23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5614608961885532---------------------------
|
|
|
|
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: 2024-05-14T07:40:20.228
|
|
Launch V∞: [7.864483067658958, -5.974872526801592, 0.16036249202376568] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0009535707929193492, 0.0006957847904599901, 0.040207687524084434] km/s
|
|
V∞_out: [-0.03743534779283364, -0.013258244718051116, 0.0062480586680111845] km/s
|
|
time of flight: 1.812172701667921e8 seconds
|
|
arrival date: 2030-02-09T17:48:10.228
|
|
thrust profile: [0.22287493876829714 -0.012347534662237508 -0.07568611169450046; 0.10892613767767129 0.05265398806698712 -0.1284023726381088; 0.06272123324130995 0.048023707759845866 -0.13051178683645204; 0.031201968791871842 0.03006794263700194 -0.09504753302137954; 0.022960395487553683 0.028037504240320844 -0.09338511509766534; 0.013404351298524507 0.019396098528240927 -0.07229853959850994; 0.012641942980063785 0.017345690263914235 -0.07528191242917842; 0.019378797463869845 0.031625428739002884 -0.13542690825106596; 0.002768189088927419 0.007225357767934706 -0.04600438777730141; 0.003080937847615102 0.0032714591389976957 -0.015437164536230433; 0.003074686582232716 0.00020869771963046176 -0.0023835602029459576; -0.0011852915336412078 0.0030038014175936554 -0.0012012474369562653; 0.00014641400494971564 9.719661673115814e-5 -0.000889322188238598; 0.0026054626856251506 -0.0013892121622620258 0.0014332831251515528; 0.008615577059132535 -0.003284121211657498 -0.000977122627997986; -0.002986608822690303 -0.0030788609361262105 0.003312326562161034; -0.0013268377815343698 -0.00014457500082940204 -0.0013844950356199158; -0.0002852464147096158 -0.0038099176187281784 0.009222001191824612; -0.0028634713927664325 0.0031446054227571626 0.012133957828215303; 0.0030262013908753096 -0.0009485781830451149 0.011555072690742227] %
|
|
|
|
Mass Used: 85.85072694239807 kg
|
|
Launch C3: 97.57491176187098 km²/s²
|
|
||V∞_in||: 0.04022501149491643 km/s
|