37 lines
5.0 KiB
Plaintext
37 lines
5.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-30T16:38:03.240/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: 2023-12-14T15:10:10.657
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Launch V∞: [-5.324790803109733, -2.6773113758857146, 0.3590879071328112] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-7.8280744026110485, -4.482906734167364, -0.5270128091140733] km/s
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V∞_out: [-8.714629007362692, -2.3006682785347587, -0.6459280917863456] km/s
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time of flight: 1.4074379597755253e8 seconds
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arrival date: 2028-05-30T14:40:05.657
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thrust profile: [-0.09620569960732477 -0.09890174838841997 -0.006304928381722739; 0.01019673300605273 -0.15089658441406675 -0.0021554349727457207; 0.07822408798843489 -0.11071926046790218 0.004988054677396156; 0.09762767912264393 -0.058415019885606094 0.010174486469221193; 0.09596476555630318 -0.005224025746863998 0.004950216517465728; 0.08806191952377797 0.049822770611354 -0.0010597096470122361; 0.052574331589681 0.12454094146924233 0.015095231992096524; -0.04001716917664013 0.21428169922925022 0.018454940281947503; -0.19982535032247195 0.251124726671319 0.015258419491383634; -0.42902456010053436 0.03773585135440942 0.01861953896594965; -0.2620621821264161 -0.3783347111418361 0.004523163861194378; 0.05160537420225073 -0.3786420625260984 -0.011042008482375406; 0.20360488108938318 -0.27582667506971054 -0.012821162414732887; 0.2561047977346709 -0.14853261531425635 -0.005634983638021486; 0.260486703242627 -0.01792491318881055 0.0011583161900218508; 0.23894329094312064 0.10878274252152975 0.0042064519174942515; 0.19707710072889273 0.2344075946499166 0.011104691405835861; 0.13172705128797849 0.35645392804648396 0.01747201373387731; -0.03343397706399435 0.37057486224934993 0.01628713138328902; -0.3349092116148668 0.40830706963065616 0.015783429576975126] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-5.164409827607087, -2.4015213190761244, 0.3886272138412419] km/s
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V∞_out: [-0.10084295997962195, 5.705933697922466, -0.1469580047293293] km/s
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time of flight: 8.148046230775028e7 seconds
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arrival date: 2030-12-29T16:07:47.657
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thrust profile: [-0.4843312801347405 0.17832592220013307 0.006256115010001196; -0.5117377393427821 -0.03515133875253644 0.01594069776607602; -0.4802829543105851 -0.22759690897497922 0.023218676108680135; -0.41688069406794315 -0.3255769239533844 0.02846987059703982; -0.3518609568473908 -0.3513841428236102 0.03707709560472825; -0.28197549119514226 -0.35416420109695057 0.04330975091368633; -0.22056035580872335 -0.34012444589770013 0.048672605940703245; -0.17030162641170815 -0.3176042986233552 0.054624244098160656; -0.12962198776772624 -0.29003617152610467 0.0600491991040185; -0.09552548126143237 -0.25742381683081617 0.06663476650221734; -0.06576162258943327 -0.22042535210328865 0.07376790136845905; -0.03794666493372705 -0.18080040001875886 0.07922467457462902; -0.017587190801326653 -0.144409275958737 0.07885131961718507; -0.0005846137879528368 -0.11383597257615993 0.06598144523941014; 0.012437749223779474 -0.08192500429520043 0.050363659542438856; 0.025006348976223614 -0.05271986038900855 0.03688810130605497; 0.03735035082457269 -0.023245071824888237 0.025225516789865676; 0.048771155783688964 0.00930403641764618 0.015175514053442753; 0.056121259671254586 0.03626182021235461 0.007719603871138727; 0.06549848774435021 0.06199167605994548 0.0029712452019925654] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-2.4750372046001954, 4.13041506892929, -0.09291157556920056] km/s
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V∞_out: [-0.9590001742156767, 0.00014166531615410308, -0.00017399656356734708] km/s
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time of flight: 2.204227460822756e8 seconds
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arrival date: 2037-12-23T20:40:13.657
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thrust profile: [0.1749523615814178 0.02337696203170268 -0.007290082696294586; 0.17710130749974723 0.04583257449906523 -0.00719233870000948; 0.174350248316964 0.07510311268410168 -0.00750473770426303; 0.16444589553075314 0.10998364297019214 -0.007106342278531456; 0.1384257291897476 0.1488418684122407 -0.006173412802780041; 0.08428653747267639 0.1721787470978516 -0.003985402948896598; 0.019687460364805707 0.15515729051991808 -0.0013753294272070818; -0.021656527704037976 0.12042770713394904 0.0001864640450765926; -0.039588280724834786 0.09367324460087394 0.0010034140790897994; -0.04673002735050872 0.07208768567973076 0.0013797248342607789; -0.04399767552371756 0.05335024899625606 0.0015132659877072718; -0.04235029705061875 0.03689185722542479 0.001509047848856101; -0.037623976049185055 0.022006890975873494 0.0010667085694236217; -0.031346917825053985 0.00585591622491494 0.00023425066193087632; -0.0193407989640302 -0.012237196189479828 -0.0032635963200177364; -0.011688504812844338 0.004985875856387392 -0.0034950987669932717; -0.013753919383294908 -0.020294143888963282 0.0018680092927586343; -0.0042296107469379065 -0.03029078043837534 0.002437090971995948; 0.010887719248873684 -0.04459982317696947 0.003041721188427454; 0.02500057674047783 -0.052736469222675816 0.0029604218341606117] %
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Mass Used: 662.0977457761205 kg
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Launch C3: 35.650337425378076 km²/s²
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||V∞_in||: 4.816094929158691 km/s
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