44 lines
6.4 KiB
Plaintext
44 lines
6.4 KiB
Plaintext
/home/connor/projects/thesis/archive/EMMJS_2022-02-21T05:29:13.100/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: 2024-08-13T21:37:18.613
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Launch V∞: [-1.6901867322791075, 5.280615079261146, -2.032003347094416] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-1.7461250307138758, 2.7488621400103193, 1.513513215864433] km/s
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V∞_out: [1.2027265638973148, 3.3257187268143342, 0.6259917731579052] km/s
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time of flight: 2.4051597753353596e7 seconds
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arrival date: 2025-05-19T06:37:15.613
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thrust profile: [-0.0017599460808520734 0.021939823461937586 -0.07860824048711292; 0.0038057476482388137 0.01317123732517402 -0.0925516242969978; -0.012111500711155023 0.009175602331176976 -0.10689934082194484; -0.0057786091800751385 0.004785500911625599 -0.11802387642642173; -0.014871641299940966 -0.005768817944699136 -0.12261622402101267; -0.004758948871952711 -0.0018517590809734616 -0.1312674708448622; 0.007589952947205352 -0.009441179217149816 -0.13265233200159024; 0.02957759948608535 0.012559088860055839 -0.1178470071574203; 0.029293581498403685 -0.0027693172907246807 -0.12277829992312493; 0.00043915486764571567 0.012598754358696054 -0.12458999384207707; 0.039545288569820244 0.03314430343814683 -0.10624529827972352; 0.03219377536903767 0.050819916158926205 -0.09961115577485845; 0.03399569316999455 0.04298795510617496 -0.09578630843591786; 0.030077287420831947 0.08313823965268496 -0.06933023697506474; 0.037127301703059834 0.09397497850832547 -0.052654905925240816; 0.022412917519582787 0.10765616559310794 -0.025717008847364307; 0.025327703848176397 0.11276690546887153 0.004843267678066204; 0.007650286567218721 0.11949746525926046 0.021216184066767087; -0.0038980974979574835 0.1248646921852295 0.028322916840977087; -0.019178665908750572 0.12278762564523467 0.04346269663142969] %
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Phase 2:
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Planet: Mars
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V∞_in: [2.043297951821988, 1.6820451775844232, 1.823788193968268] km/s
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V∞_out: [0.4882307516881071, -1.2152266867358175, 2.9360573603089075] km/s
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time of flight: 1.14134402513377e8 seconds
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arrival date: 2028-12-30T06:37:17.613
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thrust profile: [0.22291730975859356 0.5098248034605009 0.24720522565212524; -0.4469925923761469 -0.007661162151150529 -0.08117095118772306; -0.5525078400371499 -0.4741527168000471 -0.14631851618865835; 0.18040546081731915 -0.7460124551180657 -0.05214179589449932; 0.6953342845058121 -0.5331751797010302 0.16302204627027528; 0.6185646245916668 0.06025626130956423 0.30205781678787413; 0.44949631635524223 0.03858256309628191 0.34300503738181515; 0.32691770627377126 -0.3565152659582362 0.26806235880669743; 0.3909860773308049 -0.4856009661776308 -0.060179414964323774; 0.3979512624499183 -0.3974411990059185 -0.2619149915820402; 0.4866100975196277 -0.41623220426978347 -0.05594094246998931; 0.43622582167391594 -0.21713526052371673 0.29394158670200404; 0.20594952174764747 -0.4177558340479653 0.3892322018647292; 0.25453944143605217 -0.6261670137409058 0.3258204997833534; 0.5749031989207859 -0.6800207997886729 0.12429472580187996; 0.7530954315757951 -0.3098572647533813 -0.2144972990721993; 0.4851334634524593 0.64491549530751 -0.26752525551583867; -0.5764002596860117 0.3646707634147813 0.14796405075327934; -0.5901573878990791 -0.41314618778501866 0.3805666596159053; -0.42700527824297163 -0.6826390179287234 0.4045024615945392] %
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Phase 3:
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Planet: Jupiter
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V∞_in: [3.7114411433504815, -4.460792211249508, -1.1805018431500913] km/s
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V∞_out: [1.7805895932237876, -4.309492902052931, 3.6498067710496795] km/s
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time of flight: 1.6335000237429604e8 seconds
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arrival date: 2034-03-04T21:37:19.613
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thrust profile: [-0.5046672735197064 -0.7996955535271304 0.2112934255095142; 0.5077989036864389 -0.7649454581859021 0.20409797991337683; 0.5808566386587612 -0.6364303545112504 0.18542744111458456; 0.5006095090625132 -0.48372727317177533 0.13748541541649756; 0.36800706000490335 -0.4274801913323154 0.04508051614164652; 0.23616890612114982 -0.4106281022924214 -0.07422701918557366; -0.02614107297996989 -0.4044558701986192 -0.16223559260078177; -0.2964744410521455 -0.34839867086847304 -0.21078013212233546; -0.5176405945957604 -0.3288038834641507 -0.19405120809950877; -0.6330040108688543 -0.42206025464387953 -0.15342166355020417; -0.7099262633889031 -0.6237883136733828 -0.07027765831937338; -0.7822443063582115 -0.7257522470091892 0.046372365248012457; 0.15416780610066894 -0.8145688662272869 0.11743307333391405; 0.6452194124175534 -0.678910631324967 0.054691069558399794; 0.5771299498788154 -0.4641832360664856 0.018420229596808394; 0.4457565039423475 -0.3040316838235003 0.01783058099504133; 0.23801401595031418 -0.13216754190081506 0.010767856013003372; 0.2587404825219754 0.09782617488793967 0.003859597411132576; -0.08344625676841577 0.2827272664297725 -0.026493133998743063; -0.3933999656322405 0.24332107698735156 -0.027081715518899548] %
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Phase 4:
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Planet: Saturn
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V∞_in: [-0.0246480076721461, 0.06541562927953826, 0.07516568061471392] km/s
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V∞_out: [-0.5848111974561183, 0.18686923783075082, -0.03206665093199944] km/s
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time of flight: 2.1155400016049725e8 seconds
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arrival date: 2040-11-16T10:37:19.613
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thrust profile: [-0.1627110678115485 0.22700671143458248 0.029986080505317234; -0.16214080594693478 0.23967493565533463 0.08955363564847629; -0.1745196970984745 0.25483610546962543 0.12716395184957408; -0.1952524515982284 0.2505218299754148 0.17036723627980027; -0.21614749560569926 0.24089984374439646 0.19877853523817543; -0.22618695860284732 0.24715274229193332 0.2135402310441893; -0.33485154946340523 0.2613684298843818 0.23512617093629723; -0.3725246027720915 0.15599299255433202 0.25303578361261436; -0.36926821691311146 0.07153107899757735 0.26760363975946333; -0.35478356034012126 0.0018475578322651304 0.26116841888769105; -0.3312470217412482 -0.04985111461820565 0.25331488736816143; -0.30012674484829766 -0.07703821603688417 0.24136867711498777; -0.2634342927812894 -0.096191631413734 0.22794344262127944; -0.22575690873415977 -0.09889406062182618 0.199660205553818; -0.1887069515840364 -0.08881084245979123 0.17583719753517285; -0.14879690447972715 -0.07592681830346394 0.15115513011894557; -0.11724449357420508 -0.058526105092731553 0.11562822849360169; -0.08722592614665677 -0.03788553733718045 0.08344591269592441; -0.05347117156910084 -0.019641127134930575 0.052723601226170855; -0.024200395926615395 -0.005375747843091736 0.013406461289335841] %
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Mass Used: 2059.4133968003325 kg
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Launch C3: 34.87066440789543 km²/s²
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||V∞_in||: 0.10264798282731782 km/s
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