23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5618173409028855---------------------------
|
|
|
|
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: 2023-05-01T04:13:13.495
|
|
Launch V∞: [6.302213207145994, -7.458362533063383, 0.11517000913658623] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0015438783950462635, 0.0013820590943912495, 0.00161886493110792] km/s
|
|
V∞_out: [-0.0017953578912598526, -0.0009174697614109243, 0.0016883148169879372] km/s
|
|
time of flight: 1.8329834360011867e8 seconds
|
|
arrival date: 2029-02-19T16:25:36.495
|
|
thrust profile: [0.4431412795479208 -0.1489310387076754 -0.16793161809134644; 0.04748997546914024 0.007189405071981327 -0.05700217100364162; 0.045816628165193336 0.015681148798907776 -0.09265805125273446; 0.0635912376737072 0.028440253293418184 -0.17500339233620113; 0.05641648147765174 0.029250875552064494 -0.19504401487630746; 0.02370131744937129 0.014395833897199036 -0.10278346768205099; 0.015730819713182687 0.010175435768901923 -0.07897907738877695; 0.009019763357737446 0.0063278093325362175 -0.05235278354311539; 0.0020092256702781636 0.001541610537029651 -0.013643940302638035; 0.001869745630045114 0.0015326335502354222 -0.014481042959615897; 0.0011390246751846373 0.0008232510576358273 -0.008298147950542402; 0.00038837857370848554 0.00037260349475237096 -0.0032764393518586506; 0.00022389277015488757 -7.79476521565179e-6 -0.00041024635189926663; -0.000617090194226648 0.00047328363042460506 -0.0009864957392643771; -8.511149798592042e-6 -0.00011976969304527626 -0.0005994616755506403; 0.00021137592026628063 -0.0003642305049193831 -0.0006864332873609858; 0.0008351221184584491 -6.007165902030122e-6 -0.0008131528354183362; 0.00028770242845202075 0.00019662445369238125 -0.0010610524466105802; 0.00029724128843039974 0.0003561371531888803 -0.0016814525329756774; -0.0005123345543069711 -0.0009790303059050382 0.0003783544950813615] %
|
|
|
|
Mass Used: 99.19665622208731 kg
|
|
Launch C3: 95.35832711393356 km²/s²
|
|
||V∞_in||: 0.0026295192534475267 km/s
|