Files
thesis/archive/ES_0.6596274845816918
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.6596274845816918---------------------------
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: 2023-04-24T15:17:54.610
Launch V∞: [6.039127028256713, -8.900602779200751, -2.5826975057933694] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.012173576456573172, 0.07067652530479196, -0.08521686301849944] km/s
V∞_out: [0.06775065790440084, 0.06922326688535511, 0.05498298795326775] km/s
time of flight: 9.803159697112666e7 seconds
arrival date: 2026-06-02T06:17:50.610
thrust profile: [0.34631149250879606 -0.25415595602948177 -0.20734046993410268; 0.21791575434990593 -0.04491327850639034 -0.1960227602002975; 0.139263297385662 -0.000632780517292103 -0.1705366815979958; 0.09062639063286683 0.009227977687512847 -0.13861915554851367; 0.05420736701191884 0.009062273379227302 -0.0984507443381607; 0.02733503654309313 0.005890468043888139 -0.056681032051350104; 0.013405776856422252 0.003465923536478856 -0.030774266377485267; 0.010856548672341752 0.0031109883895629824 -0.026595437865993946; 0.0069563625013018115 0.002087317884114188 -0.017084703702443357; 0.0003514890793633001 1.9606094147211106e-5 -0.001168897408208781; 0.00031615856553718195 0.00010035011938376045 -0.0008902804843213656; 0.0011092629051121907 0.000549016950892431 -0.003227144824103683; 0.000352983753269155 -0.0003505580493247366 -0.0003902242311454305; 0.00014533433805975188 -0.0001245772729919002 -0.000614577596648248; -7.781571577729373e-6 -0.0003014232567780706 -0.0005171198019923056; 0.0003580888961847802 -0.00023743902802524173 -0.0005248518080335335; 4.169727746465893e-6 -8.641777238432689e-5 -0.00013617997840656448; -1.811452378547979e-5 6.895259594739549e-5 -0.00010649284908147464; 0.00017494621644197476 -0.00042690444825831586 -0.003224572939032363; -0.0004094184565368986 -0.00035209332287134147 -0.00040943391614112364] %
Mass Used: 55.78641491132612 kg
Launch C3: 122.36211150296819 km²/s²
||V∞_in||: 0.11137899683340943 km/s