30 lines
3.5 KiB
Plaintext
30 lines
3.5 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJ_2021-11-07T15:15:24.057/mission---------------------------
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Spacecraft: bepi
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dry_mass: 2000.0 kg
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specific impulse: 2800.0 kg/s
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max_thrust: 0.0005 kN
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num_thrusters: 2
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duty_cycle: 0.9
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Launch Mass: 4000.0 kg
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Launch Date: 2023-01-23T13:44:20.247
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Launch V∞: [-0.1739597247433209, -1.5392251924256757, 0.1510741902051145] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-1.747388916324353, -2.061505608833443, 0.004246536679567164] km/s
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V∞_out: [-2.4403954507440164, -1.1573303397285044, 0.09102116739890352] km/s
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time of flight: 1.0791720765728353e8 seconds
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arrival date: 2026-06-25T14:44:27.247
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thrust profile: [-0.003437324500446065 -0.06316993477714959 -0.03227448158061817; 0.01567838811254846 -0.026330238009065726 -0.042075545977590216; 0.05142670882061399 0.03192109164526059 -0.030663473328706496; 0.18494150891704356 -0.05996396933783311 0.07272546357288993; 0.01987844881950037 -0.08012428438452728 0.14827651870110511; 0.0478009970849944 -0.02735889058433289 0.07798896298034431; -0.04075898555607768 0.11085612294078731 0.04603514580947307; -0.13952989202410981 -0.056985214724475576 -0.027200205223449195; 0.08522507291755119 -0.062139974359961894 -0.07129854782691303; 0.05351401270498842 -0.015500763055453866 -0.05259023429164523; 0.011282221363737887 0.02079500823213104 0.022523283753477914; 0.000699535966496786 0.09778479936527512 0.046529957624245714; -0.1030612853651482 0.12427737748752737 0.06708573684290235; -0.2038465893015885 0.014273665407528257 0.03802819777346354; -0.15618783028550054 -0.22318260536732798 -0.03742174282404114; 0.11410391007602544 -0.2082315215516395 -0.07040126308718953; 0.2521672881323561 -0.03769876422261141 -0.071688270611509; 0.23266831751793693 0.18743463203159552 -0.04551839351936565; 0.11519460197453685 0.3302484081094953 -0.02252892387897748; -0.18122294990431062 0.36229081369121324 0.04269874956058407] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-6.804956827112563, -4.679824047197812, 0.07151821136919514] km/s
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V∞_out: [-0.032527135720069, 0.001544851923976201, -0.00019858586424769518] km/s
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time of flight: 1.3383000099773991e8 seconds
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arrival date: 2030-09-21T13:44:27.247
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thrust profile: [-0.1392065495307979 0.004750835268938231 0.023507505308300022; -0.19310508213400865 -0.033187172798787246 0.03720253217974291; -0.08401649310562243 -0.03721535067081677 0.018686610849057983; -0.07189175926991606 -0.010086246689719958 0.002137809069141927; -0.04577388220162917 0.041578634569519 -0.018853960583673845; -0.1661362264023361 0.06506520619848838 -0.009449430204867661; -0.19796870421884868 0.04783193521476848 -0.023213922479647067; -0.12983109381999572 0.047003643397231905 -0.03086558152561419; -0.0882948553314463 0.1475664155854163 -0.017260515869025956; -0.3366163399243817 0.39553588365930525 0.015795560486203543; -0.640980062057629 0.2632981931405252 0.0812643122284222; -0.6170331837293128 -0.3303891659922319 0.08145169051162247; -0.417277476379212 -0.4064979390965165 0.057948112978786846; -0.1920015280971652 -0.28614848876207744 0.021902037419699424; -0.04488825027754133 -0.07688374836411227 -0.0050070954905793545; -0.020349917091670125 -0.03323033529641674 -0.02767377795875804; 0.0034924766822311388 -0.014218666042869754 0.006356643814839159; 0.00039701408140195273 -0.023899377007047005 0.09028397293070597; 0.052254845117264026 0.028631960813363038 0.004727246748924411; 0.03093967952976618 0.02034528891395188 -0.008818558262886378] %
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Mass Used: 1779.3184287128902 kg
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Launch C3: 2.422299589776762 km²/s²
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||V∞_in||: 8.259134663277639 km/s
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