40 lines
5.0 KiB
Plaintext
40 lines
5.0 KiB
Plaintext
missions/mbh_3_phase_archive
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---------------------------
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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: 2023-12-30T19:31:02.262
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Launch V∞: [-2.336381310504302, 0.6611197671240502, 0.515368333819228] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-0.11272517963886579, -0.16302256252244926, 0.06378439538637051] km/s
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V∞_out: [0.002792969304201863, -0.057484436403284406, -0.20003704249209486] km/s
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time of flight: 1.2592311667092939e8 seconds
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arrival date: 2027-12-27T06:09:38.262
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thrust profile: [-0.07359577344803886 -0.07004965985121933 -0.007807619171823321; 0.043716940115367385 -0.09696906663391322 -0.021035291284121637; 0.15053759331935357 -0.05794230926871806 -0.033866112736962925; 0.20610926006237767 0.0511534113841768 -0.013824814864455921; 0.14247998895987612 0.14895648069233977 0.016465691502639254; 0.033899970899824765 0.1413760732743736 0.033765822767487075; -0.031462663876756475 0.08723970741502689 0.022622665389646173; -0.060921211293504925 -0.026583703906071718 0.0072028126267209116; 0.05521899481152132 -0.05572354743233738 -0.03803266067329364; 0.06591230227849648 -0.0432693147820068 -0.028739472872060776; 0.16269932997793765 -0.016462438801152977 -0.026172416179982023; 0.20013411233717715 0.06074950755811254 0.022311277118381843; 0.14518787703981562 0.12065447079680057 0.05879531725301626; 0.09613845629727286 0.10922616684423382 0.06199408068784226; 0.08625318486313252 0.06478405529977578 0.0023557163450004174; 0.045240171138954385 0.04567139475192793 -0.021769604477046758; 0.04592748677552667 0.060844875114399566 -0.035619737179444874; 0.0804407212683229 -0.03642329187878312 -0.05296002481971273; 0.21331847937323517 0.00896049803861686 -0.05753325446312421; 0.34299417343430333 0.12023007248386997 0.0322957005600654] %
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Phase 2:
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Planet: Mars
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V∞_in: [-0.014005019530324568, 0.13244612304375988, 0.08290914548187793] km/s
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V∞_out: [-0.02364353280263756, 0.15444781952015216, -0.014432031974666977] km/s
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time of flight: 1.0032265935562963e7 seconds
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arrival date: 2028-04-21T08:54:03.262
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thrust profile: [-0.06468087317083572 0.01713477843818517 0.2072497145223751; -0.06817090268272546 0.022379474456103943 0.19523352237764163; -0.06466190699633262 0.0255932195152017 0.18504680757190148; -0.059342730861904634 0.029426412259887014 0.174021131351099; -0.054114404138384406 0.03235714045889413 0.16225743506965892; -0.04807653805996071 0.036042427078759764 0.1512460952152207; -0.04315764467216101 0.039938588900136185 0.1389467642307416; -0.038786939336882924 0.043008565514191716 0.12722354156375004; -0.03526577678074072 0.04925516219030345 0.11470911008101983; -0.03235044927513134 0.053149635505385665 0.10206946252525144; -0.03014670486994729 0.05684341793213379 0.0896246734207876; -0.028977404396851786 0.0652163530384282 0.07587210971138804; -0.027859643135747448 0.06761679131619418 0.06285226422798801; -0.02857790492958968 0.07811006965735094 0.04913666457443533; -0.02775839545031727 0.07678583628850277 0.035998823265238046; -0.028406280241582614 0.08254699374408436 0.022094948949750847; -0.029302358791746728 0.0852924409615851 0.008263056211369075; -0.030759783119304784 0.0935582591653256 -0.006356164301183838; -0.03225647939083259 0.09688810501349754 -0.020305695435992848; -0.03332559746608383 0.10297737446211802 -0.035147079795216106] %
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Phase 3:
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Planet: Jupiter
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V∞_in: [-1.5533855349488477, -0.54933117824406, 0.1996303316277416] km/s
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V∞_out: [-1.7570559978767255, 1.1363153583675671, -0.43717528976600273] km/s
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time of flight: 1.4637789443152088e8 seconds
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arrival date: 2032-12-10T13:25:37.262
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thrust profile: [-0.6645141202842072 0.6423371395484379 0.013751042498263796; -0.6671395131717702 -0.09924157003588908 0.004659679865807528; -0.44003790930216125 -0.3664663119690856 0.010688442625863746; -0.18891454451890152 -0.313514318687638 0.015602936100725717; -0.07725712172807717 -0.2160815424379723 0.015975909063353555; -0.024837854243774205 -0.15122812373661867 0.013850214915260109; 0.003917627641656827 -0.1085248645279647 0.010371457271638237; 0.02201996644065442 -0.08454038372778747 0.009321989004990271; 0.03388845898003741 -0.06745670404324332 0.008856982967798533; 0.04309282117740803 -0.053386654501724744 0.008719256737668418; 0.05160359506780744 -0.04166179990240016 0.008149701990869269; 0.05175963695335609 -0.026857606206935496 0.007776339351354358; 0.038796656264694244 -0.008231506041670077 0.005319243332846338; 0.030477068690802474 -0.0005391678971376555 0.002805208510592914; 0.021902353489560968 0.007139818756776372 0.00129759746267181; 0.023229339517858272 0.009106625479845766 -0.0009346891747994962; 0.04577321246719308 -0.011464605937068278 0.004192845438408305; 0.017603006711693223 0.027784064222860144 -0.002885487605696617; 0.05029298986098882 0.03435916705436917 -0.002619919338002586; 0.12026613656214907 0.17439044082372335 -0.003745065383345971] %
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Mass Used: 1755.9134038194406 kg
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Launch C3: 6.161361494059565 km²/s²
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||V∞_in||: 1.6597058874647421 km/s
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