 8.774838738312428e-6] km/s
+ time of flight: 1.874957778749387e8 seconds
+ arrival date: 2029-04-09T02:34:14.592
+ thrust profile: [0.5198612039120794 -0.1353637277785583 -0.17400903459257927; 0.03269551165725329 0.024181971354474946 -0.04230123287962912; 0.07034564526381892 0.04307671166758801 -0.12885447841389788; 0.05938927941656858 0.05044571453062009 -0.15698462152626075; 0.03555074386439104 0.039847675026786177 -0.12914584337650714; 0.015612998184772778 0.025055734434884527 -0.08005919036138119; -0.0005216439910929243 -0.003226561663295614 -0.007401273942229053; 0.0023279271639203448 -0.0037001744774717293 -0.031840419470765186; 0.05804234268533269 0.04920604523939329 -0.07362357220645283; 0.03323357156509452 -0.004721596314542828 0.002844294153535265; 0.018496133844834416 -0.0195648092709452 -0.03233518794023925; -0.010210513028819472 0.00988414620687373 -0.08944647211310716; 0.02014617336586883 0.003901023755640132 -0.004110662754229579; 0.07990533223497148 0.10258268473534657 -0.02199477561246832; -0.08056219846711765 0.03832179833924903 0.045327049125626344; 0.06515469776713535 -0.06003814969164539 -0.024190385871483668; -0.03042332573537922 0.11672552079304761 -0.08536550598972925; -0.23033142999037753 -0.12266052889463658 -0.014613925152720615; 0.06997703004508177 -0.2640848783314136 0.1370282685462877; -0.026352828301879242 -0.097048576964789 -0.03861171700865309] %
+
+Mass Used: 198.3202657767174 kg
+Launch C3: 94.19500095868658 km²/s²
+||V∞_in||: 8.937060756906495e-6 km/s
diff --git a/archive/ES_0.6409987933442917 b/archive/ES_0.6409987933442917
new file mode 100644
index 0000000..0341283
--- /dev/null
+++ b/archive/ES_0.6409987933442917
@@ -0,0 +1,22 @@
+archive/ES_0.6409987933442917---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T16:13:15.669
+Launch V∞: [5.69964265054283, -8.749610194343521, -2.4322884081817393] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.746105209822715e-5, -1.2374830398754288e-5, 2.2398341226653922e-5] km/s
+ V∞_out: [2.199705328287824e-5, 1.96324946312201e-5, 9.531553791540661e-6] km/s
+ time of flight: 1.0503284855515887e8 seconds
+ arrival date: 2026-08-21T08:00:43.669
+ thrust profile: [0.40629746764351926 -0.3152067415674798 -0.250441087884205; 0.23859245259498163 -0.055586141429065046 -0.24277421792540557; 0.14446167392892342 -0.0037948554996918484 -0.20450292462367473; 0.09982602301682121 0.008627650883658888 -0.17627744424554448; 0.07190899782426546 0.01129911196122631 -0.14853974083489518; 0.038201334979074866 0.007559555340811987 -0.0885433877615983; 0.0026653667632128312 -0.0004253574971779014 -0.010277188623264696; -1.834199015939052e-5 0.0011841566756901868 0.0003636374200099708; 0.0025530459124340136 0.004425869398046526 -0.011045898491093423; 0.007566205538013501 -0.0012209713420141453 -0.021015813904903473; 0.014713283858675107 0.002972229550185924 -0.013844708591008476; 0.0032132372246240263 0.0007525469252447309 -0.01203369749607544; 0.005855028014722174 0.00454367669772957 -0.017074037011219918; 0.005363619254973525 0.0038242958082685364 -0.0060049015690180445; 0.00242733240327413 0.000605626695828484 -0.007557357728895294; -0.003616791997214972 0.0024980059044495363 -0.00342983415184013; -0.002736590026228454 0.003314774864041895 -0.00637912443952892; 0.022303410979743823 0.005926653055027285 -0.062215315396369875; -0.0018248067804396261 0.00038188749930290536 -0.0017429820494697036; -0.005244334553215002 -0.0019089125944460796 0.01690670788753667] %
+
+Mass Used: 77.24574008337731 kg
+Launch C3: 114.95763179742222 km²/s²
+||V∞_in||: 3.097919394497799e-5 km/s
diff --git a/archive/ES_0.6410329050932099 b/archive/ES_0.6410329050932099
new file mode 100644
index 0000000..94820d3
--- /dev/null
+++ b/archive/ES_0.6410329050932099
@@ -0,0 +1,22 @@
+archive/ES_0.6410329050932099---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-22T11:08:25.846
+Launch V∞: [7.092903520720482, -6.646079616447764, -1.1580883610458739] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.476426118857651e-8, -2.7447009156414513e-7, 4.006962580414587e-8] km/s
+ V∞_out: [-4.384478278368873e-8, 1.5874618395823123e-7, 2.2522424688899416e-7] km/s
+ time of flight: 1.1996620958967166e8 seconds
+ arrival date: 2028-02-09T23:05:14.846
+ thrust profile: [1.0 -0.42536688438696846 -0.3072808441387029; 0.8258293157592886 0.12817160709372938 -0.4848012794033315; 0.4605650929314743 0.20050196792789682 -0.41926940402541285; 0.3797033890422864 0.23902530364399727 -0.45008421483273436; 0.19784892544476573 0.153665356669534 -0.29802151274507266; 0.037511146761835354 0.033637525608636414 -0.06719964640779698; 0.022653179184188254 0.02259627564191924 -0.04617659575005781; 0.0060928195913953756 0.006483494657653244 -0.01323530395972342; 0.001048455836239234 0.0012075249776574543 -0.0024045697371523843; 0.0028993458379953313 0.0034917991261317646 -0.007428747600024761; 0.0005296187439487235 0.0005572124710296104 -0.0010114923495411375; 0.00013559228163667261 0.000739905767343797 -0.0004217475850548942; -0.0001901907510508036 0.0005537596119448209 -0.001459132982883687; 0.0005071145725848419 -0.00014954151979144935 -0.0008935298487319314; -0.0008241581042748288 -0.0010743940017760762 -0.002135422351314696; 0.00020804490628216515 0.00027804349818994964 -0.000366673176623755; -0.00026415827097307754 -0.0004984026888071372 -0.0017388531177521466; -0.0011675412292962875 0.00024082159684312907 -0.0005975787117173834; -0.000662296189112692 -0.00039972846747702 -0.0007175704634049542; -0.00019937019536604906 0.00020912359738513926 -0.0003425985839806962] %
+
+Mass Used: 188.9169201747368 kg
+Launch C3: 95.82082327440138 km²/s²
+||V∞_in||: 2.78482808639116e-7 km/s
diff --git a/archive/ES_0.6410459551394591 b/archive/ES_0.6410459551394591
new file mode 100644
index 0000000..b0acd90
--- /dev/null
+++ b/archive/ES_0.6410459551394591
@@ -0,0 +1,22 @@
+archive/ES_0.6410459551394591---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T13:36:57.971
+Launch V∞: [5.447214072682576, -8.865818319715883, -1.8751828700595952] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.020089032240999477, 0.39425851972508535, -0.20866445702328149] km/s
+ V∞_out: [-0.38810904691905296, -0.20189528833342663, 0.19305197597887355] km/s
+ time of flight: 1.028340000013292e8 seconds
+ arrival date: 2026-07-28T18:36:57.971
+ thrust profile: [0.7342464767958061 -0.589331937597544 -0.45089464628488113; 0.2634682711356854 -0.07548342324179644 -0.29036657000832516; 0.1589461088826669 -0.01470457445789125 -0.24829613452306284; 0.08843724741960936 0.0018510232265551954 -0.17501099050725483; 0.057074103204431584 0.004927028959845968 -0.1357119357224476; 0.04842512789013939 0.0070471288846193515 -0.1287489435823115; 0.008331593639942179 0.0010250285874009984 -0.024610278051050507; 0.014918760944644047 0.0020389202382749792 -0.04806014732821975; 0.010234231808368272 0.0017832824324971446 -0.03565341014852312; 2.113041624336807e-5 1.1445586921981796e-5 -0.0003466073513950543; 0.00019459633171178673 -1.3964279540698034e-5 -0.0004448704488166874; 0.000250350130381458 0.00040760837464017387 -0.0005542851456755651; 2.3870443685776792e-5 4.172676161083546e-5 -0.00038100545731082746; 7.421655324220747e-5 -4.4287095926503385e-5 -0.00037296871838338576; -0.00037743778196264974 0.0005937578890070835 -0.0005978792469019908; -0.0003100949424025046 0.0005347478762990402 -0.00024311323347534346; 7.023190352986326e-5 2.766423306383197e-5 -0.00028158008167862797; -0.00013908624155633642 -5.357390827855828e-5 -0.0002109829282947577; 0.0005499228542990382 0.0003360467054635461 -0.000687056271340023; -0.0004203642577832803 -0.0002109472547787188 -3.5161064664286584e-6] %
+
+Mass Used: 95.77169349933502 kg
+Launch C3: 111.79118642800582 km²/s²
+||V∞_in||: 0.44652458523245536 km/s
diff --git a/archive/ES_0.6412772158612863 b/archive/ES_0.6412772158612863
new file mode 100644
index 0000000..8fd20bc
--- /dev/null
+++ b/archive/ES_0.6412772158612863
@@ -0,0 +1,22 @@
+archive/ES_0.6412772158612863---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:09:28.270
+Launch V∞: [7.417266731919179, -7.487807324262945, -1.9953294128469685] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.26602253016193883, -0.17749503747745166, -0.43625704280480965] km/s
+ V∞_out: [-0.07878630805771869, -0.5250260729728736, -0.022513993235895] km/s
+ time of flight: 1.0339667063231117e8 seconds
+ arrival date: 2027-08-17T01:27:18.270
+ thrust profile: [0.3523986764969214 -0.16143619363436665 -0.18606116048123544; 0.19326275212066008 -0.004401703226283951 -0.19628233691451757; 0.11335628034799676 0.019674152845443507 -0.1706566485217129; 0.06884410172661913 0.019200366846574654 -0.13574418396282545; 0.11882293970129709 0.04547463222885117 -0.2780765516789619; 0.07834699568724236 0.03396531955868793 -0.21366623838140383; 0.04844862837540214 0.022246864266110878 -0.14644177652702242; 0.02566378577781701 0.012108589975385638 -0.08336039689614144; 0.0006702554086236263 0.0007927428764504935 -0.0024963324728058105; 0.0019441628331686466 0.0008832427549582464 -0.007349386160287739; 0.00021907383961187598 0.0004366413787805504 -0.0015720204425693765; 0.0005857347870587197 0.0003671055278816616 -0.0020576412864080577; 0.0011620296042050577 0.0013905446926966868 -0.0011189879344550642; 0.00013873082501051145 0.000731830156225527 -0.0010673113333547401; 0.0007176988336225583 3.841121458007427e-5 -0.00039264581568002917; 0.0004289660873957297 -2.5358706397508196e-5 -0.0006782731573136651; 0.00035615807863094933 0.00026257000312075507 -0.0010111605149612816; 0.0009511444451010076 -0.000887074415035246 0.0006125290138119818; -0.0003542638520601589 -0.0008078475634793914 -0.0003275726458302731; -0.0005831802271086648 -0.0014680278302318384 0.0007717018450204803] %
+
+Mass Used: 76.94749655112446 kg
+Launch C3: 115.06444376349305 km²/s²
+||V∞_in||: 0.5409183693309733 km/s
diff --git a/archive/ES_0.6412798924451775 b/archive/ES_0.6412798924451775
new file mode 100644
index 0000000..2e1a4ce
--- /dev/null
+++ b/archive/ES_0.6412798924451775
@@ -0,0 +1,22 @@
+archive/ES_0.6412798924451775---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T17:51:56.488
+Launch V∞: [7.218732296884951, -7.539508534493869, -2.2838033506378057] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.06969053465261218, -0.11401512977875516, -0.04349332116305265] km/s
+ V∞_out: [-0.0798064017448689, 0.0992752623087978, -0.05942129326836483] km/s
+ time of flight: 1.0243771487403344e8 seconds
+ arrival date: 2027-08-07T08:47:10.488
+ thrust profile: [0.7490445840301359 -0.388354642019332 -0.41182147001711644; 0.19827392075405673 -0.015657988888953273 -0.21062459156713398; 0.1318821427598442 0.014125307926952728 -0.2070031635018336; 0.05216512118472492 0.01091384174577705 -0.11124934593999351; 0.026444661826395786 0.00725599175877297 -0.0689977104760064; 0.031033964238000897 0.010023519888584118 -0.09098828164845427; 0.018013211556312084 0.006279614123327141 -0.05923111909733003; 0.026265501140996544 0.0098348395194044 -0.08906538885365176; 0.004906843341762862 -0.00012255345807113318 -0.01896475732414008; 0.002812462335454979 0.00057018370563064 -0.00925190184786958; 0.006358482240196703 0.0036074350608669894 -0.0215530275292294; 0.00038106978283422783 0.0037959687350674546 -0.0038732269008064867; 0.0014820375167463895 0.001138609896928714 -0.007136414632581856; 0.001370168388966717 -0.0010503268098302388 -0.004996419420932778; 0.0022863683179812047 -0.0009331235368228675 -0.0029286293562591935; -0.0011807594200401346 -0.0008301804804356399 -0.003235293386143227; -0.002977064577776624 -0.004286684610715788 -0.001790952760146662; -0.00012273431201863683 0.0004851683763870498 0.001783389444545204; -0.0015708130875487108 -0.0011607438998885726 0.003058623007596145; -0.0004092590301804168 0.0014885021037568417 0.0005544518704321392] %
+
+Mass Used: 82.16795900165562 kg
+Launch C3: 114.17004266018024 km²/s²
+||V∞_in||: 0.14052718393401956 km/s
diff --git a/archive/ES_0.6414196694167488 b/archive/ES_0.6414196694167488
new file mode 100644
index 0000000..d550c1a
--- /dev/null
+++ b/archive/ES_0.6414196694167488
@@ -0,0 +1,22 @@
+archive/ES_0.6414196694167488---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T05:19:06.944
+Launch V∞: [7.400884943424624, -7.609544059253527, -2.7017753451768374] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.14265447052027821, 0.14014303601885963, 0.014732515563448411] km/s
+ V∞_out: [-0.12890753046688877, 0.10522489674628731, -0.11183974723735671] km/s
+ time of flight: 1.0304140430448423e8 seconds
+ arrival date: 2027-08-14T19:55:50.944
+ thrust profile: [0.2609050156402238 -0.13230925145340214 -0.1570097157286562; 0.1423883135028674 -0.011584661450192019 -0.16184577698661798; 0.08917193822200645 0.009375373409090842 -0.15112244431755784; 0.05780714618970501 0.012313058410738818 -0.12839237057502315; 0.03378520887065436 0.00967884810409331 -0.091032120031278; 0.015204140476571865 0.005549387563522038 -0.0478836648841732; 0.009874282884325366 0.0051413233045920275 -0.03834807756477546; 0.01851014663654904 0.0071470296172808315 -0.06853572776018428; 0.0026010497382912097 0.001040153438477144 -0.010946131229555076; 0.0022956250652112695 -0.0019286456452828262 -0.0022633860254500167; 0.0006168632847486683 0.000990446364617886 -0.008719658295204684; -6.009388300385688e-5 0.0019540091387486966 -0.00478684915118981; 0.0015509816404004088 0.0014334727536577429 -0.0007345393955723845; 0.0001148716794075967 0.0001941366179828999 -0.0005543069476912459; 0.0027686917903902526 0.002200945475243022 -0.004465473012266165; -0.0008084986126631047 0.0025230664831057195 -0.0014267213612758059; 0.0016380632193140807 -0.009824601952739292 -0.003135485604444206; -5.747237188778476e-7 -8.667225113033472e-5 -8.067879949188918e-5; -9.056297296696349e-5 0.00014430835986090594 0.00012093793874556717; -0.003383926307335877 0.001541477645087285 0.003641485006734605] %
+
+Mass Used: 48.45216327008393 kg
+Launch C3: 119.97784875133537 km²/s²
+||V∞_in||: 0.20051786832806587 km/s
diff --git a/archive/ES_0.6415880653116097 b/archive/ES_0.6415880653116097
new file mode 100644
index 0000000..3038ad2
--- /dev/null
+++ b/archive/ES_0.6415880653116097
@@ -0,0 +1,22 @@
+archive/ES_0.6415880653116097---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T13:13:17.681
+Launch V∞: [6.837367760635981, -7.2494385270317165, -1.3259094414234982] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-6.104159369473344e-5, 2.688195982065255e-5, 0.00012436936150018112] km/s
+ V∞_out: [7.169334774245208e-5, 0.0001221116543387741, 4.104061065246249e-6] km/s
+ time of flight: 1.1430024306741254e8 seconds
+ arrival date: 2027-12-19T11:17:20.681
+ thrust profile: [0.8552478798999403 -0.40278269122054294 -0.43651502118947944; 0.4038371785522991 -0.0035429982197276145 -0.4386301801613732; 0.16788506872511827 0.031054541807564267 -0.2870923156416526; 0.1143376091809913 0.03441761635996688 -0.26117263043457073; 0.06131438892164888 0.02229692689834787 -0.1738580641121632; 0.05506792025277385 0.02353335777655577 -0.18225608196917817; 0.018844936259331025 0.006232662806903589 -0.06892735346860077; 0.0071827534935858 0.00445039640892364 -0.029717118931958577; 0.0010145129053610543 0.001630429328189294 -0.007195309210761498; -0.0017499968574650102 0.0005640600108887987 -0.0001932124633294615; -0.0006232719356149287 0.007066070628170164 0.0020776094050630606; 0.024240541261972143 0.0009360209864481923 0.0008302889150765408; 0.029057355680545672 -0.032181051749718415 0.007652300894281143; -0.0026000833498497702 0.04790818530275504 0.010343147887406244; 0.10403163359844582 -0.00030584201404950436 0.016650279758206585; -0.020014250523704584 0.018835304864995416 -0.010111459141185537; -0.026839143127961738 -0.040000838128837896 0.04821581650369039; -0.15457164972489096 -0.011286248990351477 -0.06808666466428868; -0.03072756060525439 -0.00895225624635505 0.0022580865399785452; 0.12696620927058266 0.03635649231268113 -0.1711792486591927] %
+
+Mass Used: 158.99111879040765 kg
+Launch C3: 101.06199269825204 km²/s²
+||V∞_in||: 0.00014112566741934237 km/s
diff --git a/archive/ES_0.6418682026664412 b/archive/ES_0.6418682026664412
new file mode 100644
index 0000000..68c8fbc
--- /dev/null
+++ b/archive/ES_0.6418682026664412
@@ -0,0 +1,22 @@
+archive/ES_0.6418682026664412---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T10:36:54.973
+Launch V∞: [7.32973617199997, -7.460467482252123, -2.0539294104532524] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.4485698280287085e-6, -3.228331810066195e-5, 4.202113562171714e-6] km/s
+ V∞_out: [-4.457791171882487e-6, 2.086260906282426e-5, 2.471577075253238e-5] km/s
+ time of flight: 1.023482551540629e8 seconds
+ arrival date: 2027-08-05T00:41:09.973
+ thrust profile: [0.602185081770859 -0.29202949804641537 -0.32752289044692967; 0.29571543773239073 -0.010994390727931274 -0.3074772082301627; 0.13000774897375733 0.020164395714368972 -0.20400273624473675; 0.06864073707334961 0.017219704323618506 -0.1403935118972607; 0.06563619595718796 0.02197877420641429 -0.15877611860891; 0.05631121657224267 0.022734355867175465 -0.157130592514743; 0.0366787934539746 0.01650131501308291 -0.12020167758271463; 0.013651674858122157 0.005917839114243747 -0.043669641669737365; 0.003683674185521108 0.001672209847667088 -0.013615951823876335; 0.000617372583944409 0.00020446038049346552 -0.0023527733703350142; 0.0002644407734785462 -9.228728715110946e-6 -0.0014763918982056033; 0.00015662777405016061 5.817770629626694e-5 -0.0011874117133329949; 0.0010663458840951337 0.000267203306827144 -0.00018833134543242005; 0.00037232252136926234 0.00012172328606184512 -0.0004575263016795672; 0.0009241404736980317 -0.0003517587168457545 -0.00014135462359217586; 0.0007838636922332356 -7.013187594311521e-5 -0.0009987646373300512; -0.0005898161086211752 -0.00030286874733480697 -0.0006624329971849171; 0.00010150460497722063 -0.0004921295529366759 0.0007524215525738319; 1.8330954164258356e-5 -0.0013666342205134675 0.001697703345487069; -0.0004945720779688618 6.149014273900696e-5 -0.0003001746755696039] %
+
+Mass Used: 86.1665414475674 kg
+Launch C3: 113.60223342799095 km²/s²
+||V∞_in||: 3.2647601446057984e-5 km/s
diff --git a/archive/ES_0.641957605195904 b/archive/ES_0.641957605195904
new file mode 100644
index 0000000..65eb239
--- /dev/null
+++ b/archive/ES_0.641957605195904
@@ -0,0 +1,22 @@
+archive/ES_0.641957605195904---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T08:06:59.992
+Launch V∞: [7.382965524655001, -7.5410651200062455, -2.40267262059487] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.010802184366263396, -0.007053413228951612, -0.021674905941989973] km/s
+ V∞_out: [-0.003626881650173224, -0.024928311570577406, -0.001060565151619791] km/s
+ time of flight: 1.0385041945145515e8 seconds
+ arrival date: 2027-08-23T07:27:18.992
+ thrust profile: [0.28500750241660233 -0.14005399037732272 -0.174750910608034; 0.19297661587990572 -0.012036087281196263 -0.2210800517657055; 0.1354041901850464 0.01697355639619905 -0.23116835885207826; 0.08174025091831404 0.018856825223233183 -0.18312758011442037; 0.047477406942899605 0.013736723026765553 -0.12516259207567004; 0.02757122598548008 0.008682126448812099 -0.07902985573352474; 0.01518456651696786 0.005488239154828927 -0.0474231161137873; -0.0026549242433871463 -0.004090932321865406 -0.003933345375763984; 0.003421835647878909 0.001811312411177019 -0.00857272584221747; 0.005243751037154255 0.0022010787853571725 -0.01733770787769434; 0.0009369431758647318 0.0022547009700775622 -0.011350402034827073; 0.005586430446233753 -0.0007403865767253849 -0.009220436594198219; 0.0007321444262992059 0.0005723157892915284 -0.0011131777658784732; 0.00046399690671626375 -0.007400154198647436 -0.002590681568694836; 0.00024158207137627344 0.0026194149766976937 -0.002956109487953153; 0.024387366366864564 -0.014216769732402296 -0.02760286263729671; 0.008283483555895236 0.003192304370301353 -0.03180436923708668; -1.4411498538940363e-5 0.00022785562213205104 -0.0012635828195830291; -0.00019367867255542975 -0.009478750718584865 -0.019523585762480436; 0.022530344744918093 0.0036303931252250608 -0.012514081040123854] %
+
+Mass Used: 65.58324637086525 kg
+Launch C3: 117.14867880417532 km²/s²
+||V∞_in||: 0.025223785854926836 km/s
diff --git a/archive/ES_0.6421343987597257 b/archive/ES_0.6421343987597257
new file mode 100644
index 0000000..3d7777a
--- /dev/null
+++ b/archive/ES_0.6421343987597257
@@ -0,0 +1,22 @@
+archive/ES_0.6421343987597257---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T09:08:46.885
+Launch V∞: [7.194126736229981, -7.5076769213257855, -2.3951792346584977] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.013105482197457063, -0.008748167415871432, -0.02721134872114447] km/s
+ V∞_out: [-0.004634868349473836, -0.03107217023098998, -0.00132194968105382] km/s
+ time of flight: 1.0514130697350655e8 seconds
+ arrival date: 2027-09-07T07:03:52.885
+ thrust profile: [0.585420574714833 -0.29590849754768744 -0.3287715295199046; 0.23838399820448722 -0.015339372592173859 -0.26479579154766253; 0.08974706210769365 0.01172423966770235 -0.15480015806594447; 0.043736928889374915 0.012009143848236587 -0.09823451310318718; 0.036137881273433446 0.011380533004553833 -0.09658970872764165; 0.04301442580183039 0.015954332601925438 -0.135442657407227; 0.008086294040593285 -0.0013924817722176033 -0.04021242078164416; 0.005656023449100102 0.001427918968207472 -0.027727494484714205; 0.009443104862180175 0.0013898610700443287 -0.01177481222994084; 0.006123238870287628 0.0030034088111423793 -0.02469201966270255; 0.00495973340600475 0.0009438759081224681 -0.02270559652524673; 0.014674518594964913 -0.018128699005320666 -0.012994670600672689; 0.0011384080933447237 -0.018354531851502168 -0.03869364273294283; 0.0012770589408555256 -0.004656932553171814 -0.002118962566793836; -0.003734329907447589 0.04085828743047342 -0.006583144742889027; -0.02910661129791496 0.019686190265209423 0.012525503074896374; -0.012063383013580106 -0.002770456961027066 -0.016564764153933764; 0.029419495064525333 0.046084012182116996 0.03594752860637013; -0.008800918767090125 -0.01713440895503398 0.006581316316578921; 0.0015134793582876616 0.0009499550475542198 0.011662382867907224] %
+
+Mass Used: 84.98772294751097 kg
+Launch C3: 113.85755581808613 km²/s²
+||V∞_in||: 0.03144426173386346 km/s
diff --git a/archive/ES_0.6421576685441313 b/archive/ES_0.6421576685441313
new file mode 100644
index 0000000..8d355cf
--- /dev/null
+++ b/archive/ES_0.6421576685441313
@@ -0,0 +1,22 @@
+archive/ES_0.6421576685441313---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T09:15:02.628
+Launch V∞: [7.2608747656265535, -7.439057515696474, -2.1922913999176012] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.14585769009467953, -0.7041362562925743, -1.0798592780273257] km/s
+ V∞_out: [0.5570477779036273, -0.04923455625273136, 1.170077460323762] km/s
+ time of flight: 1.0205850076522909e8 seconds
+ arrival date: 2027-08-01T14:50:02.628
+ thrust profile: [0.7249791742729459 -0.35413573649717006 -0.3710313921597275; 0.3861032395281524 -0.015094790875837889 -0.3725706762328649; 0.14913509047002288 0.02535968004145873 -0.22451441153324778; 0.06630601452882842 0.019070877333297084 -0.13463659736296768; 0.034622767697991164 0.011870000235367082 -0.08762700350574903; 0.028959008291698517 0.011513981287694191 -0.08065854988995497; 0.03273621392942592 0.01459658743803226 -0.10046231940521508; 0.010570669106786683 0.004869709935446303 -0.03558195641599158; 0.00036073302536528454 -0.00021470818443873195 -0.0007777015334965022; 0.004036859987986252 0.002186981983402362 -0.015469359323580864; 0.0008487630595899309 0.0008315537550602013 -0.0011708778909960342; 0.0016163457140835752 6.108389196377061e-5 -0.003833832405988485; -9.391800163873365e-5 9.077551119852792e-5 -0.0017869781227660344; 0.00020890490193043376 -0.0001709361535841402 -0.0007581067927121543; -0.005805456070081408 0.0036156101418751505 -0.00673480778988822; 0.0028749122764805115 0.0009516583718590556 -0.001653682571994935; -0.0012314602635178024 -0.003731138183714058 -0.0007650902930900873; 0.0069984564313662866 0.0067626504971966235 0.000242795861154106; -0.0013341302061060127 -0.00327195535521802 -0.0015543858808419243; 0.0015624100534811038 -0.002820956994054078 -0.004848420775690435] %
+
+Mass Used: 90.79882608253865 kg
+Launch C3: 112.86602066610533 km²/s²
+||V∞_in||: 1.2973736522402384 km/s
diff --git a/archive/ES_0.6422284438428917 b/archive/ES_0.6422284438428917
new file mode 100644
index 0000000..cec6b44
--- /dev/null
+++ b/archive/ES_0.6422284438428917
@@ -0,0 +1,22 @@
+archive/ES_0.6422284438428917---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T19:21:45.502
+Launch V∞: [5.472962178954977, -8.756114970443019, -2.073855928574123] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.0649810558626374e-5, 7.420535684457517e-6, 9.445303271825835e-6] km/s
+ V∞_out: [-3.985349536378856e-6, 1.071184436458136e-5, -1.1274293180064336e-5] km/s
+ time of flight: 1.0246140387285526e8 seconds
+ arrival date: 2026-07-23T16:51:48.502
+ thrust profile: [0.9073587578990866 -0.7251553958278693 -0.5360866628510335; 0.3125909476876863 -0.0830386824877292 -0.32759503709323257; 0.12273628435473999 -0.008339313097629883 -0.18853514022385584; 0.0694597809957506 0.0028907945198207827 -0.13561458506360596; 0.04690698079595153 0.005156731619722508 -0.10792337316323404; 0.020106824068965794 0.0031921438567830015 -0.05247940554702703; 0.008156699744279327 0.001754543422847873 -0.024015517602299308; 0.018426126688090672 0.003979600853841725 -0.05644781559239185; 0.01669204248756667 0.003879106306017048 -0.05382965411868731; 0.0017193637282984515 0.0023327539151295758 -0.011387055461169249; 0.001317585352673022 -0.001706267325677272 -0.0025048012590126543; 0.0013907206655405886 0.0007032973821746579 -0.004225256017455967; 0.00188881372833105 -0.0010471304847604547 -0.005309012597242886; 0.0010042696077312342 0.00014361342022156995 -0.0034748301497984535; 0.00430011991332608 8.100413644135322e-5 -0.0017676321666364374; -0.0029032095172443137 0.00526154661352711 -0.00424424543838057; -0.005771098205138116 -0.00682512598380219 -0.0031636057437482695; 0.002328867144500852 0.0029523516169466663 -0.0015012398153968487; -0.007094657869462289 0.004072824517327737 0.0017572640759109682; 0.0017532542685184008 -0.004031289234334062 0.008720926173873291] %
+
+Mass Used: 102.21135148121539 kg
+Launch C3: 110.92374280036998 km²/s²
+||V∞_in||: 1.6052930220856908e-5 km/s
diff --git a/archive/ES_0.6422853573365915 b/archive/ES_0.6422853573365915
new file mode 100644
index 0000000..5d096bc
--- /dev/null
+++ b/archive/ES_0.6422853573365915
@@ -0,0 +1,22 @@
+archive/ES_0.6422853573365915---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T16:26:20.168
+Launch V∞: [5.625606756640997, -8.814620658294986, -2.3086390799484557] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00015059832388140206, -7.841403731430346e-5, -0.00015740415959871037] km/s
+ V∞_out: [6.950192755741309e-5, -0.00014867833019831025, 0.00016332567561140712] km/s
+ time of flight: 1.0348030134948283e8 seconds
+ arrival date: 2026-08-04T08:58:01.168
+ thrust profile: [0.5510877960468882 -0.43229861850040197 -0.31746935952619393; 0.23333138085354085 -0.05603139711191804 -0.24150657482851196; 0.09667026763286937 -0.0023497705867560107 -0.14786931028331018; 0.08496576172456878 0.0072588707211660225 -0.16200401081961469; 0.07278888253193153 0.010572262471139534 -0.15946332898132254; 0.036977760569591636 0.0064084370027038375 -0.09166037198546065; 0.01879209434528018 0.004781325180726152 -0.051269503070163466; 0.011623050316110656 0.0032254729634093766 -0.0353866436947107; 0.006341864205312983 0.002176891567480015 -0.02039214574688117; 0.0022819080801283046 0.001211393978272627 -0.00416523550108856; 0.001805662156801413 0.0006944735113413677 -0.005003028119150219; 0.0018814596792648124 0.004416796358706275 -0.00498742181047334; 0.0006489959990888596 -0.0030192306662839576 -0.0019362030940698128; 2.8493405236916384e-5 0.0019315516708963464 0.002902264737294593; -0.0013354551632463593 0.0003453066987822537 0.0005891224074544886; -0.007012655514035668 0.004497722447045478 -0.003110849089067514; -0.006996794682710457 0.010713066198347977 -0.00387618214597145; -0.0006808682068023255 -0.00644619549178844 -0.014786160374915865; -0.01082389956432487 0.0033349573887427983 0.0031070298829699613; 0.0006775279952058855 -0.006799272113941775 0.016257664804933188] %
+
+Mass Used: 80.39656529244348 kg
+Launch C3: 114.67480313147084 km²/s²
+||V∞_in||: 0.0002315268577569197 km/s
diff --git a/archive/ES_0.6424366679181024 b/archive/ES_0.6424366679181024
new file mode 100644
index 0000000..b1dbd0b
--- /dev/null
+++ b/archive/ES_0.6424366679181024
@@ -0,0 +1,22 @@
+archive/ES_0.6424366679181024---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T01:49:51.612
+Launch V∞: [5.447958770257839, -8.510230009541013, -1.282451461065404] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00366005613932081, -0.00409903195837179, 0.004088710553848754] km/s
+ V∞_out: [0.26450660242135243, 0.2698424348285028, 0.23667785637218927] km/s
+ time of flight: 1.0456201094887014e8 seconds
+ arrival date: 2026-08-12T06:50:01.612
+ thrust profile: [0.8425798016580892 -0.6283876429436769 -0.3845463075859662; 0.637706487338098 -0.11949980065534217 -0.47932976876029604; 0.430110476433208 0.013677479403715505 -0.4531864418491138; 0.21855630389898012 0.029570628567819085 -0.29232677462693557; 0.185713835411306 0.041011337148810556 -0.2842251311483827; 0.04410967604932313 0.01030143275777999 -0.0753846375573211; 0.005705877942211509 0.001675532756484486 -0.005677017536656765; 0.005604413584308073 0.0010043209967402784 -0.014223330704816118; 0.0175397267531159 0.00534602485380491 -0.03961733125488947; 0.002958936094824597 0.0034817509849722787 -0.006521109675894432; 0.0006589091842836558 0.0003166062736834136 -0.0016402943188862928; 0.003898612791734774 0.00010797245987985296 -0.005362851369158428; 0.0032052310234516055 -0.001018545824816352 -0.004469260980226102; 0.0009599326797381624 0.00017556363009776682 1.1542791506765314e-5; 0.0013341382996478405 -0.006266584057068569 -0.0022436197143854016; 0.0009689233859594814 -0.0010868933479078217 -0.012654584116964773; 0.0006401812576508317 0.0008651816126296601 -0.0025032701435186576; -0.0009139720582121988 0.0011041277323606 -0.0007055243405861139; -0.000681595907020602 -0.0004922795362554723 -0.00036895769353437755; -0.0008272597617266736 -0.002015387407397683 0.003426819439844247] %
+
+Mass Used: 144.30722982614134 kg
+Launch C3: 103.74895132771053 km²/s²
+||V∞_in||: 0.006849498370821575 km/s
diff --git a/archive/ES_0.6425130421751474 b/archive/ES_0.6425130421751474
new file mode 100644
index 0000000..f4e2b54
--- /dev/null
+++ b/archive/ES_0.6425130421751474
@@ -0,0 +1,22 @@
+archive/ES_0.6425130421751474---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:03:53.524
+Launch V∞: [7.305518150149657, -7.530631033378556, -2.4520078835276693] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.9591428040264406e-5, -5.91665229600065e-5, 4.41915907274772e-5] km/s
+ V∞_out: [7.268899102580425e-5, -4.782050667814678e-5, -3.78583450454185e-5] km/s
+ time of flight: 1.0351885330731027e8 seconds
+ arrival date: 2027-08-19T14:18:06.524
+ thrust profile: [0.48716046959640497 -0.24508712995299348 -0.2745818079350069; 0.21323099247000735 -0.011042225024561201 -0.22993032561156104; 0.10661135496776253 0.015884734604435534 -0.17648696287268434; 0.04516017164440754 0.011992276628898612 -0.10213694915765566; 0.019575213470744285 0.006351476917527941 -0.05367721358147994; 0.014350073883617772 0.00594475647030837 -0.04805227432616434; 0.03495998647050522 0.014716504526980954 -0.11486927666629626; 0.03890148573189797 0.017776993959812356 -0.13965536932692107; 0.003492608572412516 0.001231634156959495 -0.01189838090018534; 0.0018146262941783494 0.002755425706582071 -0.01671020255475604; -0.0024489396189470557 -4.5961861165027596e-5 -0.0010914596524561077; -0.00031457160631843077 0.0025917200470196656 0.00804162236218857; -0.0020284857727266774 0.0017834848000965612 0.0045064955933325065; -0.002106658614392334 -0.006041829842933629 -0.010596099060118573; 0.010775252945598238 0.000915394045323671 0.0056538083226826755; 0.0007603312227455214 -0.00015476801786201737 0.004039465122379094; -0.012045133643533042 -0.0014714311580908313 0.0065862138579960965; 0.01956121680706105 -0.002970705888406146 0.0027956579035437997; 0.0013591410660023836 -0.0006003106658403041 0.0022968224724249503; -0.009908186400381108 -0.004342663385433962 0.024228940154571416] %
+
+Mass Used: 72.38738833140133 kg
+Launch C3: 116.0933418639321 km²/s²
+||V∞_in||: 9.489316322096043e-5 km/s
diff --git a/archive/ES_0.6426063194716582 b/archive/ES_0.6426063194716582
new file mode 100644
index 0000000..42b77d6
--- /dev/null
+++ b/archive/ES_0.6426063194716582
@@ -0,0 +1,22 @@
+archive/ES_0.6426063194716582---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T22:57:32.673
+Launch V∞: [5.268777719601181, -8.892541769230442, -1.8950845907178946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002981750182315782, -0.00036961502474655187, 0.0003535482732963104] km/s
+ V∞_out: [0.0003589416283419908, 0.0003667077514631565, 0.0002920150357061396] km/s
+ time of flight: 1.1002121959102683e8 seconds
+ arrival date: 2026-10-20T08:24:31.673
+ thrust profile: [0.4373544073034955 -0.3453835626821114 -0.2616138573880413; 0.21833806071153095 -0.05767626590178847 -0.23180037327142766; 0.11522495895393976 -0.014954762488629456 -0.1807395217420616; 0.10106498445642854 -0.008356030859539957 -0.23458485584833288; 0.06604768028542984 -0.008474493137392479 -0.15920873330466612; 0.0329650980527602 -0.0011433976495221257 -0.09435761707643658; 0.01784284435590707 -0.007927944875922325 -0.07165727220601609; -0.005302249556426657 0.03259868393915768 -0.05678568164633584; 0.00469585493910095 -0.0013653423558760034 -0.026125484977156783; 0.006512488633138757 -0.000251170828352834 -0.022524268259510715; 0.0042269727195593226 0.0018013280798831815 -0.016021765220249815; 0.0034784444842434585 -0.001727968054012252 -0.044253394326068826; 0.0008277091708035859 0.0030776471386156365 -0.017630058842061862; 0.03574729839992768 0.04326729910024579 -0.024652377336498527; -0.007618619735775937 0.0007937066366215848 0.015911452314342787; 0.04986059837544215 0.08357182821763832 -0.016669485384042892; -0.07283478709596253 -0.029629877613494938 -0.04411988303008868; -0.031348811666559 0.07532844386496855 0.04199245854281489; -0.011145774213538759 0.01931692681714358 0.03441271842863039; -0.049457001337603855 -0.0010845003809532012 -0.0287847476310465] %
+
+Mass Used: 105.5401696549743 kg
+Launch C3: 110.42866338205033 km²/s²
+||V∞_in||: 0.0005920472865967707 km/s
diff --git a/archive/ES_0.6427459913813716 b/archive/ES_0.6427459913813716
new file mode 100644
index 0000000..3ad4ca5
--- /dev/null
+++ b/archive/ES_0.6427459913813716
@@ -0,0 +1,22 @@
+archive/ES_0.6427459913813716---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T13:30:33.700
+Launch V∞: [7.189039056404954, -7.42093144060464, -2.1600418282119977] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005205529001018789, 0.02756850187430804, 0.004957897400841388] km/s
+ V∞_out: [0.027525377590458637, -0.004451581594300022, 0.005848692090483767] km/s
+ time of flight: 1.0266131063051467e8 seconds
+ arrival date: 2027-08-08T18:32:23.700
+ thrust profile: [0.9225853133157752 -0.460902953468922 -0.46372032631992915; 0.2915562712631413 -0.012217709593777184 -0.29658173864638837; 0.09665369406563672 0.014317195519935103 -0.15933564919629567; 0.06599071296229267 0.01546326908398376 -0.1342180806854757; 0.03971359109453087 0.01254701619492836 -0.09024857232035352; 0.031901450822263464 0.011834162516985958 -0.09799152351399679; 0.03840788736605389 0.015576626900837704 -0.11916721705732009; 0.004815329477300824 0.002232425965706125 -0.026387743801017955; 0.028058226890546833 0.014502361259867503 -0.1031416726254188; 0.0014734471458092428 0.0008934064807030814 0.0042282488527689045; -0.0030920808186091853 -0.005117740129298494 0.0007857976418881021; 0.001499066967698001 -0.0006121264595668791 0.006591265827837476; 0.001865244917328511 0.0005810994482881879 -0.0026151163735438033; -0.0034536418900480135 -0.0021697998771603834 -0.002839328213072367; -0.000533732249980082 0.00198638279881076 0.00355056682521005; 0.0031606751852762418 0.0012559288740122175 -0.01187730981712095; -0.0006791817065727756 2.9783845145423442e-5 0.0023693910446409383; 0.012538015270040177 0.012927161813107883 0.006942775016171892; -0.005015008258602927 0.010285457875963867 9.172343916913524e-5; 0.001488494502178733 0.00838367264343731 0.01928519354013571] %
+
+Mass Used: 99.93031752654178 kg
+Launch C3: 111.41828670029572 km²/s²
+||V∞_in||: 0.028490359324014208 km/s
diff --git a/archive/ES_0.6428680518943608 b/archive/ES_0.6428680518943608
new file mode 100644
index 0000000..e41a4e3
--- /dev/null
+++ b/archive/ES_0.6428680518943608
@@ -0,0 +1,22 @@
+archive/ES_0.6428680518943608---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T06:23:07.427
+Launch V∞: [7.216085778046854, -7.385933071706909, -2.113901818762706] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.24271543169573442, 0.24037028659114057, -0.18793372939172723] km/s
+ V∞_out: [-0.1729368015565272, 0.34376340345151957, -0.06255729582038684] km/s
+ time of flight: 1.0173932746645096e8 seconds
+ arrival date: 2027-07-28T19:18:34.427
+ thrust profile: [1.0 -0.5206590818971134 -0.5217719149003341; 0.283616517365221 -0.01320184514755139 -0.28463561504676; 0.12829216545993982 0.020215770610294812 -0.1955511041312672; 0.05529700662003621 0.013861176955699037 -0.10711882740237742; 0.052944600071050264 0.017585531934690625 -0.1238328971744411; 0.07055734273803312 0.028063985115964224 -0.1852587861130001; 0.03260016481121886 0.014182153971723097 -0.09234259310372565; 0.0015737120037701113 0.0004656818561064057 -0.008501068954695797; 0.003429336253217706 0.0018235085007954669 -0.006733124041600922; -0.0011602772142819155 0.0025620583801356537 -0.004880174117878583; 0.0026452248111497904 -0.0030221781165319676 -0.0025015603935837605; 0.0025685764677205597 0.0014639594365056978 -0.0035847152639960542; -0.004209524548295289 0.0013408527171355196 -0.000504665216086646; 0.0008055491873573955 0.0005467195010765112 -0.005025270263497305; 0.0028850355852232043 0.0006867341812921819 -0.008438435017257932; -0.001629624458104955 -0.00011571681346969707 0.0008475929074863008; 0.0006887449480003887 0.00033843234051727025 -0.0041300156003028065; -0.004363884152068584 -0.00612439283684886 0.00373299701607737; 0.007580914358729497 0.0005478591426443346 0.006969715924393338; 0.0020716938939039273 0.0010250227110587464 -0.006619135839779443] %
+
+Mass Used: 101.97324773789978 kg
+Launch C3: 111.09248219523221 km²/s²
+||V∞_in||: 0.38988170270254635 km/s
diff --git a/archive/ES_0.6430067205773874 b/archive/ES_0.6430067205773874
new file mode 100644
index 0000000..6184b9a
--- /dev/null
+++ b/archive/ES_0.6430067205773874
@@ -0,0 +1,22 @@
+archive/ES_0.6430067205773874---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T22:18:37.426
+Launch V∞: [7.215286873999382, -7.777071224608427, -2.5073809789105987] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.005882656437163301, -0.005791325115401038, 0.0042048315753133135] km/s
+ V∞_out: [0.0040669557574080275, -0.008082983933288795, 0.0015460636055047755] km/s
+ time of flight: 1.0276523579877031e8 seconds
+ arrival date: 2027-08-13T08:12:32.426
+ thrust profile: [0.4606912252115131 -0.24893695058404697 -0.28341287181085434; 0.13896338948506165 -0.016362894675169905 -0.1713913865196975; 0.0646514591225856 0.0029819486962342134 -0.12415209890317078; 0.0401662621880639 0.004717222565306664 -0.10114073252419889; 0.026522079185872932 0.003688871057742813 -0.07861840759289083; 0.022786141555627817 0.004101878961628954 -0.07209344362133042; 0.01602393837738928 0.003200036043479594 -0.05904252663678477; 0.010049374271513868 0.002192364999364951 -0.04463665953542409; 0.004626772456017855 0.0010344851238856003 -0.023338238829403488; 0.0022974660735714664 0.0002885525049165594 -0.0007105652321091608; 0.0011872175733743525 -0.00011115447254745147 -0.0029184845912654466; -0.0001323507846118072 3.1515553547601656e-5 -0.001382013587962229; 0.001308570651044563 -0.0002511811502895751 -0.0017266918636615505; 6.274544336633975e-5 -0.00022094578211201855 -0.0008317486994245161; 0.003947866984574186 -0.0006508087562172828 -0.0007895062497984839; 0.004046244816580785 0.0010643661145251211 -0.007090715170668034; -0.00011509737531119595 0.0009488051893742184 -0.0017750548464728526; -0.001971957977208487 -0.003491000074401659 0.0016082855182696565; 0.0031658926184019508 -0.0016557970853744895 0.004101972831367652; 0.0011326284060249863 0.0007986421674143121 -0.003276243043825908] %
+
+Mass Used: 56.9985688727852 kg
+Launch C3: 118.83016088014286 km²/s²
+||V∞_in||: 0.009264216206821035 km/s
diff --git a/archive/ES_0.6431792753418741 b/archive/ES_0.6431792753418741
new file mode 100644
index 0000000..02d8d57
--- /dev/null
+++ b/archive/ES_0.6431792753418741
@@ -0,0 +1,22 @@
+archive/ES_0.6431792753418741---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T10:17:37.693
+Launch V∞: [5.570889278734899, -8.769032216185598, -2.31990250371458] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011585781134057532, 0.2159028126167163, -0.11065154734516197] km/s
+ V∞_out: [-0.19762158154170192, -0.10085635110430619, 0.09886920584598675] km/s
+ time of flight: 1.0421244401242706e8 seconds
+ arrival date: 2026-08-12T14:11:41.693
+ thrust profile: [0.6057202281219404 -0.47111655064699204 -0.3514140203757655; 0.29443120233045933 -0.06917660619510656 -0.2931137944704023; 0.12404188797642127 -0.0037626851976143125 -0.1813052955615815; 0.049565046570830225 0.0039400075588210065 -0.09160495240008396; 0.0445531829632386 0.006623387680134111 -0.09532026350224175; 0.023813897987698424 0.005811500691779936 -0.05734850826639542; 0.015434691649090258 0.005676787588274798 -0.04728139013363954; 0.011441584390306295 0.0008418080844925064 -0.03752581951575448; 0.01322328267404392 0.002051634495401246 -0.03826720797753655; 0.008297921270335101 0.0032498402741261267 -0.028063929064736138; 0.0010558630075155682 0.00024408705822377593 -0.003926006062606157; 0.011478942059456673 0.004643829722586144 -0.03374493833897414; 0.0021104513264338124 -0.005373959758529637 -0.014779184664667685; 0.02899217092206419 -0.006991688185057194 -0.018317968142635595; -0.0007811251918783073 0.0010036247495376642 0.005483942082798161; -0.009243931869824284 0.001824803289987471 -0.046948805259387466; 0.034295354028760064 -0.0074697663858703765 -0.0464215457702914; 0.01732897178572861 -0.009388897786996794 -0.008964341689442174; 0.0008823081664503221 -0.0002674912699691298 0.0013889984878121923; 0.00743360708840469 0.005898729475208989 -0.007235159622766584] %
+
+Mass Used: 89.38518211705423 kg
+Launch C3: 113.31268099116554 km²/s²
+||V∞_in||: 0.2428827283900068 km/s
diff --git a/archive/ES_0.6432377756525058 b/archive/ES_0.6432377756525058
new file mode 100644
index 0000000..e89461b
--- /dev/null
+++ b/archive/ES_0.6432377756525058
@@ -0,0 +1,22 @@
+archive/ES_0.6432377756525058---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T12:50:01.022
+Launch V∞: [5.490520967280256, -8.673007539402912, -1.9585182766649756] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.19788826680280472, 0.0882903672500233, -0.17833644964179737] km/s
+ V∞_out: [-0.12787491842191925, 0.2041351105996016, 0.13891631882586378] km/s
+ time of flight: 1.0315469871026298e8 seconds
+ arrival date: 2026-07-30T10:54:59.022
+ thrust profile: [0.9053798022183304 -0.7118564043559621 -0.4974767224529616; 0.3437921331416767 -0.08312631019761524 -0.3230854194247639; 0.18776914427218405 -0.006220703572531117 -0.246420004565849; 0.13321791626795498 0.00969101377084138 -0.21892551010163408; 0.06195948785504654 0.008401674901093193 -0.12227418213731425; 0.0363025906866514 0.006588176239172352 -0.08355005311935042; 0.003030219616372847 0.0009878842692212016 -0.023460364043260698; 0.0061442248237764995 0.03412122025683501 -0.04067199288295529; -0.01633681089747155 -0.008804774564530235 -0.03409926001171372; -0.0008072652267998419 0.002559057746608878 -0.011372302959744618; -0.0017932997957810933 -0.002228997579406256 0.0027306001184444575; 0.002946480817806423 0.0005572962054567403 -0.004994469479464634; 0.0034706431324545636 0.00034200705339678446 -0.004962838547048584; 0.01686059641433344 -0.0030824064330053583 -0.016013685191997362; 0.0031882287580825125 0.013532292232829762 0.009966585399167515; -0.006327095797999066 0.0012994978683553123 -0.008833471682425608; 0.021104701935459394 -0.0030217234783562804 0.009165778703832726; 0.0008622791778892559 0.00010424135300559322 -0.0022895950993043375; 0.002410729490409767 -0.0010945169539755318 0.008208451765937496; -0.001967514975322368 -0.00024795519495980807 -0.0030240015566897465] %
+
+Mass Used: 113.42847261542147 kg
+Launch C3: 109.20267411071463 km²/s²
+||V∞_in||: 0.28064006192666674 km/s
diff --git a/archive/ES_0.6432654595721922 b/archive/ES_0.6432654595721922
new file mode 100644
index 0000000..6e3cc8e
--- /dev/null
+++ b/archive/ES_0.6432654595721922
@@ -0,0 +1,22 @@
+archive/ES_0.6432654595721922---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T13:47:13.124
+Launch V∞: [7.29337334088377, -7.4382518219670155, -2.2163465515373537] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0015599823149857446, 0.007793275123906443, 0.0014721325457579646] km/s
+ V∞_out: [0.007827784982972517, -0.0012380322287236499, 0.0015846434468510802] km/s
+ time of flight: 1.0119321910138087e8 seconds
+ arrival date: 2027-07-22T19:00:52.124
+ thrust profile: [0.7897667240076177 -0.39833084329628315 -0.43287491797029953; 0.32700170192451716 -0.01884995470903085 -0.3296592787093809; 0.1389290808124064 0.02054468147523518 -0.2083633167623373; 0.07855255820042549 0.021755394036309744 -0.157038026607949; 0.040798453908825 0.014839677361484217 -0.10205323366194778; 0.03352918288468674 0.014829553414245331 -0.09787626619247439; 0.01654088700718228 0.006547376510600538 -0.049289084444321486; 0.007273824663964709 0.0033038272885071024 -0.0243827473708776; 0.0057241035848180685 0.0032564838673204482 -0.022812473969303537; 0.000244449132794997 9.391298263310968e-5 -0.0007448406118852806; 0.00041493733338072785 -0.0001458960933255405 -0.0005258678023909037; 1.7104644951074634e-5 8.605846087883344e-5 -0.0001124853756154431; 0.0001217860333399903 -0.0005464646891126207 -0.0004420042034016914; 8.712664935520912e-5 -0.0004379305737077844 0.0004536268521090885; 4.0119576709619106e-5 0.00037435719172890735 -0.0003021455829904592; 0.0007505755958692429 0.0005282062439537273 0.00033312763147548097; -0.00010108113332623966 -0.0002633258434438194 0.0005980480006058401; 0.0007915998507591472 0.0005164770451421469 0.0004031002192642035; -0.0017069662842922025 -0.0010308699970881818 -0.0005133366127541638; -0.00028124227552939977 5.265844334604382e-5 -3.0509177532766878e-6] %
+
+Mass Used: 88.78342095826702 kg
+Launch C3: 113.43307689302122 km²/s²
+||V∞_in||: 0.008083059829807466 km/s
diff --git a/archive/ES_0.6433077289844933 b/archive/ES_0.6433077289844933
new file mode 100644
index 0000000..d299c4a
--- /dev/null
+++ b/archive/ES_0.6433077289844933
@@ -0,0 +1,22 @@
+archive/ES_0.6433077289844933---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T03:05:00.372
+Launch V∞: [7.329565093485649, -7.4098978389548, -2.294981046624803] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0020574034241868126, 0.028448003410305723, 0.005157284046653163] km/s
+ V∞_out: [0.02766625965719785, -0.005297544030597742, 0.006836039521746551] km/s
+ time of flight: 1.0488609048180205e8 seconds
+ arrival date: 2027-09-03T02:06:30.372
+ thrust profile: [0.5257854450839113 -0.2500681093957794 -0.27272704805036124; 0.21732995158254292 -0.0045587372508810505 -0.2321999077460934; 0.0683484515499081 0.011969710365194338 -0.11568367955863859; 0.0576320815107726 0.01733376924857793 -0.1267976894652402; 0.05670170394704458 0.020198520940236317 -0.15076133980337353; 0.04237249059282382 0.018651007915876976 -0.1311748294966017; 0.02848248881089925 0.012580712692319283 -0.09383111333095825; 0.02238318950397896 0.01151171152931034 -0.08875164008552103; 0.012252871798406832 0.005273276239000839 -0.04309099349577764; 0.007196946209264375 0.0031782460921181083 -0.02599793856527481; 0.0027634273061948682 0.0013369958818047168 -0.00884512583857363; 0.03721233539645345 0.006230941141748835 -0.0070254768968466864; -0.0019866879752116103 -0.008851514943110931 0.0006452748291329879; -0.003255995909858882 0.030260323485713177 -0.009820599820430886; -0.01036361873564028 -0.0012021197518173744 -0.03042124879956627; -0.0076939065797597865 -0.014223652244590832 -0.029128826696020505; 0.029052689350480443 0.03011648168567855 0.012073925136761806; 0.008088572892563008 0.007144463769274191 -0.0052133370400049076; -0.0031860147512680764 -0.017744312037002392 -0.019036062747629208; -0.004682731184350152 -0.005972036222343095 0.024016818647387125] %
+
+Mass Used: 86.1320678699908 kg
+Launch C3: 113.89604844775738 km²/s²
+||V∞_in||: 0.02898481301682805 km/s
diff --git a/archive/ES_0.6433381030100752 b/archive/ES_0.6433381030100752
new file mode 100644
index 0000000..3e63917
--- /dev/null
+++ b/archive/ES_0.6433381030100752
@@ -0,0 +1,22 @@
+archive/ES_0.6433381030100752---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T10:05:24.931
+Launch V∞: [7.354960704502842, -7.455407402478392, -2.2135477250951316] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.1471676016880778, -0.6996064869305773, -1.033924836559825] km/s
+ V∞_out: [0.5097665067402308, 0.23469527590569028, 1.1243220661126576] km/s
+ time of flight: 1.0232931530202626e8 seconds
+ arrival date: 2027-08-04T18:53:59.931
+ thrust profile: [0.5644845017408429 -0.27022605923659754 -0.29313779795653366; 0.2810834399133607 -0.0071567113327729425 -0.28573679865803775; 0.13973949913874834 0.02393077739397885 -0.21558488028402245; 0.05896245556586906 0.016601862079462532 -0.11959538044577284; 0.049831266678360464 0.016804804027057543 -0.11947793822869028; 0.04422321290249002 0.017385129735943944 -0.1211492315574805; 0.032892185404111804 0.014207184126694765 -0.09984777088577541; 0.011115977396826774 0.005923049803983768 -0.041792569052365065; 0.00770247731817268 0.0050724109081504995 -0.03051566342726023; 0.007005486463198559 0.005913852878325898 -0.030235138571720024; 0.006016233931117106 0.004539445439887492 -0.002418866425666419; -0.0009794617603754692 0.003928167012853798 -0.0029599397471275967; 0.0013624429307030265 0.0005453973534160896 -0.007213501362134461; 0.003841306407565426 0.0021818270866776567 -0.0052508816967039365; 0.00023838068809879849 -0.0016316724252721103 -0.0024778539900861185; 0.0002923590210910014 0.004514138214343931 -0.00026538000442378074; 0.0063210257704465304 -0.003309762099578629 -0.00021286419766551948; 0.003204904864302422 -0.00490994660640754 0.0005557326584747255; -0.005393763269795132 0.0014465327384128592 -0.00647515340022168; 0.0001447598582376364 0.0020212682569800454 0.0015724194037408119] %
+
+Mass Used: 82.18746998601227 kg
+Launch C3: 114.57834003298437 km²/s²
+||V∞_in||: 1.2570235109962047 km/s
diff --git a/archive/ES_0.6437464242995448 b/archive/ES_0.6437464242995448
new file mode 100644
index 0000000..d77d1d2
--- /dev/null
+++ b/archive/ES_0.6437464242995448
@@ -0,0 +1,22 @@
+archive/ES_0.6437464242995448---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-18T15:44:46.788
+Launch V∞: [5.645190904139691, -8.42716191018916, -1.4192427597602144] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.445801355131323e-5, 1.8080118556392456e-5, 3.863762488141893e-5] km/s
+ V∞_out: [-1.8478483608181528e-5, 3.8782436270394806e-5, -4.424102421143009e-5] km/s
+ time of flight: 1.058999736627013e8 seconds
+ arrival date: 2026-08-26T08:24:19.788
+ thrust profile: [0.7428184616477935 -0.5593791190357253 -0.35223399875559236; 0.594442598923008 -0.11500378561517345 -0.4712279322668331; 0.4043451972830859 0.012069919660367918 -0.44446866927264544; 0.24810063532823354 0.039716082170480956 -0.3404124630445137; 0.13458057989196648 0.03428554471254585 -0.21754185690605957; 0.019426203718592848 0.006309887677249954 -0.038957775178180006; 0.01524887024939202 0.005932276515702475 -0.03138921587447687; 0.015974808450734117 0.010687372689807262 -0.03494224729130374; 0.013779380093645622 0.0037383504798520614 -0.03368134741773517; 0.011203777614293477 0.0026316093956558297 -0.026428303088811715; -0.0015192840650426359 0.0005438970791463913 -0.000633184592384029; 0.0020710761016264657 -0.00031585756446673 -0.004932256334942304; 0.0031917167863923512 0.0015986544860612322 -0.007961115277555546; 0.0021049809261076526 0.001685086436789541 -0.0002943947324625701; -0.00036844417420586533 -0.008706269185774707 -0.00413111961931416; 0.0009632379004072104 0.000774252148407362 -0.0011702752445470295; 0.012398225609521567 -0.007078222909159954 -0.007696739945835524; 0.0005812933709142253 -0.010454715547141134 -0.00744989802956857; 0.0006623730222088137 0.0016019652730368712 -0.0064289777606038045; -0.0009082469536100652 -0.00484855235518156 -0.0016229014491207694] %
+
+Mass Used: 139.12381375697396 kg
+Launch C3: 104.8994882158563 km²/s²
+||V∞_in||: 6.161389220313225e-5 km/s
diff --git a/archive/ES_0.6439604236684647 b/archive/ES_0.6439604236684647
new file mode 100644
index 0000000..6c37b8e
--- /dev/null
+++ b/archive/ES_0.6439604236684647
@@ -0,0 +1,22 @@
+archive/ES_0.6439604236684647---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:34:00.516
+Launch V∞: [7.418738595250808, -7.538103018553673, -2.4985509054773947] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009024616893291376, 0.005785784008299502, 0.017688174429920895] km/s
+ V∞_out: [0.002724848143645156, 0.02049327282604503, 0.0007513719930337216] km/s
+ time of flight: 1.0304363633887592e8 seconds
+ arrival date: 2027-08-13T21:47:56.516
+ thrust profile: [0.2735877722588725 -0.1395854692598143 -0.1677036519466305; 0.20073104918356632 -0.012984809031077318 -0.22863819602739913; 0.12652508208620958 0.015681746518758113 -0.2139392572843896; 0.0820395365447074 0.01952056202053469 -0.17943501431677059; 0.050064650133458524 0.017014899012050777 -0.12978483846591932; 0.026676821865240136 0.012163869426867133 -0.07845837797713336; 0.010160087838761177 0.005267624554441212 -0.03265685938518811; 0.005912707319794731 0.0025443034272837053 -0.015455517374850857; 0.0052121522547530046 0.006049492296343644 -0.012360298527583484; 0.004644415800077019 0.008587233483866811 -0.004898699754888337; 0.003277978381225393 0.002630804224993213 -0.009442761223072109; -0.002610363070778189 -0.005411561359512412 0.0014463320712715159; -0.0001973604196239795 -0.0017842154652541607 -0.00393066825761983; 0.007066914871415217 0.0014913868232626294 0.00846322973734114; 0.01248451410412543 0.014130104843681502 0.0007028939340421149; -0.00010272513249073292 -0.0266252211670263 6.441086710949422e-5; -0.0010845016676782975 0.002468569633207703 0.0009361851841142269; 0.0006157417375258138 -6.120020324831311e-5 -0.0017896510228605183; -0.0001288369024942959 0.006669804295876006 0.0038021504735481506; 0.00853279137569464 0.017386857714068123 0.018876683510759034] %
+
+Mass Used: 62.35045042006141 kg
+Launch C3: 118.10343609025384 km²/s²
+||V∞_in||: 0.020683097478972574 km/s
diff --git a/archive/ES_0.644220389094668 b/archive/ES_0.644220389094668
new file mode 100644
index 0000000..e10e822
--- /dev/null
+++ b/archive/ES_0.644220389094668
@@ -0,0 +1,22 @@
+archive/ES_0.644220389094668---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:49:31.754
+Launch V∞: [7.221233211637998, -7.444502571771289, -2.109831137678862] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.008296226253526714, 0.008403583667687274, -0.006247582215303485] km/s
+ V∞_out: [-0.005982857286236189, 0.01181753260213204, -0.0022212710002803273] km/s
+ time of flight: 1.0263737539516994e8 seconds
+ arrival date: 2027-08-08T17:12:26.754
+ thrust profile: [0.8924436896905902 -0.44067725956665244 -0.4590942506046001; 0.21032207064961975 -0.008456940534966232 -0.2329420200938076; 0.0914687632246897 0.0124762314728685 -0.15397570820528764; 0.07992041128639356 0.017852072191962907 -0.1652012392072749; 0.043154159200871976 0.015228309190633556 -0.1127438710466135; 0.023246833090231622 0.00876414312201805 -0.07194934252730924; 0.03410008307698363 0.016481544030756988 -0.13292788930893681; 0.031530448563240235 0.01389113686540755 -0.11160951563875036; 0.008413009843538821 0.002666191031835961 -0.03197726945702958; 5.294299324051311e-5 0.002307231454896894 -0.009876737243345052; -8.987914582182224e-5 0.0002639533361244702 8.607098819641765e-5; 0.0018352646964374096 0.0010313961148756567 -0.015705603475119918; -0.0025482998832277847 -0.0011635617112220494 -0.0006907295316223691; 0.0021191678723756118 -0.0018871988232129781 0.001207973319408787; -0.020164973714924476 0.016941115709092944 0.012255330745701332; 0.0033703157954636125 0.007749163632844473 -0.0029717968833579272; -0.005996051100861077 0.0032052649099148477 0.007362541136283636; 0.019393136216631433 -0.014172449757047872 -0.0027937764356434584; 0.017932141112103443 -0.011320656685339932 -0.010236844536654445; -0.002888021453066956 -0.0023818321604352566 -0.013094753439736598] %
+
+Mass Used: 98.15086605007446 kg
+Launch C3: 112.01821506749225 km²/s²
+||V∞_in||: 0.013359635924923351 km/s
diff --git a/archive/ES_0.6442998281628873 b/archive/ES_0.6442998281628873
new file mode 100644
index 0000000..4b3a822
--- /dev/null
+++ b/archive/ES_0.6442998281628873
@@ -0,0 +1,22 @@
+archive/ES_0.6442998281628873---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-13T14:26:51.814
+Launch V∞: [6.139546110262305, -7.04300746395591, 0.5415551542466354] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.643368671631152e-6, 3.796628272417236e-6, 4.620143137862143e-6] km/s
+ V∞_out: [6.5346652954383365e-6, 3.8149754569015995e-6, 1.2484242251466794e-7] km/s
+ time of flight: 1.87495777874927e8 seconds
+ arrival date: 2029-03-22T16:36:28.814
+ thrust profile: [0.8872654696708269 -0.24164817888379553 -0.09761392114054056; 0.7854201402945962 0.30126269693400654 -0.2791902518884328; 0.3078312668574695 0.2412133414932545 -0.19438834805055827; 0.05862739339751052 0.067932809823157 -0.05371020389994584; 0.03732058929930581 0.05612032796279986 -0.045315244764215036; 0.032564533203177606 0.059161748403847296 -0.049208281514700136; 0.04379855697034468 0.09284925198284243 -0.08270515718828884; 0.014895362213135366 0.03516913709113214 -0.024489398800751124; -0.01715747181146146 -0.014304065992565907 -0.011901295132584346; -0.006360453465599793 -0.0036697903759162166 -0.027926104306784744; 0.000961537677929403 0.00972432587361921 0.0030779417460902467; 0.04098955294718932 0.03288144940134033 0.02418890901720106; 0.0002614336758001264 0.0003267051925704503 -0.01156424840213756; 0.0337717203364105 -0.024613774546999707 -0.006190499888695996; 0.017706289442082326 0.005948944385953968 -0.034787153643469224; 0.05081773702561107 -0.0428151077631853 -0.02987692697323445; 0.006119571301752134 -0.00046784797560801806 -0.018413166862677077; 0.07132676800643123 0.03358650133678418 0.01982501783899356; -0.06964983025399542 -0.041187374696653484 0.030553010928610007; 0.006309766196027652 -0.01936121370441749 0.050493507161589596] %
+
+Mass Used: 240.7341012423126 kg
+Launch C3: 87.59126256246675 km²/s²
+||V∞_in||: 7.571062110030415e-6 km/s
diff --git a/archive/ES_0.6443320751164328 b/archive/ES_0.6443320751164328
new file mode 100644
index 0000000..3f7aac8
--- /dev/null
+++ b/archive/ES_0.6443320751164328
@@ -0,0 +1,22 @@
+archive/ES_0.6443320751164328---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T15:53:45.172
+Launch V∞: [5.701407782614188, -8.839934999416146, -2.38179771939329] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.000182845578362385, -8.881919715802709e-5, -0.00017404606236056378] km/s
+ V∞_out: [7.556988721248906e-5, -0.00018570340902204655, 0.00017723016100009808] km/s
+ time of flight: 1.0353507486498295e8 seconds
+ arrival date: 2026-08-04T23:38:19.172
+ thrust profile: [0.3674455731191626 -0.2941089229891389 -0.23689049636301016; 0.2453025228151277 -0.0634407318398256 -0.25519078465934397; 0.1465869065696188 -0.008830524353729293 -0.21120452802294418; 0.09627281280192716 0.004432607593330663 -0.1723201799863858; 0.057191224579897115 0.006885439953777309 -0.11755333877092214; 0.024707037401075764 0.004453576429157673 -0.05408456076418761; -0.004403251465623027 0.004525832443717724 -0.008839364110887676; 0.011731414831634385 -0.007033517477329051 -0.03695767023947887; 0.0014022410371951361 0.0007007268116784389 -0.0020213844700780297; 0.007230588425431754 0.0004221798674619777 -0.015619792222992656; -0.0005842475431275152 -0.001044280816758926 -0.01864304881105011; 0.01050117621750859 -0.004191648690575183 -0.014438495178402472; 0.01321798355265831 -0.0001272685114118476 -0.015566398585907736; 0.016759742587253587 -0.013641346926058277 -0.018747144270814434; 0.003241057093159554 -0.01460855233679046 -0.0262105069856886; 0.002532016845209614 -0.005001337002853469 -0.004898192017866218; 0.0043699285504667255 -0.0011346736609154809 0.007124080338939517; 0.016615768722360508 0.016364983056816523 -0.011717268877136528; -0.0006456818284679214 -0.0010803518276950612 -0.005502605893678833; 0.002576345430513034 -0.007615635390161753 0.004297361550231152] %
+
+Mass Used: 73.1672267061358 kg
+Launch C3: 116.32346187366326 km²/s²
+||V∞_in||: 0.00026760677706980595 km/s
diff --git a/archive/ES_0.6445451007702193 b/archive/ES_0.6445451007702193
new file mode 100644
index 0000000..c1dc92f
--- /dev/null
+++ b/archive/ES_0.6445451007702193
@@ -0,0 +1,22 @@
+archive/ES_0.6445451007702193---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T05:21:26.064
+Launch V∞: [5.5237698457121285, -8.584347699437776, -1.7430688325312655] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.9459912474039335e-5, -6.075751965952286e-5, -8.171462173447152e-5] km/s
+ V∞_out: [-0.00010116561720160318, -6.044883535032515e-5, -2.798247601709448e-6] km/s
+ time of flight: 1.0172923416335487e8 seconds
+ arrival date: 2026-07-12T15:28:40.064
+ thrust profile: [0.9729773734134634 -0.7618567755463033 -0.5276016577002997; 0.6158244077333591 -0.14727508300538975 -0.5484734007175041; 0.25707564164130126 -0.007036977849921574 -0.32064130073072833; 0.12784212065404998 0.011831979532976471 -0.20121476631144336; 0.07743785966273446 0.013237466952295869 -0.14428736588901303; 0.016020620429677373 0.003674972254249208 -0.03588886766268066; 0.0062868609036499995 0.0017421820219510396 -0.015614918456256052; 0.01893189942451212 0.006005813302477919 -0.048680878196671155; 0.0007857670558273543 0.00021713655507618184 -0.002158225405655528; -0.0001771710016889922 -1.5728847312851998e-5 0.00026833307048929533; -0.0005631054800064594 -0.00024142649154780294 0.0014745762706674475; 4.526114503180641e-5 -6.815119688899013e-5 0.0007086586099762961; -0.0001957200530301062 4.5846727956472806e-6 0.0006964502122621765; -0.0002745752195938421 -0.0005710788993831891 -2.859456916183621e-6; 0.00016975907024603196 4.367259454328965e-5 -0.0009862268116339824; -0.0009300727190655444 -0.0012799224631828302 -0.0007737188480732685; 0.0010005053330750216 0.00013291260948393902 0.0007497566441734725; 2.5891311062611463e-5 0.0005582713069640632 -0.0007364456168106989; -0.0011557762361007785 0.0025398913139265435 0.0010439330299673397; -0.00047484267485447645 -0.0004878334150581275 0.001539244569138224] %
+
+Mass Used: 126.39475605085408 kg
+Launch C3: 107.24134768818315 km²/s²
+||V∞_in||: 0.0001179162278560737 km/s
diff --git a/archive/ES_0.6446898457938419 b/archive/ES_0.6446898457938419
new file mode 100644
index 0000000..f716137
--- /dev/null
+++ b/archive/ES_0.6446898457938419
@@ -0,0 +1,22 @@
+archive/ES_0.6446898457938419---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T01:26:52.688
+Launch V∞: [7.271125396500423, -7.325440052905698, -2.100148221676532] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.875759236056177e-6, -4.856062376682958e-5, 6.881135417770307e-6] km/s
+ V∞_out: [-6.721494070981616e-6, 3.0517656609498556e-5, 3.542686987949928e-5] km/s
+ time of flight: 1.0171864243985339e8 seconds
+ arrival date: 2027-07-27T08:37:34.688
+ thrust profile: [0.8298124654983673 -0.40445470964905456 -0.40832811322001733; 0.4587336195236853 -0.013079442336378007 -0.4143852009354124; 0.22144148950077985 0.03955670444818341 -0.2967802114550891; 0.12316198869188329 0.03734518622913313 -0.21512534959758328; 0.05607504954430992 0.0190668782595459 -0.1169549855507227; 0.013239152680169126 0.006859807774764191 -0.034724175464709864; 0.018442429104582093 0.010236412726258288 -0.0610324203776372; 0.007280625230242978 0.003600419091912925 -0.021253851090763477; 0.0008791251214486759 -0.0008206491823267955 -0.00018865569184969106; 0.00335553366679555 0.003057113561841027 -0.007615626370612255; -0.0051323749911512725 -0.0015892550893084891 -0.0007659485018247973; -0.00355043447562992 -0.006886252293709943 0.000349869992322515; 0.0002247248267837306 -0.001156059414281012 -0.000641610114863629; -0.0002916931596958199 -0.00024258455037210955 0.0015765427613031306; -0.004771496164150098 -0.0033988302706277123 0.0014296895989145287; -2.5816836145533086e-5 -0.0018104497166324379 -0.0018506650681416078; 0.0005821692632684767 -0.00011941681062125116 -0.0021373207315271772; -0.0004682219848048487 -0.0041721660618190244 0.007344533893538542; 0.0033629788165840994 -0.011683223399405593 -0.01063616258474072; -0.013832283054176803 0.01638444251663016 -0.008576704705346399] %
+
+Mass Used: 104.9767256148848 kg
+Launch C3: 110.94195905335955 km²/s²
+||V∞_in||: 4.9198635295271575e-5 km/s
diff --git a/archive/ES_0.6447400298911162 b/archive/ES_0.6447400298911162
new file mode 100644
index 0000000..56be1ca
--- /dev/null
+++ b/archive/ES_0.6447400298911162
@@ -0,0 +1,22 @@
+archive/ES_0.6447400298911162---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T09:40:50.207
+Launch V∞: [7.2842216660023995, -7.402031906444582, -2.1393677854287483] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.5282365195125639, 0.2732103413249227, 0.03719641538241492] km/s
+ V∞_out: [-0.49439336450189614, -0.25785442780283896, 0.2925174958890701] km/s
+ time of flight: 1.0068480004936701e8 seconds
+ arrival date: 2027-07-16T17:40:50.207
+ thrust profile: [0.9572261184016914 -0.4819959809882939 -0.5212238873641689; 0.28080688716722035 -0.01698092816823274 -0.2965433515535247; 0.14797264752526462 0.020870382432665036 -0.23153224021276103; 0.08436371939491008 0.021771470120984272 -0.16983381143534587; 0.045547416676551176 0.014724429150747304 -0.1117437808035844; 0.022869907824637915 0.008426680201348657 -0.06524254876444754; 0.014733181030352472 0.006127517374809323 -0.04649045020369337; 0.009425802612016232 0.004740380323584015 -0.03225087806549738; 0.012011712653096704 0.005587185998185661 -0.0439668573755965; 0.0002840972335383558 -8.994453447973036e-5 -0.0005987042431400417; 0.0013228669880099551 0.0007167004538835163 -0.005489429814542293; 0.00040579508113117754 0.0007993092313869599 0.00017506771839943575; 0.00040474766936093875 2.776043214243923e-5 -0.0002008729202221584; -6.400041463708192e-6 -3.6483436039288684e-6 0.00012049260787619045; -0.00011246357875880877 -0.00016980879062619897 -0.00020318628354526916; -5.9316244968751473e-5 0.0003701464548368204 -0.0021111559305991186; -0.0023025684389548543 0.00016654109334784977 -0.00031363849665631274; -0.0006193246229038462 0.0008575475568550666 0.0006950105633964727; 0.0006945134960319749 -0.0004890752985658375 -0.0008063292701137496; 0.0008344851470716961 9.528267250961996e-5 0.0013665553876944958] %
+
+Mass Used: 96.37337402822823 kg
+Launch C3: 112.42685614481269 km²/s²
+||V∞_in||: 0.5958701909568301 km/s
diff --git a/archive/ES_0.6451269647669393 b/archive/ES_0.6451269647669393
new file mode 100644
index 0000000..9e4f5c3
--- /dev/null
+++ b/archive/ES_0.6451269647669393
@@ -0,0 +1,22 @@
+archive/ES_0.6451269647669393---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T16:31:25.499
+Launch V∞: [7.355066739235558, -7.533494991097685, -2.479971854880723] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.05353843374495036, -0.08562848243809, -0.03406654696495833] km/s
+ V∞_out: [-0.05975006506340657, 0.07699829167166825, -0.04313915648821596] km/s
+ time of flight: 1.0141605664117867e8 seconds
+ arrival date: 2027-07-26T11:39:01.499
+ thrust profile: [0.5826454064677142 -0.30389350249543823 -0.35016332387994065; 0.2036792853466787 -0.018591379805079612 -0.23835861930002603; 0.129859865215094 0.012085860718359372 -0.22304003749889276; 0.060605201676185556 0.011892705662643027 -0.13429894901389863; 0.026642586305371214 0.00696094544845067 -0.070370040612603; 0.013246622231464352 0.004272451002159908 -0.04078391759065762; 0.013285707951773586 0.004481125933275055 -0.04460621711867842; 0.00020757811710266018 -0.001484536743205723 -0.006975458070356618; 0.0026400524985365275 0.0015267462455578825 -0.01195601260286959; 0.004185971879707118 0.0016044563304428046 -0.018023771824581463; -0.0007768101181056611 -0.00041457145154224725 -0.003121675158169356; 0.0007086187778317523 0.003956865302076317 -0.003636436492928021; -0.0008930321471598509 -0.0007508423612684304 0.00287462100720789; 3.833994165952854e-5 -0.0014481010510877346 0.0021970198611507845; 0.0006325053933015916 0.0005249959544402199 -0.0037683859551253833; 0.004800519478448178 -0.0027980485230274096 -0.003467915456905919; 0.009693398005165147 0.002351741871199553 -0.0022195551725488903; 0.005841488406980369 0.0016385841314524943 0.009285568003773234; -0.011399828689365111 -0.002302012398401901 0.011320833823753776; 0.005773357124725889 0.002069609581449368 -0.0012900285473894672] %
+
+Mass Used: 70.14337769182475 kg
+Launch C3: 117.00081392050362 km²/s²
+||V∞_in||: 0.10657922177717587 km/s
diff --git a/archive/ES_0.6451997231861639 b/archive/ES_0.6451997231861639
new file mode 100644
index 0000000..931a089
--- /dev/null
+++ b/archive/ES_0.6451997231861639
@@ -0,0 +1,22 @@
+archive/ES_0.6451997231861639---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:34:15.776
+Launch V∞: [7.259276248309351, -7.492269925064619, -2.217509613909862] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.1921877421582959, -0.9303135462700334, -1.4055207303150856] km/s
+ V∞_out: [0.5377228907030003, 0.25541542448329335, 1.5902359896760963] km/s
+ time of flight: 1.0059835653144914e8 seconds
+ arrival date: 2027-07-16T14:33:31.776
+ thrust profile: [0.8482477198609365 -0.43328732151320326 -0.45883943728073723; 0.35310746017201544 -0.025520420287158164 -0.3571966288958434; 0.09146693437832559 0.010345975461227641 -0.14635462562838322; 0.06194248560098646 0.01471749297642781 -0.12749754990489043; 0.04082208317308492 0.012475671292189147 -0.10340917607532346; 0.022556876573759356 0.007875357250936636 -0.06727015961916051; 0.014194570093189647 0.0047235960044274385 -0.048461571147523225; 0.01326887775824018 0.005540912306226583 -0.04694825840672974; 0.006298435363702722 0.0026996380663929236 -0.024181548175604386; 0.005716677904537981 0.002451294237695005 -0.022868116254798485; 0.0019022237411136969 0.0011458494667583544 -0.009797001388514942; 0.0009033387834391519 0.0002387425080426597 -0.0002875865718980531; 0.00022345325549887046 0.00026223737847847584 -0.0005936053549821851; 0.0004560836281042 0.0014789880619800614 -0.0004095036236142313; -0.0007981137568929266 0.0004437552283715066 -0.0002460151742930052; 0.0004027415289251708 -0.0013524446003191004 -4.189959462066583e-7; 0.0009007709354344792 0.0008264122710775359 -0.0001703228031251709; 0.000850000606128068 -0.0005255274124482902 0.0010508394056991071; 0.00020624163268771284 0.000100713367812599 -0.0003628762309487515; 0.0003472791554601399 0.00039021146036630693 8.927232059324975e-5] %
+
+Mass Used: 89.19980690923194 kg
+Launch C3: 113.74854916707874 km²/s²
+||V∞_in||: 1.6964397855376065 km/s
diff --git a/archive/ES_0.645247416620453 b/archive/ES_0.645247416620453
new file mode 100644
index 0000000..2b79b27
--- /dev/null
+++ b/archive/ES_0.645247416620453
@@ -0,0 +1,22 @@
+archive/ES_0.645247416620453---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T14:16:29.550
+Launch V∞: [7.24043191014495, -7.573343373239882, -2.060283252585515] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.519619514933937e-5, -7.64033780490469e-5, 5.54524745182656e-5] km/s
+ V∞_out: [9.175140099153983e-5, -6.351292265224136e-5, -5.026202176766214e-5] km/s
+ time of flight: 1.0166193859003359e8 seconds
+ arrival date: 2027-07-29T05:42:07.550
+ thrust profile: [0.6070368910523286 -0.30554460660874944 -0.31509576211203294; 0.4131283067154587 -0.03000635689608641 -0.3978270703517003; 0.10982427438975371 0.013084821066445972 -0.17339235986200024; 0.038068186944529535 0.008712097785589939 -0.08148459718068256; 0.041048967622178203 0.012271469761554434 -0.10319519145304906; 0.05266335681473148 0.01740409888701224 -0.14681647391954744; 0.013908324433054616 0.005026897095423711 -0.04531142286008876; 0.039981695438412235 0.01538176906136736 -0.13029884680274303; 0.00861494325935639 0.0037361646995154726 -0.03300308043908276; 0.0011094709565062084 0.000450917226180548 -0.0042244467071161414; 0.0031071343982232895 0.0011599533035392064 -0.010959049822725478; 0.002118301978619616 0.0005487701222512772 -0.0033823675186872544; -0.0031920772271811057 0.004078701229647079 -0.0030036119695705326; -0.0025097392700068255 -0.0004501015459983811 0.0016161443876892183; -0.004764694956432413 -0.0006623221509177077 0.0006559531156355745; -0.0036828477123807433 -0.0031311457069241318 -0.0012002244233872573; 0.0013838428354699356 -8.064551380972927e-5 0.0006000085541922417; 0.006346749164115206 0.0024899049527959886 -0.0016454799237501398; 0.003270901737639312 0.0019167213458359835 0.0022420147633269052; -0.004129274900927937 -0.001952567027929573 0.004308640082007403] %
+
+Mass Used: 87.6477708677935 kg
+Launch C3: 114.02415117532601 km²/s²
+||V∞_in||: 0.00012069349971080467 km/s
diff --git a/archive/ES_0.6453307371562995 b/archive/ES_0.6453307371562995
new file mode 100644
index 0000000..86b2135
--- /dev/null
+++ b/archive/ES_0.6453307371562995
@@ -0,0 +1,22 @@
+archive/ES_0.6453307371562995---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T14:50:35.995
+Launch V∞: [7.1842168266194255, -7.419245086400881, -2.215773805058095] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.24661445827713518, 0.22595817056016368, 0.02594503376318539] km/s
+ V∞_out: [-0.21684260034229547, 0.17705150183340684, -0.184116843860161] km/s
+ time of flight: 1.0137500622659321e8 seconds
+ arrival date: 2027-07-24T22:34:01.995
+ thrust profile: [0.9930396609965622 -0.5052588709067225 -0.5087446100116327; 0.38755834370622205 -0.02245900726696509 -0.3739280832386495; 0.10271179553733852 0.015931575041978237 -0.1568406200588432; 0.06642869008888933 0.017479894004449343 -0.12796303912839882; 0.024059844557412172 0.00786195761313153 -0.057125173383872636; 0.026650471994263923 0.011226722783894532 -0.07791923849222074; 0.04708933823267737 0.022250063564135805 -0.13870175380300995; 0.009593561005053399 0.004178057867017121 -0.03217146812959567; 0.0014997738269864086 0.0006245073659413438 -0.006002995747272641; 0.0005108436075662315 0.0001667521663871077 -0.0004101130840186264; -0.00151730818751533 9.025563279397978e-5 0.001316746408493366; -0.0028955372129453342 0.003831621450509178 0.0018654392741215796; -0.001135743936357314 0.0034663041751506647 0.008596918591205854; 0.002605509296524842 0.0006251932560835437 -0.0007221210265767482; -0.015214599100489933 -0.011443106069902344 0.0052276399639612624; -0.020836939697037572 -0.0048439343413395775 0.006018616594523961; 0.0014393475970475899 7.773630600049417e-5 -0.0077777971742534055; 0.0015609698370514507 0.0006687684421495504 -0.011767894860726349; 0.004012205161666774 0.0011243248430563664 0.012623077256075402; 0.0009774506658050226 -0.0017841509874700716 0.001644351357824021] %
+
+Mass Used: 102.07356140399224 kg
+Launch C3: 111.56782261914695 km²/s²
+||V∞_in||: 0.3354831302035822 km/s
diff --git a/archive/ES_0.645493967600568 b/archive/ES_0.645493967600568
new file mode 100644
index 0000000..5393ac6
--- /dev/null
+++ b/archive/ES_0.645493967600568
@@ -0,0 +1,22 @@
+archive/ES_0.645493967600568---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T02:47:24.993
+Launch V∞: [7.2138299908220365, -7.258874162035739, -1.8968389538260038] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.09939877025196009, -0.06900675033212167, -0.3626127622048084] km/s
+ V∞_out: [-0.05738227216062077, -0.3774875593256848, -0.016951157779971682] km/s
+ time of flight: 1.0183565848948273e8 seconds
+ arrival date: 2027-07-27T18:28:22.993
+ thrust profile: [0.9689307465486598 -0.47310674977057965 -0.44539566058384505; 0.5788215511694471 -0.012389059891434682 -0.4753131678831678; 0.21317798629687534 0.043619168732546565 -0.2651972730281357; 0.11546907806241706 0.03827053750715646 -0.1915932073936472; 0.06244126468385357 0.026020422437970713 -0.12528018404837524; 0.022195251109839945 0.009746676975640804 -0.05139118460062093; 0.022540034652803596 0.011625412672112381 -0.05716726046622515; 0.020254379018030705 0.011482583753017783 -0.059518768620191384; 0.029471342801527536 0.01725195649749515 -0.08857131233930071; 0.0027044348231951548 0.0008732461890026469 -0.0008758439046096644; 0.0001519259746454039 0.0017855289848805614 -0.006229280780935227; 0.00017739530744318496 -0.00013356105882671328 0.0007622822960317165; -0.006211664997561102 0.0029023965226754305 -0.006444672005229404; 0.008276847370953124 0.007081756867508789 -0.010474782180777721; 0.003100078407092812 -0.0016010740526382333 -0.0034588363115323115; 0.001224384853691491 0.0003411969419805608 -0.01526338379769363; 0.0017572565254731975 0.004326120436189665 -0.005223378610628413; 0.0023085904692985754 0.0021789397458036 0.003977432900495695; 0.005438667514849758 0.011391804101259093 -0.0019300792527281005; 0.0011343164642206808 2.4246533534476186e-5 0.0013520411795429417] %
+
+Mass Used: 121.1594898885487 kg
+Launch C3: 108.32859525350524 km²/s²
+||V∞_in||: 0.3822696200756773 km/s
diff --git a/archive/ES_0.6455830620593396 b/archive/ES_0.6455830620593396
new file mode 100644
index 0000000..4b07710
--- /dev/null
+++ b/archive/ES_0.6455830620593396
@@ -0,0 +1,22 @@
+archive/ES_0.6455830620593396---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-18T19:53:40.604
+Launch V∞: [6.542831827288053, -8.462516453517507, -1.9197423532741322] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.749448374640284e-10, -1.2117726012718372e-9, 6.078453142029589e-10] km/s
+ V∞_out: [4.577636304074901e-10, -1.5336202561362508e-9, 2.5382512389943427e-10] km/s
+ time of flight: 1.2409723661074024e8 seconds
+ arrival date: 2028-04-24T03:20:56.604
+ thrust profile: [0.27203950528564047 -0.19550570753799193 -0.21004136752987534; 0.028052726824596804 -0.016867279590106782 -0.06385444759676223; 0.029972061103233017 -0.023757771370200388 -0.10501899507247976; 0.025154950235880828 -0.027622903066000987 -0.12603210390346561; 0.015996891464380703 -0.02284348601260585 -0.10471861201457573; 0.019573179467469646 -0.030634752530455066 -0.1371530690416416; 0.014096995013065713 -0.024807890703822895 -0.11041353309868743; 0.0024123101663353604 -0.007055257202355882 -0.03850796533513981; 0.012457634858329012 0.0004573524565501684 -0.025670426435197565; 0.0012717362579324572 -0.008069416862912088 -0.0325262479570593; 0.006534630181357145 -0.006737018849765175 -0.008190343423222855; 0.003229288621689261 -0.0018072284367781496 -0.012336294647992012; -0.0002675665064839365 0.000599445313636661 -0.0014754359902690133; -0.016726151111678376 0.008158836467733818 -0.031008210751521312; 0.012664859824491139 0.00947245882687444 -0.010193683566065235; 0.005016535701541196 0.008173623765366116 0.0019020276598789565; -0.013747630199919507 -0.004213243078924748 -0.004978174623127463; 0.0010782142849711605 -0.0006007418681896908 -0.0005264123366613164; 0.0031675874801477657 0.013715580587452585 -0.0005857600231627272; -0.0002510148323933635 -0.000877848768569474 0.00077958071197183] %
+
+Mass Used: 64.21548386566474 kg
+Launch C3: 118.10824374918253 km²/s²
+||V∞_in||: 1.6698461603660889e-9 km/s
diff --git a/archive/ES_0.645646239403213 b/archive/ES_0.645646239403213
new file mode 100644
index 0000000..42f25c9
--- /dev/null
+++ b/archive/ES_0.645646239403213
@@ -0,0 +1,22 @@
+archive/ES_0.645646239403213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T20:34:56.617
+Launch V∞: [5.693388953001466, -8.741570857693475, -2.21338923469723] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2714513295519526e-5, -1.2870484599226897e-5, 3.025549290691468e-5] km/s
+ V∞_out: [2.699679971396744e-5, 2.704464811317896e-5, 1.1703848451770158e-5] km/s
+ time of flight: 1.0171484201364945e8 seconds
+ arrival date: 2026-07-14T02:42:18.617
+ thrust profile: [0.6839451375576734 -0.5331958781333331 -0.391557284453324; 0.33905106477539493 -0.08281645525342632 -0.33385713175626874; 0.13925810592462262 -0.0035682139826807976 -0.2049338713468118; 0.07648977162270185 0.0056676122149951534 -0.140367188121375; 0.054530415918832044 0.007672169681129121 -0.11558143215016121; 0.028078900307546034 0.005363133207568672 -0.06615256870120698; 0.018825010695011184 0.0042327039145775005 -0.048326036480572744; 0.010814584365029335 0.002323448957651642 -0.029690310736546245; 0.004772671610165131 0.0020067305514691004 -0.012377196411322466; 0.011194845540448691 0.00365297362509891 -0.03404383059133922; 9.248217124971478e-5 0.001313775474819335 -0.0037815651499727146; 0.0029099799852569937 0.0007429133248210276 -0.0064331232818807; 0.00115910003802116 0.0018202870677103836 -0.0034131535744328914; 0.00015119678267235567 -0.00023175133469272198 -0.001974458232598659; 0.0018751871064915993 -0.00016437586222579383 -0.0058691259296347765; 0.001216686961866299 -0.00040924734619205523 -0.0027966578879980806; -0.0002623688756988434 -0.0025574062621168984 -0.001367126159555537; 0.0005290398964310514 -0.0009557203592921813 -0.005856638825657125; -0.0013014982860927956 -0.0007284280132027756 0.0015120113834992633; -0.00044205936223899365 -0.0007761840313635702 0.005101864128945787] %
+
+Mass Used: 89.83576668578189 kg
+Launch C3: 113.72883073450855 km²/s²
+||V∞_in||: 3.9962399066017476e-5 km/s
diff --git a/archive/ES_0.6456578738158363 b/archive/ES_0.6456578738158363
new file mode 100644
index 0000000..459e575
--- /dev/null
+++ b/archive/ES_0.6456578738158363
@@ -0,0 +1,22 @@
+archive/ES_0.6456578738158363---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T19:05:36.928
+Launch V∞: [5.6924712965428474, -8.83651026306206, -2.563014978327554] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.011729254200333734, 0.2287063817103379, -0.0974218988397139] km/s
+ V∞_out: [-0.20404341382571206, -0.1059751102682988, 0.09530643595879078] km/s
+ time of flight: 1.0370899081592824e8 seconds
+ arrival date: 2026-08-07T03:08:46.928
+ thrust profile: [0.39688837444643615 -0.30700434492893197 -0.25262707141072505; 0.21957693281784088 -0.051394297706821745 -0.2294169403913236; 0.1321426066595484 -0.0031545251710446733 -0.19225500223519718; 0.08192366196327744 0.007950959444825113 -0.14899164385889516; 0.047415059721311756 0.008219959074260366 -0.10035014461973206; 0.02304145794138689 0.003636750133462803 -0.0531340744783216; 0.008587892831150573 0.0011944726792232135 -0.03731050177628386; 0.0033531080278472476 -0.0031408073293180015 -0.00936221159971267; -0.005737755075107051 0.01626828795714705 -0.02086329626390609; -0.0008995969191762402 -0.0005929944711330916 0.004020739959761821; 0.003284195710954857 -0.0015603290903294115 -0.0015880871015082646; -0.00885303410266432 -0.00042734669532657626 -0.014820265545985175; -0.0010836632663989137 -0.0003536831138268291 -0.002165011799724462; -0.020039407619473704 -0.0005904146056184049 0.004626003339498653; 0.004474572294553692 -0.009334172917642611 0.00665123118472186; 0.008963094483247152 -0.016263143232400988 0.0023989909820668637; 0.004751600080285745 -0.01286273296960769 -0.007017971088915177; -0.0013162698844417227 0.0030297351404306966 0.0042121872508283425; 0.0033980746336720008 0.02113318845291349 -0.02696699388299744; -0.03663571085697299 -0.010300475739356 -0.0077265382539399] %
+
+Mass Used: 70.43391770841163 kg
+Launch C3: 117.0571888702967 km²/s²
+||V∞_in||: 0.24886785813492726 km/s
diff --git a/archive/ES_0.6458348548455325 b/archive/ES_0.6458348548455325
new file mode 100644
index 0000000..63bb608
--- /dev/null
+++ b/archive/ES_0.6458348548455325
@@ -0,0 +1,22 @@
+archive/ES_0.6458348548455325---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T15:16:21.662
+Launch V∞: [7.298805382840118, -7.480381778588484, -1.9690133348880516] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.2891630089637728, 0.1496428007942427, 0.020373715570973963] km/s
+ V∞_out: [-0.2543856740538431, -0.13713839259808042, 0.15187202500348237] km/s
+ time of flight: 1.017045750884461e8 seconds
+ arrival date: 2027-07-28T18:32:36.662
+ thrust profile: [0.7055979730501357 -0.35144191478300074 -0.35425533323981157; 0.21124185107257556 -0.009411810532064564 -0.20850999399819684; 0.1952938420740324 0.02796538307868943 -0.2743513905547505; 0.09627154570748604 0.026000724801193212 -0.18010237963780362; 0.05062293364204318 0.017868044368067847 -0.11547842477344517; 0.027765134322677756 0.011276128718917141 -0.07356077527022445; 0.07260914896408968 0.03060628993552257 -0.18820618823487997; 0.003753926292601237 0.0014597181091260576 -0.013165855670352729; 0.03513274357094138 0.01700545030100508 -0.11329215758092062; 0.004341754871302256 0.0004810442142682723 -0.016034236357282277; 0.0019558527727430303 0.0009718474575455454 -0.001265355571635136; -1.9336114619233327e-5 -0.0002673766196350251 -0.0038221098672866745; -0.001008591152093927 0.00034856413977570446 0.0009076607506833281; 0.00037245496248315257 0.00036983832420599977 0.00047948771959956983; 0.002472934995743364 -0.00607283006014204 0.00019039448584306107; -0.0032935901292907785 0.0026818915398985383 -0.0026695980218180244; 0.0020762946080576366 -0.0013943848730533833 -0.00342147944116389; -0.0031046245780725276 -0.0014353030140727514 0.005702862410043477; -0.0012001133430367002 -0.001556368573666012 0.00220094341701659; 0.0018721731218632894 0.006094341973318139 -0.012009390462884148] %
+
+Mass Used: 93.6908343357295 kg
+Launch C3: 113.10568508298145 km²/s²
+||V∞_in||: 0.32622584488157175 km/s
diff --git a/archive/ES_0.6460746953916008 b/archive/ES_0.6460746953916008
new file mode 100644
index 0000000..fe9c114
--- /dev/null
+++ b/archive/ES_0.6460746953916008
@@ -0,0 +1,22 @@
+archive/ES_0.6460746953916008---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T08:53:45.607
+Launch V∞: [7.443623830532165, -7.51627542986256, -2.461546034022452] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.806869714498327e-5, -0.000838622425167826, 0.00011424888376010094] km/s
+ V∞_out: [0.00025485782081825255, 0.0005440652258631785, 0.0006000364057680866] km/s
+ time of flight: 1.0067906880750838e8 seconds
+ arrival date: 2027-07-17T15:18:13.607
+ thrust profile: [0.5029233713364502 -0.25928308888025153 -0.29416720403769986; 0.21173537217391097 -0.016480730817907442 -0.23038687657656312; 0.11068793113273556 0.011835417357807425 -0.18140992577368775; 0.08952598112974788 0.01861582556904238 -0.18986354724896606; 0.044200255935823586 0.012492044065448222 -0.11377166904753722; 0.014165606807611697 0.004661229333521733 -0.04030353322889887; 0.007244378353125538 0.001264477770383152 -0.023091758273428742; 0.008714504872061336 0.0042567621030144285 -0.03522462785133937; 0.0017898080824324213 0.000831459613085983 -0.007169701765191981; 0.006672918786073544 0.0044789398334471545 -0.017705537235030443; 0.00014902253331400083 0.00032168107577215264 -0.0002982733280600607; 0.0001462065856855511 0.0009624628464273416 -6.578849739105911e-5; -2.7992668619460537e-5 8.317145931858216e-5 -0.0010491924412001836; 0.0008449490860829745 -0.0004569289431436775 -4.708349893925781e-5; 0.00014107203935206868 -0.0010555227051595765 -0.00016877015121456024; -0.00013597657334394418 -0.001107908165665271 0.0001643315599519689; -0.0004095359021096171 -0.00018065668367957705 -0.0005910626139062891; -0.00038420488009707266 -0.0004362676796358821 -0.00047783448354832595; -0.000499082159185766 0.0008740852801460272 -0.0008551571227561302; -0.00035677773753636327 0.0007571750467310789 0.000684846474369777] %
+
+Mass Used: 65.64715577400466 kg
+Launch C3: 117.96114094563363 km²/s²
+||V∞_in||: 0.000849101717679225 km/s
diff --git a/archive/ES_0.646179572495116 b/archive/ES_0.646179572495116
new file mode 100644
index 0000000..96cfec2
--- /dev/null
+++ b/archive/ES_0.646179572495116
@@ -0,0 +1,22 @@
+archive/ES_0.646179572495116---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T12:27:01.115
+Launch V∞: [7.354243973254691, -7.464091057367094, -2.348357614771211] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0049992889178023005, 0.02655742544625958, 0.004593244084135498] km/s
+ V∞_out: [0.026587214464803714, -0.0040719641462785535, 0.005278537644372223] km/s
+ time of flight: 1.0350863555376512e8 seconds
+ arrival date: 2027-08-18T12:50:56.115
+ thrust profile: [0.4248793860614857 -0.2150340370982686 -0.24481978905466792; 0.2522517902193292 -0.01008076162250151 -0.25584967096000927; 0.14074285130434064 0.022541148909805325 -0.2143479200095581; 0.1364028905833704 0.037559292876774786 -0.2693588674719763; 0.05086360518863578 0.017509221293342793 -0.12362106166834709; 0.02600059859999158 0.009061465616364443 -0.07104811715265977; 0.008288457159982157 0.005280476958173671 -0.03365936695661564; 0.004032908926948421 0.0019952832131314422 -0.016168416404764234; -0.0030466078977729595 -0.00042146501256070925 0.0011576188959544528; 0.010008021740973276 0.00646776152816582 -0.041907894495592055; -0.0009319124604138193 -0.0005807689108933672 0.0008596235158678613; -0.008314260835559698 -0.005098308304187338 -0.0013618149937352755; -0.005333644362428226 -0.003710895667637195 0.005972986286200072; 1.0853448891302767e-5 0.00013086023579468513 0.006447150786985569; 0.010278697294836702 -0.021793809004731636 -0.005584679282487605; 0.024791751892247423 0.014378796167952883 0.011733284018374542; -0.02278702442480527 -0.015614515898794836 0.024118566608561254; -0.01619201890912074 0.0005621826874219077 0.01876259976678507; -0.014419619625300785 0.015243601767155002 0.023983449962103436; 0.006519950896307659 0.027558410554191934 0.005230897030319348] %
+
+Mass Used: 81.2208324745352 kg
+Launch C3: 115.31234321767431 km²/s²
+||V∞_in||: 0.02741145065905383 km/s
diff --git a/archive/ES_0.6465343875989432 b/archive/ES_0.6465343875989432
new file mode 100644
index 0000000..d2a41bc
--- /dev/null
+++ b/archive/ES_0.6465343875989432
@@ -0,0 +1,22 @@
+archive/ES_0.6465343875989432---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T11:28:25.716
+Launch V∞: [5.649826053953857, -8.992689335674022, -2.44564371327997] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0009370525921151215, 0.0005720092396252383, 0.0010188274575961764] km/s
+ V∞_out: [-0.000437794399566557, 0.0009560085978258895, -0.0010664786561432077] km/s
+ time of flight: 1.0154339231013782e8 seconds
+ arrival date: 2026-07-14T17:58:17.716
+ thrust profile: [0.4226964287964765 -0.33937680093932987 -0.26072331015168926; 0.18853172362707588 -0.05504131257965667 -0.20602507832636976; 0.09566197530734191 -0.008342033286382833 -0.14946152626212902; 0.050886864817358844 0.0010172882468083484 -0.10217996075683358; 0.028579932904628846 0.002172265771063968 -0.06755891468302601; 0.03976809699743439 0.004959982638227052 -0.10412773523775122; 0.018638988715470695 0.0026617127697714403 -0.05375647186405097; 0.01237781506518056 0.0019321519761913702 -0.03769720671411763; 0.0019921587653285787 0.0010357375338181255 -0.008802724368947659; 0.0010986124782196294 0.0007864704251243936 -0.006177052309794917; 0.002723696190179983 0.0018819424170405303 -0.007862977004881106; 0.0025102304345427633 3.7066888482329904e-5 -0.00765255515463047; 0.00019866044257841622 3.70288519659039e-5 -0.00017399653619793115; 0.0007721434458826722 0.0002432013823144278 -0.0028458985220512685; -0.00041455851883197 0.0006295303837094271 -0.001156558341628949; -0.0011080190219977734 0.0015849163228647068 -0.0016715100575672975; 0.0005675782879023825 -7.928643512488016e-6 -0.0014276019920992523; 0.005935391183931901 -0.004521889369515838 -0.008706689791858681; -0.005220937090418399 -0.0004468754013030134 0.0007148709153899906; 0.0011556068571261947 -0.0005937521661124765 -0.0027808946292176605] %
+
+Mass Used: 61.46413244767655 kg
+Launch C3: 118.77016910018695 km²/s²
+||V∞_in||: 0.0014977554937165814 km/s
diff --git a/archive/ES_0.6465619581576532 b/archive/ES_0.6465619581576532
new file mode 100644
index 0000000..dc6c229
--- /dev/null
+++ b/archive/ES_0.6465619581576532
@@ -0,0 +1,22 @@
+archive/ES_0.6465619581576532---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T11:58:03.385
+Launch V∞: [7.427418998253629, -7.359679808169638, -2.331390696619377] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.6872591408458186e-6, -4.478651259384703e-5, 6.6313887934669464e-6] km/s
+ V∞_out: [-6.325109502922317e-6, 2.8784378864136052e-5, 3.456587869506021e-5] km/s
+ time of flight: 1.0052846274435951e8 seconds
+ arrival date: 2027-07-14T00:32:25.385
+ thrust profile: [0.6546074606037663 -0.31467401943486484 -0.3428696780154922; 0.38725612407813736 -0.010785922736892108 -0.3640860017259006; 0.19384626402340044 0.03484910232774243 -0.2733391164637454; 0.10442669764491341 0.03137676819721492 -0.1911142294552967; 0.03862997944315043 0.014084113362261926 -0.08539770397450401; 0.021471488441583985 0.008795949403293785 -0.05233071175676777; 0.01194769418135068 0.005413778590446361 -0.032484326886618134; 0.006061364367146573 0.002878065843699535 -0.017650721745880043; 0.00035592469054515706 0.00025260591586357404 -0.0010293577914748315; 0.0014723301495962347 0.0001684752460402224 -0.001954550910459006; 0.0012844929323354436 0.0002854584800941324 -0.0022267290823148773; 0.00012437576533197756 -4.783723184849923e-5 -0.001423449009468732; 0.00028192004737194964 0.00015711629631769575 -0.0007012038575612967; 0.0004155097954825216 0.0003047864028767394 -0.00032329108558987315; 0.0001456671276368115 0.002004652841703675 -0.0010377229350457661; 8.058860477708945e-5 6.704213114688438e-5 -0.0002560891358025304; 0.0006210539471131048 -0.00015891372230760034 -0.004198421604994304; 0.001850863408033559 -0.0014364935298393279 -0.002559601706166429; 0.0008808867364048017 -0.00035767123501910026 -0.0020201637519332754; 8.766932436200196e-5 0.00046096376258845245 -0.00021489021987606128] %
+
+Mass Used: 84.84915364828248 kg
+Launch C3: 114.76682243468221 km²/s²
+||V∞_in||: 4.542469490949487e-5 km/s
diff --git a/archive/ES_0.6467254773167073 b/archive/ES_0.6467254773167073
new file mode 100644
index 0000000..623260c
--- /dev/null
+++ b/archive/ES_0.6467254773167073
@@ -0,0 +1,22 @@
+archive/ES_0.6467254773167073---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:37:38.643
+Launch V∞: [7.4212952907924326, -7.4386644968498254, -2.2841730443865838] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.18396705845536046, -0.09168780215745126, -0.01272169250658017] km/s
+ V∞_out: [0.16096979468287484, 0.08419410398296175, -0.09774959807248039] km/s
+ time of flight: 1.0163527170073995e8 seconds
+ arrival date: 2027-07-27T16:38:49.643
+ thrust profile: [0.5964141020784733 -0.27282403011510575 -0.31502761227093085; 0.176868528214096 -0.00596245867506103 -0.1837413202127863; 0.12323208345170714 0.021159786666221994 -0.18404122209671017; 0.09953707759295112 0.0271350183970426 -0.19381348106716215; 0.047894190582042626 0.01619348970305115 -0.11022552673404477; 0.054696525329837264 0.02041572881102141 -0.1309685558743342; 0.03968042963153963 0.018374915551767526 -0.11376164591293461; 0.002572921239919026 0.0021920575058548063 -0.009218883022070802; 0.0040839028400601884 0.0034277509007795857 -0.015211960462829077; 0.011022136614446672 0.007649548442567794 -0.033535497719350806; 0.01055947960297312 0.00933587571140014 -0.02527965593109053; -0.0060113289230072295 -0.0038905853797379488 -0.010138776758690512; 0.004495354596686569 -0.010427702827436353 -0.0002821775433372604; -0.00043015138492310395 0.0015336375939882364 -0.0008506397060654633; -0.006186243565073423 0.0012886384172796856 -0.0060108821703403325; 0.003906171192146316 0.00468929966690066 0.0025799288928529344; -0.0005890349032277079 -0.0001630224672961823 -0.000913193641560319; -0.004196918968412759 -0.002052320076525862 0.011286885727048494; -0.01265978403312625 -0.011303561220518088 -0.004129710668808672; 0.0027541201074528683 0.0007320570474215944 0.0017492049158152603] %
+
+Mass Used: 80.02339144804182 kg
+Launch C3: 115.62679978653429 km²/s²
+||V∞_in||: 0.20594264522292102 km/s
diff --git a/archive/ES_0.6467264940608112 b/archive/ES_0.6467264940608112
new file mode 100644
index 0000000..ef929cb
--- /dev/null
+++ b/archive/ES_0.6467264940608112
@@ -0,0 +1,22 @@
+archive/ES_0.6467264940608112---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T21:41:32.911
+Launch V∞: [7.165742931988689, -8.003857277880357, -2.695541527189297] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.174635330277548e-6, 1.4319000824296516e-5, -2.0046589247908367e-6] km/s
+ V∞_out: [1.9920328160482036e-6, -9.110288149763645e-6, -1.1123122678322028e-5] km/s
+ time of flight: 1.03133124092928e8 seconds
+ arrival date: 2027-08-19T13:46:56.911
+ thrust profile: [0.2988129614297015 -0.17233125831421484 -0.20488048282169877; 0.07814265395770544 -0.014160681683758678 -0.10894521768859708; 0.040319755222791645 -0.0020421001446753947 -0.0857364532591259; 0.026148725613380594 5.423246921603787e-5 -0.0720585961523526; 0.02684868952360245 0.0007270738465288323 -0.08958824195546602; 0.009311210598852385 0.00037623052283986235 -0.03546441599264913; 0.009276553311160434 0.00025070247213500806 -0.04073295579983966; 0.007776838435416959 -0.00018685888950653422 -0.0371190278664134; -0.0006073261676717578 -0.00017216667610851742 -0.0018873440742081464; 0.0007029097760683469 0.0007091001461789037 -0.0015954126368313405; -0.0009113756938455006 -0.0014355884355633426 0.0009954378752334205; -0.0009593861765434044 -0.00038440177150321324 0.0012888032172438547; 8.999665265123661e-5 0.0001469901320510419 -0.0006436345576721536; 0.0014486123658632305 -0.000350298456286654 0.003977449159198767; -0.0006185136488966356 0.00019403090402043637 5.392859024599256e-5; -0.004607446393126408 -6.288674902434973e-5 -0.0011377180734890894; -0.00017187960075995494 0.0003218684800328348 0.0026544068130134497; 0.0028908767069075495 0.00043609970913129656 -0.001369067393391969; 0.0008817038750424676 8.016704998818971e-5 0.00020441987167902536; 0.001501339946020774 -0.0018483344245913168 0.004898258560584414] %
+
+Mass Used: 38.90688430612681 kg
+Launch C3: 122.67554721682622 km²/s²
+||V∞_in||: 1.4506281748610982e-5 km/s
diff --git a/archive/ES_0.646791690477411 b/archive/ES_0.646791690477411
new file mode 100644
index 0000000..8c8bc29
--- /dev/null
+++ b/archive/ES_0.646791690477411
@@ -0,0 +1,22 @@
+archive/ES_0.646791690477411---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T23:33:24.383
+Launch V∞: [5.607666179701518, -8.837274623748588, -2.1408988492415597] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0021515456508377382, -0.002626887608498038, 0.0023824330369551935] km/s
+ V∞_out: [0.0023089557087961495, 0.0025086337236953854, 0.002351523935932914] km/s
+ time of flight: 1.0060064693084681e8 seconds
+ arrival date: 2026-07-02T08:10:50.383
+ thrust profile: [0.6788602415471329 -0.5436606712911565 -0.4160153691521292; 0.38758658832092036 -0.10491289412794505 -0.38733246626175644; 0.18946536021711247 -0.013266929435850491 -0.26540453918241613; 0.09375187683136686 0.003842037577392747 -0.16670444225405082; 0.025781351523254236 0.0028016292101309846 -0.05626314969049934; 0.017330989779473113 0.002600515047566721 -0.04259929562870375; 0.004266500334995477 0.0012559445779187352 -0.012558161172770864; 0.004424172358969433 0.000906268536101072 -0.013604531167711528; 0.005702946407638482 0.0012456750052983632 -0.01817821887644845; 0.002285676313690758 0.0010693121124924487 -0.006937398348171961; -0.0002768225830199427 -0.00018729733766946428 -0.0003419419329903136; 0.0006588912328315934 0.00017306482094534654 -0.003106680726428243; 0.0010148770877213254 0.00029533712938775204 -0.0022413172495922827; 0.0004889588106732829 0.0006088886848695726 -0.0017922369386796466; 0.000897244822713321 0.00021026909759969104 -0.0019755047761310617; 0.0009256832252070924 -0.0008611621102308824 -0.0009678187216280157; 2.995689019908614e-5 7.609768583277372e-6 -0.0005897857595170263; -0.00020617350553699945 -5.656188736670651e-5 0.0006901051832594104; -0.0013371951121266584 -0.0004245616072196879 -0.0009595179100443819; -0.0005909398243456945 -9.590502585678104e-5 -0.001212366911534118] %
+
+Mass Used: 88.85069348329671 kg
+Launch C3: 114.12679064120277 km²/s²
+||V∞_in||: 0.004147972320410887 km/s
diff --git a/archive/ES_0.646817859947368 b/archive/ES_0.646817859947368
new file mode 100644
index 0000000..d1d774a
--- /dev/null
+++ b/archive/ES_0.646817859947368
@@ -0,0 +1,22 @@
+archive/ES_0.646817859947368---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T23:52:25.757
+Launch V∞: [7.332173990896162, -7.464659774308879, -2.388819720180716] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.023043335451834374, -0.04147147785294097, -0.03141106370935174] km/s
+ V∞_out: [-0.0471766468299239, 0.027586439212558406, 0.015828845307888133] km/s
+ time of flight: 9.995480545995268e7 seconds
+ arrival date: 2027-07-08T21:05:50.757
+ thrust profile: [0.7919557356749596 -0.3837054810052795 -0.4166331635668281; 0.3732178737231278 -0.02453288230026748 -0.3783301411111846; 0.13231544988088878 0.018377958892081946 -0.20801789772066273; 0.04683216133528352 0.011389348325528242 -0.09857486074338265; 0.019898669831365307 0.006145521882830515 -0.050028963944601657; 0.014419091746568847 0.005151898499709609 -0.041915166170987346; 0.010918303684687661 0.004448379879726061 -0.03742849909312744; 0.010100982323952326 0.00385728199495711 -0.03375709135472768; 0.0013987851392452402 0.0006888633185216044 -0.005097624577878896; 0.003290017271073461 0.0007596996833881533 -0.014374590918430276; 0.0006139726657015409 0.0003646587858801264 -0.0034630435667879853; 0.000642592501161154 2.7137600437112568e-5 -0.0010697173904292163; 0.0009186879906845538 0.0010118679842951782 -0.0006445975846871401; 0.0009019421476083802 0.0001384395619185425 -0.0020507772488332463; -4.0763570859182275e-5 0.00042595819382042004 0.00012722530166783125; -0.0003888716039464448 -0.00029012881089008073 0.0015914916870564972; -0.0010983151247800555 -0.001345047606427086 -0.0017923885905934106; -0.0024278436049971442 0.00044501435079706363 -0.0023024510086682836; -0.0011381635879600344 0.002502711166037405 -0.0026130434376056147; 0.0007558641518855061 0.00040296956013548393 -0.0005725659811007377] %
+
+Mass Used: 82.68861623744215 kg
+Launch C3: 115.18838063448351 km²/s²
+||V∞_in||: 0.05689932958661019 km/s
diff --git a/archive/ES_0.646862937498053 b/archive/ES_0.646862937498053
new file mode 100644
index 0000000..0fe1dad
--- /dev/null
+++ b/archive/ES_0.646862937498053
@@ -0,0 +1,22 @@
+archive/ES_0.646862937498053---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T13:19:38.088
+Launch V∞: [7.0986916186762805, -7.509416113125887, -2.4062905368880183] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.768824929532588e-6, -3.5488343668664352e-6, 1.9787884999206212e-7] km/s
+ V∞_out: [3.907522054933168e-6, -2.587888154447536e-6, -2.1893606334908767e-6] km/s
+ time of flight: 1.0978829168345827e8 seconds
+ arrival date: 2027-10-31T06:04:29.088
+ thrust profile: [0.4124050712199185 -0.20704484865763717 -0.2433761072815041; 0.18454702136680454 -0.009459312277523097 -0.20636622778335775; 0.12946252094646418 0.01753061036119081 -0.21582917360043266; 0.0857976030153707 0.02053084095295749 -0.18322924484506645; 0.04530863672454939 0.013324209809296723 -0.1091049515061577; 0.01831608581364142 0.0038666251914607204 -0.04502530613103118; 0.015524633858003222 -0.0034648256610455043 -0.032678524295677434; -0.0012714918570216412 0.013723383735232632 -0.027212198033399228; -0.0035059308169837315 -0.015580796490384208 -0.04703151026846384; -0.030788589533276758 -0.016015590604932687 -0.009787675799499058; 0.04278108614038056 0.00017123630036632346 -0.03341159208453753; -0.0005185374640149015 0.009955983082417567 -0.00026780186892798145; -0.03908863695529184 -0.03162383133069095 -0.02050401097939559; 0.001397850994906349 0.009866742546415022 -0.017662281131552885; 0.10183195800504675 -0.09531818385235004 -0.10513892533387736; 0.006207930404633662 -0.015488498941657033 -0.015795870138954254; 0.06507158933289374 0.10809129921875922 0.0531604636379496; -0.014297176150757885 -0.021999391226829756 0.080992278054126; -0.02680903780431632 0.015993348870961894 -0.0018110192610280521; -0.028020466117756777 0.006564252022509825 0.07170830691312367] %
+
+Mass Used: 97.9976683848995 kg
+Launch C3: 112.57298720505639 km²/s²
+||V∞_in||: 5.180484798953934e-6 km/s
diff --git a/archive/ES_0.6469342765023213 b/archive/ES_0.6469342765023213
new file mode 100644
index 0000000..f980209
--- /dev/null
+++ b/archive/ES_0.6469342765023213
@@ -0,0 +1,22 @@
+archive/ES_0.6469342765023213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T17:53:11.217
+Launch V∞: [7.605879336291703, -7.0609079831931, -3.2286021325053156] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.036766786206946955, 0.096877476866614, 0.16170635646819181] km/s
+ V∞_out: [0.1663343955883821, 0.04066801214067424, -0.08711913122592607] km/s
+ time of flight: 1.0629830767497845e8 seconds
+ arrival date: 2027-09-16T01:11:38.217
+ thrust profile: [0.4425937977249236 -0.19085007638072418 -0.21859543900349176; 0.17366959320907405 0.010950460563400637 -0.16872733163457207; 0.1226020033322171 0.037469075593399515 -0.17373364458464668; 0.051356578816589595 0.02491959150286737 -0.10004367738606874; 0.04475093169782878 0.025083281918444177 -0.09654406616411683; 0.04257259034357809 0.02854039674858213 -0.11024555175485805; 0.016299718132246562 0.011816697538555156 -0.05162462803011026; 0.01973484402352472 0.0147681505075837 -0.05642283071020933; 0.00046668617457364895 0.0003805691763420268 -0.008882984935940776; -0.00010248684609235562 0.0008441362083003849 -0.0037700547958691944; 0.001740809934540948 0.0021269331714217025 -0.0022654421176851874; -0.005477172459352425 0.007038801898813776 -0.0022392021307372743; 0.005649145494208697 0.0017205605281826028 -0.005371940696302956; -0.008581961589282296 -0.0072808657905099146 -0.003875568824554631; -0.00014244672272949304 0.001184933876474466 -0.00482783773168723; 0.015421444331127344 -0.004842433665122937 -0.005319245166252018; 0.005880328840485713 -0.004430849523714539 0.005172251368312527; 0.010664129649438397 -0.006246175271572841 -0.002081382024263977; -0.0023660665486898956 -0.004702429718467644 0.006964545102681745; -0.0007700207619620145 -0.001219072282203657 0.0027925966056596575] %
+
+Mass Used: 65.66677567973375 kg
+Launch C3: 118.12969375536704 km²/s²
+||V∞_in||: 0.1920572513971982 km/s
diff --git a/archive/ES_0.646945435080171 b/archive/ES_0.646945435080171
new file mode 100644
index 0000000..1b603d3
--- /dev/null
+++ b/archive/ES_0.646945435080171
@@ -0,0 +1,22 @@
+archive/ES_0.646945435080171---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T19:48:39.245
+Launch V∞: [7.009390748790582, -7.640928553183067, -2.052656882528493] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00282669994518319, -0.0028223038406905124, 0.0020751769395543473] km/s
+ V∞_out: [0.0033472606465401386, -0.0023743357878937637, -0.001849482730749478] km/s
+ time of flight: 1.0038215318090415e8 seconds
+ arrival date: 2027-07-15T15:44:32.245
+ thrust profile: [1.0 -0.5860641779428926 -0.506751459046862; 0.525760659045853 -0.0707046747035796 -0.5081664330494382; 0.1275098672867836 0.006536612503533226 -0.1983904226992054; 0.0657216555368716 0.009329769977043656 -0.13381465527123806; 0.022739030795419377 0.004402532126029257 -0.05678820465644498; 0.013263476130023924 0.002901898224015038 -0.03761639330999528; 0.007527698756868274 0.002429371333653884 -0.0242964354618649; 0.0009195676751933002 0.0007516188311942963 -0.007242679056289068; -0.0020923007202777737 0.001863699490931863 -0.0063464730056684605; 0.0027858964689066864 0.00012216068816423876 -0.006433341098921016; 0.0005882242825185026 -0.0007816916832594289 -0.0022713419184710905; -0.0007618269254186652 0.0010998300717508951 0.0020932641286436782; 0.0006199915559271486 -0.00408113241056063 -0.0030961101360102126; -0.0029910509108695593 0.005764176400770685 -0.0016003300832379689; -0.001680715643672294 0.005981957634289185 -0.004331669707288292; -0.0003917855404845079 0.0024207784674776522 0.00042669296843458665; 0.0009622487003184729 -0.0013448719477264807 -0.0011639197617655426; -0.0035167724201701058 0.0019409611298391739 0.002418624764830541; -0.0005084531505087255 0.005178856127813705 0.0033031824165646925; -0.0006968138112697763 -0.003288041174734644 -0.0029697384258152463] %
+
+Mass Used: 103.01864366828613 kg
+Launch C3: 111.72874810147087 km²/s²
+||V∞_in||: 0.004501332122798007 km/s
diff --git a/archive/ES_0.646948849396373 b/archive/ES_0.646948849396373
new file mode 100644
index 0000000..2173be1
--- /dev/null
+++ b/archive/ES_0.646948849396373
@@ -0,0 +1,22 @@
+archive/ES_0.646948849396373---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T07:52:45.428
+Launch V∞: [7.396389692567436, -7.521815996942809, -2.391924406363089] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.019860961654389834, -0.03534344045373427, -0.026100523550349645] km/s
+ V∞_out: [-0.040472355237761666, 0.022619659284605034, 0.013234304539755468] km/s
+ time of flight: 1.0091906088369246e8 seconds
+ arrival date: 2027-07-20T08:57:05.428
+ thrust profile: [0.5274272635431192 -0.2679399162624523 -0.29876090100846636; 0.2441068474858675 -0.016369110496580883 -0.25320626827104087; 0.15711363524236588 0.019397721737589833 -0.23874258472648202; 0.06937028833633267 0.016352496519871494 -0.1399761742461117; 0.0340691463329943 0.010821414404589016 -0.08344783016970729; 0.02779833600864612 0.009428284278056545 -0.07626278726022595; 0.005609585698486358 0.0009348254490351537 -0.018916501443367456; 0.015597888663456341 0.0043790632131248215 -0.0462535280049594; 0.005233427855609161 0.003028148158193579 -0.0215196996010606; 0.0023209969885053926 0.0009456553932029117 -0.002652525483159335; 0.0056051077594889 0.0037844690012669288 -0.0036375317003670355; 0.0017807976000343596 -0.003770791875900883 -0.002660966885808467; 0.0007309891628791662 0.0012068486330375336 -0.002436579849534645; -0.0037736384056003113 -0.003981598327618671 -0.006576513605368263; -0.005285482804482541 -0.0028805690239901245 -0.0073040124341567205; -0.002112158306972634 -0.007637470748876126 -0.0036253366993028984; -0.006049522235997771 0.0022876548567776164 -0.0004862408145721877; -0.002012518323026068 0.001372568126722399 -0.003157707394772811; -0.004750591480130789 -0.001366623549693888 -0.00641508686625138; 0.006291568855717085 -0.008333908310789628 0.004362572385464268] %
+
+Mass Used: 72.24099830113028 kg
+Launch C3: 117.00559874193799 km²/s²
+||V∞_in||: 0.048216738904100095 km/s
diff --git a/archive/ES_0.6471722706121784 b/archive/ES_0.6471722706121784
new file mode 100644
index 0000000..1b7e0fb
--- /dev/null
+++ b/archive/ES_0.6471722706121784
@@ -0,0 +1,22 @@
+archive/ES_0.6471722706121784---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T07:00:44.145
+Launch V∞: [7.2977722974796775, -7.364191470579203, -1.872267088184814] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.008000232275108293, 0.04339634808176212, 0.00760136682145305] km/s
+ V∞_out: [0.04327300894241055, -0.006875535446718684, 0.00926053165292674] km/s
+ time of flight: 1.0028803632308543e8 seconds
+ arrival date: 2027-07-11T00:48:00.145
+ thrust profile: [0.8553807652052305 -0.41781726275347403 -0.41644097337133057; 0.4622697103007247 -0.017616284916607154 -0.4172536548548168; 0.2453280754495812 0.03932187350051587 -0.3258480285735781; 0.09702283444720146 0.027471257015693366 -0.17128943397190166; 0.1026235136465033 0.03715270481042631 -0.21111437272999478; 0.03819920299735479 0.016406949033889926 -0.09426651365355922; 0.02087929462534307 0.010421506350527394 -0.05894936757707209; 0.004376109607462357 0.0018977773177936913 -0.012291896893749604; 0.00019902206875818028 0.00010190254793967341 -0.0006446614691036494; 0.00029068926253926724 0.0002292815107348765 -0.0008608179787466658; 0.00015312697672170412 3.9595806791713965e-5 -0.00041730336636470057; 7.891779005913911e-5 0.00014501581558127788 -0.000313779375590749; 0.00019792462087382011 3.1333817649251806e-5 -0.0004767068407957227; 1.7170426984780022e-5 -3.740063666973035e-5 0.00014652329858033436; 0.00022942278933753664 0.00022903289280871075 -0.0006017936259744108; -0.0002418419881625291 -0.00017393203928832616 -0.0004723881599586899; -0.00012524467186093228 -0.00013451352183230315 -0.0006234731303983394; 0.0001661168770116506 -2.2937094322700936e-5 -0.00012220501715427273; -2.2523922427808332e-5 -0.000386086281912446 -0.0001455738491700774; -0.00015636910742775192 0.00013538431944698872 -3.522307635029078e-5] %
+
+Mass Used: 107.56826238504709 kg
+Launch C3: 110.99418057071333 km²/s²
+||V∞_in||: 0.04477753366190941 km/s
diff --git a/archive/ES_0.6473644843536879 b/archive/ES_0.6473644843536879
new file mode 100644
index 0000000..d5f5995
--- /dev/null
+++ b/archive/ES_0.6473644843536879
@@ -0,0 +1,22 @@
+archive/ES_0.6473644843536879---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T00:59:04.642
+Launch V∞: [7.320344791774553, -7.313500755304259, -2.138336156279436] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.7823840073856796e-6, -4.5909961667885424e-5, 6.879095093880427e-6] km/s
+ V∞_out: [-6.301084320378098e-6, 2.8576023505744435e-5, 3.623587393278726e-5] km/s
+ time of flight: 1.0021020278624453e8 seconds
+ arrival date: 2027-07-09T21:09:06.642
+ thrust profile: [0.9104890735044064 -0.436792442621099 -0.4409553865516094; 0.4912775614915341 -0.014337033669794422 -0.42974214100860575; 0.2152678300697991 0.037533317204632835 -0.27915765012472327; 0.08316008139763538 0.02518745768226594 -0.14443139922856002; 0.042462134281591596 0.016376201018187635 -0.09052587853781428; 0.038938433403753143 0.017284776234942515 -0.09331366847538111; 0.008172603397368845 0.004146546010069051 -0.02140225610345835; 0.004577396968411315 0.0030199627357514777 -0.015500204116944777; 0.0199121254245247 0.011049421462148363 -0.06102054702144075; 0.0009342844038748159 0.0006742003720859656 -0.0032266321538663573; 0.000727142080299657 0.0003743133814607 -0.0016670775728670146; 0.0007029335522625603 0.0002500343018266033 -0.0003145049809826862; -8.603846392183478e-5 0.0009376881251198159 -0.0008531940802937552; 0.00023339607837505983 -0.0014048054658047607 7.129153342408986e-5; 0.00041692168749908154 -0.001505721233668835 -0.0016542064129371403; -0.0001452430463979859 -0.000345662268739277 -0.0015814546741411272; -0.0021773896372680283 -0.00024780697286857074 -0.0007518765120758122; -0.0007672787084538181 -0.0005622319818104217 -6.657373200503092e-5; 0.00038548275382847006 0.0005013473158489178 -0.0010612358505146732; -0.0006820809517802649 -0.0019581162105474343 -0.0003967526418168648] %
+
+Mass Used: 103.98309941360185 kg
+Launch C3: 111.6472226855487 km²/s²
+||V∞_in||: 4.657631327656458e-5 km/s
diff --git a/archive/ES_0.6474305622542008 b/archive/ES_0.6474305622542008
new file mode 100644
index 0000000..2dc837e
--- /dev/null
+++ b/archive/ES_0.6474305622542008
@@ -0,0 +1,22 @@
+archive/ES_0.6474305622542008---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T10:32:04.381
+Launch V∞: [5.748310278538655, -8.747149837857451, -2.1721189078289056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.18121134361097874, 0.0802891930510992, -0.16295433513926738] km/s
+ V∞_out: [-0.12175318957496238, 0.18559253419435534, 0.12870285822868438] km/s
+ time of flight: 1.0230349391765775e8 seconds
+ arrival date: 2026-07-20T12:10:17.381
+ thrust profile: [0.5499455500642616 -0.41305652664756126 -0.321135839448722; 0.29678371058136754 -0.06994412534661759 -0.3041150932688861; 0.18243611196126405 -0.0052060186652081435 -0.2606097508107157; 0.12517453748065857 0.010773016576650408 -0.2229411065359362; 0.07013818549970678 0.010950560203064008 -0.14584168274582282; 0.033849136345556086 0.006750637523870821 -0.07873949098915936; 0.00017823876386872679 0.0004789039447416804 -0.009411884490091104; 0.008177961784969403 0.0009625792204237585 -0.010576060648035584; 0.002975972266986813 0.0008791341876118641 -0.008652621781677007; 0.001972387731109368 -0.0016059736025978476 0.0002829770220574802; 0.002486122991094937 0.0006935194235167796 -0.005247136493993418; 0.000320537121482143 0.0014800537254540031 -0.005312242896630619; 0.01606268367336098 0.002797583502009085 -0.0048987767675907476; 0.0045292399460164015 0.0029240887766644567 -0.003726513226267167; 0.0014839756411197226 -0.002004540224091019 -0.0020761055851053556; 0.009552057841646125 0.008221568740784767 -0.0038781028986652998; -0.008797455077202917 0.006295817431772362 -0.016762057004261997; -0.009571084392702645 2.9353415910820353e-5 -0.016945477328065714; 0.00781666712257527 0.003599259227764876 -0.03340658852400518; -0.0017807327868050102 -0.00010289549078191119 0.006287482987763242] %
+
+Mass Used: 88.7384782480558 kg
+Launch C3: 114.27380189403061 km²/s²
+||V∞_in||: 0.2565892065437936 km/s
diff --git a/archive/ES_0.6475923220521881 b/archive/ES_0.6475923220521881
new file mode 100644
index 0000000..a76dae4
--- /dev/null
+++ b/archive/ES_0.6475923220521881
@@ -0,0 +1,22 @@
+archive/ES_0.6475923220521881---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T08:43:39.965
+Launch V∞: [5.617089249830727, -8.765776739530097, -1.9943589092729488] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.018987634969995146, 0.1111562863381049, -0.12881251226345836] km/s
+ V∞_out: [0.11172461755762103, 0.10896914759049647, 0.07038860605069154] km/s
+ time of flight: 1.0053170641041322e8 seconds
+ arrival date: 2026-06-30T22:12:05.965
+ thrust profile: [0.8557456458137879 -0.6731978242124856 -0.4927594962260133; 0.317496283817431 -0.08245296734090599 -0.31634924243922236; 0.17255396760004119 -0.00917126403470598 -0.2422308514167013; 0.08230189955214737 0.0034438335367313346 -0.14721724696270394; 0.07941092871838001 0.009019941396776619 -0.1642995375300248; 0.017466435072233794 0.002712838550893691 -0.04259371517711413; 0.02914558938034819 0.00696730190054826 -0.07889114177558103; 0.0051780166147157814 0.0020248152545538295 -0.015990513138845957; 0.016070256019379923 0.002389862062556336 -0.039671704708618354; -1.3480166533203853e-5 9.411041806595306e-5 -6.503646527113773e-5; -0.0004370143973499061 -0.0008660169960090966 -0.0008017546581093921; -0.0004029404538120221 0.0001874591451997362 -0.0005404868013967623; 0.00036217842017152344 0.000246980033954637 -0.002208577879599041; 0.0003957835550063796 2.3007986939449225e-5 -0.00034308144195534853; -0.0005773684420344124 0.0004517685982954707 0.000506670283182491; 0.00021634592080285335 0.0002376469989332031 -0.00012324075452892062; -7.10246909560015e-5 -6.952162518191493e-5 0.00037460057419852043; 0.0002547186962949116 -0.0004632280516043976 0.0003622970119721811; 0.000778308492555283 0.0006250270306688956 -0.00015576407889461257; 0.00044793196149718134 0.0006156951653468268 0.0005995940442834166] %
+
+Mass Used: 100.04437020427758 kg
+Launch C3: 112.36800094684719 km²/s²
+||V∞_in||: 0.1711984625802935 km/s
diff --git a/archive/ES_0.6479309078153461 b/archive/ES_0.6479309078153461
new file mode 100644
index 0000000..46dbb17
--- /dev/null
+++ b/archive/ES_0.6479309078153461
@@ -0,0 +1,22 @@
+archive/ES_0.6479309078153461---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:54:14.405
+Launch V∞: [7.146770981989242, -7.503746317935004, -2.0864914034989703] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.002787497576526189, -0.008201885115924486, 0.025304829485569846] km/s
+ V∞_out: [0.007240557558663553, 0.010502215369598963, -0.023506057393110468] km/s
+ time of flight: 1.0039959287595664e8 seconds
+ arrival date: 2027-07-14T07:40:46.405
+ thrust profile: [0.9750799712203485 -0.5027289132024588 -0.4886624946894325; 0.4255590499246912 -0.03254157845979661 -0.40236185826433357; 0.17621033239142211 0.01981552820282576 -0.2514849762030155; 0.06269908129330892 0.013768533281275523 -0.11906060192395872; 0.037898023217901124 0.011495610154792854 -0.08626136805067673; 0.025652272495021246 0.008630140778649263 -0.06582758902644138; 0.014060463097222088 0.005149253262233127 -0.03914270069411151; 0.01126057643463071 -0.001137152361927957 -0.022579780808505687; 0.002954342702582965 0.004067863612748171 -0.009784258805648207; -0.0017829425100408516 -0.0021429688972485566 -0.00804540647282284; 0.0027575590859779836 0.0018894396533247495 -0.011011178977935326; 0.0037786528937065736 0.004734379842970295 -0.005366605030349033; 3.571227454287999e-5 0.0017414926737694468 0.0004264060467735805; 0.0026990626643992985 -0.0015289937264147731 0.004098680001834714; 0.0022840216770334066 0.011619059573985333 -0.010642451110815573; 0.007061649431820784 -0.0036866643672758548 -0.003978453983271718; 0.017583045195493224 -0.01489651827161514 -0.020283915579212004; 0.009398303724076502 0.006733836201820933 -0.015234406310937728; 0.001393045123937785 0.0040259751940265815 -0.007197988299819493; -0.0071336951923005945 -0.0021742282572126464 -0.00908252190256195] %
+
+Mass Used: 104.12611366072724 kg
+Launch C3: 111.7359906498017 km²/s²
+||V∞_in||: 0.026746503649780623 km/s
diff --git a/archive/ES_0.6480896010823733 b/archive/ES_0.6480896010823733
new file mode 100644
index 0000000..e778a24
--- /dev/null
+++ b/archive/ES_0.6480896010823733
@@ -0,0 +1,22 @@
+archive/ES_0.6480896010823733---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:36:37.728
+Launch V∞: [7.326029186387886, -7.525713118024719, -2.1220890869535665] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00167728795043114, 0.0031206201953427803, -0.004638871368994573] km/s
+ V∞_out: [-0.002992326232366455, 0.00355898296971568, -0.003522549347763895] km/s
+ time of flight: 1.0101873404102333e8 seconds
+ arrival date: 2027-07-21T10:22:11.728
+ thrust profile: [0.6093169072682707 -0.3056960592495238 -0.337671201263643; 0.33221579863731054 -0.024699535790144243 -0.34877600682328186; 0.14385664020118535 0.013704054175696753 -0.22717558721396017; 0.08911210029856916 0.018203057879796536 -0.18481007026658403; 0.04386965926688765 0.012878599008974931 -0.11336237623737723; 0.025488635859074037 0.008896919551554626 -0.0755433354446476; 0.00810770445654039 0.0032882473858267124 -0.028319092559671966; 0.013536861878530917 0.005228769973714297 -0.046504142058411316; 0.005938419084087139 -0.0013203534358008045 -0.008829291934646667; 0.012461389105368832 0.005682930919925947 -0.049322872417204275; 0.0013920093297497917 -0.005815482709565131 -0.0005049517113009392; 0.003565807163118462 0.0027816414659275913 -0.009101260822935841; -0.004144153786906385 0.004416223786693344 0.0018136575037454358; -0.00042502976260666244 -0.004646274616268698 -0.0016165506351594233; -0.0006231123568302686 0.00207149573303369 0.0065797899696589685; -0.012128413888247352 -0.0004275733211974018 0.0006137200685468968; -0.004515918515083367 -0.0015649178847236007 0.01323289555718691; -0.00015849847163270574 0.00863247694728694 0.006848188241406882; 0.0012107278172709805 0.00013873456602616556 -0.0011390437214261087; -0.010188093811253233 -0.008227211573959208 -0.0007322670925499594] %
+
+Mass Used: 86.37764653519616 kg
+Launch C3: 114.8103236675839 km²/s²
+||V∞_in||: 0.005837010609063538 km/s
diff --git a/archive/ES_0.6482587315303893 b/archive/ES_0.6482587315303893
new file mode 100644
index 0000000..5a832dc
--- /dev/null
+++ b/archive/ES_0.6482587315303893
@@ -0,0 +1,22 @@
+archive/ES_0.6482587315303893---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T12:22:55.535
+Launch V∞: [7.1296020401903855, -7.908447936433135, -2.4304358805791715] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.033952674186731494, -0.03450809387132536, 0.02691339726399978] km/s
+ V∞_out: [0.024407979450349917, -0.048840875630626425, 0.008910921140541962] km/s
+ time of flight: 1.0362354610329461e8 seconds
+ arrival date: 2027-08-23T20:42:01.535
+ thrust profile: [0.30362592315952375 -0.10653158590427009 -0.10844043520252356; 0.19933452659575177 -0.014029460784873809 -0.208290984378286; 0.11232006990850488 0.011896466105530091 -0.17898346922093566; 0.062108195308732336 0.012113057422709638 -0.1340389138580615; 0.04086475349358952 0.010183213420374586 -0.10862707107584706; 0.028232511524530476 0.008057577834172028 -0.08836123812944757; 0.011853385629928376 0.0031265882930566684 -0.03888606042422853; 0.0067232095431682785 0.0017234806714765826 -0.016865982159773075; -0.001608048648517318 0.0009923708799442917 -0.006927829223039394; -0.0006483391207142144 9.185550288702896e-5 -0.0012957196025095478; -0.016055676973898928 -0.008543549011483081 -0.02158038501597651; 0.0007802114837185917 0.00024225069077192876 -0.0013149802561855627; 0.010595599525169443 0.0009512008418426551 -0.008730928240717337; 0.02906325581575891 0.009915344183415473 -0.01950022246607611; 0.018408934393841732 -0.00209784723033104 0.012736673473916767; 0.02605450104476141 -0.00020897131424774278 -0.00030482815059331954; -0.005730136248008234 -0.0007030462229280863 0.007579039165721511; -0.016259506277159646 0.0005996426214279686 -0.006423663407822678; -0.006686023818607268 -0.008099423841480349 0.01847359051461407; -0.009298707736741976 -0.0032490920782930104 0.021872000533081935] %
+
+Mass Used: 60.491396709979654 kg
+Launch C3: 119.28179258436707 km²/s²
+||V∞_in||: 0.055388839844795604 km/s
diff --git a/archive/ES_0.6482777052445017 b/archive/ES_0.6482777052445017
new file mode 100644
index 0000000..74c671b
--- /dev/null
+++ b/archive/ES_0.6482777052445017
@@ -0,0 +1,22 @@
+archive/ES_0.6482777052445017---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T01:12:45.025
+Launch V∞: [7.3924308426433765, -7.579219203544606, -2.780349365205352] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.044448704768293545, -0.07406840611433928, -0.02767974245861697] km/s
+ V∞_out: [-0.0515672176737818, 0.06417127985277268, -0.03807675846914472] km/s
+ time of flight: 1.0334211928864399e8 seconds
+ arrival date: 2027-08-18T03:21:24.025
+ thrust profile: [0.312480528717063 -0.1483828100997582 -0.1896703550203287; 0.12655991643075773 -0.004885982610017958 -0.14823177360774986; 0.08218696813905334 0.012918971784518559 -0.14137840313053301; 0.04984379678290619 0.012609227585818925 -0.10855562920291519; 0.031709529386758854 0.009759260344057077 -0.08070075535500093; 0.020352545923681162 0.006983270705269978 -0.057386642652399275; 0.007190736120771664 0.0018868795563137695 -0.01952845376171475; 0.01141544265903617 0.004042603710887343 -0.036722115189946315; 0.00036593398772105917 0.009158534867913255 -0.007010381756738539; -0.0034128144090023235 0.001174390630821539 -0.024567160218456473; 0.0062570276227551375 -0.002158489213412166 -0.008951534372431416; 0.0004059941107182547 -0.004377001043147647 -0.0051012410139818914; 0.0018940006528342145 -0.0018828977743138922 -0.006800187241443773; 0.001922473346061191 -0.0009859542158189142 0.0009521149594839441; -0.015111690917100937 0.018730040358362624 0.018050163947759074; -0.016409799335951145 -0.01692425225885171 -0.054302498236258365; -0.0030688705327234517 -0.024105381934915796 0.0007823570229878937; -0.007451267059869621 0.0030939511942935493 -0.0013869968176767992; 0.01388797728163301 -0.01952690465928389 -0.057710431073650044; 0.03072422667849695 0.02276934223751424 -0.051242672656981444] %
+
+Mass Used: 57.356838919672555 kg
+Launch C3: 119.8229400912422 km²/s²
+||V∞_in||: 0.09070823712581441 km/s
diff --git a/archive/ES_0.6483846174413699 b/archive/ES_0.6483846174413699
new file mode 100644
index 0000000..e26763f
--- /dev/null
+++ b/archive/ES_0.6483846174413699
@@ -0,0 +1,22 @@
+archive/ES_0.6483846174413699---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T15:57:53.177
+Launch V∞: [5.789693785376422, -8.831538616162057, -2.4987149580420183] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.02573927133276344, -0.0105064454548187, 0.025308035933752616] km/s
+ V∞_out: [0.012715937373102481, -0.02034301734555959, -0.028945505670727113] km/s
+ time of flight: 1.0070204938372229e8 seconds
+ arrival date: 2026-07-03T04:45:22.177
+ thrust profile: [0.5103321463953614 -0.4008138050930158 -0.3076197553083875; 0.2910892519306157 -0.07365807506121069 -0.2873272705475566; 0.13610413969877797 -0.006488730303504902 -0.19614174968915318; 0.05864708720607161 0.003996572084734522 -0.11161446397971554; 0.031752303205322324 0.004638921371267894 -0.07145189386173867; 0.027847897926962906 0.005553743366507148 -0.07082697848535376; 0.005866402799603671 0.0014817628259246529 -0.01627609876778649; 0.0063506404027765615 0.001990485200742408 -0.019421450783269907; 0.003936038227581302 0.0009242402947137813 -0.011960241092242462; 0.0044879943460945804 0.0017832973363826664 -0.01548274907043298; -0.0010626778533480818 0.00015489506846056353 0.0008998243447081069; -1.4331970434094677e-5 -0.0006970604540417804 0.0016361831619423795; 0.001041926137128679 0.0001714170810303377 0.0007412025006516012; 0.0002052020880661822 0.00028414918632071003 0.0011134549547358384; 0.0005331181393239251 0.0001498283727468584 -0.0007464341506701638; -0.0006994139858427982 0.00014147204772993322 0.0004838475072817544; 0.0006099203078148626 -0.0005214695078598761 0.00022718625158232213; -0.00028235950491212354 -1.8697692376190914e-5 0.0008117353758239074; 0.0006456924588290291 0.0001660967988576427 -0.003595492389485372; 0.00035027009952055474 -0.00041052423964895867 -0.0004891710415198982] %
+
+Mass Used: 69.51419177233447 kg
+Launch C3: 117.7602048987309 km²/s²
+||V∞_in||: 0.03759510829430888 km/s
diff --git a/archive/ES_0.6483908240414462 b/archive/ES_0.6483908240414462
new file mode 100644
index 0000000..429bd4b
--- /dev/null
+++ b/archive/ES_0.6483908240414462
@@ -0,0 +1,22 @@
+archive/ES_0.6483908240414462---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:44:49.454
+Launch V∞: [7.336732028238084, -7.515076608286203, -2.359967917663452] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.011512349437379478, -0.007191422189736418, -0.02421775347198576] km/s
+ V∞_out: [-0.004356900041131716, -0.027395575992326, -0.001174268003416437] km/s
+ time of flight: 1.0073742414774458e8 seconds
+ arrival date: 2027-07-18T10:21:53.454
+ thrust profile: [0.729737278945817 -0.3727688178914925 -0.3993854850457594; 0.19652875995833619 -0.01513870256016083 -0.2130330097278539; 0.09235543363281667 0.009387493722146794 -0.14945890633418166; 0.07034496663274419 0.014209806920553642 -0.14763698179739396; 0.08360443984197485 0.02242493575320712 -0.20176621207296183; 0.026260584513323304 0.008916507041932803 -0.0782696694354542; 0.00548404514073892 0.0018476471448037966 -0.020859088650114082; 0.0030075939443224542 -0.0006702528829158241 -0.008474406091096762; -0.0010456970887106486 0.0006497174463678736 -0.005191904370332397; -0.00588483800241725 -0.00321147190323111 -0.012903453412022549; 0.0021950270926041713 -0.0021299415095196233 -0.004360846176223019; 0.0016202573596663856 0.003485584923746702 0.005194910373068097; 0.0007330540107837651 0.013566624200010721 -0.001704860760490673; -0.005353292913933563 0.008871653167849932 -0.00014822408857454936; 0.0062853211610427225 0.01229104261824604 0.0010305024744600268; 0.008021752935976123 0.002287693632316067 0.002452117413061605; -0.001050297268490403 0.004584962239172424 0.0030271663563021384; -0.0005929705509254157 0.0011700718067777695 -0.007844147036527603; -0.000191182279715658 0.008339689432850145 -0.006964452946250977; 0.015282053811891964 0.018196780243578483 -0.017801917392740917] %
+
+Mass Used: 80.52743389427042 kg
+Launch C3: 115.87346185498575 km²/s²
+||V∞_in||: 0.027762390493421912 km/s
diff --git a/archive/ES_0.6485064829377606 b/archive/ES_0.6485064829377606
new file mode 100644
index 0000000..8ecfd90
--- /dev/null
+++ b/archive/ES_0.6485064829377606
@@ -0,0 +1,22 @@
+archive/ES_0.6485064829377606---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T09:09:07.494
+Launch V∞: [7.5012120739220025, -7.472555476412223, -2.2450611878008093] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003133592066346995, -0.0049537217048602235, -0.001914035663982345] km/s
+ V∞_out: [-0.0036248989823375955, 0.004420034720999341, -0.002311131899926675] km/s
+ time of flight: 1.0264952142168418e8 seconds
+ arrival date: 2027-08-08T10:54:28.494
+ thrust profile: [0.2751512643842752 -0.12800363872400541 -0.15224186892491873; 0.1880169687829395 -0.006334440035498984 -0.19759976093965687; 0.13484788369954182 0.02175697619312583 -0.2065521977957608; 0.09869628367811495 0.026916212172257488 -0.19427519958437753; 0.07246414342558051 0.025129580742938716 -0.16960137238441234; 0.05113905259661968 0.02038866953634482 -0.13529443401091598; 0.03295385965926879 0.014659614135812989 -0.09384789763559563; 0.014900358400435923 0.006780716040118074 -0.04386920839448984; 0.0009548675557807104 -0.0037188601309493573 -0.011270995492465878; 0.006828128070062308 0.009302289039570108 -0.013421674856948425; 0.001750525921706972 0.0035542407478812263 0.0010972601427857481; -0.0004211469533803795 -0.001131106213353739 -0.002409572891280568; -0.01288157444305159 -0.02525225384254906 -0.032272049742191694; 0.002089038227186812 0.002558651098215851 0.0015108014569233993; 0.010891661913542185 0.0021907954857530772 -0.04472368327307189; -0.0027987308250016344 3.432355768331681e-5 -0.000636494148828187; 0.0006027398732330263 0.0006020330119305588 0.004728588704781306; -0.00698116029211858 -0.018605001838828374 -0.014794131488485325; 0.048220127032530626 0.008115489114461256 -0.009700579417394713; -0.007566694844145351 0.012594801195408296 0.015157711560148421] %
+
+Mass Used: 73.23008539333068 kg
+Launch C3: 117.14756766298113 km²/s²
+||V∞_in||: 0.006166221735428628 km/s
diff --git a/archive/ES_0.6486596222028239 b/archive/ES_0.6486596222028239
new file mode 100644
index 0000000..575a50d
--- /dev/null
+++ b/archive/ES_0.6486596222028239
@@ -0,0 +1,22 @@
+archive/ES_0.6486596222028239---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T09:59:44.226
+Launch V∞: [5.830408074451337, -8.825822567513498, -2.6898887561310563] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00011718407187143226, -5.8970262971872454e-5, -0.00011660839083741748] km/s
+ V∞_out: [3.477897306467986e-5, -0.0001227836724987138, 0.00012054562018379542] km/s
+ time of flight: 1.0156283990566225e8 seconds
+ arrival date: 2026-07-12T21:53:43.226
+ thrust profile: [0.4055180953143717 -0.3152793861573408 -0.240784792038166; 0.23198340629136402 -0.05375005295986878 -0.21798838059892867; 0.11237222522605922 -0.0004689370651070596 -0.14606075179592645; 0.0491787229675948 0.006392726371608967 -0.0813302351607685; 0.030692946211900024 0.006300253917142578 -0.059845648235551684; 0.054939067064415856 0.017082737783862163 -0.1044453237619567; 0.0176030163357231 0.0048926441065403 -0.036372158154079584; 0.007093019010405424 0.002307013446454554 -0.01814411373389241; 0.02083256671310199 0.007814962309859806 -0.05364039413078733; 0.004857402462188891 0.0006781516511852308 -0.0020322516349163765; 0.0017119481206351159 0.0015220149477430602 -0.002424312774745002; -0.0011855028138625262 0.0010200303447772834 -0.0013119516040686772; 0.0016234345883404163 5.703654231008926e-5 -0.0012685024157802224; 0.005012495533830152 -0.00315115277546692 -0.0008406168568823324; 0.004604314572059195 0.006515405088766083 -0.0048308321454872405; 0.0007996437905995761 -0.0002362441829434561 -0.0018818250147130378; -0.006034305637915193 -0.0006500774366992601 -0.0021679994781411563; -0.0025774937493595043 0.0013129231172193541 0.0017006162416272866; 0.006109934706288331 0.0024775307547599506 -0.005153330157386858; -0.0021081546339124448 0.004122522098945839 0.005138826839157156] %
+
+Mass Used: 61.87778690535515 kg
+Launch C3: 119.12430382821819 km²/s²
+||V∞_in||: 0.0001755195585370266 km/s
diff --git a/archive/ES_0.6488186522675999 b/archive/ES_0.6488186522675999
new file mode 100644
index 0000000..81e4885
--- /dev/null
+++ b/archive/ES_0.6488186522675999
@@ -0,0 +1,22 @@
+archive/ES_0.6488186522675999---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T15:49:47.056
+Launch V∞: [7.330583140377264, -7.5235898097651575, -2.49902683507329] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.05604606324673234, -0.08978864440816738, -0.034217475401112814] km/s
+ V∞_out: [-0.06244570527635023, 0.08020612340939828, -0.04519688030901636] km/s
+ time of flight: 9.981983433382067e7 seconds
+ arrival date: 2027-07-07T23:33:41.056
+ thrust profile: [0.7236966175225327 -0.38856888557403346 -0.399886819938483; 0.31022033027862683 -0.02251586869236617 -0.2990436060775412; 0.15690919635804498 0.018449437520830593 -0.22271993695726516; 0.040949360074317764 0.00942794902102019 -0.07649596358675147; 0.015607728649820796 0.005859222458311354 -0.03493405144764031; 0.015236813416603746 0.00507217684818895 -0.04274288616182673; 0.010619978239713791 0.0038167966014201727 -0.029267917689823324; 0.0035288202363710787 0.0014545361595171033 -0.008573273062402876; 0.005269545686051861 -0.001126113921561742 -0.010376743994969411; 0.0027112740045937955 0.0030847400320663937 -0.005285403573580972; 0.00013369882842132917 0.0037246416335710983 -0.005578082044081193; 0.0002107133484173327 -9.708968477488422e-5 -0.004628839763759023; -0.004579259708533975 0.0006674560056957934 -0.010093763188698764; 0.0006356931077955841 0.003083255358227115 -0.003536739919083983; -0.008454047470739004 -0.0066103494872024795 -0.01609932169616199; 0.004304612071870877 -0.0028194388646915402 -0.0014460988337231511; 0.0068183471108309406 0.0005770758831004103 -0.0006904882351991776; -0.001549681066827571 0.00011792532166689847 0.001036463380682559; 0.010736061728776974 0.00694126006568953 -0.01177848922382218; 0.00045018370642304923 -0.0065683184772745585 -0.002106385053016439] %
+
+Mass Used: 76.86433141052203 kg
+Launch C3: 116.58698792600194 km²/s²
+||V∞_in||: 0.11123847128102222 km/s
diff --git a/archive/ES_0.6488459433214822 b/archive/ES_0.6488459433214822
new file mode 100644
index 0000000..6ef7343
--- /dev/null
+++ b/archive/ES_0.6488459433214822
@@ -0,0 +1,22 @@
+archive/ES_0.6488459433214822---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:49:39.122
+Launch V∞: [7.125348853727696, -7.633057458457243, -1.6436767658086457] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.13583315163111404, -0.21724684573117953, -0.0844299903886635] km/s
+ V∞_out: [-0.14998745703941288, 0.17977695041176972, -0.10754854036139451] km/s
+ time of flight: 1.014515999254437e8 seconds
+ arrival date: 2027-07-27T04:49:38.122
+ thrust profile: [0.7152487943036435 -0.3798220381172371 -0.36461411766136953; 0.3800145285601531 -0.038729241183665136 -0.3676373019418099; 0.20273128712032035 0.016836669069650943 -0.29448662690426736; 0.11423728481484506 0.020199451465833483 -0.2154219739049765; 0.05081616924971609 0.012299800364035053 -0.11929356806401374; 0.08733491381465072 0.023499694312577916 -0.21869624605531982; 0.0104885067597687 0.0029108270288724777 -0.02836254314485633; 0.01810830848022978 0.005650274947720162 -0.055991883663298984; 0.005977061119380754 -0.006702006103062033 -0.011458652308191807; 7.022498071638196e-5 6.508184717278636e-6 0.0011300055069916157; 0.0034289827669263953 -0.005170432690930331 -0.020786254884061103; 0.0033815736780742184 -0.0025940158714430825 -0.004442076171063989; 0.0017111126686900722 0.006143291887662725 0.004120090322106721; 0.009873607226946666 -0.005403312177908546 -0.012180499901456702; -0.00010596997576667756 0.000674660615013542 -0.003987025822175778; -0.005439827970299464 0.004051461317412847 -0.012228389872912715; 0.0037304722342477365 0.010580445714996448 -0.011568301196644778; 0.0002862339435776528 0.0006657001900546628 0.0013331170657115612; 0.010539998536817656 0.0018254482047921651 -0.009128301826426486; -0.004062805509882712 -0.0003480019269664755 -0.008338753858257924] %
+
+Mass Used: 105.19455859738537 kg
+Launch C3: 111.7358357618875 km²/s²
+||V∞_in||: 0.2697689017274192 km/s
diff --git a/archive/ES_0.6488986014354468 b/archive/ES_0.6488986014354468
new file mode 100644
index 0000000..b57235f
--- /dev/null
+++ b/archive/ES_0.6488986014354468
@@ -0,0 +1,22 @@
+archive/ES_0.6488986014354468---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T19:32:55.447
+Launch V∞: [5.535798116945387, -8.954253331754751, -1.6222108055839561] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.08249244396780767, 0.07810006393189547, 0.07975170210632682] km/s
+ V∞_out: [-0.06012384348619417, -0.10101401429386156, 0.07375726930085671] km/s
+ time of flight: 1.0173048295086695e8 seconds
+ arrival date: 2026-07-16T06:00:57.447
+ thrust profile: [0.5172924407206839 -0.42648342841230386 -0.32220559690539613; 0.32905806625138223 -0.09591105835983506 -0.3459238838177568; 0.1908507206284227 -0.018602825364118353 -0.28248941557485424; 0.0646673243668044 -0.0005672381990590939 -0.13154434416218416; 0.07535233259982006 0.0049270868271476635 -0.17688163189141637; 0.03488892865819455 0.002682192340600517 -0.09298693905712196; 0.03893190071399288 0.00373649711501295 -0.1125983202323396; 0.037663023602014865 0.001628467461343637 -0.11592285154838684; 0.010350286306653203 0.0008401569360991404 -0.03412910476215579; 0.00915999565673871 0.0005473797913397704 -0.032807341268954314; 0.0012428819072161435 0.00017243257168888835 -0.003626907263467814; 0.0015003532797569414 -0.00021362565666502818 -0.0031913675075103585; -0.0005516421829498289 0.003437858118994507 -0.001595585016743062; 0.00165974574326616 -0.003328275027498571 -0.002076013929419108; -0.0017016197209102084 -0.0013804005794128189 0.0012119713689409935; 0.0010358233569431434 -0.0014315675487274596 -0.0014266469841955679; 0.0001609079002487658 -0.0023856669524457788 -0.0024973119541953437; -8.087484937913982e-5 4.991894898065028e-6 -0.0008469509906406736; 0.0018788314132974085 0.0010869333903324742 -0.0029492309254378975; 0.00033438093388031835 -0.0001844653988430319 -0.0011885474997194471] %
+
+Mass Used: 95.22589339969318 kg
+Launch C3: 113.45528141857051 km²/s²
+||V∞_in||: 0.13879826110871973 km/s
diff --git a/archive/ES_0.6496415947873566 b/archive/ES_0.6496415947873566
new file mode 100644
index 0000000..4a4d0eb
--- /dev/null
+++ b/archive/ES_0.6496415947873566
@@ -0,0 +1,22 @@
+archive/ES_0.6496415947873566---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-14T02:33:29.844
+Launch V∞: [5.126115519425252, -8.231029413285292, -0.49815680711497357] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.16164595205650845, -0.0028071289385774058, 0.08082410527296176] km/s
+ V∞_out: [-0.2758603226166672, 0.0027792881283479954, 0.058670107912654305] km/s
+ time of flight: 1.0816200123724887e8 seconds
+ arrival date: 2026-09-16T23:33:30.844
+ thrust profile: [1.0 -0.7596396939422246 -0.3188579775756951; 1.0 -0.17952971827524625 -0.5730740500101662; 0.8274429025536895 0.06444473629653993 -0.5881904313478777; 0.6823567849475556 0.14505496867422668 -0.5980032006879428; 0.21044463969964727 0.06565093287782159 -0.22997713880230486; 0.031144125964784393 0.011987784248592552 -0.04006235803163633; 0.001913348801690252 0.0001558744462728718 -0.0027328355889543895; 0.0008384166360874486 -9.594929712831383e-5 -0.001972910773841603; 0.01321318828811388 0.005020512586069803 -0.01878812625015455; 0.0008691044892796747 0.0013536365202148552 -0.00262848101569819; 0.0023779240493882305 0.0006468333808203184 -0.0010220282919839797; -0.0003697369491876385 0.0016101978903620025 -0.0011538719833057043; 0.00010777937532013273 0.0026601876819758695 0.0003045358246730808; -0.0001615669719810147 0.00036502082531407747 -0.0027188091680572343; 0.002745283399739808 0.0008603935238441538 -0.0012158281189186086; 0.00544954870557637 0.0011051963148749765 -0.0008370013927222557; 0.0014842320785587052 0.002602275538056321 2.0482815207760506e-5; 0.002583617032464399 -0.0010491199085820692 -0.0028639817393303723; -0.0003090765764582402 -0.00023183932524760214 -0.0015809712750073568; -6.918007414117547e-5 -9.505500228181892e-5 0.000439365528091875] %
+
+Mass Used: 207.97731052079507 kg
+Launch C3: 94.27506572533501 km²/s²
+||V∞_in||: 0.1807479731070521 km/s
diff --git a/archive/ES_0.6496914839361481 b/archive/ES_0.6496914839361481
new file mode 100644
index 0000000..b157b20
--- /dev/null
+++ b/archive/ES_0.6496914839361481
@@ -0,0 +1,22 @@
+archive/ES_0.6496914839361481---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T13:16:12.564
+Launch V∞: [7.399834154175563, -7.516526984048928, -2.4676220674940885] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.875587184834645e-5, -0.0009742176112085692, 0.00013213484715974075] km/s
+ V∞_out: [0.0002882023788983517, 0.00063398279990126, 0.0006985637431109642] km/s
+ time of flight: 9.979614541517328e7 seconds
+ arrival date: 2027-07-07T14:25:17.564
+ thrust profile: [0.703997478524298 -0.35710314529729165 -0.38483325241064975; 0.1834452939192208 -0.011462944991501236 -0.18780142417910484; 0.0846335202299834 0.010700743168148437 -0.12727352780881782; 0.09825833693526077 0.02357009839942632 -0.18278921983174937; 0.05571450905183757 0.016624356630048694 -0.12570009942411067; 0.01436525202443938 0.005188616378239584 -0.03893989126400019; 0.0075869251126363495 0.0021566900424042157 -0.018351890588210483; 0.008976892040693702 0.004024508172550177 -0.028827519247327058; 0.010750278565107884 0.0047815926194436096 -0.034934582367295235; 0.0019250634807329295 -0.001309262879790831 -0.007012324227707813; -0.002167833815570894 0.0003847187638922497 -0.003826697762564845; 0.0025307204466217042 0.00091345854787226 -0.010484014407368947; 0.0008543263878588457 0.0013265008761108679 0.002728553096462456; 0.003763009390476849 -0.002316698394272089 -0.010801816365960903; -0.004852921111188031 0.0029092318627370294 -0.0027141133013936017; 0.0012604054426521758 0.003346080778684191 -0.002182126181147893; 0.008100510795676238 -0.0013997316485257778 -0.0040193891651287665; 0.002524409340197111 0.0012150814581284853 0.0027114342773306055; -0.008711486649695701 -0.00033471991157861525 0.00852601777094988; -0.001220389684200604 0.0026029491293619303 0.003868179773129474] %
+
+Mass Used: 73.46158579670737 kg
+Launch C3: 117.34488207922264 km²/s²
+||V∞_in||: 0.0009862870064912405 km/s
diff --git a/archive/ES_0.6497643112841089 b/archive/ES_0.6497643112841089
new file mode 100644
index 0000000..4a6dfd7
--- /dev/null
+++ b/archive/ES_0.6497643112841089
@@ -0,0 +1,22 @@
+archive/ES_0.6497643112841089---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T11:25:03.607
+Launch V∞: [7.362196487457475, -7.471645784500661, -2.297286988786873] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.006538258407965021, 0.004491158950190617, 0.013428597672692142] km/s
+ V∞_out: [0.0020034287049082453, 0.0155205306682148, 0.0005445482152160488] km/s
+ time of flight: 9.992842251457813e7 seconds
+ arrival date: 2027-07-08T01:18:45.607
+ thrust profile: [0.6608925481549406 -0.2929484391760971 -0.30598771819245846; 0.3813406206300695 -0.004671336896504794 -0.3263973420633323; 0.187541152744169 0.034451557878854254 -0.24420365797191798; 0.09237461823540175 0.027022627750387447 -0.16006199504147645; 0.044549123180061045 0.01600858190675317 -0.09447920595571933; 0.038963833396714186 0.015770762390987247 -0.09300638034634424; 0.012523345798519709 0.005400274812216422 -0.0324814818526416; 0.01506312293785594 0.007051238286191979 -0.043612991515626566; 0.003402951255481901 0.0011781880922413913 -0.00640631820561182; 0.0029167547728416376 0.0018562684224336832 -0.004954741366379805; 0.0015213482701284867 0.0007695467950057071 -0.003494918486287617; 0.0015260322891325747 -0.000821146969229899 0.0006968013845731549; 0.00015274397520212532 -2.2001700620203246e-5 0.000894771311620805; -0.0004139004996374376 -0.0008620569203440002 0.0004201904484012163; -0.0025569148410254133 -0.0003821934536012181 -0.0016568239427980653; 0.006593614705691027 0.013983538740688016 -0.005800444698496653; -0.0014676032250338315 -0.0014974105892569213 0.0013624086601584967; -0.0012158324929778344 -0.002918519006330934 0.005247046173892265; 0.00449370990460591 -0.009444691482345014 -0.0069979434960050135; 0.004084231284882304 -0.008777263453075317 0.0075631206533843245] %
+
+Mass Used: 85.44612357746882 kg
+Launch C3: 115.30495535782715 km²/s²
+||V∞_in||: 0.015596363908944783 km/s
diff --git a/archive/ES_0.6498269358769477 b/archive/ES_0.6498269358769477
new file mode 100644
index 0000000..1ed85bd
--- /dev/null
+++ b/archive/ES_0.6498269358769477
@@ -0,0 +1,22 @@
+archive/ES_0.6498269358769477---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T18:13:17.545
+Launch V∞: [7.470684675641508, -7.3762828735480745, -2.2306123451786837] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0037825008086085025, 0.0069997160692640975, -0.009865939982058123] km/s
+ V∞_out: [-0.006612453573774353, 0.007689344755030591, -0.007603558925092378] km/s
+ time of flight: 9.96651270446011e7 seconds
+ arrival date: 2027-07-04T06:58:44.545
+ thrust profile: [0.7064161271794984 -0.34000807287115054 -0.36574215271220656; 0.3378949528914187 -0.010769494783653105 -0.3220826988149283; 0.13884096653856637 0.02537804517643872 -0.20279701611183185; 0.09459374108154181 0.026616819209554818 -0.17980685108900615; 0.0417949218931411 0.016833144610119373 -0.0976895726666956; 0.051677485473031304 0.02380370864980918 -0.13278104864112095; 0.01759076852845811 0.0082376892327723 -0.051843750356692996; 0.008285467688269932 0.004054683290007759 -0.026446006316342332; 0.012501580117571506 0.006045960603362657 -0.04495649201830938; 0.00018269485913275513 0.00013975157635335244 -0.00016640562649888023; -9.947312006595879e-5 -9.997467891960271e-5 -0.000127797311503424; -7.827632686842306e-5 -3.603049332411756e-5 0.0002861643409555512; -0.0003278162352809422 0.00016144438276154333 9.339454184708414e-5; -0.0002829736090205914 6.776166950625163e-6 -0.0002466883331594612; 6.544652953938341e-5 -0.00012561245879681777 0.0006927896033809801; 0.0002087095940127904 2.829345430434109e-5 -0.000343378980893164; -2.8228918743874315e-5 9.902082152245435e-5 0.0005306289451729876; -0.000393444410487103 -4.2760242857883574e-5 0.00019437131148293733; -3.062689683718269e-5 -0.00024068224831845934 0.0002762008592497486; -0.00025196516767413254 -0.00028367384450472225 0.0001735688243242922] %
+
+Mass Used: 86.15295026019794 kg
+Launch C3: 115.19630998792705 km²/s²
+||V∞_in||: 0.01267438792001456 km/s
diff --git a/archive/ES_0.6501354585848504 b/archive/ES_0.6501354585848504
new file mode 100644
index 0000000..9190620
--- /dev/null
+++ b/archive/ES_0.6501354585848504
@@ -0,0 +1,22 @@
+archive/ES_0.6501354585848504---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T05:54:23.117
+Launch V∞: [7.448372875997003, -7.399000418475566, -2.359008751507778] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.02675744840946697, 0.14558254391164627, 0.02641144620165551] km/s
+ V∞_out: [0.14528757394531652, -0.021408245983304666, 0.03224153614290387] km/s
+ time of flight: 9.89659464405894e7 seconds
+ arrival date: 2027-06-26T16:26:49.117
+ thrust profile: [0.7764418460780097 -0.3821048359490972 -0.41983161036623823; 0.32666140196020477 -0.015111419307903702 -0.3188063968509486; 0.16274979852324495 0.02410921850130945 -0.231813798440972; 0.08935284451640109 0.02300223806048265 -0.1627307438727761; 0.04977257707872771 0.016379978537013704 -0.10778677123050401; 0.02151720973741809 0.00810332247526373 -0.05292282701776388; 0.006988270298851908 0.003010619859247566 -0.019634053654754676; 0.003767976174648764 0.0016820773865584297 -0.011494098052789897; 0.0007316184169774315 0.00035787369008943946 -0.0024274568310945796; 0.0005083552264829238 0.00020953998719283476 -0.0016702079149773408; 0.00011097798169844373 0.00012094219780547097 -0.0005677753215221309; 0.0002545339102065498 0.00022437857948753547 -0.0005701223841672396; 7.126899595623728e-5 7.663027613336582e-5 -4.519753752777079e-5; 3.352613024695375e-5 0.00016263223285440214 -0.0001476263071100428; -3.5657257140304933e-5 -0.00016083409923531156 -0.00021549164614822965; 1.4925452733081788e-5 4.633502387846512e-5 -0.00011089998116775694; -7.50473692442907e-5 0.00010197568447329664 -0.0001267668739195684; 7.645636443122516e-5 -0.00010713500527025585 -0.00011060185214189198; -0.00016455485822074122 0.00019763647049967785 -0.00010102371983452201; -5.288468414549089e-5 -1.812166132769468e-5 7.637998251168817e-5] %
+
+Mass Used: 83.0591051196102 kg
+Launch C3: 115.78838798217976 km²/s²
+||V∞_in||: 0.15035891269770024 km/s
diff --git a/archive/ES_0.6501587361030429 b/archive/ES_0.6501587361030429
new file mode 100644
index 0000000..937b305
--- /dev/null
+++ b/archive/ES_0.6501587361030429
@@ -0,0 +1,22 @@
+archive/ES_0.6501587361030429---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T13:35:33.139
+Launch V∞: [7.22439374798311, -7.849875700109362, -2.3939337004902903] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.030577165616691132, -0.028171059810279325, 0.02356291975613783] km/s
+ V∞_out: [0.02656937704655412, -0.03892820973490564, 0.007393158035463254] km/s
+ time of flight: 1.0034017393255606e8 seconds
+ arrival date: 2027-07-16T21:51:46.139
+ thrust profile: [0.5890010265134081 -0.3254145598196517 -0.3203350676810296; 0.10513302835485525 -0.013844605491368275 -0.12367888299325122; 0.08858688790563786 0.002461184489996243 -0.1507010419498582; 0.09575174723615162 0.008973787145385085 -0.19815364061783514; 0.023583140762578565 0.003381464963319191 -0.06547493778440772; 0.005543315837556083 0.0010220083777464069 -0.01811451089711567; 0.03241900702566487 0.005584585634725189 -0.10701463425649763; 0.0029385758105625872 0.0006385362715837419 -0.011418081025242438; 0.00044015462317657046 -2.150499683555563e-5 -0.0025307428816653027; 0.00039443946315266315 -0.00045662328773407135 -0.00045221215014049825; 0.0004914294274822795 0.00011493309799606044 -0.0014309584515206624; -0.00019713643019334112 0.0003382661003687142 -1.4559039297722554e-5; 0.0012339258487257384 0.0011623066344819714 0.0006887225670770265; -0.000517930045700997 3.5415378506945986e-5 -0.00015409120383273918; 0.0006297693302987893 -0.0001965841313017921 -0.0016304533060852913; 0.00021150169960777515 0.00045294851203892564 -0.00019380120370727605; -4.9087030694485026e-5 0.00030857461278754086 0.0004048008936103555; 0.00042081093277147657 -0.0002858586630538469 -0.0021403335047796303; -0.0009048882381002242 -0.0002966394552393847 0.0003049040689510966; 0.0013080158496902546 0.0007938410866089943 0.0013027665935094912] %
+
+Mass Used: 61.18242156366978 kg
+Launch C3: 119.54333209540803 km²/s²
+||V∞_in||: 0.047788940722923376 km/s
diff --git a/archive/ES_0.650240156560698 b/archive/ES_0.650240156560698
new file mode 100644
index 0000000..d847db6
--- /dev/null
+++ b/archive/ES_0.650240156560698
@@ -0,0 +1,22 @@
+archive/ES_0.650240156560698---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T17:47:32.618
+Launch V∞: [7.278529979043717, -7.456528026735456, -1.5332724355374736] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.038173061638423406, -0.061947191231451974, -0.026415796200106544] km/s
+ V∞_out: [-0.04182175536742392, 0.05578900267998761, -0.033599458983463885] km/s
+ time of flight: 1.0113297454194817e8 seconds
+ arrival date: 2027-07-21T06:17:06.618
+ thrust profile: [0.6560307197984251 -0.3255046854786018 -0.3189720974265757; 0.39652853435021784 -0.016481285012810175 -0.3580894335675622; 0.25193879165945443 0.038102783563992354 -0.33145808870277815; 0.17786049958704528 0.04562322230074519 -0.2985983714350465; 0.11422904614763527 0.03631125377406154 -0.229572368666999; 0.062316295644221906 0.022454646955847594 -0.14334549671167; 0.013038270730465006 0.0051120320422216765 -0.032519708888618125; 0.02729080728086348 0.011421330866434043 -0.07404304346892944; 0.0018405677366641708 0.00224698443883217 -0.006881966386830717; 0.0036817927975657237 0.0018970311657236427 -0.008068426087992402; 0.012513972249544992 0.00016934337769396909 -0.0063456834472629285; 0.0012444393679835568 -0.0007818503618420826 -0.002110721140480955; 0.00016809637391195694 -0.0009446596836989086 -0.0009134864969001437; -0.0004566072092767019 0.007109332066915501 -0.02560335903872641; 0.003799447445578105 -0.00817331752166346 -0.02264670620818338; -0.003221946855825088 0.01001662762317465 -0.009619009060508102; -0.001629684980090173 -5.2692238262150484e-5 -0.006515126635691967; 0.005642469773819697 -0.0007211744919333568 -0.01454554022325471; 0.0006175285930746542 -0.003553112460903237 -0.0013801462141635867; 0.0038474684942119463 0.001051395705528025 -0.008967416973189896] %
+
+Mass Used: 111.53507214051479 kg
+Launch C3: 110.9277332309085 km²/s²
+||V∞_in||: 0.07741079656742021 km/s
diff --git a/archive/ES_0.6502980236990206 b/archive/ES_0.6502980236990206
new file mode 100644
index 0000000..3cddc65
--- /dev/null
+++ b/archive/ES_0.6502980236990206
@@ -0,0 +1,22 @@
+archive/ES_0.6502980236990206---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-02T08:34:47.564
+Launch V∞: [7.796994089381058, -7.517158368029384, -2.416556763970642] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.1145021067223586e-5, -1.5206751016453946e-5, -0.001037935800447528] km/s
+ V∞_out: [0.0009197883279991565, 0.0003058353392815356, -0.0003727284804768377] km/s
+ time of flight: 1.848340492770204e8 seconds
+ arrival date: 2030-04-11T15:22:16.564
+ thrust profile: [0.06772364153799365 -0.0351231005796721 -0.04695070588709518; 0.0009074257775598233 -0.0011814118170384005 -0.0022220241478872007; 0.009935366807957336 -0.017403089300876314 -0.039846444639293335; 0.007807473789338396 -0.01627019535614426 -0.036757868349050586; 0.018951349059267517 -0.04140033544405295 -0.09220150356282572; 0.0162530884800133 -0.035773409440413774 -0.07998106904910786; 0.0086177784572697 -0.01862797926953864 -0.04217013935890234; 0.006101840957704262 -0.012711821939878956 -0.02907107851262008; 0.006379826637206514 -0.013049872747931476 -0.029968599233992144; 0.006535680353895415 -0.013065123461260156 -0.030289144458736192; 0.0018136578893569522 -0.0036245092131468536 -0.00871557725311363; 0.0012623081849754301 -0.0015415617201783658 -0.004235412745738347; -0.0024136949869159796 -0.0009626847065813582 -0.0037813477865533403; 0.0009421550040619043 -0.0009986153946974243 -0.00014862508600574985; 4.013586497703228e-5 -7.645603052822879e-5 -0.0004508943955004468; 0.0007243880218139796 0.0007954570841463347 -0.003979936187146562; 0.000866075463424979 0.00024456121403931364 -0.0007664315363178295; 0.0003559102208676022 -0.00010836639456543833 -0.0006669361760613746; -0.0006126841183582048 0.0020216722233813273 -0.004266516267829755; -0.0008068056401918705 0.00018026989706368315 -0.0004737913582063787] %
+
+Mass Used: 40.36124975420125 kg
+Launch C3: 123.1405333533696 km²/s²
+||V∞_in||: 0.0010382625308866058 km/s
diff --git a/archive/ES_0.6506541710223458 b/archive/ES_0.6506541710223458
new file mode 100644
index 0000000..5da5fd6
--- /dev/null
+++ b/archive/ES_0.6506541710223458
@@ -0,0 +1,22 @@
+archive/ES_0.6506541710223458---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T14:48:49.383
+Launch V∞: [7.363846586599314, -7.630627327680949, -2.459457643774229] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0026436002031732147, -0.002285353878244672, 0.0018626005929947996] km/s
+ V∞_out: [0.0029287832432161568, -0.002109627968563303, -0.0016283536590296125] km/s
+ time of flight: 9.936670428692754e7 seconds
+ arrival date: 2027-07-03T16:40:33.383
+ thrust profile: [0.6489101492480036 -0.32493245670639137 -0.3518531275211825; 0.22308808482834927 -0.019056325207435564 -0.2416844119098063; 0.09236053113728192 0.008946550255695266 -0.15126241912304503; 0.03865808485002407 0.008766551492699367 -0.08422147900678122; 0.03919565828432127 0.011060842456440827 -0.09846196518330165; 0.028682472828169853 0.008928925959691449 -0.08399747413251697; 0.010651514548366109 0.0037560750712483967 -0.03541869361550323; 0.007074429402928098 0.002560596464381739 -0.02509850542630444; 0.0031156721081448614 0.0012271313368520328 -0.011367157695527718; 0.00048048955642870776 0.0005623107963047847 -0.0005797595751720615; 0.0005896624414245665 0.0005128106999254679 -0.0026954434047745416; -0.0003098983148379987 0.000819842747001108 0.00033380041588926236; -0.0029686656818006933 -0.005481855571592781 -0.0019068140303508932; 0.0018251446514397265 -0.005804012640292516 -0.00034307497151800674; -0.0006606159883291309 0.0016268459735030213 0.0029564631203817396; 4.602346991042397e-5 -0.00027154367905090417 0.0008490957903424657; 0.003517883928348994 0.0017062072167797235 0.0018197006459769172; 0.0041366175531448515 -0.0020059779275390754 0.0014078428158689866; 0.0012250059671081884 0.00013222130053000737 0.0011310386878754673; 0.0005331699534380176 0.002398636174115009 -0.0038477132860998066] %
+
+Mass Used: 67.83695530516343 kg
+Launch C3: 118.50164186644115 km²/s²
+||V∞_in||: 0.003959892088434987 km/s
diff --git a/archive/ES_0.6507800229883202 b/archive/ES_0.6507800229883202
new file mode 100644
index 0000000..6d93433
--- /dev/null
+++ b/archive/ES_0.6507800229883202
@@ -0,0 +1,22 @@
+archive/ES_0.6507800229883202---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T21:36:07.795
+Launch V∞: [5.830489884389274, -8.858580055552823, -2.5601951468316426] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.03085770830670453, -0.014622558209069873, 0.030219366336665908] km/s
+ V∞_out: [0.021796607074641393, -0.032168650708459985, -0.023856953820676745] km/s
+ time of flight: 9.984047931829366e7 seconds
+ arrival date: 2026-06-23T11:04:06.795
+ thrust profile: [0.49032285888043425 -0.3868976071607893 -0.3061639005524554; 0.27057085298029443 -0.07049433675842227 -0.2695161102209596; 0.14355222900104966 -0.008595939885377647 -0.19589992332481163; 0.07485455472673451 0.0034997955650890662 -0.1261843047544844; 0.032388671479309 0.0037848514053915767 -0.064043325157633; 0.008411892790506314 0.0018584777221404766 -0.020104948464809865; 0.006511602449907348 0.001575619576071361 -0.01670365085910957; 0.003474401438301571 0.0011280217484487796 -0.011371391088090972; 0.0033426643366993337 0.0012915489177077338 -0.01216428254528738; 0.0024280686638124345 0.0009888839815502092 -0.006831525543763071; 0.0012201812209437582 0.0008119611000485813 -0.002766154261842983; 0.00048598602476974484 -0.00031093145831811823 -0.0013951722481416835; 0.00019981646010532289 -7.388516386498364e-5 -0.0002378751497353975; 0.001002923433567902 -0.0004538661304765647 -0.0015911480051139717; 0.0006367002446739244 -3.484618223431786e-5 -0.0016315857769320142; 0.001403765537562893 0.0007119553305672296 -0.0015178145848313653; 0.0001763139259572037 0.001004920888396928 -0.0016049392870164632; -0.00020579774647085406 0.00022191984776447982 -0.00036574372376665856; 4.69439630430544e-5 0.00018996465430796495 -0.0012981144770614446; -0.0002295178854515162 0.0008050910295499297 0.0012847340785787963] %
+
+Mass Used: 64.93872300533258 kg
+Launch C3: 119.02365208246418 km²/s²
+||V∞_in||: 0.04559854682233761 km/s
diff --git a/archive/ES_0.6509814219222114 b/archive/ES_0.6509814219222114
new file mode 100644
index 0000000..69d3b96
--- /dev/null
+++ b/archive/ES_0.6509814219222114
@@ -0,0 +1,22 @@
+archive/ES_0.6509814219222114---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T15:12:31.799
+Launch V∞: [7.434918685069897, -7.541542472963322, -2.510983725404141] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.04477930260091653, -0.07319182234759859, -0.02763124495567733] km/s
+ V∞_out: [-0.051186324089002797, 0.06419095890530577, -0.03723489189890927] km/s
+ time of flight: 1.0081456690792675e8 seconds
+ arrival date: 2027-07-19T11:15:17.799
+ thrust profile: [0.505194015919772 -0.25380226375352094 -0.27221875001411583; 0.169748230364329 -0.011698461972921225 -0.1776867219971955; 0.0964858107518324 0.011845495425661887 -0.15165293310894581; 0.06035956282225458 0.014288493892794962 -0.1246596189134361; 0.035557976089689636 0.011229165205823437 -0.08838255554881264; 0.01661497306818055 0.0057596783507253176 -0.049602552001409464; 0.027633131130428958 0.011887437175222917 -0.08946816314632418; 0.009875100994437091 0.002247953663356618 -0.02577695931619941; 0.022170209312569703 0.003780504321631664 -0.033941734641407845; 0.008791251186958601 0.006581867869166428 -0.03219762783911968; 0.003244968916935833 0.006103054336518277 -0.006511096016952311; -0.014058812730955526 -0.004967186615995304 -0.004300530720048042; -0.0010882584173210006 -0.0042096481782591625 -0.014753037585081057; 0.005851528026940906 -0.003956538366620502 -0.004918462221827003; -0.0024448085719556262 0.008889969264877961 -0.009445028036921464; 0.0046683447941557625 -0.0005298535567133003 -0.013669106522765827; 0.01375426456942559 0.0010476320706649812 0.005289908207917426; -0.015171802464842937 0.02531696968800472 -0.01753642466990513; 0.010682944185030664 -0.008929343870264606 -0.02232971205372019; 0.011728957298892805 0.0062726156544752765 0.007767917045116453] %
+
+Mass Used: 68.4738039421718 kg
+Launch C3: 118.4579179943557 km²/s²
+||V∞_in||: 0.09014274512010119 km/s
diff --git a/archive/ES_0.6510870555226759 b/archive/ES_0.6510870555226759
new file mode 100644
index 0000000..7a9a057
--- /dev/null
+++ b/archive/ES_0.6510870555226759
@@ -0,0 +1,22 @@
+archive/ES_0.6510870555226759---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T04:45:37.998
+Launch V∞: [7.185319186483685, -7.682291729149582, -2.3910243610030597] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004487138699212509, -0.004465615419893314, 0.0030261146977402387] km/s
+ V∞_out: [0.005102878267661105, -0.003715739678756511, -0.0029662274157327482] km/s
+ time of flight: 1.0135981097702178e8 seconds
+ arrival date: 2027-07-27T08:15:47.998
+ thrust profile: [0.7164318462435791 -0.38924235174419297 -0.4313798706789381; 0.1989268234210205 -0.026898791520759326 -0.22218251870208222; 0.12809296286282354 0.004095491220716537 -0.2088954307789155; 0.042410800482228304 0.00402427945150774 -0.0822233864714878; 0.022800664702204917 0.003660387566722669 -0.04892503006048766; 0.021084120517685115 0.0037370943764260564 -0.052003249285242324; 0.007172370935748604 -0.002373003237165742 -0.017329528890963335; 0.008174638713451978 0.0007052542709251246 -0.016526611417663435; 0.0009666228947317263 0.001921678068813569 -0.026143495518742683; 0.0015693408579614545 -0.0037090759395232635 -4.195251006205384e-5; -0.002329004999596606 0.002008890357966215 -0.0015895142249325804; -0.012759998408721232 -0.0052676557304474556 -0.02701501808352194; 0.004189636518148041 -0.006118665569646903 0.0023944192853993097; -0.0002033595411989591 7.69487586129926e-5 -0.0004813716298737586; 0.03154237881437141 0.005287447381280253 -0.028980898200833105; 0.008858598026244599 0.04007541895610006 -0.024145447240808086; -0.0006721702452332202 -0.006541062957488771 -0.017658185708480854; 0.008672332670150655 4.2213286830093135e-5 -0.03612138786404754; 0.020608676336738446 0.028515030414955872 -0.012230556602106092; -0.017299921211970694 0.002538346805046633 0.03451691008816718] %
+
+Mass Used: 80.81497425291764 kg
+Launch C3: 116.36341551832072 km²/s²
+||V∞_in||: 0.007016659101612316 km/s
diff --git a/archive/ES_0.651489567491603 b/archive/ES_0.651489567491603
new file mode 100644
index 0000000..4fa67c7
--- /dev/null
+++ b/archive/ES_0.651489567491603
@@ -0,0 +1,22 @@
+archive/ES_0.651489567491603---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-05T04:39:17.716
+Launch V∞: [7.346518387800483, -7.276336135021585, -1.6976113031249818] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.7166018611151528, 0.7413101221519395, 0.09257947929776672] km/s
+ V∞_out: [-0.6766047125758017, 0.5372307319024346, -0.5702799034370203] km/s
+ time of flight: 9.996039597305384e7 seconds
+ arrival date: 2027-07-06T03:25:52.716
+ thrust profile: [0.9593003939353728 -0.46259625137752136 -0.45250362276471684; 0.42966409270697575 -0.009688173181942717 -0.3753129757225554; 0.24947205613374865 0.044782835198674056 -0.31679754687548783; 0.15122436961792882 0.04712144759072454 -0.24852012448658165; 0.14911454930987533 0.057966309445382384 -0.2867320010666115; 0.02111635000799547 0.009237452942236865 -0.048178732548430185; 0.014936160249787774 0.007149314877534779 -0.03717446753578827; 0.04153851775329111 0.020485370910123764 -0.1070250048761869; 0.0012118208567413653 0.0008329788257035598 -0.004901223076101772; -0.0008120235620370912 -0.0002914361419069488 -0.0012204403762366921; 0.0002906113063922711 -0.0005518590176070913 -0.0017531451527765985; -0.0003602805710663741 -0.00023845868807179874 0.000681020652170789; 0.00293915255611849 0.00046853619580617057 -0.0034329642885870086; 0.003327992786353131 -0.0024161439716569363 -0.0002547867115649887; 0.0029636251787723026 -0.0009455624815483468 3.390515684103656e-5; 0.0007515849181007832 -0.0015948148116984352 -0.0023792527704936868; -0.0007721788457070539 0.0002536455703039046 0.0005870255542807345; 0.0006736567109791716 -0.00028577712339212386 -0.00042326070477866377; -0.0018100370588736985 -0.0001974432757303826 3.67751871488039e-5; 0.0011296611141510362 0.005623272805388905 0.007441962001804123] %
+
+Mass Used: 119.58117143998334 kg
+Launch C3: 109.79828410860917 km²/s²
+||V∞_in||: 1.0351955779202642 km/s
diff --git a/archive/ES_0.6514959047372968 b/archive/ES_0.6514959047372968
new file mode 100644
index 0000000..8482668
--- /dev/null
+++ b/archive/ES_0.6514959047372968
@@ -0,0 +1,22 @@
+archive/ES_0.6514959047372968---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T06:10:33.584
+Launch V∞: [7.4098902096912145, -7.501018594898577, -2.407861239854223] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.12276713770332519, 0.11599256848485949, 0.013010123285811108] km/s
+ V∞_out: [-0.11196106172243964, 0.08512004123580977, -0.09448455209779685] km/s
+ time of flight: 9.95410627720028e7 seconds
+ arrival date: 2027-07-04T08:28:15.584
+ thrust profile: [0.6949371021921412 -0.35143321342514766 -0.3399412235209442; 0.1957135961265746 -0.010730858990532997 -0.19099452217529106; 0.1742262316719874 0.021714290972398232 -0.2329872909954008; 0.08734402367130599 0.02101775839055662 -0.16061538145330923; 0.01937467947242674 0.00617014465866288 -0.04328674450530147; 0.033323569682483234 0.012187490996508388 -0.08481202757493739; 0.025155438186539727 0.009946097819610821 -0.052444086159494606; 0.008819252545534223 0.008008685986459707 -0.0400884646694028; 0.0035719912399447447 0.0018869146900011324 -0.01089688148450795; 0.004352091204013608 0.009139282801895557 -0.023960245209493664; -0.0018830654843478216 -0.006104951809891645 -0.002603022155224478; 0.0035390006745054537 0.005896427505826685 -0.002534335541024307; -0.005657520478414757 -0.0013689879357389188 -0.010783278514449476; -0.0008322872982539533 -0.0017646368909135578 -0.0027483159112778382; 0.0014112627235739503 0.003515140076641149 -0.008134723615293745; 0.003497965007645285 -0.009616100752929822 -0.0016262981636386443; -0.0014660798964336711 -0.007992700508575971 -0.003353290377987873; 0.002833780938452215 -0.004126751791322755 0.004811623351464733; -0.002314960184650493 0.002872307835863851 0.00040846157641955764; -0.012474911180328695 0.005669753450671794 0.0077362059832786646] %
+
+Mass Used: 77.75618851218815 kg
+Launch C3: 116.96954863108425 km²/s²
+||V∞_in||: 0.1693968988839348 km/s
diff --git a/archive/ES_0.6515713254691005 b/archive/ES_0.6515713254691005
new file mode 100644
index 0000000..ea67284
--- /dev/null
+++ b/archive/ES_0.6515713254691005
@@ -0,0 +1,22 @@
+archive/ES_0.6515713254691005---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T15:29:15.813
+Launch V∞: [7.48875295675032, -7.625305361251228, -2.663539122848139] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.658948868026826e-5, -0.0006798086993476626, 9.263283657549092e-5] km/s
+ V∞_out: [0.00019929699104205404, 0.0004343713911654085, 0.0004955543644034207] km/s
+ time of flight: 9.898982015207286e7 seconds
+ arrival date: 2027-06-29T08:39:35.813
+ thrust profile: [0.501570449366092 -0.26218311889543844 -0.2831203944420169; 0.11575255342510778 -0.009687923702231467 -0.13070864643500626; 0.06614233786612159 0.00570475490059963 -0.11053228630087228; 0.08669621598474929 0.01623399091976637 -0.17451491413685014; 0.03471940611087557 0.008272561557083608 -0.08330834876127102; 0.008979707233387825 0.0028104167192359126 -0.02780425527465971; 0.013696316377967597 0.004124801957471159 -0.0425588122128125; 0.0035302489443224954 0.0013427624972322904 -0.013498947068305851; 0.0019971149516543525 0.0007330958044843184 -0.007742639224666118; 0.0004428886105018028 -0.0004357554215458201 -0.00025069301486454657; 0.0005846232348011123 0.000200082883893468 -0.002493744381746571; -0.0004252326007547258 0.00027238450577312095 0.0009586574874494902; -9.882522434201635e-5 -1.219510732099828e-5 -0.0002954747761690236; 4.9681432648554015e-5 4.913850464211567e-5 0.0005220330785674042; -0.0007759150400772852 -0.0004545075253835141 0.0007284258253205199; 0.00028620800371896056 -5.135206869039333e-5 9.125260650514309e-5; 0.00018268241191360748 -0.0001897560744261667 0.0010894171560675904; -0.00031538441841151175 -0.0013007839058454128 0.0012232581609804834; -0.00039293856528973116 -6.412341064472085e-5 0.0009502562733754317; -0.00025407224927698083 0.0006649833683660568 -0.0009871412057385217] %
+
+Mass Used: 52.45987678933216 kg
+Launch C3: 121.321143358506 km²/s²
+||V∞_in||: 0.0006884207146432163 km/s
diff --git a/archive/ES_0.6523154668311518 b/archive/ES_0.6523154668311518
new file mode 100644
index 0000000..e5b00e3
--- /dev/null
+++ b/archive/ES_0.6523154668311518
@@ -0,0 +1,22 @@
+archive/ES_0.6523154668311518---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T01:17:50.133
+Launch V∞: [5.861886875279479, -8.815163399324957, -2.4143711174354943] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.15523160555365412, 0.07928252183916913, -0.3115732400148524] km/s
+ V∞_out: [-0.1626191130167143, 0.2659106701173127, 0.17405049758884167] km/s
+ time of flight: 1.0206378812355423e8 seconds
+ arrival date: 2026-07-18T08:20:58.133
+ thrust profile: [0.39002722229108105 -0.2965958160305659 -0.2341694698582924; 0.16902429807570424 -0.041769774221697184 -0.18407042348021674; 0.13847579393531953 -0.005574401417389895 -0.21415053087292782; 0.09951853356804267 0.007552818555816367 -0.19252330625730718; 0.06391357451421563 0.009770537527686644 -0.14624449913602589; 0.03950640109495203 0.008282193932377434 -0.10440582774893559; 0.016697002127592776 0.004614977137221403 -0.05538564021268419; 0.0033338578719558287 0.000597108703216999 -0.022104712187195445; 0.0047381143885667255 -0.005553133970205179 -0.004231217510317882; -0.009586535981008929 -0.0004896698825984312 -0.0016466770711597674; -0.0023479066354372452 -0.0032715704777144103 0.0047581173481929554; 0.007990030718693931 0.024410245164058247 0.007941864839362003; 0.0011904665949526683 0.022882643722726033 -0.004117144926859682; 0.003880654730333555 -0.00036713450739428026 0.00015162435935671143; -0.014490460834356973 -0.005681915311146651 0.01539746256007311; -0.0010081772123308494 0.004778202034822382 0.0027285528261502424; 0.0009685453067537805 -0.001398704369006321 0.0021428219855476674; -0.015467887332651739 0.005994349475455921 0.02338738116705556; 0.018707340251720384 -0.008126949809258982 -0.03943713596154154; 0.00035393493143522103 0.00010894662883085345 -0.0010705865588378242] %
+
+Mass Used: 73.29631153921719 kg
+Launch C3: 117.89801138807886 km²/s²
+||V∞_in||: 0.35701604099157286 km/s
diff --git a/archive/ES_0.6527651908045202 b/archive/ES_0.6527651908045202
new file mode 100644
index 0000000..4b3024b
--- /dev/null
+++ b/archive/ES_0.6527651908045202
@@ -0,0 +1,22 @@
+archive/ES_0.6527651908045202---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T04:12:41.472
+Launch V∞: [7.468530357527514, -7.592883655882208, -2.520470841099647] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0025104813329302907, -0.002495107348875672, 0.001828640332487643] km/s
+ V∞_out: [0.0028684671261920034, -0.0022054874377641334, -0.00166641892510669] km/s
+ time of flight: 9.946911679557613e7 seconds
+ arrival date: 2027-07-04T10:31:17.472
+ thrust profile: [0.4820971064503837 -0.2481109340686565 -0.2848814342286654; 0.21448904806114183 -0.018254101653745865 -0.24106488802388082; 0.09291787730789024 0.00849945198773604 -0.15440940630337413; 0.05254634303887853 0.009845228129117511 -0.11199289909594203; 0.022958287742184707 0.005895699984929241 -0.059527146575075636; 0.017828133930020158 0.004893403297437392 -0.05221380169791449; 0.02941693947332308 0.009041646993629807 -0.09266840751201483; 0.008175116639023556 0.0028762768123503663 -0.029350054947631987; 0.004967382279026885 -0.0006420602390724272 -0.004141816593518197; -0.0031275746174155837 0.001348892878405521 -0.006794337672765735; -0.0008459168023635704 -0.0001131567650594985 0.0005045857225288251; -0.001737941987572933 0.0006555698740413026 -0.0018906880452611184; 0.0017938288580385889 -3.719676105427635e-6 0.0035334623798484086; 0.0065070895466903126 0.0005432715555604124 0.00038752948189848396; -0.009189150531887756 0.0037619129021239923 0.003922978412660245; 0.0003939120725696046 0.00010159518779601247 -0.0023386847009784486; 0.014954835558084353 0.002466902612526656 -0.005103535647305682; -0.010312140319722257 0.005214105355103728 0.010248643378682625; 0.010555144873281751 -0.0028850051570528754 -0.02068836629489141; -0.00041263686836867273 -0.001415370092666285 -0.0014536414996351435] %
+
+Mass Used: 62.82171575748407 kg
+Launch C3: 119.78360117390677 km²/s²
+||V∞_in||: 0.003983968206575619 km/s
diff --git a/archive/ES_0.6528690504135903 b/archive/ES_0.6528690504135903
new file mode 100644
index 0000000..4e80010
--- /dev/null
+++ b/archive/ES_0.6528690504135903
@@ -0,0 +1,22 @@
+archive/ES_0.6528690504135903---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T21:09:53.118
+Launch V∞: [7.223567586938398, -7.695309241970081, -1.7965298948112811] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00546814710146847, -0.005401964716759075, 0.0027153718707173423] km/s
+ V∞_out: [0.005944526084772295, -0.004322470208880346, -0.0035236174913663644] km/s
+ time of flight: 1.0027732927553765e8 seconds
+ arrival date: 2027-07-14T11:58:42.118
+ thrust profile: [0.6608679367214542 -0.3658661479930914 -0.3878395957595038; 0.3298060431620602 -0.03912086269400331 -0.366030373157353; 0.1367474171583129 0.0074806616137027505 -0.23520716391581942; 0.05070738491758834 0.005586079961494079 -0.11211318940820225; 0.06156205561410788 0.007542062108988061 -0.15964021195654776; 0.04264991798434546 0.006758669148527144 -0.12421531205608369; 0.0322829274437013 0.0062945365666329835 -0.10469230413808349; 0.01662496140118428 0.0033798783377983147 -0.0585247189773119; 0.0047351248302372785 0.0012839034804252294 -0.018782640845177404; 0.000776013253241063 0.0013544533311241808 -0.002470177353181169; 0.0025430523493268162 -0.001888095262304434 -0.00571616687735588; 0.004032785997954644 0.0010771804530982647 -0.013150165734846352; 0.001987929006713373 0.0006838997748219301 -0.002734673488946156; -0.004501815465722097 0.0020681391825887515 -0.0069654882528034385; 5.9783471421416545e-6 0.00020622866367140665 0.0006058531235193436; 0.01278883570398376 0.0037894684966051665 -0.010336025702614961; 0.004663044831124811 -0.0012598526004549229 -0.0027574361206283114; -0.0024551131835857834 0.002207776839634381 0.0036560858116160997; -0.003084133493777654 -0.017793681150752493 0.005671375179634341; -0.01525751017506257 0.005223880880145851 -0.0012641029415367533] %
+
+Mass Used: 93.03336820837649 kg
+Launch C3: 114.6252326755678 km²/s²
+||V∞_in||: 0.008151999749797039 km/s
diff --git a/archive/ES_0.6531506393873823 b/archive/ES_0.6531506393873823
new file mode 100644
index 0000000..5fa3f59
--- /dev/null
+++ b/archive/ES_0.6531506393873823
@@ -0,0 +1,22 @@
+archive/ES_0.6531506393873823---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T12:58:06.036
+Launch V∞: [7.448662040127088, -7.5278812208919295, -2.521565911452984] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0021233229864929134, -0.006101402528423062, 0.019259736158687313] km/s
+ V∞_out: [0.005385546107722849, 0.007959947283871852, -0.017897922869259075] km/s
+ time of flight: 9.946375894538505e7 seconds
+ arrival date: 2027-07-03T17:47:24.036
+ thrust profile: [0.5681375932871139 -0.29338153091666397 -0.3189114211974711; 0.26642844414018463 -0.020386552660663717 -0.268136874918466; 0.11773466736567306 0.013099837994570906 -0.173227830479023; 0.06474467079679766 0.013927308510334087 -0.12287222187564711; 0.023744923335929535 0.006028038268268979 -0.055663911521550744; 0.01756665944759802 0.005281112671871893 -0.0458165201283664; 0.007044187186446299 0.0025206273733342716 -0.02207301120437434; 0.006776939345332331 0.0029365702953069693 -0.023914234901661714; 0.006335498587659779 0.0026630726830928026 -0.022154925873120984; 0.004963239060860554 0.0013191186208766524 -0.010890490060506911; 0.0015796040307844072 0.0011698791627930555 -0.00921788177606233; -0.006465560510232792 0.013429888192751118 -0.02007605668339284; -0.0006146466738728719 0.0030140392590869147 0.00046211847794844045; 0.0007690511585645785 -0.0014484967527733574 0.0015022342905391447; 0.0010760942104548125 -0.00025162543548822285 0.0022272454562893996; 0.001170418632674866 0.0008175961811994837 -0.005541845466769238; -0.01099648383112652 0.021871043282873603 -0.014526594352649953; 0.004324548652431512 0.0003324475981290006 -0.028131687764314066; 0.004708330791546688 0.03150378553643466 -0.01725159242384022; 0.006914328814486739 0.0030632664198092466 0.001710688335247357] %
+
+Mass Used: 70.70158297875832 kg
+Launch C3: 118.50985650968931 km²/s²
+||V∞_in||: 0.020314355766823226 km/s
diff --git a/archive/ES_0.653265293242946 b/archive/ES_0.653265293242946
new file mode 100644
index 0000000..1e5c1f5
--- /dev/null
+++ b/archive/ES_0.653265293242946
@@ -0,0 +1,22 @@
+archive/ES_0.653265293242946---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T13:17:53.737
+Launch V∞: [7.482234307229095, -7.49893349927947, -2.6290406613885713] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.561820588044504e-5, -0.0008106927283067262, 0.00011062300985530008] km/s
+ V∞_out: [0.0002817361660095344, 0.000620265616660327, 0.00045797056905449654] km/s
+ time of flight: 9.885642989499569e7 seconds
+ arrival date: 2027-06-26T17:25:02.737
+ thrust profile: [0.657164601776612 -0.34278697382800283 -0.37863780204099073; 0.22374923237897557 -0.016369152869109886 -0.22295125772547772; 0.08557754478510604 0.01068762958002728 -0.12696631174781137; 0.05035320974458465 0.012290445307771939 -0.09874738309294435; 0.01227483592425866 0.003877146884763227 -0.031006800604470672; 0.021296903794382274 0.008117204400481423 -0.05872502583079148; 0.021492619805624637 0.00890013097359865 -0.06460287898060935; 0.0012794251306966426 0.0004411893106554257 -0.00904571344092164; 0.009949131748921343 0.004382902699241585 -0.03327166963425301; 0.00039326366292649205 -0.0009736495125672196 0.0007586579278955757; 0.00397386358694446 0.004113440341537453 -0.015516530705827437; 0.005939064592776324 -0.0014284006705613168 0.0033306648628978006; 0.0017861744600258648 -0.0013119201023205486 -0.0037463482086175412; -0.003858364805466423 -0.004410379561105228 0.003203361212969725; 0.005289692838862263 0.0034828376941808716 0.006531298769648358; 0.00291071593569965 -0.002946785481647658 -0.001981206189468345; -0.0018595292175424096 0.0002910564006507633 -0.0060647761909177695; 0.0002599913371332612 0.0009103053015183723 -0.004893802885474022; 0.006037569882281254 -0.000716946951764808 0.002706857040012579; -0.0009707609545743679 -0.005476550047899143 -0.01624504976737778] %
+
+Mass Used: 67.21965830103318 kg
+Launch C3: 119.12968865412635 km²/s²
+||V∞_in||: 0.0008208324426957171 km/s
diff --git a/archive/ES_0.6535768054328793 b/archive/ES_0.6535768054328793
new file mode 100644
index 0000000..1f4495f
--- /dev/null
+++ b/archive/ES_0.6535768054328793
@@ -0,0 +1,22 @@
+archive/ES_0.6535768054328793---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T16:15:06.796
+Launch V∞: [5.778459731757773, -8.953852755432145, -2.296875496911229] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03200461953961666, 0.18720332976309312, -0.19481014971320187] km/s
+ V∞_out: [0.1753009962774146, 0.17606819884839162, 0.11298590553565761] km/s
+ time of flight: 9.972718016327591e7 seconds
+ arrival date: 2026-06-22T22:14:46.796
+ thrust profile: [0.43826124966060886 -0.3503878256964017 -0.26263130488781167; 0.24533508118063835 -0.06492449832025576 -0.23921816369760096; 0.11220440639596174 -0.007214504926128877 -0.1556509247034281; 0.052256788919011185 0.002656859051787079 -0.09105230113533654; 0.04172685180184659 0.0031332647853980354 -0.0837438203869283; 0.06150637110586555 0.009153370493160949 -0.13697613794008834; 0.04827720203011909 0.009054620466227207 -0.11723987018764528; 0.004878421329366769 0.002574412135366552 -0.011590255107803997; 0.008913204204635585 0.0016019039364008635 -0.022722704467126223; 0.0001375805719877419 -0.0009673009943567303 -0.008909966829057318; 0.002542798211782039 0.001249566604731714 -0.008220967537645642; 0.0011517997435494722 6.156153848366252e-5 -0.004368506544500427; 0.0015226723236368665 0.0006266433322235979 -0.005314397590580601; -0.001084105806441256 -0.0012064780490448706 -0.0027357626057177373; -0.0006353288278328996 -0.00014378533595617846 -0.0006942220221097728; 0.004128497495475215 0.0006060586769284204 -0.010350026498356743; 0.011693517434619584 0.003131956882385574 -0.0010106381022211616; -0.004832819058318284 0.0005554082304400315 -0.0017037564299355852; 0.0015663308430368564 0.0006780997297896113 -0.004025340824146735; 0.004227561750431038 -0.001849598554886241 -0.004301562396827035] %
+
+Mass Used: 69.28628000442586 kg
+Launch C3: 118.83771308581714 km²/s²
+||V∞_in||: 0.2720668608587697 km/s
diff --git a/archive/ES_0.6537729994270098 b/archive/ES_0.6537729994270098
new file mode 100644
index 0000000..5d5eb19
--- /dev/null
+++ b/archive/ES_0.6537729994270098
@@ -0,0 +1,22 @@
+archive/ES_0.6537729994270098---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T05:12:54.064
+Launch V∞: [7.691808430109205, -7.622329098574237, -2.760688581939663] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0014211169010560363, -0.0012806383604121738, 0.0010613219299235816] km/s
+ V∞_out: [0.0016679766273592128, -0.0011226451762086, -0.0008628765761140208] km/s
+ time of flight: 9.916704743067868e7 seconds
+ arrival date: 2027-06-30T23:37:01.064
+ thrust profile: [0.08128927470371286 -0.04076879394703848 -0.05345836108733848; 0.09130877308728491 -0.0055555513526672545 -0.1032520571616378; 0.08364554197329396 0.01121624450479071 -0.13661682335521835; 0.060401118807653385 0.014596752266695706 -0.12729838487387113; 0.043358012378052375 0.013472958191447108 -0.11055091254271632; 0.02854086536616249 0.010181627672886289 -0.08506478897967164; 0.016724838775710155 0.006521544528584322 -0.05709398039201795; 0.008069624836304764 0.003365764633577214 -0.03128834693571072; 0.003067316573771935 0.00119511020112518 -0.012019817350853518; 0.0004325275674672139 5.9167477278974126e-5 -0.0007983435152326453; -0.0001983789107227377 -3.0584993859840404e-5 -0.00040288830106929537; 0.0003813536469743853 -0.00020353001575637664 -0.0003304287529994269; 0.0006523370240128744 9.548957707135944e-5 -0.0007777949565320147; 0.00010900320532758962 -0.00020539928593174282 0.0006309590254971395; 0.000333682275389908 0.000375159916250417 1.6636806981031526e-5; -7.531133958902099e-5 0.00041393086698232324 -0.00016481300295796204; -2.3719069875272026e-5 -0.00018004047838761947 -0.0005040590082074242; -0.00015931170830172907 8.619666566924127e-5 -0.0006603652179871449; 0.00020449100874368633 0.00016296749624851258 0.0003525204910551781; -0.0001181731200623682 -8.94466536717751e-5 0.0005502860986408089] %
+
+Mass Used: 34.238053654462874 kg
+Launch C3: 124.88521925892262 km²/s²
+||V∞_in||: 0.0021876956130968054 km/s
diff --git a/archive/ES_0.6537838056942934 b/archive/ES_0.6537838056942934
new file mode 100644
index 0000000..378072d
--- /dev/null
+++ b/archive/ES_0.6537838056942934
@@ -0,0 +1,22 @@
+archive/ES_0.6537838056942934---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T11:23:43.744
+Launch V∞: [5.606768555252042, -8.774492701550917, -2.353825136196704] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0001268191581654383, -6.491055548485698e-5, -0.00011371233945810922] km/s
+ V∞_out: [5.3497936777423725e-5, -0.00012091016473659612, 0.00012548533729324254] km/s
+ time of flight: 1.0243796626085654e8 seconds
+ arrival date: 2026-07-23T02:23:09.744
+ thrust profile: [0.6599616711153407 -0.5222053395624224 -0.40251877178781975; 0.32403580311379077 -0.08138254073987129 -0.3277444865573433; 0.1499139515908569 -0.007536380968806237 -0.22014775522529226; 0.0612781631292876 0.0012015597792688491 -0.12019275626559674; 0.030080111916457278 -0.0008801466235205998 -0.07251255869794224; 0.018380964263648214 -0.0016899785730604307 -0.05055764751527463; 0.0232088036044783 0.0001642797075402467 -0.05828366250140799; 0.010713787071779116 0.012718826386411081 -0.02423153748459978; 0.00424344498947778 0.0033667512464852414 -0.024319705716766213; 0.01337847412141847 0.001335718730188624 -0.00026464998402602304; 0.005634463076130564 2.804122954395711e-5 -0.013166804841128695; 0.015474606912089434 0.005209611687094462 -0.02793215840291663; 0.024430047454754775 -0.0027249161141387423 0.016895802492884054; 0.00367884890799987 -0.008695245438411894 0.004417699912961176; 0.020212575823320478 0.005381717358728782 0.03929595721829983; -0.02744628015811903 -0.03458452190947478 0.015288819379394622; 0.010321530858425774 0.05720612662958559 0.030423511519756155; -0.008267923280875894 -0.008309164753599845 -0.001783345585193657; -0.039915675266704406 -0.010377538701279321 0.022254341695803162; -0.012682079492003655 0.006320149703781333 0.030200036976940806] %
+
+Mass Used: 97.93403996444749 kg
+Launch C3: 113.96806857352482 km²/s²
+||V∞_in||: 0.00018228267947388588 km/s
diff --git a/archive/ES_0.6538117081299957 b/archive/ES_0.6538117081299957
new file mode 100644
index 0000000..205f642
--- /dev/null
+++ b/archive/ES_0.6538117081299957
@@ -0,0 +1,22 @@
+archive/ES_0.6538117081299957---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T02:00:01.797
+Launch V∞: [7.430266810944674, -7.590225309464484, -2.369309636544418] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01860261268240305, -0.0404561845879987, -0.025862457444020628] km/s
+ V∞_out: [-0.04268361298073193, 0.024771365489358797, 0.014707279895445192] km/s
+ time of flight: 9.9018580743808e7 seconds
+ arrival date: 2027-06-29T03:09:41.797
+ thrust profile: [0.5975537312146394 -0.3077094788767277 -0.3287648750655911; 0.21148462135639842 -0.01569903473327477 -0.21655152858815477; 0.11559812251897111 0.014077940066503735 -0.17931029002197332; 0.07944129099154536 0.018193853986438926 -0.15907303038486068; 0.04921254723941965 0.015405779450255388 -0.12290923031918476; 0.021961901841331382 0.00943011174890249 -0.061868014272221494; 0.012986005418322477 0.0047278037020428145 -0.04030470901629322; 0.013575356770433807 0.005100544101207484 -0.04451584254543578; 0.0016695883931484832 0.001554538731149253 -0.005711714939259151; -0.00030072057158453446 0.00034226803366956926 0.0009734668751112075; 0.006050774952357906 -0.0009281929282281148 -0.006879483264783915; -0.005013502429977972 -0.002032205479365027 0.0024040750363703363; 0.0004897881718444322 0.001472368643582116 0.002649393670392513; 0.0011109695087700823 -0.0008709854045616668 -0.006602301997080356; -0.0009072192298826855 0.0007651123544158764 0.004702458188193303; -0.013274380887036428 -0.004010507924070117 -0.00031323990693927616; -0.006593597249911371 0.0026415365520077805 0.005251419256780474; -0.000644677461346384 0.001313849023886075 0.0019331180293217995; 0.000802268722717806 0.010450063559709786 -0.008206773223560584; -0.009778957433461567 -0.009893857772607284 -0.007022798730245932] %
+
+Mass Used: 71.91524866117516 kg
+Launch C3: 118.43401328408339 km²/s²
+||V∞_in||: 0.05149394891706698 km/s
diff --git a/archive/ES_0.6539972056893552 b/archive/ES_0.6539972056893552
new file mode 100644
index 0000000..7d93243
--- /dev/null
+++ b/archive/ES_0.6539972056893552
@@ -0,0 +1,22 @@
+archive/ES_0.6539972056893552---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T14:45:10.046
+Launch V∞: [5.690211588175193, -8.801647478641828, -2.024543049507217] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001017380114061766, 0.0006061789409311578, 0.0011012929027614307] km/s
+ V∞_out: [-0.00047553441648726834, 0.001015870250534697, -0.001165107034716642] km/s
+ time of flight: 9.895477524362344e7 seconds
+ arrival date: 2026-06-12T22:11:25.046
+ thrust profile: [0.8701859915665033 -0.6883017916407034 -0.43289304750781504; 0.3059612950071027 -0.07668653372965718 -0.28569667969818663; 0.13112925437742998 -0.006115680847195933 -0.17745859688404297; 0.06878706919952471 0.004345542708715939 -0.11416867411975865; 0.0851445244188068 0.010605642242978422 -0.1610533393859268; 0.030766210111235204 0.005600423839684125 -0.06767085376257813; 0.0297654027465442 0.00667716702566786 -0.07285111522998296; 0.06552754665556622 0.016844290624502985 -0.15990214843632225; 0.0010164494897982829 0.0003183037761520049 -0.0021503004467795252; -0.0002612485722971428 -1.3706469658084715e-5 -0.0008575456453886638; 2.3480678861726692e-5 3.973341796236331e-6 -0.0006974814501507949; 0.0010101045046102492 0.00019643308006260193 -0.0024660883046284296; 0.0007038666987306744 2.9571457345364425e-5 -0.001766104799203728; 0.0005020081537413523 -2.8274851814391708e-5 -0.0012204554190588814; 0.0011201683557253385 -3.337055372829977e-6 -0.0010495084072692333; 0.00035889657195615457 -0.00021182423262711234 -0.0004308349037494523; 0.00021063710299164558 -0.0003448112499298274 0.00017848929097040683; 0.00023898382852379255 0.00020663510820175522 -0.0008919843462015539; 0.0005313224653066958 -0.0004927281813386023 -0.00029689612781151305; -0.00021323093850845445 -0.00025955614488932664 -0.0004210137924461713] %
+
+Mass Used: 98.31010187878701 kg
+Launch C3: 113.94628081579326 km²/s²
+||V∞_in||: 0.0016172078600444192 km/s
diff --git a/archive/ES_0.654049350628175 b/archive/ES_0.654049350628175
new file mode 100644
index 0000000..a64d2bb
--- /dev/null
+++ b/archive/ES_0.654049350628175
@@ -0,0 +1,22 @@
+archive/ES_0.654049350628175---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:36:02.158
+Launch V∞: [7.384931513887987, -7.451064543300228, -2.164158299259665] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03131259517064371, 0.1517090196189386, 0.0270162024971073] km/s
+ V∞_out: [0.1518139900195004, -0.022362817768421653, 0.03427723104521293] km/s
+ time of flight: 9.782297271396372e7 seconds
+ arrival date: 2027-06-14T03:38:54.158
+ thrust profile: [0.9845992554955691 -0.49950467310810576 -0.5136874225328574; 0.2710755868410266 -0.016873381417130743 -0.2655971161210498; 0.20303009986027487 0.02627513837851121 -0.2860387210264975; 0.06657310500120504 0.016050861241427742 -0.12521509837734113; 0.04973199517434405 0.015781550615383912 -0.11104373848887043; 0.041335872373439025 0.014674586307218325 -0.10290520848286411; 0.007720400169490959 0.0030564011918512383 -0.022118455798144365; 0.005046563911503484 0.0019925004987114874 -0.016248053837741618; 0.0020662810442571766 0.0010926724218346293 -0.007699927679101306; 0.002143641730446633 0.001020996264055924 -0.0076208725016557784; 0.0011694082717019702 0.0004430479164616711 -0.0035534578576130148; 0.0011713306568938084 0.0005233518230332647 -0.0031754648918452958; 0.002076554892849458 -0.0010335926233639786 -0.0022377937672451724; 0.0006759906965540907 0.00042463138898056116 -0.0004487248797616065; 0.0003480622735440752 0.0014349268387414882 -0.0030124023009296115; -0.00014152921729045965 -0.00021814485406942166 -0.00014048525605974598; 0.0017028624535302803 -0.0013098056892211728 -0.0010894944218298305; 2.9422550708773103e-5 -0.0015926724349221055 -0.00010380130824791964; -0.0010696454485973335 -0.0010144849862104763 -0.0023020744803482563; -0.0001380995858828054 -0.00014988363801299943 0.001557923386492447] %
+
+Mass Used: 93.74582401414273 kg
+Launch C3: 114.73915743749625 km²/s²
+||V∞_in||: 0.1572449695456895 km/s
diff --git a/archive/ES_0.6540686657307949 b/archive/ES_0.6540686657307949
new file mode 100644
index 0000000..50be62c
--- /dev/null
+++ b/archive/ES_0.6540686657307949
@@ -0,0 +1,22 @@
+archive/ES_0.6540686657307949---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T03:15:41.597
+Launch V∞: [7.187839525865077, -7.90509492293374, -2.52036536365824] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03361022776387035, -0.030553053075765592, 0.024567730885062374] km/s
+ V∞_out: [0.02434316529506176, -0.04474299075872957, 0.007993349929595843] km/s
+ time of flight: 1.0080692660090601e8 seconds
+ arrival date: 2027-07-22T21:11:07.597
+ thrust profile: [0.5342444357946243 -0.3034936746377878 -0.3350526985113195; 0.18434236383034272 -0.030044880824742454 -0.21709181338962721; 0.04900133982769914 0.00014301630242798618 -0.08925080667346057; 0.02928556144615094 0.0020521969833535497 -0.06944190021971215; 0.008046108904059482 0.0011112541178994128 -0.03867114100641359; 0.008120392497580167 0.004757878068336165 -0.025460243243124313; 0.009895847729814031 0.001251871062409516 -0.036671336092078406; 0.017101873372750664 0.0025339392229695393 -0.05937406148208436; 0.009010137573607076 -0.0029941566065300293 -0.010572043102765154; -0.00203794707967789 0.002797439187192384 -0.009891320971904292; -0.009399670835877649 0.0004575863787966779 -0.01629736784900595; 0.0010101947832072105 -0.003377082125212469 -0.007613034138147122; 0.004055259947509974 -0.0019087252850742988 -0.012487897480488803; 0.002967763145060841 -0.003958540567829356 0.0006085872212633408; 0.0017767327722954937 0.00133714122457146 0.00975601643418854; -0.00451187987057397 -0.0024780548778994102 0.019967161746177697; -0.012917836077716282 0.009894699504957642 0.0019844740609557317; 0.007471906497048023 0.004215327889783317 -0.018995145178062327; -0.00197696966716482 0.004296296130903933 0.021996113539772016; 0.004132571664030088 -0.004694477324447915 -0.003649412861375951] %
+
+Mass Used: 60.11791793962357 kg
+Launch C3: 120.50780435650923 km²/s²
+||V∞_in||: 0.05164019619860713 km/s
diff --git a/archive/ES_0.6540870897847402 b/archive/ES_0.6540870897847402
new file mode 100644
index 0000000..f211228
--- /dev/null
+++ b/archive/ES_0.6540870897847402
@@ -0,0 +1,22 @@
+archive/ES_0.6540870897847402---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T17:19:49.022
+Launch V∞: [7.2449241078899504, -7.563469434625708, -2.3584513223349344] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.10137774888782444, -0.16198799649706314, -0.06482446418715461] km/s
+ V∞_out: [-0.11828240614176397, 0.14111828469626614, -0.08254290112557175] km/s
+ time of flight: 1.0284736212483789e8 seconds
+ arrival date: 2027-08-12T02:02:31.022
+ thrust profile: [0.5632050523555721 -0.29049147198223596 -0.32265613293811507; 0.23784705689730481 -0.020121495876044237 -0.2569486686330897; 0.13373168215849307 0.012279209073249581 -0.2129352035880481; 0.08919151684666954 0.016612444808614357 -0.18293921006015207; 0.035724843493035736 0.007997905322614542 -0.08674494567580594; 0.00621653127301844 0.000711160669532902 -0.040275816336838674; 0.014239883172597506 -0.012292277615592841 -0.012821723063712898; 0.002105335554020144 -0.022233090175576134 -0.02666873323451447; 0.02591702857084037 0.01100202798483353 -0.040887285416437845; 0.0015078465896694701 -0.0033458761948782895 -0.008907401936939154; 0.01434735391690296 0.012114289173378645 0.004377319579259907; 0.031536342048578456 0.03385180362502478 0.010025115974027362; -0.03940121589822193 0.020387562537904937 -0.02091106344273253; 0.04218139810307164 0.03305292529627967 0.005521991634664821; -0.019460425152991248 0.0032951828730769963 0.0033142431659914044; 0.058437406746179435 0.0010441119047813036 -0.004887960260160642; -0.013455810681254302 -0.007351050600126804 -0.08575495758087205; -0.01653398874463375 -0.01628679060796344 0.009624449425120547; 0.017356185739622727 -0.0010397697916146723 -0.05226443098264526; 0.023215218820996118 -0.02106223665437285 6.871495421361556e-5] %
+
+Mass Used: 90.76742558054684 kg
+Launch C3: 115.25728785742572 km²/s²
+||V∞_in||: 0.20179140253203806 km/s
diff --git a/archive/ES_0.6544801582302724 b/archive/ES_0.6544801582302724
new file mode 100644
index 0000000..43d18bb
--- /dev/null
+++ b/archive/ES_0.6544801582302724
@@ -0,0 +1,22 @@
+archive/ES_0.6544801582302724---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T14:08:46.254
+Launch V∞: [7.524359236013846, -7.510338132501804, -2.530429448414841] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003024820896825414, -0.008585825395663969, 0.026576769695643404] km/s
+ V∞_out: [0.007823247245387877, 0.011357734738741385, -0.024476806796528593] km/s
+ time of flight: 9.792716111549386e7 seconds
+ arrival date: 2027-06-16T00:08:07.254
+ thrust profile: [0.6688013843385157 -0.3365934581013069 -0.3688678075629734; 0.23160656413555505 -0.017259938439296813 -0.23874260061290734; 0.08608756025635972 0.01131224192614214 -0.13559172984462017; 0.06137448830079712 0.014797914385115095 -0.12354577350352731; 0.027398469016465532 0.008420367778936117 -0.0669580276700466; 0.022107360635085074 0.007901084864628776 -0.062245032777079635; 0.015331391116237917 0.0060108375054849115 -0.04740557660880007; 0.005693218502120513 0.0022074556393268207 -0.018532562766841735; 0.003944775976206951 0.0015808857902551616 -0.01378153975143276; -0.00035980786712178775 0.00022391369123938722 -0.0021963028636890827; 0.0014908183941648614 0.0006089818797425943 -0.005406047251806722; 0.001231822088732973 0.00024112252717650278 -0.0014314100552035329; 0.0008391181641968323 4.305753374127316e-5 -0.0022852433940069067; -0.0013675319938697913 0.0015146474766639974 -0.002913686381271134; -4.9500908334162074e-5 0.00036787210857161095 -0.0001961077049593648; -0.001014054245468459 0.0008457404163652913 -0.0017118893430975654; -0.0007651998558144747 0.000607693369640128 -0.0011636448144011807; -0.0007446745415771799 0.0003685920540901263 -0.0011576682764132063; 0.00010213249196681191 -0.0008141409145602266 -0.0001241909333263323; 0.0015228782885002028 -0.0008686735953085882 -0.002500468299218013] %
+
+Mass Used: 66.91881977405274 kg
+Launch C3: 119.4242339705026 km²/s²
+||V∞_in||: 0.02809253684945469 km/s
diff --git a/archive/ES_0.654498935075527 b/archive/ES_0.654498935075527
new file mode 100644
index 0000000..7d38d7f
--- /dev/null
+++ b/archive/ES_0.654498935075527
@@ -0,0 +1,22 @@
+archive/ES_0.654498935075527---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T15:57:48.631
+Launch V∞: [7.492668778280944, -7.546673981553565, -2.3169413414769546] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00012625348013859517, -0.0015416801593571188, 0.00020972096318956808] km/s
+ V∞_out: [0.0004609467230017581, 0.0010125252007460875, 0.0010948967288974259] km/s
+ time of flight: 9.831214295286682e7 seconds
+ arrival date: 2027-06-20T12:53:30.631
+ thrust profile: [0.5965384170196718 -0.3051591072366751 -0.3368774978675052; 0.25762112289929073 -0.01993562311526428 -0.2713579090215876; 0.11411401193620786 0.011491538020472213 -0.17692705504649903; 0.07360355938907877 0.014801927408161636 -0.14570351252536037; 0.05626563259455481 0.014804507846864897 -0.1320132140178784; 0.03626979741345428 0.010916394883850763 -0.09673420841478038; 0.0058647603794958906 0.0019705432726178683 -0.018952307870844766; 0.012761180327429069 0.004587373971142037 -0.04113512800150826; 0.0006481624494941583 0.0002562988011958712 -0.0020230173921744225; 0.0012923132932161241 0.0005287578228537886 -0.0038505192197385426; -0.00023547478583604018 -0.00016090409953244675 -0.00026642048228429184; 0.0006150437593423017 -0.00152542257576431 -0.0011108960190541282; -0.0015588848523073414 -0.0006774129636961236 -0.0032907077083547485; 0.00010891558982618118 9.197876768113453e-5 -0.0024113074345091783; 0.0009126797885596632 -0.0012550536653793487 -0.0006537488284554653; 0.004679976936317414 0.004698358531692917 0.0009682414082966921; 0.0006652189788082697 0.004352628932022608 -0.005470470730016472; 0.0009260160053207599 -0.0002089748712020016 0.002839947275092774; -0.0022284089198478466 -0.0018534478515882164 0.0013350755189124354; -0.005547456177668624 0.0032065788767761073 0.0003624849044725749] %
+
+Mass Used: 72.56197801053122 kg
+Launch C3: 118.46059078472862 km²/s²
+||V∞_in||: 0.0015609934456632603 km/s
diff --git a/archive/ES_0.6549358321993052 b/archive/ES_0.6549358321993052
new file mode 100644
index 0000000..174e519
--- /dev/null
+++ b/archive/ES_0.6549358321993052
@@ -0,0 +1,22 @@
+archive/ES_0.6549358321993052---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T21:51:47.306
+Launch V∞: [7.3814205708843925, -7.74124677889252, -2.736971685142021] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.3335874855056996, -0.33307208283171197, -0.038480892213679695] km/s
+ V∞_out: [0.30444438455660616, -0.25016484746771933, 0.2617975491371703] km/s
+ time of flight: 9.87901808218225e7 seconds
+ arrival date: 2027-06-28T07:34:47.306
+ thrust profile: [0.5842244363382534 -0.32106608402252357 -0.3313782076592171; 0.14885275679043505 -0.016542749003427466 -0.16176909111404453; 0.038052005919025134 0.002327062593817473 -0.061941555662495894; 0.02844775422722324 0.0038677142207423983 -0.05796077317354717; 0.015944518363399798 0.003437472014734269 -0.03951463042853181; 0.017172596099262687 0.004181452848802308 -0.048487071581291855; 0.009232747759851254 0.0023032970116312165 -0.027386453670599734; 0.002368787814408311 -0.0008918194910494776 -0.0027888267020826996; 0.00042238755713532033 0.0008056088456351322 -0.00054660826446102; 0.0007363878944252018 0.0005687266958930166 -0.006504024797995117; -3.676334782079646e-5 0.0002710088592010253 -0.008774136057567924; 0.0009356075429959899 -0.001315014638360585 -0.010311785018664497; 0.0013762049754202602 0.0028447908097093254 -0.010671666441661152; 0.0011516685460493427 0.00042738696237189667 -0.0036092061918254004; -0.00028358368293858547 0.0013847107481656813 -0.0024237703199179433; 0.0008642136881827192 0.00463626575792052 -0.0028825452138213133; -0.0001744595316894278 0.0007714574204149824 0.0007334783920883328; 0.0006129661883740661 -0.025058926578629168 -0.01899731857765409; -6.441221856759959e-5 -0.014497457759243049 -0.024609973432147474; -0.005366968330283183 -0.0032531822635360557 -0.0012235202255380067] %
+
+Mass Used: 52.98930640851631 kg
+Launch C3: 121.90328534125824 km²/s²
+||V∞_in||: 0.4729676541936361 km/s
diff --git a/archive/ES_0.6551199042439777 b/archive/ES_0.6551199042439777
new file mode 100644
index 0000000..70605f8
--- /dev/null
+++ b/archive/ES_0.6551199042439777
@@ -0,0 +1,22 @@
+archive/ES_0.6551199042439777---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T17:26:58.534
+Launch V∞: [7.393873481877149, -7.552697047045602, -2.2033724752881696] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.11900072907251531, -0.19035321836624738, -0.07517731402000893] km/s
+ V∞_out: [-0.1489922298938324, 0.1549922384172173, -0.09911364103115795] km/s
+ time of flight: 9.791906994187506e7 seconds
+ arrival date: 2027-06-16T01:11:27.534
+ thrust profile: [0.762058967640303 -0.38660985979846957 -0.39993004714996866; 0.3679655851083436 -0.026507736573396133 -0.35603650471801823; 0.13044003138319446 0.015363218331711871 -0.1958065762263565; 0.06185376909113025 0.014755947871751201 -0.12463069462999499; 0.048328695104120106 0.01682511273356066 -0.11567071406315041; 0.031293263426398175 0.009136824657454959 -0.07963486716226553; 0.013471494242963152 0.004807366855429779 -0.04202605078743083; 0.0038072222308522547 0.001586015966992984 -0.022034044795779962; 0.0031262317936136433 0.0020106856229041327 -0.008532620450982334; 6.924217107725952e-5 0.0002822919109423975 -0.0025025273961265405; 0.0014432058523823521 -0.000626106203430456 -0.003484334342806846; 0.0004999120772021751 -0.0002236804628855671 -0.0023803119269606154; -0.0017313928043381117 0.0022885172355361005 -0.0007309164256353758; -0.0010343570824487263 -0.00010860413195851572 -0.0024556722865720676; 0.0016040644300525397 0.0012705525665280273 -0.004056148738343458; -0.005074412287616808 0.0016912802199330213 0.001355900244661071; -0.0025120198761373314 0.0022796599421016257 0.00046457740912165483; -0.0018438789035229528 0.0022019570398124013 -0.003386762571932109; -0.0010117954857507103 2.3701635745539866e-5 0.0026110597453754708; -0.0025511812072859614 -0.006545888679537818 0.001436975437898991] %
+
+Mass Used: 84.32977486196978 kg
+Launch C3: 116.567448015315 km²/s²
+||V∞_in||: 0.2367427925100181 km/s
diff --git a/archive/ES_0.6553893514387072 b/archive/ES_0.6553893514387072
new file mode 100644
index 0000000..559777d
--- /dev/null
+++ b/archive/ES_0.6553893514387072
@@ -0,0 +1,22 @@
+archive/ES_0.6553893514387072---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T17:45:50.412
+Launch V∞: [7.43099974725116, -7.545666002807789, -2.710842861617018] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.762467182988433e-5, -0.0006815138240892939, 9.574867361540226e-5] km/s
+ V∞_out: [0.0002059119706774157, 0.00045133335772272866, 0.0004804984681046699] km/s
+ time of flight: 1.0079591077546892e8 seconds
+ arrival date: 2027-07-19T08:37:40.412
+ thrust profile: [0.4679282432608015 -0.2429895220751489 -0.2744966889022248; 0.18826664976023358 -0.017149356515745003 -0.2012116133533584; 0.08983305731731268 0.006492149555161837 -0.14571855658715013; 0.05658443514051329 0.008277965300388468 -0.12230968031326186; 0.02148469807163685 0.0022219158116104504 -0.05465418783223305; 0.0038550542865952433 -0.0014266515290721135 -0.014230437474365577; 0.03625228615014986 0.010620129310995301 -0.03462031343491494; 0.02682097485535806 0.0023980968486235358 -0.05074592470845718; 0.020650475968311172 0.001720111761154394 -0.007476468412556341; 0.0031809233955666077 0.013490928111785042 -0.010878462139171863; -0.00019327401790669057 0.026284137803528784 -0.015474999878488657; 0.0029866802611261374 0.002369712663375042 -0.01576846387594575; 0.0005215408733695035 5.2605857413709316e-5 0.0006440153413167747; 0.006908665179123331 0.010427631617255871 -0.0033154663629086784; 0.003919480970499029 0.0016362122549476118 -0.00027524433343983565; 0.006409270506826093 -0.0017189952222067192 -0.005691882861785902; -0.005809524317158792 -0.0041820552304198105 0.007405604282427716; -0.06623817875665958 0.016311903697798558 -0.0013373795869258617; 0.045623315722821405 0.03849435241570628 0.03989050258612717; -0.014931116772038785 -0.05594114414350302 0.012982496343065083] %
+
+Mass Used: 67.50548348708162 kg
+Launch C3: 119.50550168995603 km²/s²
+||V∞_in||: 0.0006906153080604453 km/s
diff --git a/archive/ES_0.6558445565760461 b/archive/ES_0.6558445565760461
new file mode 100644
index 0000000..f9e4a17
--- /dev/null
+++ b/archive/ES_0.6558445565760461
@@ -0,0 +1,22 @@
+archive/ES_0.6558445565760461---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-03T23:59:02.372
+Launch V∞: [6.279440526317252, -7.763332434255909, -0.13372832012862532] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.5768129861601466e-9, -2.1650098438964242e-9, 2.8701896416723735e-9] km/s
+ V∞_out: [1.2931109236344489e-9, -3.12759834278989e-9, -4.086455094069368e-9] km/s
+ time of flight: 1.7989531093684968e8 seconds
+ arrival date: 2029-01-14T02:54:12.372
+ thrust profile: [0.16776775645228792 -0.05054470333515385 -0.05689736715483331; 0.06934877166820683 0.010479078198163821 -0.07483876302686775; 0.06023635569802312 0.02125204442114274 -0.08572263798901149; 0.05916586505365605 0.029134884266865974 -0.11782081607696099; 0.052375893168712176 0.029187398492764544 -0.13734148903769808; 0.030121829023730614 0.02581515005970059 -0.0996381286151181; 0.013787121262035225 0.01735184965888386 -0.07071546495036747; 0.002723117465613155 0.009199949026370124 -0.04036764537374191; -0.014717577899005452 -0.014193673680953978 -0.009241756806511132; -0.020010282684351316 -0.04200147839444681 -0.12493299526480085; -0.004550921093969779 -0.004693370411631806 -0.03342803232671529; 0.021129427220352655 0.005829428338345511 -0.024834914317852175; -0.01942279361811304 -0.15394917658749369 -0.06776197287328503; -0.13789262700635507 -0.14894247224295698 -0.11157022676609815; -0.15195050204319635 -0.05219960636848292 -0.09203286614492834; -0.008208459407034272 0.009649221292568665 -0.05424583996576532; -0.16174698718856065 0.08751807705536165 0.10553721816318161; -0.1385478998820064 0.20016022713012818 0.1371058080846409; 0.09421183903113203 -0.05893542486911959 0.20518867987962464; 9.034257166938248e-5 -0.022086335355059314 0.06662875413800971] %
+
+Mass Used: 183.460224752464 kg
+Launch C3: 99.71858707192969 km²/s²
+||V∞_in||: 5.071375290914257e-9 km/s
diff --git a/archive/ES_0.6558789908015318 b/archive/ES_0.6558789908015318
new file mode 100644
index 0000000..0dba6b9
--- /dev/null
+++ b/archive/ES_0.6558789908015318
@@ -0,0 +1,22 @@
+archive/ES_0.6558789908015318---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:51:39.169
+Launch V∞: [7.458716988792306, -7.538787308772539, -2.3849316788352017] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.022813501212399865, 0.01974176295153453, 0.002440504277174752] km/s
+ V∞_out: [-0.01947014921156495, 0.015503272949435794, -0.017247385726358717] km/s
+ time of flight: 9.753506015988164e7 seconds
+ arrival date: 2027-06-11T16:55:59.169
+ thrust profile: [0.7643917396234456 -0.37481727882230853 -0.42132030352633276; 0.2809106297162443 -0.025093072120677126 -0.2974038134529675; 0.12881810477143674 0.011497172769763694 -0.1988816107285893; 0.05614732415696561 0.010523513696287031 -0.109790605050451; 0.03595098696528699 0.008886739046325934 -0.0831458764782911; 0.021216126042938904 0.006096748244692679 -0.055513129550880294; 0.0027257451674416924 0.001154835000224995 -0.012064671616544183; 0.004061588779447736 0.0013056991440551875 -0.01003849803858084; 0.0015721164557379024 0.00018834264492391633 -0.008742899217269985; 0.002573323935328425 0.0021759206350473927 -0.009655685577724234; 0.0007678435881188616 0.00041510615562084585 -0.0037107478389388033; 0.00011944583471835014 1.9007688676336582e-5 -0.002571022256171936; 0.0010848271037017364 -0.0013577917614725238 -0.002699746931259129; 0.003434405918674837 -0.001978792195946771 0.0004730111035352322; -0.0015817643309238654 0.000683000421002953 -0.0011394467904278231; 0.0022584642816048843 -0.0002895080915319652 -0.003210495900027274; 0.0009159692429288563 0.002439568459605068 -0.0004787240641373333; 0.00032982127422241886 0.0003234545864013792 0.0012716397529126547; 0.004192725135407804 -0.0011459555915199334 -0.0027660758348324694; -0.003708369452403159 -0.000997910698259333 0.012628463015757945] %
+
+Mass Used: 75.96240074375055 kg
+Launch C3: 118.15367231852055 km²/s²
+||V∞_in||: 0.030267955053648068 km/s
diff --git a/archive/ES_0.6560723113930567 b/archive/ES_0.6560723113930567
new file mode 100644
index 0000000..047815d
--- /dev/null
+++ b/archive/ES_0.6560723113930567
@@ -0,0 +1,22 @@
+archive/ES_0.6560723113930567---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-22T16:51:35.766
+Launch V∞: [5.378122230744136, -8.156115096554329, -0.46340916612132244] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0002064757995727344, 8.821226785561729e-5, -0.0002029358206482952] km/s
+ V∞_out: [-8.077784022956258e-5, 0.0002004297210368016, 0.0002117815840040048] km/s
+ time of flight: 1.4210995079587454e8 seconds
+ arrival date: 2027-10-23T11:50:45.766
+ thrust profile: [0.4494739265755561 -0.2632478722991777 -0.19015959420133685; 0.12267808214246351 -0.008836737982524143 -0.1089946519209061; 0.10231298979592575 0.01565935116678991 -0.14564108945992563; 0.09038099821737772 0.030353650859286915 -0.17993207719531668; 0.08359940286823897 0.0316875446308953 -0.1944264397028802; 0.06289127377950166 0.02870150155126642 -0.16725170790937022; 0.052844998825244904 0.007421046767492256 -0.08920813054808002; 0.1575947775558399 0.024485024084145733 -0.1603323845281368; 0.059381167834787654 0.000773572583705473 -0.16440341987543663; 0.04503163967477891 0.005267867805728381 -0.07389361919483337; 0.1200078802463998 -0.023816787121216883 0.0010121116414699254; 0.2338951883297835 -0.09861817282044846 -0.09304723322512436; -0.006841910371656337 0.004314199778677031 0.06737785210796868; 0.009499462476571045 -0.013804969423957383 -0.02547099585153692; 0.09643280667380355 -0.011909509871720353 0.003051194286260356; 0.021408162482172016 -0.0246471517523682 0.006845006065413106; 0.14372551384303567 -0.03966162116509232 0.05474156900909122; 0.1457800884351052 -0.11040078796780657 -0.023632746565111558; -0.16463824742043023 0.025421886040607425 -0.16949416521964972; 0.11580599628521202 0.05675899831301226 -0.3519536637120141] %
+
+Mass Used: 207.39426182008538 kg
+Launch C3: 95.66116025231098 km²/s²
+||V∞_in||: 0.0003026493140775776 km/s
diff --git a/archive/ES_0.6561566832448091 b/archive/ES_0.6561566832448091
new file mode 100644
index 0000000..d034003
--- /dev/null
+++ b/archive/ES_0.6561566832448091
@@ -0,0 +1,22 @@
+archive/ES_0.6561566832448091---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T08:11:26.274
+Launch V∞: [7.436360716245945, -7.539640268458702, -2.5869221864084286] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002633842762429374, -0.0032347229296055026, 0.000846259077626412] km/s
+ V∞_out: [0.0009379139532991579, 0.002180881584177023, 0.0023694158458683443] km/s
+ time of flight: 9.699180566993216e7 seconds
+ arrival date: 2027-06-05T22:21:31.274
+ thrust profile: [0.9662256394872482 -0.5018594805959329 -0.5057122435587362; 0.19349366287707642 -0.015939679726359613 -0.19299795093783825; 0.04642991007802924 0.005289525429479067 -0.0734393627612691; 0.023291288203675424 0.005022735184090175 -0.0487088920435339; 0.04623530847655166 0.013262140181233851 -0.10732653058324727; 0.011971056083461133 0.003898579853089399 -0.03365033698468705; 0.010657193797748396 0.0038369474556137727 -0.03288004129722652; 0.011659945756868191 0.004297470841780781 -0.036276176167494456; 0.001357426597533105 0.0004944912062525614 -0.004095831792094297; 0.0038975595662929003 0.0015554748464500104 -0.014670518045214406; -0.00013545022818726234 -4.509322650019296e-5 3.928826012314672e-5; -0.000340881767876116 0.0007031838201380066 -0.0010972411396066779; -0.00013805203771895106 7.893151702483307e-5 -0.000767962768893859; 0.000344694712863346 -0.0004942820653986691 0.0010246901773955427; 0.0008271581682672218 -0.0002378613141571434 0.00042173388640436764; -0.00015273403588273143 -0.00033038676140756027 0.0011398067460694097; 0.00037205285514607157 -0.0001241188591259171 -0.0008467679255258642; -0.0005950332227930426 -0.00015639419486299094 0.00034453104090744326; -0.00023740302268839336 3.452991127500815e-5 0.0005076536767054929; -0.0003502882707824034 0.00020032589063757173 0.0022651927423085584] %
+
+Mass Used: 72.29561599481531 kg
+Launch C3: 118.83780247842206 km²/s²
+||V∞_in||: 0.0033539466505525584 km/s
diff --git a/archive/ES_0.6562974708461055 b/archive/ES_0.6562974708461055
new file mode 100644
index 0000000..5c2938c
--- /dev/null
+++ b/archive/ES_0.6562974708461055
@@ -0,0 +1,22 @@
+archive/ES_0.6562974708461055---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T19:07:50.363
+Launch V∞: [7.485281718239835, -7.540600261512695, -2.485292585685957] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.03127488647609146, 0.05899187169181998, -0.0831185148764724] km/s
+ V∞_out: [-0.053456928388616334, 0.06567955301244012, -0.06462689670421119] km/s
+ time of flight: 9.803311886862154e7 seconds
+ arrival date: 2027-06-17T10:33:08.363
+ thrust profile: [0.6632119089566226 -0.3391388871610564 -0.3610857130188469; 0.22129686708044538 -0.01751151305926756 -0.22224619237742704; 0.11910571134448299 0.012096272474758151 -0.1709052836378854; 0.07550460679587177 0.014879244884229927 -0.1368000978678955; 0.041737848046629056 0.01038695313174357 -0.08855720405691352; 0.025834474238608827 0.007552097170637004 -0.062033116158382126; 0.0016684006590327591 -0.0007040657662489931 -0.0053156064307588674; 0.004623884448070411 0.0017086536071022115 -0.0145159821663372; 0.01642957659465781 0.003842228085243592 -0.022757814249713744; 0.002095190762283335 -0.00039007251903311796 -0.006078914365574906; -0.00463174287974014 -0.0017938427106570197 -0.01134196030748517; -0.0015678053989627572 -0.0010329310075669021 -0.0010007203768353443; 0.0024405915024270928 0.003093052710784332 -3.640957747357704e-5; 0.006360182744081462 -0.00023725688294202497 -0.0117510766344351; 0.003048703811997089 0.00015147594949900187 -0.0021602063900502365; -0.0027540289818359914 0.010552941497208437 -0.0013357489798668278; -0.0013107835235293555 0.0012388106410560458 0.0021402428246718643; -0.000808866938957001 -0.004091113426962471 -0.0038356106942373704; -0.0012269978472932014 0.004943400959397215 0.0072150451730401514; -0.009653412212022587 -0.002757369723655585 0.027048857590807274] %
+
+Mass Used: 71.12420132658553 kg
+Launch C3: 119.06677394180642 km²/s²
+||V∞_in||: 0.1066154161698341 km/s
diff --git a/archive/ES_0.656364508582092 b/archive/ES_0.656364508582092
new file mode 100644
index 0000000..293ab39
--- /dev/null
+++ b/archive/ES_0.656364508582092
@@ -0,0 +1,22 @@
+archive/ES_0.656364508582092---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:22:00.268
+Launch V∞: [7.450044510845533, -7.443511406676776, -2.284068306345141] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.223607120740691e-7, 1.4456951609068762e-6, -3.5828035665606675e-5] km/s
+ V∞_out: [-1.565437942641175e-6, 3.580932886739246e-5, -2.6450825913802626e-7] km/s
+ time of flight: 9.698885207540207e7 seconds
+ arrival date: 2027-06-04T11:42:52.268
+ thrust profile: [0.9160611691912505 -0.4662465332328695 -0.4852568292885135; 0.355136117868503 -0.026940528902655168 -0.342922118764267; 0.21355057356547666 0.024189889489003007 -0.2977087011849139; 0.04898070914000209 0.009953183553174535 -0.08999275815003334; 0.03741746158327282 0.010872374449830162 -0.08268934695580193; 0.017927766888277737 0.005953605987134249 -0.04556128694207721; 0.00625933999878198 0.0023694517914843614 -0.01821457010224329; 0.0021324606450395657 0.001044110606931384 -0.008722047501251566; 0.0005681102284351972 6.613961108226302e-5 -0.0019204051505657105; 0.0009466293526361127 0.0002701880515003531 -0.0028016530993487357; 2.620711834404435e-5 0.0017300942744135626 -0.0019217617118012184; -0.0014895084093059386 -0.0014219637150851663 0.000598637950419852; -0.00023572626055710894 -0.0001285308754214965 0.0005318717471248678; 6.979599256618946e-5 -0.00045664307058490626 0.0003047966563368631; 0.0002154159209929033 -0.00012148737366843271 0.0009688614517037683; 5.773664047405375e-5 0.00024084536689358577 -0.0007704815661771919; 0.001185496676186198 -0.001186579274718251 0.00010689750874541695; 0.0004127064782117713 -0.0005675531954124727 -0.00044792941253583705; -0.0012734334288322213 0.000618424256198016 0.0009231802045667142; 0.00010158529671257904 0.00022210941994671955 -0.0005532429040174913] %
+
+Mass Used: 88.35696574518988 kg
+Launch C3: 116.1259933029573 km²/s²
+||V∞_in||: 3.585788084146255e-5 km/s
diff --git a/archive/ES_0.6565866024133596 b/archive/ES_0.6565866024133596
new file mode 100644
index 0000000..d38ecc6
--- /dev/null
+++ b/archive/ES_0.6565866024133596
@@ -0,0 +1,22 @@
+archive/ES_0.6565866024133596---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T23:38:06.751
+Launch V∞: [7.181515240495631, -7.254248061955292, -1.450004237584665] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.5569620596595112e-6, 2.2572783083256495e-6, -1.632132487511248e-6] km/s
+ V∞_out: [6.747063461253978e-7, 3.7122758098358346e-6, -2.4258086836298704e-7] km/s
+ time of flight: 1.0239972466862187e8 seconds
+ arrival date: 2027-08-03T04:00:10.751
+ thrust profile: [1.0 -0.5089832329092627 -0.4645639569330508; 0.5498844015155253 -0.014876604270867138 -0.48883003219852006; 0.19880641831560952 0.03610911634673995 -0.2532229464238786; 0.14745700684371504 0.04379704999505864 -0.2436369593231415; 0.11522042625239232 0.04557829809236113 -0.22056571390201207; 0.06360715867506603 0.02475502267212246 -0.13612234413429636; 0.02661564560987938 0.010714622735056195 -0.05872819204312942; -0.005625657395623262 -0.006229861210937151 -0.012393017921552686; 0.03609446347303258 -0.00889267393902207 -0.042048048615289206; 0.0076715191522788205 -0.0026037808458829574 -0.02034110169495454; 0.015812575398898524 -0.0027141850164412364 -0.012165146028169769; 0.006304229387954895 0.007294544943947696 -0.04600322318436499; -0.044621837827874974 0.035626487310654785 -0.08431308904957707; 0.0009295673080211104 -0.0029545527813420605 0.0038557671880266736; -0.0005553215214524941 0.0033533091994829437 -0.0013908151120624636; 0.01024560934031871 -0.03981936206784392 -0.016893665837765373; 0.02938353520470571 0.02331907183458145 0.005815963223889168; 0.05132704095053541 -0.07159596022082924 -0.011969309385794883; 0.06940644938025642 -0.010779216315240668 0.04348225131077757; -0.004879792126412466 -0.00410216111922658 -0.020404398756670262] %
+
+Mass Used: 145.92977058219776 kg
+Launch C3: 106.30078838286661 km²/s²
+||V∞_in||: 3.7811660625480827e-6 km/s
diff --git a/archive/ES_0.6570535991024186 b/archive/ES_0.6570535991024186
new file mode 100644
index 0000000..d17c5d0
--- /dev/null
+++ b/archive/ES_0.6570535991024186
@@ -0,0 +1,22 @@
+archive/ES_0.6570535991024186---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T13:58:08.386
+Launch V∞: [7.553932891171966, -7.520144308055574, -2.6817329215808274] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.495701068773734e-5, -0.0007360108247461193, 0.00011012064719552248] km/s
+ V∞_out: [0.00022020864826472893, 0.0004916293689353453, 0.0005189342119900457] km/s
+ time of flight: 9.885853697840375e7 seconds
+ arrival date: 2027-06-26T18:40:24.386
+ thrust profile: [0.47673674589183174 -0.2519707233928128 -0.2903040771162744; 0.20484828069476207 -0.011853877956066626 -0.21663803888801622; 0.09945249065751836 0.0131654652680219 -0.1584856852446909; 0.07363239296702313 0.017785657588138798 -0.15143200034255036; 0.02706132534260647 0.008535475387344805 -0.07345653020866448; 0.006198281380252047 0.003058436596130763 -0.014564522331911026; -0.002192558315211084 0.00259450329379633 -0.01550716327594036; -0.0005272288940019352 -0.0009552144712594761 -0.003769491600724818; 0.007330585149496821 0.00013798463994342536 -0.01768820302715686; 0.0011047056138664751 -0.00033712525061609187 -0.017626783042403397; -0.0005932970235824906 -0.0005854492565751596 -0.006746321807156864; 0.0021670928895252232 0.005026092049418854 0.00473300425016147; 0.014397407238574973 0.008323153542101142 3.7666082255991516e-5; -0.007908265074881383 0.00021681741397982417 0.0017734495297553618; 0.0019158273794847832 -7.332032673126521e-5 0.007253711775281695; -0.016822329886250747 -0.0018607187781036322 0.0115258731231158; 0.01775711267147596 0.001645119466648085 0.01232165411466506; 0.00019908537310478654 -0.0013498183639861342 0.018092662438439332; -0.0076630352266297535 -0.0036605017909912695 0.009371053333314323; -0.0021360919789395875 0.021976052859617543 -0.024633411093396666] %
+
+Mass Used: 61.85990894698398 kg
+Launch C3: 120.80616400100075 km²/s²
+||V∞_in||: 0.0007479686119974989 km/s
diff --git a/archive/ES_0.6571027490757085 b/archive/ES_0.6571027490757085
new file mode 100644
index 0000000..39105cf
--- /dev/null
+++ b/archive/ES_0.6571027490757085
@@ -0,0 +1,22 @@
+archive/ES_0.6571027490757085---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T16:17:31.088
+Launch V∞: [7.397392241328327, -7.641382316115041, -2.4382751114749093] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.49390785992873826, -0.49227961667055714, -0.0562033826852556] km/s
+ V∞_out: [0.4483284153056244, -0.3650548300091252, 0.39391120798816737] km/s
+ time of flight: 9.785422131069715e7 seconds
+ arrival date: 2027-06-16T06:01:12.088
+ thrust profile: [0.6774004555643455 -0.34097759799209076 -0.370490268891399; 0.2978443648379849 -0.021532084049433017 -0.29716110618768954; 0.10898061262890356 0.012470062762483733 -0.16230765326414473; 0.04886392265123951 0.009756389862239942 -0.09418916281329852; 0.044817209513415765 0.011791166180589962 -0.10049808654583704; 0.011065421908612124 0.002943190204749096 -0.027154889582880155; 0.003223584903401583 -0.00047352327581106144 -0.008088713036620385; 0.00574526253188136 0.0017798787529873764 -0.016321614915446113; 0.003148744319908682 -0.0004869717928706613 -0.010968141045508768; 0.0006917248608722586 0.0017336704617549967 -0.0055734245119145745; 0.0006630695979508098 0.000563340248873878 -0.0023347132518039093; -0.0014856288891429896 -0.004753151007049527 -0.005422001475123315; -0.00746144337992363 0.007539875294290138 -0.003853766899814039; -0.0012414062786844583 0.003725396777217821 0.0004170546050967361; 0.0009775024043627194 -8.731349815608397e-5 -0.0005401350011387067; -0.009237994332663462 0.005880095026926866 0.0013646189307279395; 0.010651748974422063 0.0052222646174584905 -0.009800409184381267; 0.005709294331779809 -0.0027327346459443424 0.0054795047212684925; 0.01691346974486128 -0.007429717045979873 -0.004821469320937631; 0.013721339391341323 0.013676654140217754 -0.0017731381139771837] %
+
+Mass Used: 72.11883363302059 kg
+Launch C3: 119.05732119233818 km²/s²
+||V∞_in||: 0.6996020406730973 km/s
diff --git a/archive/ES_0.6571830723198436 b/archive/ES_0.6571830723198436
new file mode 100644
index 0000000..2c12655
--- /dev/null
+++ b/archive/ES_0.6571830723198436
@@ -0,0 +1,22 @@
+archive/ES_0.6571830723198436---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T08:05:53.476
+Launch V∞: [7.544273016651068, -7.613105831400824, -2.625343185659401] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003062001344975225, -0.003685305929344166, 0.0009552285202092762] km/s
+ V∞_out: [0.00111246566156315, 0.0025774001158082385, 0.002589586982995658] km/s
+ time of flight: 9.792688926168817e7 seconds
+ arrival date: 2027-06-16T18:00:42.476
+ thrust profile: [0.46554067126489934 -0.2353777251703485 -0.24482426462846485; 0.17497501778392124 -0.010892282049856495 -0.16409183884728412; 0.12891851202478724 0.015490802254753815 -0.17588018086712878; 0.04141217696037911 0.00998682434455506 -0.07830143560278345; 0.03958772230251557 0.01337383184211217 -0.0861429099109337; 0.016656428846715688 0.009193431441660335 -0.043652035416630784; 0.024446362287890423 0.009877742181524323 -0.06706543211471817; 0.005579474902116865 0.003204005687770178 -0.02136556909794488; 0.0011466196058235799 0.00028256578367481485 -0.003932893100616145; 0.0016597358140194667 0.00040002880154237254 4.1174879038870715e-5; -0.0014126164278304237 0.003823625508165454 -0.003377025648503287; 0.002756831385676756 0.00029633293759596057 -0.002480509681672058; -0.006773154575944667 0.001755975470165309 -0.0009943349975383626; 0.008591743885239674 0.005978236907027477 -0.0062111278462436015; 0.009203824850074167 -0.005943091598920104 -0.0075147305680740035; 0.00997536817453204 -0.0010958158942666572 -0.004609790796391457; 0.0014123995868884367 0.0022663669137944235 -0.0032805630571700775; 0.0041944745343696545 -0.0046546040842174825 -0.008897602380943387; 0.0008565453624025058 -0.002240505972542257 -0.008665085512880725; -0.0011796948859207272 -0.0014551691120892403 0.0008215820478383708] %
+
+Mass Used: 56.40105258434414 kg
+Launch C3: 121.76786259236687 km²/s²
+||V∞_in||: 0.0038193847464018035 km/s
diff --git a/archive/ES_0.6572296681786398 b/archive/ES_0.6572296681786398
new file mode 100644
index 0000000..5b3057d
--- /dev/null
+++ b/archive/ES_0.6572296681786398
@@ -0,0 +1,22 @@
+archive/ES_0.6572296681786398---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T16:29:59.394
+Launch V∞: [7.403971383969931, -7.655579889131952, -2.1124603846362042] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.02947756052126185, 0.15819761568981952, 0.027941094580490832] km/s
+ V∞_out: [0.1580438840777431, -0.02291154558656412, 0.03427816892877218] km/s
+ time of flight: 9.784114871602184e7 seconds
+ arrival date: 2027-06-16T02:35:47.394
+ thrust profile: [0.6587737309119955 -0.3558465259928656 -0.3650714333971656; 0.23510214196140866 -0.029301164395685347 -0.24885330728214544; 0.1581368563233402 0.007289050910781734 -0.2404367226770587; 0.07799674456307003 0.01148436039417995 -0.15455773774967044; 0.09475623338144314 0.0176667884796709 -0.22160543030232369; 0.010016507361891414 0.0027432916880577776 -0.026785700522971936; 0.005377523973865173 0.001329998660638997 -0.015940128814821902; 0.014033130192263078 0.0051969151726122195 -0.041757832160409195; 0.0016618151338473074 0.00046240997954881706 -0.0011704142061107756; -0.0005564763171162024 -0.0023015631617532826 -0.00602401354049494; 0.002658520868133899 -0.0017762072452497547 -0.005095736710347866; 0.0020992560732882733 0.0004024233620806726 -0.007344476308786313; 0.0022369201399713764 0.0017004688350733092 -0.004412150421956732; -0.002955361140562761 -0.00038327652525545837 -0.004938594712917225; 0.0007150322857189283 0.0001429919217891878 -0.000805284501820101; 0.00016105938993548263 0.00018466529262321774 -0.006340392784324633; 0.0003497722432956685 0.00013369414014987625 -0.001040908989390682; 0.002492896750748894 -0.0031348584831254827 -0.0017929886976260773; 0.0009953264093228026 -0.0007827474729343858 0.007817902065583571; -0.0009337899484389797 -0.0004613110201052825 -0.0060804903629179865] %
+
+Mass Used: 79.08103621566988 kg
+Launch C3: 117.88918457018457 km²/s²
+||V∞_in||: 0.16332824908932447 km/s
diff --git a/archive/ES_0.6573166130612218 b/archive/ES_0.6573166130612218
new file mode 100644
index 0000000..50eed66
--- /dev/null
+++ b/archive/ES_0.6573166130612218
@@ -0,0 +1,22 @@
+archive/ES_0.6573166130612218---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T21:08:17.152
+Launch V∞: [5.803834252870955, -8.829232626648086, -2.337290536601728] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.08821797177140085, -0.5309806792298443, 0.5364222325119744] km/s
+ V∞_out: [-0.47872416044970634, -0.4930284162959207, -0.3252635919652413] km/s
+ time of flight: 9.79916839393585e7 seconds
+ arrival date: 2026-06-02T01:03:00.152
+ thrust profile: [0.7550758441007756 -0.5949095689977306 -0.4306108974774697; 0.3519965660260834 -0.09167012976194024 -0.33379710091426246; 0.10927387550453209 -0.005901484722778477 -0.14968751820503376; 0.07177197814734927 0.004076041106891502 -0.1219472920851041; 0.037022574204826034 0.004880140699838259 -0.07289240890975873; 0.02487378356444231 0.004889814110227541 -0.05330018522707181; 0.01405854804857325 0.0030479424437029304 -0.03396339330400207; 0.00870720639031945 0.0020190502560569487 -0.022670000706623117; 0.0005096620485692552 -0.002019185894479747 0.00010604807096278629; 0.0010557674886518965 0.00046236660796876954 -0.0024258963311709946; -0.0045457785913624645 -0.004604936185267668 -0.004062212532447527; 0.0031325765041829547 -0.0033734306948059647 -0.005784031382471379; 0.0009222166137017423 0.006761816606510674 -0.005302133837198244; 0.002462443933988821 0.008050606021035349 -0.0018567449591174502; -0.0002524112095682855 0.0011460604082883135 -0.0022988769990916324; -0.00022566959277748867 0.0028874684974127293 -0.00749540815713692; 0.004628188953019228 -0.0012431016638244103 -0.008844218536413824; -0.0031356773384072084 -0.003444702016088038 0.004585562383834474; -0.005320480177208811 -0.003170330014802855 0.000845784104122339; 6.581288524274602e-5 0.00013210098613225746 -0.0001144086381091465] %
+
+Mass Used: 83.76990270536498 kg
+Launch C3: 117.10276786275321 km²/s²
+||V∞_in||: 0.7599155899124437 km/s
diff --git a/archive/ES_0.6577763503207862 b/archive/ES_0.6577763503207862
new file mode 100644
index 0000000..db0e7f6
--- /dev/null
+++ b/archive/ES_0.6577763503207862
@@ -0,0 +1,22 @@
+archive/ES_0.6577763503207862---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T21:14:40.893
+Launch V∞: [5.871843291326935, -8.80906353381374, -2.2528065676794604] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.13512158075201877, -0.8336758411606405, 0.8217786448076985] km/s
+ V∞_out: [-0.7865472722468538, -0.7555352891068248, -0.5257267080433466] km/s
+ time of flight: 9.917298946540408e7 seconds
+ arrival date: 2026-06-14T17:17:49.893
+ thrust profile: [0.5139914953177579 -0.4030483807421011 -0.29547862676279274; 0.38084245932719496 -0.09525774581992773 -0.3458064922841706; 0.19914539214304913 -0.009271171136884925 -0.25160135822625623; 0.09712739369442872 0.004345659541681726 -0.15598930442023656; 0.03842735087446779 0.0027374413324147535 -0.07601750802495587; 0.01549699400193594 0.007667940580518895 -0.021895993929100615; 0.017091479390374958 0.008085168014140092 -0.04508743552331838; 0.030053917449107563 0.019617198717454848 -0.07104422664534214; -0.00026364144090425734 0.0005066974246701787 0.0024153339371945637; 0.004568311827646464 0.001003784134807386 -0.009376208858282581; -0.0033258753858062128 0.007685142875939294 -0.00040142146064765967; 0.0029313623307455714 -0.0022062562878653307 -0.009414186400176891; -0.004410136135506087 -0.004197860646057417 -0.01971774997755453; 0.0017400616405966577 0.0034285703865120226 -0.0029535291901015477; 0.006903775532623236 -0.004043647654180391 -0.004496987723976967; -0.004624676448369067 -0.002709723678748245 -0.003932588774085288; 0.014265662829215627 0.016355439627033973 -0.028002549592080185; 0.0006238927669728457 0.011479515128997943 -0.012703195095042873; 0.005856357223048418 0.0015946155502318208 0.0038837622121564858; 0.0028294732009056488 0.00025307703500873505 -0.007923199350537912] %
+
+Mass Used: 84.01160047063786 kg
+Launch C3: 117.15328141204787 km²/s²
+||V∞_in||: 1.1783859260793144 km/s
diff --git a/archive/ES_0.6579322483280391 b/archive/ES_0.6579322483280391
new file mode 100644
index 0000000..daf321a
--- /dev/null
+++ b/archive/ES_0.6579322483280391
@@ -0,0 +1,22 @@
+archive/ES_0.6579322483280391---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T05:24:59.015
+Launch V∞: [5.851175250255026, -8.743842279096743, -2.040427103825458] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0819933370900334, 0.5315332079828119, -0.4981767368042949] km/s
+ V∞_out: [0.4315308560909752, 0.5265231465463361, 0.2826049248548159] km/s
+ time of flight: 9.833828261812046e7 seconds
+ arrival date: 2026-06-04T09:36:21.015
+ thrust profile: [0.7236297245052914 -0.5530219675063662 -0.3661455277180001; 0.44581525424033897 -0.10243554068013426 -0.36390526059609934; 0.1641170369965996 -0.0022246199667370127 -0.19984763068259828; 0.08414467705473201 0.00845166108039835 -0.12851452563878998; 0.13749061685256833 0.024150667619594873 -0.2331498336682674; 0.04647814792334609 0.009897517345115407 -0.091725531448946; 0.02827780061210261 0.007205941539536918 -0.06140108894924705; 0.02007211110223145 0.005717769603851994 -0.04653353807696856; 0.0043748189588993375 0.0011885308251905675 -0.010177313607268517; 0.0005213769131151495 3.7140808360055936e-5 -0.0010675610534416889; 0.0007854315289541422 3.011770323750856e-5 -0.001418396349570055; 0.0004001626473017667 0.00011917024352909862 -0.0009943012536631718; 0.00037555165610865396 -0.00010149673885935366 -0.0008847165662408177; 0.0003618748176994354 -8.059573904348476e-5 -0.0006500708159193343; 0.000551740161275872 -0.00010055066310605176 -0.00036297636010652055; -0.00023886892497490498 -5.959395239183319e-5 -9.864542296742466e-5; 0.0001304836851151425 0.00011640141166452877 -0.0003293154526141683; -0.0002487301490233429 -2.2703305578714245e-5 0.000685599241634366; 0.0003202814269861082 0.0003557612177271551 -0.0006362870487293306; 6.19411984771357e-5 -8.455673508216187e-5 0.0004028107397607266] %
+
+Mass Used: 97.60378418388245 kg
+Launch C3: 114.85437237694225 km²/s²
+||V∞_in||: 0.7330965281657217 km/s
diff --git a/archive/ES_0.6581334644592185 b/archive/ES_0.6581334644592185
new file mode 100644
index 0000000..fc467f7
--- /dev/null
+++ b/archive/ES_0.6581334644592185
@@ -0,0 +1,22 @@
+archive/ES_0.6581334644592185---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-10T20:08:37.388
+Launch V∞: [5.492976788447366, -8.18906257596328, -0.7118753008546601] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0006494412015807459, 0.00042204337184017463, -0.0003702761241952708] km/s
+ V∞_out: [0.0004882897086413766, -0.0006187565020507429, 0.00033979282509108893] km/s
+ time of flight: 1.1141255785931829e8 seconds
+ arrival date: 2026-10-21T08:04:34.388
+ thrust profile: [0.8295384956330202 -0.6077708557588934 -0.24884776981621695; 0.8476396027173949 -0.10253438897486561 -0.4438851815060035; 0.7522670406889764 0.09486846194100185 -0.5188502974675142; 0.5313751534023349 0.14638309544658015 -0.46120945232967425; 0.3275235757908824 0.12381659262782534 -0.3389836979183177; 0.16457991400904826 0.0742394880848998 -0.19627891041561576; 0.009354457310843462 0.004861623635294699 -0.013190694630612149; 0.004304788304052272 0.0024213204140745206 -0.005955095597438018; 0.0013896818777434207 0.0007032371876664739 -0.0024471412974099763; 0.0006343356104112254 0.0005316390128221176 -0.0015499575269664174; 6.435642317576809e-5 6.188100166494573e-5 -0.0005985210120643331; 0.0005061568893245849 0.00025858145465017506 -0.0010430455443601982; 0.0010291732401749181 -0.0003550786663010881 -0.0010387342628833426; 0.000205031200666688 -0.00040020389889042305 -0.0008355809474277073; -0.0017560746570245967 0.0003138328285133944 0.0005162075555816704; -0.00013016002834563531 4.3900182807599065e-5 0.00028119531820572363; -0.0001292711636073833 -0.0006272962863580998 0.001003649835319378; -0.0011479227635522507 0.0010608965764576008 0.0013308226197154837; 0.0016982609083793314 0.0016885132901010773 -0.00033129808860360053; 0.0018129690036898468 0.001611374328842955 0.0007030762233016957] %
+
+Mass Used: 197.67058836240858 kg
+Launch C3: 97.74030631543081 km²/s²
+||V∞_in||: 0.0008584863948682813 km/s
diff --git a/archive/ES_0.6581347829210079 b/archive/ES_0.6581347829210079
new file mode 100644
index 0000000..89e5c03
--- /dev/null
+++ b/archive/ES_0.6581347829210079
@@ -0,0 +1,22 @@
+archive/ES_0.6581347829210079---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:55:46.398
+Launch V∞: [7.431912631819949, -7.454474441789282, -2.1789735884801646] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.02520848686592945, -0.044502734066426165, -0.03307579125927849] km/s
+ V∞_out: [-0.0456160643834423, 0.03539261344816766, 0.01940868245020996] km/s
+ time of flight: 9.683497106018357e7 seconds
+ arrival date: 2027-06-02T13:31:57.398
+ thrust profile: [0.843439329805657 -0.4302424959296277 -0.4394341175817327; 0.512595293594384 -0.038023972835830186 -0.468436211627818; 0.2008937054201601 0.023395793417110046 -0.2687928120302537; 0.08554540365519074 0.019057835261900646 -0.14782293528869056; 0.025405409677822635 0.007179219296681079 -0.05311448465531999; 0.004802042878021873 0.0015849773435725812 -0.013477044001487684; 0.0076548468966678145 0.002096538102085855 -0.018489109399212604; 0.008940294772242938 0.0021446026499152664 -0.020398014211463478; 0.00661266268447456 0.0018649866778267079 -0.015695749275051407; 0.00583491560793061 -0.0011983320953594867 -0.00565164509487571; 0.002123686692402353 0.002139943819409219 -0.004156606258640281; 0.002387325014481383 0.0006052520198339241 -0.003588724234445488; -0.0002936425765145375 -0.0005340442462656611 -0.0034965058975503617; 0.00463025784280857 -0.0009292509592519339 -0.0014552676263716543; 0.00023455655057149965 -0.00016013264505336045 -0.00036877774583518076; -0.001709770757983749 0.0006028248807352055 -0.0035870573466488262; -0.00037691678059804273 -0.007242659068559802 -0.007729008486791132; 0.0007107994250769257 -0.00029818244412631897 0.0007710788415118764; 0.002100844936487656 0.0010923826187101415 -0.006336600260000383; -0.001219618435686999 -0.0008565921754657762 0.0015427747732349277] %
+
+Mass Used: 93.77967733524201 kg
+Launch C3: 115.55044046958866 km²/s²
+||V∞_in||: 0.060909515815545184 km/s
diff --git a/archive/ES_0.6586366138788979 b/archive/ES_0.6586366138788979
new file mode 100644
index 0000000..6b3c5ea
--- /dev/null
+++ b/archive/ES_0.6586366138788979
@@ -0,0 +1,22 @@
+archive/ES_0.6586366138788979---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T02:35:02.581
+Launch V∞: [5.696717947939889, -8.862395753718465, -2.1224913298703916] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001756543882613652, 0.0009265843309443784, 0.0018572142282822575] km/s
+ V∞_out: [-0.0008330347475616594, 0.0018170344589567885, -0.0018432912442213044] km/s
+ time of flight: 9.763460627695338e7 seconds
+ arrival date: 2026-05-29T03:18:28.581
+ thrust profile: [0.7370269861110286 -0.5921543183965083 -0.38255036402977466; 0.5544876958214232 -0.1519536288541545 -0.4490209537059307; 0.1399784780173626 -0.01248331016558555 -0.17959832929486594; 0.0645193132919425 0.0017625189795050778 -0.10756988493459106; 0.04928806097012447 0.004453731027318788 -0.09519846888907513; 0.03883402523551911 0.005048272713230539 -0.08344735595126164; 0.017119209558368743 0.0030524218760328023 -0.039796952487056024; 0.007506117897681043 0.000983844357876505 -0.019185602579778933; 0.0010746363138667773 0.0002746781769815336 -0.003369762538345712; 0.001879535310090657 -9.809087187716628e-5 -0.005951668946006032; 0.0016396479012323376 0.0003797718121140445 -0.003485066260742543; -0.00021767390582110512 0.000617133702394348 0.0017196066525593514; 0.00176392516211836 -0.0011339080553723797 -0.009375797659815784; -0.0025647427981645692 -0.00021113513396093077 -0.005457037976967684; 0.0032438369226881368 0.008423305686137613 -0.005139168384650765; -0.0022543220346261175 -0.0021640387960203903 0.003334399589725712; 0.0041994620941361365 0.004092718892738202 0.0015267468193808573; -0.0033936247781726735 0.0035837353647040267 0.0027533501621252333; 0.0006769967519121782 0.0011838824206857712 0.001449845329534363; -0.001502967553459383 0.0025884528297646374 -0.008133463003522464] %
+
+Mass Used: 94.66158016289955 kg
+Launch C3: 115.49962331928252 km²/s²
+||V∞_in||: 0.002719053074809895 km/s
diff --git a/archive/ES_0.659464667688947 b/archive/ES_0.659464667688947
new file mode 100644
index 0000000..27d652e
--- /dev/null
+++ b/archive/ES_0.659464667688947
@@ -0,0 +1,22 @@
+archive/ES_0.659464667688947---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:20:50.196
+Launch V∞: [7.406948583297187, -7.3973413063519, -2.026158423669344] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2070104913849612e-7, 8.75341566012917e-7, -2.073643473918621e-5] km/s
+ V∞_out: [-8.800069861681404e-7, 2.0724380975908458e-5, -2.4932248813017704e-7] km/s
+ time of flight: 9.674600534334747e7 seconds
+ arrival date: 2027-06-01T02:14:15.196
+ thrust profile: [1.0 -0.580670528935306 -0.5567131074192371; 0.45007924223983464 -0.026246513110746838 -0.3817901932023735; 0.18731181379661 0.0270341774503313 -0.23125488502839325; 0.14649934719035637 0.03766164216551354 -0.22835890702172912; 0.01697210550155599 0.005861041847201693 -0.03287668752756465; 0.03914254351847557 0.016481964771315496 -0.0851953468689043; 0.044482219010502824 0.018054089007222145 -0.10387701343937486; 0.003571110628609764 0.0009870989581407836 -0.00928394850382111; 0.001170567685641501 0.0006211091872467708 -0.003874126278265595; 0.0012715745050003206 0.002359648897801831 -0.0013537963024551664; -0.0007600993206210418 7.843103562695756e-5 0.00035475247011068395; 0.00012063145361717762 -3.391239515423625e-5 -0.002219719538226477; -8.515017140553688e-6 0.0002608449295183595 0.000330122475888474; 0.0006945340324466557 0.00035731629697129336 -0.0016555967076704755; -0.0014740339670396706 -0.0019321390999334903 0.0014821000838621092; -0.0011635962814645928 0.0017006983045143832 -0.00404964595702492; 0.003574241431795865 -0.003807340026309289 -0.0003836943160828582; -0.001248354709439853 -0.0004941154462923527 0.003411184125591301; 0.007305100052844599 -0.011262415566253625 -0.004730578537312466; -0.008319041094763138 -0.002646907027001602 0.003944891942410834] %
+
+Mass Used: 106.19040752667024 kg
+Launch C3: 113.68886367607449 km²/s²
+||V∞_in||: 2.075525276389044e-5 km/s
diff --git a/archive/ES_0.6595025613220897 b/archive/ES_0.6595025613220897
new file mode 100644
index 0000000..56895a7
--- /dev/null
+++ b/archive/ES_0.6595025613220897
@@ -0,0 +1,22 @@
+archive/ES_0.6595025613220897---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-03T22:49:24.809
+Launch V∞: [8.173816073003628, -7.231778061450774, -0.47430363588023755] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.66907026788998e-8, 5.153988162319127e-7, -1.0229246923268614e-5] km/s
+ V∞_out: [-2.9013871270254587e-7, 1.0235533359310986e-5, -1.2085868215962185e-7] km/s
+ time of flight: 1.8749577787411994e8 seconds
+ arrival date: 2030-05-14T00:59:01.809
+ thrust profile: [-0.0010537313612019807 -0.0033494970348484955 0.0012598256832311487; 0.0403743560362587 -0.06791547884510508 -0.09426615835360964; 0.009997721329589909 -0.032785031127584074 -0.04741265884361999; 0.02620835943325516 -0.06033639298458007 -0.0858094355216811; 0.03344001637984845 -0.07640980294487884 -0.10952812460328777; 0.035207513527191085 -0.07698231629862473 -0.11078927588345953; 0.025992756816216333 -0.05380162677517708 -0.07889511548938503; 0.02439053879604175 -0.04607562223594701 -0.07174896349726471; 0.018850607805707638 -0.041649788510678076 -0.06300394149608123; 0.0026762848460182495 -0.00798147318261426 -0.014192985304888094; -0.0021805817847435106 0.0018809939736087152 -0.0002873329684557627; -0.0018438770982218565 0.004109559313412064 0.0051855421458067595; -0.0009811907170885089 -0.0004388196798886369 0.005723464020132936; 0.004885834029334217 0.009926423236417936 0.0023024237829615416; -0.005213388357647719 0.003599400418377951 0.0008956615356759352; 0.010475547420841506 0.0029564094757969952 -0.0022713610825993488; 0.012395062637582192 -0.017070169130735235 0.004035232405148727; -0.01181406925563513 -0.003120959345815806 0.01633282045784075; -0.01808087873999249 0.003250207357570453 0.00796022077218111; -0.019153946978860338 -0.012209865129469581 0.0038218909116820663] %
+
+Mass Used: 73.29971366687414 kg
+Launch C3: 119.33484706438237 km²/s²
+||V∞_in||: 1.024243995378042e-5 km/s
diff --git a/archive/ES_0.6596274845816918 b/archive/ES_0.6596274845816918
new file mode 100644
index 0000000..9e6ca60
--- /dev/null
+++ b/archive/ES_0.6596274845816918
@@ -0,0 +1,22 @@
+archive/ES_0.6596274845816918---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T15:17:54.610
+Launch V∞: [6.039127028256713, -8.900602779200751, -2.5826975057933694] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012173576456573172, 0.07067652530479196, -0.08521686301849944] km/s
+ V∞_out: [0.06775065790440084, 0.06922326688535511, 0.05498298795326775] km/s
+ time of flight: 9.803159697112666e7 seconds
+ arrival date: 2026-06-02T06:17:50.610
+ thrust profile: [0.34631149250879606 -0.25415595602948177 -0.20734046993410268; 0.21791575434990593 -0.04491327850639034 -0.1960227602002975; 0.139263297385662 -0.000632780517292103 -0.1705366815979958; 0.09062639063286683 0.009227977687512847 -0.13861915554851367; 0.05420736701191884 0.009062273379227302 -0.0984507443381607; 0.02733503654309313 0.005890468043888139 -0.056681032051350104; 0.013405776856422252 0.003465923536478856 -0.030774266377485267; 0.010856548672341752 0.0031109883895629824 -0.026595437865993946; 0.0069563625013018115 0.002087317884114188 -0.017084703702443357; 0.0003514890793633001 1.9606094147211106e-5 -0.001168897408208781; 0.00031615856553718195 0.00010035011938376045 -0.0008902804843213656; 0.0011092629051121907 0.000549016950892431 -0.003227144824103683; 0.000352983753269155 -0.0003505580493247366 -0.0003902242311454305; 0.00014533433805975188 -0.0001245772729919002 -0.000614577596648248; -7.781571577729373e-6 -0.0003014232567780706 -0.0005171198019923056; 0.0003580888961847802 -0.00023743902802524173 -0.0005248518080335335; 4.169727746465893e-6 -8.641777238432689e-5 -0.00013617997840656448; -1.811452378547979e-5 6.895259594739549e-5 -0.00010649284908147464; 0.00017494621644197476 -0.00042690444825831586 -0.003224572939032363; -0.0004094184565368986 -0.00035209332287134147 -0.00040943391614112364] %
+
+Mass Used: 55.78641491132612 kg
+Launch C3: 122.36211150296819 km²/s²
+||V∞_in||: 0.11137899683340943 km/s
diff --git a/archive/ES_0.6596943881449358 b/archive/ES_0.6596943881449358
new file mode 100644
index 0000000..d8a7986
--- /dev/null
+++ b/archive/ES_0.6596943881449358
@@ -0,0 +1,22 @@
+archive/ES_0.6596943881449358---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T05:35:13.004
+Launch V∞: [7.4333355645477, -7.623719294513436, -2.6106846280741585] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.16260616037665618, 0.30234801671880634, -0.3555870160160198] km/s
+ V∞_out: [-0.25228480948370335, 0.2948453866855423, -0.3061220833024192] km/s
+ time of flight: 9.623237641682786e7 seconds
+ arrival date: 2027-05-29T00:48:09.004
+ thrust profile: [0.988489384183162 -0.5214229903772613 -0.5180758950318333; 0.1394939037208442 -0.013414154517998973 -0.14326278748277244; 0.030606550709756562 0.0022795664310397905 -0.0492131280996734; 0.022312895077455083 0.004158948149605772 -0.04693969424304386; 0.04656266495847603 0.011404523925922554 -0.10705752621118791; 0.010413016839757453 0.0035354947435634982 -0.029575477060905027; 0.005459887260966272 0.0014424086491783507 -0.017110201868976514; 0.008337531646932789 0.00285673345260563 -0.027575276126179212; 0.001547013859217512 0.000643226607202768 -0.006138440591606059; 0.0009565388582075086 0.00022525911816759518 -0.0024571337789615214; 0.00181372930778187 0.0006565550877412411 -0.0023176166090118993; 0.0011789172476774972 -0.001028460212898727 -0.003238675915397454; 0.0018173642989567085 0.0009696611694698922 -0.006558088433955875; 0.0006716250601104864 -0.0002503194780995319 -0.004194022646113408; 0.003963523687554571 -0.0028011623783423655 -0.002256869059508531; 0.001435645838973264 0.000980802514735079 -0.0008412246740892222; 0.0014034676848813932 0.00015130907176961043 -0.006081958155457133; -0.0008679451415618065 0.003961275377549683 0.0030291399494213837; 0.0007314152090436029 -0.0008635902659281658 -0.002918800812288915; -0.0003402624164543505 -0.00020501733275705384 0.0016494042553296547] %
+
+Mass Used: 68.5278411126069 kg
+Launch C3: 120.19124772396883 km²/s²
+||V∞_in||: 0.4942643144769927 km/s
diff --git a/archive/ES_0.6598950184687299 b/archive/ES_0.6598950184687299
new file mode 100644
index 0000000..dd64317
--- /dev/null
+++ b/archive/ES_0.6598950184687299
@@ -0,0 +1,22 @@
+archive/ES_0.6598950184687299---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T06:16:09.713
+Launch V∞: [7.5934721315950355, -7.687483326309873, -2.7562477408102803] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.08429030626015585, -0.04393124608961853, -0.005952716698944643] km/s
+ V∞_out: [0.0767714982271264, 0.0374934088546149, -0.0425555386382343] km/s
+ time of flight: 9.6636984585373e7 seconds
+ arrival date: 2027-06-02T17:52:33.713
+ thrust profile: [0.4619611359307013 -0.22002203370542966 -0.252066843375733; 0.16106532539126237 -0.014729514502114745 -0.1707343530575513; 0.07624809011198484 0.006812950525233621 -0.11851153408489241; 0.03810207113906634 0.00726711024514024 -0.076925018110278; 0.015499468713189617 0.00406956751805946 -0.03881089737944756; 0.008519190858611478 0.0025262025149201555 -0.024418337805828198; 0.004892115585468376 0.0016962591469496548 -0.016067497393249152; 0.0030539249080044806 0.0011592728554561075 -0.010853880566419769; 0.0017379916004313322 0.0010907914486932206 -0.006822300008800585; 0.0013354255062621536 0.0015096384524100012 -0.007807457197680739; 0.00024243916633143967 -5.237456188506484e-5 -0.0007879395687531636; 0.0005697980020048845 0.0004936046653528307 -3.538116624898194e-5; 4.210331414519162e-5 0.0007219943422994623 -0.0005691890354119944; -0.0008437554729994485 -0.0011175896846367182 6.185157391476437e-5; 2.251259400096593e-5 2.985401628076553e-6 -0.00014379632475558404; 4.595154376112945e-5 4.3143882759617713e-5 -0.002218190432695942; -0.0006382332786708574 -0.0003789913411356363 0.0004774590421473446; -0.0005649535240120356 0.0010454487896458052 -0.00010951099960202501; -0.00036199691073900196 -6.0631393017232646e-5 0.0011303914577469826; 0.001734293197554156 0.0005204743351324494 0.0008751747033676678] %
+
+Mass Used: 44.47265187995845 kg
+Launch C3: 124.35512051432454 km²/s²
+||V∞_in||: 0.09523783359839401 km/s
diff --git a/archive/ES_0.6600318417630374 b/archive/ES_0.6600318417630374
new file mode 100644
index 0000000..fbb2e7a
--- /dev/null
+++ b/archive/ES_0.6600318417630374
@@ -0,0 +1,22 @@
+archive/ES_0.6600318417630374---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T20:50:15.043
+Launch V∞: [7.440751611047492, -7.6801114087868845, -2.1601082699767433] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.5475198594096093, -0.5103231919669784, -0.058258516311550455] km/s
+ V∞_out: [0.4833649118444065, -0.39615859990399227, 0.41638463085007543] km/s
+ time of flight: 9.684612874924362e7 seconds
+ arrival date: 2027-06-04T18:32:23.043
+ thrust profile: [0.6163632836856306 -0.3294352013215769 -0.34936810840575117; 0.3227096945791794 -0.035470120915439544 -0.3323724328346466; 0.14708444811577626 0.009747107014753526 -0.22141011846133624; 0.09030622611179712 0.014366267605606964 -0.17328119070309095; 0.05431213951587406 0.011626525306337974 -0.12379113680578895; 0.019649230818070438 0.004739102079948441 -0.05141793552777896; 0.005320448343216786 0.001941392584108716 -0.01609666616223926; 0.0013024246741111054 0.0018225152439931371 -0.007493406726467794; 0.0010844912187936706 -0.0007411816951612908 -0.008613411389893355; -0.0005328384707675281 0.001924407786207076 -0.003938821282854829; 0.0016505133301074931 0.000405781741715657 -0.006976952293655454; -1.024499741957512e-5 -0.0006318430336174979 8.98417031861506e-5; -0.0015730126283751544 0.0008325178931937819 -0.0007996514527554932; 0.0007642603302840707 -0.001019744952815311 0.0002134955090882316; -0.00019291786698636196 -0.0007143767342952191 -0.003234827620019687; 0.00031780821465164665 0.0005719948198019603 -0.0018232218619964919; -0.0018519344139045428 -0.00013291580905844995 0.0014734349446017597; -0.0011897701223931877 3.996163567011388e-5 0.0005453008144694413; 0.00010319768700919494 0.0028957344820051247 -0.0011072429848282335; 0.0002551461628100339 -0.0013957870084395866 -0.005052712510771773] %
+
+Mass Used: 75.78319481775725 kg
+Launch C3: 119.01496352670624 km²/s²
+||V∞_in||: 0.7507341816049853 km/s
diff --git a/archive/ES_0.6607757121893783 b/archive/ES_0.6607757121893783
new file mode 100644
index 0000000..355ed89
--- /dev/null
+++ b/archive/ES_0.6607757121893783
@@ -0,0 +1,22 @@
+archive/ES_0.6607757121893783---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T18:38:27.318
+Launch V∞: [5.70069732158337, -8.81892297711638, -1.995860048164283] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.014489568308340995, -0.02000483304133004, -0.020368719171071505] km/s
+ V∞_out: [-0.03940018430863138, -0.022011120289379262, -0.0011586020910012967] km/s
+ time of flight: 9.718559967791085e7 seconds
+ arrival date: 2026-05-23T14:38:26.318
+ thrust profile: [0.8569641812043536 -0.691108803952856 -0.46764466738717914; 0.5408535531116941 -0.15120499173153895 -0.4813420869785984; 0.15763878526393604 -0.0120274543750863 -0.19805021838578735; 0.12718950391109976 0.003779572618509239 -0.1960575012759141; 0.05327290800583003 0.005091025727508825 -0.09580531185615396; 0.007208914616487703 0.0027664811645264358 -0.018091593668826008; 0.004792040722266814 0.004537827698613458 -0.018266896303469015; 0.014744984875895375 0.0037250542566983646 -0.03484153959864616; -0.0014663705486944 0.0004422358663927504 -0.00779369230019036; 0.00304493242589436 -0.00248171114434358 -0.006301116516320561; 0.00380691233458432 -0.0037074814240858267 -0.0029839057583646734; -0.005627145358584749 -0.0010073160074082746 0.0028281803982233727; 0.0019617589278244666 0.0039138517541762 0.003020497681657551; 0.0032777121221059533 -0.0038913948063263844 -0.009381066450829088; 0.003159327111943874 -0.002139522179919497 0.0007837742788238617; -0.003100883385505547 -0.0035018377735819657 0.0017821505611612318; -0.00784670296878797 -0.004393053025860329 0.005700729793553314; 0.003533366005319671 0.0026456487032048685 -0.0031240611434241805; 0.00032474548531346995 -0.00021740784550536773 -0.0019893476210001847; 0.003450677304046292 -0.017350208842985486 0.0002473565658947104] %
+
+Mass Used: 104.41860728482334 kg
+Launch C3: 114.25480976047737 km²/s²
+||V∞_in||: 0.03201602185537025 km/s
diff --git a/archive/ES_0.6611261228206298 b/archive/ES_0.6611261228206298
new file mode 100644
index 0000000..04e2372
--- /dev/null
+++ b/archive/ES_0.6611261228206298
@@ -0,0 +1,22 @@
+archive/ES_0.6611261228206298---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T07:28:40.421
+Launch V∞: [7.457446368802676, -7.386220861975069, -2.1057868957851515] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.003719223417069495, -0.005807327658869117, -0.0021755212560674655] km/s
+ V∞_out: [-0.004013643922036176, 0.005407104855957401, -0.0026348398452468373] km/s
+ time of flight: 9.643588378662483e7 seconds
+ arrival date: 2027-05-28T11:13:23.421
+ thrust profile: [1.0 -0.5659895355835964 -0.5197548452498866; 0.4456090308070404 -0.01753966836432289 -0.3732574746538644; 0.16220778076273282 0.026237625972397476 -0.21006894471220014; 0.08067641007715477 0.02202948502023032 -0.1354182723759191; 0.022156704709850678 0.007733094461794723 -0.04600429670031722; 0.053288247927651196 0.02128873504853672 -0.11891030385651521; 0.032355059356337555 0.014312909600338182 -0.08011688102392885; 0.021213812753314173 0.010050371443657835 -0.057686906058307286; 0.006475022725985829 0.0030557051555887985 -0.016345041243482843; -0.0010785486602970956 0.004189154778362593 -0.0035898007194760722; 0.003763449002001691 0.0011902260800977567 -0.0058543683253791876; 0.0005359395932809981 0.0003225496215974484 -0.0018238493162389532; -0.0018238613387255944 0.0010357895377937306 -0.0034310804099455154; -0.0005567657926772301 -0.00010035245492376853 0.0009185338799217319; -0.0007319127638471606 0.0014208176241608103 0.00509666455502019; -0.0024444847380598873 -0.0015006761961570622 0.002226268152217126; -0.0016225958777512756 -3.227670823073247e-5 0.002187474192041417; 0.0019987660163470022 -0.00534102194065561 -0.010387727652864095; -0.0008785166303405352 0.0021789495206213927 -0.008953015243062329; -0.000753515063605277 6.425059775237198e-5 -0.004316024509611233] %
+
+Mass Used: 102.78987336462569 kg
+Launch C3: 114.60410341590442 km²/s²
+||V∞_in||: 0.007231221895305504 km/s
diff --git a/archive/ES_0.6612778542018805 b/archive/ES_0.6612778542018805
new file mode 100644
index 0000000..59fa187
--- /dev/null
+++ b/archive/ES_0.6612778542018805
@@ -0,0 +1,22 @@
+archive/ES_0.6612778542018805---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T01:49:02.353
+Launch V∞: [7.606191224775047, -7.695887085922882, -2.5895468665599597] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.031976691145662234, 0.16156999587026016, 0.030413101547968883] km/s
+ V∞_out: [0.16180614996008252, -0.023888601140674228, 0.036014249428654194] km/s
+ time of flight: 9.698315046346937e7 seconds
+ arrival date: 2027-06-06T13:34:52.353
+ thrust profile: [0.34568354440669113 -0.1750573755694172 -0.19734451972503156; 0.19489055187232665 -0.016196086562798022 -0.2037406027816796; 0.07937739239908113 0.006712602431150406 -0.12262519027531334; 0.0491074662286124 0.009203946809984934 -0.09947415385062482; 0.046015189440472636 0.01051230066885562 -0.10395516043401709; 0.020141612873058327 0.0056650689741413185 -0.05555049414284276; 0.005855068948440886 0.002510348013753295 -0.020943325599513295; 0.002674659159710827 0.0012345038429925834 -0.010594600838337902; 0.007297293116256183 0.0027471324883452143 -0.026513675479027794; -0.00020520523424550415 0.0007255810468514156 -0.0012730267774796948; 0.0039323550218932374 -0.0009087040181138405 -0.0011315721495494561; 0.0030469453562273026 0.002934267871323632 -0.005302964108366669; 0.0025248702991467215 0.00143914305096888 0.0005187404205122107; -0.003277648192513828 -0.0054372268669195855 -0.001013525475958745; 0.0012972104918894732 0.005652619449640224 -0.004420811692035649; -0.001002958470072701 0.007810172813907159 -0.01186823129294275; 0.00023977111509420517 -0.00017700101887616797 -0.0016093312437490022; 0.008240066055748046 -0.006338011693378491 -0.005774041916123547; 0.00121892819618738 -6.325679342610024e-5 -0.006221245504868796; -0.00035326521400514516 0.0009072465363093492 0.007113406682523565] %
+
+Mass Used: 49.40247012835198 kg
+Launch C3: 123.78657596123003 km²/s²
+||V∞_in||: 0.16748829537585017 km/s
diff --git a/archive/ES_0.6614624987131213 b/archive/ES_0.6614624987131213
new file mode 100644
index 0000000..f917d20
--- /dev/null
+++ b/archive/ES_0.6614624987131213
@@ -0,0 +1,22 @@
+archive/ES_0.6614624987131213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T15:39:33.607
+Launch V∞: [5.704280199137043, -8.795388861274109, -2.1167423258608085] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.055432913723126635, -0.30751398448800427, 0.34917660365403225] km/s
+ V∞_out: [-0.29338763433163906, -0.3036349964250367, -0.20340043567912888] km/s
+ time of flight: 9.71406716889906e7 seconds
+ arrival date: 2026-05-22T23:10:44.607
+ thrust profile: [0.9596605280851144 -0.7682403632602448 -0.48270390534811575; 0.3960331841953218 -0.10683145171077205 -0.31862630984129436; 0.12219920525443119 -0.006899018740103532 -0.137195890652697; 0.20743805495344173 0.008753306971541157 -0.26521272948640046; 0.06417081043926459 0.007101974177054393 -0.10026817357406077; 0.00921674001129192 0.0044295914564105735 -0.0191304517092173; 0.007519543231145048 -0.003328375242871602 -0.012722959760156452; 0.019572003535331374 0.007829586694073222 -0.030858220953801457; 0.009523782923041246 0.001053346577822426 -0.018544096874461853; 0.011597691546624352 0.0024419920261589995 -0.0252455531985484; -0.0009485091847169507 0.00015275065652834672 -0.006937178112775551; -0.000885666242381774 -0.00030655270255780086 0.0030124821105955903; 0.0025964988502869893 0.0012445929593100126 -0.011500784998149322; -0.0006015498174535838 -0.0026640615113591596 -0.007673509208148781; 0.004293872734160757 0.00044399441140331757 -0.00523927569527151; 0.0009683915908033913 0.0035777909500256328 -0.0018894865654271783; 0.004672710908702015 0.0005558928169658657 -0.009957670967537531; -0.006569600476174899 -0.006718590633677006 0.0049914257023233365; 0.00047850923800668197 -0.01527899962812285 -0.012013907755376921; 0.01013487052119729 0.0011732746795554245 -0.01289237376072501] %
+
+Mass Used: 104.49963916724528 kg
+Launch C3: 114.37827588538222 km²/s²
+||V∞_in||: 0.46857439016541363 km/s
diff --git a/archive/ES_0.6620409048795199 b/archive/ES_0.6620409048795199
new file mode 100644
index 0000000..48cfa5c
--- /dev/null
+++ b/archive/ES_0.6620409048795199
@@ -0,0 +1,22 @@
+archive/ES_0.6620409048795199---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T23:25:15.309
+Launch V∞: [7.522281759014362, -7.416499445821283, -2.342917835763853] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.689117909868094e-5, 0.00017040349828385378, 0.00027519127244558355] km/s
+ V∞_out: [0.0002861490388087599, 2.9742251852978055e-5, -0.0001556937919778597] km/s
+ time of flight: 9.542462587155268e7 seconds
+ arrival date: 2027-05-17T10:15:40.309
+ thrust profile: [1.0 -0.5512905935740294 -0.5495400867724692; 0.4287527439818845 -0.028191025159975614 -0.37789986304788814; 0.11164045713246719 0.014833406233304298 -0.14713645140117126; 0.05434186754104532 0.013452409516667744 -0.09394632721220102; 0.03440941884820105 0.01247208889280128 -0.07293469394327314; 0.02172224499817008 0.006611681425063835 -0.04895483289917199; 0.016756634672660472 0.008743428101918077 -0.04550001005838594; 0.002318200911963874 0.0011862187014461617 -0.006679496049527965; 0.0006684745302197867 -5.3486947685588745e-5 -0.0004154792336252065; 0.0011778428722156844 0.0006642130408713863 -0.0036774152106057146; 0.00045078401038661244 0.0001581991952255753 -2.558061059447915e-5; 0.0010701454259493819 0.0016715819852243657 -0.003952435482683862; 0.0016866278441088859 0.0006519804699356596 -0.005342368337939348; 0.0010823205993956081 0.0006666135772872594 -0.0038206448503710134; 0.0007361265600435386 0.000417344994153111 -0.0002568079771851496; -0.00038997390225566954 0.0017151735044307424 -0.0002766044545027919; 0.0005174503467270742 -0.0007445568163657348 -0.0015178810850723333; -0.002103009709144726 -0.0002647020713391358 -0.00020690074524794613; -0.0004954456968749607 0.00024276877794330415 0.00040092086426233133; -9.404563361614757e-5 0.00039557883458727055 -0.0006659118663186652] %
+
+Mass Used: 89.42342557689335 kg
+Launch C3: 117.07845087700798 km²/s²
+||V∞_in||: 0.00032705713772192665 km/s
diff --git a/archive/ES_0.6621065118513791 b/archive/ES_0.6621065118513791
new file mode 100644
index 0000000..4145e22
--- /dev/null
+++ b/archive/ES_0.6621065118513791
@@ -0,0 +1,22 @@
+archive/ES_0.6621065118513791---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T18:42:28.853
+Launch V∞: [7.782136980010125, -7.536954905521049, -2.9281294088526613] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00039914725958232973, -0.001139993695211334, 0.003615423871269303] km/s
+ V∞_out: [0.0010646836268621103, 0.0015377819870975756, -0.0033246965029069993] km/s
+ time of flight: 9.679496885335071e7 seconds
+ arrival date: 2027-06-03T02:11:56.853
+ thrust profile: [0.27568051850443226 -0.13308749258765074 -0.1481548309571137; 0.14005687038170944 -0.005609952814980432 -0.129960420850455; 0.07587068400155021 0.012212665765070987 -0.10435616555982151; 0.04480871982273895 0.012436721618788388 -0.08024429127087516; 0.025044680929980544 0.00882071509254874 -0.054254025454300865; 0.015760160198257527 0.006392774818234396 -0.03968963310315397; 0.012997973714307234 0.005785029582655016 -0.036543218433006314; 0.008469641641023186 0.003622941971463126 -0.02272750466332038; 0.002482844044143862 0.0013155410474088125 -0.00662621977328201; 0.0011565001273991975 0.000474796332908106 -0.0036256825361239103; 0.004058649832634131 0.00047866952116633376 -0.003242685507520094; -0.0005326931119351763 -0.0029279234442456392 -0.002858080825307481; -0.0022726504790951084 0.0027406846398789157 -0.001437851916079833; -0.0009834690653220141 0.0004703228990751002 -0.0011741556382772662; -0.001025098055459664 -0.0021888233119210596 -0.0015153667325789517; 0.0004651987256970762 0.0005651420905586374 0.0005218686142276861; -0.00552750169336471 -0.0012097825279996188 -0.0006736668763425201; 0.009538478826231753 -0.0010574457608322472 -0.0027555305552554735; 0.0018259328121400908 -0.010030418546947265 -0.005270527226719467; 3.007937710442361e-5 -0.002052509707554922 0.0023187664367756177] %
+
+Mass Used: 37.80008931876955 kg
+Launch C3: 125.94128705848675 km²/s²
+||V∞_in||: 0.0038118491482346975 km/s
diff --git a/archive/ES_0.6623593708288258 b/archive/ES_0.6623593708288258
new file mode 100644
index 0000000..1b8909e
--- /dev/null
+++ b/archive/ES_0.6623593708288258
@@ -0,0 +1,22 @@
+archive/ES_0.6623593708288258---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:15:39.394
+Launch V∞: [7.558947266848577, -7.524508402791153, -2.1971961346957087] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0017559754200700574, -0.005263425208365888, 0.01665913569052676] km/s
+ V∞_out: [0.004783603640028102, 0.006881233559135895, -0.015429869776741262] km/s
+ time of flight: 9.630040593625483e7 seconds
+ arrival date: 2027-05-27T19:22:24.394
+ thrust profile: [0.6210112412082379 -0.3106848931290569 -0.29828236554111887; 0.369901666625603 -0.022681709463693224 -0.3207677551134969; 0.17776747107113244 0.024862759192813454 -0.23537598669474583; 0.09269792933903524 0.021370789964909348 -0.15853064642398798; 0.07544028695879576 0.02308629330586625 -0.15898226818514263; 0.04467079807560206 0.013345430594390114 -0.09798665355648557; 0.015296435001114357 0.005656302958901059 -0.03539562839227281; 0.003928121953947927 0.002114647718312287 -0.009095290261512703; 0.002973689885446257 -0.001096820805138633 -0.003444572419240819; 0.0038773473840572606 -0.00012889836381844836 -0.0060416815569654045; -0.0015278256550005026 -0.0007986531331112159 0.0010384970564519956; -0.0005700647111364916 -0.0013243306307274326 -0.0010377272363045226; 0.0010157480531082018 0.00021087321870209288 -0.00034060107133413375; 0.003977032404390891 0.0007185755610394337 -0.0008335140022636197; 0.0036445611377192676 -0.003183917729327321 0.00012465648136841334; 0.0018111575142051985 -0.0027217109117654613 -0.0007291937667790816; 0.0005841680432763648 0.006245102771039224 -0.008016530816710521; 0.00248576179623524 0.004570919352204305 -0.007353130750144855; 5.460836457917028e-6 -0.00023390407514755165 -0.00033037146954889134; -0.0006992011470718785 -0.0016894187747757755 0.0012615989006778527] %
+
+Mass Used: 81.0150414778318 kg
+Launch C3: 118.583581340994 km²/s²
+||V∞_in||: 0.017558869455501232 km/s
diff --git a/archive/ES_0.6631636608938193 b/archive/ES_0.6631636608938193
new file mode 100644
index 0000000..da74fdc
--- /dev/null
+++ b/archive/ES_0.6631636608938193
@@ -0,0 +1,22 @@
+archive/ES_0.6631636608938193---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T18:26:59.812
+Launch V∞: [7.3362432874327554, -7.726571206185449, -2.188867660601456] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.06736848794277916, -0.15446475681312552, -0.20252843886216998] km/s
+ V∞_out: [-0.2323167877274408, -0.03718324109491831, 0.11855290212362514] km/s
+ time of flight: 9.66838448265596e7 seconds
+ arrival date: 2027-06-03T19:04:23.812
+ thrust profile: [0.9795754047784617 -0.49366862138765866 -0.4834216826794168; 0.14074191127426497 -0.018041426083111513 -0.15508569923551138; 0.05511214233390918 0.0028929222067997696 -0.09007144730438116; 0.05903679196930662 0.006037686913523189 -0.11247533636341374; 0.04175512218400191 0.0012189421392882012 -0.09209661074680656; 0.015184541296695771 0.003798656538274986 -0.04518719752406161; 0.0675780103145378 0.015948584888361338 -0.19803618408885973; 0.0253625348892571 0.006538730180819346 -0.07854638237942646; 0.001053882601212278 -0.0014066783976904645 -0.002864699019391046; -0.0007082992473932205 7.641895676980035e-5 -0.0021847960900578177; 0.001049403287006184 0.0006287994467959234 -0.0020138860754555492; 0.000612441175266702 -0.0007433602695973659 -0.003186149980804905; 0.004743910251447681 -0.0011376361919583989 0.002160928239872048; 0.005992128098414129 -0.005287235632824322 -0.006269173092604384; 0.0010367538125081906 0.008907167178661236 0.0010457700049751129; 0.00553377590030322 0.002712998354942639 -0.014494041806896351; 0.01353021538548733 -0.007049654567487731 -0.007890581257820155; -0.0003783769806354063 0.0013720973655312733 -0.0013495436281639917; 0.005067158242404982 0.006391545809224385 -0.0021283625827963203; 0.006485916487545498 0.0018211455469704044 0.0031336459310112134] %
+
+Mass Used: 83.54046380447107 kg
+Launch C3: 118.31150981228312 km²/s²
+||V∞_in||: 0.2634684854265916 km/s
diff --git a/archive/ES_0.6634943445682183 b/archive/ES_0.6634943445682183
new file mode 100644
index 0000000..3a3d3d5
--- /dev/null
+++ b/archive/ES_0.6634943445682183
@@ -0,0 +1,22 @@
+archive/ES_0.6634943445682183---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T04:45:58.272
+Launch V∞: [5.858926130364765, -8.866557233731996, -2.272252294014127] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007631554937567418, -0.013905268873036442, -0.014221334944358177] km/s
+ V∞_out: [-0.01871313696115926, -0.010163356421283149, -0.0005735403656644488] km/s
+ time of flight: 9.612598753473675e7 seconds
+ arrival date: 2026-05-11T18:25:45.272
+ thrust profile: [0.809287768320456 -0.6387831158024926 -0.44031918161661643; 0.32812455017892556 -0.08780741480776554 -0.29900591194738524; 0.16662344815363048 -0.011342641064999142 -0.21274367647654757; 0.09935546751866063 0.003814844024954391 -0.1575651079055864; 0.05402700032056027 0.005798854432682776 -0.10065311427659197; 0.010200058718066875 0.0013527470844783547 -0.023443326655021704; 0.004491987740220644 0.0008979813332593904 -0.013029516399037521; 0.0007868446001004655 0.00044730515782994134 -0.0021964414200089342; 0.0009173531570930398 0.00016992980919353716 -0.003276512135567817; -0.00015370539021515182 -0.00025998433963849354 -0.0002891714940195405; 0.0006307040509080321 -0.00039065738919762875 -0.0008546209482266965; 0.0009575592650449416 0.0009389256131113507 0.0024314237048038007; 0.000296960121314994 -0.0003991305204377961 0.0023317852989662136; -0.0010721102044842557 0.001502011843310059 0.002712856283443913; -0.0002492073538819808 -0.000550556797101111 0.0013791905771653244; -0.0027263118876253226 0.0003062930323648193 0.004326313149781278; -0.002383397427826344 -7.641628849042746e-5 0.0016930140999534742; -0.0013149504606295506 -0.0007615191219208585 0.0009465432113257273; 0.0003109775008215815 0.0005674205993783951 0.0012081180293482543; -0.0004199177288787166 -0.008779591307717759 0.0070400596415164446] %
+
+Mass Used: 85.12516743427068 kg
+Launch C3: 118.10598306776869 km²/s²
+||V∞_in||: 0.02130360300034172 km/s
diff --git a/archive/ES_0.6635592296703813 b/archive/ES_0.6635592296703813
new file mode 100644
index 0000000..16df207
--- /dev/null
+++ b/archive/ES_0.6635592296703813
@@ -0,0 +1,22 @@
+archive/ES_0.6635592296703813---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-03T22:12:30.646
+Launch V∞: [8.013116959239136, -7.582542068589142, -0.523944289517925] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.0209082763368812e-8, 1.4362075249074602e-7, -3.0097152457558523e-6] km/s
+ V∞_out: [-1.28613900349213e-7, 3.0099830883617174e-6, -3.641398024062834e-8] km/s
+ time of flight: 1.8262563264058548e8 seconds
+ arrival date: 2030-03-18T15:33:02.646
+ thrust profile: [0.005030181285126628 -0.003532668481572535 -0.003289978585003641; 0.01085114108259939 -0.01760869534864988 -0.025485951629350415; 0.012699596676825579 -0.029204235778858043 -0.04202530671603515; 0.0222019606188833 -0.05432807032187725 -0.07789174579132081; 0.0363121584380442 -0.08673674433214755 -0.12499330309764176; 0.029533447964681176 -0.06796867591551728 -0.09911245262822273; 0.06757112671635813 -0.14754138289965382 -0.2168634547430206; 0.0055883506208578605 -0.011779614348052407 -0.018079073307617027; 0.007480898120047031 -0.014593493764520078 -0.02309107535984635; 0.014045028804663226 -0.02784109222171482 -0.042747127572133566; 0.0010662707892986128 -0.002259924649131527 -0.003495848784957678; 0.00010364333864825988 -0.0001995335120513555 -0.00028339728120937573; 0.0003914557025913117 -0.00044407399304386254 -0.0009892146199629865; -1.568171120340727e-5 0.00012027378403803941 -3.185976156952833e-5; -0.00182121978814098 -0.0009880941979469985 -0.0014180790482515957; 0.0008573620823303786 -0.001343923749077879 0.00018593753581803713; 0.001834903053953539 -0.00040002166516595614 9.285832296687988e-5; 0.0007578124752383362 5.6203680177254774e-5 -0.0017808309363063694; -0.0009181334936983272 0.000691256552030113 0.0013480810238996035; 0.00014995564717529093 -0.0002262776047632058 -0.0006121605683436898] %
+
+Mass Used: 62.60532069859573 kg
+Launch C3: 121.97950524288841 km²/s²
+||V∞_in||: 3.013207790396699e-6 km/s
diff --git a/archive/ES_0.6636430327079206 b/archive/ES_0.6636430327079206
new file mode 100644
index 0000000..1b2f6c8
--- /dev/null
+++ b/archive/ES_0.6636430327079206
@@ -0,0 +1,22 @@
+archive/ES_0.6636430327079206---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T07:00:39.442
+Launch V∞: [7.5298457416344355, -7.638826011585176, -2.1972889726861102] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.019989635861035103, 0.10454745257164755, 0.018886908824152723] km/s
+ V∞_out: [0.10486095535391067, -0.013088300377820624, 0.022809227188232258] km/s
+ time of flight: 9.610080698218572e7 seconds
+ arrival date: 2027-05-26T13:40:45.442
+ thrust profile: [0.5374214641669907 -0.27901491888311747 -0.2543436867258354; 0.32318877516043326 -0.03164302851080995 -0.278823905511331; 0.24166245775641934 0.02016461935387969 -0.30467826215590216; 0.05752689628982863 0.01374182586133441 -0.10783026025753678; 0.037548591267283674 0.011191538324114072 -0.08059468711757636; 0.05085030520264365 0.01593522680310956 -0.11516535894926071; 0.015330337221817062 0.0054078977837673185 -0.039521570546712306; 0.007188699542274108 0.0024864915412712474 -0.01848950326950403; 0.015954860504062033 0.00788298222257774 -0.04674022143236386; -0.00013836993110509207 0.00025805100879621443 -0.0024148931077460174; -0.00054283975996486 -0.0006836683607417205 -0.0018795092948952902; 0.00047975302285466973 0.0017588988980468765 -0.0017113181089640338; 0.00015048682230858648 -0.0009365189230411345 -0.0019920497391184215; 0.0017202839824256135 -0.0006176122570982973 -0.0017828913046189835; 0.0012371922474048375 -0.0016647281394769143 -0.0034350876997204178; 0.001605499754504614 0.0005360328427031491 -0.0036192715442811803; 0.00031916786164764817 0.00030907776281068034 -0.0012566043922117168; -0.0001571694525837478 0.0011719519997930388 0.0009493787451320922; -0.004810714130719442 -0.001617042517534039 0.0029879905355042263; 0.0028669793506773955 0.0006362921100219788 -0.0026392138583927003] %
+
+Mass Used: 74.96001324009103 kg
+Launch C3: 119.8783185575685 km²/s²
+||V∞_in||: 0.10810398099057006 km/s
diff --git a/archive/ES_0.6638214676531023 b/archive/ES_0.6638214676531023
new file mode 100644
index 0000000..7bfa984
--- /dev/null
+++ b/archive/ES_0.6638214676531023
@@ -0,0 +1,22 @@
+archive/ES_0.6638214676531023---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T00:27:32.740
+Launch V∞: [7.545393145060082, -7.365615332073699, -2.104740560187557] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.11017472753029, -0.31658774534783357, 1.0253955484181765] km/s
+ V∞_out: [0.06139363775309202, 0.08694638477149419, -0.1700678661772584] km/s
+ time of flight: 9.578520000036803e7 seconds
+ arrival date: 2027-05-20T15:27:32.740
+ thrust profile: [1.0 -0.5084851570527676 -0.49797206938809846; 0.37794696398973254 -0.01570813995179208 -0.33233569207149566; 0.15576946427297256 0.021500852763068023 -0.19960869338598497; 0.1174494363633702 0.03154563669825824 -0.1913913060794847; 0.06818586686044528 0.024444519684197356 -0.1344192391870468; 0.046634505088912 0.01626345983408495 -0.10381498284437932; 0.017261313208780618 0.007511708667930577 -0.04263350071206933; 0.01652395519919401 0.0076682844490843565 -0.043573609317078744; 0.0017978171862802828 0.0003741270210982676 -0.0026069534730898116; 0.0008862571782833825 0.0004048401899686625 -0.0023990150334085034; 0.0012722743573406771 0.0004751523299078157 -0.003249601671388003; 4.284645082961347e-5 -0.0007526927595045369 0.002409509681333631; -0.0012990431136961599 -0.0009902408560575437 -0.005313011398034318; 0.0021010490518352824 0.00131183197138868 -0.001187633648481593; 0.0012223177489322115 0.002646516876434612 -0.007977136516982277; -0.0033237432045858445 -0.0018737291587622169 0.004186374004288591; -0.0029045166674415094 0.003772868330966882 -0.003277949398837927; -0.00021388074033398715 0.0006938952291248119 -0.0003994304922409267; -0.0028096297168605684 -0.0017216277444390268 0.0007359460353046754; -0.0019660473255658376 -0.00014371122049356084 0.004874649568347346] %
+
+Mass Used: 100.03649699938433 kg
+Launch C3: 115.61517975929745 km²/s²
+||V∞_in||: 1.0787966915997709 km/s
diff --git a/archive/ES_0.6643525791689563 b/archive/ES_0.6643525791689563
new file mode 100644
index 0000000..dc7ad80
--- /dev/null
+++ b/archive/ES_0.6643525791689563
@@ -0,0 +1,22 @@
+archive/ES_0.6643525791689563---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:09:43.952
+Launch V∞: [7.670075935639434, -7.420611751558962, -2.3351722301701834] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.02818642541946886, -0.04894245630129135, -0.03565708888441728] km/s
+ V∞_out: [-0.049738608938818187, 0.03878662085028009, 0.020462465870900934] km/s
+ time of flight: 9.564551836065815e7 seconds
+ arrival date: 2027-05-19T08:21:41.952
+ thrust profile: [0.676675432064213 -0.32869171076763626 -0.3426876569452269; 0.3496209203076008 -0.014744173940970952 -0.30148767757331135; 0.17562489353730787 0.03126741553991698 -0.21796833980263486; 0.09901015847716466 0.028147467103288307 -0.1587980873660797; 0.054954970160994716 0.019781306045057075 -0.1072137300617407; 0.029137761867667256 0.012037281759699573 -0.06530282278095759; 0.03671472699446741 0.016668999223242425 -0.0874146864922637; 0.0018540646482796978 0.0009480813149671069 -0.004714911987611856; 0.0011811529308603415 0.0006050308510850424 -0.0032008888243281455; 0.00012880626998447713 8.042914895983069e-5 -0.0004911216877063458; -2.29700961190657e-5 3.40512491248275e-5 4.7217366432991594e-5; 0.00017884866519751578 -0.00041559368941440915 0.0008400451167405581; 0.00021916651665393716 0.00019834026461754514 0.000777790407694882; -0.0002947279767011227 -0.0005560790859613926 0.0003641811084487274; -0.00047908772371394777 -0.0011373730626254904 0.0001881242454738656; 0.0010289194203914733 -0.0008134511770314442 0.00020806837928711826; 0.0004518603941278331 9.551758908512154e-5 -0.0007574028214544713; -0.00036914951411983686 -0.0001612763396257569 0.000693623464064002; 0.0016245043951999666 0.0004648120716575677 -8.188103915146499e-5; -0.0009272652979864191 0.0029540452408082377 0.0002374133820713077] %
+
+Mass Used: 78.87800003640177 kg
+Launch C3: 119.3485729704081 km²/s²
+||V∞_in||: 0.06679271363286812 km/s
diff --git a/archive/ES_0.6644526051860163 b/archive/ES_0.6644526051860163
new file mode 100644
index 0000000..6d4d3e3
--- /dev/null
+++ b/archive/ES_0.6644526051860163
@@ -0,0 +1,22 @@
+archive/ES_0.6644526051860163---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T19:50:26.224
+Launch V∞: [5.7960082502456585, -8.897316166661906, -2.2263538844568647] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.026154240735442744, 0.14014616331196753, -0.16290852474625883] km/s
+ V∞_out: [0.13275575888710903, 0.1471368051526889, 0.08743322195774886] km/s
+ time of flight: 9.567660973293532e7 seconds
+ arrival date: 2026-05-07T04:40:35.224
+ thrust profile: [0.8928263835470563 -0.7235118776339203 -0.5055862676730807; 0.36065292038769553 -0.1054254805877327 -0.3243118166346027; 0.14712502176770823 -0.01359928343434773 -0.18717572826942686; 0.04799281088041744 0.0019724556087837384 -0.07937564239030297; 0.05547757210449875 0.006060175576365489 -0.10453812410830181; 0.00930057344299271 0.0011093128439027785 -0.01878345188458759; 0.01885694479771066 0.0033839315966210396 -0.043336840625918784; -5.383744088317138e-5 -0.0016929072822987712 -0.007059255493185584; 0.003091562095663505 -0.0007019441107744738 -0.0004431018575944356; 0.005497776899089535 0.00029234014920923425 -0.005264773046333268; -0.0029933992595215673 -0.0028628722382542443 0.0011526825286396918; 0.002599371562465774 0.003264096243292218 -0.0046314271989388; 0.0009578690949513533 0.0009164175741018083 -0.002977299831606711; -0.0005259101971301254 -0.0029301592976215328 -0.0006993275722295608; -0.0008411535975770513 -0.0005235108649564296 -0.0019086237176831977; 0.0005626410806268455 -0.002717546128005726 -0.0012452264842195064; -0.0017676604086653757 0.0021757727293479703 -0.00039403868973386224; -0.0015608824055079024 0.001187851131392013 0.0049157926089711725; 0.0026969489629720825 0.001622956418153753 -0.0012243785832587442; 0.00021415877061857063 0.0021419753221662533 -0.0010908371127547106] %
+
+Mass Used: 88.53788306946353 kg
+Launch C3: 117.71259822529522 km²/s²
+||V∞_in||: 0.2164813590924507 km/s
diff --git a/archive/ES_0.6648262660814833 b/archive/ES_0.6648262660814833
new file mode 100644
index 0000000..32189f1
--- /dev/null
+++ b/archive/ES_0.6648262660814833
@@ -0,0 +1,22 @@
+archive/ES_0.6648262660814833---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T14:54:11.877
+Launch V∞: [7.594681720572263, -7.515733871196338, -2.8321739084397457] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.1272291494871833, 0.06648929813868407, 0.009158002032356647] km/s
+ V∞_out: [-0.11298034339089706, -0.05723140348493622, 0.06789454654367513] km/s
+ time of flight: 9.901672673147134e7 seconds
+ arrival date: 2027-06-28T15:32:57.877
+ thrust profile: [0.39536557860803945 -0.19905776383155724 -0.2297937367270833; 0.18742776989118856 -0.011947783882292009 -0.19857784702642323; 0.08464020233190139 0.010228946660916796 -0.1301404363682165; 0.0361415803689073 0.007238504763674464 -0.06729505304565633; 0.02639817588767518 0.006968512514462181 -0.05796863716416254; 0.012483392124414926 0.003334386451553691 -0.028832697604691208; 0.00592256386293793 -0.0008810865532194915 -0.013115862896969525; 0.02153081791654481 0.00572104994098971 -0.06015392082382835; 0.0034657252340491006 0.01899397251672512 -0.015477720150277223; 0.009342368507473877 8.662556482760998e-5 -0.02401886800660661; -0.001092644304106705 -0.0026599051934898463 -0.018907183837588645; -0.00737206035605772 -0.015220254551985737 -0.010016926911083732; -0.0007550526110218349 -0.017676744673983558 0.0026183396013746167; 0.036507678205790664 -0.009223300950038886 0.008417860617448907; 0.022175690269129637 0.009604270331703527 -0.008809025927094162; 0.0010566329740652651 0.005162139737111986 0.019348520517136064; 0.0397877139063675 -0.01371703688618008 0.02758810722705775; -0.0037041863530277424 -0.05781348985826403 0.03306775677216013; -0.019667872534191985 0.010854486809176011 0.04915225342296677; -0.025020298044886136 0.0467331413288626 0.007084897536011857] %
+
+Mass Used: 62.87515563704346 kg
+Launch C3: 122.18665510708922 km²/s²
+||V∞_in||: 0.14384697510699174 km/s
diff --git a/archive/ES_0.6650035223263249 b/archive/ES_0.6650035223263249
new file mode 100644
index 0000000..2f0ac89
--- /dev/null
+++ b/archive/ES_0.6650035223263249
@@ -0,0 +1,22 @@
+archive/ES_0.6650035223263249---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T17:48:03.422
+Launch V∞: [7.585292372325127, -7.620032824293524, -2.4802680302493414] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.43798817778430577, -0.39375066280309073, -0.047668621746017534] km/s
+ V∞_out: [0.28881176004466924, -0.44604971811959393, 0.25856710247116893] km/s
+ time of flight: 9.5263012571878e7 seconds
+ arrival date: 2027-05-17T07:44:55.422
+ thrust profile: [0.7227434113717562 -0.37731092257294563 -0.34267397950128553; 0.17744402342756296 -0.015593866172718868 -0.16796578187792985; 0.12638989632141637 0.009399062573636176 -0.171742119827342; 0.033164255557111666 0.006670357258194593 -0.06314902206226196; 0.07641947305615154 0.018972083186472904 -0.15358034242950153; 0.02207156817627243 0.007248445197524856 -0.056314580020347435; 0.003477129382480448 0.001366491185257591 -0.009153972765189014; 0.0066613528261028265 0.002662841224668163 -0.01997574596847875; 0.008119760253042186 0.0034635513705187702 -0.02547370385952138; -0.000768015981252719 -0.00016906634783726778 -0.0013253444726725899; 0.0003279199311671887 -0.0012943310045977615 -0.0007889814134881834; 0.0008832688018441722 -0.0004959908169024603 -0.0010130758847680071; 3.9026363116439425e-5 0.0009554695998250234 0.00027758866268431503; -0.0004628601445008302 -0.001142813726142315 0.0016141308261797664; 0.0003222490187398934 0.0016877369034661407 0.0017542299726660637; 0.002155385616519915 -0.002358102995943076 0.0009968942213189947; -0.0030744542460601817 -0.0011914938014687152 -0.0030479035692773213; -0.0023135110821613618 0.0005272237643209629 0.001486086477524826; 5.877718094401424e-5 -0.0005610771522311078 0.0027660903828932923; 0.00028296818389275506 2.962156157386893e-5 -4.047331981325592e-6] %
+
+Mass Used: 65.609917020804 kg
+Launch C3: 121.75329011884143 km²/s²
+||V∞_in||: 0.5908853745320278 km/s
diff --git a/archive/ES_0.6650139525400298 b/archive/ES_0.6650139525400298
new file mode 100644
index 0000000..ec4b31d
--- /dev/null
+++ b/archive/ES_0.6650139525400298
@@ -0,0 +1,22 @@
+archive/ES_0.6650139525400298---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T03:10:00.870
+Launch V∞: [7.5429894534436315, -7.537829304308067, -2.4786208416214626] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [9.806339388879426e-5, -0.0013616009446785538, 0.00022963424359308162] km/s
+ V∞_out: [0.00034949275770625746, 0.0008118892702607432, 0.0010654490291764893] km/s
+ time of flight: 9.54080121173359e7 seconds
+ arrival date: 2027-05-18T09:23:32.870
+ thrust profile: [0.8884580084548759 -0.45868182966086857 -0.4481605930441747; 0.2764633738200723 -0.02342061020645671 -0.25345885455659434; 0.0786079380864564 0.00908405431937062 -0.1126310584646258; 0.028226018083604178 0.004497864462766536 -0.04934712772791467; 0.034521582890002504 0.008954995874127666 -0.06484871814803658; 0.03929869323503244 0.009839453713557534 -0.07886662596306117; 0.01843438971007086 0.006455066695266571 -0.034143287509271855; -0.0028836132466817928 0.004827449042639561 -0.0225296532345621; 0.005617345810597847 0.004679262298726516 -0.016064612783250904; 0.006789842244452339 -0.0006260041339263356 -0.0024580921976196262; -0.0008985345720297351 0.0017788777696839115 -0.007996231408274223; 0.002967959127874768 0.006498197525624955 -0.013087368258335808; 0.00018861382327637873 -0.0010297345295787888 -0.0013720792199729687; 0.00017539477893934282 0.0006081533845985014 0.00032533621707940726; 0.00068761701709511 -0.0013803154074009155 -0.006820925712184494; -0.010300390268137827 0.007479533429964408 -0.017610362843941175; -0.0031382807554891515 -0.001433641740052356 -0.01620889446260662; 0.004331905558319403 0.0058468243786097066 -0.01202365234601234; 0.010997732403471721 0.0024797295351632097 -0.0026124606480405297; -0.003935327462070242 -0.0035786078304017328 0.000523991533159645] %
+
+Mass Used: 76.67140084239054 kg
+Launch C3: 119.85912179216758 km²/s²
+||V∞_in||: 0.0013843068473431337 km/s
diff --git a/archive/ES_0.6651005473066154 b/archive/ES_0.6651005473066154
new file mode 100644
index 0000000..868b8a6
--- /dev/null
+++ b/archive/ES_0.6651005473066154
@@ -0,0 +1,22 @@
+archive/ES_0.6651005473066154---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T18:09:25.329
+Launch V∞: [5.836205228288034, -8.797597123113215, -2.386544756229195] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.08527655859385341, -0.5240030815032196, 0.5311326603768078] km/s
+ V∞_out: [-0.46980671838573185, -0.4856364884970834, -0.3277141461754176] km/s
+ time of flight: 9.665889545984791e7 seconds
+ arrival date: 2026-05-17T11:51:00.329
+ thrust profile: [0.9046270657355913 -0.6906085420367678 -0.4889073719993689; 0.4065737572362791 -0.10700568366838617 -0.35455837559651; 0.08672209763535192 -0.005168696813606699 -0.11558046913871524; 0.04392674722518173 0.001993742388645361 -0.07294360683892283; 0.04067176605873718 0.006576894648703829 -0.08299222872527877; 0.024048886438986065 0.005060002517687625 -0.055164432532852525; 0.00842062029792434 0.00033284072464405184 -0.01655435038595622; 0.010020154421483459 0.00257080911727047 -0.01799399863436372; 0.005657709809525489 0.0010649594104616177 -0.012574516319196469; 0.01714991663723313 -0.0018480981036454575 -0.0036013476252242313; 0.012458199838654723 -0.017555497517628225 -0.007578982992511186; 0.003555401942838581 -0.0029054997357537203 -0.0013391384015072807; 0.01749220614159125 -0.0022177227557148736 0.0026686252181649106; 0.00031818919328415764 0.003613574593937076 0.004299990990355907; -0.0003134164147049435 -0.00045601522211920415 0.0004494527312477511; -0.007805327722854466 0.007547601854862977 -0.01283407427675087; 0.033705100112302676 -0.01785852944034084 -0.008133473777250865; -0.0049030837239429255 -0.001426375408731386 -0.0003365357862652311; -0.030660683944245967 -0.0014824852582741971 -0.0032081791942621483; -0.01688918091393758 8.59625159061259e-5 0.008181160413319732] %
+
+Mass Used: 92.54879071976711 kg
+Launch C3: 117.15460248079157 km²/s²
+||V∞_in||: 0.7509681909304989 km/s
diff --git a/archive/ES_0.665306564022647 b/archive/ES_0.665306564022647
new file mode 100644
index 0000000..4f69445
--- /dev/null
+++ b/archive/ES_0.665306564022647
@@ -0,0 +1,22 @@
+archive/ES_0.665306564022647---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T02:07:32.220
+Launch V∞: [7.621788255203263, -7.58435960069559, -2.3404059799574313] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.08091482336392639, 0.15874920848991733, -0.17226010947295495] km/s
+ V∞_out: [-0.12839966605015352, 0.14730138843334487, -0.15233786670823257] km/s
+ time of flight: 9.528605466974388e7 seconds
+ arrival date: 2027-05-16T22:28:26.220
+ thrust profile: [0.6164791465298787 -0.3132721166762874 -0.3172225715939027; 0.26507271234508234 -0.02183869244421748 -0.24412800605961074; 0.17447017274702928 0.017688227411769536 -0.23006122448215285; 0.07126824401433274 0.015217193211233784 -0.1265289495261582; 0.0496033307392838 0.014369169545840452 -0.10361580321812149; 0.01794520614849785 0.0060819668599587165 -0.044626128434351355; 0.016086964336544572 0.005502582802267409 -0.042476366376877836; 0.015831580278991838 0.006349084362407895 -0.045115762054211445; 0.0009292824901018221 0.0007595468430304537 -0.0028599595277140778; 0.0008883176658323711 0.0005139356326894567 -0.0015573064501295175; 0.00012783440830025673 -0.00030172886056044216 -0.0022438498018331077; 0.0001235358145578167 4.819345088878416e-5 -0.003536180033680359; 0.00035050305886175136 0.00015970224852570775 -0.0015658116065281995; 0.0003054833753292175 0.00020544154806108425 -0.0006446194829786457; 0.0010416891005074966 0.0017815011120650547 0.0001797394956927305; -0.0009569930505674987 -0.0001994328375560016 0.0006060971074614008; 0.00018714329876724084 -4.06790805408463e-5 -0.0022821959499066385; 0.0016819491545211865 5.403955652451784e-5 -0.0018798302577601013; 0.00032484840977631534 -0.0005416138413519727 -0.0004707848289084891; -0.0023977164974823737 -0.0016196210333574751 0.0005646317056541127] %
+
+Mass Used: 69.82293437986482 kg
+Launch C3: 121.09166691083828 km²/s²
+||V∞_in||: 0.24783475372075053 km/s
diff --git a/archive/ES_0.6654995802845826 b/archive/ES_0.6654995802845826
new file mode 100644
index 0000000..5f0b8d3
--- /dev/null
+++ b/archive/ES_0.6654995802845826
@@ -0,0 +1,22 @@
+archive/ES_0.6654995802845826---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:34:22.947
+Launch V∞: [7.572093144589937, -7.4482025824965445, -2.2974530549287056] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.004781635329135574, 0.025139849954309085, 0.004515278339253271] km/s
+ V∞_out: [0.025097777094849616, -0.004166941846689472, 0.005286750360556579] km/s
+ time of flight: 9.514954833478771e7 seconds
+ arrival date: 2027-05-14T01:00:10.947
+ thrust profile: [0.7922893173235056 -0.39273672955566963 -0.37876582231192535; 0.5403229731634165 -0.03567890460559022 -0.4444543911437099; 0.1747776424328518 0.023434234768652796 -0.21495489863592163; 0.04689683226198498 0.012451665211446186 -0.07954512962927825; 0.03964925169759822 0.01336494980855628 -0.0792542322525956; 0.020806595656258118 0.008571072514835831 -0.04602894152230283; 0.020964242154984776 0.00857100489117167 -0.05014202624931058; 0.001735718161918769 0.0020191449387262283 -0.005539940713279661; 0.0035050567740941094 0.0011743586021658171 -0.007557070904694233; -0.0014002341007889295 -0.0007803750168764137 -0.003711947997690354; 0.0033806076817442083 0.0016309640207108778 -0.010419565604517638; -0.002198964474279464 -0.00010715885842770402 -0.007350927004944146; 0.0030014813635675878 0.00041277699614250193 -0.007381648299059128; 0.0015978725887695593 0.0003948728731898034 -0.0023219226247702326; 0.00034170249492540376 0.0036380342274888212 -0.005726923404975685; -0.0025961034716221964 0.0016459403686984978 -0.0038993661802546485; 0.00013895299916063337 -0.002130817287418974 -0.0040270875474403695; 0.003122834063758936 -0.005367818738743502 -0.008454284204557237; 0.003465196475487067 -0.0009119379352387376 -0.001429370358788944; 0.0005557917180098609 -0.0009187989069735277 -0.0021814735010025777] %
+
+Mass Used: 87.55430376619006 kg
+Launch C3: 118.09060683985535 km²/s²
+||V∞_in||: 0.025985839040272334 km/s
diff --git a/archive/ES_0.6655770387630899 b/archive/ES_0.6655770387630899
new file mode 100644
index 0000000..c7d2d7c
--- /dev/null
+++ b/archive/ES_0.6655770387630899
@@ -0,0 +1,22 @@
+archive/ES_0.6655770387630899---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T12:45:16.989
+Launch V∞: [5.805379216723745, -8.907708665917719, -2.0935704090022367] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.11194135726996539, -0.6748589189344291, 0.6823842895266404] km/s
+ V∞_out: [-0.7047863747546441, -0.5435642061545507, -0.3755834583528572] km/s
+ time of flight: 9.624164979056023e7 seconds
+ arrival date: 2026-05-13T10:32:45.989
+ thrust profile: [0.7792051927474027 -0.609036107802385 -0.42833604892155014; 0.4075257501390936 -0.11812933823850709 -0.3672070672088624; 0.1389905549969532 -0.01108063137939383 -0.1832311780804799; 0.056815678171076994 0.0023460317180544563 -0.09941648787500702; 0.03736137798288472 0.004014297292198691 -0.07719056648394013; 0.012844261985129272 0.0033386540644921234 -0.02724360213708677; 0.06468288049594269 0.01062792005371958 -0.14859354960065763; 0.006420554919766482 0.004250885404610815 -0.02254463326663612; 0.01040385199281195 -0.0006076127515609864 -0.018765661212355553; 0.0008958945467685672 -0.00022308458954972818 -0.005712860918275671; -0.0002799949987686925 -0.0011912551654826966 0.0010244988505023322; 0.0008682335834413679 0.00047932202999440867 0.0018318770780014282; -0.0017394029250587203 0.004445437055358273 -0.0028550713437725224; 0.000577735907962307 -0.0006748393178398721 -0.007474850521861864; -0.00029133022776151344 -0.00023867814500114947 0.003881553838666594; -0.0011629564118882255 0.0016414184137773123 -0.006637772549401476; -0.009736274527183432 0.0039071528927536285 0.008320711986655658; -0.005805430936179622 0.005112768789864261 -0.005570500778934331; -0.004594843163885316 -0.001732387285507929 0.0022120994243218263; -0.01197480384892188 0.0015931880200884038 0.013266188580309106] %
+
+Mass Used: 91.48223681528498 kg
+Launch C3: 117.43273858428343 km²/s²
+||V∞_in||: 0.9662368997950587 km/s
diff --git a/archive/ES_0.6671167918726149 b/archive/ES_0.6671167918726149
new file mode 100644
index 0000000..192b8fe
--- /dev/null
+++ b/archive/ES_0.6671167918726149
@@ -0,0 +1,22 @@
+archive/ES_0.6671167918726149---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T19:48:43.507
+Launch V∞: [7.600782788429937, -7.4192794277667025, -2.283246438921638] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.10540921367301812, -0.10506175804386289, 0.07114154101026632] km/s
+ V∞_out: [0.11801423684134578, -0.08718075290772528, -0.07537346196063699] km/s
+ time of flight: 9.429815042420894e7 seconds
+ arrival date: 2027-05-04T05:44:33.507
+ thrust profile: [1.0 -0.506017474731048 -0.5002116485207526; 0.3443481973981093 -0.024017805049572225 -0.295065058458773; 0.21960163995736226 0.026161086267078137 -0.2650236023341135; 0.10404906614893716 0.024205597973033587 -0.16222881304401598; 0.029458663974630334 0.01102483793448754 -0.058838973956053774; 0.020928671324192693 0.008865819958888433 -0.04896690027362525; 0.008252899211965349 0.003974915666056796 -0.02116689363708909; 0.004867281841722519 0.002148038222299822 -0.013062484462471312; 0.0003553588571240752 0.0003370344575324984 -0.001165862652128229; 0.0008628805109088548 0.00041078107344578297 -0.0024779551606521817; 0.00039381127046567805 -9.837013589777125e-5 -0.0005676355365023915; 6.915924390941806e-5 -6.777195543477204e-5 -0.00011996011610390341; -4.369338424905036e-5 0.0003166005973994679 -0.0008114529638019452; 0.0005718216826052292 0.0004697634975425371 -0.00034549505231916866; 6.266703672376441e-5 1.2306429113308974e-5 -0.00017331528232796553; 0.0006159124385256499 -0.00021023922997819608 -0.0005751996738180103; 0.000511274874292977 -0.00014832129902748198 -0.00012000364648667684; 0.0012757761171417869 0.00030862522733816775 -0.0003559636610833976; 0.0003691322580913744 -0.0005733364294172741 -0.0005609794925465037; 0.0017186392596126871 -0.0015042111518750179 -0.00014530952359697973] %
+
+Mass Used: 89.78980412208148 kg
+Launch C3: 118.0308205250233 km²/s²
+||V∞_in||: 0.16495512780070398 km/s
diff --git a/archive/ES_0.6674311514049295 b/archive/ES_0.6674311514049295
new file mode 100644
index 0000000..b408926
--- /dev/null
+++ b/archive/ES_0.6674311514049295
@@ -0,0 +1,22 @@
+archive/ES_0.6674311514049295---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T23:10:54.324
+Launch V∞: [7.459251623483306, -7.770542690522611, -2.1841988532346206] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0378782143101268, 0.18101858475436572, 0.03224339975535667] km/s
+ V∞_out: [0.18035367709760447, -0.025928679567776045, 0.03896184928314272] km/s
+ time of flight: 9.515879979602243e7 seconds
+ arrival date: 2027-05-17T08:10:53.324
+ thrust profile: [0.7214094852292967 -0.38281263982115404 -0.355108627609654; 0.32569849236103876 -0.054878354794204186 -0.3133588806979828; 0.07710932753758676 0.002948348760733906 -0.1260616545120299; 0.03060740885316534 0.0030864535464228196 -0.06356520392868095; 0.06808223279604533 0.011923889560284702 -0.15881785596004774; 0.030756597913265078 0.005809605110478959 -0.08964710150837518; 0.012993222195204261 0.0027842713054578023 -0.04056287116508138; 0.017959899608751134 0.004193055367808483 -0.054367286477193785; 0.0054541152185365645 0.0010677429392400846 -0.01632277038369108; 0.00010154543666080016 4.132010212143944e-5 -0.00033631841029603397; -0.0001003796146230891 -9.74574477610459e-5 -0.00032905277621836403; 0.00017969239130946287 -0.0001299404096297749 -0.0004444996673055303; 0.00020040942453088215 -6.763194646337259e-5 -0.0007145456705035026; -0.0001886039447047619 -2.0578277359804603e-5 -0.00011930516876094315; 2.080119506457752e-5 0.00014886160853873738 0.00026353613793569035; 7.005077636604665e-5 0.0005349089751847599 -0.00027401820193851626; 0.0003072211329363465 -8.614263318593998e-5 -0.00029287354996094546; -0.0001296336864971712 0.00020994480375698105 -0.00024097874562416832; 0.00019661104725792174 9.797631410798547e-5 -1.0884025731496645e-5; -0.0002889186055169304 -0.00013577231446727686 0.0001398311965407825] %
+
+Mass Used: 74.04680011657683 kg
+Launch C3: 120.79249311814415 km²/s²
+||V∞_in||: 0.1877288575940873 km/s
diff --git a/archive/ES_0.6676127631490584 b/archive/ES_0.6676127631490584
new file mode 100644
index 0000000..cc4e563
--- /dev/null
+++ b/archive/ES_0.6676127631490584
@@ -0,0 +1,22 @@
+archive/ES_0.6676127631490584---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T22:59:56.138
+Launch V∞: [7.359210823827814, -7.493717827815998, -2.781025124259328] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.028352514048435907, -0.04536361513486961, -0.018764324120862964] km/s
+ V∞_out: [-0.03032471481753998, 0.041298237921821856, -0.024282404168795485] km/s
+ time of flight: 1.0498984869643213e8 seconds
+ arrival date: 2027-09-05T02:50:44.138
+ thrust profile: [0.2615329673361639 -0.13603849703840595 -0.13900509326852678; 0.20110222861825594 -0.013541237302479997 -0.20524728357375835; 0.1239959729898584 0.016258732885068683 -0.19173649525750697; 0.08035921344255618 0.021185559257310773 -0.16286268081217697; 0.05208449979267978 0.019083292818129406 -0.13032195967693797; 0.029480773074306795 0.013744203311895593 -0.09051399394440415; 0.009768485690414637 0.006543707338834708 -0.04369310222758016; -0.00826470900911358 -0.0014253511111221172 0.007355233474051075; -0.008879234232893544 0.00910277563930344 -0.03446389183858917; 0.08050970971021328 -0.034411442483372516 0.002509329052367058; -0.008701304138865017 -0.024051168042018213 0.014513059550162136; -0.06661665394372149 0.06345803674213771 0.0065543337216942546; -0.0656054660039855 0.06029691833214891 0.00417934949612556; -0.029480718011006705 -0.001128342169487034 0.05090979707253607; 0.003192080963917111 4.015624354138884e-5 -0.0042258024264141755; -0.04557422991620714 0.025086869288824778 0.10390336618780187; 0.015107466612313249 -0.006717005346098485 -0.0255627485777419; -0.03277364324843331 -0.009134817782233911 0.08876816648468942; 0.02304589945207594 -0.06855789389008657 -0.047136224973786084; 0.0575890068518686 0.0009822608026164217 -0.09642134306362961] %
+
+Mass Used: 90.26885615754009 kg
+Launch C3: 118.04789157423338 km²/s²
+||V∞_in||: 0.05669058555601739 km/s
diff --git a/archive/ES_0.6683041800691364 b/archive/ES_0.6683041800691364
new file mode 100644
index 0000000..a85e6aa
--- /dev/null
+++ b/archive/ES_0.6683041800691364
@@ -0,0 +1,22 @@
+archive/ES_0.6683041800691364---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T00:23:08.357
+Launch V∞: [7.8213093638481395, -7.263676867940388, -2.437863393145155] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.11650033946876298, -0.11763780353552382, 0.07900852160116434] km/s
+ V∞_out: [0.13320763072356315, -0.09546986825544927, -0.08258547241201748] km/s
+ time of flight: 9.527594242512456e7 seconds
+ arrival date: 2027-05-13T17:55:30.357
+ thrust profile: [0.7312949201711165 -0.36732312268839246 -0.3810160194134106; 0.35129203517499996 -0.015956580712453382 -0.3262698585429409; 0.16210030336460501 0.026719928311081678 -0.21377046451042636; 0.10671546830283836 0.030771626318543296 -0.17993145460170276; 0.02948439324690372 0.010952496435461541 -0.05950423470820045; 0.02547025264529493 0.010838258667784 -0.058098910643195806; 0.011629135295207656 0.005329894768230812 -0.029067887173745113; 0.01851591077070908 0.009745547280940346 -0.050107213835418836; 0.0019939708232403317 0.0004471859874887955 -0.004167168094112242; 0.002067348594350748 0.0012721240024557029 -0.004749368886982595; -0.0006674147592417097 -0.0008452108614533794 -0.0008081289723038379; 0.0010474751270672354 0.00042435220677098664 -0.002788470666081754; 0.00012099558873658264 0.0001628924821036629 -0.00023141504229320952; 0.0015366825866338677 0.00048353244971657827 -0.0020285121047162466; -0.0006368490523913062 0.0001914563781432409 -0.0025376538834222333; 0.0010833423559757588 -0.0004764250592137336 -0.001325639876568827; 0.0007571883018343749 0.003853126660253497 -0.0023349842653989992; -0.0011003842049056747 0.0012419793161967682 1.1089375660324505e-5; -0.0021487947427134436 0.0029932250361114393 -0.00150137729124354; -0.003410929277159933 0.003989552688562544 0.003597200240515734] %
+
+Mass Used: 80.40536165269532 kg
+Launch C3: 119.8770597305081 km²/s²
+||V∞_in||: 0.18344843526888194 km/s
diff --git a/archive/ES_0.6683317278288022 b/archive/ES_0.6683317278288022
new file mode 100644
index 0000000..79e9f0c
--- /dev/null
+++ b/archive/ES_0.6683317278288022
@@ -0,0 +1,22 @@
+archive/ES_0.6683317278288022---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T07:04:40.184
+Launch V∞: [7.573337532911851, -7.6702713317713025, -2.408589611736309] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.1597164629814274, 0.30733890069547226, -0.3681389392529205] km/s
+ V∞_out: [-0.25666978917372507, 0.3053698143781674, -0.3104366601131742] km/s
+ time of flight: 9.442760670604034e7 seconds
+ arrival date: 2027-05-08T04:58:06.184
+ thrust profile: [0.7846441439196509 -0.41603461361010063 -0.41116435209961566; 0.19465812706582547 -0.019433904596410347 -0.1923404436747782; 0.13588575079821694 0.010838181551778929 -0.18874690123406773; 0.03127445837718624 0.005376194817561606 -0.05878611143227603; 0.05853975349555991 0.013251002820178746 -0.12501911378974964; 0.01583878999280459 0.0046253138053868525 -0.03979505109585106; 0.005885848926385981 0.0017902936441198324 -0.016307144377159098; 0.002799300572415473 0.0007820282310007946 -0.008121085811208704; 0.005187139030182559 0.0016794876448341604 -0.016326621487878355; 0.0013179790356450615 0.000455797539736558 -0.004187164003325124; 0.0003632720685826866 -0.0011182623256530495 -0.0005668572993803077; 0.0004900239832776733 -3.088777822744327e-5 -0.002541632707521746; 0.0006228564096817242 0.0004209580793683099 -0.00013371040068093677; -0.0007108072445048009 -0.0003322807316626672 -0.002913800938422915; 0.0019141854147174421 -0.001027454176399011 0.002242221303490501; -0.002173724410479974 0.0003955621686223485 -0.0002327590250306354; -0.00222726806396506 -0.0016740911252867705 -0.0004204952316010375; 0.00166880548644023 -0.002206756066592668 -0.0038462397652423833; 0.0020881172286119926 0.0012034086960932206 0.001844121443071744; -0.004497700611921583 -0.0011802314001926975 -0.003483717819247189] %
+
+Mass Used: 68.11313808595514 kg
+Launch C3: 121.98980760816814 km²/s²
+||V∞_in||: 0.5054629828407462 km/s
diff --git a/archive/ES_0.6683648672952885 b/archive/ES_0.6683648672952885
new file mode 100644
index 0000000..3a78733
--- /dev/null
+++ b/archive/ES_0.6683648672952885
@@ -0,0 +1,22 @@
+archive/ES_0.6683648672952885---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T19:59:59.373
+Launch V∞: [5.988296626448164, -8.975142897232814, -2.4246670666064882] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0019228430134693995, 0.0009694589815097379, 0.0020045098662270847] km/s
+ V∞_out: [-0.0009242893519641091, 0.0019727501618984895, -0.0019769836712157226] km/s
+ time of flight: 9.589292991855013e7 seconds
+ arrival date: 2026-05-09T16:55:28.373
+ thrust profile: [0.4868186217595121 -0.398685880883744 -0.2753263644221887; 0.31514503303165786 -0.09043377438234629 -0.2660848471221104; 0.09956096762161003 -0.00942522106024 -0.12506508585417417; 0.027630187940019653 0.001587501234550543 -0.04384855386065674; 0.021888515834866718 0.0025911758731942914 -0.040158684751002004; 0.02201065651529536 0.0036538524334563637 -0.04112827919991203; 0.01839973779874327 0.005136490435910041 -0.03903497074333639; 0.08546903488518931 0.01117961409953839 -0.17516842000615662; 0.0031642350995992265 0.001439861634123095 -0.008362333378969208; 0.002672794695790305 0.0018692938221789464 -0.0063728367133893404; 0.0002031102059233213 0.0004626319549466848 0.0002736724350381328; -0.000600974254300764 -0.0008852578898481578 -0.0014250452737733512; -0.0010964228941604036 -0.0005898192262435279 0.001892218450521413; 0.008203955075616626 -0.009879681563864838 -0.014136485081859508; -0.0037707074083035176 -1.846777243262841e-5 -0.002499977519119151; 0.006494058709496856 -0.006338228546652312 0.0023240401988231744; 0.009616045023570266 0.009341911972411486 -0.0027140650555370644; -4.75025950727992e-5 0.0021288202078945323 -0.0010486009010772948; 0.0039346532306314165 -0.0002308109877574799 1.989693112372569e-5; 0.0025322138681684783 -0.002601900363940292 0.011970958640298263] %
+
+Mass Used: 66.38961328470623 kg
+Launch C3: 122.29189689596521 km²/s²
+||V∞_in||: 0.0029419782077846368 km/s
diff --git a/archive/ES_0.6692336758593997 b/archive/ES_0.6692336758593997
new file mode 100644
index 0000000..4870b83
--- /dev/null
+++ b/archive/ES_0.6692336758593997
@@ -0,0 +1,22 @@
+archive/ES_0.6692336758593997---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T16:24:19.438
+Launch V∞: [7.53251291756622, -7.869311110598882, -2.497390384257352] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0034762811877161437, -0.003223286747511386, 0.002023200785870401] km/s
+ V∞_out: [0.00393405949507229, -0.002431944267374938, -0.00243662747455983] km/s
+ time of flight: 9.555602048963378e7 seconds
+ arrival date: 2027-05-22T15:44:39.438
+ thrust profile: [0.42803369630091337 -0.2151234955598955 -0.22675983920792014; 0.21884454462297492 -0.02775939552593178 -0.22316336896486405; 0.10492078576455588 0.004598055696695316 -0.16136887606585446; 0.03378055883596207 0.004340467080158175 -0.07252105745415921; 0.016653061495051327 0.0023494243238388656 -0.04128077872983874; 0.013320497413447596 0.0027101788241385314 -0.0432797794501818; 0.015033119833981645 0.003160399978144726 -0.04919605573584847; 0.0021613005757183616 0.0005810468665027066 -0.009976896138791139; 0.002512390477356355 0.00031453415442315243 -0.012152051960723397; 0.001550948966044431 0.0008264826023964977 0.0012710757170094145; -0.0007230949613136222 -0.005964670407275727 -0.0026135229267951424; -0.0015573288794014815 -0.002206189503556296 0.0034891737597012784; 0.005867012823213377 -0.0011614202316155265 -0.000886600663563771; -0.0018317577012601366 0.0023650870194781705 0.0038465919102793934; 0.003387059533780057 -0.004201004626928925 -0.0021501228444339637; 0.006103625849134848 0.011057525505558746 -0.001642294931253627; -0.006695299230179379 0.011978037616109013 -0.005650646910679554; 0.00872038004229478 0.0038031802991602805 0.003028724981898118; -0.0028972316650747953 0.0002921102722022274 0.012741735569420532; 0.000982616782177019 0.004106432217860573 -0.009371815025172939] %
+
+Mass Used: 52.17898135217774 kg
+Launch C3: 124.90176694007805 km²/s²
+||V∞_in||: 0.005154362208139655 km/s
diff --git a/archive/ES_0.6694575882686058 b/archive/ES_0.6694575882686058
new file mode 100644
index 0000000..3d7f4db
--- /dev/null
+++ b/archive/ES_0.6694575882686058
@@ -0,0 +1,22 @@
+archive/ES_0.6694575882686058---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T10:36:33.519
+Launch V∞: [7.657426248972643, -7.629616629727228, -2.3133107766407783] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.021686018178533988, 0.1097267880575028, 0.02065655298079977] km/s
+ V∞_out: [0.11014829851504394, -0.01591557711166781, 0.023204305203668053] km/s
+ time of flight: 9.470487717562015e7 seconds
+ arrival date: 2027-05-10T13:31:10.519
+ thrust profile: [0.48983083170313146 -0.2403978552231064 -0.26160395444731976; 0.387170481900026 -0.043932861098041294 -0.38615562965406663; 0.15398731605206445 0.009401046264050264 -0.21336224766960551; 0.07737221431458419 0.012458892186618508 -0.13095629792017383; 0.04177912534641096 0.009184767987690077 -0.08003105339619705; 0.003172396881836686 0.00017961384948346135 -0.010665724975672565; 0.004098890099379441 -0.0013343584996533603 -0.009343334817754977; 0.007171272255752464 -0.002455358628587847 -0.02564033692453597; -7.427533601706698e-5 0.0021593658909697597 -0.006946840246827419; 4.1883385153009683e-5 0.003046352175530823 -0.004217566571816017; -6.974443119919099e-6 0.006267574641808159 -0.024486324789961458; -0.0002517223698847073 0.00024606513049010544 -0.0057349006947302605; 0.0008791061404703673 -0.0003749613500903144 -0.00443311994528544; 0.0014226317723305465 0.0005396391722137877 -0.003064829528875929; 0.005008296630902627 -0.008292208072797217 -0.000993987148100928; 0.010132027942623962 -0.003227166522065601 -0.006330446265654515; 0.0045444262901408565 -0.0013548729358309457 6.087970830463002e-5; 0.0011759968719707772 0.0006168231978770928 -0.0061155683131687445; -0.004927513192856105 0.002446790722026205 0.003179468451374963; 0.0006864738685558575 0.0018431047426161365 0.009090072294627528] %
+
+Mass Used: 68.20849133777756 kg
+Launch C3: 122.19863342438786 km²/s²
+||V∞_in||: 0.113740690093319 km/s
diff --git a/archive/ES_0.6694881101706576 b/archive/ES_0.6694881101706576
new file mode 100644
index 0000000..7fa575d
--- /dev/null
+++ b/archive/ES_0.6694881101706576
@@ -0,0 +1,22 @@
+archive/ES_0.6694881101706576---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T09:56:45.205
+Launch V∞: [7.646358329692367, -7.29018423786219, -2.380411060389357] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.770406457531261, -0.7189805043150448, -0.0836845377708538] km/s
+ V∞_out: [0.5683330826533646, -0.6517212586247569, 0.6079763431255092] km/s
+ time of flight: 9.444674992517969e7 seconds
+ arrival date: 2027-05-04T13:09:14.205
+ thrust profile: [0.9999999076236376 -0.49169242563472787 -0.4649057071860396; 0.5553336799910898 -0.02409046866393314 -0.4285234257670401; 0.2038704075095927 0.03528401747056637 -0.2337611755915886; 0.0344401319319433 0.011681880042150055 -0.05444727240302612; 0.06280600986132266 0.024403068990845676 -0.11362947833318945; 0.01977208429710149 0.009359586137789224 -0.042894977059703125; 0.0070730434682717384 0.001959806860025686 -0.014353976486190368; 0.007439808277445101 0.0044624222512158924 -0.019809226564254857; 0.006415239100089797 0.002698007840652202 -0.014494775482700362; -0.0029708427691395867 -0.002372713214905166 -0.0013266719766997178; 0.0016940666582448312 -0.0048434500826096275 -0.0010022618457551568; -0.00209612418635885 0.0011844793824341549 -0.0005802501521073406; 0.0009307542232494876 0.0006440046087749159 0.0008966585742883493; -0.001032220351607395 -0.0014811645633272998 0.003466777087039066; 0.0026056169195341383 0.004906226401678351 0.0009246856031615257; -0.004436115527413848 -0.0009028477078545172 0.0018929569871128718; -0.0008533274241588554 0.0018047864084751244 -0.0031637029223579595; 0.009863477946776543 -0.0037487643522587004 -0.0002822133550775753; 0.010375852269558564 0.003299907417458624 -0.004231116994819394; 8.85422189353943e-5 0.0005050520913952013 -0.0028899220145131455] %
+
+Mass Used: 96.93648585645133 kg
+Launch C3: 117.27993874445414 km²/s²
+||V∞_in||: 1.0571008358964173 km/s
diff --git a/archive/ES_0.6696923477614585 b/archive/ES_0.6696923477614585
new file mode 100644
index 0000000..365fa10
--- /dev/null
+++ b/archive/ES_0.6696923477614585
@@ -0,0 +1,22 @@
+archive/ES_0.6696923477614585---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T18:44:02.318
+Launch V∞: [7.583811660163614, -7.706650578457614, -2.462416429426745] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0030876283741168966, -0.005229278068620744, -0.003949131149089705] km/s
+ V∞_out: [-0.005463490570581773, 0.004246052650548182, 0.002347436320238731] km/s
+ time of flight: 9.402451525980811e7 seconds
+ arrival date: 2027-05-04T00:39:17.318
+ thrust profile: [0.8106597443645702 -0.4305512784295305 -0.4300865868389702; 0.18118733622935757 -0.020253603987889033 -0.19127633155692586; 0.07701526159025501 0.003895714711494078 -0.11974070968690255; 0.048126722678751656 0.0068074796276182065 -0.09521137683321791; 0.030736453509792136 0.005932557713185148 -0.07223475173849613; 0.0093193913517406 0.0023209626405176625 -0.025611463630545655; 0.008907490780517556 0.0023558223599841597 -0.026055740275880437; 0.007840777258275167 0.0023890140516866225 -0.026149682140141513; 0.00022385253386855545 0.000769622082565336 -0.0018337152503925924; 0.00023263969310529425 -0.00020453997976681526 -0.0011213375199022352; 0.00030903883042707496 2.432368932272339e-5 -0.0005231142667538078; -0.00012867079395618826 -8.036852881477405e-5 0.0008763037889833981; -0.0006306236630832361 -0.0016945841846265563 0.0012716503345400333; 0.00018073607000452342 -0.001668774105287087 0.0002511915733105359; 0.0004571963723119831 0.00017135377522563896 -0.00038266075978207; 0.0004050381857089129 -0.00027273910130244585 -0.0007424032653618127; 0.0002825871931506315 -2.374543560648419e-5 -0.0020085971584669323; -0.0016943580464145484 0.002538582881081843 -0.0020913219726350165; 0.00014540558629663416 0.0003214337464834331 -0.002473631995426538; 0.0012861628386367486 0.0009469354817379678 -0.0016132681261586015] %
+
+Mass Used: 63.981822596453185 kg
+Launch C3: 122.97015710718544 km²/s²
+||V∞_in||: 0.007243924000727798 km/s
diff --git a/archive/ES_0.6705575961214509 b/archive/ES_0.6705575961214509
new file mode 100644
index 0000000..dc150ae
--- /dev/null
+++ b/archive/ES_0.6705575961214509
@@ -0,0 +1,22 @@
+archive/ES_0.6705575961214509---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T05:38:47.087
+Launch V∞: [7.560614983127217, -7.557808386007004, -2.214162639520625] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.21093866507972175, 0.2046887122218564, -0.16307450477077012] km/s
+ V∞_out: [-0.14495751607342336, 0.2976011472431496, -0.05813750402311813] km/s
+ time of flight: 9.424380140163589e7 seconds
+ arrival date: 2027-05-05T00:28:48.087
+ thrust profile: [0.9893717385274212 -0.5064560804435617 -0.47682116142304126; 0.18940280483390523 -0.016241826841319477 -0.1753708941740848; 0.14513267274556457 0.013598120372960253 -0.18520161725395426; 0.10603003955073569 0.019621436397764376 -0.1723326661164778; 0.05390224537127673 0.012713214003279405 -0.10605298815829871; 0.05261071259466591 0.014688890483875679 -0.1103821299219412; 0.01213073095313923 0.0037141836040031667 -0.030327409935761326; 0.010737361171025122 -0.009072179424303682 -0.015995640597332245; 0.004890614505952797 0.001742964481238887 -0.016183811481489795; 0.0030008803572414058 0.0013028320389240023 -0.009282860928049974; 0.0030318139266229662 -0.0013617279777868403 -0.005841638639300978; 0.004788461007952405 0.0038532193736634185 -0.00636011821062705; 0.0021512435651312844 0.004938177678971964 -0.007488252916709119; 0.00452776532752538 -0.001161086159877054 -0.011218798217543062; 0.0023134301629533075 -0.0022362216710191327 0.0024499655986538037; 0.0020457948876597977 0.00012388645070971594 -0.004922525558862623; 0.00861365131238568 0.0030729403074860584 0.0016109389881805575; 0.0008190053150150209 -0.0015256650002031529 -0.006089659331096505; -0.017550674085862788 0.007599437013184508 -0.0027432637468143162; -0.001162191465316969 -0.00260119920220743 -0.007468943629764111] %
+
+Mass Used: 87.06621295957484 kg
+Launch C3: 119.1858827169345 km²/s²
+||V∞_in||: 0.3361337285112711 km/s
diff --git a/archive/ES_0.6706246448529066 b/archive/ES_0.6706246448529066
new file mode 100644
index 0000000..326eaa5
--- /dev/null
+++ b/archive/ES_0.6706246448529066
@@ -0,0 +1,22 @@
+archive/ES_0.6706246448529066---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T01:13:49.537
+Launch V∞: [7.561531303351862, -7.613574285697982, -2.398681059546541] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.11960413110451108, 0.23650055982860718, -0.2956935826831073] km/s
+ V∞_out: [-0.20690600388974878, 0.245756936101976, -0.2334577823396604] km/s
+ time of flight: 9.343062915989152e7 seconds
+ arrival date: 2027-04-26T10:10:58.537
+ thrust profile: [0.9999932785025054 -0.522544602208734 -0.4928859756961482; 0.3304890931795283 -0.03482108074069687 -0.30594744848773203; 0.05813222858227802 0.005272286268952939 -0.08537290543380771; 0.04322881528430029 0.008341997491255937 -0.08015234406151656; 0.034050501769421336 0.008642670815693483 -0.0743541479955501; 0.008916880884420698 0.00282528073090198 -0.02384294557766033; 0.01240305422944762 0.004144765241825118 -0.036019546449681444; 0.007238144641812918 0.0024719819183083988 -0.021703069162770424; -1.3803583802318774e-5 -0.0001764787892558395 0.00027680108600745335; 0.004146243589336356 0.001107675517536273 -0.015054322237407635; -0.0008970337663192306 -0.0004056843715532151 0.0008333458119365215; 0.00028064833706788845 -0.0006138590118953062 -0.0004406784615683302; -3.769109239444373e-5 0.00013727898693082028 -2.4959914837721165e-5; -0.0006822716978209143 0.00015878181249450772 -0.0003607549474406275; -0.00022672409971464757 -0.0002364659764000662 -0.00016625557981838536; 0.0005695139597086195 0.0016247370005985477 0.0018935362066237079; 0.00032856822888539133 -0.0010205166684849193 0.0006229607298386059; 0.00013568782056773513 0.00044338728257200226 0.0005614717348211715; -0.0012743169505750912 3.92069888509388e-5 -0.0005197703027493366; 0.0013413064135947789 -0.0010533275587836883 0.0006257257686541023] %
+
+Mass Used: 77.16326969016382 kg
+Launch C3: 120.89693988083897 km²/s²
+||V∞_in||: 0.39707978772090796 km/s
diff --git a/archive/ES_0.6717223858461665 b/archive/ES_0.6717223858461665
new file mode 100644
index 0000000..078664e
--- /dev/null
+++ b/archive/ES_0.6717223858461665
@@ -0,0 +1,22 @@
+archive/ES_0.6717223858461665---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-13T07:19:29.062
+Launch V∞: [7.4046677262502785, -8.076846095540024, -2.5193114432821386] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.17032034602964577, 0.14380714632251382, 0.016650422180777003] km/s
+ V∞_out: [-0.03900886773073375, -0.21563031734953936, -0.040579920399455974] km/s
+ time of flight: 9.58951056610946e7 seconds
+ arrival date: 2027-05-28T04:51:14.062
+ thrust profile: [0.4177820440141873 -0.1664017465337469 -0.2078680833427188; 0.1976089841974758 -0.02348264340567862 -0.18240469205570814; 0.08412165405639835 -0.0030898395254148957 -0.14661956288710012; 0.03644200091769154 -0.00018243897611085387 -0.08551805603037697; 0.021307944300180504 -1.414781063469473e-6 -0.059474092350539125; 0.005278748434057946 -0.00034758990296222467 -0.015978755679864867; 0.003054795616748038 0.0008219245862545132 -0.0023398505707102344; 0.0025531878914338826 0.0024016166333183137 -0.000965310827560523; 0.0011029384856984727 0.0015160150773808167 -0.0034889758364873716; -0.0002934921221558152 -0.0029922198765924817 -0.001054074612662409; -0.0014827227263662377 -0.003754934002024035 -3.6684786444864895e-5; 0.011975162410430517 -0.0005114667840577835 -0.0005407455981847244; 0.006990191820514148 0.006561143899011768 -0.003088848203041751; 0.014675469962160027 0.001532759039576333 0.000501602998889232; 0.0018504716632142134 -0.0006050508767920671 -0.00033542957546083343; -0.002894322285408356 -0.004090831227485171 0.0012841551355279104; -0.0027601724043898167 -0.0027386178891913885 -0.007970419675441782; 0.0011923044940241783 0.0011815171250702371 0.00660809739676514; 0.014108626935138901 0.0019591332766154407 -0.013862045213105838; 0.003979252643697945 -0.00023693278054990957 -0.0047481257942608825] %
+
+Mass Used: 46.275833530315595 kg
+Launch C3: 126.41147713546492 km²/s²
+||V∞_in||: 0.22353244096524622 km/s
diff --git a/archive/ES_0.6718035175190289 b/archive/ES_0.6718035175190289
new file mode 100644
index 0000000..9edd075
--- /dev/null
+++ b/archive/ES_0.6718035175190289
@@ -0,0 +1,22 @@
+archive/ES_0.6718035175190289---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T13:17:53.543
+Launch V∞: [7.680781843521841, -7.632550557727022, -2.2569028578471406] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0003204767386880717, -0.0038252970788065347, 0.0010003739829549914] km/s
+ V∞_out: [0.0011204318689280017, 0.002697811404516959, 0.002665971370501911] km/s
+ time of flight: 9.425717169185059e7 seconds
+ arrival date: 2027-05-05T11:50:44.543
+ thrust profile: [0.6234777066707646 -0.3210833351965195 -0.29280217847310885; 0.13669745655967372 -0.011148940458304871 -0.1323851257106734; 0.14818552053826245 0.016098112027726107 -0.19679885428957603; 0.13938325854494282 0.02598857174269254 -0.22690946851025076; 0.0879666876600223 0.023430480736935256 -0.1749841171569339; 0.030385877782045122 0.009133404990003672 -0.06998796045098951; 0.022478640638192184 0.00715618174967093 -0.05669969647796397; 0.004224496534106505 0.0015012879949569508 -0.001521603048226383; 0.0011204444045307604 -0.0007817354127887259 -0.0012484172115697595; 0.0038175010107771015 0.0006521929220429811 -0.0004254024839833422; 0.0017012968310776873 0.0025811210190704037 -0.0004117753565886064; 0.0011991080029918064 0.00018364290249135582 -0.0042676503396011775; 0.001170069072533707 -0.004450794307063617 -0.0014909830560115092; -0.002990877712537569 -0.006214900276013269 -0.0066908190635480294; 0.00844191195433511 0.0007204213371921055 -0.007141099120530866; -0.002896094811364389 -0.008008935354943016 -0.0047149937989341; -0.001682958594291844 -0.003701426382975907 0.0017756390957630978; -0.0007551987484919667 0.004913429180925925 -0.0012595184483674858; 0.00023473395537640385 4.4129845129440914e-5 -0.0009451732485610187; -0.00104129168708691 0.0017736045368253557 -0.002589149831164433] %
+
+Mass Used: 70.09832229174435 kg
+Launch C3: 122.34384825379244 km²/s²
+||V∞_in||: 0.003966907005078286 km/s
diff --git a/archive/ES_0.6720975635710669 b/archive/ES_0.6720975635710669
new file mode 100644
index 0000000..98ce51d
--- /dev/null
+++ b/archive/ES_0.6720975635710669
@@ -0,0 +1,22 @@
+archive/ES_0.6720975635710669---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T14:40:43.689
+Launch V∞: [5.866462240876077, -9.02176933253182, -2.1277198359269094] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.41144278376560656, -0.39531607083338544, 0.016543177597892932] km/s
+ V∞_out: [0.09491785347395285, -0.002759981594965546, -0.7181714069564776] km/s
+ time of flight: 9.48715032193274e7 seconds
+ arrival date: 2026-04-28T15:52:26.689
+ thrust profile: [0.6889843165416567 -0.5609522533067414 -0.3957960002245784; 0.3480338422266496 -0.10629935164220977 -0.3237518632234372; 0.12877340135701673 -0.014166612706727626 -0.1724849123342844; 0.04885184271507626 -0.00031082932397052433 -0.08592205257602382; 0.02581245706206156 0.0014932006034167422 -0.054595070150406884; 0.01910102266365795 0.0015539786789197318 -0.04437758811094437; 0.036651761977323116 0.007240362801877688 -0.09123834396744217; 0.031170091865418366 0.005627989968103862 -0.08205256477907871; 0.0013427825034808129 0.005250568176284023 -0.004792120897248216; 0.0077528871935742556 -0.0039165873042008754 -0.0020298358572267304; 0.0020970354442145143 0.0016676443625742467 0.0004825051494541572; -4.471540186892428e-5 0.0015892298510522406 -0.007110741029253795; -0.0010475732939696737 0.015887976217647117 -0.0058192580120559065; 0.002626545773429294 -0.002961005843070508 0.003948366683123778; 0.0087886679758378 -0.010718984501743927 -0.01428418637702979; -0.004500372390219115 0.0015847748331114303 -0.0038308014292276473; 0.00798462073567681 -0.0007114953182737647 0.006039982726942368; -0.0013537655112934128 -0.001776222011936383 0.0002983680647529177; -0.005925281902902743 0.008185193583031092 0.010956322407028589; -0.002201209291544502 -0.0020147455892957416 -0.001617509184202244] %
+
+Mass Used: 82.16028275571762 kg
+Launch C3: 120.33489281323322 km²/s²
+||V∞_in||: 0.5708183922203044 km/s
diff --git a/archive/ES_0.6727626108755769 b/archive/ES_0.6727626108755769
new file mode 100644
index 0000000..5030c73
--- /dev/null
+++ b/archive/ES_0.6727626108755769
@@ -0,0 +1,22 @@
+archive/ES_0.6727626108755769---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T08:29:21.270
+Launch V∞: [7.81579973703683, -7.693997960140088, -2.6977921724076266] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.20470014155410196, 0.20440927484591398, -0.1380992613306135] km/s
+ V∞_out: [-0.23743600394518824, 0.1688617361987297, 0.1338108948868813] km/s
+ time of flight: 9.41504990233068e7 seconds
+ arrival date: 2027-05-05T01:24:20.270
+ thrust profile: [0.34690827048572254 -0.17477018434009062 -0.19658969317506508; 0.1285318268246258 -0.01029722874067681 -0.13439396309658833; 0.039711139263950146 0.003072171941173003 -0.06270826755415314; 0.05891108895254826 0.010501641259765205 -0.10272352892276303; 0.03221446881897914 0.008149355065026882 -0.0710053904318954; 0.016224510402578603 0.005054796741856791 -0.04381515474974622; 0.009106208689241573 0.0030634790129094236 -0.027292615043271233; 0.010582823327003546 0.0044368056387643455 -0.03886185104313201; 0.004595509598392843 0.000623514009894611 -0.01839505531215575; -0.00016917915692098683 0.003487942694410436 -0.005830508303700595; 0.0011368661790676568 -0.0004862042642024405 -0.001545776658939256; 0.00022341903594098747 -0.0011776563048698106 0.003226847919884426; -0.0005437669596156775 8.9623071651473e-5 -0.0014782007662771674; -0.005995167499439611 -0.001060657710628346 0.005930114315954474; -0.0005428445271290288 -0.005783900616085041 -0.0014249855054209188; -0.0012478943129358246 0.002160910134134466 0.0027599060701569036; -0.0018611168980472203 -0.00011682240704269172 0.007947982442020968; 6.406823578729813e-5 -0.00025010430030414593 -0.0052237493293927195; 0.006003613012109772 -0.007004489109575486 -0.005495800623629651; 0.0022760932734135404 0.00011628861653646043 0.001828477107231643] %
+
+Mass Used: 40.77563833878912 kg
+Launch C3: 127.56241274560867 km²/s²
+||V∞_in||: 0.32055686792730376 km/s
diff --git a/archive/ES_0.6729109438046279 b/archive/ES_0.6729109438046279
new file mode 100644
index 0000000..cf89232
--- /dev/null
+++ b/archive/ES_0.6729109438046279
@@ -0,0 +1,22 @@
+archive/ES_0.6729109438046279---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T23:05:06.158
+Launch V∞: [7.614150414703965, -7.406196151839542, -2.314126205906104] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.08295960967248947, -0.23701205634778202, 0.7661850513374869] km/s
+ V∞_out: [0.23050158323128725, 0.3292662800226312, -0.6991891552707392] km/s
+ time of flight: 9.442454689813998e7 seconds
+ arrival date: 2027-05-05T20:07:32.158
+ thrust profile: [1.0 -0.5584838785462728 -0.5561076397069064; 0.38654479384338386 -0.0206511816182778 -0.3412621554378154; 0.11566871333615869 0.016508149652944858 -0.15183754694430415; 0.06153821430217332 0.01492029375145292 -0.10378735747179553; 0.01433703283982856 0.003446211630276431 -0.03624939367140665; 0.004169538002886893 0.0006215723539403156 -0.008451376405619935; 0.022214785651730677 0.008894854583462073 -0.05621696075749167; 0.029635467455898956 0.009524041526761593 -0.0749922837614385; 0.007087490688884446 0.004980777120738015 -0.028484368183048454; 0.0010788601420167003 -1.598205207019223e-5 -0.008433703400547471; 0.011807720291888974 0.005088142651735701 -0.03682402940346722; 0.0002674433906301012 -0.00349002268789317 3.550404488166653e-7; 0.005393073565045681 0.0013981592748761643 -0.010088038639220873; 0.0265475193094293 0.004336747758083745 0.018375395878211947; 0.0024090355824494033 -0.0011082137323976634 -0.0008848547823897671; 0.0014481742188776929 -0.008827968814390783 -0.000619867297158354; -0.013248344696601942 0.011391146130748795 0.004078326128943804; 0.021025988483610043 0.003664629768979068 0.021242689367981422; -0.02393312814296323 -0.00879291794920206 0.006305090180253919; -0.025946542336503328 -0.007240403834371731 0.02970003658876142] %
+
+Mass Used: 95.66655400636137 kg
+Launch C3: 118.18220807412078 km²/s²
+||V∞_in||: 0.8062856470161449 km/s
diff --git a/archive/ES_0.6733538593181823 b/archive/ES_0.6733538593181823
new file mode 100644
index 0000000..fef1df2
--- /dev/null
+++ b/archive/ES_0.6733538593181823
@@ -0,0 +1,22 @@
+archive/ES_0.6733538593181823---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T00:22:06.528
+Launch V∞: [6.080208184161847, -8.96965295809641, -2.4366693363582135] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0024714744598132925, 0.0013138490158394005, 0.0025854286769126426] km/s
+ V∞_out: [-0.001232354207456028, 0.002581500718672633, -0.0025168434859120462] km/s
+ time of flight: 9.381781238643846e7 seconds
+ arrival date: 2026-04-15T20:52:18.528
+ thrust profile: [0.682372547382676 -0.5387547942354074 -0.36304296611926234; 0.25186050720341535 -0.06838730036907337 -0.2242556332915564; 0.0795449367835255 -0.005646748090427428 -0.10225796156118193; 0.06644616441857368 0.002689759181354675 -0.10429752817619402; 0.04203898020352377 0.004334578213772547 -0.07698561142398899; 0.017380191908672054 0.0029156421680470324 -0.03622633828469289; 0.018619196428494182 0.0024036497249933435 -0.042932629889142336; 0.011591860742585933 0.002338624513717791 -0.025498850631466577; 0.006300537477842123 0.0004770962060025901 -0.015924751371575636; 0.0007310148125748527 0.00011876874275950603 -0.0018010948963946957; 0.0001685514179077583 1.55772360221413e-5 -0.00043637371714516464; 0.0002602241931152784 0.00041512466315154453 -0.0008310412495031744; 2.071186016179029e-5 1.4611873249656138e-5 -0.0007025169866656767; 9.856460343198091e-5 1.8315755879970256e-5 -5.9476099538126965e-5; 0.00013801319001896344 3.433702957063582e-5 -0.0003330036139408814; 9.038295300845805e-5 -1.8528597509653974e-5 -0.00029044201734187703; 3.978532255942627e-5 1.810182073146501e-5 -0.0006190971040692845; 4.317397652167491e-5 1.8294993500181508e-5 -9.451130979967783e-5; 3.697001925225701e-6 -3.6846522391306745e-5 -0.0003047174252944887; 3.938632224460381e-6 3.285567300741441e-6 0.0002764502183228792] %
+
+Mass Used: 65.97388383513498 kg
+Launch C3: 123.36096320618475 km²/s²
+||V∞_in||: 0.003810357815918844 km/s
diff --git a/archive/ES_0.6745846357405142 b/archive/ES_0.6745846357405142
new file mode 100644
index 0000000..97170a1
--- /dev/null
+++ b/archive/ES_0.6745846357405142
@@ -0,0 +1,22 @@
+archive/ES_0.6745846357405142---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T23:14:20.365
+Launch V∞: [7.835644528039958, -7.731059220615141, -2.8290467884916204] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.158918535644758, 0.3068959277540627, -0.37037131577173255] km/s
+ V∞_out: [-0.2561932042873854, 0.2976470993269486, -0.3120780913289133] km/s
+ time of flight: 9.318100056082167e7 seconds
+ arrival date: 2027-04-24T10:51:00.365
+ thrust profile: [0.42376031487294674 -0.22005554151035678 -0.2233606270623246; 0.08224870677075283 -0.00877572116831416 -0.08565246530926182; 0.0521640081009954 0.0036182556362899425 -0.07744293640008942; 0.024040919063196553 0.004044892150733776 -0.04578018940275708; 0.00693398160755423 0.0015982073668348896 -0.01673500493125984; 0.01376340801002933 0.003632507558059942 -0.03525565222424202; 0.007120582788943675 0.002312658177741123 -0.020267127025628558; 0.0015758873225348766 0.00046053231557580034 -0.005019355497554288; 0.00026941178100540846 0.0008623453988626498 -0.002742510226326018; 0.0013466703714294067 0.00017616799974299702 -0.0023729581702088493; 0.0018355379481074215 0.0005439297266921414 -0.007593234171534715; 0.001700518370062003 -0.0007114257289413963 -0.00238062231655366; -0.00028679279366937947 -0.00010327918074552582 0.0003089523006793429; 0.001332206194782058 0.0012430841736421818 -0.0008236857975397224; 0.000954433802286698 -8.660764941819662e-5 -0.000330612750048673; -0.00013958082176416045 -0.0008329806947626852 -0.00153261729077046; -0.0005406838867803802 -0.0009097549965545039 -0.0005532711150249318; -0.0002705568065953395 -0.0005382901955095946 0.00019503421758301537; 0.00038752320863754395 -0.00021541550948826643 -0.001070193421205299; -0.0014601071826848312 -0.0002030038953900531 0.003958679252019169] %
+
+Mass Used: 33.52311418264162 kg
+Launch C3: 129.1701075739357 km²/s²
+||V∞_in||: 0.5065719326906944 km/s
diff --git a/archive/ES_0.6746221922183859 b/archive/ES_0.6746221922183859
new file mode 100644
index 0000000..2135a88
--- /dev/null
+++ b/archive/ES_0.6746221922183859
@@ -0,0 +1,22 @@
+archive/ES_0.6746221922183859---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T01:36:45.787
+Launch V∞: [7.862753651211386, -7.455296642361194, -2.5320969369362474] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.08767079385268395, -0.09319624774078983, 0.06259106669748596] km/s
+ V∞_out: [0.10145526430563677, -0.07645693767151186, -0.06441037846539335] km/s
+ time of flight: 9.340715198259634e7 seconds
+ arrival date: 2027-04-24T04:02:36.787
+ thrust profile: [0.6366488927484031 -0.2750777678748984 -0.3083042611413524; 0.24360220831307033 -0.014385100578189047 -0.22938620593756684; 0.14934953372841736 0.0189091215157318 -0.20162174691175358; 0.0824884852174875 0.01856003807342224 -0.13955537810242816; 0.03936162620221904 0.010804947429094422 -0.07572082210790566; 0.018831352976539175 0.005592841857420473 -0.04001687707195929; 0.003917045149084374 0.001331823966154814 -0.003970306006381224; 0.005804793149526781 0.0009056308205702963 -0.005988947773012844; 0.001476068986490357 0.0007016959795242726 -0.005614913696446558; 0.0019455515317443244 0.002048758964549463 -0.008725266096787313; 0.006883033050683874 0.0014357704684699083 -0.008310999817331872; 0.008867690143379459 0.003342828069176228 -0.006394958089038472; 0.002573901872779375 0.0008323948794648712 -0.006523324307474286; 0.008530713867380692 0.0016745348870691485 -0.01174175953356511; 0.00235410480516392 0.0005914874882514101 -0.00276075449924515; -0.0016671514840780957 -0.0011781902861390096 0.0022651087860238095; 0.001594218134474351 0.0005617068205835238 -0.00485112598530447; 0.0021831364749149342 0.0006837968222782671 -0.0028685663446117414; 0.006367184447349377 0.004668088654819949 -0.005890703853657294; -0.0012007300149502295 -0.0011457706862502506 -0.004105691853136357] %
+
+Mass Used: 64.80005315230528 kg
+Launch C3: 123.815857903282 km²/s²
+||V∞_in||: 0.14244069052785308 km/s
diff --git a/archive/ES_0.674722100198476 b/archive/ES_0.674722100198476
new file mode 100644
index 0000000..c85dc4e
--- /dev/null
+++ b/archive/ES_0.674722100198476
@@ -0,0 +1,22 @@
+archive/ES_0.674722100198476---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T13:59:13.710
+Launch V∞: [7.253070550019325, -7.43647116134401, -2.015308207024838] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.05424722934491126, -0.028645005605389854, -0.0053980074498713206] km/s
+ V∞_out: [0.03970889411310455, -0.033189467937554035, 0.03341286536257876] km/s
+ time of flight: 1.002248115121602e8 seconds
+ arrival date: 2027-07-11T14:12:44.710
+ thrust profile: [1.0 -0.5537568719688135 -0.5381402450884831; 0.28131860850239215 -0.01997139777073984 -0.24741276716246374; 0.15864296585446577 0.017372241227248474 -0.19142911653404882; 0.11242282179912387 0.024063996423394865 -0.16520199126072915; 0.06281707351044277 0.017725838386682867 -0.09234072062520891; 0.012113051932277259 -0.004998535926095973 -0.07329621914393006; -0.0008136649641203203 0.025141967752731968 -0.057056775942740966; 0.00648078349909236 -0.018275419346359234 -0.016953243340586975; -0.003087389764417266 -0.00509801439844886 -0.014298828889157468; 5.619341884456261e-5 0.025029728104009323 0.0023554143202516274; -0.0016399332504530954 0.0015071089485045018 -0.004933803403916065; -0.05827202321932977 -0.007264276286042511 -0.03832319036188764; -0.04444442010720302 0.10188481535868245 -0.13145230320967385; 0.01136080789919276 0.028543730715047285 -0.010944753969867554; -0.03364986229132203 0.08938099653842461 -0.10838030606917774; 0.019977062201382272 0.007985776760605131 -0.013235704259240536; 0.09337070601157842 -0.04208345218903562 -0.10789101837538441; -0.10774332381771799 0.05589427862176948 -0.029935990462339652; -0.08273694117096456 0.04978664171172239 0.05972737037499912; -0.04398295551647553 0.10203898518555574 0.03139791935877177] %
+
+Mass Used: 134.0197666111194 kg
+Launch C3: 111.96960290636044 km²/s²
+||V∞_in||: 0.061582763190369136 km/s
diff --git a/archive/ES_0.6753342768975439 b/archive/ES_0.6753342768975439
new file mode 100644
index 0000000..c5b0f95
--- /dev/null
+++ b/archive/ES_0.6753342768975439
@@ -0,0 +1,22 @@
+archive/ES_0.6753342768975439---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T14:58:53.832
+Launch V∞: [5.188664954437768, -8.69559126410038, -1.5850577751211663] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.010911950304024682, 0.00915748653856197, -0.00017743769607333115] km/s
+ V∞_out: [-0.006226727772974724, 6.284862414420746e-5, 0.012813218095439028] km/s
+ time of flight: 1.1685953464475638e8 seconds
+ arrival date: 2027-01-06T03:57:47.832
+ thrust profile: [0.4370712450932371 -0.3579476688205932 -0.22690690426071863; 0.22724383445622587 -0.06564125993369528 -0.20913809834849284; 0.1555565641572186 -0.017862662144565385 -0.20705056577498676; 0.10089526990343595 -0.0017850685528580455 -0.1740284704496643; 0.06008881081500356 0.006587209741714789 -0.1305914180360775; 0.02528591087463506 0.015086543292932984 -0.08345966076341527; -0.009195566618461068 0.03583122860179353 -0.0446397128176165; -0.005751676404994363 0.04273093786868023 -0.03513957808219291; 0.03457983465176976 -0.016315092804652206 0.0254854513745232; 0.03667596533294636 0.044311515248903637 -0.032142615833098374; 0.12339254212432467 -0.04189176774925628 -0.012056829390372052; 0.009844277759355948 0.00042242897056397823 -0.04992533574226569; -0.03433097770275908 0.12710090961748294 -0.06943421469632274; 0.055473148040419806 0.029967743433513508 -0.31552093154557864; 0.14074039193826235 -0.0732971523208034 -0.12709879160066476; -0.05719206506362631 -0.33782340938533867 -0.22629195112941566; 0.05370877065025925 0.05484738991547703 0.04119799158844805; 0.15960810050991692 -0.1353455127141707 -0.18032637769654616; -0.06766046741284862 0.056758432946770514 -0.08125498898482142; -0.16068613518327504 -0.03555162442234342 0.044170685558696625] %
+
+Mass Used: 175.11022542607543 kg
+Launch C3: 105.04795959218157 km²/s²
+||V∞_in||: 0.01424646283389094 km/s
diff --git a/archive/ES_0.6754423718053657 b/archive/ES_0.6754423718053657
new file mode 100644
index 0000000..a927627
--- /dev/null
+++ b/archive/ES_0.6754423718053657
@@ -0,0 +1,22 @@
+archive/ES_0.6754423718053657---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T11:24:47.508
+Launch V∞: [5.902485088900232, -8.816462422663774, -2.3992186457172346] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0037316903055869093, -0.06479092067868213, 0.2924843778121384] km/s
+ V∞_out: [0.24495110534533357, 0.12327093245966995, -0.12254803637171906] km/s
+ time of flight: 9.814943592834337e7 seconds
+ arrival date: 2026-06-03T11:08:42.508
+ thrust profile: [0.657408254535592 -0.5094998188443788 -0.36896350272083817; 0.29509310190528876 -0.07292173870329324 -0.27890208324708177; 0.09455883093815073 -0.004738831888031873 -0.13103607367564318; 0.08171753730238951 0.0002632805984979728 -0.13526043821978984; 0.05769978667283827 0.008093961784471325 -0.09503733762659786; 0.05708249763405907 0.007103518959777845 -0.11142357909534352; 0.0178263266994557 0.0095830660681235 -0.051487732733882845; 0.0029627840946831923 2.1858356371994448e-5 -0.01207933178134844; 0.005286153437572267 0.001206527625056679 -0.002521952303439993; 0.015157380938951305 0.005571072709414156 -0.004853619750723185; -0.004668749864373115 0.005304063762989489 -0.0010389706113684673; -0.008115225073743178 -0.01298121098970683 0.004676004137283755; -0.04220301657406112 -0.039528678531125086 -0.03673837094304932; -0.025144119372501314 -0.029707172792013015 0.00238569817515499; -0.0005732674260579807 -0.002463181943078087 0.029914085985577623; 0.018711311172753733 -0.0030353663905334227 0.0447820334443598; -0.0107118165141548 0.11356867301968629 -0.003337042214317777; 0.10027701556091231 -0.056647975997070554 -0.0083951218059794; -0.0029511779293083015 -0.010480084869602757 0.008608248934843365; -0.015341683223875434 0.010182656599527513 0.07746741414016209] %
+
+Mass Used: 97.78349219440634 kg
+Launch C3: 118.32558998488919 km²/s²
+||V∞_in||: 0.2995978974877524 km/s
diff --git a/archive/ES_0.6765228206744213 b/archive/ES_0.6765228206744213
new file mode 100644
index 0000000..ff8dc99
--- /dev/null
+++ b/archive/ES_0.6765228206744213
@@ -0,0 +1,22 @@
+archive/ES_0.6765228206744213---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T03:39:32.032
+Launch V∞: [6.085141532349091, -8.920301690124369, -2.3808102924599996] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0026842214800516114, 0.0014701949090222116, 0.0028219576612881266] km/s
+ V∞_out: [-0.0013478612158405174, 0.002869417964996613, -0.0026978252151511634] km/s
+ time of flight: 9.279321213126943e7 seconds
+ arrival date: 2026-04-04T03:33:04.032
+ thrust profile: [0.8621090064010025 -0.8097227240460175 -0.4967979265738658; 0.2460024525809371 -0.06827993839545218 -0.226366565060489; 0.11679658195705707 -0.012227030661946425 -0.14515836831873813; 0.037090907915071344 -0.0007207151315684954 -0.061599757840188944; 0.021567924830440555 0.00018918697219979957 -0.04099592988485701; 0.015259879052714835 0.0015256010112595399 -0.03352537899944041; 0.011043585274216236 0.0016354299408727752 -0.025770783921905998; 0.016040828731015935 0.001245224936255995 -0.04540967759091418; 0.0022983095560080826 0.0003938454606127171 -0.006094904177390747; 0.00029853190693575826 -1.1381275521519233e-5 -0.0005241834275376799; 0.0004500043775939914 -1.4456873443230705e-6 -0.0009706065798003664; 0.00012085969256046627 -0.0004086560195018089 -0.0008262327816544533; 0.0004396156912165283 -6.876111563685786e-5 -0.0009501016001841983; -0.0003292144904562642 0.0006980645176212859 -0.0009234752646733745; 0.0005959133166097747 -0.00021310534142067849 -0.0008079151353390764; 2.2455370022368974e-5 9.055381639685563e-5 -0.0004554372714555387; -1.883851384609325e-5 -1.6858174326542697e-5 8.792011476885112e-5; 0.0008632597719158125 -0.0004753370157013219 0.00031514025859588667; -0.000695412525635339 0.0007652310453435898 -0.00022516326933025025; -0.0005643533395592575 0.00040866539680017855 0.00038078193413234256] %
+
+Mass Used: 76.04086451876401 kg
+Launch C3: 122.26898736023898 km²/s²
+||V∞_in||: 0.004162927223311506 km/s
diff --git a/archive/ES_0.6765978525531317 b/archive/ES_0.6765978525531317
new file mode 100644
index 0000000..1b1c29e
--- /dev/null
+++ b/archive/ES_0.6765978525531317
@@ -0,0 +1,22 @@
+archive/ES_0.6765978525531317---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T23:54:43.317
+Launch V∞: [7.820292939316839, -7.432762226669163, -2.5196591824847787] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.684855553493271, -0.6372143447485528, -0.07435832673120484] km/s
+ V∞_out: [0.5064579781896054, -0.565469803758804, 0.5516618986918053] km/s
+ time of flight: 9.321961478881282e7 seconds
+ arrival date: 2027-04-21T22:14:57.317
+ thrust profile: [0.7272852210355721 -0.339817338334374 -0.356948822029332; 0.3548201860506273 -0.023574672244059465 -0.3201154604849486; 0.14825690275688166 0.017434648307505327 -0.19133293300198378; 0.05601266578324155 0.012128637391325355 -0.08839983825999576; 0.03411016259214591 0.009570205150059269 -0.06367576739486339; 0.007470062445881402 0.0015815621166089188 -0.014889184702291107; 0.0063806311659434616 0.002221492616824067 -0.023213210991867777; -0.0001951800661901936 0.0018585558762656655 -0.0068185637034359255; 0.009001522799814298 0.0006434990998543393 -0.015844180887394185; 0.006090513573379327 0.00042049698004794234 -0.011549999174607962; -0.0013192559312428798 0.000559189446426957 -0.005793960044421016; 0.0018182844710890995 0.004116391860669032 -0.0015093779095517962; 0.010956770729016413 0.002771073596145206 0.005341164260298171; 0.0043085996995007765 -3.6490487186050316e-5 -0.007391052724678715; 0.0023268483855806424 -0.0008496876148956813 -0.004882053433051082; -0.013707737814987485 -0.008010372208804867 -0.001529051481709294; -0.004191303268043792 -0.0014811162736805678 -0.0074056923757078; -0.0028288438371366484 -0.001632341218328668 0.014888136375035242; 0.021009496475000625 -0.010607646688099765 0.030003610111883246; -0.0006147002126365674 3.883149198078122e-5 -0.002614897309051129] %
+
+Mass Used: 73.31305414893677 kg
+Launch C3: 122.7516183708086 km²/s²
+||V∞_in||: 0.9384020519255947 km/s
diff --git a/archive/ES_0.6766901123337817 b/archive/ES_0.6766901123337817
new file mode 100644
index 0000000..e58cef7
--- /dev/null
+++ b/archive/ES_0.6766901123337817
@@ -0,0 +1,22 @@
+archive/ES_0.6766901123337817---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T12:56:28.076
+Launch V∞: [5.935375972894729, -8.956822336946578, -2.0268159434173096] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.2293210992174478, -0.257645920412314, 0.009705112903004026] km/s
+ V∞_out: [0.04521799774638205, -0.001401729682584353, -0.3421188195622037] km/s
+ time of flight: 9.406681127608977e7 seconds
+ arrival date: 2026-04-18T06:36:39.076
+ thrust profile: [0.6651920199214096 -0.5287302872539239 -0.3653940922882113; 0.4994626630691717 -0.1425486713226408 -0.42081713464353376; 0.16930618765654576 -0.01484208553100114 -0.19458508336639246; 0.14779648239411772 0.0026214862829903045 -0.2055912189311581; 0.06990699244939244 0.005598796084326578 -0.1145546393490203; 0.01983665753442784 0.0045043796427116835 -0.0352980543510332; 0.009639239058285027 -0.000536268075773291 -0.024278518014065012; 0.002609429197938738 0.004526060382697163 -0.0012226840320053154; 0.0003311975914365897 9.914346332002058e-5 -0.00022541020746536617; -0.007214117875308672 -0.001604219281366798 -0.005058076656975707; 0.0005466618141388135 -0.0007417136823761588 0.0001275102699965748; 0.0056080038392249745 0.009351756688514545 -0.004786017640677059; 0.008720343422537151 0.020180179866085838 -0.023264234121777333; -0.0007377807839616104 0.0004809044420383607 -0.0024233291283089035; -0.0007157001377567516 -0.0013938293799323448 -0.00132096326878123; -0.0023784644752345664 -0.0088291369241105 0.006192496514231344; 0.01819109060873176 -0.00375174869077567 -0.009854920138703985; 0.00483501175517693 -0.007431258657349664 -0.020653263646269675; -0.01309641042658729 -0.00043579561237162075 0.004852200856275673; 0.01390892015128439 0.010998851155167836 0.0034926175321934824] %
+
+Mass Used: 92.03066415097646 kg
+Launch C3: 119.56133718373181 km²/s²
+||V∞_in||: 0.3450561926235595 km/s
diff --git a/archive/ES_0.6768588202781685 b/archive/ES_0.6768588202781685
new file mode 100644
index 0000000..5e7c4bd
--- /dev/null
+++ b/archive/ES_0.6768588202781685
@@ -0,0 +1,22 @@
+archive/ES_0.6768588202781685---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T23:01:37.191
+Launch V∞: [7.831158944469202, -7.611070649599251, -2.612410299049388] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002661384533189253, -0.003342508730692686, 0.000718100943292397] km/s
+ V∞_out: [0.0009039435913148742, 0.0022849256022102835, 0.0023917600706287972] km/s
+ time of flight: 9.228871564229101e7 seconds
+ arrival date: 2027-04-13T02:46:52.191
+ thrust profile: [0.6701782089646118 -0.34005881750821476 -0.35847542139487937; 0.1988200303868483 -0.01805118507585683 -0.18930375764906793; 0.09955466118860037 0.008966972152603846 -0.13589601616354585; 0.03295504972095402 0.006308958274955276 -0.05771925423213707; 0.01835872623720532 0.004756836745967204 -0.038568699720575965; 0.015050551317619815 0.0045579908455825316 -0.0355212522317343; 0.0064343889455214754 0.0022166538273595067 -0.01706973717307541; 0.002496370893345874 0.0009392821060876818 -0.006846676172109585; 0.0021845455364701916 0.0009818102112102397 -0.007435944221980184; 0.000542779263729887 0.00018787175588071662 -0.002687904547493501; -8.112444437515854e-5 0.00032403300952621526 -8.644789729429412e-5; -0.0006104211475873196 6.740085011125809e-5 -0.0010878454176060151; -0.00033468773046671724 0.0006816287894873274 -0.0005137963686776376; -6.281971751212782e-5 8.296331755836303e-5 -0.0006376263596702004; 0.0004550424540501496 7.974799434726893e-5 -0.00034242824809698836; -0.00040335159773070443 -0.0005122021282053708 -0.002011519139823709; -0.001083985845644555 0.00019851285723624046 0.0006518465920876001; 0.0009346632040386539 -0.0011485863724430357 -0.00030332333477027214; 0.00015394856222124146 5.185878888397757e-5 -0.0036731282797495095; -0.0010531372031548803 0.000721997308789935 1.898486861883538e-5] %
+
+Mass Used: 54.20117289021891 kg
+Launch C3: 126.08013441731046 km²/s²
+||V∞_in||: 0.0034291198952281113 km/s
diff --git a/archive/ES_0.6768852956906453 b/archive/ES_0.6768852956906453
new file mode 100644
index 0000000..61b0821
--- /dev/null
+++ b/archive/ES_0.6768852956906453
@@ -0,0 +1,22 @@
+archive/ES_0.6768852956906453---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T18:45:27.697
+Launch V∞: [7.641069346506576, -7.595715183893838, -2.303598594754592] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.2787160366466621, -0.29032863892532035, 0.18593830200949762] km/s
+ V∞_out: [0.3522202380425182, -0.18585400440692879, -0.19386675200093217] km/s
+ time of flight: 9.204852891736221e7 seconds
+ arrival date: 2027-04-10T03:47:35.697
+ thrust profile: [0.9934036356088985 -0.5169430908842099 -0.4692598052100671; 0.3691487435268192 -0.033722200051466554 -0.299710048295371; 0.15536640639854102 0.01468612664975015 -0.18985700232682085; 0.029078371203094627 0.00588993863569435 -0.047345672288840075; 0.04834816016186172 0.012804936431649972 -0.09187887308629966; 0.03831321075364393 0.011865452522081025 -0.08068684373404614; 0.010261056287907314 0.0035152692124329503 -0.02469393323853777; 0.0013403668456240545 0.00046028221960228 -0.0035579707556257596; 0.0006133650000782541 0.00020795655373231426 -0.0016591026312353715; 0.00034813408273860936 -6.258159807870503e-5 -0.0006865791021810304; 0.00018784664091633542 -0.00012489455393511784 -0.0008077519364134606; 7.175197848397874e-5 -2.0877692567237375e-5 -0.0006524361919852444; 0.00019734323971426132 -6.213497250311066e-5 -0.0002791190687987851; 0.0005760618849436645 0.0001372254575931526 -0.0008835317603958664; 0.00023174607736711024 -0.0006185639873641778 -0.0003379599243904475; -0.00015228912897594581 0.0003920025898194378 -0.00026565631778957587; -0.0005843477530342268 0.0001862825918200326 -0.00010637605012374032; 0.00022061064032663405 -3.315652492967982e-5 3.888555154935285e-5; -0.0003257041766122914 0.0002762972535823795 -0.00038135644993547333; -9.244307954327713e-5 -4.640590096077684e-6 0.0002841287954224018] %
+
+Mass Used: 81.60636597992607 kg
+Launch C3: 121.38739639871316 km²/s²
+||V∞_in||: 0.443335538636852 km/s
diff --git a/archive/ES_0.6772273232378083 b/archive/ES_0.6772273232378083
new file mode 100644
index 0000000..91506fb
--- /dev/null
+++ b/archive/ES_0.6772273232378083
@@ -0,0 +1,22 @@
+archive/ES_0.6772273232378083---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T09:24:09.872
+Launch V∞: [7.8367030894625564, -7.546883845536729, -2.6459244569747526] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.11068573150494547, -0.2475178978070026, -0.3251585450951014] km/s
+ V∞_out: [-0.38123709920550086, -0.05478687950177161, 0.17574393196578894] km/s
+ time of flight: 9.217490830821897e7 seconds
+ arrival date: 2027-04-11T05:32:37.872
+ thrust profile: [0.7099162861134379 -0.35984558846566883 -0.3644998456771031; 0.3033132806227392 -0.024654956060479228 -0.26877513976001005; 0.09853226765788729 0.009961257186721884 -0.12661603439664273; 0.031917816835966145 0.006284675469098952 -0.05237303972739282; 0.018394151865180657 0.004712058293979821 -0.03550957617541848; 0.0010268254905303176 0.00033270528510698986 -0.004142733114162381; 0.004785062525579898 0.0013444452253554532 -0.007141499410072278; 0.0018194555830477754 0.00011775585789194117 -0.004643194476862541; -0.0008821436081993905 0.002874413970112434 -0.007363773021115174; 0.0011394933462462791 -0.0001762820478609997 -0.0013142675812983346; 0.0014077032212156902 0.0005677803015966714 -0.0007770496660540523; -0.0007988919913864564 0.0015673852965757138 -0.0025734162817586835; 0.0005574730966264505 0.00020219396265203015 -0.0009374140154073465; 0.00013956086052403349 0.00016670564501271496 -0.00013409978114812269; -0.001096259709462747 0.0019509288399897511 -0.0006060917217744523; 0.0039033915989586986 0.0011619409736952015 0.0028308006125704792; -0.0019833120098495835 0.0005295287501698224 0.0019486606478961747; -0.004661233929113964 0.0015484466360876031 0.0074155264078008005; 0.0022607002252022696 0.0018484863912946001 -0.00015254006303105493; -0.00042161465786267173 0.0011633903231865147 -0.0006610530508646001] %
+
+Mass Used: 58.771867729920814 kg
+Launch C3: 125.37028732243238 km²/s²
+||V∞_in||: 0.4233727912159044 km/s
diff --git a/archive/ES_0.6774471494691678 b/archive/ES_0.6774471494691678
new file mode 100644
index 0000000..02b4ad3
--- /dev/null
+++ b/archive/ES_0.6774471494691678
@@ -0,0 +1,22 @@
+archive/ES_0.6774471494691678---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T14:22:37.458
+Launch V∞: [7.70100940849946, -7.854334082452253, -2.363371041025006] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.5430520808904101, 0.5206325758300564, -0.3755038178466009] km/s
+ V∞_out: [-0.6069533098465184, 0.4641174431454605, 0.35086403238996805] km/s
+ time of flight: 9.31747447848476e7 seconds
+ arrival date: 2027-04-25T00:15:01.458
+ thrust profile: [0.43012845908944664 -0.2275079721503271 -0.22688789530808207; 0.171259654999009 -0.021164900497503032 -0.16501660748790048; 0.11722969274726838 0.004484532553529329 -0.16012195329471068; 0.05483370639752174 0.007995811747417926 -0.09995321807318432; 0.06598878440788113 0.013011112593644583 -0.13754683488888977; 0.018994046637049167 0.004986059979931793 -0.050129563849059616; 0.010856120915620037 0.003701411372515223 -0.03263177059892887; 0.007012779323416047 0.0024239349336084913 -0.022200395842654794; 0.010985296841188597 0.0022980157550184506 -0.03646216909868366; 0.0006226004630809204 -0.0002936585432651076 -0.001197133411869529; 8.887160842576585e-5 0.0004329022748451231 -4.768007686998231e-5; -0.0009608598807850037 -6.865435697403232e-5 -0.00045938357068982325; 0.0011656391053241236 -8.498761809716733e-5 -0.00027703008748621743; 0.0013368856186504246 0.00039457096490290764 -0.000534698084904987; 2.052571595938821e-5 -0.0002253884231391415 0.00047426563895200467; 0.0002669134253174019 0.00024678982181497975 0.00018587493559276314; 6.544010199316993e-5 4.141558792031044e-5 -0.00036952574415049946; 0.00024752477285357893 -0.0009781376819878976 0.00028490262581774286; 0.00023662392258598934 -2.029578620343575e-5 -0.0007146942287648981; 0.00028624096553222904 2.69446606178863e-5 0.0001274636589958907] %
+
+Mass Used: 51.96215166163984 kg
+Launch C3: 126.58163246612389 km²/s²
+||V∞_in||: 0.8408132722502764 km/s
diff --git a/archive/ES_0.6774849905425682 b/archive/ES_0.6774849905425682
new file mode 100644
index 0000000..5c95ae9
--- /dev/null
+++ b/archive/ES_0.6774849905425682
@@ -0,0 +1,22 @@
+archive/ES_0.6774849905425682---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T23:55:57.043
+Launch V∞: [7.647568868259055, -7.869535566637857, -2.56739171306601] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.5811973544760908, 0.5873488136328748, -0.4144735288985608] km/s
+ V∞_out: [-0.6737898613115625, 0.4866929903139039, 0.4044777172499005] km/s
+ time of flight: 9.395696671316269e7 seconds
+ arrival date: 2027-05-04T11:05:23.043
+ thrust profile: [0.49962531260760057 -0.2696500345491363 -0.25888327929116994; 0.09446261635865809 -0.01156374181340402 -0.09639361154730047; 0.059300852781429866 0.0022045902652956593 -0.0857966848148154; 0.054326175333975456 0.0068476612452493734 -0.09802920995339166; 0.02738857566735139 0.004373763738715077 -0.05780272372531453; 0.011269945303127341 0.0023970984902197006 -0.03139316551280625; 0.003692317096978551 0.0006652998993141196 -0.012312094269411367; -0.0004080555036149641 -0.0004206521875232456 -0.0012826306229303075; 0.0021514688455804313 0.001660232290935054 -0.0051086047156824075; -8.113265331398995e-5 0.0008689396441964531 -0.005581624291945401; -0.001968921302534189 0.0034466620225247265 -0.01618057216663614; 0.003051654193135597 -0.01683729338212345 -0.034399039212011456; -0.002577842953960961 0.010775719271808152 -0.019237764676261863; 0.02172521846621689 -0.003533269914937948 -0.014416196116171391; 0.031802941178706114 0.002407394373766764 -0.03908680759347928; 0.024346319440668052 -0.00849916604817291 -0.013355459732898048; 0.002280329858622201 -0.0024072256662153037 -0.008570315568868227; 0.007830157463916698 -0.014895257727581004 -0.0006270338050051673; 0.002707319090161685 0.0065493789278792975 -0.001393311212233943; 0.006640776429915969 0.0011838766997019703 -0.004643981738264799] %
+
+Mass Used: 49.52848991329347 kg
+Launch C3: 127.00639983766332 km²/s²
+||V∞_in||: 0.9244226846435447 km/s
diff --git a/archive/ES_0.6776117578886246 b/archive/ES_0.6776117578886246
new file mode 100644
index 0000000..069346a
--- /dev/null
+++ b/archive/ES_0.6776117578886246
@@ -0,0 +1,22 @@
+archive/ES_0.6776117578886246---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T12:08:54.598
+Launch V∞: [5.943933056965435, -9.011390749773444, -2.1190034573958227] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.45728655839490223, -0.45448395354631355, 0.01877206252315851] km/s
+ V∞_out: [0.0842473442176711, -0.0024212763813029237, -0.6396128736796048] km/s
+ time of flight: 9.307050686949794e7 seconds
+ arrival date: 2026-04-07T17:04:00.598
+ thrust profile: [0.7719113825462931 -0.6317688177138963 -0.3968986389389771; 0.4294434329539712 -0.12496625270535323 -0.3494751604834451; 0.07338192216204961 -0.006173308604781567 -0.095922280071682; 0.1451720421046817 0.00426600228642901 -0.2116391589758066; 0.04729396446777591 0.0014939023196889774 -0.08586832047917646; 0.020610987950976403 0.003367454047106585 -0.043600555229325114; 0.024142528116424547 0.0026791486920929937 -0.05362984012010628; 0.001923342135687309 -0.00040933266112480897 -0.00770426683912265; 0.004486292012242609 0.0010443417587643715 -0.013015877859894207; 0.0011924925962112053 -0.0018072195867325264 -0.006284087499051039; 0.0023202789437937353 0.0015671260739414275 -0.0005033849492951832; 8.987033245883564e-5 -0.001135536713552274 0.0016892229485516148; -0.001972385150524694 0.000874016257423064 0.0008600097568107474; -0.00018193778585745047 0.0016047823704344506 0.00023965939888685197; -0.0006253649620454739 -0.00031131907749903904 0.00195266736469043; -0.0013800158651522455 0.004780623384171348 -5.1162169102192965e-5; -0.004950919657944129 0.0017498555246855392 0.0009731990620727605; 0.0016112664456042938 0.0015824388851971636 -6.096946111954174e-5; 0.0023482017524164584 -6.0636204624720414e-5 0.002961071976190765; -0.0006217108456951633 -0.0019215379530050022 -0.0006802461470759789] %
+
+Mass Used: 84.56392288447023 kg
+Launch C3: 121.0256790832443 km²/s²
+||V∞_in||: 0.6449953882401915 km/s
diff --git a/archive/ES_0.6780882541172518 b/archive/ES_0.6780882541172518
new file mode 100644
index 0000000..92db4bb
--- /dev/null
+++ b/archive/ES_0.6780882541172518
@@ -0,0 +1,22 @@
+archive/ES_0.6780882541172518---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T21:31:53.556
+Launch V∞: [7.615494124656389, -7.3101397706932865, -2.279368893237275] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.039147592464241904, 0.0752268783020729, -0.09145299319546807] km/s
+ V∞_out: [-0.06253262693309691, 0.07473798758118523, -0.0776487150769431] km/s
+ time of flight: 9.472879979628317e7 seconds
+ arrival date: 2027-05-08T07:05:12.556
+ thrust profile: [1.0 -0.5811401089309897 -0.5597003574455439; 0.4904210457777529 -0.020545860635205044 -0.4069689922169841; 0.13666412923299545 0.021258097186764913 -0.16363528735188712; 0.10541565144246769 0.027819362174093108 -0.15765452027205348; 0.05164208604995321 0.016770755314011208 -0.08797477808030549; 0.0216500789414957 0.006889202527161734 -0.0392439574117941; 0.012550311479129635 -0.004284157879428155 -0.021242159193307696; 0.010574249404280948 0.005106261305320955 -0.014069411371193124; 0.0089018934332102 0.004260783395136275 -0.013618112095335663; 0.019155584540479567 -0.0017385650589029186 -0.027984654465660643; 0.01510853526290431 -0.00882157333810987 -0.006097311803430493; -0.00011446189793198076 -0.00011794978202816833 0.0005975525555804541; 0.008310722676175343 -0.00738230474371874 0.013924569784207369; 0.009049289514754305 -0.0067075309887024235 -0.004295981696497222; 0.0160834494098285 -0.004932921503129887 0.010230802453727896; -0.000803963872469275 -0.06587256969552856 -0.01506535383376337; 0.011829434531398678 0.022162629919296843 -0.00040858443695846125; -0.0058349424504209775 0.02873009740878619 0.021027155151162123; 0.017404749847713362 -0.07419379404799986 0.008232689568217683; 0.026428230091497976 0.06362079895100864 0.05947371050672345] %
+
+Mass Used: 110.76469857976235 kg
+Launch C3: 116.6294167812054 km²/s²
+||V∞_in||: 0.12472075680988945 km/s
diff --git a/archive/ES_0.6786510691264909 b/archive/ES_0.6786510691264909
new file mode 100644
index 0000000..1d6ff25
--- /dev/null
+++ b/archive/ES_0.6786510691264909
@@ -0,0 +1,22 @@
+archive/ES_0.6786510691264909---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T13:48:06.612
+Launch V∞: [5.541813596297596, -8.800404908882074, -2.3539114165918735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00011875776195185788, -6.582745817436946e-5, -0.00011806946338181835] km/s
+ V∞_out: [5.218027879652468e-5, -0.00011875151479647383, 0.0001247130031818499] km/s
+ time of flight: 1.0477817216233343e8 seconds
+ arrival date: 2026-08-19T06:50:58.612
+ thrust profile: [0.5166168294034894 -0.42159355006765886 -0.29838585693023645; 0.2613694539774006 -0.07583112457673323 -0.24362198860493578; 0.14267185487947917 -0.01680974045361836 -0.1851968964542207; 0.05963690949253759 -0.006639172258966266 -0.09211009168105118; -0.0005913934399714785 -0.03296499244175606 -0.04924779424611121; 0.07447849004547287 -0.003935838614050122 -0.07024061122497827; 0.05706673623851734 -0.013484273477286078 -0.08651065732337279; 0.013222323271434286 0.00490552245522012 -0.029553696309997737; 0.008195719336596352 0.009801823200051962 -0.026710979660392275; 0.0075113543756136145 0.015144210850312366 -0.0434361738027845; 0.01282922634716346 -0.01916886725576724 -0.003381748545668639; 0.004592515124317955 0.008785930312560204 0.012186717891221877; 0.03812806122214163 0.05718459315868231 -0.06277704738333836; 0.06616997786241434 0.05316694581842777 -0.014132455875622467; -0.04133506176594507 0.02993236336782946 0.02781284510061073; -0.05980846987555781 0.07271416559110527 -0.21331715488252903; 0.07331309311480232 -0.10167870068271054 0.1228231758343177; -0.08896636452447687 0.22348712372712087 -0.15012700832249765; 0.06558515758498433 0.0916181658857709 -0.15685072038092496; -0.0011756140859066463 -0.07260650614284078 0.07344818387970319] %
+
+Mass Used: 128.51119383522018 kg
+Launch C3: 113.69972345354616 km²/s²
+||V∞_in||: 0.00017993626220632418 km/s
diff --git a/archive/ES_0.6792212696533744 b/archive/ES_0.6792212696533744
new file mode 100644
index 0000000..81b6ab0
--- /dev/null
+++ b/archive/ES_0.6792212696533744
@@ -0,0 +1,22 @@
+archive/ES_0.6792212696533744---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T09:32:25.124
+Launch V∞: [7.729553794729574, -7.556399541330958, -2.430958054150046] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.08070847319802307, 0.07084099814020609, -0.04989506377144985] km/s
+ V∞_out: [-0.049915931348053146, 0.10517367990198725, -0.02123498347984584] km/s
+ time of flight: 9.290818382567564e7 seconds
+ arrival date: 2027-04-19T17:22:08.124
+ thrust profile: [0.8879731481227897 -0.45230741458942886 -0.4088034598692775; 0.1325423092412821 -0.010077894126318543 -0.12336838953729239; 0.11348109479074232 0.012556223344088967 -0.14684254762339408; 0.0561155371497336 0.011511112636537098 -0.09279399804258753; 0.12003534547660781 0.032579822890173984 -0.21466372842148407; 0.014592198350427646 0.004478422741560627 -0.02950654150956289; 0.013895784607534977 0.004848482914577839 -0.03030809693833446; 0.003764514225334965 0.0022667775233392133 -0.0035440459413940643; 0.00872799273306566 0.0012090835679844315 -0.00934737101531366; 0.0038795413672254803 0.0007479874908858371 -0.0027392803445378845; 0.0020582925382092486 0.0012435683717780042 -0.009628620862757929; 0.0021710583559904234 0.012419225927732334 -0.00023193642277289858; -0.006245860242987376 -0.0027858892277843016 -0.0036649645412999213; 0.007602610210850857 -0.016739553537342872 -0.003590152450477585; -0.008908273370433376 -0.018537270065292002 -0.0065430588933752835; -0.0070059371130086825 -0.004239705354628144 0.012785727342220055; 0.010643222361682234 -0.016768695547476623 0.013442613524797902; -0.019327781385860287 0.03323652476446104 -0.010852725689050893; 0.0036046588440500783 -0.0019784796833712285 0.00023796409206067442; -0.011402588276000566 0.013766803269239224 -0.0036704503967487346] %
+
+Mass Used: 76.35553902545826 kg
+Launch C3: 122.75473295488204 km²/s²
+||V∞_in||: 0.11841377475705155 km/s
diff --git a/archive/ES_0.6792841542034902 b/archive/ES_0.6792841542034902
new file mode 100644
index 0000000..3a280ad
--- /dev/null
+++ b/archive/ES_0.6792841542034902
@@ -0,0 +1,22 @@
+archive/ES_0.6792841542034902---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T03:26:40.787
+Launch V∞: [7.837951596561497, -7.338265427666281, -2.445012153342333] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.6692128297356942, -0.5957266059134928, -0.07301379890016556] km/s
+ V∞_out: [0.4903655963149343, -0.5382212903205417, 0.5272170333847522] km/s
+ time of flight: 9.224658707029794e7 seconds
+ arrival date: 2027-04-09T19:29:47.787
+ thrust profile: [0.9492932507401416 -0.4384759402995864 -0.43689116888938384; 0.4542053475617615 -0.02541702964684657 -0.3574003859271881; 0.12818734032232293 0.01932454061917812 -0.14448692716490932; 0.06951696150097142 0.020410289648306254 -0.09759513358629389; 0.07255902701907774 0.026957737485469088 -0.13001208425011962; 0.011204094053586237 0.004806258643961203 -0.022288528403601418; 0.009274280322182887 0.004057695401506405 -0.021713016573831814; 0.0035736661736410743 0.0010518505934667636 -0.005879717726484421; 0.002419639118044533 0.004860153944364661 -0.004519270474890474; -0.004017680600736392 0.0005119441880047713 -0.003878676315190869; 5.714357087944488e-5 0.001988762014475293 1.8865881550093316e-5; 0.00964156950070656 -0.0031069886353282923 -0.012286173150398668; 0.0019241702724187223 -0.006246320291131317 -0.0061547047390474365; 0.0006799623263773653 0.0011685168986915258 -0.00039430551495298863; 0.0009414397487966257 -0.0006109212907527944 -0.005710774596598309; 0.010563592286889328 0.003336945164096348 -0.005921497177834945; 0.0002221015931027826 -0.0003044251148827593 0.0014729536889887093; 0.006447891841283308 0.0013257899489276088 -0.00889018795761424; 0.000252848660259747 0.0041155167832589035 -0.00519461420685287; -0.001937224802689443 -0.00046310095436485205 -0.003683817554184292] %
+
+Mass Used: 85.13820988040197 kg
+Launch C3: 121.26170914691482 km²/s²
+||V∞_in||: 0.8989254781715217 km/s
diff --git a/archive/ES_0.679523126994694 b/archive/ES_0.679523126994694
new file mode 100644
index 0000000..dc3c01e
--- /dev/null
+++ b/archive/ES_0.679523126994694
@@ -0,0 +1,22 @@
+archive/ES_0.679523126994694---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-27T23:32:06.254
+Launch V∞: [7.464300077352203, -6.936265444736429, -0.932620408393694] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.5148286938115035e-9, -1.5978093903544277e-9, -1.570204666895203e-9] km/s
+ V∞_out: [1.2047382898869194e-11, -1.0784768080702804e-11, -8.986871166181782e-12] km/s
+ time of flight: 9.85588058577487e7 seconds
+ arrival date: 2027-06-12T16:58:51.254
+ thrust profile: [0.9999999178054151 -0.540896512513839 -0.4004716906571025; 0.999999997552941 0.03125724912628607 -0.6400269529503331; 0.7810598834438205 0.2052889882350109 -0.6518758426568264; 0.37454695378434416 0.15464284787941637 -0.4187120683994983; 0.14759469292137015 0.07300347472095234 -0.2018683942719841; 0.11683847985750201 0.06757678418783677 -0.18169147894235957; 0.02653529642374019 0.016451836609658335 -0.04591522659835492; 0.021151851946725815 0.013790651492959816 -0.038973541432620024; 0.0008819125763947064 -0.0006423206424882976 -0.0017537977159123202; 0.0032455172683688357 0.0019786072283076474 -0.0049443052013432446; 0.0003314464270533613 0.0003438407686382122 -0.0006132043403321324; 8.061980053128993e-5 0.001580578133310314 0.00039566375237074707; 0.00019046815540481446 0.0006012203073051122 -2.145529805838779e-5; -0.0016662348845893783 0.0005046354792631248 0.0014819656498264654; -0.0040143758427825926 -0.00020227177956183033 0.002351965250842805; 0.004689373790000388 -0.002437219722242699 0.0014353814893760118; -0.0004625774587855193 0.00012524029033319755 -0.0005822542764764619; 0.0026766729700191763 -0.0020307948485227137 -0.00021150857766446158; 0.0011992353718220398 -0.00038716092483392765 -0.004041695363326287; 0.0023726412379488117 0.003229227280008557 -0.0006347844513084017] %
+
+Mass Used: 182.0425285477263 kg
+Launch C3: 104.69733479075717 km²/s²
+||V∞_in||: 2.7043009291569103e-9 km/s
diff --git a/archive/ES_0.6795734528325021 b/archive/ES_0.6795734528325021
new file mode 100644
index 0000000..11e4897
--- /dev/null
+++ b/archive/ES_0.6795734528325021
@@ -0,0 +1,22 @@
+archive/ES_0.6795734528325021---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-02T01:22:24.891
+Launch V∞: [6.003002777331781, -7.279348602770998, 0.7974341245084436] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.56907359939379e-6, 5.87832300662855e-6, 6.41418088515678e-6] km/s
+ V∞_out: [-8.079484315722553e-6, -3.684646887140821e-6, 6.327992828707016e-6] km/s
+ time of flight: 1.847564424678462e8 seconds
+ arrival date: 2029-02-07T10:36:26.891
+ thrust profile: [1.0 -0.4809901806010763 -0.06385809836584697; 1.0 0.34066067280930357 -0.211503423732993; 0.5087799139261789 0.3668086703535903 -0.18572404173489976; 0.26375129815250753 0.26813102228873487 -0.13842586166909884; 0.1507439494908119 0.19442088652155912 -0.10374236759576967; 0.06575169568463267 0.1024878466116814 -0.0566430042774589; 0.006876605016506854 0.011971268337054034 -0.006968693247144462; 0.0009094768193404263 0.002017628906814312 -0.0012071964791250899; 0.0004029400225646774 0.001006848535378933 -0.0004893856097449611; 0.00022175786366632005 0.0005274756248859412 -0.0002067372622170866; -0.00011647713415411249 8.782276742885512e-5 -6.744635345689178e-5; 0.00032544508066875976 -4.4185437812584226e-5 -0.00011825502549123979; -3.312759291813592e-5 -1.9277937626006403e-5 -0.0001840110995711123; 4.8809275768197e-5 -7.556813303683373e-5 -9.057996117346446e-5; 0.00014661866035289397 -5.215852020824184e-5 0.00014293564815701435; 7.036671075684228e-5 0.00021057467419677086 -0.00011822903237058665; 0.0002630265737635547 0.0006853255414569564 -0.0003622283896872415; 0.00016769211259915102 -3.405439972656735e-5 -0.00010870861270027699; 1.5128857228110519e-5 1.009323954335042e-5 2.6809897520575567e-5; 5.735775508796424e-5 0.0002765994794716089 -0.00011613744191019378] %
+
+Mass Used: 269.8140139231409 kg
+Launch C3: 89.6608596082477 km²/s²
+||V∞_in||: 1.09017946115317e-5 km/s
diff --git a/archive/ES_0.679738221166476 b/archive/ES_0.679738221166476
new file mode 100644
index 0000000..a03dedb
--- /dev/null
+++ b/archive/ES_0.679738221166476
@@ -0,0 +1,22 @@
+archive/ES_0.679738221166476---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T17:36:13.799
+Launch V∞: [7.852081866620805, -7.3761558286841815, -2.5033616648209973] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.6422541984082725, -0.5980257250536409, -0.0714032778854217] km/s
+ V∞_out: [0.4670829256303863, -0.5457456323707841, 0.5090928865390216] km/s
+ time of flight: 9.159749268742356e7 seconds
+ arrival date: 2027-04-02T21:21:05.799
+ thrust profile: [0.9998893463495452 -0.44556669740454735 -0.4412101712282065; 0.43033440264709855 -0.024156563690718932 -0.34108344779308664; 0.0986536303273027 0.014109673610044974 -0.1265456444008681; 0.07625343278580822 0.019408681105670466 -0.12144289372857936; 0.03162571556423161 0.010579974409002395 -0.059350603008652386; 0.008863685501320636 0.003233314618223236 -0.01905471326823718; 0.0075038811004683684 0.0030551517515785085 -0.01777071307894466; 0.007015202823390487 0.0030882447189618874 -0.01783053433071387; 0.0001321054032169337 0.0003078164959963845 -0.000816626376274189; 0.000402485484382021 -0.00014082075681223907 -0.0011576471235990743; -5.4963353034488574e-5 -7.355754075910182e-5 -0.0002652923129239818; -0.0003226644588030787 -6.183937582803306e-5 0.00016792742949272156; -0.0002445282894341781 0.001067870770213862 -0.00019914024309715102; 0.0017398089121604316 0.000966943374820293 -0.0008686178018625411; 0.0024301454701314415 0.0008836470152435805 -0.0015613476960831796; 0.0011322001982979255 0.0016578118331296715 -0.001498555961036588; 4.831295938277408e-5 -7.94450870578483e-5 -0.0002979747146720942; -0.0003995311121172625 -0.0002687766744156694 0.000800683103545919; 0.0002166811301188393 -0.0004869848830300347 0.0006119856163517812; -0.00016608257393176015 8.057849617942078e-5 -0.0003525498715739994] %
+
+Mass Used: 79.43810092897547 kg
+Launch C3: 122.32968407404226 km²/s²
+||V∞_in||: 0.8804678593178562 km/s
diff --git a/archive/ES_0.6802028794769404 b/archive/ES_0.6802028794769404
new file mode 100644
index 0000000..8219a69
--- /dev/null
+++ b/archive/ES_0.6802028794769404
@@ -0,0 +1,22 @@
+archive/ES_0.6802028794769404---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-15T08:48:21.403
+Launch V∞: [6.968501041069467, -5.921325083108335, 1.4549449457211217] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.8941181380884958e-6, -3.4022101198942264e-6, -1.3389380676361563e-5] km/s
+ V∞_out: [-1.2608809819604975e-5, -1.4226614235537589e-6, 5.029457067405176e-6] km/s
+ time of flight: 1.8749577787946093e8 seconds
+ arrival date: 2030-03-25T10:57:58.403
+ thrust profile: [1.0 -0.1658543436575036 -0.004051040335535767; 1.0 0.6166071124635462 -0.10548512527599369; 0.5167411424574556 0.5818288732779207 -0.11083689122225018; 0.20472142044042535 0.3478283008679858 -0.0754530537155473; 0.07923373216132079 0.19783156976415603 -0.04662204285317392; 0.051539858003774815 0.17288039078150652 -0.042465008924287714; 0.015631075730466324 0.06147383120307523 -0.016635188437831527; 0.006421957764711719 0.03600562129286619 -0.010370015560293426; 0.0015380796942918331 0.008123547463853702 -0.002124749304437673; 0.0022355432682422305 0.001300544084879635 0.00039400028943879653; -0.0004863440512317598 0.0007026912315716697 -0.0006720003507685819; 0.002665210560124627 0.0006236511058850206 -0.0004413365522879953; -0.0006221232252339602 0.0011072755612846893 0.0021699610696952272; 0.0011378286170341916 -0.0007157983827024833 -0.0015967740030106443; -4.720360001734527e-5 -0.0011682647826959888 0.00041769977073345536; -0.0005158283206885277 -0.00016663025483058314 -0.0005175835271408799; 0.0005477874025024115 -0.001441837263681094 3.335566952163236e-5; 0.0025552627398353505 0.0008312754216315413 -0.0017073387940209504; 1.432919170291471e-6 0.002382525575652207 -0.0023796870361217953; -0.0030798877357397334 0.0018564461930393162 -0.0003384352672052024] %
+
+Mass Used: 293.4260793396011 kg
+Launch C3: 85.73896229431361 km²/s²
+||V∞_in||: 1.3944111019260817e-5 km/s
diff --git a/archive/ES_0.6803869295733185 b/archive/ES_0.6803869295733185
new file mode 100644
index 0000000..1eaaadc
--- /dev/null
+++ b/archive/ES_0.6803869295733185
@@ -0,0 +1,22 @@
+archive/ES_0.6803869295733185---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T11:12:24.203
+Launch V∞: [7.753011504532303, -7.448690841551544, -2.2886855155047714] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.13776054342628322, 0.1254400260044416, -0.09891851214249746] km/s
+ V∞_out: [-0.09254461101598126, 0.18597227652053017, -0.036695241905476] km/s
+ time of flight: 9.145638397104925e7 seconds
+ arrival date: 2027-04-01T23:45:27.203
+ thrust profile: [1.0 -0.5417574792200026 -0.5005663865653492; 0.5395345088922036 -0.03819926434000146 -0.42316332421253083; 0.09861588133308272 0.012328805151810415 -0.12288243025129011; 0.052292607990063675 0.011898638047189722 -0.0806883789737686; 0.03969818013780405 0.011585763353772887 -0.07125002873293274; 0.020081690665499478 0.007108642558477181 -0.04077987877523004; 0.03259322708000775 0.012196910085756237 -0.07106856535638759; 0.005711832495569636 0.0021759788734811475 -0.011692838863840876; 0.0007129902894058415 0.0007248422260323204 -0.0034986080401487535; 0.0029847024776707455 0.0013851358376751376 -0.0010288913202826698; 0.0019267966205006853 -0.0004340757570869985 -0.0023852937488416034; 0.0016762837703812785 0.0002662858536970127 -0.0025025324670374643; 0.0003319527818467446 0.0006839827200908184 -0.0020721746522562767; 0.0018925604247565318 -3.309941400399659e-5 -0.004182025877241216; 0.002661346486481313 -0.0003760523750599063 0.00016428447586968415; 0.0004127887080887225 -0.0013269624037917545 0.0008200244546461392; -0.0009630279334668562 -0.005090298210063301 -0.002362017443439141; 0.0005035744459656502 0.0001730480139484228 -0.0004554227165916452; -0.00010396544928169109 0.0014650645104928263 0.0005114771390838896; 0.004975995395897654 -0.0007773201941705767 -0.00022073361972671537] %
+
+Mass Used: 88.94154431958987 kg
+Launch C3: 120.83026403130543 km²/s²
+||V∞_in||: 0.21094558420025117 km/s
diff --git a/archive/ES_0.6811824241100768 b/archive/ES_0.6811824241100768
new file mode 100644
index 0000000..f937a17
--- /dev/null
+++ b/archive/ES_0.6811824241100768
@@ -0,0 +1,22 @@
+archive/ES_0.6811824241100768---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T15:17:28.971
+Launch V∞: [7.817866452884574, -7.520658303265274, -2.375547002680302] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.624063849667154e-5, -0.0009771358422098228, 0.00013850735208624065] km/s
+ V∞_out: [0.00029110016717572257, 0.0006470611692861397, 0.0006901232091621308] km/s
+ time of flight: 9.24500486489391e7 seconds
+ arrival date: 2027-04-13T15:51:36.971
+ thrust profile: [0.6615845131788229 -0.311172686836744 -0.30384181516351344; 0.3811606718427978 -0.02381907500774582 -0.304134427263579; 0.15556835285150178 0.020872445159921246 -0.19200263998358874; 0.07024365638378777 0.017206984036922092 -0.11703590303112357; 0.027699693160826842 0.008134170553162345 -0.05347791555241411; 0.02135134321042181 0.008256570702791002 -0.04616534740443849; 0.028780398649709237 0.007538772380815157 -0.06017310971629327; 0.024582765768783047 0.008884222091580875 -0.05488843751597826; 0.003391487062497753 0.002441640698925001 -0.01167000388773905; 0.0010500459959407022 0.00063314376898939 -0.0032794584052629064; -0.0012867252876175464 -0.0008634579828346477 0.005346351125888428; 0.0005916784564665142 -0.003727201576983321 0.001254105410010939; 0.002209186495697517 0.0007544673816816321 0.011055050751515244; 0.014130097217781521 0.009844741269399816 -0.008737097463172545; 0.0009954174927890645 0.004940938608920249 0.00033100757269674476; 0.0002937299181956867 -0.01259339142197654 -0.0256610647424269; 0.00487508780478994 -0.010856792111848281 -0.0020406134603098906; 0.0022636398609724717 0.001619398281858387 -0.002887735908095689; -0.012948063102404456 -0.013822563789556524 -0.0017008261968409113; 0.010896262236769058 -0.001588501731726967 -0.011339598413073252] %
+
+Mass Used: 75.33122374435607 kg
+Launch C3: 123.32256075155432 km²/s²
+||V∞_in||: 0.000989844116854478 km/s
diff --git a/archive/ES_0.6814305452844973 b/archive/ES_0.6814305452844973
new file mode 100644
index 0000000..94ddc5d
--- /dev/null
+++ b/archive/ES_0.6814305452844973
@@ -0,0 +1,22 @@
+archive/ES_0.6814305452844973---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T10:45:56.448
+Launch V∞: [7.794602140440913, -7.436334980628247, -2.343057777838724] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007087380072372034, 0.03803762452630273, 0.0067506026678326395] km/s
+ V∞_out: [0.03777003844550301, -0.0063883237014896385, 0.008669779062782162] km/s
+ time of flight: 9.122456200669667e7 seconds
+ arrival date: 2027-03-30T06:55:18.448
+ thrust profile: [1.0 -0.5542769539432936 -0.5286670388649761; 0.4508107927916041 -0.031734626538403705 -0.36428135881921914; 0.12889679078247773 0.015651768358462968 -0.14848264029038824; 0.11045671537532341 0.026586050576497156 -0.1568877355992529; 0.02223349712087855 0.0067768568665033295 -0.038912395058689; 0.005282743344274823 0.001902394924212048 -0.0106243098941309; 0.0033717712732511656 0.0011535435616990806 -0.007033508898372596; 0.005624262542697518 0.0023343889448274287 -0.012361630304454101; 0.0022154803322749534 0.0008594701780994529 -0.005129897166544834; 0.0020692915786236876 -0.001482914769869054 -0.005612416084757394; 0.00031516042260717005 -0.00027051894054576126 -0.0023348636689896327; 0.005377364937359188 0.001805761541073337 -0.0009711773442649989; 0.003644918989788571 0.0018778493579248152 -0.004832145049590662; 0.0010031204639671452 0.0003036790045238499 -0.001902309648977084; -0.00034754704056699087 -0.0002056839308862135 -0.0041469395266445965; 0.005708620076666531 0.00034315075195905125 -0.0006509524757100419; -0.0007491918057102168 -0.0032956630902875976 -1.6256518005564307e-5; 0.0014541698829108284 -0.0023213049878055498 -0.0014028054607864032; 0.001467223242682592 0.0029409779138321736 0.0018551507787965757; 0.008123518899054173 0.001500734838224051 -0.002401403297051798] %
+
+Mass Used: 85.99085153591068 kg
+Launch C3: 121.54482022217192 km²/s²
+||V∞_in||: 0.039276742129066566 km/s
diff --git a/archive/ES_0.6815505451666272 b/archive/ES_0.6815505451666272
new file mode 100644
index 0000000..5fbcd9b
--- /dev/null
+++ b/archive/ES_0.6815505451666272
@@ -0,0 +1,22 @@
+archive/ES_0.6815505451666272---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T13:48:17.557
+Launch V∞: [7.868337294424175, -7.259155414140317, -1.9906463928067133] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.9117346908241589, -0.771718075837648, -0.0968897575191693] km/s
+ V∞_out: [1.15093596345884, -1.05624128172864, 1.1502351564014097] km/s
+ time of flight: 9.366120007219455e7 seconds
+ arrival date: 2027-04-23T14:48:17.557
+ thrust profile: [0.6197745382052957 -0.28282438606536225 -0.25913185587837706; 0.43860505473115863 -0.006602983068086598 -0.30942888854923334; 0.42183002296824834 0.07544448129428319 -0.39323760226810767; 0.21102586847047336 0.0713132609215991 -0.2578915880360795; 0.23178225374600994 0.07995766900699294 -0.3117883098713774; 0.07162308432795604 0.033430276657136326 -0.11784946273346694; -0.0003098588328845082 0.0005646616465135317 -0.002468660906805701; 0.00044615671487863027 -0.0001891405433689538 -0.0004567532082886465; -0.0008182859531465106 -0.00039134698154167887 0.0005714784955626397; -0.0011256709858114028 -0.0013255069205780946 -0.0009422256315644916; -0.0007783513071174455 -0.0008188422200890118 0.0005940626645989992; -0.0022818825465138826 -0.0012288204454240796 -0.0017298580646954817; 0.0005977423984600423 -0.0014623777625370528 0.0017904193867319385; -0.00013372414133015244 -0.0007492540878156124 0.0005122981639213444; -3.999103209321206e-5 -0.00101264775942944 0.0022210164115680844; -0.00036527683366266276 -0.0004979078380243377 -0.005604394701730064; 0.0032384796846315887 0.0012560567285475142 -0.0068163846429481565; 0.0018444377283112839 0.003231245124140633 -0.004717616387934165; 0.004035397746783101 0.0023708134727853133 0.003570971186671152; 0.006652566961984225 0.0010032774806100705 -0.00029991300441304004] %
+
+Mass Used: 103.49130672219508 kg
+Launch C3: 118.56874216666341 km²/s²
+||V∞_in||: 1.198414185554773 km/s
diff --git a/archive/ES_0.6816692038021889 b/archive/ES_0.6816692038021889
new file mode 100644
index 0000000..b1f2741
--- /dev/null
+++ b/archive/ES_0.6816692038021889
@@ -0,0 +1,22 @@
+archive/ES_0.6816692038021889---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T11:15:56.270
+Launch V∞: [7.625152997322286, -7.890284711766156, -2.465173393434745] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.5979478744996065, -0.6492403979164014, -0.3922831781744543] km/s
+ V∞_out: [-0.7128042775050459, 0.4870874824459631, 0.4211126686654931] km/s
+ time of flight: 9.217783211455722e7 seconds
+ arrival date: 2027-04-14T08:13:08.270
+ thrust profile: [0.7602922230815048 -0.41426653463328444 -0.39990072214811506; 0.18381586538257452 -0.027821847983763196 -0.18769184496358426; 0.05931125053792925 -0.00031022160271070964 -0.09783682385053614; 0.017142712519336245 0.0010401281407500245 -0.0336383114285484; 0.024030447862974758 0.0018083194768772418 -0.05329350825438067; 0.00988887248087716 0.0011278899109990808 -0.025355906829811533; 0.009081330703317727 0.0012150403591114816 -0.02551994481149338; 0.004821995139499909 0.0004403092768766565 -0.01432654142697021; 0.0010165708911806445 0.0004655004886763548 -0.002639687566147089; 0.001544190131946642 -0.00029253601722676334 -0.002103854278358421; -0.00043661230755080694 -5.393451814578312e-5 -0.0015019949837233797; 0.007092488576852859 0.0010071785194379072 -0.0009437228060876802; -0.0013376098570793181 -0.0009605650108825189 -0.0005846488145562975; -0.0069653888499378435 0.0011386688394844587 -0.005033138915115938; -0.0003979592432314808 -0.00042664282204371833 -1.960594976062411e-6; -0.004026226643942143 0.007173453710356757 -0.008529869955457698; -0.0017115582688728586 0.00514930769482628 0.001743908169016854; 0.0015912504369901914 0.006155627390742258 0.0009209930320859621; -0.003385383177233774 -0.008618099060414821 -0.0010336358911034102; 0.008847560716199122 0.0045823517806805 -4.936114075398306e-6] %
+
+Mass Used: 57.50039070670664 kg
+Launch C3: 126.47663092500234 km²/s²
+||V∞_in||: 0.9658886306318628 km/s
diff --git a/archive/ES_0.6816999581128896 b/archive/ES_0.6816999581128896
new file mode 100644
index 0000000..9019df2
--- /dev/null
+++ b/archive/ES_0.6816999581128896
@@ -0,0 +1,22 @@
+archive/ES_0.6816999581128896---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T08:48:01.200
+Launch V∞: [7.668143456203273, -7.649583632146831, -2.349081360633043] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.14135544718062037, 0.2624079233935797, -0.3299056260259291] km/s
+ V∞_out: [-0.22096992508343816, 0.25486978389350995, -0.2894537400269836] km/s
+ time of flight: 9.176966546778019e7 seconds
+ arrival date: 2027-04-07T12:22:26.200
+ thrust profile: [0.9774152516877095 -0.48611449661718986 -0.4652948073319081; 0.3062167969692634 -0.03803339153333424 -0.2778282025898541; 0.12329095919556586 0.005822672506839094 -0.16195669684087338; 0.03785313376639648 0.005618197390070375 -0.064101056427681; 0.03564627071694385 0.007417378969420683 -0.07003081133196258; 0.005238510916345574 0.002398344130696724 -0.013090620023500175; 0.007390925480221037 0.003013773081080946 -0.013657704660812772; 0.00986812503103174 0.002282746005465675 -0.019074386488871775; -0.00241119378003128 0.004455321804539217 -0.010758872147368264; -0.0008693340394546111 -0.0075749614380778915 -0.012648112145773202; 0.0010683179525215157 0.004831059980126539 -0.011125864635870696; -0.0030416172256957333 0.006360353471929546 -0.004684575568406413; 0.00519246368150721 0.0032442575423355293 -0.018373513631207126; -0.0033069613661117795 0.0003427468860194287 0.0007888643112282379; -0.012373119369010968 -0.0008582770645143626 -0.008052421744210048; 0.005518939650617621 0.011382433734539177 -0.004613542826165827; -0.005992295245993632 0.002868893713864399 0.012826093182082388; 0.0007884962202395259 8.715211318341279e-5 0.009422014410716696; -0.001671733759304631 0.0032820321592984944 0.0032436947835677975; 0.0031824418986751003 -0.009627390750304861 -0.014820374114463323] %
+
+Mass Used: 78.7806516792316 kg
+Launch C3: 122.83473704899536 km²/s²
+||V∞_in||: 0.44460881996528606 km/s
diff --git a/archive/ES_0.6822394363533053 b/archive/ES_0.6822394363533053
new file mode 100644
index 0000000..01565fb
--- /dev/null
+++ b/archive/ES_0.6822394363533053
@@ -0,0 +1,22 @@
+archive/ES_0.6822394363533053---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-06T18:08:37.059
+Launch V∞: [8.330593216100656, -7.373188211464181, -0.792015035216008] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.183897192928887e-5, -9.639238620608787e-6, -7.64444099643253e-6] km/s
+ V∞_out: [-1.4656413992252486e-6, 1.0960505287374608e-5, -1.2997710123785488e-5] km/s
+ time of flight: 1.874957778751348e8 seconds
+ arrival date: 2030-05-16T20:18:14.059
+ thrust profile: [0.0015711959672841612 -0.0013559658990181247 -0.001236504498562517; 0.014232717230222547 -0.033027670714973666 -0.028637734735745945; 0.018522010635571788 -0.05686145821846088 -0.0499349055006167; 0.04353390581791822 -0.13179998433140014 -0.11173063338870293; 0.03448989609590799 -0.09172219273292151 -0.08143909749248873; 0.056355953746159176 -0.14295823598437266 -0.12811423060559146; 0.03667048887537307 -0.08619895638012974 -0.07948629183171609; 0.023883622764208867 -0.05216972729762638 -0.0492379746833267; 0.01351866617716842 -0.02752436993441589 -0.026852595726665093; 0.009829132079396875 -0.018513359441684977 -0.018389520734572885; 0.0020403388533876206 -0.004224348189974316 -0.0061050750230524226; 0.004900860653955615 -0.004155713888710896 -0.0034480565456519903; 0.0015658865296962522 -0.0025713072772885477 -0.0031003784296287163; -0.00018687359061966358 -0.0030612866286395834 -0.0013546065089139134; -0.0007642047735673938 -0.0009526849657002503 -0.0038294733338663; -0.00044430553331317735 -0.006072260530905209 -0.001945276530345394; -0.0014714990441768716 0.0009653465817501029 0.003772818154904503; -0.0015960469545140722 -0.0033958634087623485 -0.0018276481756078857; -5.91411390321768e-5 -0.0010147364410716632 -0.00017132261299868893; 0.00041320778142633127 0.0003494895649835787 -0.0002692550761187952] %
+
+Mass Used: 70.33781837154447 kg
+Launch C3: 124.38997554982487 km²/s²
+||V∞_in||: 1.7073770985797605e-5 km/s
diff --git a/archive/ES_0.6828275233522477 b/archive/ES_0.6828275233522477
new file mode 100644
index 0000000..908ac3f
--- /dev/null
+++ b/archive/ES_0.6828275233522477
@@ -0,0 +1,22 @@
+archive/ES_0.6828275233522477---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T03:12:25.628
+Launch V∞: [7.998535529077012, -7.541172776174834, -2.576657928933158] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.09492316358393459, -0.2559539867299974, -0.336326566663287] km/s
+ V∞_out: [-0.38751306808971847, -0.05708905700298076, 0.18491609370362494] km/s
+ time of flight: 9.138229647842924e7 seconds
+ arrival date: 2027-04-01T19:10:41.628
+ thrust profile: [0.5490785432080668 -0.24208002495933836 -0.25885215249860904; 0.23134286211725955 -0.018246489585148715 -0.21860821364408223; 0.10766216372321885 0.01126456228978453 -0.15352890473636124; 0.05937338059967415 0.012153728917313929 -0.10635493845837271; 0.03786663788168918 0.010394508296298437 -0.07996601162579219; 0.014714499197156254 0.004879481601016414 -0.035144326747693626; 0.0069899366590451045 0.0022622807936178643 -0.018987610329703267; -0.0005594140485678578 -0.00038612670796730455 -0.0008792515493174013; 0.0019739438057054456 0.0006024392285906455 -0.005918700140137821; 0.001719716289766041 0.0003291818731197988 -0.0023192881093853815; 0.0003388192837402009 0.0003106889576490891 -0.0014807661661823967; 8.458136741032148e-5 -0.0003666242579711997 0.00033103931985351486; 0.0004972583180755962 -1.982074819772747e-5 -0.0008220313857503549; 9.077090393411614e-5 -0.00026087899682644396 0.0010690787835476085; -0.0007612068836347389 -0.000981051962399469 -0.0016744416163673522; 6.525206997080944e-5 1.7049279265357766e-5 -0.000218420833538013; 0.0005733523031856031 -0.00011963257886019794 0.0005610762238135112; 0.0003032372183514136 3.4516769863246374e-5 -0.00025769807276674104; 0.002084364648118615 0.0009148783806494816 -0.0023329079085040935; 0.0013054283513340204 0.0036803823393738912 0.001097393201491497] %
+
+Mass Used: 52.96947330317835 kg
+Launch C3: 127.48502353276183 km²/s²
+||V∞_in||: 0.43317249422288634 km/s
diff --git a/archive/ES_0.6831537037407742 b/archive/ES_0.6831537037407742
new file mode 100644
index 0000000..00304a8
--- /dev/null
+++ b/archive/ES_0.6831537037407742
@@ -0,0 +1,22 @@
+archive/ES_0.6831537037407742---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T14:33:01.548
+Launch V∞: [7.8513575734657355, -7.602513719801059, -2.6868423361473033] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002082043515547004, -0.002584029428474327, 0.0006715684631797353] km/s
+ V∞_out: [0.0008480424434961076, 0.0019120415005193386, 0.0016726136679616108] km/s
+ time of flight: 9.349802778417546e7 seconds
+ arrival date: 2027-04-26T18:13:28.548
+ thrust profile: [0.4477267918633286 -0.22560071922700875 -0.2415307275335546; 0.21117820013461183 -0.017028483016325893 -0.20092425126934899; 0.08816549556736515 0.009504611682503184 -0.12454354990149617; 0.025494386439283118 0.00426045953843867 -0.044611143720467074; 0.03151738074309598 0.008028310347806426 -0.06458242815481884; 0.02158000616562885 0.0062684205609285035 -0.05098997723880399; 0.014551059903930167 0.004871649355368282 -0.03951952407992012; 0.008269231452043207 0.002697265163780804 -0.02289386596448076; -0.014811329734150783 0.00944983250864162 -0.004281114595087194; -0.006799211253913753 0.009880587421008964 0.009133327212245546; -0.00011844311110217952 -0.004172541010199485 0.014587302631566674; -0.01751189619996003 0.002437612057268078 -0.004902653587968521; 0.001348680460978113 -0.00914552443308113 -0.014377606480549518; -0.012287022090643949 -0.0011183124731780029 0.01649115994366382; 0.01783258823597713 -0.00864774244770922 0.014441789845043646; 0.004883710607488297 -0.0019946468036877805 0.003884647572236189; -0.02247589066767851 -0.0006131261047019756 -0.027402202183733296; -0.0048703634509017334 0.008128148089329735 -0.009355364806249628; 0.033194869887361755 0.0029528453039102047 0.032821590509181854; 0.030759497788872808 -0.04192387194421562 0.06500341985119619] %
+
+Mass Used: 58.155932348851366 kg
+Launch C3: 126.6611523454946 km²/s²
+||V∞_in||: 0.002677977098476621 km/s
diff --git a/archive/ES_0.6834434048305029 b/archive/ES_0.6834434048305029
new file mode 100644
index 0000000..97cac91
--- /dev/null
+++ b/archive/ES_0.6834434048305029
@@ -0,0 +1,22 @@
+archive/ES_0.6834434048305029---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T08:15:06.141
+Launch V∞: [7.59098802226239, -7.812513262799189, -2.345470953972569] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.5270642955342113, 0.5165113462232142, -0.3739919691094354] km/s
+ V∞_out: [-0.6027456140190135, 0.45246649822184143, 0.34114078965890304] km/s
+ time of flight: 9.473974748275372e7 seconds
+ arrival date: 2027-05-12T20:50:53.141
+ thrust profile: [0.5599871484971836 -0.30409889150806024 -0.3241938163342637; 0.11719770242823017 -0.019553333272717098 -0.14155084886625524; 0.11131546599543737 -0.00033541427083726844 -0.19607051564686648; 0.049257979341769446 0.0012622362174785663 -0.11174744585177525; 0.027073918028667914 0.001552036550471654 -0.06761390770805034; 0.05146242928411106 0.006379165061573916 -0.15280780821415993; 0.019937393732184987 -0.002233771492583818 -0.06892863783386066; -0.0051718318432913 0.00162638578358399 0.007715656439229526; -0.007506942374617874 0.0029659193472898137 -0.001429168583219679; -0.004171760952285092 0.0014175463752101145 0.009053880799086278; 0.0014247613303332443 -0.0006851511038573734 0.0259368132936346; 0.003336108433254481 0.012223909636320404 0.008034736196410751; 0.0361868157414465 0.011812489713567943 0.0201361363510891; -0.012775300952642238 0.03226329401169448 0.006537815080139899; 0.00042023832811172065 0.0026610718916525583 -0.01957158116506934; -0.010038804929760161 -0.0077906209470770815 -0.008152325937402664; -0.04933427385131928 0.03079379278398159 0.0004067777523094683; 0.03675626951145714 -0.0440583396452889 0.035537572438408806; -0.051679787987998695 0.012694419081706798 0.05300337312766463; -3.1320811224403304e-5 0.00043163987623013944 -0.0012465942756837872] %
+
+Mass Used: 73.08574195199253 kg
+Launch C3: 124.15969663147328 km²/s²
+||V∞_in||: 0.8273153784154168 km/s
diff --git a/archive/ES_0.6834714466572724 b/archive/ES_0.6834714466572724
new file mode 100644
index 0000000..5d89d07
--- /dev/null
+++ b/archive/ES_0.6834714466572724
@@ -0,0 +1,22 @@
+archive/ES_0.6834714466572724---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T14:46:36.217
+Launch V∞: [8.022060022486338, -7.469736400904679, -2.6966679944970453] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0001675211800719599, -0.002053598568068577, 0.0005525924731345358] km/s
+ V∞_out: [0.0006313116857898493, 0.0014448753850232034, 0.0014370079841136436] km/s
+ time of flight: 9.109214481577043e7 seconds
+ arrival date: 2027-03-28T22:09:00.217
+ thrust profile: [0.571760613434047 -0.2980490502005914 -0.2726611287007519; 0.32783635207430833 -0.022458581110265288 -0.25829445759844266; 0.14835874203000085 0.01891283506662272 -0.17096660125958021; 0.03449916900406163 0.008452838233560127 -0.05329352335672431; 0.009225830753682704 0.0029097692026193904 -0.017124142506184457; 0.014194891425759635 0.005099181783952624 -0.029053855125796137; 0.004865340489172339 0.0019547013100804783 -0.011081861300468373; 0.0003628959484519342 0.00022152707365017947 -0.0007247605685957194; 0.0004423533607842887 0.0003276919855285497 -0.0008405525230968031; 0.00033616419912612934 0.00023385749403464573 -0.001283236919672423; 0.0009589250910261086 -0.0001743134792772241 -0.0010394963993658143; 0.0005862285943905844 0.0004255939235704714 -0.0025173547387020434; 0.0010457572747450605 0.0006828338774530911 -0.001886728527886754; 0.0003156329083397781 0.0013814836712011964 -0.0010329797249855298; 0.00013750505927646048 8.717400623289872e-5 -0.0003912350171189474; 0.00027045600664110604 0.00011116556991674201 -0.0006579900517029059; 0.00032595188471336284 0.00030894988916536806 -0.001118606019276776; 8.204358064490851e-5 -5.846533004689089e-6 0.0013773796342068448; -0.0012367288781336403 -0.0016408682439895464 -0.00027384843946608173; 4.5792373526822115e-6 -5.253194932580197e-5 -0.0001642777558049604] %
+
+Mass Used: 54.085862573959275 kg
+Launch C3: 127.42242717591861 km²/s²
+||V∞_in||: 0.002133234367319014 km/s
diff --git a/archive/ES_0.6845074374455145 b/archive/ES_0.6845074374455145
new file mode 100644
index 0000000..7c9205d
--- /dev/null
+++ b/archive/ES_0.6845074374455145
@@ -0,0 +1,22 @@
+archive/ES_0.6845074374455145---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T04:46:11.854
+Launch V∞: [7.811415301415785, -7.5005963184927555, -2.3182456630211132] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.009352276081914777, -0.06642997553905172, 1.273823811692871] km/s
+ V∞_out: [0.1844727669477199, -1.193119021818638, 0.011695942560325802] km/s
+ time of flight: 9.068760019121075e7 seconds
+ arrival date: 2027-03-24T19:46:11.854
+ thrust profile: [1.0 -0.5697821104281386 -0.5319814027050159; 0.3897573358084227 -0.030007343218952695 -0.3278854900783721; 0.13450222442298115 0.015284247527712846 -0.16608698363673885; 0.053064641928233076 0.011225845012553016 -0.08345686591635369; 0.02362212295515599 0.006055281095491356 -0.04392313318083971; 0.01928150195820302 0.006253247942097038 -0.04122467585305669; 0.011913340448508952 0.003933918463115343 -0.027172196130567892; 0.007101865131323272 0.00312518388093312 -0.017437312296256276; 0.0014682685693042374 0.0005528334541678608 -0.002926845934399714; 0.0022558916477403547 0.0004942399339230388 -0.00446888016863304; 0.007458007215768111 0.0021867133733345753 -0.007989108165793917; 0.0003865081954440828 -0.0013032007469928365 -0.005314540384789194; 0.0005265776728903757 0.00040092871820131775 -0.002559735989604354; 0.0015038211664969092 -0.0003116397018094045 -0.0031576286635783997; 0.0005005179668401019 0.0006272146114250758 0.00294969514522247; 0.005628523411801015 0.0004965929528383791 0.0014555163908228502; -0.005854594560826916 0.0029811398352218 -0.001250957157243377; -0.0027188956651292805 -0.002130217240655573 0.004613081457472867; -0.00024778454653148155 -0.00023515215288384878 0.00028996450774716883; -0.004511495989567369 0.0026625529418118983 0.010659200260377824] %
+
+Mass Used: 83.12541061304046 kg
+Launch C3: 122.65141709829595 km²/s²
+||V∞_in||: 1.2755890835036912 km/s
diff --git a/archive/ES_0.6853870973846712 b/archive/ES_0.6853870973846712
new file mode 100644
index 0000000..01a07f0
--- /dev/null
+++ b/archive/ES_0.6853870973846712
@@ -0,0 +1,22 @@
+archive/ES_0.6853870973846712---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T06:29:32.373
+Launch V∞: [7.863725115208858, -7.8783301156769445, -2.7006711482371144] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004576796032011638, -0.024433827949741627, -0.004422769667686998] km/s
+ V∞_out: [-0.024455393755736802, 0.0035054988447450436, -0.005328707829777568] km/s
+ time of flight: 9.118450758165744e7 seconds
+ arrival date: 2027-04-02T15:31:19.373
+ thrust profile: [0.438184424695412 -0.22597890052798883 -0.21483045088337127; 0.1036569274010868 -0.012414636926521732 -0.09833596880743063; 0.07166053509363511 0.0027470128302409347 -0.09558502049535976; 0.023400877836032005 0.0027410423712635823 -0.03848132273823666; 0.017064419438853867 0.0011365547546119165 -0.030851349706312384; 0.005884886671135604 0.0014645125781934578 -0.011888129782538906; 0.003803313805523722 0.00011411820396522944 -0.00550537094610537; 0.0069475580606533065 0.0013443265319513275 -0.006822214254043328; 0.0011707218939655015 -0.001382668454093122 -0.0059087131608338865; 0.0001840396443671731 -0.0009449759333196594 -0.0030137445944986695; 0.0011559631311293588 -0.0005256382382356197 -0.003385338503197481; 5.3830812395110755e-6 0.0012242637921897523 -0.0012791301770355016; 0.0008071146383538332 0.00016228371728074396 -0.001911435786629973; -0.000511271943044444 -0.00015832522727240355 -0.00011963023566503557; 0.002300327280320531 -0.000683245966603345 -0.0035470910065501975; -0.00016471948358771481 0.00038128672731237113 -0.0010598620346073066; -0.0011539705992093764 0.0007418828877482266 -0.0001060582243998633; -0.0017558461941497483 -0.0011671189748643342 0.0003682544360878367; 0.001752147856555261 -0.0009339353847213293 -0.005404244544762975; -0.0006609075853724125 -0.0010616582491507261 -2.401700948073812e-5] %
+
+Mass Used: 34.28563090671241 kg
+Launch C3: 131.19988275006924 km²/s²
+||V∞_in||: 0.025249156455803126 km/s
diff --git a/archive/ES_0.6857758466052526 b/archive/ES_0.6857758466052526
new file mode 100644
index 0000000..ae76119
--- /dev/null
+++ b/archive/ES_0.6857758466052526
@@ -0,0 +1,22 @@
+archive/ES_0.6857758466052526---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T02:04:01.288
+Launch V∞: [7.867717718342373, -7.56208660602346, -2.6261941306898104] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.4010040676589095, 0.4879536080544077, -0.5121324773512056] km/s
+ V∞_out: [-0.41501341953376636, 0.47845457620790716, -0.5099078103590711] km/s
+ time of flight: 9.02044767969345e7 seconds
+ arrival date: 2027-03-20T02:51:57.288
+ thrust profile: [1.0 -0.5290835101593986 -0.4957093148671327; 0.2767496649466696 -0.02647427689720853 -0.21367883578980826; 0.03832947945571593 0.0038585209303283238 -0.04323070525081332; 0.026146572310375534 0.005500558376851795 -0.036913751120010246; 0.010463158371771052 0.003271699206020538 -0.018668885812977192; 0.005351022030085871 0.0011921455679620393 -0.012613440176589934; 0.0014853844512788031 -0.00011209434796565008 -0.006486520570849907; 0.0046678417676476415 0.0021047277539842347 -0.011864120989095025; 0.0027902788089901416 0.0007849167500804924 -0.00548768005151196; 0.003138932472014253 0.0016185585882225672 -0.008699388613193686; 0.003056477331033569 0.000801838890297039 -0.010445460400713376; 0.0007820371817124343 0.002116171506026104 -0.0038079939053095183; -0.0003083764825585092 0.003176684713253478 -0.005119388843815098; 0.0009284062131513808 0.00047768842135761415 -0.0035376730666783424; -0.002952881145112147 0.0014100561486808123 0.0010830265244265265; 0.005363221448000523 0.0009722543513236829 0.002109848763590448; -0.005991974565597516 -0.0013316094468196094 0.005972503525810138; 0.0012109989791442071 -0.00014289029787553122 -0.0051505531540916956; 0.0025645676475386852 0.0016992331616538891 0.00044706078703376714; -0.0006333724426979817 -0.001958874075204213 -0.0024759513879500043] %
+
+Mass Used: 65.170803696034 kg
+Launch C3: 125.98303154458753 km²/s²
+||V∞_in||: 0.8131313917505515 km/s
diff --git a/archive/ES_0.6858417649878312 b/archive/ES_0.6858417649878312
new file mode 100644
index 0000000..ed71a4a
--- /dev/null
+++ b/archive/ES_0.6858417649878312
@@ -0,0 +1,22 @@
+archive/ES_0.6858417649878312---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-03T18:20:52.496
+Launch V∞: [7.892969492094258, -7.081718308810295, -2.3066961877852914] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.3708558963412957, 0.3217802763799994, -0.2533776626672232] km/s
+ V∞_out: [-0.1844288552259729, 0.36874217095589146, -0.07416116986325845] km/s
+ time of flight: 9.290500962298322e7 seconds
+ arrival date: 2027-04-14T01:17:41.496
+ thrust profile: [1.0 -0.5171639843414151 -0.4632184023299217; 0.677354152959613 -0.0023736892642740154 -0.47184692685505325; 0.2944251639898682 0.062359239601729115 -0.2936455912527564; 0.15344466736548917 0.052510692652233744 -0.19357381568170293; 0.09181879437324565 0.039616263571429215 -0.13672294149666947; 0.013197970072764855 0.0060348405872177185 -0.022454895287219653; 0.0067501820005945005 0.003353281853227112 -0.012224150998710635; 0.0008869476707827713 0.0003419908271721675 -0.0042995863374537145; 0.004792409373843026 -0.0015354931777258087 -0.004561836473991638; 0.004894254820022507 0.0005793919797184756 0.0038576235454255924; 0.002107992708890463 0.0004952588473626275 0.0010183675064626778; 0.009095101195885434 -0.0054214814404638795 0.0014484093206271597; -0.0014583121684496542 0.0004930888607555086 -0.002118038666748842; -0.0018749097116143461 0.0013952828059530594 0.0013534886627380289; -0.0015471128738759558 0.00314218393693392 0.000772490864285482; 0.024797052233997266 -0.007151434587658643 -0.0074121197747045; -0.0021741767763410595 -0.0020297731431972647 -0.008663077978227629; 0.006197088888000133 0.003948735881815922 0.013805551896143374; -0.005976695085116194 0.0069264980759581474 -0.0030137968852411955; 0.025891734472160952 0.014473400266797332 -0.010907388885778717] %
+
+Mass Used: 113.15385717039499 kg
+Launch C3: 117.77054891121281 km²/s²
+||V∞_in||: 0.5525186712293078 km/s
diff --git a/archive/ES_0.6861538361898801 b/archive/ES_0.6861538361898801
new file mode 100644
index 0000000..761aee6
--- /dev/null
+++ b/archive/ES_0.6861538361898801
@@ -0,0 +1,22 @@
+archive/ES_0.6861538361898801---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T11:04:39.519
+Launch V∞: [8.071491870274965, -7.072504013910246, -2.4901336475937956] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.1311916029574951, 0.251486830000325, -0.30543272255493964] km/s
+ V∞_out: [-0.20065551897692882, 0.23926098666432566, -0.27592721732140746] km/s
+ time of flight: 9.213641262254673e7 seconds
+ arrival date: 2027-04-05T20:31:31.519
+ thrust profile: [1.0 -0.5283638460815246 -0.5020080633046383; 0.4162801239264146 -0.017595191085143087 -0.3374354287904418; 0.23449120558306497 0.042485708151565375 -0.26409884913877896; 0.08860253629413571 0.02809778728659519 -0.12565231283966172; 0.04844525356424377 0.019674690880207544 -0.07933134600538758; 0.035564500850756145 0.01662273722736013 -0.06518240073660173; 0.009018700569822116 0.005015170538105535 -0.018461830398159858; 0.004652613199959003 0.00261419238090317 -0.010507737540062548; 0.0036977302827152932 0.002314138389527311 -0.007655396717053481; -0.0001528650206172442 0.0003566408246411854 -0.000737666812339564; -4.495963904917275e-5 -0.0006428666460734158 -0.0009491974562195389; -0.0003522078958977323 1.864178733892763e-5 0.00032870646739213; 0.0011693427690427504 -0.0006715547022149704 0.001836288901691826; -0.0004522274699600595 0.0017890532929702406 -0.0003624319239494255; -0.002660558028087545 -0.0023411517196316256 -0.000359391215637655; -0.0008476744831118311 -0.002381800850602179 -0.0025310885827445006; -0.0008757510560695952 -0.00019077613789678902 0.0033181249406399427; -0.000352941348298586 0.0008797972748779762 0.0013471425619706757; -0.0006509420232980812 -0.0006230452994318351 0.0012700655711361465; -0.000575179790049739 -0.0017219541548875038 -0.0023892628925171666] %
+
+Mass Used: 92.52079442903414 kg
+Launch C3: 121.37005962157018 km²/s²
+||V∞_in||: 0.4168285143287251 km/s
diff --git a/archive/ES_0.6861974405593663 b/archive/ES_0.6861974405593663
new file mode 100644
index 0000000..34ec44b
--- /dev/null
+++ b/archive/ES_0.6861974405593663
@@ -0,0 +1,22 @@
+archive/ES_0.6861974405593663---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T09:35:19.018
+Launch V∞: [5.877244165717691, -8.820425024030643, -2.6139141502805963] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00011974994022153025, -7.5162427813695e-5, -0.00011527609095929142] km/s
+ V∞_out: [4.0404185029948734e-5, -0.00012265941200248191, 0.00012887982908016453] km/s
+ time of flight: 1.0138000682945055e8 seconds
+ arrival date: 2026-07-10T18:42:05.018
+ thrust profile: [0.393496091314075 -0.3105810442871079 -0.2302350662665042; 0.22403011165185077 -0.05609583057619189 -0.20567590013985107; 0.09587270323783795 -0.009272840284947056 -0.12726676086158034; 0.05377820162480467 0.0037324408815057808 -0.09198868520515918; 0.09405965158362158 -0.005316828137046857 -0.14594386306686236; 0.02806599769931476 0.005200588307353554 -0.06610668895030437; -0.007043287833211349 0.018591848166237435 -0.01323095883728855; 0.0032094872942070233 -0.0024209817692276425 -0.01210032046302147; 0.010664831166833012 0.0027447130478019 -0.017476441512070246; 0.01956415558511213 -0.018079096139092213 -0.03706613174899969; -0.02518642859822714 0.010387184429287401 0.010955304890803869; -0.025559981565487777 -0.07066489831099529 0.0020221686106910667; 0.06634950569677223 -0.030726436850367186 -0.08736852585178477; 0.009021546348653054 0.046372175476460296 0.07644468600419926; 0.02853912315765047 0.01282852120778526 -0.009613118353803438; -0.007021907408808893 0.0032531530587101456 0.013403425768231149; -0.0777706071287239 0.06263707082759964 -0.08864329263783846; -0.05455279898070775 0.08774603745901667 -0.016783020039990305; 0.022508326750788475 -0.1447428143833515 -0.1938081944520581; -0.164822951453936 0.1882425349611529 -0.15998337409045965] %
+
+Mass Used: 105.37942530982718 kg
+Launch C3: 119.17444377304574 km²/s²
+||V∞_in||: 0.00018242262985924694 km/s
diff --git a/archive/ES_0.6873427847798791 b/archive/ES_0.6873427847798791
new file mode 100644
index 0000000..a31369b
--- /dev/null
+++ b/archive/ES_0.6873427847798791
@@ -0,0 +1,22 @@
+archive/ES_0.6873427847798791---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:22:08.933
+Launch V∞: [7.331242604852995, -7.474919655703497, -2.1089469254703106] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.030121058513281028, -0.05344202168837886, -0.03909852589382159] km/s
+ V∞_out: [-0.05560896067419315, 0.04130464824863515, 0.022212210383379026] km/s
+ time of flight: 9.961267481567135e7 seconds
+ arrival date: 2027-07-04T16:33:22.933
+ thrust profile: [0.7949014087162942 -0.40555716987233964 -0.4161723229036039; 0.3465952325537939 -0.022897310811469264 -0.3325358321098495; 0.17974506464346185 0.021627115423354253 -0.24860396210188807; 0.11583809694121688 0.026595517089280124 -0.20295581804340895; 0.05330536512710664 0.007198162418900205 -0.08642356189338221; 0.023386145686500198 0.0047777081030159615 -0.01407716410055461; -0.006488410004231935 0.047187235144850785 0.00018540429795734469; -0.033735218750137505 -0.016536832955279954 -0.011849269005262338; -0.00850714801796818 0.017302163468128257 -0.030387105691005428; -0.013051291263613174 0.008903488910888765 -0.00840332606060516; -0.016328231000346805 -0.05856362192016302 -0.004996719445584369; -0.007452578650226098 1.2950011448239563e-5 -0.017716831120360772; 0.1112918588331684 0.020012877866977884 0.025300780109785957; 0.08634823924466066 0.026609648522107166 -0.09502475593174332; -0.17434576314186473 0.06448064686546306 -0.01278554444235309; -0.057597541472953664 0.012198047716574312 -0.0760191937949915; -0.016209148825836316 0.002253304329369597 0.006129673460550581; 0.14173852521886254 0.028149821506297613 -0.18122120420804902; 0.10688837798191075 -0.06548505301732824 -0.028012286977000873; -0.060313073127808384 -0.04959670459607657 -0.15680075776970798] %
+
+Mass Used: 136.49625401469712 kg
+Launch C3: 114.06919912488489 km²/s²
+||V∞_in||: 0.07274628908179093 km/s
diff --git a/archive/ES_0.6876755502292476 b/archive/ES_0.6876755502292476
new file mode 100644
index 0000000..dc65cdf
--- /dev/null
+++ b/archive/ES_0.6876755502292476
@@ -0,0 +1,22 @@
+archive/ES_0.6876755502292476---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T07:18:34.632
+Launch V∞: [7.83480500373753, -7.39495071555031, -1.917705691443183] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.11723537754167992, -0.12572139250378467, 0.08156146310309263] km/s
+ V∞_out: [0.1770674659573756, -0.06418674051325113, -0.10958685043016349] km/s
+ time of flight: 9.10608881408819e7 seconds
+ arrival date: 2027-03-27T06:00:02.632
+ thrust profile: [1.0 -0.48947171715315385 -0.44594486784530857; 0.42784430596900924 -0.017152314279586474 -0.3358189678129328; 0.15085901273129687 0.021680677168124145 -0.1788867925116078; 0.15333962490283215 0.040745148395320716 -0.21943282220362098; 0.12828022707916167 0.044290944479624554 -0.2104974265818231; 0.059713378791557976 0.022662281590932074 -0.11515990127266797; 0.07849486161648059 0.03380991517064091 -0.16182955169516575; 0.0008739668437006551 0.0005165918445118634 -0.000840610622107341; 0.002563546034878843 0.0014748529942884155 -0.005708306105048175; 0.00011438535075134845 -0.0006052455036952742 0.00041892919701943317; 0.0018401299581911274 0.0002129902301665779 -0.003928358858602401; 0.0005439285470061055 0.0005769714816301077 -0.0003963291774916498; 0.002718397676833511 -0.00038991369280247487 -0.0004903327427389624; -0.0007050583166141421 -8.614581812378116e-5 0.0009737858520757916; 0.0029330771301563125 0.0034325611713649454 -0.005021587248865435; 0.0005451853329205724 0.0007522034350708109 -0.0016474737353944975; -0.0010732813783025119 -0.001974379639487942 -0.006937760467050767; -0.0002869365527567341 0.001917584577400831 0.0021400956953208415; -0.002332904374129743 0.003303819041393317 0.0026265918455476087; -0.004274218470062704 0.0027199779428728477 0.002942283695137979] %
+
+Mass Used: 103.76362146994234 kg
+Launch C3: 119.74706065100226 km²/s²
+||V∞_in||: 0.19026895317930367 km/s
diff --git a/archive/ES_0.687958926876987 b/archive/ES_0.687958926876987
new file mode 100644
index 0000000..2303178
--- /dev/null
+++ b/archive/ES_0.687958926876987
@@ -0,0 +1,22 @@
+archive/ES_0.687958926876987---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T06:02:40.265
+Launch V∞: [6.1372054463270755, -8.918932702575496, -2.309525987183858] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0028593328063616524, 0.0016427211447748984, 0.003133225866703539] km/s
+ V∞_out: [-0.001483177488420643, 0.0031854469561977557, -0.0030047312240755455] km/s
+ time of flight: 9.062794080308144e7 seconds
+ arrival date: 2026-03-10T04:28:20.265
+ thrust profile: [1.0 -0.9145386163196588 -0.5656586212458321; 0.44418085240550154 -0.12940909027224928 -0.3319726968254414; 0.09859544401301315 -0.009757544365536152 -0.10359873565674337; 0.04206879601923489 9.550849539586607e-5 -0.0555466921923738; 0.010529433529815094 0.0007621018044157665 -0.01732269531556008; 0.0073949351185341895 0.000483273243373694 -0.01331074654946407; 0.006265239256216826 0.0004292446285205098 -0.011631668653614534; 0.007511659485892772 0.0005652346006230961 -0.01314036050142905; 0.002355644477894694 0.0025990014607329233 -0.0048450288163534245; 0.002630585824562286 0.0012623603519564689 -0.005020587428933922; 0.0010767233725411862 -0.00018760120441886543 -0.00728474930684179; 0.007450358695207681 0.005771100810910966 -0.016490543923077028; 0.002265436073435422 -0.000529611753764168 -0.018601516422222172; 0.002610812851073922 0.0018982478580823405 -0.006378398451395184; 4.858051479522153e-5 -0.0008239768172539595 -0.009105865979883995; 0.010537339623737277 -0.0012270624667501465 -0.0011545204517684985; 0.0015245342517857885 0.00339029070084881 -0.0033224252987602856; -0.00047140440843236814 -0.0019634682854474143 -0.005948292587885241; -0.009460364871436509 0.0015769985387983107 -0.0009574209913695998; 0.001826123811062535 -0.011382693753190034 -0.004659809033603844] %
+
+Mass Used: 87.76380577079772 kg
+Launch C3: 122.54656152897493 km²/s²
+||V∞_in||: 0.0045487823852990265 km/s
diff --git a/archive/ES_0.6880457644617323 b/archive/ES_0.6880457644617323
new file mode 100644
index 0000000..bf165e4
--- /dev/null
+++ b/archive/ES_0.6880457644617323
@@ -0,0 +1,22 @@
+archive/ES_0.6880457644617323---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-05T23:28:59.845
+Launch V∞: [4.92133727347306, -9.892471948189327, -2.2322835831428107] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.5801200430970507, -4.867335256364876, 4.958676710542138] km/s
+ V∞_out: [-3.523481834162395, -5.219830938062398, -2.2206691650033306] km/s
+ time of flight: 9.824039978278787e7 seconds
+ arrival date: 2026-06-16T00:28:58.845
+ thrust profile: [0.7879716057608156 -0.8962941759143015 -0.4729905046386906; 0.030789509260738552 -0.022922429537880568 -0.055047250981449594; 0.018925889785500572 -0.013705608334906512 -0.05074697730978915; 0.009950779329789619 -0.00769150671881571 -0.035478959848156695; 0.006589522886519628 -0.0056838819503513905 -0.03064829962801749; 0.003992613532832486 -0.003418497897709381 -0.020520267194971874; 0.0029468788255244635 -0.0029248204020003053 -0.016581552772319312; 0.004480570998701439 -0.004985415375105286 -0.027361771506134665; 0.0015313870122990476 -0.0021407235493407185 -0.0057625439200000555; 0.00022050490818358004 -0.00015263393811259642 -0.0005855155189844675; 0.00019934446592913743 0.0003975511424654588 -0.0013290586632107636; 0.0011492596380733445 -0.001414819718013292 -0.006090665835214448; 0.00018054396669180248 3.437324180688702e-5 -1.4015225776642642e-5; 0.001502245193681165 -0.0027675121677610427 -0.002940948978124848; 0.00048542052588825875 -0.0010216521222267201 -0.0009693741792017282; 0.0006789161513139507 -0.0005144746037804113 -0.0026764480620345334; -0.0008008038514829095 -0.0006314985168679613 -0.0019991191088830533; -0.0005836498191001073 0.0005858517138434094 0.0002489577612454359; -0.0008691974521130037 -0.0012718027158055804 -0.001976702733297161; 0.00043785976641995644 0.0005736741728062694 -0.00018107848593183545] %
+
+Mass Used: 61.5154230354392 kg
+Launch C3: 127.06365180055688 km²/s²
+||V∞_in||: 6.972515075776348 km/s
diff --git a/archive/ES_0.6886754602904747 b/archive/ES_0.6886754602904747
new file mode 100644
index 0000000..2d6dbae
--- /dev/null
+++ b/archive/ES_0.6886754602904747
@@ -0,0 +1,22 @@
+archive/ES_0.6886754602904747---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-20T14:03:41.243
+Launch V∞: [6.749624412743849, -9.016985497507932, -2.603338767542831] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01100018738433798, -0.008026294736605663, -0.017843908600638846] km/s
+ V∞_out: [-0.0032366070569698614, -0.02265294906598536, -0.0009581691364337954] km/s
+ time of flight: 1.0463834105186868e8 seconds
+ arrival date: 2027-09-13T16:16:02.243
+ thrust profile: [0.2761188120949253 -0.2241383183098992 -0.20581869073630826; 0.006888383129680059 -0.004631744204341435 -0.014296993809681384; 0.0035592311650235638 -0.0032471532730666114 -0.012873345893774656; 0.0030867086292827766 -0.003697108684399308 -0.015991031442761712; 0.004265689131767381 -0.005645289044087061 -0.025666584831095088; 0.0022499147314858636 -0.002980065078986946 -0.012584480115057842; 0.0018579822845899742 -0.003191027783827528 -0.013731081017367065; 0.001316274346136077 -0.0021013942164401847 -0.010965003419575034; 0.0011600182188745097 -0.002156787351962132 -0.009072700216328599; 0.001450133219944621 -0.003432321287246486 -0.015326625298161242; 0.00023893740250622664 -0.0007992628523805478 -0.0033223964569648427; 0.001585987045476292 -0.0007530894570642681 -0.002976414547039099; 0.0014072272564035 -0.000788867436255384 -0.0020931847013692323; -2.3914215722595483e-5 -0.00041003430641680923 -0.0020278086811062893; -0.0007021177525782152 -9.0470907466296e-5 -0.0008166797569615347; -0.002135120757780097 -0.0011951146108221146 -0.0016145647911763243; 0.0011067747114141 -0.004088434146154098 -0.0019579302961520413; 0.0002455526918071667 -0.00031000256978496506 -0.0017925713049667348; 0.0014523980318543336 0.0008807767021375688 -0.0014952176224469562; 0.0004843113738373021 0.00028612082549138305 -0.00010996452926445447] %
+
+Mass Used: 23.883195840743156 kg
+Launch C3: 133.64082991396754 km²/s²
+||V∞_in||: 0.022446171251181465 km/s
diff --git a/archive/ES_0.6896664611939396 b/archive/ES_0.6896664611939396
new file mode 100644
index 0000000..9ff86c6
--- /dev/null
+++ b/archive/ES_0.6896664611939396
@@ -0,0 +1,22 @@
+archive/ES_0.6896664611939396---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-06T16:25:04.530
+Launch V∞: [8.40424725320214, -7.220322395860943, -0.046238662645927985] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.067036564820903e-9, -5.664532894049517e-10, -6.237004445110744e-10] km/s
+ V∞_out: [-1.9522464422266538e-10, 9.429017257808772e-10, 2.4699791290054554e-9] km/s
+ time of flight: 1.8749577787221158e8 seconds
+ arrival date: 2030-05-16T18:34:41.530
+ thrust profile: [-0.0032981424696596298 -0.006549437120995297 -0.004246873407002484; 0.011685518230192999 -0.0007627939864180967 -0.001211402095556411; 0.0180482817723946 -0.05159952016511646 -0.044023501516438045; 0.052234894678826596 -0.14037814289383838 -0.12124856626833361; 0.060232039006434174 -0.1501390424846767 -0.13191002285290476; 0.07534837629730154 -0.1743405196985364 -0.1550641601264161; 0.06123761448404423 -0.1333497631686811 -0.12144367541612132; 0.02378284967265961 -0.04951670123578573 -0.04612514107306306; 0.015797845371769568 -0.0313328910302708 -0.029269879775496263; 0.008420489739899345 -0.015810178311234827 -0.014457932548281729; -0.0028471397011618645 0.0026181955187409363 -0.004948608537173333; 0.0048610048186172785 -0.008803651145295802 -0.006409917852099311; 0.0026740123045018447 0.0022664480049596693 -0.0022981077066319107; 0.0031964266475685787 -0.002288409054765808 -0.004640861436221063; 0.00036568177903223913 -0.0011721739598286487 -0.0005069468653802657; -0.0034233095975056125 0.008504371421300776 -0.01186024780940403; -0.0010281509045283123 -0.0014543260229510026 -0.001159527415135699; -0.000628603390574983 -0.0016859898583983215 -9.672405361507223e-5; -0.027279855852352857 -0.021757087027317615 0.016460931818284844; -0.016893203573599278 0.02275706465455602 0.008986858211249091] %
+
+Mass Used: 88.47257318513721 kg
+Launch C3: 122.76656540705011 km²/s²
+||V∞_in||: 3.1806579293456577e-9 km/s
diff --git a/archive/ES_0.6899706648409263 b/archive/ES_0.6899706648409263
new file mode 100644
index 0000000..8a41579
--- /dev/null
+++ b/archive/ES_0.6899706648409263
@@ -0,0 +1,22 @@
+archive/ES_0.6899706648409263---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T17:36:39.674
+Launch V∞: [6.360517345208715, -8.820088272071557, -2.29284641962692] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.001505669000397128, 0.0008831698021292553, 0.0016843162809726529] km/s
+ V∞_out: [-0.0007923148960416396, 0.0016709878888546362, -0.001569311252379786] km/s
+ time of flight: 9.185724064823626e7 seconds
+ arrival date: 2026-03-21T21:30:39.674
+ thrust profile: [0.7046205681129616 -0.5361814506408457 -0.3541770154320949; 0.434141950135056 -0.10659807469075815 -0.332894743281783; 0.19742601831975928 -0.0047150981129057195 -0.21312976972284553; 0.06423033692717894 0.0045890707089724465 -0.08480718147221888; 0.06746178398053622 0.009837492266346805 -0.10422876867388066; 0.04816213635932187 0.00946589596513187 -0.08313488066511932; 0.012343009177821941 0.0035088596270870832 -0.022127766646417097; 0.003982891982385094 0.002477207443649952 -0.0071295478859062355; 0.009138756620990736 -0.0020263144657885475 -0.015628893701866448; 0.0036141718687667103 0.0021867909091322093 -0.0033739758472354333; -0.0013183927462107141 0.00048286438280861066 0.0003905221794300814; 0.003593465774718565 -0.009996136728995967 -0.0006363631346752489; -0.0005338888235853568 -0.0003722515831175819 -0.0016424909847890744; 0.00879239709832308 -0.008645324174126853 -0.007761591447026282; 0.007483781045101251 0.004508201752668293 -0.022092003207685996; 0.0086935891591942 0.0027881930561395605 -0.01926499433352747; -0.0034678546690438154 0.012082519918232391 -0.0068930997310170175; 0.0006498745024210153 -0.0030408415199421274 0.0039463688057128875; -0.008830258176916081 -0.0010336582586931051 -0.001774791949899083; -0.0022181901319541387 -0.0051602789379023295 0.020840656590496127] %
+
+Mass Used: 84.5066263903991 kg
+Launch C3: 123.50728272983112 km²/s²
+||V∞_in||: 0.0024256853407850455 km/s
diff --git a/archive/ES_0.6926539584798348 b/archive/ES_0.6926539584798348
new file mode 100644
index 0000000..8588e41
--- /dev/null
+++ b/archive/ES_0.6926539584798348
@@ -0,0 +1,22 @@
+archive/ES_0.6926539584798348---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T23:44:44.847
+Launch V∞: [7.488152305692046, -7.531224334261823, -2.3085380329663643] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.06977779282942363, 0.13781252002126268, -0.09447707449547028] km/s
+ V∞_out: [-0.09779219042329029, 0.10010639579854662, -0.11494298182077395] km/s
+ time of flight: 9.546200930017787e7 seconds
+ arrival date: 2027-05-18T20:58:13.847
+ thrust profile: [0.981412849492685 -0.5081027999568661 -0.4836908481272221; 0.27907783028974686 -0.02672726570983382 -0.2056241092109608; 0.15086823676995154 0.011495282404192595 -0.14390003441342047; 0.01893603575998231 0.0032123958334465477 -0.0525355644323557; 0.02096875280933528 0.0003986681999684684 -0.04373027935425763; 0.05510706058773764 0.04827358882649534 -0.031200360991368796; 0.010827310573384468 0.012149610553080118 -0.02302874676473398; 0.029601227041567906 -0.01340074572165947 -0.029601544257609445; 0.008180415828864595 -0.00012028716303284792 -0.011165434692302776; 0.012693185357834702 0.0034834428616196235 -0.013936733716792682; -0.0023259236322242015 -0.001635224793201532 0.00401389070096396; 0.015546071684703698 0.04766349369834922 -0.03759505392426734; -0.031918839603694835 0.09883424010286168 -0.07657113487580594; -0.057046049081504895 -0.026160925207826376 -0.12527909851799507; 0.0438268207613292 -0.052837757125191245 -0.1370519019851096; 0.019862021200594143 0.005030725697945109 -0.1428831834538389; 0.00969731368310784 -0.03465350112384319 0.03927821433575766; -0.00884638950208499 -0.1547471053472429 0.017572136055501175; -0.01382399631497394 -0.09372851722138431 -0.09599796043613454; -0.020840552740516535 0.0992881308888025 -0.002833076881230275] %
+
+Mass Used: 119.05646036722783 kg
+Launch C3: 118.12111277587076 km²/s²
+||V∞_in||: 0.18107221943738233 km/s
diff --git a/archive/ES_0.6929992010378614 b/archive/ES_0.6929992010378614
new file mode 100644
index 0000000..a1975a8
--- /dev/null
+++ b/archive/ES_0.6929992010378614
@@ -0,0 +1,22 @@
+archive/ES_0.6929992010378614---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-22T01:35:12.990
+Launch V∞: [7.405643242534519, -6.790012671623056, -1.037955992373217] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.3129275972053087, -0.8925764399134228, -2.2998889664598914] km/s
+ V∞_out: [-0.4020497141356015, -2.891412553604348, -0.11495596667624604] km/s
+ time of flight: 1.0240560036343874e8 seconds
+ arrival date: 2027-07-21T07:35:12.990
+ thrust profile: [1.0 -0.5843391411371213 -0.33439437950776374; 1.0 0.08368187664238648 -0.5508347331608979; 1.0 0.36149341360272774 -0.6818583731060077; 0.6821540432775476 0.333011040989861 -0.5355830410617959; 0.19172026769455222 0.1186600652218076 -0.19436015939469534; 0.06473646912204253 0.045320569976063915 -0.07509223814319775; 0.08983352132737069 0.07153532856292336 -0.11578059460264871; 0.044008245122022116 0.036860552389084554 -0.060734754472730246; 0.0004976143553658581 0.0018194387027619036 0.00020617852659023822; -0.00025512883059373217 0.0007294040824820166 -0.0006456158817812748; 0.0005898784114148948 0.0005471927040826639 -0.0017170136012518785; 0.0009163607441194275 -9.312609621926044e-5 -0.0018074508370512221; 0.0005502239610284323 -0.00172162276565338 0.0019685871165976013; 0.003114486555935371 0.0037329611189781636 -0.002238263927082951; 0.00213489419643298 -0.002528120270900739 -0.0011658570963795454; 0.0036023419183177415 -0.0005956064230257894 -0.0017161438193062932; -0.0012976520038334345 4.760895773937951e-6 -0.0018452064410831553; 0.0004588386826662575 -0.0005264132646953265 0.0015536963720104544; 0.0019592144175012757 0.0003995434682450936 -0.005690216362578117; -0.0019232823836933734 0.0017294700315395003 0.0030603545726039898] %
+
+Mass Used: 213.35220461899144 kg
+Launch C3: 102.02517655860231 km²/s²
+||V∞_in||: 2.79463071525305 km/s
diff --git a/archive/ES_0.6931203651045026 b/archive/ES_0.6931203651045026
new file mode 100644
index 0000000..fe41f3d
--- /dev/null
+++ b/archive/ES_0.6931203651045026
@@ -0,0 +1,22 @@
+archive/ES_0.6931203651045026---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T07:21:38.306
+Launch V∞: [6.298594174814999, -8.981272276378006, -2.4236967502642535] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0026094028360481537, 0.0015115126815152384, 0.0027759474557031614] km/s
+ V∞_out: [-0.0013801111513626978, 0.002772514640230777, -0.002684348303517045] km/s
+ time of flight: 8.976026348143181e7 seconds
+ arrival date: 2026-02-28T04:46:01.306
+ thrust profile: [0.8834205042090175 -0.7100802740135032 -0.42335024079385053; 0.3423418778201218 -0.09335646862264182 -0.23137597901896112; 0.07124168635887619 -0.004075229513165409 -0.07643215880628576; 0.046797278897335336 0.0024203030963782274 -0.06514237773319012; 0.02823168141393653 0.0029553402986477635 -0.044851545715894066; 0.04333645106735368 0.007441877733719227 -0.07048677195021527; 0.005387395212784161 0.0005995265946606036 -0.00852125382098454; 0.011825299991287468 0.00029608326197107487 -0.022071147078358885; 0.004166890031185228 0.0013554549379282891 -0.008794407128434085; 0.0006715665249218845 0.000870113581845272 -0.00015494407566152952; 0.0020329741968206703 -0.00048185009368229177 -0.0017103523864372546; -0.0004904847208775564 -0.0003623501895064044 -0.001840425145565421; 0.0021023507365442694 0.0010677921625709607 0.001164746608306433; -0.00197175189812266 0.0002677355162566753 -0.0013427447855437215; 0.0014126523147112461 0.00018250812945110517 -0.001501508862168276; -0.002737482630857925 -0.0003164989488577388 0.001086609872553363; 0.00021618701292385432 0.0019176870606328414 0.002005537930735779; -0.0024266536933443576 -0.0006862123071426688 0.002218162974672777; -0.0016197722325303656 -0.0007563581769265089 -0.0028595366648855626; -0.0009608744586041911 0.0006140632638761592 -0.0006738896030406993] %
+
+Mass Used: 72.41632301288837 kg
+Launch C3: 126.2098462186911 km²/s²
+||V∞_in||: 0.0040987239506927505 km/s
diff --git a/archive/ES_0.6935473111227979 b/archive/ES_0.6935473111227979
new file mode 100644
index 0000000..cf8d44a
--- /dev/null
+++ b/archive/ES_0.6935473111227979
@@ -0,0 +1,22 @@
+archive/ES_0.6935473111227979---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-07T15:10:36.048
+Launch V∞: [8.327371504957965, -7.547659518440534, -0.2697792822361393] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-3.762248784588998e-9, -2.056487687221077e-9, -5.331589901002656e-10] km/s
+ V∞_out: [-2.0766692697030697e-9, 5.255139420029508e-10, -2.5332312832256627e-10] km/s
+ time of flight: 1.8749577804636472e8 seconds
+ arrival date: 2030-05-17T17:20:14.048
+ thrust profile: [0.0025358170433624812 -0.0024675101333196305 -0.001959255938353095; 4.4648608735247644e-5 -0.0018146771147561002 -0.0008533168441125025; 0.0171104676359999 -0.04319544297122647 -0.04589288882383436; 0.04487027651248712 -0.11208498408530651 -0.11818475477365856; 0.06340407972895132 -0.1504424682819357 -0.1599464058874636; 0.0583303491439511 -0.13035310729307162 -0.14117531678471906; 0.04391313517909932 -0.09286870611853604 -0.10275318858971146; 0.025098839312266055 -0.050734804541490146 -0.05765864479807142; 0.0032323339519740734 -0.006340128400738186 -0.007311102226342274; 0.0022567271314527337 -0.00429635243282258 -0.005013001125429301; 0.0007094909109167482 -0.0012904883259484874 -0.0016071899066506063; 0.0015239408795269572 -0.0022013776390665675 -0.0028675924502012096; 0.0020312340879119085 -0.0033982745935589105 0.0010199114885881338; -0.0024472425207740373 -0.0014832823170463354 4.7783240020821604e-5; -0.0015214845917726843 0.0026038203616847956 -0.003671186275522615; 0.0005124551034110363 0.001438241012689302 -0.0065847671804114; 4.437232853375176e-5 -0.004753416675726373 0.0010598039972277763; 0.0003945899341749943 0.00039129473621795003 0.0007189486524365195; 0.0026069869476562603 -0.00773798846713748 -0.004124303594502339; -0.004438801548059942 -0.0021232377342799615 0.00928454879281118] %
+
+Mass Used: 71.89233902400565 kg
+Launch C3: 126.38506124901573 km²/s²
+||V∞_in||: 4.320638382641855e-9 km/s
diff --git a/archive/ES_0.6936646075883711 b/archive/ES_0.6936646075883711
new file mode 100644
index 0000000..00d4b17
--- /dev/null
+++ b/archive/ES_0.6936646075883711
@@ -0,0 +1,22 @@
+archive/ES_0.6936646075883711---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T20:14:31.790
+Launch V∞: [7.9691361279919475, -7.473433229858774, -2.372536919493408] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.08753313137250486, -0.2667572905376379, -0.36126845919417133] km/s
+ V∞_out: [-0.4106679630232077, -0.0627885221466312, 0.1914440911293111] km/s
+ time of flight: 8.977604697894137e7 seconds
+ arrival date: 2027-03-13T22:01:57.790
+ thrust profile: [0.8960502480659505 -0.4528675265676886 -0.3919111173054129; 0.3457595261935925 -0.030129943904994575 -0.2563497819506963; 0.1447308547223985 0.01296900171799549 -0.15651626392377171; 0.06448393509328035 0.004768005848555057 -0.09148796546925554; 0.051941950405457855 0.00730159500138868 -0.09383424576645019; 0.02641211741393646 0.0021655945619930986 -0.045643709478998526; 0.007610769965191982 0.007019076993675339 -0.013663997026067971; 0.004262766189273225 -0.0009268012645266919 -0.005197583739282181; 0.021589593424267004 -0.002328822298032404 -0.06479734132169004; 0.012801706192160523 0.005424479054043771 -0.023633244832721646; -0.00852700381499263 -0.000810358242457321 -0.00668967553198344; 0.0017001367842181606 0.00210410420838878 -0.004573014090777919; 0.006456687013461422 0.005018731379623871 -0.013200744518256941; 0.004797273226790194 0.002192098687012748 0.003153954397699523; -0.003770610590318999 -0.010168786521646482 -0.007711370912088599; -0.0020969154810184226 -0.002032962098678568 -0.003100466262907123; -0.002119587832582229 0.017992650642539076 -0.000587808063857992; 0.0032925034128467277 0.015697734673835544 0.004087319818453788; -0.014675652914310854 -0.014885164392477866 0.010322553965533427; -0.0015268648412845955 -0.012984738985315316 -0.006529868916987307] %
+
+Mass Used: 80.17715542486485 kg
+Launch C3: 124.9882663019831 km²/s²
+||V∞_in||: 0.457532950454269 km/s
diff --git a/archive/ES_0.6948430596063674 b/archive/ES_0.6948430596063674
new file mode 100644
index 0000000..6f46721
--- /dev/null
+++ b/archive/ES_0.6948430596063674
@@ -0,0 +1,22 @@
+archive/ES_0.6948430596063674---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T03:02:42.606
+Launch V∞: [6.4075553526819125, -8.91556253316329, -2.417085637107635] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0008728327825721828, 0.0005243829053816098, 0.0009260212365036257] km/s
+ V∞_out: [-0.00042142821316798815, 0.0008476571168963508, -0.0009990032951236738] km/s
+ time of flight: 8.975391773356885e7 seconds
+ arrival date: 2026-02-26T22:41:19.606
+ thrust profile: [0.8229719656096393 -0.6151924137153822 -0.3891929524016696; 0.3597454924503545 -0.08596363323210726 -0.2551600542003408; 0.13930318602369549 -0.004252870250355174 -0.13477727496255612; 0.05798150476067218 0.0036148964703088325 -0.07059930442934528; 0.1036624722926341 0.016240257605100894 -0.13174744351648907; 0.007646933208622697 0.001363683257732841 -0.012129127482189788; 0.01067738381932901 0.0022486663184107763 -0.017926215690220064; 0.0003970192342844691 -0.00018326809316421505 -0.0008548173031111743; 0.0007394797810365024 8.16038843131748e-5 -0.0010789476882528076; 0.0012566438703708915 0.0005067931194802974 -0.001967665597941231; 0.0005416471771647159 2.004530609923255e-5 -0.0004771447816949887; 0.00038878249874877476 0.00014088753127955065 -0.00039097426910858555; 0.0011860263281587634 0.00025729813182865714 -0.0013782094827536346; 0.0010000891421589526 -0.0003391429854996495 -0.0015538935258797187; -0.00024328361111353083 0.0007310474127511959 -0.0005164012818051169; 6.837070440080027e-5 -7.524725125159708e-5 -0.0005034420747369859; 0.0007917077624186459 -0.0002774172677100029 -0.0015313660855643917; -0.0010400465739933006 0.0017152782301648498 -0.0003127053979051829; 0.00018007276214438363 0.0005722875181888433 -0.00015722966137176502; -0.00021594013844678775 0.0009139254088200274 0.00024705918223735085] %
+
+Mass Used: 73.39668037178035 kg
+Launch C3: 126.3863238575397 km²/s²
+||V∞_in||: 0.001376346550925624 km/s
diff --git a/archive/ES_0.6950184616027781 b/archive/ES_0.6950184616027781
new file mode 100644
index 0000000..4454e1e
--- /dev/null
+++ b/archive/ES_0.6950184616027781
@@ -0,0 +1,22 @@
+archive/ES_0.6950184616027781---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T03:41:12.558
+Launch V∞: [7.996818859687033, -7.59693810773943, -2.519158505460632] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.425443286915188, 0.48183510787994654, -0.5050914960055045] km/s
+ V∞_out: [-0.43004284118661124, 0.5088725907486799, -0.4736239421837124] km/s
+ time of flight: 8.909226520447189e7 seconds
+ arrival date: 2027-03-07T07:32:17.558
+ thrust profile: [0.8063057733887306 -0.4119272702205904 -0.3964904067834379; 0.2683332599739919 -0.02839337007179287 -0.2162169073651219; 0.12740706711305574 0.00853536710767791 -0.14061041100185265; 0.04531866464014264 0.007017179322386953 -0.05986600682355064; 0.01209590275079078 0.0021461079382154393 -0.009337098552362923; 0.008744651254329317 -1.0458645717170137e-5 -0.003573216344007443; 0.016063958793738967 -0.004883693644090574 -0.014750184433230583; 0.0028071587333367183 -0.0035924065701962594 -0.018430881421995598; 0.006124489224745362 0.002347927201855533 -0.013686806754143958; 0.005278936418187618 0.0035463841457527984 -0.011685373274894965; 0.01535454207286838 -0.001989579636326717 -0.015868002053956054; 0.015585590019320066 0.003414527833138897 -0.008232867162878296; -0.0029461092068539256 0.004077165857692157 -0.003078546298879675; -0.0024458255810094138 0.0042490811560888155 -0.003843775873759574; 0.0023174884138844865 -0.0016677185063856711 -0.0005312571743309193; 0.01884000124758544 0.005022033431453295 -0.014487929088022357; 0.0002027359004596308 0.0007007503691680605 0.0009391410636963096; 0.005088395463953085 -0.00611498933317834 -0.006709126314454203; 0.010760976966904853 0.00779350589344905 -0.012801182279541842; 0.00038837926398255576 0.002777149744247894 0.0030837718430253933] %
+
+Mass Used: 64.13722150179865 kg
+Launch C3: 128.00874006310443 km²/s²
+||V∞_in||: 0.8174866854597433 km/s
diff --git a/archive/ES_0.6950467099917514 b/archive/ES_0.6950467099917514
new file mode 100644
index 0000000..921b377
--- /dev/null
+++ b/archive/ES_0.6950467099917514
@@ -0,0 +1,22 @@
+archive/ES_0.6950467099917514---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T22:14:13.496
+Launch V∞: [7.845966571971527, -7.569917835494668, -2.2444917788617054] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0036501469252053554, -0.041448635049762546, 0.011592943599092964] km/s
+ V∞_out: [0.01483225271266119, 0.02842519091591311, 0.029658127628244046] km/s
+ time of flight: 8.845933776797901e7 seconds
+ arrival date: 2027-02-27T18:16:30.496
+ thrust profile: [1.0 -0.6020867854823606 -0.4981648596832241; 0.6260544915253095 -0.07007761169047926 -0.4406032665025618; 0.16870540407802895 0.010524453839328447 -0.15219392396805656; 0.06733920119307828 0.014589958236334551 -0.07459955799777; 0.03842530746725617 0.013948472911779263 -0.05704784606022561; 0.012119037794378675 0.0046134244479998894 -0.02106264285595843; 0.01501919295114977 0.003548388635306147 -0.02237798199483783; 0.002571328839509762 0.0012060331305802662 -0.005885550705390875; 7.036521840815112e-5 -0.0002439187245950306 -0.00038250935657289307; -0.00011941578515014154 -0.0005770959123899244 -0.00011515732544503958; -0.0003970857760319374 -0.00018743441814597246 -0.00012613363627147237; -0.00011746797457164062 -5.9904437662076205e-5 0.00029953660777112963; 8.084576013302316e-5 0.0002109351081915217 0.00032987221499431157; 0.0002333242104178897 -1.837875460407435e-5 6.077962106356563e-5; 0.00011180520732213903 -0.0007181848838022888 0.0003156308328451764; 0.00021909766783075895 -0.00014840509215888052 0.0006366726122731523; 0.00019112599735764645 0.000266044245966315 0.0009131502766886355; 5.764304842631422e-5 -2.115348767593641e-5 -0.0002707538496549278; 0.0004705366573195202 -0.0008629657633720347 0.000944714296781912; -3.351673666689343e-5 1.2190478021213518e-5 -5.600363901700928e-6] %
+
+Mass Used: 88.13438181530273 kg
+Launch C3: 123.90059083001269 km²/s²
+||V∞_in||: 0.04319385675481805 km/s
diff --git a/archive/ES_0.6950845006562383 b/archive/ES_0.6950845006562383
new file mode 100644
index 0000000..1e6832f
--- /dev/null
+++ b/archive/ES_0.6950845006562383
@@ -0,0 +1,22 @@
+archive/ES_0.6950845006562383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T09:36:36.387
+Launch V∞: [8.074672942591663, -7.6499808568454295, -2.518627666916399] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.057133704051680646, -0.1812914716819847, -0.22887978681932253] km/s
+ V∞_out: [-0.28421094504734135, -0.02790512287349192, 0.08333436902303133] km/s
+ time of flight: 8.90160370313961e7 seconds
+ arrival date: 2027-03-06T16:17:13.387
+ thrust profile: [0.5747187648551132 -0.29035526831579656 -0.27378105347593845; 0.2590428897034554 -0.02472033369553412 -0.20721676324584112; 0.1021785138605246 0.009416468090843613 -0.11996111000806005; 0.04771505907014154 0.008821589502660869 -0.07311711465217337; 0.018654672467766836 0.004276407744725797 -0.033493693312161954; 0.028855362137348236 0.008113848205167563 -0.05611382148398878; 0.0176857146666712 0.0053575871412586806 -0.037381727773441176; 0.01003622951454821 0.003239327360769924 -0.022861064901658644; 0.00010056034113244431 0.0007322875691492145 -0.003742452364948698; -0.001181800696557627 0.000543211810790834 -0.0012485165223908015; 0.001855790750243435 0.00016748287732849045 -0.001906923463717601; 0.0011744281897257184 -0.0014324589951266484 -0.002326581384360908; 0.0011868343372251427 0.0007740202746498953 -0.00152816299414283; 0.0006362997270814224 -0.0007064706799666386 0.0010200197189815237; 0.002270742001143514 0.0005644826562812876 -0.0018473884837611222; -0.0013004043715635265 -0.0025936202040255318 -0.0014834114156683106; 0.001547045836655437 0.00026857950520106324 -0.0021923897699741846; 2.068630163211318e-5 -0.00020205733763796105 -0.0006802865261092801; 0.0007601728307586265 0.00014426203673218645 -0.0008849245657206041; -0.0003761250277687924 -0.00026890825475464923 0.00016617747335420532] %
+
+Mass Used: 52.21337663947679 kg
+Launch C3: 130.0660355644802 km²/s²
+||V∞_in||: 0.2975177551974729 km/s
diff --git a/archive/ES_0.6964135801004295 b/archive/ES_0.6964135801004295
new file mode 100644
index 0000000..5a4df89
--- /dev/null
+++ b/archive/ES_0.6964135801004295
@@ -0,0 +1,22 @@
+archive/ES_0.6964135801004295---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-27T08:24:35.331
+Launch V∞: [6.189010312123412, -9.032184657165224, -2.257040997448067] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.09962360408532854, 0.06675142282625997, 0.1235609090274915] km/s
+ V∞_out: [-0.055657988734206076, 0.1167842569417847, -0.11360493482400895] km/s
+ time of flight: 8.888783968570797e7 seconds
+ arrival date: 2026-02-19T03:28:34.331
+ thrust profile: [1.0 -0.912555178180571 -0.5345321390902776; 0.44267124304884364 -0.13351974999836913 -0.3154157791361182; 0.07799931141046376 -0.006375428530351986 -0.08393734979378419; 0.03843163734563034 0.001313775911391553 -0.053241223845234616; 0.03136554698216834 0.003046908617080231 -0.05350999950151559; 0.017412369497967643 0.0021744805330009245 -0.0309058202451753; 0.004239686727695683 -0.0002734365101370622 -0.006591461156908401; 0.007227702851295962 0.0022872629495891946 -0.011344530632068845; 0.001151757240453521 0.0010946437582688789 -0.009229859005840144; -0.0013819076476665193 0.0017457243857838243 -0.0033097707197890097; -0.0006672138492093108 -0.0006780179900488716 -0.0011870796035920882; -6.59808512147083e-5 -0.001324996641033391 0.0009615291788712434; 0.000534536203146787 -0.002932370176073119 0.004219036773188727; 0.0014177532266098952 -2.8316464269005854e-5 -0.00030038637606611806; 0.003403085587491225 -0.0007867301180634335 0.0017989417489220048; 0.00020218592624084505 -0.0033792814434725578 -4.590392085585678e-5; 0.0017400506569416347 -0.0017977226108663045 0.0007085495433876183; 0.0008371218467089906 0.0002017951864594764 -0.0014373855890759462; 0.000547342586592261 0.00013926234365551683 -0.0011214664117306285; 0.0061909035437434515 -0.002660745251404345 0.00014557728237261371] %
+
+Mass Used: 83.44159618213826 kg
+Launch C3: 124.97844238886219 km²/s²
+||V∞_in||: 0.17218569388883753 km/s
diff --git a/archive/ES_0.6966526079729011 b/archive/ES_0.6966526079729011
new file mode 100644
index 0000000..ddf401d
--- /dev/null
+++ b/archive/ES_0.6966526079729011
@@ -0,0 +1,22 @@
+archive/ES_0.6966526079729011---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T12:49:55.067
+Launch V∞: [8.085103275454559, -7.5825176564592764, -2.4242567175597354] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.02270410598993695, -0.06819089008745073, -0.09067522973121815] km/s
+ V∞_out: [-0.10455326041781976, -0.015740475818825626, 0.046962667009463145] km/s
+ time of flight: 8.897156339180575e7 seconds
+ arrival date: 2027-03-05T07:09:18.067
+ thrust profile: [0.5588876236741526 -0.27283585204285965 -0.2606914075931861; 0.31095098860059317 -0.024665506018385613 -0.24255595655537585; 0.2453816042375776 0.024727387018457767 -0.2613422101354956; 0.09453598491005151 0.019815230365360786 -0.13399114893889283; 0.012221521270900048 0.0032144690834041596 -0.019637317365562314; 0.012156258120855988 0.003644918451119207 -0.021615238987145416; 0.008617752328916258 0.003226038367048902 -0.017617862736907436; 0.0015809359479675654 0.0009059323148657431 -0.0034297802834258187; 0.003153502099122879 0.001415828408193326 -0.002435481866706092; -0.0005050188566578912 -0.0009991566079359567 -0.0006829346208807911; 0.0031096142005298073 0.0003908748276229929 0.0004183171683916023; 0.004929888187139235 -0.00021455635944018825 -0.0035317137831284147; 0.002200886252256499 0.00026561011063230144 -0.0006152933360312011; -0.0004839693317762646 -0.0029992751387853825 -0.013321503715712151; -0.003524030766505518 -0.003833845265119904 -0.010762549674849551; 0.001845809979399746 0.003059823201074202 -0.010155925455160036; 0.003962087260569598 0.0022320661211943822 -0.006163681937489293; 0.007529974938405016 0.0006299136158429064 -0.003870978669112887; -0.0024124672126120197 0.0034444251792926346 -0.002457572146537486; -0.00021698720935979944 -0.0006573480631799326 0.002960789122764476] %
+
+Mass Used: 61.77518653053994 kg
+Launch C3: 128.7404896179162 km²/s²
+||V∞_in||: 0.11570424022709913 km/s
diff --git a/archive/ES_0.6973992584663383 b/archive/ES_0.6973992584663383
new file mode 100644
index 0000000..eb3a5b9
--- /dev/null
+++ b/archive/ES_0.6973992584663383
@@ -0,0 +1,22 @@
+archive/ES_0.6973992584663383---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T17:39:07.493
+Launch V∞: [8.129347074583727, -7.536731468279831, -2.625022621513272] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.3982234939371799, 0.4510038440588157, -0.46021412070683354] km/s
+ V∞_out: [-0.40849981495992443, 0.47003932301409396, -0.431209439636751] km/s
+ time of flight: 8.823305409040666e7 seconds
+ arrival date: 2027-02-24T22:50:01.493
+ thrust profile: [0.8240676499527322 -0.3756615928732833 -0.3658197895854441; 0.2661478262516029 -0.025278102867259865 -0.20924899520861756; 0.08648600661375311 0.008118536105846556 -0.09596816106808216; 0.03292245737618869 0.006483983257961501 -0.04509089223897999; 0.018770460081524158 0.005176138122556128 -0.030772220160531872; 0.012005731556935269 0.003950448119052969 -0.022145755668246003; 0.00621363998249671 0.0022330870885717657 -0.01244047269807284; 0.0019275626119987996 0.000844613022494254 -0.004060650786800639; 0.0006121761045475349 0.0003911089720026971 -0.0021307713920245405; 0.00024699830323697807 0.00035321922174953767 -0.0020450482442024654; 0.0040192692243759 0.0031343177411800776 -0.005773503528636532; -0.00027105585481595454 0.0003780031582361089 -0.0004319205079739381; 0.0013340871130880858 0.0009855371303742646 -0.0012804528691043688; 0.000401998192090431 0.0002958117396912654 -0.0006177827424640335; 0.0004158649128241207 0.0001709076794872955 -0.0009014279179416673; 0.0016724376799285975 9.331019719233569e-5 -0.001808059370391296; -0.00027127884321457435 0.00011993264633794443 -0.0008379752767665794; 0.00289409395692174 -0.00016476297157215318 0.0013525485182517177; -0.00029943013275243475 0.0011369907902129455 -0.002632987261162679; 0.0019598517814593793 0.0006393031215745238 -0.0005299311215168322] %
+
+Mass Used: 56.586266600551426 kg
+Launch C3: 129.77934884745886 km²/s²
+||V∞_in||: 0.7574849538950115 km/s
diff --git a/archive/ES_0.6974231266636229 b/archive/ES_0.6974231266636229
new file mode 100644
index 0000000..2aed460
--- /dev/null
+++ b/archive/ES_0.6974231266636229
@@ -0,0 +1,22 @@
+archive/ES_0.6974231266636229---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-11T21:30:40.675
+Launch V∞: [7.890962459212581, -7.749139546135011, -2.516704142192777] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.04142285760972504, -0.11510257227087663, -0.1498172076236473] km/s
+ V∞_out: [-0.1686655262368514, -0.02837427489402829, 0.09030487900822318] km/s
+ time of flight: 8.82882690650502e7 seconds
+ arrival date: 2027-02-27T18:01:49.675
+ thrust profile: [1.0 -0.5558252952059779 -0.4923010240673764; 0.29888454360636435 -0.04029914668193309 -0.2273036437112116; 0.02350857901944269 0.0015567869385755468 -0.029143876267977455; 0.028061133419214134 0.0038952252165737875 -0.039565326735358605; 0.010044007097771363 0.002090887008199356 -0.01825558311114659; 0.0032424776452201535 0.002063849695898261 -0.009505834832803577; 0.00016259798255927396 0.0007653654270569344 -0.0031635972985109935; 0.00017049356161371806 0.00014950720731372533 0.00169148880825356; 0.0008086636880958889 -0.0002637736169814735 -0.0024517443758945833; -0.001444632668929894 0.0018322060516287075 3.767964717024761e-5; 0.0011744035261306764 0.002186071359191062 -0.0013009422187394296; 0.004306222481481544 0.0018170551358413327 -0.005696693384911366; -0.0026488348025364493 0.001121048927333453 -0.0011054133926516885; 0.00017815726001269364 -0.0015878106805084988 0.0038100309704215546; -0.005111946825687101 0.0020534979702374135 0.0011783261526846205; -0.005946717750505916 0.0004388184508684567 0.002812415373872188; -0.0024189479555510296 -0.00048471190221277235 0.0044716031533416625; -0.000531787641347632 -0.00047748870422566984 0.001622127388311809; -0.0008138228921715819 0.008475454220346334 -0.001756145888360281; 0.001721234101570755 -0.0008535249872918118 0.0009905039500769548] %
+
+Mass Used: 63.20051123877465 kg
+Launch C3: 128.6502519775061 km²/s²
+||V∞_in||: 0.1934157464532683 km/s
diff --git a/archive/ES_0.6996533737912992 b/archive/ES_0.6996533737912992
new file mode 100644
index 0000000..53e0925
--- /dev/null
+++ b/archive/ES_0.6996533737912992
@@ -0,0 +1,22 @@
+archive/ES_0.6996533737912992---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T13:56:25.247
+Launch V∞: [8.041546570124602, -7.605460494029443, -2.4757827594009396] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.02234331206624727, 0.022788771340545994, -0.015047076609298306] km/s
+ V∞_out: [-0.02632818023007851, 0.0178789763736128, 0.01521234041509155] km/s
+ time of flight: 8.764230074073885e7 seconds
+ arrival date: 2027-02-18T23:01:25.247
+ thrust profile: [0.9993466605650326 -0.5142571973210087 -0.43682760335903725; 0.29795445730520936 -0.029006187082092814 -0.22218694547530216; 0.06406633696708379 0.005734923705307382 -0.08281837458387736; 0.04548854969551932 0.008820721010322819 -0.07601164911852079; 0.025781483765173002 0.006343639557547439 -0.050829654681743865; 0.012736777499803193 0.003871203554316825 -0.028071101288945636; 0.0027465634978438977 0.0008456034637358565 -0.0066238809141680255; 0.0031712851348033038 0.0009949513373035508 -0.00825154370623874; 0.0014004261884039912 0.0003976394201411739 -0.0033763181590993284; 0.0008593166480523976 0.00024254457608826016 -0.002181471742341094; 3.206377594255791e-5 1.9986902477180743e-5 -0.0006590922090358585; -0.0005036937811678085 -5.2311258360959764e-5 -0.00032551405124230716; -0.00010421090756929585 0.0001657554558402357 -0.0005696089430558768; -7.038153813335992e-5 5.698809074747757e-5 -9.925676417609056e-5; -3.462668443887686e-5 0.0002716678752397598 -6.0503633780631654e-5; -0.00026478340768001013 0.00010622321290083142 0.0001984483671609838; 6.231159331919153e-5 0.00016300685268885555 -0.00047996289319932213; -0.0003669967063020176 -4.131743117947389e-5 0.00032251935142482593; -0.0002503580942673272 -6.317699972791088e-5 6.541334693889206e-5; -0.00040274560162875206 -0.00020711342597445241 0.00012600569817646003] %
+
+Mass Used: 65.86809787126094 kg
+Launch C3: 128.63900083747225 km²/s²
+||V∞_in||: 0.03528407867278801 km/s
diff --git a/archive/ES_0.701577307886667 b/archive/ES_0.701577307886667
new file mode 100644
index 0000000..6a8d64f
--- /dev/null
+++ b/archive/ES_0.701577307886667
@@ -0,0 +1,22 @@
+archive/ES_0.701577307886667---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T04:36:58.254
+Launch V∞: [8.024605860236361, -6.997466196550515, -1.7410319097814595] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.529010356605148e-9, -1.913514840212887e-9, -1.294265390122343e-9] km/s
+ V∞_out: [-2.2905909698453896e-9, 2.1556163001404086e-9, -7.850501988503089e-10] km/s
+ time of flight: 9.179331674120589e7 seconds
+ arrival date: 2027-03-29T14:45:34.254
+ thrust profile: [0.9542054604430326 -0.44393459438984373 -0.38408060823932416; 0.7823243767576418 -0.010982018937211053 -0.5118930538529155; 0.5474096782874136 0.11034612389224162 -0.4905173497497015; 0.32340588730620845 0.10681602855890479 -0.35807386927525986; 0.1555035361482322 0.06461057705605684 -0.19997931419626938; 0.08628165745595787 0.04116200104369439 -0.12342709590263443; 0.005020658566810596 0.00293079172429872 -0.008213836422775147; 0.010388880466536392 0.005742370391363793 -0.01999049597166566; 0.0037177375321098666 0.0021486457471592943 -0.00677622166397241; 0.003309867564271398 0.001088558833312394 -0.006808911382522121; 0.0024931270288833895 0.003102943268810818 -0.005701714730459969; 0.0017810773400270528 0.007212577751921058 -0.004737214041434068; 0.0026278758610413003 0.0006840845965793234 -0.0020891838153207455; 0.0002236706404951963 -0.0028907514229737806 -0.006278818154520636; 0.0020171668383775366 0.0022252220532361384 -0.0018088675182603526; 0.0006711010962211438 0.005181198707367381 0.0030056769645589567; -0.0019159931373697375 -0.0020354150336018167 0.0019539027758283187; 0.0009938101728527143 -0.003918612086721158 0.003904542732677772; -0.0017525490536294541 -0.0031312352250866034 -0.002791828841453604; -0.0034361611819351584 0.006614713984415419 0.00643192189824029] %
+
+Mass Used: 139.56504964762053 kg
+Launch C3: 116.39002449488416 km²/s²
+||V∞_in||: 3.4252817880576756e-9 km/s
diff --git a/archive/ES_0.7017586001932162 b/archive/ES_0.7017586001932162
new file mode 100644
index 0000000..fd232fc
--- /dev/null
+++ b/archive/ES_0.7017586001932162
@@ -0,0 +1,22 @@
+archive/ES_0.7017586001932162---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T17:41:51.458
+Launch V∞: [8.111655822936301, -7.653002165818471, -2.5093197432198378] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.47961819522281696, 0.5322042426034119, -0.5697067248676435] km/s
+ V∞_out: [-0.49516433888365285, 0.5465080514644602, -0.5412914235676267] km/s
+ time of flight: 8.799482616467172e7 seconds
+ arrival date: 2027-02-23T04:42:17.458
+ thrust profile: [0.7182871065517883 -0.36656043040217934 -0.3350831479022635; 0.24094449213079155 -0.024682480492832115 -0.20114974561261675; 0.05894459053137202 0.004054748050972885 -0.07224290107643812; 0.042387440347361936 0.006380965797935171 -0.062395699660466465; 0.030371938282248566 0.006701684026228018 -0.05220042976303206; 0.015505731028379361 0.004107613889817942 -0.03067779248868332; 0.02142107961836663 0.006502232657945155 -0.045778623058363825; 0.005820669767773092 0.0009426315640442108 -0.010186026975047608; 0.0036308672310506143 0.001000262873115181 -0.007288254862066701; -0.00021453677285682865 -0.00012122593461935904 -2.498015374534585e-5; 0.0003201171534843422 -0.0020918087258281776 -0.00628738381316128; 0.0002845186998235964 -0.004967130865763454 -0.002926432729476531; 0.002303371886696913 0.0024330901069732165 -0.009351450636881115; 0.009328173399445853 -0.000552614787696343 0.0005355692128120875; 0.01274110600493131 -0.0050535773456866625 -0.0037271686017739036; 0.0006087932960491634 -0.00021910228232749655 -0.00011472097897982582; 0.0028448351971167296 0.0068353189011667835 -0.014035969575982648; 0.003526253040605036 0.0006181407980979049 0.00793043167963061; 0.010839237711382971 0.005354335008902422 0.0013293954658719373; 0.00230393699777493 0.0026502594677625508 0.004661744981125469] %
+
+Mass Used: 56.511187396602054 kg
+Launch C3: 130.66408791351148 km²/s²
+||V∞_in||: 0.9153363979397303 km/s
diff --git a/archive/ES_0.7021369882851014 b/archive/ES_0.7021369882851014
new file mode 100644
index 0000000..039f03c
--- /dev/null
+++ b/archive/ES_0.7021369882851014
@@ -0,0 +1,22 @@
+archive/ES_0.7021369882851014---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T19:14:51.888
+Launch V∞: [8.17535524956199, -7.633817868913468, -2.6807794715515074] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.4163539238944632, 0.4401699401245497, -0.4848465715534171] km/s
+ V∞_out: [-0.3942726028488468, 0.501135305558365, -0.44222866678038086] km/s
+ time of flight: 8.73369993538532e7 seconds
+ arrival date: 2027-02-15T15:31:30.888
+ thrust profile: [0.7853386648605156 -0.36652664383905237 -0.3393211397451489; 0.21260213889390203 -0.020813494241965432 -0.1653603221255374; 0.05064856645775392 0.004396787471753838 -0.05607411351638655; 0.024828202554626477 0.004481679917762966 -0.03268052615362334; 0.008151711841171853 0.0019930151322616082 -0.012867487548137583; 0.006739851298944863 0.0018404467690821438 -0.011436302956979597; 0.0006403178041207864 0.0003465859619025468 -0.0013326921464573613; 0.0009143755681407829 0.0002063998714849698 -0.0013398328339911765; 0.0006358440566604968 0.00021596373498059034 -0.0008162326732910315; 0.0012085773588395804 0.00028350680023787205 -0.001240814261236888; 0.0004124021309428494 0.00043229659000574466 -0.0004565657505266468; 0.0007269694197891011 0.00016960501922751208 -0.0017320037392889375; 0.0004963936367991482 0.0004984116938781898 -0.001475519910027989; -2.0746946063959684e-6 0.0005789002863499657 -0.0010673411051382192; -0.000358019186726425 0.0017148236773434876 -0.0015057980560430953; 9.117326927764278e-5 0.0006336691836862082 -0.0007334620508798468; -0.00034372433730285557 -0.00025079618294102926 0.0006651336925812617; -0.00034460072579407537 0.00010219286607736366 -0.0002075199003635994; -0.0007899079154755836 4.422159796009923e-5 -0.00027801360814807386; -2.412181571713641e-7 3.194150030174259e-5 -0.00018220290306436603] %
+
+Mass Used: 47.42039382292887 kg
+Launch C3: 132.29818728737533 km²/s²
+||V∞_in||: 0.7760002345867357 km/s
diff --git a/archive/ES_0.7026112014184177 b/archive/ES_0.7026112014184177
new file mode 100644
index 0000000..aa892bf
--- /dev/null
+++ b/archive/ES_0.7026112014184177
@@ -0,0 +1,22 @@
+archive/ES_0.7026112014184177---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T08:24:54.324
+Launch V∞: [6.297614598703248, -7.655398752748918, 0.043371676300171] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.230290884847257e-11, -2.2250698433242856e-9, -8.301637759375859e-9] km/s
+ V∞_out: [3.1807192460527813e-9, 4.5835616188918e-9, 2.0269625964819719e-10] km/s
+ time of flight: 1.7980385364350194e8 seconds
+ arrival date: 2029-01-09T09:55:47.324
+ thrust profile: [0.11125676285979033 -0.04476601020401203 -0.0059973498908864435; 0.0462594056917315 0.008988903499007713 -0.00017774032798717823; 0.049225674305170185 0.0017907235036409078 -0.10177467302466206; 0.003326221054384855 -0.031550949057877586 -0.05677256699442769; 0.07876356012444805 0.02830149549653351 -0.09415906477750341; 0.05175824476046889 0.020983193972784617 -0.09558504418496097; 0.04094615426665513 -0.01854594021415433 -0.02709365764795764; 0.10641495315574062 0.13347930052506063 0.0011226071261166495; 0.04298744420561873 0.04947337268092422 -0.010126883179699231; 0.04871658698762079 0.09484981555982845 -0.08655721769698632; 0.06951313314223109 0.06867278361536659 -0.007147722473818785; 0.024339925321807197 0.003197240344354261 -0.0440351333951863; 0.0078077037057925815 0.08331624380519098 0.002878574328195549; 0.01110780666286166 0.011536916613899176 -0.1419087304654773; 0.018101827901848125 0.2608907163508956 -0.08326730765603475; 0.06223672135097045 -0.25686523240245157 -0.06842642285346612; 0.3369301866858181 -0.15948479288872103 -0.40446552143666603; -0.03342921226438539 -0.06860331248140279 -0.2865540133386863; 0.2138426168776956 -0.2837495786018267 -0.2086847084351472; 0.04890886049107772 0.05110827721520253 -0.24279009194852852] %
+
+Mass Used: 246.48913032326618 kg
+Launch C3: 98.26696079969506 km²/s²
+||V∞_in||: 8.594960907775797e-9 km/s
diff --git a/archive/ES_0.7049298306383058 b/archive/ES_0.7049298306383058
new file mode 100644
index 0000000..50ef63d
--- /dev/null
+++ b/archive/ES_0.7049298306383058
@@ -0,0 +1,22 @@
+archive/ES_0.7049298306383058---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T06:28:06.391
+Launch V∞: [8.040579062916805, -7.499757303556497, -2.1926921428920814] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.027201016638570788, -0.08589354421797232, -0.1108520317701858] km/s
+ V∞_out: [-0.13249904809026536, -0.019574816079202938, 0.055392174715433624] km/s
+ time of flight: 8.739987070193554e7 seconds
+ arrival date: 2027-02-14T20:12:36.391
+ thrust profile: [1.0 -0.5741472791350408 -0.4616130310787835; 0.47524918941300265 -0.03372190367072537 -0.33198477126974246; 0.10429984996649883 0.013530847818760601 -0.11314335404087154; 0.1697543120730348 0.04294335369384432 -0.21345984141244018; 0.07904164300630447 0.02229771927658592 -0.1171976323261369; 0.02507268062774774 0.011246179093340893 -0.04608706798275359; 0.004192304187206042 0.001426666490758192 -0.0035179322524014353; 0.002753577018343995 0.0015933281846525155 -0.00665371401063152; 0.008086203747680135 0.00489634145120164 -0.021911126182623763; 0.003159945221786068 0.0024045145386363126 -0.0008709330866061053; 0.006196137958570831 -0.0035979989339830543 0.006302920504843749; 0.0014452431040572042 0.0007470479841899986 -0.0017970580012860462; 0.0018520364088166826 -0.0005655713770872611 -0.004221241891280191; -0.009907648645811298 -0.005347806346300339 -0.005379016627481919; 0.0035838179311287375 -0.006239036812274029 0.004491464197562179; 0.0013006160835679274 0.004125300608989741 -0.003834975274530489; -0.005794186886749543 0.003660000239225085 -0.00892117325221188; -0.0010332415225956073 0.00022887772773457805 -0.001357092857182349; 0.005063675524205621 0.007372340247611058 -0.006316818032158349; 0.0014286745007129177 0.0009998366133902954 0.0024060287448274256] %
+
+Mass Used: 89.13797675355636 kg
+Launch C3: 125.70517011276579 km²/s²
+||V∞_in||: 0.14284876335507724 km/s
diff --git a/archive/ES_0.7054154090508199 b/archive/ES_0.7054154090508199
new file mode 100644
index 0000000..51a0a7a
--- /dev/null
+++ b/archive/ES_0.7054154090508199
@@ -0,0 +1,22 @@
+archive/ES_0.7054154090508199---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T13:15:57.672
+Launch V∞: [8.126968054886751, -7.517014055298748, -2.339882913096559] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.02141124806520088, 0.11657792366265146, 0.021566970149194224] km/s
+ V∞_out: [0.11628655022534856, -0.017934085224517626, 0.025858574338945624] km/s
+ time of flight: 8.693299395247903e7 seconds
+ arrival date: 2027-02-09T17:19:10.672
+ thrust profile: [0.9506440213361989 -0.47489796330218 -0.42924291901886186; 0.45500327433959803 -0.04145213395756471 -0.33494598728246533; 0.09840729956542972 0.01057381676702846 -0.11157948411087784; 0.1245416993291736 0.026202864183444835 -0.1639825576839947; 0.031737426591763956 0.00857665051767458 -0.05047752472911965; 0.007247325758735076 0.0019932324578874586 -0.012726195265344487; 0.011074865051383848 0.0034916241480365995 -0.021703293136074282; 0.0012839938228636702 0.0004444481729122418 -0.002866705781802879; -5.695253136140104e-5 0.00047218313959282833 -0.000876751754865384; 0.0006037478990668497 0.0012541263361331907 -0.0008749175799459732; 0.0012854573057449197 0.00037439952294959084 -0.00407951794342153; -0.00026628997551506755 -0.00011729783888779998 0.0009297674290255674; -0.0012648533056256346 0.0007479129505685018 0.0011463050833782505; 0.0026829882742226622 -4.3336037022148286e-5 -0.002354589265577836; -0.0009568725945547542 0.0006208008524566795 -0.0010999003599285553; 0.00015863009718356034 -0.0015194855053040292 0.0009518269186609691; 0.000568288318296758 -0.00038445691229253517 0.00035190897738994085; 0.0028575407648951693 0.0030038628925942103 0.0004949141070515486; 3.14789406132907e-5 -0.0016275384477056104 0.0004109024874524931; -0.0011360281433551878 -0.0021827592685125675 0.0037502895476599794] %
+
+Mass Used: 76.15369819431544 kg
+Launch C3: 128.02816211970992 km²/s²
+||V∞_in||: 0.1204740139225916 km/s
diff --git a/archive/ES_0.7059200527022844 b/archive/ES_0.7059200527022844
new file mode 100644
index 0000000..72351a4
--- /dev/null
+++ b/archive/ES_0.7059200527022844
@@ -0,0 +1,22 @@
+archive/ES_0.7059200527022844---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T07:21:41.503
+Launch V∞: [5.347657014108514, -8.446040993535144, -1.9703234612230816] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-4.7252720004262435e-6, 2.357363886922983e-6, 4.492849619282846e-6] km/s
+ V∞_out: [-3.0334037544730216e-6, 4.364891243949767e-6, -4.455399853729173e-6] km/s
+ time of flight: 1.2844346581015225e8 seconds
+ arrival date: 2027-05-18T22:06:06.503
+ thrust profile: [0.2508928310757564 -0.16839783744050868 -0.15394292827397985; 0.1497493629833447 -0.01580422528070588 -0.18896912739096253; 0.14561962587762747 0.016274964077760568 -0.26792302658001593; 0.12110506751790223 0.029438698453759835 -0.29036820025576165; 0.08008871304561573 0.02846767508437284 -0.24086883946350507; 0.02976168857862409 0.018174924137805536 -0.1380876315849644; -0.03121291827838735 -0.02004221837783908 -0.12783783013380606; 0.10866765881998955 -0.008008547195784942 -0.04574692696075756; 0.01918777265908566 0.017226075903047845 -0.0011168223919559156; 0.028466748253105897 -0.025252412758083143 -0.0582932011843876; 0.18204191856353996 0.07685526445036606 0.06433509304356733; 0.16771169935460442 -0.2335539856048301 -0.04107759954464611; -0.12562161195097787 0.1559362471442369 -0.13307877271527574; 0.07527849747483438 0.030697633050902902 0.1944693377156965; 0.026815798464955028 -0.09793039114475607 0.08840050902644644; 0.10968742742770168 -0.2025269389018637 -0.026954586406143524; 9.162520142719211e-6 0.07771948925814168 -0.02216087302257045; -0.24826164399564826 -0.05087048766519422 0.11101234609124483; -0.02376808993348636 -0.035211450697626406 0.0998533026459278; -0.04986985278800439 -0.241329633687976 0.47310059257520437] %
+
+Mass Used: 217.98461996261221 kg
+Launch C3: 103.81521854686622 km²/s²
+||V∞_in||: 6.933329479757245e-6 km/s
diff --git a/archive/ES_0.7084124096212076 b/archive/ES_0.7084124096212076
new file mode 100644
index 0000000..c39d65b
--- /dev/null
+++ b/archive/ES_0.7084124096212076
@@ -0,0 +1,22 @@
+archive/ES_0.7084124096212076---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T18:50:23.105
+Launch V∞: [7.4460624664867625, -7.47972105582765, -2.3084771039388103] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00010201210068111245, -0.0012568262699026922, 0.00032363202775845777] km/s
+ V∞_out: [0.0003695053932902023, 0.0008030525619356994, 0.0009558655330841463] km/s
+ time of flight: 9.779623629490551e7 seconds
+ arrival date: 2027-06-13T16:27:39.105
+ thrust profile: [0.7014004205558874 -0.3713564664190846 -0.36879599465326185; 0.3089789526797018 -0.036757119162515506 -0.2809783056959382; 0.14367131604589534 0.0009386058532719519 -0.1786327810192271; 0.11592323594423326 0.009790466402712644 -0.18186275432359192; 0.036805308651212135 -0.006275702669903057 -0.03635151643584415; 0.027609586460508033 0.014938235941740582 -0.010408684626312736; 0.03578444348931642 0.051724923130006116 -0.12037547529840377; 0.03517674125255074 -0.0036672409237722406 0.052409033614015145; 0.03980668058783179 -0.004826804144870981 -0.11675119248271221; 0.023901143123474668 -0.02556175268755166 -0.11900349182843303; 0.032891843622970034 0.10248770903039242 -0.02260530878610599; 0.05148195344939988 0.10228205705849708 -0.008155489824708777; -0.008050391492702445 -0.13111536628694348 0.027230153072636612; 0.008885500025697556 0.008048243250645248 -0.033641079623141806; 0.03536146141056837 -0.014611145054250043 0.007608886331160296; 0.09777972207642709 0.013179295493935043 0.13580812515028834; 0.048648371812409094 -0.016754900664322427 0.002129395136151498; 0.30659146511264096 0.13773889618080404 -0.0062767223651840585; 0.03646992634503202 0.03679703806437264 -0.03396772525120896; -0.018178775913238274 -0.23027567201712498 -0.34724875178782144] %
+
+Mass Used: 145.61949533260122 kg
+Launch C3: 116.71913986722414 km²/s²
+||V∞_in||: 0.001301828111078394 km/s
diff --git a/archive/ES_0.7085338490018759 b/archive/ES_0.7085338490018759
new file mode 100644
index 0000000..d7b0f4b
--- /dev/null
+++ b/archive/ES_0.7085338490018759
@@ -0,0 +1,22 @@
+archive/ES_0.7085338490018759---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T12:49:22.640
+Launch V∞: [6.818661412038466, -9.040324514873744, -2.688174566908497] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0010906387053894373, 0.0006005022835749319, 0.0011523594737183473] km/s
+ V∞_out: [-0.0005879920760801823, 0.001153468328378006, -0.001096566046852046] km/s
+ time of flight: 8.826788309179583e7 seconds
+ arrival date: 2026-02-10T03:40:45.640
+ thrust profile: [0.3094379750907703 -0.23164497255477376 -0.1410953220631138; 0.18319107255930642 -0.04705634307864633 -0.12604664653046363; 0.05913793930215743 -0.0024926602610397964 -0.058085275771356214; 0.07157197557012891 0.004590317998640019 -0.07990475844881523; 0.08911856215491257 0.008304027662420362 -0.10670183629511232; 0.03034590727151985 0.005694993550349514 -0.04568405810265874; 0.0017600685076705261 0.0003387929942253841 -0.0027676856323145265; 0.0026607103709974035 0.0006817323303220891 -0.004537757652964216; 0.00026374196548695905 0.00015304890907520945 -0.000423256252010228; -3.9360865483765604e-5 0.00015871630543149134 -9.266887512374792e-5; 0.0004744243613943888 -0.00018207392508156047 -0.00045741863710461577; 0.00035384311540167905 0.00011513285172614406 -0.00033657180615892583; 4.2617395986071626e-5 1.908192014017126e-6 -0.00028543530106891856; 5.4660916380074926e-5 -9.199707245902155e-5 1.9797079381247452e-5; 0.0007264843318882783 0.00038472952439646646 -0.00021016310649707337; 0.0002891165164538379 0.0003760931800684113 -0.00019154092428584645; -0.0004865932075295608 0.0005541766700491012 -0.0005525843019436437; -0.0001920849387175176 -0.000113557878015279 -0.0007628400157305635; 0.0003080120180570123 -5.526686742185515e-5 -0.0007625286300949973; 4.73476561897089e-5 0.00023647966353621065 -0.0004265378874650658] %
+
+Mass Used: 36.51011298638605 kg
+Launch C3: 135.44789328842327 km²/s²
+||V∞_in||: 0.0016964752090557298 km/s
diff --git a/archive/ES_0.7092865972047595 b/archive/ES_0.7092865972047595
new file mode 100644
index 0000000..e62d458
--- /dev/null
+++ b/archive/ES_0.7092865972047595
@@ -0,0 +1,22 @@
+archive/ES_0.7092865972047595---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-08T12:38:26.350
+Launch V∞: [8.65993274530606, -7.002687542986991, -0.40381409915132527] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012110595797604684, 0.07240067097851446, 0.0893200275332611] km/s
+ V∞_out: [-0.048512287498298716, 0.039466846431924635, -0.09709940524733807] km/s
+ time of flight: 1.87495777875467e8 seconds
+ arrival date: 2030-05-18T14:48:03.350
+ thrust profile: [0.004505862152116836 -0.005037072564500129 -0.002112374098423517; 0.006075879383702263 -0.017646205529371038 -0.00950925694719818; 0.03527363579871972 -0.11591129036512529 -0.062038112615110136; 0.06430535481707596 -0.18790125909030425 -0.10119983790014671; 0.11066501988975821 -0.29009245184539423 -0.1552069942648133; 0.07831244799911254 -0.18936034082762196 -0.10709832441601606; 0.05965824282392989 -0.1349402727531395 -0.07855904855987884; 0.06870986908727532 -0.14587407873695032 -0.08595775116056055; 0.00383730669919725 -0.007682520036104407 -0.004873053130328659; 0.019042981762216155 -0.03676881734991965 -0.023026534144728064; 0.000357419142328245 -0.0006662108318113703 -0.00038032320143470964; 0.0005051338775340253 -0.00019737641632952313 -0.00014356507433120733; 0.000554835076633863 -0.0005701323019383924 -8.206935427484616e-5; -1.6055787429694143e-5 0.00027732445915657796 0.0004441529104484282; 0.00021327143022455052 -0.0002934079010263965 -0.00011631168035306802; -4.836181476621838e-5 -0.0003292572992714447 -0.00043949309626494903; 0.0017374058766313565 -0.0007512883894038275 -2.326884258323312e-5; -3.931630244130807e-5 -0.00027676637779902493 -9.451361313357945e-5; -2.435376502802006e-5 0.0005200356905198391 -0.0010056701347337718; 0.0001842493848310628 1.5052090258472182e-5 0.00047512704168215447] %
+
+Mass Used: 103.02941621203672 kg
+Launch C3: 124.19513380460273 km²/s²
+||V∞_in||: 0.11561397410025566 km/s
diff --git a/archive/ES_0.7095651248229892 b/archive/ES_0.7095651248229892
new file mode 100644
index 0000000..b7b93ac
--- /dev/null
+++ b/archive/ES_0.7095651248229892
@@ -0,0 +1,22 @@
+archive/ES_0.7095651248229892---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T20:24:24.708
+Launch V∞: [8.152642159898935, -7.574909013478245, -2.2559511262593666] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.007328647691213388, -0.051656499513930663, 1.0278059145583953] km/s
+ V∞_out: [0.16675431775776164, -1.0154355157449186, 0.01085955525483851] km/s
+ time of flight: 8.64035115812454e7 seconds
+ arrival date: 2027-02-03T21:22:55.708
+ thrust profile: [0.8211823486469534 -0.40554192867405076 -0.3629036278016129; 0.46848625062281435 -0.03457155872951386 -0.3377749692206691; 0.23562455692789186 0.02265849614742718 -0.24355729671374426; 0.10396229343491546 0.018987139192927143 -0.1352795987931744; 0.04847207174376856 0.01156362195590863 -0.07318156945870605; 0.004687061174653947 0.0010859230515424046 -0.007438969196203247; 0.0012104917456283244 0.0007831169503605064 -0.0018747539516531203; 0.0008424499079562044 0.0002440126660343591 -0.0018826472927754032; 0.0003685287243320595 0.00017672683401964625 -0.0021856463704622337; 0.0002935664741470993 0.0002141651717709132 -0.002591199557971998; 0.00013165735216022918 0.0008469454871136384 -0.001508755407005475; 0.0009577345201493302 7.16514450122452e-5 -0.0008249963674011162; 0.0012708699121657119 -0.0003976773748316552 0.000534918912811751; 0.0017387508669329053 0.0005231089550123517 -0.0029570247674418825; 0.0005955947988013176 0.0002553745861728205 -0.001541878366651052; 0.0014794151488039435 0.0014302852820283797 -0.0007105982545335665; -2.922356970144844e-5 0.0008993471142997873 -0.0008671280384918746; 0.0005723454138225341 0.000757203002347977 0.0014129656093686766; 0.0013670426786081995 0.001702647891122856 -0.0017703106675086915; 0.0004934642807428213 0.0007062451560645391 0.001003722389735665] %
+
+Mass Used: 75.71018426236651 kg
+Launch C3: 128.93413623390643 km²/s²
+||V∞_in||: 1.0291292926645486 km/s
diff --git a/archive/ES_0.7106277508797827 b/archive/ES_0.7106277508797827
new file mode 100644
index 0000000..e75423b
--- /dev/null
+++ b/archive/ES_0.7106277508797827
@@ -0,0 +1,22 @@
+archive/ES_0.7106277508797827---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-08T05:48:08.812
+Launch V∞: [7.058700408366555, -7.477548608063417, -1.8219530142498643] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0004299239158571619, -0.0002146352845620137, -0.00106028366502546] km/s
+ V∞_out: [-0.0005250049573648633, -0.0010383607544386254, -3.325137301242741e-5] km/s
+ time of flight: 1.0927073665824285e8 seconds
+ arrival date: 2027-10-24T22:47:04.812
+ thrust profile: [0.553124858381225 -0.2872966687067561 -0.34631520542602723; 0.2740368123390711 -0.0345577652378042 -0.3706382653099568; 0.15913397753537134 -0.013423090460876055 -0.30191479740568217; 0.10983202135001408 -0.014048627607135655 -0.27514039042948313; 0.07374961420030328 -0.013714059620688307 -0.2301758125304599; 0.04395451672199563 -0.01470404504431547 -0.17578663755088558; 0.018674286603498187 -0.01628760672155779 -0.1144921204202807; -0.0010052650850220501 -0.02075122838622195 -0.039330925088602364; -0.01773264361096044 -0.025646566232511624 0.05087144606899305; -0.040333179708999016 -0.04095826202469321 0.14091605803691468; -0.006614980812110688 0.012629960352267683 0.0006106330866166142; -0.0570946533962408 0.18653169839946834 0.03887820965313852; 0.023120740806969 0.14207689332833767 0.03372283011723242; 0.05925471728014284 -0.0898333519888513 0.08977829946879606; -0.06342964972295569 -0.22032467844520986 0.030229174197665187; -0.05127988525376297 -0.023165962345824253 0.11002535206255244; -0.008458515107989398 0.020976518104329385 -0.011405533686304849; -0.03942488681665506 0.09320625041234037 -0.18658733539321498; 0.16525350117901955 0.07754420581850657 0.33502707874850385; -0.05691545437245159 0.19046189334947491 -0.2847755951363308] %
+
+Mass Used: 192.89114103464954 kg
+Launch C3: 109.05849742715948 km²/s²
+||V∞_in||: 0.0011640894850159908 km/s
diff --git a/archive/ES_0.7108735196419596 b/archive/ES_0.7108735196419596
new file mode 100644
index 0000000..e321c32
--- /dev/null
+++ b/archive/ES_0.7108735196419596
@@ -0,0 +1,22 @@
+archive/ES_0.7108735196419596---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T08:59:16.010
+Launch V∞: [6.636120312355136, -9.062835074600471, -2.5129528716276797] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.07453967522605967, 0.050968624014962625, 0.09420481357635103] km/s
+ V∞_out: [-0.04237940814409329, 0.08963547110402116, -0.08484493061985303] km/s
+ time of flight: 8.812229936581476e7 seconds
+ arrival date: 2026-02-09T07:24:15.010
+ thrust profile: [0.5706093050976743 -0.43256646614565725 -0.2769840695409991; 0.2206316734117003 -0.06088997570344648 -0.17163073454226963; 0.0599420079170459 -0.0050082681759998785 -0.06590546378762228; 0.0416786992272192 0.0016509888613389062 -0.053323540972976625; 0.066406223736814 0.006123976253426823 -0.10073301058332118; 0.04091144720793393 0.0034299700507539692 -0.06831431497194548; 0.0037327425759777384 0.0031081077294287797 -0.004137817556081025; 0.0061312766193650885 0.00022633224662385793 -0.011326690412420667; -0.0029033438395254575 -0.002519058168409026 -0.0015124209518248511; -1.4204108351099226e-5 0.00033796844136307143 -0.002312991244180997; 0.006625817485535977 0.0019180961611494384 -0.0005238779753748716; -0.004447011778851783 -0.0006086067788897166 0.007106137437403626; 0.0012002633265303716 -0.0056565563805537275 -0.011200621116457803; -0.02558412767410058 0.004383528251754068 -0.007120700860011395; 0.0007171771356153619 0.0012023430054972676 -0.0062130023896693285; 0.016467644903038144 -0.015123508810938754 0.013943645804738565; 0.0009464092103305946 -0.00013178824141531513 0.002462174690735573; -0.022857703490786526 0.0046221119555822955 0.028160842673622583; -0.014175201041075766 -0.0036136290719581752 0.029106176933656712; -0.007997716818450362 0.0035454859891463817 0.01092762967038463] %
+
+Mass Used: 56.50574652280329 kg
+Launch C3: 132.48800452448276 km²/s²
+||V∞_in||: 0.13049333591314205 km/s
diff --git a/archive/ES_0.7114646297784627 b/archive/ES_0.7114646297784627
new file mode 100644
index 0000000..a0910dd
--- /dev/null
+++ b/archive/ES_0.7114646297784627
@@ -0,0 +1,22 @@
+archive/ES_0.7114646297784627---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T05:48:25.361
+Launch V∞: [6.591100239917693, -9.048965815393737, -2.3713843829362036] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0751859491677453, 0.05217293250457546, 0.09498701916569294] km/s
+ V∞_out: [-0.041386840390287484, 0.09207819264079664, -0.08487596369014591] km/s
+ time of flight: 8.73623358180955e7 seconds
+ arrival date: 2026-01-31T09:07:20.361
+ thrust profile: [0.6667323885304457 -0.5217726397629096 -0.30270975326155974; 0.3467885219648863 -0.10689141302291465 -0.25762162949649137; 0.1056730489575207 -0.007837247094065695 -0.1009725378496145; 0.12386498619542027 0.009417985282657977 -0.12963117345926994; 0.08167033527503742 0.009637901845350525 -0.09602182779737084; 0.0006828519520869086 0.001572337535606109 -0.001457093781744893; 0.006297303600164518 -0.000858774303802678 -0.009037547588060168; 0.002297809843292723 0.0022279439859003106 -0.0044437695058993955; 8.189862296133221e-5 0.0013714938845847493 -0.0005062540018855354; 0.0019412499367716094 0.00207774921809611 -0.0010923237842051185; -0.0014558231520522098 -0.004362053555914309 -0.004569761688403808; -0.0007424992345522014 0.009923236492223295 -0.003498327529708115; 0.008200402791885572 0.0032010050131608416 0.0009687542776051492; 0.0008955528929986111 0.002734834993290751 -0.0007983730015116738; -0.0002002105726567949 0.001675955408275782 -0.00039728098922380104; -0.002218353319808927 0.012252496266964362 -0.0006007953687822982; 0.0008477754675917191 0.00452013090046673 -0.002119269635055125; 0.00317209587491613 0.0006885306736863408 -0.00562657477396658; 0.00019486799038716585 -0.01134505518720947 -0.005595203184875535; 0.007398031144783656 -0.0038159901863921526 -0.012523989858124838] %
+
+Mass Used: 66.16795128563263 kg
+Launch C3: 130.94984859244124 km²/s²
+||V∞_in||: 0.13189949070548182 km/s
diff --git a/archive/ES_0.7139814539786293 b/archive/ES_0.7139814539786293
new file mode 100644
index 0000000..e2bab12
--- /dev/null
+++ b/archive/ES_0.7139814539786293
@@ -0,0 +1,22 @@
+archive/ES_0.7139814539786293---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T07:53:38.113
+Launch V∞: [7.953302569540452, -7.5127702869347255, -2.223449709220247] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0002182555167615519, -0.00267963581594737, 0.0007643009896819524] km/s
+ V∞_out: [0.0006700311153278017, 0.0018637568991037698, 0.0019722987148613896] km/s
+ time of flight: 8.830317485422151e7 seconds
+ arrival date: 2027-02-25T08:33:12.113
+ thrust profile: [1.0 -0.5639886988328527 -0.46001560101668815; 0.4436980856410141 -0.03871767389440145 -0.30584690495937544; 0.18290103874647426 0.014784745850907775 -0.16847851439335063; 0.12662625303605887 0.022147432874575452 -0.14127683056636958; 0.026106602401838475 0.007224904827417473 -0.020311670286050108; 0.04948002517424371 -0.006606058383136949 -0.017734051535159355; 0.018254870331710332 0.004143443509486903 -0.020609936828209857; 0.01381449719572673 -0.008991233393252814 -0.02059059077877637; 0.021027929789626785 0.0070019681706686675 -0.006120608231759943; -0.014817925275864405 -0.019538785288298312 -0.006848371949554684; -0.009375790359345678 0.003950701053857555 -0.010523552161273415; 0.00015565810643424762 -0.003015896677958504 0.0018124078393628661; 0.011536969010238126 0.009960704967000085 -0.020730866485115188; 0.0004990075551325503 -0.004502659080205818 -0.02743841287095463; 0.003177904411556295 -0.007241667431463089 -0.09837712678385346; -0.028092324664122197 0.1151755318280605 -0.08346280989061161; -0.010514792355245543 -0.007474536632885066 0.005423311558980845; -0.008482616329108895 -0.001023322068853434 -0.09909241144133812; 0.05337887907591832 0.04270657795291534 -0.06465404314190026; 0.04091502507048238 -0.0705791188572433 0.011787579051664797] %
+
+Mass Used: 105.90896772975293 kg
+Launch C3: 124.64046775633965 km²/s²
+||V∞_in||: 0.002795038386057263 km/s
diff --git a/archive/ES_0.7141585759386689 b/archive/ES_0.7141585759386689
new file mode 100644
index 0000000..f6f2488
--- /dev/null
+++ b/archive/ES_0.7141585759386689
@@ -0,0 +1,22 @@
+archive/ES_0.7141585759386689---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-24T08:54:17.899
+Launch V∞: [6.125196824097343, -9.480720388447564, -0.4086740916385957] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.9683918798125325e-8, 1.6061454877995996e-5, -1.0735212337993156e-5] km/s
+ V∞_out: [3.497051466980139e-7, -1.892160282443366e-5, 3.8353308379700606e-6] km/s
+ time of flight: 1.7909056132745296e8 seconds
+ arrival date: 2029-01-25T04:16:58.899
+ thrust profile: [0.009438225232782831 -0.016433669581797754 -0.010267987871550024; 0.006796876130337534 -0.03767420108563165 -0.03468416272506687; 0.003260922994846099 -0.048013575321714706 -0.04485150871561597; 0.013162540739876239 -0.1663663116025297 -0.15222605293529873; 0.010995768391255153 -0.11764441647984607 -0.11092549110820975; 0.019192848506256462 -0.15571113499446562 -0.14602298852154086; 0.020557339606324956 -0.1417302263308921 -0.13438705573635157; 0.017983266829877137 -0.10982696482098653 -0.10601211699393026; 0.009111758320617003 -0.04984065208568458 -0.04956813274282456; 0.004343418744558086 -0.01971411390140123 -0.0181207089756105; 0.004312765304037969 -0.012938217568879503 -0.012111701911506713; -0.004229553270199979 0.0003312902340517148 0.00013609596333599662; 0.0009513860247414571 0.0025119788356207035 0.002179158867529029; 0.0007189001513120572 -0.0022798840402234546 -0.0013641147924458095; -0.0072674551518418645 0.0054223137250117015 0.005299606674959722; 0.001241980903784429 -0.0012674274600358417 0.003364843200755435; 0.00364253301979645 -0.0033275515572414884 0.0023253883362935944; -0.0004154509680502548 0.0009423744184505487 0.001974914534768197; 0.005188848507168487 0.0022007331204827213 -0.005668494110976505; -3.265370862553176e-5 -0.0002938430028378176 -0.0003055791989830574] %
+
+Mass Used: 89.03186516408141 kg
+Launch C3: 127.56910973103412 km²/s²
+||V∞_in||: 1.9318817032963302e-5 km/s
diff --git a/archive/ES_0.7144947454169017 b/archive/ES_0.7144947454169017
new file mode 100644
index 0000000..d29931b
--- /dev/null
+++ b/archive/ES_0.7144947454169017
@@ -0,0 +1,22 @@
+archive/ES_0.7144947454169017---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T17:09:46.800
+Launch V∞: [6.517855135289844, -8.955818930849535, -2.275928481775568] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.09777075127601104, 0.06688363624692797, 0.1268628498938963] km/s
+ V∞_out: [-0.05786156516435492, 0.11589998610710628, -0.11555345204656324] km/s
+ time of flight: 8.728594063048638e7 seconds
+ arrival date: 2026-01-29T23:15:26.800
+ thrust profile: [0.9498240680541659 -0.7290037095650034 -0.4175637508704313; 0.4102282702298949 -0.10841362439229119 -0.28321188921344553; 0.18406712636325728 -0.015327260458353486 -0.17504692719887144; 0.10155446890388468 0.0021646862433575996 -0.11442949951017593; 0.042912946105224205 0.005381679907799681 -0.05526711644417083; 0.014377527069602582 0.0016429980021667044 -0.020655990654270588; 0.006824545312623514 -0.00044821871437386975 -0.017044931130446174; 0.013719569192505391 -9.797870918864351e-5 -0.015916008989823264; -0.005414153804683191 0.0013446333007887522 -0.012387129543161153; -0.006709109604422413 0.010927675466404293 -0.009214671339038267; -0.00032701933109954774 0.0009861835018281297 0.008340089312273136; -0.00332172017999487 -0.0015491016135801947 -0.0038978821720442635; -0.017599746671496205 -0.010119488839567498 -0.0005604729123981416; 0.004485388273114178 -0.006844590109230872 0.02051055194481032; -0.01609833655613232 0.012894141568920624 0.005194147481802296; 0.023763188387537826 0.004537441950081451 0.0048938100382730915; 0.015162663194289385 -0.015742179681562798 -0.00905292157194941; -0.0019715686753235023 0.012852951700138187 0.004070518848619888; 0.0024041472173668027 0.001541542660706924 -0.0022466153920151933; -0.014845690608487193 0.004901328928081708 0.025240837796951576] %
+
+Mass Used: 87.67482699754328 kg
+Launch C3: 127.86897874094436 km²/s²
+||V∞_in||: 0.17357051387228262 km/s
diff --git a/archive/ES_0.7147336424301873 b/archive/ES_0.7147336424301873
new file mode 100644
index 0000000..70ca538
--- /dev/null
+++ b/archive/ES_0.7147336424301873
@@ -0,0 +1,22 @@
+archive/ES_0.7147336424301873---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-29T00:10:18.497
+Launch V∞: [6.279563498878469, -7.443238645346673, -0.12881030889281234] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.2815208513685269e-9, -1.8361212833781008e-9, -1.275883969519786e-9] km/s
+ V∞_out: [1.1974870133089178e-10, -2.5382337079149974e-10, 3.849807893100264e-10] km/s
+ time of flight: 1.8118670857980534e8 seconds
+ arrival date: 2029-01-24T01:48:46.497
+ thrust profile: [0.4641603227265268 -0.1451139413801847 -0.13930324834385283; 0.019898611878432376 0.001595833025431568 -0.05086849626943207; 0.05125363780689901 0.02828299961731172 0.003324998383651967; 0.0546190692943736 0.004840268156027203 -0.12250280228174079; 0.06067352712145431 0.012126171408888789 -0.23250664608568147; 0.027966479779706302 -0.0008639868844048139 -0.15034950351544824; 0.02424385721000459 0.013312535908830669 -0.07189621807546631; -0.02792939886507178 0.06860743744593205 -0.014383288672201837; 0.006023570961345908 0.0002061886510303292 -0.0833876183369962; -0.03417306929864722 -0.09803525591142527 -0.087253845482051; 0.02374029728733915 0.03505478896203923 -0.004939906763706561; 0.03682186926504505 0.11084622578322027 -0.04297782800209732; -0.0395281290516324 0.06066711185006937 0.041726205336622545; -0.01494915038075974 -0.08797974862292153 0.00772672557391145; 0.22276983125857203 0.05600787688150215 -0.0648943371726816; 0.09172025535030218 0.08278897156367207 0.03130251549450451; 0.062251824545085085 0.3211761141977274 -0.028713879115260008; 0.2674197802380159 -0.24448246942897955 -0.08996902335980764; 0.39021851898909415 0.03740274032651875 0.2412607393689995; -0.45452022857233165 -0.005616125864269111 -0.2122056286585054] %
+
+Mass Used: 280.55659988026673 kg
+Launch C3: 94.85131136370603 km²/s²
+||V∞_in||: 2.5771140765290004e-9 km/s
diff --git a/archive/ES_0.7159904978382032 b/archive/ES_0.7159904978382032
new file mode 100644
index 0000000..79b6b71
--- /dev/null
+++ b/archive/ES_0.7159904978382032
@@ -0,0 +1,22 @@
+archive/ES_0.7159904978382032---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-22T22:59:17.026
+Launch V∞: [7.605638590536802, -6.844049956113111, -0.984230224487684] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.34370652559214665, 0.5803299718142363, 0.4349841692480302] km/s
+ V∞_out: [0.5931211658619207, -0.47375633444927756, -0.241026058421744] km/s
+ time of flight: 9.657000026361541e7 seconds
+ arrival date: 2027-05-15T15:59:17.026
+ thrust profile: [1.0 -0.5791721006777192 -0.3075163002225379; 1.0 0.03236503622589058 -0.5174094796822174; 1.0 0.2732688699534307 -0.5882211022911369; 0.8259209496297045 0.34740465768731654 -0.5933917453652886; 0.6067339290812186 0.3194452823524064 -0.5017300244805657; 0.09443045236280725 0.05897754953384141 -0.09384744173692565; 0.03407216492984167 0.02389698037850792 -0.0384010673486992; 0.012959205984030105 0.010400172249600425 -0.01706101757407561; 0.01135658013025852 0.008794346961491574 -0.014193977274992548; 0.0011596764867948723 0.0008917735953492744 -0.0015628016199722159; 0.00038177116754436146 -0.00023814213640642597 -0.0005027850380400337; 0.001158982216624835 0.0005440618360987328 -0.0007230708796881744; 0.00036548486008179627 0.0005891408065505973 -0.000552055642528999; 1.5591032117422403e-5 0.00037384409743231186 2.6418382678152625e-5; -9.151072176454635e-5 0.00022801036100909578 0.00044514300545185983; 3.4224309232348186e-5 0.0005476413531308369 -0.0003693758944725621; 0.000771463389102245 0.0002563059378841994 -0.00022096903544894104; 0.0001525861389060168 -0.0005603526412737761 0.00021041423834003008; -0.0004921952590696565 -0.00021948377359720563 0.0009333166512418456; -0.0011835376601324118 9.807491449924719e-5 -0.00022236618034590975] %
+
+Mass Used: 218.99868819039784 kg
+Launch C3: 105.65546730642959 km²/s²
+||V∞_in||: 0.8025760271880392 km/s
diff --git a/archive/ES_0.7169248965472063 b/archive/ES_0.7169248965472063
new file mode 100644
index 0000000..ff547db
--- /dev/null
+++ b/archive/ES_0.7169248965472063
@@ -0,0 +1,22 @@
+archive/ES_0.7169248965472063---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-06T17:35:55.451
+Launch V∞: [8.32605785521903, -7.359950528708196, 1.454866097854272] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0013454073763417328, 0.0008054092111134315, 5.229183698390092e-5] km/s
+ V∞_out: [-1.0813387482666367e-5, -5.97023951041024e-6, 9.009308090990684e-6] km/s
+ time of flight: 1.833117469152075e8 seconds
+ arrival date: 2030-03-29T09:31:41.451
+ thrust profile: [0.005204949996589699 -0.003924633537511397 -0.002650383585136816; 0.001460967890080618 -0.0022816303155181634 -0.002447999635020942; 0.05608567075325921 -0.12349907770551996 -0.12620562317141013; 0.07026060994543147 -0.15713463489315038 -0.16138472880119328; 0.06137153191409448 -0.13199839343133496 -0.1379520175668597; 0.09817481719535857 -0.20250563930805354 -0.21158039473202223; 0.07225934310788885 -0.14198653046580137 -0.15151879562754758; 0.04130806356969707 -0.07792467531922488 -0.08500174186220666; 0.03802632329755955 -0.06924305820349837 -0.07647685327224436; 0.003346210238678274 -0.005933887192877415 -0.006670835607496436; 0.0002613516238862053 -0.0014287019397521352 -0.0007102283563044921; 0.001042514795495586 -0.0005603681996931716 -0.0009627622179642849; 0.00019568769111859004 -0.001425100589994311 -0.0012918633257463065; 0.00036023106373080354 -0.0006563725273043557 -0.0007583330997466406; 0.00024392762831152207 -0.0006753381173596061 -0.0012057789897320067; 0.0002284556882467105 6.077548537675436e-5 -0.0007531925130589963; -0.00038608379666576 -0.0014828122588511853 -0.0003254292180459427; 0.00012379089180386028 -0.00015377934503137776 2.308457460267787e-5; 0.0014292584461768165 0.0005970601922313987 -0.0010207978698738383; 0.0002736603227043342 -0.005358698085517945 -0.0010392425570520168] %
+
+Mass Used: 103.69469106073575 kg
+Launch C3: 125.60874655617228 km²/s²
+||V∞_in||: 0.0015689293935280378 km/s
diff --git a/archive/ES_0.7179513215391323 b/archive/ES_0.7179513215391323
new file mode 100644
index 0000000..55ea40d
--- /dev/null
+++ b/archive/ES_0.7179513215391323
@@ -0,0 +1,22 @@
+archive/ES_0.7179513215391323---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-04T19:37:47.491
+Launch V∞: [8.13449692321803, -7.152380085100097, -1.9711922315162218] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.045980662523286066, 0.5254975148613225, -0.1490956929161043] km/s
+ V∞_out: [-0.17898623811765743, -0.289124875507492, -0.3585259536405586] km/s
+ time of flight: 8.699040003990117e7 seconds
+ arrival date: 2027-02-05T15:37:47.491
+ thrust profile: [0.9990864447152996 -0.5837458495030735 -0.4607833521026554; 0.9980149576564251 -0.0408569273609896 -0.5768853960982762; 0.5233349991924467 0.08708264099348456 -0.40748420689126286; 0.2170540524810489 0.062219449351424816 -0.21198574396428732; 0.07518717382565591 0.02317713757008796 -0.08169981095704115; 0.02669411986685458 0.004456878740152211 -0.028114869521097326; 0.004420087233387715 0.0023264104982396185 -0.009462396954268166; 0.011694500416075811 0.00252207387671106 -0.030821131370883853; 0.016709241502060115 -9.629342356469095e-5 -0.015696853101231097; 0.00397882876817678 0.004114662402530136 -0.006823921015586517; 0.004756299352080816 0.003992928829423108 -0.009194552192686034; 0.014533377081788345 0.0031070485323364573 0.0023966357847722067; 0.004708597697200537 0.002934649886321058 -0.0038618892411011194; 0.001321999149946461 0.002131403690711582 -0.0015336393183267084; 0.020581016492253974 0.015948746330032522 0.002418723115298777; -0.011048699013126679 0.009902181320487823 -0.005469848481334746; 0.0055347337880216375 -0.016321750674686983 -0.03274585059848675; 0.01687367078640818 -0.0010143918664172612 -0.014127101701381536; -0.0029596237521403532 0.01846711804230159 -0.003782643892645248; -0.005605158976344289 0.004089483878832156 0.0006512383743243325] %
+
+Mass Used: 130.5388257754962 kg
+Launch C3: 121.21217988916997 km²/s²
+||V∞_in||: 0.5481709451417864 km/s
diff --git a/archive/ES_0.7184537785719708 b/archive/ES_0.7184537785719708
new file mode 100644
index 0000000..c332ef0
--- /dev/null
+++ b/archive/ES_0.7184537785719708
@@ -0,0 +1,22 @@
+archive/ES_0.7184537785719708---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T19:52:32.357
+Launch V∞: [8.248121134795204, -7.508657058104971, -2.2564725013041156] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.22721385325360474, -0.7066376754574374, -0.8637954004367607] km/s
+ V∞_out: [-1.0369407711474312, -0.15850319059675325, 0.44361915029532223] km/s
+ time of flight: 8.485074484804764e7 seconds
+ arrival date: 2027-01-16T21:31:36.357
+ thrust profile: [1.0 -0.5801911321297696 -0.4703450378738949; 0.5584477498293959 -0.048950346638669484 -0.3600612685874144; 0.21176277606926877 0.023170898290572742 -0.19515582627382785; 0.0652421160870537 0.0141752440229816 -0.07891093369344004; 0.020202002923730367 0.005408846052167935 -0.028521182961922662; 0.038525870154962186 0.012148585255491314 -0.05894187172635446; 0.00765095689272333 0.0024516578636509636 -0.012487985570810422; 0.0009527958209274757 0.0006948703395532378 -0.00200201370885077; 0.0015578301584990178 0.0016393525862830622 -0.0025626628649129367; 0.0015548252908391112 0.00034388641260142097 -0.002428391021115372; 0.0002868512345477908 -0.00023111505516671077 -0.0013708240458264686; 0.00018766961097455373 0.0006510410767857414 -0.0012427839064119057; 0.0003990338416022211 0.00017604266425373812 -0.0011094460999497993; 0.0005431962055691485 -0.0001707156955424098 -0.0009720925624789904; 0.00047882659300398425 0.0007023847360210654 -0.0016291670761083704; 0.00042543619471838287 0.0007075134140076495 -0.00025224371740596154; 0.00014987253111143142 0.00016027797877326763 -0.0003022736948271516; 0.0016074873333144007 -0.000385325161801497 -0.0014477080707118483; -0.0004274098730327843 0.0010968907311073798 -5.9095360652010917e-5; -0.00029207433675876803 -0.0006037346334594779 -0.0006410840792098624] %
+
+Mass Used: 82.7613178861443 kg
+Launch C3: 129.50310121962656 km²/s²
+||V∞_in||: 1.138905366262687 km/s
diff --git a/archive/ES_0.7186094411406051 b/archive/ES_0.7186094411406051
new file mode 100644
index 0000000..3ef36b3
--- /dev/null
+++ b/archive/ES_0.7186094411406051
@@ -0,0 +1,22 @@
+archive/ES_0.7186094411406051---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T01:41:03.188
+Launch V∞: [6.688124645520938, -8.993940361600169, -2.2854579488093254] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.037170998776997304, 0.024567537054493865, 0.048134182316867946] km/s
+ V∞_out: [-0.022684766901013797, 0.043327454840023254, -0.04373296084736511] km/s
+ time of flight: 8.642079774176699e7 seconds
+ arrival date: 2026-01-19T07:27:40.188
+ thrust profile: [0.5074952338176403 -0.3832852672523965 -0.21796494791036422; 0.7156943706132727 -0.19807403860209535 -0.40055607751084105; 0.33380595792185763 -0.024092540044595823 -0.2540914646421223; 0.06764845127272746 0.004667186952675681 -0.0765811881514568; 0.03679690367216384 0.0046487496104803475 -0.04786879927233222; 0.018325238552743185 0.0029727408734408125 -0.026749505279592054; 0.006232332196649203 0.0011229766441279748 -0.009387774497316488; 0.014258428337440095 0.0031411833669877267 -0.021179075799921013; -0.0002848629364984711 -1.0877231688599524e-5 0.00019164581036186577; 0.000700197523356054 -0.00046701221268557504 -0.0006218735820145995; 0.0005343397090729015 -0.00034038439807853866 -0.00010882533866077727; 0.0004976681145380537 -4.176910036049902e-5 -0.0006045624937788374; 0.000663076908015053 0.0005800632081730392 -0.0003051854912939614; 0.001201812317892212 -0.0002984563308200475 -0.0007226885846542628; -5.0381693629959735e-5 0.0011264095459893701 -5.32000452102419e-5; 0.0016392963711351204 1.2312368500165915e-5 0.00044486538639698745; 0.001210550331743386 -0.001484326219104859 -0.0009776661377648124; 0.0008623324023789056 0.0005837495085754066 -0.0012014364896468593; 6.398925806803772e-5 0.0012507944566941512 -0.0002549445602003477; -0.0005329447831042773 -0.0002687085807614516 -0.0008816914021334426] %
+
+Mass Used: 75.11347486008435 kg
+Launch C3: 130.84529253782085 km²/s²
+||V∞_in||: 0.06559075037165642 km/s
diff --git a/archive/ES_0.7188628243295501 b/archive/ES_0.7188628243295501
new file mode 100644
index 0000000..b974365
--- /dev/null
+++ b/archive/ES_0.7188628243295501
@@ -0,0 +1,22 @@
+archive/ES_0.7188628243295501---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T14:40:28.437
+Launch V∞: [8.31652266724318, -7.48745610032021, -2.388905586097654] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00023166657031431, 0.0035766280434349545, -5.484395438909427e-5] km/s
+ V∞_out: [0.0034608955982901833, -0.0005742527285557723, 0.0007353744328167253] km/s
+ time of flight: 8.498558732493699e7 seconds
+ arrival date: 2027-01-18T05:46:55.437
+ thrust profile: [0.9795249859749108 -0.47421186036770024 -0.41123091376267823; 0.47206478685170344 -0.03942425519514001 -0.317375805210335; 0.18692595694425074 0.01835638538254342 -0.17488709916075326; 0.03598598966341836 0.0077857589211865865 -0.043965952285783864; 0.007349483611194868 0.0025781452847168317 -0.008101861747221946; 0.03819657592031285 0.012082360720459782 -0.0570925135021736; -0.004201959900036306 0.0035775900151196853 -0.004186508913632253; 0.004371164682725687 -0.0008988058534284602 -0.011000507851268973; -0.0015063536594080414 -0.003130608342190804 -0.014766375950839294; 0.0026302272119167235 0.0012326005561682975 -0.005860732890535075; 0.003954227947465571 -0.002063621569830235 -0.0023911018118556704; -0.002406778044916925 -0.004887904246472863 -0.003095245967993509; 0.002369494120916157 -8.115156265421078e-5 -0.0010187419727517378; 0.0009463455901804652 0.0008742754722243795 -0.002323678274888684; -0.002849587709723673 0.0019217612554482844 -0.0021040398564978035; -0.002488846821798607 -0.0009367701683339987 0.0031731767038468695; -0.00017350447829194918 0.0015537482430339122 0.002618520271375858; 2.5683610325860087e-5 -0.002200835369175002 -0.00231809531080791; -0.005125968671033263 0.004097752308201006 -0.006382214896332744; 0.0020929350971460696 -0.0032708649201949056 0.000894313018536378] %
+
+Mass Used: 74.89502321950522 kg
+Launch C3: 130.93341802828053 km²/s²
+||V∞_in||: 0.003584542567778988 km/s
diff --git a/archive/ES_0.7196074483410565 b/archive/ES_0.7196074483410565
new file mode 100644
index 0000000..8b9c41c
--- /dev/null
+++ b/archive/ES_0.7196074483410565
@@ -0,0 +1,22 @@
+archive/ES_0.7196074483410565---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-31T21:38:53.095
+Launch V∞: [7.204964631043961, -8.871146395570968, -0.3227702345439427] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.1228758067440452e-9, -1.3181194843434377e-9, 1.5202745380836845e-10] km/s
+ V∞_out: [3.6293826884733936e-10, -1.2303548380555534e-9, 1.97757950711272e-10] km/s
+ time of flight: 1.5352894484367666e8 seconds
+ arrival date: 2029-04-12T20:34:37.095
+ thrust profile: [0.000465557980349396 -0.00018044239226547035 -0.0012491045026793166; 0.010230925049813308 -0.017708428019675312 -0.026716286415239966; 0.0119945140359656 -0.032604439426707474 -0.050709793610863106; 0.04650482225352745 -0.14516049990340912 -0.2253451034863484; 0.06299105169110408 -0.2054280192659658 -0.3067747185573506; 0.04753712961033866 -0.15244308825134617 -0.23567200601505586; 0.02955888590574148 -0.09160422806354929 -0.1447502178698093; 0.002897836436554751 -0.008785908127212808 -0.013728476573849426; 0.002196029981109633 -0.0066064821342419104 -0.010485615046298491; -0.0015754053491828252 -0.00024692490539130656 -0.004058118090748148; -2.6152964822889974e-5 -0.000488993189061277 -0.000877677240253774; 0.0002141332309936724 -0.0003771098287593698 0.0011877096574878145; -0.0006713912666837963 -0.0005381476013508535 0.0016217596113566979; 0.0013926290034162498 -0.0011523408667276891 -0.0017404208255126091; -0.00044634290874858535 -0.0016577757554577396 -0.002076388739388432; -0.0004831582852927443 -0.00010725626794767492 -0.00027987320687182933; 0.0023523442196916053 -0.0024582190059880458 0.0015245865932173334; -0.004247529752096933 0.0012345902006684075 0.00023658668589877918; 0.001909754538797861 -0.0037474668162264316 -0.003996483273003133; -0.00016586047276242306 0.0003164746507987033 -0.0014034748259042456] %
+
+Mass Used: 77.04990613633572 kg
+Launch C3: 130.71293433055376 km²/s²
+||V∞_in||: 1.7382178802119012e-9 km/s
diff --git a/archive/ES_0.7206567385999842 b/archive/ES_0.7206567385999842
new file mode 100644
index 0000000..11a498a
--- /dev/null
+++ b/archive/ES_0.7206567385999842
@@ -0,0 +1,22 @@
+archive/ES_0.7206567385999842---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T12:54:07.899
+Launch V∞: [8.302532440480947, -7.467481704297554, -2.3459935059969905] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0060911211197067884, -0.019192650550309786, -0.019967410433635528] km/s
+ V∞_out: [-0.02608373381573658, -0.004067630184699465, 0.010495156589063394] km/s
+ time of flight: 8.460694497406344e7 seconds
+ arrival date: 2027-01-13T18:49:51.899
+ thrust profile: [1.0 -0.5485399911327862 -0.4656818864638447; 0.6157319898297744 -0.05239916011401225 -0.3972210108126865; 0.2099265527200621 0.0196323801775247 -0.1851917319827252; 0.03933641522259702 0.007620560602047288 -0.04519708536855332; 0.009045327518564563 0.0018244257850189452 -0.011344958681938574; 0.0030605948005088257 0.0004916120164423193 -0.0038877648081581933; 0.0010248379839261539 0.0011784816690789779 -0.00198038728846376; 0.002841863648275405 -0.0007882799458717605 -0.003311197667549946; 0.001510611170971992 -0.00017874235103189644 0.0010139933323900377; 0.0008148126149100677 0.000908818514321277 -0.00028964884718642777; 0.0009110642208846533 0.0009923461079612873 -0.0014283043105864954; 0.006203420187769709 0.004521494783440548 -0.009654632285351548; 0.008861485736031485 5.933231853614705e-5 -0.004241962414049589; 0.001997807905249777 -0.0005762833208236499 -0.010802074400927909; 0.007757082621810504 0.0026388172760371063 -0.005552554464797892; 0.006430214541526695 0.0020564940280448523 -0.007927321241300288; 0.0005624632243346338 0.0005796059886103344 -0.0024303327127764103; -0.0013840462350781161 -0.0018482134549582196 -0.0009578361402404144; -0.0029868473966404322 0.009537319648914846 -0.005760115809836867; 0.0028783842832782584 -0.0010410478021142837 0.0004486475400049348] %
+
+Mass Used: 81.27194985326423 kg
+Launch C3: 130.19901345943728 km²/s²
+||V∞_in||: 0.028357663356956997 km/s
diff --git a/archive/ES_0.7211810940812462 b/archive/ES_0.7211810940812462
new file mode 100644
index 0000000..e4901ca
--- /dev/null
+++ b/archive/ES_0.7211810940812462
@@ -0,0 +1,22 @@
+archive/ES_0.7211810940812462---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T21:14:36.328
+Launch V∞: [8.296233674778259, -7.871100635365314, -2.6030011155758177] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.003096612146541454, -0.036872734550527524, 0.010050300117256527] km/s
+ V∞_out: [0.013556802178309709, 0.024525053848564807, 0.02616445637674759] km/s
+ time of flight: 8.557623323364975e7 seconds
+ arrival date: 2027-01-28T08:25:09.328
+ thrust profile: [0.523958472445852 -0.274470758925456 -0.23050096499518852; 0.147131036429763 -0.02026027857241947 -0.11618134084684553; 0.027302820838294467 0.0016577854534857476 -0.033584083370911656; 0.03684707305383091 0.005807966491571015 -0.05488688432376062; 0.01580107661771202 0.0030294234411495135 -0.027792539803673875; 0.0050586209139833116 0.0038983982338910814 -0.010818157967918492; 0.002241858639486769 0.0029652431796285757 0.0010666436475166392; -0.0026334092499951116 -0.007637913793529737 -0.0021725605341860665; 0.0011418626502773396 0.000721027489287296 0.0016684271895806811; -0.006496676915146599 -0.006045842478955765 -0.00047698080030569986; -0.004514485539048947 -0.0025564316290330874 -0.003043895999606456; 0.0041312644281804 0.002897476968276585 0.002796289928825206; 0.0047516265986086385 0.0014376614961581127 -0.0007951401635342408; -0.004893710560785023 0.007979921265922337 0.005801831083343418; 0.0066159984249610036 -0.008266320099786215 -0.00972618669646359; -0.007007723286631364 0.004171146691848841 0.006348939931536001; 0.023675995261051457 -0.005356188601581973 -0.009227734281839274; 0.01598743470439183 -0.015611165242632589 -0.006591022809361756; 0.023229807977144627 -0.01139980992714129 -0.0066116163931560935; -0.009532228239297648 0.004397040161845089 0.009001404896259389] %
+
+Mass Used: 38.96016605825889 kg
+Launch C3: 137.557333206262 km²/s²
+||V∞_in||: 0.03834313618454678 km/s
diff --git a/archive/ES_0.7213194367901296 b/archive/ES_0.7213194367901296
new file mode 100644
index 0000000..d289cc1
--- /dev/null
+++ b/archive/ES_0.7213194367901296
@@ -0,0 +1,22 @@
+archive/ES_0.7213194367901296---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-06T08:26:15.922
+Launch V∞: [8.286491932086015, -7.2243641975902, -2.1725300932011735] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.016035346495850113, 0.04972703802337492, 0.06238631896231554] km/s
+ V∞_out: [0.07512404472896914, 0.01078740900987863, -0.029278870933701438] km/s
+ time of flight: 8.597252255298255e7 seconds
+ arrival date: 2027-01-26T09:41:37.922
+ thrust profile: [1.0 -0.556491679860309 -0.4648961291351403; 0.7372059533489949 -0.036984111543562376 -0.4476629996563119; 0.39814675170265484 0.05709590986505949 -0.32466607797413205; 0.08899384393335248 0.02089138976996168 -0.08238645752970553; 0.08475764164064 0.026100670550362203 -0.0907524495767223; 0.014989709147499499 0.0037725551636252743 -0.009265553994657776; 0.019616296677172785 0.00779208532974952 -0.0211088531275061; 0.05078369101269816 0.01319155670330346 -0.048387739718579015; 0.0011933890878012684 0.0038764976024092627 -0.01799452333336548; 0.0007303231276612962 0.0076601705522692295 -0.011455359767182718; 0.0024761715680874513 0.008333948129389437 -0.005814734209795943; -0.004087566660721834 -0.0011502164375569398 0.0025057602454175605; 0.006481333640610147 0.00594295450153012 -0.01806105259426037; 0.004861317225204126 -0.0006045998114799084 -0.0018555465347688486; 0.00459880911278423 -0.011589512210531942 -0.012761722415645344; 0.038218505746487594 -0.008727958438010967 -0.01741336300122591; -0.015704736771304934 -0.013251167337766072 -0.037700157842325395; 0.0024639985007948017 0.0025691016175315873 -0.006030932804579864; -0.006048127616967321 -0.009300970340361094 0.008545849695558948; -0.0017022510168041328 0.0003091874327070254 -0.0008248993737888718] %
+
+Mass Used: 109.00524688790028 kg
+Launch C3: 125.57727360581443 km²/s²
+||V∞_in||: 0.08137544741190625 km/s
diff --git a/archive/ES_0.7214305592909108 b/archive/ES_0.7214305592909108
new file mode 100644
index 0000000..8b6c3cd
--- /dev/null
+++ b/archive/ES_0.7214305592909108
@@ -0,0 +1,22 @@
+archive/ES_0.7214305592909108---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-16T05:21:03.415
+Launch V∞: [7.910017912125655, -8.279729798669797, -2.482343744436139] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.4106101130616304, 0.30189064490072726, 0.043215443809636225] km/s
+ V∞_out: [-0.1900071650348521, 0.3306030111519312, -0.3486483362791376] km/s
+ time of flight: 8.641386455786349e7 seconds
+ arrival date: 2027-02-10T09:12:07.415
+ thrust profile: [0.8040660067025556 -0.48281519567921377 -0.3569867220085379; 0.038677414124214944 -0.008475664164809927 -0.03449363430573331; 0.02502579871564452 -0.002239433588064594 -0.031192851825220816; 0.007822052167358536 -0.0001238993866254427 -0.013410640795370138; 0.003641750852701789 0.0003143442440834061 -0.007340979935083961; 0.002679098904488013 0.0003470165986972592 -0.005958107316726782; 0.0024311598307366167 0.001417376460267933 -0.00555113734085049; -0.00018957667467469665 -0.0004605203636247336 -0.0042487442259679705; 0.0014597182218601147 -0.0020698530698382424 -0.003856046921699319; -0.0032890560178113802 0.002021913469718617 -0.00410020211662206; 0.0011631136730489919 0.001773907645148253 0.0030037641778832254; 0.0017975736261772344 -0.0019642120616437542 -0.0026771804126168516; -0.001781626983843162 -0.0011842805592879755 0.0026407323558570294; -0.0037640891572232526 -0.001014372420407289 -0.0003469795468283845; 0.0052535306194673665 -0.0008111624004931901 0.0011469970118755148; 0.0024516449173713995 0.001179246290620892 -0.002969394109457599; 0.0008396571886096493 -0.0004839796515793914 -0.00014230387098215; 0.003953504906089993 0.0001622529145283125 -0.0007083967912870953; 0.00012780673234274293 -0.0009660868972643107 -0.005389036224268524; 7.591330664534696e-7 -0.0006139739177201638 0.005144522946500468] %
+
+Mass Used: 40.8436728204847 kg
+Launch C3: 137.2843393746705 km²/s²
+||V∞_in||: 0.5114745360335408 km/s
diff --git a/archive/ES_0.7217185221826274 b/archive/ES_0.7217185221826274
new file mode 100644
index 0000000..188556e
--- /dev/null
+++ b/archive/ES_0.7217185221826274
@@ -0,0 +1,22 @@
+archive/ES_0.7217185221826274---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T17:04:37.077
+Launch V∞: [8.345346242874188, -7.519848609969729, -2.5136258404576908] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.1740521609394065, -0.44525516455076075, -0.660621105202349] km/s
+ V∞_out: [-0.7400633993357436, -0.11464260401340401, 0.3220779321862654] km/s
+ time of flight: 8.59116669601457e7 seconds
+ arrival date: 2027-01-29T01:25:43.077
+ thrust profile: [0.7816698724617391 -0.36300110915860506 -0.2964518231450083; 0.28614216834899475 -0.02480577158440201 -0.18936757526045625; 0.07531472229252027 0.00607876021389858 -0.07175314106340425; 0.0628213678066721 0.011084191835937233 -0.07174128627790058; 0.08230029346640327 0.01672937203476381 -0.10578781811639461; 0.050892591417045066 0.014691818259437439 -0.07345729761801863; -0.003249921414108038 0.003680059774529631 -0.01273526959172175; 0.0045990943445993575 0.0049522430697620835 -0.00808134455757978; 0.0015974862529376452 0.0006059187842077478 -0.001941908681614998; -0.002470393212151572 0.008843171210241484 -0.008539346417700672; 0.0076143082728354836 -0.00447700220994535 -0.0027909586385149064; 0.01942599847252153 -0.03209337298685755 -0.019941087876968484; 0.00397905324188275 -0.0029545790497036116 -0.005122667446074347; 0.011357236983102124 0.016344500925911866 0.027469301426784012; -0.008340879915939951 -0.03476062739578349 -0.01683279940907204; -0.006907022077164598 0.02822928324083098 0.004558432380521952; 0.06444417170740516 -0.02704405791261235 -0.014217985997752982; 0.002976752265301838 0.0016992881013452345 0.009826355613012788; -0.003176008359818395 -0.008368463378383713 0.005578671738484694; -0.020204147601380267 0.0377320261843766 -0.004935038008251156] %
+
+Mass Used: 69.0226981522801 kg
+Launch C3: 132.5112418961346 km²/s²
+||V∞_in||: 0.8154548184452496 km/s
diff --git a/archive/ES_0.7217336041709278 b/archive/ES_0.7217336041709278
new file mode 100644
index 0000000..348c357
--- /dev/null
+++ b/archive/ES_0.7217336041709278
@@ -0,0 +1,22 @@
+archive/ES_0.7217336041709278---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-03-25T00:16:13.797
+Launch V∞: [3.952523646522946, -7.805810933069656, 1.8494534942740026] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [6.744714254659307e-7, -7.405338588452131e-7, -9.885125736147624e-7] km/s
+ V∞_out: [5.549558658199959e-6, 3.4037443245899012e-6, 1.5664581536916626e-7] km/s
+ time of flight: 1.6674315792517945e8 seconds
+ arrival date: 2028-07-05T21:48:50.797
+ thrust profile: [0.9999894878382325 -0.5915806081659667 0.01640197522335157; 0.999999954704645 0.15679873253685997 -0.07242491709547816; 0.9932330646371123 0.44539738979889454 -0.11512354965041606; 0.7530011417957673 0.5199540801338834 -0.12587884391347462; 0.5162902515067485 0.46232825615121026 -0.11318170245606383; 0.3075156588063335 0.3321522725959464 -0.0844872050287583; 0.132853099175871 0.16761696260840928 -0.04430564941201763; 0.001436021979972195 0.000810188617529479 -0.0006619492509433314; 0.020082747417313876 0.03042638398189488 -0.008311609291644966; 0.0017515036501815312 -7.721965456603257e-5 -0.0005982433762700556; 0.0021783451214821706 0.0029857951972195942 -0.001703346228468809; -0.0010209769395145237 0.0017403172929644985 -0.003329172173211531; -0.0019840211048272162 -0.0005885681112554812 0.0019676224114589837; 0.00023499185360649938 0.0023480277760294394 -1.905635885679106e-5; 0.0007169906021181844 0.0017134043630250278 -0.0006194559581431938; 0.001225508884624983 0.004755041652268835 0.0026712437573176554; 0.003683515020482501 -0.0009027577543735169 -0.0020554127546105923; -0.0002710549279228127 0.00012026245535852258 -0.0011443610083376578; 0.0028821367839832242 0.006228342961757001 -0.0011830946392540776; 0.0010031890485618202 0.002628729854874286 -0.004428333820065452] %
+
+Mass Used: 375.5098381273774 kg
+Launch C3: 79.97360572663514 km²/s²
+||V∞_in||: 1.4072878909664175e-6 km/s
diff --git a/archive/ES_0.7220205036187417 b/archive/ES_0.7220205036187417
new file mode 100644
index 0000000..af19b9a
--- /dev/null
+++ b/archive/ES_0.7220205036187417
@@ -0,0 +1,22 @@
+archive/ES_0.7220205036187417---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-06T10:29:07.658
+Launch V∞: [6.056566958773899, -8.184338560606928, -0.8683390397101842] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.7433394806413862, 0.7742403764330484, -1.6445877120248897] km/s
+ V∞_out: [-1.1988809924039303, 1.805856190779908, 1.2696569176338697] km/s
+ time of flight: 1.0170360000727147e8 seconds
+ arrival date: 2026-06-26T13:29:07.658
+ thrust profile: [1.0 -0.9135972424088958 -0.31402174826921964; 1.0 -0.2111813865522835 -0.5357527610229444; 1.0 0.11082701330907203 -0.6091511934293549; 0.8633724568777029 0.20943129538100977 -0.550260901968512; 0.4529785783561372 0.15532209529062693 -0.3265405768723896; 0.2742318513199047 0.11468830613371402 -0.2188646682376554; 0.008420215518412478 0.004285178361821143 -0.007319847760062676; 0.009472431688318243 0.00496972563993111 -0.008965202030954333; 0.0009888312274811423 0.0005804917044969874 -0.0008297089214799806; 0.002530728339801747 0.0014496470179954678 -0.002415794454257164; 0.0034362834783110384 0.0017456951378767094 -0.0038524760839044633; 0.00035512444451632106 0.00010328937268886128 -0.0003891124153273276; 0.0001849685484794534 0.0004543809328014938 -0.000977740123399531; 0.00033206710827650865 0.0006849346840875926 0.00048098844375191023; 0.0009172193357316342 0.0003298233364996148 -0.000491712075488469; -6.298457496019033e-5 -0.00026602817942096216 -0.0005888532483162255; 0.0005239394983828079 0.000429673825811998 -0.00042336802461456215; -0.0005460181262088423 -0.00021624356704913212 -0.0002950091105455189; -0.00031355398700797345 -0.000228196636690871 0.0006239801529138989; 0.002088229212638117 -0.0003763796739312477 -0.0003975382316619675] %
+
+Mass Used: 233.24400770483362 kg
+Launch C3: 104.41941368863401 km²/s²
+||V∞_in||: 2.5186006924094633 km/s
diff --git a/archive/ES_0.7229658741792592 b/archive/ES_0.7229658741792592
new file mode 100644
index 0000000..aa0cf57
--- /dev/null
+++ b/archive/ES_0.7229658741792592
@@ -0,0 +1,22 @@
+archive/ES_0.7229658741792592---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T04:58:22.374
+Launch V∞: [6.817415198660851, -9.050186328316482, -2.5497544749861007] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.18036929735982798, 0.11780648735228626, 0.22343357031044783] km/s
+ V∞_out: [-0.10477967874491005, 0.20983230372792613, -0.20326861464195797] km/s
+ time of flight: 8.595403584418784e7 seconds
+ arrival date: 2026-01-15T01:05:37.374
+ thrust profile: [0.6207796013332625 -0.4734784760949419 -0.26927337520627753; 0.33737146286563063 -0.09938736619226989 -0.20567046054287422; 0.08948587978421023 -0.010671230929828673 -0.06913025888433494; 0.030013300962707976 -0.001857509240817201 -0.03196419318914327; 0.017950672317508125 -0.0009619234772463097 -0.02380270304894358; 0.01966881661959937 0.0018889008343605388 -0.02325517129843572; 0.015600729949247315 0.008539953681030912 -0.002083342384499748; 0.006291242987827764 0.0010940630043272783 -0.01075814033729755; 0.0059183178088441325 0.00808994689161095 -0.002310630472914118; 0.019008365203213987 -0.011618556832259624 -0.014582140831576761; 0.01674749658440002 0.010846975394147102 -0.008898089560404297; 0.011414027610637836 -0.0003646199357775527 -0.007854316765338851; -0.012655924680223352 0.00026741402492224124 -0.014266000675066233; 0.009040983156963465 0.0016557168087949978 -0.014336757306941506; 0.015646690846797505 0.0052492429093055 -0.002192748514076335; 0.006616617090472825 0.002407404862278792 -0.007319155955145786; -0.000847178801116644 0.011984121724496755 -0.006185400035078891; -0.0007684775392023651 0.0004947046541609419 -0.004046188363472475; -0.004451781328127392 0.007737648739197037 -0.009750453074899308; 0.006622812490502887 0.0015708059003953917 -0.00011777321590291344] %
+
+Mass Used: 56.63527557894304 kg
+Launch C3: 134.88427045089017 km²/s²
+||V∞_in||: 0.31037720959187104 km/s
diff --git a/archive/ES_0.723051144570667 b/archive/ES_0.723051144570667
new file mode 100644
index 0000000..1aa9c4d
--- /dev/null
+++ b/archive/ES_0.723051144570667
@@ -0,0 +1,22 @@
+archive/ES_0.723051144570667---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T08:42:47.895
+Launch V∞: [7.152828094911789, -7.414899147873033, -2.1172460958801302] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.20558537518394945, 0.16954560632397586, 0.0215637450111708] km/s
+ V∞_out: [-0.1728213558155897, 0.1379076599366388, -0.15022312518061437] km/s
+ time of flight: 1.0372837990344004e8 seconds
+ arrival date: 2027-08-20T22:09:06.895
+ thrust profile: [0.8080585976821513 -0.4042799480341829 -0.43096014816121514; 0.39968135767513896 -0.018848765328998988 -0.3845954780405658; 0.16980409815662623 0.02797903125923218 -0.2228063303348119; 0.09627125407858557 0.030565764269643733 -0.1484335484302719; 0.02587667605258764 0.014043026119807483 -0.042025050115259976; 0.009479549982496432 0.008227307790088376 -0.015701514199754945; 0.09857787906649734 -0.02161776899242402 0.007817732000153614; 0.0035159364957274408 0.028370353692004253 -0.018375527593470643; -0.03415599218499986 0.007607216055770306 0.03491561445024274; 0.010347892577004213 0.0061738258846286065 -0.05407161676994101; 0.08574390178549834 -0.030755545540481363 -0.09151190161138907; -0.04500495651875149 0.03359578439823552 -0.006318117103527853; -0.01791125816004757 0.0031958895128004813 0.061014976176691035; -0.044929329518973625 0.31553910639772426 -0.06080433498839516; -0.060332243619076624 -0.3147284480436024 -0.22535556017699798; -0.018679919381674123 -0.010880090452072848 -0.029100830483129985; -0.10059504397131147 -0.24913509315277363 -0.1558693490385519; -0.06435582494025434 -0.019836933350007815 -0.3433393425817294; -0.3679767021029245 -0.0439568776960443 0.3458042364930179; 0.10077026659881971 -0.05099597243598219 0.27988144072783144] %
+
+Mass Used: 198.23894273823544 kg
+Launch C3: 110.6264101590073 km²/s²
+||V∞_in||: 0.2673500593083844 km/s
diff --git a/archive/ES_0.7234984079714507 b/archive/ES_0.7234984079714507
new file mode 100644
index 0000000..6fbe4d7
--- /dev/null
+++ b/archive/ES_0.7234984079714507
@@ -0,0 +1,22 @@
+archive/ES_0.7234984079714507---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T03:40:01.290
+Launch V∞: [8.129356830889162, -7.522072040799554, -2.2569447934957707] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [4.2101534211699354e-5, -0.0005341710037536648, 7.027984463067727e-5] km/s
+ V∞_out: [0.00015171930524633253, 0.000349760215440228, 0.00038304340954476937] km/s
+ time of flight: 8.689197783595364e7 seconds
+ arrival date: 2027-02-08T20:19:38.290
+ thrust profile: [0.8832638505665177 -0.4295781191563863 -0.3338048564801807; 0.43727620013661556 -0.03557780074758101 -0.27361991043509476; 0.08534722145376983 0.007660346586766808 -0.07314882509214483; 0.1786381481176486 0.04025943945283047 -0.18239973393400968; 0.11671523239037009 0.029804698728197656 -0.13984120095779365; -0.024028755439167764 0.0062603731893155915 -0.026234439935676805; 0.03134953223684325 0.0016817269663999288 0.003014393556068189; -0.006540913564837612 -0.0019215518940269246 -0.004527589123550226; 0.0045128167678467335 0.03338835089881326 -0.02889062812792781; 0.03357933062163702 -0.005395480289438729 -0.005662203459080812; 0.024237862274955245 0.049325048157080845 -0.02900800529712064; 0.0015913029939599052 -0.010789828458987136 -0.029489575610949077; -0.01677228861065979 0.05880369483435452 -0.03453418870344884; 0.01849276788286199 -0.03669108084620195 -0.009368493487856906; 0.048884634451105885 0.007018445536528901 -0.06477808917875548; 0.07282625777051457 -0.03104110055736942 -0.08731570367629952; 0.08502261734781712 0.0011666451365295193 -0.03503830608156047; 0.023075201779291687 0.043279040378909575 -0.029795599079941632; 0.014385516712846635 -0.010665917442166564 0.01100638662478621; -0.003996095628764243 0.00819009881327577 0.012146190421326895] %
+
+Mass Used: 98.80425054791567 kg
+Launch C3: 127.76181007179031 km²/s²
+||V∞_in||: 0.0005404169288572378 km/s
diff --git a/archive/ES_0.7262870355006881 b/archive/ES_0.7262870355006881
new file mode 100644
index 0000000..2ca171c
--- /dev/null
+++ b/archive/ES_0.7262870355006881
@@ -0,0 +1,22 @@
+archive/ES_0.7262870355006881---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T10:15:29.626
+Launch V∞: [8.079797633632998, -7.632239916437493, -2.6552111319318126] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0008389287025807978, -0.009267824975283534, 0.0025334514082607515] km/s
+ V∞_out: [0.00319258647946067, 0.006373958755269792, 0.006503260095402368] km/s
+ time of flight: 8.922385784532982e7 seconds
+ arrival date: 2027-03-09T02:39:46.626
+ thrust profile: [0.611427480480305 -0.31077124308841714 -0.3109839259191444; 0.22489681375459986 -0.022754353530267675 -0.20223324829060718; 0.06680431990202808 0.009231966836721029 -0.08523922924135217; 0.04090887673218634 0.008451110633730661 -0.06398764487255773; 0.01623625704376949 -0.004450979966514514 -0.04901922064584795; 0.007364128334499892 -0.00046419444120808745 -0.020888490733408288; 0.013757567623964254 0.009412610550310375 -0.03161099269261573; -0.014211107488079558 0.014777562344222717 -0.01972882315269676; 0.006582050871722664 0.007475658425339039 -0.015206147414250063; -0.004087829996838835 0.028335572584508667 0.017882487391387; 0.028279492155592306 -0.0327685316856403 0.009843954744590442; 0.003102104536931812 -0.016652850723919102 0.006827861896322161; -0.14749307017067972 -0.04222101515691489 -0.011060817417426008; -0.0012291337584774886 -0.014389897802460742 0.04092803194785819; 0.08030685369331168 0.019366577937212245 0.1177026099323; 0.060345896107759395 -0.015718984000741943 0.022863124314907723; 0.02543731123048057 0.015278860645460888 -0.017437601266377542; -0.06438730621797789 0.10600385966102409 0.0287628126732982; -0.1562356404635762 0.04797183421973296 -0.007231107399371021; 0.052253537480789675 0.04056632766576476 -0.16970025097363575] %
+
+Mass Used: 85.59276251446545 kg
+Launch C3: 130.58436209765782 km²/s²
+||V∞_in||: 0.009644415854706883 km/s
diff --git a/archive/ES_0.7290074656059045 b/archive/ES_0.7290074656059045
new file mode 100644
index 0000000..b24c064
--- /dev/null
+++ b/archive/ES_0.7290074656059045
@@ -0,0 +1,22 @@
+archive/ES_0.7290074656059045---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-27T03:12:19.009
+Launch V∞: [8.279562153476801, -6.749228015343227, -2.0999360279881847] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.2762264600732687e-7, 1.7138249725056731e-6, -3.612442046057855e-5] km/s
+ V∞_out: [-1.3522936621672475e-6, 3.610796875002602e-5, -3.705016850033932e-7] km/s
+ time of flight: 9.139968729907428e7 seconds
+ arrival date: 2027-03-21T00:00:26.009
+ thrust profile: [1.0 -0.5753303639166572 -0.4498231853763222; 1.0 0.037863518223634055 -0.6450579187720803; 0.7314571469533068 0.1943521428776876 -0.5118329705511118; 0.41378977623601915 0.1705894913490041 -0.35898101379279806; 0.10300522894235381 0.0538033938569479 -0.10586104148805744; 0.06427989226126234 0.038359180221615816 -0.07386256068149047; 0.010878168707596088 0.00797630971972508 -0.014081245549867363; 0.005185097581346366 0.00015047409637881232 -0.003645899944708283; 0.002754754536311115 4.5831135903925783e-5 -0.0031832679972535055; -0.005766104178953708 0.0009805998312201157 -0.002922410083877368; -0.004892844297811089 -0.0034940521899910065 0.003103192523420559; -0.009323947629692105 -0.0033898647810544887 -0.006677921349901767; 0.014112231121937735 0.0007252895868020588 -0.004464979916574685; -0.002131243080615324 0.0003021174636728579 -0.00014579280468561637; -0.0001447578285185304 0.003568853233389526 -0.014056609287059795; -8.664798203153815e-5 0.0009896238522672412 -0.00026236522564656185; 0.015273488035635222 0.00964407244526353 0.014940215868120235; 0.02273005060842498 0.01900239693094135 0.003520075962942629; 0.02950926877567977 0.0033254606796539916 -0.005706709435462306; 0.021781906019182045 -0.004627892814737714 0.008482080773125792] %
+
+Mass Used: 159.18311233509303 kg
+Launch C3: 118.51295957802208 km²/s²
+||V∞_in||: 3.6165767815961355e-5 km/s
diff --git a/archive/ES_0.7301927661212666 b/archive/ES_0.7301927661212666
new file mode 100644
index 0000000..be3714c
--- /dev/null
+++ b/archive/ES_0.7301927661212666
@@ -0,0 +1,22 @@
+archive/ES_0.7301927661212666---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-23T00:40:45.527
+Launch V∞: [5.392007027792653, -8.123059097862892, -0.5670962448175367] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.9274625827901368e-5, -4.2533167575045836e-6, 5.506488054642648e-6] km/s
+ V∞_out: [-1.9189225825574354e-5, 6.404427620881228e-6, -3.261984565913945e-6] km/s
+ time of flight: 1.4411032778475815e8 seconds
+ arrival date: 2027-11-15T23:19:32.527
+ thrust profile: [0.5735068337502158 -0.31782336442225484 -0.22424916465406597; 0.13043781104545427 -0.010827631541648695 -0.08682834834868114; 0.11516706580675345 0.014510168024276954 -0.1177898790484759; 0.060904687406054536 -0.17098054795882275 -0.1939014441849342; 0.031568146567960476 -0.002488730696482533 -0.06122131862509472; -0.1420634479537978 0.11896744880405502 -0.1224330630892044; 0.004497466174096618 0.0030920867590894276 -0.013538712393546565; 0.04283562065512913 -0.016196839443357966 -0.03888336174940721; 0.1418967687959886 0.0756337260359479 -0.3009588254196408; 0.059276369519601024 0.045578240844086265 -0.2700097326784016; 0.001096708326168208 0.09733288089053917 -0.13009156167929892; 0.019442109379128263 0.03812701041384088 0.1584226141950706; -0.0004496869743570858 -0.029567562686791213 -0.008170819122229951; 0.07542011775723234 0.28875567818951103 0.00999183682357803; 0.009009118276613937 0.018099367391138682 -0.06938961728285666; -0.010698226812495413 -0.03376181282903638 -0.03675704972226447; 0.4809804111421316 -0.08086034825402003 -0.09367641319106298; 0.18632846319980417 0.03500053522989362 -0.11352264830753322; -0.25883248233771367 -0.5763234168208422 -0.2383316451793681; -0.23846738807928206 -0.6184135169439129 0.25354315816573314] %
+
+Mass Used: 295.51156937300084 kg
+Launch C3: 95.37942704602462 km²/s²
+||V∞_in||: 2.0492030522649383e-5 km/s
diff --git a/archive/ES_0.73021180634164 b/archive/ES_0.73021180634164
new file mode 100644
index 0000000..6d975d4
--- /dev/null
+++ b/archive/ES_0.73021180634164
@@ -0,0 +1,22 @@
+archive/ES_0.73021180634164---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T00:12:06.839
+Launch V∞: [5.832419869274506, -7.906668136814774, -1.3066944142302237] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.137304187428496e-10, -4.2484560862523107e-10, -5.197613769621772e-10] km/s
+ V∞_out: [1.3590478317027193e-9, -1.883833628032183e-9, 2.1353849796123364e-9] km/s
+ time of flight: 1.518461066508771e8 seconds
+ arrival date: 2028-02-10T11:40:32.839
+ thrust profile: [0.27601642394558074 -0.13741604047530068 -0.08858182493502696; 0.23709224237367918 0.016686387276852614 -0.16184102917878404; 0.19010613056205194 0.0593582859689693 -0.20331362128407732; 0.1382468870962633 0.06655269719402924 -0.19476262229840502; 0.0834704376273542 0.05097015294727653 -0.13963413901064733; 0.03221328603808846 0.021137961734985458 -0.07801667371174478; -0.006589792522661682 -0.007268589677775071 -0.026096998740469033; 0.05200581943416034 -0.014050752284031364 -0.022960160281449333; 0.0022584672381738315 0.02049900555266187 -0.07415960899838933; 0.055797784928634006 -0.2673087703230773 -0.08921015484407789; -0.1161410110550779 0.26473060625880906 -0.029769039373420472; -0.014693758358865848 -0.008517843901381859 -0.023879906363806474; -0.26904700720868274 0.08827490573448725 -0.36221630970123064; -0.03990811166829022 0.013853596951968694 0.015352225853830602; 0.20628319426928057 0.4295233976550647 0.006218196691432101; -0.04670412167292231 -0.18416048604480761 0.019394554536545837; -0.029634305906021563 -0.035996310327876216 0.08876801235634775; 0.08161062188656061 -0.2733811025858357 -0.24336944738284944; -0.26595888292017267 0.46002782990356894 0.12849163207305525; 0.07100712822149359 -0.2377746451730295 0.015669094416281955] %
+
+Mass Used: 278.8472657770185 kg
+Launch C3: 98.23997284941053 km²/s²
+||V∞_in||: 9.798248776126296e-10 km/s
diff --git a/archive/ES_0.7319652748631024 b/archive/ES_0.7319652748631024
new file mode 100644
index 0000000..919d0bb
--- /dev/null
+++ b/archive/ES_0.7319652748631024
@@ -0,0 +1,22 @@
+archive/ES_0.7319652748631024---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T07:08:03.510
+Launch V∞: [8.456356937031149, -7.593414061664385, -2.2879651521425868] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.01966261500948628, -0.06164654786074578, -0.08354377377706697] km/s
+ V∞_out: [-0.09686194090467629, -0.014546747729383296, 0.03961772965858665] km/s
+ time of flight: 8.361062401353738e7 seconds
+ arrival date: 2027-01-03T00:18:27.510
+ thrust profile: [0.7155762513399926 -0.3436629882351951 -0.28359712455016944; 0.3602050847493212 -0.029033614926686494 -0.23075640577614775; 0.3199878554045437 0.030212380123454907 -0.26794155521257584; 0.1296539527679169 0.02604704651486367 -0.14161379918183165; 0.06391296748741782 0.016494787254215507 -0.08190747831800642; 0.011896460361526655 0.0025563684615029754 -0.01479368199390714; 0.0011401429351442188 -0.0001777960468645329 0.0013085290171939105; 0.0014445551843405438 -0.0004153013180115909 -0.0033161717834041824; 0.004180076288394602 -0.0027986517138747164 -0.0024907721695810554; 0.0006683142299290412 -0.0002671354803717345 -0.004268152347736903; -0.00012460056435251643 0.002744913084665671 -0.013058506155827664; 0.005585793608962143 -0.0025072695099610555 -0.00021729337314187712; 0.0137317475958583 0.0037491464846211233 -0.007662210421548576; -0.00042659199795060544 5.337178073225139e-5 0.0019951382483636097; -0.010379980532358066 -0.0004933736410633453 0.0007922327882903475; -0.0017003997906564969 -0.0049896885744284344 -0.00473460849481461; -2.964379018970768e-5 -0.0013082785341739928 0.0014075615785437093; -0.0038703400991017475 -0.0003764713131289223 0.0021412312025081356; -0.0013844983609744765 -0.0021366521996677643 0.0006221075603507573; -0.00730391402499057 -0.002442763054129031 0.010138794902029] %
+
+Mass Used: 69.93210394825883 kg
+Launch C3: 134.4046942957761 km²/s²
+||V∞_in||: 0.10567155449349762 km/s
diff --git a/archive/ES_0.7322010742780904 b/archive/ES_0.7322010742780904
new file mode 100644
index 0000000..0473275
--- /dev/null
+++ b/archive/ES_0.7322010742780904
@@ -0,0 +1,22 @@
+archive/ES_0.7322010742780904---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T00:11:39.711
+Launch V∞: [8.379121589612877, -7.417082220654217, -2.1402297559222174] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.40422101682931616, -1.210422144372799, -1.554046186082543] km/s
+ V∞_out: [-1.9813523469780017, -0.29292437559814166, 0.844706371095993] km/s
+ time of flight: 8.373239999951418e7 seconds
+ arrival date: 2027-01-03T03:11:38.711
+ thrust profile: [1.0 -0.6152151572341708 -0.4782301319056794; 0.7671817871229858 -0.055272800284431725 -0.46135494017611595; 0.14446407780547021 0.0167634098033262 -0.13315805932975552; 0.05514981628489152 0.011717557165499463 -0.06498068212261374; 0.048382176477467675 0.02132935416131789 -0.06958299067282116; 0.03500625080190879 0.010367422433132604 -0.06105484327176681; 0.05092692116585679 0.017305906253325065 -0.06922816078010775; 0.03116230332487587 0.015484980416676555 -0.04714817000085655; 0.002826461980245474 0.0027135653840364947 -0.012410843530952315; -0.004768015387144864 0.007893373820529733 -0.004122500684639967; -0.006259018033896604 0.0013204264877142336 -0.0045600884254238475; -0.004675393388168015 0.02378942617130543 0.0029107298420126618; 0.0004256681420505824 0.005898249220397743 -0.006074701297359838; -0.004619711345284377 -0.003572611656235015 0.004223046649245586; 0.0014003893409515484 0.0024264245267100384 -0.005391697823992085; 0.00948744146301647 0.006946305832250306 -0.014000802299728526; 0.0018898831506962699 0.0014035463190556624 -0.005993553803882404; 0.029209151768110057 -0.0027540288295237834 -0.024002459055056193; 0.00080815466677704 -0.0026492036136833413 0.0006755862757768906; 0.007037708446627186 -0.012646074853302512 -0.005320569620343172] %
+
+Mass Used: 97.04825763512645 kg
+Launch C3: 129.80337068959642 km²/s²
+||V∞_in||: 2.010864477410715 km/s
diff --git a/archive/ES_0.7323257688429421 b/archive/ES_0.7323257688429421
new file mode 100644
index 0000000..93d19ea
--- /dev/null
+++ b/archive/ES_0.7323257688429421
@@ -0,0 +1,22 @@
+archive/ES_0.7323257688429421---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T04:41:27.322
+Launch V∞: [6.867194079982391, -9.049753586929013, -2.2905348542730297] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.4091589479041566e-5, -7.541885970229568e-6, -1.475666819031298e-5] km/s
+ V∞_out: [6.447460580152125e-6, -1.4144294061025952e-5, 1.525423910476185e-5] km/s
+ time of flight: 8.415179660162874e7 seconds
+ arrival date: 2025-12-25T04:11:23.322
+ thrust profile: [0.7542527279971083 -0.5767966986395189 -0.32232419155086695; 0.503022701841106 -0.14407516072564963 -0.3030828309318834; 0.1843840139412133 -0.01608894785308622 -0.15245268876192358; 0.05525143400863083 0.00126220091435517 -0.05848848221573256; 0.10089751554927773 0.009236296564045806 -0.11229712276384902; 0.007668636080165553 0.0008156261897800833 -0.010018230785734893; 0.0029969059141179036 0.00046599953063609386 -0.004379832395745105; 0.0017206408393812289 0.0002526620741037453 -0.0025921335876662606; 0.0012892986872097892 -4.913785942391386e-5 -0.0007819343248231074; 0.0010166982291387923 3.466033914280834e-5 -0.0011419107085930032; 0.0007219484789356752 9.600485474507163e-5 -0.0011722970188223296; 0.0009260563653217396 -0.0003280854060452493 -1.3003282578451236e-5; 0.0002533775003192272 -0.000579380295595808 -0.000303091849949263; -0.001588951903557673 0.0009391573634754019 -0.0016812251190105767; 0.00022720363136847534 0.00036764604301172245 0.0002028308345823199; -0.0009797634930982708 -0.0003801642857988052 0.0018475373924296632; 0.0007246710860894058 -0.00010958552253301392 -0.0004042318586837628; -0.0002565085948584892 -0.00036805476297271044 -0.00040276483420213674; 0.0017622802301641327 -3.980195968611929e-6 -0.00027206322478916977; 0.00198335284998301 0.000364255555663641 0.0019629441163554716] %
+
+Mass Used: 70.9462211130699 kg
+Launch C3: 134.3029444349193 km²/s²
+||V∞_in||: 2.175344097178135e-5 km/s
diff --git a/archive/ES_0.7334340466001801 b/archive/ES_0.7334340466001801
new file mode 100644
index 0000000..03fd452
--- /dev/null
+++ b/archive/ES_0.7334340466001801
@@ -0,0 +1,22 @@
+archive/ES_0.7334340466001801---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T14:52:39.865
+Launch V∞: [8.460175966649537, -7.5226581003756054, -2.3883597301251482] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-9.227366908283383e-10, -1.1504775826795068e-9, -7.273564185791066e-10] km/s
+ V∞_out: [2.4810725753087707e-10, 5.747762952615526e-10, 1.3272137459064329e-11] km/s
+ time of flight: 8.283087237509099e7 seconds
+ arrival date: 2026-12-25T07:27:11.865
+ thrust profile: [1.0 -0.6236249757787141 -0.4841413476436852; 0.6407801863033763 -0.06493945581127541 -0.37776993714453566; 0.04638061854766369 0.0026636334572519293 -0.03893274355816419; 0.018139357887317225 0.0034007206315872875 -0.017710066272766778; 0.002444809109196952 0.003516197637156954 -0.01316930989329212; 0.016130726519662176 0.00428871626862648 -0.02080246194012622; 0.01046489838657881 0.022869278213414522 -0.010553016653543143; 0.014657305731209009 -0.00579294834007521 -0.009509514950742676; 0.0016462229285703883 0.001990904718534965 -0.005033548572119264; -6.982949441396597e-5 -0.0018640316818341936 0.0015358310201227551; 0.0001574026339026063 0.0001464085740742134 -0.0015582977752820327; 0.008141332236487464 0.0034167566905075244 -0.009380625247163986; 0.008798539246396318 0.0019752040456475547 -0.0127770623137234; 0.00570100335507545 -0.0006653701261741668 -0.012271946416338537; 8.545983556494988e-5 0.0010516288910390186 0.0029960712991367123; -0.00022761692071189684 0.0008835125300523388 0.0005076105176381318; 0.003017202813369103 0.0004306748928965406 -0.00019372247788491948; 0.004029121410350126 -0.0011617676428930382 -0.001552877279246443; 0.003241027484331707 0.0009312413592910025 -0.0028338593161569203; -0.005911696511969266 -0.00015506407231952627 -6.833924914518522e-5] %
+
+Mass Used: 74.7692448867665 kg
+Launch C3: 133.86922448230462 km²/s²
+||V∞_in||: 1.6444114535289332e-9 km/s
diff --git a/archive/ES_0.7335203919884936 b/archive/ES_0.7335203919884936
new file mode 100644
index 0000000..6ad42d5
--- /dev/null
+++ b/archive/ES_0.7335203919884936
@@ -0,0 +1,22 @@
+archive/ES_0.7335203919884936---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T02:59:38.419
+Launch V∞: [6.957399616739743, -9.05204981928914, -2.444162507362703] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.18937874911061825, 0.11834102705354467, 0.24068986291764996] km/s
+ V∞_out: [-0.10867447131942606, 0.21776894127214555, -0.2204114479359076] km/s
+ time of flight: 8.423953477161391e7 seconds
+ arrival date: 2025-12-26T02:51:52.419
+ thrust profile: [0.6977020724746023 -0.5223996717311955 -0.28419263900100133; 0.33608442403168165 -0.09165791919493396 -0.19621179799421046; 0.16481848262564597 -0.013323604392430712 -0.12434655318872058; 0.13818469084866344 0.0026291904540107817 -0.12270607540004311; 0.007961598358334612 0.00015790950307735703 -0.009375696923560505; 0.003791594780134882 0.0009014213270113331 -0.0025771107123636026; 0.005472986706659055 0.0015067014017098486 -0.004859848885999997; 0.007358466722865117 0.0022788806879593805 -0.009961691495150304; 0.00214742737248279 0.0017751661734959094 -0.004349562071981166; 0.0008517183883728022 -0.001478723349639445 -0.0016712353140815954; 0.0005336629261051716 -0.0008942909119633907 -0.003274352284910991; -0.00038898039819423684 -0.00043439800564752315 -0.0020585131743354633; 0.0029388127699688927 -0.0011835893450094323 -0.008831529552499197; 0.0036597800013386697 0.0030087494608896067 -0.005342370187926999; -0.0008317088468701313 0.0009141182845958783 0.0002330442694052884; -0.003728537850452665 0.006143077449080716 -0.0017909773739046004; 0.0016920340000515892 -0.0016623161549029993 -0.0014196174290942998; -0.005951447710425122 0.0007277674807035406 0.002167057603164045; 0.0014061570917419173 -0.003001575221259691 -0.0034720588578483337; -0.0008681038403771419 0.00716427143461436 0.004355263514558602] %
+
+Mass Used: 60.5799406181568 kg
+Launch C3: 136.3189457203004 km²/s²
+||V∞_in||: 0.32832989417673714 km/s
diff --git a/archive/ES_0.7349996121285542 b/archive/ES_0.7349996121285542
new file mode 100644
index 0000000..97ea899
--- /dev/null
+++ b/archive/ES_0.7349996121285542
@@ -0,0 +1,22 @@
+archive/ES_0.7349996121285542---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-19T10:23:40.704
+Launch V∞: [7.573512657504108, -8.758307369561573, -2.3456284696769862] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.2574836427309357, 0.313980113249055, -0.32956159981577465] km/s
+ V∞_out: [-0.27257719998696406, 0.3212245690343578, -0.3098702796073137] km/s
+ time of flight: 8.816766922130966e7 seconds
+ arrival date: 2027-03-05T21:24:49.704
+ thrust profile: [0.7194286200541069 -0.49999834298663515 -0.34727428593398774; 0.09539129810719986 -0.036124383776142875 -0.07686792061418653; 0.008230832081372659 -0.00030846269893888443 -0.00940404442204876; 0.005842600179306833 0.0003091630776524308 -0.011683980021538075; -0.00037176113552970765 -0.005545141696430447 -0.00407716857942988; 0.004187095131410542 -0.0009391359722109409 -0.0064047853074336684; 0.0025165810992096396 -0.0007344369224909498 -0.004762847352763592; 0.0010867597726822431 -0.006967314163017824 0.0007644879565007526; -0.0017365155745078784 0.004626916579858648 -0.0008966454122174231; 0.0007941056113826487 -0.0023200782859645205 -0.005212595884095978; -0.002556226213877624 -0.003862071136394849 0.003279412946932726; -0.0027557092173007224 -0.0027103012919507926 0.004713825763864724; -0.011784536707841794 0.006898127288910389 -0.005856415683711254; -6.095026519878973e-5 -0.003071388864120022 -0.0044400629218429395; 0.0046626850818330115 -0.00028015847464670255 -0.02388624184859618; -0.0021688299009619376 0.001036612073456102 -0.006913129130742476; 0.005204400949192964 0.001087388182898894 0.006272355028416183; 0.013279778972659124 -0.010802471072250403 0.004437486884634856; -0.004392085664331786 0.005110116600174977 -0.007450552383427354; 0.0008443506332158487 -4.7114589850012756e-5 -0.0013372498147138229] %
+
+Mass Used: 43.35279407001781 kg
+Launch C3: 139.56801487085067 km²/s²
+||V∞_in||: 0.5229648036560532 km/s
diff --git a/archive/ES_0.7364364374985957 b/archive/ES_0.7364364374985957
new file mode 100644
index 0000000..73202eb
--- /dev/null
+++ b/archive/ES_0.7364364374985957
@@ -0,0 +1,22 @@
+archive/ES_0.7364364374985957---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T23:48:48.657
+Launch V∞: [6.7726522005460374, -8.988601770738644, -2.21043825578808] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.19409166885554333, 0.12140850620975754, 0.2504227643388954] km/s
+ V∞_out: [-0.11092449450918074, 0.22703795150549919, -0.22643379811582373] km/s
+ time of flight: 8.354900481439586e7 seconds
+ arrival date: 2025-12-17T23:52:12.657
+ thrust profile: [1.0 -0.8117908529528925 -0.42034177139535983; 0.659146394716627 -0.18160452468261054 -0.32995474814231396; 0.25765791354908646 -0.019707251664744692 -0.17196993779118777; 0.11027025753035052 0.003728135513833561 -0.09617310208775848; 0.05398498108944144 0.0060616300843757505 -0.05705542547420293; 0.01568133179763358 0.0023453553840195305 -0.019731282107063937; 0.006116332451982686 0.0006858869955988613 -0.007464076183989781; 0.0009620489138459989 0.0001348258243533294 -0.001134406744429541; 0.0035581137787997113 -0.0007295861114781379 -0.003464470069713153; 0.00011090188492033303 -0.0007223280581343465 -0.00557156547267729; 0.0025391179730919217 0.0001224956405171991 -0.0023340806367502273; -0.00016949187217978165 0.004664886438721015 -0.004009005587848378; 0.0009746822961564068 0.0004142956486385327 0.0044466855270185145; 0.0035071508983849182 -0.0005026544897209264 0.0026071848367262337; 0.005816838622045773 0.005041201263955349 0.0027520799041103852; 0.0023622341078888987 0.00260907874420702 -0.004110107380167175; 0.010119304318811763 0.005112803873896745 -0.004837915381673145; -0.0011461357688548014 -0.0006398430664060388 -0.004157526216215712; -0.0012035355557682874 0.0020188930980005685 -0.002652782475201245; 1.9838813249222246e-5 0.009692813685504266 0.003585749250853132] %
+
+Mass Used: 91.80191180172096 kg
+Launch C3: 131.5498169051384 km²/s²
+||V∞_in||: 0.33929804331641605 km/s
diff --git a/archive/ES_0.7379692607110546 b/archive/ES_0.7379692607110546
new file mode 100644
index 0000000..615ce7b
--- /dev/null
+++ b/archive/ES_0.7379692607110546
@@ -0,0 +1,22 @@
+archive/ES_0.7379692607110546---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T05:34:24.463
+Launch V∞: [8.399596030805299, -7.552781394079261, -2.1524244371831927] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.3726676383905887, -1.7175136056792375, -2.698629583733477] km/s
+ V∞_out: [0.7075540105239045, 0.31482491720135225, 1.86158778075177] km/s
+ time of flight: 8.255520006996433e7 seconds
+ arrival date: 2026-12-21T17:34:24.463
+ thrust profile: [1.0 -0.49506870032830597 -0.39530029833331726; 0.6635699137342901 -0.06107905068908643 -0.4029955872838214; 0.28409286750263235 0.02402523757768811 -0.2440678039069501; 0.1570043128580855 0.028769722788836712 -0.16645446074193357; 0.041454473764130986 0.009998394637918764 -0.05137117491579234; 0.0017303503321880053 0.0005397554453969389 -0.0018592369822706001; 0.0011118253540347725 -0.0023551896190031163 -0.0005424111701248813; 0.0018684291739891306 0.000659818442885532 -0.0023571944433493737; 0.0023201354946431893 0.0007634437246170922 -0.003946067234590115; 0.002499578039837281 0.0032634245931594972 4.294996168854534e-5; -0.0009928410169608452 0.0006156173754291222 -0.0004361409948390746; 0.0007451183729088275 -0.002759426784884538 -0.003539896256546113; 2.9083276952308098e-5 -0.0027957408017111694 0.00046953926447598163; -0.003423523794844477 -0.00011796557738487438 0.00237782957981684; -0.010762193467100133 0.005080211131835865 -0.004630833512415982; 0.0003889885736242329 0.0005962357390914305 -0.001990192272527033; 0.004989750556592767 -0.005541487503605025 0.009692905990788075; 0.012878824614166087 0.014399979761105455 -0.0029345882750762293; 0.0006892999106472362 0.0006740986717568515 -0.0019689615008520217; 0.004071563556144581 -0.0076385045458076724 -0.008686605957541487] %
+
+Mass Used: 89.61867201558562 kg
+Launch C3: 132.23065122525338 km²/s²
+||V∞_in||: 3.2204558349088463 km/s
diff --git a/archive/ES_0.7380962292906041 b/archive/ES_0.7380962292906041
new file mode 100644
index 0000000..7d1d44b
--- /dev/null
+++ b/archive/ES_0.7380962292906041
@@ -0,0 +1,22 @@
+archive/ES_0.7380962292906041---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-11T11:03:37.224
+Launch V∞: [6.444388290473087, -8.28399241364588, -1.2708685129073338] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0005889408443694386, -0.003514345500206482, 0.004619665664048592] km/s
+ V∞_out: [-0.004108720203867912, -0.0032869395029889634, -0.0025141083198522303] km/s
+ time of flight: 9.286523276214539e7 seconds
+ arrival date: 2026-03-21T06:57:29.224
+ thrust profile: [1.0 -1.0 -0.4308667744619553; 1.0 -0.25781137289803463 -0.5501160558131616; 1.0 0.05973867706780822 -0.6220701056841503; 0.9237528532045053 0.1686386663434996 -0.5611006280829022; 0.37899171967750467 0.10274262668291642 -0.26964766332163115; 0.045225491605166736 0.015085116074582941 -0.03605813792421971; 0.109606890465507 0.03991395361649555 -0.09393253310619944; 0.01027457465372993 0.004470332725699268 -0.009477276836510534; 0.004351512930342927 0.0029101771786360455 -0.004642323119996465; 0.000825186928023346 -0.0003363362620108541 0.0008985265133867563; 0.0030538208060255203 0.0014795444235905534 -0.0008452585199802143; -0.0004165054198378758 -0.0002194327498331644 -0.0004612915335129074; 0.0017535649356211058 -0.00015459274083005567 -0.0018931582354498409; -0.0005741004155312775 0.00027431279806853836 0.000829403625293632; -0.0009125513672218975 -0.0005826422246184143 -0.0013786691332893575; 0.002744247240009215 -5.405954564168767e-5 -0.0015718295796045007; -0.0019505059041037324 -0.0017323272280166575 -0.0007919056133668343; -0.001309437890913527 -0.0005487917735965411 0.0013178451457525964; -0.003173248890503121 -0.001294035571164786 0.0006659402523134911; 0.003117437280048802 0.001122360116835652 -0.002314384151285877] %
+
+Mass Used: 209.12189861087245 kg
+Launch C3: 111.76977752482843 km²/s²
+||V∞_in||: 0.005834276858409931 km/s
diff --git a/archive/ES_0.7413710451016542 b/archive/ES_0.7413710451016542
new file mode 100644
index 0000000..88f63c9
--- /dev/null
+++ b/archive/ES_0.7413710451016542
@@ -0,0 +1,22 @@
+archive/ES_0.7413710451016542---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-03-25T02:24:08.408
+Launch V∞: [2.8250801995900736, -7.72614765891951, -1.2396778228647647] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.00032323914169533717, -0.00031170654793965315, -0.0003219451207298184] km/s
+ V∞_out: [3.276817014382785e-10, -7.407562497212769e-10, -1.0089224745183263e-9] km/s
+ time of flight: 1.856000570424138e8 seconds
+ arrival date: 2029-02-09T05:58:25.408
+ thrust profile: [0.9950870121870576 -0.6068077521680951 -0.0832947401795521; 1.0 0.18416644553619416 -0.17619653794529608; 0.9497326140201902 0.5206670620865991 -0.24087774311701302; 0.7871877390869156 0.6448634340491758 -0.26544919044132503; 0.576181338639441 0.6137152090400753 -0.24689238850575046; 0.3559018186919085 0.46825383272696336 -0.19115300165810986; 0.158951641444275 0.24961964311122098 -0.10725271780558239; 0.0012112785459748592 0.002005321559802014 -0.0010099293368052882; -0.000772204549000988 -0.0006188546728247609 0.0019353651085029224; 0.0017769277342279091 -0.0012320314708326114 0.0026919279234005923; -0.0016200729429806586 -0.0033528120462848286 -0.004212016110955738; -0.0009455040037122308 -0.0029542833555202064 -0.0029992721585882483; 0.0011226308624016374 0.0039239080213418105 -0.0016160511593177175; -0.008552158148959597 -0.0010915609333037857 0.003082657388684343; 0.0008914250767092446 0.0017704603847865396 0.0056560487727482355; -0.005119401368143868 0.0030764166518605475 0.0038130511663676714; -0.0008712671354003483 -0.00010968803136538789 0.0021969046642873226; -0.0029174438067765523 -0.0019118522807345523 -0.002004353978761131; -0.007453885803014147 0.000655083076489434 -0.002287384609151606; 0.006231076846013389 0.0035546009055907584 0.0061342911159388] %
+
+Mass Used: 461.20067078332795 kg
+Launch C3: 69.21123688604604 km²/s²
+||V∞_in||: 0.000552533415744361 km/s
diff --git a/archive/ES_0.7418853701113484 b/archive/ES_0.7418853701113484
new file mode 100644
index 0000000..85fff5b
--- /dev/null
+++ b/archive/ES_0.7418853701113484
@@ -0,0 +1,22 @@
+archive/ES_0.7418853701113484---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T10:57:11.760
+Launch V∞: [7.749080355987572, -7.582555987537102, -2.0997716385538134] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.40845216921760386, -0.45319707278607474, -0.2735209369169806] km/s
+ V∞_out: [-0.5292169353165694, 0.26362428079507993, 0.3124623259449272] km/s
+ time of flight: 9.077211022490942e7 seconds
+ arrival date: 2027-03-26T01:25:41.760
+ thrust profile: [0.8801443353027678 -0.46207514063521377 -0.4415549767319297; 0.5050775173188683 -0.05459517270543862 -0.43151621265098117; 0.1973438315981591 0.01142789958004575 -0.2523707396426442; 0.05683585598873839 0.008488283993776175 -0.10266142268982151; 0.07322587846369191 0.01487182574912702 -0.14857285815517715; 0.03785964665910539 0.009175378164581303 -0.10060802385228361; -0.0017965992681608471 -0.0031983427567180128 -0.006323762047014684; 0.01369895530108837 0.004610468235402594 -0.03954719607841266; 0.00853530460062273 -0.04648268823900778 -0.008820964461163162; -0.01693305552535214 -0.014613214171545558 0.006949750965035376; -0.006596197513339393 0.013134069678665539 -0.048125985166291255; 0.0867190891593203 0.01940778497658708 -0.08643576357571554; 0.023178256155347843 0.0900123811934436 0.07759149666835541; 0.018713521573719465 0.042416778526680264 -0.02251116034091013; -0.03822545878589856 0.07071232716464317 0.2084945629019243; -0.10660004577671259 -0.22422139099147803 0.06693102634100591; -0.19321570888633147 0.07574750919113934 0.039625151765587764; -0.00995398032806308 -0.00190057326041313 -0.012132062622873816; -0.07037929728430123 0.1130832033708292 0.29839196272966517; -0.03130939254541629 -0.07414893382856663 0.28452090662401985] %
+
+Mass Used: 154.1436832862937 kg
+Launch C3: 121.9524426017622 km²/s²
+||V∞_in||: 0.6686063597157715 km/s
diff --git a/archive/ES_0.7422467501081177 b/archive/ES_0.7422467501081177
new file mode 100644
index 0000000..ce8e298
--- /dev/null
+++ b/archive/ES_0.7422467501081177
@@ -0,0 +1,22 @@
+archive/ES_0.7422467501081177---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T14:39:45.343
+Launch V∞: [6.880133668083208, -9.1121161442136, -2.1337323465910454] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.327257747495261, 0.1984348211070967, 0.4394185510302244] km/s
+ V∞_out: [-0.19892748225727075, 0.39765880850202334, -0.40086859016783316] km/s
+ time of flight: 8.320319401413469e7 seconds
+ arrival date: 2025-12-14T14:39:39.343
+ thrust profile: [0.7309266618045049 -0.5292353806116318 -0.32328499736891053; 0.5065921564739687 -0.13858975314325983 -0.31859356640168707; 0.33490518078176856 -0.03056488805558158 -0.27407765743250456; 0.13795746457343894 -0.0009627485524672072 -0.1381804272301421; 0.026330435600531173 0.0003862779925764445 -0.028910024428327075; 0.006035289240751728 0.0018054682176222353 -0.003756702241450103; 0.0030310265078835313 -0.001873389257638581 -0.0013349530533815232; 0.002515485367383382 -0.0003357753561992788 -0.0036034951645229863; -0.0003598280297275008 0.000539577566393324 -0.0007680169416241283; 0.0029566137090908887 -0.00895801661152739 -0.0013598601065344725; 0.00817195849412394 -0.003701730983431003 -0.007852372129753404; 0.009994101287037413 -0.012568679234120046 -0.003362665664655192; 0.013660337498225185 0.0035589340453692753 -0.011155208212861614; 0.010269112961708207 -0.0012396746608655635 -0.009155441044387926; 0.010928263444123582 0.008448240089263526 0.0027379856850190797; 0.008333494939272058 -0.005459673939052894 -0.008775975693746914; 0.014081282743688531 0.0021106786992448816 -0.0009947105566386547; -0.0021370981462601087 0.00030071680261716254 -0.0006980068319453452; 4.6194487056573294e-5 0.006115536209295188 0.005660352111429122; 0.000527203503067233 -0.002330767760583458 -0.0011620802412991862] %
+
+Mass Used: 78.92287887402563 kg
+Launch C3: 134.91971364321915 km²/s²
+||V∞_in||: 0.5827200653083601 km/s
diff --git a/archive/ES_0.742420971682566 b/archive/ES_0.742420971682566
new file mode 100644
index 0000000..eba8041
--- /dev/null
+++ b/archive/ES_0.742420971682566
@@ -0,0 +1,22 @@
+archive/ES_0.742420971682566---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T08:41:03.911
+Launch V∞: [8.666508093419631, -7.752560541240587, -2.5181080381666465] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.5489775132930546, -0.6000285410357711, -0.3726262593669531] km/s
+ V∞_out: [-0.6749130008749925, 0.4401829572113926, 0.38842385643859767] km/s
+ time of flight: 8.213397731093939e7 seconds
+ arrival date: 2026-12-18T23:40:40.911
+ thrust profile: [0.5684716752306977 -0.2799720246176664 -0.24063550081989415; 0.25086093878162136 -0.03292270747702272 -0.17631265998574877; 0.06812024984967667 0.002618251695942853 -0.06856275799202281; 0.010747343228028887 0.0010956395567381758 -0.011924388550802398; 0.014412241101343213 0.0024480069513583055 -0.018792429096086163; 0.010145415509512213 0.0017746791460993825 -0.014252941568823209; 0.010266134574324999 0.0021921439285161725 -0.01594868839827882; 0.0011295922821453978 0.0005443056941960969 -0.002326613632452261; 0.0030974304078604372 0.0003916770935481851 -0.0017911788797486177; 0.004067646870045714 -8.155916099219845e-6 -0.001241592330492502; -0.00013411630179680975 -0.0007261834189533779 0.002637874931466621; -0.0016327733283090133 0.0006613696550457417 -0.002549783092677036; -0.0015358664496892926 0.005556785861111315 -0.001385171859689284; 0.000854833182940357 -0.0033164437572710094 -0.009515646306622143; -0.0016608470182483603 0.002925981767201205 -0.01164499341001164; -0.0019780493235982436 0.006582419528037592 -0.00816641057131332; 0.002596264536512693 0.0007337836097047076 -0.010463105100055891; -0.00026331259347221313 0.00010996398866870488 -0.0009470555416283954; -0.0011319000369617808 -0.0031836890443965905 -0.002791203318490502; 0.0049765714921451674 0.002672950352234288 0.0009027323141334186] %
+
+Mass Used: 40.44115113339694 kg
+Launch C3: 141.551425570788 km²/s²
+||V∞_in||: 0.8945730206801173 km/s
diff --git a/archive/ES_0.7445752848175967 b/archive/ES_0.7445752848175967
new file mode 100644
index 0000000..11dd91a
--- /dev/null
+++ b/archive/ES_0.7445752848175967
@@ -0,0 +1,22 @@
+archive/ES_0.7445752848175967---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-25T12:58:05.042
+Launch V∞: [7.349230851010424, -9.073122752782933, -2.7247516382045367] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.01627815439089098, 0.0960698989581768, -0.10029530209517624] km/s
+ V∞_out: [0.09529031660289092, 0.08443575683679136, 0.05782371163189639] km/s
+ time of flight: 8.358852471034905e7 seconds
+ arrival date: 2025-12-18T00:00:09.042
+ thrust profile: [0.2641848875444481 -0.20070489898756425 -0.09784425268974993; 0.197911973935459 -0.052691299619987565 -0.09278263233965559; 0.13226045842864786 -0.007884939473958592 -0.07938746012120451; 0.07769648032168099 0.0037348166938150616 -0.059054036569024373; 0.03752665543531245 0.0041579301232816945 -0.03472820989843579; 0.011012991804463306 0.0015213005107382977 -0.011535590799021812; 0.001307131800361793 0.00020481968286322332 -0.001535145230498401; 0.000750279671142511 8.304528101337663e-5 -0.0008497428539980856; 0.0007588739495077094 -0.0002618350041554945 -0.0009782921957597296; 0.0006746463322574797 0.0004778834586427436 -0.0006615427323143295; 0.0005957514088918199 3.2064477810664674e-5 -0.0006411139228747888; 0.0007161060632954867 0.00011233343460686281 -0.0006399413327732891; 0.0006489049502006979 0.00020983763573463116 -0.0002111716741640095; 0.0002969664154361147 -6.712198873714962e-5 -0.0005546843965028549; 0.00029286145315720756 1.9267904928838844e-5 -0.0006473781330993099; -0.00039472575528514694 0.0001154659527874489 -0.0010959935626489055; -6.780322216921829e-5 0.00028203074383132304 -0.0005946166321515191; 0.000721031844481154 -0.00046531427776177916 -0.00113421129123107; -0.00043913092121699356 8.167394744720954e-5 -0.0006852439095800284; 0.00015318798569224587 -5.3728308836256276e-5 -0.000300414663519779] %
+
+Mass Used: 30.088536829809982 kg
+Launch C3: 143.75702207840905 km²/s²
+||V∞_in||: 0.1398340138112707 km/s
diff --git a/archive/ES_0.7458928314099984 b/archive/ES_0.7458928314099984
new file mode 100644
index 0000000..0e585f6
--- /dev/null
+++ b/archive/ES_0.7458928314099984
@@ -0,0 +1,22 @@
+archive/ES_0.7458928314099984---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-26T15:18:48.305
+Launch V∞: [7.028285668573242, -9.069265653972769, -2.3843442432542403] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.1740161783141668, 0.2303049810706103, 0.2336844411536923] km/s
+ V∞_out: [-0.1282429758485073, 0.244106849070512, -0.24878783946012512] km/s
+ time of flight: 8.245215302741091e7 seconds
+ arrival date: 2025-12-05T22:41:21.305
+ thrust profile: [0.8892159108846924 -0.6534918465440699 -0.3538849984762806; 0.47431769366930837 -0.12632120042328476 -0.25255279166801425; 0.17467272802935402 -0.014096850956281928 -0.12540335771221772; 0.057895148229359726 0.0007597157610091615 -0.050165130193299434; 0.01150488299972942 0.0019119970118860665 -0.013263063675312063; 0.001655326092526676 0.0007209818881890521 -0.0074801921321510905; 0.0003592607484772339 -0.0007596067838862958 -0.0001537595991294217; 0.003394940393151559 0.0007238278646008665 -0.003938860877567901; -0.002811357579329486 -3.641828637209859e-5 0.0010075379624259547; 0.0031589644795813232 -0.005474356450277513 -0.0025964776200394077; -0.0004589034363869432 0.0015528449000776511 0.004659248296159715; -0.003787556560302771 -0.00018387855206099957 0.0008096331132585372; -0.005216683836339276 0.004167287591545547 -0.0012878523882117804; -0.004712699809346979 -0.00022819237840889938 0.005601345066174392; 0.0021604699273518927 -0.0003779149998917494 0.001008207852433353; 0.0013807132866105207 0.0004311952287863179 -0.001515908722635122; 0.0009170233217350469 0.007534121786848744 -0.011292774300281134; -0.0009216144925215498 0.000277176025719148 -0.002700908641934397; 0.0052771372972971135 -0.0070097243056429824 -0.007761122424903852; -0.0014346424420410306 0.0034720352922734997 0.0027714126574446543] %
+
+Mass Used: 69.09635757650449 kg
+Launch C3: 137.33347641174177 km²/s²
+||V∞_in||: 0.37138986612226715 km/s
diff --git a/archive/ES_0.7492221640701897 b/archive/ES_0.7492221640701897
new file mode 100644
index 0000000..e2c8377
--- /dev/null
+++ b/archive/ES_0.7492221640701897
@@ -0,0 +1,22 @@
+archive/ES_0.7492221640701897---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T12:58:58.966
+Launch V∞: [8.816976744731265, -7.559800431075809, -2.420980178965594] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.33754731840119667, 0.4029669291127192, -0.35275515279066977] km/s
+ V∞_out: [-0.3147117481434026, 0.39602336291441953, -0.3806119545874305] km/s
+ time of flight: 8.129064326776205e7 seconds
+ arrival date: 2026-12-07T09:43:01.966
+ thrust profile: [0.6086703998453905 -0.2696040478607296 -0.23568217602937697; 0.34168712616290275 -0.023895426397885645 -0.2164178585105811; 0.20512670005125666 0.02036995148603093 -0.17856991678666762; 0.10251397907780288 0.019790734971484807 -0.11211981224641454; 0.03563048021843438 0.008471538474259905 -0.043826199867909414; 0.008617248757589475 0.002254134336866001 -0.01109848240446732; 0.0027467787773412114 0.0012987658113450718 -0.0014173607950761188; 0.002001271136876957 0.0005208184394520586 -0.003808089695576942; 0.0013462102946299255 0.001081061974296182 -0.0007439006894363529; 0.0019254309630922922 0.0008366679567443705 -0.0034916030237093277; 0.0009888968458120545 0.0002714849285583745 -0.0014586373235281494; 0.0004972220647416483 -0.00017966072489296152 -0.0019781738536393642; 0.0010673466050993806 7.040582594790008e-5 -0.0014159841095282596; 0.0020076934619439736 -0.0005463735569320122 -0.0014321387903659703; 0.000575680723551015 0.0004806314636603827 -0.0009340463937412581; -0.0006707305387823866 0.0017729994802521195 0.001386822412681352; 0.0030017865295030853 -9.684170869168828e-5 0.00011515962781311732; -8.914397008704517e-5 -0.0007624204811625514 -0.0007599947297281223; 0.00010995696160299648 6.822163294788316e-5 -0.0003191897804125411; -0.00015545197397445233 -0.0003715616139069184 -2.928526650221785e-5] %
+
+Mass Used: 53.046153488228356 kg
+Launch C3: 140.75080650177023 km²/s²
+||V∞_in||: 0.6330535016400611 km/s
diff --git a/archive/ES_0.7518603574347142 b/archive/ES_0.7518603574347142
new file mode 100644
index 0000000..fd04c23
--- /dev/null
+++ b/archive/ES_0.7518603574347142
@@ -0,0 +1,22 @@
+archive/ES_0.7518603574347142---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T20:35:38.280
+Launch V∞: [8.833950564623855, -7.462061032839446, -2.4489243957625613] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.700383185462534e-6, -2.624162594082143e-5, 3.951012107607454e-6] km/s
+ V∞_out: [-4.109444996577938e-6, 1.6474659247455933e-5, 2.0571205050598835e-5] km/s
+ time of flight: 8.107464098583187e7 seconds
+ arrival date: 2026-12-04T05:19:38.280
+ thrust profile: [0.721003428335907 -0.35219709649361847 -0.2812989362998257; 0.4559321515932038 -0.04434988692102357 -0.25606221475434593; 0.23770659364621036 0.020533453100153816 -0.1791327265006237; 0.09737463100130572 0.019792562332712343 -0.09273127702901691; 0.01725200453612236 0.0053915253639849284 -0.019487749357427107; 0.0031222415356415064 0.001906881506150944 -0.0007417234777805947; 0.0044513428162406355 0.001467854137759506 -0.005749270334138087; 0.004889823436740351 0.0007210231288620668 -0.004394063995842682; 0.002698814244801409 0.0016386808161073046 0.0002036446997903626; 0.006344770865925558 -0.0006397489483257143 -0.00642024910941294; 0.0022127332336135176 -0.0027106094835372724 -0.005823175835217078; -0.0012248328749366625 -0.006836782905778038 -0.0020523283436130555; -0.0015879086849126098 0.0024410854278245735 -0.00027086400533448676; -0.0007721208076038712 -0.0024447819743308036 0.0003291097484811158; 0.0013709371481675598 -0.0015285318177885108 -0.0008830739631450436; -0.0009522705876473683 -0.009029129989637688 0.007502468784670106; -0.007787537890339004 -0.00457095323266268 0.002036023714349611; 0.002065522795291425 0.00795014838121496 -0.0048843953608595225; -0.0008920844493379135 0.0007729990446604252 -0.0004161828744149716; -0.0035079875595290123 0.0009184001130969949 -0.004160487063743205] %
+
+Mass Used: 62.14718623599947 kg
+Launch C3: 139.71826813220008 km²/s²
+||V∞_in||: 2.6674435290007207e-5 km/s
diff --git a/archive/ES_0.7645629890886761 b/archive/ES_0.7645629890886761
new file mode 100644
index 0000000..47496f7
--- /dev/null
+++ b/archive/ES_0.7645629890886761
@@ -0,0 +1,22 @@
+archive/ES_0.7645629890886761---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-01T00:47:23.075
+Launch V∞: [8.73880313785822, -6.841212344639952, -1.8714028039678943] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-1.6732581120473174e-9, 6.860446957325391e-10, -9.282500736995751e-11] km/s
+ V∞_out: [1.2520373296398024e-9, -1.1243756593593086e-9, -9.092199948036654e-10] km/s
+ time of flight: 8.368410638254885e7 seconds
+ arrival date: 2026-12-25T14:22:29.075
+ thrust profile: [1.0 -0.7260816798125624 -0.5221109407270118; 1.0 -0.011316931989143303 -0.6866952050866189; 0.9881935702549839 0.19934038452552066 -0.6215555008566784; 0.3154718834284725 0.10216017394212862 -0.2433416646112872; 0.14711707090448456 0.060152940139807806 -0.12978235440846822; 0.007534520616440096 0.0041399447006685835 -0.011082377659710332; 0.01618670696724964 0.008306995296487547 -0.01714388189930545; 0.005254795968722959 0.002963788672743729 -0.005035034798062426; -0.0021515063363921976 0.004072224887162544 -0.002485463433734908; -0.003296859904492316 0.0011741654130089205 -0.002945407282860111; -0.000208967023188552 -0.010540017109930525 -0.001537380032761984; -0.008729610567923995 -0.004845759595065413 -0.010186553260316788; -0.005236179967622607 0.008126924716473123 0.007111589685472231; 0.01307268677621358 0.0077191986542122434 0.021391258095320578; -0.028019378449284222 -0.0003135368818428497 -0.0064059762529873835; -0.006864001827634412 0.01545260736826886 0.01304743063275955; -0.007420376723956295 -0.016135511013320458 0.005146723136338686; 0.0016214657768161105 0.004192070350132664 0.005732359502383033; -0.010097369113253684 -0.004882929238768678 -0.012899852661201902; -0.014087513138118318 -0.011511030060457393 0.017853991739108767] %
+
+Mass Used: 153.07589929532605 kg
+Launch C3: 126.67101508139362 km²/s²
+||V∞_in||: 1.8108192941506168e-9 km/s
diff --git a/archive/ES_0.7646541077971954 b/archive/ES_0.7646541077971954
new file mode 100644
index 0000000..baaf41b
--- /dev/null
+++ b/archive/ES_0.7646541077971954
@@ -0,0 +1,22 @@
+archive/ES_0.7646541077971954---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-10T17:20:08.844
+Launch V∞: [8.70630742624718, -7.433846418195579, -0.6235975499418727] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [7.813245172613275e-8, -1.9918855690060385e-6, -3.56836132518268e-8] km/s
+ V∞_out: [-2.371304081358843e-6, 3.4699163318790145e-7, -5.249082721029882e-7] km/s
+ time of flight: 1.8144078792629108e8 seconds
+ arrival date: 2030-03-11T17:33:15.844
+ thrust profile: [0.006407048441034362 -0.008169189724399376 -0.0023429904547795917; 0.01151492624295238 -0.03626513214715429 -0.014777112333653888; 0.046355123576733055 -0.1483157699560763 -0.06151495499712988; 0.13238187806157745 -0.3920540313697338 -0.1625881777781372; 0.16073016479132557 -0.43424115608453323 -0.18306302847670206; 0.1150924895543153 -0.2865225672858497 -0.1251169959932028; 0.02683569043491853 -0.06434417702460798 -0.028701100730768175; 0.018704833113991966 -0.04252651406145596 -0.019380477023321102; 0.009688960190008191 -0.02169843706001566 -0.009977352232367714; 0.019062790007140402 -0.03915380816862808 -0.018364383982556746; -0.0007597620944435893 0.001674313875091395 0.0004315876378493782; 0.00024237253587666856 0.0008434477902325402 0.0008879477325796081; -0.0025498913240554876 0.0038944976094387154 0.0007227900027656166; -0.0019183330835374967 0.000650123915095664 -0.0018526309525174363; 0.002607916265282122 0.003958996543145425 0.0026657363071861044; 0.0003731288819973745 0.0033182450440969046 -0.0023548318465270524; -0.002519471678172151 0.0034646079127951942 -0.0007145648200482437; -0.0019308936322235731 -0.0037745141366908232 -0.0002898466029331286; 0.001674230438695898 -0.002156552347174802 -0.002093333475369388; 0.006262004425394815 -0.0007159055042033165 0.006625348369442817] %
+
+Mass Used: 125.30050216541395 kg
+Launch C3: 131.45073547393955 km²/s²
+||V∞_in||: 1.9937367229105135e-6 km/s
diff --git a/archive/ES_0.76964768169224 b/archive/ES_0.76964768169224
new file mode 100644
index 0000000..5aa54c3
--- /dev/null
+++ b/archive/ES_0.76964768169224
@@ -0,0 +1,22 @@
+archive/ES_0.76964768169224---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-09T14:39:26.801
+Launch V∞: [6.921277728218928, -7.624839370725687, -2.0213236284894482] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.016667189516221367, 0.016990878038213687, 0.001804400950046681] km/s
+ V∞_out: [-0.006283203872084639, 0.023013895199796092, -0.0007348955196517658] km/s
+ time of flight: 1.1218608212179132e8 seconds
+ arrival date: 2027-11-29T01:27:28.801
+ thrust profile: [0.5907420176123385 -0.3124145477368173 -0.3160741060941656; 0.059856411998852416 0.019310846945503158 -0.17465234819775166; -0.021387782400540636 0.039745221444043986 -0.07941908559578506; 0.04246982817690181 0.022966898499370343 -0.13407013268502452; 0.053703098345657646 -0.053601034372137535 -0.2968049230965258; 0.08632569143617352 -0.016773846845608863 0.05448201858056728; 0.014555392112970168 -0.027466038718140115 -0.12967647291541634; -0.03182351389332952 -0.05589840723716813 -0.06218928686412975; -0.21451325503643046 -0.07308296724748711 0.03319811440887617; 0.13768868331172418 0.05087751499536935 -0.12765827371514454; 0.29449863001648446 0.11750842057043451 -0.1339374754146681; -0.05181080176178202 0.02007889289421421 0.11559434887700568; 0.05411006900791343 0.05555053584320457 -0.2137962266095742; 0.011033316797928107 0.06725685505475686 -0.07553435772410558; -0.07551389932815329 0.0788372398003479 0.2638004795737572; 0.27738291807297155 -0.1596389864284302 0.23397158797805997; -0.3690221589350552 0.6399641776336469 -0.1803196308912843; 0.19205268872546455 -0.18582672713553486 -0.262400871706008; 0.05884480068595305 0.04032696276261178 -0.027813895729807456; 0.08733331514802113 -0.24099807707612256 -0.7680910565261663] %
+
+Mass Used: 255.5089034566272 kg
+Launch C3: 110.12801003159761 km²/s²
+||V∞_in||: 0.023869248116931144 km/s
diff --git a/archive/ES_0.7708266646318561 b/archive/ES_0.7708266646318561
new file mode 100644
index 0000000..beabc41
--- /dev/null
+++ b/archive/ES_0.7708266646318561
@@ -0,0 +1,22 @@
+archive/ES_0.7708266646318561---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-24T07:10:51.626
+Launch V∞: [7.18595210949459, -9.497910569534671, -2.2039880539611967] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.9814652002911279, 0.9658003215468179, 0.6660240981857164] km/s
+ V∞_out: [1.1984019627234141, -0.7224586179867588, -0.6268446670504293] km/s
+ time of flight: 9.055800002582112e7 seconds
+ arrival date: 2027-04-07T10:10:51.626
+ thrust profile: [0.7759669011219986 -0.6805922623340009 -0.3945294350905995; 0.0041468800563150025 -0.00367978028032835 -0.0074920636215688756; 0.0021123569331095754 -0.0006478081961683712 -0.007612067915325479; 0.0019604742842330735 -0.002220223990912737 -0.0011730897376965007; -0.00021458171777894884 -0.00012721101928649852 0.0012572234513397716; 0.0023072257566851126 -0.0030228196438936033 -0.00571703044206111; -0.0021485625552564985 -0.00026710563075453585 -0.0027996567015462683; 0.0010669132561049075 -0.002950888483436479 -0.0049097916766478004; -0.002869602618887232 7.611322682638151e-5 -0.0036221596572486355; 0.00039995921147237734 -0.003341146280407932 -0.01080244976285254; 0.0019463608126379706 -0.0032186600258072885 -0.005983113218490137; -0.0005727570981256588 -0.00012066786593306579 -0.0009991511604624031; -0.002052710973730656 0.0006313943859860066 0.0002829069969618194; -0.0011203672884958406 -4.694584332919148e-6 0.002340427592737097; -0.0007035518843665368 -0.003074118827495869 -0.0037644302591128736; -0.0018609632107715207 -0.0012686040108571895 -0.002568474341576145; -0.008353600657365089 -0.00017100509063236588 -0.003241817613321006; -0.0006160285214324301 0.0003446729012198848 0.0026645904141301426; -0.0027873155857055113 -0.006432445688126773 0.0007389327266060525; 0.000323578505003414 -0.007647816031049866 -0.0014473034329406157] %
+
+Mass Used: 43.51408061897973 kg
+Launch C3: 146.70577624883182 km²/s²
+||V∞_in||: 1.5295856628010531 km/s
diff --git a/archive/ES_0.7743052143442224 b/archive/ES_0.7743052143442224
new file mode 100644
index 0000000..9db0ce0
--- /dev/null
+++ b/archive/ES_0.7743052143442224
@@ -0,0 +1,22 @@
+archive/ES_0.7743052143442224---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-07T23:56:07.903
+Launch V∞: [7.241245091934011, -6.906985210123064, -0.6164143372376546] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0007755880728621376, -0.0043715019091073535, -0.004170461993911833] km/s
+ V∞_out: [-0.005341152906393544, -0.0006166836178435756, 0.002863060478918891] km/s
+ time of flight: 1.462231607431396e8 seconds
+ arrival date: 2028-12-25T09:28:47.903
+ thrust profile: [0.1971827503426773 -0.11695238896712772 -0.044019206631471804; 0.01959670928655531 -0.02775765328889681 -0.04876788459056708; 0.057578671024243896 -0.07233909456322421 -0.028333223899165136; 0.05358560629208384 -0.0875510887394188 -0.031014454330973662; -0.0003146345701827112 -0.09934999023382536 -0.012895073281941616; 0.033382279905444394 -0.023993863557376274 -0.07147448322978738; 0.05112983799518981 -0.0007065451853939114 -0.14609002963705092; -0.014156907082229268 -0.060118624673692264 -0.05699468952354683; 0.25278096581204074 0.2256873219707113 -0.16139847774223737; -0.06645930394224449 0.1279634434894405 -0.08571621939688501; 0.0344042074517138 0.39636220993718996 -0.2038375133084272; -0.36491203086962026 0.18504663792736806 -0.275570940685372; 0.010574898073994789 0.01927268215930203 -0.12638316476881234; 0.1386503325766193 0.007999021241817748 -0.08033781575891921; -0.15930559781705678 -0.22778745945248555 -0.17377065620271137; 0.12172201712419288 0.5948990698536183 -0.013591909380693337; -0.1559329316782442 0.0714675387430356 0.17074309023327194; -0.45667461724179126 -0.40172264926720114 -0.3598550963270659; -0.15862291428778205 -0.19858064547764048 0.06393449183407363; 0.5290093715330506 0.28353928458088995 0.09471228310485809] %
+
+Mass Used: 316.9775061796886 kg
+Launch C3: 100.5220418094693 km²/s²
+||V∞_in||: 0.006091331467155461 km/s
diff --git a/archive/ES_0.7748330662878514 b/archive/ES_0.7748330662878514
new file mode 100644
index 0000000..2313232
--- /dev/null
+++ b/archive/ES_0.7748330662878514
@@ -0,0 +1,22 @@
+archive/ES_0.7748330662878514---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-24T13:58:00.709
+Launch V∞: [5.147203335648341, -8.55703438845335, -1.3989752951331347] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0034143572641559417, -0.002112379057881663, 0.001966984945183975] km/s
+ V∞_out: [-0.00262239717744685, 0.0030185398528519277, -0.0019994900767724504] km/s
+ time of flight: 1.2530565323584826e8 seconds
+ arrival date: 2027-04-13T21:05:33.709
+ thrust profile: [0.5097329571885071 -0.3322910490900801 -0.2924882469079728; 0.16128118148984802 0.01110303139917472 -0.2326631418620665; 0.12467286286963243 0.04289469370089566 -0.25849419758611136; 0.07504501108298083 0.04816003765547745 -0.2237257566615222; 0.05390449986720992 0.031108135571247496 -0.1469894043614276; 0.13671176678469926 -0.04769264015729386 -0.22151940845050133; -0.004594636039590046 0.06039024156161144 -0.22336184222254563; 0.048928374835719574 -0.09031000005660203 -0.024597670005029965; -0.01028291515715745 -0.09215958050146772 0.006092576110411391; 0.10412214976959078 0.10074765295491794 0.08306083968740373; -0.08961507169557466 -0.10771528933079508 0.06158654248113635; 0.0034051795740968147 -0.0416788074079853 0.10786902856705305; 0.03747624555677051 -0.06534117202919283 0.036090631094643916; -0.023293328539404946 -0.2281006842726546 0.07224282627473637; 0.14999682227701147 -0.2368658678515012 -0.02412199861247894; -0.5419574045149439 0.5827644109199104 -0.1164539802453482; 0.05171084657264916 0.21649298193619634 -0.0626883091448601; 0.18299713889497177 -0.07955974015787463 -0.06562797141667195; 0.35912605944575887 0.13763657714313646 -0.6933253770889276; 0.3774402444024937 -0.20757774585654276 -0.682777643099127] %
+
+Mass Used: 310.87549311872 kg
+Launch C3: 101.67367158007544 km²/s²
+||V∞_in||: 0.00447090713234483 km/s
diff --git a/archive/ES_0.7769936280510455 b/archive/ES_0.7769936280510455
new file mode 100644
index 0000000..2424e36
--- /dev/null
+++ b/archive/ES_0.7769936280510455
@@ -0,0 +1,22 @@
+archive/ES_0.7769936280510455---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-20T09:09:45.882
+Launch V∞: [7.352687997708827, -8.681922117152217, -2.1207602984321197] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.495782699405155e-6, 1.5772132425734653e-6, -1.1777862312401668e-6] km/s
+ V∞_out: [1.7930788406766236e-6, -2.1695487738214965e-6, 1.479501673393297e-6] km/s
+ time of flight: 8.314454419739859e7 seconds
+ arrival date: 2025-12-07T16:52:09.882
+ thrust profile: [0.9435610902150074 -0.6889790910152848 -0.37525509503834525; 0.6125330314098766 -0.14519850365942266 -0.3025875662400548; 0.41775187352335424 -0.014069541470865607 -0.25295759852466093; 0.35816589839772406 0.028675861695275726 -0.2559970619915146; 0.22486497535616878 0.032148685848929756 -0.17487263942911024; 0.012781092922760095 0.0034065488515263795 -0.01422032188463438; 0.02752824170987159 0.010595220087149314 0.023231904565109093; 0.023328569159875346 0.004514737990622438 -0.025342743189141467; 0.007269682918862535 -0.013730536196514473 -0.013114011799484595; 0.0011957178524870937 0.004693717969918204 -0.057263664655228516; -0.0010727231488889578 0.010164281463626502 -0.015931699338663605; 0.003038011795648412 0.038256794494292055 -0.01717818516250667; 0.01562989098080534 0.014002495768139063 -0.08104673324455909; -0.0006409428696990023 -0.042183643135862293 -0.03048003887749874; -0.025437135641617155 -0.02026935535259479 -0.011764448430114857; 0.07038453278160982 0.05820563064395558 -0.006536016690719979; 0.03415749842456408 -0.004769339755575053 -0.043935215938116945; 0.008548774610244309 0.001537681314902996 -0.006949289409662844; -0.0008266677124867164 0.030023470042592967 -0.005636554633070404; 0.03740353786697699 0.010311586937843443 -0.03119176686470388] %
+
+Mass Used: 125.20263540665383 kg
+Launch C3: 133.93541668335416 km²/s²
+||V∞_in||: 3.1786338734900097e-6 km/s
diff --git a/archive/ES_0.8129769673294392 b/archive/ES_0.8129769673294392
new file mode 100644
index 0000000..dd1b686
--- /dev/null
+++ b/archive/ES_0.8129769673294392
@@ -0,0 +1,22 @@
+archive/ES_0.8129769673294392---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T12:36:34.759
+Launch V∞: [8.3049474059845, -7.569784544640874, -2.295226357721686] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.347598204101537, -1.48384450141465, -2.255673713055855] km/s
+ V∞_out: [0.9696302822801812, 0.43191576423952743, 2.5049294322111453] km/s
+ time of flight: 8.337012390309563e7 seconds
+ arrival date: 2026-12-31T10:58:37.759
+ thrust profile: [1.0 -0.6415828650823978 -0.46384011159124183; 0.5257251738318173 -0.07200730306002899 -0.3188922137107601; 0.08929410898451699 -0.009894512014592271 -0.08984128445625378; 0.053929139041237056 -0.10670820567245617 -0.05770934351460263; 0.06036829439179214 -0.005429165781493682 0.046012144983413654; 0.009958240258628811 -0.05722466175579025 0.026655376907994705; 0.09355665670730579 0.04842365139857453 0.02007795340186147; 0.0058483042167744095 -0.009902493940946413 -0.06380816848424221; 0.05303317392600195 0.01171718829994684 -0.04491598755355993; 0.027910769729135455 0.028077231273861213 -0.06229592011031617; 0.2980550151905342 -0.014245166163217683 0.026493303108678208; 0.27581627176514006 0.08823615170997848 -0.1118981403048257; 0.06059834176429582 0.2802682049337076 0.11054073199776655; 0.07826047157443346 0.18620533073231646 -0.0643059029186557; 0.13028166529628696 -0.08503203622982143 0.14029441150151195; -0.2605937994032228 -0.1459744800606984 -0.17957756143453696; -0.24679700982681735 0.04413926131387592 -0.3157900098235231; -0.2836049785993019 0.005519483546363655 0.07080067091232159; 0.2737601161271743 -0.03273213810949846 -0.36346682868901864; -0.004392015052234806 -0.002548083474671524 0.004568979937481383] %
+
+Mass Used: 181.14564979148736 kg
+Launch C3: 131.5418535016329 km²/s²
+||V∞_in||: 2.7222569525385167 km/s
diff --git a/archive/ES_0.8140608735533477 b/archive/ES_0.8140608735533477
new file mode 100644
index 0000000..1392f77
--- /dev/null
+++ b/archive/ES_0.8140608735533477
@@ -0,0 +1,22 @@
+archive/ES_0.8140608735533477---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-10T03:59:44.866
+Launch V∞: [8.136273813130833, -8.680482022355276, -0.6676987516644032] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [5.022978170210289e-5, 3.089864042060603e-5, 0.0015821083120331834] km/s
+ V∞_out: [-0.0005780551419648015, -0.0013396839041041983, 0.0006138324292400283] km/s
+ time of flight: 1.6858035469569075e8 seconds
+ arrival date: 2029-10-13T07:52:18.866
+ thrust profile: [0.07376617077210428 -0.08966532384295649 -0.036448974545527424; 0.02363945375708729 -0.08663420401605894 -0.04669452996648175; 0.03483726843013675 -0.15313693604427475 -0.08141186006630591; 0.04576673044863474 -0.18766454405670185 -0.10146080288067871; 0.06682839937086954 -0.24659735771427657 -0.13433444518479434; 0.05235736191646536 -0.17597533377677602 -0.09824002799234714; 0.09689553189817689 -0.2932542643178447 -0.16600225029117033; 0.01872472597848029 -0.05457915619613928 -0.03160441528828124; 0.022684615422616117 -0.06309442485752301 -0.03842065473809385; 0.005080090812043856 -0.007662980787257334 0.00352478149260089; 0.005644509555481184 -3.26877110293361e-5 -0.002263869213758058; -0.0028659250776767262 0.0022031524441706884 0.005745662002577607; -0.013228970732802523 0.002184504329625412 0.0040822079173378645; 0.014743877813254338 0.005364932787290561 -0.008297394541756887; 0.019722220365798557 0.008904067700365129 -0.024945899067059765; -0.0016888838065589394 0.006021487218567587 -0.00903920128140916; 0.006052768931614584 -0.008481680369267905 0.017580654815649473; -0.01739477621158295 -0.013781076203018668 -0.004374825921597059; -0.0041841536656096 0.024805672945014085 0.0011542526794167864; 0.006787830328076365 -0.027550716561745955 -0.01807670233931433] %
+
+Mass Used: 121.43036141263792 kg
+Launch C3: 141.9955413256459 km²/s²
+||V∞_in||: 0.001583207019929539 km/s
diff --git a/archive/ES_0.8223919770193127 b/archive/ES_0.8223919770193127
new file mode 100644
index 0000000..ede4e2a
--- /dev/null
+++ b/archive/ES_0.8223919770193127
@@ -0,0 +1,22 @@
+archive/ES_0.8223919770193127---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-12T01:03:20.880
+Launch V∞: [6.2801509951060295, -7.596481191980322, -1.4228982502972005] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0012490959485957826, -0.0018148272969913757, -0.00015955401289316265] km/s
+ V∞_out: [0.00015721511026354297, -0.0006743307477079151, -0.0020978652650430756] km/s
+ time of flight: 1.3738317137611642e8 seconds
+ arrival date: 2028-09-18T03:02:51.880
+ thrust profile: [0.9162355654995709 -0.4482793469074367 -0.41985438384473034; 0.09332237526449066 -0.03871729021812295 -0.2506853225145068; 0.029679371377552517 0.1609846990370001 -0.219931882404862; 0.10141792952860301 0.20317411475189331 -0.19569335230787005; 0.0822616637036831 0.28337925498381333 -0.1857424613823716; -0.04540786302972602 0.12153635091622014 -0.19162256147789575; -0.0065859491535159125 -0.10338871596740948 -0.027160882329365452; -0.20138780956077587 -0.10982488768854062 0.06960651365908122; 0.030822166457856143 -0.24987152170878557 0.13533925082301873; -0.036169265052708885 0.05064551379455824 -0.2430417595543215; -0.1473819962852825 0.13151174705740123 -0.055625314832398895; 0.07681839276358322 -0.025113484847767924 -0.1907046787228516; -0.21415788406114122 0.04746021808296784 -0.14865887295523694; -0.5671148663725925 0.038317097495083025 0.23729895528264147; 0.17382546874770097 -0.41666563399058326 0.1106879371199891; -0.01967397963235001 -0.08310868877214098 0.2073869319720012; -0.10358185239013634 0.4610527796682605 0.193278969374042; 0.41126216513024355 0.3726193971637455 0.3231740181394148; 0.026333895868209486 -0.053456767084797546 0.015165952522075657; 0.25318704793228697 0.23949412757577732 0.07441909191745669] %
+
+Mass Used: 380.957108885043 kg
+Launch C3: 99.17146245214087 km²/s²
+||V∞_in||: 0.002208912920360088 km/s
diff --git a/archive/ES_0.8485968295718769 b/archive/ES_0.8485968295718769
new file mode 100644
index 0000000..9ed5936
--- /dev/null
+++ b/archive/ES_0.8485968295718769
@@ -0,0 +1,22 @@
+archive/ES_0.8485968295718769---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-17T12:05:52.482
+Launch V∞: [9.578139468322572, -6.501470055430596, 0.023956368045586034] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00019313865262200028, -0.0005456972196623935, -0.0013289751052194749] km/s
+ V∞_out: [-0.001317043352811102, -0.00015938129657251928, 0.0005756331388171925] km/s
+ time of flight: 1.8749577813158083e8 seconds
+ arrival date: 2030-05-27T14:15:30.482
+ thrust profile: [0.07869595060262992 -0.07224675679179603 -0.016371292043137094; 0.0005416538295817387 -0.0011427134403820807 -0.00032981876857020537; 0.05618127237220429 -0.12855961157876497 -0.036123836750816235; 0.21526282804429858 -0.4632036153890776 -0.12788201271366262; 0.29796619445143074 -0.5910749447544441 -0.16489027044001917; 0.2993354255595228 -0.5568542300722851 -0.15888335711845503; 0.22036948524818656 -0.3905739613245828 -0.11506601467390097; 0.08994614977120255 -0.15257356589783563 -0.047150068906066996; 0.011609040754641226 -0.020009382494857095 -0.005692444115377121; 0.00047412030924107607 -0.0007432023949210196 -0.0002530837163182802; 0.00034597585564033283 -0.0005080594873626332 -0.0001937253948234374; 0.00029795863906769955 -0.0004512260943395199 -2.9903243604831512e-5; -2.493088098074157e-5 -3.605456597627108e-5 -0.0001226377230081212; 0.00019157438032829633 -0.0001687102422012194 -5.4413338782611084e-5; 0.00020032080461579614 -0.000263845446567799 0.00022103636372038397; 4.3520474175691405e-5 -0.00030716715597239625 -7.623862143370346e-5; 8.752883741507605e-5 -7.929524601029874e-5 -4.465412296670988e-5; -0.0001693898683017628 0.0006137813640437918 4.8646815841959644e-5; 0.0003318607604823929 -0.0006452716488521523 -0.0002321243867306447; 0.0003212475577540574 0.00012289697482132782 0.00017806162307994238] %
+
+Mass Used: 208.3020534612856 kg
+Launch C3: 134.01044246386925 km²/s²
+||V∞_in||: 0.0014495733251467559 km/s
diff --git a/archive/ES_0.8533561730219879 b/archive/ES_0.8533561730219879
new file mode 100644
index 0000000..0d0bcc0
--- /dev/null
+++ b/archive/ES_0.8533561730219879
@@ -0,0 +1,22 @@
+archive/ES_0.8533561730219879---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-03-06T07:27:15.327
+Launch V∞: [2.2351465196927816, -8.160534279578052, 0.23764114991714666] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-5.6717226212899215e-5, 9.342984257107054e-6, 0.00016015132733879822] km/s
+ V∞_out: [1.9930828386843815e-8, 1.8731517964549627e-8, 9.118673266794555e-9] km/s
+ time of flight: 1.8749577786715463e8 seconds
+ arrival date: 2029-02-12T09:36:52.327
+ thrust profile: [0.9999350637957232 -0.9998960814928128 -0.012086305549804227; 0.9999652111768015 0.0750474102117487 -0.08175605086456197; 0.9999604714820137 0.5188090644614609 -0.13103333669006068; 0.9999394420252692 0.7433387592977789 -0.1516136554830832; 0.710305215613942 0.650804643781956 -0.13066890585424915; 0.5038216339618388 0.5631026652793385 -0.11279843812682605; 0.3792084151777885 0.5066581214161733 -0.10061261523771918; 0.20526453177055864 0.31270825883468 -0.062315458646044694; 0.06577213593006079 0.11016102396656256 -0.021797398980281837; -0.0005005648846355883 0.0010936651008956327 -0.0008707019799378895; -0.0023012739554981367 0.0014679579418397264 -0.0008492432224063492; 0.0004950446850307374 0.0013441453679462166 -0.0002994735740529338; 0.00046557075371709926 8.982740295412006e-5 0.0015743514873596512; 0.00185433053487073 -0.0009212947062092071 0.0017815154201362888; 0.0034640331062496753 0.0017996514266277088 0.0008506389894623529; 0.0003945873852201592 0.0014805360021674335 0.00018712458539071723; 6.485990697372741e-5 0.0016832426968628835 0.0008077422986660725; -0.004161146340561436 -0.0029584085140549558 -0.005557529654218631; -0.0005189048936627944 -0.005836268472228427 0.0032236073568525985; 0.00026774066667472945 0.004540026644137348 -0.00823678152996437] %
+
+Mass Used: 577.6432759743357 kg
+Launch C3: 71.64667300879717 km²/s²
+||V∞_in||: 0.00017015458487061884 km/s
diff --git a/archive/ES_0.8768587223701253 b/archive/ES_0.8768587223701253
new file mode 100644
index 0000000..5d4e092
--- /dev/null
+++ b/archive/ES_0.8768587223701253
@@ -0,0 +1,22 @@
+archive/ES_0.8768587223701253---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-19T10:24:44.498
+Launch V∞: [9.585322391657675, -7.174936581714741, -1.1218452354568096] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.10739488580278787, 0.6453258581236461, 0.686989055506836] km/s
+ V∞_out: [-0.17060688196457224, 0.14963854567296028, -0.9148925650120416] km/s
+ time of flight: 1.8749577788406017e8 seconds
+ arrival date: 2030-05-29T12:34:21.498
+ thrust profile: [0.0012213160508615488 -0.0010548602161144893 -0.00018256358189312926; 0.01040214396097694 -0.02413904823244764 -0.005064251795459239; 0.08150599743435819 -0.20089655408839913 -0.039566850116576915; 0.16809285310214603 -0.37990531352324886 -0.0772702345509167; 0.23517460913916352 -0.4867346272077655 -0.10411628337372825; 0.17574049667433053 -0.3428965478006146 -0.07315768726568307; 0.07302296488753214 -0.13557091748525787 -0.029859648754871074; 0.18304622707484602 -0.3141586543965469 -0.06260957990015001; 0.12331135444844896 -0.20646565281466908 -0.04325342655920208; 0.00629270144275376 -0.010545126296042037 -0.002387211645569639; 0.00021495010420757542 -0.0003669604183488926 -0.00015099607554934592; 0.0002523124297583734 -0.00041235196227067594 -3.909008929690828e-5; 0.00026684055562266345 -9.457756963263185e-5 -9.417174184196338e-5; -9.750860644988505e-5 -0.00034519579865266496 -0.0002701978872750859; 0.00026270906133854315 -0.00013707640270021516 2.1040791412445183e-5; 0.0003704376304627709 -0.00012495153771338412 0.0006354377821624934; 6.915717143783878e-5 -0.0009703252687204213 -0.0007662975667647533; 0.0006084884798334175 -9.237759633545278e-5 0.0012400790826578396; -0.0001419284211188584 -0.0003058358553086818 -0.00011721829419710995; -0.0002119385268998071 0.0005057892325013839 -0.0002253495915660745] %
+
+Mass Used: 179.40467672204886 kg
+Launch C3: 144.61665703595955 km²/s²
+||V∞_in||: 0.9486480311716188 km/s
diff --git a/archive/ES_0.9001081163408466 b/archive/ES_0.9001081163408466
new file mode 100644
index 0000000..f4183e3
--- /dev/null
+++ b/archive/ES_0.9001081163408466
@@ -0,0 +1,22 @@
+archive/ES_0.9001081163408466---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-03-09T13:14:09.516
+Launch V∞: [2.979356376897908, -7.731649801139638, 0.3230369020249006] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.0032426642405340993, 0.01946131953447114, 0.022453335609988006] km/s
+ V∞_out: [-0.013039621939654475, 0.010662112754483633, -0.024657364275392387] km/s
+ time of flight: 1.8571635628616735e8 seconds
+ arrival date: 2030-01-27T01:06:45.516
+ thrust profile: [0.9999998765814196 -0.9821366699757795 0.0048354818321583275; 0.9999999090706105 0.19055873394382747 -0.06069480178188491; 0.9999999015681417 0.7631355664142537 -0.10851972325829906; 0.9999998454484503 0.9999992749451425 -0.1359267768140522; 0.8998749271033636 0.9999999762519093 -0.13757680657497182; 0.6233468611633489 0.9373259881086107 -0.11987393035517527; 0.3712117606430761 0.6985826636820259 -0.08947734650617423; 0.1435211656494696 0.32620451829346786 -0.042427926002853535; 0.0045624834128191955 0.012512528089549328 -0.001608009279656283; 0.0007548852112328941 0.002188607295625592 -0.0003415512757837882; 0.00032701334975239677 0.0009095366137592958 -0.0003710787227093062; -0.0004414221548404388 0.0014404372928376536 0.0005020337317906988; 0.00017998893952373904 0.00035492273349691655 2.850822869372206e-5; 0.00043524959026036117 0.0007164470405169694 -0.0009347381488753096; 0.0007370584630849407 0.005673989222408218 -0.00010305275749565519; -4.310014236939507e-5 0.0012147393942738452 -5.104423710841573e-5; 2.5818925603375456e-5 0.0006435835525740591 0.0005010906209953468; 0.0005419934500789321 -0.0010748718030169219 -0.0008522272588533122; -0.00022982139551993414 0.0025884539540375804 0.00012592383309592168; -0.00030290368460315106 0.00027394847176936477 0.00035736088446012887] %
+
+Mass Used: 649.0300679337688 kg
+Launch C3: 68.75932590809468 km²/s²
+||V∞_in||: 0.029889966701459905 km/s
diff --git a/archive/ES_0.9648905828906206 b/archive/ES_0.9648905828906206
new file mode 100644
index 0000000..77e4411
--- /dev/null
+++ b/archive/ES_0.9648905828906206
@@ -0,0 +1,22 @@
+archive/ES_0.9648905828906206---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-24T16:44:09.584
+Launch V∞: [9.999998912428419, -7.609165353762185, -0.9885404813924823] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.9094995450618288e-7, -6.231467540023355e-7, -1.8121605709005575e-6] km/s
+ V∞_out: [-1.7749231405214407e-6, -2.066761634624295e-7, 7.54197209086473e-7] km/s
+ time of flight: 1.874957778671796e8 seconds
+ arrival date: 2030-06-03T18:53:46.584
+ thrust profile: [0.0763363222751099 -0.06483720168264455 -0.011323846217185098; 0.0014653080983305328 -0.0029025806967571733 -0.00052375880711249; 0.07570410574100513 -0.15898380510765914 -0.02875826092756588; 0.23661996832568274 -0.47192866811801265 -0.08509681860931283; 0.3089973406022546 -0.5761460233013861 -0.10557099864473957; 0.25676603723998026 -0.4557178382411448 -0.08619254131493975; 0.12749875602881455 -0.21642386847712122 -0.04260014929123655; 0.10598897116067371 -0.1722085183743881 -0.0346248374183628; 0.09976699142866378 -0.15592967364711396 -0.03191619988856478; 0.0019928795198599003 -0.00308173595193919 -0.0007231363850491517; 0.0003551444489595858 -0.0005247452567790894 -0.00011781075167152652; 0.00031775784816769385 -0.00042463825513632924 -3.163056754380464e-5; 0.00015575329991825848 -0.00017322691384964178 -8.436719046123125e-5; 1.3602751553560365e-5 -0.00014900855482487884 0.0001295464799172749; -0.00019929336574133242 -0.00023251049882073044 7.343691909656033e-5; 0.0001649282768219459 8.458226951302186e-6 -1.1592859082456994e-5; -2.2698803073771415e-5 2.3830567918697103e-5 1.7837344396490972e-5; -0.00021228748142038237 0.00025417274759343073 0.0001641754114813676; 5.383772025793177e-5 0.00020685647833047172 0.0001445302671717026; 0.0003935839117508285 -0.00019382833636918433 -0.00032952353754760026] %
+
+Mass Used: 198.9255838809636 kg
+Launch C3: 158.87658791281606 km²/s²
+||V∞_in||: 1.925798456972119e-6 km/s
diff --git a/archive/ES_1.0375146231089776 b/archive/ES_1.0375146231089776
new file mode 100644
index 0000000..63ed9fe
--- /dev/null
+++ b/archive/ES_1.0375146231089776
@@ -0,0 +1,22 @@
+archive/ES_1.0375146231089776---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-05T02:41:24.358
+Launch V∞: [7.551854836685511, -2.2262473990526197, -0.3178407177753899] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.00019130674051968661, 0.00015846499736227706, -0.00011870528378736181] km/s
+ V∞_out: [4.149688623142839e-5, 0.00028259994148441975, -1.2620998452645013e-5] km/s
+ time of flight: 1.874957778695672e8 seconds
+ arrival date: 2030-05-15T04:51:01.358
+ thrust profile: [0.3631594769989721 0.0749155536673463 -0.0015749373036098957; 0.0008194072096146858 -0.00019210547877198517 0.00011389839282669739; 0.20497631548593204 -0.11984217976713002 0.027033507095356683; 1.0 -0.8469320922445945 0.14906961874612126; 1.0 -0.9956949731447674 0.18503337566702696; 1.0 -0.9997033138690088 0.18389753194279965; 1.0 -0.9617775086279644 0.16811900834793775; 1.0 -0.8379714418976751 0.14308007190062136; 1.0 -0.6871737078010892 0.10790352390878633; 0.6668746710061697 -0.29305913368134273 0.03335961528515134; 0.1896071286634034 -0.09136278609547312 -0.00031995269102570587; 1.0 -1.0 -0.9703136599722595; 1.7241397513053207e-6 7.935607122097494e-6 8.327503023816445e-8; 3.90374763352124e-6 5.458680323885468e-6 2.2973091880480055e-7; 2.9650329383907666e-6 3.7828783105261452e-6 6.522350134860893e-7; 4.783066295806478e-7 1.5706193366863875e-6 -7.903306395672348e-8; -9.305529810213733e-7 6.244757988590304e-6 -1.5716076960521741e-6; -4.570860961842752e-7 1.5167792898855248e-6 -4.0408758488382376e-7; -8.620661714825902e-7 5.11973148947995e-6 -2.423069396638813e-7; -2.5924358516911006e-6 2.0789046611306967e-7 6.516330624843772e-7] %
+
+Mass Used: 848.2554088386037 kg
+Launch C3: 62.08771167803488 km²/s²
+||V∞_in||: 0.00027531866764956436 km/s
diff --git a/archive/ES_1.0738212025026774 b/archive/ES_1.0738212025026774
new file mode 100644
index 0000000..a706c3a
--- /dev/null
+++ b/archive/ES_1.0738212025026774
@@ -0,0 +1,22 @@
+archive/ES_1.0738212025026774---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-07-21T07:44:51.663
+Launch V∞: [7.09582120185737, 1.0418483860733283, 0.1870824619710649] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [2.1603383911584106e-5, 1.921570563259813e-5, 0.00105560101568233] km/s
+ V∞_out: [-0.0009411597636150051, -0.00030955899668697913, 0.00036532408760515115] km/s
+ time of flight: 1.855860283189078e8 seconds
+ arrival date: 2030-06-08T07:25:19.663
+ thrust profile: [0.2633375919084163 0.17585507294506372 -0.02440139785940584; 7.203724243051666e-6 2.7493876196225823e-6 -1.6361905568427755e-6; -3.983463022095976e-6 4.526184000624747e-6 -2.258188000408531e-6; 5.626569902524262e-7 -2.1843767685962923e-5 5.599913452408419e-6; -0.17469852075014594 -0.4940295269050607 0.07359822028324398; -0.40074221559845313 -1.0 0.17018928010672182; -0.2894014275317461 -1.0 0.17501010890757424; 0.2873005208171948 -1.0 0.14203809642274595; 1.0 -1.0 0.09700408256309916; 1.0 -1.0 -0.07112703205210712; 1.0 1.0 -0.15953189537569992; 1.0 1.0 -0.14665212285538182; 1.0 1.0 -0.1263211305047799; 0.9604521525573129 1.0 -0.09750383763069788; 0.23580031293990153 0.2677463245320255 -0.02312074277957748; 0.00047298912613043655 0.000565101627596323 -4.1660994822959556e-5; 8.397214558040246e-7 4.308003705097654e-6 -1.5893686594790193e-5; -7.357106161325681e-6 -4.363227161990519e-6 1.2533417541984207e-5; 5.218346455434379e-7 -2.1542963246027685e-5 3.6378462086162783e-6; 2.3316685728558492e-5 1.8944374285278115e-5 -9.537197439415734e-6] %
+
+Mass Used: 952.5431653772193 kg
+Launch C3: 51.47112643586932 km²/s²
+||V∞_in||: 0.0010559969004921162 km/s
diff --git a/archive/ES_1.0949531414252116 b/archive/ES_1.0949531414252116
new file mode 100644
index 0000000..2fb2bfa
--- /dev/null
+++ b/archive/ES_1.0949531414252116
@@ -0,0 +1,22 @@
+archive/ES_1.0949531414252116---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-23T21:27:01.145
+Launch V∞: [6.807115905330346, -0.22870230830279775, -0.08132785310828651] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-0.012707234483638573, 0.007467397017078201, 0.0005345671462951718] km/s
+ V∞_out: [-0.01017306965962499, -0.005709712426442979, 0.009008782004107234] km/s
+ time of flight: 1.8397989209127936e8 seconds
+ arrival date: 2030-04-23T06:58:33.145
+ thrust profile: [0.8103165326367464 0.3854175511115448 -0.03521725461081674; -0.0002654672443617776 3.949734657094911e-5 5.061645421541818e-5; 0.0003362316834222408 -5.504273189343045e-5 0.00017290955285327033; 0.00018948606135232816 -5.378321156504026e-5 7.479364389920395e-5; 0.16016220944482684 -0.14171526339314908 0.04065470883071412; 0.23811556358696942 -0.3729858465912579 0.08297842267313094; 0.2815217254643263 -0.90877375993525 0.15173414473727775; 0.1833133739911874 -1.0 0.14916862896704702; 0.2631307922678632 -1.0 0.11056487273801796; 1.0 -1.0 0.028438609702394233; 1.0 -1.0 -0.2524330561718592; 1.0 1.0 -0.21563351790986562; 1.0 1.0 -0.12701723833231301; 1.0 1.0 -0.08808077049649271; 0.8703453029711191 1.0 -0.06191719833385061; 0.38478073978260563 0.5809497508469789 -0.027489165115673467; 3.374413404691403e-5 0.00031292693107972866 -5.169753572092405e-5; 0.0005470161374374868 0.0004090610948687263 0.00014511214047151558; 0.000270800052530125 -0.00045762826188338083 -3.65020901761155e-5; -2.3899163081934868e-5 -0.0003136138980128239 -0.000782780591678357] %
+
+Mass Used: 1006.8034804970725 kg
+Launch C3: 46.39574591411561 km²/s²
+||V∞_in||: 0.014748613103161255 km/s
diff --git a/archive/ES_1.1160590966114972 b/archive/ES_1.1160590966114972
new file mode 100644
index 0000000..cf6af2d
--- /dev/null
+++ b/archive/ES_1.1160590966114972
@@ -0,0 +1,22 @@
+archive/ES_1.1160590966114972---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-24T00:48:36.266
+Launch V∞: [6.762374241108977, -1.8995969225881892, -0.42065802912560946] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.9840181377575237e-5, 2.509669728935545e-5, 2.3958516254052205e-6] km/s
+ V∞_out: [-2.957379321406089e-6, 1.3728221048187016e-5, 3.6449804922558114e-5] km/s
+ time of flight: 1.8530700773863646e8 seconds
+ arrival date: 2030-04-07T18:58:43.266
+ thrust profile: [0.9449484356448977 0.15265784599662993 -0.03407162232617072; 0.00016128968621013625 -8.58603896170562e-5 3.9328643789210574e-5; 0.011027790076231581 -0.005574471661377955 0.00342015190997176; 0.5122689486885356 -0.350049932890145 0.15514565599878943; 0.8660992260814107 -0.6212544473259712 0.24666566422323985; 1.0 -0.7495640898977531 0.27827909966868924; 0.981423007999943 -0.7965233597068561 0.26193342861366464; 0.7878794806416083 -0.8222669052145782 0.20765098240690985; 0.518549346711056 -0.960127838428525 0.13492726601030006; 0.21881983762998464 -1.0 0.02174455823912127; 1.0 -1.0 -0.9559918846710315; 1.0 1.0 -0.11927840692746813; 0.7984505321888469 1.0 -0.03574431122840408; 0.3636921253100367 0.6764373406689863 -0.005572356036180352; 0.00013908260006035265 7.259431413485221e-5 -4.7763588252468285e-5; 0.00010656041447241557 1.1835251097079853e-5 0.00012859740701802073; 0.00011774270312115905 -8.232513731217709e-5 6.309113220321464e-5; -9.32196785562413e-5 -8.354831119200572e-5 -6.471940388182824e-5; -5.02031696306545e-6 -2.381954415107187e-5 -8.76029212018712e-6; -5.779627283732218e-5 6.099270543120767e-6 -1.0894116711485716e-5] %
+
+Mass Used: 1013.2307050816466 kg
+Launch C3: 49.51512702258857 km²/s²
+||V∞_in||: 3.906431548729717e-5 km/s
diff --git a/archive/ES_1.148469222320979 b/archive/ES_1.148469222320979
new file mode 100644
index 0000000..0bc1d40
--- /dev/null
+++ b/archive/ES_1.148469222320979
@@ -0,0 +1,22 @@
+archive/ES_1.148469222320979---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-01-18T05:47:39.532
+Launch V∞: [-4.417549910925255, -5.897163172582938, 0.3311367280281343] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.004020236426475727, 0.00011823227234776388, -0.0027387450871508077] km/s
+ V∞_out: [0.004711851444026571, -4.628123695743769e-5, -0.0013497561988335854] km/s
+ time of flight: 1.8390221785801837e8 seconds
+ arrival date: 2028-11-15T17:44:36.532
+ thrust profile: [0.05014064318073163 -1.0 0.011461045655650651; 1.0 -1.0 -0.05951953393497983; 1.0 -0.6375447540282521 -0.08586812521824527; 1.0 -0.0363232956336098 -0.08649535523559387; 1.0 0.3344854524769929 -0.09694329338209909; 1.0 0.6243665041315285 -0.10749063430948069; 1.0 0.805126616436485 -0.11035145902657019; 1.0 0.8933710053774171 -0.10638128005702555; 1.0 0.9145066889017774 -0.09817654691499737; 0.9878134500090321 0.8746780543751003 -0.08623176020672403; 0.7753482143833724 0.7457849743190975 -0.06861092830597851; 0.4547913770694951 0.4782291218561762 -0.042160998501724854; 0.030812702576755592 0.03489021821430756 -0.003234716161380927; 0.0007243532730815151 0.0009397060291191669 -6.758005439942867e-5; -0.0005471889385547713 0.0018621983636613545 0.00022874404932698338; -0.00040197724227040716 -0.0003774740000732099 -0.0005178131097494307; -0.0005073724647809426 -0.0013085143770457022 0.0025048616188134386; -0.0014692750736326552 -0.00046767523696134657 -0.00038106568258965026; -0.0003348029999094244 0.0008718645566854262 0.00013545927908464774; 0.000721953677793413 0.0006850819594771289 3.1347672637998146e-5] %
+
+Mass Used: 1022.5419880197805 kg
+Launch C3: 54.40093223223338 km²/s²
+||V∞_in||: 0.004865902223368194 km/s
diff --git a/archive/ES_1.1590345050506037 b/archive/ES_1.1590345050506037
new file mode 100644
index 0000000..63bbac8
--- /dev/null
+++ b/archive/ES_1.1590345050506037
@@ -0,0 +1,22 @@
+archive/ES_1.1590345050506037---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-23T04:33:40.553
+Launch V∞: [7.525563387706056, -0.7429761058491895, -0.13152262334905598] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-7.530416273803435e-6, -6.967747407035961e-6, -5.46412707284009e-6] km/s
+ V∞_out: [6.924110320229209e-9, -6.312457312745243e-9, 2.3526654341416962e-9] km/s
+ time of flight: 1.8749577788209254e8 seconds
+ arrival date: 2030-06-02T06:43:17.553
+ thrust profile: [0.7109882515131377 0.2667918672342272 -0.026066991119891886; 0.0005506931771873764 -0.00031782469779396635 -0.0002777292866988144; 0.17361838390184592 -0.07629240518000807 0.010008194852470561; 0.38317289838441665 -0.21335183749232972 0.037745796604078; 0.5535712904238032 -0.3483302660633152 0.06563932739230627; 0.5943015724765771 -0.4295322516803339 0.08117031112690858; 0.5157524621445834 -0.4789263146173608 0.0868972376956646; 0.47878615713241107 -0.6681998943690522 0.096328756583152; 0.39941253276237365 -0.8875436667401717 0.10584046912509225; 0.28780021975788356 -1.0 0.08794873403502952; 0.5181416683881607 -1.0 0.045268031718267564; 1.0 -1.0 -0.2908815787486582; 1.0 1.0 -0.14470875532060906; 0.9628497761813349 1.0 -0.08507691112000727; 0.6718145296784159 0.9683708264191138 -0.05653078556967918; 0.36454350305902095 0.5970177208653777 -0.0279534803805373; 0.0029290150178636416 0.005274644756956232 -0.0005731589126927769; 0.005202548254201262 0.0007717426970586481 0.007348711496535154; -0.0038415581831396555 -0.0011099510503362444 -0.006537203530431032; -0.004933423762420623 -0.004694702414351584 0.007686391600078687] %
+
+Mass Used: 1018.5203292449701 kg
+Launch C3: 57.20341599669728 km²/s²
+||V∞_in||: 1.1623827160327358e-5 km/s
diff --git a/archive/ES_1.8019411464307387 b/archive/ES_1.8019411464307387
new file mode 100644
index 0000000..5b262b6
--- /dev/null
+++ b/archive/ES_1.8019411464307387
@@ -0,0 +1,22 @@
+archive/ES_1.8019411464307387---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-03-21T16:46:01.450
+Launch V∞: [9.58656184545047, -3.970937169707667, 2.2063087746538907] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [3.6303953820160487e-6, -0.00023853624892790178, -4.178248371415312e-6] km/s
+ V∞_out: [-0.00022366317941333277, 3.3931931633146954e-5, -5.259478273676722e-5] km/s
+ time of flight: 1.874957778810701e8 seconds
+ arrival date: 2030-02-28T18:55:38.450
+ thrust profile: [0.8402152736723273 -0.2691465875016191 -0.051376898789932464; 0.8260983236486968 0.6274716097728676 0.0604898877854466; 0.8096946258627372 0.6297857774248286 0.10431390343765866; 0.840846116974009 0.3992699151287581 0.07729078662824075; 0.8634105774350551 0.12174968062600099 0.09717565222506726; 0.8581567074976978 0.02264269016479872 0.09431742567924492; 0.827267087668885 -0.5119322420274552 0.10000296623403016; 0.7336156578060631 -0.7868028288743042 0.0656798470276993; 0.5157024811482248 -0.8880530682492028 0.05009160261235823; 0.445328141100846 -0.9542008185700589 0.08888443983391493; 0.9704964740606297 -0.958713862483643 -0.006032213505754519; 0.9439720683009278 0.9523064245570626 -0.17105490425415132; 0.9074332073163462 0.9288172875357916 -0.07713635722793118; 0.8663255936770708 0.06319609750396514 0.10261595976772894; 0.373061236716911 0.16527228836583324 0.22700787202283618; 0.8684331726664528 0.8804772915523542 -0.02570976814762694; 0.7252888497461953 0.8499784091749091 -0.011832978706627076; 0.5194476430411283 0.7815326545806969 0.0024255093126412594; 0.29239675001367055 0.628796684312392 -0.006225365913084095; 0.10458348166315978 0.22815559743849018 0.0006608641105584641] %
+
+Mass Used: 1445.7912049852853 kg
+Launch C3: 112.53830843152741 km²/s²
+||V∞_in||: 0.00023860046014766384 km/s
diff --git a/archive/saturn/ES_2022-04-02T14:30:27.910/mission b/archive/saturn/ES_2022-04-02T14:30:27.910/mission
new file mode 100644
index 0000000..b51fcbf
--- /dev/null
+++ b/archive/saturn/ES_2022-04-02T14:30:27.910/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/ES_2022-04-02T14:30:27.910/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T10:42:53.737
+Launch V∞: [6.471151295328684, -7.370093125495227, 0.1471444087176648] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.0011016712208284018, 0.001193317665709545, 0.0011284459950617813] km/s
+ V∞_out: [-0.0013212882247491697, -0.0006402618783858693, 0.0013249649980667188] km/s
+ time of flight: 1.8586551451242688e8 seconds
+ arrival date: 2029-03-20T16:01:27.737
+ thrust profile: [0.34816593202635143 -0.09016300532970822 -0.11984880840754134; 0.060934867329879086 0.015900377772554663 -0.06439542879673578; 0.05633720205505469 0.028914725747037226 -0.0996495075588441; 0.06330666013244533 0.04409491325404843 -0.15633154563783136; 0.0394194911156743 0.03303344724606148 -0.1252177975024216; 0.03234762325404856 0.03136698447248268 -0.12511375359960542; 0.03154342715128428 0.034121568693792986 -0.1437825111683027; 0.008289385990413433 0.009595068731611724 -0.04427632783857093; 0.002136247718622523 0.001470160769050456 -0.012444247342867514; 0.0018093799205720644 0.002089387539433632 -0.010912883437983656; 0.0002760205068699395 0.0002984621041452654 -0.002059210160487663; 0.0004273343871331427 0.0006087053409058076 -0.003795471399462705; -0.0001799331844267571 0.00012037796986719939 -0.00024659503854662103; 0.00013990951839967919 -0.00029575557397248453 -0.00011257990744582862; -0.000614150557542183 0.0008502168982850079 -0.0003376355670288909; -0.0008804534336335694 -8.269349664778052e-5 -0.000632456517603454; -0.0008316974334143153 0.0003135027300336823 -0.0004726228836000578; 0.0005727975202778207 0.00044876254245158876 -0.0005711028042968798; 3.62608887044046e-5 0.000582228987042213 -0.0015471075290508958; -0.00015234799294315781 -0.00025744481686610667 -2.9842734467018593e-5] %
+
+Mass Used: 93.53064646715393 kg
+Launch C3: 96.21572324252298 km²/s²
+||V∞_in||: 0.001977644278900276 km/s
diff --git a/archive/saturn/ES_2022-04-02T14:30:27.910/plot.html b/archive/saturn/ES_2022-04-02T14:30:27.910/plot.html
new file mode 100644
index 0000000..11050d4
--- /dev/null
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@@ -0,0 +1,30 @@
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diff --git a/archive/saturn/ES_2022-04-02T14:43:26.363/mission b/archive/saturn/ES_2022-04-02T14:43:26.363/mission
new file mode 100644
index 0000000..a16581a
--- /dev/null
+++ b/archive/saturn/ES_2022-04-02T14:43:26.363/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/ES_2022-04-02T14:43:26.363/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:57:56.612
+Launch V∞: [6.405474755176122, -7.3900240973677365, 0.06380150742647996] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [8.845477174913946e-6, 1.1595633238974296e-6, -2.53958525884217e-8] km/s
+ V∞_out: [-1.7215228302243153e-6, 3.8729325339638874e-8, 8.733327905166755e-6] km/s
+ time of flight: 1.8749577788724747e8 seconds
+ arrival date: 2029-04-08T22:07:33.612
+ thrust profile: [0.3532736189291979 -0.07957696996168889 -0.11573193739758812; 0.0739878629979336 0.02295380224798903 -0.07498400660525116; 0.09168090432856428 0.05432801353413295 -0.15285608888607036; 0.08574086950319204 0.06910585053670845 -0.19999338233636935; 0.0400414422201257 0.03875100333070956 -0.12229237709629778; 0.03258259202158226 0.03713578481743383 -0.12353513268560726; 0.012417336611257972 0.01556828980981476 -0.057033084437855104; 0.0025701620442923167 0.003718201910167825 -0.01419424338655812; 0.004068375950339169 0.006413323665496442 -0.025558683158119714; 0.0010610872645670296 0.0018118064020934408 -0.0073979852498836755; 0.0007915074644420847 0.0014371710977416085 -0.006142894293848515; 0.00011693650669376116 0.00022769271601352848 -0.0003328552699521106; 2.4353713923558043e-5 0.00010628016125793987 -0.0005927137301198118; 0.0001354521898069056 0.00010303580217391736 -0.00039219057300311604; 0.00016523814905179804 -0.00016691610666035386 -0.0002590759639041915; 0.0001266361254982333 0.00015828576308795974 -0.0006156867198432335; 0.00023176672580329702 -5.9645489892740295e-6 7.850577957903819e-5; 0.0010552143660857304 0.0008665606653972042 -0.00030929641961722186; -0.0006290351415415637 -8.118343507894017e-5 0.0010639985232273105; -0.0009023532414626753 -5.706217596898628e-5 0.0012658257422519792] %
+
+Mass Used: 96.5319026649936 kg
+Launch C3: 95.64663363122433 km²/s²
+||V∞_in||: 8.921193782413896e-6 km/s
diff --git a/archive/saturn/ES_2022-04-02T14:43:26.363/plot.html b/archive/saturn/ES_2022-04-02T14:43:26.363/plot.html
new file mode 100644
index 0000000..49f69d9
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@@ -0,0 +1,30 @@
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diff --git a/archive/saturn/ES_2022-04-02T14:59:19.235/mission b/archive/saturn/ES_2022-04-02T14:59:19.235/mission
new file mode 100644
index 0000000..3ed9266
--- /dev/null
+++ b/archive/saturn/ES_2022-04-02T14:59:19.235/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/ES_2022-04-02T14:59:19.235/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T07:57:24.826
+Launch V∞: [8.1332663571246, -5.661986515759155, 0.22766044177874376] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [1.123340652251088e-6, -3.7330513819710547e-6, -1.0846981586769346e-5] km/s
+ V∞_out: [-1.0492432785177735e-5, -1.2239051288617402e-6, 4.687451703815964e-6] km/s
+ time of flight: 1.859737203924726e8 seconds
+ arrival date: 2030-04-05T19:19:24.826
+ thrust profile: [0.22943973812293017 -0.004893967763726286 -0.0801253153441409; 0.03144507004413593 0.016005514878668727 -0.039605355975015175; 0.039054529766301194 0.03197291138034155 -0.08689490156094459; 0.0378685260709824 0.04018324616401574 -0.12252200644008435; 0.02803090143364196 0.03535274273841469 -0.12081216327733243; 0.022471665512052253 0.032497625582222536 -0.12157198448109055; 0.01926878492754949 0.03153169051058213 -0.1281842797483311; 0.004043038254003434 0.0066904694410549765 -0.031175306636595977; 0.005131609501874749 0.009234170160377442 -0.04469930754406368; 0.0003470121363472272 0.0008038663204159477 -0.0038167565883837525; 0.00017609752178919131 0.00036474064628598307 -0.001954724463038849; 1.130336567161233e-5 -3.20909344426444e-5 5.0861087076908916e-5; -1.4439041978965607e-5 6.264510601075898e-5 -3.5503708158925043e-5; 0.00012451312434083361 -0.00034084972505136796 -0.0002481717343390714; -2.1043042384554106e-5 -9.974133023427434e-5 0.00022586203596731763; 3.0325725366321253e-5 6.145296121523383e-5 -0.0003832387995866655; -0.0002927026986088235 0.0007786944928326911 0.00012097830464324579; 8.96770273673005e-6 3.9333968087291074e-5 4.9980603904861806e-5; -1.0699601379404263e-5 -2.0172052201893303e-6 0.000372228156627312; -0.0002084346014800331 0.00032609368117262434 -0.0008865061071454217] %
+
+Mass Used: 74.69249898312728 kg
+Launch C3: 98.25994221732427 km²/s²
+||V∞_in||: 1.152625595695103e-5 km/s
diff --git a/archive/saturn/ES_2022-04-02T14:59:19.235/plot.html b/archive/saturn/ES_2022-04-02T14:59:19.235/plot.html
new file mode 100644
index 0000000..699d24c
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@@ -0,0 +1,30 @@
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diff --git a/archive/saturn/ES_2022-04-02T15:31:02.065/mission b/archive/saturn/ES_2022-04-02T15:31:02.065/mission
new file mode 100644
index 0000000..382e026
--- /dev/null
+++ b/archive/saturn/ES_2022-04-02T15:31:02.065/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/ES_2022-04-02T15:31:02.065/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T00:58:50.661
+Launch V∞: [8.11320959943097, -5.645724124239646, 0.16747696452458005] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [-2.8516363421996975e-10, 4.096121164742909e-9, -2.0697877390789584e-9] km/s
+ V∞_out: [2.0790724859932675e-9, 4.127970936657118e-9, 1.0865120878585403e-10] km/s
+ time of flight: 1.874916083184456e8 seconds
+ arrival date: 2030-04-24T01:58:58.661
+ thrust profile: [0.2754868791323259 -0.004110502019187116 -0.09891196486261492; 0.04324638696098478 0.02247517183605698 -0.05675135816253204; 0.03892904890147251 0.03216852322138361 -0.09100809525201009; 0.03303057370015382 0.035080690423428366 -0.11279234928351167; 0.02181869863261611 0.025269776676374003 -0.09431813772381838; 0.0169559793237119 0.03232455050637029 -0.13374662433915915; 0.016111389795168594 0.023249907977486148 -0.09458558132535513; 0.007205435769196988 0.014290387230894463 -0.07630245560011156; 0.0015616439293485633 0.002593925533434509 -0.014198480084020042; 0.0006398647395756223 0.0011455341196065034 -0.0066362673778835824; 0.00021448383373943162 0.00048461036268397813 -0.0020121857045428612; -0.0005031708667670048 -0.0003846320758830172 -0.0002312837647398825; 4.666007485336052e-5 0.00010280240718190181 -0.000841627809911724; -8.908260282730824e-5 -5.559857473515914e-5 -0.0008097588799996763; 1.4481010457650478e-6 -0.00016875008215481904 -0.0011842708445230653; 8.682995627457883e-5 8.033742269629829e-5 -4.432971042893808e-5; -0.00029798252705925894 0.00034156180315709714 -0.0006198193274259149; -0.0003061369792923545 -3.25929632625721e-5 -0.0007753052016491007; 2.7198081862265237e-5 -0.00015657437876687814 -0.00016057616392290677; -0.0005144350151837572 0.0002711169996963231 0.0005113294575712331] %
+
+Mass Used: 77.59006675738965 kg
+Launch C3: 97.72641942496672 km²/s²
+||V∞_in||: 4.598211410905106e-9 km/s
diff --git a/archive/saturn/ES_2022-04-02T15:31:02.065/plot.html b/archive/saturn/ES_2022-04-02T15:31:02.065/plot.html
new file mode 100644
index 0000000..a8d84e5
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@@ -0,0 +1,30 @@
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diff --git a/archive/saturn/ES_2022-04-02T18:07:41.381/mission b/archive/saturn/ES_2022-04-02T18:07:41.381/mission
new file mode 100644
index 0000000..ed39dfe
--- /dev/null
+++ b/archive/saturn/ES_2022-04-02T18:07:41.381/mission
@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/ES_2022-04-02T18:07:41.381/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T21:35:13.618
+Launch V∞: [8.092028247187812, -5.690394550179761, 0.15870337020149677] km/s
+Phase 1:
+ Planet: Saturn
+ V∞_in: [0.007258340410626599, -0.004915549405160574, -0.0003090327712008995] km/s
+ V∞_out: [0.0063943921161191295, 0.0029021314271309787, -0.005208376883488668] km/s
+ time of flight: 1.8749577773970667e8 seconds
+ arrival date: 2030-04-23T23:44:50.618
+ thrust profile: [0.23623549046119796 0.001523213801416841 -0.0746418855277079; 0.04989778371798442 0.028557974139368027 -0.05866465575542369; 0.035473791749751 0.032507089227488954 -0.0752484296384085; 0.022627986747173957 0.026966919764486865 -0.07156789250913552; 0.04964790396262216 0.0738833298025964 -0.19559483393516622; 0.030631999959579347 0.05365872568512533 -0.15864114884262576; 0.00671793812371244 0.012495789298607023 -0.044004855933096255; 0.006194981641432508 0.01299461151504057 -0.04773667381981179; 0.0013970455272782531 0.0035097621778593085 -0.014148581638031872; 0.0014625087521359605 0.004576093171820035 -0.01812047518926974; 0.0003621287391874434 0.001192919920759847 -0.003924447420406894; 0.0003136102108716024 0.0009510767434047032 -0.003683238027775159; 3.55672194873085e-5 0.0002056947097665128 -0.0009531573613879192; -0.0002219678836028774 0.0002992512020633661 -8.263424581589065e-5; -4.180089723821831e-6 8.500643051220536e-5 2.6176105870720138e-5; 3.966745018590377e-5 5.7559670861396866e-5 -0.0004168195496730593; 0.0002960669240380866 -0.00015608457398720793 9.887024972396908e-6; 2.993253329593611e-5 -0.0001879527007887196 -2.49699959259209e-5; 1.3018003450243295e-5 9.194287517786575e-5 -0.00012566784156294738; -0.0002730423797779337 -0.0001543084966874625 0.0006099289590901544] %
+
+Mass Used: 76.50834802879126 kg
+Launch C3: 97.8866980497143 km²/s²
+||V∞_in||: 0.00877163797273837 km/s
diff --git a/archive/saturn/ES_2022-04-02T18:07:41.381/plot.html b/archive/saturn/ES_2022-04-02T18:07:41.381/plot.html
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diff --git a/archive/EMMJS_2022-02-21T00:09:46.922/mission b/archive/temp/EMMJS_2022-02-21T00:09:46.922/mission
similarity index 100%
rename from archive/EMMJS_2022-02-21T00:09:46.922/mission
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diff --git a/archive/EMMJS_2022-02-21T00:09:46.922/plot.html b/archive/temp/EMMJS_2022-02-21T00:09:46.922/plot.html
similarity index 100%
rename from archive/EMMJS_2022-02-21T00:09:46.922/plot.html
rename to archive/temp/EMMJS_2022-02-21T00:09:46.922/plot.html
diff --git a/archive/EMMJS_2022-02-21T05:29:13.100/mission b/archive/temp/EMMJS_2022-02-21T05:29:13.100/mission
similarity index 100%
rename from archive/EMMJS_2022-02-21T05:29:13.100/mission
rename to archive/temp/EMMJS_2022-02-21T05:29:13.100/mission
diff --git a/archive/EMMJS_2022-02-21T05:29:13.100/plot.html b/archive/temp/EMMJS_2022-02-21T05:29:13.100/plot.html
similarity index 100%
rename from archive/EMMJS_2022-02-21T05:29:13.100/plot.html
rename to archive/temp/EMMJS_2022-02-21T05:29:13.100/plot.html
diff --git a/archive/temp/EMS_2022-03-30T10:29:57.444/mission b/archive/temp/EMS_2022-03-30T10:29:57.444/mission
new file mode 100644
index 0000000..242e9fa
--- /dev/null
+++ b/archive/temp/EMS_2022-03-30T10:29:57.444/mission
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2022-03-30T10:29:57.444/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-07-26T01:19:00.624
+Launch V∞: [2.801105685523002, 3.0115505056548346, 0.24159778742184224] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [3.2638028052648225, 3.7072432967192297, -0.8111829605867894] km/s
+ V∞_out: [0.21900149303391275, 4.961281790968419, -0.625939890484093] km/s
+ time of flight: 6.496921386032952e7 seconds
+ arrival date: 2026-08-17T00:19:13.624
+ thrust profile: [0.001107934241447801 0.0018292007266687126 0.00018565119496341824; -0.0002877684209530748 0.009632735812817879 0.0006406714050849094; -0.0035925789673975825 0.0059022726977168045 0.00036911494627972225; -0.004392271410958318 0.0031496393784072986 8.278924606405449e-5; -0.012079407428345906 0.003283958003507755 -9.305089744052092e-5; -0.015663492755514506 -0.0006101977533498358 -0.0005217677979349034; -0.029609509718733208 -0.00971504175523651 -0.001751767160770895; -0.04705355140306407 -0.030874059949991765 -0.00418091862377451; -0.05338204245020876 -0.05960383790514862 -0.0069506112405576205; -0.045383579040589345 -0.09070049371237078 -0.009483908117466569; -0.022155963117973947 -0.12192130955598213 -0.011451460521380474; 0.02034768398636264 -0.15038741398848862 -0.01256625038597567; 0.08762382671508948 -0.164454623190547 -0.011797458764685229; 0.1749075281973807 -0.14059707594205492 -0.0077920703165491505; 0.2590495954572671 -0.05495769313541083 -0.0002350397416306763; 0.31078395875959064 0.1070497396901885 0.009921413122883931; 0.2315256602857458 0.2917786478366671 0.018335503207980205; 0.04114457125744563 0.356078551965574 0.01876988024197249; -0.1305310921973329 0.33131185148905967 0.014580628212375176; -0.24866263293940324 0.24969498219971523 0.0076663519574371244] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [4.11359354551261e-5, 0.00023511109390414177, -1.3035059541783836e-5] km/s
+ V∞_out: [0.00015465192792359236, -0.00012783566006589105, 0.00012992399487795776] km/s
+ time of flight: 2.516930366642689e8 seconds
+ arrival date: 2034-08-08T03:03:09.624
+ thrust profile: [-0.8184541856940203 0.2442659843524041 -0.004053340354121271; -0.18462760879748796 -0.12954689831551117 0.002015300444404607; -0.018683117374796405 -0.08274850099465172 0.0017810688184995694; 0.18605031572212896 -0.5752577339682567 0.015717634590915026; 0.7899231665527375 -0.831721605721017 0.02629677885724141; 1.0 -0.5024609495919333 0.023603267446363804; 1.0 0.08474233676614021 0.01356986253342746; 1.0 0.7682965866734364 0.0017231700304301538; 0.5800765297826053 0.9025145229862893 -0.012043262027874242; 0.049321884279686014 0.20099767542090913 -0.005729615074688785; -7.198819739380535e-5 2.5490099613361683e-5 8.115187738021953e-7; 0.00010715214961850897 -4.902284353362516e-5 -0.00010380205526740633; 4.5291168568480745e-5 -9.817442721019902e-5 -2.0023042282385832e-5; -0.00010436706033869252 2.1041010802616824e-5 0.00010686288557718574; 4.0651291248531234e-5 1.1722252477788995e-6 -3.811349494694384e-5; 4.8716963058570675e-5 -5.597438718549866e-6 3.23342078594203e-5; -7.451796699985422e-5 1.6611665890359082e-5 9.158000189350461e-5; 2.5080935965254957e-5 3.215621104195173e-5 -4.087712404794397e-5; 1.3855663221283863e-5 -2.730536790197425e-5 4.491673208203398e-6; -1.7292860098192588e-5 0.00017955629586277036 1.0628376982277733e-5] %
+
+Mass Used: 838.6230215492219 kg
+Launch C3: 16.973999000466307 km²/s²
+||V∞_in||: 0.00023903829073984847 km/s
diff --git a/archive/temp/EMS_2022-03-30T10:29:57.444/plot.html b/archive/temp/EMS_2022-03-30T10:29:57.444/plot.html
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diff --git a/archive/temp/EMS_2022-03-31T02:42:47.529/mission b/archive/temp/EMS_2022-03-31T02:42:47.529/mission
new file mode 100644
index 0000000..3a8115a
--- /dev/null
+++ b/archive/temp/EMS_2022-03-31T02:42:47.529/mission
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+/home/connor/projects/thesis/archive/EMS_2022-03-31T02:42:47.529/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-23T06:02:13.164
+Launch V∞: [4.790675190538004, -2.7827628147301513, 2.3322515350749833] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-1.4810007913292704, -3.291455435720552, 2.9831687001217015] km/s
+ V∞_out: [-0.5916884460359885, -2.770372854415817, 3.728441598440503] km/s
+ time of flight: 1.463399999793926e8 seconds
+ arrival date: 2029-01-11T00:02:12.164
+ thrust profile: [0.3803411573668084 -0.24699359911364535 -0.48327553487098146; -0.45637919416245415 0.20259655112804134 -0.4183214076160344; -0.43367448998695834 0.4136614397548196 -0.27973436226784304; -0.5190285617571937 0.29456217917248934 0.127585421435257; -0.5523405717458744 0.26680149330655734 0.3932431972939049; -0.5996656678338447 0.2522039800955279 0.4621499788811929; -0.6304800501642223 0.0890041612002452 0.5223357259424798; -0.6361153588831391 -0.24667340158896864 0.5373571355951733; -0.5825139178259425 -0.389919029978712 0.5093601462685652; -0.5454531372852401 -0.44623500436201025 0.3645214794294788; -0.4801024497934835 0.2102254586306563 0.2565776222052905; -0.579136948771309 -0.13710895068534665 -0.20134408320607608; -0.5188982220935089 -0.42618154892831445 -0.3564433259684089; -0.5230878988602696 -0.4827987429089918 -0.33730666065169657; -0.4547076944063366 -0.17486449212182634 -0.32509286969961976; -0.5648002138742563 0.1946720610839311 0.06983061891210761; -0.620774801689964 0.3715690637443947 0.19453195354416444; -0.634451658470199 0.34548391469755085 0.34375519703180396; -0.6916942031325952 0.12255205006355444 0.4731318096261815; -0.6556954878586314 0.06192414594617366 0.475764756523579] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [0.6126357305264523, 0.036628352063377154, -0.44998341351260274] km/s
+ V∞_out: [-0.40771540308617077, 0.5213716669014113, 0.1788657968644158] km/s
+ time of flight: 1.7526600019051787e8 seconds
+ arrival date: 2034-08-01T13:02:12.164
+ thrust profile: [-0.4584109571736202 0.1135715923073197 0.3475236165861346; 0.28933933320539057 -0.16213518851926365 0.3689204283653291; 0.7767123213868962 -0.30606989550403363 0.2968304361134133; 0.8171230455941187 -0.177050989819005 0.13516760011367504; 0.792566162402287 0.7145286520800527 -0.4309109115263434; 0.7426473957923972 0.8547076140253718 -0.4619343157035517; 0.6131385822232893 0.8703485610178433 -0.37934354880999643; 0.05835968610825082 0.8697084452811487 -0.20558789532136582; -0.013918439576788977 0.8562307293716963 -0.016866144920425347; 0.14989145996688175 0.8391019899698795 0.09255224234844622; 0.18019735809471005 0.8224708378791422 0.16995741266663397; 0.14139412971775753 0.8023864633039065 0.20129093897625455; 0.17968164104668602 0.7805428866365428 0.2139526044756662; 0.08498935350820547 0.7527751665441202 0.19421753791674876; 0.03954352379181277 0.7151788408627606 0.18168198769090368; 0.03303845971086855 0.6728825558974967 0.14690981920697405; 0.02940785938392452 0.6148823095722372 0.10110999555278848; 0.017750178567555636 0.5324957838020801 0.08462070573863552; 0.014357313865460512 0.37335705098385324 0.058909504167600976; 0.00697353943058537 0.10646619320896161 0.016159717939472934] %
+
+Mass Used: 1920.8181793791025 kg
+Launch C3: 36.13373488714083 km²/s²
+||V∞_in||: 0.7610185588597774 km/s
diff --git a/archive/temp/EMS_2022-03-31T02:42:47.529/plot.html b/archive/temp/EMS_2022-03-31T02:42:47.529/plot.html
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diff --git a/archive/temp/EMS_2022-03-31T04:30:39.913/mission b/archive/temp/EMS_2022-03-31T04:30:39.913/mission
new file mode 100644
index 0000000..58362b5
--- /dev/null
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@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2022-03-31T04:30:39.913/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-06-21T16:11:12.531
+Launch V∞: [4.580336710876162, -6.364445263085335, -1.5059609900586743] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [5.6917792297860474, -9.107059519584473, 0.42920737253007657] km/s
+ V∞_out: [3.8594088914119493, -9.999999222371288, 0.7899882429600399] km/s
+ time of flight: 5.002931587226731e7 seconds
+ arrival date: 2025-01-20T17:13:07.531
+ thrust profile: [0.04229136644598212 -0.06399982439053087 -0.013233794183699233; 0.0014932116715965543 -0.004640304886228213 0.0001906966014413458; 0.0033744085280022597 -0.03336977966228066 0.005257073291176034; 0.0012173486808959046 -0.01856084430561746 0.006863306751990301; 0.0013367745067847335 -0.022179557580296334 0.01087995653246621; 0.0036625606619242286 -0.03753302445241814 0.02081824310414169; 0.005693436492274217 -0.04580963409486636 0.029614451707897785; 0.005714572044249225 -0.03497915028431355 0.027438168635040377; 0.003777208567280123 -0.02455099654485904 0.024014082477313365; 0.0017502727856114895 -0.013492983296062076 0.01677139465178059; 0.0014099722203796145 -0.02258436533622781 0.03086001815589659; -0.01711851756208839 -0.038162800905698104 0.06682067973653377; -0.07222108528125802 -0.044777544067508016 0.10793792074870515; -0.14908606147640172 -0.0461559607802597 0.1385554662454927; -0.23264661878032608 -0.05133863711785919 0.1564008191048521; -0.3111436864129761 -0.06543015638494414 0.16185133869771157; -0.3775737086759714 -0.0908253829695217 0.1565721147762051; -0.4298924012671283 -0.128999814797943 0.14270289395075253; -0.4643281358807509 -0.17906953537930623 0.12257663575791145; -0.4706052520449254 -0.22992815837368674 0.09655625247918113] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [-2.246348693769835e-6, 2.3753426785927334e-7, 2.5288257778483175e-6] km/s
+ V∞_out: [-2.516669621821466e-6, -6.463053739261209e-7, 2.0443342168870033e-6] km/s
+ time of flight: 1.9486152593971774e8 seconds
+ arrival date: 2031-03-26T01:25:12.531
+ thrust profile: [-0.17633532461638057 -0.9999797294136397 0.015024325195942026; 0.9999986736375168 -0.9999918362728258 -0.1360686231839698; 0.9999988035500681 0.2439734687302935 -0.11913834595120573; 0.9999986251683992 0.8682898739883735 -0.11093379400311718; 0.9999994614450388 0.9999929666195986 -0.09303791503519601; 0.7673577770891561 0.9999839849865495 -0.06846222282089853; 0.42997221568724037 0.8288852823182677 -0.045830355401957935; 0.18215854580869686 0.4905856393977488 -0.025668582879886326; 0.030437897869578262 0.1150455831440398 -0.0044169993998817375; 0.000807513276163115 0.004402642329890393 -0.0004919165276516808; -2.7745989651617884e-6 0.00012024951636535067 5.147622876497583e-6; 4.877668061774889e-5 0.0002184086121649586 8.498500131050681e-6; 4.132626798573495e-5 8.138845277836206e-5 -3.472982010536854e-5; -6.0757100897981974e-5 0.00012392554025281714 2.6509457699324238e-5; 0.00018725736157467317 6.848523112973848e-5 6.68862906209139e-5; 3.3549665625494406e-5 0.00011153259853957193 -5.104946327333131e-5; -4.4178366374466365e-5 3.558251004156073e-5 -1.1982307674649479e-5; -0.00013762482047567344 1.3746134754174806e-5 -2.093755807885032e-6; 4.771811294273377e-5 4.731274921606212e-5 -1.1671493023451763e-5; 7.19639059100438e-5 -0.00013724663359736313 -3.071142693588584e-5] %
+
+Mass Used: 771.0879580725491 kg
+Launch C3: 63.75356639538772 km²/s²
+||V∞_in||: 3.390791175687325e-6 km/s
diff --git a/archive/temp/EMS_2022-03-31T04:30:39.913/plot.html b/archive/temp/EMS_2022-03-31T04:30:39.913/plot.html
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diff --git a/archive/temp/EMS_2022-04-01T02:57:17.862/mission b/archive/temp/EMS_2022-04-01T02:57:17.862/mission
new file mode 100644
index 0000000..5ff9bdc
--- /dev/null
+++ b/archive/temp/EMS_2022-04-01T02:57:17.862/mission
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2022-04-01T02:57:17.862/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-12-27T01:12:40.730
+Launch V∞: [1.8466699553948345, 1.3678562790010131, -0.0153057964937058] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-3.1633872892711388, 1.766847714739104, 1.5906318484460866] km/s
+ V∞_out: [-2.6570752417451518, -1.5623087854586397, 2.48153623885944] km/s
+ time of flight: 1.3537387772095194e8 seconds
+ arrival date: 2029-04-11T21:03:57.730
+ thrust profile: [0.9929900810043344 0.9999987852496462 -0.10337727636552446; -0.9999989527606722 0.9999992090099894 -0.3047289804175132; -0.9638713659439484 0.0450322438551014 -0.4055337795064804; -0.22495106561402115 0.7848677069324818 0.3831319023782979; -0.7738893421351393 0.9999990172621287 0.39494769205095726; -0.990946731002965 0.8417897053927665 -0.3815221486365675; -0.9734982361035388 0.7893313668448306 -0.2704704369660258; -0.38723803350107505 0.9976585911266805 0.3624717872401706; -0.6369591805380839 0.9888790443583878 0.2130500370042681; -0.9999988687936101 0.9999990044599046 -0.3329147869188805; -0.5789162319974664 0.1999123448513483 0.028083803862645515; 0.7985291692991425 0.7881953295377477 0.17388971281195142; 0.988850032987504 0.9999996591217118 -0.5009694317683372; -0.9999994842664317 -0.3956604351616602 0.20708177708047873; -0.4450447334188467 -0.9872965011676511 0.25277979453414506; 0.9999992382496556 -0.2261999230664443 0.0610408161667454; 0.9999995915291495 0.9999997964336237 -0.5276666165499095; -0.9999998232725931 0.9999996435539122 -0.2721356921234991; -0.9999996876222519 -0.99999900073252 0.10007758955670606; -0.4315629068159034 -0.9999994920612009 0.07571074821215397] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [1.327202961748595, -0.2335174765716992, 0.19517799010581816] km/s
+ V∞_out: [-0.10390899330694657, 0.5823202662968701, -1.2235226316464973] km/s
+ time of flight: 1.315170240574828e8 seconds
+ arrival date: 2033-06-12T01:34:21.730
+ thrust profile: [0.9999991434090886 -0.9999989109820826 -0.18840484920575698; 0.999999642574456 -0.7892776436332918 -0.12931408694138657; 0.9999997178412163 0.5267393788441906 -0.06956780561709845; 0.9999997101961674 0.9999994336962261 -0.018610639490947056; 0.9999995326675502 0.9999996674548184 0.04055505772364419; 0.9999985272401802 0.9999997166093685 0.0964843343858098; 0.5108611241098074 0.9999996665528476 0.11541241396889583; 0.11915209802429379 0.9999995788468198 0.1254892030062545; -0.06577608027600101 0.9999995097151354 0.1358163701800956; -0.15786944384121993 0.9999996754541017 0.1375960485939181; -0.19165177643017128 0.9999893885682953 0.12875243461837188; -0.1283595672922781 0.6138567630147376 0.07671724293817712; -0.012317449010467607 0.047087977571726294 0.006452581509892722; -6.34335149466746e-5 0.00091471809306928 8.53716230858717e-5; -0.0002753957972021203 0.0008379366569403406 0.000253847549893273; -0.00012249698733454806 0.000620864691591944 0.0001747719954028129; -0.0007703906582188425 0.00036864647470518063 -0.00026313495806057455; -0.0003679676279671012 0.000462432306598997 -0.0005969365300740931; 0.00010307940670236174 6.503004811360405e-5 0.00016002455788454703; 5.626567684290205e-5 0.00028538089451470705 0.0003865580217838497] %
+
+Mass Used: 2051.6186645766516 kg
+Launch C3: 5.281454991566764 km²/s²
+||V∞_in||: 1.3616506752322357 km/s
diff --git a/archive/temp/EMS_2022-04-01T02:57:17.862/plot.html b/archive/temp/EMS_2022-04-01T02:57:17.862/plot.html
new file mode 100644
index 0000000..cf2fa95
--- /dev/null
+++ b/archive/temp/EMS_2022-04-01T02:57:17.862/plot.html
@@ -0,0 +1,30 @@
+
+
+
+
+
+
+
+
+
diff --git a/archive/temp/EMS_2022-04-01T06:48:02.635/mission b/archive/temp/EMS_2022-04-01T06:48:02.635/mission
new file mode 100644
index 0000000..53da4bb
--- /dev/null
+++ b/archive/temp/EMS_2022-04-01T06:48:02.635/mission
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2022-04-01T06:48:02.635/mission---------------------------
+
+Spacecraft: mySat
+ dry_mass: 200.0 kg
+ specific impulse: 3200.0 kg/s
+ max_thrust: 0.00025 kN
+ num_thrusters: 1
+ duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-09-20T14:03:44.662
+Launch V∞: [-0.9544125442488793, 4.650055637860991, 0.8829883975591813] km/s
+Phase 1:
+ Planet: Mars
+ V∞_in: [-2.686848874040082, 5.69557833738042, -0.3426867301634786] km/s
+ V∞_out: [-5.006830246285463, 3.8244101442357286, -0.28590492992060296] km/s
+ time of flight: 1.2959473202133252e8 seconds
+ arrival date: 2028-10-29T12:35:56.662
+ thrust profile: [-0.028074398281491695 0.03725829642101633 0.011493562796176157; -0.04057241823105847 -0.0036979634745522238 0.004188100162030408; -0.018576540265103334 -0.016670623079762328 -0.0036538504180610655; -0.00926818068907572 -0.029823872248843347 -0.00788998730301693; 0.0056536273790355335 -0.039471274595512786 -0.015505661293943124; 0.01795773380852956 -0.024832086810877792 -0.012157101567918709; 0.020276654954958836 -0.008918038755765955 -0.0074245383137495295; 0.026868221096269136 0.007263820280035479 -0.004654400052923847; 0.011894893359756988 0.03223774798632351 0.004633535267024402; -0.047141055295386355 0.040019079580037704 0.013364609633569504; -0.04520469085369964 -0.010120922532993988 0.0020777538652468844; -0.024235864777124916 -0.02628842319518715 -0.005178953753261158; -0.020104196631084845 -0.08663986569488229 -0.025957813503050115; 0.04562945777248198 -0.18858114469692783 -0.07388958835417316; 0.1654642046172344 -0.19639566019786459 -0.09899123711104271; 0.20836768567311814 -0.07684473602532182 -0.06621134288112417; 0.17451643722399424 0.054856569336227734 -0.019947666848185868; 0.09171150949789851 0.24766459803783164 0.03479747010758981; -0.23524183946575974 0.2601294101394598 0.07688820773607916; -0.21879974186036938 -0.008020833470565012 0.021595583194403873] %
+Phase 2:
+ Planet: Saturn
+ V∞_in: [2.746703786000276, 2.98969776442552, -1.0550945579969648] km/s
+ V∞_out: [-2.364529965587132, -1.1050142331661583, -3.0819068226828907] km/s
+ time of flight: 2.2586692153285405e8 seconds
+ arrival date: 2035-12-26T17:24:37.662
+ thrust profile: [-0.17155197556204754 -0.12803647772004534 -0.0010987042854903337; -0.0035589134881411667 -0.06490801713537507 0.0007426295065205218; 0.25580929199297914 -0.3791453683925915 0.015541598652070847; 0.9999998062826643 -0.5828839766311769 0.041611387112901736; 0.9999998812648976 -0.13591929443541234 0.04367451973443414; 0.9999999269970672 0.45531454218125245 0.04521667689652659; 0.9999999228048742 0.9999999183342614 0.04613770201743983; 0.840757310010811 0.9999999579385513 0.026030995407658575; 0.11987829006679744 1.0 -0.0008893319442928411; -0.16626331436648592 0.8682210906007626 -0.017523530916658536; -0.010554991808101162 0.026008419906682182 -0.0010654160560760403; -0.00038326527134042613 0.00042430859777888713 0.00034930741189383597; 8.526053802782655e-5 -0.0008985199777937706 0.000160878965697085; -0.0003967771857136998 0.0010341920913412306 -0.0002243904620731941; -0.001455496554504259 -3.155267804676458e-5 0.00028821667601580344; -0.0002685807673767674 0.000826989980715048 -0.0008420052914367241; -0.0007719825562061786 -0.0008609199968383217 -5.4081725930572875e-5; -0.00011547325119660988 0.00024382875164120964 -0.0003906884145274092; 0.0010448953162641168 -0.0012700408455061536 0.001398368665761554; -0.0009243989271800159 -0.0004827763788561335 -0.00016362116690873035] %
+
+Mass Used: 896.7374359341643 kg
+Launch C3: 23.313589250046537 km²/s²
+||V∞_in||: 4.1947465879304335 km/s
diff --git a/archive/temp/EMS_2022-04-01T06:48:02.635/plot.html b/archive/temp/EMS_2022-04-01T06:48:02.635/plot.html
new file mode 100644
index 0000000..a8f696e
--- /dev/null
+++ b/archive/temp/EMS_2022-04-01T06:48:02.635/plot.html
@@ -0,0 +1,30 @@
+
+
+
+
+
+
+
+
+
diff --git a/ingest_mission2.jl b/ingest_mission2.jl
new file mode 100644
index 0000000..9d28b65
--- /dev/null
+++ b/ingest_mission2.jl
@@ -0,0 +1,98 @@
+using Thesis
+using SPICE
+using LinearAlgebra
+using Dates
+using PlotlyJS
+
+try
+ furnsh("../../spice_files/naif0012.tls")
+ furnsh("../../spice_files/de430.bsp")
+catch
+ furnsh("spice_files/naif0012.tls")
+ furnsh("spice_files/de430.bsp")
+end
+
+function cost(m::Union{Mission, Mission_Guess})
+ norm_mass = (m.start_mass - prop(m)[7]) / m.start_mass
+ norm_C3 = ( m.launch_v∞ ⋅ m.launch_v∞ ) / 200.
+ return 3norm_mass + norm_C3
+end
+
+function get_id(m::Mission)
+ letters = "E"
+ for phase in m.phases letters *= phase.planet.name[1] end
+ letters *= " "
+ letters *= cost(m)
+ return letters
+end
+
+missions = Vector{Mission}()
+folders = readdir("/home/connor/projects/thesis/archive/EM_3-29", join=true)
+for folder in folders
+ try
+ push!(missions, ingest(folder * "/mission"))
+ catch e
+ println("Ingestion failure")
+ end
+end
+
+sorted_missions1 = sort(missions, by=cost)
+
+println(get_id.(sorted_missions1[1:5]))
+
+# long, short = improve.(sorted_missions2[1:2], n=7)#, use_cost=true)
+
+# Display Orbit Plot
+# display(Thesis.plot(long,
+# title="Sample Algorithm Result Mission",
+# mode="light",
+# planet_colors=false,
+# phase_colors=["#F00","#F0F","#6AF"],
+# markers=false,
+# camera=((-0.2, -0.3, -0.2),(1.75,-1.75,1.5))));
+
+# Save Orbit Plot
+# savefig(Thesis.plot(short, title="EMS Mission Profile", mode="light", planet_colors=false,
+# phase_colors=["#F00","#F0F","#6AF"], markers=false, legend=false,
+# camera=((-0.2, 0.1, -0.3),(-2.,-2.,1.))),
+# "/home/connor/projects/thesis/LaTeX/fig/EMS_plot.png",
+# width=850, height=400)
+# savefig(Thesis.plot(short, title="EMS Mission Profile", mode="light", planet_colors=false,
+# phase_colors=["#F00","#F0F","#6AF"], markers=false, planets=false, legend=false,
+# camera=((-0.2, 0.1, -0.3),(-2.,-2.,1.))),
+# "/home/connor/projects/thesis/LaTeX/fig/EMS_plot_noplanets.png",
+# width=850, height=400)
+# savefig(Thesis.plot(long, title="EMJS Mission Profile", mode="light", planet_colors=false,
+# phase_colors=["#F00","#F0F","#6AF"], markers=false, legend=false,
+# camera=((-0.2, -0.3, -0.2),(1.75,-1.75,1.5))),
+# "/home/connor/projects/thesis/LaTeX/fig/EMJS_plot.png",
+# width=850, height=400)
+# savefig(Thesis.plot(long, title="EMJS Mission Profile", mode="light", planet_colors=false,
+# phase_colors=["#F00","#F0F","#6AF"], markers=false, planets=false, legend=false,
+# camera=((-0.2, -0.3, -0.2),(2.,-2.,1.5))),
+# "/home/connor/projects/thesis/LaTeX/fig/EMJS_plot_noplanets.png",
+# width=850, height=400)
+# Display Thrust Plots
+# display(plot_thrust(display_mission, title="Thrust Magnitude vs Time", mode="light"))
+# display(plot_thrust_components(display_mission, title="Thrust Components vs Time", mode="light"))
+
+# Save Thrust Plots
+# savefig(plot_thrust(short, title="Thrust Magnitude vs Time", mode="light", legend=false),
+# "/home/connor/projects/thesis/LaTeX/fig/EMS_thrust_mag.png",
+# width=850, height=400)
+# savefig(plot_thrust_components(short, title="Thrust Components vs Time", mode="light", legend=false),
+# "/home/connor/projects/thesis/LaTeX/fig/EMS_thrust_components.png",
+# width=850, height=400)
+# savefig(plot_thrust(long, title="Thrust Magnitude vs Time", mode="light", legend=false),
+# "/home/connor/projects/thesis/LaTeX/fig/EMJS_thrust_mag.png",
+# width=850, height=400)
+# savefig(plot_thrust_components(long, title="Thrust Components vs Time", mode="light", legend=false),
+# "/home/connor/projects/thesis/LaTeX/fig/EMJS_thrust_components.png",
+# width=850, height=400)
+
+# Save Thrust Plots (VNB)
+# display(plot_thrust_components(short, title="Thrust Components vs Time", mode="light", vnb=true))
+# display(plot_thrust_components(long, title="Thrust Components vs Time", mode="light", vnb=true))
+
+# Save mission
+# store(display_mission, "/home/connor/projects/thesis/archive/best/long_mission")
diff --git a/julia/cost_table.jl b/julia/cost_table.jl
new file mode 100644
index 0000000..5138eb7
--- /dev/null
+++ b/julia/cost_table.jl
@@ -0,0 +1,42 @@
+using Thesis
+using SPICE
+using LinearAlgebra
+using Dates
+using PlotlyJS
+
+try
+ furnsh("../../spice_files/naif0012.tls")
+ furnsh("../../spice_files/de430.bsp")
+catch
+ furnsh("spice_files/naif0012.tls")
+ furnsh("spice_files/de430.bsp")
+end
+
+function cost(m::Union{Mission, Mission_Guess})
+ norm_mass = (m.start_mass - prop(m)[7]) / m.start_mass
+ norm_C3 = ( m.launch_v∞ ⋅ m.launch_v∞ ) / 200.
+ return 3norm_mass + norm_C3
+end
+
+function get_id(m::Mission)
+ letters = "E"
+ for phase in m.phases letters *= phase.planet.name[1] end
+ letters *= " "
+ letters *= string(cost(m))
+ return letters
+end
+
+missions = Vector{Mission}()
+folders = readdir("/home/connor/projects/thesis/archive/saturn", join=true)
+for folder in folders
+ try
+ push!(missions, ingest(folder * "/mission"))
+ catch e
+ println("Ingestion failure")
+ end
+end
+
+sorted_missions = sort(missions, by=cost)
+
+@show get_id.(sorted_missions)
+
diff --git a/julia/find_neptune.jl b/julia/find_neptune.jl
index 76b4798..dab4877 100644
--- a/julia/find_neptune.jl
+++ b/julia/find_neptune.jl
@@ -1,9 +1,8 @@
-include("src/Thesis.jl")
-using .Thesis
+using Thesis
using Dates
using SPICE
using LinearAlgebra
-using PlotlyJS: savefig
+using PlotlyJS
try
furnsh("../../spice_files/naif0012.tls")
@@ -25,7 +24,7 @@ function easy_cost(m::Union{Mission, Mission_Guess}, C3::Float64, v∞::Float64)
tof += phase.tof
end
tof = tof/(20Thesis.year)
- return 3norm_mass + norm_C3 + tof
+ return 3norm_mass + norm_C3
end
sc = Sc("mySat", 200., 3200., 0.00025, 1, 1.0)
@@ -47,22 +46,25 @@ Thesis.mbh(fbs) = mbh(fbs,
max_v∞,
latest_arrival,
easy_cost,
- search_patience=10_000,
- drill_patience=200,
- verbose=true)
+ search_patience=200,
+ drill_patience=50,
+ verbose=true,
+ )
-function log(m::Mission, archive::Vector{Mission}, planets::Vector{Body})
+function log(archive::Vector{Mission}, planets::Vector{Body})
abbrev = join([ planet.name[1] for planet in planets ])
- p = plot(m, title="Best $(abbrev) Trajectory")
- savefig(p,"archive/$(abbrev).html")
- store(m, "archive/$(abbrev)")
- store(archive, "archive/$(abbrev)_archive")
+ println(length(archive))
+ for m in archive
+ println(abbrev)
+ store(m, "archive/$(abbrev)_$(easy_cost(m, 200., 200.))")
+ end
end
log(_::Nothing, _::Vector{Mission}, _::Vector{Body}) = println("No Mission Found...")
-planets = [Earth, Mars, Mars, Jupiter, Saturn]
-best, archive = mbh(planets)
-log(best, archive, planets)
-
-println("Complete!")
+planets = [Earth, Saturn]
+latest_arrival = ideal_launch + Year(5)
+best, archive, missions = mbh(planets)
+log(missions, planets)
+p = scatter(;x=1:length(missions), y=easy_cost.(missions, 200., 200.), mode="markers")
+PlotlyJS.plot(p)
diff --git a/julia/ingest_mbh.jl b/julia/ingest_mbh.jl
new file mode 100644
index 0000000..2d78c6d
--- /dev/null
+++ b/julia/ingest_mbh.jl
@@ -0,0 +1,52 @@
+using Thesis
+using SPICE
+using LinearAlgebra
+using Dates
+using PlotlyJS
+
+try
+ furnsh("../../spice_files/naif0012.tls")
+ furnsh("../../spice_files/de430.bsp")
+catch
+ furnsh("spice_files/naif0012.tls")
+ furnsh("spice_files/de430.bsp")
+end
+
+function cost(m::Union{Mission, Mission_Guess})
+ norm_mass = (m.start_mass - prop(m)[7]) / m.start_mass
+ norm_C3 = ( m.launch_v∞ ⋅ m.launch_v∞ ) / 200.
+ return 3norm_mass + norm_C3
+end
+
+files = Vector{String}()
+contents = readdir("/home/connor/projects/thesis/archive", join=true)
+for item in contents
+ if item[1:39] == "/home/connor/projects/thesis/archive/ES"
+ push!(files, item)
+ end
+end
+
+sort!(files, by=x->stat(x).ctime)
+
+missions = Vector{Mission}()
+for file in files push!(missions, ingest(file)) end
+
+best_cost = Vector{Float64}()
+global current_min = cost(missions[1])
+for mission in missions
+ if cost(mission) < current_min global current_min = cost(mission) end
+ push!(best_cost, current_min)
+end
+
+p_dots = scatter(;y = cost.(missions), mode="markers")
+p_best = scatter(;y = best_cost)
+layout = Layout(;showlegend=false,
+ title=attr(
+ font_color="rgb(0,0,0)",
+ yanchor="top",
+ y=0.95,
+ text="Cost Functions Values of Single MBH run for Earth-Saturn Trajectory"
+ ),
+ yaxis_title = "Cost Function Value",
+ )
+display(PlotlyJS.plot([p_dots, p_best], layout))
diff --git a/julia/ingest_mission.jl b/julia/ingest_mission.jl
index ed55f0d..b0e696a 100644
--- a/julia/ingest_mission.jl
+++ b/julia/ingest_mission.jl
@@ -16,14 +16,14 @@ function cost_1(m::Union{Mission, Mission_Guess})
norm_mass = (m.start_mass - prop(m)[7]) / m.start_mass
norm_C3 = ( m.launch_v∞ ⋅ m.launch_v∞ ) / 200.
tof = sum([p.tof for p in m.phases])/(20Thesis.year)
- return 2norm_mass + norm_C3 + tof
+ return 3norm_mass + norm_C3 + tof
end
function cost_2(m::Union{Mission, Mission_Guess})
norm_mass = (m.start_mass - prop(m)[7]) / m.start_mass
norm_C3 = ( m.launch_v∞ ⋅ m.launch_v∞ ) / 200.
tof = sum([p.tof for p in m.phases])/(20Thesis.year)
- return 2norm_mass + norm_C3# + tof
+ return 3norm_mass + norm_C3# + tof
end
function get_id(m::Mission)
@@ -74,16 +74,16 @@ println(get_id.(sorted_missions2[1:5]))
# camera=((-0.2, 0.1, -0.3),(-2.,-2.,1.))),
# "/home/connor/projects/thesis/LaTeX/fig/EMS_plot_noplanets.png",
# width=850, height=400)
-savefig(Thesis.plot(long, title="EMJS Mission Profile", mode="light", planet_colors=false,
- phase_colors=["#F00","#F0F","#6AF"], markers=false, legend=false,
- camera=((-0.2, -0.3, -0.2),(1.75,-1.75,1.5))),
- "/home/connor/projects/thesis/LaTeX/fig/EMJS_plot.png",
- width=850, height=400)
-savefig(Thesis.plot(long, title="EMJS Mission Profile", mode="light", planet_colors=false,
- phase_colors=["#F00","#F0F","#6AF"], markers=false, planets=false, legend=false,
- camera=((-0.2, -0.3, -0.2),(2.,-2.,1.5))),
- "/home/connor/projects/thesis/LaTeX/fig/EMJS_plot_noplanets.png",
- width=850, height=400)
+# savefig(Thesis.plot(long, title="EMJS Mission Profile", mode="light", planet_colors=false,
+# phase_colors=["#F00","#F0F","#6AF"], markers=false, legend=false,
+# camera=((-0.2, -0.3, -0.2),(1.75,-1.75,1.5))),
+# "/home/connor/projects/thesis/LaTeX/fig/EMJS_plot.png",
+# width=850, height=400)
+# savefig(Thesis.plot(long, title="EMJS Mission Profile", mode="light", planet_colors=false,
+# phase_colors=["#F00","#F0F","#6AF"], markers=false, planets=false, legend=false,
+# camera=((-0.2, -0.3, -0.2),(2.,-2.,1.5))),
+# "/home/connor/projects/thesis/LaTeX/fig/EMJS_plot_noplanets.png",
+# width=850, height=400)
# Display Thrust Plots
# display(plot_thrust(display_mission, title="Thrust Magnitude vs Time", mode="light"))
# display(plot_thrust_components(display_mission, title="Thrust Components vs Time", mode="light"))
diff --git a/julia/mars_mbh_analysis.jl b/julia/mars_mbh_analysis.jl
new file mode 100644
index 0000000..c05e513
--- /dev/null
+++ b/julia/mars_mbh_analysis.jl
@@ -0,0 +1,61 @@
+using Thesis
+using SPICE
+using LinearAlgebra
+using Dates
+using PlotlyJS
+
+try
+ furnsh("../../spice_files/naif0012.tls")
+ furnsh("../../spice_files/de430.bsp")
+catch
+ furnsh("spice_files/naif0012.tls")
+ furnsh("spice_files/de430.bsp")
+end
+
+function cost(m::Union{Mission, Mission_Guess})
+ norm_mass = (m.start_mass - prop(m)[7]) / m.start_mass
+ norm_C3 = ( m.launch_v∞ ⋅ m.launch_v∞ ) / 200.
+ return 3norm_mass + norm_C3
+end
+
+function get_id(m::Mission)
+ letters = "E"
+ for phase in m.phases letters *= phase.planet.name[1] end
+ letters *= " "
+ letters *= string(cost(m))
+ return letters
+end
+
+missions = Vector{Mission}()
+folders = readdir("/home/connor/projects/thesis/archive/EM_3-29", join=true)
+for folder in folders
+ try
+ push!(missions, ingest(folder * "/mission"))
+ catch e
+ println("Ingestion failure")
+ end
+end
+
+sorted_missions = sort(missions, by=cost)
+
+@show get_id.(missions)
+
+# long, short = improve.(sorted_missions2[1:2], n=7)#, use_cost=true)
+
+best_cost = Vector{Float64}()
+for i in 1:length(missions)
+ push!(best_cost, minimum(cost.(missions[1:i])))
+end
+
+p_dots = scatter(;y = cost.(missions), mode="markers")
+p_best = scatter(;y = best_cost)
+layout = Layout(;showlegend=false,
+ title=attr(
+ font_color="rgb(0,0,0)",
+ yanchor="top",
+ y=0.95,
+ text="Cost Functions Values of Single MBH run for Earth-Mars Trajectory"
+ ),
+ yaxis_title = "Cost Function Value",
+ )
+display(PlotlyJS.plot([p_dots, p_best], layout))
diff --git a/julia/src/mbh.jl b/julia/src/mbh.jl
index e793bc4..f3266c1 100644
--- a/julia/src/mbh.jl
+++ b/julia/src/mbh.jl
@@ -155,13 +155,15 @@ function mbh( flybys::Vector{Body},
search_patience::Int=10_000,
drill_patience::Int=50,
verbose::Bool=false,
- test::Bool=false )
+ test::Bool=false,
+ )
# Convenience Functions
random_guess() = rand_mission_guess(flybys,sc,start_mass,launch_window,max_C3,max_v∞,latest_arrival)
cost(m::Union{Mission,Mission_Guess}) = cost_fn(m, max_C3, max_v∞)
cost(_::Nothing) = Inf
- solve(g::Mission_Guess) = solve_mission(g, launch_window, latest_arrival, max_C3, max_v∞)
+ solve(g::Mission_Guess) = solve_mission(g, launch_window, latest_arrival, max_C3, max_v∞,
+ use_cost=true, CPU_multiplier=10., print_level=1)
# Initialize stuff
x_current = nothing
@@ -177,6 +179,8 @@ function mbh( flybys::Vector{Body},
print("\rMBH\t$(flyby_abbreviation)\tsearch: $(sct) drill: $(dct) archive: $(lar)\t")
end
+ all_missions = Vector{Mission}()
+
# The main loop
while search_count < search_patience
@@ -187,35 +191,37 @@ function mbh( flybys::Vector{Body},
x_star, x_lambert = solve.(random_guess())
# To improve solution time, we'll try drilling down the lambert's solution first
- if x_lambert.converged
- x_lambert_best = x_lambert
- # If it does converge we check to see if it's better than the current
- if cost(x_lambert) < cost(x_current) x_current = x_lambert end
- while drill_count < drill_patience
- verbose && log()
- # If better than the best, then keep it as current
- if x_lambert.converged && cost(x_lambert) < cost(x_current)
- x_current = x_lambert
- x_lambert_best = x_lambert
- drill_count = 0
- # If better than the best of lambert trajectories so far, keep it as lambert_best
- elseif x_lambert.converged && cost(x_lambert) < cost(x_lambert_best)
- x_lambert_best = x_lambert
- drill_count = 0
- # Otherwise, keep drilling
- else
- drill_count += 1
- end
- end
- drill_count = 0
- if x_current ∉ archive
- push!(archive, x_current)
- record(x_current, flybys)
- end
- end
+ # if x_lambert.converged
+ # x_lambert_best = x_lambert
+ # # If it does converge we check to see if it's better than the current
+ # if cost(x_lambert) < cost(x_current) x_current = x_lambert end
+ # push!(all_missions, x_lambert)
+ # while drill_count < drill_patience
+ # verbose && log()
+ # # If better than the best, then keep it as current
+ # if x_lambert.converged && cost(x_lambert) < cost(x_current)
+ # x_current = x_lambert
+ # x_lambert_best = x_lambert
+ # drill_count = 0
+ # # If better than the best of lambert trajectories so far, keep it as lambert_best
+ # elseif x_lambert.converged && cost(x_lambert) < cost(x_lambert_best)
+ # x_lambert_best = x_lambert
+ # drill_count = 0
+ # # Otherwise, keep drilling
+ # else
+ # drill_count += 1
+ # end
+ # end
+ # drill_count = 0
+ # if x_current ∉ archive
+ # push!(archive, x_current)
+ # record(x_current, flybys)
+ # end
+ # end
# Afterwards, we'll try a completely random guess
if x_star.converged
+ push!(all_missions, x_star)
x_basin = x_star
# If it does converge we check to see if it's better than the current
if cost(x_star) < cost(x_current) x_current = x_star end
@@ -226,14 +232,21 @@ function mbh( flybys::Vector{Body},
x_star = solve(perturb(x_basin))
# If better than the best, then keep it as current
if x_star.converged && cost(x_star) < cost(x_current)
+ println(cost(x_star), '\t', cost(x_basin))
+ push!(all_missions, x_star)
x_current = x_star
x_basin = x_star
drill_count = 0
# If better than the best in this particular basin, keep it as basin
elseif x_star.converged && cost(x_star) < cost(x_basin)
+ println(cost(x_star), '\t', cost(x_basin))
+ push!(all_missions, x_star)
x_basin = x_star
drill_count = 0
# Otherwise, keep drilling
+ elseif x_star.converged
+ push!(all_missions, x_star)
+ drill_count += 1
else
drill_count += 1
end
@@ -254,7 +267,7 @@ function mbh( flybys::Vector{Body},
if verbose println() end
- return x_current, archive
+ return x_current, archive, all_missions
end
diff --git a/julia/src/nlp_solver.jl b/julia/src/nlp_solver.jl
index e225a66..a9dae59 100644
--- a/julia/src/nlp_solver.jl
+++ b/julia/src/nlp_solver.jl
@@ -8,15 +8,16 @@ function constraint_bounds(guess::Mission_Guess)
for phase in guess.phases
state_constraint = [10_000., 10_000., 10_000., 0.02, 0.02, 0.02]
+ state_constraint = zeros(6)
if phase != guess.phases[end]
# Constraints on the final state
- push!(low_constraint, (-1 * state_constraint)... )
+ push!(low_constraint, (state_constraint)... )
push!(high_constraint, state_constraint... )
# Constraints on the v∞ and turning angle
- push!(low_constraint, -0.02, 100.)
- push!(high_constraint, 0.02, 1e7)
+ push!(low_constraint, 0., 100.)
+ push!(high_constraint, 0., Inf)
else
- push!(low_constraint, (-1 * state_constraint[1:3])... )
+ push!(low_constraint, (state_constraint[1:3])... )
push!(high_constraint, state_constraint[1:3]... )
end
end
@@ -39,7 +40,7 @@ function solve_mission( guess::Mission_Guess,
latest_arrival::DateTime,
max_C3::Float64,
max_v∞::Float64;
- tol=1e-4,
+ tol=1e-1,
verbose::Bool=false,
print_level=0,
use_cost=false,
@@ -100,7 +101,7 @@ function solve_mission( guess::Mission_Guess,
g[8*(length(flybys)-1)+5] = max_v∞ - norm(v∞_in)
if use_cost
- return -final[end]
+ return 3*(3500-final[end])/3500 + norm(x[2:4])^2 / 200.
else
return 1.0
end
@@ -108,8 +109,8 @@ function solve_mission( guess::Mission_Guess,
catch e
if isa(e,LaGuerreConway_Error) || isa(e, Mass_Error)
- g .= 1e10
- return 1e10
+ g .= 1e14
+ return 1e14
else
rethrow()
end
@@ -124,7 +125,11 @@ function solve_mission( guess::Mission_Guess,
g_low, g_high = constraint_bounds(guess)
ipopt_options = Dict("tol" => tol,
"acceptable_tol" => 100tol,
+ "constr_viol_tol" => 1e-1,
+ "acceptable_constr_viol_tol" => 1e3,
"max_cpu_time" => CPU_multiplier * length(guess.phases),
+ "expect_infeasible_problem" => "yes",
+ "dual_inf_tol" => 1e3,
"print_level" => print_level)
options = Options(solver=IPOPT(ipopt_options), derivatives=ForwardFD())
diff --git a/temp/presentation.bbl b/temp/presentation.bbl
deleted file mode 100644
index 19a90d2..0000000
--- a/temp/presentation.bbl
+++ /dev/null
@@ -1,13 +0,0 @@
-\begin{thebibliography}{1}
-
-\bibitem{nasa_voyager}
-Voyager - mission overview.
-
-\bibitem{jehnBepi}
-Rüdiger Jehn, Daniel García~Yárnoz, Johannes Schoenmaekers, and Vicente
- Companys.
-\newblock Trajectory design for bepicolombo based on navigation requirements.
-\newblock {\em Journal of Aerospace Engineering, Sciences and Applications},
- 4:1--9, 01 2012.
-
-\end{thebibliography}
diff --git a/temp/presentation.blg b/temp/presentation.blg
deleted file mode 100644
index 685d214..0000000
--- a/temp/presentation.blg
+++ /dev/null
@@ -1,48 +0,0 @@
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diff --git a/temp/presentation.nav b/temp/presentation.nav
deleted file mode 100644
index 395b1df..0000000
--- a/temp/presentation.nav
+++ /dev/null
@@ -1,102 +0,0 @@
-\headcommand {\slideentry {0}{0}{1}{1/1}{}{0}}
-\headcommand {\beamer@framepages {1}{1}}
-\headcommand {\beamer@sectionpages {1}{1}}
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-\headcommand {\sectionentry {1}{Introduction}{2}{Introduction}{0}}
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diff --git a/temp/presentation.snm b/temp/presentation.snm
deleted file mode 100644
index e69de29..0000000
diff --git a/temp/thesis.bbl b/temp/thesis.bbl
deleted file mode 100644
index 56dbacf..0000000
--- a/temp/thesis.bbl
+++ /dev/null
@@ -1,198 +0,0 @@
-\begin{thebibliography}{10}
-
-\bibitem{bate2020fundamentals}
-Roger~R Bate, Donald~D Mueller, Jerry~E White, and William~W Saylor.
-\newblock {\em Fundamentals of astrodynamics}.
-\newblock Courier Dover Publications, 2020.
-
-\bibitem{battin1984elegant}
-Richard~H Battin and Robin~M Vaughan.
-\newblock An elegant lambert algorithm.
-\newblock {\em Journal of Guidance, Control, and Dynamics}, 7(6):662--670,
- 1984.
-
-\bibitem{benkhoff2010bepicolombo}
-Johannes Benkhoff, Jan Van~Casteren, Hajime Hayakawa, Masaki Fujimoto, Harri
- Laakso, Mauro Novara, Paolo Ferri, Helen~R Middleton, and Ruth Ziethe.
-\newblock Bepicolombo—comprehensive exploration of mercury: Mission overview
- and science goals.
-\newblock {\em Planetary and Space Science}, 58(1-2):2--20, 2010.
-
-\bibitem{blanchard1969unified}
-RC~Blanchard and ER~Lancaster.
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