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thesis/archive/ES_0.6399928396689094
2022-04-18 10:59:25 -06:00

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archive/ES_0.6399928396689094---------------------------
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: 2024-05-08T22:09:22.409
Launch V∞: [7.104764764806629, -7.501360442381106, -2.4061581724304753] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.06413076378031075, -0.2841596412332386, -0.47723061724743043] km/s
V∞_out: [0.1748264769676494, 0.08199165516932007, 0.5305270543125051] km/s
time of flight: 1.0343079690011168e8 seconds
arrival date: 2027-08-19T00:55:58.409
thrust profile: [1.0 -0.5472858187763153 -0.5682097146425757; 0.13517995569919478 -0.007647354433998667 -0.1564594292829399; 0.0564394448091932 0.005135243026698321 -0.09628592538705155; 0.04925882010813094 0.00989250971534181 -0.1113404276830967; 0.035902526608781134 0.00865249173440687 -0.09209439904076755; 0.027185088399229475 0.007837551006187025 -0.08292521620561133; 0.01948868666988035 0.0031295202924654917 -0.061092827717697314; 0.0034045936515255133 0.003492019005844974 -0.021164319880452268; -0.0009496198568587108 -0.0011529792571563836 -0.027076651538296033; 0.008539272155693625 0.00331596561785639 -0.03656371054530466; -0.0016515710478839998 -0.0006891950388333686 -0.0032265048588490577; -0.006800354788610324 0.008118139313851285 -0.016195792081369773; -0.003079467166086092 0.001106802704112897 -0.011646271253877615; 0.005168994044209997 0.005142622276805581 -0.013039344580445287; 0.0049689735990414785 0.01090968584760723 -0.004410398792136967; 0.002997512756236813 0.0015565082811343162 -0.015427885863858924; 0.01416809396255966 0.01248458387333928 -0.0009347024211431645; -0.013465564540197516 -0.012058128350402895 0.0024921499978176453; 0.0022494513775018 0.004457032646441996 -0.0030792786722686604; 0.002094895598723391 0.015846025466641902 0.0017059437649633697] %
Mass Used: 90.18846627740868 kg
Launch C3: 112.53768800051182 km²/s²
||V∞_in||: 0.5591140479430045 km/s