Maybe nearing the final commit

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}
 

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

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

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}

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}

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

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

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

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
+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

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

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] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [0.9582177076847339, -0.19699918957632162, 0.15581630117660553] km/s
+	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

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

archive/EM_3-29/EM_2022-03-29T21:29:32.797/mission

@@ -0,0 +1,22 @@
+/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

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

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

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

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

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

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] %
+
+Mass Used: 114.99761554896395 kg
+Launch C3: 142.2343293621158 km²/s²
+||V∞_in||: 2.2413839807974726e-7 km/s

archive/EM_3-29/EM_2022-03-29T21:49:40.929/mission

@@ -0,0 +1,22 @@
+/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
+Phase 1:
+	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] %
+
+Mass Used: 0.006099916057792143 kg
+Launch C3: 67.88922780796933 km²/s²
+||V∞_in||: 0.14629566608835642 km/s

archive/EM_3-29/EM_2022-03-29T21:51:28.498/mission

@@ -0,0 +1,22 @@
+/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
+Phase 1:
+	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] %
+
+Mass Used: 1.549092758068582e-6 kg
+Launch C3: 31.109155510031766 km²/s²
+||V∞_in||: 0.4194368331281437 km/s

archive/EM_3-29/EM_2022-03-29T21:58:30.321/mission

@@ -0,0 +1,22 @@
+/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
+Phase 1:
+	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

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
+Phase 1:
+	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] %
+
+Mass Used: 2.8080553420295473e-6 kg
+Launch C3: 19.321319746248445 km²/s²
+||V∞_in||: 1.2410205341039189 km/s

archive/EM_3-29/EM_2022-03-29T22:02:40.626/mission

@@ -0,0 +1,22 @@
+/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
+Phase 1:
+	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] %
+
+Mass Used: 0.009526397249373986 kg
+Launch C3: 94.95756319119332 km²/s²
+||V∞_in||: 5.742260421097979 km/s

archive/EM_3-29/EM_2022-03-29T22:11:59.808/mission

@@ -0,0 +1,22 @@
+/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
+Phase 1:
+	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

archive/EM_3-29/EM_2022-03-29T22:26:29.640/mission

@@ -0,0 +1,22 @@
+/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
+Phase 1:
+	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] %
+
+Mass Used: 0.03575572314321107 kg
+Launch C3: 158.21906701525444 km²/s²
+||V∞_in||: 0.0488444001924202 km/s

archive/EM_3-29/EM_2022-03-29T22:29:19.608/mission

@@ -0,0 +1,22 @@
+/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
+Phase 1:
+	Planet: Mars
+	V∞_in: [-1.3206429765527528, 0.04508054081073763, -0.10860236471971149] km/s
+	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] %
+
+Mass Used: 0.04864906937473279 kg
+Launch C3: 22.508472910438055 km²/s²
+||V∞_in||: 1.3258674897215847 km/s

archive/EM_3-29/EM_2022-03-29T22:35:03.801/mission

@@ -0,0 +1,22 @@
+/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

archive/EM_3-29/EM_2022-03-29T22:38:25.802/mission

@@ -0,0 +1,22 @@
+/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] %
+
+Mass Used: 0.17400800233144764 kg
+Launch C3: 21.04290176833857 km²/s²
+||V∞_in||: 0.18628183704988058 km/s

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] %
+
+Mass Used: 7.579702014481882e-6 kg
+Launch C3: 34.82958605340684 km²/s²
+||V∞_in||: 0.8130770396493041 km/s

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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