30 lines
5.9 KiB
Plaintext
30 lines
5.9 KiB
Plaintext
archive/EMJ_2021-10-18T04:47:08.045/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: 2500.0 kg
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Launch Date: 2023-01-22T15:28:09.612
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Launch V∞: [-1.3643798210186435, -0.7159390468343555, -0.08322760218198313] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-3.7275620469034516, -2.526282437303017, -1.0076347004721333] km/s
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V∞_out: [-4.539673313316336, 0.7017217526549935, -0.43719187658020064] km/s
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time of flight: 1.6754546939656562e8 seconds
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arrival date: 2028-05-14T19:52:38.612
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thrust profile: [-0.07019019845057392 -0.09751722424670824 0.057122211183439194; 0.0054954904966895675 0.06603994792238901 -0.008236600949104998; -0.038287295416854265 0.0405637279948827 -0.00039425725045440414; -0.04489516507237624 0.062361989272701555 -0.014310337466940538; -0.06533576563765808 0.0813139155665736 -0.0230878905705352; -0.07111179879293159 0.1136744968920041 -0.025657586886562084; -0.09903331758106965 0.11244239131194846 -0.029127942276517004; -0.14519955701401654 0.0820620937929571 -0.016479200095645914; -0.18464482626947132 -0.002361270059995381 0.012541372152332043; -0.16208337606711581 -0.12323706727087957 0.029918207581927286; -0.03826611266033134 -0.19280232075714435 0.015634696312891595; 0.10357151304792918 -0.14622474430228383 -0.01476181218722382; 0.16353773698290058 -0.012783112362057128 -0.03817028509721126; 0.14128851582232346 0.10785344001133187 -0.0357190663988926; 0.06918734758690485 0.17326897933390278 -0.03712601380495417; -0.031648944921356836 0.19178367105195807 -0.04461713896061804; -0.12900802224781507 0.16641625303294064 -0.036412410125766376; -0.20558296282247013 0.0909874482041778 -0.0021859875114524693; -0.23860632053617775 -0.03131210259930334 0.03846218187802765; -0.19484928772776763 -0.16847931672520963 0.05663879489729261; -0.04458963976560391 -0.2533559110225395 0.044534431857610954; 0.13733530097702104 -0.21727091374495844 0.020002959834639213; 0.22581551276364645 -0.0879818903955467 -0.0036011782553634036; 0.22121852023447833 0.06669091700849566 -0.01880622457636459; 0.16083994824272446 0.18238419398417918 -0.03735147197382809; 0.04998538539174665 0.24212585751273832 -0.052091359689029074; -0.08535491831784932 0.25306430274112096 -0.05370930001232357; -0.20801975657401187 0.20198148753334175 -0.03429289132017696; -0.29693024644822513 0.07445503890760441 0.00618198553945368; -0.32253861894745967 -0.09834987569122858 0.04557997039335986; -0.23065143773754027 -0.2605588198318397 0.06774871350662658; -0.028464246178048404 -0.33502116968411816 0.0636187256733626; 0.16582275111214603 -0.2932667678437133 0.05643822924252577; 0.2672257697058423 -0.17437196323840912 0.04105153452041249; 0.29453382682696283 -0.016659028012792725 0.025373227704684264; 0.2744616051247645 0.1337722420145339 0.00680861610352153; 0.21887396658872654 0.24585537508513813 -0.014059142888279948; 0.12185436628160583 0.3150537318914091 -0.03596713912282804; -0.033268018178755306 0.3424760568989831 -0.05645515510274152; -0.23160537414128402 0.3196731855067364 -0.06654084457034629] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-1.4846886334994476, -1.361076096805199, 0.05466909001856985] km/s
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V∞_out: [-0.07465493192041184, 0.9283413652878699, -0.004041543084996275] km/s
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time of flight: 1.5092081191662246e8 seconds
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arrival date: 2033-02-24T14:19:29.612
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thrust profile: [-0.4535229684089248 0.35471159327155716 -0.0057850436284287; -0.5352374523210783 0.14944138395317494 -0.0029283222034505404; -0.520203501923174 -0.06176801084644443 -0.0001628737762102747; -0.5154513050657218 -0.23622401286983016 0.0025982943066399037; -0.46036154582848055 -0.34805331067818845 0.005118780974401044; -0.3959325088841016 -0.41028811107419055 0.0073409773026779646; -0.3235211652890271 -0.4441368112979632 0.009510224295634622; -0.25142435509239425 -0.4658984105671444 0.010858708474655216; -0.18119810986710946 -0.4751147453185688 0.011809185294244101; -0.11638604556530519 -0.47795070872879025 0.012081338602265604; -0.05815970358961853 -0.4728478782242188 0.009857285512696764; -0.00752295071964518 -0.4658771440630143 0.011584161063256278; 0.03545750938514277 -0.4579584297431292 0.010525899201687835; 0.07182273769651207 -0.43472741327897585 0.009533470456107824; 0.10664962568152683 -0.4187208852733485 0.007976992373517903; 0.12492727342133673 -0.3969076832621358 0.006742722154267496; 0.1431746464209061 -0.3835148744685672 0.004786582532343347; 0.1582260654641431 -0.35666588691287027 0.0030847669308384337; 0.16591018189104523 -0.3331316195175424 0.0012721008318001433; 0.17442723323913162 -0.307967948961363 -6.981549779719113e-5; 0.15132680107932436 -0.28549976037098757 -0.0018690202925421497; 0.186781574882658 -0.3306637512391842 -0.0048883590949999976; 0.17610257439350285 -0.23735446317629183 -0.006122412880973916; 0.1724622886167947 -0.21320269056261854 -0.007715271932459695; 0.1680670084063633 -0.19183024967809073 -0.009166796400500983; 0.17830509608470782 -0.16313804745160612 -0.011148105442551353; 0.1482021231934022 -0.14960161104601993 -0.011795475999042142; 0.14034852593908412 -0.12424858172274011 -0.01351806966068364; 0.12814622777773102 -0.11065483266711279 -0.014425856538434116; 0.11336824983566328 -0.09468285579432549 -0.015153154561936515; 0.1014135174333853 -0.07774054155124342 -0.01636862595604425; 0.09013879877718133 -0.06314251860721383 -0.017328209330542098; 0.07409816899410408 -0.04958972068223582 -0.017982560903710178; 0.059254084971633196 -0.037404541491299056 -0.018443983864669375; 0.04564010326731609 -0.02708329971030048 -0.01901529707592924; 0.031119604581005364 -0.013731126495017738 -0.0194930452946951; 0.01819976084858475 -0.010230335153065933 -0.01913899819718352; 0.004680675542116217 -0.0019477725404852817 -0.018630645585022216; -0.006945877458896208 0.04945640047608528 -0.019980625053223188; -0.02476220854549837 0.020757355899770503 -0.018288826690161054] %
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Mass Used: 699.0068365759485 kg
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Launch C3: 2.3810278485499135 km²/s²
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||V∞_in||: 2.014898803697196 km/s
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