23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EM_2022-03-29T22:02:40.626/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: 2024-12-05T12:41:35.605
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Launch V∞: [0.34208345982054794, 9.685722102267114, 1.0135726196799333] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-1.044189695816697, 5.606992695460721, 0.6669749140025341] km/s
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V∞_out: [-1.663147851968031, 4.139628155579746, 0.7399548282520139] km/s
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time of flight: 1.1581200001669213e7 seconds
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arrival date: 2025-04-18T13:41:35.605
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thrust profile: [-4.6079105664078877e-5 -0.00012331290696458524 3.857290588633784e-5; 1.080629253868903e-5 -7.862558725402423e-5 -1.577782579822753e-5; 0.00012294508889228685 0.0001157766111977547 -7.561217621375722e-5; 7.982229075851814e-5 -3.220285538923316e-5 -4.4317366310939693e-5; -2.379024823156827e-5 -7.848301760916924e-5 1.0173976438826385e-5; -5.0258317369872474e-5 -9.493318759847104e-5 2.0214040124684093e-5; -5.091418646156128e-5 -0.0001217205174737956 1.2898657418352046e-5; 2.8918514216456975e-6 4.8713183689657356e-5 8.218982364067898e-7; -7.013970277251351e-5 0.00016984599894599242 4.472426555147454e-5; 4.101982487628375e-5 -0.00014567448690259096 -4.20309304000344e-5; -4.70029927248979e-5 -8.284004507475568e-5 1.8925597178656232e-5; 8.670365778542101e-5 7.723828389414057e-5 -4.728960557142774e-5; -1.1273042710496325e-5 1.5796318007177794e-6 1.004719027628209e-5; 1.156788959809497e-5 -9.12107530024284e-5 -4.421958910455016e-5; 5.8489607768559684e-5 -3.186318691478282e-5 -7.568690979128904e-5; -4.101390839132036e-5 -6.912092662580811e-5 1.875683893727222e-5; -9.282793252271017e-5 1.8581365311066747e-5 0.0001607242504965489; 2.5608653889505896e-5 2.5749263651290097e-5 -2.663654795135107e-5; 6.471735913709624e-6 -1.582848279061017e-5 -3.144105357929748e-5; -2.0418356210322056e-5 -5.206011476136069e-5 1.0750219832116774e-6] %
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Mass Used: 0.009526397249373986 kg
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Launch C3: 94.95756319119332 km²/s²
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||V∞_in||: 5.742260421097979 km/s
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