37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-10T18:46:26.719/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: 1977-08-28T19:16:48.911
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Launch V∞: [-0.9048124421086198, 1.9143247567671402, 1.0655764532581016] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-2.4343783407486486, -4.687961859367619, -2.933139307760753] km/s
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V∞_out: [-4.790214200771935, -2.8588778216214474, -2.321748592254448] km/s
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time of flight: 1.2520840640242675e8 seconds
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arrival date: 1981-08-16T23:23:34.911
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thrust profile: [-0.6224581879584439 0.4288059372368617 -0.369846309902295; -0.8456103096731954 -0.5449676132404117 -0.5207697451591612; -0.8002461593492456 -0.855950096213463 -0.3124435417439843; -0.08909026312356522 -0.8654901195188492 0.07012982568146232; 0.680001252515441 -0.7588164444715032 0.36639076258430675; 0.5600241806519821 -0.5524736520531364 0.42732020550718447; 0.16764662042831702 -0.38130964149055036 0.34119753879891973; -0.731954705851045 0.09173304239444241 -0.3217028849043164; -0.8708852593282298 -0.20046295640353465 -0.47555463513488316; -0.8714792916879354 -0.8774730456609726 -0.40411815736943946; -0.7503507155222385 -0.8995426849328464 -0.19904254786993072; -0.21243617845242554 -0.8809796651748026 0.05347795073943726; 0.6472006222755674 -0.8484331643135395 0.11021347676692661; 0.7443657429086448 -0.7955146419656197 0.23886041656554424; 0.7440649663077856 -0.6390085790476502 0.3042575860828415; 0.37484890774561835 -0.37162261741629815 0.19144601961385382; -0.3550450393056071 -0.11435230249867454 -0.07617629787736838; -0.9195229993807225 0.2789170446342234 -0.2615678112840567; -0.9727616469871604 0.3446917247288234 -0.257471197235714; -0.9808492088715268 -0.5477259908772488 -0.44853687745916715] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-6.701136691962909, -8.599974967150617, 1.3162577103992203] km/s
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V∞_out: [-7.466152781006179, -7.773882414996021, -2.1024987830209496] km/s
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time of flight: 5.836177608302693e7 seconds
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arrival date: 1983-06-23T10:59:50.911
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thrust profile: [-0.9775204977097908 -0.5214058341481157 0.16197437982089447; -0.9681501773489387 -0.7500057879390385 0.22817317938497259; -0.9525762370469925 -0.832426651123316 0.28200011488079785; -0.92761259022897 -0.8555389932740242 0.3222489903321434; -0.8871450236047153 -0.8560245708679001 0.3479490816123863; -0.8195685407028787 -0.8487998122656493 0.3566147862452735; -0.7790460014892773 -0.8311841138895902 0.3582600049182118; -0.6190731426200151 -0.8078635763142238 0.3511260288381265; -0.5145129727216806 -0.7780683585790256 0.33770986872031583; -0.4148838449023785 -0.7435111238696445 0.29665258639127334; -0.328030995132986 -0.7010614327842398 0.2948502276631388; -0.2661376870905083 -0.6524456881612392 0.26648173671933306; -0.21007010595989548 -0.5926356418988066 0.23592936608072115; -0.16014790791450959 -0.5250602978661468 0.2043260162059496; -0.11439806841436284 -0.445002817701425 0.16965789733717526; -0.07922096702487279 -0.35121979340219833 0.13666559998803526; -0.04342546734347377 -0.24958467169576376 0.1009510992394805; -0.009561808725198587 -0.14116721656848708 0.06776342231966652; 0.025698079008218886 -0.029169079250700856 0.03660047680102405; 0.06723364775247613 0.09468227499819452 0.007603348452937278] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-4.879936875669879, -0.47223217562047437, 1.5644706826898132] km/s
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V∞_out: [-0.004764406068025241, 3.023809215796096, -0.006813540558789842] km/s
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time of flight: 2.520438083264169e8 seconds
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arrival date: 1991-06-18T15:09:58.911
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thrust profile: [-0.09400215473661182 -0.18945521309217062 0.1271918910889239; -0.08607974390576098 -0.15730289401708353 0.1330350509096681; -0.07832275239134029 -0.13478208666438357 0.1351441081454202; -0.07132837621235137 -0.11668356299904072 0.13473290589837142; -0.06422308680008934 -0.10329018345067097 0.13124190941207606; -0.05483219880785128 -0.09065397169544913 0.12875633044650717; -0.04534456797231015 -0.07960292266050767 0.12395016513276043; -0.0352252711827991 -0.07015964172632169 0.11766514477500203; -0.02415557927465716 -0.06150640906378341 0.11072639537362276; -0.012611759737086297 -0.05352376356987194 0.1025041600979924; -0.0005755408110000229 -0.044830667850551016 0.09493441557954609; 0.019044842896509144 -0.04345125363942511 0.07403861776967349; 0.02592414982088686 -0.030002827924179683 0.0741211457115302; 0.0402832985262284 -0.023419092869979216 0.061815224815860395; 0.054217569381438825 -0.015792813536919307 0.048795971971107605; 0.06660233013037975 -0.008291406855245277 0.03513209811142393; 0.07850378454520773 -0.0026815097750121706 0.021588614394289437; 0.09131650833507947 0.002815289108732593 0.005218753137309239; 0.1023654635811782 0.007548514976676589 -0.010865691913744062; 0.11263768787148964 0.01184198808791625 -0.025804576648942177] %
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Mass Used: 1595.0391476343098 kg
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Launch C3: 5.6187780075042495 km²/s²
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||V∞_in||: 5.146295333073091 km/s
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