Additional display functions and section 6 draft done
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@@ -32,3 +32,33 @@
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number={GSFC-E-DAA-TN14154},
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number={GSFC-E-DAA-TN14154},
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year={2014}
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year={2014}
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}
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}
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@misc{cassini,
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title={Cassini Mission Fact Sheet},
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author={NASA Jet Propulsion Laboratory},
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url={https://solarsystem.nasa.gov/missions/cassini/mission/quick-facts/},
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journal={NASA Solar System Exploration},
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year={2018}
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}
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@inproceedings{polk2001performance,
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title={Performance of the NSTAR ion propulsion system on the Deep Space One mission},
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author={Polk, J and Kakuda, R and Anderson, J and Brophy, J and Rawlin, V and Patterson, M and Sovey, J and Hamley, J},
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booktitle={39th Aerospace Sciences Meeting and Exhibit},
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pages={965},
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year={2001}
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}
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@article{stough2021nasa,
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title={NASA’s Space Launch System: Capabilities for Ultra-High C3 Missions},
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author={Stough, Robert W and Robinson, Kimberly F and Holt, James B and Smith, David A and Hitt, W David and Perry, Beverly A},
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year={2021}
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}
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@article{c3capabilities,
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author = {Vardaxis, George and Pitz, Alan and Wie, Bong},
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year = {2022},
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month = {02},
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pages = {},
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title = {AAS 12-128 CONCEPTUAL DESIGN AND ANALYSIS OF PLANETARY DEFENSE TECHNOLOGY (PDT) DEMONSTRATION MISSIONS}
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}
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249
LaTeX/thesis.tex
249
LaTeX/thesis.tex
@@ -955,32 +955,257 @@
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in order to fully traverse all basins.
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in order to fully traverse all basins.
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\chapter{Results Analysis} \label{results}
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\chapter{Results Analysis} \label{results}
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Simply highlight that the algorithm was tested on a sample trajectory to Saturn.
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\section{Sample Trajectory to Saturn}
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The algorithm described in this thesis is quite flexible in its design and could be used as
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Give an overview of the trajectory that was ultimately chosen.
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a tool for a mission designer on a variety of different mission types. However, to consider
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a relatively simple but representative mission design objective, a sample mission to Saturn
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was investigated.
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\subsection{Comparison to Less Optimal Solutions}
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\section{Mission Constraints}
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I should have a number of elite but less-optimal solutions. Honestly, I may write the
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algorithm to keep all of the solutions to provide many points of comparison here.
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\subsection{Cost Function Analysis}
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The sample mission was defined to represent a general case for a near-future low-thrust
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Give some real-world context for the mass-use, time-of-flight, etc.
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trajectory to Saturn. No constraints were placed on the flyby planets, but a number of
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constraints were placed on the algorithm to represent a realistic mission scenario.
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\subsection{Comparison to Impulsive Trajectories}
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The first choice required by the application is one not necessarily designable to the
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I may also remove this section. I could do a quick comparison (using porkchop plots) to
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initial mission designer (though not necessarily fixed in the design either) and is that
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similar impulsive trajectories. Honestly, this is a lot of work for very little gain,
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of the spacecraft parameters. The application accepts as input a spacecraft object
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though, so probably the first place to chop if needed.
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containing: the dry mass of the craft, the fuel mass at launch, the number of onboard
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thrusters, and the specific impulse, maximum thrust and duty cycle of each thruster.
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For this mission, the spacecraft was chosen to have a dry mass of only 200 kilograms for
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a fuel mass of 3300 kilograms. This was chosen in order to have an overall mass roughly
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in the same zone as that of the Cassini spacecraft, which launched with 5712 kilograms
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of total mass, with the fuel accounting for 2978 of those kilograms\cite{cassini}. The
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dry mass of the craft was chosen to be extremely low in order to allow for a variety of
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''successful`` missions in which the craft didn't run out of fuel. That way, the
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delivered dry mass to Saturn could be thought of as a metric of success, without
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discounting mission that may have delivered just under whatever more realistic dry mass
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one might set, in case those missions are in the vicinity of actually valid missions.
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The thruster was chosen to have a specific impulse of 3200 seconds, a maximum thrust of
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250 millinewtons, and a 100\% duty cycle. This puts the thruster roughly in line with
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having an array of three NSTAR ion thrusters, which were used on the Dawn and Deep Space
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1 missions\cite{polk2001performance}.
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Also of relevance to the mission were the maximum $C_3$ at launch and $v_\infty$ at
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arrival values. In order to not exclude the possibility of a non-capture flyby mission,
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it was decided to not include the arrival $v_\infty$ term in the cost function and,
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because of this, the maximum value was set to be extremely high at 500 kilometers per
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second, in order to fully explore the space. In practice, though, the algorithm only
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looks at flybys below 10 kilometers per second in magnitude. The maximum launch $C_3$
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energy was set conservatively to 200 kilometers per second squared. This is upper limit
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is only possible, for the given start mass, using a heavy launch system such as the
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SLS\cite{stough2021nasa} or the comparable SpaceX Starship, though at values below about
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half of this maximum, it begins to become possible to use existing launch solutions.
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Finally, the mission is meant to represent a near future mission. Therefore the launch
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window was set to allow for a launch in any day in 2023 or 2024 and a maximum total time
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of flight of 20 years. This is longer than most typical Saturn missions, but allows for
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some creative trajectories for higher efficiency.
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It should be noted that each of these trajectories was found using an $n$ value of 20 as
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mentioned previously, but in post-processing, the trajectory was refined to utilize a
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slightly higher fidelity model that uses 60 sub-trajectories per orbit. This serves to
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provide better plots for display, higher fidelity analyses, as well as to highlight the
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efficacy of the lower fidelity method. Orbits can be found quickly in the lower fidelity
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model and easily refined later by re-running the NLP solver at a higher $n$ value.
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\subsection{Cost Function}
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Each mission optimization also allows for the definition of a cost function. This
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cost function accepts as inputs all parameters of the mission, the maximum $C_3$ at
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launch and the maximum excess hyperbolic velocity at arrival.
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The cost function used for this mission first generated normalized values for fuel
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usage and launch energy. The fuel usage number is determined by dividing the fuel
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used by the mass at launch and the $C_3$ number is determined by dividing the $C_3$
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at launch by the maximum allowed. These two numbers are then weighted, with the fuel
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usage value getting a weight of three and the launch energy value getting a weight
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of one. The values are summed and returned as the cost value.
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\subsection{Flybys Analyzed}
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Since the algorithm itself makes no decisions on the actual choice of flybys, that
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leaves the mission designer to determine which flyby planets would make good
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potential candidates. A mission designer can then re-run the algorithm for each of
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these flyby plans and determine which optimized trajectories best fit the needs of
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the mission.
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For this particular mission scenario, the following flyby profiles were
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investigated:
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\begin{itemize}
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\item EJS
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\item EMJS
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\item EMMJS
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\item EMS
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\item ES
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\item EVMJS
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\item EVMS
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\item EVVJS
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\end{itemize}
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\section{Faster, Less Efficient Trajectory}
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In order to showcase the flexibility of the optimization algorithm (and the chosen cost
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function), two different missions were chosen to highlight. One of these missions is a
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slower, more efficient trajectory more typical of common low-thrust trajectories. The
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other is a faster trajectory, quite close to a natural trajectory, but utilizing more
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launch energy to arrive at the planet.
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It is the faster trajectory that we'll analyze first. Most interesting about this
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particular trajectory is that it's actually quite efficient despite its speed, in
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contrast to the usual dichotomy of low-thrust travel. The cost function used for this
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analysis did not include the time of flight as a component of the overall cost, and yet
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this trajectory still managed to be the lowest cost trajectory of all trajectories found
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by the algorithm.
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The mission begins in late June of 2024 and proceeds first to an initial gravity assist
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with Mars after three and one half years to rendezvous in mid-December 2027.
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Unfortunately, the launch energy required to effectively used the gravity assist with
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Mars at this time is quite high. The $C_3$ value was found to be $60.4102$ kilometers
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per second squared. However, for this phase, the thrusters are almost entirely turned
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off, allowing for a nearly-natural trajectory to Mars rendezvous.
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\begin{figure}
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\centering
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\includegraphics[width=\textwidth]{fig/EMS_plot}
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\caption{Depictions of the faster Earth-Mars-Saturn trajectory found by the
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algorithm to be most efficient; planetary ephemeris arcs are shown during the phase
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in which the spacecraft approached them}
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\label{ems}
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\end{figure}
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\begin{figure}
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\centering
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\includegraphics[width=\textwidth]{fig/EMS_plot_noplanets}
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\caption{Another depiction of the EMS trajectory, without the planetary ephemeris
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arcs}
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\label{ems_nop}
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\end{figure}
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The second and final leg of this trip exits the Mars flyby and, initially burns quite
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heavily along the velocity vector in order to increase it's semi-major axis. After an
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initial period of thrusting, though, the spacecraft effectively coasts with minor
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adjustments until its rendezvous with Saturn just four and a half years later in June of
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2032. The arrival $v_\infty$ is not particularly small, at $5.816058$ kilometers per
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second, but this is to be expected as the arrival excess velocity was not considered as
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a part of the cost function. If capture was not the final intention of the mission, this
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may be of little concern. Otherwise, the low fuel usage of $446.92$ kilograms for a
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$3500$ kilogram launch mass leaves much margin for a large impulsive thrust to enter
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into a capture orbit at Saturn.
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In this case the algorithm effectively realized that a higher-powered launch from
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the Earth, then a natural coasting arc to Mars flyby would provide the spacecraft with
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enough velocity that a short but efficient powered-arc to Saturn was possible with
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effective thrusting. It also determined that the most effective way to achieve this
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flyby was to increase orbital energy in the beginning of the arc, when increasing
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the semi-major axis value is most efficient. All of these concepts are known to skilled
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mission designers, but finding a trajectory that combined all of these concepts would
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have required much time-consuming analysis of porkchop plots and combinations of
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mission-design techniques. This approach is far more automatic than the traditional
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approach.
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The final quality to note with this trajectory is that it shows a tangible benefit of
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the addition of the Lambert's solver in the monotonic basin hopping algorithm. Since the
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initial arc is almost entirely natural, with very little thrust, it is extremely likely
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that the trajectory was found in the Lambert's Solution half of the MBH algorithm
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procedure.
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\section{Slower, More Efficient Trajectory}
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Next we'll analyze the nominally second-best trajectory. While the cost function
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provided to the algorithm can be a useful tool for narrowing down the field of search
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results, it can also be very useful to explore options that may or may not be of similar
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"efficiency" in terms of the cost function, but beneficial for other reasons. By
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outputting many different optimal trajectories, the MBH algorithm can allow for this
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type of mission design flexibility.
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To highlight the flexibility, a second trajectory has been selected, which has nearly
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equal value by the cost function, coming in slightly lower. However, this trajectory
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appears to offer some benefits to the mission designer who would like to capture into
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the gravitational field of Saturn or minimize launch energy requirements, perhaps for a
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smaller mission, at the expense of increased speed.
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The first leg of this three-leg trajectory is quite similar to the first leg of the
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previous trajectory. However, this time the launch energy is considerably lower, with a
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$C_3$ value of only $40.4386$ kilometer per second squared. Rather than employ an almost
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entirely natural coasting arc to Mars, however, this trajectory performs some thrusting
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at about the apoapsis point of its orbit in order to raise the periapsis enough to
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rendezvous at roughly the same incidence angle in Mars' orbit, but one revolution ahead.
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In this case, the launch was a bit earlier, occurring in November of 2023, with the Mars
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flyby occurring in mid-April of 2026. This will prove to be helpful in comparison with
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the other result, as this mission profile is much longer.
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\begin{figure}
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\centering
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\includegraphics[width=\textwidth]{fig/EMJS_plot}
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\caption{Depictions of the slower Earth-Mars-Jupiter-Saturn trajectory found by the
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algorithm to be the second most efficient; planetary ephemeris arcs are shown during
|
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the phase in which the spacecraft approached them}
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\label{emjs}
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\end{figure}
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\begin{figure}
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\centering
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\includegraphics[width=\textwidth]{fig/EMJS_plot_noplanets}
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\caption{Another depiction of the EMJS trajectory, without the planetary ephemeris
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arcs}
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\label{emjs_nop}
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\end{figure}
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The second phase of this trajectory also functions quite similarly to the second phase
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of the previous trajectory. In this case, there is a little bit more thrusting necessary
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simply for steering to the Jupiter flyby than was necessary for Saturn rendezvous in the
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previous trajectory. However, most of this thrusting is for orbit raising in the
|
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beginning of the phase, very similarly to the previous result. In this trajectory, the
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Jupiter flyby occurs late July of 2029.
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Finally, this mission also has a third phase. The Jupiter flyby provides quite a strong
|
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$\Delta V$ for the spacecraft, allowing the following phase to largely be a coasting arc
|
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to Saturn almost one revolution later. Because of this long coasting period, the mission
|
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length increases considerably during this leg, arriving at Saturn in December of 2037,
|
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over 8 years after the Jupiter flyby.
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||||||
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However, there are many advantages to this approach relative to the other trajectory.
|
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While the fuel use is also slightly higher at $530.668$ kilograms, plenty of payload
|
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mass is still capable of delivery into the vicinity of Saturn. Also, it should be noted
|
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|
that the incoming excess hyperbolic velocity at arrival to Saturn is significantly
|
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lower, at only $3.4774$ kilometers per second, meaning that less of the delivered
|
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payload mass would need to be taken up by impulsive thrusters and fuel for Saturn orbit
|
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capture, should the mission designer desire this.
|
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Also, as mentioned before, the launch energy requirements are quite a bit lower. Having
|
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a second mission trajectory capable of launching on a smaller vehicle could be valuable
|
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to a mission designer presenting possibilities. According to an analysis of the Delta IV
|
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and Atlas V launch configurations\cite{c3capabilities} in Figure~\ref{c3}, this
|
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reduction of $C_3$ from around 60 to around 40 brings the sample mission to just within
|
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range of both the Delta IV Heavy and the Atlas V in its largest configuration, neither
|
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of which are possible for the other result, meaning that either different launch
|
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vehicles must be found or mission specifications must change.
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\begin{figure}
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\centering
|
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\includegraphics[width=\textwidth]{fig/c3}
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\caption{Plot of Delta IV and Atlas V launch vehicle capabilities as they relate to
|
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payload mass}
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\label{c3}
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\end{figure}
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\chapter{Conclusion} \label{conclusion}
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\chapter{Conclusion} \label{conclusion}
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\section{Overview of Results}
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\section{Overview of Results}
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Quick re-wording of the previous section in a paragraph or two for reader's convenience.
|
Quick re-wording of the previous section in a paragraph or two for reader's convenience.
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\section{Applications of Algorithm}
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\section{Applications of Algorithm}
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|
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Talk a bit about why this work is valuable. Missions that could have benefited, missions that
|
Talk a bit about why this work is valuable. Missions that could have benefited, missions that
|
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this enables, etc.
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this enables, etc.
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\section{Recommendations for Future Work}\label{improvement_section}
|
\section{Recommendations for Future Work}\label{improvement_section}
|
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|
||||||
Recommend future work, obviously. There are a \emph{ton} of opportunities for improvement
|
Recommend future work, obviously. There are a \emph{ton} of opportunities for improvement
|
||||||
including parallelization, cluster computing, etc.
|
including parallelization, cluster computing, etc.
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29
archive/EJU
29
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@@ -1,29 +0,0 @@
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archive/EJU---------------------------
|
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Spacecraft: mySat
|
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||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
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|
||||||
duty_cycle: 1.0
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|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 1976-08-03T18:07:52.908
|
|
||||||
Launch V∞: [6.299916182319705, 6.240538451377015, -0.9940165103728982] km/s
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|
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Phase 1:
|
|
||||||
Planet: Jupiter
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|
||||||
V∞_in: [4.178807865103526, 3.271316108925791, 0.038831033060078735] km/s
|
|
||||||
V∞_out: [-1.3778027301160083, -5.1110224704243725, -0.38018528529187656] km/s
|
|
||||||
time of flight: 9.076893335112691e7 seconds
|
|
||||||
arrival date: 1979-06-20T07:43:25.908
|
|
||||||
thrust profile: [0.04513213164333234 0.04346394223048948 0.007180644066023622; 0.023711461445665785 0.04851693214299602 0.03207463889343553; 0.00969082323802968 0.0429167126574647 0.05027917371754633; 0.0006490219093697312 0.03432108495203708 0.05302050429400685; -0.003953708767625976 0.02834092045678569 0.05567795776724263; -0.007078446275295329 0.011750260516732298 0.05750557980134808; -0.003435272692576073 0.02122406642664124 0.06262312885175245; -0.009695677074664703 0.018479022813936753 0.06053735694521427; -0.01142145238531702 0.015117586694892556 0.0638000808444341; -0.012068039284864305 0.012122660566706385 0.06391205556608177; -0.012302230314909514 0.010908149372005694 0.06019740157959107; -0.01446161436665235 0.008373928351474595 0.059323058345291314; -0.016583035763738076 0.006299387290095585 0.06082959992214257; -0.01706759812967117 0.0065044105221593 0.05778343872547179; -0.019486845820007016 0.002193974387266614 0.057393172584176734; -0.020473650886052644 1.380648034282904e-5 0.05731896545245807; -0.018767281384997753 -0.001918872534461376 0.05612361619283167; -0.021591450801765708 -0.0042488196125658765 0.05450598919383925; -0.021478255013919884 -0.006464299578735615 0.04809767450620565; -0.022653919145895585 -0.009019740247343862 0.048362756123037046; -0.023544833613709452 -0.011660942116303467 0.04427505897015856; -0.02487650131449469 -0.01482208132042167 0.042971426063402186; -0.025304632579721677 -0.017024463752791045 0.038971334825125444; -0.02627710448532682 -0.01999518763372068 0.036273080926672384; -0.026409220881850253 -0.022340756335864343 0.03346167188312444; -0.027035811169801346 -0.026330622264995978 0.029551995901678153; -0.027294988215502632 -0.028965874411855858 0.026920943329044964; -0.02543100070917406 -0.031206127791626466 0.02244980247094962; -0.027031341088425847 -0.0340466798524574 0.018998557859187092; -0.02741737072358986 -0.03790113735478487 0.01557337910538438; -0.0272602309532185 -0.0408499812859817 0.01194792933774343; -0.025909850501463313 -0.04396390625007793 0.00813014729889798; -0.02506976623031212 -0.047397447305083704 0.004665530910703655; -0.023334361066159846 -0.048678373843736196 0.0009546486525111172; -0.023889478406793792 -0.05679728290807836 -0.002589587233405526; -0.02724340418820601 -0.05816253276542619 -0.006122379800579124; -0.021218565581682256 -0.06185180447607849 -0.009044740289425488; -0.019380826507997755 -0.06887292315771941 -0.013887128275611392; -0.01630947060752653 -0.06863416874846709 -0.01479387901178276; -0.015411951104633738 -0.07135904293057543 -0.01714932934975381] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Uranus
|
|
||||||
V∞_in: [-1.845021665733062, -5.678663565100718, 0.3029957863298556] km/s
|
|
||||||
V∞_out: [-3.909849414959923, 3.5759430497442013, 2.370770023155677] km/s
|
|
||||||
time of flight: 3.08114874485728e8 seconds
|
|
||||||
arrival date: 1989-03-25T11:11:19.908
|
|
||||||
thrust profile: [-0.06674811641031352 -0.05612757204576699 -0.027545219420525784; -0.05559395467233815 -0.05898058463022347 -0.027618778760360937; -0.05692889817706908 -0.06138740735669628 -0.024127884156966553; -0.04938597114969373 -0.05897632826574441 -0.020875930634551777; -0.04513949441889156 -0.05493677886831321 -0.017744255550718353; -0.04191267048560369 -0.0497040919280347 -0.014850616507294535; -0.03951131641179269 -0.04341382786449151 -0.009778820274569259; -0.0370863829866412 -0.03639713660534706 -0.007535292090010591; -0.037410692933588605 -0.03106890983815507 -0.0035126740989491565; -0.035384789101130805 -0.02554445172882075 -0.0017983914198710438; -0.03574977327075396 -0.02113010504624859 -0.0001328491376689744; -0.03194724079988652 -0.01638421067813942 -0.0011505498097668584; -0.034180716278068 -0.013877672988327941 0.001627089350782669; -0.03885278128497657 -0.01161056124179592 0.005447519394925048; -0.04780658577496266 -0.009642777483071765 0.008770370725385047; -0.039523274181837605 -0.00583266582504645 0.010285929551974837; -0.04054425271649562 -0.0030979021814110763 0.013538087528531879; -0.042081635316423546 0.0002896039819797671 0.020386417210395406; -0.04163111462438231 0.003378109131498211 0.018796072247663165; -0.04381682122520203 0.007198467572032381 0.024926690546142397; -0.04521110915147108 0.011920408867649519 0.029020217823105928; -0.047873959213738576 0.01694996877307094 0.029539969915417366; -0.04789681559790685 0.023080413175950897 0.03548445565572181; -0.048968821642495 0.031283457963523637 0.042288153133598176; -0.05513570922771978 0.04188862330873962 0.04315061325522542; -0.0460427824369968 0.05532672923356575 0.052911791351016764; -0.04595007962041501 0.0682098780156651 0.0545332693961846; -0.04020043790691544 0.08884049852098926 0.054905659724033544; -0.03406076232020952 0.11144075206336615 0.05094487923514953; -0.024252121467827105 0.12900503386624168 0.05115224879295048; -0.0176104293681911 0.06260126480105925 0.04470427127414733; -0.008891011397626766 0.1312405594766333 0.03624981025811338; 0.0004454420607871681 0.07329672426875136 0.03146945127603886; 0.0024886701231228332 0.1417457581542488 0.02033654814598019; 0.025071362315817032 0.19698210332984226 0.021196655967815694; 0.0324021609887447 0.15074081889051183 0.0034214591933819246; 0.03632243807074882 0.15207933955719707 -0.002120489459561229; 0.039403691731321876 0.155368573708892 -0.007770585754213655; 0.044300010743546385 0.1656092696295884 -0.009813911794334952; 0.04940888045966933 0.15430255903950427 -0.013461557013245747] %
|
|
||||||
|
|
||||||
Mass Used: 254.85590261239986 kg
|
|
||||||
Launch C3: 79.62133289026262 km²/s²
|
|
||||||
||V∞_in||: 5.978555952666198 km/s
|
|
||||||
File diff suppressed because one or more lines are too long
@@ -1,94 +0,0 @@
|
|||||||
archive/EJU_archive
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 1976-08-01T17:52:34.221
|
|
||||||
Launch V∞: [7.796110966770354, 4.8982533648856466, 0.17379030255431946] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [3.8433311299973627, 5.796528049238326, -0.2817056847145128] km/s
|
|
||||||
V∞_out: [-1.50322449690382, -5.857435376892681, 3.4467617942706994] km/s
|
|
||||||
time of flight: 6.162384733838075e7 seconds
|
|
||||||
arrival date: 1978-07-15T23:36:41.221
|
|
||||||
thrust profile: [0.05076636324847266 0.044371172883747347 -0.000466591620230539; 0.04556839732559172 0.04551590000211736 0.026305580765275827; 0.04271388990028329 0.042965827861916495 0.032904618961254566; 0.04125704453812768 0.04399260927643073 0.011906508964846164; 0.037771810990335594 0.045126058811728244 0.017892630651311324; 0.03744914320857412 0.012083627702152488 0.016408253290893425; 0.037727702899229075 0.010853738248166893 0.015148025588847367; 0.005572973923857532 0.007303529249390285 0.011121028124084267; 0.00617297452148193 0.006145429794742058 0.011859116648542195; 0.005049233699504967 0.006452625990674288 0.011772625897474782; 0.004910258402799322 0.006366537658928831 0.0005643550152455212; 0.0025763592102966957 0.003181565085352132 0.010814482610218074; 0.0031947900522401847 0.0029830417754423276 0.011402488845003961; 0.0021986537890138565 0.0021185618970616647 0.011240126352455571; 0.0021605135862789084 0.0017022912732015678 0.011004028173214985; 0.0030322536190090267 0.0018820294472968568 0.011718419553167932; 0.0052532630469893085 0.004603904299207542 6.164903056357548e-5; 0.0024841647682658998 0.0010845905123058521 0.011858883503386769; 0.001563071377480838 0.0009462415703080935 0.011862566980378264; 0.005896854767673266 0.0028068208794427836 0.0011202252826535307; 0.002706071173844264 0.0007045991278482543 0.010364875508266558; 0.002614617358353478 0.0005047462925719528 0.011994006654582877; 0.003009332161874683 0.0005393209622101327 0.011846999130271842; 0.0029998210658897548 0.0006178369699748124 0.012638274768914527; 0.0018921149244373176 0.0006649354887339559 0.013988245401282478; 0.002177285891280997 0.0024857023352974046 0.006239009472882834; 0.0032550494781518127 0.0005709372281368296 0.014013879125368014; 0.0005852851857850025 0.0004382277614539412 0.015711382271976822; 0.0025298132080876744 0.0003394549467168767 0.015487289562849919; 0.002191799418810117 0.00044848314545440916 0.01576483894176832; 0.001933556956082662 0.00011480338097624216 0.017096420744044216; -0.0015516961136410024 0.00038972226556059235 0.018475608007619732; 0.0006938723421829548 0.0010956580579377906 0.010341674361039263; 0.0008683982111957906 0.0005679039999949838 0.018589985196626108; -0.00307180125243531 0.0008616727357253755 0.020309851014784653; 0.004028984608490049 0.0001817492649660781 0.012222080913189187; -0.004075416887687787 0.003505507802004826 0.020813135596843394; -0.004602868488561299 0.0017957581680285366 0.02205614447435787; -0.005119072302644164 0.003221591585835638 0.021534843370608594; -0.002774683023403968 0.0016034106418616914 0.008955547166790926] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Uranus
|
|
||||||
V∞_in: [-2.38909099183748, -7.09851362908907, -1.4998494752601301] km/s
|
|
||||||
V∞_out: [-1.7579671813396809, -7.434026773843559, -0.5431781244031681] km/s
|
|
||||||
time of flight: 2.993961596792109e8 seconds
|
|
||||||
arrival date: 1988-01-10T05:12:40.221
|
|
||||||
thrust profile: [-0.07931776222154702 -0.09715466918867674 -0.026833250451506713; -0.09845323400323117 -0.17879388582940878 -0.04291406251121993; -0.08894254596894183 -0.09528460976651616 -0.054982106035208346; -0.06263720199951707 -0.0878116196248785 -0.05530652171544619; -0.06259005068834375 -0.09717952834183764 -0.06095027382199235; -0.06352579562023707 -0.09929139401807714 -0.07234338457248485; -0.0686236352886369 -0.09800849861144206 -0.08974924433995998; -0.05956649938146661 -0.08337006632048641 -0.1038431051473047; -0.04514195618670204 -0.08203823260227076 -0.10463027094106508; -0.06289461841109399 -0.060085191156628553 -0.10341360065396196; -0.05445769738916689 -0.09997930701298721 -0.09742267375781755; -0.05465737582266164 -0.08439167405860351 -0.09062236126374591; -0.04456643405680078 -0.07331795808665253 -0.09712534152461183; -0.06256760664966003 -0.08549758983692145 -0.12946096634923257; -0.06368110337977374 -0.0765333160455192 -0.12651913561849154; -0.06725919417261715 -0.09109284547953912 -0.12659879415802394; -0.07101397374081875 -0.08133483656944987 -0.046459438405158315; -0.04458830131822182 -0.06993359213652593 -0.10588197225202642; -0.043829644333553894 -0.06738613952355148 -0.10326501418112732; -0.043699162486397686 -0.07918563865614574 -0.09726736663887796; -0.041902410201523806 -0.05687746336476786 -0.09287616923343434; -0.05864620968926713 -0.045468494145468066 -0.08859391583215602; -0.03395345407232851 -0.03779592663169973 -0.08190251370577784; -0.032344510507555484 -0.03195310670080453 -0.07502124528522572; -0.02939009106005138 -0.027319895639058837 -0.07205569928293426; -0.02776511176948871 -0.02134845266988061 -0.07682410235978968; -0.025076508726846806 -0.01712782779219315 -0.06241551595889376; -0.023058918248386684 -0.011926231766031933 -0.056745466600086336; -0.02009516515935024 -0.007031029808761148 -0.051230718639702445; -0.011470301871887377 -0.004835200281315476 -0.04666627205144148; -0.008153291863800712 -0.009020456383335974 -0.04383434884087585; -0.0014098997805392169 -0.0026298096598901966 -0.03405966422871517; 0.014283781279323941 0.016279866267866545 -0.03609253084131848; 0.05336200053505927 0.03389800040998884 -0.040619525225581585; 0.06527766464651791 0.050216170197614575 -0.042586118795403936; 0.05723451861797406 0.03384400630020884 -0.03901891375575639; 0.08543313326117905 0.08974239510128046 -0.03621120917366133; 0.0630088316034018 0.15678763151906544 -0.005574987167467689; 0.060329780298105595 0.17485309892272635 0.013906868818896528; 0.0637300324111305 0.18467219733664741 0.016407349987587503] %
|
|
||||||
|
|
||||||
Mass Used: 292.79309729930446 kg
|
|
||||||
Launch C3: 84.80243530207245 km²/s²
|
|
||||||
||V∞_in||: 7.638468430129195 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 1976-07-29T22:56:52.810
|
|
||||||
Launch V∞: [6.949925110063542, 5.51142706678786, 1.1338882248683144] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [3.906881971734985, 4.095747067849015, -0.40798750984197163] km/s
|
|
||||||
V∞_out: [-0.9527557058881729, -3.9759295150204843, -3.9356834360151556] km/s
|
|
||||||
time of flight: 7.564082964432266e7 seconds
|
|
||||||
arrival date: 1978-12-22T10:17:21.810
|
|
||||||
thrust profile: [0.03782916575140308 0.03740282492642642 -0.002576574442432617; 0.02568719536954076 0.06252477749229525 0.01652454606912066; 0.004225260108780641 0.03649507973713675 0.026304939794628213; 0.008514278978805623 0.005632465170283442 0.028766756627515436; 0.0028553869411493105 0.032931024849802475 0.02858849466203496; -0.00011527850331830502 0.037305718745844846 0.035357183754127365; -0.0020666322700494226 0.024839987547461636 0.04207353968844954; -0.0023476551667392757 0.02636000649838633 0.03519093267459137; -0.00833472270885205 0.020312456169983457 0.0354986543813712; -0.00428513003264013 0.019154229466167877 0.03662219548118329; -0.005892176333449648 0.018130402556353894 0.03636728290676028; -0.0042365610235936425 0.017010892842012324 0.03397204406749766; -0.004192371296486345 0.014784967560659735 0.023246181586815014; -0.004293857686960709 0.012931024770742552 0.03466591912622505; -0.0042609577287841555 0.014211942842773839 0.027172019947279497; -0.0036142056237695465 0.010452500777706587 0.04150772724566025; -0.003447004422321682 0.010358097537389374 0.02465859403683769; -0.0035755555454099917 0.00835659637766665 0.036388119539083476; -0.0013460117606815386 0.00782126057923672 0.03504230558583957; -0.003072300092481179 0.007188355933796116 0.03251483120438275; -0.0024662943066748387 -0.0358537525077433 0.02685483253738143; -0.001720854005330441 0.005884381838322623 0.03190085557916671; -0.0017412241063530884 0.007099738915174783 0.02682684424390216; -0.000920278204949286 0.005139980641523795 0.029434809365784742; -0.00033636789795050845 0.0036669219846624888 0.03287519625621116; 0.0007034209115346385 0.003501767722469495 0.028377718012140195; -0.0007434279012791565 0.002702853412641308 0.029244372161310265; 0.004866286278936821 0.0017203531584147828 0.02776349992801729; 0.0027504911079692476 0.001072925117832716 0.025680825527965283; 0.0020997450984179718 0.0009711597092673997 0.02061803880756732; 0.002173038215991327 -0.00014251845859543355 0.02156905284150965; 0.0015369099274299977 -0.0021290236096534283 0.021476611388992387; 0.007050352469994045 0.00016009300506752272 0.019346144543133968; 0.0041221682815360565 -0.0025995892998613556 -0.031065081280392186; 0.0053958554268588735 -0.002792436243787968 0.02051192181733026; 0.004118509542080822 -0.0035923393947791876 0.017414374655108224; 0.007861526059596693 -0.004103181354641067 0.014557072213757004; 0.008625807637409916 -0.005142988456101897 0.012197569085466388; -0.01306453843470772 -0.0038356113866674286 0.008329884768979636; 0.033014456775355874 -0.0045647936883905236 0.006863305832741281] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Uranus
|
|
||||||
V∞_in: [-1.938316171288581, -5.830419960553641, 1.6937892024456043] km/s
|
|
||||||
V∞_out: [-4.518682402723378, 2.8551867184238096, 3.186319031020363] km/s
|
|
||||||
time of flight: 3.5891612134454197e8 seconds
|
|
||||||
arrival date: 1990-05-07T13:12:42.810
|
|
||||||
thrust profile: [-0.16989513619875685 -0.045677025710063386 -0.0030973835740971444; -0.1508597397272606 -0.05019563898711127 0.007204467510610183; -0.13420978791056495 -0.07142943296601216 0.018201689954637466; -0.11163546799447194 -0.08737032165349326 0.02732766258127402; 0.009113825963084335 -0.09585317692473423 0.05084952336647781; -0.09161229803325242 -0.09683650466428367 0.037082924841464006; 0.04125371110299494 -0.07680933686599022 0.0534261294839363; -0.07744796231792149 -0.04149385265133659 0.06712706717876639; -0.08943024907797331 -0.06791680699334988 0.07831568164802666; -0.07909240616228119 -0.06472558109648341 0.07290434329331255; -0.06743929900593662 -0.05897448140563983 0.0741408198271463; -0.07819359845202928 -0.06647016191133999 0.0660436817760916; -0.09613068470236329 -0.059166161100852675 0.08060714904979402; -0.07312572091628138 -0.05693061246215791 0.07436389578550606; -0.027570631599454522 -0.059342090803171155 0.07347329358087554; -0.08317002523720268 -0.061818515844878186 0.041467954236152335; -0.07583390698096582 -0.06567919479648035 0.06873073575145; -0.08204408482821308 -0.06168526249705727 0.017377533255748923; -0.08177518700808466 -0.06338581414826097 0.08609161332719108; -0.06598866513441994 -0.07232579202499327 0.06692776564855539; -0.06347014466905312 -0.06414871849237591 0.07897242421747777; -0.05978263664535798 -0.06933208486458832 0.07722271340402495; -0.042839660913592426 -0.0691467820960932 0.0792489224821808; -0.048220787215069935 -0.06975611644646947 0.08493324999489961; -0.049101088565368545 -0.06513558156977915 0.06154355863275868; -0.05585227084219764 -0.058795508980296285 0.07222729242954258; -0.059679510740878634 -0.05037068555696405 0.08573889901755061; 0.05943101681925227 -0.03346975509652526 0.08296424618848902; -0.002011173439567788 -0.05294783680627407 0.0794657562790766; -0.03132595187332769 -0.04585581870208009 0.06847870733055934; -0.029172177173713672 -0.04911166397541467 0.06900916577586096; -0.03419181581676224 -0.050997881676723304 0.054162115369051175; -0.03952854899176259 -0.036375329108467025 0.04088691066500227; 0.07317701734795691 -0.03019477676470679 0.017070982033922204; -0.03660809431367548 -0.03709092568306137 0.042140497725608; -0.03373273474707058 -0.04779512940475388 0.026504620225648024; -0.04557909599180323 -0.02516006761801134 0.020229804898252192; -0.039048523770669794 -0.02375522303243242 0.01420415637304866; 0.013208543377162343 -0.0032720049019988547 -0.007729033179125844; -0.057959608471409775 0.0007246097139177125 -0.011729486022561447] %
|
|
||||||
|
|
||||||
Mass Used: 324.65554095417156 kg
|
|
||||||
Launch C3: 79.96298985450858 km²/s²
|
|
||||||
||V∞_in||: 6.3733655440922625 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 1976-08-03T18:07:52.908
|
|
||||||
Launch V∞: [6.299916182319705, 6.240538451377015, -0.9940165103728982] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [4.178807865103526, 3.271316108925791, 0.038831033060078735] km/s
|
|
||||||
V∞_out: [-1.3778027301160083, -5.1110224704243725, -0.38018528529187656] km/s
|
|
||||||
time of flight: 9.076893335112691e7 seconds
|
|
||||||
arrival date: 1979-06-20T07:43:25.908
|
|
||||||
thrust profile: [0.04513213164333234 0.04346394223048948 0.007180644066023622; 0.023711461445665785 0.04851693214299602 0.03207463889343553; 0.00969082323802968 0.0429167126574647 0.05027917371754633; 0.0006490219093697312 0.03432108495203708 0.05302050429400685; -0.003953708767625976 0.02834092045678569 0.05567795776724263; -0.007078446275295329 0.011750260516732298 0.05750557980134808; -0.003435272692576073 0.02122406642664124 0.06262312885175245; -0.009695677074664703 0.018479022813936753 0.06053735694521427; -0.01142145238531702 0.015117586694892556 0.0638000808444341; -0.012068039284864305 0.012122660566706385 0.06391205556608177; -0.012302230314909514 0.010908149372005694 0.06019740157959107; -0.01446161436665235 0.008373928351474595 0.059323058345291314; -0.016583035763738076 0.006299387290095585 0.06082959992214257; -0.01706759812967117 0.0065044105221593 0.05778343872547179; -0.019486845820007016 0.002193974387266614 0.057393172584176734; -0.020473650886052644 1.380648034282904e-5 0.05731896545245807; -0.018767281384997753 -0.001918872534461376 0.05612361619283167; -0.021591450801765708 -0.0042488196125658765 0.05450598919383925; -0.021478255013919884 -0.006464299578735615 0.04809767450620565; -0.022653919145895585 -0.009019740247343862 0.048362756123037046; -0.023544833613709452 -0.011660942116303467 0.04427505897015856; -0.02487650131449469 -0.01482208132042167 0.042971426063402186; -0.025304632579721677 -0.017024463752791045 0.038971334825125444; -0.02627710448532682 -0.01999518763372068 0.036273080926672384; -0.026409220881850253 -0.022340756335864343 0.03346167188312444; -0.027035811169801346 -0.026330622264995978 0.029551995901678153; -0.027294988215502632 -0.028965874411855858 0.026920943329044964; -0.02543100070917406 -0.031206127791626466 0.02244980247094962; -0.027031341088425847 -0.0340466798524574 0.018998557859187092; -0.02741737072358986 -0.03790113735478487 0.01557337910538438; -0.0272602309532185 -0.0408499812859817 0.01194792933774343; -0.025909850501463313 -0.04396390625007793 0.00813014729889798; -0.02506976623031212 -0.047397447305083704 0.004665530910703655; -0.023334361066159846 -0.048678373843736196 0.0009546486525111172; -0.023889478406793792 -0.05679728290807836 -0.002589587233405526; -0.02724340418820601 -0.05816253276542619 -0.006122379800579124; -0.021218565581682256 -0.06185180447607849 -0.009044740289425488; -0.019380826507997755 -0.06887292315771941 -0.013887128275611392; -0.01630947060752653 -0.06863416874846709 -0.01479387901178276; -0.015411951104633738 -0.07135904293057543 -0.01714932934975381] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Uranus
|
|
||||||
V∞_in: [-1.845021665733062, -5.678663565100718, 0.3029957863298556] km/s
|
|
||||||
V∞_out: [-3.909849414959923, 3.5759430497442013, 2.370770023155677] km/s
|
|
||||||
time of flight: 3.08114874485728e8 seconds
|
|
||||||
arrival date: 1989-03-25T11:11:19.908
|
|
||||||
thrust profile: [-0.06674811641031352 -0.05612757204576699 -0.027545219420525784; -0.05559395467233815 -0.05898058463022347 -0.027618778760360937; -0.05692889817706908 -0.06138740735669628 -0.024127884156966553; -0.04938597114969373 -0.05897632826574441 -0.020875930634551777; -0.04513949441889156 -0.05493677886831321 -0.017744255550718353; -0.04191267048560369 -0.0497040919280347 -0.014850616507294535; -0.03951131641179269 -0.04341382786449151 -0.009778820274569259; -0.0370863829866412 -0.03639713660534706 -0.007535292090010591; -0.037410692933588605 -0.03106890983815507 -0.0035126740989491565; -0.035384789101130805 -0.02554445172882075 -0.0017983914198710438; -0.03574977327075396 -0.02113010504624859 -0.0001328491376689744; -0.03194724079988652 -0.01638421067813942 -0.0011505498097668584; -0.034180716278068 -0.013877672988327941 0.001627089350782669; -0.03885278128497657 -0.01161056124179592 0.005447519394925048; -0.04780658577496266 -0.009642777483071765 0.008770370725385047; -0.039523274181837605 -0.00583266582504645 0.010285929551974837; -0.04054425271649562 -0.0030979021814110763 0.013538087528531879; -0.042081635316423546 0.0002896039819797671 0.020386417210395406; -0.04163111462438231 0.003378109131498211 0.018796072247663165; -0.04381682122520203 0.007198467572032381 0.024926690546142397; -0.04521110915147108 0.011920408867649519 0.029020217823105928; -0.047873959213738576 0.01694996877307094 0.029539969915417366; -0.04789681559790685 0.023080413175950897 0.03548445565572181; -0.048968821642495 0.031283457963523637 0.042288153133598176; -0.05513570922771978 0.04188862330873962 0.04315061325522542; -0.0460427824369968 0.05532672923356575 0.052911791351016764; -0.04595007962041501 0.0682098780156651 0.0545332693961846; -0.04020043790691544 0.08884049852098926 0.054905659724033544; -0.03406076232020952 0.11144075206336615 0.05094487923514953; -0.024252121467827105 0.12900503386624168 0.05115224879295048; -0.0176104293681911 0.06260126480105925 0.04470427127414733; -0.008891011397626766 0.1312405594766333 0.03624981025811338; 0.0004454420607871681 0.07329672426875136 0.03146945127603886; 0.0024886701231228332 0.1417457581542488 0.02033654814598019; 0.025071362315817032 0.19698210332984226 0.021196655967815694; 0.0324021609887447 0.15074081889051183 0.0034214591933819246; 0.03632243807074882 0.15207933955719707 -0.002120489459561229; 0.039403691731321876 0.155368573708892 -0.007770585754213655; 0.044300010743546385 0.1656092696295884 -0.009813911794334952; 0.04940888045966933 0.15430255903950427 -0.013461557013245747] %
|
|
||||||
|
|
||||||
Mass Used: 254.85590261239986 kg
|
|
||||||
Launch C3: 79.62133289026262 km²/s²
|
|
||||||
||V∞_in||: 5.978555952666198 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
File diff suppressed because one or more lines are too long
@@ -1,191 +0,0 @@
|
|||||||
archive/EMJS_archive
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2024-12-15T22:51:31.653
|
|
||||||
Launch V∞: [1.0265298829626757, -6.097752351134353, 0.6856608803521997] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-0.685353880716249, -3.6396637778190533, -3.2013166230561305] km/s
|
|
||||||
V∞_out: [0.5302103364593528, -0.9765757196202859, -4.767844807662866] km/s
|
|
||||||
time of flight: 9.971640000084461e7 seconds
|
|
||||||
arrival date: 2028-02-13T01:51:31.653
|
|
||||||
thrust profile: [0.13284751649644205 0.9411989426214641 -0.46977683989334873; -0.968547907767294 0.9608251103851381 0.49339267132424175; -0.9787154450158303 -0.8432228864566057 -0.5543030062336614; -0.9458849725429278 -0.9442327236046363 -0.7636886633819076; -0.9667535016847152 -0.7358061408218618 -0.11636279319023346; -0.9820303864106136 0.7930475060706941 0.4962497106503541; -0.971227150319471 -0.986463218458502 0.4632222480421968; -0.9271319319791395 -0.8917240929018778 -0.6101593732712101; -0.9139137651217345 -0.5324029885065178 -0.8083289582144534; -0.9773913889808017 0.991657638900593 -0.4106474876750948; -0.990512335176245 0.7321537085435096 0.6605421761973608; -0.9581179828820583 -0.984882219664571 0.6421847460531694; 0.9803502761290055 -0.9432783942684786 -0.7125092685705092; 0.584101463120002 0.9947933997204838 -0.8808317684328829; -0.993526887524295 0.9941311908456837 -0.7387372801949493; -0.9957384470386984 0.9741994738088207 0.5708597976999408; -0.9915748324180956 -0.9960584321805054 0.8295257560724948; 0.9959387668352474 -0.9942746434271464 0.1695440717133519; 0.9960944736420316 0.8745766502055389 -0.7915289853600778; 0.9903811167032217 0.9961817491550279 -0.9573032378642442] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [2.090864620573387, -3.222147331578074, -2.509087132015622] km/s
|
|
||||||
V∞_out: [-4.488106073949989, -0.5175537490206633, 0.7987014856646427] km/s
|
|
||||||
time of flight: 1.6423199999993336e8 seconds
|
|
||||||
arrival date: 2033-04-27T21:51:30.653
|
|
||||||
thrust profile: [-0.5660855310698739 0.9967906693759188 -0.8209919327744069; -0.994170631248832 0.9947713712108747 0.1448631429571182; -0.9945000494219841 0.9274125399233997 0.4897574376167066; -0.9894742986247569 -0.4507820161619902 0.4166941133651491; -0.9714202588117182 -0.7137518679961032 0.30094666125802183; -0.9405225764860856 -0.7041104481825169 0.1892804023301685; -0.8322614400348775 -0.6078444193505477 0.10175874680514145; -0.5733990958821588 -0.4496883690491375 0.04286046670382909; -0.2872975060978055 -0.27194044695575137 0.01185750904851918; -0.03409685881889757 -0.09226785043335413 0.0007765631982848799; 0.041566915656923824 -0.02743199843891902 0.0012223583050356183; 0.03704247583337095 0.003644238002607764 -0.0017388167642256004; 0.055997436147982374 -0.022254514712059217 -0.007208925051407416; 0.24811520314082097 -0.1362846587264196 -0.02883669922015275; 0.4207497452192147 -0.19686359679762824 -0.03935341240442315; 0.5330387060152292 -0.22897802946531448 -0.04350654265126503; 0.6138159398623063 -0.27334600431296685 -0.042974346394558584; 0.7031513931411775 -0.3631789642405433 -0.03783836908358169; 0.8144978524655395 -0.5249342706264041 -0.03246396629051213; 0.8897103992638571 -0.708341160251077 -0.03341117930579575] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-9.950524772292589, 2.7136858826882397, 0.8437847433534009] km/s
|
|
||||||
V∞_out: [-3.9746513384546427, 3.419068378994426, -0.22492206192340505] km/s
|
|
||||||
time of flight: 2.4062400000004002e8 seconds
|
|
||||||
arrival date: 2040-12-11T21:51:30.653
|
|
||||||
thrust profile: [-0.026861539030662098 0.053037742486198663 -0.03998103891716118; -0.4005257165378705 0.12385064839383274 0.04228749257228828; 0.11316689356297174 -0.5002033317813458 0.0920099903831136; -0.4310529749448192 -0.3737769540652961 -0.16434453658789766; 0.524935339397772 0.326736433374278 -0.011049835879189725; 0.2870548648523757 0.9008250510979924 0.043684490460944636; -0.2578688762031856 0.6811275515417524 0.06979705435650777; -0.16643689458434993 0.44448647933073615 0.03748178826678883; 0.03135747943986613 0.09121026982102139 -0.011021906895529003; 0.2773784563100772 0.21421663651317946 -0.0939720012037749; -0.026321949219467622 -0.002583681933706951 0.0022197546795018445; 0.20252009126605577 0.5859029556414175 -0.10288257122681152; -0.5835246166241774 0.9904709316092567 0.042044833954454276; -0.7362038421319124 -0.20746802611665538 0.26205247161144074; 0.025644898980856885 0.13288887758204784 0.067531572098157; -0.1567362766945195 0.020710809244175152 -0.029197896508943184; -0.35499348849403123 0.09675115246414323 0.0008648920068945578; 0.08552766541451494 0.35786531030916835 -0.019970820204502436; 0.07564615169332112 -0.16796111456618562 -0.022460352690263453; 0.25493279832576426 0.09735303708739874 0.0929229928187175] %
|
|
||||||
|
|
||||||
Mass Used: 3003.684776260021 kg
|
|
||||||
Launch C3: 38.70647817922525 km²/s²
|
|
||||||
||V∞_in||: 10.348381854523241 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2023-11-16T09:01:46.766
|
|
||||||
Launch V∞: [-1.2358227541627522, 0.323049558821953, 2.495135844447432] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-5.492217326783208, -0.7599139192265875, -0.7445133837270346] km/s
|
|
||||||
V∞_out: [-4.404936994877108, -3.4463054890902294, 0.12597397946441688] km/s
|
|
||||||
time of flight: 1.1637720070766585e8 seconds
|
|
||||||
arrival date: 2027-07-25T08:01:46.766
|
|
||||||
thrust profile: [0.01055136636996065 0.5035473835223019 0.2144643592551079; -0.04595477215059715 0.6852423614947899 0.16820399057019442; -0.5895802429453626 0.7197253917092584 0.15157285154237687; -0.7242691347954416 0.6365969821781644 0.18351832934110204; -0.7254557218972608 0.33325583626785743 0.20650030599325478; -0.624534757383007 -0.46380253719846265 0.19914261964212518; 0.06888536686167775 -0.3659727992321626 -0.05660421386154573; 0.41960359345145115 0.5802522947366238 -0.02564875636361316; -0.43557904354293114 0.6848106459808407 0.15045741326417394; -0.5906326245605844 0.626327253137284 0.1907051751516841; -0.6145984992977067 0.6853285910994333 0.24790988830917382; -0.7852172198133732 0.397363217233713 0.22913677229660695; -0.6148113166692493 -0.6180162700085184 -0.1063370011071445; -0.3438743055901661 0.08561279547696703 0.1133320954927072; 0.24423988113626285 0.4984911769229264 0.26361771766972686; 0.6070536708822735 0.7233947175576885 0.2890649522953669; -0.39805774605395056 0.8544543105302159 0.2032769540887175; -0.877234342411992 0.5568182222065088 0.1181949174776601; -0.7848468400087453 -0.7818849886318364 -0.025654657156075657; 0.39491632368805846 -0.7677648336006526 -0.018827493121373502] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [-2.011375822763062, -4.005960504046318, 0.6209700805836994] km/s
|
|
||||||
V∞_out: [-4.246987681230396, 0.16498798356943736, 1.5540119004205253] km/s
|
|
||||||
time of flight: 1.4691600181840378e8 seconds
|
|
||||||
arrival date: 2032-03-20T18:01:47.766
|
|
||||||
thrust profile: [0.681909870255602 -0.5761969653838755 -0.02754846539663112; 0.7118573450786314 0.31247951434638493 0.043677226876746314; 0.5476987320075556 0.6581866365943503 -0.003833400581880826; 0.10725439389134384 0.7294932911664623 -0.034290527364056536; -0.5427655230030919 0.7281280491625349 -0.0299219686998862; -0.7331645357201648 0.661529122002647 -0.022598124369638494; -0.7921492428190279 0.3933778983017051 -0.021082156107776216; -0.7932731599235451 -0.41313404927011227 -0.019757316586946027; -0.7424285866522327 -0.6896359802485261 -0.021540954373280186; -0.6106751913915949 -0.7225982342788454 -0.020163701822483136; -0.37316409906634423 -0.7007771556440968 -0.011208908465949893; -0.1711206238316838 -0.6415857635215466 0.0059500126042923785; -0.08270331405821842 -0.5687506908923067 0.02659262994655598; -0.049372522261264505 -0.49783910816632987 0.048628191706214005; -0.04372663474025917 -0.41699938093001865 0.07363018971956578; -0.05490501770449129 -0.31189423172940106 0.0949294276017952; -0.09260972837599633 -0.2199470543952063 0.05957362145438097; -0.0634254159444419 -0.17400774633467572 0.16341908215231168; -0.05232699030024355 0.08812711882068765 0.1012502462026133; -0.04359653224713776 0.2114603900012656 0.04944539701697088] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-7.936261563870153, 0.192812008719828, 0.7850203435347649] km/s
|
|
||||||
V∞_out: [0.08172234404293398, -0.35122508987936396, 0.006338068922481654] km/s
|
|
||||||
time of flight: 2.9010960004261374e8 seconds
|
|
||||||
arrival date: 2041-05-30T12:01:47.766
|
|
||||||
thrust profile: [-0.1762427833398218 0.018451914856523026 -0.33296833868061293; -0.10855107710674605 0.044463310211183146 -0.33965829997250213; -0.04955955263781527 0.10666486336804054 -0.3343168817737069; -0.14933152742910255 0.1645563456813175 -0.2888802750452695; -0.011372547689235173 -0.39964858425741717 0.1289083844812905; 0.17913823101853307 0.33922366300742973 0.3624022918784145; -0.056147608885838356 0.40536943517001855 0.2345805092442894; -0.11646645449972745 0.37970664664911913 0.13215537014712256; -0.10774775336158972 0.3637144687183163 0.07982907905717164; -0.03689877185389765 0.36730516793108037 0.04229495484147119; 0.08041474785484633 0.3975271403801768 0.011450007794323156; 0.2209067582381832 0.4645747308847809 -0.016359218295681436; 0.29077903309671577 0.5746646081920227 -0.03785392741655643; -0.5440697079277356 0.7004154769551414 -0.02197571950265878; -0.5081898184366466 0.06445088273594297 0.0502311733117999; -0.19802320496526152 -0.07027856584170135 0.014625860167883831; -0.07715652979513347 -0.015846719041313496 0.0076264391612288025; 0.180938962168102 -0.0850580439905663 -0.026509928911235665; 0.28645290190644923 -0.11681132361576753 -0.037935422919142044; 0.4089515815441177 -0.14951729956288723 -0.05914131349793209] %
|
|
||||||
|
|
||||||
Mass Used: 2473.604423137509 kg
|
|
||||||
Launch C3: 7.857321779407867 km²/s²
|
|
||||||
||V∞_in||: 7.977322923176217 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2024-07-22T06:44:51.639
|
|
||||||
Launch V∞: [2.575248384952663, 2.739716813210934, -0.38893905027836745] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [4.32111461530485, 2.7960291205842593, -0.489556914131019] km/s
|
|
||||||
V∞_out: [1.7907908980924474, 4.820115223157361, -0.5379099033537726] km/s
|
|
||||||
time of flight: 6.124238397428751e7 seconds
|
|
||||||
arrival date: 2026-07-01T02:31:14.639
|
|
||||||
thrust profile: [0.02204617368488705 0.06285779065282272 0.012605171575819224; -0.011433803484298078 0.08848061166582002 0.07202092139015609; -0.07959321828350713 0.11796051271483557 0.10864894932433573; -0.16842886185138436 0.10168512037796995 0.12068506836380218; -0.23809792134546726 0.03408694703096996 0.10782537552663919; -0.2712846099916887 -0.05259050616229293 0.07714680434548718; -0.2691701026056171 -0.13114175093946576 0.03494697732427611; -0.2432473375546796 -0.19827411241093662 -0.012549713355480184; -0.19688682555894857 -0.25454624209774884 -0.060002522712937; -0.13420719992703317 -0.31198661132994665 -0.10268341121799718; -0.01782601669889528 -0.3411050774098038 -0.13846230630135042; 0.17407803978077827 -0.3653166442745793 -0.1617162480750069; 0.39405333004023496 -0.35863769585862276 -0.16764222379359453; 0.5881727003228676 -0.2918230276130316 -0.1538361990366852; 0.7349673257433222 -0.12576056403661834 -0.12169301624150872; 0.8068721878811431 0.08212623367867798 -0.06681093685570723; 0.7498334641941427 0.6273302531285769 0.0041442783835015165; 0.48778675631358515 0.768425653968566 0.07684034445879483; 0.03235026516840393 0.7961138086551178 0.1340769950940127; -0.187175909543306 0.725754663622694 0.16344645357600582] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [-2.776889048582584, 0.577121588676522, 0.007961135089457616] km/s
|
|
||||||
V∞_out: [0.7615534564462777, 2.718708568232091, 0.27004925013867337] km/s
|
|
||||||
time of flight: 1.1292109290692344e8 seconds
|
|
||||||
arrival date: 2030-01-28T01:29:26.639
|
|
||||||
thrust profile: [-0.840176369612668 0.976860342718164 0.058196195949256124; -0.8628465472635846 0.7633342124306659 0.1067403299239058; -0.8382024712014463 0.2581297893476549 0.12338258921323142; -0.8025794731065865 -0.1952513411331264 0.12149932865338556; -0.7572209152982607 -0.32000638227817424 0.10891070865997188; -0.7036267077800332 -0.3720841081186767 0.09043232925350977; -0.6463345866299025 -0.4293290426371054 0.06661829901893401; -0.5816014177883754 -0.44981649190131995 0.05067422918383243; -0.47351459443415633 -0.43975356881090427 0.028888383104343048; -0.4446429769285578 -0.4496298163012175 0.016442900362289542; -0.3753382613887226 -0.44043470262281187 0.004400618346128699; -0.3104508002843935 -0.4100796118163795 -0.004420648978465791; -0.2535633130657495 -0.3762527335843237 -0.010222789989029061; -0.12727676625203097 -0.3385883342435648 -0.016879911592349858; -0.17160701300131967 -0.303175547483604 -0.013946042678809141; -0.14486147929059093 -0.25597770208827797 -0.012578650709578849; -0.12478337244188682 -0.2047807012949446 -0.008914893875013217; -0.10754382990114088 -0.15281428358709293 -0.0036295313604368246; -0.08430003348112626 -0.09766774422527713 0.003387978072041825; -0.049542730705205464 -0.025733639517012987 0.003344362241873508] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-1.4245259099537633, 1.4291602238263075, 0.11854473850651923] km/s
|
|
||||||
V∞_out: [-0.6879338015175315, -1.3876319593718838, 0.8808502953774751] km/s
|
|
||||||
time of flight: 3.408146015783399e8 seconds
|
|
||||||
arrival date: 2040-11-15T16:12:47.639
|
|
||||||
thrust profile: [0.0209250957876161 0.07236548568951691 -0.05441358281175795; 0.04271088201266738 0.059837108824994496 -0.04570267674006564; 0.06660112060615696 0.05195757710585663 -0.03370174018627228; 0.07859207469254972 0.05915284312855131 -0.01995033274559411; 0.05470694198510173 0.07831313755730426 -0.010342114841936848; -0.01348106574647589 0.11277794394272658 -0.0034013433219311725; -0.09145707370229726 0.10312222608201255 0.005576461043330823; -0.12850299192302284 0.05752290823836534 0.01577381261339529; -0.13477884086307976 0.013206245882351258 0.018396651241394796; -0.12124443428533518 -0.016003517409004134 0.02309161441900346; -0.10385877836751767 -0.034262782555751645 0.026881849627747586; -0.08713710038230636 -0.04462790000575737 0.02664100559569609; -0.071851222306589 -0.051275998799280825 0.02033038048400631; -0.05351516590047124 -0.05503941535681956 0.024892443243640875; -0.042179454832756653 -0.05447471988772444 0.02020467463443017; -0.03024017392297153 -0.05390626764438977 0.014150662481409669; -0.01972175537440891 -0.05302868663746655 0.005230379873849089; -0.012681981493559499 -0.05225628051430802 -0.0024339834268425693; -0.0044941899601042504 -0.05698931635146416 -0.007176158051852003; 0.009984513981692316 -0.06168319332065979 -0.016333699861465947] %
|
|
||||||
|
|
||||||
Mass Used: 1015.034880811023 kg
|
|
||||||
Launch C3: 14.289226045623414 km²/s²
|
|
||||||
||V∞_in||: 2.021342590587859 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2023-12-14T15:10:10.657
|
|
||||||
Launch V∞: [-5.324790803109733, -2.6773113758857146, 0.3590879071328112] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-7.8280744026110485, -4.482906734167364, -0.5270128091140733] km/s
|
|
||||||
V∞_out: [-8.714629007362692, -2.3006682785347587, -0.6459280917863456] km/s
|
|
||||||
time of flight: 1.4074379597755253e8 seconds
|
|
||||||
arrival date: 2028-05-30T14:40:05.657
|
|
||||||
thrust profile: [-0.09620569960732477 -0.09890174838841997 -0.006304928381722739; 0.01019673300605273 -0.15089658441406675 -0.0021554349727457207; 0.07822408798843489 -0.11071926046790218 0.004988054677396156; 0.09762767912264393 -0.058415019885606094 0.010174486469221193; 0.09596476555630318 -0.005224025746863998 0.004950216517465728; 0.08806191952377797 0.049822770611354 -0.0010597096470122361; 0.052574331589681 0.12454094146924233 0.015095231992096524; -0.04001716917664013 0.21428169922925022 0.018454940281947503; -0.19982535032247195 0.251124726671319 0.015258419491383634; -0.42902456010053436 0.03773585135440942 0.01861953896594965; -0.2620621821264161 -0.3783347111418361 0.004523163861194378; 0.05160537420225073 -0.3786420625260984 -0.011042008482375406; 0.20360488108938318 -0.27582667506971054 -0.012821162414732887; 0.2561047977346709 -0.14853261531425635 -0.005634983638021486; 0.260486703242627 -0.01792491318881055 0.0011583161900218508; 0.23894329094312064 0.10878274252152975 0.0042064519174942515; 0.19707710072889273 0.2344075946499166 0.011104691405835861; 0.13172705128797849 0.35645392804648396 0.01747201373387731; -0.03343397706399435 0.37057486224934993 0.01628713138328902; -0.3349092116148668 0.40830706963065616 0.015783429576975126] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [-5.164409827607087, -2.4015213190761244, 0.3886272138412419] km/s
|
|
||||||
V∞_out: [-0.10084295997962195, 5.705933697922466, -0.1469580047293293] km/s
|
|
||||||
time of flight: 8.148046230775028e7 seconds
|
|
||||||
arrival date: 2030-12-29T16:07:47.657
|
|
||||||
thrust profile: [-0.4843312801347405 0.17832592220013307 0.006256115010001196; -0.5117377393427821 -0.03515133875253644 0.01594069776607602; -0.4802829543105851 -0.22759690897497922 0.023218676108680135; -0.41688069406794315 -0.3255769239533844 0.02846987059703982; -0.3518609568473908 -0.3513841428236102 0.03707709560472825; -0.28197549119514226 -0.35416420109695057 0.04330975091368633; -0.22056035580872335 -0.34012444589770013 0.048672605940703245; -0.17030162641170815 -0.3176042986233552 0.054624244098160656; -0.12962198776772624 -0.29003617152610467 0.0600491991040185; -0.09552548126143237 -0.25742381683081617 0.06663476650221734; -0.06576162258943327 -0.22042535210328865 0.07376790136845905; -0.03794666493372705 -0.18080040001875886 0.07922467457462902; -0.017587190801326653 -0.144409275958737 0.07885131961718507; -0.0005846137879528368 -0.11383597257615993 0.06598144523941014; 0.012437749223779474 -0.08192500429520043 0.050363659542438856; 0.025006348976223614 -0.05271986038900855 0.03688810130605497; 0.03735035082457269 -0.023245071824888237 0.025225516789865676; 0.048771155783688964 0.00930403641764618 0.015175514053442753; 0.056121259671254586 0.03626182021235461 0.007719603871138727; 0.06549848774435021 0.06199167605994548 0.0029712452019925654] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-2.4750372046001954, 4.13041506892929, -0.09291157556920056] km/s
|
|
||||||
V∞_out: [-0.9590001742156767, 0.00014166531615410308, -0.00017399656356734708] km/s
|
|
||||||
time of flight: 2.204227460822756e8 seconds
|
|
||||||
arrival date: 2037-12-23T20:40:13.657
|
|
||||||
thrust profile: [0.1749523615814178 0.02337696203170268 -0.007290082696294586; 0.17710130749974723 0.04583257449906523 -0.00719233870000948; 0.174350248316964 0.07510311268410168 -0.00750473770426303; 0.16444589553075314 0.10998364297019214 -0.007106342278531456; 0.1384257291897476 0.1488418684122407 -0.006173412802780041; 0.08428653747267639 0.1721787470978516 -0.003985402948896598; 0.019687460364805707 0.15515729051991808 -0.0013753294272070818; -0.021656527704037976 0.12042770713394904 0.0001864640450765926; -0.039588280724834786 0.09367324460087394 0.0010034140790897994; -0.04673002735050872 0.07208768567973076 0.0013797248342607789; -0.04399767552371756 0.05335024899625606 0.0015132659877072718; -0.04235029705061875 0.03689185722542479 0.001509047848856101; -0.037623976049185055 0.022006890975873494 0.0010667085694236217; -0.031346917825053985 0.00585591622491494 0.00023425066193087632; -0.0193407989640302 -0.012237196189479828 -0.0032635963200177364; -0.011688504812844338 0.004985875856387392 -0.0034950987669932717; -0.013753919383294908 -0.020294143888963282 0.0018680092927586343; -0.0042296107469379065 -0.03029078043837534 0.002437090971995948; 0.010887719248873684 -0.04459982317696947 0.003041721188427454; 0.02500057674047783 -0.052736469222675816 0.0029604218341606117] %
|
|
||||||
|
|
||||||
Mass Used: 662.0977457761205 kg
|
|
||||||
Launch C3: 35.650337425378076 km²/s²
|
|
||||||
||V∞_in||: 4.816094929158691 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2023-11-08T18:47:22.305
|
|
||||||
Launch V∞: [-4.451427517503081, 4.380713257243984, 0.9509666906856978] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-7.503625705871378, 2.9922534516224317, 0.3970744313528344] km/s
|
|
||||||
V∞_out: [-6.203985495450952, 5.1853077278089845, 0.19685948210225732] km/s
|
|
||||||
time of flight: 7.692258675246356e7 seconds
|
|
||||||
arrival date: 2026-04-17T02:10:28.305
|
|
||||||
thrust profile: [-0.05747333201815444 0.01458857211306159 0.01661972438571343; -0.07640520733942768 -0.0880498378588422 0.009291396823580423; -0.0642351947881695 -0.14583843433809482 -0.01174256444385774; -0.03591836428259514 -0.19097919421877213 -0.030455634296288725; 0.0014696729268849598 -0.21419745388390338 -0.046332000137257384; 0.043321837437152184 -0.23281386608467833 -0.057269006919827066; 0.08487576000339314 -0.23180733654869165 -0.06400789992534636; 0.12836076596832638 -0.2345880635860211 -0.06663468113711396; 0.16914897842720558 -0.2202670166100522 -0.06608715415000553; 0.20331848204335912 -0.19904198276368773 -0.06263191481516477; 0.23625994800571543 -0.18017227778817843 -0.057302223507679384; 0.26476916718248283 -0.15037417766839517 -0.05026099494873699; 0.28150073209231896 -0.11974625587737671 -0.04226763198923683; 0.2911151952723726 -0.08935809631597122 -0.032922957893997004; 0.29662192049119385 -0.05630987736862665 -0.023018382921682446; 0.3163317621362404 -0.01253021176722935 -0.013235490847343547; 0.25582892879782015 0.03994726547045516 -0.0012262871620623078; 0.20630604157449897 0.09278869993819255 0.011047803244751797; 0.13239326442164706 0.18510472327622382 0.022309378373958296; 0.0678407381537921 0.24416553319280734 0.027187329287448894] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [-2.4066983016171593, 3.60782547580802, -0.0729666504902062] km/s
|
|
||||||
V∞_out: [2.378938038105792, 3.622859356538288, -0.17162450321036135] km/s
|
|
||||||
time of flight: 1.0365627669349712e8 seconds
|
|
||||||
arrival date: 2029-07-29T19:35:04.305
|
|
||||||
thrust profile: [-0.08661540144522925 0.5452498417652726 0.01940681405322532; -0.3026836754787113 0.3296518390803253 0.005983402538334351; -0.3406876005629003 0.11833095428025397 0.003356530625833691; -0.2835305485605863 0.05826412825528092 0.02255167620704516; -0.2312925636505238 0.037264277244941184 0.05388961098566991; -0.18711959340793846 0.02248626525242582 0.07873824296078222; -0.1586634246283703 0.009933258699574466 0.0871013968397894; -0.13480225405151802 -0.0016459373751799647 0.08376814481354339; -0.11717491300808694 -0.011644771387652143 0.06591943652720958; -0.12385446642299068 -0.021486105366059834 0.04559099694744897; -0.09388047865743618 -0.028093190404018073 0.021912607207877112; -0.08329274681397837 -0.03442999409177474 0.004671009919336775; -0.074293683492257 -0.039542791582250804 -0.005853738709231158; -0.06633940754759032 -0.044531789384190786 -0.009552210711090501; -0.05819808497253237 -0.047725452096228235 -0.008621886584541672; -0.052136936558275115 -0.0524395749605876 -0.002738982045574738; -0.04346694186008132 -0.0559411143833451 0.005899905372803087; -0.019037945479989642 -0.06356156997525016 0.022900432372144015; 0.03382392128782208 -0.03750155602427737 -0.01509909397132852; 0.0372737888254289 -0.03393228709124474 -0.008856011117644847] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-1.348151617130741, 3.372644961627469, -0.15974064227398158] km/s
|
|
||||||
V∞_out: [0.5003596890905858, 0.5035022711921476, 0.4902757482488732] km/s
|
|
||||||
time of flight: 2.6430663321089447e8 seconds
|
|
||||||
arrival date: 2037-12-13T22:05:37.305
|
|
||||||
thrust profile: [0.09042797681998876 0.08185621600988492 -0.005657240382538273; 0.08801730768503421 0.06654785786786777 -0.005370519173262853; 0.08823193892876004 0.06301303625131692 -0.005301669247083464; 0.09786240449059495 0.0767776838916466 -0.005515040644430515; 0.08471215842112331 0.09323975234752191 -0.004395184816667355; 0.06296777251631458 0.13453925938779707 -0.0025772294050847586; -0.0014186632217062752 0.15454606073890062 0.000798883942976955; -0.06382656189096726 0.14369239243391718 0.004139373253375935; -0.09924285361658083 0.11731937511826053 0.006398669227156636; -0.11580556499542272 0.09241219909488727 0.007641311131976814; -0.12704630471212713 0.0755704468000314 0.008542821687616114; -0.13059068423655953 0.05648447252052886 0.008518267583078705; -0.1375065378923194 0.029657327876499343 0.007947474105719379; -0.12731258715678567 -0.013661649213132244 0.005928368352642089; -0.08615459629776862 -0.051365993070702234 0.003434419522338479; -0.06064751058410859 -0.050519207115431015 0.004480131985829094; -0.004983547686528498 -0.05050727346302307 0.028470779024005587; -0.029138511656783765 -0.04657877128192993 0.022486478212922927; -0.035824958961586245 -0.02656318094078993 -0.022032681036760468; -0.042164309076524915 -0.03952915140222731 -0.007355989451236212] %
|
|
||||||
|
|
||||||
Mass Used: 537.3508733080857 kg
|
|
||||||
Launch C3: 39.91019323257055 km²/s²
|
|
||||||
||V∞_in||: 3.6356242782715444 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
@@ -1,43 +0,0 @@
|
|||||||
archive/EMMJS---------------------------
|
|
||||||
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2023-11-08T16:33:41.148
|
|
||||||
Launch V∞: [-3.7467429728623447, -0.7427414062360022, 1.0452490382459865] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-2.885104439331886, -1.327495046167686, -0.027749058108596784] km/s
|
|
||||||
V∞_out: [-1.635967097498029, -2.7221789573242074, 0.015131202359034032] km/s
|
|
||||||
time of flight: 6.778595425260136e7 seconds
|
|
||||||
arrival date: 2026-01-01T05:59:35.148
|
|
||||||
thrust profile: [-0.05074044407568138 -0.021150582055882192 0.02730812822478398; -0.05363696950139044 -0.06016484582924907 0.04378542458137859; -0.02771035674834004 -0.10645426057233084 0.04017412625773127; 0.01630657360103497 -0.12411195034078264 0.023350505322999197; 0.05888817282501315 -0.10894637011686983 0.0004869417342207616; 0.08706942097452976 -0.07439720218837492 -0.023367157675286705; 0.09495132401480658 -0.035316011414834675 -0.04390702621881143; 0.08752285351021441 -0.004210304140208955 -0.05824943912322043; 0.06832834450779833 0.01653042551161497 -0.06490194085584605; 0.04924860864138059 0.022800133521631457 -0.062427366917489194; 0.03691868046224741 0.011541999666891671 -0.049506900069146154; 0.02451718791619906 0.019175805931995835 -0.026347851368135194; -0.032064249204675696 0.028639492606652335 0.024093899166278167; -0.08306772663523894 -0.03165903417995458 0.04031997576998134; -0.09308798794042389 -0.09539353910087413 0.04749994325844049; -0.02511528438762353 -0.14606890192307997 0.03354911283916682; 0.04310668443858089 -0.14207536740537 0.010418445496805094; 0.09246132545360927 -0.10807413652564378 -0.01547233992587798; 0.11319881808511016 -0.06123358244390861 -0.03864051024951101; 0.11067805251913554 -0.018856574108340608 -0.05612659024233843] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-5.884459586892747, -3.363236848676117, -0.5090555323000778] km/s
|
|
||||||
V∞_out: [-6.754575036027653, -0.6433971508597986, -0.39980914727121014] km/s
|
|
||||||
time of flight: 7.419247222558242e7 seconds
|
|
||||||
arrival date: 2028-05-08T23:00:47.148
|
|
||||||
thrust profile: [0.09654790671377476 -0.02421154193760562 -0.017928801450145315; -0.013697559588275829 0.2078634802144036 -0.1014668129386949; -0.1556430254864518 0.42999351341524117 -0.15436045217579106; -0.34594668129342293 0.5414366154963298 -0.18269379097659816; -0.5454038742991185 0.5440039323636802 -0.17114242041739094; -0.6681265735588777 0.3905344944333295 -0.11698706816633163; -0.7178501053667702 -0.2147414683533294 -0.03563087595180013; -0.7220121820048746 -0.6387659476154413 0.04867755848318845; -0.6341573780307701 -0.8263426625319585 0.11250663825239217; -0.42165856247956973 -0.9426406733296913 0.15700663915570923; -0.2282676099099079 -0.9148864509029049 0.18224086165253006; -0.19975433285802874 -0.7643878036213333 0.18722809378704905; -0.23887594019854455 -0.571448552171104 0.1698384408589319; -0.20476059817742176 -0.3599675936442139 0.12804247162016902; -0.021622630852921543 -0.18516594772639078 0.08091546982169469; 0.06780313268150127 -0.07159692617114882 -0.012001883119840365; 0.0737246732088521 0.19689739773217652 -0.0905687562910174; -0.07537764165798895 0.41078706656960723 -0.1422877828900227; -0.2938291349463374 0.6466716586743462 -0.17361703816996657; -0.601397213043171 0.6791254738338734 -0.16212519541868492] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [-4.520674651049057, -2.5409484551232677, 0.26037246970875744] km/s
|
|
||||||
V∞_out: [-0.8008259820354645, 5.108593255783271, -0.47079137990954545] km/s
|
|
||||||
time of flight: 8.970106359744217e7 seconds
|
|
||||||
arrival date: 2031-03-13T03:58:30.148
|
|
||||||
thrust profile: [-0.9144771548791947 0.6902760792706399 -0.02961910274543401; -0.9666896369671112 0.2364932018447611 -0.03360017687916256; -0.9297691297960539 -0.38607984447798555 -0.01355789584429883; -0.8346154484217878 -0.6214014693922587 0.0166085094653681; -0.7129033965945708 -0.700963733220583 0.041959359935916686; -0.5741438889568534 -0.6419595568492229 0.05459259074755743; -0.43236122782537784 -0.6653422888597984 0.06339767277888375; -0.32424450019548473 -0.6113143615391297 0.0649952740051996; -0.2507213613172347 -0.5715625368541332 0.06495239951441104; -0.2066973617297525 -0.5173029196105642 0.059981187403511056; -0.17530451342656214 -0.46356648825594077 0.047624841826828745; -0.1477866838400433 -0.3897245825635479 0.049242714379565865; -0.12010797428356033 -0.31542712311456955 0.03834216234998446; -0.09300258495305348 -0.23794128216440627 0.032748124103639975; -0.06465067006435225 -0.16076271327460043 0.023845385656830805; -0.03888290411251017 -0.09081101903598543 0.01503347691667522; -0.012590046428086619 -0.034506030314933926 0.008899905471236012; 0.011376964842136187 0.007648534577971764 -0.00016213377538379614; 0.03978470139669819 0.0415658896303641 -0.008546043818250205; 0.05975267589922902 0.07118967492032456 -0.006512156351974285] %
|
|
||||||
Phase 4:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-1.3584481648257494, 2.8741322587661022, -0.2546304125259141] km/s
|
|
||||||
V∞_out: [-0.03780230346481573, 0.0035967292583968646, 0.0007694792047629233] km/s
|
|
||||||
time of flight: 2.6826096516036582e8 seconds
|
|
||||||
arrival date: 2039-09-12T00:54:35.148
|
|
||||||
thrust profile: [0.15488733950530229 0.004571931625674222 0.014146553973814535; 0.1553899576809856 0.03891862438324717 0.011973507362994223; 0.14041589251623252 0.07646409264944304 0.008869602158932547; 0.11548352038842227 0.1179485961935457 0.005517550148134544; 0.06394148482320672 0.14725938798843563 0.0012092021978766729; 0.0044327089101765475 0.13700916415178752 -0.005822274387507308; -0.029434414888955224 0.100612821704748 -0.017148622938312798; -0.033398085410118725 0.07353093978663178 -0.020258407230342786; -0.022858879964930717 0.05475230911401911 -0.0235821272789971; -0.013323435304460137 0.041377292100863744 -0.02450308078568975; 0.017138449993525783 0.0028560178783815105 -0.007160323142177257; 0.001062473462116934 0.0017720804053553297 -0.03347589005736904; -0.005736640138015923 -0.01153596653687124 -0.031458002877494486; 0.0015233910519389863 -0.004860382970013982 -0.028357121836203404; 0.006148876075267932 -0.01671721636961961 2.8524011567020264e-5; -0.0025972753111940814 -0.024320445695816754 -0.02183259610480299; -0.011337447226728808 -0.029412701131799595 -0.010842354984299675; -0.008925944814787248 -0.03382785337511997 -0.002144952702459933; -0.002362954309468288 -0.03692199124600801 0.010934038390259249; 0.006643709781956786 -0.044837750975252416 0.015646911234478936] %
|
|
||||||
|
|
||||||
Mass Used: 971.9203240703632 kg
|
|
||||||
Launch C3: 15.682293253184955 km²/s²
|
|
||||||
||V∞_in||: 3.1891776846675537 km/s
|
|
||||||
File diff suppressed because one or more lines are too long
@@ -1,136 +0,0 @@
|
|||||||
archive/EMMJS_archive
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2023-02-26T04:10:12.359
|
|
||||||
Launch V∞: [-4.841701064906604, 3.475969740428134, -4.8994214190507] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [0.02729198924983877, 5.017291114045934, -2.960466892478738] km/s
|
|
||||||
V∞_out: [-0.7796648643413417, 5.029374064409783, -2.8347788324016983] km/s
|
|
||||||
time of flight: 1.9570320002726743e8 seconds
|
|
||||||
arrival date: 2029-05-10T06:10:12.359
|
|
||||||
thrust profile: [0.51200489277245 0.1491712750305638 -0.5617898782756465; 0.5985472817937932 0.4314745458970473 -0.29088252333102027; -0.45166509877363964 0.5194585980906682 0.5146294788199312; 0.390520290781806 -0.5192326236428068 0.4429840782407487; 0.5160025656800347 0.43684584169735574 -0.4960808446595455; 0.5098504634472127 0.5199893315046626 0.4441400784392527; -0.49987113488322754 -0.47893620910952606 0.48036085120848565; 0.5368410355569405 0.5166822047764457 -0.4858670271400151; 0.44238316289905827 0.547824927494726 -0.4656337244770621; 0.21668892035180595 0.6021857778661118 -0.19651661385197258; 0.4341377302277037 -0.16678624993961083 0.5761938702855823; 0.5718885908183827 0.5536579188076003 0.33795675555520704; -0.39527664332753926 0.5814857962643089 -0.4679595952307845; -0.008428218148373924 0.5415048084721836 -0.45110046854424596; 0.33161932673220734 -0.45295582817342434 0.46836263037592774; 0.5280374896116378 0.5764518977818923 0.3342129870989262; 0.3107502688966615 0.5511548090736831 -0.5014473758638118; 0.07343276836897304 0.6646323168301356 -0.33765386861899715; -0.5980335383406491 -0.5746723266973839 0.15575901290142588; 0.590900565213738 0.39693261331727714 0.20472515338144043] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [3.0241033936172084, 1.6385004369573686, -5.605711794771172] km/s
|
|
||||||
V∞_out: [2.4283811769402535, -1.1475844477691648, -6.003401620464895] km/s
|
|
||||||
time of flight: 1.1737080029703692e8 seconds
|
|
||||||
arrival date: 2033-01-27T17:10:12.359
|
|
||||||
thrust profile: [-0.1768137656168143 0.3393511738335891 -0.353565456723947; -0.15954083659688176 -0.5487799730055659 -0.24022806443793981; 0.5157742145013325 -0.7252600963065111 -0.4938126290082077; 0.698500596084941 0.03900690309877106 -0.23316637699244064; 0.6365913895344839 0.20777317872832707 -0.2830962364627441; 0.5861304271928349 -0.1184358449845895 -0.4564142893293172; 0.6860855423630463 -0.5456724995449903 -0.44617293698271493; 0.6670491113213445 -0.38498567211274926 -0.3230834818585812; 0.5283999818464645 -0.09570871485046831 -0.478027472175741; 0.6580560949600205 0.46722570225829474 -0.11535896533777851; 0.5612619202113102 -0.1931961652510376 -0.4400901944952552; 0.4590177925799 -0.6932770941014383 -0.5144556676853405; 0.7561006651195121 -0.6660301702898956 -0.558073578122206; 0.7758630959701225 -0.08472708630272804 -0.41036611726373284; 0.566096622638857 0.7122289950338151 -0.11214847640185667; -0.4306590268194921 0.4288485227605312 0.2105331105689206; -0.5085374829983493 -0.516980326040015 0.16675646570585556; -0.5812762098132924 -0.6592114464112737 -0.39525785227607435; 0.3559795650447502 -0.8283244516408661 -0.5816275654619777; 0.7220122543976706 -0.8709955103801817 -0.5752271662039113] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [5.060776761478531, -2.65457156740014, 1.2093916749224973] km/s
|
|
||||||
V∞_out: [-4.655218918764466, -2.2507227956970843, 2.7173192390054806] km/s
|
|
||||||
time of flight: 7.437600000965603e7 seconds
|
|
||||||
arrival date: 2035-06-07T13:10:12.359
|
|
||||||
thrust profile: [0.5554028628906259 -0.8562653819570508 -0.4353192179666242; 0.6836770270628973 -0.8068634065800825 -0.40691024348661053; 0.6938434264699962 -0.7253280301253697 -0.3838170511550203; 0.645874750163326 -0.6289501430894447 -0.3499668164482744; 0.5889993418389312 -0.5421974665324047 -0.3250231983004846; 0.521131977446493 -0.4767106284566455 -0.3139270110389849; 0.44907608028844187 -0.42835191134595757 -0.30427273241100156; 0.3771619836123307 -0.38593020022499613 -0.29345181442595814; 0.30758537653438345 -0.34138417397604953 -0.2806050625679753; 0.24090511199415704 -0.2908278788914028 -0.2653604699658747; 0.17676587080788508 -0.23266346298480622 -0.24755096472050972; 0.11564885705822119 -0.16792372723278565 -0.22685867498381254; 0.07637432600785862 -0.10221693792171678 -0.20194486428807676; 0.019753903444897154 -0.058193667702053815 -0.18756658332981802; -0.044040327145306354 -0.00021057373845115093 -0.15565868544825787; -0.1020149066984689 0.047297427488451 -0.11989375229021738; -0.15572852811033114 0.08561531859322227 -0.08266441800646043; -0.20039007901031922 0.11872106917143616 -0.04576729741807346; -0.24124782668690306 0.1511930898415435 -0.009960538806793113; -0.28349017928188214 0.1924753920006318 0.02615368339855036] %
|
|
||||||
Phase 4:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-7.256385977948657, 0.7771719462797614, -0.785892915072424] km/s
|
|
||||||
V∞_out: [-5.9473393974944736e-6, -7.362203906933263e-7, 6.306068555232033e-7] km/s
|
|
||||||
time of flight: 1.4662439997163886e8 seconds
|
|
||||||
arrival date: 2040-01-29T14:10:11.359
|
|
||||||
thrust profile: [-0.18959418256753224 0.13412715420236315 -0.043410183532822624; -0.19766571870169566 0.1372601657158578 -0.037968113030145044; -0.1971783405485536 0.129832118307628 -0.04157452597322259; -0.19192072677853972 0.11752160892327206 -0.04544882251204915; -0.18096355607909057 0.10099613325234727 -0.04845756455495175; -0.16440940142977603 0.0827695902679096 -0.0501168011338542; -0.14159683191947461 0.06939209018313232 -0.04938123378650775; -0.11494734465063888 0.05950353242028259 -0.04787565574075916; -0.08842871021960914 0.05331851047785903 -0.04243441932918664; -0.06244946835797671 0.049895056937498274 -0.03534701683264976; -0.0380028875571515 0.047256901837732644 -0.02725064975669285; -0.01886788294008128 0.04286456425792469 -0.019192970894846496; 0.0054749884299889135 0.041277048472854974 -0.010750429199969911; 0.02389959629376803 0.03888123568193434 -0.0015386535754099552; 0.0428231915186611 0.03753775483224003 0.00740487148339779; 0.06481451674589596 0.03713565978563092 0.014580239918154077; 0.09005525246175461 0.0369062161152353 0.018428292697994248; 0.1201760127678751 0.03212421201511818 0.04118543343400019; 0.15404590862831494 0.02789044310966664 0.043771491647338116; 0.18466591121075765 0.02447914444489793 0.052012952789042624] %
|
|
||||||
|
|
||||||
Mass Used: 2528.0301016677718 kg
|
|
||||||
Launch C3: 59.52876507974255 km²/s²
|
|
||||||
||V∞_in||: 7.3400791119043935 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2023-07-25T10:56:35.081
|
|
||||||
Launch V∞: [-0.946994040198373, 0.7451481404956214, -0.8183806644150764] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [0.014258156666681189, 2.7730331960192176, -1.1269036535413253] km/s
|
|
||||||
V∞_out: [0.5141370030166348, -0.1036905077662334, -2.9466045466696906] km/s
|
|
||||||
time of flight: 1.1404800000012271e8 seconds
|
|
||||||
arrival date: 2027-03-06T10:56:35.081
|
|
||||||
thrust profile: [0.9385530212613687 0.4901574978623852 0.10061758150690266; 0.963070949930897 0.8321550483186799 0.008076995378552753; 0.9477571571642094 0.9610236014179844 -0.3985885112414162; -0.8711740070381366 0.9585545422957218 -0.473960549642588; -0.35180875323453037 0.5538991572461103 -0.3047172625720546; 0.945857985340927 0.9318586412463802 0.07532442345652893; 0.916860585821232 0.9461601676367617 0.09256592206997157; 0.9203902037763169 0.9428723645501874 -0.3780093114569496; 0.1105180481588208 0.9388923575412604 -0.5467563429465788; 0.9600557668435807 0.08776536568096838 -0.6082094846555337; 0.9694071291822624 0.9576019390193865 0.042076881935371874; 0.7379014033007257 0.9676653528673065 0.20011181540529835; -0.7026385155061656 0.9228908375337035 -0.34668134552520397; 0.34660988424967165 0.77350231915288 -0.6692179888555208; 0.9672945056421521 -0.9455364762862372 -0.5850573257116493; 0.9859396795925156 0.16374570712498915 -0.26188762301350715; 0.9545064259275549 0.9869744571812468 0.4480444603786351; -0.9777686070631371 0.9725195168208975 0.193691849051127; -0.9708472634149672 0.7500006701210962 -0.37076685227103995; -0.9229893981992848 -0.9773469965294133 -0.6290625133929346] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-0.8165677595901083, -0.06087475377585851, 3.052309046353131] km/s
|
|
||||||
V∞_out: [-2.9671064112310424, -0.9629127612065755, 0.5071630145897023] km/s
|
|
||||||
time of flight: 2.5657200000050467e7 seconds
|
|
||||||
arrival date: 2027-12-28T09:56:35.081
|
|
||||||
thrust profile: [-0.41833750150854715 -0.23745700390485924 0.5060156710931941; -0.39335607115842763 -0.21531365718730944 0.6214127928981721; -0.3741710013483589 -0.18178973996137726 0.7015878071805001; -0.3643811289828083 -0.1509347162037813 0.751160544358552; -0.3628330570779499 -0.11199271269023013 0.7793128986864543; -0.37235570205858287 -0.07302372672984968 0.7974839419031854; -0.3874662882006923 -0.03576203680036734 0.8098641766992978; -0.4074499881135819 -0.006584284581002934 0.8169150088581699; -0.4281109131913487 0.01182349039523377 0.8189971077067131; -0.4459261627474135 0.02257293277791146 0.8172972584690744; -0.4568773433902438 0.024804843226578856 0.8108158124505926; -0.4596411297003703 0.025045134417719155 0.7994526969817127; -0.4544566197190047 0.02267340988409504 0.7798827612879172; -0.44051961933116424 0.02370501075040903 0.7512234553177294; -0.41845307963023165 0.03005154105743171 0.708359052016344; -0.3881992767298684 0.04309990454210432 0.642522507646677; -0.34752334469565116 0.06138846846654963 0.5427837231822192; -0.2956992996903972 0.07742676936562033 0.40261391380265427; -0.17065939997376794 0.03880630671620183 0.2558269001777807; -0.235765575949598 0.13041638287567744 0.1404777210162043] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [-1.7554396063175077, -4.3095849115029985, -0.1325601348507023] km/s
|
|
||||||
V∞_out: [-4.236997629309691, -1.8724795170284283, -0.4561606000854912] km/s
|
|
||||||
time of flight: 1.4433840000004688e8 seconds
|
|
||||||
arrival date: 2032-07-24T23:56:35.081
|
|
||||||
thrust profile: [-0.5079766273797471 -0.10849515042583255 -0.0073545543900051516; -0.8149330561784093 0.34076004302958 -0.10326028863924017; -0.9395306205116954 -0.6895587367092969 -0.1170733748155399; -0.8439334413601929 -0.9377459623599967 0.015887598730331222; -0.12385311413264775 -0.85754750232578 0.11388747617260146; -0.15722365998440252 -0.3713893060760601 0.07983906967712144; -0.4905066367366128 -0.27630177574765263 0.052134881351611005; -0.40323969943463034 -0.36672944173144784 0.10826813939276426; -0.5166657583603889 -0.20333001707916043 0.07190841766549783; -0.9296123351360971 0.7837821870593056 -0.035789654605662545; -0.9678260619223868 -0.13908054107117102 0.11575665020892843; -0.9440698254178282 -0.9616603904467664 0.28528753638981585; 0.16941992205087786 -0.958669585346112 0.2124940591626158; 0.6017699213284338 -0.9270140863622942 0.07796374810040851; 0.39129362583737487 -0.748999519453576 0.05494281482886338; -0.005988877690288004 0.3481376434297022 0.032216440029362; 0.011527786969304827 -0.31978413035928577 -0.004592862949742337; -0.1976671384268677 0.9049682211089798 -0.21479203411765663; 0.5371991705488778 0.9049363560121139 -0.175235712765763; 0.054168546279189246 0.9414663774468465 -0.16207020976741393] %
|
|
||||||
Phase 4:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-6.539365214334455, 2.218176712783986, -0.36626020172775725] km/s
|
|
||||||
V∞_out: [-3.665136112061718, 6.451338183645968, -0.16457889689277141] km/s
|
|
||||||
time of flight: 1.812492000000014e8 seconds
|
|
||||||
arrival date: 2038-04-22T18:56:35.081
|
|
||||||
thrust profile: [0.05264623774997263 0.215338495237562 0.003754114844726852; 0.021165626937991143 0.22155170870739663 0.0047677855635804905; -0.0033929172288595286 0.31227924099890236 0.06539164976806457; 0.5694561518181592 0.6749368464572498 -0.11566610061632827; 0.1324891033231393 0.3597380526244606 -0.022962295545894153; 0.024627138889422973 0.3245686299565964 0.04183403216303953; 0.04019245536713721 0.744671990758876 0.03457514031015897; 0.03322017112484851 0.09302676824184232 -0.04257715628694308; -0.5866822473952952 -0.1769325756395129 0.23680697649509092; -0.14301190082784437 0.09180461385600784 -0.028924399094075886; -0.18983362654037655 -0.01602479614573261 -0.1446728759943558; 0.17123430049602928 0.2161630553091436 -0.12107554476977027; 0.0336023230656082 -0.34829018802826484 -0.06164799648134331; -0.0137744016652137 0.032090633273540385 -0.01461460357642287; 0.023301081130224558 0.023046782785575825 -0.0014039211755592525; 0.04517905715080291 0.07387132921915998 0.025233349143655093; 0.019815422280705618 -0.054453865039265595 -0.04881233646684176; 0.010800262146714945 0.40350474993323376 0.07282207796248781; 0.06922178100116284 -0.38131801494106843 -0.09824591875105594; 0.3129500615782364 -0.8033474844184223 -0.09841107223379629] %
|
|
||||||
|
|
||||||
Mass Used: 2769.31857214896 kg
|
|
||||||
Launch C3: 2.1217903753437817 km²/s²
|
|
||||||
||V∞_in||: 6.915038096131817 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2023-11-08T16:33:41.148
|
|
||||||
Launch V∞: [-3.7467429728623447, -0.7427414062360022, 1.0452490382459865] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-2.885104439331886, -1.327495046167686, -0.027749058108596784] km/s
|
|
||||||
V∞_out: [-1.635967097498029, -2.7221789573242074, 0.015131202359034032] km/s
|
|
||||||
time of flight: 6.778595425260136e7 seconds
|
|
||||||
arrival date: 2026-01-01T05:59:35.148
|
|
||||||
thrust profile: [-0.05074044407568138 -0.021150582055882192 0.02730812822478398; -0.05363696950139044 -0.06016484582924907 0.04378542458137859; -0.02771035674834004 -0.10645426057233084 0.04017412625773127; 0.01630657360103497 -0.12411195034078264 0.023350505322999197; 0.05888817282501315 -0.10894637011686983 0.0004869417342207616; 0.08706942097452976 -0.07439720218837492 -0.023367157675286705; 0.09495132401480658 -0.035316011414834675 -0.04390702621881143; 0.08752285351021441 -0.004210304140208955 -0.05824943912322043; 0.06832834450779833 0.01653042551161497 -0.06490194085584605; 0.04924860864138059 0.022800133521631457 -0.062427366917489194; 0.03691868046224741 0.011541999666891671 -0.049506900069146154; 0.02451718791619906 0.019175805931995835 -0.026347851368135194; -0.032064249204675696 0.028639492606652335 0.024093899166278167; -0.08306772663523894 -0.03165903417995458 0.04031997576998134; -0.09308798794042389 -0.09539353910087413 0.04749994325844049; -0.02511528438762353 -0.14606890192307997 0.03354911283916682; 0.04310668443858089 -0.14207536740537 0.010418445496805094; 0.09246132545360927 -0.10807413652564378 -0.01547233992587798; 0.11319881808511016 -0.06123358244390861 -0.03864051024951101; 0.11067805251913554 -0.018856574108340608 -0.05612659024233843] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-5.884459586892747, -3.363236848676117, -0.5090555323000778] km/s
|
|
||||||
V∞_out: [-6.754575036027653, -0.6433971508597986, -0.39980914727121014] km/s
|
|
||||||
time of flight: 7.419247222558242e7 seconds
|
|
||||||
arrival date: 2028-05-08T23:00:47.148
|
|
||||||
thrust profile: [0.09654790671377476 -0.02421154193760562 -0.017928801450145315; -0.013697559588275829 0.2078634802144036 -0.1014668129386949; -0.1556430254864518 0.42999351341524117 -0.15436045217579106; -0.34594668129342293 0.5414366154963298 -0.18269379097659816; -0.5454038742991185 0.5440039323636802 -0.17114242041739094; -0.6681265735588777 0.3905344944333295 -0.11698706816633163; -0.7178501053667702 -0.2147414683533294 -0.03563087595180013; -0.7220121820048746 -0.6387659476154413 0.04867755848318845; -0.6341573780307701 -0.8263426625319585 0.11250663825239217; -0.42165856247956973 -0.9426406733296913 0.15700663915570923; -0.2282676099099079 -0.9148864509029049 0.18224086165253006; -0.19975433285802874 -0.7643878036213333 0.18722809378704905; -0.23887594019854455 -0.571448552171104 0.1698384408589319; -0.20476059817742176 -0.3599675936442139 0.12804247162016902; -0.021622630852921543 -0.18516594772639078 0.08091546982169469; 0.06780313268150127 -0.07159692617114882 -0.012001883119840365; 0.0737246732088521 0.19689739773217652 -0.0905687562910174; -0.07537764165798895 0.41078706656960723 -0.1422877828900227; -0.2938291349463374 0.6466716586743462 -0.17361703816996657; -0.601397213043171 0.6791254738338734 -0.16212519541868492] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [-4.520674651049057, -2.5409484551232677, 0.26037246970875744] km/s
|
|
||||||
V∞_out: [-0.8008259820354645, 5.108593255783271, -0.47079137990954545] km/s
|
|
||||||
time of flight: 8.970106359744217e7 seconds
|
|
||||||
arrival date: 2031-03-13T03:58:30.148
|
|
||||||
thrust profile: [-0.9144771548791947 0.6902760792706399 -0.02961910274543401; -0.9666896369671112 0.2364932018447611 -0.03360017687916256; -0.9297691297960539 -0.38607984447798555 -0.01355789584429883; -0.8346154484217878 -0.6214014693922587 0.0166085094653681; -0.7129033965945708 -0.700963733220583 0.041959359935916686; -0.5741438889568534 -0.6419595568492229 0.05459259074755743; -0.43236122782537784 -0.6653422888597984 0.06339767277888375; -0.32424450019548473 -0.6113143615391297 0.0649952740051996; -0.2507213613172347 -0.5715625368541332 0.06495239951441104; -0.2066973617297525 -0.5173029196105642 0.059981187403511056; -0.17530451342656214 -0.46356648825594077 0.047624841826828745; -0.1477866838400433 -0.3897245825635479 0.049242714379565865; -0.12010797428356033 -0.31542712311456955 0.03834216234998446; -0.09300258495305348 -0.23794128216440627 0.032748124103639975; -0.06465067006435225 -0.16076271327460043 0.023845385656830805; -0.03888290411251017 -0.09081101903598543 0.01503347691667522; -0.012590046428086619 -0.034506030314933926 0.008899905471236012; 0.011376964842136187 0.007648534577971764 -0.00016213377538379614; 0.03978470139669819 0.0415658896303641 -0.008546043818250205; 0.05975267589922902 0.07118967492032456 -0.006512156351974285] %
|
|
||||||
Phase 4:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-1.3584481648257494, 2.8741322587661022, -0.2546304125259141] km/s
|
|
||||||
V∞_out: [-0.03780230346481573, 0.0035967292583968646, 0.0007694792047629233] km/s
|
|
||||||
time of flight: 2.6826096516036582e8 seconds
|
|
||||||
arrival date: 2039-09-12T00:54:35.148
|
|
||||||
thrust profile: [0.15488733950530229 0.004571931625674222 0.014146553973814535; 0.1553899576809856 0.03891862438324717 0.011973507362994223; 0.14041589251623252 0.07646409264944304 0.008869602158932547; 0.11548352038842227 0.1179485961935457 0.005517550148134544; 0.06394148482320672 0.14725938798843563 0.0012092021978766729; 0.0044327089101765475 0.13700916415178752 -0.005822274387507308; -0.029434414888955224 0.100612821704748 -0.017148622938312798; -0.033398085410118725 0.07353093978663178 -0.020258407230342786; -0.022858879964930717 0.05475230911401911 -0.0235821272789971; -0.013323435304460137 0.041377292100863744 -0.02450308078568975; 0.017138449993525783 0.0028560178783815105 -0.007160323142177257; 0.001062473462116934 0.0017720804053553297 -0.03347589005736904; -0.005736640138015923 -0.01153596653687124 -0.031458002877494486; 0.0015233910519389863 -0.004860382970013982 -0.028357121836203404; 0.006148876075267932 -0.01671721636961961 2.8524011567020264e-5; -0.0025972753111940814 -0.024320445695816754 -0.02183259610480299; -0.011337447226728808 -0.029412701131799595 -0.010842354984299675; -0.008925944814787248 -0.03382785337511997 -0.002144952702459933; -0.002362954309468288 -0.03692199124600801 0.010934038390259249; 0.006643709781956786 -0.044837750975252416 0.015646911234478936] %
|
|
||||||
|
|
||||||
Mass Used: 971.9203240703632 kg
|
|
||||||
Launch C3: 15.682293253184955 km²/s²
|
|
||||||
||V∞_in||: 3.1891776846675537 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
@@ -1,43 +0,0 @@
|
|||||||
archive/EVMJS---------------------------
|
|
||||||
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2024-04-20T12:58:59.053
|
|
||||||
Launch V∞: [-8.920597561322369, -7.117372634919496, -1.472451871563068] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Venus
|
|
||||||
V∞_in: [-5.017961509289203, -5.654947873213361, -1.4864114620218827] km/s
|
|
||||||
V∞_out: [-7.390394917247088, -2.021337895911062, -0.8148956710919548] km/s
|
|
||||||
time of flight: 4.572852817115571e7 seconds
|
|
||||||
arrival date: 2025-10-01T19:21:07.053
|
|
||||||
thrust profile: [-0.21862938814794752 -0.05580927018043333 -0.036914761844326786; -0.24413346338652692 -0.02556655529310196 -0.03840768064934617; -0.26465223193143633 -0.031988862192285895 -0.03672328500867164; -0.2775111471212138 -0.0533843665242742 -0.03463858507707235; -0.282355262314745 -0.07982445428959191 -0.033636788586472385; -0.28050912409469175 -0.10607204371684377 -0.032167717475040075; -0.2733689146909765 -0.12962521272658228 -0.03161077625553056; -0.26190711303703673 -0.14877589397585794 -0.030649321801181607; -0.24697067176434023 -0.16354203331437878 -0.029534650090164597; -0.22916216500741854 -0.1736646300332696 -0.02774354605279356; -0.20930307239303453 -0.1793556553425328 -0.02624057086532488; -0.1881341647769172 -0.18020842931174086 -0.022018620586908344; -0.16781156346033524 -0.1755305190264814 -0.017713311035217196; -0.1529314715768468 -0.16133304311878607 -0.011294101805393433; -0.1439292332041623 -0.13894686830886066 -0.005512101036767262; -0.13595373894772989 -0.11376326317155387 0.008492968124788823; -0.14161082765712693 -0.0633805633113515 0.026736612907202688; -0.14271356865834361 0.024062134302168376 0.04098391846668108; -0.1414981556176295 0.035473208118311124 0.03720171942581438; -0.13060050476893825 0.04192201790827888 0.030084566679769147] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-9.28829223014179, -7.607789338281241, -0.2942705558666007] km/s
|
|
||||||
V∞_out: [-8.317437974959708, -8.663545949996019, 0.030785372299447233] km/s
|
|
||||||
time of flight: 5.8747531161094815e7 seconds
|
|
||||||
arrival date: 2027-08-12T18:06:38.053
|
|
||||||
thrust profile: [-0.174672404758962 0.02506293138125133 -0.02426121230831768; -0.05008204073446195 -0.07279118574621102 -0.08129060414874276; 0.18941101625787235 -0.07952903306738271 -0.10689582281590368; 0.35705302923506294 0.027307923111368104 -0.0479794442058468; 0.41799317552955584 0.12801887957214292 -0.029898349295167635; 0.4511914489377908 0.23489263829219467 -0.020213669874118333; 0.4656012050626349 0.3325378259130575 -0.014159348767163066; 0.4657014753978555 0.41280917091846614 -0.013135235235423743; 0.45029470699103086 0.4771859548843401 -0.012168900825375072; 0.4106794937152572 0.5294663391131441 -0.011594787023374607; 0.33819071474272516 0.5678785558859125 -0.010353193332547849; 0.2001630795815917 0.5937428427734591 -0.00709996654137991; -0.035108210746352266 0.6005435960325474 -0.0011602329790232843; -0.29361875930485426 0.5723600768872681 0.008300256500510222; -0.4548836328849185 0.4770722319186511 0.014296267759918423; -0.5113471724292226 0.19706675000368873 0.01697398652461365; -0.4134871925757221 -0.2340982056617441 0.01763457992701102; -0.17230637273503518 -0.34708241891449854 0.032309764753320355; 0.1190741484482409 -0.3404978442614275 0.03287368817385319; 0.30168780764812786 -0.2869031294203351 0.028403718812872233] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [-2.998311290651761, -5.22937520865022, 0.1407756821047572] km/s
|
|
||||||
V∞_out: [-2.856148992180316, 5.306598853387247, -0.19607428788923498] km/s
|
|
||||||
time of flight: 1.4159768899978405e8 seconds
|
|
||||||
arrival date: 2032-02-06T14:48:06.053
|
|
||||||
thrust profile: [0.37857744177475117 -0.5722922563923073 0.022790081593862904; 0.4498819042137626 -0.33368177218590706 -0.006756732610181868; 0.45137346520621063 0.2646268898149342 -0.06715401087102708; 0.3370898120722347 0.5147560334694927 -0.0942931710827749; 0.10406019537076351 0.6331750657513396 -0.10357703864723887; -0.3067722620848112 0.6948315815503575 -0.0862070073278207; -0.5894971893625187 0.7222874275705 -0.047061967331428964; -0.7438646368242161 0.7031736402976893 0.007847733426895626; -0.8153797919927924 0.4618300002958423 0.06963851455772195; -0.8054139924887445 -0.5908908470157955 0.097381115730603; -0.6892129370491469 -0.7264006520777874 0.08776061857832115; -0.45980277149808124 -0.7029156090490672 0.07926634239802542; -0.23430875626887712 -0.6386864247061581 0.07411409321833815; -0.11447347572705899 -0.5560871561049769 0.0680750057792953; -0.06705788386230047 -0.46200938046607043 0.06022766091205061; -0.049086029532628715 -0.35725786450463903 0.05078115410828272; -0.04044489185865085 -0.23996050920253587 0.04039683492314978; -0.034110498545589486 -0.10823424969630317 0.03211353029920855; -0.025504423988764145 0.06607493481717405 0.015337634169998754; -0.016379042728758193 0.201103314416455 -0.001097801876741442] %
|
|
||||||
Phase 4:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-3.7553623927693303, 3.8045661430805238, -0.0017497584909869502] km/s
|
|
||||||
V∞_out: [0.00016771014375336496, 0.02190103395006303, -0.00015322066785738935] km/s
|
|
||||||
time of flight: 2.0181733919676498e8 seconds
|
|
||||||
arrival date: 2038-06-30T11:10:25.053
|
|
||||||
thrust profile: [0.18326801514146682 0.11845670033224177 -0.0016084372043512012; 0.1675872421589649 0.14235871799128041 -0.002787329388980011; 0.14198390921850934 0.16511394888691344 -0.0037731022920933425; 0.10352323696814321 0.18228824596062612 -0.004414585252525113; 0.052724231521741716 0.18616944898352478 -0.004616750142156716; 0.0011654214657718389 0.1688827891674893 -0.004589773974233177; -0.031151502893950005 0.13429086557793365 -0.0048861485136074976; -0.0387542725070042 0.09962903031836343 -0.005697801228946161; -0.032764472688793025 0.0752213826812925 -0.006648655387876376; -0.02303421181483975 0.059664277716287864 -0.007393815905338262; -0.013366915890350172 0.04886766638458846 -0.007849749770643184; -0.004273656127481105 0.04004011769410306 -0.008128123571266301; 0.005274989439679697 0.03136991809704025 -0.008359024971909892; 0.01659789890620425 0.02034976567361285 -0.008341112112060404; 0.027347691011068397 0.0015674507187789124 -0.007372599601001636; 0.03221036017744093 -0.01353396250128953 -0.004949290348108288; 0.03641858295092107 -0.025405796803472054 -0.003362734977936097; 0.04156323966242008 -0.03555478122658915 -0.002142996490186938; 0.04760308383336786 -0.0450888885925399 -0.0011510722358481168; 0.05448090196904719 -0.0542737048917187 -0.0003050212878129177] %
|
|
||||||
|
|
||||||
Mass Used: 1175.3239683910674 kg
|
|
||||||
Launch C3: 132.40216858944106 km²/s²
|
|
||||||
||V∞_in||: 5.345790240905041 km/s
|
|
||||||
File diff suppressed because one or more lines are too long
@@ -1,46 +0,0 @@
|
|||||||
archive/EVMJS_archive
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2024-04-20T12:58:59.053
|
|
||||||
Launch V∞: [-8.920597561322369, -7.117372634919496, -1.472451871563068] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Venus
|
|
||||||
V∞_in: [-5.017961509289203, -5.654947873213361, -1.4864114620218827] km/s
|
|
||||||
V∞_out: [-7.390394917247088, -2.021337895911062, -0.8148956710919548] km/s
|
|
||||||
time of flight: 4.572852817115571e7 seconds
|
|
||||||
arrival date: 2025-10-01T19:21:07.053
|
|
||||||
thrust profile: [-0.21862938814794752 -0.05580927018043333 -0.036914761844326786; -0.24413346338652692 -0.02556655529310196 -0.03840768064934617; -0.26465223193143633 -0.031988862192285895 -0.03672328500867164; -0.2775111471212138 -0.0533843665242742 -0.03463858507707235; -0.282355262314745 -0.07982445428959191 -0.033636788586472385; -0.28050912409469175 -0.10607204371684377 -0.032167717475040075; -0.2733689146909765 -0.12962521272658228 -0.03161077625553056; -0.26190711303703673 -0.14877589397585794 -0.030649321801181607; -0.24697067176434023 -0.16354203331437878 -0.029534650090164597; -0.22916216500741854 -0.1736646300332696 -0.02774354605279356; -0.20930307239303453 -0.1793556553425328 -0.02624057086532488; -0.1881341647769172 -0.18020842931174086 -0.022018620586908344; -0.16781156346033524 -0.1755305190264814 -0.017713311035217196; -0.1529314715768468 -0.16133304311878607 -0.011294101805393433; -0.1439292332041623 -0.13894686830886066 -0.005512101036767262; -0.13595373894772989 -0.11376326317155387 0.008492968124788823; -0.14161082765712693 -0.0633805633113515 0.026736612907202688; -0.14271356865834361 0.024062134302168376 0.04098391846668108; -0.1414981556176295 0.035473208118311124 0.03720171942581438; -0.13060050476893825 0.04192201790827888 0.030084566679769147] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Mars
|
|
||||||
V∞_in: [-9.28829223014179, -7.607789338281241, -0.2942705558666007] km/s
|
|
||||||
V∞_out: [-8.317437974959708, -8.663545949996019, 0.030785372299447233] km/s
|
|
||||||
time of flight: 5.8747531161094815e7 seconds
|
|
||||||
arrival date: 2027-08-12T18:06:38.053
|
|
||||||
thrust profile: [-0.174672404758962 0.02506293138125133 -0.02426121230831768; -0.05008204073446195 -0.07279118574621102 -0.08129060414874276; 0.18941101625787235 -0.07952903306738271 -0.10689582281590368; 0.35705302923506294 0.027307923111368104 -0.0479794442058468; 0.41799317552955584 0.12801887957214292 -0.029898349295167635; 0.4511914489377908 0.23489263829219467 -0.020213669874118333; 0.4656012050626349 0.3325378259130575 -0.014159348767163066; 0.4657014753978555 0.41280917091846614 -0.013135235235423743; 0.45029470699103086 0.4771859548843401 -0.012168900825375072; 0.4106794937152572 0.5294663391131441 -0.011594787023374607; 0.33819071474272516 0.5678785558859125 -0.010353193332547849; 0.2001630795815917 0.5937428427734591 -0.00709996654137991; -0.035108210746352266 0.6005435960325474 -0.0011602329790232843; -0.29361875930485426 0.5723600768872681 0.008300256500510222; -0.4548836328849185 0.4770722319186511 0.014296267759918423; -0.5113471724292226 0.19706675000368873 0.01697398652461365; -0.4134871925757221 -0.2340982056617441 0.01763457992701102; -0.17230637273503518 -0.34708241891449854 0.032309764753320355; 0.1190741484482409 -0.3404978442614275 0.03287368817385319; 0.30168780764812786 -0.2869031294203351 0.028403718812872233] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [-2.998311290651761, -5.22937520865022, 0.1407756821047572] km/s
|
|
||||||
V∞_out: [-2.856148992180316, 5.306598853387247, -0.19607428788923498] km/s
|
|
||||||
time of flight: 1.4159768899978405e8 seconds
|
|
||||||
arrival date: 2032-02-06T14:48:06.053
|
|
||||||
thrust profile: [0.37857744177475117 -0.5722922563923073 0.022790081593862904; 0.4498819042137626 -0.33368177218590706 -0.006756732610181868; 0.45137346520621063 0.2646268898149342 -0.06715401087102708; 0.3370898120722347 0.5147560334694927 -0.0942931710827749; 0.10406019537076351 0.6331750657513396 -0.10357703864723887; -0.3067722620848112 0.6948315815503575 -0.0862070073278207; -0.5894971893625187 0.7222874275705 -0.047061967331428964; -0.7438646368242161 0.7031736402976893 0.007847733426895626; -0.8153797919927924 0.4618300002958423 0.06963851455772195; -0.8054139924887445 -0.5908908470157955 0.097381115730603; -0.6892129370491469 -0.7264006520777874 0.08776061857832115; -0.45980277149808124 -0.7029156090490672 0.07926634239802542; -0.23430875626887712 -0.6386864247061581 0.07411409321833815; -0.11447347572705899 -0.5560871561049769 0.0680750057792953; -0.06705788386230047 -0.46200938046607043 0.06022766091205061; -0.049086029532628715 -0.35725786450463903 0.05078115410828272; -0.04044489185865085 -0.23996050920253587 0.04039683492314978; -0.034110498545589486 -0.10823424969630317 0.03211353029920855; -0.025504423988764145 0.06607493481717405 0.015337634169998754; -0.016379042728758193 0.201103314416455 -0.001097801876741442] %
|
|
||||||
Phase 4:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-3.7553623927693303, 3.8045661430805238, -0.0017497584909869502] km/s
|
|
||||||
V∞_out: [0.00016771014375336496, 0.02190103395006303, -0.00015322066785738935] km/s
|
|
||||||
time of flight: 2.0181733919676498e8 seconds
|
|
||||||
arrival date: 2038-06-30T11:10:25.053
|
|
||||||
thrust profile: [0.18326801514146682 0.11845670033224177 -0.0016084372043512012; 0.1675872421589649 0.14235871799128041 -0.002787329388980011; 0.14198390921850934 0.16511394888691344 -0.0037731022920933425; 0.10352323696814321 0.18228824596062612 -0.004414585252525113; 0.052724231521741716 0.18616944898352478 -0.004616750142156716; 0.0011654214657718389 0.1688827891674893 -0.004589773974233177; -0.031151502893950005 0.13429086557793365 -0.0048861485136074976; -0.0387542725070042 0.09962903031836343 -0.005697801228946161; -0.032764472688793025 0.0752213826812925 -0.006648655387876376; -0.02303421181483975 0.059664277716287864 -0.007393815905338262; -0.013366915890350172 0.04886766638458846 -0.007849749770643184; -0.004273656127481105 0.04004011769410306 -0.008128123571266301; 0.005274989439679697 0.03136991809704025 -0.008359024971909892; 0.01659789890620425 0.02034976567361285 -0.008341112112060404; 0.027347691011068397 0.0015674507187789124 -0.007372599601001636; 0.03221036017744093 -0.01353396250128953 -0.004949290348108288; 0.03641858295092107 -0.025405796803472054 -0.003362734977936097; 0.04156323966242008 -0.03555478122658915 -0.002142996490186938; 0.04760308383336786 -0.0450888885925399 -0.0011510722358481168; 0.05448090196904719 -0.0542737048917187 -0.0003050212878129177] %
|
|
||||||
|
|
||||||
Mass Used: 1175.3239683910674 kg
|
|
||||||
Launch C3: 132.40216858944106 km²/s²
|
|
||||||
||V∞_in||: 5.345790240905041 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
@@ -1,43 +0,0 @@
|
|||||||
archive/EVVJS---------------------------
|
|
||||||
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2023-05-08T02:15:41.742
|
|
||||||
Launch V∞: [-2.6705377464328075, 1.81220401477148, -5.02986389717478] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Venus
|
|
||||||
V∞_in: [-2.6649059053371618, 1.1318437761748215, 5.5271509852418275] km/s
|
|
||||||
V∞_out: [1.5500163131788576, 3.701161902600424, 4.7781830264083816] km/s
|
|
||||||
time of flight: 1.2506637578161152e7 seconds
|
|
||||||
arrival date: 2023-09-29T20:19:38.742
|
|
||||||
thrust profile: [0.0037642309356178496 0.10817195619205817 -0.04203391806942476; 0.05018542722531452 0.011132758502156382 -0.0707574733140089; 0.01498586447762501 0.05712165647482545 -0.10331663549941099; -0.0021220081754707142 0.0427284404881686 -0.10738096661568876; 0.013851176936053975 0.06635540579133767 -0.11531028068050167; -0.03624664271973954 0.047411452014984014 -0.11058601864180033; -0.0020740631910354575 -4.710072118612996e-6 -0.1403320235583719; 0.004134084837005339 0.057833143727503075 -0.148726306245634; -0.000824882662939474 0.025545600899810554 -0.15811601473591735; 0.0033733625666936226 0.04310334955731879 -0.16265530338633763; 0.023284082987077983 0.07815514642145437 -0.14787129186662162; 0.011438920106420706 0.06298800208929839 -0.17089396585927522; -0.0028167264681480965 0.07221556852886035 -0.1682949193772566; 0.023003412445979414 0.07615232250394104 -0.12486622266414714; 0.05055936441931101 0.05061773551323538 -0.15558369926288854; 0.046376273514580145 0.05443645190395452 -0.15984218654287824; 0.02887318678938868 0.050242274973224 -0.11451690883278194; 0.05903220624034955 0.07663020899986919 -0.08872470614243323; 0.05646442157593271 0.0236833115162622 -0.12328998635670442; 0.052708769586655 0.04647341445165668 -0.08471778910840236] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Venus
|
|
||||||
V∞_in: [5.03318023152429, 6.280182305174015, -6.060996943876664] km/s
|
|
||||||
V∞_out: [8.771878835411606, 1.7271436802598803, -4.64552460331829] km/s
|
|
||||||
time of flight: 1.2805978832351272e8 seconds
|
|
||||||
arrival date: 2027-10-21T00:29:26.742
|
|
||||||
thrust profile: [0.5166054641522004 0.38040574934818894 0.39483837842584535; 0.4828952263457908 -0.47829862312158744 0.40557553493743564; 0.6185006656113567 -0.4295308551988002 -0.3475134331936448; 0.4770039152011964 0.5271154524060135 -0.20000575030699538; 0.5412450144942943 -0.20886043145622096 0.43938036856081814; 0.5276789680667877 -0.5277616228639487 0.13628061369394617; 0.6415309466397165 -0.2678331791426979 -0.39558929497740725; 0.4343573860170071 0.502582921064376 -0.3318784701248486; 0.5800947529139152 -0.20204579937793274 0.3774150731579229; 0.5354834813587176 -0.4173102990305924 0.3796235568137587; 0.6184505220409655 -0.4417968378543587 -0.34238794209436774; 0.5080341201037585 0.5014345398019467 -0.33763169791467246; 0.5877098153802596 0.14114025736151312 0.3238083516450284; 0.5805187604081549 0.03982949798901487 0.38515870224511417; 0.5643130843803069 -0.5179163072176047 -0.19901273562840677; 0.618939895817285 0.389447844276657 -0.39925503596953016; 0.5411273409128876 0.3226806107049277 -0.37714997177083703; 0.6071744258656793 0.2911843912661802 0.28415164075125104; 0.5573265691088601 0.17823434208894331 0.4018394191685452; 0.5666337146024757 -0.5288498735192672 0.03819884543376086] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [0.7405450398567593, -7.5098445542472945, -2.40833325065344] km/s
|
|
||||||
V∞_out: [-3.959320578944167, 5.7458190962386, -3.749068046202953] km/s
|
|
||||||
time of flight: 1.421097770757432e8 seconds
|
|
||||||
arrival date: 2032-04-21T19:25:43.742
|
|
||||||
thrust profile: [0.6668749885535331 0.7119439515000974 -0.47217742545747104; -0.6469564667143733 0.7765188128496617 0.1574004795502485; -0.773633525867842 0.7394373999282712 0.4027317982639249; -0.8166053790607609 0.6473990001925622 0.5207562510569261; -0.8373014340476008 0.18359240688570228 0.5993895358042353; -0.8390303451637329 -0.42462892361099186 0.6142766346586279; -0.8350359388066501 -0.6239649730883396 0.6256719643517975; -0.821756634573213 -0.7144142912083659 0.6297147364166188; -0.7958608968982823 -0.7601769494789784 0.6210466135863127; -0.7510364885805915 -0.7850808235066821 0.5966784108754225; -0.6657999775087994 -0.7894095061990805 0.5609708009540707; -0.5101942765778178 -0.7782021262749327 0.5141768423449582; -0.27236357899533525 -0.7487127433927561 0.4618021651904532; -0.054244989960793334 -0.6945361755047911 0.4108890323914806; 0.025980362043212305 -0.6152046918846878 0.35533971599792835; 0.03884979852161373 -0.5000474202661694 0.3091329458166366; 0.0001114281549689611 -0.3447827035482281 0.256908008578505; -0.045624236967968704 -0.10554833156388801 0.20144441453096268; -0.09710696728868398 0.19152555422247225 0.1087766532370442; -0.1282579442088115 0.39646864777852725 0.009236041193641553] %
|
|
||||||
Phase 4:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-4.741234768251964, 4.13190320501828, -0.5695428106723406] km/s
|
|
||||||
V∞_out: [-3.1515712454769806e-6, 5.189115178770385e-6, -1.6627213931492873e-7] km/s
|
|
||||||
time of flight: 1.8121908456931648e8 seconds
|
|
||||||
arrival date: 2038-01-18T06:03:47.742
|
|
||||||
thrust profile: [0.13625040297481736 0.14933905804631312 0.2757743121789037; 0.1192604239518539 0.14450577052892158 0.21001652823369818; 0.09497180738630677 0.1436206134610816 0.1304125477411028; 0.05660650818705413 0.14397646798764285 0.029638921674881153; 0.0033026815164827928 0.128393265450669 -0.08364054831257349; -0.046298739509475266 0.09498117676572271 -0.17204312101516736; -0.07826400300811034 0.05748675105859162 -0.23458089715837857; -0.0898822681455277 0.026068150966949772 -0.27381493027410114; -0.08817956687074757 0.003963795201985765 -0.29324311165103717; -0.08006421778460109 -0.010427589988313526 -0.297505213206217; -0.06850428258195482 -0.019821792080172117 -0.2909679340025451; -0.055774010972997286 -0.02726836207051607 -0.2762869825770171; -0.04157864032693081 -0.03339735152686053 -0.25548472609696515; -0.02660891319542901 -0.03894896063483435 -0.22960782433619792; -0.010643007042148598 -0.04490858196263294 -0.19956755059053796; 0.00580413466562435 -0.05025272650756578 -0.16582165226689483; 0.022646438724084665 -0.055672928642956324 -0.12919013606158447; 0.03956702474738428 -0.06069755736325737 -0.09167033305435902; 0.0569563523141951 -0.06556824149960896 -0.053646667488796825; 0.07561851012706877 -0.0723267563955561 -0.016753115096183893] %
|
|
||||||
|
|
||||||
Mass Used: 2137.3878774591703 kg
|
|
||||||
Launch C3: 35.71538607037856 km²/s²
|
|
||||||
||V∞_in||: 6.31476921482568 km/s
|
|
||||||
File diff suppressed because one or more lines are too long
@@ -1,91 +0,0 @@
|
|||||||
archive/EVVJS_archive
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2024-06-24T03:41:10.468
|
|
||||||
Launch V∞: [-2.5086977090763227, -5.909009701214558, -3.6145624632193294] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Venus
|
|
||||||
V∞_in: [-8.641740181450986, -2.7358765971708188, 5.979083178622357] km/s
|
|
||||||
V∞_out: [-8.782585218349974, -2.7633891948741853, 5.757128066064576] km/s
|
|
||||||
time of flight: 1.3058425505068028e8 seconds
|
|
||||||
arrival date: 2028-08-13T13:05:25.468
|
|
||||||
thrust profile: [-0.7066166088184461 0.694440248124216 0.7479354980537709; -0.6327447429640423 -0.8354350485844262 0.7834527345864157; 0.9020568747016394 0.8877052626244303 -0.6463263227561554; -0.7301431150683071 0.6609966418814177 -0.7438889151598259; 0.730852451440183 -0.7320972842184537 0.7604738505723868; 0.7972709043563252 0.721855932933707 0.7718028396811908; -0.8037412340829777 0.8087516989811351 -0.7172943955497878; 0.7648238186384819 0.6552635836307407 -0.721155847669259; 0.7291150156338002 0.748678684325491 0.7866560258556328; -0.7570680522417093 0.7690073045139784 -0.6461755325555683; -0.6468702385091074 -0.8148737116229223 -0.7704229798858344; -0.4993264506198249 0.7454968352904051 0.7338556974594883; 0.7368764981991002 -0.6117948959055127 0.8068497932656402; -0.7962857723296427 0.7491959753561124 -0.654565239742625; -0.7127612827380243 0.6906152690232072 -0.77926816829975; -0.6834549942628344 -0.7126511442816399 0.7270169479529096; 0.6623991589464917 -0.6788349696325189 0.817241726963756; 0.7045461026526441 0.6832122117875238 -0.6923017984092904; -0.7118848172229095 0.6940290158932474 -0.7555659392711116; -0.6684106313303576 -0.695492267513801 0.7927961883463502] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Venus
|
|
||||||
V∞_in: [-7.955987785349071, -1.7429230646850489, 7.048560055803307] km/s
|
|
||||||
V∞_out: [-8.38468808776243, 4.638807911180807, 4.920220822386981] km/s
|
|
||||||
time of flight: 3.903384248532212e7 seconds
|
|
||||||
arrival date: 2029-11-08T07:49:27.468
|
|
||||||
thrust profile: [0.35184470451251054 -0.3489438480396312 0.22003829255796042; 0.5775112094730798 0.3466350775731712 0.10768869846318309; 0.5151690947404881 0.6922646119099484 -0.2079306947550997; 0.03820729926768738 0.7645099364102405 -0.003934023466790116; -0.5310966588437559 0.6960577720418427 -0.2806379441488921; -0.4888319757324884 0.6421514470556614 -0.3174191597815846; -0.34372723910767994 0.6560895563596227 -0.16929444361647178; -0.3645888618705135 0.634917562387229 0.1666892583656993; -0.3850511801341504 0.7324174772643002 0.5376102954603407; -0.6275951088762817 0.7623544346482719 0.6418628750791122; -0.7919929569477481 0.5902287990856233 0.45549206134198506; -0.793859142829226 -0.27621743364089885 -0.03426934297306585; -0.6072979328607674 -0.6138362647581398 -0.4816955133844994; 0.13432682697115447 -0.5431982957931105 -0.6262239404967714; 0.5688082709851283 -0.21021884608354516 -0.5260160342268195; 0.6818162423845489 0.5160256516002725 -0.4092906774489981; 0.7130018091756617 0.7341633847919329 -0.15724287718021424; 0.6616897627009751 0.8195554298912001 0.3135759308050811; 0.1872587594296505 0.8726717894768014 0.6224150121537937; -0.6414995880519144 0.8901062055995407 0.7300574454135067] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [3.616389218491424, -5.528555297073314, 2.6454669550732093] km/s
|
|
||||||
V∞_out: [-4.714476188428925, 3.7327085648268112, 3.805565087766136] km/s
|
|
||||||
time of flight: 1.0083979624306786e8 seconds
|
|
||||||
arrival date: 2033-01-18T10:52:43.468
|
|
||||||
thrust profile: [-0.9659103696906655 0.9517515910607882 0.8168373781737548; -0.9561283643434136 -0.8761699655545768 -0.1939995320784213; -0.9275867912262411 -0.9136864536027992 -0.4060037610832777; -0.8853757072400111 -0.9132743466476493 -0.3994899790867979; -0.8271257223116684 -0.9063668321809316 -0.341644963512146; -0.7251990654980359 -0.8962396229655277 -0.2630714822249463; 0.18838507258195641 -0.8860877807707359 -0.15307132464698348; 0.6622301460691353 -0.8684657561454765 0.07422800726056446; 0.6152410169116248 -0.8481784036097828 0.2658920782241131; 0.6215425470318906 -0.8230726802555173 0.32667501700810464; 0.6389070189564778 -0.7921065374330535 0.34021110523295184; 0.6318769085000678 -0.7547402247270236 0.3362004802720032; 0.616705490069356 -0.708911815572844 0.32003622824074046; 0.5945544151167129 -0.6524425628293116 0.29334179519703246; 0.5663787104667805 -0.5830242242373314 0.2574479200400718; 0.5347064309525714 -0.49844216424182536 0.2142037683145213; 0.4986839302662462 -0.39909400732377337 0.16566817479325446; 0.45286850381956695 -0.28918436173239803 0.1141785086594864; 0.37710967383789334 -0.1678572767236383 0.06149121277195424; 0.25394438978570527 0.02043569238203405 0.009191155783547409] %
|
|
||||||
Phase 4:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-3.2880012796332987, 2.1211606572569277, 0.48142650562617806] km/s
|
|
||||||
V∞_out: [-8.731880472477191e-6, 9.666612310001054e-6, -6.225039409550941e-7] km/s
|
|
||||||
time of flight: 2.1161982067082927e8 seconds
|
|
||||||
arrival date: 2039-10-03T18:09:43.468
|
|
||||||
thrust profile: [0.022423037123395814 0.08059850157352823 -0.1327356604236625; 0.01554844506706407 0.07575167965809157 -0.08215431382545887; 0.004436644366473565 0.0665844137373235 -0.028828351796870644; -0.008131707121939417 0.055075456865770506 0.017731675612583327; -0.02018941938325407 0.045096951581116415 0.06687637224142223; -0.02543873854159729 0.02905260962667718 0.11099986430188423; -0.022683647304998084 0.014600108269522964 0.14240131923790691; -0.01635725372584873 0.005199870254546869 0.1603574566237192; -0.009646680596205824 -0.0005145097922692435 0.16718880257957977; -0.0034057298966922184 -0.0044319774679023915 0.16564089244298724; 0.0024575970566733775 -0.007624658692633722 0.15799198592156033; 0.008185905684027191 -0.010539011665542544 0.14597553943022623; 0.013987314799160704 -0.013330717852839631 0.13093216092661572; 0.020037882876062143 -0.01605336859123858 0.11391525190686709; 0.02646489450515348 -0.018721137962794496 0.09575475738764945; 0.033373123348953045 -0.021357123294403972 0.07717404261022846; 0.04100633524272448 -0.02409647883011826 0.05884172751529372; 0.04996375895080879 -0.02726627285470597 0.041127114982092414; 0.061081932228138576 -0.031206207742307278 0.02360571733260185; 0.07466681359328371 -0.03585261547468276 0.005215821732814806] %
|
|
||||||
|
|
||||||
Mass Used: 2591.3951917643953 kg
|
|
||||||
Launch C3: 54.27502164508673 km²/s²
|
|
||||||
||V∞_in||: 3.9423402223912998 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
---------------------------
|
|
||||||
Spacecraft: mySat
|
|
||||||
dry_mass: 200.0 kg
|
|
||||||
specific impulse: 3200.0 kg/s
|
|
||||||
max_thrust: 0.00025 kN
|
|
||||||
num_thrusters: 1
|
|
||||||
duty_cycle: 1.0
|
|
||||||
Launch Mass: 3500.0 kg
|
|
||||||
Launch Date: 2023-05-08T02:15:41.742
|
|
||||||
Launch V∞: [-2.6705377464328075, 1.81220401477148, -5.02986389717478] km/s
|
|
||||||
Phase 1:
|
|
||||||
Planet: Venus
|
|
||||||
V∞_in: [-2.6649059053371618, 1.1318437761748215, 5.5271509852418275] km/s
|
|
||||||
V∞_out: [1.5500163131788576, 3.701161902600424, 4.7781830264083816] km/s
|
|
||||||
time of flight: 1.2506637578161152e7 seconds
|
|
||||||
arrival date: 2023-09-29T20:19:38.742
|
|
||||||
thrust profile: [0.0037642309356178496 0.10817195619205817 -0.04203391806942476; 0.05018542722531452 0.011132758502156382 -0.0707574733140089; 0.01498586447762501 0.05712165647482545 -0.10331663549941099; -0.0021220081754707142 0.0427284404881686 -0.10738096661568876; 0.013851176936053975 0.06635540579133767 -0.11531028068050167; -0.03624664271973954 0.047411452014984014 -0.11058601864180033; -0.0020740631910354575 -4.710072118612996e-6 -0.1403320235583719; 0.004134084837005339 0.057833143727503075 -0.148726306245634; -0.000824882662939474 0.025545600899810554 -0.15811601473591735; 0.0033733625666936226 0.04310334955731879 -0.16265530338633763; 0.023284082987077983 0.07815514642145437 -0.14787129186662162; 0.011438920106420706 0.06298800208929839 -0.17089396585927522; -0.0028167264681480965 0.07221556852886035 -0.1682949193772566; 0.023003412445979414 0.07615232250394104 -0.12486622266414714; 0.05055936441931101 0.05061773551323538 -0.15558369926288854; 0.046376273514580145 0.05443645190395452 -0.15984218654287824; 0.02887318678938868 0.050242274973224 -0.11451690883278194; 0.05903220624034955 0.07663020899986919 -0.08872470614243323; 0.05646442157593271 0.0236833115162622 -0.12328998635670442; 0.052708769586655 0.04647341445165668 -0.08471778910840236] %
|
|
||||||
Phase 2:
|
|
||||||
Planet: Venus
|
|
||||||
V∞_in: [5.03318023152429, 6.280182305174015, -6.060996943876664] km/s
|
|
||||||
V∞_out: [8.771878835411606, 1.7271436802598803, -4.64552460331829] km/s
|
|
||||||
time of flight: 1.2805978832351272e8 seconds
|
|
||||||
arrival date: 2027-10-21T00:29:26.742
|
|
||||||
thrust profile: [0.5166054641522004 0.38040574934818894 0.39483837842584535; 0.4828952263457908 -0.47829862312158744 0.40557553493743564; 0.6185006656113567 -0.4295308551988002 -0.3475134331936448; 0.4770039152011964 0.5271154524060135 -0.20000575030699538; 0.5412450144942943 -0.20886043145622096 0.43938036856081814; 0.5276789680667877 -0.5277616228639487 0.13628061369394617; 0.6415309466397165 -0.2678331791426979 -0.39558929497740725; 0.4343573860170071 0.502582921064376 -0.3318784701248486; 0.5800947529139152 -0.20204579937793274 0.3774150731579229; 0.5354834813587176 -0.4173102990305924 0.3796235568137587; 0.6184505220409655 -0.4417968378543587 -0.34238794209436774; 0.5080341201037585 0.5014345398019467 -0.33763169791467246; 0.5877098153802596 0.14114025736151312 0.3238083516450284; 0.5805187604081549 0.03982949798901487 0.38515870224511417; 0.5643130843803069 -0.5179163072176047 -0.19901273562840677; 0.618939895817285 0.389447844276657 -0.39925503596953016; 0.5411273409128876 0.3226806107049277 -0.37714997177083703; 0.6071744258656793 0.2911843912661802 0.28415164075125104; 0.5573265691088601 0.17823434208894331 0.4018394191685452; 0.5666337146024757 -0.5288498735192672 0.03819884543376086] %
|
|
||||||
Phase 3:
|
|
||||||
Planet: Jupiter
|
|
||||||
V∞_in: [0.7405450398567593, -7.5098445542472945, -2.40833325065344] km/s
|
|
||||||
V∞_out: [-3.959320578944167, 5.7458190962386, -3.749068046202953] km/s
|
|
||||||
time of flight: 1.421097770757432e8 seconds
|
|
||||||
arrival date: 2032-04-21T19:25:43.742
|
|
||||||
thrust profile: [0.6668749885535331 0.7119439515000974 -0.47217742545747104; -0.6469564667143733 0.7765188128496617 0.1574004795502485; -0.773633525867842 0.7394373999282712 0.4027317982639249; -0.8166053790607609 0.6473990001925622 0.5207562510569261; -0.8373014340476008 0.18359240688570228 0.5993895358042353; -0.8390303451637329 -0.42462892361099186 0.6142766346586279; -0.8350359388066501 -0.6239649730883396 0.6256719643517975; -0.821756634573213 -0.7144142912083659 0.6297147364166188; -0.7958608968982823 -0.7601769494789784 0.6210466135863127; -0.7510364885805915 -0.7850808235066821 0.5966784108754225; -0.6657999775087994 -0.7894095061990805 0.5609708009540707; -0.5101942765778178 -0.7782021262749327 0.5141768423449582; -0.27236357899533525 -0.7487127433927561 0.4618021651904532; -0.054244989960793334 -0.6945361755047911 0.4108890323914806; 0.025980362043212305 -0.6152046918846878 0.35533971599792835; 0.03884979852161373 -0.5000474202661694 0.3091329458166366; 0.0001114281549689611 -0.3447827035482281 0.256908008578505; -0.045624236967968704 -0.10554833156388801 0.20144441453096268; -0.09710696728868398 0.19152555422247225 0.1087766532370442; -0.1282579442088115 0.39646864777852725 0.009236041193641553] %
|
|
||||||
Phase 4:
|
|
||||||
Planet: Saturn
|
|
||||||
V∞_in: [-4.741234768251964, 4.13190320501828, -0.5695428106723406] km/s
|
|
||||||
V∞_out: [-3.1515712454769806e-6, 5.189115178770385e-6, -1.6627213931492873e-7] km/s
|
|
||||||
time of flight: 1.8121908456931648e8 seconds
|
|
||||||
arrival date: 2038-01-18T06:03:47.742
|
|
||||||
thrust profile: [0.13625040297481736 0.14933905804631312 0.2757743121789037; 0.1192604239518539 0.14450577052892158 0.21001652823369818; 0.09497180738630677 0.1436206134610816 0.1304125477411028; 0.05660650818705413 0.14397646798764285 0.029638921674881153; 0.0033026815164827928 0.128393265450669 -0.08364054831257349; -0.046298739509475266 0.09498117676572271 -0.17204312101516736; -0.07826400300811034 0.05748675105859162 -0.23458089715837857; -0.0898822681455277 0.026068150966949772 -0.27381493027410114; -0.08817956687074757 0.003963795201985765 -0.29324311165103717; -0.08006421778460109 -0.010427589988313526 -0.297505213206217; -0.06850428258195482 -0.019821792080172117 -0.2909679340025451; -0.055774010972997286 -0.02726836207051607 -0.2762869825770171; -0.04157864032693081 -0.03339735152686053 -0.25548472609696515; -0.02660891319542901 -0.03894896063483435 -0.22960782433619792; -0.010643007042148598 -0.04490858196263294 -0.19956755059053796; 0.00580413466562435 -0.05025272650756578 -0.16582165226689483; 0.022646438724084665 -0.055672928642956324 -0.12919013606158447; 0.03956702474738428 -0.06069755736325737 -0.09167033305435902; 0.0569563523141951 -0.06556824149960896 -0.053646667488796825; 0.07561851012706877 -0.0723267563955561 -0.016753115096183893] %
|
|
||||||
|
|
||||||
Mass Used: 2137.3878774591703 kg
|
|
||||||
Launch C3: 35.71538607037856 km²/s²
|
|
||||||
||V∞_in||: 6.31476921482568 km/s
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
36
archive/best/long_mission
Normal file
36
archive/best/long_mission
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29
archive/best/short_mission
Normal file
29
archive/best/short_mission
Normal file
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22
archive/non_saturn/EJ_2022-02-20T15:35:42.756/mission
Normal file
22
archive/non_saturn/EJ_2022-02-20T15:35:42.756/mission
Normal file
@@ -0,0 +1,22 @@
|
|||||||
|
/home/connor/projects/thesis/archive/EJ_2022-02-20T15:35:42.756/mission---------------------------
|
||||||
|
|
||||||
|
Spacecraft: bepi
|
||||||
|
dry_mass: 2000.0 kg
|
||||||
|
specific impulse: 2800.0 kg/s
|
||||||
|
max_thrust: 0.0005 kN
|
||||||
|
num_thrusters: 2
|
||||||
|
duty_cycle: 0.9
|
||||||
|
Launch Mass: 4000.0 kg
|
||||||
|
Launch Date: 2027-05-07T16:42:16.204
|
||||||
|
Launch V∞: [1.7378678187417211, -2.46862158520496, -0.6330916686471314] km/s
|
||||||
|
Phase 1:
|
||||||
|
Planet: Jupiter
|
||||||
|
V∞_in: [-7.0779894637956104, -6.322884251065928, 0.08249231159415504] km/s
|
||||||
|
V∞_out: [-9.886721268095892e-5, -5.2044547868849095e-5, -1.4279616788653462e-7] km/s
|
||||||
|
time of flight: 9.753480002947423e7 seconds
|
||||||
|
arrival date: 2030-06-09T13:42:16.204
|
||||||
|
thrust profile: [0.3496133127402798 0.21627658848562392 -0.09375257020030825; 0.33049519901462543 0.4914216730807561 -0.04333085534469271; 0.015695434994927256 0.6376829912952088 -0.010776108385759698; -0.44272307995336146 0.6725191353780019 0.02401109287371488; -0.6273162232623738 0.6534499707573249 0.04855355942035699; -0.7062446552268619 0.5648886015889624 0.06359834741284556; -0.7337027908428936 0.34137315135163543 0.06893276201071429; -0.7263479369913934 -0.04280550187252788 0.06504582329795826; -0.6907323077547943 -0.29916252254363473 0.05655854617201239; -0.6304099965747246 -0.39539357580226175 0.04777470251604466; -0.546644598339376 -0.41045795909146016 0.03986867238422301; -0.4449769658797206 -0.3791551577739326 0.03302815362892815; -0.3343801111760648 -0.3170155537328812 0.027015156520834947; -0.22238014374440118 -0.2330409572673364 0.021363765089885373; -0.113202981166323 -0.1334888611558203 0.015342498857529623; -0.017481222034237697 -0.026432427062662682 0.0036199536612145674; 0.00010928351095286555 -0.0017246713395881355 -0.002344486658782495; 0.0003606569072872833 0.0017587019964605832 -0.00047445201553678664; 0.0018193454249226754 0.0015129170111366306 0.0008999344832791579; 0.08640210944237164 0.058949618519573616 0.004429993495706424] %
|
||||||
|
|
||||||
|
Mass Used: 1720.4129974933717 kg
|
||||||
|
Launch C3: 9.515082147268366 km²/s²
|
||||||
|
||V∞_in||: 9.491238332454378 km/s
|
||||||
30
archive/non_saturn/EJ_2022-02-20T15:35:42.756/plot.html
Normal file
30
archive/non_saturn/EJ_2022-02-20T15:35:42.756/plot.html
Normal file
File diff suppressed because one or more lines are too long
Some files were not shown because too many files have changed in this diff Show More
Reference in New Issue
Block a user