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thesis/archive/ES_0.7217185221826274
2022-04-18 10:59:25 -06:00

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archive/ES_0.7217185221826274---------------------------
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: 2024-05-09T17:04:37.077
Launch V∞: [8.345346242874188, -7.519848609969729, -2.5136258404576908] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.1740521609394065, -0.44525516455076075, -0.660621105202349] km/s
V∞_out: [-0.7400633993357436, -0.11464260401340401, 0.3220779321862654] km/s
time of flight: 8.59116669601457e7 seconds
arrival date: 2027-01-29T01:25:43.077
thrust profile: [0.7816698724617391 -0.36300110915860506 -0.2964518231450083; 0.28614216834899475 -0.02480577158440201 -0.18936757526045625; 0.07531472229252027 0.00607876021389858 -0.07175314106340425; 0.0628213678066721 0.011084191835937233 -0.07174128627790058; 0.08230029346640327 0.01672937203476381 -0.10578781811639461; 0.050892591417045066 0.014691818259437439 -0.07345729761801863; -0.003249921414108038 0.003680059774529631 -0.01273526959172175; 0.0045990943445993575 0.0049522430697620835 -0.00808134455757978; 0.0015974862529376452 0.0006059187842077478 -0.001941908681614998; -0.002470393212151572 0.008843171210241484 -0.008539346417700672; 0.0076143082728354836 -0.00447700220994535 -0.0027909586385149064; 0.01942599847252153 -0.03209337298685755 -0.019941087876968484; 0.00397905324188275 -0.0029545790497036116 -0.005122667446074347; 0.011357236983102124 0.016344500925911866 0.027469301426784012; -0.008340879915939951 -0.03476062739578349 -0.01683279940907204; -0.006907022077164598 0.02822928324083098 0.004558432380521952; 0.06444417170740516 -0.02704405791261235 -0.014217985997752982; 0.002976752265301838 0.0016992881013452345 0.009826355613012788; -0.003176008359818395 -0.008368463378383713 0.005578671738484694; -0.020204147601380267 0.0377320261843766 -0.004935038008251156] %
Mass Used: 69.0226981522801 kg
Launch C3: 132.5112418961346 km²/s²
||V∞_in||: 0.8154548184452496 km/s