37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EVMS_2021-12-13T17:44:34.669/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: 2024-01-06T04:29:48.093
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Launch V∞: [0.5457290374235895, 4.341334791096552, -0.7559687755701914] km/s
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Phase 1:
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Planet: Venus
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V∞_in: [0.8335159107192338, 6.90456105315263, 3.5067701274587337] km/s
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V∞_out: [6.76973645767487, 3.7624182770964607, 0.8285997001531188] km/s
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time of flight: 1.0236386879690988e8 seconds
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arrival date: 2027-04-04T22:54:16.093
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thrust profile: [0.20124636719972494 0.28871460999851783 -0.24826466053632043; 0.21757301989581354 0.24241685861764573 -0.2950961505210993; 0.271442849091815 0.07872734315816171 -0.19097989520692127; 0.1879742866678929 0.27655633192716367 0.10042573300235896; -0.14244608091005748 0.33201061328346854 0.19340046097242167; 0.17387986662182686 0.3014608753850556 -0.15431719711609648; 0.18777345028680853 0.2673897380502672 -0.25525617202163087; 0.2556315993639935 0.17739994769888612 -0.27159167007539076; 0.26609722508102157 0.2783459216563457 0.051977998587726774; 0.0438700045849084 0.37141025221234536 0.20109295136087044; 0.06232447288714108 0.35663405987308516 0.024990128722474907; 0.026521151688839967 0.3160983251683631 -0.16548739972882243; 0.19612956542640614 0.24782370475857005 -0.2471047602651378; 0.31651280507021246 0.18621565754181835 -0.19804312266917037; 0.24435157836852087 0.3468639663937176 0.1852596358565247; -0.00965870127546034 0.3979396968294011 0.22213565307438407; 0.023169341463938578 0.30016276019204574 -0.18664622656660942; 0.1268886531461076 0.20680899035126646 -0.25936562207083624; 0.2125169373278653 0.24319285890159614 -0.22236991044858823; 0.35244171182303646 0.25085960304558635 -0.1638088094827891] %
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Phase 2:
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Planet: Mars
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V∞_in: [8.963228181916202, 3.147920284899006, -0.7449749580149643] km/s
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V∞_out: [9.377239868662178, 1.0270817933951877, -1.3450268054813155] km/s
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time of flight: 1.22946548225175e8 seconds
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arrival date: 2031-02-25T22:43:24.093
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thrust profile: [0.2815247284876436 0.4687108668970388 0.07024363175566978; -0.28575122080824394 0.3851477052454153 0.016801525539966562; -0.3747967738284827 0.29808121010819033 -0.07185502866615309; -0.442929227216859 0.19222627634169495 -0.135743553778548; -0.4487478745447117 0.1327038699880746 -0.09503248552633654; -0.49852432866134694 -0.13114566918915876 0.14249733878062454; -0.4800686097933296 -0.20421918036330872 -0.007593654428925882; -0.29831925246774027 -0.05272129811015332 -0.01656649869964936; 0.035964682967361335 -0.09683145552380305 -0.15527299210182244; -0.09302182221116087 -0.33887428309830736 -0.2404084153476241; 0.5923912702376002 -0.02542163181573757 0.2009826493089844; -0.02623028033428319 0.13880579512402433 0.24850570533865052; 0.29039130962158227 0.3062352881282009 0.1527335375754828; -0.12082271353315516 0.4096496613048553 0.02796560796386028; -0.027194067272572214 0.35743634565580396 -0.04064730736657738; 0.04127166490432071 0.24768556235295525 0.09118781754436289; -0.11854966698415786 0.22553475056440592 0.08555412347860751; -0.1806405003127596 0.10096300132551984 -0.15472306505086783; -0.20075020241889296 -0.009061662245205257 -0.11023054116740935; -0.2987954790790834 -0.230652241463122 -0.11725959697110766] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-3.1812528488033522, 8.51185716671171, -0.7460758734937367] km/s
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V∞_out: [-0.21505538492794815, 6.349830695161589, -0.12985627371130587] km/s
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time of flight: 1.315250993552624e8 seconds
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arrival date: 2035-04-28T05:28:23.093
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thrust profile: [0.7987730439865184 -0.41345767452772897 0.001505324112112355; 0.8674728852573501 0.6602259691893515 -0.0759345729834176; 0.7597133759248544 0.8594908841609692 -0.19125255627342094; 0.2872093106917861 0.8668264267695036 -0.18904379386155162; -0.5401943922623963 0.8498080030613695 -0.16437663889563423; -0.6896408194237241 0.8199272255247071 -0.15201175224165175; -0.7134753635114731 0.7870386683779858 -0.14239308646192794; -0.7170346050334127 0.7501463142097656 -0.13294598405115826; -0.7002315120575128 0.7090750008587086 -0.12315905659225605; -0.6872097378697336 0.6676696143275933 -0.11572226052465101; -0.6627939184703779 0.6168905813867107 -0.10527146741337202; -0.633554979686539 0.5685903428331747 -0.09336745543158023; -0.5918530549537074 0.508122677783068 -0.07972015422869783; -0.5468540100379315 0.43929599357406623 -0.06477133727408631; -0.48985935766804956 0.3608169402041227 -0.04832795620510983; -0.42117899759427235 0.2697982895066768 -0.030347981218191687; -0.3351818344708077 0.16466291198509436 -0.01189485088684984; -0.23232691164467884 0.0500315224688059 0.00787577036146254; -0.1131949765395752 -0.06833292217756129 0.02847742053557143; 0.005991615157979781 -0.182291757352861 0.05024929371428449] %
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Mass Used: 1536.01990119313 kg
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Launch C3: 19.71649674030971 km²/s²
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||V∞_in||: 9.117494794269444 km/s
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