37 lines
5.0 KiB
Plaintext
37 lines
5.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-30T15:47:59.016/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: 2024-07-22T06:44:51.639
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Launch V∞: [2.575248384952663, 2.739716813210934, -0.38893905027836745] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [4.32111461530485, 2.7960291205842593, -0.489556914131019] km/s
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V∞_out: [1.7907908980924474, 4.820115223157361, -0.5379099033537726] km/s
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time of flight: 6.124238397428751e7 seconds
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arrival date: 2026-07-01T02:31:14.639
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thrust profile: [0.02204617368488705 0.06285779065282272 0.012605171575819224; -0.011433803484298078 0.08848061166582002 0.07202092139015609; -0.07959321828350713 0.11796051271483557 0.10864894932433573; -0.16842886185138436 0.10168512037796995 0.12068506836380218; -0.23809792134546726 0.03408694703096996 0.10782537552663919; -0.2712846099916887 -0.05259050616229293 0.07714680434548718; -0.2691701026056171 -0.13114175093946576 0.03494697732427611; -0.2432473375546796 -0.19827411241093662 -0.012549713355480184; -0.19688682555894857 -0.25454624209774884 -0.060002522712937; -0.13420719992703317 -0.31198661132994665 -0.10268341121799718; -0.01782601669889528 -0.3411050774098038 -0.13846230630135042; 0.17407803978077827 -0.3653166442745793 -0.1617162480750069; 0.39405333004023496 -0.35863769585862276 -0.16764222379359453; 0.5881727003228676 -0.2918230276130316 -0.1538361990366852; 0.7349673257433222 -0.12576056403661834 -0.12169301624150872; 0.8068721878811431 0.08212623367867798 -0.06681093685570723; 0.7498334641941427 0.6273302531285769 0.0041442783835015165; 0.48778675631358515 0.768425653968566 0.07684034445879483; 0.03235026516840393 0.7961138086551178 0.1340769950940127; -0.187175909543306 0.725754663622694 0.16344645357600582] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-2.776889048582584, 0.577121588676522, 0.007961135089457616] km/s
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V∞_out: [0.7615534564462777, 2.718708568232091, 0.27004925013867337] km/s
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time of flight: 1.1292109290692344e8 seconds
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arrival date: 2030-01-28T01:29:26.639
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thrust profile: [-0.840176369612668 0.976860342718164 0.058196195949256124; -0.8628465472635846 0.7633342124306659 0.1067403299239058; -0.8382024712014463 0.2581297893476549 0.12338258921323142; -0.8025794731065865 -0.1952513411331264 0.12149932865338556; -0.7572209152982607 -0.32000638227817424 0.10891070865997188; -0.7036267077800332 -0.3720841081186767 0.09043232925350977; -0.6463345866299025 -0.4293290426371054 0.06661829901893401; -0.5816014177883754 -0.44981649190131995 0.05067422918383243; -0.47351459443415633 -0.43975356881090427 0.028888383104343048; -0.4446429769285578 -0.4496298163012175 0.016442900362289542; -0.3753382613887226 -0.44043470262281187 0.004400618346128699; -0.3104508002843935 -0.4100796118163795 -0.004420648978465791; -0.2535633130657495 -0.3762527335843237 -0.010222789989029061; -0.12727676625203097 -0.3385883342435648 -0.016879911592349858; -0.17160701300131967 -0.303175547483604 -0.013946042678809141; -0.14486147929059093 -0.25597770208827797 -0.012578650709578849; -0.12478337244188682 -0.2047807012949446 -0.008914893875013217; -0.10754382990114088 -0.15281428358709293 -0.0036295313604368246; -0.08430003348112626 -0.09766774422527713 0.003387978072041825; -0.049542730705205464 -0.025733639517012987 0.003344362241873508] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-1.4245259099537633, 1.4291602238263075, 0.11854473850651923] km/s
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V∞_out: [-0.6879338015175315, -1.3876319593718838, 0.8808502953774751] km/s
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time of flight: 3.408146015783399e8 seconds
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arrival date: 2040-11-15T16:12:47.639
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thrust profile: [0.0209250957876161 0.07236548568951691 -0.05441358281175795; 0.04271088201266738 0.059837108824994496 -0.04570267674006564; 0.06660112060615696 0.05195757710585663 -0.03370174018627228; 0.07859207469254972 0.05915284312855131 -0.01995033274559411; 0.05470694198510173 0.07831313755730426 -0.010342114841936848; -0.01348106574647589 0.11277794394272658 -0.0034013433219311725; -0.09145707370229726 0.10312222608201255 0.005576461043330823; -0.12850299192302284 0.05752290823836534 0.01577381261339529; -0.13477884086307976 0.013206245882351258 0.018396651241394796; -0.12124443428533518 -0.016003517409004134 0.02309161441900346; -0.10385877836751767 -0.034262782555751645 0.026881849627747586; -0.08713710038230636 -0.04462790000575737 0.02664100559569609; -0.071851222306589 -0.051275998799280825 0.02033038048400631; -0.05351516590047124 -0.05503941535681956 0.024892443243640875; -0.042179454832756653 -0.05447471988772444 0.02020467463443017; -0.03024017392297153 -0.05390626764438977 0.014150662481409669; -0.01972175537440891 -0.05302868663746655 0.005230379873849089; -0.012681981493559499 -0.05225628051430802 -0.0024339834268425693; -0.0044941899601042504 -0.05698931635146416 -0.007176158051852003; 0.009984513981692316 -0.06168319332065979 -0.016333699861465947] %
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Mass Used: 1015.034880811023 kg
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Launch C3: 14.289226045623414 km²/s²
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||V∞_in||: 2.021342590587859 km/s
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