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Succesful MBH runs, with some improvements

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Connor
2021-10-12 21:49:46 -06:00
parent c7913d2944
commit bb78578d9a
19 changed files with 426 additions and 146 deletions
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25
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missions/mbh_1_phase_archive
---------------------------
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: 2022-03-06T01:59:18.919
Launch V∞: [-1.1356413222408823, -4.788069365262547, 2.7000635369246] km/s
Phase 1:
Planet: Jupiter
V∞_in: [0.606990343209641, 4.407893426470118, 0.9244860672598548] km/s
V∞_out: [1.2183577357736917, -3.9826645468861925, 2.3687041043301797] km/s
time of flight: 1.194581479969281e8 seconds
arrival date: 2025-12-17T16:48:25.919
thrust profile: [0.2047491180715187 -0.37019469041025893 -0.10453549807669095; 0.4301220091095493 -0.12441963747750297 -0.006770873233015344; 0.43924678986775806 0.1285374874465679 -0.07977271709638968; 0.42297198253230855 0.31380495510861767 -0.07919431310255642; 0.3614168205981836 0.39602843825488454 -0.05704653521018108; 0.2902414389460733 0.4053822027059241 -0.02821739799974643; 0.22430933743909634 0.43938508487263367 -0.00930631106824115; 0.13232647607691467 0.4188738913138919 0.007567873851875307; 0.054141732819826004 0.39551671259361465 0.010428460581952593; -0.012077434841877642 0.3792721276901153 0.0231446451624962; -0.042939891420425445 0.367704668401295 0.04590678245879779; -0.06832185713480624 0.39461571349444186 0.06647905984921844; -0.06871098668169624 0.3943544952193675 0.07996958584990013; -0.043122107121887 0.3236627227698529 0.06434542295394348; 0.0002258095938542581 0.3100245138960139 0.08315646808686966; 0.024384212213495196 0.1820219401839858 0.049878939508001104; 0.014803074731020839 0.09226807883171781 0.03031339291970727; 0.04882521682144194 0.07182823075104046 0.030435679401299; 0.07679479397181303 0.04220157719360384 0.024296177838332548; 0.07770574743624227 0.006328096858830944 0.01324607153162614] %
Mass Used: 1527.1786215537763 kg
Launch C3: 31.505632562776483 km²/s²
||V∞_in||: 4.544517160758207 km/s

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missions/mbh_1_phase_best---------------------------
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: 2022-03-06T01:59:18.919
Launch V∞: [-1.1356413222408823, -4.788069365262547, 2.7000635369246] km/s
Phase 1:
Planet: Jupiter
V∞_in: [0.606990343209641, 4.407893426470118, 0.9244860672598548] km/s
V∞_out: [1.2183577357736917, -3.9826645468861925, 2.3687041043301797] km/s
time of flight: 1.194581479969281e8 seconds
arrival date: 2025-12-17T16:48:25.919
thrust profile: [0.2047491180715187 -0.37019469041025893 -0.10453549807669095; 0.4301220091095493 -0.12441963747750297 -0.006770873233015344; 0.43924678986775806 0.1285374874465679 -0.07977271709638968; 0.42297198253230855 0.31380495510861767 -0.07919431310255642; 0.3614168205981836 0.39602843825488454 -0.05704653521018108; 0.2902414389460733 0.4053822027059241 -0.02821739799974643; 0.22430933743909634 0.43938508487263367 -0.00930631106824115; 0.13232647607691467 0.4188738913138919 0.007567873851875307; 0.054141732819826004 0.39551671259361465 0.010428460581952593; -0.012077434841877642 0.3792721276901153 0.0231446451624962; -0.042939891420425445 0.367704668401295 0.04590678245879779; -0.06832185713480624 0.39461571349444186 0.06647905984921844; -0.06871098668169624 0.3943544952193675 0.07996958584990013; -0.043122107121887 0.3236627227698529 0.06434542295394348; 0.0002258095938542581 0.3100245138960139 0.08315646808686966; 0.024384212213495196 0.1820219401839858 0.049878939508001104; 0.014803074731020839 0.09226807883171781 0.03031339291970727; 0.04882521682144194 0.07182823075104046 0.030435679401299; 0.07679479397181303 0.04220157719360384 0.024296177838332548; 0.07770574743624227 0.006328096858830944 0.01324607153162614] %
Mass Used: 1527.1786215537763 kg
Launch C3: 31.505632562776483 km²/s²
||V∞_in||: 4.544517160758207 km/s

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missions/mbh_2_phase_archive
---------------------------
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

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missions/mbh_2_phase_best---------------------------
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

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missions/mbh_3_phase_archive
---------------------------
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: 2023-12-30T19:31:02.262
Launch V∞: [-2.336381310504302, 0.6611197671240502, 0.515368333819228] km/s
Phase 1:
Planet: Mars
V∞_in: [-0.11272517963886579, -0.16302256252244926, 0.06378439538637051] km/s
V∞_out: [0.002792969304201863, -0.057484436403284406, -0.20003704249209486] km/s
time of flight: 1.2592311667092939e8 seconds
arrival date: 2027-12-27T06:09:38.262
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] %
Phase 2:
Planet: Mars
V∞_in: [-0.014005019530324568, 0.13244612304375988, 0.08290914548187793] km/s
V∞_out: [-0.02364353280263756, 0.15444781952015216, -0.014432031974666977] km/s
time of flight: 1.0032265935562963e7 seconds
arrival date: 2028-04-21T08:54:03.262
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] %
Phase 3:
Planet: Jupiter
V∞_in: [-1.5533855349488477, -0.54933117824406, 0.1996303316277416] km/s
V∞_out: [-1.7570559978767255, 1.1363153583675671, -0.43717528976600273] km/s
time of flight: 1.4637789443152088e8 seconds
arrival date: 2032-12-10T13:25:37.262
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] %
Mass Used: 1755.9134038194406 kg
Launch C3: 6.161361494059565 km²/s²
||V∞_in||: 1.6597058874647421 km/s

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missions/mbh_3_phase_best---------------------------
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: 2023-12-30T19:31:02.262
Launch V∞: [-2.336381310504302, 0.6611197671240502, 0.515368333819228] km/s
Phase 1:
Planet: Mars
V∞_in: [-0.11272517963886579, -0.16302256252244926, 0.06378439538637051] km/s
V∞_out: [0.002792969304201863, -0.057484436403284406, -0.20003704249209486] km/s
time of flight: 1.2592311667092939e8 seconds
arrival date: 2027-12-27T06:09:38.262
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] %
Phase 2:
Planet: Mars
V∞_in: [-0.014005019530324568, 0.13244612304375988, 0.08290914548187793] km/s
V∞_out: [-0.02364353280263756, 0.15444781952015216, -0.014432031974666977] km/s
time of flight: 1.0032265935562963e7 seconds
arrival date: 2028-04-21T08:54:03.262
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] %
Phase 3:
Planet: Jupiter
V∞_in: [-1.5533855349488477, -0.54933117824406, 0.1996303316277416] km/s
V∞_out: [-1.7570559978767255, 1.1363153583675671, -0.43717528976600273] km/s
time of flight: 1.4637789443152088e8 seconds
arrival date: 2032-12-10T13:25:37.262
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] %
Mass Used: 1755.9134038194406 kg
Launch C3: 6.161361494059565 km²/s²
||V∞_in||: 1.6597058874647421 km/s

22
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missions/nlp_1_phase---------------------------
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: 3600.0 kg
Launch Date: 1992-11-12T00:00:00.013
Launch V∞: [9.695409643750917, 1.230412386785293, 1.5011804102426267] km/s
Phase 1:
Planet: Venus
V∞_in: [9.994449927209848, -4.805887921122601, -1.7920512221893674] km/s
V∞_out: [4.259960619082596, 0.11640502561369129, -0.5256309278562422] km/s
time of flight: 1.0342080020964487e7 seconds
arrival date: 1993-03-11T16:48:00.013
thrust profile: [-0.07885937833013125 0.22082346279052664 0.22422618119726967; -0.6387970581030095 0.0823441238202798 0.08742955630508423; -0.8174616778872149 0.032772077981831405 0.048108011372234014; -0.883356063802344 -0.009816430786569194 0.029466362717018645; -0.9090289869704303 -0.06412247350619477 0.01579427507721176; -0.9229025007601358 -0.1348848870891437 0.0038074996913229635; -0.9323419038216932 -0.22247834673542874 -0.007553280139873255; -0.9393524504557308 -0.3233146674906946 -0.018599372537661026; -0.9447442065007597 -0.4307195557715542 -0.02948583920082983; -0.948951862234041 -0.5355674747579858 -0.040180510105645155; -0.9522429476394983 -0.6288580191320197 -0.05048177408167433; -0.9547920892312391 -0.704185334520697 -0.060067918029030234; -0.9567196352746482 -0.7592160354782643 -0.06849167659927999; -0.9581161960060807 -0.79533985266094 -0.0750231011768658; -0.959058595284678 -0.8151694427669934 -0.07867130196153184; -0.959627487063727 -0.8196811744278104 -0.07803378433478286; -0.959931461581211 -0.8044527869739441 -0.07118021416582515; -0.9601423578460804 -0.7501732041729071 -0.05552220537456991; -0.9605351740691301 -0.596546633077274 -0.027695673262336473; -0.9614858974879196 -0.22563892811165903 0.016331234996720147] %
Mass Used: 386.3550491309211 kg
Launch C3: 97.76842542578919 km²/s²
||V∞_in||: 11.233745396832147 km/s

29
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missions/nlp_2_phase---------------------------
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: 3600.0 kg
Launch Date: 2021-10-31T23:59:59.740
Launch V∞: [1.0519139174671255, -2.532396776578504, -2.3181056242189095] km/s
Phase 1:
Planet: Venus
V∞_in: [0.4221053576448278, -3.5275571377673485, 4.891092995284791] km/s
V∞_out: [2.663171797047433, -4.912541295851552, 2.3063442275330837] km/s
time of flight: 1.2614399648580924e7 seconds
arrival date: 2022-03-26T23:59:58.740
thrust profile: [0.07998955511503905 0.014645901175208607 0.032059542365265536; 0.061271963308267355 0.010496084457312739 0.06456227213436845; 0.03653858968490382 0.004095269984271039 0.08778809213169904; 0.012597606226571892 -0.0035843497513941024 0.10156429358711754; -0.007823696996985706 -0.012212563689391798 0.1092387978999297; -0.024470397395360978 -0.022164965343914263 0.11328387576041525; -0.03764018531138568 -0.03305106575614711 0.11485841832796724; -0.046956531921797474 -0.04462741732738438 0.1147527426828988; -0.052986295209290435 -0.056908842131396964 0.11331606017641183; -0.05501214840088177 -0.0698229298399496 0.11102391517980509; -0.0539274775951607 -0.08225923304281293 0.1080571865577752; -0.04900248855811753 -0.09498380663479362 0.10399629481809765; -0.040344197913873656 -0.10681215838405833 0.09912867572917736; -0.028118935327375093 -0.11715254048024237 0.09312311669260512; -0.012343877715426374 -0.12544654901191046 0.08544366039001013; 0.006110502843051679 -0.1305027433772816 0.07629177701281903; 0.026362754169644998 -0.13201279652190237 0.06480681138449274; 0.046333885834596335 -0.129332099528906 0.05156965147459962; 0.06457348912678001 -0.12274635759961078 0.036509818421423236; 0.07952353937438418 -0.11313097843352427 0.019798449229470383] %
Phase 2:
Planet: Mars
V∞_in: [3.880922081076609, -3.8756380279560982, -1.179545632109947] km/s
V∞_out: [-0.006991844594378784, 0.007675557473077985, 0.0017824029323501372] km/s
time of flight: 1.330560006563769e7 seconds
arrival date: 2022-08-27T23:59:58.740
thrust profile: [0.12305856757522188 -0.14464704712095547 -0.01690236351704525; 0.13429815673794188 -0.1195285218500703 -0.023483980378131736; 0.1396586011579744 -0.09516174490601491 -0.0293944316107087; 0.1405117586368446 -0.07304441529598331 -0.03420656443020225; 0.13837132835970684 -0.05371429903466249 -0.03776391678703145; 0.13446436956407476 -0.03753581708426115 -0.04027955684165351; 0.12971675491549636 -0.02368494568417238 -0.041313837916754456; 0.12476791885955194 -0.011918609837526017 -0.04089459243732129; 0.11990410375769957 -0.0013599111496390207 -0.039013892415853124; 0.11535184137947554 0.008625420550911504 -0.03547549318320644; 0.11060362891923352 0.01858862039347281 -0.03026382720393468; 0.1051121620536058 0.02900798484914558 -0.02356021862070372; 0.09847113469008412 0.040066844453614206 -0.014965931800162527; 0.08971089782921067 0.051422184661349964 -0.005111452945431483; 0.07802582953613077 0.06259376060544532 0.0051850295654957725; 0.06311411546227669 0.07276616262027279 0.015795273832386957; 0.04546470094052957 0.08070053397671015 0.025466309765173768; 0.026472095432748317 0.08567894187220633 0.03355591354621125; 0.006854607387209108 0.08788158299954184 0.03976962429050834; -0.011956529938837489 0.08738091721577941 0.04450602440724739] %
Mass Used: 121.82108539595492 kg
Launch C3: 12.893170008821572 km²/s²
||V∞_in||: 5.6101206957923 km/s

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missions/nlp_5_phase---------------------------