23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EM_2022-03-29T21:46:54.102/mission---------------------------
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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: 2024-11-11T17:47:11.536
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Launch V∞: [-2.637789291564701, 7.365806125093766, 1.1946168639279173] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-0.044388255339722446, 0.05279424355864281, 0.05040248633053719] km/s
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V∞_out: [-0.014690038570962082, 6.047928149069252, 0.0402218040709599] km/s
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time of flight: 9.338400004077721e6 seconds
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arrival date: 2025-02-27T19:47:11.536
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thrust profile: [4.550817449124052e-7 7.763476095695704e-6 -8.951834889878114e-5; -1.683989066220231e-5 6.926242475714976e-5 -2.8801022778955843e-6; -3.2857446755970286e-5 0.000111131319945128 5.116462056209784e-6; -1.8729031546388233e-5 5.436146435025702e-5 8.422047807261321e-5; -3.937488649940267e-5 0.00012696227955243206 -8.532134224201484e-5; -1.0059863865866885e-5 2.4658136117281536e-5 -1.684375841787375e-5; 4.906742377377519e-5 -0.00012829316592757872 0.00011336735200215563; 2.089328062485444e-5 -4.091796173674061e-5 4.91054297730873e-5; 3.6303103564460345e-6 -8.192507389662463e-6 0.00018463100624064758; 9.183017844786658e-5 -0.000102961513685098 -2.2996942742832565e-5; -3.570454906404795e-6 7.063475253086773e-7 4.489457323974194e-5; 4.501722144285221e-6 -1.4070298502410475e-5 0.00012324041685903012; -1.7478055220611036e-6 2.873220524346435e-5 -0.0002474631986841141; -2.3178341505326345e-7 6.162662443854e-5 -0.00036775871159988626; 5.113474717292926e-6 0.00011622972164925676 -6.003368153265286e-5; 3.496467618704115e-6 2.008310733865503e-6 -3.261195379666672e-5; 7.630237920042993e-6 1.1841800841292385e-5 -5.3531357169394734e-5; -2.435474741947106e-5 -3.088566762921298e-5 8.568030368819686e-5; 2.05686426229734e-5 2.1197875883934535e-5 -3.1608864977248355e-5; 2.6389349541919505e-5 2.927984365861755e-5 9.508078462673436e-6] %
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Mass Used: 0.00865322013714831 kg
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Launch C3: 62.64014167074321 km²/s²
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||V∞_in||: 0.08542809838298922 km/s
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