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thesis/archive/EMMJS_archive
2021-12-13 22:23:31 -07:00

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archive/EMMJS_archive
---------------------------
Spacecraft: mySat
dry_mass: 200.0 kg
specific impulse: 3200.0 kg/s
max_thrust: 0.00025 kN
num_thrusters: 1
duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2023-02-26T04:10:12.359
Launch V∞: [-4.841701064906604, 3.475969740428134, -4.8994214190507] km/s
Phase 1:
Planet: Mars
V∞_in: [0.02729198924983877, 5.017291114045934, -2.960466892478738] km/s
V∞_out: [-0.7796648643413417, 5.029374064409783, -2.8347788324016983] km/s
time of flight: 1.9570320002726743e8 seconds
arrival date: 2029-05-10T06:10:12.359
thrust profile: [0.51200489277245 0.1491712750305638 -0.5617898782756465; 0.5985472817937932 0.4314745458970473 -0.29088252333102027; -0.45166509877363964 0.5194585980906682 0.5146294788199312; 0.390520290781806 -0.5192326236428068 0.4429840782407487; 0.5160025656800347 0.43684584169735574 -0.4960808446595455; 0.5098504634472127 0.5199893315046626 0.4441400784392527; -0.49987113488322754 -0.47893620910952606 0.48036085120848565; 0.5368410355569405 0.5166822047764457 -0.4858670271400151; 0.44238316289905827 0.547824927494726 -0.4656337244770621; 0.21668892035180595 0.6021857778661118 -0.19651661385197258; 0.4341377302277037 -0.16678624993961083 0.5761938702855823; 0.5718885908183827 0.5536579188076003 0.33795675555520704; -0.39527664332753926 0.5814857962643089 -0.4679595952307845; -0.008428218148373924 0.5415048084721836 -0.45110046854424596; 0.33161932673220734 -0.45295582817342434 0.46836263037592774; 0.5280374896116378 0.5764518977818923 0.3342129870989262; 0.3107502688966615 0.5511548090736831 -0.5014473758638118; 0.07343276836897304 0.6646323168301356 -0.33765386861899715; -0.5980335383406491 -0.5746723266973839 0.15575901290142588; 0.590900565213738 0.39693261331727714 0.20472515338144043] %
Phase 2:
Planet: Mars
V∞_in: [3.0241033936172084, 1.6385004369573686, -5.605711794771172] km/s
V∞_out: [2.4283811769402535, -1.1475844477691648, -6.003401620464895] km/s
time of flight: 1.1737080029703692e8 seconds
arrival date: 2033-01-27T17:10:12.359
thrust profile: [-0.1768137656168143 0.3393511738335891 -0.353565456723947; -0.15954083659688176 -0.5487799730055659 -0.24022806443793981; 0.5157742145013325 -0.7252600963065111 -0.4938126290082077; 0.698500596084941 0.03900690309877106 -0.23316637699244064; 0.6365913895344839 0.20777317872832707 -0.2830962364627441; 0.5861304271928349 -0.1184358449845895 -0.4564142893293172; 0.6860855423630463 -0.5456724995449903 -0.44617293698271493; 0.6670491113213445 -0.38498567211274926 -0.3230834818585812; 0.5283999818464645 -0.09570871485046831 -0.478027472175741; 0.6580560949600205 0.46722570225829474 -0.11535896533777851; 0.5612619202113102 -0.1931961652510376 -0.4400901944952552; 0.4590177925799 -0.6932770941014383 -0.5144556676853405; 0.7561006651195121 -0.6660301702898956 -0.558073578122206; 0.7758630959701225 -0.08472708630272804 -0.41036611726373284; 0.566096622638857 0.7122289950338151 -0.11214847640185667; -0.4306590268194921 0.4288485227605312 0.2105331105689206; -0.5085374829983493 -0.516980326040015 0.16675646570585556; -0.5812762098132924 -0.6592114464112737 -0.39525785227607435; 0.3559795650447502 -0.8283244516408661 -0.5816275654619777; 0.7220122543976706 -0.8709955103801817 -0.5752271662039113] %
Phase 3:
Planet: Jupiter
V∞_in: [5.060776761478531, -2.65457156740014, 1.2093916749224973] km/s
V∞_out: [-4.655218918764466, -2.2507227956970843, 2.7173192390054806] km/s
time of flight: 7.437600000965603e7 seconds
arrival date: 2035-06-07T13:10:12.359
thrust profile: [0.5554028628906259 -0.8562653819570508 -0.4353192179666242; 0.6836770270628973 -0.8068634065800825 -0.40691024348661053; 0.6938434264699962 -0.7253280301253697 -0.3838170511550203; 0.645874750163326 -0.6289501430894447 -0.3499668164482744; 0.5889993418389312 -0.5421974665324047 -0.3250231983004846; 0.521131977446493 -0.4767106284566455 -0.3139270110389849; 0.44907608028844187 -0.42835191134595757 -0.30427273241100156; 0.3771619836123307 -0.38593020022499613 -0.29345181442595814; 0.30758537653438345 -0.34138417397604953 -0.2806050625679753; 0.24090511199415704 -0.2908278788914028 -0.2653604699658747; 0.17676587080788508 -0.23266346298480622 -0.24755096472050972; 0.11564885705822119 -0.16792372723278565 -0.22685867498381254; 0.07637432600785862 -0.10221693792171678 -0.20194486428807676; 0.019753903444897154 -0.058193667702053815 -0.18756658332981802; -0.044040327145306354 -0.00021057373845115093 -0.15565868544825787; -0.1020149066984689 0.047297427488451 -0.11989375229021738; -0.15572852811033114 0.08561531859322227 -0.08266441800646043; -0.20039007901031922 0.11872106917143616 -0.04576729741807346; -0.24124782668690306 0.1511930898415435 -0.009960538806793113; -0.28349017928188214 0.1924753920006318 0.02615368339855036] %
Phase 4:
Planet: Saturn
V∞_in: [-7.256385977948657, 0.7771719462797614, -0.785892915072424] km/s
V∞_out: [-5.9473393974944736e-6, -7.362203906933263e-7, 6.306068555232033e-7] km/s
time of flight: 1.4662439997163886e8 seconds
arrival date: 2040-01-29T14:10:11.359
thrust profile: [-0.18959418256753224 0.13412715420236315 -0.043410183532822624; -0.19766571870169566 0.1372601657158578 -0.037968113030145044; -0.1971783405485536 0.129832118307628 -0.04157452597322259; -0.19192072677853972 0.11752160892327206 -0.04544882251204915; -0.18096355607909057 0.10099613325234727 -0.04845756455495175; -0.16440940142977603 0.0827695902679096 -0.0501168011338542; -0.14159683191947461 0.06939209018313232 -0.04938123378650775; -0.11494734465063888 0.05950353242028259 -0.04787565574075916; -0.08842871021960914 0.05331851047785903 -0.04243441932918664; -0.06244946835797671 0.049895056937498274 -0.03534701683264976; -0.0380028875571515 0.047256901837732644 -0.02725064975669285; -0.01886788294008128 0.04286456425792469 -0.019192970894846496; 0.0054749884299889135 0.041277048472854974 -0.010750429199969911; 0.02389959629376803 0.03888123568193434 -0.0015386535754099552; 0.0428231915186611 0.03753775483224003 0.00740487148339779; 0.06481451674589596 0.03713565978563092 0.014580239918154077; 0.09005525246175461 0.0369062161152353 0.018428292697994248; 0.1201760127678751 0.03212421201511818 0.04118543343400019; 0.15404590862831494 0.02789044310966664 0.043771491647338116; 0.18466591121075765 0.02447914444489793 0.052012952789042624] %
Mass Used: 2528.0301016677718 kg
Launch C3: 59.52876507974255 km²/s²
||V∞_in||: 7.3400791119043935 km/s
---------------------------
Spacecraft: mySat
dry_mass: 200.0 kg
specific impulse: 3200.0 kg/s
max_thrust: 0.00025 kN
num_thrusters: 1
duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2023-07-25T10:56:35.081
Launch V∞: [-0.946994040198373, 0.7451481404956214, -0.8183806644150764] km/s
Phase 1:
Planet: Mars
V∞_in: [0.014258156666681189, 2.7730331960192176, -1.1269036535413253] km/s
V∞_out: [0.5141370030166348, -0.1036905077662334, -2.9466045466696906] km/s
time of flight: 1.1404800000012271e8 seconds
arrival date: 2027-03-06T10:56:35.081
thrust profile: [0.9385530212613687 0.4901574978623852 0.10061758150690266; 0.963070949930897 0.8321550483186799 0.008076995378552753; 0.9477571571642094 0.9610236014179844 -0.3985885112414162; -0.8711740070381366 0.9585545422957218 -0.473960549642588; -0.35180875323453037 0.5538991572461103 -0.3047172625720546; 0.945857985340927 0.9318586412463802 0.07532442345652893; 0.916860585821232 0.9461601676367617 0.09256592206997157; 0.9203902037763169 0.9428723645501874 -0.3780093114569496; 0.1105180481588208 0.9388923575412604 -0.5467563429465788; 0.9600557668435807 0.08776536568096838 -0.6082094846555337; 0.9694071291822624 0.9576019390193865 0.042076881935371874; 0.7379014033007257 0.9676653528673065 0.20011181540529835; -0.7026385155061656 0.9228908375337035 -0.34668134552520397; 0.34660988424967165 0.77350231915288 -0.6692179888555208; 0.9672945056421521 -0.9455364762862372 -0.5850573257116493; 0.9859396795925156 0.16374570712498915 -0.26188762301350715; 0.9545064259275549 0.9869744571812468 0.4480444603786351; -0.9777686070631371 0.9725195168208975 0.193691849051127; -0.9708472634149672 0.7500006701210962 -0.37076685227103995; -0.9229893981992848 -0.9773469965294133 -0.6290625133929346] %
Phase 2:
Planet: Mars
V∞_in: [-0.8165677595901083, -0.06087475377585851, 3.052309046353131] km/s
V∞_out: [-2.9671064112310424, -0.9629127612065755, 0.5071630145897023] km/s
time of flight: 2.5657200000050467e7 seconds
arrival date: 2027-12-28T09:56:35.081
thrust profile: [-0.41833750150854715 -0.23745700390485924 0.5060156710931941; -0.39335607115842763 -0.21531365718730944 0.6214127928981721; -0.3741710013483589 -0.18178973996137726 0.7015878071805001; -0.3643811289828083 -0.1509347162037813 0.751160544358552; -0.3628330570779499 -0.11199271269023013 0.7793128986864543; -0.37235570205858287 -0.07302372672984968 0.7974839419031854; -0.3874662882006923 -0.03576203680036734 0.8098641766992978; -0.4074499881135819 -0.006584284581002934 0.8169150088581699; -0.4281109131913487 0.01182349039523377 0.8189971077067131; -0.4459261627474135 0.02257293277791146 0.8172972584690744; -0.4568773433902438 0.024804843226578856 0.8108158124505926; -0.4596411297003703 0.025045134417719155 0.7994526969817127; -0.4544566197190047 0.02267340988409504 0.7798827612879172; -0.44051961933116424 0.02370501075040903 0.7512234553177294; -0.41845307963023165 0.03005154105743171 0.708359052016344; -0.3881992767298684 0.04309990454210432 0.642522507646677; -0.34752334469565116 0.06138846846654963 0.5427837231822192; -0.2956992996903972 0.07742676936562033 0.40261391380265427; -0.17065939997376794 0.03880630671620183 0.2558269001777807; -0.235765575949598 0.13041638287567744 0.1404777210162043] %
Phase 3:
Planet: Jupiter
V∞_in: [-1.7554396063175077, -4.3095849115029985, -0.1325601348507023] km/s
V∞_out: [-4.236997629309691, -1.8724795170284283, -0.4561606000854912] km/s
time of flight: 1.4433840000004688e8 seconds
arrival date: 2032-07-24T23:56:35.081
thrust profile: [-0.5079766273797471 -0.10849515042583255 -0.0073545543900051516; -0.8149330561784093 0.34076004302958 -0.10326028863924017; -0.9395306205116954 -0.6895587367092969 -0.1170733748155399; -0.8439334413601929 -0.9377459623599967 0.015887598730331222; -0.12385311413264775 -0.85754750232578 0.11388747617260146; -0.15722365998440252 -0.3713893060760601 0.07983906967712144; -0.4905066367366128 -0.27630177574765263 0.052134881351611005; -0.40323969943463034 -0.36672944173144784 0.10826813939276426; -0.5166657583603889 -0.20333001707916043 0.07190841766549783; -0.9296123351360971 0.7837821870593056 -0.035789654605662545; -0.9678260619223868 -0.13908054107117102 0.11575665020892843; -0.9440698254178282 -0.9616603904467664 0.28528753638981585; 0.16941992205087786 -0.958669585346112 0.2124940591626158; 0.6017699213284338 -0.9270140863622942 0.07796374810040851; 0.39129362583737487 -0.748999519453576 0.05494281482886338; -0.005988877690288004 0.3481376434297022 0.032216440029362; 0.011527786969304827 -0.31978413035928577 -0.004592862949742337; -0.1976671384268677 0.9049682211089798 -0.21479203411765663; 0.5371991705488778 0.9049363560121139 -0.175235712765763; 0.054168546279189246 0.9414663774468465 -0.16207020976741393] %
Phase 4:
Planet: Saturn
V∞_in: [-6.539365214334455, 2.218176712783986, -0.36626020172775725] km/s
V∞_out: [-3.665136112061718, 6.451338183645968, -0.16457889689277141] km/s
time of flight: 1.812492000000014e8 seconds
arrival date: 2038-04-22T18:56:35.081
thrust profile: [0.05264623774997263 0.215338495237562 0.003754114844726852; 0.021165626937991143 0.22155170870739663 0.0047677855635804905; -0.0033929172288595286 0.31227924099890236 0.06539164976806457; 0.5694561518181592 0.6749368464572498 -0.11566610061632827; 0.1324891033231393 0.3597380526244606 -0.022962295545894153; 0.024627138889422973 0.3245686299565964 0.04183403216303953; 0.04019245536713721 0.744671990758876 0.03457514031015897; 0.03322017112484851 0.09302676824184232 -0.04257715628694308; -0.5866822473952952 -0.1769325756395129 0.23680697649509092; -0.14301190082784437 0.09180461385600784 -0.028924399094075886; -0.18983362654037655 -0.01602479614573261 -0.1446728759943558; 0.17123430049602928 0.2161630553091436 -0.12107554476977027; 0.0336023230656082 -0.34829018802826484 -0.06164799648134331; -0.0137744016652137 0.032090633273540385 -0.01461460357642287; 0.023301081130224558 0.023046782785575825 -0.0014039211755592525; 0.04517905715080291 0.07387132921915998 0.025233349143655093; 0.019815422280705618 -0.054453865039265595 -0.04881233646684176; 0.010800262146714945 0.40350474993323376 0.07282207796248781; 0.06922178100116284 -0.38131801494106843 -0.09824591875105594; 0.3129500615782364 -0.8033474844184223 -0.09841107223379629] %
Mass Used: 2769.31857214896 kg
Launch C3: 2.1217903753437817 km²/s²
||V∞_in||: 6.915038096131817 km/s
---------------------------
Spacecraft: mySat
dry_mass: 200.0 kg
specific impulse: 3200.0 kg/s
max_thrust: 0.00025 kN
num_thrusters: 1
duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2023-11-08T16:33:41.148
Launch V∞: [-3.7467429728623447, -0.7427414062360022, 1.0452490382459865] km/s
Phase 1:
Planet: Mars
V∞_in: [-2.885104439331886, -1.327495046167686, -0.027749058108596784] km/s
V∞_out: [-1.635967097498029, -2.7221789573242074, 0.015131202359034032] km/s
time of flight: 6.778595425260136e7 seconds
arrival date: 2026-01-01T05:59:35.148
thrust profile: [-0.05074044407568138 -0.021150582055882192 0.02730812822478398; -0.05363696950139044 -0.06016484582924907 0.04378542458137859; -0.02771035674834004 -0.10645426057233084 0.04017412625773127; 0.01630657360103497 -0.12411195034078264 0.023350505322999197; 0.05888817282501315 -0.10894637011686983 0.0004869417342207616; 0.08706942097452976 -0.07439720218837492 -0.023367157675286705; 0.09495132401480658 -0.035316011414834675 -0.04390702621881143; 0.08752285351021441 -0.004210304140208955 -0.05824943912322043; 0.06832834450779833 0.01653042551161497 -0.06490194085584605; 0.04924860864138059 0.022800133521631457 -0.062427366917489194; 0.03691868046224741 0.011541999666891671 -0.049506900069146154; 0.02451718791619906 0.019175805931995835 -0.026347851368135194; -0.032064249204675696 0.028639492606652335 0.024093899166278167; -0.08306772663523894 -0.03165903417995458 0.04031997576998134; -0.09308798794042389 -0.09539353910087413 0.04749994325844049; -0.02511528438762353 -0.14606890192307997 0.03354911283916682; 0.04310668443858089 -0.14207536740537 0.010418445496805094; 0.09246132545360927 -0.10807413652564378 -0.01547233992587798; 0.11319881808511016 -0.06123358244390861 -0.03864051024951101; 0.11067805251913554 -0.018856574108340608 -0.05612659024233843] %
Phase 2:
Planet: Mars
V∞_in: [-5.884459586892747, -3.363236848676117, -0.5090555323000778] km/s
V∞_out: [-6.754575036027653, -0.6433971508597986, -0.39980914727121014] km/s
time of flight: 7.419247222558242e7 seconds
arrival date: 2028-05-08T23:00:47.148
thrust profile: [0.09654790671377476 -0.02421154193760562 -0.017928801450145315; -0.013697559588275829 0.2078634802144036 -0.1014668129386949; -0.1556430254864518 0.42999351341524117 -0.15436045217579106; -0.34594668129342293 0.5414366154963298 -0.18269379097659816; -0.5454038742991185 0.5440039323636802 -0.17114242041739094; -0.6681265735588777 0.3905344944333295 -0.11698706816633163; -0.7178501053667702 -0.2147414683533294 -0.03563087595180013; -0.7220121820048746 -0.6387659476154413 0.04867755848318845; -0.6341573780307701 -0.8263426625319585 0.11250663825239217; -0.42165856247956973 -0.9426406733296913 0.15700663915570923; -0.2282676099099079 -0.9148864509029049 0.18224086165253006; -0.19975433285802874 -0.7643878036213333 0.18722809378704905; -0.23887594019854455 -0.571448552171104 0.1698384408589319; -0.20476059817742176 -0.3599675936442139 0.12804247162016902; -0.021622630852921543 -0.18516594772639078 0.08091546982169469; 0.06780313268150127 -0.07159692617114882 -0.012001883119840365; 0.0737246732088521 0.19689739773217652 -0.0905687562910174; -0.07537764165798895 0.41078706656960723 -0.1422877828900227; -0.2938291349463374 0.6466716586743462 -0.17361703816996657; -0.601397213043171 0.6791254738338734 -0.16212519541868492] %
Phase 3:
Planet: Jupiter
V∞_in: [-4.520674651049057, -2.5409484551232677, 0.26037246970875744] km/s
V∞_out: [-0.8008259820354645, 5.108593255783271, -0.47079137990954545] km/s
time of flight: 8.970106359744217e7 seconds
arrival date: 2031-03-13T03:58:30.148
thrust profile: [-0.9144771548791947 0.6902760792706399 -0.02961910274543401; -0.9666896369671112 0.2364932018447611 -0.03360017687916256; -0.9297691297960539 -0.38607984447798555 -0.01355789584429883; -0.8346154484217878 -0.6214014693922587 0.0166085094653681; -0.7129033965945708 -0.700963733220583 0.041959359935916686; -0.5741438889568534 -0.6419595568492229 0.05459259074755743; -0.43236122782537784 -0.6653422888597984 0.06339767277888375; -0.32424450019548473 -0.6113143615391297 0.0649952740051996; -0.2507213613172347 -0.5715625368541332 0.06495239951441104; -0.2066973617297525 -0.5173029196105642 0.059981187403511056; -0.17530451342656214 -0.46356648825594077 0.047624841826828745; -0.1477866838400433 -0.3897245825635479 0.049242714379565865; -0.12010797428356033 -0.31542712311456955 0.03834216234998446; -0.09300258495305348 -0.23794128216440627 0.032748124103639975; -0.06465067006435225 -0.16076271327460043 0.023845385656830805; -0.03888290411251017 -0.09081101903598543 0.01503347691667522; -0.012590046428086619 -0.034506030314933926 0.008899905471236012; 0.011376964842136187 0.007648534577971764 -0.00016213377538379614; 0.03978470139669819 0.0415658896303641 -0.008546043818250205; 0.05975267589922902 0.07118967492032456 -0.006512156351974285] %
Phase 4:
Planet: Saturn
V∞_in: [-1.3584481648257494, 2.8741322587661022, -0.2546304125259141] km/s
V∞_out: [-0.03780230346481573, 0.0035967292583968646, 0.0007694792047629233] km/s
time of flight: 2.6826096516036582e8 seconds
arrival date: 2039-09-12T00:54:35.148
thrust profile: [0.15488733950530229 0.004571931625674222 0.014146553973814535; 0.1553899576809856 0.03891862438324717 0.011973507362994223; 0.14041589251623252 0.07646409264944304 0.008869602158932547; 0.11548352038842227 0.1179485961935457 0.005517550148134544; 0.06394148482320672 0.14725938798843563 0.0012092021978766729; 0.0044327089101765475 0.13700916415178752 -0.005822274387507308; -0.029434414888955224 0.100612821704748 -0.017148622938312798; -0.033398085410118725 0.07353093978663178 -0.020258407230342786; -0.022858879964930717 0.05475230911401911 -0.0235821272789971; -0.013323435304460137 0.041377292100863744 -0.02450308078568975; 0.017138449993525783 0.0028560178783815105 -0.007160323142177257; 0.001062473462116934 0.0017720804053553297 -0.03347589005736904; -0.005736640138015923 -0.01153596653687124 -0.031458002877494486; 0.0015233910519389863 -0.004860382970013982 -0.028357121836203404; 0.006148876075267932 -0.01671721636961961 2.8524011567020264e-5; -0.0025972753111940814 -0.024320445695816754 -0.02183259610480299; -0.011337447226728808 -0.029412701131799595 -0.010842354984299675; -0.008925944814787248 -0.03382785337511997 -0.002144952702459933; -0.002362954309468288 -0.03692199124600801 0.010934038390259249; 0.006643709781956786 -0.044837750975252416 0.015646911234478936] %
Mass Used: 971.9203240703632 kg
Launch C3: 15.682293253184955 km²/s²
||V∞_in||: 3.1891776846675537 km/s