23 lines
1.9 KiB
Plaintext
23 lines
1.9 KiB
Plaintext
archive/ES_0.8223919770193127---------------------------
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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: 2024-05-12T01:03:20.880
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Launch V∞: [6.2801509951060295, -7.596481191980322, -1.4228982502972005] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [0.0012490959485957826, -0.0018148272969913757, -0.00015955401289316265] km/s
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V∞_out: [0.00015721511026354297, -0.0006743307477079151, -0.0020978652650430756] km/s
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time of flight: 1.3738317137611642e8 seconds
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arrival date: 2028-09-18T03:02:51.880
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thrust profile: [0.9162355654995709 -0.4482793469074367 -0.41985438384473034; 0.09332237526449066 -0.03871729021812295 -0.2506853225145068; 0.029679371377552517 0.1609846990370001 -0.219931882404862; 0.10141792952860301 0.20317411475189331 -0.19569335230787005; 0.0822616637036831 0.28337925498381333 -0.1857424613823716; -0.04540786302972602 0.12153635091622014 -0.19162256147789575; -0.0065859491535159125 -0.10338871596740948 -0.027160882329365452; -0.20138780956077587 -0.10982488768854062 0.06960651365908122; 0.030822166457856143 -0.24987152170878557 0.13533925082301873; -0.036169265052708885 0.05064551379455824 -0.2430417595543215; -0.1473819962852825 0.13151174705740123 -0.055625314832398895; 0.07681839276358322 -0.025113484847767924 -0.1907046787228516; -0.21415788406114122 0.04746021808296784 -0.14865887295523694; -0.5671148663725925 0.038317097495083025 0.23729895528264147; 0.17382546874770097 -0.41666563399058326 0.1106879371199891; -0.01967397963235001 -0.08310868877214098 0.2073869319720012; -0.10358185239013634 0.4610527796682605 0.193278969374042; 0.41126216513024355 0.3726193971637455 0.3231740181394148; 0.026333895868209486 -0.053456767084797546 0.015165952522075657; 0.25318704793228697 0.23949412757577732 0.07441909191745669] %
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Mass Used: 380.957108885043 kg
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Launch C3: 99.17146245214087 km²/s²
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||V∞_in||: 0.002208912920360088 km/s
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