Files
thesis/archive/ES_0.5927208682470759
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5927208682470759---------------------------
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: 2024-05-06T18:54:54.439
Launch V∞: [7.061042582461715, -7.137178453372955, -1.4586995624468768] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.005367311484540544, -0.004775474985884387, 0.0035871586327918315] km/s
V∞_out: [0.0032711227913015573, -0.007265749461450176, 0.0009968304259374543] km/s
time of flight: 1.2925315611987047e8 seconds
arrival date: 2028-06-10T18:34:10.439
thrust profile: [0.28730817593259794 -0.12173064542907532 -0.15294460468018303; 0.14037685833858915 0.007048286259825752 -0.17474255935319719; 0.10495674768080553 0.025943788986153515 -0.20677905110113062; 0.08335960383454288 0.030240771556268163 -0.2223521376096642; 0.05965803114816345 0.026248106785306646 -0.19783930847584089; 0.02627209079132878 0.01296022566457369 -0.1041836726746995; 0.03597363877535828 0.01880210799486713 -0.15982624742563842; 0.03191425210497097 0.01771110596343373 -0.15535256830754626; 0.006850715090216529 0.003912017561670733 -0.037467434308249926; 0.0020730830295158454 0.0014786594393280423 -0.013310334331245233; 0.002827720080480995 0.0017415262659607792 -0.017980108587537697; 0.0004598674494069141 0.0003372444818380288 -0.002519276128726075; -0.0002615232450969735 -3.683403558780925e-5 -0.0003615227605913296; 0.00039395075514035135 0.00016732454882948956 -0.0017222197973295263; 0.0007104306663171319 0.0003132901749916773 -0.0022201125582451756; -0.00020769898150766884 0.0004932158507961435 -2.8768819697484347e-5; -0.0008927349829246541 0.000985247765436753 0.0004764734362873112; -0.0016020308666608368 0.0002920687215984972 -0.00252493299927408; -0.0005494130662241775 -0.0003797877110960668 -0.0004499042024278064; 0.0001228757769877755 0.0004463490493200082 -0.0016476380709787033] %
Mass Used: 91.10926188760504 kg
Launch C3: 102.92544304011147 km²/s²
||V∞_in||: 0.008030000060379905 km/s