23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5638014292518135---------------------------
|
|
|
|
Spacecraft: mySat
|
|
dry_mass: 200.0 kg
|
|
specific impulse: 3200.0 kg/s
|
|
max_thrust: 0.00025 kN
|
|
num_thrusters: 1
|
|
duty_cycle: 1.0
|
|
Launch Mass: 3500.0 kg
|
|
Launch Date: 2023-05-04T08:05:13.192
|
|
Launch V∞: [6.511881786132343, -7.5143826030996665, 0.10679567236815793] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-6.334126075107828e-7, -8.53230284888172e-8, 1.6893870652428308e-9] km/s
|
|
V∞_out: [1.0073414406031763e-7, -2.638487305454299e-9, -6.363685760733993e-7] km/s
|
|
time of flight: 1.874957778743262e8 seconds
|
|
arrival date: 2029-04-12T10:14:50.192
|
|
thrust profile: [0.20955799249075105 -0.058066443452777304 -0.08385402275581055; 0.0380358047586097 0.008375614328648508 -0.05565914559775056; 0.024590561376370862 0.009252194846292713 -0.054962385636327944; 0.024878164749512807 0.012631308984646651 -0.07661957493269071; 0.04670221386013496 0.027322035039335002 -0.1733912121903577; 0.027770816117952627 0.019632806206172675 -0.12794322493247826; 0.006972387510477282 0.004830958647519359 -0.0409034928847089; 0.01624951069172827 0.012102481036147195 -0.10275637154265335; 0.01814082704251478 0.01270997645210885 -0.11663115675081633; 0.001400732405277767 0.0007742430213033348 -0.012088788755005546; 0.0034604103481923622 0.0024878150776630912 -0.02460395879281595; 0.0006460194448323954 0.0004619239589501306 -0.004520623413113432; 0.0004066447657081252 0.0003621046110900974 -0.0027563666522430466; 0.0006014016440630107 -0.00026680914160262027 -0.0035806966687450207; -0.0009603473435551668 0.0006404362893938269 -0.0018978413273944882; 0.00027764149777333505 0.001166785415513774 0.00017504706690646583; -0.00016372065600314518 -0.0036859256451814947 -0.0032159535490964776; 0.0011578565515130168 -0.0005737519820062521 -0.00010738428085575827; -0.00011750895869174448 -8.305917376223726e-5 -0.002562291544276366; 0.0006069769336811337 0.0004171248770748182 0.001017828509518569] %
|
|
|
|
Mass Used: 80.95692635564956 kg
|
|
Launch C3: 98.88195561796564 km²/s²
|
|
||V∞_in||: 6.391356699267916e-7 km/s
|