23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EM_2022-03-29T21:49:36.826/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: 2024-05-15T10:56:11.057
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Launch V∞: [6.441902798268679, 10.0, -0.8580312930039031] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [1.1346777920325148e-7, -1.6337616718675993e-7, 1.0330204534180961e-7] km/s
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V∞_out: [-1.0317733873112507e-7, 2.3171717331048837e-6, -1.93986714938645e-8] km/s
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time of flight: 3.4632733537038654e7 seconds
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arrival date: 2025-06-20T07:08:24.057
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thrust profile: [-1.6714820918342543e-8 -1.528466539382287e-8 -2.1954025843586096e-8; -3.349740604524035e-8 1.7981805687302658e-7 -7.022649953046174e-9; 1.8833170950448843e-8 8.548553623260635e-8 -4.108646810746605e-9; 0.015250670354150446 0.8084120898285189 0.022810952919723303; -0.4471453131878308 0.9999999903024106 0.04006905981158459; -0.940578331193299 0.999999993466643 0.0463151648707486; -0.9999999926560775 0.8872505298154237 0.043065678915645736; -0.9999999865564515 0.5078822642356666 0.04002774379588722; -0.962703858267274 0.25286276492713566 0.031382869157176016; -0.7756546264427393 0.08215017131953659 0.018158411737504068; -0.5391748150704597 -0.00685832535402532 0.010123577086814562; -0.28342464446445065 -0.029810747488727737 0.006770186169348639; -1.123224049355356e-8 -1.3141710495594749e-8 -1.7542653699628666e-8; -1.7528478886241226e-7 5.358445351823748e-9 -6.699375227774894e-8; -1.3135303081170559e-7 -1.2185271425829965e-7 -3.228097411495359e-10; 1.1373627184214759e-8 3.001014188079098e-8 -2.51036875849398e-8; 3.6364423359808617e-12 -1.1453961586869118e-7 3.15681037477465e-8; -2.2731576792249495e-8 -7.140875056921905e-9 -4.234566273922648e-9; -8.105071719032486e-8 -1.2311649733884225e-7 5.2532523546505e-9; 3.7930997639741155e-9 2.2050999807275034e-9 -1.6994076482759186e-8] %
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Mass Used: 114.99761554896395 kg
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Launch C3: 142.2343293621158 km²/s²
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||V∞_in||: 2.2413839807974726e-7 km/s
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