30 lines
3.5 KiB
Plaintext
30 lines
3.5 KiB
Plaintext
/home/connor/projects/thesis/archive/EMS_2021-12-11T12:46:58.095/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: 2024-06-27T20:44:12.105
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Launch V∞: [7.331043976806805, -1.4831196012007795, -2.0245623512046933] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [7.494654195262718, -6.0609925282532195, -1.5465164285364046] km/s
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V∞_out: [8.361426259111628, -4.4394354885497, -2.3823072505126612] km/s
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time of flight: 1.0927270179201613e8 seconds
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arrival date: 2027-12-14T14:15:53.105
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thrust profile: [0.023332265026031952 0.009104569108764901 0.00629954147585845; -0.0016557218791188077 0.01962631342128255 0.025705762368190936; -0.024093977262103067 0.034136267923482864 0.04127784193457851; -0.05716526136359704 0.04151655990433137 0.04937581881860671; -0.08978841140825183 0.037467471815706095 0.04965327321348644; -0.11993513223616677 0.026533967699871562 0.046755622510516306; -0.1531417398423054 0.011465166956525712 0.0450015339745295; -0.1798910024661249 -0.010958035234353167 0.040725164468314354; -0.19949258297853104 -0.03912791834137119 0.03496282370942105; -0.2095378189457459 -0.0715570982112501 0.027651575768606357; -0.21854976076053584 -0.10808558698891595 0.02118335219201054; -0.19007677121186733 -0.14660854579446153 0.009316164763448933; -0.20623923432304714 -0.19574889973495846 0.006342495476503129; -0.1946190022918896 -0.250488140357656 2.0902619062690796e-5; -0.1631047479714882 -0.31008060921369185 -0.007131331834578688; -0.11255143746171749 -0.37370964738271606 -0.013811169750461278; -0.019515019669034205 -0.43369153744750616 -0.020445519976909028; 0.19816480144351972 -0.44821129856705755 -0.03362906769054827; 0.5110188524621195 -0.31112343771146783 -0.05819048814446341; 0.6288004165000244 -0.04917320571657702 -0.04513050099902747] %
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Phase 2:
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Planet: Saturn
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V∞_in: [5.293734358571078, 2.8678408184561692, 0.013339550220484931] km/s
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V∞_out: [0.04716000390909402, 0.22366680587637539, -0.5447644595624558] km/s
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time of flight: 1.425235096053826e8 seconds
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arrival date: 2032-06-20T04:07:42.105
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thrust profile: [0.6576686143235253 0.3983282167692387 -0.040657820784520814; 0.35898947395338654 0.482213895760015 -0.01457736331055029; 0.2418918180398632 0.40917465296239935 -0.027235944158173563; 0.18693029836434163 0.3001309863445353 -0.04795078143893266; 0.17245763177523526 0.24020298673049806 -0.04814251518646192; 0.14210932515321834 0.1971999216967911 -0.04644978179421798; 0.13551601813035644 0.16075235436433832 -0.04687487556492608; 0.10999571544133116 0.13945505978150918 -0.04018977645283118; 0.09389237369435716 0.12249824726225744 -0.034147954132379775; 0.07817603467998095 0.1091061330560275 -0.027512895131446207; 0.06000859121748583 0.10654100938138575 -0.015903939946752932; 0.044248657050263394 0.1002027939962748 -0.0037526170023857133; 0.017432466468028006 0.09844081095460211 0.015736280260922626; -0.0028322518503023707 0.08407047604089865 0.03216268095410213; -0.009665030744853838 0.05418448600092389 0.054271394924132535; 0.00829991223524997 0.03671735113395197 0.07037788504936107; 0.05287971274655226 0.010024909695991463 0.04123949561959472; 0.03098994422797628 0.013396671609721751 9.284814456508857e-5; -0.002877075807447608 0.0005192110683645124 -0.004545971900385684; -0.028522171379334084 -0.019564193850904677 -0.005660284903915027] %
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Mass Used: 462.9647257745969 kg
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Launch C3: 60.04270225525677 km²/s²
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||V∞_in||: 6.020657137117126 km/s
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