37 lines
5.0 KiB
Plaintext
37 lines
5.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJN_2021-11-29T20:07:38.430/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: 2023-05-27T23:45:19.477
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Launch V∞: [0.07060914008148668, -4.847892797001834, 0.5290687721885886] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-2.8376948696397957, -6.866970594886355, -1.1016914014907047] km/s
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V∞_out: [-4.226081909733871, -6.202110186999845, -0.3094281797413773] km/s
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time of flight: 1.596037143160738e8 seconds
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arrival date: 2028-06-17T06:07:13.477
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thrust profile: [-0.08820762853917691 -0.14898517184082533 -0.09820752341370556; -0.16244500639383114 -0.007014189727643575 -0.042114530446779465; -0.11504442623490056 0.058307478489750215 0.012249450040533938; -0.17383665852971933 -0.02660802135748719 0.026296611919654635; -0.133605782067695 -0.18132533878993642 0.026002941407235212; -0.04006331095609107 -0.20273912830830298 0.004427347789879819; 0.10608908750365087 -0.14243574598913397 -0.040859364773162925; -0.1334058871429112 0.07395229686780111 0.017691464102652134; -0.19635497913555464 0.04582057433286239 0.014753056279381485; -0.22659830579310275 -0.1361676942645219 0.028039092180629516; -0.056452159199491696 -0.282304137567597 0.01760271375341965; -0.055869205300458795 -0.07521165313474892 0.07001754063761095; -0.10815326401024924 0.03975665673607279 0.08633566772197054; -0.15411574858207477 0.11420315814948176 0.020068825808757306; -0.2842273817584412 -0.0034013997105323997 0.024345468294325344; -0.1943513861122515 -0.28856449475866197 0.024667879112035683; 0.06001359666756579 -0.2750814648121676 -0.016222720706101045; 0.1634047690981133 0.0633323684514685 0.037052952793005536; -0.06358457091065511 0.19606506430779863 -0.061016941617662156; -0.21816429202004126 0.10669767546640854 0.03444638959744015] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [3.7354750271686217, -5.88285076118926, 0.3565930630644914] km/s
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V∞_out: [-0.34319042907183317, 6.967067331497001, -0.17523613192719362] km/s
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time of flight: 1.599110498440805e8 seconds
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arrival date: 2033-07-12T01:51:22.477
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thrust profile: [-0.40987114064695546 -0.3774240932862401 -0.03561424162645277; -0.3658595283634409 -0.649925100592242 -0.03267051158991308; 0.3459098563469254 -0.6438693437660852 -0.04635788737542222; 0.5043654957163684 -0.3232526513194753 -0.01450355602555917; 0.42491000056144884 -0.21802276807884619 0.030992274127171215; 0.34082656017644314 -0.17376917376621892 0.04325816043964533; 0.1376056849711479 -0.12166741048661384 0.05225660923751248; -0.13620705214465267 0.022867431783402784 0.06787427526509686; -0.3502016747280746 0.1254089210892246 -0.03219035055838345; -0.7729039185116515 0.050166197257457634 -0.07418896319497846; -0.8826906384645422 -0.42770154496434787 -0.09066661080452741; -0.8697879488343527 -0.8989912582247904 -0.11292428779799557; -0.3012587410720149 -0.8933703434566561 -0.10271304251295864; 0.7595659924014233 -0.8695220977621636 -0.049116949463447176; 0.7872267924160511 -0.6662320332198877 -0.011350265126440771; 0.7392293426195585 -0.33787052962012654 0.00950541251523341; 0.6603814845566363 -0.005691408214699979 0.01737841943566633; 0.5573136293405954 -0.158764215359649 0.021196329449577604; 0.40957430642093684 0.1915873694381741 0.028239988792705437; 0.18146188186458964 0.1883476561832824 0.03330416774233607] %
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Phase 3:
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Planet: Neptune
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V∞_in: [8.506155596263332, -7.214120420207235, -0.09860913292565265] km/s
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V∞_out: [4.053253594386909, 0.1372094566434354, -0.11675704795783998] km/s
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time of flight: 4.156831849103214e7 seconds
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arrival date: 2034-11-05T04:36:40.477
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thrust profile: [-0.04831977082461104 0.02886785140102746 -0.0015969011424151007; -0.04917765507361394 0.029203456393022745 -0.0014934586981430707; -0.05007927680116305 0.02937008233469106 -0.0014606345664627358; -0.05064789643929198 0.029683169999243322 -0.0013262520866866735; -0.051317004632228186 0.02971960728170897 -0.0012160227437881396; -0.051520874234056616 0.02977614467368215 -0.001115494384017753; -0.056261871812928875 0.03168558834789489 -0.0011825214765981728; -0.05393084917042745 0.030529761089447334 -0.0010052780980467106; -0.0545540520950892 0.030843664255386857 -0.0008871465845663635; -0.05481610839179922 0.030675652290316765 -0.0007096252268282277; -0.05535607825958336 0.030792442226543953 -0.000613617898828771; -0.05621636785416013 0.031177946238027898 -0.00048131038774713544; -0.05674803704179758 0.031109150076321142 -0.00042081760152222307; -0.057490162528803464 0.03146649637736389 -0.00031633576187554854; -0.057978129725565604 0.031470064297792776 -0.00021040663675848088; -0.059695605398968794 0.03214040241964867 4.28282466982456e-5; -0.0598515487471952 0.03219101178897971 -8.932622689143771e-6; -0.060385880377208864 0.03228344074846185 8.425209789811808e-5; -0.06140170323745024 0.03255841183319602 0.0001927115343330996; -0.06185254886048141 0.03268815199448967 0.00029588992432612673] %
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Mass Used: 1125.3822536870607 kg
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Launch C3: 23.786963987590454 km²/s²
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||V∞_in||: 11.153830742224367 km/s
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