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Connor
2022-02-27 23:56:22 -07:00
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/home/connor/projects/thesis/archive/EMMJS_2022-02-21T00:09:46.922/mission---------------------------
Spacecraft: mySat
dry_mass: 200.0 kg
specific impulse: 3200.0 kg/s
max_thrust: 0.00025 kN
num_thrusters: 1
duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2024-12-30T12:47:20.643
Launch V∞: [-0.8585858913059945, 5.43163312454597, -0.21719547468177308] km/s
Phase 1:
Planet: Mars
V∞_in: [-2.5856773315583745, 2.4609561275200487, 0.7295849474445574] km/s
V∞_out: [0.6194643215165332, 3.2309327456082855, 1.5650004450735309] km/s
time of flight: 8.21340000011604e7 seconds
arrival date: 2027-08-08T03:47:20.643
thrust profile: [0.18708793577518806 0.5313802548498593 0.20444668942359182; -0.06350657961080429 0.7363728402067601 0.14591280353760663; -0.5915522558225289 0.7847434950188144 0.026651112465872404; -0.7542562554239148 0.7746896783865607 -0.1237392373650896; -0.7866125946706723 0.6465409532772359 -0.181921929015919; -0.6858815963696551 0.5510566480853467 -0.17868708799185337; -0.7594148821784542 0.7476306773551871 -0.11848928569756635; -0.8151098482182527 0.36136227575490387 -0.07980840799214974; -0.7401577445019838 -0.3095683994157624 0.03448173859798725; -0.6080245532967408 -0.0062406255431043806 0.06699727498541076; -0.43741470194423654 0.4730679368243737 0.0339770148854078; -0.18490322648998495 0.6426379090283426 -0.13028954478184662; 0.47254893347274096 0.7718760888207634 -0.1551009557943166; 0.5190900646391018 0.8753585966827419 -0.08611250544188818; -0.8855993838016015 0.8714238270161355 -0.08045710930215778; -0.8920483208731022 0.293979266137998 -0.1008142011864752; -0.8306385396979714 -0.8016800304530476 -0.043159471100223716; -0.6873350930031549 -0.7928126872627601 -0.02124194344649641; -0.07252547075225568 -0.7402808067151411 -0.037972567496587895; 0.6875211020649464 -0.5605655534502224 -0.13311603635138225] %
Phase 2:
Planet: Mars
V∞_in: [1.1180674616624362, 4.566462924317003, 1.4292875212918483] km/s
V∞_out: [1.2322985249643665, 4.3433091442560645, 1.9398620619570397] km/s
time of flight: 6.237720000073707e7 seconds
arrival date: 2029-07-30T02:47:20.643
thrust profile: [0.5134182009488921 -0.31555188364900766 -0.055374803379038676; 0.5541643860557178 -0.10936971458523223 0.0007152948743699293; 0.5460385559170413 0.1530957100358743 0.05129389787053946; 0.46239205959354684 0.3541230771326737 0.0837352480895128; 0.2788761074398226 0.42401413505230207 0.09850448091487779; 0.0861711281015175 0.3771366798387737 0.08680527911942301; -0.0019793970085822893 0.2716311958716949 0.057899476045225384; -0.02438647027237024 0.1785456275302977 0.03356359507342958; -0.0460851975884734 0.13513224341732036 -0.0075472317756282775; -0.05051028634319777 0.13458427170959206 -0.056361751862420054; -0.059757482177925196 0.1155277298538939 -0.10695473795359935; -0.06308060055392012 0.08656293882186156 -0.14897716336334949; -0.060709990203287566 0.053581479830941116 -0.17880651728419109; -0.05399581102575967 0.019928172160662616 -0.19586000706017498; -0.04455159724330247 -0.012018413567160578 -0.20023332232742197; -0.03435074656279236 -0.04090428121904396 -0.19247441119311592; -0.02473533778237781 -0.06625905911693483 -0.17311082652131804; -0.017001426993727434 -0.08901248109333483 -0.14173368541223236; -0.01492966583523356 -0.11182046547456173 -0.09626664779027602; -0.02419545780950693 -0.1333838006203212 -0.04006325619060162] %
Phase 3:
Planet: Jupiter
V∞_in: [1.0425933248043313, 9.761014809328087, -0.4217373616811835] km/s
V∞_out: [-9.345457932936196, -2.8317056643741645, 1.0859916102035037] km/s
time of flight: 2.6687520000038186e8 seconds
arrival date: 2038-01-12T22:47:20.643
thrust profile: [0.5628431836674769 0.47506205926522466 0.01494314598245946; 0.21922079590638668 0.04171051990989757 0.2601684761848701; 0.6837155305781677 0.5152279955386716 0.0013884449392686086; 0.11204795410174831 0.7194929944329855 -0.05582598783813832; -0.5437076444290293 -0.5507865585159418 0.05488176961971801; 0.3946907920290721 0.3553045067960959 -0.0009333191781478536; 0.6286527350564048 0.15811539062067848 0.0010593852696665147; 0.5244115910894975 0.5054313632357015 0.06734970951936782; 0.16947323257204125 -0.25342029906455155 0.041224265782725; 0.8184810643617919 0.6150207802837899 -0.0007312998992708492; -0.29400957489332924 0.5349618499607386 -0.0022793003860954167; -0.1813961648289101 0.39314833358368484 0.02463460931711496; -0.24079119813027802 0.22304978428092506 -0.0452896662834434; 0.0692938115099807 0.2174985639878364 -0.039548706790466105; -0.055133140610399506 -0.3023901220512069 -0.10050398589752965; 0.4405772740882254 -0.5714961854289461 0.010199886302938704; 0.5508873740881252 0.7290499177697591 -0.009434982976593908; -0.3394222681154409 0.47080066387267466 0.1182603751716305; -0.2838812749863273 -0.14939589284636337 0.05198509208395944; -0.08739787411558196 -0.48848414007930296 -0.019353445078579605] %
Phase 4:
Planet: Saturn
V∞_in: [-0.12467502011680599, -0.21941891947700304, 1.1210048424481494] km/s
V∞_out: [-1.836549550435177, -1.0274249385233098, 0.15074571437514825] km/s
time of flight: 7.985519999979527e7 seconds
arrival date: 2040-07-25T04:47:19.643
thrust profile: [0.9015449791987612 -0.4135045547482888 -0.10493150953252237; 0.8281237041407337 -0.4199865377311189 -0.10871363555015406; 0.5865495210885522 -0.18888729221478687 -0.05376150916405686; 0.5536125796492021 -0.21710904361394967 -0.08288273835216246; 0.5226797275283863 -0.20596461753201076 -0.0816923569899679; 0.492356358914814 -0.1952282536684453 -0.07970598541671017; 0.4625023188662105 -0.18413996987155215 -0.07694322290334572; 0.4328711669558749 -0.17242291902938622 -0.07345517917885007; 0.4032239447511029 -0.16009204113840642 -0.06931306800923256; 0.3733858215361839 -0.14725361285778707 -0.06460897748518732; 0.3432505744179203 -0.13401143205085617 -0.05943463295918488; 0.3127627286749208 -0.12044462830785903 -0.053859778958435967; 0.2819001737662793 -0.10660684717642485 -0.04798048977198586; 0.2505956888019982 -0.09251745970413862 -0.04183914117857803; 0.21859841440967404 -0.07812693858807919 -0.03547943926291368; 0.18535858791227242 -0.06324296041863105 -0.02894834505985858; 0.15015303093566526 -0.047669454737263 -0.02232276989900783; 0.11229167669542692 -0.032210071289352 -0.015683269811579196; 0.07065162071067796 -0.01828153555341133 -0.0091544483837168; 0.02434581489906545 -0.005871680237325595 -0.002964910300780224] %
Mass Used: 2233.4875953911933 kg
Launch C3: 30.286982006636965 km²/s²
||V∞_in||: 1.149060650991836 km/s

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/home/connor/projects/thesis/archive/EMMJS_2022-02-21T05:29:13.100/mission---------------------------
Spacecraft: mySat
dry_mass: 200.0 kg
specific impulse: 3200.0 kg/s
max_thrust: 0.00025 kN
num_thrusters: 1
duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2024-08-13T21:37:18.613
Launch V∞: [-1.6901867322791075, 5.280615079261146, -2.032003347094416] km/s
Phase 1:
Planet: Mars
V∞_in: [-1.7461250307138758, 2.7488621400103193, 1.513513215864433] km/s
V∞_out: [1.2027265638973148, 3.3257187268143342, 0.6259917731579052] km/s
time of flight: 2.4051597753353596e7 seconds
arrival date: 2025-05-19T06:37:15.613
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] %
Phase 2:
Planet: Mars
V∞_in: [2.043297951821988, 1.6820451775844232, 1.823788193968268] km/s
V∞_out: [0.4882307516881071, -1.2152266867358175, 2.9360573603089075] km/s
time of flight: 1.14134402513377e8 seconds
arrival date: 2028-12-30T06:37:17.613
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] %
Phase 3:
Planet: Jupiter
V∞_in: [3.7114411433504815, -4.460792211249508, -1.1805018431500913] km/s
V∞_out: [1.7805895932237876, -4.309492902052931, 3.6498067710496795] km/s
time of flight: 1.6335000237429604e8 seconds
arrival date: 2034-03-04T21:37:19.613
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] %
Phase 4:
Planet: Saturn
V∞_in: [-0.0246480076721461, 0.06541562927953826, 0.07516568061471392] km/s
V∞_out: [-0.5848111974561183, 0.18686923783075082, -0.03206665093199944] km/s
time of flight: 2.1155400016049725e8 seconds
arrival date: 2040-11-16T10:37:19.613
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] %
Mass Used: 2059.4133968003325 kg
Launch C3: 34.87066440789543 km²/s²
||V∞_in||: 0.10264798282731782 km/s

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