23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5943937736503155---------------------------
|
|
|
|
Spacecraft: mySat
|
|
dry_mass: 200.0 kg
|
|
specific impulse: 3200.0 kg/s
|
|
max_thrust: 0.00025 kN
|
|
num_thrusters: 1
|
|
duty_cycle: 1.0
|
|
Launch Mass: 3500.0 kg
|
|
Launch Date: 2023-04-22T19:00:55.442
|
|
Launch V∞: [5.405345204434152, -8.39581540426038, -1.339982008356526] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.06761818733937937, -0.10031035197925604, 0.01625347995389304] km/s
|
|
V∞_out: [-0.11415850372713592, 0.038287596840285876, -0.02004974517554302] km/s
|
|
time of flight: 1.3146041398495483e8 seconds
|
|
arrival date: 2027-06-22T07:47:48.442
|
|
thrust profile: [0.2814442244810004 -0.19727431277777838 -0.15029318504309855; 0.1428114095231844 -0.01898779003937858 -0.1593394831680275; 0.1424767304111736 0.009941626373755926 -0.2368382123404071; 0.1164776934716537 0.021789824289087916 -0.2538891528600108; 0.08716088123763657 0.023445373075395622 -0.23158984140690508; 0.057083382099321456 0.019381474255838905 -0.17732800435427176; 0.03121407486915182 0.012992584785223894 -0.11059731612914993; 0.006784230785919465 0.002115876094184599 -0.02589338811994058; 0.017444411306170006 0.007574245702305216 -0.07367673795836253; 0.012733199141891178 0.0068521963543271 -0.05667329002384886; 0.0009532177703154381 -0.0008485045830507728 -0.002468817452801175; -0.0006087476641691221 0.004206743747663104 -0.0014370650610811217; 1.501350638025427e-5 0.0007616797628599917 -0.00318606164562138; -0.002334177563805723 -0.00026188965877517066 -0.008185214614283566; 0.0005247158487685981 0.002141120674330426 -0.0013419953788875653; 0.0017303236690289167 0.003994578933863831 -0.0008178495031128568; -0.002087774802063465 0.008989046872220767 -0.016882862249414935; 0.0025592580551483095 0.0020494987008744516 -0.019386171163250865; -0.0069792146708415655 -0.004874287522341985 0.005854704249928239; 0.00017606281612003467 -7.904208450898215e-5 -0.001371720502722577] %
|
|
|
|
Mass Used: 101.35842421733423 kg
|
|
Launch C3: 101.50302486423438 km²/s²
|
|
||V∞_in||: 0.12205966403311638 km/s
|