37 lines
4.8 KiB
Plaintext
37 lines
4.8 KiB
Plaintext
/home/connor/projects/thesis/archive/EVMS_2021-12-13T10:50:18.877/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: 2024-09-04T21:45:02.327
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Launch V∞: [-5.6873787586821285, -5.786560442422183, 0.9648939525882495] km/s
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Phase 1:
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Planet: Venus
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V∞_in: [-7.006322293689667, -9.989734050925524, 1.6254097214081484] km/s
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V∞_out: [-4.934010055766463, -9.703163112990516, 5.746968526613558] km/s
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time of flight: 6.009580685315006e7 seconds
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arrival date: 2026-08-01T11:01:48.327
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thrust profile: [0.9617110897949794 -0.8739870599865779 0.8811871230841061; 0.9871206021010024 0.9481933351857079 0.8854228336153014; 0.9863523895604293 0.994327102707624 0.946716091473592; -0.9902056621813372 0.9875449005030636 0.9064066950201374; -0.9820144764851901 0.9653224112558945 -0.8337378769726054; -0.9555449311854642 0.9657521915091073 -0.8456397221554082; 0.8186521316331613 0.967179361186583 -0.8354191171549058; 0.9767230165471376 0.9633104362664976 0.8377573650125992; -0.923042165035667 0.9919872228857152 0.9072115878002239; -0.9795463340184644 0.9795259853082192 0.8043752807295302; -0.9406150428550025 0.9782073002286426 -0.8112902954782957; -0.9274513227444565 0.9828383292971064 -0.7908058073919068; -0.9533956589270561 0.9748228662065541 0.7281952198186104; 0.9661510428771182 0.9785109691567555 0.8177356035250066; -0.9664218820049025 0.9817142137862231 0.7757757339784036; -0.41334310959750825 0.9802838606130235 -0.7678896522100085; -0.45597066444496603 0.9873708363619297 -0.7744051986443704; -0.9751395557218714 0.9865324811670309 0.015824267622547083; -0.9280161403357648 -0.21108826761839836 0.6838857520556988; -0.9068916875233747 0.9712348792258906 0.6625057816879225] %
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Phase 2:
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Planet: Mars
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V∞_in: [0.9553442830870951, -4.417820869496186, 0.18766425709383633] km/s
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V∞_out: [3.7230072885828505, -2.499904853935827, 0.5960484347667763] km/s
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time of flight: 1.0487898448288682e8 seconds
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arrival date: 2029-11-27T08:04:52.327
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thrust profile: [0.6774159131877868 0.6493226854927665 -0.532007553101398; 0.3302022275238012 0.6809208454980107 0.6535627201607142; 0.19857305554347673 -0.15250831748180288 0.670517038923704; 0.7186153785765315 -0.29289494991471887 -0.6203374026439823; 0.7630231141068492 0.7474131605948617 -0.34388402323483247; -0.14653416819603318 0.7578630202380595 0.6440008885838143; -0.5716565111866172 0.05476072550231505 0.5826761302304793; 0.7550937919052704 -0.5973801143592986 -0.5772563443665387; 0.8445567824974203 0.7474760718003378 -0.39238459367822853; 0.4972794197237329 0.8504015084039828 0.5954464117194335; -0.6051101474071697 0.6920479334729668 0.6384433528223871; -0.5485003210233016 -0.6848384869177934 -0.17001698436070412; 0.8818645425824932 -0.5572287228442382 -0.6059169981172697; 0.9056867468320952 0.8620079636158319 -0.21179500810720392; 0.4498657884312737 0.9206863989478159 0.626472113013419; -0.7063855626923453 0.8392260172345695 0.6657911934666387; -0.7725890297740363 -0.6321620848297606 0.35516589931735515; 0.7603264864364883 -0.8557533022845115 -0.6311629259349868; 0.9561247545973677 -0.5017701499231864 -0.6272119558821079; 0.9705083590037089 0.91129864219974 -0.2888985356409027] %
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Phase 3:
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Planet: Saturn
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V∞_in: [5.038952819515676, 7.9798066215675565, -0.8715896824986642] km/s
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V∞_out: [-0.012236099214684017, -0.9981497941651291, -0.828378100790254] km/s
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time of flight: 2.2176624458787963e8 seconds
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arrival date: 2036-12-07T01:48:56.327
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thrust profile: [0.9561858721260394 0.9849199946256132 0.5225438470279931; -0.027932742829215068 0.9733888937163413 0.43219740244487903; -0.44415834968745566 0.9310525799775682 0.30834923084684457; -0.41854368011913534 0.8702966170896927 0.208080577565248; -0.32933795593388565 0.815451911934079 0.1254126724065932; -0.23552180201632114 0.7723076604175301 0.06921155682993804; -0.1614904990435074 0.73600434327184 0.037191049603114215; -0.10093276866257177 0.7015622404196313 0.01739015687986595; -0.07061055518612644 0.6657821229767328 0.004884538754076532; -0.04673703754899972 0.625817515327918 -0.0025122978941227465; -0.041112337800284074 0.5793466390354832 -0.006303799076519013; -0.04283624698244216 0.5243842265930279 -0.007497163409016717; -0.05346092222703407 0.459582480493242 -0.0067340993382808785; -0.06895608005212821 0.3833475120313622 -0.004880957209105144; -0.09923125957632768 0.29425585856793157 -0.0013249599275947555; -0.13231914932868194 0.1912438331345806 0.00453604080839281; -0.15508316129336963 -0.043236971591321775 0.007944115104287169; -0.17629889261241166 -0.11291544563125626 0.012864022185234279; -0.14568672081150158 -0.25880004071832907 0.015796279090581688; -0.1516335446629711 -0.3568240854796575 0.021534187052804105] %
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Mass Used: 2773.596934253452 kg
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Launch C3: 66.76157923825527 km²/s²
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||V∞_in||: 9.477764916347974 km/s
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