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thesis/julia/test/missions/mbh_2_phase_archive
2021-10-12 21:49:46 -06:00

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missions/mbh_2_phase_archive
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Spacecraft: bepi
dry_mass: 2000.0 kg
specific impulse: 2800.0 kg/s
max_thrust: 0.0005 kN
num_thrusters: 2
duty_cycle: 0.9
Launch Mass: 4000.0 kg
Launch Date: 2024-10-23T01:57:04.645
Launch V∞: [-2.756658080311089, 5.4981544960382, 1.2354164981485998] km/s
Phase 1:
Planet: Mars
V∞_in: [-6.97287754424969, 6.962353258098406, 0.0607051347526173] km/s
V∞_out: [-6.685432199487985, 6.971638091675174, 1.9494641006878624] km/s
time of flight: 1.16503060035366e7 seconds
arrival date: 2025-03-06T22:08:50.645
thrust profile: [0.0007372127333915423 -0.0014732374607987512 -0.0001436849126190515; 0.0015863792714624523 -0.0020954380857885 -3.9222886974518435e-5; 0.0028749200111876953 -0.0029070168117665577 -6.834239668653902e-5; 0.00400664873911032 -0.0036102638724926027 -0.0011534186183358992; 0.003002315886422529 -0.004155862034974375 -0.0019852589032208707; 0.003937369046006624 -0.003292245456470277 -0.00033744520390480056; 0.004022116761090881 -0.0014747882735426667 0.0009925828352185433; 0.0028363477848649932 -0.0006118542455278574 0.0011994525100711487; 0.0010235706279971136 -0.0007807187007764947 0.0007198591227898102; 1.9987192194599394e-5 -0.0011241077612402291 0.00021045682481486607; 0.0007623347096515055 -0.001326552903003275 0.00047334230828265155; -0.0019176703329012404 -0.003664068924494901 -0.0007926699243678642; -0.0034278750339086722 -0.005605775872095162 -0.001640142456026017; -0.003879314794056328 -0.007180423427345347 -0.0021627562917433257; -0.00457576381748711 -0.009085671380846889 -0.0027950147837868416; -0.00496447070432947 -0.011003150581070032 -0.0033564467543545713; -0.005782291476516903 -0.013187396198780097 -0.0040189185350814815; -0.005773642750057005 -0.015126117254672524 -0.00448918463406626; -0.006039589107819558 -0.017206354330223952 -0.00500209304716878; -0.0059712529665976325 -0.019287648124267687 -0.005416379053301935] %
Phase 2:
Planet: Jupiter
V∞_in: [-2.501340292332268, 1.6226626635888894, -0.637397317769162] km/s
V∞_out: [-0.39137693018363046, -0.6158439855618857, -0.6179155724361174] km/s
time of flight: 1.634809557285843e8 seconds
arrival date: 2030-05-12T01:31:25.645
thrust profile: [-0.26518247245545706 -0.09071259046697609 -0.06169797323040991; -0.08236380894068383 -0.03242059745452859 -0.0437757891207446; -0.0040559771435419905 -0.006989709543848695 -0.015529763525228361; 0.007774341207249076 -0.008985090840076109 -0.01850530400329914; 0.0012813370577481318 0.0011348539591867289 -0.0155496567606658; -0.007785092497807246 0.05338536306193304 0.019317990985589086; -0.0009728321119441025 0.08815185628620617 0.03949499622566367; 0.04305174658529387 0.2568399121830553 0.055654966170718544; -0.2720351356694226 0.46384420969664153 0.03864258122986833; -0.4887396982520584 0.11774562801231306 0.0008189965640148597; -0.3013298404095551 -0.13014726189273046 -0.05096356023658363; -0.13491430696546597 -0.11875243254479609 -0.04906685950011366; -0.07101074561201698 -0.09571411749724586 -0.04115396467769674; -0.03429442666375736 -0.08608492077264626 -0.032404742164699976; -0.005411454576501817 -0.08226389770332371 -0.021813716609185803; 0.01648826033313751 -0.08220086232228146 0.011531267107186598; -0.0514818142417244 -0.08481514714903496 -0.00037084018174361565; 0.04041503097410506 -0.045097405358868914 -0.044059162529628035; 0.22484925497674185 -0.023660465666373143 -0.05114459775451727; 0.4409715896106006 -0.006503526378072674 -0.04283633117576671] %
Mass Used: 1093.7042742756403 kg
Launch C3: 39.355120557947245 km²/s²
||V∞_in||: 3.0489363257617543 km/s