30 lines
3.4 KiB
Plaintext
30 lines
3.4 KiB
Plaintext
/home/connor/projects/thesis/archive/EJS_2021-11-10T17:39:50.182/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: 1977-06-03T12:59:37.799
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Launch V∞: [2.037663352777953, -8.43490917599047, 4.662061679317432] km/s
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Phase 1:
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Planet: Jupiter
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V∞_in: [2.0543036098784477, -9.13281943510734, 0.46707958098685376] km/s
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V∞_out: [-9.062292345569814, -2.3925561030248113, 0.012115863710008418] km/s
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time of flight: 2.651327999769022e8 seconds
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arrival date: 1985-10-28T04:59:36.799
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thrust profile: [-0.3666137901495707 -0.46957429211809487 -0.06095376292954174; -0.4665558706644106 -0.10394413351183696 0.28610656396587303; -0.4953660695905247 0.24271134488915128 0.26741901645132793; -0.5238470521312512 -0.14904137588352487 0.11667074352725965; -0.3130301366808927 -0.5555434925364752 -0.06526933016356705; -0.5423650979399098 -0.5620740091733915 -0.20854153512243992; -0.5246082788630371 -0.5025978253322431 -0.21135002916159024; -0.5697267878022093 0.06321816977663988 0.22886544507082332; -0.6120311447829342 0.412763321448428 0.15616795632012262; -0.6539149704504248 -0.4641829118760538 -0.12954694971592742; -0.20129129722008116 -0.6165039554386057 -0.13481895080818976; -0.3977328905362448 -0.5756437901430289 -0.1442400227486695; -0.41396000033260266 -0.4597767223691828 0.014956812046032929; -0.5419266443658755 -0.3913185005375316 0.10340560958225044; -0.653821761083701 0.0029065521912539248 0.1254968793250296; -0.7392954157600166 0.41739296978429474 0.048387346920351154; -0.2993155496706189 -0.862564466919382 -0.18789013527425982; 0.54061683054975 -0.6077177484151901 -0.38511905650494493; 0.3595047789991687 -0.26996788568129604 -0.058521775645983334; 0.6079025381989944 0.7866364488796997 -0.002816798435360894] %
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Phase 2:
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Planet: Saturn
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V∞_in: [-1.5527277061928566, -9.290875340376942, 0.043699679303627025] km/s
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V∞_out: [-0.7664706270913678, 0.08215083439603876, 0.01420153594858485] km/s
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time of flight: 1.4356440000946072e8 seconds
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arrival date: 1990-05-16T19:59:36.799
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thrust profile: [-0.45363346920243913 0.007414553001916338 0.024833395801696717; -0.42929594280033395 0.029217209524867983 0.025014737699506233; -0.40759184786564384 0.06351691143576771 0.02515016106459692; -0.39712301899974733 0.12845858528432538 0.022572693508776966; -0.4009114657635113 0.21043524639923297 0.029274749214758526; -0.45017496865976625 0.2843178178382748 0.03516955271197208; -0.6353367593618829 0.007373393962796029 0.061015069673970156; -0.17636211915789957 -0.5399824298560856 0.046019016312036976; 0.10022826993820261 -0.4452055922359326 0.005465675250313729; 0.12030211019389436 -0.30664235607958396 -0.014741914655282726; 0.13606528305073498 -0.24140989738984756 -0.01809230195253888; 0.14886416528008864 -0.14793802290529368 -0.024870924926003683; 0.1573360419373063 -0.037299267927507894 -0.0326622325810398; 0.15533491321993567 0.08595709158871023 -0.03599171154371347; 0.1456345166609902 0.1981225994755318 -0.03517653838413347; 0.1357020340234525 0.2942201982026304 -0.033486517711519836; 0.12603250981007186 0.3753587231244459 -0.031672415654865504; 0.11656119662828038 0.4425819361389264 -0.030365847244885866; 0.1075278998670041 0.4980664219019285 -0.02910770547729163; 0.09630035393180529 0.5468861781276572 -0.02846997433085122] %
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Mass Used: 1956.4800896757313 kg
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Launch C3: 97.03458384822258 km²/s²
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||V∞_in||: 9.419832141921349 km/s
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