23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EM_2022-03-29T21:49:25.266/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: 2024-01-22T05:21:14.524
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Launch V∞: [9.999636707630842, -9.999711031426283, 0.11421476860707167] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-0.0005668718069816592, -0.00031760816291536434, -0.000716139266867567] km/s
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V∞_out: [4.602661802552677e-5, -0.0002767853386654524, -0.0009253970079822862] km/s
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time of flight: 1.8504181207751602e7 seconds
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arrival date: 2024-08-23T09:24:15.524
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thrust profile: [7.857635262435799e-9 -1.3269126706634187e-9 -2.6678444933858832e-8; -1.0637360281620793e-8 -2.286988515481341e-8 -8.80823866575928e-9; 6.0952069265027294e-9 -2.83469800266583e-8 -1.490175153809855e-8; 0.0226345802482894 -0.0425037954420528 0.00013571022638739796; 0.3150512263564853 -0.3307029057599246 6.642556817831003e-5; 0.7436637294478844 -0.4801347645399363 -0.0017893772307274593; 0.8606779112586623 -0.24141142990090325 -0.0037932113948367296; 0.8040060250257044 0.016198399857395514 -0.004471603451557433; 0.6399746211803117 0.16197029278741412 -0.0044542497883041455; 0.3727551022451268 0.16851762370795223 -0.0032249765404340643; 2.1347115495508663e-7 1.2358201767787164e-7 -9.95030121314948e-9; -3.2446413607840104e-9 -4.6723722793820385e-9 -1.7929106379494995e-8; 5.182519495541647e-9 3.4030707061963687e-9 1.3576577417457207e-9; 7.77921539082814e-9 8.910703811213887e-9 -2.795024270457183e-9; -6.239445899255738e-9 -5.3493145318475e-9 -1.0884699785346293e-8; -4.6105410818633964e-8 1.0422534641378147e-8 -3.1989587412074714e-8; -5.043811123979896e-10 -1.5735249773983739e-9 -2.485221976312311e-9; -2.9761057764991258e-9 5.873921191568738e-9 -9.103537944568155e-9; 5.14444314540825e-9 2.6244355859150998e-8 -4.4579652417185817e-8; 1.7864549904100225e-9 -5.672782066774026e-9 -8.346804698233242e-9] %
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Mass Used: 30.632832509893888 kg
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Launch C3: 200.00000000999466 km²/s²
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||V∞_in||: 0.0009669922648350091 km/s
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