37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EVMS_2021-12-13T21:46:30.548/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: 2024-05-14T22:50:54.151
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Launch V∞: [1.1286314645978788, 6.894494804991318, -0.8285243221011761] km/s
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Phase 1:
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Planet: Venus
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V∞_in: [-0.4975358362817743, 7.143314145080825, 1.4331811045093779] km/s
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V∞_out: [6.0255649206667625, 4.05582288696785, 0.7567303017536462] km/s
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time of flight: 5.201873526429285e7 seconds
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arrival date: 2026-01-07T00:29:49.151
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thrust profile: [-0.13658867986140374 -0.24246001363888786 -0.0018351721366561648; -0.19874653605027093 -0.42347951183192895 0.059887224602709746; -0.006030933718274198 -0.6165659086877646 0.05143110252875157; 0.5690891294297716 -0.6337278673409295 -0.012184805314118167; 0.6969370055919233 -0.3303175586786053 -0.07217788171252011; 0.64128971249768 0.26314536468162564 -0.09952967531295756; 0.5208719713422499 0.32770505919622234 -0.10513933945114934; 0.4271266849981205 0.20190088190483316 -0.10365532774681949; 0.4176630482221774 -0.011898915901332388 -0.08241345687785652; 0.47262980673060484 -0.13896143178119608 -0.03374381004058062; 0.4421659456699236 -0.17124612763461697 0.02403617877878262; 0.3583106766681072 -0.28808344084851756 0.06553065121634129; 0.4748177430173668 -0.46986296014010215 0.04039987329214622; 0.5807725097378242 -0.2734128860609197 -0.035376229041435836; 0.5547393823521555 0.03932247507743895 -0.09732884535240749; 0.4576988071163949 0.017725627686673677 -0.1304971469405435; 0.40441128328564385 -0.22624714092575637 -0.12589052393340233; 0.5227891982702978 -0.37951138376215193 -0.08197543798043004; 0.6869211599682585 -0.3895945340441026 -0.04215815195764137; 0.6943636261137554 -0.06601804604492464 0.0018331949690765612] %
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Phase 2:
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Planet: Mars
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V∞_in: [6.338828850719935, 0.2060782119786431, -0.4977472310639235] km/s
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V∞_out: [5.762367354839256, -2.687069620550792, -0.2168349056959969] km/s
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time of flight: 3.949974283472407e7 seconds
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arrival date: 2027-04-09T04:38:51.151
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thrust profile: [0.458336717149733 0.1771870373806907 0.056427191918473445; 0.403817033597994 0.351117374215139 0.15075644725276122; 0.048711917893504396 0.41093296017258263 0.16380972666043295; -0.18354926599538152 0.4256482504531366 0.15401233744770568; -0.42370527996013474 0.23794979462159155 0.1314849420842794; -0.5679456579714863 0.1393409941124382 0.09924531892954472; -0.6520211065270787 0.025161300456823018 0.0635649864433606; -0.6989667221671542 -0.10489669213488008 0.0253021698618907; -0.7262214288474695 -0.24555410262257685 -0.0121562278547937; -0.743313608223649 -0.384644672098393 -0.05649462601447925; -0.7525404848639327 -0.507291521547137 -0.08734741229955949; -0.7578561155541664 -0.5996752434898261 -0.12360313032488564; -0.7592183352851313 -0.665338122647058 -0.15810104649178947; -0.7558073245676104 -0.7094328622253643 -0.19027889839324838; -0.7464517819119382 -0.7464555301053758 -0.21801144025375926; -0.7296456019615701 -0.7634101584430326 -0.24323055639952082; -0.7009447676318107 -0.7794725581151669 -0.262851486143965; -0.6543199308894584 -0.7903707443682346 -0.2772415958605197; -0.5827848217677881 -0.8004854095656452 -0.28523650701311554; -0.4849301355226277 -0.8048943851748858 -0.28659470269055276] %
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Phase 3:
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Planet: Saturn
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V∞_in: [4.322617308702803, 2.354348521583675, -0.7376335957485771] km/s
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V∞_out: [3.011554362103189, -2.0958590497922804, -2.908427301510971] km/s
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time of flight: 1.8820349650227648e8 seconds
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arrival date: 2033-03-26T11:23:47.151
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thrust profile: [0.9368347194497842 -0.965371940721398 -0.5613882989973752; 0.9714384488821548 -0.7607872705031594 -0.09024131587466705; 0.9505668891632969 0.8312812365923358 0.07095989545704967; 0.8695060114456342 0.8325193176250749 0.07116267827484891; 0.6939833190653248 0.8028129129322639 0.031577569215995506; 0.49217044040756264 0.7963553158741095 -0.021466953451174452; 0.3421171062041329 0.6993381181757932 -0.06563494914488495; 0.24925579641473375 0.4813067954039389 -0.1267909830819491; 0.19205090715099823 0.2932984515362608 -0.11766481272251779; 0.15209938030796544 0.1642850960501914 -0.12314405675789696; 0.11581486470625263 0.09373283562323559 -0.12395161654174959; 0.08005933539569969 0.07505479185768685 -0.11065807756901873; 0.04290428379494743 0.06421252941862582 -0.09362719990942882; 0.009670159523961858 0.05833849578599656 -0.07211230161173374; -0.05839187604989335 0.06373138672808198 -0.06233551857721689; -0.012522824962244553 0.049309431568300005 -0.040752415650939504; -0.04320895480635503 0.05485848479687612 0.0021594467585038988; -0.03809749205187863 0.0378883881221725 0.04099809276024048; -0.035012269320380346 -0.006618884738808792 0.05971979961122836; -0.03288959167972974 -0.001403295597270634 0.07024375436873588] %
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Mass Used: 1258.284359858289 kg
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Launch C3: 49.49432015124584 km²/s²
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||V∞_in||: 4.977155882645959 km/s
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