37 lines
4.8 KiB
Plaintext
37 lines
4.8 KiB
Plaintext
/home/connor/projects/thesis/archive/EVMS_2021-12-13T15:09:50.799/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: 2023-03-26T07:12:24.150
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Launch V∞: [-4.691695981755256, 2.4100997067687473, -1.107625419239362] km/s
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Phase 1:
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Planet: Venus
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V∞_in: [-4.566977871130657, 4.760076803915006, -1.7341280162885988] km/s
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V∞_out: [-6.208492431552701, -1.9096233111972523, -2.080047657050257] km/s
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time of flight: 2.0717178639097057e7 seconds
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arrival date: 2023-11-21T01:58:42.150
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thrust profile: [-0.14461666591877725 -0.010674923527958081 0.07319622237982218; -0.2632510872185629 0.01896952413347131 -0.11219362381384182; -0.35509253776259864 0.05130847606843313 -0.1020767266141743; -0.43017679281809584 0.05045981562535008 -0.1422217250671829; -0.5045985167824136 0.01741583415172031 -0.16844373611917648; -0.569330040676884 -0.05201323466205199 -0.18486385532265195; -0.6249141520690602 -0.13905479590410533 -0.19964164942840817; -0.668271188513656 -0.2602797013356586 -0.20608604356710608; -0.6652598099366694 -0.39412254799113705 -0.19894484200845694; -0.71516785653991 -0.49228396872807745 -0.21106475073434702; -0.7140520681258179 -0.6492058751655467 -0.1932030922695093; -0.6868766770794695 -0.7396924869993249 -0.17353711242581565; -0.6152532209931442 -0.8020815173678328 -0.14764124943790446; -0.4622171233071141 -0.8398654668968106 -0.11185995276929935; -0.16854886447084155 -0.849107084555043 -0.06766821177549498; 0.23324400917872504 -0.8297560629709333 -0.01536095606168015; 0.5186243199535893 -0.769610557984718 0.03995200418629567; 0.6187570125005067 -0.6500477297841986 0.08764709560669148; 0.5808087120622782 -0.5121872212939763 0.11783856477232442; 0.4583737403324055 -0.3712720822360683 0.13462225195583247] %
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Phase 2:
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Planet: Mars
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V∞_in: [-9.200127095735333, -6.894307184186653, -0.4734726391357551] km/s
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V∞_out: [-7.90745728238742, -8.353687515473082, -0.3001668168215188] km/s
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time of flight: 5.676487860450122e7 seconds
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arrival date: 2025-09-08T02:00:00.150
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thrust profile: [0.9450818166379835 -0.39326487285299566 0.08478396733763034; 0.5033926889693318 -0.49600851782195465 -0.09864181576764529; 0.593874568813462 -0.5134648071397765 -0.21563608217734162; 0.6726275954838512 -0.44694734612516734 -0.3151164039729524; 0.6947676879446373 -0.29388960390973834 -0.3690682632127033; 0.7117640920103931 0.07243876441940703 -0.41029659430010107; 0.7001034602049846 0.6195031306652655 -0.4186969404202771; 0.695103119957999 0.6808867140504492 -0.4033934445136916; 0.6468162520522805 0.7276709960247509 -0.3673200063653498; 0.5786083720048963 0.7618030225293763 -0.2740863676479381; 0.43998280657362615 0.7813682905260836 -0.09859638125917183; -0.04546726863354173 0.7884156184890568 0.05317843281930274; -0.6546093330399981 0.7727091843423107 0.11218174811377148; -0.7965171690457952 0.7496124509846286 0.19970259425421277; -0.8736983626104139 0.6200392713895918 0.2654841797347523; -0.9103125128246278 -0.6456308917849752 0.27992773703210205; -0.9019970750226028 -0.9023670767015256 0.1864233187998923; -0.6771646049748614 -0.9414644139448815 0.011110810182933379; 0.3521154040459276 -0.9440844390692263 -0.16519285405497774; 0.7774895055238358 -0.9371489950391606 -0.2516063758929405] %
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Phase 3:
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Planet: Saturn
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V∞_in: [5.616813665429002, 6.787110157183047, 1.2069938406439464] km/s
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V∞_out: [2.1970387730495697, 3.225023288265242, 4.175802839196012] km/s
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time of flight: 1.6257487956751725e8 seconds
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arrival date: 2030-11-02T17:41:19.150
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thrust profile: [0.9505134233163771 -0.979494400300436 -0.30984147298673975; 0.9511180319113616 -0.9647970604644283 -0.6501969016781382; 0.9424633459203795 -0.9926658842113464 -0.6207418959532092; 0.9304882859838348 0.23850084565208374 -0.5933249374851602; 0.9098194053379338 0.5493464195536784 -0.5111960642202787; 0.8829443918138722 0.6659627102171121 -0.3774953044827189; 0.8472666578022966 0.7031440366152961 -0.2698632635749556; 0.8051838923072202 0.7113118353482547 -0.23246846453046197; 0.7503491889394095 0.7106325372593361 -0.03813921871732603; 0.6848270191956657 0.702152969321232 0.03334922254887817; 0.6172988381336922 0.6882916490356381 0.08048503574576253; 0.5480320293122681 0.6685098976431961 0.10512250251977935; 0.4755966950131009 0.636871879957033 0.11757167935113788; 0.3912388892675421 0.5870441077418865 0.12131662398055057; 0.3071016125028102 0.5153387959524959 0.11568557231704885; 0.2061494535664333 0.42029155244133604 0.10481292164087117; 0.14105224096703986 0.31043414548479376 0.09141235006535123; 0.04128524414299072 0.18984755798020106 0.07349121047003337; 0.015873438623124358 0.05896310201745711 0.05559998369192176; -0.03554622243905677 -0.04901685480247809 0.04100049118737373] %
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Mass Used: 1688.2891346811068 kg
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Launch C3: 29.04742585113039 km²/s²
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||V∞_in||: 8.892147894026486 km/s
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