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thesis/archive/EMJ_2021-10-18T05:50:38.255/mission
2021-12-13 22:23:31 -07:00

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archive/EMJ_2021-10-18T05:50:38.255/mission---------------------------
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: 2500.0 kg
Launch Date: 2023-02-05T01:45:05.243
Launch V∞: [-3.0858219124135338, -1.9843415638102107, -0.5164890400755199] km/s
Phase 1:
Planet: Mars
V∞_in: [-4.057237445286011, -4.383306689219025, -0.9345749583183188] km/s
V∞_out: [-5.708063773850215, -1.9703162053834726, -0.2898885846278176] km/s
time of flight: 1.7154989176181787e8 seconds
arrival date: 2028-07-13T14:29:56.243
thrust profile: [-0.05903412749179622 -0.11072573240494099 -0.046313134098117194; 0.01830167102423096 -0.06087146903047021 -0.033049847954461684; 0.07560298617807773 -0.01056944361432975 -0.028709358840799726; 0.09546806703287268 0.03818316915239496 -0.01815506148240239; 0.087072908846325 0.08753619540094806 -0.010262863619545785; 0.07369552306131616 0.12499222126459184 -0.006697651325533921; 0.04251662528606648 0.15925223632421193 -0.004792029859755092; -0.010226965163121535 0.17556129615047028 -0.003737106470399883; -0.07525867128506282 0.17117299059876928 -0.0026437347892256744; -0.1429171951031634 0.13309299620733395 0.0009660268333295966; -0.17674866813873913 0.04237741241467234 0.011493155256722482; -0.1512076116827121 -0.08040347524944479 0.02330619578530688; -0.05115883020169031 -0.14141553541705287 0.017131006896436887; 0.05087583129540856 -0.1315744035343398 0.010336510514475119; 0.1120126200517782 -0.0799539576707552 0.002371562967016136; 0.1443467696695813 -0.018236726608329784 -0.004456458124353138; 0.15584788026095098 0.051389436140585935 -0.008686824078125708; 0.14558302648535318 0.11755108446303067 -0.010892189302993153; 0.11394327968434129 0.17080316758040615 -0.012668785007190191; 0.06296089219227079 0.21032613587651547 -0.014424861687090097; -0.007319181749241606 0.23302483496293394 -0.015775127894478227; -0.09208540070014654 0.23384051362199884 -0.016036796645284054; -0.17801224449074027 0.1988282553478485 -0.013451405628367928; -0.2405987292175941 0.11053687540893897 -0.0037755605782861168; -0.26274834968674954 -0.03215539584325131 0.011401533519479992; -0.18944534529519497 -0.16935814231584914 0.023680470151096394; -0.062492398971191944 -0.226809847819523 0.025148014577392675; 0.058741104153245675 -0.20710110554056518 0.02325277700839408; 0.13496703268042476 -0.14953850565375484 0.02002722387428528; 0.17788592589491933 -0.0842582776450467 0.01576195229274432; 0.2134153344492731 -0.01219022142044608 0.011716260687670104; 0.221133806934409 0.06664309280990648 0.009067992486418756; 0.20670820225401887 0.13977111236609446 0.007216324831558612; 0.17685233175682644 0.2009155862624451 0.004901929518232841; 0.13210453725383495 0.25576220417288764 0.0019161352306033082; 0.06729420380240994 0.30354914394899996 -0.0015851356597052838; -0.021728498222142328 0.31746498514577615 -0.006950254934209666; -0.12282179274563348 0.31897417027587177 -0.01342616228297283; -0.22216672837379955 0.28264007424096826 -0.021319790289976142; -0.3061983927615912 0.20656298357463285 -0.02872946037718458] %
Phase 2:
Planet: Jupiter
V∞_in: [-3.099527737126561, -0.7982552067237872, 0.5013266698433383] km/s
V∞_out: [0.041592732646317895, 1.627725242681464, 1.3244467950891392] km/s
time of flight: 1.2785674190820272e8 seconds
arrival date: 2032-08-01T10:15:37.243
thrust profile: [-0.41604742347230705 0.06737894984312282 -0.04205491392883786; -0.3861211958007792 -0.0758091335673133 -0.05360756017666809; -0.38159338209724647 -0.18683783846640528 -0.060539772129709346; -0.3350949731987023 -0.2563119526230099 -0.06133971353596192; -0.2871521785597488 -0.32348412532931814 -0.05786399726102912; -0.22253747113558456 -0.3141454362424642 -0.05305353968999086; -0.1648658017684768 -0.29697975715716984 -0.04751117142541355; -0.12442069988353341 -0.3116638659514345 -0.038228092969129816; -0.08111462090829119 -0.3069867266716785 -0.029740118494018575; -0.04613498335535642 -0.2951117896245657 -0.021059313316040384; -0.018598978169875633 -0.2815182543648192 -0.012932002016639724; 0.0045256419165849065 -0.2669272627444781 -0.004427429319138051; 0.0234811875972447 -0.25209972076750015 0.0029723567713946576; 0.039274945308955506 -0.24056465141722116 0.00993362495845694; 0.051426343418473616 -0.22281194727419235 0.016345479125692383; 0.06086343873321743 -0.2081388161322731 0.02188664991008354; 0.0685065126238841 -0.1926572918357054 0.026839097522788475; 0.07525744827143042 -0.18093945742485354 0.031075223064810226; 0.079392823582722 -0.16606035049084994 0.03454357195394954; 0.08295943887786963 -0.15412750790018656 0.03740347939202216; 0.08613999214593006 -0.1428938322974369 0.0395012677076581; 0.08772834490249906 -0.1310169948154417 0.04092188439412888; 0.08895334110394983 -0.1202339756399574 0.041849591117764914; 0.08730997577811128 -0.10626040353133856 0.04252301660314416; 0.08869148570645749 -0.09867056588432131 0.04236667383009366; 0.08803735659001409 -0.08883483723685866 0.0409433140159136; 0.08655169773377087 -0.07939821085862654 0.039500208451252544; 0.08531407495440747 -0.07069193052001756 0.037483909758018345; 0.0839157998172722 -0.06262433392398156 0.03491784670387027; 0.08241104639095365 -0.05456127680876876 0.031905310581824844; 0.08029247052881323 -0.047080198594668 0.028489062021749233; 0.07785957445382675 -0.039291190198784826 0.02477996888593748; 0.0764785313388362 -0.03234957407371497 0.020441460714379626; 0.07364576084853765 -0.02495977005348136 0.016149035754968472; 0.07045328958061775 -0.01772137162673052 0.011686575379395969; 0.0683660123350372 -0.010636482284919705 0.006942049179465146; 0.06625158462271445 -0.0033382009537524177 0.0022901113272747508; 0.06165831780883017 0.004819216901214894 -0.0015177666265392743; 0.05770562649405053 0.012951600227321435 -0.003618598699498523; 0.05264085001752809 0.021136344288158682 -0.003411686116928844] %
Mass Used: 495.9436459575345 kg
Launch C3: 13.726669245514401 km²/s²
||V∞_in||: 3.239693195068747 km/s