37 lines
5.0 KiB
Plaintext
37 lines
5.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-30T02:33:04.261/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: 2024-10-05T00:35:20.996
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Launch V∞: [-3.2137533909207794, 5.084712824855146, 1.430949155734375] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-6.255155316138288, 6.606484457110347, -0.23100377774853306] km/s
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V∞_out: [-7.465384617443416, 5.187341596386573, -0.43088705744489453] km/s
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time of flight: 1.3257925555072227e7 seconds
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arrival date: 2025-03-07T11:20:45.996
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thrust profile: [-0.007759166593782 0.008081441978955738 0.004825043238403784; -0.011235947824502553 0.006629595221827023 0.005298768481147631; -0.014134476908100888 0.004950559801138478 0.006335721099905584; -0.016912120418734602 0.0032538753168045408 0.00722543103380731; -0.019615343774186608 0.0015764448870706 0.00791543407768123; -0.02224614170581595 -0.0003222442781983473 0.008542627265521198; -0.024752022364092727 -0.002502638264186997 0.009081125608978445; -0.027074692908356103 -0.0049669389909122045 0.009549338120131428; -0.02919125492967198 -0.007632280649054239 0.00984618903400726; -0.031034823850380824 -0.0105147854228823 0.010076901834442997; -0.03258867449421671 -0.013557927955447253 0.010239842439460488; -0.033896907887579285 -0.01664233072935544 0.01017836634561616; -0.034798910393570345 -0.01976899064579983 0.0104762622470642; -0.035510243080800585 -0.023010543051237668 0.010185800368979887; -0.035958245848237244 -0.026088542265344326 0.00997354827689359; -0.03616255540821458 -0.029107623361033046 0.009767283341448791; -0.03613539245186166 -0.03208125702710542 0.009490588816176345; -0.03594590447689291 -0.03485698552669035 0.009220695825097646; -0.03554558605538018 -0.037576230560006675 0.008899820851614233; -0.034817304760338785 -0.040399339549697474 0.008549184269071997] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-4.869253095327301, -1.0830259181507658, 0.41420291406622983] km/s
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V∞_out: [0.7972771522364179, 4.941460361504594, 0.0211284831130985] km/s
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time of flight: 1.7681537153208575e8 seconds
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arrival date: 2030-10-13T22:43:36.996
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thrust profile: [-0.4667533593525884 -0.39491731925461715 0.09187802488824132; -0.2763903182910042 -0.37035074693961667 0.09861113689219381; -0.16222846365284407 -0.29220875981191247 0.08972904873143848; -0.12809339133608721 -0.19599395109677922 0.06703442708591248; -0.12151618016164137 -0.04686965062834339 0.033439069587540726; -0.10811409035917058 -0.009477194232797893 -0.012143321662504066; -0.10924801926559909 0.14082268122578098 -0.05670682044948156; -0.029758444441605168 0.28004126085284164 -0.08287077095226834; -0.005277793889388453 0.43294397265469803 -0.08212135825686287; -0.32054145122009575 0.5753532885361126 -0.03968329559118082; -0.6812467539999161 0.3089367113933967 0.051808034060789085; -0.6510836214832658 -0.4873937421666415 0.12520004751950561; -0.49557588979996686 -0.512322294250635 0.15992845574394862; -0.34374129520368857 -0.5135522557199093 0.16537305271566424; -0.2240792189464561 -0.45518516492142325 0.1550538281965299; -0.13865236852037352 -0.37950308770911234 0.13394772771689303; -0.0785171269810383 -0.2978976352535766 0.10596692987800144; -0.035327531433840355 -0.21564018776939112 0.07474526871132638; -0.005605243694407901 -0.12702627457742785 0.04128648833249606; 0.01020681436565993 -0.02502132504960536 0.004261721313786419] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-1.9690596099587732, 3.2707822497004333, 0.03981900780395632] km/s
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V∞_out: [5.114183571314532e-5, -0.00028059524048684205, -1.0322857139071202] km/s
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time of flight: 2.4691764297066832e8 seconds
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arrival date: 2038-08-10T18:57:38.996
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thrust profile: [-0.010548481282575234 0.04258751351881362 -0.025726963732731655; -0.01128130800439453 0.05537735517283375 -0.02522998253773597; 0.009886584360292121 0.08885355612430626 -0.02421777901196621; 0.034425823426465496 0.1204073126801249 -0.020057117827333014; 0.039281760158963876 0.14271215958548816 -0.013510596261601598; 0.018736852336642556 0.15327407334940432 -0.006130067311322509; -0.022719461407261828 0.1451025891518733 0.0027035496704120453; -0.04847577536899553 0.1212275153694897 0.010891420241408132; -0.06628322085560583 0.08574069656011961 0.01754569902422787; -0.0744351565286978 0.045598034397603175 0.023036321178276163; -0.06578589050933895 0.03204645107589838 0.02550340232781789; -0.06050564660450317 0.014954861896586048 0.022962687464765534; -0.054168514931042216 -0.0014952150532753753 0.025171195023900708; -0.04623865244234472 -0.016264370557547467 0.0242622456069454; -0.036824077689454164 -0.0297205445345202 0.026079813616960393; -0.0019119020757232493 -0.03990997756665856 0.02228921048798602; 0.00955546353811231 -0.039278332497075394 0.01302479870315554; 0.023384650419100452 -0.03759767262766218 0.006978165358701964; 0.03212872391392216 -0.041380395386008566 0.002045914746881736; 0.042058274941623244 -0.040048678289472804 -0.002284527484416767] %
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Mass Used: 739.6059104634573 kg
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Launch C3: 38.23013085519812 km²/s²
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||V∞_in||: 3.817957284453156 km/s
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