44 lines
6.4 KiB
Plaintext
44 lines
6.4 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJSU_2021-11-11T04:50:20.773/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: 1977-08-29T00:28:42.235
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Launch V∞: [-5.993015939919875, 2.5730948883971196, 1.0995056788128965] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-4.912918793015281, -5.749282630615395, 3.500451711966386] km/s
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V∞_out: [-3.4658376295259443, -6.128480904546313, 4.458055817928218] km/s
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time of flight: 9.655561330465347e7 seconds
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arrival date: 1980-09-19T13:28:55.235
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thrust profile: [-0.6848479340229933 -0.6317473532438761 -0.6789410387377113; -0.7283373129568128 -0.6597015909585692 -0.6860291664652663; 0.5143122109172585 -0.7554166841816019 0.6548911297971178; 0.650987105546092 -0.739938250992294 0.686244011796856; -0.567349081163571 -0.7171322204555259 0.7176501535009572; -0.6060664652754209 -0.6881472823274762 0.7152061841403491; -0.6457752364426499 -0.6793453331017747 0.6901800477645527; 0.6373998427205125 -0.6901370973195071 0.6440943571979044; 0.6232981297616063 0.6245585478937647 -0.7042650672249426; -0.7173110561506139 0.47022815205529234 -0.6937264189108627; -0.6298819082617076 -0.7335307650242696 0.6794508601033687; -0.5840798229168693 -0.7117652775560642 0.71673753565496; 0.6518652084909865 -0.679625481136191 0.7150981814535525; 0.6269343446266082 -0.6783434977916609 0.7005711370434008; 0.6192953242902497 -0.6895768905181153 0.66192822798728; 0.6249355751156056 0.6111710277362319 -0.6978924565831346; -0.7127959821946511 0.5739058413985498 -0.7071394367657958; -0.7027946745383137 -0.7495505439357887 0.5974000176561298; -0.5796183131865142 -0.7574601098030497 0.6961759879457895; 0.6831171982226909 -0.7168789234373818 0.7163908572195994] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-4.687613669172795, -9.137643103467221, 2.7610043724460294] km/s
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V∞_out: [-6.84902175973724, -8.134664345135159, -0.10743273528963516] km/s
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time of flight: 1.0295640390127918e8 seconds
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arrival date: 1983-12-25T04:28:58.235
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thrust profile: [0.6995410218848744 -0.6393230267422165 0.7647526533373915; 0.6698438420960121 0.7948373479414468 0.7488466112399416; 0.6133803630656508 0.8721432241652148 -0.10503387899547705; -0.7975752189273541 0.8967673181002215 -0.620565856208428; -0.8810777959243058 0.9109617670598268 -0.7447072404898911; -0.9255982733383775 0.9048235938487734 -0.81044200796326; -0.9451974194019941 0.8324645836800456 -0.8403473305611608; -0.9491498129909374 -0.8041118034787202 -0.8374748559038501; -0.9403374896987303 -0.9097804605905754 -0.7972210189785967; -0.9169616625063207 -0.9275441774549357 -0.7103882336630395; -0.8728172615404418 -0.9276214940959352 -0.5569943225350228; -0.7993897280663421 -0.920066591499417 -0.33089228095477646; -0.6888132887887403 -0.907363288341434 -0.10712622625205351; -0.5426334991349746 -0.8897807303349454 0.01545869967612042; -0.3845125217852459 -0.8660959201232201 0.0595623181632033; -0.25074420932651464 -0.8328879482223247 0.06618674123489034; -0.1562010398806513 -0.782506799826215 0.05663281267460723; -0.08963029099274077 -0.6955803608136205 0.040725635567769376; -0.03579683914976781 -0.5103095698513694 0.022483515806162563; 0.054945234199508655 0.14977661902108105 -0.025469760738754343] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-6.161620202786709, -3.655571526334963, 0.5856830695389122] km/s
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V∞_out: [-2.7002022006751494, -6.66028396264326, 0.14619073909240218] km/s
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time of flight: 1.8962639976772875e8 seconds
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arrival date: 1989-12-27T22:28:57.235
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thrust profile: [-0.26791212662068803 -0.40688812850114925 0.026691805648649283; -0.266793262589658 -0.3778696834005156 0.027900181098762564; -0.26200529242073944 -0.35378473637283925 0.028633111777203325; -0.25347619440111424 -0.3336772131637166 0.028924627456557037; -0.24128366780550617 -0.3168630085153627 0.02882736146831922; -0.22545597377689272 -0.3028665621167754 0.028380909055401932; -0.20591220119170045 -0.2913793749692859 0.02765148313386833; -0.18239201753865897 -0.2821988061853844 0.026654956702915733; -0.15441194468233171 -0.27517644001068375 0.025384839841290315; -0.12120497217280553 -0.27008163471193997 0.02382575134158362; -0.08180423743214563 -0.26638133593843133 0.021853200343975244; -0.03559861184211625 -0.26289589134190455 0.019323333554878752; 0.01615550067601636 -0.2577838661570208 0.016091495954574812; 0.06905746459059815 -0.2497412095969394 0.012226229591249709; 0.11810325646272977 -0.2395703028520304 0.00804111956320996; 0.16128017869471004 -0.22936084855668964 0.003803922133384859; 0.19913721147690577 -0.22075888291860724 -0.0002865981573597917; 0.23289402715561758 -0.21456195491530816 -0.00412606331776826; 0.2635970662374559 -0.21101943812025215 -0.007646212949431516; 0.29197382006432404 -0.21013550409926826 -0.010839526103107245] %
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Phase 4:
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Planet: Uranus
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V∞_in: [-0.6121969849040167, -7.150375871374237, -0.13070109116611242] km/s
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V∞_out: [0.0007739939100291959, -0.03314950424200176, -7.94754221529655e-5] km/s
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time of flight: 1.767996002536118e8 seconds
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arrival date: 1995-08-05T05:28:57.235
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thrust profile: [0.06556180290998989 -0.4810097896203703 0.001892764138566078; 0.05798846767670954 -0.45547090983767 0.0021156315191879025; 0.051689770885915726 -0.42832132722472177 0.0022959057542090914; 0.04648700280108465 -0.39928121074291384 0.0024336442919551666; 0.0422028841595979 -0.3680710941209755 0.002508087270289503; 0.03867267523413679 -0.3344021401798511 0.002525995849605425; 0.03572097003592147 -0.29802013051252274 0.0024864926364152923; 0.03318882991262833 -0.2587147803564456 0.0023938091349767227; 0.03090542603076421 -0.2163770501304412 0.0022582652803209927; 0.028677181687678518 -0.17104667286314865 0.002097118557040994; 0.02619154533459498 -0.12299356889209265 0.0019574717120907272; 0.022731235300107018 -0.07291026524510676 0.0019498981886554635; 0.013464668655989014 -0.024663380581525153 0.0024792489578653563; 0.022851842286257088 -0.0034654943191003017 -0.0014195501664108637; 0.01695459135761096 0.042960833303929385 0.00027136301763064255; 0.019109715763285105 0.0939108023750647 -0.0006238697198316213; 0.019041699615714294 0.14424641548655956 -0.001297833776791727; 0.0181625271663931 0.1928667562989665 -0.0018850620022324046; 0.016846067007602567 0.23934680582993179 -0.002459940248822858; 0.015214354318562582 0.2834687949061578 -0.003064218239253031] %
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Mass Used: 2673.1939593971797 kg
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Launch C3: 43.74597009857089 km²/s²
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||V∞_in||: 7.1777254771611645 km/s
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