37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-30T14:09:25.262/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: 2023-11-16T09:01:46.766
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Launch V∞: [-1.2358227541627522, 0.323049558821953, 2.495135844447432] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-5.492217326783208, -0.7599139192265875, -0.7445133837270346] km/s
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V∞_out: [-4.404936994877108, -3.4463054890902294, 0.12597397946441688] km/s
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time of flight: 1.1637720070766585e8 seconds
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arrival date: 2027-07-25T08:01:46.766
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thrust profile: [0.01055136636996065 0.5035473835223019 0.2144643592551079; -0.04595477215059715 0.6852423614947899 0.16820399057019442; -0.5895802429453626 0.7197253917092584 0.15157285154237687; -0.7242691347954416 0.6365969821781644 0.18351832934110204; -0.7254557218972608 0.33325583626785743 0.20650030599325478; -0.624534757383007 -0.46380253719846265 0.19914261964212518; 0.06888536686167775 -0.3659727992321626 -0.05660421386154573; 0.41960359345145115 0.5802522947366238 -0.02564875636361316; -0.43557904354293114 0.6848106459808407 0.15045741326417394; -0.5906326245605844 0.626327253137284 0.1907051751516841; -0.6145984992977067 0.6853285910994333 0.24790988830917382; -0.7852172198133732 0.397363217233713 0.22913677229660695; -0.6148113166692493 -0.6180162700085184 -0.1063370011071445; -0.3438743055901661 0.08561279547696703 0.1133320954927072; 0.24423988113626285 0.4984911769229264 0.26361771766972686; 0.6070536708822735 0.7233947175576885 0.2890649522953669; -0.39805774605395056 0.8544543105302159 0.2032769540887175; -0.877234342411992 0.5568182222065088 0.1181949174776601; -0.7848468400087453 -0.7818849886318364 -0.025654657156075657; 0.39491632368805846 -0.7677648336006526 -0.018827493121373502] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-2.011375822763062, -4.005960504046318, 0.6209700805836994] km/s
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V∞_out: [-4.246987681230396, 0.16498798356943736, 1.5540119004205253] km/s
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time of flight: 1.4691600181840378e8 seconds
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arrival date: 2032-03-20T18:01:47.766
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thrust profile: [0.681909870255602 -0.5761969653838755 -0.02754846539663112; 0.7118573450786314 0.31247951434638493 0.043677226876746314; 0.5476987320075556 0.6581866365943503 -0.003833400581880826; 0.10725439389134384 0.7294932911664623 -0.034290527364056536; -0.5427655230030919 0.7281280491625349 -0.0299219686998862; -0.7331645357201648 0.661529122002647 -0.022598124369638494; -0.7921492428190279 0.3933778983017051 -0.021082156107776216; -0.7932731599235451 -0.41313404927011227 -0.019757316586946027; -0.7424285866522327 -0.6896359802485261 -0.021540954373280186; -0.6106751913915949 -0.7225982342788454 -0.020163701822483136; -0.37316409906634423 -0.7007771556440968 -0.011208908465949893; -0.1711206238316838 -0.6415857635215466 0.0059500126042923785; -0.08270331405821842 -0.5687506908923067 0.02659262994655598; -0.049372522261264505 -0.49783910816632987 0.048628191706214005; -0.04372663474025917 -0.41699938093001865 0.07363018971956578; -0.05490501770449129 -0.31189423172940106 0.0949294276017952; -0.09260972837599633 -0.2199470543952063 0.05957362145438097; -0.0634254159444419 -0.17400774633467572 0.16341908215231168; -0.05232699030024355 0.08812711882068765 0.1012502462026133; -0.04359653224713776 0.2114603900012656 0.04944539701697088] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-7.936261563870153, 0.192812008719828, 0.7850203435347649] km/s
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V∞_out: [0.08172234404293398, -0.35122508987936396, 0.006338068922481654] km/s
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time of flight: 2.9010960004261374e8 seconds
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arrival date: 2041-05-30T12:01:47.766
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thrust profile: [-0.1762427833398218 0.018451914856523026 -0.33296833868061293; -0.10855107710674605 0.044463310211183146 -0.33965829997250213; -0.04955955263781527 0.10666486336804054 -0.3343168817737069; -0.14933152742910255 0.1645563456813175 -0.2888802750452695; -0.011372547689235173 -0.39964858425741717 0.1289083844812905; 0.17913823101853307 0.33922366300742973 0.3624022918784145; -0.056147608885838356 0.40536943517001855 0.2345805092442894; -0.11646645449972745 0.37970664664911913 0.13215537014712256; -0.10774775336158972 0.3637144687183163 0.07982907905717164; -0.03689877185389765 0.36730516793108037 0.04229495484147119; 0.08041474785484633 0.3975271403801768 0.011450007794323156; 0.2209067582381832 0.4645747308847809 -0.016359218295681436; 0.29077903309671577 0.5746646081920227 -0.03785392741655643; -0.5440697079277356 0.7004154769551414 -0.02197571950265878; -0.5081898184366466 0.06445088273594297 0.0502311733117999; -0.19802320496526152 -0.07027856584170135 0.014625860167883831; -0.07715652979513347 -0.015846719041313496 0.0076264391612288025; 0.180938962168102 -0.0850580439905663 -0.026509928911235665; 0.28645290190644923 -0.11681132361576753 -0.037935422919142044; 0.4089515815441177 -0.14951729956288723 -0.05914131349793209] %
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Mass Used: 2473.604423137509 kg
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Launch C3: 7.857321779407867 km²/s²
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||V∞_in||: 7.977322923176217 km/s
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