30 lines
3.5 KiB
Plaintext
30 lines
3.5 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJ_2021-11-07T16:44:24.602/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: 2027-07-20T13:17:34.631
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Launch V∞: [-2.3530089890058954, 1.806546373465246, -0.8246183971035168] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-3.557079179490031, 2.2348168420384456, 1.4054671292663363] km/s
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V∞_out: [-4.074087303045588, -1.0849670349142753, 1.3593729379381074] km/s
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time of flight: 1.0695600026560412e8 seconds
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arrival date: 2030-12-09T11:17:34.631
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thrust profile: [-0.0022189023782523748 0.023365002143236557 -0.010993409331132617; 0.2153019288203301 -0.16440845543934793 0.012979033551565024; 0.3639464079118591 0.18422132432552532 0.04272023217963688; 0.11466184077416293 0.3079055688420129 0.008827434981649196; 0.030850502559811713 0.10710583581109685 -0.0392443866311469; 0.12842405226198722 0.13471500586493157 -0.046470788171139685; 0.022178550605493758 0.08362899413062866 0.012804941168562645; 0.12528977866442487 0.07930598418341506 0.05523752701719965; 0.11036663197880708 0.06908833586375046 0.030544670010797404; 0.2621885557666051 0.017745488649470693 -0.043256804103609825; 0.32712194273437595 0.3540199595758462 -0.06793264883835635; -0.12456921081136497 0.30022659769281007 0.011877569185517847; -0.111118550048934 -0.0012849144456734945 0.0618346466936284; 0.0664475480767869 -0.20857672555247925 0.05232162118008461; 0.4674741919141163 -0.27665818135554127 -0.010294403145171388; 0.6235722276862998 0.33893717906065446 -0.08396785235072478; 0.06141376840855648 0.6645340284197009 -0.04540915059549516; -0.4950753135059394 0.4265532645880646 0.04403645965499313; -0.4790065958792388 -0.05470792785400573 0.08950665085522541; -0.31489858710635427 -0.3741453611976776 0.10307557908026614] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [0.38917010093640664, -4.172653280725571, -0.38172849726338637] km/s
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V∞_out: [-0.19079117316696953, -0.697272265566823, -3.556895184028567] km/s
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time of flight: 9.204480003834815e7 seconds
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arrival date: 2033-11-08T19:17:34.631
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thrust profile: [-0.28696988915862254 -0.5466775279353076 0.0161784825048141; -0.05201138624094085 -0.5103548545163037 0.022399691416144073; 0.09258223397854948 -0.42700369632306956 0.02864531312701303; 0.1544195747765251 -0.3175042943871396 0.03319962132309101; 0.16629852231537434 -0.20372710365454566 0.033385847516108444; 0.14766618426707362 -0.10862149045095645 0.026893053884926972; 0.10680433249395786 -0.047590669692367006 0.013917994143247845; 0.05372607652222386 -0.024738666039118885 0.004540404069389168; 0.0454652164291245 -0.03203318353562152 0.003800593821863827; 0.06019445610850742 -0.07020561382583693 -0.0007266034614935319; 0.031747954241254955 -0.05399780408669305 0.0026705429420879126; 0.008868957922568855 -0.0550458335463559 0.003204913050222715; -0.0001325460641792178 -0.0009815769471698307 -0.0004937922234238575; -0.0006857531267272214 -0.007291536557149579 -0.0032616756502396376; -0.002795903533707593 -0.01051173235400901 -0.00025468873326567386; -0.0011701726557658773 0.007181885264360277 0.019496153473968613; -0.00244282675331443 -0.004315368336196475 -0.00303667834001964; -0.005725948352347262 -0.005635872428339283 -0.003961276803316091; -0.017216802798993906 -0.013717525082576966 -0.016160860429875766; -0.026100664086817275 -0.009712024123055465 -0.043657502180151124] %
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Mass Used: 1804.5751392877032 kg
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Launch C3: 9.48025660266455 km²/s²
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||V∞_in||: 4.208111858569789 km/s
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