30 lines
6.0 KiB
Plaintext
30 lines
6.0 KiB
Plaintext
archive/EJU---------------------------
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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: 1976-08-03T18:07:52.908
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Launch V∞: [6.299916182319705, 6.240538451377015, -0.9940165103728982] km/s
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Phase 1:
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Planet: Jupiter
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V∞_in: [4.178807865103526, 3.271316108925791, 0.038831033060078735] km/s
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V∞_out: [-1.3778027301160083, -5.1110224704243725, -0.38018528529187656] km/s
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time of flight: 9.076893335112691e7 seconds
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arrival date: 1979-06-20T07:43:25.908
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thrust profile: [0.04513213164333234 0.04346394223048948 0.007180644066023622; 0.023711461445665785 0.04851693214299602 0.03207463889343553; 0.00969082323802968 0.0429167126574647 0.05027917371754633; 0.0006490219093697312 0.03432108495203708 0.05302050429400685; -0.003953708767625976 0.02834092045678569 0.05567795776724263; -0.007078446275295329 0.011750260516732298 0.05750557980134808; -0.003435272692576073 0.02122406642664124 0.06262312885175245; -0.009695677074664703 0.018479022813936753 0.06053735694521427; -0.01142145238531702 0.015117586694892556 0.0638000808444341; -0.012068039284864305 0.012122660566706385 0.06391205556608177; -0.012302230314909514 0.010908149372005694 0.06019740157959107; -0.01446161436665235 0.008373928351474595 0.059323058345291314; -0.016583035763738076 0.006299387290095585 0.06082959992214257; -0.01706759812967117 0.0065044105221593 0.05778343872547179; -0.019486845820007016 0.002193974387266614 0.057393172584176734; -0.020473650886052644 1.380648034282904e-5 0.05731896545245807; -0.018767281384997753 -0.001918872534461376 0.05612361619283167; -0.021591450801765708 -0.0042488196125658765 0.05450598919383925; -0.021478255013919884 -0.006464299578735615 0.04809767450620565; -0.022653919145895585 -0.009019740247343862 0.048362756123037046; -0.023544833613709452 -0.011660942116303467 0.04427505897015856; -0.02487650131449469 -0.01482208132042167 0.042971426063402186; -0.025304632579721677 -0.017024463752791045 0.038971334825125444; -0.02627710448532682 -0.01999518763372068 0.036273080926672384; -0.026409220881850253 -0.022340756335864343 0.03346167188312444; -0.027035811169801346 -0.026330622264995978 0.029551995901678153; -0.027294988215502632 -0.028965874411855858 0.026920943329044964; -0.02543100070917406 -0.031206127791626466 0.02244980247094962; -0.027031341088425847 -0.0340466798524574 0.018998557859187092; -0.02741737072358986 -0.03790113735478487 0.01557337910538438; -0.0272602309532185 -0.0408499812859817 0.01194792933774343; -0.025909850501463313 -0.04396390625007793 0.00813014729889798; -0.02506976623031212 -0.047397447305083704 0.004665530910703655; -0.023334361066159846 -0.048678373843736196 0.0009546486525111172; -0.023889478406793792 -0.05679728290807836 -0.002589587233405526; -0.02724340418820601 -0.05816253276542619 -0.006122379800579124; -0.021218565581682256 -0.06185180447607849 -0.009044740289425488; -0.019380826507997755 -0.06887292315771941 -0.013887128275611392; -0.01630947060752653 -0.06863416874846709 -0.01479387901178276; -0.015411951104633738 -0.07135904293057543 -0.01714932934975381] %
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Phase 2:
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Planet: Uranus
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V∞_in: [-1.845021665733062, -5.678663565100718, 0.3029957863298556] km/s
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V∞_out: [-3.909849414959923, 3.5759430497442013, 2.370770023155677] km/s
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time of flight: 3.08114874485728e8 seconds
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arrival date: 1989-03-25T11:11:19.908
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thrust profile: [-0.06674811641031352 -0.05612757204576699 -0.027545219420525784; -0.05559395467233815 -0.05898058463022347 -0.027618778760360937; -0.05692889817706908 -0.06138740735669628 -0.024127884156966553; -0.04938597114969373 -0.05897632826574441 -0.020875930634551777; -0.04513949441889156 -0.05493677886831321 -0.017744255550718353; -0.04191267048560369 -0.0497040919280347 -0.014850616507294535; -0.03951131641179269 -0.04341382786449151 -0.009778820274569259; -0.0370863829866412 -0.03639713660534706 -0.007535292090010591; -0.037410692933588605 -0.03106890983815507 -0.0035126740989491565; -0.035384789101130805 -0.02554445172882075 -0.0017983914198710438; -0.03574977327075396 -0.02113010504624859 -0.0001328491376689744; -0.03194724079988652 -0.01638421067813942 -0.0011505498097668584; -0.034180716278068 -0.013877672988327941 0.001627089350782669; -0.03885278128497657 -0.01161056124179592 0.005447519394925048; -0.04780658577496266 -0.009642777483071765 0.008770370725385047; -0.039523274181837605 -0.00583266582504645 0.010285929551974837; -0.04054425271649562 -0.0030979021814110763 0.013538087528531879; -0.042081635316423546 0.0002896039819797671 0.020386417210395406; -0.04163111462438231 0.003378109131498211 0.018796072247663165; -0.04381682122520203 0.007198467572032381 0.024926690546142397; -0.04521110915147108 0.011920408867649519 0.029020217823105928; -0.047873959213738576 0.01694996877307094 0.029539969915417366; -0.04789681559790685 0.023080413175950897 0.03548445565572181; -0.048968821642495 0.031283457963523637 0.042288153133598176; -0.05513570922771978 0.04188862330873962 0.04315061325522542; -0.0460427824369968 0.05532672923356575 0.052911791351016764; -0.04595007962041501 0.0682098780156651 0.0545332693961846; -0.04020043790691544 0.08884049852098926 0.054905659724033544; -0.03406076232020952 0.11144075206336615 0.05094487923514953; -0.024252121467827105 0.12900503386624168 0.05115224879295048; -0.0176104293681911 0.06260126480105925 0.04470427127414733; -0.008891011397626766 0.1312405594766333 0.03624981025811338; 0.0004454420607871681 0.07329672426875136 0.03146945127603886; 0.0024886701231228332 0.1417457581542488 0.02033654814598019; 0.025071362315817032 0.19698210332984226 0.021196655967815694; 0.0324021609887447 0.15074081889051183 0.0034214591933819246; 0.03632243807074882 0.15207933955719707 -0.002120489459561229; 0.039403691731321876 0.155368573708892 -0.007770585754213655; 0.044300010743546385 0.1656092696295884 -0.009813911794334952; 0.04940888045966933 0.15430255903950427 -0.013461557013245747] %
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Mass Used: 254.85590261239986 kg
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Launch C3: 79.62133289026262 km²/s²
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||V∞_in||: 5.978555952666198 km/s
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