37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-29T21:56:54.243/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: 2024-02-03T22:31:58.060
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Launch V∞: [-9.983658485652342, 5.052584189132008, 8.454011703658189] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-9.953421438043394, 3.213281933198845, -5.745066702073697] km/s
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V∞_out: [-9.111152118008471, 4.863192665850899, -5.978278871452932] km/s
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time of flight: 6.973930850639665e7 seconds
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arrival date: 2026-04-21T02:33:46.060
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thrust profile: [-0.9327909510849908 -0.5004864936548854 0.5880652125453542; -0.9029912019179394 0.5317310327031032 -0.479053583548179; -0.8739292812639873 0.6883047550245208 -0.5367631771071988; -0.8429685817072956 0.7298891216769086 -0.5130875244914932; -0.7976818801439988 0.7445652374517617 -0.43930087061099776; -0.7138755130219845 0.7567268126061615 -0.12248962250324259; 0.3962540499696817 0.7641554988596735 0.46486366383018496; 0.734311596231425 0.7455876887812815 0.47150616674759604; 0.8174592629690127 0.7463739223262722 0.5121440363573074; 0.8611866709577258 0.7575379533647393 0.5286900263176879; 0.8878359656973905 0.7764148245561391 0.5284942874419258; 0.9054328385770163 0.799696138207671 0.5134234416727862; 0.9175793861615414 0.8244011769369346 0.4786693481341792; 0.9260901378249389 0.8482781912744276 0.4059545252589148; 0.931827122595938 0.8695510665682376 0.27969911096378186; 0.9351654063561202 0.8873770941740391 0.0557896800207434; 0.9359855094240302 0.9011770122818098 -0.21365898834998476; 0.9338922411647969 0.910802339678919 -0.365757719064907; 0.9278284047571169 0.9146993842728531 -0.45267349649595484; 0.9177962416138067 0.9074601171998934 -0.48335462518998995] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-4.046083430194879, 6.572285306163753, 0.7499685576972142] km/s
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V∞_out: [-6.445354159446693, 3.323503238892241, 2.745880595515267] km/s
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time of flight: 6.991559948627624e7 seconds
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arrival date: 2028-07-08T07:33:45.060
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thrust profile: [0.5340118690878064 0.8946355483481895 -0.6067329080424446; -0.3678947664519958 0.8593146540157065 -0.5131755344574285; -0.39005831784853146 0.7991144657043887 -0.41508437369833046; -0.10776295134122015 0.7502923022084157 -0.3752944615562001; 0.17190209160722916 0.7255675171054287 -0.36441383578999126; 0.2980908476585895 0.7135279015946394 -0.35965213622497433; 0.3456788185986325 0.704810230513307 -0.3538631475411222; 0.3583977073758296 0.6949801520421466 -0.3447797296975572; 0.35356864150294026 0.6822744172223295 -0.3320858164407262; 0.33890034451249423 0.6658132457508765 -0.3160568300648956; 0.31830164408791184 0.6448711256196155 -0.29701300971671146; 0.29395968164603875 0.6185806040894148 -0.2752331841044432; 0.2672555928298822 0.5857596234549681 -0.25095251239959365; 0.23904121980768947 0.5447808233719543 -0.22439601711290494; 0.20994568191742563 0.4934318160029573 -0.1957402258157503; 0.18033604818385496 0.42882214377711125 -0.16518210760018237; 0.15047492443932542 0.34753119746438316 -0.13293973479266868; 0.12055531050530945 0.24650927403513742 -0.09927152610592575; 0.09086119930934154 0.1254331780451551 -0.06454483894976729; 0.061810968904553794 -0.011869676978603206 -0.028875376938032212] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-1.7080958958005663, 1.0532975410358802, -0.5234285178154677] km/s
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V∞_out: [-0.042057638575385886, 0.01628965046711138, 0.0014262587493817428] km/s
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time of flight: 5.410008000022286e8 seconds
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arrival date: 2045-08-29T21:33:45.060
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thrust profile: [-0.0006869622475465983 -0.05655873970732918 -0.08006272268398595; 0.003873967057859684 -0.05311730345001728 -0.07482636442553423; 0.006727479367092001 -0.04684548439756908 -0.06417959013850079; 0.008028763484199715 -0.039535927541232405 -0.04928157856745151; 0.007320491169929365 -0.0336280046809453 -0.02966715910096899; -0.005028754990363752 -0.02826953540745633 0.014881687165696877; -0.001695926581312149 0.007613100970810841 0.050070217801999904; -0.0023998275768972828 0.0206376998032102 0.06370073498988323; -0.006452242213360922 0.03719762725683077 0.06583225244312285; -0.05603050531565261 0.05854878555357484 0.025067239804525545; -0.09154744763319163 -0.03948563977311411 -0.03805667977702517; -0.05562816267322614 -0.08822935587386244 -0.06523679311574879; -0.024248131898468382 -0.09707814140258143 -0.07671757975959173; -0.0030870165238090197 -0.09430812478084437 -0.07870021435343663; 0.012035011271421321 -0.08691656821902476 -0.07510940925295292; 0.023445741439504515 -0.07733785582837824 -0.06757603737096467; 0.03215470722975334 -0.06621504620132651 -0.057202473970260556; 0.03899097797944084 -0.0541010495031209 -0.04437035069889279; 0.04467776739937306 -0.04067992873557019 -0.02923518241367051; 0.04933972022676261 -0.024386103562346783 -0.010272768238740664] %
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Mass Used: 1444.6973474601969 kg
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Launch C3: 196.6723576319944 km²/s²
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||V∞_in||: 2.0738863788707107 km/s
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