37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EVMS_2021-12-14T16:31:21.927/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: 2023-07-04T03:26:06.312
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Launch V∞: [1.0595449194495574, -5.179046997413335, -0.710854272622436] km/s
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Phase 1:
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Planet: Venus
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V∞_in: [0.7167821480418011, -5.3523238156588455, 1.2976343649115025] km/s
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V∞_out: [4.57208952781187, -2.763307224201735, 1.5182287145267939] km/s
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time of flight: 5.770490213360378e7 seconds
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arrival date: 2025-05-02T00:34:28.312
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thrust profile: [-0.012518442262623266 -0.2846133058802652 0.036714163181811914; 0.04598892978893719 -0.4496628555421884 0.050821562545283167; 0.23858170610390916 -0.5534890194603386 0.053378611889742245; 0.45971698047001736 -0.6075384006689931 0.049225674552565796; 0.6103599468173085 -0.5939492998556735 0.02390794631734322; 0.48631512404956767 -0.5016073617028688 -0.0035970332832769504; 0.7205092838499264 -0.06817749918391544 -0.030568869866240404; 0.6554236549877296 0.43397088287936925 -0.04092445445978924; 0.4426214422172243 0.5233653736000612 -0.04291086849556375; 0.1265987354418195 0.37111271167996557 -0.04211705533923255; 0.14291026132925347 0.10951608658101342 -0.03253146989706353; 0.043819468335856315 -0.2760884262553685 0.027757067112302112; 0.12296287504557858 -0.4824942105922541 0.039565941973149145; 0.34178968176729657 -0.5570754798887297 0.042557000779956305; 0.525918072341391 -0.5414835388569836 0.028260866562936558; 0.6470594344300419 -0.5105003019983401 0.0030006706220706667; 0.5771986338738871 -0.2149560721661336 -0.021449899364102736; 0.6724367414193944 0.3342772748116172 -0.034581763000182654; 0.4545022153210568 0.4845067333568687 -0.03498154387686175; 0.15460631758712481 0.30947276279006714 -0.034528617189168165] %
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Phase 2:
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Planet: Mars
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V∞_in: [6.053679269318452, -2.70754196571206, -0.561868816241759] km/s
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V∞_out: [6.62831028724014, -0.0335448848261144, -0.598213998623492] km/s
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time of flight: 9.066465712235557e7 seconds
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arrival date: 2028-03-16T09:12:05.312
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thrust profile: [-0.14077705817283215 0.17219038983580243 0.0010673207963448805; -0.09076911485954396 0.3656127875299659 0.07959031496882961; -0.22901583771408088 0.3398208518705999 0.1109715317716953; -0.32670071352071345 0.2280441403604959 0.1147286298393803; -0.628253671808909 0.07416681520769915 0.07809920940474491; -0.3363546214364444 -0.0738216870465495 0.051587092016739784; -0.22220741723836346 -0.1904607293157175 -0.008841671167926259; -0.032348160495606626 -0.20217939877808486 -0.09753767695663382; 0.29315934163115015 0.09200142472327252 -0.05343148185045425; 0.24059656978259783 0.37859909374997347 0.022698241631866987; -0.0271078201127222 0.4659834877302928 0.08034951421535458; -0.3164477633221403 0.42340838072348136 0.106820004124928; -0.4327826247755731 0.29532199369082585 0.10616547737632574; -0.46971892563271284 0.07217513538995383 0.07291051527360017; -0.4205532859364489 -0.17888301219299818 0.049620946374109944; -0.31397875164405536 -0.3499883855343491 -0.01722453765780476; 0.055748170553023536 -0.4155273836848591 -0.05564285735614245; 0.4306072283821911 -0.1907071754065535 -0.06468622506578485; 0.46309518107140285 0.3221076719593664 -0.026634119992690917; 0.2485211129542623 0.5082032846330088 0.04664261897154823] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-0.15931607365900702, 6.659982567616171, -0.7147859007662032] km/s
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V∞_out: [-0.03141285197558282, 0.00666134026526007, -5.85929449610048] km/s
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time of flight: 2.264417121463342e8 seconds
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arrival date: 2035-05-20T05:40:37.312
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thrust profile: [-0.3528081960729175 0.5957253626842559 -0.04112855090660253; -0.4498696875407646 0.3599016941813443 -0.008926830351384682; -0.4296518057984319 -0.20738905197149196 0.009333332557682678; -0.14954953849570887 -0.3435796518536134 0.035875098563252904; 0.39678430953935184 -0.5168745604329268 0.02935112983491381; 0.571454084996011 -0.46813508275649046 0.012118057152003993; 0.7040073430650443 0.38813276418344744 -0.0015818210549435883; 0.6929710132849697 0.6613684228669995 0.041556415408789134; 0.47766142600053263 0.7290623000841082 0.057207252732303655; -0.20126978731123335 0.6865609825371612 0.04700537721488603; -0.1726478786848928 0.5473873161459025 0.033978777160795566; -0.23702248937731904 0.5103684148600998 0.011996785197593873; -0.25066827594702035 0.42611462142301987 -0.006783200240873317; -0.19809970132181848 0.42158636663551524 -0.01768186691013301; -0.1581469693984499 0.3721724862460802 -0.026688684037946272; -0.11314582650191973 0.3541426305930295 -0.030452326114901382; -0.08143085687847508 0.2759935128733878 -0.043735992358310494; -0.025930504510641876 0.18682783519552412 -0.06228985999553243; -0.01540965514296248 0.09256748216309786 -0.0716228215794782; 0.0639416491137141 -0.15066247627007892 -0.10320894780723987] %
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Mass Used: 1536.9108057812873 kg
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Launch C3: 28.450477034653016 km²/s²
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||V∞_in||: 6.700124498560573 km/s
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