37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-10T17:54:03.858/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: 1977-07-15T09:14:38.873
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Launch V∞: [2.5147318268598355, -1.1103623444144004, -6.402642134012201] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [1.4161036678756145, -1.1612060546662615, 2.9720800484503234] km/s
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V∞_out: [-0.90804226462538, -3.0734160134493123, 1.3849536778316178] km/s
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time of flight: 8.105040003981963e7 seconds
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arrival date: 1980-02-08T11:14:38.873
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thrust profile: [0.627838637604648 -0.12503628432096117 0.7855611132388014; -0.5289458287476022 0.6777841575676512 0.7075837038292085; -0.2373838703336668 0.7909345611869171 0.4331633366544985; 0.5432353517595965 0.7768839631178791 -0.783167310773754; 0.5396869301168233 0.7683167946626912 -0.7571970728573518; 0.23588696621684396 0.7769451734643089 -0.7270972946851668; -0.7694041770581667 0.601335658849241 -0.6637596322235111; -0.7921780190588894 -0.600905356962876 -0.44048431937604654; -0.7622543155226738 -0.7373700209872003 0.7911418295324951; -0.6606019028334599 -0.7987421962324748 0.7323144603647144; -0.1388661271934692 -0.7740008599199898 0.8060677773780438; 0.6499414579435336 -0.7130596280638938 0.7498586673145985; 0.817143568445207 -0.36590025267892895 0.3893357714242182; 0.7221677618564997 0.7956815784628078 -0.8027852216637569; 0.35730904625294274 0.8181592617310386 -0.8193971102980425; -0.7933587691663879 0.791605697884167 -0.8000227654400738; -0.8367294372565426 0.7202574934137008 -0.7630351620402276; -0.8524884295875419 0.527782602224365 -0.6846066726355504; -0.8673603491643094 -0.809433634144834 0.39335608125780586; -0.8116407828303132 -0.8844460508958141 0.7943966816976175] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-6.284565742386362, -9.76715307446354, 0.5888918727291137] km/s
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V∞_out: [-9.279749880105083, 6.689786284603497, 2.0909888468209963] km/s
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time of flight: 1.1491560055966887e8 seconds
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arrival date: 1983-09-30T12:14:38.873
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thrust profile: [-0.9127396122468532 -0.9218277687731674 -0.4263668054485564; -0.9127835283943397 0.5076311793916051 0.6901653820507275; -0.9277032940195239 0.8072913628070539 0.7376714170725708; -0.9413418283270233 0.8224253560321766 0.7734378668742132; -0.9475800103183779 0.7633312809013366 0.7988746215077034; -0.9543633564369559 0.47787598052458224 0.8062149670969349; -0.9559692329051825 -0.8194886763245005 0.5560168723764345; -0.9513976484586338 0.33441960267381193 -0.13333116315754445; -0.9427922092415756 0.8485944388724405 -0.37802038562147244; -0.9554914463244739 0.9253215472599327 -0.6472191305079521; -0.975933074552162 0.7725813929691159 -0.7667329121636777; -0.9712483448360393 -0.9635899350612177 -0.5468548163709348; -0.9443483595384782 -0.9692759844140697 -0.28668950342079663; -0.8886926888299911 -0.964158515619833 -0.20020199822347967; -0.7777727089323969 -0.9583099186800864 -0.17642040634769085; -0.5484454199881573 -0.9475574807265811 -0.16061558441899781; -0.16145042784627028 -0.9295820744714413 -0.14398087412630792; 0.1489729267980805 -0.8875509875058407 -0.12186518694197303; 0.3863989762520739 -0.7243671949614064 -0.10506111941783687; 0.550866374411865 0.6515340599054279 -0.09506697653138528] %
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Phase 3:
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Planet: Saturn
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V∞_in: [5.425276900065363, -6.401959760024709, 1.628957215805309] km/s
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V∞_out: [-2.078410685140159, -3.155305729801939, 0.0008586072596457413] km/s
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time of flight: 2.122127999843037e8 seconds
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arrival date: 1990-06-21T16:14:37.873
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thrust profile: [0.4137213553359692 -0.3123419166895793 -0.07413066083839148; 0.3866860426238052 -0.22444859437512898 -0.06473683963171227; 0.31555810889484437 -0.16704122103878502 -0.05672742473286491; 0.22729716039326592 -0.12827357453673835 -0.031539395787956954; 0.143207212399456 -0.12782196637060753 -0.020925701304977146; -0.055315287904767946 -0.1596070863670293 -0.15698789612711658; 0.0855670371677483 -0.3691654213130422 -0.22727650425327833; 0.296362079592094 -0.36205016550808794 -0.08720444491924713; 0.3416336893889104 -0.37382177982174647 -0.05355021694096375; 0.3922447283373164 -0.35961171719778656 -0.03138748595138845; 0.4272895758116155 -0.3267679698520526 -0.017497312957446522; 0.4465876315319068 -0.2826782360645849 -0.008534675888530218; 0.4531265921438839 -0.2323243789797917 -0.002376606148144884; 0.4495616785265872 -0.18074814564085967 0.0023041257879340494; 0.4380764579262854 -0.1330536192097116 0.005943447204693447; 0.42071889349085684 -0.09344905521564274 0.008645824111706685; 0.3990398415062969 -0.06332998130635517 0.011593397065563935; 0.3717084241277894 -0.04056062633087571 0.0157282909739208; 0.33657096418837157 -0.017725329809315477 0.03801942779075905; 0.32630435662337576 0.0002709235371287296 0.033211487884096974] %
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Mass Used: 2627.443374929516 kg
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Launch C3: 48.55060699314355 km²/s²
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||V∞_in||: 8.548229045965172 km/s
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