37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-30T13:52:11.363/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: 2024-12-15T22:51:31.653
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Launch V∞: [1.0265298829626757, -6.097752351134353, 0.6856608803521997] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-0.685353880716249, -3.6396637778190533, -3.2013166230561305] km/s
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V∞_out: [0.5302103364593528, -0.9765757196202859, -4.767844807662866] km/s
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time of flight: 9.971640000084461e7 seconds
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arrival date: 2028-02-13T01:51:31.653
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thrust profile: [0.13284751649644205 0.9411989426214641 -0.46977683989334873; -0.968547907767294 0.9608251103851381 0.49339267132424175; -0.9787154450158303 -0.8432228864566057 -0.5543030062336614; -0.9458849725429278 -0.9442327236046363 -0.7636886633819076; -0.9667535016847152 -0.7358061408218618 -0.11636279319023346; -0.9820303864106136 0.7930475060706941 0.4962497106503541; -0.971227150319471 -0.986463218458502 0.4632222480421968; -0.9271319319791395 -0.8917240929018778 -0.6101593732712101; -0.9139137651217345 -0.5324029885065178 -0.8083289582144534; -0.9773913889808017 0.991657638900593 -0.4106474876750948; -0.990512335176245 0.7321537085435096 0.6605421761973608; -0.9581179828820583 -0.984882219664571 0.6421847460531694; 0.9803502761290055 -0.9432783942684786 -0.7125092685705092; 0.584101463120002 0.9947933997204838 -0.8808317684328829; -0.993526887524295 0.9941311908456837 -0.7387372801949493; -0.9957384470386984 0.9741994738088207 0.5708597976999408; -0.9915748324180956 -0.9960584321805054 0.8295257560724948; 0.9959387668352474 -0.9942746434271464 0.1695440717133519; 0.9960944736420316 0.8745766502055389 -0.7915289853600778; 0.9903811167032217 0.9961817491550279 -0.9573032378642442] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [2.090864620573387, -3.222147331578074, -2.509087132015622] km/s
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V∞_out: [-4.488106073949989, -0.5175537490206633, 0.7987014856646427] km/s
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time of flight: 1.6423199999993336e8 seconds
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arrival date: 2033-04-27T21:51:30.653
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thrust profile: [-0.5660855310698739 0.9967906693759188 -0.8209919327744069; -0.994170631248832 0.9947713712108747 0.1448631429571182; -0.9945000494219841 0.9274125399233997 0.4897574376167066; -0.9894742986247569 -0.4507820161619902 0.4166941133651491; -0.9714202588117182 -0.7137518679961032 0.30094666125802183; -0.9405225764860856 -0.7041104481825169 0.1892804023301685; -0.8322614400348775 -0.6078444193505477 0.10175874680514145; -0.5733990958821588 -0.4496883690491375 0.04286046670382909; -0.2872975060978055 -0.27194044695575137 0.01185750904851918; -0.03409685881889757 -0.09226785043335413 0.0007765631982848799; 0.041566915656923824 -0.02743199843891902 0.0012223583050356183; 0.03704247583337095 0.003644238002607764 -0.0017388167642256004; 0.055997436147982374 -0.022254514712059217 -0.007208925051407416; 0.24811520314082097 -0.1362846587264196 -0.02883669922015275; 0.4207497452192147 -0.19686359679762824 -0.03935341240442315; 0.5330387060152292 -0.22897802946531448 -0.04350654265126503; 0.6138159398623063 -0.27334600431296685 -0.042974346394558584; 0.7031513931411775 -0.3631789642405433 -0.03783836908358169; 0.8144978524655395 -0.5249342706264041 -0.03246396629051213; 0.8897103992638571 -0.708341160251077 -0.03341117930579575] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-9.950524772292589, 2.7136858826882397, 0.8437847433534009] km/s
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V∞_out: [-3.9746513384546427, 3.419068378994426, -0.22492206192340505] km/s
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time of flight: 2.4062400000004002e8 seconds
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arrival date: 2040-12-11T21:51:30.653
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thrust profile: [-0.026861539030662098 0.053037742486198663 -0.03998103891716118; -0.4005257165378705 0.12385064839383274 0.04228749257228828; 0.11316689356297174 -0.5002033317813458 0.0920099903831136; -0.4310529749448192 -0.3737769540652961 -0.16434453658789766; 0.524935339397772 0.326736433374278 -0.011049835879189725; 0.2870548648523757 0.9008250510979924 0.043684490460944636; -0.2578688762031856 0.6811275515417524 0.06979705435650777; -0.16643689458434993 0.44448647933073615 0.03748178826678883; 0.03135747943986613 0.09121026982102139 -0.011021906895529003; 0.2773784563100772 0.21421663651317946 -0.0939720012037749; -0.026321949219467622 -0.002583681933706951 0.0022197546795018445; 0.20252009126605577 0.5859029556414175 -0.10288257122681152; -0.5835246166241774 0.9904709316092567 0.042044833954454276; -0.7362038421319124 -0.20746802611665538 0.26205247161144074; 0.025644898980856885 0.13288887758204784 0.067531572098157; -0.1567362766945195 0.020710809244175152 -0.029197896508943184; -0.35499348849403123 0.09675115246414323 0.0008648920068945578; 0.08552766541451494 0.35786531030916835 -0.019970820204502436; 0.07564615169332112 -0.16796111456618562 -0.022460352690263453; 0.25493279832576426 0.09735303708739874 0.0929229928187175] %
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Mass Used: 3003.684776260021 kg
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Launch C3: 38.70647817922525 km²/s²
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||V∞_in||: 10.348381854523241 km/s
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