37 lines
5.0 KiB
Plaintext
37 lines
5.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-30T00:34:25.423/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: 2024-04-23T20:49:35.793
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Launch V∞: [-2.4450865737116274, -4.101829409199476, -0.21378743337924264] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-3.9454321781223207, -4.3349983737367435, -0.23163519766252774] km/s
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V∞_out: [-5.484540365422154, -1.7912021635297986, -1.0612283164832435] km/s
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time of flight: 1.3168651513492899e8 seconds
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arrival date: 2028-06-26T00:24:50.793
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thrust profile: [-0.120722733695335 -0.012176360827686798 -0.030518390794883023; -0.11679617667506606 0.0014999178722870938 -0.035606031789671; -0.07727822397577828 0.3037973459191278 -0.0585534522901871; -0.223884565034074 0.38469778038311786 -0.018658505423278564; -0.5047726947284132 0.1198586588428443 0.04363822566057665; -0.36008917896849646 -0.046966759269397945 -0.012020139167426613; -0.2303697349032088 -0.18990779273074385 -0.1162523931176612; -0.009059953396105604 -0.1826064551186425 -0.09566243569922224; 0.06464171493355703 0.15348717344682897 -0.03592117858719949; 0.039222535062581575 0.45251270837425567 -0.002237551646205031; -0.3129537896040898 0.5005808668195679 0.06976206030714757; -0.6334356581244346 0.342167669148952 0.08785885490233064; -0.6259891593556097 0.07036975867629339 -0.029340487056482453; -0.45498760154179435 -0.5093792240633872 -0.13924939952781157; 0.03362679051118392 -0.46176686054217253 -0.15798494014212214; 0.4358161230258788 -0.13839418528576888 -0.05039097669674436; 0.3044870713576448 0.4992315283787602 -0.0039116386904277205; 0.17193614377332783 0.7613325121786818 0.03200649181430257; -0.5572427328043519 0.7854289375339618 0.10069718693059672; -0.7044302858314516 0.6325274227780806 0.1358242855667267] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-4.177197074414225, -0.9720140804548069, 0.2337469329489975] km/s
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V∞_out: [-1.1897818013258668, 4.123843236773216, -0.16384853893411477] km/s
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time of flight: 1.0354715657281214e8 seconds
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arrival date: 2031-10-07T11:30:46.793
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thrust profile: [-0.9480754862164437 0.3056342864181156 0.04775925131934315; -0.9545036085062072 -0.08916062469268374 0.07006956877613481; -0.8556415500647792 -0.5308952023053652 0.07581953613413958; -0.6525116764830651 -0.6804771046594907 0.072044066669931; -0.4141337602665943 -0.687613497545176 0.06325121629083955; -0.2876119881822729 -0.56915707346219 0.04608924218869737; -0.23061087236806183 -0.4285889382631892 0.0353521662171739; -0.21444588630200445 -0.2987113553031206 0.00894677998389626; -0.2042602334001383 -0.19716033565885058 -0.010540546258761902; -0.19797650808153522 -0.05516030431031445 -0.02296358167357804; -0.17870024970353923 -0.051487903415797315 -0.028673002243452296; -0.16087764941466745 -0.006028156883433786 -0.029496266489663633; -0.13249691125920962 0.010594568264314964 -0.03373869555595076; -0.1023119680343583 0.024125699413220757 -0.03194152432595998; -0.06667052712715316 0.022162434908797966 -0.0413032534053769; -0.02650461479736716 0.019860230188950657 -0.02825273461209873; 0.008483997200284142 0.010514866140007597 -0.027548374980192067; 0.044674954681201196 0.010390355078242345 -0.02558959064331584; 0.0698391445723141 0.01711123350841671 -0.025534958302052144; 0.07369308900718043 0.036955143265610016 -0.01808340139735954] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-2.855151769198392, 1.832432120626587, 0.030050486577809125] km/s
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V∞_out: [0.043566731882813375, 0.1453515199166137, 1.1921829828355344] km/s
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time of flight: 2.616408348306797e8 seconds
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arrival date: 2040-01-21T17:31:20.793
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thrust profile: [0.04225281791313958 0.029025037669065452 -0.0022530954062099607; 0.03735188618997079 0.03969404585926613 -0.001990942517015921; 0.027816672613794786 0.05946905402188188 -0.0018579377168727645; 0.013243713257944257 0.07889753909094255 -0.0012755910819474462; -0.012739124713320801 0.09684893162964908 1.027454400474268e-5; -0.04822800674369958 0.09918628844749049 0.0017567047619653946; -0.07935450012796613 0.08394550684634153 0.0037636317001541555; -0.096945253591464 0.05610257601854072 0.005447062756033347; -0.09806004451336248 0.030655118745335445 0.006892840256261471; -0.09160482001962598 0.01129333668797376 0.00817823646747505; -0.08125465088354236 -0.0016801849370562216 0.00916589692955618; -0.07057826106211562 -0.012831389696222687 0.009635922957337987; -0.0608971186898785 -0.022237451930920055 0.009413611150840169; -0.04763682121829541 -0.030887917780507177 0.00991332083072347; -0.03427587291576678 -0.038223126040402684 0.0087593563060389; -0.020871167351686367 -0.042373328878652756 0.00605668309720862; -0.00993028466867035 -0.04326291873459541 0.004363203651694872; 0.0023913294032781693 -0.04518734156701757 0.0026868963953325204; 0.01211694278076428 -0.04625260852612796 0.0010932842321948841; 0.022158514510870343 -0.047555924847739336 0.0009362531581306844] %
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Mass Used: 988.3534236974547 kg
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Launch C3: 22.84915792178947 km²/s²
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||V∞_in||: 3.3927278307586537 km/s
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