37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-29T22:43:36.591/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: 2024-06-09T17:38:19.762
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Launch V∞: [-1.1540177007372212, 5.360837098498792, 0.2984944317979115] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-2.0043098166092546, 1.5028334917558672, 1.4743578319466457] km/s
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V∞_out: [-0.8356117752464607, 0.15439829082406908, 2.7798876463250943] km/s
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time of flight: 1.5586920017281148e8 seconds
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arrival date: 2029-05-18T18:38:19.762
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thrust profile: [0.1725379661821492 0.3028636782963449 -0.14594530225449512; 0.24010663973374377 0.25478985696879275 0.09151945430842105; 0.11381352719375167 0.3130894749849403 0.2091089750468684; 0.30283734986847677 0.21701222794179637 0.09824137709532094; 0.03630275234501889 0.41675693248956935 -0.1012386700554873; -0.2418245491826651 0.18118147964342593 0.21825116267504735; 0.2915470156543983 -0.03388072887705498 0.24410561878006867; 0.412361768542535 0.2999336398088819 -0.03160436499097794; -0.3812539424180171 0.37480489610907414 -0.03459460167463225; -0.2611116851421491 -0.2829019647433105 0.18194015849684886; 0.38117772281170925 -0.25992909797801095 0.11794074908818503; 0.47844764750593854 0.40046145886582907 -0.038809743471385535; -0.46688744880086946 0.4632135549542049 -0.04628160942646042; -0.38034093441997535 -0.3405512606021152 0.10677210042434881; 0.31086761425082576 -0.4048490143871347 0.1223843991365784; 0.563950253001912 0.04920151532400937 0.02450398411122806; 0.3683993286573054 0.6302412619336084 -0.0857920129848164; -0.5891033244964972 0.368112076435439 -0.020783964084951624; -0.43285871121985753 -0.4273820767487316 0.09610577284114862; 0.2491356450509427 -0.508230954127345 0.12331066638000482] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [5.611204987956414, 1.0148015551991953, -0.05634775428610248] km/s
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V∞_out: [-1.1695945563190893, -1.5488819990446605, 5.3620550672788685] km/s
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time of flight: 2.0545559999887675e8 seconds
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arrival date: 2035-11-21T17:38:18.762
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thrust profile: [0.5107734951887763 -0.3946064078009902 -0.0045676369422384165; 0.4598697444727305 -0.20748812220867774 0.059353622926187184; 0.33581510576782936 -0.407189511957922 0.15987153660020692; 0.3794276589018478 -0.37511266169747637 0.14960397348233373; 0.13533934017940225 -0.5031320027541039 0.08209543124670671; 0.4245206324807559 -0.6227802169786933 0.05650960675506308; 0.6558675736258086 -0.3397032003626548 0.03308794472495331; 0.5120131659823914 0.2924383586904873 0.05184380445957168; 0.34826053012663044 0.014522849649912385 0.19696263006429715; 0.041523907241033706 -0.3360187093015938 0.21706268681577065; -0.3475762260365926 -0.48685037074106274 0.1315856784159298; -0.3743319370307219 -0.6764350725170731 0.0903118551039194; 0.5097342414424403 -0.7734829334242606 0.09514159989066195; 0.7845273733985942 -0.5753935364819165 0.029842770779258728; 0.7315778039847924 0.3432605037934376 0.004749315755486527; 0.5968872158984753 0.44198729718418783 0.051253635005704054; 0.42636307680116 0.379616657506637 0.10303815501796434; 0.22195498303040814 0.27300879237608766 0.14632762929547719; -0.024188484440234567 0.13680033465416566 0.18166786525750667; -0.25695040241576644 -0.0340498293709866 0.19810666574939037] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-5.337830290816849, -1.2797414036157133, -2.7683894000988465] km/s
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V∞_out: [-0.10980431423849103, -0.03384798680602295, 0.02827033505965302] km/s
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time of flight: 1.8897119999873626e8 seconds
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arrival date: 2041-11-16T21:38:17.762
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thrust profile: [-0.18827080027303889 -0.0037944481429670707 -0.03587675027570545; -0.19565231042967327 0.005129353701615244 -0.0491082915163806; -0.20133676663900688 0.006029178811167082 -0.061481112982642354; -0.20302516058528305 0.0007224209388200189 -0.07282963982737341; -0.1992472102885178 -0.008123574893217902 -0.08261210764249102; -0.18966342972050407 -0.01766000522047062 -0.09006550432571891; -0.17498658801374278 -0.025605649979007036 -0.09448626862190662; -0.1565946658088734 -0.030702577951425794 -0.09546452816058656; -0.13601668286185079 -0.03270754112415236 -0.09297644549658375; -0.11452486200770591 -0.03205112806212533 -0.087329135163873; -0.09295108976564484 -0.029437401451120573 -0.07902523194922431; -0.07170872328897128 -0.025556470851551057 -0.06862784111694957; -0.050921087058557565 -0.02094394138963416 -0.05666105407220744; -0.030593668268616675 -0.015951410990809784 -0.04355220139864001; -0.01089690262146556 -0.010781661120095435 -0.029616221718477793; 0.007122614981337976 -0.005737608245027011 -0.015721445566949432; 0.02554588657835649 -0.0012054841338314535 -0.004144072671787097; 0.04638165061824139 0.003923812353691581 0.008511361629231926; 0.06771364374279902 0.00950332978700583 0.021885568118429555; 0.08936998361099453 0.01545954630179973 0.03535590621212607] %
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Mass Used: 1812.515221885309 kg
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Launch C3: 30.15943017607013 km²/s²
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||V∞_in||: 6.147694701615383 km/s
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