37 lines
5.0 KiB
Plaintext
37 lines
5.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EVMS_2021-12-14T01:43:41.263/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: 2023-05-20T09:06:35.288
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Launch V∞: [-1.8438889475809765, 6.120059172103301, -0.7981747861634966] km/s
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Phase 1:
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Planet: Venus
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V∞_in: [-2.56509812262509, 8.726298030365955, 1.2653783448963722] km/s
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V∞_out: [3.933875520715713, 8.182318027927845, 1.3797206772984685] km/s
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time of flight: 6.3150638478290446e7 seconds
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arrival date: 2025-05-20T06:57:13.288
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thrust profile: [-0.1673002601441919 -0.26883139314945603 -0.004056802930588146; -0.23150973398793398 -0.5422926057887579 -0.01424916584017891; 0.5216279513936498 -0.7201035092402946 -0.05026572450882597; 0.7619564949501179 -0.017659100038672788 -0.050798263624736634; 0.5942837250609073 0.5263617574161898 -0.0070195713227723154; 0.3410765842139262 0.41102934542119196 0.0003621379767194054; 0.23648394719297353 0.14198690462048363 -0.009581961375511473; 0.0056202015516126 -0.32693032741518907 -0.010162609157081665; -0.026379909967065362 -0.5874916310490459 -0.021494316985701284; 0.693629555909135 -0.61456318000757 -0.054644453501477036; 0.6749160281202036 0.3944492779701146 -0.021084849056050275; 0.4403512073946586 0.404989286932993 -0.0014708947868851455; 0.3219167787670785 0.1274096536884702 -0.008385265303928385; 0.27124921840307187 -0.19763134120286302 -0.014529551099335972; 0.08063379563374638 -0.44308484663335224 -0.017300342160510865; 0.5868779992877718 -0.6080198456071109 -0.04284179805368043; 0.6638767318711757 0.23800863124179605 -0.023418413571253783; 0.44792722794577955 0.3189162484584814 -0.0034061188086769605; 0.3654940275210002 -0.01822248382616463 -0.011103744313695233; 0.3671390691769647 -0.1877557855665406 -0.017972667398621946] %
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Phase 2:
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Planet: Mars
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V∞_in: [3.740909417528976, 4.969698645681673, -0.1836371554650627] km/s
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V∞_out: [1.6805078934236426, 5.988466382534255, 0.2011389183183449] km/s
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time of flight: 9.967373816267239e7 seconds
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arrival date: 2028-07-16T22:06:11.288
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thrust profile: [0.2889046493274145 0.35172813894699617 0.005750881627058749; -0.2891211816810922 0.2856217397496342 -0.01070529954797825; -0.4076909207469804 -0.04788044763953207 -0.020561543485485726; -0.37899315325138216 -0.30969571658846323 -0.020466381356948952; -0.27651505042097296 -0.43501262129876456 -0.018271754879646666; -0.03992270374633847 -0.4908301495597925 -0.014401728962937026; 0.28778598754683493 -0.4545602376768821 -0.0064508479743784625; 0.46150433893131715 -0.1880814631199537 0.0021626109204597446; 0.2788204255677078 0.360854942969168 0.006831262006997803; -0.2566515872209155 0.32209934564164727 -0.007836893916662625; -0.4100446444003415 0.054443015280224105 -0.01751477422173226; -0.41902900656224723 -0.23975107675376675 -0.019442357179398642; -0.3644374200145407 -0.4010601518340647 -0.01891998107003531; -0.23193420972805218 -0.48910794102085664 -0.01726021542869752; 0.04132505041766476 -0.5223896099070574 -0.013713715632566187; 0.3300017630006415 -0.4784824951035753 -0.008331679149800309; 0.48040380368063845 -0.26935494128032167 -0.0016253936871342854; 0.4263256047487922 0.26594823500945197 0.005887216845594874; 0.028855636881693788 0.40742654653958477 0.004203409756847152; -0.30902036281985135 0.2999387343974258 -0.004381705457322128] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-1.2399121705505638, 6.956855519313853, -0.5166911303842717] km/s
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V∞_out: [-0.00013639678575079212, 0.00045388258983991705, 0.00010352289927939363] km/s
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time of flight: 2.156567539242905e8 seconds
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arrival date: 2035-05-17T22:45:24.288
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thrust profile: [-0.5883389325549248 0.34393534356111716 -0.04223302913356034; -0.5094157452497227 -0.32578128865408745 -0.0418290876544073; -0.2837278960528077 -0.5200051898159135 -0.015714467863770183; 0.234663577149613 -0.5778749576697557 0.007285867554073748; 0.5269009945794882 -0.5533424499427229 0.029448586498405305; 0.6588494889448501 -0.42596433225988556 0.03990667436449693; 0.7104940582670465 0.09976028717408182 0.04288674512400733; 0.6731412653152242 0.5520777962943062 0.03383456434541915; 0.5144161575829512 0.6548774334195933 0.016436082603795563; 0.18808395700108824 0.6460817168459387 -0.006174956813691272; -0.08944132984324173 0.5852109928553235 -0.02412032985192145; -0.1777044504999653 0.5026107885439219 -0.0332038631526247; -0.18602955062431278 0.4183028818306649 -0.035496117853459554; -0.16885700381769508 0.33802299933222757 -0.033691289488692565; -0.14420336819801963 0.2608351709154188 -0.029504852011938868; -0.11794830800737324 0.1841852103036704 -0.02391639449132369; -0.09183314607853647 0.1059536639685903 -0.017483392600732773; -0.06633021176691514 0.02374701364948183 -0.010504070567046215; -0.035138504389099774 -0.06203575677661479 -0.0031448184775343894; -0.004807991844724756 -0.13909256410647852 0.004015212913470968] %
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Mass Used: 1533.705930555565 kg
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Launch C3: 41.49213371032417 km²/s²
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||V∞_in||: 7.085350424044305 km/s
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