/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