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archive/ES_0.5698192220056314
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archive/ES_0.5698192220056314---------------------------
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Spacecraft: mySat
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dry_mass: 200.0 kg
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specific impulse: 3200.0 kg/s
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max_thrust: 0.00025 kN
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num_thrusters: 1
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duty_cycle: 1.0
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Launch Mass: 3500.0 kg
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Launch Date: 2024-05-21T02:26:09.575
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Launch V∞: [7.903081661490054, -6.224214646638824, -0.11373027352988842] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-0.008230644344250923, 0.00416637009886815, 0.00030275570582208756] km/s
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V∞_out: [-0.00583692958734029, -0.003336991164369138, 0.006323091324544844] km/s
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time of flight: 1.8749577786936948e8 seconds
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arrival date: 2030-04-30T04:35:46.575
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thrust profile: [0.1558328382420952 -0.0006863795153885049 -0.0628050619780735; 0.06417648305351342 0.031025526719879876 -0.08677094609868904; 0.020401212154336597 0.014685537857519786 -0.05104449543532627; 0.01610397592079764 0.01447736145462221 -0.05823499675972425; 0.015950227672063094 0.01649806329178643 -0.07444828823275196; 0.017864588732396814 0.019376755473692917 -0.0984607822552028; 0.021771833535033064 0.028829819459684887 -0.14776178305297902; 0.010441880586289474 0.013994052063723953 -0.09084646897356148; 0.0062792789525638075 0.00863827391185933 -0.055535246223853564; 0.0027078109514683335 0.003505335574442602 -0.025206631375282926; 0.001963569866116637 0.003107006058660413 -0.02499557180421679; -0.0007287759940937256 0.0005261376887130784 -0.00021646771311147148; 0.0006542447127750638 -0.0005036237752344933 -0.0030721426503590448; 0.001552265371222104 0.0005263501973010456 -0.00216409044334547; 0.0005008547370580917 -0.0007328804164842246 0.004017532853813864; -0.0003058483550675889 9.055421391808872e-6 0.008711020917083104; 0.005147355008198134 -0.010234315321061935 -0.007664845727475102; 0.000905699752393287 -0.0016437908243699486 0.011724561042528673; 0.005001754135184241 0.0028451300939553534 -0.004437794384578658; -0.0037281354270525873 -0.001918940015572866 0.011798687606106998] %
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Mass Used: 74.38294564397347 kg
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Launch C3: 101.21248229073083 km²/s²
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||V∞_in||: 0.009230049140698013 km/s
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