23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6408780933335794---------------------------
|
|
|
|
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: 2023-04-23T09:59:36.878
|
|
Launch V∞: [5.756301975455712, -8.741845788970608, -2.495225838119645] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.0005638064810550995, 0.010753368912733447, -0.004779010972597566] km/s
|
|
V∞_out: [-0.009194922453644581, -0.005464654472374795, 0.004961459903066318] km/s
|
|
time of flight: 1.039325367407597e8 seconds
|
|
arrival date: 2026-08-08T08:08:32.878
|
|
thrust profile: [0.393790909832668 -0.3021166430838973 -0.23917283591936614; 0.29281024924895427 -0.06528415399847465 -0.2869926863847661; 0.17078175809720142 -0.0016028043429340776 -0.23250444412783366; 0.10972571854832887 0.012162094873983766 -0.18682458518192377; 0.06340332821354275 0.01212056158993727 -0.12730315807967; 0.011693787317713486 0.0031057090777966614 -0.02827654143068637; 0.009630950271779749 0.003003075435779993 -0.02584767194352958; 0.002423937506240429 0.001717499084077537 -0.007068860957988678; 0.008651601626267123 0.0031304632609080512 -0.02549052210131559; 0.0028473323729982696 0.0012828854421875725 -0.00949515145833607; 0.0019314861975039306 0.0003595822933591442 -0.007776367096342939; 0.0012217516487069945 0.0004637842314666968 -0.004713348719995885; -0.0005445353779184061 0.00016713109951072428 -0.00034609059289157813; -3.541068042788747e-5 0.0001964962701479209 0.0016750584469734625; 0.0001908930003664568 0.0009572120780987261 0.0006765617906413172; 0.0006522437641413684 -0.0017986545735062017 0.0006704544206231317; -0.0001189205671670798 -0.00041467127580464944 -0.0011630768495742405; 0.00041869196329361865 -0.004274537295440792 0.0031367096566849925; 0.0018927926699553565 5.5046739966005626e-5 -0.0003514950512311525; 0.0006575362701309805 6.703084741485794e-6 -0.0023816127576274655] %
|
|
|
|
Mass Used: 72.30175430751888 kg
|
|
Launch C3: 115.78103221399836 km²/s²
|
|
||V∞_in||: 0.01178099174932356 km/s
|