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Maybe nearing the final commit

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Connor
2022-04-18 10:59:25 -06:00
parent 0fb875c777
commit 5b6656a9a6
3598 changed files with 79349 additions and 572 deletions
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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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/home/connor/projects/thesis/archive/EMS_2022-03-30T10:29:57.444/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: 2024-07-26T01:19:00.624
Launch V∞: [2.801105685523002, 3.0115505056548346, 0.24159778742184224] km/s
Phase 1:
Planet: Mars
V∞_in: [3.2638028052648225, 3.7072432967192297, -0.8111829605867894] km/s
V∞_out: [0.21900149303391275, 4.961281790968419, -0.625939890484093] km/s
time of flight: 6.496921386032952e7 seconds
arrival date: 2026-08-17T00:19:13.624
thrust profile: [0.001107934241447801 0.0018292007266687126 0.00018565119496341824; -0.0002877684209530748 0.009632735812817879 0.0006406714050849094; -0.0035925789673975825 0.0059022726977168045 0.00036911494627972225; -0.004392271410958318 0.0031496393784072986 8.278924606405449e-5; -0.012079407428345906 0.003283958003507755 -9.305089744052092e-5; -0.015663492755514506 -0.0006101977533498358 -0.0005217677979349034; -0.029609509718733208 -0.00971504175523651 -0.001751767160770895; -0.04705355140306407 -0.030874059949991765 -0.00418091862377451; -0.05338204245020876 -0.05960383790514862 -0.0069506112405576205; -0.045383579040589345 -0.09070049371237078 -0.009483908117466569; -0.022155963117973947 -0.12192130955598213 -0.011451460521380474; 0.02034768398636264 -0.15038741398848862 -0.01256625038597567; 0.08762382671508948 -0.164454623190547 -0.011797458764685229; 0.1749075281973807 -0.14059707594205492 -0.0077920703165491505; 0.2590495954572671 -0.05495769313541083 -0.0002350397416306763; 0.31078395875959064 0.1070497396901885 0.009921413122883931; 0.2315256602857458 0.2917786478366671 0.018335503207980205; 0.04114457125744563 0.356078551965574 0.01876988024197249; -0.1305310921973329 0.33131185148905967 0.014580628212375176; -0.24866263293940324 0.24969498219971523 0.0076663519574371244] %
Phase 2:
Planet: Saturn
V∞_in: [4.11359354551261e-5, 0.00023511109390414177, -1.3035059541783836e-5] km/s
V∞_out: [0.00015465192792359236, -0.00012783566006589105, 0.00012992399487795776] km/s
time of flight: 2.516930366642689e8 seconds
arrival date: 2034-08-08T03:03:09.624
thrust profile: [-0.8184541856940203 0.2442659843524041 -0.004053340354121271; -0.18462760879748796 -0.12954689831551117 0.002015300444404607; -0.018683117374796405 -0.08274850099465172 0.0017810688184995694; 0.18605031572212896 -0.5752577339682567 0.015717634590915026; 0.7899231665527375 -0.831721605721017 0.02629677885724141; 1.0 -0.5024609495919333 0.023603267446363804; 1.0 0.08474233676614021 0.01356986253342746; 1.0 0.7682965866734364 0.0017231700304301538; 0.5800765297826053 0.9025145229862893 -0.012043262027874242; 0.049321884279686014 0.20099767542090913 -0.005729615074688785; -7.198819739380535e-5 2.5490099613361683e-5 8.115187738021953e-7; 0.00010715214961850897 -4.902284353362516e-5 -0.00010380205526740633; 4.5291168568480745e-5 -9.817442721019902e-5 -2.0023042282385832e-5; -0.00010436706033869252 2.1041010802616824e-5 0.00010686288557718574; 4.0651291248531234e-5 1.1722252477788995e-6 -3.811349494694384e-5; 4.8716963058570675e-5 -5.597438718549866e-6 3.23342078594203e-5; -7.451796699985422e-5 1.6611665890359082e-5 9.158000189350461e-5; 2.5080935965254957e-5 3.215621104195173e-5 -4.087712404794397e-5; 1.3855663221283863e-5 -2.730536790197425e-5 4.491673208203398e-6; -1.7292860098192588e-5 0.00017955629586277036 1.0628376982277733e-5] %
Mass Used: 838.6230215492219 kg
Launch C3: 16.973999000466307 km²/s²
||V∞_in||: 0.00023903829073984847 km/s

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/home/connor/projects/thesis/archive/EMS_2022-03-31T02:42:47.529/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: 2024-05-23T06:02:13.164
Launch V∞: [4.790675190538004, -2.7827628147301513, 2.3322515350749833] km/s
Phase 1:
Planet: Mars
V∞_in: [-1.4810007913292704, -3.291455435720552, 2.9831687001217015] km/s
V∞_out: [-0.5916884460359885, -2.770372854415817, 3.728441598440503] km/s
time of flight: 1.463399999793926e8 seconds
arrival date: 2029-01-11T00:02:12.164
thrust profile: [0.3803411573668084 -0.24699359911364535 -0.48327553487098146; -0.45637919416245415 0.20259655112804134 -0.4183214076160344; -0.43367448998695834 0.4136614397548196 -0.27973436226784304; -0.5190285617571937 0.29456217917248934 0.127585421435257; -0.5523405717458744 0.26680149330655734 0.3932431972939049; -0.5996656678338447 0.2522039800955279 0.4621499788811929; -0.6304800501642223 0.0890041612002452 0.5223357259424798; -0.6361153588831391 -0.24667340158896864 0.5373571355951733; -0.5825139178259425 -0.389919029978712 0.5093601462685652; -0.5454531372852401 -0.44623500436201025 0.3645214794294788; -0.4801024497934835 0.2102254586306563 0.2565776222052905; -0.579136948771309 -0.13710895068534665 -0.20134408320607608; -0.5188982220935089 -0.42618154892831445 -0.3564433259684089; -0.5230878988602696 -0.4827987429089918 -0.33730666065169657; -0.4547076944063366 -0.17486449212182634 -0.32509286969961976; -0.5648002138742563 0.1946720610839311 0.06983061891210761; -0.620774801689964 0.3715690637443947 0.19453195354416444; -0.634451658470199 0.34548391469755085 0.34375519703180396; -0.6916942031325952 0.12255205006355444 0.4731318096261815; -0.6556954878586314 0.06192414594617366 0.475764756523579] %
Phase 2:
Planet: Saturn
V∞_in: [0.6126357305264523, 0.036628352063377154, -0.44998341351260274] km/s
V∞_out: [-0.40771540308617077, 0.5213716669014113, 0.1788657968644158] km/s
time of flight: 1.7526600019051787e8 seconds
arrival date: 2034-08-01T13:02:12.164
thrust profile: [-0.4584109571736202 0.1135715923073197 0.3475236165861346; 0.28933933320539057 -0.16213518851926365 0.3689204283653291; 0.7767123213868962 -0.30606989550403363 0.2968304361134133; 0.8171230455941187 -0.177050989819005 0.13516760011367504; 0.792566162402287 0.7145286520800527 -0.4309109115263434; 0.7426473957923972 0.8547076140253718 -0.4619343157035517; 0.6131385822232893 0.8703485610178433 -0.37934354880999643; 0.05835968610825082 0.8697084452811487 -0.20558789532136582; -0.013918439576788977 0.8562307293716963 -0.016866144920425347; 0.14989145996688175 0.8391019899698795 0.09255224234844622; 0.18019735809471005 0.8224708378791422 0.16995741266663397; 0.14139412971775753 0.8023864633039065 0.20129093897625455; 0.17968164104668602 0.7805428866365428 0.2139526044756662; 0.08498935350820547 0.7527751665441202 0.19421753791674876; 0.03954352379181277 0.7151788408627606 0.18168198769090368; 0.03303845971086855 0.6728825558974967 0.14690981920697405; 0.02940785938392452 0.6148823095722372 0.10110999555278848; 0.017750178567555636 0.5324957838020801 0.08462070573863552; 0.014357313865460512 0.37335705098385324 0.058909504167600976; 0.00697353943058537 0.10646619320896161 0.016159717939472934] %
Mass Used: 1920.8181793791025 kg
Launch C3: 36.13373488714083 km²/s²
||V∞_in||: 0.7610185588597774 km/s

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/home/connor/projects/thesis/archive/EMS_2022-03-31T04:30:39.913/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: 2023-06-21T16:11:12.531
Launch V∞: [4.580336710876162, -6.364445263085335, -1.5059609900586743] km/s
Phase 1:
Planet: Mars
V∞_in: [5.6917792297860474, -9.107059519584473, 0.42920737253007657] km/s
V∞_out: [3.8594088914119493, -9.999999222371288, 0.7899882429600399] km/s
time of flight: 5.002931587226731e7 seconds
arrival date: 2025-01-20T17:13:07.531
thrust profile: [0.04229136644598212 -0.06399982439053087 -0.013233794183699233; 0.0014932116715965543 -0.004640304886228213 0.0001906966014413458; 0.0033744085280022597 -0.03336977966228066 0.005257073291176034; 0.0012173486808959046 -0.01856084430561746 0.006863306751990301; 0.0013367745067847335 -0.022179557580296334 0.01087995653246621; 0.0036625606619242286 -0.03753302445241814 0.02081824310414169; 0.005693436492274217 -0.04580963409486636 0.029614451707897785; 0.005714572044249225 -0.03497915028431355 0.027438168635040377; 0.003777208567280123 -0.02455099654485904 0.024014082477313365; 0.0017502727856114895 -0.013492983296062076 0.01677139465178059; 0.0014099722203796145 -0.02258436533622781 0.03086001815589659; -0.01711851756208839 -0.038162800905698104 0.06682067973653377; -0.07222108528125802 -0.044777544067508016 0.10793792074870515; -0.14908606147640172 -0.0461559607802597 0.1385554662454927; -0.23264661878032608 -0.05133863711785919 0.1564008191048521; -0.3111436864129761 -0.06543015638494414 0.16185133869771157; -0.3775737086759714 -0.0908253829695217 0.1565721147762051; -0.4298924012671283 -0.128999814797943 0.14270289395075253; -0.4643281358807509 -0.17906953537930623 0.12257663575791145; -0.4706052520449254 -0.22992815837368674 0.09655625247918113] %
Phase 2:
Planet: Saturn
V∞_in: [-2.246348693769835e-6, 2.3753426785927334e-7, 2.5288257778483175e-6] km/s
V∞_out: [-2.516669621821466e-6, -6.463053739261209e-7, 2.0443342168870033e-6] km/s
time of flight: 1.9486152593971774e8 seconds
arrival date: 2031-03-26T01:25:12.531
thrust profile: [-0.17633532461638057 -0.9999797294136397 0.015024325195942026; 0.9999986736375168 -0.9999918362728258 -0.1360686231839698; 0.9999988035500681 0.2439734687302935 -0.11913834595120573; 0.9999986251683992 0.8682898739883735 -0.11093379400311718; 0.9999994614450388 0.9999929666195986 -0.09303791503519601; 0.7673577770891561 0.9999839849865495 -0.06846222282089853; 0.42997221568724037 0.8288852823182677 -0.045830355401957935; 0.18215854580869686 0.4905856393977488 -0.025668582879886326; 0.030437897869578262 0.1150455831440398 -0.0044169993998817375; 0.000807513276163115 0.004402642329890393 -0.0004919165276516808; -2.7745989651617884e-6 0.00012024951636535067 5.147622876497583e-6; 4.877668061774889e-5 0.0002184086121649586 8.498500131050681e-6; 4.132626798573495e-5 8.138845277836206e-5 -3.472982010536854e-5; -6.0757100897981974e-5 0.00012392554025281714 2.6509457699324238e-5; 0.00018725736157467317 6.848523112973848e-5 6.68862906209139e-5; 3.3549665625494406e-5 0.00011153259853957193 -5.104946327333131e-5; -4.4178366374466365e-5 3.558251004156073e-5 -1.1982307674649479e-5; -0.00013762482047567344 1.3746134754174806e-5 -2.093755807885032e-6; 4.771811294273377e-5 4.731274921606212e-5 -1.1671493023451763e-5; 7.19639059100438e-5 -0.00013724663359736313 -3.071142693588584e-5] %
Mass Used: 771.0879580725491 kg
Launch C3: 63.75356639538772 km²/s²
||V∞_in||: 3.390791175687325e-6 km/s

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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: 2024-12-27T01:12:40.730
Launch V∞: [1.8466699553948345, 1.3678562790010131, -0.0153057964937058] km/s
Phase 1:
Planet: Mars
V∞_in: [-3.1633872892711388, 1.766847714739104, 1.5906318484460866] km/s
V∞_out: [-2.6570752417451518, -1.5623087854586397, 2.48153623885944] km/s
time of flight: 1.3537387772095194e8 seconds
arrival date: 2029-04-11T21:03:57.730
thrust profile: [0.9929900810043344 0.9999987852496462 -0.10337727636552446; -0.9999989527606722 0.9999992090099894 -0.3047289804175132; -0.9638713659439484 0.0450322438551014 -0.4055337795064804; -0.22495106561402115 0.7848677069324818 0.3831319023782979; -0.7738893421351393 0.9999990172621287 0.39494769205095726; -0.990946731002965 0.8417897053927665 -0.3815221486365675; -0.9734982361035388 0.7893313668448306 -0.2704704369660258; -0.38723803350107505 0.9976585911266805 0.3624717872401706; -0.6369591805380839 0.9888790443583878 0.2130500370042681; -0.9999988687936101 0.9999990044599046 -0.3329147869188805; -0.5789162319974664 0.1999123448513483 0.028083803862645515; 0.7985291692991425 0.7881953295377477 0.17388971281195142; 0.988850032987504 0.9999996591217118 -0.5009694317683372; -0.9999994842664317 -0.3956604351616602 0.20708177708047873; -0.4450447334188467 -0.9872965011676511 0.25277979453414506; 0.9999992382496556 -0.2261999230664443 0.0610408161667454; 0.9999995915291495 0.9999997964336237 -0.5276666165499095; -0.9999998232725931 0.9999996435539122 -0.2721356921234991; -0.9999996876222519 -0.99999900073252 0.10007758955670606; -0.4315629068159034 -0.9999994920612009 0.07571074821215397] %
Phase 2:
Planet: Saturn
V∞_in: [1.327202961748595, -0.2335174765716992, 0.19517799010581816] km/s
V∞_out: [-0.10390899330694657, 0.5823202662968701, -1.2235226316464973] km/s
time of flight: 1.315170240574828e8 seconds
arrival date: 2033-06-12T01:34:21.730
thrust profile: [0.9999991434090886 -0.9999989109820826 -0.18840484920575698; 0.999999642574456 -0.7892776436332918 -0.12931408694138657; 0.9999997178412163 0.5267393788441906 -0.06956780561709845; 0.9999997101961674 0.9999994336962261 -0.018610639490947056; 0.9999995326675502 0.9999996674548184 0.04055505772364419; 0.9999985272401802 0.9999997166093685 0.0964843343858098; 0.5108611241098074 0.9999996665528476 0.11541241396889583; 0.11915209802429379 0.9999995788468198 0.1254892030062545; -0.06577608027600101 0.9999995097151354 0.1358163701800956; -0.15786944384121993 0.9999996754541017 0.1375960485939181; -0.19165177643017128 0.9999893885682953 0.12875243461837188; -0.1283595672922781 0.6138567630147376 0.07671724293817712; -0.012317449010467607 0.047087977571726294 0.006452581509892722; -6.34335149466746e-5 0.00091471809306928 8.53716230858717e-5; -0.0002753957972021203 0.0008379366569403406 0.000253847549893273; -0.00012249698733454806 0.000620864691591944 0.0001747719954028129; -0.0007703906582188425 0.00036864647470518063 -0.00026313495806057455; -0.0003679676279671012 0.000462432306598997 -0.0005969365300740931; 0.00010307940670236174 6.503004811360405e-5 0.00016002455788454703; 5.626567684290205e-5 0.00028538089451470705 0.0003865580217838497] %
Mass Used: 2051.6186645766516 kg
Launch C3: 5.281454991566764 km²/s²
||V∞_in||: 1.3616506752322357 km/s

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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: 2024-09-20T14:03:44.662
Launch V∞: [-0.9544125442488793, 4.650055637860991, 0.8829883975591813] km/s
Phase 1:
Planet: Mars
V∞_in: [-2.686848874040082, 5.69557833738042, -0.3426867301634786] km/s
V∞_out: [-5.006830246285463, 3.8244101442357286, -0.28590492992060296] km/s
time of flight: 1.2959473202133252e8 seconds
arrival date: 2028-10-29T12:35:56.662
thrust profile: [-0.028074398281491695 0.03725829642101633 0.011493562796176157; -0.04057241823105847 -0.0036979634745522238 0.004188100162030408; -0.018576540265103334 -0.016670623079762328 -0.0036538504180610655; -0.00926818068907572 -0.029823872248843347 -0.00788998730301693; 0.0056536273790355335 -0.039471274595512786 -0.015505661293943124; 0.01795773380852956 -0.024832086810877792 -0.012157101567918709; 0.020276654954958836 -0.008918038755765955 -0.0074245383137495295; 0.026868221096269136 0.007263820280035479 -0.004654400052923847; 0.011894893359756988 0.03223774798632351 0.004633535267024402; -0.047141055295386355 0.040019079580037704 0.013364609633569504; -0.04520469085369964 -0.010120922532993988 0.0020777538652468844; -0.024235864777124916 -0.02628842319518715 -0.005178953753261158; -0.020104196631084845 -0.08663986569488229 -0.025957813503050115; 0.04562945777248198 -0.18858114469692783 -0.07388958835417316; 0.1654642046172344 -0.19639566019786459 -0.09899123711104271; 0.20836768567311814 -0.07684473602532182 -0.06621134288112417; 0.17451643722399424 0.054856569336227734 -0.019947666848185868; 0.09171150949789851 0.24766459803783164 0.03479747010758981; -0.23524183946575974 0.2601294101394598 0.07688820773607916; -0.21879974186036938 -0.008020833470565012 0.021595583194403873] %
Phase 2:
Planet: Saturn
V∞_in: [2.746703786000276, 2.98969776442552, -1.0550945579969648] km/s
V∞_out: [-2.364529965587132, -1.1050142331661583, -3.0819068226828907] km/s
time of flight: 2.2586692153285405e8 seconds
arrival date: 2035-12-26T17:24:37.662
thrust profile: [-0.17155197556204754 -0.12803647772004534 -0.0010987042854903337; -0.0035589134881411667 -0.06490801713537507 0.0007426295065205218; 0.25580929199297914 -0.3791453683925915 0.015541598652070847; 0.9999998062826643 -0.5828839766311769 0.041611387112901736; 0.9999998812648976 -0.13591929443541234 0.04367451973443414; 0.9999999269970672 0.45531454218125245 0.04521667689652659; 0.9999999228048742 0.9999999183342614 0.04613770201743983; 0.840757310010811 0.9999999579385513 0.026030995407658575; 0.11987829006679744 1.0 -0.0008893319442928411; -0.16626331436648592 0.8682210906007626 -0.017523530916658536; -0.010554991808101162 0.026008419906682182 -0.0010654160560760403; -0.00038326527134042613 0.00042430859777888713 0.00034930741189383597; 8.526053802782655e-5 -0.0008985199777937706 0.000160878965697085; -0.0003967771857136998 0.0010341920913412306 -0.0002243904620731941; -0.001455496554504259 -3.155267804676458e-5 0.00028821667601580344; -0.0002685807673767674 0.000826989980715048 -0.0008420052914367241; -0.0007719825562061786 -0.0008609199968383217 -5.4081725930572875e-5; -0.00011547325119660988 0.00024382875164120964 -0.0003906884145274092; 0.0010448953162641168 -0.0012700408455061536 0.001398368665761554; -0.0009243989271800159 -0.0004827763788561335 -0.00016362116690873035] %
Mass Used: 896.7374359341643 kg
Launch C3: 23.313589250046537 km²/s²
||V∞_in||: 4.1947465879304335 km/s

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