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thesis/archive/ES_0.6034409405098868
2022-04-18 10:59:25 -06:00

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archive/ES_0.6034409405098868---------------------------
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: 2023-04-23T00:59:52.432
Launch V∞: [5.313017971391461, -8.352170320618889, -0.6818852077366573] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.09343199999865491, -0.10795817117510247, 0.023947486737157592] km/s
V∞_out: [-0.13088615781136348, -0.05736721540450638, -0.0231222563424899] km/s
time of flight: 1.3497387387884116e8 seconds
arrival date: 2027-08-02T05:44:25.432
thrust profile: [0.3999243692344135 -0.2561298160056433 -0.19755400970708287; 0.143178756974432 -0.01684581728153864 -0.15969973814354485; 0.1291197498212529 0.011145708928860503 -0.21788729372819132; 0.08326572029272203 0.015919871187915366 -0.18678585760591082; 0.0893912498280836 0.025002111005176703 -0.24070079709911588; 0.04484778833309347 0.013643391902480042 -0.1421425300056081; 0.05219547268691606 0.01931580575186822 -0.18303210067966835; 0.041298976107274524 0.017095061730501605 -0.164672578913591; 0.0066620959850750144 -6.560682574559447e-5 -0.03204559742760619; 0.0030605777876958717 0.001753369557989899 -0.006766818327989919; 0.008248537163270286 0.006625111915320178 -0.016184294213738543; 0.005309401522850924 0.006812732129915846 0.006150658661822533; 0.023961127437411273 0.015320122171649362 0.010946175629643852; 0.04956289785106356 0.02935935998376863 -0.03854862716359985; 0.022608926893061817 -0.0038428473121193993 -0.029363605204673168; 0.0015286073944890432 0.009476990217424671 -0.0005599467934834365; 0.003374272942006291 0.02889251794354967 -0.049496265950256274; 0.06059650660865727 -0.023411156864094434 -0.004480068752032868; -0.041838607992111615 -0.000298454175652119 -0.02542947623789535; -0.008754154965341482 0.06541700244831933 -0.0129721285788977] %
Mass Used: 129.71181787953446 kg
Launch C3: 98.45187646548574 km²/s²
||V∞_in||: 0.14476873788303785 km/s