37 lines
5.0 KiB
Plaintext
37 lines
5.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-30T08:40:36.355/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: 2024-11-29T10:54:51.469
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Launch V∞: [-3.0580432001025106, 2.2375690420359073, 1.0588738801940067] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-4.571073362651481, 1.5280878123442105, -0.45427388957404374] km/s
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V∞_out: [-2.4964790697852464, 4.131812654452342, -0.3633277130442272] km/s
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time of flight: 4.098218966605439e7 seconds
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arrival date: 2026-03-18T18:51:20.469
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thrust profile: [0.02250623498780786 0.056715344804171675 -0.034873620216503566; -0.01586442265299213 -0.06295338578554689 0.08519483155847359; -0.01017916810128589 -0.13656445837778508 0.13681516443703864; 0.016841859589487678 -0.20255260280181142 0.20891399350975495; 0.062143156420800975 -0.28723660826482245 0.19358888229070814; 0.12715651158662364 -0.3394613038803359 0.20147574219826075; 0.20972581667196719 -0.36860712178143235 0.1951519573601803; -0.09233171629208815 -0.37108179526235385 0.17885323373772358; 0.3963663785610897 -0.36411236763263627 0.13917684957996404; 0.4803269916210104 -0.3294208336249097 0.09820475158586775; 0.5482500580902477 -0.26964129417960103 0.048521784619223775; 0.5975936677510483 -0.19019649689789742 -0.002336850116568105; 0.6325139378587388 -0.09620606406958827 -0.051883810140986475; 0.6526011444191557 -0.033184627930530654 -0.09806508414837138; 0.6603449674456996 0.03554980785042415 -0.14075413564780873; 0.6548829138633075 0.1249977655026878 -0.17838380784227764; 0.6314304294837665 0.25982925441811655 -0.21188069709202154; 0.5851498705012528 0.4073099939525669 -0.23422861887565163; 0.5033984822411408 0.5327877791886333 -0.2470941526499058; 0.37097506574856026 0.6250076852929124 -0.25134269316042973] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-2.888718591099067, 2.98093500374621, -0.03527346962365893] km/s
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V∞_out: [2.3790932465957977, 3.378686597227906, 0.3953591906305017] km/s
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time of flight: 1.0806802469609727e8 seconds
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arrival date: 2029-08-20T13:45:04.469
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thrust profile: [-0.23488496954455496 0.9896419507072445 -0.11601157743285787; -0.948717799093386 0.9810049502433882 -0.11137913018095054; -0.9878845940359288 0.8353827321448694 -0.08704039668042218; -0.9873512008683539 0.283891063339361 -0.05113640206170415; -0.9867884331885424 0.06209683131941994 -0.023752079481471355; -0.9535019575354626 0.09042898307599517 -0.006869177979295686; -0.8629780107614938 0.07500054807185184 0.004358596231624515; -0.7266566061890536 0.04691475374478784 0.014062645283394093; -0.5808329590842135 0.03171216226293981 0.01492806895495031; -0.45651135691182687 0.02498400153146004 0.02067482320548018; -0.35501493081559393 0.019422083647277044 0.02044779215749133; -0.27657576243518855 0.011215381224156324 0.02020194799272021; -0.21016915317145918 0.0012589829531977736 0.018128327930858827; -0.1540086140112979 -0.00846566443167276 0.014833095420263493; -0.11001947393418925 -0.017257120988655155 0.010078742680114872; -0.08042976828632163 -0.026027288334698796 0.0033185622120666994; -0.0629225614505061 -0.03930242635942339 -0.00425731557389946; -0.039084131760545315 -0.04757303261125456 -0.007171372481770967; -0.02892366311071207 -0.04758562095515022 -0.027423761082656064; -0.032231185187749124 -0.05078891683404573 -0.03274525516746696] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-1.031508320728017, 3.034062901615318, 0.15878852483474554] km/s
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V∞_out: [0.2528673092202353, -0.0017020120539992514, -3.464904646047938] km/s
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time of flight: 2.8592742241253144e8 seconds
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arrival date: 2038-09-11T22:02:06.469
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thrust profile: [0.061035494563444134 0.11929805743419754 -0.05461112133488575; 0.031266058641029826 0.10685642176058087 -0.06293750177877995; 0.027970653885991688 0.09862792518563299 -0.045534907819447135; 0.04107581844710626 0.09322334760151729 -0.04122709275105615; 0.028048942877953027 0.07458987618035917 -0.0293725553620492; 0.024315747642101215 0.10122639432961994 -0.018308088524984865; -0.020351662679905323 0.12588983468280268 -0.003296359905923822; -0.07496938768838549 0.13064499952764547 0.02049090758833104; -0.11466260045345358 0.10481780256514156 0.04012703743869543; -0.13862140670508313 0.07032047401299907 0.05293678290006058; -0.12563192616320198 0.03543281578759781 0.05260279035660168; -0.10942634615118742 0.010406138047878839 0.04847794436412976; -0.0883793299482217 -0.005946135827960692 0.04035916568664598; -0.06302255227760427 -0.014764403237537608 0.02898877705275781; -0.04498980023607455 -0.018979702934655323 0.018607571396221836; -0.04140068077722925 -0.021838625953655242 0.012261185161105725; -0.012314656602333676 -0.007156039336999209 -0.0015716845681593603; -0.010603730130079583 -0.0013797109292671373 -0.006338804956808768; -0.017028324565081396 -0.005918175097290475 -0.004776176869816615; -0.020105440868362738 -0.009689084862531186 -0.0020482929935368567] %
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Mass Used: 847.3804986047398 kg
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Launch C3: 15.479557325727804 km²/s²
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||V∞_in||: 3.2085449821233127 km/s
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