23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5572844554976675---------------------------
|
|
|
|
Spacecraft: mySat
|
|
dry_mass: 200.0 kg
|
|
specific impulse: 3200.0 kg/s
|
|
max_thrust: 0.00025 kN
|
|
num_thrusters: 1
|
|
duty_cycle: 1.0
|
|
Launch Mass: 3500.0 kg
|
|
Launch Date: 2024-05-14T23:19:49.220
|
|
Launch V∞: [8.108166873812628, -5.696966223751774, 0.15360538488823738] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-3.727888217316075e-7, 9.080881114338038e-7, -5.858897737422581e-7] km/s
|
|
V∞_out: [-1.224097349888263e-7, -6.558380394861945e-7, -9.315897157228473e-7] km/s
|
|
time of flight: 1.874957778740231e8 seconds
|
|
arrival date: 2030-04-24T01:29:26.220
|
|
thrust profile: [0.17707743792848335 -0.00022761593484336594 -0.054471773711166294; 0.11166966829465717 0.06277100333151206 -0.12011295783360224; 0.03335703429165077 0.03065489249064752 -0.06918782542073591; 0.0223929112079949 0.025666101205554518 -0.06778205403620138; 0.020324347204505978 0.030325886830245244 -0.08547993740452842; 0.020616546946069417 0.03753925907011939 -0.11804919842771222; 0.015326692418924263 0.030385358758053115 -0.0999451033639915; 0.004301503227668133 0.009596531556777003 -0.035405958307113454; 0.005818438574325066 0.013741082451023488 -0.054935993645659376; 0.004581277655590877 0.012652901050693706 -0.04743674721880923; 0.0022250164393832904 0.006481604037067452 -0.023011664061603692; -0.0002094600213777408 0.0003447216085417245 -0.008536032708683652; -0.0007881600896904741 5.015246146374783e-5 -0.00023527481866331005; 0.00018039055835995446 0.0003866398272000762 -9.192553647528203e-5; -0.0006897237422596791 0.00048359848796798114 4.067569797341301e-5; 0.0007312685878646296 0.0005200213406077646 0.0011493783081711509; -0.0016605820748106558 0.0010178953913932006 -0.0015951028171913941; 0.00046217995180829316 0.00039113944036722845 0.00010150296827321666; 0.0015256065445882424 0.0013697090486752038 -0.0013424793607930675; 0.0023860450474033636 0.005192207970948499 0.0002464129135628535] %
|
|
|
|
Mass Used: 77.2070966164506 kg
|
|
Launch C3: 98.22138882242767 km²/s²
|
|
||V∞_in||: 1.1431808040337307e-6 km/s
|