23 lines
2.1 KiB
Plaintext
23 lines
2.1 KiB
Plaintext
/home/connor/projects/thesis/archive/EM_2022-03-29T22:49:56.957/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: 2024-09-12T20:18:50.704
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Launch V∞: [-1.2901325972737976, 3.5232401246782135, -4.555427856822656] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-0.47357409467459016, 0.6120735570744102, 0.2493748383223478] km/s
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V∞_out: [-0.5474046060397546, 0.593375716049692, -0.4503838007744617] km/s
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time of flight: 2.33568000005211e7 seconds
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arrival date: 2025-06-10T04:18:50.704
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thrust profile: [-3.7741093121961535e-8 -2.6257971335176648e-8 -2.1606384855810645e-8; -2.1363083523959785e-8 -4.234571308044473e-8 -8.269824340036801e-9; -1.7179727443085232e-8 -4.817903392853783e-9 1.1405733095493886e-8; 6.543773827193354e-8 7.63399812774497e-8 3.918240890364693e-8; 1.3414420888442994e-8 1.4060087327107107e-8 -8.242716667432803e-8; -1.8088388278070475e-10 -4.1359611682043475e-10 -9.03470171888568e-9; 4.3064264083954854e-9 3.2442366380236367e-9 -1.598356883588943e-8; 3.261934834405667e-8 6.450483621536437e-8 8.2007353416575e-8; -1.7993125019529573e-8 3.862145335097065e-9 5.231141768695811e-9; 2.5346874206765178e-8 2.0165133642770633e-8 5.961057304477184e-9; -1.8904868856526572e-8 -1.201092354618878e-8 -2.4170378084370648e-8; -1.1110813643371359e-8 -9.930972424447597e-9 -2.2310217231961474e-8; -2.3010965850571813e-8 -4.590923869358927e-9 -5.082758311888812e-8; -1.064446394813755e-8 -1.6835335671720645e-8 -4.524794179174139e-8; 1.6919283931076332e-9 2.0866300176185552e-9 -1.1111279350528446e-8; -4.352351680251087e-9 -5.215082497858078e-9 -1.2228449319478551e-8; 6.0054113300816905e-9 -7.05448971432868e-9 -5.6941027568265595e-9; -1.951082125424566e-8 1.1499547353566501e-8 -5.019589935213733e-8; 1.197134200084507e-8 -2.127430780809517e-9 4.800535709688631e-9; -1.311850186946498e-8 2.508766374053081e-8 3.5397163567430844e-8] %
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Mass Used: 7.579702014481882e-6 kg
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Launch C3: 34.82958605340684 km²/s²
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||V∞_in||: 0.8130770396493041 km/s
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