30 lines
3.4 KiB
Plaintext
30 lines
3.4 KiB
Plaintext
/home/connor/projects/thesis/archive/EMS_2021-12-12T14:59:57.936/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: 2023-10-25T14:05:40.189
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Launch V∞: [-2.237183685934752, -2.721647916047431, 1.299312276740919] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-0.678207962240434, -3.5504123945109747, -1.2418379495810854] km/s
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V∞_out: [2.332007819175787, -2.421453655328241, -1.8183105258695256] km/s
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time of flight: 1.855655995918323e8 seconds
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arrival date: 2029-09-11T08:05:39.189
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thrust profile: [0.19727184520667015 -0.3838952007487214 0.17961473110199166; 0.2077514036189871 0.5200804821813247 -0.10558577682756237; -0.022196502289827003 0.3282119359443656 -0.17880640948902576; 0.022167314146114503 0.3526089664383984 0.35012764112560996; 0.3025719335339175 0.3093777519487111 -0.17023625811931237; 0.15995107289139296 0.3622712142968187 -0.1750157659189659; -0.2760617452549359 0.41412522749535996 0.17764253337734176; 0.32935922189339817 0.1968557028627668 -0.026495445347781893; 0.2681770910187345 0.4086838063855519 -0.18928477304761748; -0.24197868619321736 0.45257178565912115 0.10670805906910212; -0.30369774778452496 -0.386093378582689 0.10490688892166344; 0.5108677715826049 0.1835799494496108 -0.2034993601786804; 0.045093348543829 0.5895547713851573 -0.034986947864212484; -0.5736310275454822 0.23658188722553572 0.18619609441669782; 0.23133883855583576 -0.5862475003689892 -0.05214808227492976; 0.6442849903188875 0.40530400231961805 -0.21464210977314127; -0.020964246471072177 0.7236236640594544 0.012492389285940016; -0.7227867443191269 0.34102536963229013 0.22159525812592265; -0.39003244325739894 -0.719098783178554 0.04735599030806113; 0.7348700748588787 -0.5860442405640622 -0.2239590199604165] %
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Phase 2:
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Planet: Saturn
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V∞_in: [1.2532005419075063, 2.905447896432199, -0.443912289899149] km/s
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V∞_out: [0.009293489123982904, -0.022791627564424932, 0.00035910126775256265] km/s
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time of flight: 3.841884000189513e8 seconds
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arrival date: 2041-11-13T23:05:39.189
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thrust profile: [0.8354818174826176 0.8278651352879969 -0.019139799616379415; 0.07789587464121626 0.807772028598289 0.09208866935020069; -0.4371258372752062 0.7097083046464899 0.07648931927262204; -0.4593926819327141 0.5921013650423435 0.05279771473551259; -0.41803959049762845 0.4756823109687688 0.03511376028590402; -0.36046979629046133 0.37325588585291325 0.023223381248584807; -0.30164482520132996 0.2891579617780395 0.01559727222329367; -0.24852711164559912 0.2211224649200195 0.01083260426477029; -0.20341018128087673 0.16521746219046313 0.00787777038183007; -0.166313250377776 0.11914245715911004 0.006052029723090913; -0.13685498996724776 0.07579955310252746 0.0051696709685845; -0.11590045234482386 0.03683619622380138 0.005503034114011019; -0.09714808717387836 -7.510913642337649e-5 0.005881543716786649; -0.07947906741787436 -0.03636451674166609 0.006573855151556507; -0.060762284460828354 -0.07185315172378559 0.007324504256710228; -0.040146440269578795 -0.10503734607332527 0.008063012601483146; -0.01826447390719847 -0.13480682166408572 0.008650026851941802; -0.0014999731370244022 -0.16167322260227676 0.010344109911906468; 0.019647516899938273 -0.18187401707529088 0.008884133379429506; 0.07031314483210122 -0.20333200721827405 0.010747903674476903] %
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Mass Used: 1995.6659445951054 kg
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Launch C3: 14.1005706160276 km²/s²
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||V∞_in||: 3.1951834373386236 km/s
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