23 lines
2.1 KiB
Plaintext
23 lines
2.1 KiB
Plaintext
/home/connor/projects/thesis/archive/EM_2022-03-29T21:58:30.321/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: 2024-12-10T18:17:03.345
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Launch V∞: [-0.22142913746497983, 8.613702367564114, 0.395646369589788] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-0.003807700964755288, -0.05635954129158412, -0.008059749565666045] km/s
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V∞_out: [-0.004673762071972183, 0.023969198600263253, 0.0032827185153388007] km/s
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time of flight: 2.211840042633046e7 seconds
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arrival date: 2025-08-23T18:17:03.345
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thrust profile: [-2.7099961488351806e-5 -1.4871074056565297e-5 -2.4409683044127975e-5; 9.646611740529691e-6 -0.0003420396277143331 -1.4868108643254946e-5; 2.133935422770787e-5 -4.4306217453697985e-6 -4.803508959276009e-5; 2.4459845792704493e-5 -3.6995123289765117e-5 -2.9925040076576046e-5; -3.650950167903471e-6 -7.838803352580581e-5 2.4747499455879648e-5; -6.523041671648795e-5 3.5087934323253556e-6 -2.4005599476677803e-5; 2.5824401386028627e-5 -5.305113471826212e-5 4.630647640937965e-5; 3.106981203665597e-5 3.544948660180863e-5 5.523446183421823e-5; 5.22286273436312e-5 0.000123040814806458 -0.00012676926781162037; -7.230267382777404e-5 -0.000260285686999283 0.00028378411056846934; -6.687818964937921e-5 0.00010386642943476749 -1.7433504223833023e-5; 1.628396440937132e-5 9.706470918419143e-6 -2.010464752776144e-5; 1.7691694085809603e-5 1.8769928239818888e-5 8.64374415484856e-5; -1.9940109128613944e-5 -2.4978683584950083e-5 8.154400491960929e-5; 3.746496390446149e-5 -7.996841154215747e-5 8.731190252691787e-5; 8.384626723016047e-5 0.00012055180341030887 -9.12903721447452e-5; 0.00030557244279303915 -1.0874417231438263e-5 0.00027076266521899666; 0.00010797337086871226 2.418131034629288e-6 2.46314050788356e-7; -4.8544246038547224e-5 8.023388406493804e-6 -1.3321622294600293e-6; -2.1337222473883922e-5 0.000161247930621023 -9.715049457277587e-5] %
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Mass Used: 0.024185192960430868 kg
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Launch C3: 74.4014353896677 km²/s²
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||V∞_in||: 0.05706010904560232 km/s
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