Additional display functions and section 6 draft done
This commit is contained in:
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@@ -32,3 +32,33 @@
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number={GSFC-E-DAA-TN14154},
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year={2014}
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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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\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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Give an overview of the trajectory that was ultimately chosen.
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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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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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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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\section{Mission Constraints}
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\subsection{Cost Function Analysis}
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Give some real-world context for the mass-use, time-of-flight, etc.
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The sample mission was defined to represent a general case for a near-future low-thrust
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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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I may also remove this section. I could do a quick comparison (using porkchop plots) to
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similar impulsive trajectories. Honestly, this is a lot of work for very little gain,
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though, so probably the first place to chop if needed.
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The first choice required by the application is one not necessarily designable to the
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initial mission designer (though not necessarily fixed in the design either) and is that
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of the spacecraft parameters. The application accepts as input a spacecraft object
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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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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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\section{Overview of Results}
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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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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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\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
|
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including parallelization, cluster computing, etc.
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29
archive/EJU
29
archive/EJU
@@ -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
|
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specific 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
|
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Phase 1:
|
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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
@@ -1,94 +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
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36
archive/best/long_mission
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29
archive/best/short_mission
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29
archive/best/short_mission
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22
archive/non_saturn/EJ_2022-02-20T15:35:42.756/mission
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22
archive/non_saturn/EJ_2022-02-20T15:35:42.756/mission
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@@ -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
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30
archive/non_saturn/EJ_2022-02-20T15:35:42.756/plot.html
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Some files were not shown because too many files have changed in this diff Show More
Reference in New Issue
Block a user